N355UP

Service difficulty reports · 48

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

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N355UP' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR IPXA2026092286713Cowling · crackedCRACKED SKIN, NR 1 ENG RT CORE COWL LOWER FWD SKIN NEAR NO.1 LATCH. PERFORM REPAIR I.A.W UPS EO-98690-REQ1 REV.1.Sep 17, 2026 · N355UP · Boeing 76734AF · Nacelle/Pylon, Main FrameSDR IPXA2026092191640Panel · erodedERODED VERTICAL STAB LE PANEL 321E. REMOVED THE DAMAGE MATERIALS AND CLEAN. BONDED THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 260 F FOR 130 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG I.A.W. 767-300F SRM 55-30-01-2R-6 REFER TO SRM 51-70-07-0G-0 REV. 96.Sep 17, 2026 · N355UP · Boeing 76734AF · Vertical Stabilizer, Plate/SkinSDR IPXA2026092289443Nose Cowl · dentedDENTED NR 1 NOSE COWL INLET AT 7 O'CLOCK POSITION. BOND THE SPACER WITH FILM ADHESIVE CURED AT 250°F FOR 2 HOURS AND FILL THE CUT OUT WITH ADHESIVE CURED AT 200°F FOR 1 HOUR I.A.W. B767-300F SRM 54-15-01-2R-3 REV. 96. CONDITION CHECK IS SATISFACTORY.Sep 17, 2026 · N355UP · Boeing 76734AF · Nacelle/Pylon, Main FrameSDR IPXA2026092290656Nose Cowl · dentedDENTED NR 1 ENG NOSE COWL INLET AT 5 O'CLOCK POSITION. BOND THE SPACER WITH FILM ADHESIVE CURED AT 250°F FOR 2 HOURS AND FILL THE CUT OUT WITH ADHESIVE CURED AT 200°F FOR 1 HOUR I.A.W. B767-300F SRM 54-15-01-2R-3 REV. 96. CONDITION CHECK IS SATISFACTORY.Sep 17, 2026 · N355UP · Boeing 76734AF · Nacelle/Pylon, Main FrameSDR IPXA2026092290813Nose Cowl · dentedDENTED SKIN, NR 2 ENG NOSE COWL INNER BARREL NEAR 2:00 TO 6:00 POS. BOND THE SPACER WITH FILM ADHESIVE CURED AT 250°F FOR 2 HOURS AND FILL THE CUT OUT WITH ADHESIVE CURED AT 200°F FOR 1 HOUR I.A.W. B767-300F SRM 54-15-01-2R-3 REV. 96. CONDITION CHECK IS SATSep 17, 2026 · N355UP · Boeing 76734AF · Nacelle/Pylon, Main FrameSDR IPXA2026092290842Nose Cowl · dentedDENTED NR 1 ENGINE NOSE COWL INLET AT 6 O'CLOCK POSITION. UT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( ‘  DIA : 0.2", 27" FROM FWD EDGE, 31.5" FROM UPPER EDGE ‘¡ DIA : 0.4", 32.4" FROM FWD EDGE, 31" FROM UPPER EDGE, AT 6 O'CLOCK ON THE INNER BARREL OFSep 17, 2026 · N355UP · Boeing 76734AF · Nacelle/Pylon, Main FrameSDR IPXA2026092186627Floor Panel · crackedCRACKED PANEL, AFT CARGO FLOOR STRUCTURE, BS 1329, BL 0. REMOVED DAMAGE PANEL I.A.W SRM 51-40-02-0G REV. 96. INSTALLED FABRICATED PANEL I.A.W SRM 51-40-02-0G REV. 96 AND BOEING DWG NO: 451T2612 SHEET 2 REV. B.Sep 17, 2026 · N355UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2026092267592Fairing · debondedDEBONDED SKIN , RT AFT WING TO BODY FAIRING LATCH PANEL 198 CR. REMOVE THE DISBOND MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH RESIN CURED AT 200°F FOR 220 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG. BOND THE FOIL WITH RESIN CURED AT 200°F FOR 220 MINUTES Sep 16, 2026 · N355UP · Boeing 76734AF · Aerodynamic FairingsSDR IPXA2026092166138Skin · puncturedSKIN, RT MLG W/W DOOR MID PUNCTURED. PERFORMED NDT/UT FOR THE REWORKED AREA AND PLUS 6 INCHES AROUND HEATED AREA, IAW NDT MANUAL PART 1, 51-01-01, REV 144. REMOVE THE DELAMINATION MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH RESIN CURED AT 200°F FOR 220 Sep 16, 2026 · N355UP · Boeing 76734AF · Landing Gear DoorsSDR IPXA2026092172110Bracket · crackedCRACKED BRACKET, LT WING INBD SLAT TORQUE TUBE SUPPORT AT INBD L/E CAVITY AT ISS 285.233. REMOVED DAMAGE BRACKET I.A.W SRM 51-40-02-0G REV. 96. INSTALLED NEW BRACKET I.A.W SRM 51-40-02-0G REV. 96 AND BOEING DWG NO. 114T1240 SH. 6 REV. -.Sep 16, 2026 · N355UP · Boeing 76734AF · Wing, Attach FittingsSDR IPXA2026092172477Angle · crackedCRACKED ANGLE, NR 1 PYLON AFT BULKHEAD REAR LT ANGLE. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G REV. 96. INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G REV. 96 AND DWG 313T2303 SH. 141 REV. A AND BOEING DWG NO. 313T2303 SH. 146 REV. -.Sep 16, 2026 · N355UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous StructureSDR IPXA2026092150993Former · crackedCRACKED FORMER, RT WING OTBD L/E CAVITY CURTAIN SUPPORT BRACKET, NEAR WS 441.596. REMOVED DAMAGE FORMER I.A.W SRM 51-40-02-0G REV.96. INSTALL NEW FORMER I.A.W SRM 51-40-02-0G REV.96 AND BOEING DWG NO:1142241 SH 4 REV: - AND UPS SREO-54290-REQ1 REV.3.Sep 15, 2026 · N355UP · Boeing 76734AF · Wing Main, Frame StructureSDR IPXA2026091850925Bracket · crackedCRACKED BRACKET, RT WING INBD L/E CAVITY TORQUE TUBE SUPPORT BRACKET. REMOVED DAMAGE BRACKET I.A.W SRM 51-40-02-0G REV.96. INSTALL NEW BRACKET I.A.W SRM 51-40-02-0G REV.96 AND BOEING DWG NO:114T1240 SH 6 REV: - .Sep 15, 2026 · N355UP · Boeing 76734AF · Wing Miscellaneous StructureSDR IPXA2026091850918Angle · crackedTHE BULK CARGO OUTBOARD ANGLE AT STA 1578 LBL 80 IS CRACKED. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G REV. 96. INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G REV. 96 AND BOEING DWG NO. 146T5650 SH. 5 REV. C.Sep 15, 2026 · N355UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA2026091850822Angle · crackedTHE BULK CARGO OUTBOARD ANGLE AT STA 1578 RBL 80 IS CRACKED. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G REV. 96. INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G REV. 96 AND BOEING DWG NO. 146T5650 SH. 5 REV. C.Sep 15, 2026 · N355UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA2026091850792Angle · crackedTHE BULK CARGO INBOARD ANGLE AT STA 1578 RBL 80 IS CRACKED. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G REV. 96. INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G REV. 96 AND BOEING DWG NO. 146T5650 SH. 5 REV. C.Sep 15, 2026 · N355UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA2026091850818Angle · crackedTHE BULK CARGO INBOARD ANGLE AT STA 1578 LBL 80 IS CRACKED. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G REV. 96. <BR>2. INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G REV. 96 AND BOEING DWG NO. 146T5650 SH. 5 REV. C.Sep 15, 2026 · N355UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA2026070613325Oxygen Mask · no testOBSERVERS OXYGEN MASK DOES NOT FLOW WHEN EMERGENCY BUTTON IS PUSHED. REMOVED AND REPLACED OBSERVER`S OXYGEN MASK IAW AMM 35-11-51. OPS CHKD GOOD.Jul 5, 2026 · N355UP · Boeing 76734AF · Crew Oxygen SystemSDR IPXA2024092758398Drain · none(FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) COMPLETED SDR.Sep 18, 2024 · N355UP · Boeing 76734AF · Standard Practices/StructuresSDR IPXA2024091858398None · no discrepancy**SDR FILED OPEN** ADD SDR FOR EO-82173-JIC001 (FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R)Sep 18, 2024 · N355UP · Boeing 76734AF · Standard Practices/StructuresSDR IPXA2024091811151Floor Panel · brokenMAJOR REPAIR. FOUND MAIN DECK CARGO FLOOR PANEL BROKEN PART NUMBER : 146T5869-135 (REPAIR) I.A.W AMM 53-01-06-400-801 REV.142 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL.Sep 15, 2024 · N355UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2024092710203Cover · wornFOUND CREW ENTRY DOOR FORWARD DOORWAY ARMING LEVER COVER SCREW WORN (REPLACE) REPLACED DOORWAY ARMING LEVER COVER I.A.W AMM 20-11-00-910-802 REV.142.Sep 15, 2024 · N355UP · Boeing 76734AF · Passenger/Crew DoorsSDR IPXA2024091811112Floor Panel · brokenMAJOR REPAIR. FOUND MAIN DECK CARGO FLOOR PANEL BROKEN PART NUMBER : 146T5869-134 (REPAIR) I.A.W AMM 53-01-06-400-801 REV.142 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL.Sep 15, 2024 · N355UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2024091610203Lever · worn**SDR FILED OPEN** FAULT - FOUND CREW ENTRY DOOR FORWARD DOORWAY ARMING LEVER COVER SCREW WORN (REPLACE) OK TO WORKSep 15, 2024 · N355UP · Boeing 76734AF · Passenger/Crew DoorsSDR IPXA2024092052030Skin · dented**SDR FILED OPEN** LH INBD FLAP, TRAILING EDGE AND MID FLAP HAS DENT/DAMAGE INSTALLED L/H INBD MID FLAP LWR PNL I.A.W SRM 51-40-02-0G REV.90 AND BOEING DWG NO:113T2224 SH1 REV: BJul 28, 2024 · N355UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA2023082171352Battery · dischargedEMERGENCY ESCAPE LIGHTING INOP. R&R'D EMERGENCY EXIT LIGHT BATTERY ASSY. OPS CK GOOD, REF AMM 33-51-07-201.Aug 21, 2023 · N355UP · Boeing 76734AF · Emergency LightingSDR IPXA2022111588129Floor Panel · damagedINSPECTION TYPE:C5, DAMAGE ON MAIN DECK CARGO FLOOR PANEL BETWEEN STA 930 AND STA 972, AND BETWEEN LBL 11.0 AND RBL 11.0FABRICATE REPLACEMENT FLOOR PANEL PER UPS EO NO.:B767-5320-9693-INov 13, 2022 · N355UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2022111588126Floor Panel · damagedINSPECTION TYPE:C5, DAMAGE ON MAIN DECK CARGO FLOOR PANEL BETWEEN STA 1114.8 AND STA 1197+22, AND BETWEEN LBL 11.0 AND RBL 11.0FABRICATE REPLACEMENT FLOOR PANEL PER UPS EO NO.:B767-5320-9693-INov 13, 2022 · N355UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA2022111588123Floor Panel · damagedINSPECTION TYPE:C5DAMAGE ON MAIN DECK CARGO FLOOR PANEL BETWEEN STA 1351 AND STA 1480, AND BETWEEN LBL 11.0 AND RBL 11.0.FABRICATE REPLACEMENT FLOOR PANEL PER UPS EO NO.:B767-5320-9693-INov 13, 2022 · N355UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2022111588128Floor Panel · damagedINSPECTION TYPE:C5, DAMAGE ON MAIN DECK CARGO FLOOR PANEL BETWEEN STA 972 AND STA 1114.8, AND BETWEEN LBL 11.0 AND RBL 11.0FABRICATE REPLACEMENT FLOOR PANEL PER UPS EO NO.:B767-5320-9693-INov 10, 2022 · N355UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2022111588125Floor Panel · damagedINSPECTION TYPE:C5, DAMAGE ON MAIN DECK CARGO FLOOR PANEL BETWEEN STA 1197+22 AND STA 1208, AND BETWEEN LBL 11.0 AND RBL 11.0FABRICATE REPLACEMENT FLOOR PANEL PER UPS EO NO.:B767-5320-9693-INov 10, 2022 · N355UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2022111588124Floor Panel · damagedINSPECTION TYPE:C5DAMAGE ON MAIN DECK CARGO FLOOR PANEL BETWEEN STA 1208 AND STA 1351, AND BETWEEN LBL 11.0 AND RBL 11.0FABRICATE REPLACEMENT FLOOR PANEL PER UPS EO NO.:B767-5320-9693-INov 10, 2022 · N355UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2021082473122Lamp · inoperativeINSPECTION TYPE:N/AEXTERNAL EMERGENCY EXIT LIGHT INOPEXTERNAL EMERGENCY EXIT LIGHT RELAMPED AND TESTED SERVICEABLE IAW B767 AMM 33-51-16-962-001Aug 24, 2021 · N355UP · Boeing 76734AF · Emergency LightingSDR IPXA2020111462354Skin · brokenINSPECTION TYPE: C4 BROKEN ON LOWER SKIN (P/N:114T4114-23) OF NR 8 SLAT TRAILING EDGE WEDGE NEAR OSS 432.15. REPAIR IAW B767-300F SRM 57-43-02-2R-1 SRM 51-70-10-2R REPAIR GENERAL SRM 51-70-10-2R-4, REV.78.00.Nov 9, 2020 · N355UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA2020111462352Skin · brokenINSPECTION TYPE: C4 BROKEN ON LOWER SKIN (P/N:114T4114-23) OF NR 8 SLAT TRAILING EDGE WEDGE NEAR OSS 498. REPAIR IAW B767-300F SRM 57-43-02-2R-1, SRM 51-70-10-2R REPAIR GENERAL, SRM 51-70-10-2R-4 REV 78.00.Nov 9, 2020 · N355UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA2020083159644Floor Panel · damagedINSPECTION TYPE:N/A MAIN CARGO DECK POSITION 2L INTERIM REPAIR TO FLOOR PANEL DAMAGE 20IN FWD OF BALLMAT AND 15IN FROM CENTER LINE. FABRICATE NEW PANEL REF EO B767-5320-9693-I APPENDIX B.Aug 31, 2020 · N355UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2020083159643Floor Panel · crackedINSPECTION TYPE:N/A MAIN CARGO DECK POSITION 2L INTERIM REPAIR TO FLOOR PANEL 26 INCH FWD OF BALL AMOUNT AND 20 INCH FROM LEFT SIDE WALL. FABRICATED NEW FLOOR PANEL 143T5876-63U REF: EO B767-5320-9693-I APPENDIX B.Aug 30, 2020 · N355UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2020021051991Seal · tornATB - HEAVY VIB CLIMBING OUT OF 7000 FT AND GOT WORSEW AS WE ACCELERATED ABOVE 10,000 FT, VIB WAS FELT IN BOTH CONTROL COLUMNS AND FLOOR. SLOWED TO 290 / 0.78 AND VIB DECREASED. APPEARS LESS VIB IN DESCENTC/W AIRFRAME CONDITIONAL INSP PER M/M 05-51-38-202-001 Feb 8, 2020 · N355UP · Boeing 76734AF · Landing Gear DoorsSDR IPXA2019072945020Warning System · false activationINSPECTION TYPE:INSPL FWD ENTRY DOOR EICAS MESSAGE. T/S PER FIM 52-90-17-41, CKD SENSOR S194 & LATCHING MECHANISM, NO FAULTS NOTED. FWD ENTRY DOOR IND OPS CKD NORMAL PER AMM 52-12-00-501. THIS CLEARS M677817.Jul 29, 2019 · N355UP · Boeing 76734AF · Door Warning SystemSDR IPXA2019011537866Warning System · false activationINSPECTION TYPE:ETOP LEFT FUEL QUANTITY BLANK & EICAS STATUS MSG "FUEL QTY IND" CONDITION INTERMITTENT. FOUND AT BITE CHECK FUEL COMPUTER LM TANK UNIT 9 OPEN LOZ OR HIZ WIRE G IAW FIM 28-41-815-851-004 REV 125.04. A/C DISPATCH IAW MEL 28-41-1-1B REV 48. DMP PEJan 15, 2019 · N355UP · Boeing 76734AF · Fuel Quantity IndicatorSDR IPXA2016121611787Engine · malfunctionedDURING DESCENT, THE RT ENGINE FAILED TO RESPOND TO ANY THROTTLE MOVEMENTS. EGT REMAINED HIGH AT 670'C WITH N1 & N2 BACK AT IDLE. LOST CONTROL OF ANY THRUST ON RT ENGINE, EMERGENCY DECLARED. R & R NR 2 ENGINE IAW TC6001 AND 6002.Dec 13, 2016 · N355UP · Boeing 76734AF · Engine (Turbine/Turboprop)SDR IPXA2016111810785Counterbalance · failedCREW ENTRY DOOR STUCK HALF WAY OPEN. REPLACED COUNTERBALANCE SYSTEM L1 DOOR IAW AMM 52-12-16.Nov 17, 2016 · N355UP · Boeing 76734AF · Passenger/Crew DoorsSDR IPXA2016051103204Floorboard · gougedFLOORBOARD IS GOUGED BEYOND SRM LIMITS. FABRICATED NEW FLOORBOARD IAW REO B767-5320-9693-I.May 11, 2016 · N355UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2016051103236Floorboard · gougedFLOORBOARD GOUGED BEYOND SRM LIMITS. FABRICATED NEW FLOOR PANEL IAW SREO B767-5320-9693-I.May 11, 2016 · N355UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2014071683611Stringer · damagedSTRINGER 31L DAMAGED 7 INCHES FWD OF BS 1285. REPAIRED IAW EO B767-5310-54925-A.Jul 14, 2014 · N355UP · Boeing 76734AF · Fuselage Main, Longeron/StringerSDR IPXA2014071683610Skin · damagedFUSELAGE SKIN DAMAGE BS 1270-1285 BETWEEN S30L AND S32L. REPAIRED IAW EO B767-5330-54923-A.Jul 14, 2014 · N355UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR IPXA2014071683609Skin · damagedFOUND DAMAGE TO THE FUSELAGE SKIN, BS 1197-1222. REPAIRED IAW EO B767-5330-54924-A.Jul 14, 2014 · N355UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR IPXA13678924Cdu · inoperativeALL KEYS ON CAPTAIN`S CDU INOPERATIVE WITH NORMAL AND ALTERNATE FMC SELECTED. R & R NR 1 CDU IAW AMM 34-61-02-022-195 AND IPC 34-61-02-02A.Jun 18, 2013 · N355UP · Boeing 76734AF · Central Display
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