F-16 Reference
5th Gen Fighters
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Found 419 aircraft, displaying 1-15
[Sorted by Date]
| Date |
Status |
Local S/N |
Aircraft |
AF/Unit |
Version |
Info |
Details |
| 08 May 1975 |
[i/a] |
01568 |
72-1568
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YF-16
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Article
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Details
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Belly landed on a grass area next to the runway at Carswell AFB, Texas. The right main landing gear jammed due to gyroscopic forces from right max-rate roll while the gear was being retracted. The aircraft was only slightly damaged (inlet duct buckling, FS227 bulkhead cracks, etc.). It was scheduled to appear at the Paris air show but due to the mishap the first prototype was sent.
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| Jan 1981 |
[act] |
75745 |
75-0745
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F-16A
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Details
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Dead stick landing but was repaired.
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| Oct 1980 |
[act] |
75747 |
75-0747
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F-16A
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Details
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The aircraft crash landed on Rogers dry lake bed at Edwards AFB due to a blown nose gear tire on take off during the annual open house air show. It was shipped to General Dynamics Fort Worth in a C-5 and rebuilt into the first F-16XL, flying back to Edwards one year later on December 2nd, 1981. The pilot survived unharmed but very shaken.
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| Nov 1989 |
[i/a] |
78002 |
78-0002
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USAF 310 TFTS |
F-16A
Block 1
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Details
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Engine turbine failed during a take-off roll sending pieces of the turbine blades through the fuel cell. Pilot aborted take off after seeing the fire light and shut down the engine. After the pilot opened the canopy and jumped out found the entire tail of the F-16 on fire. The aircraft was sent to depot but was never repaired.
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| 11 Feb 1985 |
[w/o] |
78004 |
78-0004
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USAF 310 TFTS |
F-16A
Block 1
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Details
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Destroyed near Luke AFB, Arizona at Gila Bend Auxillary Air Field due to an engine failure. Pilot ejected safely.
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| 01 Oct 1979 |
[w/o] |
78006 |
78-0006
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USAF 16 TFTS |
F-16A
Block 1
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Details
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Crashed in Nevada due to an engine problem. 78-0002 and 78-0006 were coming from Hill AFB to bring spare parts. The unit was on a TDY to Nellis at the time of the mishap. 78-0002 landed first and 78-0006 was second in line. The aircraft was on a normal landing approach. On touchdown the main landing gear collapsed. This was supposed to be impossible but it happened. Probable cause was that the gear was not fully down. The centerline fuel tank exploded on contact with the runway. The pilot selected full afterburner and managed to get the aircraft airborne again. The pilots logic would be that the entire ramp at Nellis was packed with aircraft and that he didn't want his disabled aircraft to slide off the runway and cause a major accident. The pilot climbed to approximately 500 feet, trailing about a 100 feet of flames, banked the aircraft left towards the desert, leveled out and ejected. There was a cheer from everyone who witnessed the accident when the pilots' chute opened. As an additional note: The Thunderbirds had been practicing just moments before the accident. Every practice is videotaped. They missed capturing the entire event on film by just a few moments. Also as a bit of irony: the spare parts were being carried by the aircraft that crashed.
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| 24 Jan 1991 |
[w/o] |
78009 |
78-0009
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USAF 184 TFG |
F-16A
Block 1
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Details
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Collided with F-16A (80-0536), near Beaumont, Kansas. One of the pilots, Major Cary Carlin, was killed.
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| 06 Apr 1981 |
[i/a] |
78013 |
78-0013
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USAF 388 TFW |
F-16A
Block 1
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Details
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Crashed at Holloman AFB, New Mexico due to fuel starvation. After being written-off, it was transferred to Lowry TTC as a GF-16A
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| 12 Apr 1982 |
[i/a] |
78016 |
78-0016
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USAF 16 TFTS |
F-16A
Block 1
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Details
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Flew into the ground at Dugway range, Utah at Michael AAF. Aircraft lost control during an attempted emergency landing. Pilot was able to eject safely. It was then put in the dump at Hahn Air Base. Later used for ABDR.
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| Unknown |
[act] |
78019 |
78-0019
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USAF 388 TFW |
F-16A
Block 1
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Details
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Ran off the runway at Salt Lake City International Airport in/about 1981. Had extensive damage to the right wing and fuselage. The wing was replaced from a block 10 aircraft. An interesting note to this repair is that the fuselage was reassembled on wooden cradles, with no precision alignment. The misalignment was discovered when the boresight was accomplished after repair, the fuselage was "twisted" to the right approx .250" from the F.S. 189 bulkhead forward. The gun and HUD mounts had to be moved .250" to compensate. It actually turned out to be the 466th TFS's best bomber after that. Anyone know the exact date of this mishap or more information please let us know.
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| 26 Mar 1980 |
[w/o] |
78023 |
78-0023
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USAF 388 TFW |
F-16A
Block 5
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Details
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Destroyed in a fire due to an engine failure that sent some turbine parts through the main fuel cells. The pilot, who's last name as Bell, was from the Operational, Test & Evaluation squadron but using 388th TFW aircraft ejected safely after trying to restart the engine. The fact that the aircraft did not blow up was a relief to some early pilots as they were not convinced that the new designed fuel cells would preform as advertised. The fuel cells are sealed partitions in the fuselage. However, the major concern was about the fly by wire flight control system and what happened if the power was totally lost if the flight controls went "stupid". It was well understood that loss of flight controls could cause 20 Gs in less than a quarter of a second. Pilot DW Bells ejected safely.
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| 22 Mar 1990 |
[w/o] |
78041 |
78-0041
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USAF 466 TFS |
F-16A
Block 5
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Details
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Had a mid-air collision with F-16A (#78-0045) near Wendover, Utah
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| 20 Mar 1982 |
[act] |
78044 |
78-0044
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USAF 34 TFS |
F-16A
Block 5
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Interview
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Details
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In Lt. Col. Pat "Gums" McAdoo's words:
"I was the first Viper pilot to successfully land the thing with a failed leading edge flap. Was early spring/late winter 1982. Maybe 20 March, tail number 044, as that log entry shows 0.3 hours and a precision approach. Weather was not ll that keen. Have the HUD video in VHS format."
"Maintenance troops had failed to insert a 'keeper' bolt that is supposed to keep the flap drive tubes from slipping apart. It's like a cotter key on a bolt. The flap drive motor has a spline gear on it and the drive tube has gear teeth that match up. So the drive tube gradually slipped out from the motor spline gear. When I rotated, the drive tube slid all the way out and the leading edge flap went up until the wing upper surface stopped it. Maybe 50-60 degrees. Another troop had his fail a few months later and the flap went to 90 degrees because he was going a lot faster when the drive tube failed. So I was at 160 knots and holding full left stick. Post-flight data revealed that I had about one pound of control authority for banking left. So I was holding 15-16 pounds of left stick the whole time. "
"I stayed at 170-180 knots, as I could still maintain control and wasn't gonna play Chuck Yeager more than I had to. Nevertheless, I was the first troop to fly the thing in that configuration, so everything was new territory. Bunted over to get opposite flap 2 degrees up and locked the flaps( LEF's go up when bunting over, or when weight is on wheels). I now had both LEF's up, and it seemed to help with the roll authority. Additionally, that other flap wasn't gonna be moving all over the place, and this kept things a little more predictable. "
"Came around on the ILS and landed in one helluva crab. The drag was so great that I almost landed short when I pulled off the power. As I was coming in a lot hotter than normal, I thought I would land long. heh heh, sucker dropped like a rock and I was able to make a mid-field turn off."
Exact date of this mishap is not known, but did happen in 1982.
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| 22 Mar 1990 |
[w/o] |
78045 |
78-0045
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USAF 466 TFS |
F-16A
Block 5
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Details
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Had a mid-air collision with F-16A (#78-0041) near Wendover, Utah.
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| 05 Aug 1981 |
[w/o] |
78046 |
78-0046
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USAF 388 TFW |
F-16A
Block 5
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Details
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Crashed in the Utah Test & Training Range, killing the pilot, Captain J. Edgington Moats. All USAF F-16's were grounded two days later. It was the F-16's second grounding. Cause of accident was a malfunctioning bleed air valve which allowed bleed air to leak out onto the EPU, causing an electrical surge that shut down the flight control computer
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Abbreviations and symbols:
| [act] |
Active |
[msh] |
Involved in Mishap |
[sto] |
Stored (e.g. at AMARC) |
| [cld] |
Cancelled order |
[o/o] |
On Order |
T/V |
LM Aero Type/Version (Construction) number |
| [emb] |
Embargoed |
[pre] |
Preserved (museum, gateguard) |
[w/o] |
Write-off |
| [i/a] |
Instructional Airframe |
[scr] |
Scrapped |
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Photo Available |
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