N322FE

No registry detail on file · not in current registry

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.

19 reports on file, 1995-01-07 – 2004-08-14.

OTHER · 2004-08-14 Unresolved
ATA 2780

Part: FUSE LINK — SHEARED (SLATS) · airframe 93,766 hrs · 24,877 cycles

RT OB SLAT RETAINER MECHANISM MECHANICAL FUSE SHEARED. (REFERENCE MM 27-83-08 PAGE 202 FIGURE 201) REFERENCE NON-ROUTINE 39546.

Source: SDR 2004F00236
OTHER · 2004-08-14 Unresolved
ATA 7830

Part: SLEEVE — CRACKED (THRUST REVERSER) · airframe 93,766 hrs · 24,877 cycles

NR 3 ENGINE IB THRUST REVERSER EXTRUDED TORQUE RING, AT THE LEADING EDGE OF TRANSLATING SLEEVE, CRACKED AROUND FASTENER HOLE AT 10 O'CLOCK (REVERSER DEPLOYED). REFERENCE NON-ROUTINE 39502.

Source: SDR 2004F00237
OTHER · 2004-08-06 Unresolved
ATA 2782

Part: FUSE PIN — SHEARED (DROOP MECHANISM) · airframe 93,766 hrs · 24,877 cycles

RT WING OB SLAT CONTROL MECHANISM HAS ANTI-DROOP FUSE PIN SHEARED. REFERENCE NON-ROUTINE 39501.

Source: SDR 2004FA0000678
OTHER · 2004-08-06 Unresolved
ATA 5341

Part: ATTACH FITTING — CORRODED (WING ROOT) · airframe 93,766 hrs · 24,877 cycles

LOWER AFT WING TO CENTER BOX ATTACH SKATE FITTING IS EXFOLIATED, LT WHEEL WELL, FUSELAGE STATION 1366 TO 1381. REFERENCE NON-ROUTINE NR 39431.

Source: SDR 2004FA0000679
Earlier reports · 1995–2001 · 15 reports

2001

WARNING INDICATION · 2001-03-20 Matched by certificate designator
ATA 3220

Part: PIN — DEFECTIVE (NLG)

NOSE GEAR DID NOT RETRACT ON T/O. REMOVED AND REPLACED NOSE GEAR PIN. AC OK TO CONTINUE.

Source: SDR 01FDEA00218

2000

OTHER · 2000-06-20 Matched by certificate designator
ATA 5320

Part: STIFFENER — CORRODED (BULKHEAD)

SNRM 0327 LOWER AUX FUEL TANK AFT BULKHEAD, LT MOST VERTICAL STIFFNER FOUND WITH CORROSION. R&R PER 51-31-01, 21-11-06-2.

Source: SDR 00FDEA00400
OTHER · 2000-06-20 Matched by certificate designator
ATA 5720

Part: SUPPORT BRACKET — CRACKED (RT WING)

SNRM 0338 RT WING PANEL SUPPORT FOR PANEL NR 618GB WAS CRACKED, LOCATED APPROX 4 INCHES OB OF SLAT DRIVE MECH ACCESS PANEL. R&R PER SRM 51-31-01.

Source: SDR 00FDEA00399
OTHER · 2000-06-19 Matched by certificate designator
ATA 5753

Part: SKIN — CRACKED (TE FLAP)

SNRM 0196 LT WING OB FLAP UPPER SKIN SURFACE FOUND CRACKED APPROX 3 5/32 INCHES. R&R PER SRM 51-31-01, 57-10-00, 57-52-02.

Source: SDR 00FDEA00403
OTHER · 2000-06-19 Matched by certificate designator
ATA 5730

Part: SKIN — CRACKED (LT WING)

SNRM 0222 LT WING L/E LOWER ACCESS PANEL CUTOUT NR 526AB FWD SIDE FOUND CRACKED. R&R PER SRM 51-31-01.

Source: SDR 00FDEA00401
OTHER · 2000-06-19 Matched by certificate designator
ATA 5753

Part: SKIN — CRACKED (TE FLAP)

SNRM 0198 LT WING IB FLAP UPPER SKIN FOUND PATCH REPAIR CRACKED APPOX 6 INCHES. R&R PER CMM 57-52-01.

Source: SDR 00FDEA00402
OTHER · 2000-06-19 Matched by certificate designator
ATA 5320

Part: CHANNEL — CORRODED (FUSELAGE)

SNRM 0252 AFT FUSELAGE WATER TANK BAY STA 1996, FUSELAGE FRAME AFT LWR CHANNEL TOP SURFACE CORRODED, LONGERON 50 RT TO LT. R&R CHANNEL & STRAP PER SRM 53-30-00 FIG 8, VOL 1.

Source: SDR 00FDEA00398

1998

FALSE WARNING · 1998-06-20 Matched by certificate designator
ATA 2621

Part: FIRE BOTTLE — DISCHARGED (NR 2 ENGINE)

ENGINE NR 2, NR 1 BOTTLE LOW PRESSURE LIGHT ILLUMINATING JUST PRIOR TO DEPARTURE. FOUND NR 1 BOTTLE OF APU FIRE EXTINGUISHER SYSTEM HAD DISCHARGED THRU APU PORT (NR 2 ENG FIREX CONTAINER 1). REPLACED NR 2 ENG FIREX CONTAINER 1 PER M/M 26-21-02 AND SQUIB FOR SAME (P/N 876296-2). ALSO, REPLACED DISCHARGE HEAD STRAINER (P/N 260968).

Source: SDR 98FDEA00413
FALSE WARNING · 1998-04-05 Matched by certificate designator
ATA 5230

Part: SLIDER — BROKEN (CARGO DOOR)

SHORT FINAL, LEFT AFT CARGO DOOR LIGHT ON F/E PANEL ILLUM FOLLOWED BY IMMEDIATE PRESSURE DROP IN CABIN. ACFT WAS ALREADY CONFIGURED FOR LANDING, LANDED SUCCESSFULLY, NO FURTHER PROBLEMS. DOOR 4L SWITCH NOT WORKING DUE TO TRACK CAM AND SLIDER BROKEN. REPLACED TRACK CAM AND SLIDER, OPS OK. C/B'S DO NOT POP.

Source: SDR 98FDEA00250

1996

INADEQUATE Q C · 1996-09-16 Matched by certificate designator
ATA 5530

Part: HI-LOCK COLLARS — MISSING (VERT STAB)

SNRM NR 0352, VERTICAL STABILIZER ALL COLLARS MISSING FROM HI-LOCKS BETWEEN AFT H-11 BOLTS THAT ATTACH UPPER VERICAL STABILIZER TO LOWER VERTICAL STABILER. REF LAX C-CH-02, SNRM NR 0352.

Source: SDR 96FDEA01489
OTHER · 1996-09-14 Matched by certificate designator
ATA 5720

Part: TENSION STRAP — CRACKED (RT WING)

SMRM NR 00506, RT WING, O/B FLAP I/B HINGE O/B SIDE TENSION STRAP IS CRACKED AT THE LOWER BOLT HOLE LOWER FLANGE. *S/D* REMOVED AND REPLACED TENSION STRAP BRACKET AS PER SRM 51-00-01 VOL NR I.

Source: SDR 96FDEA01490
INFLIGHT SEPARATION · 1996-09-04 Matched by certificate designator
ATA 5400

Part: V-PANEL — MISSING (NR 3 PYLON)

UPON WALK AROUND, FOUND THE V-PANEL ON NR 3 ENGINE PYLON RIPPED AWAY. INSTALLED V-PANEL ON PYLON FARING. ALSO, REPAIRED DAMAGED PYLON FARING HONEYCOMB PANEL OUTBOARD PER DC-10 STRUCTURE REPAIR MANUAL 51-10-00.

Source: SDR 96FDEA01435

1995

WARNING INDICATION · 1995-09-26 Matched by certificate designator
ATA 7530

Part: DUCT — FAILED (NR 1 ENGINE)

DURING T/O ROLL, NR 1 ENG N1 IND DROPPED APPROX 10 PERCENT. ADJUSTED THROTTLE TO MATCH N2 AND FUEL FLOW, NO CHANGE NOTED IN N1, EGT IND 910 DEGREES, APPROX 50 DEGREES HIGHER THAN ENG NR 2 AND NR 3. AT APPROX 300 FEET NR 1 FIRE WARNING AND BELL RECEIVED. ACCOMP EMERGENCY CHECKLIST, DUMPED FUEL, DECLARED EMERGENCY AND RETURNED TO ANC. MX DISCOVERED THE 14TH STAGE CROSSOVER DUCT FAILED AND IT WAS REPLACED ALONG WITH BOTH REVERSER HALVES. ALSO, REPLACED WERE 2 FUEL NOZZLE TUBES.

Source: SDR 95FDEA01428
FALSE WARNING · 1995-03-10 Matched by certificate designator
ATA 2612

Part: FIRE WARNING — MALFUNCTIONED (APU)

THE APU FIRE LIGHT ILLUMINATED INTERMITTENTLY DURING FLIGHT. IT ALSO ILLUMINATED DURING TAKEOFF OUT OF MEM. FOUND APU FIRE LIGHT ASSY RETAINER PIN MISALIGNED, REMOVED AND REPLACED LIGHT ASSY. OPS CKD GOOD.

Source: SDR 95FDEA00214
WARNING INDICATION; OVER TEMP · 1995-01-07 Matched by certificate designator
ATA 3610

Part: DUCT — FAILED (14TH STAGE)

ENG FIRE IN NR 2 ENG SHORTLY AFTER ROTATION. OBSERVED EGT REACHED 899 DEG. MEMORY ITEMS ACCOMP, CKLT PROCED COMPLIED WITH, RETURNED TO OAK FOR UNEVENTFUL LANDING (FIRE HANDLE PULLED, BOTTLE NOT DISCHARGED). REPLACED 14TH STAGE LWR CROSSOVER DUCT, LPT COOLING MANIFOLD RIGHT SIDE. REPLACED B, C AND D OIL SUMP SCAVENGE TUBES. REPLACED PYLON DRAW TUBES 3 FWD STRUTS AND 2 AFT STRUTS.

Source: SDR 95FDEA00005