# N715AA: Anduril Industries ROADRUNNER

- Status: Valid registration
- Airframe: [Anduril Industries ROADRUNNER](https://openairdocs.org/model/anduril-industries-roadrunner) (registry code 06102I4)
- Serial number: 3165
- Type: Fixed wing multi engine
- Engine type: Turbo-jet
- Mode S code: A98EA1
- 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=715AA
- Page: https://openairdocs.org/aircraft/N715AA

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 ROADRUNNER)

None in force.

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N715AA.

## FAA accident and incident reports

None matched to N715AA.

## Reports on N715AA not matched to an aircraft (4)

They name N715AA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 20040805025479I](https://openairdocs.org/incident/20040805025479I), Aug 5, 2004: Boeing 727223 (N715AA), Toledo, OH. (-23) Flt 708 started to lose oil pressure in the #1 engine at FL 210. Crew performed inflight engine shutdown and landed returned to Toledo without incident.…
- [Incident 20030429005519I](https://openairdocs.org/incident/20030429005519I), Apr 29, 2003: Boeing 727223 (N715AA), Miami, FL, Minor damage. (-23) N715AA, a B-727-223, blew all four tires on landing at mia, it appears number 3 tire locked up on landing, causing a chain reaction failure of the…
- [Incident 19850614028879I](https://openairdocs.org/incident/19850614028879I), Jun 14, 1985: Boeing 727200 (N715AA), Cleveland, OH. Rapid decompression at FL310. Finally regained pressurization in standby. Auto pressure controller replaced.
- [Incident 19841205074049I](https://openairdocs.org/incident/19841205074049I), Dec 5, 1984: Boeing 727200 (N715AA), Dallas, TX, Minor damage. Applied thrust after power back from gate. Raised catering truck tipped over striking N860. Wind also a factor.

## 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 N715AA not matched to an aircraft (116, newest 50)

They name N715AA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR C8GA20120208003](https://openairdocs.org/sdr/C8GA20120208003), Feb 8, 2012: GYRO. INACCURATE. DURING CRUISE, BOTH CAPTAIN'S AND FIRST OFFICER'S ADI SHOWED A 10 DEGREE LT TURN. AN EMERGENCY WAS DECLARED AND THE ACFT LANDED WITHOUT INCIDENT. POST FLIGHT IN
- [SDR C8GA2011000027](https://openairdocs.org/sdr/C8GA2011000027), Nov 18, 2011: WARNING HORN. FALSE ACTIVATION. DURING TAKEOFF ROLL AT APPROX 60 KNOTS THE TAKEOFF WARNING HORN SOUNDED. THE TAKEOFF WAS ABORTED AND THE ACFT RETURNED TO THE BLOCKS WITHOUT INCIDENT. POST FLIG
- [SDR C8GA2011000020](https://openairdocs.org/sdr/C8GA2011000020), Sep 9, 2011: ACTUATOR. STICKING. AFTER TAKEOFF AND DURING CLIMB, THE NR 8 L/E SLAT IN TRANSIT LIGHT STAYED ON DURING FLAP RETRACTION AND ACFT ROLLED TO THE LT. THE ACFT RETURNED TO DEPARTURE, L
- [SDR C8GA2011000018](https://openairdocs.org/sdr/C8GA2011000018), Aug 19, 2011: RELIEF VALVE. LEAKING. WHILE EN-ROUTE, THE CREW NOTED THAT THE B-SYSTEM HYD QUANTITY WAS DECREASING AND THE LOW LIGHT ILLUMINATED. ACFT DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDE
- [SDR C8GA2011000015](https://openairdocs.org/sdr/C8GA2011000015), Jul 29, 2011: CARRIAGE. BROKEN. DURING CLIMB OPERATION, THE OTBD FLAPS FROZE AT 3 DEGREES ON CLIMBOUT, 9 UNITS OF AILERON TRIM WAS REQUIRED FOR LEVEL FLIGHT. THE ACFT RETURNED TO DEPARTURE WHE
- [SDR C8GA2011000008](https://openairdocs.org/sdr/C8GA2011000008), Jun 24, 2011: FLAP SYSTEM. LACK OF LUBE. DURING DEPARTURE, ON FLAP RETRACTION THE OTBD FLAPS WOULD NOT RETRACT ABOVE 4 DEGREES. ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. POST FLIGHT INSPE
- [SDR C8GA2011000006](https://openairdocs.org/sdr/C8GA2011000006), Jun 17, 2011: POWER SUPPLY. INOPERATIVE. DURING TAKEOFF ROLL OUT, ALL 3 ENGINE FUEL FLOW INDICATIONS FLUXUATED BY + / - 5000 LBS. THE TAKEOFF WAS ABORTED AND THE ACFT RETURNED TO BLOCKS WITHOUT INCIDEN
- [SDR C8GA2011000004](https://openairdocs.org/sdr/C8GA2011000004), Jun 10, 2011: ENGINE. DAMAGED. ON TAKEOFF DEPARTING, WHILE CLIMBING THROUGH 1000' A LOUD BANG EMERGED FROM THE NR1 ENGINE. AN EMERGENCY WAS DECLARED AND THE ACFT RETURNED TO DEPARTURE WHERE I
- [SDR C8GA2010000072](https://openairdocs.org/sdr/C8GA2010000072), Nov 6, 2010: FLOORBEAM. CORRODED. DURING HEAVY MX INSP, IT WAS NOTED THAT THE FLOORBEAM FLANGE AT STA 1110 LBL 64. REMOVED CORROSION AND FABRICATED REPAIR ANGLES FROM 7075 T6, .090" DIM 13.5" X 
- [SDR C8GA2010000071](https://openairdocs.org/sdr/C8GA2010000071), Nov 6, 2010: FITTING. CORRODED. DURING HEAVY MX INSP, IT WAS NOTED THAT THE NLG RT TRUNNION FITTING HAVE CORROSION. REMOVED CORROSION AND REWORKED AREA. NO OTHER DEFECTS NOTED. ACFT WAS RETURN
- [SDR C8GA2010000070](https://openairdocs.org/sdr/C8GA2010000070), Nov 6, 2010: FITTING. CORRODED. DURING HEAVY MX INSP IT WAS NOTED THAT THE NOSE LANDING GEAR LT TRUNNION FITTINGS HAVE CORROSION. REMOVED CORROSION AND REWORKED AREA. NO OTHER DEFECTS NOTED. A
- [SDR C8GA2010000069](https://openairdocs.org/sdr/C8GA2010000069), Nov 6, 2010: FITTING. CORRODED. DURING HEAVY MX INSP IT WAS NOTED THAT THE LT MLG FWD TRUNNION FITTING HAS CORROSION. REMOVED CORROSION AND REWORKED AREA AND INSTALLED 2EA LOWER BUSHINGS AND 2
- [SDR C8GA2010000068](https://openairdocs.org/sdr/C8GA2010000068), Nov 6, 2010: FITTING. CORRODED. DURING HEAVY MX INSP IT WAS NOTED THAT THE RT MLG FWD TRUNION FITTING HAS CORROSION. REMOVED CORROSION AND REWORKED AREA AND INSTALLED 2 EA LOWER BUSHINGS. NO O
- [SDR C8GA2010000067](https://openairdocs.org/sdr/C8GA2010000067), Nov 6, 2010: SHEAR TIE. CORRODED. DURING HEAVY MX INSP IT WAS NOTED THAT THE AFT CARGO STA 1148, BL 0 SHEAR-TIE IS CORRODED. REMOVED SHEAR-TIE AND FABRICATED NEW FROM 2024 T3 .050". INSTALLED RE
- [SDR C8GA2010000066](https://openairdocs.org/sdr/C8GA2010000066), Nov 6, 2010: FLOORBEAM. CORRODED. DURING HEAVY MX IT WAS NOTED THAT THE MAIN CARGO FLOORBEAM IS CORRODED AT STA 1110 LBL 35. CORROSION WAS REMOVED, FABRICATED DOUBLER FROM 7075 T6 .090", FILLER 
- [SDR C8GA2010000065](https://openairdocs.org/sdr/C8GA2010000065), Nov 6, 2010: FLOORBEAM. CORRODED. DURING HEAVY MX INSP IT WAS NOTED THAT THE AFT CARGO FLOORBEAM STAT 1010, LBL 10 IS CORRODED. CUT OUT DAMAGE, FABRICATED REPAIR PARTS FROM 7075 T6 .063" DIM 18"
- [SDR C8GA2010000064](https://openairdocs.org/sdr/C8GA2010000064), Nov 6, 2010: FLOORBEAM. CORRODED. DURING HEAVY MX INSP IT WAS NOTED THAT THE AFT CARGO FLOORBEAM STA 1030, RBL 20 IS CORRODED. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR. NO OTHER DEFECTS W
- [SDR C8GA2010000063](https://openairdocs.org/sdr/C8GA2010000063), Nov 6, 2010: BULKHEAD. CRACKED. DURING HEAVY MX, WHILE PERFORMING INSPECTIONS, IT WAS NOTED THAT THE RT INBD WHEEL WELL FWD BULKHEAD SKIN IS CRACKED AT APU OUTLET DUCT CUT-OUT LOWER. FABRICATE
- [SDR C8GA2010000062](https://openairdocs.org/sdr/C8GA2010000062), Nov 6, 2010: DUCT. CORRODED. DURING HEAVY MX, WHILE PERFORMING INSP, IT WAS NOTED THAT THE NR2 ENGINE "S" DUCT AT STATION 1203 6 O'CLOCK POSITION HAS CORROSION. REMOVED CORROSION AND FABRIC
- [SDR C8GA2010000061](https://openairdocs.org/sdr/C8GA2010000061), Nov 6, 2010: SKIN. CORRODED. DURING HEAVY MX, WHILE PERFORMING INSPECTIONS, IT WAS NOTED THAT THE LT MLG WW INBD CTR CEILING AREA BL 0, STA 930 ABOVE APU SCREEN HAS CORROSION. REMOVED CORRO
- [SDR C8GA2010000060](https://openairdocs.org/sdr/C8GA2010000060), Nov 6, 2010: WEB. DENTED. DURING HEAVY MX WHILE PERFORMING INSPECTIONS IT WAS NOTED THAT THE FWD CARGO DOOR FRAME AFT SIDE OF CUT-OUT AT BS 620 BETWEEN RBL 25-30 STRINGER 25R. REMOVED DA
- [SDR C8GA2010000059](https://openairdocs.org/sdr/C8GA2010000059), Nov 6, 2010: WEB. DENTED. DURING HEAVY MX PERFORMING INSPECTIONS IT WAS NOTED THAT THE FWD CARGO COMPARTMENT RT SIDE OF CARGO DOOR FRAME CUT-OUT AT BS 560 BETWEEN STR 23R & 25R. REMOVED 
- [SDR ABXR201005260002](https://openairdocs.org/sdr/ABXR201005260002), May 26, 2010: STRAP. CRACKED. DURING A HEAVY MX EVENT THE LT WHEEL WELL STA 930 DECK STRAP WAS DISCOVERED CRACKED AND CORRODED JUST ABOVE THE HYD LINK CLUSTER. FABRICATED PRESSURE DECK STRAP
- [SDR C8GA20090298](https://openairdocs.org/sdr/C8GA20090298), Dec 30, 2009: ACTUATOR. MALFUNCTIONED. DURING CLIMB OPERATION THE NR 7 L/E SLAT FAILED TO RETRACT. CREW PERFORMED REQUIRED CHECKLISTS AND RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. POST 
- [SDR C8GA20090297](https://openairdocs.org/sdr/C8GA20090297), Nov 23, 2009: BEAM. CORRODED. WHILE PERFORMING AN "A" MX CHECK, CORROSION WAS NOTED ON THE RT HORIZ STAB T/E UPPER BEAM APPROX 24" FROM HORIZ TIP. CORROSION WAS EVALUATED AND REMOVED, INSTAL
- [SDR C8GA20090067](https://openairdocs.org/sdr/C8GA20090067), May 7, 2009: WIRE. BROKEN. FLT 1740 FROM BNA TO CLT, DURING APPROACH THE NOSE LANDING GEAR FAILED TO INDICATE DOWN AND LOCKED. THE RED LIGHT WAS ILLUMINATED AND THE GREEN LIGHT WAS OUT. T
- [SDR C8GA20090066](https://openairdocs.org/sdr/C8GA20090066), May 7, 2009: WIRE. CHAFED. FLT 715 FROM MEM TO BNA, DURING SHORT APPROACH THE NOSE LANDING GEAR DID NOT INDICATE DOWN AND LOCKED. THE RED LIGHT WAS ILLUMINATED AND THE GREEN LIGHT WAS OUT
- [SDR C8GA20090065](https://openairdocs.org/sdr/C8GA20090065), May 6, 2009: ACCESSORY UNIT. DEFECTIVE. FLT 716 FROM BNA TO MEM, WHILE ON APPROACH INTO MEM THE NOSE GEAR FAILED TO INDICATE DOWN AND LOCKED. THE GREEN NOSE GEAR LIGHT WAS OUT, AND THE RED LIGHT WAS I
- [SDR C8GA20080103](https://openairdocs.org/sdr/C8GA20080103), Nov 17, 2008: STIFFENER. CORRODED. WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE WING CENTER SECTION LOWER FORWARD STIFFENER ON FORWARD CHORD AT BS 740 LBL-45 CORRODED. C
- [SDR C8GA20080102](https://openairdocs.org/sdr/C8GA20080102), Nov 17, 2008: STRUCTURE. CRACKED. WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE NR 3 SLAT OTBD STOP CUTOUT CORNER CRACKED. STOP DRILLED CRACK, PERFORMED HFEC WITH NO DEF
- [SDR C8GA20080101](https://openairdocs.org/sdr/C8GA20080101), Nov 17, 2008: VENT LINE. CHAFED. WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE LT WING TANK VENT LINE IS CHAFED AT CLAMP WBL 686.50. REPAIRED LT WING TANK FUEL VENT LIN
- [SDR C8GA20080099](https://openairdocs.org/sdr/C8GA20080099), Nov 17, 2008: VENT LINE. CHAFED. WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE LT WING TANK VENT LINE IS CHAFED AT CLAMP WBL 601.50. REPAIRED LT WING TANK FUEL VENT LIN
- [SDR C8GA20080100](https://openairdocs.org/sdr/C8GA20080100), Nov 17, 2008: VENT LINE. CHAFED. WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE LT WING TANK VENT LINE IS CHAFED AT CLAMP WBL 656.50. REPAIRED L/WING TANK FUEL VENT LINE
- [SDR C8GA20080098](https://openairdocs.org/sdr/C8GA20080098), Nov 17, 2008: VENT LINE. CHAFED. WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE LT WING TANK VENT LINE IS CHAFED AT CLAMP WBL 601.50. REPAIRED LT WING TANK FUEL VENT LIN
- [SDR C8GA20080097](https://openairdocs.org/sdr/C8GA20080097), Nov 17, 2008: VENT LINE. CHAFED. WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE LT WING TANK VENT LINE IS CHAFED AT CLAMP WBL 519. REPAIRED LT WING TANK FUEL VENT LINE A
- [SDR C8GA20080096](https://openairdocs.org/sdr/C8GA20080096), Nov 17, 2008: VENT LINE. CHAFED. WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE LT WING TANK VENT LINE IS CHAFED AT TOP CLAMP WBL 442. REPAIRED LT WING TANK FUEL VENT LI
- [SDR C8GA20080095](https://openairdocs.org/sdr/C8GA20080095), Nov 17, 2008: VENT LINE. CHAFED. WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE LT WING TANK VENT LINE IS CHAFED AT CLAMP WBL 383.50. REPAIRED LT TANK FUEL VENT LINE AT 
- [SDR C8GA20080094](https://openairdocs.org/sdr/C8GA20080094), Nov 17, 2008: VENT LINE. CHAFED. WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE LT WING TANK VENT LINE IS CHAFED AT TOP OF CLAMP WBL 348.00. REPAIRED LT WING TANK FUEL V
- [SDR C8GA20080093](https://openairdocs.org/sdr/C8GA20080093), Nov 17, 2008: FITTING. CORRODED. WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE AFT I BEAM SUPPORT SHACKLE FITTING HAS EXFOLIATING CORROSION AT BS 307-0. REMOVED FITTING
- [SDR C8GA20080092](https://openairdocs.org/sdr/C8GA20080092), Nov 17, 2008: SKIN. CRACKED. WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE LT WING L/E WS 530 AT HOOK CUTOUT AFT REPAIR HAS CRACK. REMOVED PREVIOUS REPAIR, FABRICAT
- [SDR C8GA20080091](https://openairdocs.org/sdr/C8GA20080091), Nov 17, 2008: INTERCOSTAL. CORRODED. WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE INTERCOSTAL WEB AT BS 490-510 STR 28R HAS CORROSION. REMOVED INTERCOSTAL AND FABRICATED A
- [SDR C8GA20080087](https://openairdocs.org/sdr/C8GA20080087), Nov 17, 2008: SKIN. DENTED. WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS 2 EA DENTS WERE NOTED AT BS 575-583 BETWEEN STR. 26R-27R. CUT OUT 2 EA DAMAGED AREAS, FABRICATED DOUBLER, AND 
- [SDR C8GA20080085](https://openairdocs.org/sdr/C8GA20080085), Nov 17, 2008: INTERCOSTAL. BROKEN. WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE INTERCOSTAL SKIN ATTACH FLANGE WAS BROKEN AT BS 950A - 950B STR 28L. REMOVED BROKEN INTE
- [SDR C8GA20080086](https://openairdocs.org/sdr/C8GA20080086), Nov 17, 2008: SKIN. CORRODED. WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT FUSELAGE SKIN IS CORRODED BELOW STR 28R AT BS 490-510.CORROSION OUT OF LIMITS. CUT OUT DAMAG
- [SDR C8GA20080070](https://openairdocs.org/sdr/C8GA20080070), Nov 5, 2008: STRINGER. CORRODED. WHILE IN HEAVY MX PERFORMING INSP, IT WAS NOTED THAT STRINGER 29L STA 950C - 1000 IS CORRODED. REMOVED AND REPLACED STRINGER 29L P/N 65-56441-7. INSTALLED STRIN
- [SDR C8GA20080067](https://openairdocs.org/sdr/C8GA20080067), Nov 5, 2008: STRINGER. CORRODED. WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT STRINGER 29R WAS CORRODED UNDER BS 950E FRAME EXTENDING TO BS 1000. CORROSION AT STR. 29R WAS OUT OF LIMITS.
- [SDR C8GA20080064](https://openairdocs.org/sdr/C8GA20080064), Nov 5, 2008: STRINGER. CORRODED. WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT STR. 27R LOCATED AT BS. 1010-1030 HAD EXFOLIATED CORROSION. REMOVED CORROSION, CORROSION AFTE
- [SDR C8GA20080084](https://openairdocs.org/sdr/C8GA20080084), Nov 1, 2008: STRUCTURE. CRACKED. WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE LOWER CHORD RUNNING ALONG STR 27R BY THE C2 DOOR IS CORRODED AND CRACKED AT BOTH ENDS, S
- [SDR C8GA20080083A](https://openairdocs.org/sdr/C8GA20080083A), Oct 29, 2008: INTERCOSTAL. CORRODED. WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS SURFACE CORROSION WAS NOTED ON INTERCOSTAL BS 695 STR 27R. DAMAGED INTERCOSTAL WAS REMOVED, A NEW INTERCOSTAL 
- [SDR C8GA20080083](https://openairdocs.org/sdr/C8GA20080083), Oct 29, 2008: FRAME. CORRODED. WHILE IN HEAVY PERFORMING INSPECTIONS IT WAS NOTED THAT THE FRAME WAS DENTED AT BS 1110 JUST ABOVE STR 26R CUT OUT DAMAGED FRAME AND FABRICATED NEW FRAME FROM 7

All 116: https://openairdocs.org/aircraft/N715AA/unmatched-reports.md

## STCs that may be installed (OpenAirDocs)

None matched to this aircraft's models.

## Earlier aircraft with N715AA

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N715AA before.

- [Cancelled 2022-01-21](https://openairdocs.org/deregistered/N715AA-2022-01-21): Gulfstream Aerospace GV-SP (G550), S/N 5364. Exported to Greece. Owner: [Tvpx Aircraft Solutions Inc Trustee](https://openairdocs.org/faa-owner/TVPX%20AIRCRAFT%20SOLUTIONS%20INC%20TRUSTEE), [North Salt Lake, UT](https://openairdocs.org/faa-place/UT/North%20Salt%20Lake)

## Related

- Other Anduril Industries ROADRUNNER aircraft: https://openairdocs.org/model/anduril-industries-roadrunner/aircraft.md

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