# N875AA: Anduril Industries FALCON - Status: Valid registration - Airframe: [Anduril Industries FALCON](https://openairdocs.org/model/anduril-industries-falcon) (registry code 06102I8) - Serial number: 648 - Type: Fixed wing single engine - Engine type: 2 cycle - Mode S code: AC08EA - Registered owner: [Anduril Industries Inc](https://openairdocs.org/faa-owner/ANDURIL%20INDUSTRIES%20INC) - Location: [Costa Mesa, CA](https://openairdocs.org/faa-place/CA/Costa%20Mesa) - Owner type: Corporation - Owner's area on the map: 33.6796° N, 117.9085° W: Placed by OpenAirDocs at the center of ZIP code 92626, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=875AA - Page: https://openairdocs.org/aircraft/N875AA From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. ## ADs that may apply (OpenAirDocs): 0 in force ### Matched by airframe (Anduril Industries FALCON) None in force. ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N875AA. ## FAA accident and incident reports None matched to N875AA. ## Reports on N875AA not matched to an aircraft (2) They name N875AA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [Incident 19910510030439I](https://openairdocs.org/incident/19910510030439I), May 10, 1991: Boeing 727223 (N875AA), Newark, NJ. Passenger smoked a cigarette while flying on a no-smoking flight between san juan and Newark airport. - [Incident 19850512024459I](https://openairdocs.org/incident/19850512024459I), May 12, 1985: Boeing 727223 (N875AA), Chicago, IL, Minor damage. Pressurization problems during climb. Emergency descent. Replaced water separator, temp controller, sensor, valve. ## Service difficulty reports None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. ## Service difficulty reports on N875AA not matched to an aircraft (52, newest 50) They name N875AA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR 2003F00486](https://openairdocs.org/sdr/2003F00486), Jul 5, 2003: ENGINE. LEAKING. DURING DESCENT AT FORT LAUDERDALE (KFLL), THE CREW SHUTDOWN NR 3 ENGINE DUE TO EXCESSIVELY HIGH OIL TEMPERATURE, FLICKERING FILTER BYPASS LIGHT, LOW OIL PRESSUR - [SDR AALA20011838](https://openairdocs.org/sdr/AALA20011838), Sep 27, 2001: STRINGER. CORRODED. TUL - FOUND CORROSION ON STRINGER TIE STATION 1133 ON INBOARD SIDE OF STRINGER 27L. CUT OUT CORRODED SECTION OF STRINGER STATION 1116 TO 1134. INSTALLED NEW STR - [SDR AALA20011840](https://openairdocs.org/sdr/AALA20011840), Sep 26, 2001: SHEAR TIE. CORRODED. TUL - FOUND CORROSION ON SHEAR TIE STATION 680 BETWEEN STRINGER 28R AND STR 29R. REMOVED CORRODED SHEAR TIE FLANGE AND INSTALLED REPAIR ANGLE PER SRM 53-10-4 FI - [SDR AALA20011839](https://openairdocs.org/sdr/AALA20011839), Sep 26, 2001: SHEAR TIE. CORRODED. TUL - FOUND CORROSION ON SHEAR TIE STATION 700 BETWEEN STRINGER 28R AND 29R. TRIMMED OFF DAMAGED SECTION OF SHEAR TIE AND INSTALLED REPAIR AT SKIN ATTACHMENT AS - [SDR AALA20011367](https://openairdocs.org/sdr/AALA20011367), Jul 5, 2001: LIGHT. INOPERATIVE. DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 27 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT STRIP AT ROW 27. SYSTEM GROUND CHECKED NORMAL OPER - [SDR AALA20010073](https://openairdocs.org/sdr/AALA20010073), Jan 10, 2001: ANGLE. CORRODED. TUL - FOUND CORROSION ON UPPER CHORD ANGLE AT STATION 1213. REMOVED CORROSION AND INSTALLED .032 17-7PH ANGLE REPAIR WITH .25 INCH HI-LOCK PER ESO 11697 DATED 1 - [SDR AALA20010121](https://openairdocs.org/sdr/AALA20010121), Jan 9, 2001: SKIN. CORRODED. TUL - FOUND BOTTOM CENTER WING SKIN HAS CORROSION AROUND HI-LOCK IN PLEUM CHAMBER ABOVE RIGHT PRIMARY HEAT EXCHANGER STRINGER 5 RBL 27. REMOVED CORROSION AND IN - [SDR AALA20010069](https://openairdocs.org/sdr/AALA20010069), Jan 9, 2001: FITTING. CRACKED. TUL - FOUND NR 6 FLAP TRACK FORWARD SUPPORT FITTING CRACKED. REMOVED AND REPLACED FITTING PER 51-10-01. (M) - [SDR AALA20010070](https://openairdocs.org/sdr/AALA20010070), Jan 8, 2001: SKIN. CORRODED. TUL - FOUND BULGE IN FUSELAGE SKIN STATION 1013 BETWEEN STRINGER 9R/10R, CORROSION ON SKIN. REPAIRED PER SRM 53-30-3, PART 1 FIG 1 SHEET 4, INSTALLED DOUBLER. ( - [SDR AALA20010072](https://openairdocs.org/sdr/AALA20010072), Jan 2, 2001: FRAME. CRACKED. TUL - FOUND FS 303 FRAME CRACKED .625 INCH AT STRINGER 16L CUTOUT. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER SB 727-53-153 R5. (M) - [SDR AALA20010068](https://openairdocs.org/sdr/AALA20010068), Dec 21, 2000: BEAM. CORRODED. TUL - FOUND CORROSION ON UPPER LEFT HORIZONTAL TIE (BEAM) 8 INCHES FROM INBOARD END. REMOVED CORROSION, TREATED AND PRIMED AND INSTALLED DOUBLER PER SRM 55-10-6 - [SDR AALA20010067](https://openairdocs.org/sdr/AALA20010067), Dec 21, 2000: BEAM. CORRODED. TUL - FOUND CORROSION ON TIE OF LEFT HORIZ STABILIZER OUTBOARD END 6 INCHES INBOARD OF OUTBOARD END, T/E BEAM. REMOVED CORROSION, TREATED AND PRIMED AND INSTALL - [SDR AALA20010071](https://openairdocs.org/sdr/AALA20010071), Dec 20, 2000: TORQUE BOX. CRACKED. TUL - FOUND LEFT LOWER TORQUE BOX VERTICAL WEB CRACKED AT LIGHTENING HOLE STATION 1283. ROUTED OUT CRACK AND INSTALLED DOUBLER PER SRM 51-40-2. (M) - [SDR AALA20002096](https://openairdocs.org/sdr/AALA20002096), Dec 14, 2000: SPLICE. FAULTY. DFW - DURING OVERNIGHT MAINTENANCE, CABIN FLOOR PATH EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH SPLICES AT AFT CABIN. SYSTEM GROUND CH - [SDR AALA20001966](https://openairdocs.org/sdr/AALA20001966), Nov 25, 2000: LIGHT. INOPERATIVE. DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD VENTRAL STAIR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED OVERHEAD VENTRAL STAIR EMERGENCY EXIT LIGHT ASSEMBLY. SYST - [SDR AALA20001608](https://openairdocs.org/sdr/AALA20001608), Oct 1, 2000: PCU. DEFECTIVE. MIA - FLT 331 - ON CLIMB-OUT MIA AT 6500 FEET WITH CLIMB POWER SET, AND 250 KNOTS AIRCRAFT YAWED RIGHT AND DID NOT RESPOND TO YOKE IMPUTS. AS WINGS WERE LEVELED - [SDR AALA20001209](https://openairdocs.org/sdr/AALA20001209), Jul 23, 2000: LIGHT. INOPERATIVE. MIA DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHTS AT AFT STAIRS INOPERATIVE. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECK NORMAL OPERATION. - [SDR AALA20000446](https://openairdocs.org/sdr/AALA20000446), Mar 9, 2000: LIGHT. INOPERATIVE. MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHT ASSEMBLY IN COCKPIT INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY IN COCKPIT. SYSTEM GROUND CHECK NORMAL OP - [SDR AALA20000159](https://openairdocs.org/sdr/AALA20000159), Jan 26, 2000: LIGHT. INOPERATIVE. DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SIGN AT AFT GALLEY INOPERATIVE. REPLACED EMERGENCY EXIT SIGN LIGHT ASSEMBLY AT AFT GALLEY. SYSTEM GROUND CHEC - [SDR AALA991847](https://openairdocs.org/sdr/AALA991847), Dec 2, 1999: LIGHT. INOPERATIVE. TUL - EMERGENCY EXIT LIGHT INOPERATIVE OVERAFT END OF AFT AIRSTAIRS. REPLACED LIGHT ASSEMBLY, OPS CHECK OK. (M) - [SDR AALA991846](https://openairdocs.org/sdr/AALA991846), Dec 1, 1999: ANGLE. CRACKED. TUL - RIGHT 760 CHORD ANGLE HFEC INDICATES CRACK BELOW RPR DOUBLER. INSTALLED REPAIR DOUBLER AT STATION 760 RIB CHORD ANGLE IAW SERVICE BULLETIN 727-57-0112, RE - [SDR AALA991845](https://openairdocs.org/sdr/AALA991845), Nov 29, 1999: LIGHT. INOPERATIVE. TUL - AFT CARGO DOOR EMERGENCY EXIT LIGHT ASSEMBLY HAD WIRE THAT WAS INTERMITTENT RT AFT EXT EMERGENCY LT ON AFT CARGO DOOR HAS 1 LAMP OUT. REPLACED LIGHT ASSEM - [SDR AALA991657](https://openairdocs.org/sdr/AALA991657), Nov 2, 1999: LIGHT. INOPERATIVE. DFW - DURING OVERNIGHT MAINTENANCE, AFT AIRSTAIR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT STAIR EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMA - [SDR AALA991269](https://openairdocs.org/sdr/AALA991269), Aug 24, 1999: SWITCH. DEFECTIVE. PHL - FLT 1845 - AFTER TAKEOFF PHL/MIA - ALL 3 RED GEAR WARNING LIGHTS AND TAIL SKID LIGHT ILLUMINATED WITH GEAR HANDLE IN UP POSITION. AIRCRAFT RETURNED TO PHL - [SDR AALA991266](https://openairdocs.org/sdr/AALA991266), Aug 24, 1999: UNIT. DEFECTIVE. PHL - FLT 0880 - AFTER TAKEOFF MIA/PHL - GEAR AND TAIL SKID UNSAFE LIGHTS REMAINED ILLUMINATED WHEN GEAR HANDLE WAS IN UP AND OFF POSITION. GEAR OPERATION WAS N - [SDR AALA991247](https://openairdocs.org/sdr/AALA991247), Aug 22, 1999: LIGHT. DEFECTIVE. DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING STRIP FORWARD OF FIRST CLASS INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHTING STR - [SDR AALA991246](https://openairdocs.org/sdr/AALA991246), Aug 22, 1999: LIGHT. DEFECTIVE. DFW - DURING OVERNIGHT MAINTENANCE, AFT AIRSTAIR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT AIRSTAIR EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NO - [SDR AALA990463](https://openairdocs.org/sdr/AALA990463), Apr 6, 1999: SWITCH. DEFECTIVE. MIA - FLT 808 - EN ROUTE POP, NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED IN FLIGHT. CREW FOLLOWED CHECKLIST AND SHUTDOWN NR 1 ENGINE. ENGINE WINDMILL TIME - [SDR AALA990145](https://openairdocs.org/sdr/AALA990145), Feb 3, 1999: LIGHT. DEFECTIVE. DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT OVER AFT LEFT GALLEY DOOR INOPERATIVE. REPLACED OVERHEAD GALLEY DOOR LIGHT ASSEMBLY. SYSTEM GROUND CHEC - [SDR AALA980964](https://openairdocs.org/sdr/AALA980964), May 13, 1998: LIGHT. INOPERATIVE. TPA - EMERGENCY EXIT LIGHT OVERHEAD IN AFT STAIRS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY IN AFT STAIRS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) - [SDR AALA980819](https://openairdocs.org/sdr/AALA980819), Apr 21, 1998: LIGHT. INOPERATIVE. MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHT ABOVE LEFT ENTRY DOOR IN AFT GALLEY INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY ABOVE LEFT ENTRY DOOR IN - [SDR AALA980553](https://openairdocs.org/sdr/AALA980553), Mar 21, 1998: LIGHT. DEFECTIVE. DFW - DURING OVERNIGHT CHECK, AFT EMERGENCY EXIT SIGN HAD TWO BULBS INOPERATIVE. REPLACED AFT EMERGENCY EXIT SIGN LIGHT STRIP ASSEMBLY. SYSTEM GROUND CHECKED NO - [SDR AALA972455](https://openairdocs.org/sdr/AALA972455), Dec 13, 1997: FLOORBEAM. CORRODED. TUL - CHORD ANGLE AT STATION 1177 CORRODED TOP AND BOTTOM RBL 27, SEE E58 0093393. REMOVED AND REPLACED CHORD ANGLE RBL 66 TO LBL 19 PER SRM 51-10-1, SEE E58 00 - [SDR AALA972454](https://openairdocs.org/sdr/AALA972454), Dec 13, 1997: FLOORBEAM. CORRODED. TUL - UNDERSIDE OF FLOORBEAM AT SEAT TRACK JUNCT, HOLES CORRODED, RIGHT OUTBOARD SEAT TRACK. REMOVED CORROSION FROM FLOORBEAM IAW SRM 51-10-6 OUT OF LIMITS. REP - [SDR AALA972453](https://openairdocs.org/sdr/AALA972453), Dec 13, 1997: STRINGER. CORROSION. TUL - SKIN BULGED UNDER STRINGER 28 LEFT STATION 707-710, CORROSION ON STRINGER 28L, STATION 700-720, NO CORROSION ON SKIN. REMOVED DAMAGED SECTION OF STRINGER - [SDR AALA972452](https://openairdocs.org/sdr/AALA972452), Dec 13, 1997: WEB. CORRODED. TUL - LOWER WEB CORRODED INBOARD STRINGER 17R STATION 373-377 AT CREASE ANGLE. REMOVED AND REPLACED WEB IAW SRM 51-10-1. (M) - [SDR AALA972451](https://openairdocs.org/sdr/AALA972451), Dec 13, 1997: FRAME. CORRODED. TUL - FORWARD RIGHT GALLEY DOOR LOWER FRAME CORRODED INBOARD OF STRINGER 17R. CUT OUT CORRODED AREA AND INSTALLED DOUBLER IAW SRM 51-40-3 PAGES 1-5. (M) - [SDR AALA972449](https://openairdocs.org/sdr/AALA972449), Dec 13, 1997: SILL. CORRODED. TUL - BELOW CREASE ANGLE STATION 414R SILL WEB CORRODED, BOTTOM SIDE AROUND DRAIN LINE HOSE, FORWARD GALLEY DOOR CUTOUT. REMOVED AND REPLACED WEB IAW SRM 51-10- - [SDR AALA972448](https://openairdocs.org/sdr/AALA972448), Dec 13, 1997: DOUBLER. CORRODED. TUL - FOUND CORROSION ON SKIN SPLICE DOUBLER ABOVE STRINGER 26R, STATION 1010. INSTALLED DOUBLER SPLICE REPAIR, ESO 11697, DATED 14 NOV. (M) - [SDR AALA972447](https://openairdocs.org/sdr/AALA972447), Dec 13, 1997: SPLICE. CORRODED. TUL - STRINGER 26L, UPPER SIDE CORRODED AT STATION 1008. REMOVED AND REPLACED STRINGER SPLICE PER SRM 53-10-3. (M) - [SDR AALA972446](https://openairdocs.org/sdr/AALA972446), Dec 13, 1997: FRAME. CORRODED. TUL - BOTTOM INBOARD END FRAME 416 CORODED AT STRINGER 17R ABOVE AND BELOW SILL PLATE. BLENDED CORROSION, OUT OF LIMITS PER SRM. INSTALLED DOUBLER IAW SRM 51-40 - [SDR AALA972445](https://openairdocs.org/sdr/AALA972445), Dec 13, 1997: FRAME. DENTED. TUL - FOUND STATION 950B BELL FRAME DENTED STRINGER 26R. REPAIRED STATION 950B BELL FRAME AT STRINGER 26R IAW SRM 51-40-3. (M) - [SDR AALA972444](https://openairdocs.org/sdr/AALA972444), Dec 13, 1997: FRAME. CRACKED. TUL - BELL FRAME CRACKED AT FLOORBOARD SUPPORT STATION 950B RBL 4 INCH. CRACK WAS CUT OUT. REPAIRED BELL FRAME STATION 950B RBL 4 INCH IAW SRM 51-40-3. (M) - [SDR AALA972443](https://openairdocs.org/sdr/AALA972443), Dec 13, 1997: FLOORBEAM. CORRODED. TUL - STATION 380 FLOORBEAM 12 INCHES RBL TO RIGHT FWD SERVICE DOOR FRAME HAS CORROSION. INSTALLED REPAIR PER 53-10-6 ON FLOORBEAM. (M) - [SDR AALA972442](https://openairdocs.org/sdr/AALA972442), Dec 13, 1997: ANGLE. CORRODED. TUL - FOUND CORROSION ON TOP OF HORIZONTAL STAB T/E ALONG LT ELEVATOR HINGE LINE, APPROX 5 INCHES LONG 2 INCHES WIDE. INSTALLED DOUBLER PER ESO 11697. (M) - [SDR 98ZZZX496](https://openairdocs.org/sdr/98ZZZX496), Dec 13, 1997: FRAME. CORRODED. TUL- FOUND CORROSION ON LOWER FRAME STA 370 RIGHT LOWER END AT STR 17R INBOARD. CUT OUT CORRODED AREA. INSTALLED DOUBLER IAW SRM 51-40-3 PAGES 1 THROUGH 5. - [SDR AALA971213](https://openairdocs.org/sdr/AALA971213), Sep 15, 1997: FRAME. CORRODED. TUL - FOUND CORROSION ON LWER FRAME STATION 370 RIGHT LOWER END AT STRINGER 17R INBOARD. CUT OUT CORRODED AREA. INSTALLED DOUBLER IAW SRM 51-40-3 PAGE 1 THROUGH - [SDR AALA970891](https://openairdocs.org/sdr/AALA970891), May 9, 1997: MOTOR. LEAKING. MIA - FLT 919 - AFTER TAKEOFF MIA DURING CLIMB-OUT, SYSTEM 'A' QTY BEGAN TO DECREASE BELOW 2. ACCOMP LOSS OF SYSTEM A ABNORMAL PROCEDURE AND AIRCRAFT RETURNED T - [SDR AALA970482](https://openairdocs.org/sdr/AALA970482), Mar 7, 1997: STRINGER. CORRODED. TUL - FOUND CORROSION ON STRINGER 29 LEFT FROM STATION 950F TO 990. REMOVED CORROSION, PRIMED AND TREATED AREA, INSTALLED REPAIR DOUBLER PER ESO 11697, DATED 2- - [SDR AALA961380](https://openairdocs.org/sdr/AALA961380), Sep 21, 1996: RETRACT MECH. MALFUNCTIONED. MIA - FLT 2157 - AFTER TAKEOFF MIA WHEN LANDING GEAR RETRACTED, NOSE LANDING GEAR DID NOT RETRACT. RECYCLED LANDING GEAR WITH SAME RESULTS. EXTENDED LANDING GEA All 52: https://openairdocs.org/aircraft/N875AA/unmatched-reports.md ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## Related - Other Anduril Industries FALCON aircraft: https://openairdocs.org/model/anduril-industries-falcon/aircraft.md --- 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.