# N791FT: 1969 Douglas DC-8-73F, registration cancelled 2006-05-17 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 17, 2006 - Status when cancelled: Valid registration - Airframe: [Douglas DC-8-73F](https://openairdocs.org/model/douglas-dc-8-73f) (registry code 302199F) - Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802) - Data sheets: [TCDS 4A25](https://openairdocs.org/tcds/4A25) (OpenAirDocs) - Serial number: 46045 - Year built: 1969 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: March 30, 1984 - Certificate issued: November 18, 2004 - Last registry action: December 15, 2004 - Mode S code: AABC4B - Owner when cancelled: [Aeroturbine Inc](https://openairdocs.org/faa-owner/AEROTURBINE%20INC) - Location: [Miami, FL](https://openairdocs.org/faa-place/FL/Miami) - Owner type: Corporation - Owner's area on the map: 25.8050° N, 80.3151° W: Placed by OpenAirDocs at the center of ZIP code 33122, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N791FT - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=791FT - Page: https://openairdocs.org/deregistered/N791FT-2006-05-17 From the FAA registry file of October 31, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Douglas DC-8-73F: https://openairdocs.org/model/douglas-dc-8-73f.md ## Service difficulty reports (159, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR RRXA1136](https://openairdocs.org/sdr/RRXA1136), Jul 26, 2001: SKIN. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LOWER BELLY SKIN AT STA. 600-680 AND L33R-L34L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE A - [SDR RRXA11337](https://openairdocs.org/sdr/RRXA11337), Jul 26, 2001: DOOR. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO R/H KEEL PRESSURE PANEL AT STA. 705, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// - [SDR RRXA011048](https://openairdocs.org/sdr/RRXA011048), Jun 19, 2001: SKIN. CORRODED. AFTER LANDING DISCOVERED CORROSION ON OUTER FUSELAGE, LEFT LOWER SIDE AT FS 1320. - [SDR RRXA001056](https://openairdocs.org/sdr/RRXA001056), Sep 20, 2000: LANDING GEAR. NOISY. AFTER T/O UPON GEAR RETRACTION THERE WAS A LOUD NOISE FROM NOSE GEAR THAT SOUNDED LIKE NOSE WHELL SCRUBBER WASN'T STOPPING ONE OF THE TIRES HOWEVER AS A/S INCRE - [SDR RRXA001050](https://openairdocs.org/sdr/RRXA001050), Aug 22, 2000: CONNECTOR. LOOSE. PRECAUTIONARY SHUTDOWN OF NR 3 ENG DUE TO NO EGT, ANALOG OR DIGITAL AT 1123Z. NO OIL PRESSURE IND WITH WINDMILLING ENGINE. INSPECTED NR 3 EGT INDICATION SYS, FO - [SDR RRXA001046](https://openairdocs.org/sdr/RRXA001046), Aug 12, 2000: INDICATOR. INOPERATIVE. NR 4 EGT INOP, NR 4 EGT 870 DEG ON CLIMBOUT 3000 FT. N1 89 PERCENT, ALL OTHER PARAMETERS NORMAL. REMOVED AND REPLACED EGT INDICATOR, LEFT AND RIGHT HARNESS IAW - [SDR RRXA001045](https://openairdocs.org/sdr/RRXA001045), Aug 11, 2000: DOOR. MALFUNCTIONED. AFTER T/O FROM MTY AND AFTER GEAR RETRACTION, LOUD VIBRATION AND NOISE WAS PRESENT FROM NOSE WHEEL AND FWD RIGHT SIDE OF FUSELAGE. ON APP GEAR LOWERED AND NOISE - [SDR RRXA001019](https://openairdocs.org/sdr/RRXA001019), Jul 21, 2000: BALLAST. DEFECTIVE. STRONG ELECTRICAL SMELL COMING FROM GLARESHIELD AREA. FOUND GLARESHEILD OVERHEAD LIGHTS BALLAST DEFECTIVE. ORDERED PARTS. LIGHTS DEFFERED PER MEL 33-1, CAT C, D - [SDR RRXA000260](https://openairdocs.org/sdr/RRXA000260), Apr 20, 2000: SKIN. CORRODED. CORROSION STA 1260 L36 SKIN PANEL A. IN WORK (OPEN).CLOSING ACTION. REMOVED PAINT IAW DC8 SRM 51-1-8. CUTOUT CORROSION AT L36,L35R & L35L AT STA. 12600 AND FABR - [SDR RRXA991587](https://openairdocs.org/sdr/RRXA991587), Nov 25, 1999: SWITCH. MALFUNCTIONED. LM GEAR DOWN (GREEN) LIGHT WILL NOT ILLUMINATE GEAR WARNING (RED) LIGHTS NORMAL RECYCLED GEAR. NO HELP LIGHT CAME ON DURING FINAL APPROACH. REMOVED AND REPLACED - [SDR RRXA991525](https://openairdocs.org/sdr/RRXA991525), Nov 8, 1999: RECTIFIER. FAILED. LOST POWER TO EGT INDICATORS ANS SAI WHILE IN FLIGHT AT FL330. FOUND DC BUS BLOCKER RECTIFIER R7-5 WDM 24-4-1 P44 BAD. REMOVED AND REPLACED SAME, OPS CKS NORMAL - [SDR RRXA991685](https://openairdocs.org/sdr/RRXA991685), Sep 6, 1999: SKIN. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FORWARD PRESSURE PANEL BETWEEN Y=-52 TO Y=-12 AND Z=-8. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED D - [SDR RRXA991683](https://openairdocs.org/sdr/RRXA991683), Sep 5, 1999: SKIN. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LEFT WING, LEADING EDGE, UPPER SURFACE SKIN BETWEEN XFS=20 TO XFS=38.750. DAMAGE EXCEEDED LIMITATIONS IAW D - [SDR RRXA991511](https://openairdocs.org/sdr/RRXA991511), Sep 5, 1999: SKIN. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FINGER DOUBLER AT LONGERON 31 LEFT BETWEEN STA 440 AND STA 460 LT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMA - [SDR RRXA991507](https://openairdocs.org/sdr/RRXA991507), Sep 5, 1999: SKIN. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, WING, SCREWS PULLING THROUGH SKIN LEFT WING INBOARD LEADING EDGE UPPER BETWEEN STA XFS 20 AND STA XFS 38.750 AT FRON - [SDR RRXA991488](https://openairdocs.org/sdr/RRXA991488), Sep 5, 1999: SKIN. DAMAGED. DURING A MAINTENANCE VISIT, FOUND FASTENERS LOOSE RIGHT WING O/B SLOT L/E O/B END AT STA XS 491.193. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREAT - [SDR RRXA991495](https://openairdocs.org/sdr/RRXA991495), Sep 3, 1999: SKIN. CRACKED. DURING A MAINTENANCE VISIT FOUND 4 CRACK EXTENDING FROM RIVET RT WING UPPER SURFACE AT STA 69.5 AT REAR SPAR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAG - [SDR RRXA991502](https://openairdocs.org/sdr/RRXA991502), Sep 2, 1999: INSERT. STRIPPED. DURING A MAINTENANCE VISIT, FOUND NUMEROUS TRAY TIE DOWN INSERTS STRIPPED. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1- - [SDR RRXA991501](https://openairdocs.org/sdr/RRXA991501), Aug 31, 1999: SUPPORT. DAMAGED. DURING A MAINTENANCE VISIT, REMOVED AND REPLACED FLAP LINK SUPPORT ASSY RT O/B STA 340. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW D - [SDR RRXA991500](https://openairdocs.org/sdr/RRXA991500), Aug 31, 1999: SUPPORT. DAMAGED. DURING A MAINTENANCE VISIT REMOVE AND REPLACE FLAP LINK SUPPORT ASSY RT MID STA 219. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 - [SDR RRXA991719](https://openairdocs.org/sdr/RRXA991719), Aug 28, 1999: FLOOR PANEL. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL E-2 BETWEEN Y=1500 TO Y=1540. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGED, - [SDR RRXA991513](https://openairdocs.org/sdr/RRXA991513), Aug 28, 1999: SKIN. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, AT FINGER DOUBLERS ABOVE M/W/W BETWEEN STA 940 AND STA 980, 8 CENTER OF FLOOR PRESS PANEL. DAMAGE EXCEEDED - [SDR RRXA991496](https://openairdocs.org/sdr/RRXA991496), Aug 28, 1999: DUCT. DAMAGED. DURING A MAINTENANCE VISIT FOUND DUCT THAT GOES UNDER CONSTANT SECTION HAS HOLE (EO). DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC- - [SDR RRXA991749](https://openairdocs.org/sdr/RRXA991749), Aug 27, 1999: FLOOR PANEL. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL E-2 BETWEEN Y=1580 TO Y=1680. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, T - [SDR RRXA991747](https://openairdocs.org/sdr/RRXA991747), Aug 27, 1999: FLOOR PANEL. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL C-2 BETWEEN Y=1500 TO Y=1540 AND X=-10. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED - [SDR RRXA991720](https://openairdocs.org/sdr/RRXA991720), Aug 27, 1999: FLOOR PANEL. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL D-2 AT Y=1560. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW - [SDR RRXA991504](https://openairdocs.org/sdr/RRXA991504), Aug 25, 1999: RETRACT PIN. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, MAIN LANDING GEAR STRUT, LT AND RT MLG RETRACT PIN ASSY (EO). DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, - [SDR RRXA991491](https://openairdocs.org/sdr/RRXA991491), Aug 25, 1999: SKIN. DAMAGED. DURING A MAINTENANCE VISIT, FOUND NR 4 STUB WING MOUNTING HOLE BROKEN OUT AT DOUBLER AT STA XS 515.720, 26 FWD OF FRONT SPAR. DAMAGE EXCEEDED LIMITS IAW DC-8 SR - [SDR RRXA991696](https://openairdocs.org/sdr/RRXA991696), Aug 24, 1999: FINGER DOUBLER. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FINGER DOUBLER BETWEEN Y=940 TO Y=960 AND BETWEEN X=0 TO X=-6 AND Z=-8. DAMAGE EXCEEDED LIMITATIONS IAW DC- - [SDR RRXA991510](https://openairdocs.org/sdr/RRXA991510), Aug 20, 1999: FLOOR PANEL. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, UPPER CARGO COMPARTMENT FLOOR PANEL CORRODED (EXFOLIATION) REQUIRES REPAIR DOUBLERS. DAMAGE EXCEEDED LIMIT - [SDR RRXA991508](https://openairdocs.org/sdr/RRXA991508), Aug 20, 1999: FLOOR PANEL. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, UPPER CARGO COMPARTMENT FLOOR PANEL CORRODED (EXFOLIATION) REQUIRES SKIN REPLACEMENT. DAMAGE EXCEEDED LIMI - [SDR RRXA991498](https://openairdocs.org/sdr/RRXA991498), Aug 19, 1999: SUPPORT. DAMAGED. DURING A MAINTENANCE VISIT, REMOVED AND REPLACED FLAP LINK SUPPORT ASSY LT MID STA 219. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW D - [SDR RRXA991494](https://openairdocs.org/sdr/RRXA991494), Aug 18, 1999: SKIN. CRACKED. DURING A MAINTENANCE VISIT FOUND RT W/W FWD PRESS WEB CRACKED IN RECESS OF REMOVEABLE PANEL O/B OF PANEL AT STA 849 XCW 64. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. - [SDR RRXA991492](https://openairdocs.org/sdr/RRXA991492), Aug 18, 1999: DOOR TRACK. BENT. DURING A MAINTENANCE VISIT FOUND A PIT RT TRACK WORN AND BENT AT STA 360. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8 - [SDR RRXA991493](https://openairdocs.org/sdr/RRXA991493), Aug 17, 1999: PANEL. MISSING. DURING A MAINTENANCE VISIT FOUND ROBBED PYLON PANEL ASSY FOR A/C N8085U NR 3 PYLON (EO). DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW - [SDR RRXA991499](https://openairdocs.org/sdr/RRXA991499), Aug 12, 1999: SUPPORT. DAMAGED. DURING A MAINTENANCE VISIT, REMOVED AND REPLACED FLAP LINK SUPPORT ASSY LT O/B AT STA 340. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IA - [SDR RRXA991489](https://openairdocs.org/sdr/RRXA991489), Aug 11, 1999: DUCT. CRACKED. DURING A MAINTENANCE VISIT FOUND UPPER CARGO COMPT AIR DUCT AT STA 70, LT SIDE DUCT CRACKED. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA - [SDR RRXA991725](https://openairdocs.org/sdr/RRXA991725), Jul 27, 1999: FLOOR PANEL. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL B-3 BETWEEN Y=280 TO Y=580 AND X=40. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DA - [SDR RRXA991723](https://openairdocs.org/sdr/RRXA991723), Jul 27, 1999: FLOOR PANEL. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL C-1 BETWEEN Y=280 TO Y=580 AND X=30. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DA - [SDR RRXA991698](https://openairdocs.org/sdr/RRXA991698), Jul 27, 1999: FLOOR PANEL. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL E BETWEEN Y=280 TO Y=580 AND X=45. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMA - [SDR RRXA991483](https://openairdocs.org/sdr/RRXA991483), Jul 22, 1999: BULKHEAD. CRACKED. DURING A MAINTENANCE VISIT FOUND CRACK, AFT PRESSURE BULKHEAD AT STA 1766 BETWEEN LONGERONS 10 LEFT AND LONGERON 11 LEFT, APPROX 2-1/2, BETWEEN BL 25.0 RIGHT AN - [SDR RRXA991481](https://openairdocs.org/sdr/RRXA991481), Jul 22, 1999: BULKHEAD. CRACKED. DURING A MAINTENANCE VISIT FOUND CRACK, AFT PRESSURE BULKHEAD AT STA 1766, I/B AREA BETWEEN LONGERONS 10 RIGHT AND LONGERON 11 RIGHT, A 2.75 CRACK BETWEEN BL 24 - [SDR RRXA991490](https://openairdocs.org/sdr/RRXA991490), Jul 21, 1999: SKIN. DENTED. DURING A MAINTENANCE VISIT FOUND DENT, NR 1 ENGINE RING COWL AT 5 O'CLOCK POSITION. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 - [SDR RRXA991713](https://openairdocs.org/sdr/RRXA991713), Jul 20, 1999: FLOOR PANEL. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL BETWEEN Y=968 TO Y=973 AND BETWEEN X=45 TO X=59. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM - [SDR RRXA991712](https://openairdocs.org/sdr/RRXA991712), Jul 20, 1999: FLOOR PANEL. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL BETWEEN Y=949 TO Y=952 AND BETWEEN X=45 TO X=59. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM - [SDR RRXA991752](https://openairdocs.org/sdr/RRXA991752), Jul 19, 1999: SKIN. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO EXTERIOR SKIN PANEL BETWEEN Y=857 TO Y=980 AND LONGERON 36. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOV - [SDR RRXA991684](https://openairdocs.org/sdr/RRXA991684), Jul 19, 1999: SKIN. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO EXTERNAL SKIN BETWEEN Y=857 TO Y=980 AND LONGERON 36. REMOVED DAMAGE SKIN, TREATED AREA IAW DC-8 SRM. FABRI - [SDR RRXA991509](https://openairdocs.org/sdr/RRXA991509), Jul 17, 1999: WEB. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION BLISTER AT STA 1766, LONGERON 10 RIGHT, 24 LEFT OF RBL ON STAB FRONT SPAR ANGLED WEB DIRECTLY BEHIND AFT BULKHEAD INS - [SDR RRXA991505](https://openairdocs.org/sdr/RRXA991505), Jul 17, 1999: SKIN. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, AT STA 718, LONGERON 35 RIGHT ON EXTERNAL SKIN UNDER FWD FILLET PANEL. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM - [SDR RRXA991711](https://openairdocs.org/sdr/RRXA991711), Jul 16, 1999: FLOOR PANEL. CORRODED. DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL A-3 BETWEEN Y=940 TO Y=980 AND X=50. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DA All 159: https://openairdocs.org/deregistered/N791FT-2006-05-17/reports.md ## NTSB investigations (2) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB SEA88IA121](https://openairdocs.org/ntsb/SEA88IA121), Jun 30, 1988: Mcdonnell Douglas DC-8-73F (N791FT), Seattle, WA, incident, minor damage - [NTSB NYC70IN083](https://openairdocs.org/ntsb/NYC70IN083), Feb 4, 1970: Douglas DC-8 (N791FT), Las Vegas, NV, incident, no damage ## FAA accident and incident reports (6) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 19900123003969I](https://openairdocs.org/incident/19900123003969I), Jan 23, 1990: Doug DC873F (N791FT), Dayton, OH. Stabilizer trim did not respond to control efforts. Trim system sprocket housing gear box had sheared pin. - [Incident 19880630042539I](https://openairdocs.org/incident/19880630042539I), Jun 30, 1988: Doug DC873F (N791FT), Seattle, WA, Minor damage. Right main landing gear brakes locked on landing. Blew all 4 tires and ground down wheel and brake assembly. - [Incident 19850312012219I](https://openairdocs.org/incident/19850312012219I), Mar 12, 1985: Doug DC863F (N791FT), Los Angeles, CA, Minor damage. Main system hydraulic problem en route. Blew 4 tires on landing. Engine driven hydraulic system anti skid failure. - [Incident 19800421049619I](https://openairdocs.org/incident/19800421049619I), Apr 21, 1980: Doug DC863F (N791FT), Houston, TX. Engine shut down and flight returned. Found compressor blade damaged. - [Incident 19790103002059I](https://openairdocs.org/incident/19790103002059I), Jan 3, 1979: Doug DC863F (N791FT), Detroit, MI. Nr 3 engine driven hydraulic pump malfunctioned. Pn mumber 29147 4516. - [Incident 19780523039729I](https://openairdocs.org/incident/19780523039729I), May 23, 1978: Doug DC863F (N791FT), Jamaica, NY, Minor damage. Wheel rim failed on landing. ## Other aircraft with N791FT - [Cancelled 2025-09-23](https://openairdocs.org/deregistered/N791FT-2025-09-23): Swift Engineering SULE, S/N SULE_001. Owner: [Swift Engineering Inc](https://openairdocs.org/faa-owner/SWIFT%20ENGINEERING%20INC), [San Clemente, CA](https://openairdocs.org/faa-place/CA/San%20Clemente) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.