N290AA
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
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.
38 reports on file, 1995-07-23 – 2010-07-20.
Part: CONNECTOR — DAMAGED (CABIN) · airframe 73,039 hrs · 38,894 cycles
SEAT EGRESS LIGHT ON SEAT 12D INOPERATIVE. REPLACED DAMAGED CONNECTOR FOR EGRESS LIGHT AT SEAT 12D.
Earlier reports · 1995–2009 · 37 reports
2009
Part: REGULATOR VALVE — FAILED (LT PACK) · airframe 70,790 hrs · 37,649 cycles
DURING CLIMB CREW NOTICED A STRONG SMELL LIKE SOMETHING BURNING THROUGH OUT THE CABIN. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED THE PRESSURE REGULATOR VALVE ON LEFT PACK. SYSTEM CHECKED NORMAL OPERATION.
Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,499 hrs · 36,963 cycles
CORROSION ON SUB FLOOR AT STATION 170 RIGHT JUST ABOVE COOLING DUCT. INSTALLED DOUBLER PER AARD 53-20-00-16.
Part: SKIN — CRACKED (FUSELAGE) · airframe 69,499 hrs · 36,963 cycles
CRACK IN FUSELAGE SKIN AT LONGERON 22L, 2ND RIVET FORWARD OF STATION 200. INSTALLED DOUBLER PER EA MD80-53-005845 AND EA MD80-53-005856.
Part: PLATE — CRACKED (FUSELAGE) · airframe 69,499 hrs · 36,963 cycles
RIGHT AFT OVERWING EXIT CUTOUT FORWARD GUIDE RECESS PLATE IS CRACKED. INSTALLED DOUBLER PER SRM 53-05-00 FIGURE 32.
Part: LIGHT — NOT SEATED (CABIN) · airframe 69,281 hrs
LGA SEAT MOUNTED EMERGENCY LIGHT AT SEAT 12D INOPERATIVE. RESEATED EMERGENCY LIGHT ASSEMBLY FOR SEAT 12D.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 69,282 hrs
LGA CEILING MOUNTED EMERGENCY LIGHTS IN FORWARD CABIN AND COCKPIT INOPERATIVE. REPLACED BATTERY PACK.
2008
Part: LENS — MISSING (EMERGENCY LIGHTS) · 68,149 cycles
LGA EMERGENCY LIGHT AT OVERHEAD AFT SERVICE AREA MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT OVERHEAD AFT SERVICE AREA. SYSTEM GROUND CHECKED NORMAL OPS.
Part: CONTACT — DIRTY (EMERGENCY LIGHTS) · 68,149 cycles
LGA EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 23 TO 30 INOPERATIVE. CLEANED AND ADJUSTED CONTACT AT ROW 25 FOR EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 23 TO 30. SYSTEM GROUND CHECKED NORMAL OPS.
Part: CONTACT — DIRTY (EMERGENCY LIGHTS) · 68,149 cycles
LGA EXTERIOR EMERGENCY LIGHTS AT RT HAND OVERWING EXIT INOPERATIVE. CLEANED AND ADJUSTED CONTACT FOR EXTERIOR EMERGENCY LIGHTS AT RT HAND OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPS.
Part: CONTACT — DIRTY (EMERGENCY LIGHT) · 68,149 cycles
LGA EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 23 TO 30 INOPERATIVE. CLEANED AND ADJUSTED CONTACT AT ROW 28 FOR EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 23 TO 30. SYSTEM GROUND CHECKED NORMAL OPS.
Part: CONTACT — DIRTY (EMERGENCY LIGHTS) · 68,149 cycles
LGA EXTERIOR EMERGENCY LIGHTS AT LT HAND OVERWING EXIT INOPERATIVE. CLEANED AND ADJUSTED CONTACT FOR EXTERIOR EMERGENCY LIGHTS AT LT HAND OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPS.
2007
Part: PROXIMITY SWITCH — INOPERATIVE
ORD INFLIGHT T1101/28SEP - DURING CLIMB CREW RECEIVED STALL THEN SLAT OVERSPEED INDICATION. ON APPROACH ANTI-SKID CIRCUIT BREAKER POPPED. LANDED ORD WITHOUT INCIDENT. REPLACED GROUND PROXIMITY BOX. SYSTEM GROUND CHECKED NORMAL OPERATION.
2006
Part: BATTERY PACK — DISCHARGED (CABIN)
ORD - CEILING EMERGENCY LIGHTS AT ROWS 12 TO 22 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT ROWS 12 TO 22. SYSTEM GROUND CHECKED NORMAL OPERATION.
2005
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
ORD - OVERWING FORWARD RIGHT AND LEFT HAND EMERGENCY EXIT UPPER EXIT SIGNS INOPERATIVE. REPLACED BATTERY PACK FOR OVERWING FORWARD RIGHT AND LEFT HAND EMERGENCY EXIT UPPER EXIT SIGNS. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
ORD - EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACKS FOR EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)
SJC - EMERGENCY LIGHTS AT FLIGHT ATTENDANT STATION INOPERATIVE. REPLACED PIN ON CONNECTOR P11161 FOR EMERGENCY LIGHTS AT FLIGHT ATTENDANT STATION. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LIGHT — INOPERATIVE (CABIN)
DFW - SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY AT 12D INOPERATIVE. REPLACED THE SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT 12D. SYSTEM GROUND CHECKED NORMAL OPERATION.
2004
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
PHX - BATTERY CHARGER AT STATION 902R FOR CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK/CHARGER ASSEMBLY AT STATION 902R FOR CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.
2003
Part: BATTERY PACK — DISCHARGED (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING WAS OBSERVED TO BE INOPERATIVE IN THE FLIGHT DECK AND THE FIRST CLASS GALLEY. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: STRUT — DEFECTIVE (NLG)
MIA - FLT 1578 - EN ROUTE MIA-ATL, ON TAKEOFF, NOSE LANDING GEAR DID NOT RETRACT PROPERLY. SEVERAL LOUD THUMPS HEAD AT HIGH SPEED ON TAKEOFF ROLL. RETURNED MIA WITHOUT INCIDENT. INSTALLED SERVICEABLE NOSE GEAR STRUT. ACCOMPLISHED NOSE GEAR SWING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2001
Part: BATTERY PACK — DISCHARGED (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT ESCAPE PATH LIGHTS BETWEEN ROW 18 AND 21 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT ESCAPE PATH LIGHTS BETWEEN ROW 18 AND 21. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
2000
Part: SKIN — DAMAGED (VERTICAL STAB)
TUL - LEADING EDGE SKIN BUTT JOINT BELOW LOWER VOR ANTENNA SEVERAL FASTENERS PULLED BELOW SKIN LEVEL L/E AREA. REPAIRED PER ESO 80559 DATED 2/11/00. (M)
Part: SEAT TRACK — CORRODED (BS 483-485)
TUL - FOUND CORROSION IN NR 6 SEAT TRACK STATION 483-485. REMOVED DAMAGED AREA AND INSTALLED SEAT TRACK PLUG REPAIR PER SRM 53-05. (M)
Part: SEAT TRACK — CORRODED (BS 671-673)
TUL - FOUND CORROSION IN SEAT TRACK. REMOVED DAMAGED AREA INSTALLED SEAT TRACK PLUG REPAIR PER SRM 53-05. (M)
Part: SEAT TRACK — CORRODED (BS 732 - 733)
TUL - FOUND CORROSION IN NR 6 SEAT TRACK. REMOVED DAMAGED AREA. INSTALLED SEAT TRACK PLUG REPAIR PER SRM 53-05. (M)
Part: TIE DOWN — CORRODED (BS 160)
TUL - FOUND GALLEY TIE DOWN CORRODED AT STATION 160 RIGHT APPROX 8 INCHES AND APPROX 15 INCHES FROM OUTBOARD FUSELAGE. INSTALLED NEW GALLEY TIE DOWN PER SRM 51-01. (M)
Part: ANGLE — CRACKED (BS 1485)
TUL - CANT FRAME ATTACH ANGLE CRACKED 3 INCH LONG RIGHT SIDE OF STAIRS AT STAIR ACT. FOUND PREVIOUS REPAIR DOUBELR HAD 2 INCH CRACK, PREVIOUS CANT ANGLE REPAIR CRACKED PAST STOP DRILL. STOP DRILLED CRACKED CANT FRAME AND REPLACED CRACKED DOUBLER PER SRM 53-01 FIG 2 PAGE 10. (M)
Part: SEAT TRACK — CORRODED (BS 1208)
TUL - FOUND CORROSION IN 'U' CHANNEL OF NR 1 SEAT TRACK STATION 1208. REMOVED AND REPLACED SEAT TRACK. (M)
Part: WEB — CRACKED (BS 180)
TUL - FOUND CRACK IN WEB MEMBRANE BELOW WETBOARD FC4 STATION 180 RBL 24 INCH. STOP DRILLED CRACK INSTALLED DOUBLER PER AARD 53-00-00-02 PG 1 AND SRM 53-01 FIG 4 SHEET 5. (M)
Part: WEB — CRACKED (BS 1309)
TUL - BS 1309 CRACKED AT RADIUS, BELOW LONGERON 14R, REF E58 NR 3291721. REMOVED AND REPLACED MARKED SHEAR TIE PER SRM 51-01 REF E58 NR 3291721. (M)
Part: SHEAR TIE — CRACKED (BS 1309)
TUL - FOUND CRACK IN RADIUS OF SHEAR TIE. REMOVED AND REPLACED SHEAR TIE. (M)
Part: CARGO TRACK — CORRODED (BS 1220-1320)
TUL - LEFT TIED DOWN TRACK CORRODED AT CLIPNUT HOLES, UPPER AND LOWER SURFACES) FROM STATION 1220-1320. INSTALLED NEW TIE DOWN TRACK PER SRM 51-01. (M)
Part: WEB — PUNCTURED (BS 1248)
TUL - FOUND RIGHT CUSP PUNCTURED AT STATION 1248. REMOVED DAMAGED AREA INSTALLED REPAIR DOUBLER ON CUSP PER SRM 53-05 PART 1 FIG 2. (M)
1999
Part: CONNECTOR — BROKEN (TAIL COMPT)
DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD TAIL COMPARTMENT EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED OVERHEAD TAIL COMPARTMENT EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
1996
Part: SILL — CORRODED (BS 200)
TUL - DURING DETAIL INSPECTION OF CARD 4002. FOUND HEAVY CORROSION ON FORWARD SERVICE DOOR FLOOR PANEL AT LOWER AFT CORNER STATION 200. REPAIRED PER ESO 80559 DATED 6-21-96. (M)
Part: FITTING — CRACKED (WS 807)
FOUND 12 INCH FITTING ON UPPER FORWARD LEFT SIDE OF WING SPAR IS CRACK VERT AT RADIUS. E58 1780872 REPLACED FITTING AND SHIM TO FIT USING GENERAL PROCEDURES SRM 51-10. (M)
1995
Part: EEL WIRE — MIS INSTALLED (CABIN)
DFW - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT FLOOR PATH LIGHTS FROM OVERWING EXIT TO FORWARD GALLEY CYCLING ON AND OFF. REVERSED POLARITY IN EMERGENCY EXIT FLOOR PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)