N465A
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.
39 reports on file, 1997-07-27 – 2010-06-19.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,774 hrs · 33,412 cycles
CORROSION BETWEEN AFT LAVATORY PAN AND SKIN AT LOWER FORWARD CORNER OF CUTOUT. INSTALLED SKIN DOUBLER AT AFT LAVATORY SERVICE PAN PER EA MD80-53-011325.
Part: STRAP — CORRODED (FUSELAGE) · corrosion level 3 · airframe 63,774 hrs · 33,412 cycles
REMOVED CORRODED STRAP IN LONGERON CHANNEL. NO CORROSION FOUND UNDER STRAP IN LONGERON CHANNEL. INSTALLED NEW STRAP IN LONGERON 23 LEFT AT STATION 1309 PER SRM 51-30-02.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 63,774 hrs · 33,412 cycles
DENT IN FUSE STATION 266 BETWEEN LONGERON 16 LEFT AND LONGERON 17 LEFT. INSTALLED DOUBLER PER SRM 53-04-00.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,584 hrs · 33,314 cycles
CEILING EGRESS LIGHTS INOPERATIVE IN ROWS 18 TO 22. REMOVED AND REPLACED EMERGENCY BATTERY PACK AT ROW 20DEF. OPS CHECKED NORMAL.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,584 hrs · 33,314 cycles
SEAT EGRESS LIGHTS INOPERATIVE AT ROWS 21 TO 32. REMOVED AND REPLACED EMERGENCY BATTERY PACK AT ROWS 20DEF. OPS CHECKED NORMAL.
Part: INDICATOR — FAULTY (COCKPIT) · airframe 63,381 hrs · 33,194 cycles
MCI - INFLIGHT MSP-DFW. HEADING ANNUNCIATOR ON BOTH FLIGHT MODE ANNUNCIATORS CAME ON. UNABLE TO DETERMINE WHICH SYSTEM WAS CORRECT DUE TO LARGE DEVIATIONS ON BOTH SYSTEMS COMPARED TO MAGNETIC COMPASS. FLIGHT DIVERTED MCI LANDED WITHOUT INCIDENT. REPLACED CAPTAIN AND FIRST OFFICER COMPASS INDICATORS. SYSTEM GROUND CHECKED NORMAL OPERATION.
Earlier reports · 1997–2009 · 33 reports
2009
Part: BATTERY PACK — LOOSE (CABIN) · airframe 61,806 hrs · 32,331 cycles
CENTER RIGHT CEILING EMERGENCY LIGHTS INOPERATIVE BETWEEN AFT LAVATORIES. RESEATED BATTERY PACK AT RIGHT LAVATORY. OPS CHECKS NORMAL.
Part: CONNECTOR — LOOSE (CABIN) · airframe 61,806 hrs · 32,331 cycles
SEAT MOUNTED EMERGENCY LIGHT INOP AT SEAT 10D. CONNECTED LOOSE PLUG AT SEAT 10D. OPS CHECKS NORMAL.
Part: STRAP — BROKEN (FLASHLIGHT) · airframe 61,806 hrs · 32,331 cycles
AFT FLASHLIGHT AT AFT JUMPSEAT HAS SECURITY STRAP BROKEN. INSTALLED NEW SECURITY STRAP.
2008
Part: BATTERY — WEAK (EMERGENCY LIGHTS) · airframe 60,013 hrs · 31,302 cycles
BATTERY PACK TESTED DIM, REF- AMM 33-60-98-4. INSTALLED SERVICABLE BATTERY PACK.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,013 hrs · 31,302 cycles
BATTERY PACKS TESTED DIM.
Part: CASTING — CRACKED (RT WING SPOILER) · airframe 60,013 hrs · 31,302 cycles
GROUND SPOILER CASTING CRACKED ON OUTBOARD SIDE ABOVE GROUND SPOILER ACTUATOR FORWARD ATTACH BOLT. REPLACED CASTING.
Part: LIGHT — FAULTY (CABIN) · airframe 60,013 hrs · 31,302 cycles
CABIN EMERGENCY LIGHTS TEST DIM.
2007
Part: SHROUD — MISSING (EMERGENCY LIGHTS)
LAX - EMERGENCY LIGHT AT SEAT 10D MISSING SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 10D. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LENS — MISSING (EMERGENCY LIGHT)
LAX - EMERGENCY LIGHT AT SEAT 10D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 10D. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BULB — MISSING (EMERGENCY LIGHT)
LAX - EMERGENCY LIGHT AT SEAT 10D MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 10D. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
LGA - OVERHEAD EMERGENCY EXIT LIGHTS AT SEAT ROWS 20 TO 34 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY EXIT LIGHTS AT SEAT ROWS 20 TO 34. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: MODULE — INOPERATIVE (EMERGENCY LIGHT)
LGA - OVERHEAD EMERGENCY EXIT LIGHTS AT SEAT ROWS 20 TO 34 INOPERATIVE. REPLACED MODULE FOR OVERHEAD EMERGENCY EXIT LIGHTS AT SEAT ROWS 20 TO 34 . SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: GEARBOX — FAILED (LT ENGINE)
STL INFLIGHT T2491 ORD TO AUS - LEFT ENGINE UNCOMMANDED SHUTDOWN AT FLIGHT LEVEL 340. POSSIBLE FLAMEOUT. LANDED STL WITHOUT INCIDENT. SINGLE ENGINE TIME 12 MINUTES. FOUND CASE DAMAGE AT GEAR BOX MOUNT. REPLACED LEFT ENGINE ON 02JUN AT STL.
2006
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)
LGA - EMERGENCY LIGHTS AT FORWARD GALLEY INOPERATIVE. REPLACED BATTERY PACK AT FORWARD GALLEY FOR INOPERATIVE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)
SFO - OVERHEAD EMERGENCY LIGHT AT ROW 18 INOPERATIVE. REPLACED BATTERY PACK ASSEMBLY AT B5 104 FOR OVERHEAD EMERGENCY LIGHT AT ROW 18. SYSTEM GROUND CHECKED NORMAL OPERATION.
2005
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
SAT - EMERGENCY LIGHTS AT FORWARD ENTRY AND FLIGHT DECK INOPERATIVE. REPLACED BATTERY PACK AT FORWARD ENTRY DOOR CEILING FOR EMERGENCY LIGHTS AT FORWARD ENTRY AND FLIGHT DECK. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: ENGINE — LEAKING (RIGHT)
RIGHT ENGINE OIL QUANTITY WENT TO ZERO. RIGHT OIL PRESSURE STARTED SOEN TO 20 PSI. STAYED AT 20 PSI FOR ONE TO TWO MINUTES THEN WENT TO ZERO. OIL TEMPERATURE WAS NORMAL THE ENTIRE TIME. SHUT DOWN ENGINE PER CHECKLIST. REPLACED RIGHT HAND ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION.
2004
Part: LINE — FAILED (HYD SYSTEM)
RT HYDRAULIC SYSTEM FAILED AFTER LANDING. EMERGENCY DECLARED. REPLACED NR 4 MAIN LANDING GEAR BRAKE LINE AND SERVICED LEFT HAND AND RIGHT HAND HYDRAULIC SYSTEM. PERFORMED ENGINE RUN. SYSTEM GROUND CHECKED NORMAL OPERATION.
2003
Part: BATTERY PACK — DISCHARGED (CABIN)
DURING OVERNIGHT MAINTENANCE, OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT SEAT ROWS 20 THROUGH 25. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING WAS INOPERATIVE AT THE AFT HALF OF THE CABIN. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: WIRE — DAMAGED (EMERGENCY LIGHT)
DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS IN TAILCONE AND SEATS ROWS 21-31 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY, CLEANED CONTACTS, AND REPLACED WIRE FROM SIDEWALL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: DOWNLOCK SENSOR — DEFECTIVE (MLG)
ORD - FLT 854 - EN ROUTE FLL-ORD, ON APPROACH ORD, AFTER PUTTING LANDING GEAR HANDLE DOWN. RGHT GEAR WARNING LIGHT ILLUMINATED. USED MANUAL GEAR EXTENSION TO EXTEND LANDING GEAR. GEAR SHOWED DOWN AND LOCKED. LANDED ORD WITHOUT INCIDENT. REPLACED D1-27 SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2001
Part: APU — LEAKING (APU BAY)
LAX - FLT 2430 - EN ROUTE LAX-DFW, FLIGHT ATTENDANT DETECTED SMOKE IN CABIN AND COCKPIT. RETURNED LAX AND LANDED WITHOUT FURTHER INCIDENT. PRECAUTIONARY REPLACED APU. NO ABNORMAL WEAR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: CLAMP
DFW - FLT 1580 - EN ROUTE DFW-DCA, TAIL HIGH TEMP LIGHT ILLUMINATED. RETURNED DFW LANDED WITHOUT INCIDENT. REPOSITIONED CLAMP ON LEFT PACK ANTI-ICE VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2000
Part: APU — LEAKING (TAIL)
DFW - FLT 441 - IMMEDIATELY AFTER TAKEOFF DFW, A BURNING SMELL IN THE CABIN WAS REPORTED. AIRCRAFT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED APU AND ACCOMPLISHED PACK BURNOUT AND LEAK CHECK. NO SMELL OR SMOKE NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — INOPERATIVE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTS AT SEAT 21D INOPERATIVE. REPLACED EMERGENCY EXIT ESCAPE PATH LIGHT AT SEAT 21D. SYSTEM GROUND CHECK, NORMAL OPERATION. (X)
1999
Part: LONGERON — CORRODED (BS 235-237)
TUL - DEEP CORROSION ON L-30 STA 325 - STA 237. INSTALLED LONGERON SPLICE AT STA 235 ON LONGERON 30 PER ESO 80559 DATED 11-16-99. (X)
Part: CUSP — CORRODED (BS 927-946)
TUL - FOUND CORROSION AROUND LIGHTING HOLES IN LEFT CUSP BETWEEN STATION 927 TO 946. CUTOUT CORRODED SECTION OF LEFT CUSP. INSTALLED REPAIR DOUBLER PER SRM 53-01, FIG 4. (M)
Part: SEAT TRACK — CORRODED (BS 794)
TUL - NR 4 CABIN TIE DOWN TRACK CORRODED AT STATION 794. CUTOUT DAMAGED SECTION OF TRACK. SPLICED IN SECTION PER SRM 53-05 PART 1. (M)
Part: SEAT TRACK — CORRODED (BS 237)
TUL - FOUND NR 4 CABIN TIE DOWN TRACK CORRODED AT STATION 237. CUTOUT DAMAGED AREA IN NR 4 TRACK. INSTALLED PLUG REPAIR PER SRM 53-05 FIG 6A. (M)
Part: CONNECTOR — LOOSE (EMERGENCY EXIT)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT OVERWING EXITS INOPERATIVE. MAINTENANCE FOUND A LOOSE CONNECTOR. RESECURED LOOSE CONNECTOR TO EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1998
Part: AIR DISTRIBUTION — ODOR (CABIN)
DFW - FLT 1684 - DURING TAKEOFF, CREW NOTICED SEWAGE SMELL FOLLOWED BY A BURNING SMELL. FLIGHT AIR INTERRUPTED AND RETURNED DFW AND LANDED OVERWEIGHT WITHOUT INCIDENT. ACCOMPLISHED OVERWEIGHT INSPECTION WITH NO DAMAGE NOTED. PACKS INSPECTED FOR POSSIBLE INGESTION WITH NO INGESTION NOTED. GROUND RAN ENGINES AT POWER UTILIZING BLEED AIR FOR PACK, UNABLE TO DUPLICATE ORDER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1997
Part: FRAME — CRACKED (BS 1309)
TUL - BELT FRAME CRACKED AT STA 1309 L28K UPPER FLANGE. INSTALLED DOUBLER UPPER FLANGE PER AARD 53-10-00-15, SRM 53-01, FIGURE 2. TST, 26,393.34 HOURS. CYCLES, 14,764. (X)