N370UP
Registered owner: UNITED PARCEL SERVICE CO, KY (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| UNITED PARCEL SERVICE CO. (IPXA) | Operator | on 2023-02-04 | Operator named in NTSB report |
Accident & incident history
Operated by UNITED PARCEL SERVICE CO (per NTSB report)
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.
26 reports on file, 2020-07-13 – 2026-03-17.
Part: UNKNOWN — ODOR (COCKPIT/CARGO) · airframe 13,083 hrs · 5,293 cycles
STRONG ODOR IN FLIGHT DECK. EVEN STRONGER ODOR IN CARGO BAY, CREW NOTICED PHYSIOLOGICAL EFFECTS.
Part: UNKNOWN — ODOR (CABIN) · airframe 13,091 hrs · 5,298 cycles
STRONG ODOR IN FLIGHT DECK. EVEN STRONGER ODORIN CARGO BAY (MCD) CREW NOTICED PHYSIOLOGICAL EFFECTS. CLEANED AND DISINFECTED FLIGHT DECK AND MAIN CARGO DECK BY ACFT MAINTENANCE AND AN OUTSIDE VENDOR TO REMOVE ODER REF 767 M/M 25-00-00 107-001. OK FOR CONTINUED SERVICE
Part: UNKNOWN — ODOR (COCKPIT) · airframe 13,083 hrs · 5,293 cycles
AIRCRAFT HAS BEEN SERVICED 3 TIMES FOR A STRONG ODOR IN THE COCKPIT. MECHANIC ON ARRIVAL YESTERDAY SMELLED IT OUTSIDE. LAV FUNCTIONS NORMALLY. LOAD CREW COULD SMELL IN THE MAIN DECK. LAV SERVICED. INSPECTED CABIN AND MAIN DECK. REF: AMM 05-41-02. INSPECTED E&E AND LOWER CARGOS PER 05-41-01. INSPECTED PACK BAY AND OPERATED PACKS PER AMM 21-00-00. PACK BAY CLEAN AND NO SMELL COMING FROM PACKS. SMELL SEEMS TO ORIGINATE FROM BACK OF MAIN CARGO DECK AROUND POSITION 12 AND 13. MOC NOTIFIED. AIRCRAFT OK FOR SERVICE.
Part: RUB STRIP — GOUGED (ZONE 400) · airframe 13,008 hrs · 5,266 cycles
GOUGED WEAR STRIP, NR 2 ENG RT CORE COWL T/E INNER SIDE UPPER PLATE. INSTALLED A NEW WEAR STRIP IAW SRM 51-40-02-0G, REV 94 AND CMM IPL 71-13-24 REV.50.
Part: RUB STRIP — CHAFED (ZONE 400) · airframe 13,008 hrs · 5,266 cycles
CHAFED WEAR STRIP, NR 1 ENG LT CORE COWL INNER FACE T/E UPPER SIDE. INSTALLED A NEW WEAR STRIP IAW SRM 51-40-02-0G, REV 94 AND CMM IPL 71-13-23 REV.47.
Part: LATCH — WORN (ZONE 400) · airframe 13,008 hrs · 5,266 cycles
WORN OUT - LATCH 3 EA, NO.1 ENG R/H FAN COWL OIL TANK ACCESS DOOR. (REPLACE). INSTALL NEW LATCH I.A.W SRM 51-40-02-0G REV.94 AND BOEING AIPC 71-11-10-51 REV. 141.
Part: ANGLE — CRACKED (ZONE 400) · airframe 13,008 hrs · 5,266 cycles
CRACK - ANGLE, NO.2 PYLON AFT FAIRING AFT BULKHEAD L/H AFT SIDE. (REPLACE). INSTALL NEW CLIP I.A.W SRM 51-40-02-0G REV.94 AND BOEING DWG NO. 313T2303 SH 166 REV: - AND 313T2303 SH 161 REV -.
Part: SPRING — BROKEN (ZONE 400) · airframe 13,008 hrs · 5,266 cycles
BROKEN SPRING, NR 2 PYLON AFT FAIRING PANEL 446CL. INSTALLED A NEW SEAL STRIP IAW SRM 51-40-02-0G, REV 94, AND DWG 311T2570, SHT 16, REV -.
Part: BRACKET — CRACKED (ZONE 400) · airframe 13,008 hrs · 5,266 cycles
FAULT - CRACK - BRACKET, NO.1 PYLON HYDRAULIC RESERVOIR VENT TUBE AT CENTER AREA. (REPLACE). FABRICATE BRACKET (P/N:313T2380-836) PER BOEING DWG NO.:313T2380 SH 105 REV."-";PL 313T2380-836 REV."A" AND ORIGINAL PART AS A SAMPLE I.A.W GMM-MTX CH 9.08 REV: 14 REQUIREMENT. INSTALL FABRICATE BRACKET I.A.W SRM 51-40-02-0G REV.94 AND BOEING DWG NO. 313T2380 SH 198 REV: - REVIEW COMPLETE
Part: DOOR — GOUGED (ZONE 400) · airframe 13,008 hrs · 5,266 cycles
GOUGE - PLATE, NO.2 ENG R/H T/R COWL LOWER BLOWOUT DOOR L/E. (REPLACE). INSTALL BLOWOUT DOOR I.A.W SRM 51-40-02-0G REV.94 AND BOEING AIPC 78-31-51-03 REV. 141 AND ST ENGINEERING IPC 78-32-22 REV.94.
Part: ANGLE — CRACKED (ZONE 100) · airframe 13,008 hrs · 5,266 cycles
FAULT - FOUND THE ANGLE CRACK AT STA 1578 RBL 80 INBOARD IN BULK CARGO COMPARTMENT RIGHT AREA. (REPLACE). I.A.W SRM 51-40-02-0G REV. 94 AND BOEING DWG NO.146T5650 SH.5 REV.C INSTALLED NEW ANGLE. REVIEW COMPLETE
Part: ANGLE — CRACKED (ZONE 100) · airframe 13,008 hrs · 5,266 cycles
FAULT - FOUND THE ANGLE CRACK AT STA 1578 LBL 80 INBOARD IN BULK CARGO COMPARTMENT LEFT AREA. (REPLACE). I.A.W SRM 51-40-02-0G REV. 94 AND BOEING DWG NO.146T5650 SH.5 REV.C INSTALLED NEW ANGLE. REVIEW COMPLETE
Part: ANGLE — CRACKED (ZONE 100) · airframe 13,008 hrs · 5,266 cycles
FOUND THE ANGLE CRACK AT STA 1578 LBL 80 OUTBOARD IN BULK CARGO COMPARTMENT LEFT AREA. (REPLACE). I.A.W SRM 51-40-02-0G REV. 94 AND BOEING DWG NO.146T5650 SH.5 REV.C INSTALLED NEW ANGLE.
Part: ANGLE — CRACKED (ZONE 100) · airframe 13,008 hrs · 5,266 cycles
FOUND THE ANGLE CRACK AT STA 1578 RBL 80 OUTBOARD IN BULK CARGO COMPARTMENT RIGHT AREA. (REPLACE). I.A.W SRM 51-40-02-0G REV. 94 AND BOEING DWG NO.146T5650 SH.5 REV.C INSTALLED NEW ANGLE.
Part: FORMER — CRACKED (ZONE 500) · airframe 13,008 hrs · 5,266 cycles
CRACK-FORMER, FWD SIDE OF L/H WING OUTBD L/E NOSE BEAM, OSS 717.29 (REPLACE). INSTALL NEW NOSE FORMER IAW SRM 51-40-02-0G REV.94 AND BOEING DWG NO. 114T2164 SH 6 REV - AND UPS EO-96624-REQ1 REV1 .
Part: DOOR — BROKEN (ZONE 500) · airframe 13,008 hrs · 5,266 cycles
BROKEN PANEL, LOWER FACE OF LT WING NR 3 SLAT OTBD SEAL DOOR. INSTALL NEW SEAL DOOR IAW SRM 51-40-02-0G, REV 94, AND AIPC 57-41-51-15 REV. 141.
Earlier reports · 2020–2025 · 10 reports
2025
Part: SKIN — DENTED (NR 4 SLAT) · airframe 13,008 hrs · 5,266 cycles
MAJOR REPAIR, NR 4 LEADING EDGE SLAT TRAILING EDGE WEDGE HAS MULTIPLE HAIL DENTS. MULTIPLE DENTS ON UPPER SURFACE OF NR 4 SLAT TRAILING EDGE WEDGE EXCEPT DENT 132,133 AND 134, LEAVE THE CONDITION AS-IS IAW EGAT EI NR 2026A57M-370 REV.0 AND EO-92826-REQ3, REV 12. CONDITION CHECK IS SATISFACTORY. ATTACHMENTS ARE UPLOADED. CLOSE DMI NR 2836936.
Part: SKIN — DENTED (NR 5 SLAT) · airframe 13,008 hrs · 5,266 cycles
MAJOR REPAIR, NR 5 LEADING EDGE SLAT TRAILING EDGE WEDGE HAS MULTIPLE HAIL DENTS. NR 5 LEADING EDGE SLAT TRAILING EDGE WEDGE HAS MULTIPLE HAIL DENTS. MULTIPLE DENTS ON UPPER SURFACE OF NR 5 SLAT T/E WEDGE EXCEPT DENT 95, LEAVE THE CONDITION AS-IS IAW EGAT EI 2026A57M-372 REV.0 AND EO-92827-REQ3 REV.1 CONDITION CHECK IS SATISFACTORY. ATTACHMENTS ARE UPLOADED. CLOSE DMI NR 2836937.
2024
Part: DRAIN — DAMAGED (FUSELAGE) · airframe 8,899 hrs · 3,463 cycles
FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R
2023
Part: UNKNOWN — FAILED · airframe 8,434 hrs · 3,269 cycles
*DIVERSION* ENROUTE AT FL350 ISFD FAILED.SCREEN WENT BLANK/DARK. DIVERTED TO KSDF R/R ISFD IAW MM-34-24-03-410-010. GROUND OPS CK NORMAL. OK FOR SERVICE.
2022
Part: VALVE — FAULTED (ENGING FUEL) · airframe 5,637 hrs · 2,221 cycles
INSPECTION TYPE:ETOPR ENG FUEL VALVE EICAS MSG. ENG VALVE LT ON PEDESTAL ILLUM.RAN R ENG PER FIM 76-11-00-815-808-H00. MSG CLEARED. ACFT OK TO COTINUE.
Part: EEC — FAULTED (POWERPLANT) · airframe 4,568 hrs · 1,836 cycles
INSPECTION TYPE:ETOP**ETOPS FILED OPEN** R ENG EEC C1 STATUS MESSAGE DISPLAYED. MSG ASSOCIATED WTH ABOVE MEL 73-21-3-2 FUEL SHUTOFF VALVE RT ENG. MSG CLEARED.
Part: NONE — NONE (LOWER SKIN PNL) · airframe 4,467 hrs · 1,805 cycles
INSPECTION TYPE:C1MULTIPLE DENTS AT THE LOWER SKIN PANEL OF THE RH WING OUTBOARD FLAP.REPAIR I.A.W BOEING SR 4-5430984791 AND UPS EO B767-5730-83126-A.
2021
Part: WINDOW — ARCED (COCKPIT L2) · airframe 3,704 hrs · 1,494 cycles
DIVERSION, NO EMERGENCY DECLARED, AT FL360, L2 WINDOW BEGAN ARCING ALONG ENTIRE BOTTOM AND APPEARED TO CATCH FIRE IN ONE AREA. REMOVED POWER AND FOUND WINDOW CRACKED AND DEFORMED.REMOVED AND REPLACED L2 WINDOW. IAW MM CHT 56-11-02-401. OP'S,LK CK AND PRESSURE CK'S GOOD. P/N ON/OFF 141T4835-97, S/N 15135H2901, 19213H2010. IPC 56-11-02-10E ITEM 017M
2020
Part: A/C PACK — ODOR (FLIGHT DECK) · airframe 1,003 hrs · 400 cycles
ON DECENT BETWEEN 10,000 AND 8000 FEET ENCOUNTERED DIRTY WATER SOCK SMELL FROM AIR CONDITIONING.RAN BOTH PACKS FOR 1 HOUR IAW AMM 21- 00-00-862-001. NO ODOR DETECTED, COULD NOT DUPLICATE MALFUNCTION. OK TO CONTINUE.
Part: CIRCUIT CARD — FAULTY (FIRE WARNING) · airframe 837 hrs · 322 cycles
INSPECTION TYPE:N/A ATB - EMERGENCY DECLARED WHEEL WELL FIRE LIGHT AND EICAS MESSAGE SHORTLY AFTER GEAR RETRACTION. RAN QRH PROCEDURE LIGHT REMAINED ON FOR ABOUT 10-15 MINUTES THEN WENT OUTT/S PER FIM 26-17-815-803, FIG 1, SHT B, BLK 7 NO FAULTS NOTED. CONTINUED T/S BY ACCOMPLISHING FIM 26-17-815-803, FIG 1 SHT 6, BLK 15 AND BLK 31. ALL DETECTOR ELEMENT RESISTANCE FELL W/IN LIMITS. REPLACED DUCT LEAK & WW FIRE CARD, M691, IN THE P54 PNL REF 26-10-01. OPS CK GOOD AT THIS TIME.