Service history of F-104
The service history of the Starfighter by nation
BELGIUM
Beginning in February of 1963, the Force Aerienne Belge (Belgian Air
Force) received a total of 100 SABCA-built F-104G (including 25 from MAP funding)
and twelve Lockheed-built TF-104Gs (three of them from MAP funding). They
were assigned to four squadrons, the 23 squadron and 31 squadron (both of
10 Wing) at Kleine Brogel and the 349 squadron and s50 Squadron (both of 1
Wing) at Beauvechain (Bevekom). 1 Wing was an all-weather air defense organization
whereas 10 Wing was a tactical strike/fighter-bomber unit. Serials were FC01/FC12
for the Lockheed-supplied TF-104G and FX1 through FX100 for the SABCA-built
F-104G. An extra F-104G was built to replace FX27 which crashed before delivery
but was given the same serial number.
The Starfighters remained in service with the FAB (Force Aerienne Belge) until
the 1980s when they were replaced by General Dynamics F-16A/B Fighting Falcons.
First to convert was 1 Wing which transferred its F-104Gs to 10 Wing pending
that outfit's receipt of its own F-16s. The last Starfighter left Belgian
service in September of 1983. A total of 41 Belgian Starfighters, including
three TF-104G, were lost in accidents, or nearly 37 percent of the force.
18 Belgian F-104G were later transferred to Turkey.
The following FAB units operated the Starfighter:
1 Wing, Beauvechain: All-weather Air Defense: 349 Squadron (mid-1963 to July
1979) and 350 Squadron (April 1963 to April 1981)
10 Wing, Klein Brogel: Tactical Strike/Fighter-Bomber: 23 Squadron (April
1964 to mid-1982 and 31 (Tiger) Squadron (mid-1964 to early 1983).
CF-104 from Canada
On July 2, 1959, it was announced that Canada had chosen the F-104 Starfighter as the replacement for the Sabre
Mk.6 in service with the RCAF's European Air Division. However, since the
Canadian government wanted equipment to be fitted that was specific to RCAF
requirements, it opted to manufacture the aircraft under license in a Canadian
factory rather than to buy the aircraft outright from Lockheed. On August
14, it was announced that Canadair of Montreal had been selected to manufacture
200 aircraft for the RCAF under license from Lockheed. In addition, Canadair
was to manufacture wings, tail assemblies, and rear fuselage sections for
66 Lockheed-built Starfighter that were destined for the West German Luftwaffe.
The license production contract was signed on September 17, 1959.
The Canadian-built Starfighter was initially designated CF-111 by the RCAF,
but this was later changed to CF-104. They were designated CL-90 by the Canadair
factory.
The CF-104 was basically similar to the F-104G, but was fitted with equipment
specialized for RCAF requirements. It differed from the F-104G in being optimized
for the nuclear strike role rather than being a multi-mission aircraft. The
F-104G was fitted with NASARR F15A-41B equipment which was optimized for both
air-to-air and air-to-ground modes, but the CF-104 was fitted with R-24A NASARR
equipment which was dedicated to the air-to-ground mode only. The main undercarriage
was fitted with longer-stroke liquid springs and carried larger tires. The
CF-104 also differed from the F-104G in retaining the removable refueling
probe that was fitted to the F-104C and F-104D of the USAF. Another difference
from the F-104G was the ability of the CF-104 to carry a ventral reconnaissance
pod equipped with four Vinten cameras. The 20-mm M61A1 cannon and its associated
ammunition were initially omitted from the CF-104, and an additional fuel
cell was fitted in their place.
In parallel with the production of the Starfighter by Canadair, Orenda Engines,
Ltd. acquired a license to build the J-79 engine which was to power it. The
CF-104 was powered by a Canadian-built J-79-OEL-7 rated at 10,000 lb.s.t.
dry and 15,800 lb.s.t. with afterburning.
Lockheed sent F-104A-15-LO serial number 56-0770 to Canada to act as a pattern
aircraft for CF-104 manufacture. It was later fitted with CF-104 fire control
systems and flight control equipment (but not the strengthened airframe of
the true F-104G) and turned over to the RCAF, where it was assigned the serial
number of 12700. The first Canadair-constructed CF-104 (RCAF serial number
12701) was airlifted to Palmdale, California in the spring of 1961, where
it made its first flight on May 26. The second CF-104 (12702) also made its
first flight at Palmdale. The first two CF-104 to fly at Montreal were Nos.
12703 and 12704, which both took to the air on August 14, 1961.
CF-104s were initially assigned Canadian serials 12701 through 12900. On May
18, 1970, they were reserialed as 104701 through 104900. The Lockheed-built
F-104A pattern aircraft was reserialled from 12700 to 104700.
The 200th and last CF-104 (No. 12900) was completed on September 4, 1963 and
delivered to the RCAF on January 10, 1964. Many early production aircraft
were modified to the standard of the last production machines. Following the
delivery of the last CF-104, Canadair switched to the manufacture of F-104Gs
for delivery to NATO allies under the provisions of MAP.
Beginning in December of 1962, the RCAF used its CF-104 to equip eight European-based
squadrons of its 1 Air Division. Other CF-104s were assigned to the 6 OTU
based at Cold Lake, Alberta. Apart from the operational conversion unit established
at Cold Lake, Alberta in late 1961 (eventually redesignated 417 Squadron),
RCAF CF-104s were all committed to the support of NATO's nuclear deterrent
mission in Europe. 427 Squadron was the first to form, with initial deliveries
to Zweibrucken in December of 1962. In February of 1964, even before France
withdrew from NATO in 1966, 2 Wing at Grostenquin was disbanded, and its 2
CF-104 squadrons were transferred elsewhere, 421 moving to 4 Wing at Baden-Sollingen
and 430 moving to Zweibrucken. The RCAF's other French base at Marville was
closed by March of 1967, and its two CF-104 reconnaissance squadrons (439
and 441) moved to Lahr in Germany. 434 and 444 Squadrons were disbanded in
1967-1968, reducing CF-104 strength to four nuclear strike squadrons and two
tactical reconnaissance squadrons.
In May of 1969, 3 Wing at Zweibrucken was closed, and 427 Squadron was relocated
to Baden and 430 to Lahr.
In 1970, the Canadian government decided to reduce the strength of the Air
Division to only 3 squadrons and to relinquish its nuclear strike role in
favor of conventional attack by 1972. By January of 1972, the CF-104 had been
converted from their nuclear role to that of conventional ground attack. A
20-mm Vulcan cannon was installed, and the fairing was removed from the cannon
port. Twin bomb ejector rack carriers and multi-tube rocket launchers were
installed.
In 1972, 1 Air Division was redesignated 1 Canadian Air Group with headquarters
at Baden-Sollingen. Lahr was closed, and 422, 427 and 430 Squadrons were disbanded.
439 and 441 replaced all but 421 Squadron in 3 and 4 Wings at Baden. Of the
remaining 3 squadrons, 421 was committed to converting to ground attack roles,
together with 431 Squadron, leaving only 441 Squadron to continue tactical
reconnaissance missions with the Vinten VICON underfuselage camera pod.
A number of former Canadian Forces single-seat CF-104 fighter-bombers and
CF-104D two-seat trainers were transferred to Denmark and Norway after having
been brought up to F-104G/TF-104G standards. By the end of 1980, these transfers
along with attrition had brought European-based RCAF strength down to only
3 Starfighter squadrons. These were 421, 439 and 441, all based at Baden-Soellingen
in West Germany. At that time 417 Squadron at Cold Lake was still functioning
as a CF-104 Operational Conversion Unit.
Beginning in 1983, the CF-104 Starfighter were replaced in Canadian Armed
Forces service by McDonnell Douglas CF-18 Hornets. The last CF-104 was phased
out by 441 Squadron on March 1, 1986. Canada then offered Turkey an initial
batch of 20 CF-104, later increased to 50, including six CF-104D. Thirty of
these were sent to MBB at Manching in Germany in March of 1986 for overhaul
before being transferred to Turkey. The remainder were broken down for spares.
About 110 CF-104/CF-104D were lost in accidents, out of 238 delivered-a loss
rate of no less than 46 percent.
The following Canadian Armed Forces units operated the CF-104:
Central Experimental and Proving Establishment/Aerospace Engineering and Test
Establishment, Cold Lake, Alberta (1962). To 6 Strike-Recce OTU, reformed
as 417 Operational Training Squadron (1962-1983)
No 421 (Red Indian) Squadron, 2 Wing, Grostenquin/Baden-Sollingen Dec 1963 to Dec 1985
No 422 (Tomahawk) Squadron, 4 Wing, Baden-Sollingen, July 1963 to 1972
No 427 (Lion) Squadron, 3 Wing, Zweibrucken/Baden-Sollingen, Oct 1962 to 1972
No 430 (Silver Falcon) Squadron, 2 Wing, Grostenquin/Lahr, September 1963 to 1972
No 434 (Bluenose) Squadron, 3 Wing, Zweibrucken, April 1963 to March 1967
No 439 (Sabre-Toothed Tiger) Squadron, 1 Wing, Marville/Baden-Sollingen, March 1964 to April 1987
No 441 (Silver Fox) Squadron, 1 Wing, Marville/Baden-Sollingen, September 1963 to Feb 1986
No 444 (Cobra) Squadron, 4 Wing, Baden-Sollingen, May 1963 to 1967
RCAF serials of CF-104 12701/12900, Canadair CF-104 c/n 1001/1200, reserialed 104701/104900 in 1970.
Specification of the CF-104:
One Orenda Engines-built J79-OEL-7 rated at 10,000 lb.s.t. dry and 15,800
lb.s.t. with afterburning. Maximum speed (dash): 1550 mph (Mach 2.35) at 40,000
feet, 915 mph (Mach 1.2) at sea level. Climb to 30,000 feet in 1.5 minutes.
Weights were 13,909 pounds empty, 21,005 pounds loaded (clean), 28,891 pounds
maximum takeoff. Dimensions were wingspan 21 feet 11 inches, length 54 feet
9 inches, height 13 feet 6 inches, wing area 196.1 square feet. External stores
could be carried on five hardpoints (one underneath the fuselage, one underneath
each wing, and one at each wingtip).
CF-104D two-seater for Canada
Lockheed built 38 two-seat trainer versions of the TF-104G Starfighter for the Royal Canadian Air Force.
These aircraft were similar to the TF-104Gs built by Lockheed for other NATO
allies, but were powered by Canadian-built J79-OEL-7 engines. They were given
the Lockheed designation of Model 583-04-15, and were initially designated
CF-113 in Canadian service. However, this designation was later changed to
CF-104D. No CF-104Ds were built in Canada.
The first CF-104D made its maiden flight on June 14, 1961. The last 16 aircraft
on the order had slightly different equipment and were designated CF-104D
Mk. II. The CF-104Ds were initially given the serials 12631 through 12668,
but on May 18, 1970 they were reserialed as 104631 through 104668.
In 1971-1973, seven former Canadian Forces CF-104D were transferred to Denmark
after having brought up to TF-104G standards. In 1973, two other CF104D were
transferred to Norway. Following their withdrawal from CAF service, six CF-104D
were transferred to Turkey following an overhaul in Germany.
Serials of Lockheed CF-104D: 12631/12668, Lockheed CF-104D c/n 583A-5301/5338, reserialed 104631 through 104668 in 1970.
DENMARK
In 1962 it was decided that the Kongelige Danske Flyvevaben (Royal Danish Air Force) received 25
Canadian-built F-104G and 4 Lockheed-built TF-104Gs through the US Mutual
Aid Program. These equipped two units (Esk 723 and Esk 726), both based at
Aalborg. Delivery of the first 8 F-104Gs and 2 TF-104Gs started in November
1964. In fact, the aircraft were delivered by ship and then towed from the
harbor to Aalborg Air Base where they were thoroughly checked before entering
service in December 1964. The F-104 was officially handed over to the RDAF
on June 29, 1965.
ESK726 became the first Danish F-104 squadron in December 1964 with Esk 723
following suit in September 1965. Initially, training was carried out in Esk
726 only, but this was changed later on.
During the first years of operational service the maintainers worked hard
to produce the number of required flight hours. Lack of spare parts necessitated
cannibalization of two F-104Gs, R-699 and R-700.
Attrition was made up by the transfer in 1972-74 of 22 ex-Canadian Forces
Starfighters (15 CF-104 and 7 CF-104D). The CF-104D were specially modified
for use by Esk 726 in the electronics countermeasures role.
Since the TF/F-104G supplied under the MAP programme were supposed to be returned
to the US once their service in the RDAF was over, the first Danish F-104s
to be retired were the CF-104s and CF-104Ds. This way the RDAF could continue
to use the TF/F-104G operationally and then use the CF-104 and CF-104Ds as
sources for spare parts. All CF-104s and CF-104Ds were retired by January
1985.
Esk 723 was disbanded on January 1, 1983. The F-104 was eventually retired
on April 30, 1986, marked with a 5-ship flyby over Aalborg AB. The TF/F-104Gs
supplied under the MAP programme were all returned to the US. Some were later
passed on to the Republic of China Air Force. The Starfighter were then retired
with the exception of four aircraft retained for target-towing duty.
Of the 51 Starfighter operated by the RDAF between 1965 and 1986, 12 were
lost in accidents, a rate of 23.5 percent. The surviving Lockheed-built MAP-funded
F-104G and 3 TF-104G were transferred to Taiwan in 1987.
RDAF units using the Starfighter:
Esk 723, Aalborg, 1965 to January 1, 1983
Esk 726, Aalborg, 1956 to April 30, 1986
GERMANY
The Luftwaffe was the primary user of the Starfighter, operating over thirty-five percent of all F-104s
built. Luftwaffe F-104G came from all five production lines of the Starfighter
consortium. The West German Luftwaffe received a total of 916 Starfighter:
30 F-104F, 96 F-104G, and 136 TF-104G from Lockheed; 255 F/RF-104G from the
North Group; 210 F-104G from the South Group; 88 F-104G from the West Group;
50 F/RF-104G from the Italian Group; plus 50 replacement F-104G from MBB to
replace some of those lost in crashes.
At their peak in the mid-1970s, Starfighter equipped five nuclear-armed Luftwaffe
Fighter-Bomber wings, two Interceptor wings, and two Reconnaissance wings.
In addition, two Attack wings of the Marineflieger (Federal German Navy) were
equipped with Starfighter.
The first German Starfighter were the Lockheed-built two-seat F-104F which
were initially used in the USA to train German instructors. At that time,
the F-104F were painted with standard USAF insignia and carried USAF serial
numbers. These machines were then handed over to Waffenschule 10, which was
based at Norvenich in Germany. After handover, they were repainted in Luftwaffe
insignia and assigned German serial numbers. They began converting pilots
for JaboG 31 in July of 1960.
The first operational unit to be equipped with the F-104G was Jagdbombergeschwader
31 "Boelcke" (JaboG 31), also based at Norvenich. JaboG 31 became fully operational
in 1963. Other Jagdbombergeschwader (Fighter-Bomber wings) to receive the
F-104G were JaboG 32 at Lechfeld, JaboG 33 at Buchel, JaboG 34 at Memmingen
and JaboG 36 at Rheine-Hopsten. Two Fighter wings (Jagdgeschwader) received
the F-104G: JG 71 at Wittmundhafen and JG 74 at Neuburg. Two Aufklärungsgeschwader
(reconnaissance wings) received the RF-104G: AG 51 at Ingolstadt/Manching
and AG 52 at Leck. In addition, two Marinefliegergeschwader of the Bundesmarine
(West German Navy) received F-104G. These were MFG 1 at Schleswig and MFG
2 at Eggebek. They operated in the armed reconnaissance and anti-shipping
strike roles.
With new aircraft being delivered almost daily to the new Luftwaffe, a massive
pilot training was required in order to get them into service quickly. Northern
European weather and operational restrictions placed severe limitations on
the amount of training that could be done in Germany. The immediate answer
was to set up a Luftwaffe training operation in the southwestern United States,
where there was a lot of space, where the air was clear, and where the weather
was good most of the time. Many Luftwaffe Starfighter remained in the United
States and were stationed at Luke AFB in Arizona for pilot training. They
were assigned to the 4512th, 4518th and 4443rd Combat Crew Training Squadrons
of the USAF. Although remaining Luftwaffe property, these aircraft carried
USAF insignia and were assigned USAF serial numbers. Final F-104G training
for the European environment was done at the Waffenschule 10 at Jever.
In Luftwaffe service, the F-104G got a bad reputation because of the large
number of accidents, many of them resulting in fatalities. Intensive flying
operations with the Starfighter did not start in Germany until 1961, when
only two crashes took place. There were seven crashes in 1962, 12 in 1964,
and 28 in 1965, or more than two a month. By mid-1966, 61 German Starfighter
had crashed, with a loss of 35 pilots. At the height of the crisis, the Starfighter
accident rate peaked at 139 per 100,000 flying hours. As a result, the German
press went into a feeding frenzy and the F-104G was given derogatory nicknames
such as the "Flying Coffin" or the "Widowmaker", which brings to mind all
of the flak that surrounded the Martin B-26 Marauder during World War 2. One
running joke at the time was that if you waited long enough, just about every
square mile of Germany would have a Starfighter crash onto it. The press left
many people with the impression that there was something intrinsically wrong
with the F-104G, that it was just too difficult an airplane to fly for the
new and relatively inexperienced Luftwaffe pilots. The high loss rate generated
a flurry of criticism of the Bonn government, some critics claiming that the
entire Starfighter program had been politically-motivated and should be cancelled
outright.
During its period of service with the German armed forces, about 270 German
Starfighter were lost in accidents, just under 30 percent of the total force.
About 110 pilots were killed. However, the attrition rate in German service
was not all that much greater than that of the F-104 in service with several
other air forces, including the United States Air Force. Canada had the unenviable
record of losing over 50 percent of its 200 single-seat CF-104s in flying
accidents. The loss rate of Luftwaffe Starfighter was not all that extraordinary,
since the Luftwaffe had suffered a 36 percent attrition rate with the Republic
F-84F Thunderstreak, the Starfighter's immediate predecessor. There was nothing
intrinsically dangerous about the Starfighter, since the Royal Norwegian Air
Force operating identical F-104G suffered only six losses in 56,000 flying
hours, and the Spanish Air Force lost not a single one of its Starfighter
to accidents.
Nevertheless, some of the Luftwaffe crashes could indeed be traced to technical
problems with the F-104G itself. Engine problems, including difficulties with
the J-79's variable afterburner nozzle, and contamination of the Starfighter's
liquid oxygen system causing loss of consciousness of the pilot were listed
as contributing factors in some of the accidents. There were also problems
with the automatic pitch-up limiter during high-speed low-altitude flying
and in tight turns, resulting in its temporary removal, with accompanying
restrictions on the maneuverability.
However, the high rate of crashes while in Luftwaffe service could be blamed
more on the hazards of flying low-altitude missions at high speeds in the
bad weather of Northern Europe than on any intrinsic flaw with the F-104G.
Human error was probably the major cause of the majority of the accidents.
The Starfighter required 38-45 hours of maintenance for every hour in the
air, and many of the Luftwaffe ground crew personnel were conscripts who were
probably too hastily trained. In addition, German Starfighter pilots were
only flying 13-15 hours a month, compared with the NATO average of about 20
hours. Another factor may have been the fact that the initial training of
Luftwaffe aircrews took place in the USA rather than in Germany. The reason
given for training Luftwaffe pilots in the USA rather than in Germany was
that the clear air and good flying weather in the American Southwest was much
more conducive to pilot training than was the often lousy weather of Northern
Europe. However, one might fairly point out that were war to break out, the
actual fighting would be done in the nasty weather of Europe rather than in
the clear desert air of the American West. The sudden transition from the
clear desert skies of Arizona to the winter skies of northern Europe may have
been another factor in the rash of crashes.
At the height of the Starfighter political crisis in mid-1966, the Luftwaffe
chief, General Wernher Panitzki, was forced to resign after he had criticized
the FRG's Starfighter procurement program as being politically-motivated.
His successor was the World War II ace Lieutenant General Johannes Steinhoff,
who had flown Me 262 jets during the war. Steinhoff had not initially been
a Starfighter booster, and he had complained about the Bonn Defence Ministry's
failure to implement the recommendations of his 1964 report on F-104G survival
measures. One of Steinhoff's first moves was to review the F-104G's ejection
system to enhance the probability of a successful escape by a pilot at low
level. The Lockheed C-2 ejection seat initially fitted to the F-104G had been
fitted with a more powerful Talley Corp 10100 rocket booster by November 1966
to give it true zero-zero capability. However, it was found that the Talley
rockets had a destabilizing effect after ejection, and had to be removed.
After the German Starfighter had to be grounded once again for fixes to the
C-2 seats in December of 1966, it was decided to switch over to Martin-Baker
Mk GQ7A Zero-Zero ejection seats. A contract was signed on March 8, 1967 to
re-equip the entire German F-104G force with the Martin-Baker seats. This
took about a year to get done. The first successful use of a GQ7 seat to escape
from a German F-104G took place during a ground-level overshoot at Ramstein
on September 24, 1968.
Another part of the program to reduce the Starfighter accident rate was the
revision of the training techniques and procedures. It soon began to pay off.
The Starfighter accident rate dropped by about half in 1968. However, this
was only temporary, and between 15 and 20 Starfighter crashed every year between
1968 and 1972. Crashes continued at a rate of 9 to 11 aircraft per year until
the early 1980s, when all German F-104Gs began to be replaced by Tornados.
In the nuclear role, the Luftwaffe F-104G could carry a single 1 Megaton B-43
nuclear store underneath the fuselage on the centerline. A maximum of 250
Luftwaffe Starfighter were committed to NATO's nuclear forces. At the height
of the Cold War, each of the Fighter-Bomber wings maintained a 24-hour force
of six nuclear-armed Starfighters on Quick Reaction Alert, fueled and ready
to take off within 17 minutes of authorization. I remember some concern being
expressed at the time about a German finger being on the nuclear trigger.
However, although these nuclear weapons were carried underneath German aircraft,
these bombs remained under American control at all times, and could be released
for delivery only under a direct order passed down the chain of command from
the President of the United States. A typical load of conventional weapons
for ground attack included Lepus flare bombs, CBU-33 cluster bombs, various
iron bombs and LAU-3A unguided rocket packs.
Some 151 of the F-104G were allocated to the Marineflieger of the German Navy,
the Bundesmarine. They were assigned to two Naval Attack Wings from 1964 onwards
- Marinefliegergeschwader (MFG) 1 and 2 - replacing the Hawker Sea Hawk. The
F-104G of the Bundesmarine usually carried a MBB Kormoran anti-ship missile
on each of the underwing pylons. The Kormoran missile had a range of up to
23 miles. The missile had a 350 pound warhead with 16 radially-mounted projectile
charges and fuse delays designed for penetration of ship armor. After launch,
the Kormoran used an inertial midcourse guidance in conjunction with a radio
altimeter to hold an altitude of less than 100 feet off the wave tops during
the approach to the target. The radar seeker in the nose could operate either
as an active radar seeker or as a passive receiver. When it found a target
it locked onto it, and the impact point was intended to be just above the
waterline of the enemy ship in order to ensure maximum damage.
The Luftwaffe became worried about the possible vulnerability of its airfields
to Warsaw Pact attacks, and started searching for means of dispersing its
Starfighters around the country. Under contract from the Luftwaffe, Lockheed
carried out tests with an F-104G launched by rocket from a platform. The Luftwaffe
envisaged fleets of nuclear-armed Starfighter being trucked out to the countryside
and mounted on pre-positioned ramps. From there, the aircraft would be launched
under the power of a huge rocket motor, which would take the Starfighter to
flying speed before dropping away. After the mission, recovery would take
place at hastily prepared landing strips, perhaps even using the Autobahn,
that were equipped with runway arrester gear for short landings. Luftwaffe
F-104G DA+102 (the third Lockheed-built Starfighter for the Luftwaffe, assigned
to JaboG 31) was modified for a series of zero-length launch (ZELL) tests
in 1963 at Edwards AFB in California. The F-104G was mounted on a trailer,
and a 130,000 lb.s.t. Rocketdyne solid-fuel rocket booster was attached to
the rear of the fuselage. For takeoff, the pilot would run up the J-79 engine
to full thrust, then light the rocket motor. Within four seconds after ignition,
the F-104G would be flying at 300 mph and the rocket booster would drop off.
The program was not disclosed to the public until March 21, 1966. From 1966,
ZELL testing was carried out at Lechfeld, home of JaboG 32. Two of the wing's
aircraft (DB+127 and DB+128) were assigned to the project. Although tests
were successful, the scheme was not adopted for operational use. After the
ZELL test program was completed, the test F-104G was returned to service in
Germany.
MBB became interested at an early date in highly-maneuverable aircraft. A
Fokker-built F-104G (23+91, later renumbered 98+36) was modified by MBB as
part of a five-year research program into control-configured vehicle (CCV)
and fly-by-wire technologies. Natural stability was replaced with computer-controlled
fly-by-wire systems that allowed the aircraft to be made unstable. This natural
instability could then be controlled to provide extra agility. The aircraft
was provided with a triple-redundant fly-by-wire system in 1977. The transition
from the naturally-stable Starfighter aerodynamics was taken in gradual stages,
first by adding ballast to alter the center of gravity. In 1980, a complete
F-104 tailplane section was then grafted to the spine on the upper fuselage
forward of the wing to further destabilize the aircraft. Fairings were added
over the wings, and the aircraft was marked with extra Day-Glo panels for
high visibility. 20 percent negative stability was finally achieved within
the specified limits of Mach 1.3 and 650 knots by the time the trials were
successfully concluded. The data gathered was of great assistance to the design
of the EFA and was also used during the development of the Rockwell/MBB X-31
testbed. The F-104CCV was then transferred to the Wehrtechnisches Museum in
Koblenz.
The German Starfighter operated by training units in the USA bore full USAF
markings and serial numbers, whereas those in Europe were in Luftwaffe insignia
and carried German serial numbers. Originally, these serials consisted of
two letters and three digits.
The serial numbers of German Starfighters were as follows:
Lockheed-built:
F-104G: DA+101/DA+121, KF+101/KF+172, plus aircraft which served in the USA with USAF serial numbers.
TF-104G: KE+201/KE+243, KF+201/KF+241, plus aircraft which served in the USA with USAF serial numbers
Fiat-built:
F-104G: KC+117/KC+131
RF-104G: KC+132/KC+166
Fokker-built:
F/RF-104G: KG+101/KG+450, with gaps in the sequence for those aircraft built for the Netherlands.
The gaps in this sequence were an artifact of the rather unusual numbering
system used by the Luftwaffe to identify Fokker-built F-104G. The Luftwaffe
serial numbers tracked with the Fokker company's manufacturing numbers. The
missing numbers in this sequence correspond to those aircraft which were delivered
to Holland. There were corresponding gaps in the list of Dutch Starfighter
serial numbers which identified Starfighters delivered to Germany.
Messerschmitt-built:
F-104G: KE+301/KE+510. Some aircraft in this batch served in the USA with USAF serial numbers.
TF-104G: KE+201/KE+223
SABCA-built:
F-104G: KH+101/KH+188. Some aircraft in this batch served in the USA with USAF serial numbers.
On January 1, 1968, the original two letter-three digit serial numbers were
replaced by new four-digit serials. Surviving German Starfighter were reserialed
as follows: DA+101/DA+121, KF+101/KF+172 to 20+01/20+84; KC+117/KC+166 to
20+85/21+32; KE+301/KE+510 to 21+33/23+26; KG+101/KG+450 to 23+27/25+55; KH+106/KH+188
to 25+56/26+37; KE+201/KF+243, KF+201/KF+241 and KE+201/KE+223 (by Messerschmitt)
to 27+01/28+35; BB+361/BB+389 to 29+01/29+21
More information about the
Tactical number system
In late 1968, the unexpectedly heavy accident rate had led the Federal Defence
Ministry to order another 50 F-104G as attrition replacements. The MBB concern
built 50 F-104G as replacements between the years 1970 and 1973. These 50
planes had uprated J-79-MTU-J1K turbojets, rated at 15,950 lb.s.t. maximum.
This engine had been developed by MAN Turbo (later MTU), which had taken over
J-79 license rights from BMW. Their serials were 26+41 through 26+90. This
brought overall German Starfighter procurement to 916.
The Starfighter began to be phased out of Luftwaffe service in 1971, when
the AG 51 and AG 52 reconnaissance squadrons received McDonnell RF-4E Phantoms.
JG 71 and JG 74 reequipped with F-4E in 1973-74, and JaboG 36 received Phantoms
in 1976. In the Bundesmarine, MFG 1 converted to the Panavia Tornado in July
of 1982. In 1983, the Luftwaffe training unit at Luke AFB was closed down.
By the mid-1980s, most Starfighter were gone from West German service. Most
German F-104G were transferred to the air forces of Greece, Turkey, and Taiwan.
The last Luftwaffe operational unit to operate the F-104G was JaboG 34, which
retired its aircraft at the end of 1987.
Although the last Starfighter had left German front-line service by October
of 1987, a few F-104G and TF-104G remained flying with WTD 61 at Manching
for another three years or more on various avionics trials and systems development
programs. The last flight of a German Starfighter (98+04) took place from
Manching on May 22, 1991.
The following units flew the Starfighter:
Luftwaffe:
AG 51 "Immelmann": Ingolstadt/Manching, Bremgarten, RF-104G, November 1963 to April 1971
AG 52: Leck, RF-104G, November 1964 to September 1971
JaboG 31 "Boelcke": Norvenich, February 1962 to May 1983
JaboG 32: Lechfeld, January 1965 to April 1984
JaboG 33: Buchel, August 1962 to May 1985
JaboG 34: Memmingen, July 1964 to October 1987
JaboG 36: Hopsten, February 1965 to February 1975
JG 71 "Richthofen": Wittmundhaven, April 1963 to September 1974
JG 74: Neuburg, May 1964 to July 1974
4510 CCTW Luke AFB; Arizona: (4512, 4518 and 4443 USAF Combat Crew Training Squadrons of the 4510th CCTW), becoming the 69 TFTS and 418 TFTS, 58th TTW
of the USAF at Luke AFB. Acted as US-based training unit from February 1964 until disbanded in March 1983 (administration at 2 Dt.Lw.Ausb.Stff, USA)
Waffenschule 10: Norvenich, (May 1960-1963), Jever (1963 to September 1983)
Erprobungsstelle 61: Manching, established 1960 as test unit, redesignated WDT 61 and operated the F-104G from February 1962 until the last German Starfighter
sortie on May 22, 1991
Luftwaffenversorgungsregiment 1: Erding, (LwSchleuse 11) for maintenance and technical support, May 1984 to September 1988
Marineflieger:
MFG 1: Schleswig-Jagel, September 1963 to October 1981
MFG 2: Eggebek, March 1965 to September 1986
More information about the German wings
GREECE
The Elliniki Polemiki Aeroporia (Royal Hellenic Air Force) of Greece was initially allocated 35 Canadair-built
F-104G plus 4 Lockheed-built TF-104G. Deliveries began in 1964. Another 10
MAP-funded Lockheed-built F-104G and 2 TF-104G were later delivered to Greece
from USAF stocks.
The Starfighter were first issued to 335 Mira "Tiger" squadron in the 114th
Pterix (Wing) based at Tanagra. It was soon followed by 336 "Olympus" Mira
of the 116th Wing at Araxos. These two squadrons were initially dedicated
to nuclear strike roles within the 1st Tactical Air Force as a part of Greece's
commitment to NATO, but they reverted to the conventional strike role in the
early 1970s.
Attrition was made up by the transfer of nine F-104G from Spain in 1972 and
two TF-104G from Germany in 1977. In mid-1982, 10 Fiat-built F-104G were transferred
from the Netherlands to Greece.
Throughout the 1980s, the Federal Republic of Germany continuously transferred
ex-Luftwaffe and ex-Marineflieger Starfighter to Greece as part of Bonn's
"Minerva" military aid program to Greece. This eventually involved 22 RF-104G,
38 F-104G, and 20 TF-104G. However, not all of these aircraft were placed
in HAF service, some remaining in storage or used for spares.
In the history of the Hellenic Air Force the Starfighter has played an important
role.
A big number of aircraft have been in use during 30 years, between 1964 and
1993. The first Starfighter came from the Canadair factory in Montreal and
a few years later some aircraft arrived directly from Luke AFB after being
used intensively for NATO F-104 pilot training in the early sixties.
Greece lost a reasonable number of aircraft, which were compensated between
1977 and 1988 when ex-German and ex-Dutch Starfighter arrived after they had
been replaced in their subsequent countries by more modern fighter aircraft.
Only 2 Hellenic Air Force squadrons have used the Starfighter, being 335 "Tiger"
Mira and 336 "Olympus" Mira.
The first F-104 squadron became 335 Mira from the 114 Pterix (Wing) based
at Tanagra AB. The first aircraft arrived there in April 1964.
Sister squadron 336 Mira, also based at Tanagra AB, received their Starfighter
between December 1964 and January 1965.
Almost 2 years later, at December 21, 1966, the 336 Mira moved to the 116
Pterix based at Araxos AB.
The 335 Mira kept flying from Tanagra AB until June 1977 when it joined the
336 Mira at Araxos AB.
From that day until early 1993 all the remaining F-104s flew from Araxos AB
(116 Pterix) until their retirement.
335 "Tiger" Mira Anachaitisis (Interceptor Squadron) deactivated
in May 1992.
336 "Olympus" Mira Diokseos Bombardismou (Fighter-Bomber Squadron)
deactivated March 31, 1993.
March 31, 1993 was the official date for the withdraw from service in the
Hellenic Air Force.
HAF units using the Starfighter:
335 "Tiger" Mira, 114 Pterix, Tanagra AB, April 1964; then 116 Pterix, Araxos AB, June 1977 to May 1992
336 "Olympus" Mira, 114 Pterix, Tanagra AB, January 1965; 116 Pterix, Araxos AB, December 1966 to March 31, 1993
ITALY
In the mid-1960s, the Aeronautica Militare Italiana (AMI) received 125 Fiat-built F-104G (including 20 RF-104G)
plus 12 Lockheed-built TF-104G and 16 Fiat-built TF-104G. The F-104G and TF-104G
first entered service at Grosseto with 4°Stormo in 1963. These aircraft ultimately
equipped four interceptor/fighter-bomber Gruppi, two reconnaissance Gruppi, and one training Gruppo.
6 Lockheed TF-104G were transferred to the AMI from the Luftwaffe in 1984/85 and were refurbished by Aeritalia.
AMI serials of the 125 Fiat-built F-104G were as follows: MM6501 pattern aircraft),
MM6502/MM6599, MM6601, MM6603, MM6608/MM6611, MM6631/MM6638, MM6643/MM6651,
and MM6658/MM6660. The AMI serials tracked with Fiat's company numbers, and
the gaps in the sequence correspond to machines which were delivered to Germany
and Holland. Serials of the 12 Lockheed-built TF-104G were MM54226 to MM54237.
The 12 Aeritalia-built TF-104G were MM54250 to MM54261. Serials of the 6 ex-Luftwaffe
TF-104Gs were 5712 (ex 27+11), 5738 (ex 27+36), 5739 (ex 27+37) 5743 (ex 27+41),
5902 (ex 27+43), 5919 (ex 27+89), 5946 (ex 28 +16).
In late 1965, the 154°Gruppo based at Ghedi received a NATO Flight Safety
Award after it had flown more than 5000 hours on the F-104G without a single
accident. However, like the air forces of other European operators of the
Starfighter, the accident rate of AMI single-seat F/RF-104G and two-seat TF-104G
was fairly high, with about 37.5 percent of the force having been lost.
The AMI continued to use the F/RF-104G in large numbers long after other European
air forces had passed their Starfighter along to other users. Beginning in
1968, the F-104G was supplemented by the much improved F-104S. The AMI last
F-104G Fighter-Bomber unit (154°Gruppo/6°Stormo) exchanged its Starfighters
for Panavia Tornadoes from early 1983, leaving 28° Gruppo/3°Stormo as the
last operator of earlier-generation Starfighter with Orpheus sensor pod-equipped
RF-104G. These were finally withdrawn from service in June of 1993. The TF-104G
two-seaters remained in limited service in 1995. Although the earlier-generation
F-104G Starfighter are gone from AMI service, substantial numbers of the later
F-104S type remained in service until 2004.
The following AMI units have operated the F/TF/RF-104G:
9°Gruppo/4°Stormo: Grosseto from March 1963 to 2004
10°Gruppo/9°Stormo: Grazzanise from 1964 to 2004
12°Gruppo/36°Stormo: Gioia del Colle from 1972 to 1994
18°Gruppo/3°Stormo: Villafranca, RF-104G from 1973 to 1977; 18°Gruppo/3°Stormo, Trapani from 1985 to 2003
20°Gruppo/4°Stormo: Grosseto from 1965 to 2004
21°Gruppo/53°Stormo: Cameri/Novara from 1967 to 1997
22°Gruppo/51°Stormo: Treviso/Istrana from June 1969
23°Gruppo/5°Stormo: Rimini/Miramare (formed as 101°Gruppo/5°Aerobrigata) from 1964 to 2000
28°Gruppo/3°Stormo: Villafranca, RF-104G from 1970 to June 1993
102°Gruppo/5°Stormo: Rimini from May 1964 to 1993
132°Gruppo/3°Stormo: Villafranca, RF-104G from 1972 to 1991
154°Gruppo/6°Stormo: Ghedi from 1963 to 1982
155°Gruppo/51°Stormo: (formerly in 50°Stormo Piacenza) F-104G until 1974, then Istrana
156°Gruppo/36°Stormo: Gioia del Colle, 1970 to 1983
F-104S from Italy
The F-104S (S for "Sparrow") was the most potent version of the Starfighter to be built. It was an upgraded
and improved version of the F-104G that was built by FIAT. The aircraft was
initially built to meet a requirement issued by the Aeronautica Militare Italiana
(AMI). However, it has also been exported to Turkey.
The F-104S was the winner of the AWX (All-Weather Interceptor) design competition
held in 1965 by the Italian Air Force for a new all-weather interceptor. The
Lockheed CL-980 design (ultimately to be named F-104S) was selected for this
requirement after extensive evaluation of other designs such as the Dassault
Mirage III, McDonnell Douglas F-4 Phantom, Northrop F-5, and North American
F-100.
The F-104S is fitted with the more powerful J-79-GE-19, rated at 11,870 lb.s.t.
dry and 17,900 lb.s.t. with afterburner. This engine provides 13 percent more
power than the engine of the F-104G, and requires auxiliary inlet doors on
the intake sides to provide additional air during takeoff.
The F-104S differs from the F-104G in being equipped with an NASARR R-21G/H
radar which has moving-target indication and tracking capability that acts
in association with a medium-range radar-guided missile fit. All previous
Starfighter could fire only infrared-homing air-to-air missiles. The R21G/H
also has contour/ground mapping and terrain avoidance modes, so that it can
also act as a Fighter-Bomber.
The F-104S had more underwing and fuselage stores attachments, including two
extra fuselage pylons underneath the air intakes, increasing the total number
of strongpoint provisions to nine (two on the wingtips, four underneath the
wings, two underneath the forward fuselage, and one on the fuselage centerline).
Two hard points under each wing are for fuel/bombs (inner) and BVR missiles
(outer). The wingtips usually carry fuel tanks, as does the centerline. The
underfuselage pylons usually carried AIM-9 Sidewinder missiles. In order to
accommodate extra fuel and avionics, the F-104S had to dispense with the internal
20-mm M-61A1 cannon, the port being faired over.
Extra keel area was added by fitting a slightly larger ventral fin, with two
extra ventral fins on either side of the original. As an interceptor, the
F-104S could carry two underwing AIM-7 Sparrow semi-active radar homing and/or
two AIM-9 Sidewinder infrared homing missiles. As a fighter-bomber it could
carry up to 7500 pounds of bombs, napalm tanks, or rocket pods on nine external
attachment points
The improvements which led to the F-104G were first flight-tested by Lockheed
on a modified RF-104G (USAF serial number 64-2624). Lockheed then received
an Italian contract to modify two Fiat-built F-104Gs (MM6658 and MM6660) as
prototypes for an advanced all-purpose aircraft with improved capabilities.
The first Lockheed-modified F-104S flew in December 1966, and the first Fiat-built
F-104S flew on December 30, 1968.
Most of the Italian aerospace industry participated in the F-104S program.
65 percent of the F-104S production was handled by Italian firms. FIAT (later
to be retitled Aeritalia) headed up a group including Alfa Romeo and Macchi
which manufactured the airframes. The J-79 engines were built by FIAT and
GE International, whereas Selenia undertook license production of the Sparrrow
III AAM. FIAR of Milan co produced the NASAAR R21-G radar in collaboration
with NAA's Autonetics Division.
The initial AMI order was for 165 F-104S aircraft. Deliveries started in the
spring of 1969. The first AMI F-104S entered service in June of 1969 with
22° (Interceptor) Gruppo. They went to equip eight multi-role squadrons, although
the first 40 aircraft were completed as Fighter-Bomber, apparently because
their full air defense systems were not yet ready. In the early 1970s, AMI
orders were increased by an other 40 to 206. In addition, in October of 1974
Turkey ordered 40 F-104S.
The FIAT group produced a total of 246 F-104S, 206 of them for the AMI and
40 for Turkey. AMI serials were MM6701/6850, MM6869/MM6881, MM6886/MM6887,
MM6890, and MM6907/MM6494, a total of 206 being delivered. A further 20 were
laid down for a subsequently-cancelled Turkish order. Only one of these-MM6946-was
completed as a replacement for MM6766 which crashed before delivery. Turkey's
forty F-104S were interspersed through the production run. The forty Turkish
F-104S were 6851/6868, 6888/6889, and 6891/6906.
F-104S deliveries were completed by March of 1979. The delivery of the last
F-104S marked the end of Starfighter production throughout the world, with
a total of 2579 being built in the US, Canada, Belgium, Germany, Italy, Japan
and the Netherlands.
The more powerful J-79-GE-19 engine of the F-104S provided vastly improved
acceleration, rate of climb, and maneuverability at all speeds and altitudes.
In addition, the lower specific fuel consumption of this engine allowed for
increased range. The F-104S was the most potent version of the Starfighter
to be built.
The F-104S was supplied to the following AMI units:
9°Gruppo of 4°Stormo based at Grosseto (1970 to 1988)
10°Gruppo of 9°Stormo at Grazzanise (1973 to 1990)
12° Gruppo of 36°Stormo at Gioia del Colle (1971 to 1988)
18° Gruppo of 37°Stormo based at Trapani/Birgi (1984 to 1989)
20° Gruppo of 4°Stormo based at Grosseto (1988 to 1991), Starfighter OCU at Grosseto
21°Gruppo of 53°Stormo based at Cameri/Novara (1971 to 1991)
22°Gruppo of 51°Stormo based at Istrana (1969 to 1989)
23°Gruppo of 5°Stormo based at Rimini (1973 to 1987); formed as 101°Gruppo/5°Aerobrigata, to Cervia 1995
102°Gruppo of 5°Stormo based at Rimini (1973 to 1988)
155°Gruppo of 51°Stormo, formerly in 50° Stormo, Piacenza (1972 to 1984)
156°Gruppo of 36° Stormo at Gioia del Colle (1970 to 1983)
Flight tests of a modernized demonstrator, the F-104S ASA (Aggiornamento Sistema
d'Arma, or Updated Weapons System) began in December of 1984. The ASA upgrade
was designed to extend the operating lives of the surviving AMI F-104S interceptors
to the end of the century and beyond. It had a Fiat R21G/M1 radar with automatic
frequency-hopping and a moving target indicator that conferred true look-down/shoot-down
capability. New avionics included a four-digit NATO IFF, an improved weapons
delivery computer, and the addition of an automatic pitch control computer.
The ASA F-104S had provision for the use of the all-aspect AIM-9L Sidewinder
in place of the original rear-attack AIM-9Bs. It had the ability to carry
the Selenia Apside 1A medium-to long-range radar-guided air-to-air missile
in place of the AIM-7E Sparrow III. The Apside 1 is a developed version of
the AIM-7E Sparrow with a new CW monopulse seeker head with home-on-jam capability,
improved ECCM, active radar fuse, longer range (22 miles) and new wing control
actuators. In order to accommodate the extra avionics required for BVR missile
capability, the F-104S had to dispense with the internal cannon. The effect
of miniaturization allowed the ASA program to reinstate the gun. Most Italian
F-104S were brought up to this standard.
The Apside entered service with the F-104S ASA in 1988. For air intercept
missions, the F-104S ASA typically carries an AIM-9L Sidewinder under the
port wing, an Alenia Aspide 1A missile underneath the starboard wing, and
two wingtip tanks. In the fully-loaded (but seldom used) configuration, the
F-104S ASA carries four Sidewinders (two underneath the fuselage and two on
the wingtips), two Aspides, and two drop tanks.
Although the last AMI single-seat F-104Gs were withdrawn from service in 1983,
substantial numbers of F-104S fighters remained in service with the AMI until
2004.
The ASA-M program was introduced in 1992 to build on the ASA upgrade with
further enhanced air defense capability. In early 1996, ninety F-104S ASA
aircraft were slated for ASA-M upgrade. Italy maintained its F-104S fleet
in first-line survive more than 50 years after the first flight of the XF-104
prototype, which must be some sort of record for a combat aircraft.
AMI Serials of F-104S: MM6701/MM6850, MM6869/MM6881, MM6886/MM6887,
MM6890, MM6907/MM6946 MM6946 was replacement for MM6766 which crashed before
delivery)
Specification of the F-104S ASA:
One General Electric J79-GE-19 turbojet, 11,870 lb.s.t. dry and 17,900 lb.s.t. with afterburner.
Performance: Maximum speed 1450 mph at 36,000 feet, 913 mph (Mach 1.2) at sea level. Stalling speed 196 mph. Takeoff run with two AIM-7 Sparrows was
2700 feet. Initial climb rate was 55,000 feet per minute. Service ceiling was 58,000 feet. Normal range was 1550 miles, and maximum range with four
drop tanks was 1815 miles.
Dimensions: wingspan 21 feet 11 inches, length 54 feet 9 inches, height 13 feet 6 inches, wing area 196.1 square feet.
Weights: 14,900 pounds empty, 21,690 pounds combat, 31,000 pounds maximum takeoff.
Armament: One 20 mm M61A1 rotary cannon with 750 rounds plus two AIM-7 Sparrow
semi-active radar homing air-to-air missiles and two AIM-9 Sidewinder infrared
homing air-to-air missiles. In place of the Sparrows, a pair of Selenia Apside
radar homing air-to-air missiles can be carried. Up to 7500 pounds of bombs,
rockets, napalm tanks, and fuel tanks could be carried on nine hardpoints
(four underneath the wing, two at wingtips, one centerline, and one at each fuselage side).
Fuel: Standard internal fuel capacity 896 US gallons, which can be supplemented
by two 195-US gallon underwing tanks and two 170-US gallon wingtip tanks.
In addition, 121 US gallons could be carried in an auxiliary tank in the ammunition bay.
F-104J for Japan
On November of 1960, the Japanese government announced that it would acquire the Starfighter as its standard
air superiority fighter. An industrial cartel headed by Mitsubishi Heavy Industries
was given the responsibility for the license manufacture of the Starfighter
in Japan. The first few Japanese Starfighter would be assembled in Japan from
Lockheed-supplied components, but ultimately the Starfighter would be built
in Japan entirely from Japanese-manufactured components.
The Japanese Starfighter was given the designation F-104J, the J standing
for Japan. It was similar in overall structure to the F-104G, but was equipped
as an all-weather interceptor rather than as an air-to-ground strike aircraft.
One of the reasons for the choice of this option was that treaty restrictions
at the time prevented Japan from acquiring any aircraft which had even a hint
of an offensive role.
The F-104J was powered by a Japanese-built J-79-IHI-11A engine built under
license by Ishikawajima-Harima. It had an Autonetics NASARR F-15J-31 fire
control system optimized for the air-to-air mode, and was armed with a 20-mm
M61A1 cannon and four AIM-9 Sidewinder air-to-air missiles, two mounted underwing
and two carried on a rack on the fuselage centerline.
The first Lockheed-built F-104J (Model 683-07-14) flew on June 30, 1961. The
first three F-104J were built and assembled entirely by Lockheed. 29 more
F-104J were assembled by Mitsubishi from knocked-down kits provided by Lockheed
between March of 1962 and March of 1965. Further F-104J were built from scratch
by Mitsubishi, with a total of 178 Mitsubishi-manufactured F-104J being delivered
from March of 1965 through 1967.
The F-104DJ (Model 583B-10-17) was the two-seat trainer version of
the F-104J for Japan. They had electronics and other items that were compatible
with those of the single-seat version. Twenty examples were built by Lockheed
and reassembled in Japan between July of 1962 and January 1964. No F-104DJ
two-seaters were built from scratch in Japan.
The F-104J entered with the Koku Jietai (Japanese Air Self Defense Force,
or JASDF) in October of 1966. The first JASDF units to convert to the F-104J
were the 201st and 202nd Fighter Interceptor Squadrons (Hikotais) based at
Chitose and Nyutabaru. The 210 F-104J and the 20 F-104DJ operational trainers
were used exclusively in the interceptor role by seven Hikotais (the 201st
to 207th) of the Koku Jietai.
Beginning in December of 1981, the Japanese Starfighter were replaced by Mitsubishi-built
F-15J/F-15DJ Eagles. The last JASDF F-104J was retired by the 207th Hikotai
in March of 1986. During JASDF service, at least 34 F-104J and two F-104DJ
(about 15 percent of the force) were written off in accidents.
As JASDF F-104Js were retired, some were transferred to Taiwan. By 1987, the
ROCAF had received at least 22 F-104J and five F-104DJ through the "ALISAN 9" project.
Units of the JASDF flying F-104J:
201st Hikotai, 2nd Kokudan, Chitose Air Base, March 8, 1963 to October 1,
1974
202nd Hikotai, 5th Kokudan, Nyutabaru Air Base, 1964 to 1981
203rd Hikotai, 2nd Kokudan, Komatsu Air Base, 1965 to 1983
204th Hikotai, 5th Kokudan, Tsuiki Air Base, 1964 to 1984
205th Hikotai, 6th Kokudan, Komatsu Air Base, 1964 to 1984
206th Hikotai, 7th Kokudan, Hyakuri Air Base, 1966 to 1978
207th Hikotai, 7th Kokudan, Hyakuri Air Base, 1966 to 1970; to Naha Air Base, 1972 to 1985-1986
JASDF serial numbers:
Lockheed-built F-104DJ Starfighter c/n 583B-5401/5420
Lockheed-built F-104J Starfighter c/n 683B-3001/3003
Mitsubishi-built F-104J Starfighter c/n 683B-3004/3210
NETHERLANDS
A total of 138 Starfighter was delivered to the Koninklijke Luchtmacht (Royal Netherlands Air
Force, or KLu). These consisted of 95 F/RF-104G manufactured by the North
(Fokker) group, 25 F-104G manufactured by Fiat and the Italian group, and
18 TF-104Gs built by Lockheed. They were intended to replace the Republic
F-84F/RF-84F and Lockheed RT-33A that were serving with the KLu.
The F-104G entered Dutch service in December of 1962 with No. 306 Squadron
based at Twenthe. No 306 served as the operational conversion unit for the
training of Starfighter crews for all the other KLu F-104G squadrons that
were forming at the time. In January of 1964, this unit converted from F/TF-104G
to RF-104G reconnaissance aircraft, and its responsibility for Starfighter
crew training was transferred to the "Dutch Masters" operational conversion
unit based at Leeuwarden. The F-104Gs were operated in the interceptor role
by Nos. 322 and 323 Squadrons based at Leeuwarden and in the fighter-bomber
role with Nos. 311 and 312 Squadrons based at Volkel.
In the early 1980s, the Dutch Starfighter were replaced by European-built
F-16A/B Fighting Falcons. Conversion from F-104G was begun by the two interceptor
squadrons in 1979, and in June of 1984, No 312 Squadron stood down as the
last KLu operational F-104G unit. When No. 312 Squadron disbanded, its 18
F-104G and two four TF-104G were transferred to the CAV at Volkel until their
last formal Flypast on November 21, 1984.
Some 43 KLu Starfighter (35.8 percent of the force) were lost in accidents.
Following their withdrawal from service, the surviving KLu Starfighter were
transferred to Greece and Turkey.
KLu serials were assigned according to the manufacturer's construction numbers,
so there are some gaps which correspond to Starfighters delivered to other
nations.
The following units of the KLu operated Starfighter:
306 Squadron OCU at Twenthe from December 1962 until January 1964. Then to
tactical reconnaissance role and moved to Volkel in September 1969 to late 1983
311 Squadron, Volkel Tactical strike June 1964 to August 1982
312 Squadron, Volkel Tactical strike April 1965 to June 1984
322 Squadron, Leeuwarden All-weather interception August 1963 to mid 1979
323 Squadron, Leeuwarden All-weather interception March 1964 until August 1980
Training and Conversion Unit A, Leeuwarden, January 1964 until March 1978
Conversie Afdeling Volkel, Volkel January 1969 to November 1984
NORWAY
The Kongelige Norske Luftforsvaret (Royal Norwegian Air Force) was
at first equipped with MAP-supplied Starfighter. The KNL received the first
of 16 Lockheed-built RF-104G, 3 Canadair-built F-104G, and 2 Lockheed-built
TF-104G in 1963. The Lockheed-built RF-104G were converted to the F-104G configuration
and served with No. 331 Skvadron at Bodo. Following the arrival of Northrop
RF-5A for No. 717 Squadron, these aircraft reverted to the fighter configuration
and served until 1981.
Two ex-Luftwaffe TF-104G were later transferred to Norway from the Luke AFB
contingent operating in the United States.
In 1973, a second KNL Starfighter unit, No. 334 Skvadron, was formed with
eighteen ex-Canadian Forces CF-104 and four CF-104D. These aircraft were modified
to carry Martin Bullpup air-to-surface missiles and were employed in the anti-shipping
role.
In the early 1980s, the KNL Starfighter were withdrawn from service. At least
12 of the machines were transferred to Turkey in 1981. The last Norwegian
Starfighter, the CF-104/CF-104D of No. 334 Squadron, were phased out of service
during the winter of 1982-83. During their service with the KNL, only six
of the 44 Starfighter were lost in accidents.
KNL units operating the Starfighter:
331 Skvadron, Bodo, late 1973 to June 1981
334 Skvadron, Rygge, April 1973 to 1983
SPAIN
Eighteen Lockheed-built F-104G and three Lockheed-built TF-104G were delivered under MAP to Spain's Ejercito
del Aire in 1965. They replaced the F-86F Sabres of 61 Escuadron in Ala
6 at Torrejon. In Spanish service, they were designated C.8 (serials C.8-1
to C.8-18) and CE.8 (serials CE.8-1 to CE.8-3). The Ala 6 Wing was later renumbered
Ala 16 and the squadron 61 became 161 Esc and later 104 Esc.
The EdA (Ejercito del Aire) Starfighter had the distinction of operating without
a single accident during their seven years of service. They were formally
retired from EdA service in May of 1972, when they were replaced by the F-4C
Phantom. All of the EdA Starfighter were returned to the USAF for transfer
to Greece and Turkey.
More information about Spanish F-104 serials
Taiwan (Republic of China)
Accurate accounts of deliveries of Starfighter to Taiwan are hard to come
by, but it is known that an initial batch of 24 ex-USAF F-104A and 5 F-104B
were delivered to Taiwan in 1960-1961.
In 1964-69, Taiwan received 46 Lockheed-built F-104G, eight TF-104G, plus
21 RF-104G from Canadair. Another six F-104D were received in 1975 from former
Air National Guard squadrons In 1983, these Starfighter were augmented by
ex-Luftwaffe machines (38 F-104G and 27 TF-104G), these aircraft being from
the batch of Luftwaffe-owned Starfighter retained at Luke AFB for training
purposes and operating in USAF insignia and serials. By 1987, the ROCAF had
received at least 22 F-104J and five F-104DJ from Japan, together with 15
F-104G and three TF-104G from Denmark.
All in all, Taiwan has received at least 166 single-seat Starfighter and about
53 two-seater, plus possible additional and unknown quantities from Japan.
They have operated with the following units:
2nd (499th) Tactical Fighter Wing, Hsinchu 41st, 42nd and 48th Tactical Fighter
Squadrons (1984 to 1990)
3rd (427th) Tactical Fighter Wing, Ching Chuan Kang Air Base 7th, 8th, 28th
and 35th Tactical Fighter Squadrons (1965 to date)
5th (401st) Tactical Combined Wing, Taoyuan 12th Special Mission Squadron
Earlier plans to upgrade ROCAF Starfighter to F-104ASA standard by the installation
of FIAR Grifo fire control radar which would give them beyond-visible-range
AAM capability were abandoned.
All of the early series F-104A and B were withdrawn from service by the early
1980s, some of them having been transferred to Pakistan and Jordan. Others
were expended as drones or decoys. The F-104G were replaced by the Ching-Kuo
IDF in 1998.
More information about ROCAF F-104 serials
TURKEY
Turkey was one of the first NATO countries to receive Starfighter through
Mutual Aid Program (MAP) funding. Beginning in May of 1963, the Turk Hava
Kuvvetleri (THK) received an initial batch of 32 F-104G built by Lockheed
and Canadair, plus 4 TF-104G built by Lockheed. These aircraft equipped 141
and 142 Filo, plus an OCU, in AJU 4 at Murted.
In 1972, nine F-104G and two TF-104G from Spain were received to reinforce
two squadrons in 4 Wing at Murted.
In late December of 1974, the first six of an initial batch of 18 F-104S interceptors
were purchased new from Italy, with funds reportedly provided by Libya in
return for Turkish assistance in building up the Libyan Arab Republic Air
Force. These were delivered to 9 Wing. The remainder followed at a rate of
three per month. The THK F-104S order was doubled in May of 1975, and finally
increased to 40. These planes initially equipped Filos 142 and 182.
These aircraft took part in the 1976 Turkish invasion of Cyprus, but so far
as I know Greek and Turkish Starfighter never faced off against each other.
Beginning in n 1980-81, large numbers of CF-104/F-104G/TF-104G being phased
out of service in Belgium, Canada, Germany, Norway and the Netherlands began
to be transferred to Turkey. 18 F-104G were transferred from Belgium in 1981-83.
These were withdrawn by 1987. 43 F-104G (including 22 RF) and 10 TF-104G were
transferred from the Netherlands from August 1980 to March 1984. 9 F-104G,
3 CF-104, and 1 TF-104G were transferred from Norway in June and July of 1981.
From October of 1980, 170 ex Luftwaffe Starfighter were delivered to the THK,
the last ones arriving in 1988. Following their replacement in Canadian Forces
service by CF-18, 50 CF-104 (including six CF-104D) were transferred to Turkey
following an extensive overhaul in Germany.
Over the years, the THK has received just over 400 Starfighter from various
sources. The Turkish F-104s fulfilled both air defense and ground attack roles.
Over the years, many THK Starfighter were either withdrawn from service or
were cannibalized for spares to keep the others flying. Large numbers have
also been lost in crashes, but no overall accident statistics are available.
Starfighter have equipped the following squadrons of the THK:
4 Ana Jet Us Murted AB: 141 Filo, 142 Filo, Oncel Flight (OCU)
6 Ana Jet Us (Bandirma): 161 Filo, 162 Filo
8 Ana Jet Us (Diyarbakir): 181 Filo, 182 Filo
9 Ana Jet Us (Balikesir): 191 Filo, 192 Filo, 193 Filo
In 1987, the F-16C/D Fighting Falcon began to replace the F-104G in THK service.
First to convert were 141 Filo and 142 Filo at Murted, which exchanged their
F-104G for F-16s beginning in 1989. 161 and 162 Filo at Bandirma and 191 and
192 Filo at Balikesir had exchanged their Starfighter for F-16s by the early
1990s. Filo 181 finally relinquished its F-104G in favor of F-16s in April
of 1994, marking the final departure of the F-104G from THK service. This
still left Filo 182 of 8 AJU with CF-104, it stopped flying the 104 officially
on June 20, 1994. And it was 182 Filo which was the last unit also final flight
104 on June 20, 1994.
F-104N for NASA
Over the years, the National Aeronautics and Space Administration (NASA) has operated no less than 11 Starfighter
for flight test purposes.
In August of 1956, the seventh YF-104A (serial number 55-2961) was transferred
to NACA (later reorganized as NASA). It was initially numbered 818, but was
later renumbered with the civilian registration N818NA (the "NA" standing
for NASA). This airplane was used by NASA for various test flight purposes
until it was finally retired in November of 1975. It is on display at the
National Air and Space Museum in Washington.
In October of 1957, NASA acquired 2 ex-USAF F-104A single seaters (USAF serials
56-0734 and 56-0749) for use in flight testing. These planes were never assigned
NASA serial numbers, F-104A 56-749 crashed in 1962.
In December of 1959, F-104B serial number 57-1303 was transferred to NASA.
It was assigned the NASA number of 819. It served until 1978, when it was
finally retired.
Between August and October of 1963, Lockheed delivered 3 single-seat F-104G
Starfighter to NASA, these planes being designated F-104N (N for NASA). They
were to serve as high-speed chase aircraft. These three planes were the only
purpose-built Starfighter produced by Lockheed for NASA, all other Starfighter
operated by NASA were transferred to it from the USAF.
These 3 NASA F-104N were initially numbered 011, 012, and 013. 013 was lost
on June 8, 1966 when it became involved in a mid-air collision with the second
North American XB-70A Valkyrie during a General Electric-sponsored advertising
publicity photographic flight. The pilot flying the F-104N, the experienced
test pilot Joseph A. Walker, was killed. The XB-70A pilot, Alvin S. White
ejected with injuries, but the XB-70A copilot, Major Carl S. Cross, went down
with the Valkyrie and was killed.
The two surviving F-104N were later given the civilian registrations N811NA
and N812NA.
In December of 1966, NASA acquired another ex-USAF F-104A (serial number 56-0790)
as a replacement for NASA 813. It was assigned the NASA number 820, and was
withdrawn from use on October 30, 1983.
Later, NASA also received some additional F/TF-104G from military sources.
In 1975, NASA received 2 TF-104Gs and 1 single-seat F-104G, giving them the
civilian numbers N824NA, N825NA and N826NA respectively. N824NA and N825NA
are ex-Luftwaffe TF-104G two-seaters (carrying USAF serials 61-3065 and 66-13628),
whereas N826NA was originally a Fokker-built single-seat RF-104G which had
originally been built for the Luftwaffe (original German serial number was
KG+313). All of their military equipment was removed, and they were used by
NASA for various flight test purposes.
More information at NASA research aircraft
RTF-104G1
The RTF-104G1 was an all-weather day and night reconnaissance development
of the TF-104G which was proposed to meet a Luftwaffe requirement. The RTF-104G1
was to carry photographic cameras, infrared sensors, and was to be equipped
with sideways-looking radar. The RTF-104G1 was not proceeded with because
the Luftwaffe selected the McDonnell RF-4E Phantom II for this mission.
F-104H "Stripped Starfighter"
The F-104H was a projected simplified version of the F-104G with less sophisticated
and less costly equipment. It was designed for export to nations which wanted
a Mach 2-capable fighter but which could not afford the full-blown all-weather
F-104G version. An optical gunsight was to be fitted in place of the NASARR
of the F-104G. A two-seat version was also proposed, which was to be designated
TF-104H.
Very little interest was expressed by anyone for the F-104H, and neither version
ever got past the initial design stage.
Lancer
The Lockheed CL-1200 Lancer was a late 1960s company-funded proposal for a
new and improved Starfighter. It was intended for the export market and was
in direct competition with the Northrop F-5E Tiger II.
The CL-1200 retained the basic F-104 fuselage but was fitted with a shoulder-mounted
wing of larger area which was moved further aft. The new wing had a span of
29 feet and still featured leading- and trailing-edge flops plus inner strakes.
The tailplane was moved from the tip of the vertical fin to the base of the
rear fuselage. in order to avoid the downwash effects from the high set wings
at high angles of attack and to eliminate the Starfighter's inherent pitch-up
problems.
The first version was to be the CL-1200-1, still with the now well- proven
J79-GE-19 engine. The more advanced CL-1200-2 was to have had a redesigned
rear fuselage that could accommodate a modern turbofan engine rather than
the J79 turbojet. This turbofan engine was to be either the Pratt & Whitney
TF30-P-100 or the F100-P-100. These engines offered an increase of 60 percent
in thrust at maximum power. The air intakes were located in the same place
that they were on the F-104, but they incorporated translating shock cones
with four-inch movement in place of the F-104's fixed cones.
The Lancer retained the 20-mm General Electric M61 A1 cannon as its primary
built-in armament, although a 30-mm DEFA gun could be fitted as an alternative
if the customer so desired. Nine weapons stations were provided, one under
the fuselage, three under each wing, and one at each wingtip. Up to 12,000
pounds of ordinance could be carried.
The estimated gross weight was 35,000 pounds and a top speed of 1700 mph at
35,000 feet was envisaged. The takeoff run was 1450 feet in the intercept
configuration, only 52 percent of that required for the F-104G. Kelly Johnson
projected that the CL-1200-2 would be superior in air-to-air combat to any
known fighter.
At one time, the USAF had considered acquiring one or more examples of the
Lancer. The USAF planned to buy at least one experimental Lancer under the
experimental designation X-27. The X-27 was to be similar in overall configuration
to the Lancer but was to feature modified engine air intakes having a rectangular
shape. However, the X-27 program was terminated due to lack of funds before
anything could be built.
The CL-1200 was entered in the International Fighter Aircraft competition
to find a replacement for the Northrop F-5 Freedom Fighter in the international
market. It was projected that CL-1200 deliveries could begin in 1974. However,
in November 1970 the Northrop F-5-21 was named the winner of the competition,
and the primary market for the Lancer was lost. The project was then terminated.
Another stillborn Starfighter derivative was the CL-704 VTOL strike and reconnaissance
aircraft originally proposed in 1962. For VTOL operations, it was to have
had seven vertically-mounted Rolls Royce RB.181s in each of the enlarged wingtip
pods. The main forward propulsion was to have been provided by a fuselage-mounted
Rolls Royce RB.168.
A larger-winged F-104 derivative was proposed as an alternative to the MRCA
(Multi-Role Combat Aircraft) then being designed as a multi-national European
project. Nothing ever emerged, and the MRCA eventually emerged as the Panavia
Tornado.
Specification of the Lockheed CL-1200-2 Lancer:
One Pratt & Whitney TF30-P-100 turbofan, rated at 15,000 lb.s.t. dry and 25,000 lb.s.t. with afterburner.
Performance: Maximum speed 1700 mph at 35,000 feet (Mach 2.57), 920 mph (Mach 1.21) at sea level. Initial climb rate 60,000+ feet per minute. 420 miles
combat radius with 4000-pound bomb load. Takeoff run was 1450 feet to liftoff, landing run was 2060 feet.
Dimensions: length 57 feet 3 inches, wingspan 29 feet 2 inches, height 17 feet 2 inches, wing area 300 square feet.
Weights: 16,640 pounds empty, 24,385 pounds normal loaded, 35,000 pounds maximum takeoff.
Armament: One 20-mm General Electric M61A1 cannon with 725 rounds. An external offensive load of up to 12,000 pounds could be carried on nine external weapons
hardpoints.
Sources:
The World's Great Interceptor Aircraft, Gallery Books, 1989.
Lockheed F-104 Starfighter, Steve Pace, Motorbooks International, 1992.
Lockheed Aircraft Since 1913, Rene J. Francillon, Naval Institute Press, 1987.
The American Fighter, Enzo Angelucci and Peter Bowers, Orion, 1987.
The World's Fighting Planes, William Green, Doubleday 1968.
American Combat Planes, Ray Wagner, Third Enlarged Edition, Doubleday, 1982.
Lockheed F-104 Starfighter, John Fricker and Paul Jackson, Wings of Fame,
Vol 2, Aerospace Publishing Ltd, 1996.
The Illustrated Encyclopedia of Aircraft Armament, Bill Gunston, Orion Books, 988.
The Lockheed F-104G/CF-104, Gerhard Joos, Aircraft in Profile No. 131, Doubleday,1969.
Mikoyan MiG-21, Bill Gunston, Osprey, 1986.
Lancer, Air Enthusiast, September 1971.
The Aircraft of the World, William Green and Gerald Pollinger, Doubleday, 1965.
Joe Baugher
To my best knowledge!!! Given information is based on best available references! |
Any contribution is highly welcome, please contact the webmaster |
compiled by: Hubert Peitzmeier |
update: @ February 20, 2022 |