N293AA

ANDURIL INDUSTRIES INC ROADRUNNER · Fixed-wing multi-engine · 2 engines · 0 seats · Valid Registration

Registered owner: ANDURIL INDUSTRIES INC, CA (owner ≠ operator)

Operators of this aircraft

Who operated this tail, and how firmly we know it.

No operator established for this aircraft.

Accident & incident history

No NTSB accidents or incidents on file for this aircraft.

Maintenance disclosures

Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.

37 reports on file, 1997-11-15 – 2010-11-22.

SMOKE/FUMES/ODORS/SPARKS · 2010-11-22 Matched by certificate designator
ATA 2150

Part: SHUTOFF VALVE — INOPERATIVE (AC PACK) · airframe 74,118 hrs · 39,605 cycles

MSP - CREW REPORTED A BURNING PLASTIC SMELL IN CABIN DURING CLIMBOUT. AFTER REACHING CRUISE SMELL DISSIPATED THEN ON DESCENT THE ODOR RETURNED. EMERGENCY DECLARED LANDED MSP WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT PACK PRESSURE REGULATING SHUT-OFF VALVE AND ACCOMPLISHED PACK BURN. SYSTEM GROUND CHECK NORMAL OPERATION.

Source: SDR AALA20101122TUL12
OTHER · 2010-10-25 Matched by certificate designator
ATA 5330

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,940 hrs · 39,500 cycles

SKIN CRACKED AT TOP FASTENER IN THE SHEAR TIE JUST OUTBOARD OF VERTICAL STAB RIGHT SKATE ANGLE STATION 1437. INSTALLED EXTERNAL DOUBLER AT STATION 1437 PER EA MD80-53-013708.

Source: SDR AALA20101025TUL05
OTHER · 2010-10-24 Matched by certificate designator
ATA 5313

Part: LONGERON — CRACKED (FUSELAGE) · airframe 73,940 hrs · 39,500 cycles

LONGERON 2 RIGHT HAS CRACK AT STATION 1418. NEW SPLICE LONGERON REPAIR INSTALLED PER AARD 53-30-00-2.

Source: SDR AALA20101024TUL01
OTHER · 2010-10-22 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,940 hrs · 39,500 cycles

STATION 1497 CANT FRAME CRACKED BELOW RIGHT LOUVER BOX. REPAIRED CANT FRAME 1497 PER EA MD80-53-011694.

Source: SDR AALA20101022TUL01
OTHER · 2010-10-22 Matched by certificate designator
ATA 5312

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 73,940 hrs · 39,500 cycles

STATION 37 BULKHEAD HAS CRACK AT LOWER LEFT RADOME GUIDE PIN AREA. REPAIR DOUBLER INSTALLED PER AARD 53-10-00-19.

Source: SDR AALA20101022TUL10
NO TEST · 2010-06-09 Matched by certificate designator
ATA 3350

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 72,993 hrs · 38,935 cycles

PORTABLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR PORTABLE EMERGENCY LIGHT. OPS CHECKED NORMAL.

Source: SDR AALA20100610LGA02
NO TEST · 2010-06-09 Matched by certificate designator
ATA 3350

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 72,993 hrs · 38,935 cycles

FOUND GALLEY EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK AT RIGHT NUMBER 1 DOOR. OPS CHECKED NORMAL.

Source: SDR AALA20100610LGA01
Earlier reports · 1997–2009 · 30 reports

2009

OTHER · 2009-05-12 Matched by certificate designator
ATA 5230

Part: FITTING — CRACKED (ZONE 800) · airframe 70,025 hrs · 37,314 cycles

FWD CARGO DOOR, FWD EDGE LOWER STOP PAD FITTING CRACKED. REMOVED AND REPLACED STOP PAD FITTING PER ESO 80174.

Source: SDR AALA20090513TUL02
OTHER · 2009-05-12 Matched by certificate designator
ATA 5230

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 70,024 hrs · 37,314 cycles

AFT CARGO DOOR LOWER FORWARD STOP FITTING CRACKED. REMOVED AND REPLACED STOP PAD FITTING PER ESO 80174.

Source: SDR AALA20090609TUL45
OTHER · 2009-05-12 Matched by certificate designator
ATA 5230

Part: FITTING — CRACKED (ZONE 800) · airframe 70,025 hrs · 37,314 cycles

FWD CARGO DOOR, FWD EDGE SECOND FROM BOTTOM STOP PAD FITTING CRACKED. REMOVED AND REPLACED STOP PAD FITTING PER ESO 80174.

Source: SDR AALA20090513TUL03
OTHER · 2009-05-11 Matched by certificate designator
ATA 5320

Part: WEB — CRACKED (ZONE 200) · airframe 70,025 hrs · 37,314 cycles

WEB CRACKED AT FASTENER, AT CANT FRAME 1485 AT UPPER LT SIDE. STOP DRILLED AND INSTALLED DOUBLER PER AARD 53-10-00-32.

Source: SDR AALA20090513TUL05

2008

OTHER · 2008-04-18 Matched by certificate designator
ATA 3350

Part: LIGHT — BROKEN (CABIN)

RDU - EMERGENCY LIGHT LAMP AT SEAT ROW 3AB BROKEN BY PASSENGER. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 3AB. SYSTEM GROUND CHECKED NORMAL OPERATION.

Source: SDR AALA200801003
FLUID LOSS; SMOKE/FUMES/ODORS/SPARKS · 2008-03-30 Matched by certificate designator
ATA 4990

Part: APU — LEAKING · airframe 66,848 hrs

DFW INFLIGHT T2034/30MAR - CREW REPORTED SMOKE IN CABIN DURING CLIMB. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED AUXILLIARY POWER UNIT ON 04 APR AT DWH DUE TO OIL LEAK. SYSTEM GROUND CHECKED NORMAL OPERATION.

Source: SDR AALA200800765
OTHER · 2008-01-05 Matched by certificate designator
ATA 3350

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 66,413 hrs

LGA - EMERGENCY LIGHT AT OVERHEAD AFT LAVATORY MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT OVERHEAD AFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Source: SDR AALA200800034

2007

NO TEST · 2007-08-27 Matched by certificate designator
ATA 3350

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

LGA - EMERGENCY LIGHTS IN COCKPIT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Source: SDR AALA20071631
OVER TEMP; WARNING INDICATION · 2007-08-03 Matched by certificate designator
ATA 2120

Part: DUCT — LEAKING (LT A/C PACK)

TAIL COMPARTMENT OVERHEAT INDICATION ON CLIMB OUT. LEFT AIR CONDITIONING PACK WAS TURNED OFF AND LIGHT EXTINGUISHED AFTER ONE MINUTE. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED DUCT. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Source: SDR AALA20071396

2006

FALSE WARNING · 2006-05-18 Matched by certificate designator
ATA 7930

Part: PRESSURE SWITCH — INOPERATIVE (LT ENGINE)

COS - LEFT HAND ENGINE OIL CLOG LIGHT ILLUMINATED. SHUT DOWN ENGINE. SINGLE ENGINE TIME APPROXIMATELY THREE MINUTES. LANDED COS WITHOUT INCIDENT. FOUND LEFT HAND OIL FILTER FULL OF CARBON. DRAINED AND RESERVICED LEFT HAND ENGINE OIL. REPLACED LEFT HAND ENGINE OIL FILTER. REPLACED LEFT ENGINE OIL CLOG LIGHT PRESSURE SWITCH PER ENGINEERING.

Source: SDR AALA20060308

2004

FALSE WARNING · 2004-07-26 Matched by certificate designator
ATA 7997

Part: WIRE — LOOSE (SENSOR)

DFW - INFLIGHT T402/26 RIGHT ENGINE OIL TEMPERATURE WENT OFF SCALE. HIGH DURING CLIMBOUT THROUGH 27,000 FEET AT CRUISE. GAUGE WAS ERRATIC DURING DESCENT. ALL OTHER ENGINE INDICATIONS WERE NORMAL. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FOUND GROUND WIRE TO ENGINE OIL TEMPERATURE SENSOR WAS LOOSE. SECURED LOOSE GROUND WIRE AND REPLACED TEMPERATURE SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Source: SDR AALA20040778
NO TEST · 2004-06-08 Matched by certificate designator
ATA 3350

Part: BATTERY — DEFECTIVE (EMERGENCY LIGHT)

DFW - EMERGENCY EXIT CEILING LIGHTS AT SEAT 17D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Source: SDR AALA20040627

2003

NO TEST · 2003-01-03 Matched by certificate designator
ATA 3350

Part: LIGHT — INOPERATIVE (EXTERIOR)

DURING OVERNIGHT MAINTENANCE, RT EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED RT EXTERIOR EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Source: SDR AALA20030001

2002

OTHER · 2002-10-29 Matched by certificate designator
ATA 5330

Part: SKIN — CRACKED (FUSELAGE)

TUL - FOUND FUSELAGE SKIN HAS .75 INCH CRACK AT STATION 1380, L13R. EXTERNAL DOUBLER APPLIED AFTER CRACK HAD BEEN STOP DRILLED PER SRM 53-01. (M)

Source: SDR AALA20021559
NO TEST · 2002-01-05 Matched by certificate designator
ATA 3350

Part: LIGHT — INOPERATIVE (COCKPIT)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Source: SDR AALA20020008

2000

OTHER · 2000-05-20 Matched by certificate designator
ATA 5311

Part: FRAME — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON AFT SIDE OF FRAME STATION 1338 LEFT AND RIGHT OF CENTER VERTICAL STIFFENER. REPAIRED PRESSURE BULKHEAD, T-CAP AND SPLICE PER SRM 53-03 PAGE 150-160, PAGE 159 FIG 37 (SHEET 2). (M)

Source: SDR AALA2000832
OTHER · 2000-05-16 Matched by certificate designator
ATA 5320

Part: SUPPORT FITTING — CRACKED (BULKHEAD)

TUL - FOUND REDOME BULKHEAD, CENTERING PIN SUPPORT CRACKED AT FASTENER LWL RT LINE UP PIN. REPAIRED CRACK AT FASTENER PER AARD 53-10-00-19. (M)

Source: SDR AALA2000833
OTHER · 2000-05-15 Matched by certificate designator
ATA 5320

Part: BEAM — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON LOWER HORIZONTAL LEG OF THRESHOLD BEAM OF DOOR CUTOUT STATION 1155 TO STATION 1212. REMOVED CORROSION AND INSTALLED REPAIR DOUBLER PER ESO 80559 DATED 5-11-00 AND AARD 53-10-00-13 AND AARD 53-10-00. (M)

Source: SDR AALA2000829
OTHER · 2000-05-12 Matched by certificate designator
ATA 5311

Part: FRAME — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON BELLFRAME STATION 1170 FROM STRINGER 18L TO 21L. REMOVED AND INSTALLED NEW ANGLE AND BELLFRAME PER SRM 51-60-0 PAGE 3. (M)

Source: SDR AALA2000828
OTHER · 2000-05-12 Matched by certificate designator
ATA 5311

Part: FRAME — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON BELTFRAME. REMOVED CORROSION, INSTALLED Z-FRAME SECTION PER Z-FRAME REPAIR SPLICE SRM 53-03 FIG 2A. (M)

Source: SDR AALA2000830
OTHER · 2000-05-11 Matched by certificate designator
ATA 5340

Part: MOUNT — BROKEN (TAIL CONE)

TUL - FOUND STATION 1497 CANT CRACKED, LEFT SIDE AT TAILCONE RELEASED MECHANISM MOUNT BRACKET ATTACH (MRKD). INSTALLED REPAIR PER AARD 53-10-00-15 OF LIKE MATERIAL ONE GAGE HEAVIER MIN FASTENER USING PR1422 SEALANT. (M)

Source: SDR AALA2000834
OTHER · 2000-05-10 Matched by certificate designator
ATA 5310

Part: DOOR FRAME — CORRODED (FUSELAGE)

TUL - FOUND DOOR CUTOUT LOWER JAMB FRAME CORRODED, BULDGED CORROSION EMITTING FROM UNDER FLANGE AND FASTENER HEAD MISSING JUST FORWARD OF AFT DOOR STOP PAN. PERFORMED LOWER CARGO DOOR JAMB PAN SPLICE REPAIR PER M080 SRM 53-05 PART 1. (M)

Source: SDR AALA2000826
OTHER · 2000-05-09 Matched by certificate designator
ATA 5347

Part: CARGO TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON RIGHT TIE DOWN TRACK FROM STATION 1041 TO 1155. REPLACED TIE DOWN TRACK SRM 51-01. (M)

Source: SDR AALA2000827
OTHER · 2000-05-09 Matched by certificate designator
ATA 5310

Part: SHEAR TIE — CRACKED (FUSELAGE)

TUL - FOUND 1380 SHEAR TIE AT L-14 CRACKED LEFT. REPAIRED SHEAR TIE PER AARD 53-10-00-20. INSTALLED DOUBLER WET WITH 1422 AND .1875 HI-LOCKS. (M)

Source: SDR AALA2000838
OTHER · 2000-05-05 Matched by certificate designator
ATA 5310

Part: SHEAR TIE — CRACKED (FUSELAGE)

TUL - FOUND SHEAR TIE AT STATION 1307 BETWEEN LONGERON 14-16L WAS CRACKED. REPLACED CRACKED SHEAR TIE PER SRM 51-01. (M)

Source: SDR AALA2000835
OTHER · 2000-05-04 Matched by certificate designator
ATA 5310

Part: SHEAR TIE — CRACKED (FUSELAGE)

TUL - FOUND SHEAR TIE CRACKED, RIGHT BETWEEN R-14 AND R-16 AT STATION 1307. REMOVED CRACKED SHEAR TIE AND INSTALLED NEW SHEAR TIE PER SRM 51-01. (M)

Source: SDR AALA2000837
OTHER · 2000-05-04 Matched by certificate designator
ATA 5313

Part: LONGERON — CRACKED (FUSELAGE)

TUL - FOUND CRACK IN LONGERON 5R, RT STATION 160. REMOVED SECTION OF LONGERON 5R FROM STATION 148.5 TO STATION 169 AND SPLICED IN NEW SECTION PER SRM 53-02 FIG 18. (M)

Source: SDR AALA2000836

1998

NO TEST · 1998-06-16 Matched by certificate designator
ATA 3397

Part: WIRE — BROKEN (CABIN)

ORD - AFTER TAXI TO HANGAR THE SLIDE EMERGENCY LIGHTS WOULD NOT EXTINGUISH. REPAIRED WIRE ON EMERGENCY LIGHT PACK B5-28. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Source: SDR AALA981185
NO TEST · 1998-03-15 Matched by certificate designator
ATA 3350

Part: CONNECTOR — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, MID CABIN EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTORS AT MID GALLEY. SYSTEM GROUD CHECKED NORMAL OPERATION. (M)

Source: SDR AALA980493

1997

OTHER · 1997-11-15 Matched by certificate designator
ATA 5313

Part: LONGERON — CORRODED (BS 1287)

TUL - LONGERON CORRODED, BLOWN OUT JUST AFT OF FRAME AT STA 1287 BELOW FORWARD LOWER CORNER OF THRUST RECOVERY VALVE. REMOVED DAMAGED LONGERON SECTION AND INSTALLED FILLER AND REPAIR DOUBLERS PER SRM 53-02 PAGE 50. TST: 37,318 HOURS. CYCLES, 20,999. (X)

Source: SDR AALA972183