N295AA
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.
34 reports on file, 1996-07-28 – 2009-06-11.
Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 62,044 hrs · 32,973 cycles
RIGHT CUSP MEMBRANE HAS OLD STYLE DOUBLER AND CRACK AT STATION 1271 TO 1307. INSTALLED NEW CUSP MEMBER STATION 1271 TO 1309 PER AARD 53-20-00-16.
Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 62,044 hrs · 32,973 cycles
LEFT CUSP MEMBRANE HAS OLD STYLE REPAIR DOUBLER AND CRACKED 1271 TO 1307. INSTALLED NEW CUSP FROM 1251 TO 1309 PER SRM 53-05-00 FIG 97 AND AARD 53-20-00-16 FIG 3.
Part: STOP FITTING — CRACKED (DOOR) · airframe 62,044 hrs · 32,973 cycles
SECOND FROM TOP AFT SIDE STOP PAD FITTING CRACKED. INSTALLED NEW STOP PAD FITTING PER ESO 80174.
Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 62,044 hrs · 32,973 cycles
LOWER FORWARD STOP PAD FITTING CRACKED ON AFT CARGO DOOR. INSTALLED NEW STOP PAD PER ESO 80174.
Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 62,044 hrs · 32,973 cycles
MID CARGO DOOR, 3 STOP BRACKETS CRACKED, FORWARD TOP, FORWARD MID AND FORWARD BOTTOM. REPLACED 3 STOP BRACKETS PER ESO 80174.
Part: FITTING — CRACKED (DOOR) · airframe 62,044 hrs · 32,973 cycles
SKIN TO WEB T-ANGLE AT LOWER FORWARD STOP PAD SUPPORT FITTING CRACKED. INSTALLED NEW FITTING PER ESO 80174.
Part: PAN — CRACKED (CARGO DOOR) · airframe 62,044 hrs · 32,973 cycles
AFT CARGO DOOR PAN IS CRACKED AT LOWER FORWARD STOP. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 52-03-00 FIG 8 SHEET 4.
Part: ANGLE — CRACKED (DOOR) · airframe 62,044 hrs · 32,973 cycles
SKIN TO WEB T-ANGLE AT LOWER AFT STOP PAD SUPPORT FITTING CRACKED. INSTALLED NEW FITTING PER ESO 80174.
Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 62,044 hrs · 32,973 cycles
HFEC INDICATES CRACKS ON 3 EACH STOP BRACKETS OF MID CARGO. REPLACED 3 EACH STOP BRACKETS PER ESO 80174.
Earlier reports · 1996–2005 · 25 reports
2005
Part: CONNECTOR — LOOSE (BATTERY PACK)
SFO - RIGHT NR 1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. FOUND BATTERY PACK CONNECTOR LOOSE. RESECURED CONNECTOR FOR BATTERY PACK FOR RIGHT NR 1 DOOR EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.
2004
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
DFW - CEILING EMERGENCY LIGHTS AT ROWS 13 THROUGH 16 INOPERATIVE. REPLACED BATTERY PACK B5-102 FOR CEILING EMERGENCY LIGHTS AT ROWS 13 THROUGH 16. SYSTEM GROUND CHECKED NORMAL OPERATION.
2003
Part: SENSOR — DEFECTIVE (A/C BAY)
DFW - FLT 1698 - EN ROUTE DFW-IAD, ON CLIMB-OUT AT 24,000 FEET, TAIL COMPARTMENT TAIL HIGH LIGHT ILLUMINATED. FOLLOWED CHECKLIST AND LIGHT EXTINGUISHED. LIGHT ILLUMINATED AGAIN WHEN POER ADVANCED. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED HIGH AND LOW TEMPERATURE SENSORS FOR LEFT BLEED AIR LEFT AIR CONDITIONING PACKS. RAN PACKS ON APU AIR, ENGINE BLEED AIR ON BOTH. CHECKED FOR PNEUMATIC AIR LEAKS NONE FOUND. SYSTEM GROND CHECKED NORMAL OPERATION. (M)
Part: SEAL — LEAKING (A/C BAY)
DFW - FLT 1938 - DFW-CLE, ON CLIMB-OUT, TAIL COMPARTMENT HIGH LIGHT ILLUMINATED. FOLLOWED CHECKLIST AND LIGHT EXTINGUISHED WHEN LEFT PACK WAS TURNED OFF. LIGHT ILLUMINATED AGAIN WHEN POWER ADVANCED TOWARD CLIMB POWER. RETARDED POWER AND LIGHT EXTINGUISHED. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED LEFT PACK HEAT EXCHANGER EXHAUST SLIP DUCT SEAL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — INOPERATIVE (CABIN)
MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT AFT DOOR SERVICE LIGHT INOPERATIVE. REPLACED AFT SERVICE DOOR EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — INOPERATIVE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, DETACHABLE EMERGENCY EXIT DOOR LIGHT INOPERATIVE. REPLACED DETACHABLE EMERGENCY EXIT DOOR LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: BATTERY — NOT SEATED (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, FIRST CLASS OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BATTERY AT FIRST CLASS BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2002
Part: SKIN — CRACKED (FUSELAGE)
TUL - FOUND FUSELAGE SKIN IS CRACKED, 3 PLACES, AT STATION 1380, L12R. INSTALLED DOUBLER PER SRM 53-01 FIG 2 SHEET 3. (M)
Part: SOCKET — DEFECTIVE (CABIN)
DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING AT SEAT 11D HAS BULB, INOPERATIVE. REPLACED EMERGENCY EXIT PATH LIGHTING AT SEAT 11D SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: CHARGER — INOPERATIVE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTS IN CEILING ROW 23 THROUGH 26 INOPERATIVE. REPLACED BATTERY CHARGER ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: BATTERY — DISCHARGED (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS WILL NOT ILLUMINATE. REPLACED EMERGENCY EXIT LIGHTS BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: BATTERY — DISCHARGED (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, LOWER RIGHT SIDE WALL FORWARD EXIT SIGN AT ROW 20 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2000
Part: BEAM — CORRODED (FUSELAGE)
TUL - FOUND AFT CARGO DOOR CUT OUT LOWER BEAM CORRODED FROM STATION 1155 TO 1212 ON VERTICAL AND HORIZ FLANGES. REMOVED CORRODED BEAM. INSTALLED NEW BEAM, FROM STATION 1155 TO 1226 PER SRM 51-30 AND 53-10. (M)
Part: CONNECTOR — LOOSE (CABIN)
DFW - EMERGENCY EXIT ESCAPE PATH LIGHTS AFT LAST SEGMENT INOPERATIVE. REPAIRED CONNECTOR FOR LAST SEGMENT. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
Part: LIGHT — INOPERATIVE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SIGN AT C2 DOOR IS INOPERATIVE. REPLACED EMERGENCY EXIT SIGN LIGHT ASSEMBLY AT C2 DOOR. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
1999
Part: ACM — MALFUNCTIONED (AC BAY)
BDL - FLT 1180 - ON ARRIVAL BDL, CABIN FILLED WITH SMOKE. LANDED BDL WITHOUT INCIDENT. REPLACED RIGHT AIR-CONDITIONING AIR CYCLE MACHINE. ALSO, REPLACED COALESCER BAGS AND ACCOMPLISHED PACK BURN OUT. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
Part: HYDRAULIC LINE — LEAKING (LT TR UNIT)
ORD - FLT 2326 - EN ROUTE DFW-ORD, LEFT HYDRAULC FLUID QTY DROPPED TO RED BAND. ABNORMAL PROCEDURE FOR SLAT/FLAP EXTENSION ACCOMPLISHED AND AIRCRAFT LANDED ORD WITHOUT INCIDENT. REPLACED LEFT THRUST REVERSER CONTROL VALVE HYDRAULIC PRESSURE LINE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1997
Part: SLIDE — LOW PRESSURE (FWD ENTRY DOOR)
RDU - DURING OVERNIGHT CHECK, FOUND FORWARD ENTRY DOOR SLIDE BOTTLE PRESSURE LOW. REPLACED FORWARD ENTRY DOOR EMERGENCY EVACUATION SLIDE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
1996
Part: JAMB BEAM — CORRODED (BS 370-427)
TUL - FORWARD CARGO DOOR JAMB LOWER BEAM HAS CORROSION STATION 370 TO 427. REPLACED FORWARD CARGO DOOR JAMB BEAM. (M)
Part: FRAME — CORRODED (BS 1322)
TUL - FOUND FORWARD LOWER ANGLE ON BELT FRAME CORRODED. CORROSION CUT OUT DOUBLER INSTALLED PER SRM 53-03 FIG 2A. (M)
Part: FRAME — CORRODED (BS 1309)
TUL - FOUND CORROSION AFT LOWER BELT FRAME STATION 1309 LONGERON 29R TO 29L. CUT OUT CORROSION, INSTALLED DOUBLER PER AARD 53-10-00-17. (M)
Part: CUSP — CORRODED (BS 188)
TUL - FOUND CORROSION ON CUSP MEMBRANE INBOARD OF ENTRY DOOR AT BS 188. DOUBLER INSTALLED SRM 53-01 PAGE 7, FIG 2. (M)
Part: FITTING — CORRODED (DOOR OPENING)
STA 115.5 FORWARD LOWER CORNER OF CARGO DOOR OPENING. CORROSION AROUND HI-LOCK FASTENERS. INSTALLED NEW SUPPORT FITTING. TST: 33,327.4. CYCLES, 19,146. (X)
Part: DUCT — RUPTURED (RT ACM)
ABQ - FLT 203 - EN ROUTE DFW/SFO - DURING CRUISE, TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. AIRCRAFT DIVERTED TO ABQ AND LANDED WITHOUT INCIDENT. PLACARDED LEFT AIR CYCLE MACHING. ACCOMPLISHED FUNCTIONAL CHECK FLIGHT WITH NO DEFECTS FOUND. SYSTEM OPERATIONAL CHECKED NORMAL. SUBSEQUENTLY, AT DFW, REPLACED RUPTURED WATER SEPARATOR DUCT AT RIGHT AIR CYCLE MACHINE. ACCOMPLISHED LEAK AND GROUND CHECK WITH NO DEFECTS FOUND. SYSTEMS GROUND CHECKED NORMAL OPERATION AND PLACARD FOR LEFT AIR CYCLE MACHINE REMOVED. (M)
Part: CHECK VLV — STUCK CLOSED (TAIL COMPT)
ABQ - FLT 1191 - DFW-SFO - DURING CRUISE TAIL COMPART HIGH TEMP LIGHT ILLUMINATED. A/C DIVERTED TO ABQ AND LANDED OVERWEIGHT W/O INCIDENT. CHECKED AIR CONDITIONING DUCT AT ACM AND APU SUPPLY DUCTS WITH NO DEFECTS FOUND. ACCOMP GROUND ENG RUN AND CHECKED AUGMENTATION VLV AND ENG SUPPLY DUCTS WITH NO DEFECTS FOUND. CLEANED AND FREED UP OVERHEAT SENSOR, CHECK VLV FOUND STUCK CLOSED. PRECAUTIONARY PLACARDED LEFT ACM. SYSTEM GROUND CHECKED NORMAL OPERATION. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION WITH NO DEFECTS FOUND. A/C REDEPARTED ABQ-SFO, SUBSEQUENTLY AT DFW, ACCOMP GROUND CHECK OF BOTH PACK AND HIGH TEMP SYSTEM W/NO DEFECTS FOUND. SYSTEMS GROUND CHECKED NORM OP AND PLACARD REMOVED. (M)