N362UP
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.
48 reports on file, 2018-07-12 – 2026-08-05.
Part: BUSHING — MIGRATED (NR 7 SPOILER) · airframe 57,187 hrs · 20,803 cycles
NR 7 SPOILER ACTUATOR , ROD END BOLT BEARING MIGRATION. REPLACED. IAW CMM:57-70-11 REV.43 REPAIR:2-1 PAGE:601 STEP:3, COMPLETED NEW BUSHING REPLACEMENT OF THE NO.7 SPOILER ACTUATOR ROD END.
Part: BUSHING — MIGRATED (ZONE 500 SPOILER) · airframe 57,187 hrs · 20,803 cycles
MIGRATION - BUSHING , LT WING T/E OTBD SPOILER NR 1 UPPER. I.A.W AMM 27-61-02-024-001 REV.148 DISCONNECT LT WING NR 1 SPOILER PCA ROD END. IAW CMM 57-70-51, REV.38, REPAIR 2-1, PAGE 601, STEP 2, COMPLETED NEW BUSHING REPLACEMENT OF THE NR 1 SPOILER ACTUATOR ROD END.
Part: CAP — CRACKED (ZONE 500) · airframe 57,187 hrs · 20,803 cycles
CRACK CAP , L/H WING T/E OUTBD FLAP INBD END CAP. (REPAIR). I.A.W UPS SREO-70175-REQ001 REV. 1 PERFORM REPAIR AS BELOW. REMOVED THE CRACKED MATERIALS AND CLEANED. MEASURED DAMAGE AREA ( L : 1.1", W : 0.1", 6.5" FROM AFT EDGE , AT INBD EDGE ). BOND THE REPAIR PLIES WITH RESIN CURED CONDITION CHECK IS SATISFACTORY.
Part: BRACKET — CHAFED (ZONE 400) · airframe 57,187 hrs · 20,803 cycles
CHAFED BRACKET, NR 1 ENG LT LOWER T/R COWL FWD CLOSURE DOOR T/E ATTACHED. REMOVED DAMAGE BRACKET IAW SRM 51-40-02-0G, REV 55. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV.55, AND IPC 78-32-21 REV.96.
Part: WEDGE — DAMAGED (ZONE 500 FLAP) · airframe 57,187 hrs · 20,803 cycles
RIGHT OUTBOARD FLAP, INBOARD T/E WEDGE UPPER AND LOWER SKIN DAMAGE. (REPAIR). I.A.W UPS SREO-70175-REQ001 REV. 1 PERFORM REPAIR AS BELOW. REMOVED THE CRACK MATERIALS AND CLEANED. MEASURE THE DAMAGE AREA ( L : 0.8", W : 0.05", 6" FROM AFT EDGE , AT INBD EDGE ). BOND THE REPAIR PLIES WITH RESIN CURED. CONDITION CHECK IS SATISFACTORY.
Part: BRACKET — CHAFED (ZONE 400) · airframe 57,187 hrs · 20,803 cycles
CHAFED BRACKET , NR 1 ENG RT T/R COWL LOWER FWD CLOSURE DOOR T/E ATTACHED. REMOVED DAMAGE BRACKET IAW SRM 51-40-02-0G, REV.55. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV.55 AND IPC 78-32-22, REV 96.
Part: ANGLE — CRACKED (ZONE 100) · airframe 57,187 hrs · 20,803 cycles
CRACK-ANGLE, BULK CGO OVERHEAD M/D FLOOR BEAM STRUCTURE ATTACHED AT STA 1580 , ADJACENT RBL 70 AREA.(REPLACE) ACCOMPLISHED JOB I.A.W UPS EO-98247-REQ1 REV 1 AND SRM 51-40-02-0G REV.55 AND BOEING DWG:657T1332 SHEET 5 REV: A.
Part: PLATE — WORN (ZONE 100) · airframe 57,187 hrs · 20,803 cycles
NR 1 STRUT AFT FAIRING,INBOARD SUPPORT STIFFENER LINK PLATE BEARING WORN , BS 376.20. (REPLACE)1 ACCOMPLISHED JOB I.A.W UPS E0-98274-REQ1 REV.1 AND EGAT EI F2026A54M-1622 REV.1 AND SRM 51-40-02-0G REV.55 AND DWG 313T2303, SH.96, REV.C AND DWG 313T2303 SH.99 REV.B.
Part: SKIN — DEBONDED (ZONE 500) · airframe 57,187 hrs · 20,803 cycles
DISBOND - SKIN , LT WING T/E OUTBD FLAP INBD LWR. (REPAIR). IAW SRM 57-53-01-2R-1 REFER TO SRM 51-70-07-0G-0 REV.55. PERFORM REPAIR AS BELOW STEP:1.1 REMOVED THE DISBOND MATERIALS AND CLEANED. MEASURE THE DAMAGE SIZE AND LOCATION (L:4.5", W:2", 1.3" FROM AFT EDGE, 0.5" FROM INBD EDGE). BOND THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 260F FOR 130 MINUTES AND KEEP A MINIMUM VACUUM OF 22 IN/HG.CONDITION CHECK IS SATISFACTORY.
Part: SUPPORT — CRACKED (ZONE 400) · airframe 57,187 hrs · 20,803 cycles
NR 1 STRUT AFT FAIRING, INBD ZEE CRACK , BS 376.20. REMOVED DAMAGE ZEE INBD SEAL IAW SRM 51-40-02-0G, REV.55. INSTALLED NEW ZEE INBD SEAL IAW SRM 51-40-02-0G REV.55 AND DWG 313T2380, SH 48, REV -, DWG 313T2303, SH 92, REV: C, SH 93 REV: C, SH 98 REV B.
Part: FORMER — CRACKED (ZONE 600) · airframe 57,187 hrs · 20,803 cycles
RIGHT WING OUTBOARD L/E NOSE FORMER CRACK , OSS 499 (NR 8 SLAT OUTBOARD SEAL DOOR UPPER AREA). REMOVED DAMAGE FORMER IAW SRM 51-40-02-0G, REV 55. INSTALLED A NEW FORMER IAW SRM 51-40-02-0G, REV 55 AND DWG 114T2161, SH 3, REV B, AND SREO-50900-REQ001, REV 2.
Part: CHANNEL — CRACKED (ZONE 200) · airframe 57,187 hrs · 20,803 cycles
CRACKED CHANNEL, NR 1 PYLON RT AFT FAIRING TRAILING EDGE NUTPLATE BRACKET. (REPLACE) REMOVED DAMAGE CHANNEL IAW SRM 51-40-02-0G, REV.55. FABRICATE CHANNEL (P/N: 313T2380-741) IAW DWG 313T2380, SH 57, REV-; PL REV BJ; PSDL REV C AS A SAMPLE IAW GMM-MTX CH 9.08, REV 17. INSTALLED A FABRICATE CHANNEL IAW SRM 51-40-02-0G REV.55 AND DWG 313T2380 SH 82 REV: A, 313T2303 SH 94 REV: C, 313T2362 SH 5 REV: B
Part: ANGLE — CRACKED (ZONE 100) · airframe 57,187 hrs · 20,803 cycles
CRACKED ANGLE, BULK CGO COMPT CEILING AREA, BS 1577, LBL 74 INBD SIDE. (REPLACE) FABRICATE ANGLE IAW DWG 657T1338 SH 3 REV-; PL REV.- AS A SAMPLE IAW GMM-MTX 9.08, REV: 17 REQUIREMENT. INSTALLED FABRICATED ANGLE IAW SRM 51-40-02-0G REV.55, AND DWG 657T1332, SH 5. REV A.
Part: ANGLE — CRACKED (ZONE 100) · airframe 57,187 hrs · 20,803 cycles
CRACK - ANGLE, BULK CGO COMPT CEILING AREA, BS 1577, LBL 74 OUTBD SIDE. (REPLACE). REMOVED DAMAGE ANGLE IAW SRM 51-40-02-0G, REV.55. INSTALL NEW ANGLE I.A.W SRM 51-40-02-0G REV.55 AND BOEING DWG NO. 657T1332 SH 5 REV: A .
Part: ANGLE — DAMAGED (ZONE 400) · airframe 57,187 hrs · 20,803 cycles
ENLARGE HOLE - FITTING, NO.1 PYLON R/H AFT FAIRING DOOR NO.2 HINGE UPPER SIDE CONNECTION. (REPLACE).INSTALL FABRICATE ANGLE (P/N: 313T3310-889) I.A.W SRM 51-40-02-0G REV.55 AND DWG 313T2310 SH 42 REV: B, 313T2310 SH 36 REV: A, 313T2310 SH 38 REV: A.
Part: SKIN — CRACKED (ZONE 400) · airframe 57,094 hrs · 20,751 cycles
NR 1 ENG INLET COWL LIP CRACKED BETWEEN 11 AND 1 O'CLOCK POSITIONS REMOVED #1 ENGINE INLET IAW AMM 71-11-01
Part: COWLING — CRACKED (ZONE 400) · airframe 57,094 hrs · 20,751 cycles
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.
Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 57,071 hrs · 20,740 cycles
EMERGENCY LIGHTS BATTERY DEPLETED. EMERGENCY LIGHTS BATTERY REPLACED BY SERVICEABLE. IAW AMM 33-51-07/401 REV 148. OPERATIONAL TEST C/O O.K.
Earlier reports · 2018–2024 · 30 reports
2024
Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 54,801 hrs · 19,151 cycles
FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N:657T1126-57 (REPAIR) THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 05.04. REPAIR IAW B767-300BCF (REV. 49) SRM 53-00-50-2R-0.
Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 54,801 hrs · 19,151 cycles
FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 814T3538-30 (REPAIR) ++ THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 05.04. REPAIR IAW B767-300BCF (REV. 49) SRM 53-00-50-2R-0.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 54,801 hrs · 19,151 cycles
EO-82173-JIC001 (FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) OPEN
Part: DRAIN — NONE (NONE) · airframe 54,810 hrs · 19,152 cycles
*** SUPPLEMENTAL SDR *** ADD SDR FOR EO-82173-JIC001 (FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) ACCOMOPLISH SDR.
Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 54,801 hrs · 19,151 cycles
FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N : 814T3538-27 (REPLACE) I.A.W AMM 25-57-05-404-006, AMM 25-58-01-404-005 AND AMM 25-58-03-404-004 REV.142 RESTORED MAIN DECK CARGO HANDLING JOB COMPLETED AND CONDITION CHECK NORMAL
Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 54,801 hrs · 19,151 cycles
FOUND MAIN DECK FLOOR DAMAGE, P/N: 814T3538-30 (REPLACE) THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 05.04. REPAIR IAW B767-300BCF (REV. 49) SRM 53-00-50-2R-0.
Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 54,801 hrs · 19,151 cycles
FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N:814T3538-25 (REPAIR) I.A.W AMM 25-57-05-404-006 AND AMM 25-58-01-404-005 REV.142 RESTORED MAIN DECK CARGO HANDLING. JOB COMPLETED AND CONDITION CHECK NORMAL
Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 54,801 hrs · 19,151 cycles
FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 657T1126-57 (REPAIR) I.A.W AMM 25-57-05-404-006, AMM 25-58-01-404-005, AMM 25-58-04-404-015, AMM 25-57-02-404-016 AND AMM 25-57-06-404-006 REV.142 RESTORED MAIN DECK CARGO HANDLING JOB COMPLETED AND CONDITION CHECK NORMAL
Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 54,801 hrs · 19,151 cycles
FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N : 814T3538-23 (REPLACE) I.A.W AMM 25-57-05-404-006, AMM 25-58-05-404-052 AND AMM 25-58-01-404-005 REV.142 RESTORED MAIN DECK CARGO HANDLING. JOB COMPLETED AND CONDITION CHECK NORMAL
Part: WARNING MESSAGE — ILLUMINATED (MLG) · airframe 54,439 hrs · 18,889 cycles
GEAR DISAGREE - GEAR DOORS ON TAKEOFF - CHECKLIST HAD US BRING GEAR HANDLE UP UNTIL LANDING THEN LANDED NORMALLY. ALL LIGHTS EXTINGUISHED WHEN HANDLE WAS BROUGHT UP. CHECKED ADJUSTMENT OF LANDING GEAR CONTROL SYSTEM IAW. AMM 32-31-00-825-014, REV. 141. LIFTED THE AIRPLANE WITH JACKS IAW. AMM 07-11-01-582-015 REV. 141. PERFORMED EXTENSION AND RETRACTION OF THE LANDING GEAR IAW. AMM 32-32-00 PB 501 REV. 141. NO FAULTS FOUND AND NO ABNORMAL INDICATIONS DURING OPERATIONAL TEST. PRECAUTIONARY PERFORMED LUBRICATION OF MAIN LANDING GEARS AND DOORS IAW. AMM 12-21-14/301 AND AMM 12-21-15/301 REV. 141. LOWERED THE AIRPLANE IAW. AMM 07-11-01-582-017 REV. 141. SYSTEM OK TO CONTINUE. PROPER COMPANY QUALIFIED TO PERFORM THE ABOVE TASK C/O O.K I.A.W GMM REV 07A
Part: PROXIMITY SENSOR — FAULTED (MLG) · airframe 54,433 hrs · 18,886 cycles
GEAR DISAGREE - GEAR DOORS ON TAKEOFF - CHECKLIST HAD US BRING GEAR HANDLE UP UNTIL LANDING THEN LANDED NORMALLY. ALL LIGHTS EXTINGUISHED WHEN HANDLE WAS BROUGHT UP. ACCOMPLISHED PROXIMITY SWITCH ELECTRONICS UNIT TEST IAW AMM 32-09-04-704-013 REV141 UNTIL E STEP F. RESET NOT ACCOMPLISHED. TEST WITHOUT FAULTS.<BR>RAZLAF CRN97067976
2023
Part: FILTER — WARNING MESSAGE (ENG FUEL) · airframe 54,026 hrs · 18,596 cycles
**AIR TURNBACK**ON CLB OUT R ENG FUEL FILT EICAS MESSAGE. REPLACED R ENG FUEL FILTER IAW TASK 73-11-02-004-001-H00. FUEL FILTER PN: AC9227F1740 SN: LOT 45731740<BR>PACKING PN: M83248/1-243 SN: LOT 2213-243
2021
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,027 hrs · 16,205 cycles
INSPECTION TYPE:N/AFOUND EMERGENCY LIGHT AFT U/S.REPLACEMENT OF LAMP PERFORMED IAW AMM 33-51-03 PB201 REV 132.05.
2019
Part: CONNECTOR — DIRTY (CABIN) · airframe 49,526 hrs · 14,851 cycles
INSPECTION TYPE:PDC UNARMED LIGHT DOESN'T TURN ON WHEN EMERGENCY LIGHT SWITCH IS IN OFF POSITION. CLEANED CONNCETOR D868 AND S1 SWITCH ON M43 EMERGENCY LTS CONTROL PANEL.
2018
Part: STIFFENER — DAMAGED (BS 1373) · airframe 48,863 hrs · 14,236 cycles
AFT CARGO WEB STIFFENER AT BS 1373, LBL 3.5 DAMAGED. REPLACED THE STIFFENER.
Part: STIFFENER — DAMAGED (BS 1373) · airframe 48,863 hrs · 14,236 cycles
AFT CARGO WEB STIFFENER AT BS 1373, LBL 25 DAMAGED. REPLACED THE STIFFENER.
Part: STIFFENER — DAMAGED (BS 1373) · airframe 48,863 hrs · 14,236 cycles
AFT CARGO WEB STIFFENER AT BS 1373, LBL 33 WAS DAMAGED. REPLACED THE STIFFENER.
Part: STIFFENER — DAMAGED (BS 1373) · airframe 48,863 hrs · 14,236 cycles
AFT CARGO WEB STIFFENER AT BS 1373, LBL 17, DAMAGED. REPLACED THE STIFFENER.
Part: STIFFENER — DAMAGED (BS 1373) · airframe 48,863 hrs · 14,236 cycles
AFT CARGO WEB STIFFENER AT BS 1373, LBL 8, WAS DAMAGED. REPLACED THE STIFFENER.
Part: STIFFENER — DAMAGED (BS 1373) · airframe 48,863 hrs · 14,236 cycles
AFT CARGO WEB STIFFENER AT BS 1373, RBL 8, DAMAGED. REPLACED THE STIFFENER.
Part: STIFFENER — DAMAGED (BS 1373) · airframe 48,863 hrs · 14,236 cycles
AFT CARGO WEB STIFFENER AT BS 1373, RBL 3.5 WAS DAMAGED. REPLACED THE STIFFENER.
Part: STIFFENER — DAMAGED (BS 1373) · airframe 48,863 hrs · 14,236 cycles
AFT CARGO WEB STIFFENER AT BS 1371, RBL 30, WAS DAMAGED. REPLACED THE STIFFENER.
Part: STIFFENER — DAMAGED (BS 1373) · airframe 48,863 hrs · 14,236 cycles
AFT CARGO WEB STIFFENER AT BS 1373, RBL 12, WAS DAMAGED. REPLACED THE STIFFENER.
Part: STIFFENER — DAMAGED (BS 1373) · airframe 48,863 hrs · 14,236 cycles
AFT CARGO WEB STIFFENER AT BS 1373, LBL 44, DAMAGED. REPLACED THE STIFFENER.
Part: STIFFENER — DAMAGED (BS 1373) · airframe 48,863 hrs · 14,236 cycles
ATF CARGO WEB STIFFENER AT BS 1373, RBL 20, WAS DAMAGED. REPLACED THE STIFFENER.
Part: STIFFENER — DAMAGED (1373) · airframe 48,863 hrs · 14,236 cycles
AFT CARGO WEB STIFFENER AT BS 1373, RBL 38, DAMAGED. REPLACED THE STIFFENER.
Part: FLOORBEAM — DAMAGED (BS 1373) · airframe 48,862 hrs · 14,235 cycles
THE LOWER, AFT CARGO FLOORBEAM ASSY WAS DAMAGE AT BS 1373. REPAIRED THE FLOORBEAM.
Part: HANDLE — OUT OF RIG (CREW DOOR) · airframe 48,859 hrs · 14,233 cycles
CREW ENTRY DOOR HANDLE EXTREMELY DIFFICULT TO OPERATE, CHECKED RIGGING. DOOR FOUND TO BE OUT OF RIG, 27LBS TO OPEN, 57LBS TO CLOSE. IAW MM 52-12-00-715-119.
Part: FRAME — CRACKED (BS 883.5) · airframe 48,806 hrs · 14,205 cycles
FRAME TRANSITION RADIUS FOUND CRACKED FOUND APPROXIMATELY 5/16 INCH IN LENGTH, FOUND DURING HFEC INSPECTION AT BS 883.5, LBL 89, BELOW WL 200. THE FRAME WAS REPAIRED IAW EO B767-5310-69149, APPENDIX B.
Part: FRAME — CRACKED (BS 903.5) · airframe 48,806 hrs · 14,205 cycles
A CRACK WAS FOUND APPROXIMATELY 3/8 INCH IN LENGTH IN THE FRAME TRANSITION RADIUS., FOUND DURING HFEC INSPECTION AT BS 903.5, RBL 89, BELOW WL 200. THE FRAME WAS REPAIRED IAW EO B767-5310-69148, APPENDIX B.