N326FE
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.
16 reports on file, 2004-07-10 – 2005-10-21.
Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 74,592 hrs · 18,258 cycles
UPON CONFIG, A/C ROLLED LEFT REQ 3/4 DEFLECTION TO RIGHT TO HOLD A/C LEVEL. A/C WAS CONTROLLABLE TO TOUCHDOWN. ON POST FLIGHT WALK AROUND, DISCOVERED THAT THE MIDDLE OF THE LEFT OUTBD FLAP VANE HAD DEPARTED THE A/C. REMOVED RT INBD FLAP SPRING CARTRIGDE. REMOVED AND REPLACED LT OB FLAP ASSY AND PERFORMED ADJUSTMENT/TEST IAW UAL DC10-30 MM 27-50-02. INSTALLED INBOARD AND OUTBOARD FLAP VANES ON LT OUTER FLAP, REF UAL M/M 27-50-03. INSTALLED LT OUTBOARD FLAP VANE CARTRIDGE, REF UAL M/M 27-51-04. REMOVED AND REPLACED NR 5 SPOILER PER UAL M/M27-60-01. REMOVED AND REPLACED NR 4 SPOILER PANEL PER M/M 27-60-01.
Earlier reports · 2004 · 15 reports
2004
Part: HINGE BRACKET — DAMAGED (LT OUTBD FLAP) · airframe 72,683 hrs · 17,049 cycles
C/W WITH EA 8-5740-78234 WING LT OTBD FLAP OUTBD HINGE BRACKET, ACT MOUNT HOLES REPAIR P/N ARC0503. COMPLIED WITH EA 8-5740-78234 TO INCLUDE REV A WINGS LT OUTBD FLAP, OUTBD HINGE BRACKET ACTUATOR MOUNT HOLES REPAIR, P/N ARC0503 AT MAE.
Part: SUPPORT — CRACKED (R1 DOOR) · airframe 72,683 hrs · 17,049 cycles
R-1 AFT UPPER CHAIN GUARD BRACKET CRACKED. REMOVED AND REPLACED CHAIN GUARD BRACKET AND CHAIN GUARD IAW MM 52-11-09 AT MAE.
Part: INTERCOSTAL — CORRODED (NLG WW) · corrosion level 2 · airframe 72,683 hrs · 17,049 cycles
NOSE GEAR WHEEL WELL FWD PRESSURE BULKHEAD ACCESS DOOR 115AZ INSIDE BOTTOM CORRODED. REMOVED AND REPLACED INTERCOSTALS IAW SRM 51-31-01 AND SRM 51-35-01 ON N/R N00743 AT MAE.
Part: RIB — CRACKED (ZONE 600) · airframe 72,683 hrs · 17,049 cycles
RIGHT WING I/B LEADING EDGE ACCESS PANEL 616ET SEVERAL RIBS CRACKED. REMOVED CRACKED RIBS AND REPLACED WITH NEW RIBS IAW SRM 51-31-01. PAINTED IAW SRM 51-23-01.
Part: RIB — CRACKED (ZONE 500) · airframe 72,683 hrs · 17,049 cycles
LEFT WING I/B LEADING EDGE ACCESS PANEL 516FE RIB WITH CRACK. REMOVED AND REPLACED STIFFENER IAW SRM 51-35-01.
Part: FRAME — CRACKED (ZONE 400) · airframe 72,683 hrs · 17,049 cycles
NR 2 ENGINE RIGHT CORE COWL FORTH RIB AFT CRACKED JUST ABOVE ACCESS DOOR. REMOVED DOUBLER IAW SRM 51-31-01. RECEIVED FROM WELD SHOP CORE COWLING FRAME WELDED BY TRAVLER T4/445038 AND DPS10-301. INSTALLED DOUBLER STIFFENER AND CLIP IAW SRM 51-33-01 AND SRM 51-31-01.
Part: FITTING — CORRODED (LT OB FLAP) · corrosion level 2 · airframe 72,683 hrs · 17,049 cycles
COMPLY WITH EA 8-5750-79540; WINGS OUTBOARD FLAP, FLAP SPINDLE CARRIAGE SUPPORT FITTING CORROSION REPAIR, P/N ARC2177. COMPLIED WITH EA 8-5750-79540, WINGS OUTBOARD FLAP, FLAP SPINDLE CARRIAGE SUPPORT FITTING CORROSION REPAIR, P/N ARC2177 AT MAE.
Part: PLATE — CORRODED (ZONE 100) · airframe 72,683 hrs · 17,049 cycles
FUSELAGE RT BASE PLATE INBOARD FLAP SUPPORT SURFACE CORROSION REPAIR P/N ANB7170-2. COMPLIED WITH EA 8-5310-80573.
Part: FITTING — CORRODED (ZONE 600) · airframe 72,683 hrs · 17,049 cycles
C/W EA 8-5720-79541 WINGS INBOARD FLAP SIDE LOAD SUPPORT FITTING CORROSION REPAIR P/N ANB7434. COMPLIED WITH EA 8-5720-79541.
Part: FITTING — GOUGED (ZONE 700) · airframe 72,683 hrs · 17,049 cycles
NOSE WHEEL WELL RT OVERHEAD FLIGHT BRAKE FITTING HAS GOUGED AREAS. REMOVED AND REPLACED FITTING IAW DC10-30 M/M 32-42-02-7.
Part: FITTING — CORRODED (ZONE 700) · airframe 72,683 hrs · 17,049 cycles
RIGHT MAIN GEAR DOOR FWD UPPER H-11 BOLT POSITION NR 1 PER DWG ARC2859 HAS GOUGES AND CORROSION. REMOVED FITTING AND FOUND TO BE OUT OF LIMITS. INSTALLED NEW FITTING IAW EO 8-5710-7-5005 AND DWG ARC2859 AND SRM 51-31-01.
Part: FITTING — GOUGED (ZONE 700) · airframe 72,683 hrs · 17,049 cycles
NOSE WHEEL WELL LT OVERHEAD FLIGHT BRAKE FITTING HAS GOUGED AREAS. REMOVED AND REPLACED FITTING IAW DC-10-30 M/M 32-42-02-7.
Part: HINGE — CORRODED (ZONE 600) · airframe 72,683 hrs · 17,049 cycles
C/W EA 8-5740-80575 WINGS RT INBD FLAP OUTBD HINGE UPPER HOLE LUG CORROSION REPAIR P/N ARC0154-2. COMPLIED WITH EA 8-5740-80575.
Part: VANE — GOUGED (LT OB FLAP) · airframe 72,683 hrs · 17,049 cycles
COMPLY WITH EA 8-5710-79550 WINGS REWORK OF GOUGE IN OUTBD FLAP VANE SUPPORT RIB ARB1860-3. COMPLIED WITH EA 8-5710-79550 WINGS REWORK OF GOUGE IN OUTBD FLAP VANE SUPPORT RIB ARB 1860-3 AT MAE.
Part: LATCH — BENT (THRUST REVERSER) · airframe 72,683 hrs · 17,049 cycles
NR 3 ENG LEFT T/R UPPER LATCH ROD IS BENT. REMOVED AND REPLACED UPPER LATCH ROD IAW MM 78-32-19 AND 20-50-02 AT MAE.