N632UP
Registered owner: UNITED PARCEL SERVICE CO, KY (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.
8 reports on file, 2024-10-21 – 2026-08-18.
Part: LIFE VEST — MISSING (ZONE 200) · airframe 17,323 hrs · 2,568 cycles
FO'S LIFEVEST MISSING. INSTALLED LIFEVEST PER MM 25-62-05.
Part: TRUNNION — DAMAGED (ZONE 700) · airframe 16,626 hrs · 2,468 cycles
RIGHT BODY GEAR TRUNION OUTBOARD BUSHING MIGRATING OUT AND APPEARS TO HAVE AXIAL SPLIT AT FORWARD 90 DEGREE POSITION. GA TELESIS REPAIRED MIGRATING BUSHING ON 8130 FORM TRACKING NUMBER WO450757 DOCUMENT ATTACHED. GEAR R & R ON MXP-32-410-90-02-JIC ((RII) RST - RIGHT BODY LANDING GEAR [T3F18E00090U1].
Part: CRASH AXE — CORRODED (ZONE 200) · airframe 16,624 hrs · 2,467 cycles
MCD CRASH AXE DAMAGED/CORRODED. REMOVED DAMAGED CRASH AXE FROM HOLDER. INSTALLED NEW AXE AND SECURED IN HOLDER IAW IPC 25-63-51-33.
Part: ELEVATOR — NOT REPORTED (NOT REPORTED) · airframe 14,532 hrs · 2,159 cycles
ADD SDR FOR EO-85445-JIC2 STEP 137. LT OUTBOARD ELEVATOR FRONT SPAR AND RIB REINFORCEMENT. COMPLETE PER SB 747-55-2069.
Part: ELEVATOR — NOT REPORTED (NOT REPORTED) · airframe 14,532 hrs · 2,159 cycles
ADD SDR FOR EO-85445-JIC1 STEP 137. LT OUTBOARD ELEVATOR FRONT SPAR AND RIB REINFORCEMENT. COMPLETE PER SB 747-55-2069.
Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 13,265 hrs · 1,978 cycles
CAPT EMERG FLASHLIGHT FLASHING RED AT TEST. FLASHLIGHT BATTERY REPLACED IAW AMM 25-60-60-960-801 REV.47. OPERATIONAL TEST OF CAPT FLASHLIGHT PERFORMED IAW AMM 25-60-60-710-801 REV.47. FOUND SATIS.
Part: FMS — FAILED (ZONE 100) · airframe 13,064 hrs · 1,952 cycles
EMERGENCY DECLARED, DURING DESCENT DUAL FMS FAILURE WITH MULTIPLE ADDITIONAL DISCONNECTS, FAILURE MESAAGES .LANDING ALT ADVISORY , FLIGHT CONTROL SYSTEM STS. AP AND AT FAILED BEGAN TO COMPLY WITH FMS NIL STATUS MESSAGE ON ARRIVAL. NIL EXISTING FAULTS IN CMC.MAINT MSG 34738 NOT ACTIVE IN PLF. FMC L AND FMC R CMC GROUND TEST PERFORMED IAW AMM 34-61-00-745-222.TEST PASSED NIL FAULTS.
Part: SKIN — GROUND DAMAGE (ZONE 100) · airframe 10,634 hrs · 1,588 cycles
LOAD CREW STRUCK AIRCRAFT WITH CAN CAUSING PUNCTURE DAMAGE NEAR STA 2020 BETWEEN STRINGERS 38L & 39L. COMPLETED/ VERIFIED ALL STEPS OF EO-91798-REQ1 LISTED ARE C/W. THIS IS A MAJOR REPAIR, CAT B REPAIR. REFEO-91798-REQ1 (SECTION 46 LEFT FUSELAGE SKIN PUNCTURE BETWEEN STA 2020 - 2040 AND S-37L - 38L - CATEGORY B REPAIR)