# N890AA: Anduril Industries FALCON - Status: Valid registration - Airframe: [Anduril Industries FALCON](https://openairdocs.org/model/anduril-industries-falcon) (registry code 06102I8) - Serial number: 649 - Type: Fixed wing single engine - Engine type: 2 cycle - Mode S code: AC4555 - 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=890AA - Page: https://openairdocs.org/aircraft/N890AA 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 N890AA. ## FAA accident and incident reports None matched to N890AA. ## Reports on N890AA not matched to an aircraft (2) They name N890AA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [Incident 19940116003409I](https://openairdocs.org/incident/19940116003409I), Jan 16, 1994: Boeing 727223 (N890AA), Raleigh-Durham, NC. Narrative: at approximately 1015 on 1/17/94, aircraft departed rdu enroute to gcm. During climb crew observed a decrease in oil pressure indication along with… - [Incident 19920628029999I](https://openairdocs.org/incident/19920628029999I), Jun 28, 1992: Boeing 727223 (N890AA), Atlantic Ocean, NJ. Physical fight occurred between two female passengers. Both passengers and two flight attendants were slightly hurt ## 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 N890AA not matched to an aircraft (69, newest 50) They name N890AA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR AALA20011677](https://openairdocs.org/sdr/AALA20011677), Aug 21, 2001: LIGHT. INOPERATIVE. DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING IN AFT STAIRWELL INOPERATIVE. REPLACED AFT STAIRWELL LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORM - [SDR AALA20011593](https://openairdocs.org/sdr/AALA20011593), Aug 5, 2001: LIGHT. INOPERATIVE. DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING IN AFT STAIRWELL INOPERATIVE. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20011007](https://openairdocs.org/sdr/AALA20011007), May 14, 2001: VALVE. FAILED. BNA - FLT 1216 - EN ROUTE DFW-PHL, AIR INTERRUPTED BNA, AFTER NR 3 ENGINE FLAME OUT AND NO FUEL TRANSFER FROM NR 2 TANK. REPLACED NR 2 CROSSOVER FEED VALVE. SYS - [SDR AALA20010988](https://openairdocs.org/sdr/AALA20010988), May 13, 2001: RIB. CRACKED. TUL - FOUND DURING SCHEDULED C-CHECK INSPECTION, A CRACK WAS FOUND IN THE LBL 70.5 UPPER RIB CHORD AT BS 760. INSTALLED THE PREVENTATIVE MODIFICATION 65C33202-9 - [SDR AALA20010847](https://openairdocs.org/sdr/AALA20010847), Apr 19, 2001: SKIN. CRACKED. TUL - FOUND FORWARD ENTRY DOOR LOWER HINGE CUTOUT SKIN CRACKED, FS 303. TRIMMED OUT CRACK, INSTALLED DOUBLER IAW SB 727-53-0198 FIG 4. (M) - [SDR AALA20010846](https://openairdocs.org/sdr/AALA20010846), Apr 18, 2001: SKIN. CRACKED. TUL - FOUND FORWARD ENTRY DOOR UPPER HINGE CUTOUT CRACKED. INSTALLED DOUBLER IAW SB 727-53-0198 FIG 4, TRIMMED OUT CRACK. (M) - [SDR AALA20010845](https://openairdocs.org/sdr/AALA20010845), Apr 18, 2001: BEAM. CORRODED. TUL - FOUND LEFT HORIZONTAL T/E BEAM CORRODED AT OUTBOARD END. REMOVED CORROSION AND INSTALLED DOUBLER PER ESO 11697 DATED 4/17/01. (M) - [SDR AALA20010844](https://openairdocs.org/sdr/AALA20010844), Apr 18, 2001: STIFFENER. CRACKED. TUL - FOUND AFT BULKHEAD 1183 RIGHT BL 9 VERTICAL STIFFENER HAS CRACK UNDER OUTBOARD TOWER RADIUS BLOCK. STOP DRILLED CRACK AND INSTALLED REPAIR AS PER SB 727-5 - [SDR AALA20010848](https://openairdocs.org/sdr/AALA20010848), Apr 17, 2001: SKIN. GOUGED. TUL - FOUND 1.5 INCH BY .125 INCH GOUGE LOCATION NEAR RIGHT NLG DOOR. DAMAGE IS APPROX 12 INCHES AFT AND 18 INCHES ABOVE AFT AND OF RIGHT NLG DOOR. REMOVED AREA - [SDR AALA2000562](https://openairdocs.org/sdr/AALA2000562), Mar 28, 2000: CHANNEL. DAMAGED. TUL - FOUND ELONGATED HOLE IN VERTICAL CHANNEL AT OUTBOARD HINGE OF NR 2 SPOILER. REMOVED VERTICAL CHANNEL AND INSTALLED NEW PART USING FIRST OVERSIZE HI-LOCKS - [SDR AALA20000227](https://openairdocs.org/sdr/AALA20000227), Feb 6, 2000: LIGHT. INOPERATIVE. DFW - FOUND DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT FORWARD CENTER CEILING INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT FORWARD CENTER C - [SDR AALA20000224](https://openairdocs.org/sdr/AALA20000224), Feb 3, 2000: LIGHT. INOPERATIVE. DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT IN AFT AIRSTAIR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY IN AFT AIRSTAIR. SYSTEM GROUND CHEC - [SDR AALA991290](https://openairdocs.org/sdr/AALA991290), Aug 27, 1999: CONNECTOR. DEFECTIVE. DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT SEATS 17D, 20D, AND 24D INOPERATIVE. REPLACED CONNECTORS TO EMERGENCY EXIT FLOOR PATH LI - [SDR AALA990590](https://openairdocs.org/sdr/AALA990590), Apr 20, 1999: BEAM. CORRODED. TUL - FOUND CORROSION ON LIGHTENING HOLE ON BOTTOM OF DELTA BEAM AT STATION 786 TO 790. REPAIRED WITH DOUBLER IAW SRM 51-40-2 AND 51-20-0. (M) - [SDR AALA990584](https://openairdocs.org/sdr/AALA990584), Apr 20, 1999: FRAME. CORRODED. TUL - FOUND OUTBOARD SIDE STRINGER 26R AFT SIDE 620 FRAME LOWER CHORD ANGLE CORRODED. REPAIRED CHORD ANGLE PER SRM 51-40-3. (M) - [SDR AALA990565](https://openairdocs.org/sdr/AALA990565), Apr 20, 1999: SKIN. CORRODED. TUL - FOUND CORROSION AROUND INNER SKIN AROUND ICE LIGHT HOUSING LANDING AT BS 720B-720C AND STRINGER 14L-16L. REPAIRED PER SRM 53-30-3 AREA AROUND ICE LIGHT HO - [SDR AALA990606](https://openairdocs.org/sdr/AALA990606), Apr 19, 1999: STRINGER. CRACKED. TUL - REF E58 NR 3150893, STRINGER 15L CRACKED AT BS 720B PLUS 15 INCHES AT AFT EDGE OF ICE LIGHT HOUSING. REPAIR STRINGER 15L BS 720B PLUS 15 INCHES AT AFT EDG - [SDR AALA990566](https://openairdocs.org/sdr/AALA990566), Apr 19, 1999: SPAR. CORRODED. TUL - FOUND LEFT HORIZ STAB REAR SPAR CHORD UPPER END HAS 1 INCH AREA OF CORROSION BETWEEN NR 6 AND NR 7 ELEV HINGE BEARING. REPAIRED AREA OF CORROSION REMOVAL - [SDR AALA990594](https://openairdocs.org/sdr/AALA990594), Apr 16, 1999: FRAME. DENTED. TUL - FOUND BELL FRAME FLANGE DENTED STATION 1110, STRINGER 27 AND 25R. INSTALLED DOUBLER PER SRM 51-40-3. (M) - [SDR AALA990596](https://openairdocs.org/sdr/AALA990596), Apr 15, 1999: ANGLE. CORRODED. TUL - FOUND OUTBOARD SIDE STRINGER 26R AFT SIDE 620 FRAME LOWER CHORD ANGLE CORRODED. REPAIRED CHORD ANGLE PER SRM 51-40-3 DOUBLER 17-7 MATERIAL .063 THICK 2.5 - [SDR AALA990574](https://openairdocs.org/sdr/AALA990574), Apr 14, 1999: STRAP. CORRODED. TUL - FOUD STRINGER 614-619 ABOVE STRINGER 26R UPPER CHORD ANGLE LOWER TAPERED STRAP DOUBLER CORRODED AROUND 3 NUT PLATES. REMOVED AND REPLACED TAPERED STRAP. ( - [SDR AALA990593](https://openairdocs.org/sdr/AALA990593), Apr 13, 1999: FRAME. BENT. TUL - FOUND STATION 1030 BELL FRAME BENT (FLANGE/WEB) STRINGER 26-25 LEFT. REMOVED DAMGED SECTIONS, 1 INCH BY 2.8125 INCH BY 1 INCH BY 1.3125 INCH FROM BELL FRA - [SDR AALA990573](https://openairdocs.org/sdr/AALA990573), Apr 12, 1999: FLOORBEAM. CORRODED. TUL - FOUND CORROSION AT FASTENER HOLES FOR CEILIG PANEL ATTACHMENT. REMOVED CORROSION AND REPAIRED PER ESO 11697 DATED 4-9-99 USING 7075T6 .080 1 INCY BY 16.5 - [SDR AALA990599](https://openairdocs.org/sdr/AALA990599), Apr 9, 1999: SPAR. CORRODED. TUL - RIGHT WING FSS 213-216 LOWER CHORD ANGEL LOWER LEFT HAS EXFOLIATING CORROSION, UPPER SURFACE AROUND AND UNDER STRUT ROD MOUNT BRACKET. REMOVED AND BLENDED - [SDR AALA990611](https://openairdocs.org/sdr/AALA990611), Apr 8, 1999: FRAME. BENT. FOUND BELL FRAME BENT IN WEB STATION 1130, STRINGER 26R TO STRINGER 25R. CUT OUT DAMGED AREA AND INSTALLED DOUBLER REPAIR PER 51-40-5 (AARD 53-10-07-3). (M) - [SDR AALA990592](https://openairdocs.org/sdr/AALA990592), Apr 8, 1999: FRAME. BENT. TUL - FOUND BELL FRAME BENT FLANGE AND WEB STATION 1030 STRINGER 26R TO STRINGER 25R. CUT OUT DAMAGED AREA AND INSTALLED DOUBLERS PER SRM 51-40-3. (M) - [SDR AALA990591](https://openairdocs.org/sdr/AALA990591), Apr 7, 1999: SPLICE. CRACKED. TUL - FOUND BELL FRAME (SPLICE) STRAP CRACKED STATION 1030 BETWEEN STRINGER 24L AND 25L. REPLACED (SPLICE) STRAP PER 51-10-1. (M) - [SDR AALA990572](https://openairdocs.org/sdr/AALA990572), Apr 7, 1999: SHEAR TIE. CORRODED. TUL - FOUND CORROSION ON SHEAR TIE AFT OF FS 1130 AT STRINGER 29 LEFT. REMOVED CORRODED SHEAR TIE AND INSTALLED NEW SHEAR TIE USING ORIGINAL FASTENER LOCATIONS. - [SDR AALA990571](https://openairdocs.org/sdr/AALA990571), Apr 7, 1999: SHEAR TIE. CORRODED. TUL - FOUND CORROSION ON SHEAR TIE AFT SIDE FS 1130, STRINGER 28 LEFT OUTBOARD. REMOVED CORRODED SHEAR TIE AND INSTALLED NEW SHEAR TIE USING ORIG FASTENER LOCAT - [SDR AALA990570](https://openairdocs.org/sdr/AALA990570), Apr 7, 1999: SHEAR TIE. CORRODED. TUL - FOUND CORROSION ON SHEAR TIE FS 1130 AT STRINGER 30. REMOVED CORRODED SHEAR TIE AND INSTALLED NEW SHEAR TIE USING ORIGINAL FASTENER LOCATIONS. FASTENERS T - [SDR AALA990598](https://openairdocs.org/sdr/AALA990598), Apr 6, 1999: FRAME. CORRODED. TUL - FOUND STATION 1070 BELLFRAME FLANGE AND WEB STRINGER 26 AND 25 LEFT. INSTALLED DOUBLER PER SRM 51-40-3. (M) - [SDR AALA990597](https://openairdocs.org/sdr/AALA990597), Apr 6, 1999: FRAME. BENT. TUL - FOUND STATION 1050 BELLFRAME FLANGE 8 WEB BENT STATION 1050, STRINGER 26 AND 25 LEFT. REPAIRED BELLFRAME PER SRM 51-40-3. (M) - [SDR AALA990605](https://openairdocs.org/sdr/AALA990605), Apr 4, 1999: STRINGER. CRACKED. TUL - CUT OUT CRACK AND REPAIRED STRINGER 15R FORWARD SIDE OF WING SCANNING LIGHT. MATERIAL PER SRM 53-10-3 FIG 5. FASTENERS SIX .1875 HI-LOCKS THROUGH SKIN AND - [SDR AALA990604](https://openairdocs.org/sdr/AALA990604), Apr 4, 1999: STRINGER. DAMAGED. TUL - CUT OUT DAMAGE AT FS 720A PLUS 10 INCHES SPLICED IN NEW STRINGER. MATERIAL PER SRM 53-10-3 FIG 5. FASTENERS THROUGH SKIN FOUR .1875 HI-LOCKS PER SIDE OF S - [SDR AALA990595](https://openairdocs.org/sdr/AALA990595), Apr 4, 1999: FRAME. BENT. TUL - FOUND BELL FRAME FLANGE/WEB BENT. INSTALLED DOUBLER PER SRM 51-40-3. (M) - [SDR AALA990576](https://openairdocs.org/sdr/AALA990576), Apr 3, 1999: STRINGER. CORRODED. TUL - FOUND STRINGER 30 CORRODED AT STATION 1177. INSTALLED NEW SECTION OF STRINGER STATION 1156-1183 WITH NEW SPLICE BETWEEN STATION 1148 AND 1166 PER SRM 51-1 - [SDR AALA990577](https://openairdocs.org/sdr/AALA990577), Apr 1, 1999: STRINGER. CORRODED. TUL - FOUND STRINGER 29L CORRODED AROUND FASTENER, OUTBOARD LEG AFT OF STATION 950B TO 950B PLUS 1 INCH. REPAIRED PER ESO 11697 DATED 4-1-99 USING GENERAL GUIDE - [SDR AALA990567](https://openairdocs.org/sdr/AALA990567), Apr 1, 1999: FRAME. DAMAGED. TUL - REMOVED DAMAGE BY CUTTING OUT. INSTALLED DOBULER AND FILLER SRM 51-40-3 DOUBLER MATERIAL 7075-T6 .063 INCH THICK FILLER .050 INCH 7075-T6 FASTENERS (10 EA - [SDR AALA990580](https://openairdocs.org/sdr/AALA990580), Mar 31, 1999: FRAME. DENTED. TUL - FOUND STATION 560 BELLFRAME DENTED IN BETWEEN STRINGERS 24L AND 25L. CUT OUT DAMAGE 1 INCH BY 1.25 INCH AND INSTALLED DOUBLER PER SRM 51-40-3 PAGE 1-5. MA - [SDR AALA990568](https://openairdocs.org/sdr/AALA990568), Mar 31, 1999: SILL. CORRODED. TUL - FOUND STATION 970 STRINGER 27 RIGHT DOOR CUT OUT CORRODED CHORD ANGLE, SILL PLATE LOWER. BLENDED CORROSION, HFEC FASTENER HOLES. LIGHTLY SPOTFACED FASTENE - [SDR AALA990609](https://openairdocs.org/sdr/AALA990609), Mar 30, 1999: FRAME. BENT. TUL - BELT FRAME, BENT FLANGE AND WEB STATION 950F BETWEEN 26L AND 25L. INSTALLED DOUBLER ON BELT FRAME AT STATION 950F BETWEEN STRINGER 25L AND 26L IAW AARD 53 - [SDR AALA990588](https://openairdocs.org/sdr/AALA990588), Mar 30, 1999: FRAME. BENT. TUL - FOUND STATION 1070 BETWEEN STRINGER 26R-25R, BELLFRAME BENT IN WEB. REMOVED 3.5 INCH BY 1.25 INCH DAMAGED AREA. INSTALLED .071 T6 DOUBLER PER SRM 51-40-3. - [SDR AALA990569](https://openairdocs.org/sdr/AALA990569), Mar 30, 1999: FRAME. DAMAGED. TUL - STATION 950A STIRNGER 19R, BELT FRAME HAS DEEP WEAR FROM CEILING PANEL, DAMAGE ON FREE FLANGE. INSTALLED DOUBLER PER 51-40-3. NO CUT OUT REQUIRED. DOUBLER - [SDR AALA990602](https://openairdocs.org/sdr/AALA990602), Mar 29, 1999: FLOORBEAM. CORRODED. TUL - FOUND TOP OF FLOORBEAM AT BS 380 IS CORRODED FROM RBL 48 TO 64 RBL. FLOORBEAM REPAIR COMPLETE AFT FLANGE OF UPPER CHORD STATION 380 RBL 48 TO 65 AS PER AA - [SDR AALA990589](https://openairdocs.org/sdr/AALA990589), Mar 29, 1999: ANGLE. CRACKED. TUL - FOUND ANGLE ON FRAME CRACKED AT FASTENER HOLE AT ATTACH POINT TO STRINGER 14R. REMOVED CRACKED PART AND INSTALLED NEW PART WITH HI-LOCKS. (M) - [SDR AALA990586](https://openairdocs.org/sdr/AALA990586), Mar 29, 1999: FRAME. DENTED. TUL - FOUND STATION 990 BELL FRAME FLANGE AND WEB BENT LEFT STRINGER 25-27. CUT OUT 6.75 INCH BY 1.25 INCH DAMAGED AREAS. INSTALLED .071 T-6 DOUBLER PER SRM 51- - [SDR AALA990581](https://openairdocs.org/sdr/AALA990581), Mar 29, 1999: FRAME. DENTED. TUL - FOUND STATION 580 BELLFRAME DENTED FROM STRINGER 24L TO 22L. REMOVED AND CUTOUT 3 DAMAGED AREAS (SIZES NOTED ABOVE). INSTALLED .063 DOUBLER, 7075-T6, 20 I - [SDR AALA990578](https://openairdocs.org/sdr/AALA990578), Mar 29, 1999: FRAME. BENT. TUL - FOUND STATION 680 BELLFRAME BENT BETWEEN STRINGER 24L AND 23L. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 51-40-3. (M) - [SDR AALA990564](https://openairdocs.org/sdr/AALA990564), Mar 29, 1999: SKIN. CORRODED. TUL - HEAVY CORROSION ON OUTER SKIN OF NR 2 FUEL CELL AT STATION 847, LBL 28, WING CENTER SECTION. REMOVED 4 FASTENERS, BLENDED CORROSION. REMOVED .051 THICKNES - [SDR AALA990583](https://openairdocs.org/sdr/AALA990583), Mar 26, 1999: FRAME. DENTED. TUL - FOUND FRAME 660 DENTED FROM STATION 24L TO 23L. REMOVED TWO DAMAGED AREAS, .75 INCH BY 6.5 INCH, .75 INCH BY .75 INCH. INSTALLED DOUBLER (7075 T-6, .063) All 69: https://openairdocs.org/aircraft/N890AA/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.