UNITED PARCEL SERVICE CO.
Also recorded as: UNITED PARCEL SERVICE CO, UNITED PARCEL SERVICE CO.
Accident & enforcement record
Events that happened, regardless of the operator's own reporting. Each links to its public source.
NTSB accidents & incidents
Operated by UNITED PARCEL SERVICE CO (per NTSB report)
Not yet finalized — may be revised.Operated by United Parcel Service Co (per NTSB report)
Operated by UNITED PARCEL SERVICE CO (per NTSB report)
Operated by UNITED PARCEL SERVICE CO (per NTSB report)
Operated by UNITED PARCEL SERVICE CO (per NTSB report)
Operated by UNITED PARCEL SERVICE CO (per NTSB report)
Operated by United Parcel Service Company (per NTSB report)
Operated by UNITED PARCEL SERVICE CO (per NTSB report)
FAA enforcement actions
FAA enforcement records haven't been loaded into GroundCheck yet, so none can be shown — a gap in our data, not evidence of a clean enforcement history.
Maintenance disclosure history
Service Difficulty Reports are self-reported maintenance findings. The NUMBER of reports is not a measure of reliability — diligent operators file more, not fewer. These are shown for transparency, not as a negative signal.
73,199 reports on file — showing most recent 50.
AIR TURN BACK, GEAR DISAGREE EICAS MSG AND GEAR LIGHT PRESENT AFTER T/O. ATB AS DIRECTED BY FLIGHT CONTROL. GEAR OPERATED NORMALLY DURING EXTENSION. FOUND FAULT S10065 AND S10078 ON PSEU. C/W OPS OF PSEU IAW AMM 32-61-03. OPS CHECK GOOD. LUBRICATED NLG LOCK ACTUATOR AND LOCK MECHANISM IAW AMM 12-21-12. RETRACTED AND EXTEND NLG IAW 32-34-00. NO FAULTS NOTED AT THIS TIME.
MAIN DECK CRASH AXE FOUND DAMAGED/CORRODED REINSTALLED CRASH AXE INTO HOLDER ON MAIN CARGO DECK IAW AMM 25-60-00.
PASSING BELOW 4000 ON ARRIVAL STRONG ODOR OF DIRTY SOCKS. CLEARED CONTAMINATION PER AMM 21-00-01. RAN APU AND RIGHT ENGINE.
MAJOR REPAIR, FOUND MAIN DECK FLOOR PANEL DAMAGE , P/N : 145T5876-81 PANEL NO : 241MFF.
NR 1 ENG INLET COWL LIP CRACKED BETWEEN 11 AND 1 O'CLOCK POSITIONS REMOVED #1 ENGINE INLET IAW AMM 71-11-01
AERODYNAMIC SEAL BROKEN, FWD LH ENTRY DOOR (REPLACE) 1. I.A.W AMM 52-12-01-004-001 REV. 148 REMOVE CREW ENTRY DOOR.
FOUND NO.1 ENTRY DOOR LOWER SEAL DAMAGED
RIGHT SIDE BEHIND FIRST OFFICER, OBSERVER LIFE VEST MISSING. RIGHT FO CONSOL LIFE VEST INSTALLED REF AMM 25-64-00
EMERGENCY DECLARED, FLAP INDICATOR DISAGREE ,RAN QRH CHECKLIST.RT TE PLAP INDICATOR EVENTUALLY UNSTUCK REMOVED AND REPLACED FLAP INDICATOR AS PER AMM 27-58-02, OPS TEST OK
SMALL EMERGENCY EXIT LIGHT IN LAV INOP IN THE ALWAYS ON LOW POSITION. SMALL RECTANGLE LIGHT. RELAMPED LAV AUX/MIRROR LIGHT PER 33-51-21. OPS CHECK GOOD
SMALL LIGHT IN LAV INOP.
NR 1 ENG INLET COWL LIP CRACKED BETWEEN 11 AND 1 O'CLOCK POSITIONS. INSTALLED NR 1 ENGINE INLET COWL IAW AMM 71-11-01.
SMALL LIGHT IN LAV INOP. FOUND SMALL AUX LAV LIGHT TO BE OPERATIONAL WHEN DOOR IS LOCKED. IAW AMM 33-51-21
CRACK - WEDGE, RT WING OUTBD FLAP INBD WEDGE. IAW SREO-70175-REQ001 REV.1 PERFORM REPAIR AS BELOW STEP. REMOVED THE CRACK MATERIALS AND CLEANED. MEASURE THE DAMAGE AREA ( L : 0.5", W : 0.2", D : 2 PLIES, 6.6" FROM AFT EDGE, AT INBD EDGE ). BOND THE REPAIR PLIES WITH RESIN CURED AT 200 F FOR 220 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG. CONDITION CHECK IS SATISFACTORY.
FOUND CRACK - ANGLE, BULK CGO COMPT CEILING AREA, STA 1577 LBL 74 OUTBD SIDE. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G REV. 95. INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G REV. 95 AND DWG 146T5650 SH. 5 REV. C. JOB COMPLETED.
FOUND CRACKED ANGLE, BULK CARGO COMPT CEILING AREA, STA 1577 LBL 74 INBD SIDE. MAIN DECK CARGO FLOOR PANEL AND DADO PANEL OK TO INSTALL CHECK OK
FOUND MAIN DECK DOORWAY LINING BROKEN TTL:1AREA.
DISCONECT EMERGENCY LIGHT ELECTRICAL WIRES FROM CREW DOOR SURROUND PANEL
FOUND RT WING OTBD FLAP SUPPORT STRUT LOWER INSERT, COVE ATTACH WORN OUT , WBL 695. PERFORMED NDT/UT FOR THE REWORKED AREA & PLUS 2" AROUND HEATED AREA , IAW NDT MANUAL PART 1 51-01-01 REV:182. NO DEFECT WAS FOUND
CRACKED PANEL, LT WING L/E NO.1 SLAT LOWER SURFACE INBD CLOSURE PNL. IAW NDT MANUAL PART 1, 51-01-01 & PART 4, 51-00-03, REV.144 TO PERFORM NDT/UT FOR THE POST REPAIRED AREA INCLUDED THE AREA WAS HOT PLUS WITHIN 6" ALL AROUND. RESULT: NO DEFECT FOUND.
FOUND THE CREW ENTRY DOOR AFT DOORWAY LINING SEAL BROKEN.
MDC FR 24 FLOOR PNL 232SG SEAT TRACK EVIDENCE OF CORROSION. CORROSION WAS FOUND ON THE MAIN DECK CARGO CLS ADAPTER BETWEEN FR26 & FR27 Y0 RH. AFTER FURTHER EVALUATION, EXFOLIATION CORROSION WAS IDENTIFIED. DAMAGE WAS FOUND OUTSIDE LIMITS IAW SRM 53-10-15-101
FOUND MAIN DECK SIDE CARGO DOOR SAFETY NET FRAYED. (REPLACE)
THE BUMPER IS MISSING FROM THE CREW ENTRY DOORWAY LINING.
FOUND THE CREW ENTRY DOOR FORWARD DOORWAY SEAL MISSING.
LEFT PILOTS DV WINDOW IS SCRATCHED. WHEN TURNING LEFT INTO PARKING SPOT & SUN HITTING DIRECTLY ON WINDOW MARSHALER COULD NOT BE SEEN. REMOVED CAPTAINS L2 WINDOW PER AMM 56-11-02-004-001.
MAIN ENTRY DOOR LATCH UNABLE TO LOCK. PERFORMED OPERATIONAL TEST OF CREW ENTRY DOOR REF AMM 52-11-00. OPS CHECKED GOOD. DOOR CLOSES AND LOCKS AS INTENDED
(APG) RT AFT TRUNNION SUPPORT FITTING BEARING ASSY INSIDE HOUSING HAS CORROSION PRODUCTION AUDIT C/W
(APG) L/H AFT TRUNNION SUPPORT FITTING BEARING ASSY INSIDE HOUSING HAS CORROSION PRODUCTION AUDIT C/W
LEFT PILOTS DV WINDOW IS SCRATCHED. WHEN TURNING LEFT INTO PARKING SPOT & SUN HITTING DIRECTLY ON WINDOW MARSHALER COULD NOT BE SEEN. C/W RII IAW GMM 04-02 REMOVED AND REPLACED CAPTAINS SIDE #2 WINDOW PER AMM 56-11-02, OPS CHECK AND LEAK CHECKS GOOD.
THE BUMPER IS MISSING FROM THE CREW ENTRY DOORWAY LINING. (REPLACE) INSTALL THE BUMPER IS FROM THE CREW ENTRY DOORWAY LINING. IAW PSDL 411T2240 SH DL REV.A AND DWG 411T2036 SH1 REV.H.
FOUND FLOOR SUPPORT CORROSION IN THE AREA AFT OF BULK CARGO COMPARTMENT AT BS 1588 LBL 33. REMOVED DAMAGE ANGLE IAW SRM 51-40-02-0G REV. 95.
MAIN CABIN DOOR HARD TO CLOSE. FLIGHT CREW NOTED TO MX UPON ARRIVAL THAT THE L1 DOOR FUNCTIONS NORMALLY. OPENED & CLOSED L1 DOOR NUMEROUS TIMES PER A300 AMM 52-10-00. NO ABNORMAL RESISTANCE NOTED. ARMED & DISARMED SLIDE MULTIPLE TIMES PER A300 AMM 52-73-00. NO ABNORMAL RESISTANCE NOTED. VERIFIED DOOR SLIDE & OPEN/CLOSE INDICATIONS OPERATE PROPERLY PER A300 AMM 52-71-00. ALL INDICATIONS OPERATE CORRECTLY. THIS CLEARS MEL. PLACARD REMOVED.
THE PAWL BEHIND THE CREW ENTRY DOOR EXTERNAL HANDLE IS WORN.
FOUND NR 1 MAIN ENTRY DOOR ROTARY SNUBBER OUT OF LIMITS.
WHILE EVALUATING CORROSION AT APU INLET SURROUND STRUCTURE FOUND CORROSION AT APU INLET AFT STRAP AT STA 1825 BETWEEN STR 3R-6R. ATA 49-11 OKAY TO FABRICATE PER DOCUMENTS AND GMM RII 04-02
CREW ENTRANCE DOOR FWD EDGE UPPER AND LOWER LATCHES BARE METAL EXPOSED.
LEFT UPPER FWD FUSELAGE CREW ENTRANCE DOOR FWD EDGE UPPER LATCH GOUGED AT INNER SIDE.
CHAFING - BRACKET , NR 1 ENG LT CORE COWL SUPPORT ROD SUPPORT FITTING. (REPLACE). INSTALLED NEW BRACKET I.A.W SRM 51-40-02-0G REV.107 AND GOODRICH CMM IPL 71-13-23 REV.47. REVIEWED TASK PER GMM-MTX 09.05.01.09.
AFT OF BULK CARGO COMPARTMENT, DECK PLATE FLOOR STRUCTURE SUPPORT ANGLE ASSY HAS CORROSION ON NUT PLATE STRAP APPROX AT BS 1715, LBL 12,
AFT OF BULK CARGO COMPARTMENT, DECK PLATE FLOOR STRUCTURE SUPPORT ANGLE ASSY HAS CORROSION ON NUT PLATE STRAP APPROX AT BS 1715, LBL 24, ID STICKER NUM. (085-006) ATA 53-20. .INSP. VERIFIED STEP 13.
AFT OF BULK CARGO COMPARTMENT, DECK PLATE FLOOR STRUCTURE SUPPORT ANGLE ASSY HAS CORROSION ON NUT PLATE STRAP APPROX AT BS 1715, LBL 36,
LH FWD UPPER FUSELAGE CREW DOOR CUTOUT AFT EDGE BULB SEAL TORN.
DEBONDED SKIN, LOWER FACE OF LT WING NR 3 FLAP TRACK AFT FAIRING. PERFORMED NDT/UT FOR THE REWORKED AREA & PLUS 2" AROUND HEATED AREA , NDT MANUAL PART 1 51-01-01 REV:182. NO DEFECT WAS FOUND.
CHAFING- EDGE, NR 2 ENG RT T/R LOWER FORWARD DOOR AFT SIDE. (REPLACE) PAPER FINAL CHECK COMPLETED
AIR TURN BACK. EMERGENCY DECLARED, LOAD SHED ISLN BUSS TIE 1, 3, 4 ALL OFFLINE ONLY NR 2 BUSS TIE CLOSE, EICAS MESSAGES FOR ALL LOAD SHED. ATB 24:00 FOR PAN PAN. ELEC GEN SYS 2, ADVISORY MESSAGE 24261 DISPLAYED, FIM TASK 24-11-00-810-805 (GCU & IDG REPLACEMENT), SO R/R ENG2 IDG PER 24-11-01/401, ACFT STILL HAVING ELEC GEN 2 OFF MSG ON, NEED MORE T/S. CONFIRMED ENG 1, 3, AND 4 GENS ARE FUNCTIONING WITH ENG 2 DISCONNECTED.
EMERGENCY LIGHTS BATTERY DEPLETED. EMERGENCY LIGHTS BATTERY REPLACED BY SERVICEABLE. IAW AMM 33-51-07/401 REV 148. OPERATIONAL TEST C/O O.K.
RIGHT WING TO BODY OVER WING BRACKET HAS SIGNS OF CORROSION. VERIFIED ITEM STILL CORRODED AFTER CLEAN UP. FOR STEP 3 ITEM OUT OF LIMITS PER DOCUMENTS.
RIGHT WING TO BODY OVER WING BRACKET HAS SIGNS OF CORROSION. VERIFIED ITEM STILL CORRODED AFTER CLEAN. ITEM OUT OF LIMITS. PER DOCUMENTS ON STEP 3.
AFT CARGO COMPARTMENT FLOOR STRUCTURE SIDE PANEL HAS CORROSION ON MULTIPLE AREAS, APPROX BTW BS 1410 AND BS 1530, LBL 16.10 THRU LBL 25,
Linked aircraft
| N-number | Make / model | Year | Status | Link basis |
|---|---|---|---|---|
| N137UP | AIRBUS INDUSTRIE A300 F4-622R | 2001 | Valid Registration | Operator named in NTSB report |
| N155UP | — | — | Operator named in NTSB report | |
| N162UP | AIRBUS A300 F4-622R | 2005 | Valid Registration | Operator named in NTSB report |
| N173UP | AIRBUS A300 F4-622R | 2006 | Valid Registration | Operator named in NTSB report |
| N259UP | — | — | Operator named in NTSB report | |
| N270UP | — | — | Operator named in NTSB report | |
| N296UP | — | — | Operator named in NTSB report | |
| N305UP | BOEING 767-34AF | 1995 | Valid Registration | Operator named in NTSB report |
| N323UP | BOEING 767-34AF | 1997 | Valid Registration | Operator named in NTSB report |
| N324UP | BOEING 767-34AF | 1998 | Valid Registration | Operator named in NTSB report |
| N342UP | BOEING 767-34AF | 2011 | Valid Registration | Operator named in NTSB report |
| N370UP | BOEING 767-300F | 2020 | Valid Registration | Operator named in NTSB report |
| N571UP | — | — | Operator named in NTSB report | |
| N573UP | BOEING 747-44AF | 2008 | Valid Registration | Operator named in NTSB report |
| N578UP | BOEING 747-45E | 1993 | Valid Registration | Operator named in NTSB report |
| N624UP | BOEING 747-8F | 2020 | Valid Registration | Operator named in NTSB report |