Registered owner
United Parcel Service Co
Owner type
Corporation
Serial number
40363
Year built
2010
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
June 14, 2024
Certificate issued
March 17, 2023
Expires
March 31, 2030
Mode S code
A49E9A

From the FAA registry file of October 24, 2026.

On this page

Airworthiness directives that may apply · 409

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

1983In forceSuperseded2026
ADs by the year they took effect: 469 ADs
19835
19854
19869
19876
19888
19899
199021
199117
199211
199311
199418
19957
199610
19975
19989
19999
200024
200125
200215
200318
200418
200519
200611
200715
200815
200914
201013
20119
201216
201310
201414
20158
20168
20179
20189
20192
20207
20218
20224
20235
20242
20256
20266
See all 471 ADs

Information bulletins that may apply · 15

Advisory, not mandatory.

NTSB investigations

No NTSB investigations matched to N397UPMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Boeing 767-346 aircraft

FAA incident reports

No FAA accident or incident reports matched to N397UPMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Boeing 767-346 aircraft

Service difficulty reports · 14

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR IPXA2026061535378Skin · debondedFAULT - DISBOND - SKIN , INBD EDGE OF L/H WING T/E OUTBD FLAP T/E UPPER SKIN , WBL 355. I.A.W CMM 57-53-51 REV 39 REMOVE THE RETAINER AND SEAL. REMOVE THE DISBOND MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH RESIN CURED AT 200°F FOR 220 MINUTES WITH MINIMUJun 6, 2026 · N397UP · Boeing 767346 · Trailing Edge FlapsSDR IPXA2026061235691Skin · debondedFAULT - DEBONDED SKIN , LOWER FACE OF LT WING T/E OTBD FLAP WEDGE LOWER SKIN , WS 663. IAW SRM 57-53-01-2R-1 REFER TO SRM 51-70-06-0G-0 REV. 55 PERFORM REPAIR AS BELOW STEP : 1.REMOVE THE DISBOND MATERIALS AND CLEAN. MEASURE THE DAMAGE SIZE AND LOCATION ( DIJun 6, 2026 · N397UP · Boeing 767346 · Trailing Edge FlapsSDR IPXA2026061235713Skin · debondedDEBONDED SKIN , FORWARD FACE OF LT WING T/E OUTBD FLAP L/E SKIN , WBL 420. REMOVE THE DISBOND MATERIALS AND CLEAN. MEASURE THE DAMAGE SIZE AND LOCATION ( DIA : 1", 5.4" FROM LOWER EDGE, 67" FROM INBD EDGE ). BONDED THE REPAIR PLIES WITH RESIN CURED AT 150°F FJun 6, 2026 · N397UP · Boeing 767346 · Trailing Edge FlapsSDR IPXA2026061035846Former · crackedCRACK - FORMER , FWD SIDE OF LT WING OUTBD L/E NOSE BEAM , OSS 565.9 (REPLACE) REMOVE DAMAGE FORMER IAW SRM 51-40-02-0G REV.55. INSTALL NEW FORMER IAW SRM 51-40-02-0G REV.55 AND BOEING DWG 114T2162 SH 5 REV. - AND EO SREO-50900-REQ001 REV2.Jun 6, 2026 · N397UP · Boeing 767300 · Wing Main, Frame StructureSDR IPXA2026061035797Former · crackedCRACK-FORMER , FWD SIDE OF LT WING OUTBD L/E NOSE BEAM , OSS 441.6. INSTALLED NEW FORMER I.A.W SRM 51-40-02-0G REV.55 AND BOEING DWG NO: 114T2241 SH 4 REV. - AND UPS EO NO: SREO-54290-REQ1 REV3.Jun 6, 2026 · N397UP · Boeing 767300 · Wing Main, Frame StructureSDR IPXA2026060935790Former · crackedCRACKED FORMER , R/H WING L/E NO. 8 SLAT INBD AUXILEARY TRACK FORMER OSS 441. INSTALL NEW FORMER IAW SRM 51-40-02-0G REV.55 AND DWG 114T2241 SH 4 REV. - AND EO NR SREO-54290-REQ1 REV3.Jun 6, 2026 · N397UP · Boeing 767300 · Leading Edge DevicesSDR IPXA2026060925846Former · crackedCRACKED FORMER, RT WING L/E NR 9 SLAT INBD DOOR LINK FORMER OSS 565. INSTALL NEW FORMER I.A.W SRM 51-40-02-0G REV.55 AND BOEING DWG NO: 114T2162 SH 5 REV. - AND UPS EO NO: SREO-50900-REQ001 REV2.Jun 5, 2026 · N397UP · Boeing 767300 · Leading Edge DevicesSDR IPXA2026060804787Bracket · crackedCRACKED R/H WING L/E INBD PANEL. 611KB BRACKET AREA TORQUE TUBE SUPPORT LES 281. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G REV.55 AND BOEING DWG NO.114T1240 SH.6 REV.-Jun 4, 2026 · N397UP · Boeing 767300 · Wing Miscellaneous StructureSDR IPXA2026060462876Antenna · erodedFOUND V.S.T HF ANTENNA ( 321E ) EROSION. PERFORMED NDT/UT FOR REWORKED AREA AND PLUS 6" AROUND HEATED AREA I.A.W. B767 NTM PART 1, 51-01-01 REV.143 RESULT: NO DEFECT FOUND. I.A.W AMM 55-35-01-308-023 REV 148 , REPAINT REWORK AREA. 2.JOB COMPLETED AND CONDITJun 2, 2026 · N397UP · Boeing 767300 · Communications SystemSDR IPXA2025080978295Lens · unserviceableFL DK EMERGENCY EXIT LIGHT A FEW LENS FOUND U/S. U/S LENS REPLACED BY SERVICEABLE IAW AMM 33-51-01-402-030 REV 145.Aug 8, 2025 · N397UP · Boeing 767346 · Emergency LightingSDR IPXA2024081642841Panel · damagedAIRCRAFT COLLISION TO RH HORIZONTAL TIP. INSTALLED R/H OUTBD HORIZONTAL STAB L/E PANEL 342DR IAW B767 SRM 51-40-02. INSTALLED RH HOR OUTBD LOWER EDGE PANEL AND HORIZONTAL END CAP IAW B767 SRM 51-40-02. REPAIR INSTALLATION VERIFIED.Jul 16, 2024 · N397UP · Boeing 767346 · Horizontal Stabilizer StructureSDR IPXA2024071742841Stabilizer · ground damageAIRCRAFT COLLISION TO RH HORIZONTAL TIPJul 16, 2024 · N397UP · Boeing 767346 · Standard Practices/StructuresSDR IPXA2024051148518Shear Tie · mechanic errorLH SHEAR TIES INSTALL FLOOR TO SKIN SECTION MOD FOUND (03 QTY) HOLES WITH SHORT EDGE MARGIN CONDITION AND (01 QTY) HOLE RIDING ON RADIUS OF THE FTG(P/N 657T172-10) (CAT.B MAJOR REPAIR) REVIEW COMPLETEMar 14, 2024 · N397UP · Boeing 767346 · Standard Practices/StructuresSDR IPXA2023122648565Unknown · unknown*SDR FILED OPEN* FAULT - FUSELAGE SKIN AT STA 1050.25 BETWEEN S21L AND S22L FOUND WITH BLEND MARK RECOMMENDED ACTION TO MEASURE BLEND OUT MARKDec 26, 2023 · N397UP · Boeing 767300 · Fuselage Main, Plate/Skin

STCs that may be installed · 757

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

See all 757 STCs