N411AA
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.
39 reports on file, 1996-04-30 – 2008-09-26.
Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · 66,311 cycles
EMERGENCY LIGHT AT OVERHEAD SEAT ROWS 18 TO 24 INOPERATIVE. REPLACED BATTERY PACK AT STATION 900 FOR EMERGENCY LIGHT AT OVERHEAD SEAT ROWS 18 TO 24. SYSTEM GROUND CHECKED NORMAL OPS.
Part: BATTERY PACK — DISCHARGED (CABIN) · 65,953 cycles
LGA SEAT MOUNTED EMERGENCY LIGHTS AT SEAT ROW 20 INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 20 FOR INOPERATIVE SEAT MOUNTED EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPS.
Part: BATTERY PACK — DISCHARGED (CABIN) · 65,953 cycles
LGA EMERGENCY LIGHTS AT OVERHEAD SEAT ROW 20 AND AFT LAVATORY INOPERATIVE. REPLACED BATTERY PACK AT OVERHEAD SEAT ROW 20 FOR INOPERATIVE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPS.
Part: STRUT — INOPERATIVE (NLG) · airframe 64,529 hrs
ORD INFLIGHT T2481/02FEB - NOSE GEAR UNSAFE LIGHT ILLUMINATED AFTER NOSE GEAR RETRACTION. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. ACCOMPLISHED NOSE GEAR SHOCK STRUT SEAL REPLACEMENT AND REPLACED TURNING TUBE CYLINDER AND LOWER BEARING ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: SCHRADER VALVE — INOPERATIVE (NLG) · airframe 64,477 hrs
RSW INFLIGHT T1093/26JAN - CREW REPORTED NOSE GEAR RED LIGHT AFTER RETRACTION. RETURNED TO RSW AND LANDED WITHOUT INCIDENT. ACCOMPLISHED NOSE LANDING GEAR STRUT REPACK AND REPLACED SCHRADER VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION.
Earlier reports · 1996–2007 · 34 reports
2007
Part: BATTERY PACK — DISCHARGED (CABIN)
LGA - EMERGENCY LIGHT AT SEAT ROW 25 INOPERATIVE. REPLACED BATTERY PACK AT OVERHEAD BIN FOR EMERGENCY LIGHT AT SEAT ROW 25. SYSTEM GROUND CHECKED NORMAL OPERATION.
2006
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)
JAX - EMERGENCY LIGHTS IN CABIN INOPERATIVE. EMERGENCY LIGHTS LEFT IN ARMED POSITION. REPLACED ALL CABIN BATTERY PACKS FOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY PACK — DISCHARGED (CABIN)
DFW - AFT SEAT EMERGENCY ESCAPE PATH LIGHT AT 7D INOPERATIVE. REPLACED AFT SEAT EMERGENCY ESCAPE PATH LIGHT AT SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION.
2005
Part: BATTERY PACK — INOPERATIVE (CABIN)
LGA - INTERIOR OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR INTERIOR OVERWING EXIT EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
SFO - EMERGENCY EGRESS LIGHT INOPERATIVE AT ROW 20 AFT. REPLACED BATTERY FOR EMERGENCY EGRESS LIGHT AT ROW 20 AFT. SYSTEM GROUND CHECKED NORMAL OPERATION.
2004
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
SFO - OVERHEAD EMERGENCY LIGHT ABOVE TAIL CONE SLIDE INOPERATIVE. RESET BATTERY PACK FOR OVERHEAD EMERGENCY LIGHT ABOVE TAIL CONE SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
SFO - OVERHEAD EMERGENCY LIGHT ABOVE AIRSTAIR WALKWAY INOPERATIVE. RESET BATTERY PACK FOR OVERHEAD EMERGENCY LIGHT ABOVE AIRSTAIR WALKWAY. SYSTEM GROUND CHECKED NORMAL OPERATION.
2003
Part: BATTERY — DISCHARGED (AFT AIRSTAIRS)
DFW AFT AIRSTAIRS CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY FOR AFT AIRSTAIRS CATWALK EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY — DISCHARGED (CABIN)
DFW FORWARD LEFT OVERWING EXIT LIGHT INOPERATIVE. REPLACED BATTERY FOR FORWARD LEFT OVERWING EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY — DISCHARGED (CABIN)
DFW FORWARD RIGHT OVERWING EXIT LIGHT INOPERATIVE. REPLACED BATTERY FOR FORWARD RIGHT OVERWING EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY — DISCHARGED (CABIN)
STL FIRST CLASS OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY FOR FIRST CLASS OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED
Part: SPAR CAP — DAMAGED (RT WING)
RT WING REAR SPAR LOWER CAP DAMAGED (GROUND DAMAGE). INSTALLED SERVICEABLE LOWER CAP DOUBLER AND FILLER IAW ESO 80559.
Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)
DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT SEATS 21 AND AFT INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT BATTERY CHARGER CONNECTOR ABOVE ROW 21. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — INOPERATIVE (CABIN)
DURING OVERNIGHT MAINTENANCE, ENTRY WAY EMERGENCY EXIT IGHT ACROSS FROM FIRST CLASS LAVATORY BROKEN. REPLACD ENTRY WAY EMEGENCY EXIT LIGHT ACROSS FROM FIRST CLASS LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2002
Part: BATTERY PACK — DISCHARGED (CABIN)
DFW - FOUND CEILING LIGHTS INOPERATIVE AT 8B, 9B/D, 11B, 22BD, 24B, AND 26BD. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT ROWS 9-12 AND 22-26. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: FLASHLIGHT — INOPERATIVE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED EMERGENCY FLASHLIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2001
Part: CARGO TRACK — CORRODED (CARGO BAY)
TUL - FOUND CORROSION AT ATTACH FASTENER AND NUT CLIPS FROM 1211 TO 1322. REPLACED LEFT CARGO TIE DOWN TRACK STATION 1007-1322, PER SRM 51-01. (M)
Part: BEAM — CORRODED (AFT CARGO BAY)
TUL - FOUND STATION 1155-1212 CARGO DOOR CUTOUT LOWER CHORD SUPPORT ANGLE CORRODED MULTIPLE AREA. REMOVED AND REPLACED LOWER DOOR CUTOUT BEAM STATION 1117-1250 PER SRM 51-01. (M)
Part: WEB — DAMAGED (AFT CARGO BAY)
TUL - FOUND STATION 1215-1216, WEB DOOR FRAME BELOW NUTPLATE HAS HOLE, STATION 1216. INSTALLED NEW WEB SPLICE PER AARD 53-10-00-24 AND SRM 53-01. (M)
Part: FITTING — CORRODED (AFT CARGO BAY)
TUL - FOUND STATION 1210 TO STATION 1212 DOOR CUTOUT FRAME CORNER FITTING CORRODED, OUTBOARD LONGERON 28R. INSTALLED NEW FITTING PER SRM 51-01. (M)
Part: LONGERON — CRACKED (FUSELAGE)
TUL - FOUND VISUAL INDICATION OF CRACK ON LONGERON 20R, STATION 1003. STOP DRILLED CRACK AND REPAIRED LONGERON PER AARD 53-10-00-18 PAGE 1 TO PAGE 3. (M)
Part: FRAME — CORRODED (FUSELAGE)
TUL - FOUND CORROSION ON CHORD ANGLE STATION 1003 LONGERON 26L. REPAIRED ANGLE PER ESO 80559 DATED 1-30-01 CORROSION BLENDED OUT AND DOUBLER INSTALLED. (M)
Part: FRAME — GOUGED (FUSELAGE)
TUL - FOUND TWO DEEP GOUGES ON BELLFRAME AT STATION 370 BETWEEN LONGERON 16R AND 17R. BLENDED OUT GOUGES TO 20 PERCENT TO 50 PERCENT THICKNESS REMOVAL AND INSTALLED DOUBLER PER AARD 53-10-00-14. (M)
Part: WINDOW FRAME — CRACKED (COCKPIT)
TUL - FOUND CRACK IN F/O AFT WINDOW RETAINER BETWEEN SKIN AND WINDOW POST, UPPER FORWARD CORNER OF WINDOW. REMOVED DAMAGE AND INSTALLED DOUBLER PER ESO 80559, DATED 1/30/2001. (M)
Part: SEAT TRACK — CORRODED (CABIN)
TUL - FOUND CORROSION BEYOND LIMIT ON SEAT TRACK NR 1 AT STA 825. INSTALLED REPAIR PER AARD 53-20. (M)
Part: SKIN — CRACKED (FUSELAGE)
TUL - FOUND FUSELAGE SKIN CRACKED AT STATION 1380 BELOW L13R. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-01 FIG 2 SHEET 3. (M)
Part: SEAT TRACK — WORN (CABIN)
TUL - FOUND NR 3 SEAT TRACK WORN, BS 296. INSTALLED SEAT TRACK PLUG PER SRM 53-05 PART 1. (M)
Part: SKIN — DENTED (FUSELAGE)
TUL - FOUND DENT AND SCRATCH IN FUSELAGE BELOW RIGHT ENGINE 3 FEET ABOVE FRESH WATER DRAIN HOLE, FS 1309. REF ADL NR 0024. INSTALLED TITANIUM SCUFF PLATE PER AARD 53-30-00-8 AND INTERNAL DOUBLER PER SRM 53-04 FIG 38. (M)
2000
Part: OVEN — DIRTY (GALLEY)
DFW - FLT 490 - AFTER TAKEOFF ELECTRICAL SMOKE SMELL REPORTED IN AFT CABIN BY FLIGHT ATTENDANT. RETURNED AND LANDED DFW WITHOUT FURTHER INCIDENT. REPLACED OVEN. GROUND CHECK NORMAL OPERATION. (M)
1997
Part: FLOOR — CORRODED (BS 200)
TUL - FOUND CORROSION ON UNDER FLOOR MEMBRANE, JUST RIGHT OF CENTER AT STATION 200 (MARKED). REMOVED CORROSION AND INSTALLED DOUBLR PER SRM 53-01 FIG 4. (M)
Part: LIGHT — INOPERATIVE (CABIN)
DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY FORWARD GALLEY INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP BY FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1996
Part: CONTROLLER — DEFECTIVE (COCKPIT)
DFW - FLT 1358 - AFTER TAKEOFF DFW DURING INITIAL CLIMB-OUT, CABIN PRESSURIZATION WHEEL BEGAN OSCILLATING AND CABIN TEMPERATURE BECAME HOT ACCOMPANIED BY FUMES AND SMOKE. AIRCRAFT RETURNED TO DFW AND LANDED OVERWEIGHT WITHOUT INCIDENT. REPLACED CABIN TEMPERATURE CONTROLLER. ACCOMP GROUND ENGINE RUN WITH PACKS OPERATING AND SYSTEM GROUND CHECKED NORMAL OPERATION. ACCOMP PACK BURNOUT PROCEDURE. ACCOMP OVERWIGHT LANDING INSPECTION WITH NO DEFECTS FOUND. ACCOMP FUNCTIONAL CHECK FLIGHT WITH NO DEFECTS FOUND. SYSTEM OPERATIONAL CHECKED NORMAL. (M)
Part: SKATE ANGLE — CRACKED (BS 1474)
TUL - FOUND LEFT VERTICLE SKATE ANGLE DOUBLER CRACKED FS 1474. ACCOMPLISHED REPAIR PER AARD 53-10-00-2. (M)
Part: CLIP — CORRODED (BS 1220)
TUL - FOUND CLIP CORRODED AFT SIDE OF FRAME BELOW RIGHT TIEDOWN TRACK IN AFT CARGO. REMOVED CLIP. INSTALLED NEW CLIP. (M)