# Service difficulty reports: N331UP

A list on [N331UP](https://openairdocs.org/aircraft/N331UP.md).

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

Page 1 of 3 · 133 reports

- [SDR IPXA2026093002770](https://openairdocs.org/sdr/IPXA2026093002770.md): Trim Panel · detached · Sep 30, 2026 · N331UP · Boeing 76734AF · Passenger/Crew Doors
  > MAIN ENTRY DOOR SEAL TRIM CAME OFF WHEN CLOSING DOOR REINSTALLED SEAL ITEM 15 INTO RETAINER ITEM 20 PER IPC 52-11-02-10A NO AMM REFERENCE COULD BE FOUND FOR THE INSTALLATION OF THIS DOOR CUTOUT/LINING SEAL
- [SDR IPXA2026081461884](https://openairdocs.org/sdr/IPXA2026081461884.md): Former · cracked · Aug 7, 2026 · N331UP · Boeing 76734AF · Wing Main, Frame Structure
  > CRACKED FORMER, RT WING FIXED L/E NOSE BEAM SUPPORT STRUCTURE AT STA OSS 499. REMOVE DAMAGE FORMER IAW SRM 51-40-02-0G, REV 95. INSTALL NEW FORMER IAW SRM 51-40-02-0G, REV 95 AND DWG 114T2161, SH 1, REV E, & EO SREO-50900-REQ001, REV 2.
- [SDR IPXA2026081146435](https://openairdocs.org/sdr/IPXA2026081146435.md): Floor Panel · cracked · Aug 6, 2026 · N331UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND AFT CARGO FLOOR PANEL CRACKED. IAW SRM 53-00-50-2R-0 REV. 95, CUT OUT THE DAMAGE AND CLEANED. BONDED THE REPAIR PLIES WITH RESIN CURED AT 170F FOR 2 HOURS WITH A MINIMUM VACUUM OF 20 IN/HG IAW SRM 53-00-50-2R-0, REV 95.
- [SDR IPXA2026081244447](https://openairdocs.org/sdr/IPXA2026081244447.md): Cowling · dented · Aug 6, 2026 · N331UP · Boeing 76734AF · Nacelle/Pylon, Plate/Skin
  > DENTED NR 2 ENG NOSE COWL INLET AT 7 & 5 O'CLOCK POSITIONS. CUT OUT THE DAMAGE & CLEAN, MEASURE THE CUT OUT ( (1) DIA: 1", 15.5" FROM FWD EDGE AT 7 O'CLOCK, (2) DIA: 1", 15.3" FROM FWD EDGE AT 5 O'CLOCK ON THE INNER BARREL OF NR 2 ENG INLET COWL. BONDED T
- [SDR IPXA2026080944690](https://openairdocs.org/sdr/IPXA2026080944690.md): Former · cracked · Aug 6, 2026 · N331UP · Boeing 76734AF · Wing Main, Frame Structure
  > CRACKED FORMER, LT WING OTBD FXD LE NOSE SKIN SUPPORT, OSS 499.60. INSTALLED A NEW FORMER IAW SRM 51-40-02-0G REV.95 AND DWG 114T2161 SH 1 REV. E AND EO SREO-50900-REQ001 REV2.
- [SDR IPXA2026080842558](https://openairdocs.org/sdr/IPXA2026080842558.md): Fairing · debonded · Aug 6, 2026 · N331UP · Boeing 76734AF · Aerodynamic Fairings
  > DEBONDED SKIN, RT AFT WING TO BODY FAIRING EXTERNAL, PANEL 198CR. IAW SRM 52-40-02-2R-4, REF SRM 51-70-17-0G-0, & SRM 51-70-14-0G-0, REV 95. REMOVED DEBONDED MATERIAL & CLEANED. BONDED THE REPAIR PLIES WITH RESIN CURED AT 200F FOR 220 MINUTES WITH MINIMUM VA
- [SDR IPXA2026081527200](https://openairdocs.org/sdr/IPXA2026081527200.md): Shaft · corroded · Aug 5, 2026 · N331UP · Boeing 76734AF · Trailing Edge Flap Control System
  > FOUND LT WING OTBD FLAP NR 2 SUPPORT CRANK ARM AND INPUT SHAFT CORROSION. IAW AMM 27-51-21-024-001, REV 148, REMOVED LT WING NR 2 FLAP ACTUATOR CRANK ARM & INPUT SHAFT. IAW AMM 27-51-21-424-032, REV 148. INSTALLED LT WING NR 2 FLAP ACTUATOR CRANK ARM & INPUT
- [SDR IPXA2026081903745](https://openairdocs.org/sdr/IPXA2026081903745.md): Skin · cracked · Aug 4, 2026 · N331UP · Boeing 76734AF · Fuselage Main, Plate/Skin
  > MAJOR REPAIR, SKIN, DURING PERFORM T/C: EO-24301-JIC001 FOUND SKIN CRACK AT BS 1725.5, S-7R. ACCOMPLISH THE REPAIR I.A.W EO-24301-JIC3 REV7 AND SRM 53-80-01-2R-5 REV.95 AND EGAT WORK SHEET NO.60614 AND EO-98363-REQ1 REV1.
- [SDR IPXA2026081706832](https://openairdocs.org/sdr/IPXA2026081706832.md): Ring · cracked · Aug 4, 2026 · N331UP · Boeing 76734AF · Engine Thrust Reverser
  > FOUND NR 1L T/R AFT CASCADE SUPPORT RING CRACK. COMPLETED THRUST REVERSER AFT CASCADE SUPPORT RING (ACSR) REPLACEMENT IAW EO-87822-REQ01L-REPL REV3.
- [SDR IPXA2026081706840](https://openairdocs.org/sdr/IPXA2026081706840.md): Ring · cracked · Aug 4, 2026 · N331UP · Boeing 76734AF · Engine Thrust Reverser
  > FOUND NR 1R T/R AFT CASCADE SUPPORT RING CRACK. COMPLETED THRUST REVERSER AFT CASCADE SUPPORT RING (ACSR) REPLACEMENT I.A.W EO-87822-REQ01R-REPL REV4.
- [SDR IPXA2026081303363](https://openairdocs.org/sdr/IPXA2026081303363.md): Angle · cracked · Aug 4, 2026 · N331UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FOUND THE FIRE DETECTION LOOP FASTENER STRIP CRACKED AT BS 1562 LBL 76 IN BULK CARGO COMPARTMENT. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G REV.95. INSTALL NEW ANGLE I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO: 218T4100 SH 3 REV: B AND BOEING DWG NO: 218T4
- [SDR IPXA2026081107438](https://openairdocs.org/sdr/IPXA2026081107438.md): Angle · cracked · Aug 4, 2026 · N331UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > THE BULK CARGO INBOARD ANGLE AT BS 1578, LBL 80 IS CRACKED. REMOVED DAMAGE ANGLE IAW SRM 51-40-02-0G REV.95. INSTALL NEW ANGLE IAW SRM 51-40-02-0G, REV 95 AND DWG 146T5650, SH 5, REV C.
- [SDR IPXA2026081107416](https://openairdocs.org/sdr/IPXA2026081107416.md): Angle · cracked · Aug 4, 2026 · N331UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > THE BULK CARGO OUTBOARD ANGLE AT BS 1578 LBL 80 IS CRACKED. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G REV.95. INSTALLED NEW ANGLE IAW SRM 51-40-02-0G, REV.95 AND DWG 146T5650, SH 5, REV C.
- [SDR IPXA2026081107408](https://openairdocs.org/sdr/IPXA2026081107408.md): Angle · cracked · Aug 4, 2026 · N331UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > THE BULK CARGO OTBD ANGLE AT BS 1578, RBL 80 IS CRACKED. REMOVED DAMAGE ANGLE IAW SRM 51-40-02-0G REV.95. INSTALL NEW ANGLE IAW SRM 51-40-02-0G REV.95 AND DWG 146T5650 SH 5 REV.C.
- [SDR IPXA2026080803361](https://openairdocs.org/sdr/IPXA2026080803361.md): Floor Panel · cracked · Aug 4, 2026 · N331UP · Boeing 76734AF · Fuselage Floor Panel
  > CRACKS ON THE FLOOR PANEL NO. 251XFF (P/N 146T5869-89) IN THE MAIN DECK CARGO COMPARTMENT. REMOVED THE FLOOR PANEL IAW AMM 53-01-06-000-801 REV. 148. IAW AMM 53-01-06-400-801 REV.148. INSTALLED THE FLOOR PANEL 251XFF.
- [SDR IPXA2026081187679](https://openairdocs.org/sdr/IPXA2026081187679.md): Angle · cracked · Aug 3, 2026 · N331UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > THE BULK CARGO INBOARD ANGLE AT BS 1578, RBL 80 IS CRACKED. INSTALLED A NEW ANGLE IAW SRM 51-40-02-0G, REV 95 AND DWG 146T5650 SH 5 REV.C.
- [SDR IPXA2026080988147](https://openairdocs.org/sdr/IPXA2026080988147.md): Former · cracked · Aug 3, 2026 · N331UP · Boeing 76734AF · Wing Main, Frame Structure
  > CRACKED FORMER, LT WING OTBD FXD LE NOSE SKIN SUPPORT, OSS 648.60. INSTALLED A NEW FORMER IAW SRM 51-40-02-0G REV.95 AND DWG NR 114T2163 SH 1 REV. E, AND EO SREO-50900-REQ001 REV2.
- [SDR IPXA2026080790105](https://openairdocs.org/sdr/IPXA2026080790105.md): Wedge · debonded · Aug 3, 2026 · N331UP · Boeing 76734AF · Leading Edge Devices
  > DEBONDED SKIN, LT WING NR 4 SLAT TE WEDGE INBD. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE DAMAGE AREA I.A.W. 767-300F SRM 57-43-02-2R-1. INSTALL THE REPAIR CORE PLUG, FILLER AND INTERNAL DOUBLER WITH FILM ADHESIVE AND COMPOUND I.A.W. 767-300F SRM 51-70-10-2R-
- [SDR IPXA2026080792047](https://openairdocs.org/sdr/IPXA2026080792047.md): Antenna · eroded · Aug 3, 2026 · N331UP · Boeing 76734AF · HF Communications System
  > FOUND V.S.T HF ANTENNA (321E) EROSION. REMOVE THE EROSION MATERIALS AND CLEAN IAW SRM 55-30-01-2R-6 REFER TO SRM 51-70-07-0G-0 REV. 95. BOND THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 260°F FOR 130 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG.
- [SDR IPXA2026042834448](https://openairdocs.org/sdr/IPXA2026042834448.md): Handle · broken · Apr 16, 2026 · N331UP · Boeing 76734AF · Passenger/Crew Doors
  > CREW DOOR INTERIOR EMERGENCY PANEL HANDLE BROKEN REMOVED AND REPLACED EMERGENCY ASSIST HANDLE PER AMM 20-11-00. THIS CLOSES DMI 2875106.
- [SDR IPXA2026022593982](https://openairdocs.org/sdr/IPXA2026022593982.md): Cover · broken · Feb 25, 2026 · N331UP · Boeing 76734AF · Passenger/Crew Doors
  > CREW ENTRY DOOR PLUNGER HANDLE PLASTIC COVER PLATE IS BROKEN AND WILL NOT STAY DOWN. SAFETY DOOR LATCH HANDLE COVER DOES NOT APPEAR TO BE BROKEN. COVER CLOSES AND COVERS HANDLE AS INTENDED IAW 52-12-02.
- [SDR IPXA2026022328374](https://openairdocs.org/sdr/IPXA2026022328374.md): Cover · bent · Feb 21, 2026 · N331UP · Boeing 76734AF · Passenger/Crew Doors
  > SAFETY DOOR LATCH COVER WILL NO CLOSE. FOUND BENDED FLAP ON SAFETY DOOR LATCH COVER. REWORKED AND REINSTALLED PER AMM 52-12-02/401 AT REV. 147 WITH SATIS. FUNCTION IS GIVEN. COVER OPENS AND CLOSES AS DESIGNED. OK TO CONTINUE. CONFIRMED ALL TOOLS AND PARTS REM
- [SDR IPXA2025082525414](https://openairdocs.org/sdr/IPXA2025082525414.md): Switch · damaged · Aug 23, 2025 · N331UP · Boeing 76734AF · Emergency Lighting
  > FOUND UNARMED? KORRY SWITCH ON EMERGENCY LIGHT PANEL DAMAGED. R & R EMERGENCY LIGHT PANEL IAW AMM 33-51-08/401. OPS CHECK GOOD.
- [SDR IPXA2025080451310](https://openairdocs.org/sdr/IPXA2025080451310.md): Adc · inoperative · Aug 1, 2025 · N331UP · Boeing 76734AF · Air Data Computer
  > ***AIR TURN BACK*** AIRCRAFT DISPLAYED FLAP LIM & SPD LIM AT 255 KTS AND 3000 FT ON CLIMBOUT. FLAP LEVER WAS IN UP POSITION AND INDICATED UP ON FLAP INDICATOR. ++REPLACED R ADC IAW AMM 34-12-01. OPS CHECK SATISFACTORY PER AMM 34-12-00. RESEATED R SWC PER AMM
- [SDR IPXA2024071998349](https://openairdocs.org/sdr/IPXA2024071998349.md): Indicator · faulted · Jul 13, 2024 · N331UP · Boeing 76734AF · Fuel Quantity Indicator
  > AIR TURN BACK DUE FUEL CONFIG EICAS MESSAGE AT TOP OF CLIMB (LOGPAGE ATTACHED) ACCOMPLISHED DETAILED EXTERNAL VISUAL INSPECTION FOR LEAK OF CENTER & LEFT FUEL TANK AREA. NO LEAK FOUND. ACCOMPLISHED DETAILED INTERNAL AUXILIARY CENTER TANK INSPECTION #3 RIB SEA
- [SDR IPXA2024071598349](https://openairdocs.org/sdr/IPXA2024071598349.md): Warning Message · illuminated · Jul 13, 2024 · N331UP · Boeing 76734AF · Aircraft Fuel System
  > ATB, EMERGENCY DECLARED, DUE FUEL CONFIG EICAS MESSAGE AT TOP OF CLIMB DEFERRED PER EO-90886-REQ1 1 FLT CYCLE.
- [SDR IPXA2024070239483](https://openairdocs.org/sdr/IPXA2024070239483.md): Floor Panel · dented · Jun 27, 2024 · N331UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND MAIN DECK FLOOR PANEL DENT, PANEL NO: 231FFF, P/N: 143T5876-85. I.A.W AMM 25-57-02-404-016 AND AMM 25-57-03-404-005 AND AMM 25-57-90-424-011 AND AMM 25-58-01-404-018 AND AMM 25-58-03-404-017 AND AMM 25-58-03-404-004 REV 142 REINSTALLED MAIN DECK CARGO H
- [SDR IPXA2024070239397](https://openairdocs.org/sdr/IPXA2024070239397.md): Floor Panel · dented · Jun 27, 2024 · N331UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND MAIN DECK FLOOR PANEL DENT, PANEL NO: 231NFF, P/N: 143T5876-69. (REPAIR). I.A.W AMM 25-57-02-404-016 AND AMM 25-57-05-404-006 AND AMM 25-58-01-404-005 AND AMM 25-58-05-404-052 REV 142 RESTORED MAIN DECK CARGO HANDLING. JOB COMPLETED AND CONDITION CHECK N
- [SDR IPXA2024070239518](https://openairdocs.org/sdr/IPXA2024070239518.md): Floor Panel · dented · Jun 27, 2024 · N331UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND MAIN DECK FLOOR PANEL DENT, PANEL NO: 231CFF, P/N: 143T5876-75. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.2.
- [SDR IPXA2024070239299](https://openairdocs.org/sdr/IPXA2024070239299.md): Floor Panel · dented · Jun 27, 2024 · N331UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND MAIN DECK FLOOR PANEL DENT, PANEL NO: 222AFF, P/N: 141T5856-48. (REPAIR)..I.A.W AMM 25-57-05-404-006 AND AMM 25-58-01-404-005 AND AMM 25-57-02-404-016 REV 142 RESTORED MAIN DECK CARGO HANDLING. JOB COMPLETED AND CONDITION CHECK NORMAL.
- [SDR IPXA2024070239435](https://openairdocs.org/sdr/IPXA2024070239435.md): Floor Panel · dented · Jun 27, 2024 · N331UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND MAIN DECK FLOOR PANEL DENT, PANEL NO: 231PFF, P/N: 143T5876-67. (REPAIR)..I.A.W AMM 25-57-02-404-016 AND 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.
- [SDR IPXA2024070239555](https://openairdocs.org/sdr/IPXA2024070239555.md): Floor Panel · dented · Jun 27, 2024 · N331UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND MAIN DECK FLOOR PANEL DENT, PANEL NO: 222CFF, P/N: 141T5856-50. (REPAIR). I.A.W AMM 25-57-05-404-006 AND AMM 25-58-05-404-052 AND AMM 25-58-01-404-005 REV 142 RESTORED MAIN DECK CARGO HANDLING. OB COMPLETED AND CONDITION CHECK NORMAL.
- [SDR IPXA2024070239463](https://openairdocs.org/sdr/IPXA2024070239463.md): Floor Panel · dented · Jun 27, 2024 · N331UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND MAIN DECK FLOOR PANEL DENT, PANEL NO: 232GFF, P/N: 143T5876-82. (REPAIR)..I.A.W AMM 25-57-02-404-016 AND AMM 25-57-03-404-005 AND AMM 25-58-01-404-018 AND AMM 25-58-05-404-026 AND AMM 25-58-05-404-052 REV 142 RESTORED MAIN DECK CARGO HANDLING. JOB COMPL
- [SDR IPXA2024070239341](https://openairdocs.org/sdr/IPXA2024070239341.md): Floor Panel · dented · Jun 27, 2024 · N331UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND MAIN DECK FLOOR PANEL DENT, PANEL NO: 231RFF, P/N: 143T5876-58. (REPAIR). I.A.W AMM 25-57-05-404-006 AND AMM 25-58-03-404-004 AND AMM 25-58-01-404-005 REV 142 REINSTALLED MAIN DECK CARGO HANDLING. JOB COMPLETED AND CONDITION CHECK NORMAL.
- [SDR IPXA2024071245387](https://openairdocs.org/sdr/IPXA2024071245387.md): Angle · cracked · Jun 25, 2024 · N331UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > ANGLE, L/H E/E COMPARTMENT, STA 246. (REPLACE) FABRICATE P/N(141T5146-16) PER BOEING DWG NO.141T5146 SH 15 REV."B";PL REV."F";PSDL REV."-"AND ORIGINAL PART AS A SAMPLE I.A.W. GMM-MTX CH 9.08 REV 7B REQUIREMENT. INSTALLED FABRICATED PART I.A.W SRM 51-40-02-0G R
- [SDR IPXA2024070904702](https://openairdocs.org/sdr/IPXA2024070904702.md): Handle · inoperative · Jun 25, 2024 · N331UP · Boeing 76734AF · Service Doors
  > FOUND FORWARD LH ENTRY/ SVCE DOOR HANDLE MECHANISM PAWL DAMAGE. (REPLACE). I.A.W AMM 52-11-26-004-001 REV.142 AND AMM 52-11-26-404-003 REV.142 REPLACED PAWL. JOB COMPLETED AND CONDITION CHECK NORMAL.
- [SDR IPXA2024062504702](https://openairdocs.org/sdr/IPXA2024062504702.md): Pawl · damaged · Jun 25, 2024 · N331UP · Boeing 76734AF · Passenger/Crew Doors
  > FOUND FORWARD LH ENTRY/ SVCE DOOR HANDLE MECHANISM PAWL DAMAGE. (REPLACE) OK TO WORK
- [SDR IPXA2024062507531](https://openairdocs.org/sdr/IPXA2024062507531.md): None · none · Jun 25, 2024 · N331UP · Boeing 76734AF · Standard Practices/Structures
  > FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R. ACCOMPLISHED EO-82173-JIC001.
- [SDR IPXA2023102652049](https://openairdocs.org/sdr/IPXA2023102652049.md): Flap System · warning message · Oct 25, 2023 · N331UP · Boeing 76734AF · Trailing Edge Flap Control System
  > *** EMERGENCY DECLARED *** TRAILING EDGE FLAP DISAGREE EICAS CAME ON DURING APPROACH. RAN QRH PROCEDURE. PERFORMED FIM PROCEDURE 27-90-30-00. FSEU BITE PER 27-51 FAULT TREE 808. NO FAULTS FOUND. PERFORMED OPERATIONAL TEST OF TRAILING EDGE FLAPS PER AMM 27-51-0
- [SDR IPXA2023112142140](https://openairdocs.org/sdr/IPXA2023112142140.md): Slat · cracked · Oct 12, 2023 · N331UP · Boeing 76734AF · Leading Edge Devices
  > *SUPPLEMENTAL SDR* L/H LEADING EDGE SLAT #6 DAMAGED. METAL TRIM PIECE FROM WING EMBEDDED IN SLAT CAUSING CRACK***SM80/LMX6***HGR*** LEFT WING NO. 6 SLAT CLOSURE PANEL CRACK REPAIR. FOLLOW ON ACTION. COMPLETED EO-88445-REQ3
- [SDR IPXA2023101242140](https://openairdocs.org/sdr/IPXA2023101242140.md): Unknown · unknown · Oct 12, 2023 · N331UP · Boeing 76734AF · Leading Edge Devices
  > *SDR FILED OPEN* L/H LEADING EDGE SLAT #6 DAMAGED. METAL TRIM PIECE FROM WING EMBEDDED IN SLAT CAUSING CRACK***SM EVAL REQ*** DEFERRED PER EO-88445. NO DMP REQUIRED.
- [SDR IPXA2023092650947](https://openairdocs.org/sdr/IPXA2023092650947.md): Unknown · broken · Sep 14, 2023 · N331UP · Boeing 76734AF · Cargo/Baggage Doors
  > LOWER AFT CARGO DOOR FORWARD FRAME DOOR LATCH GUARD BROKEN AND SEAL RETAINER BENT.***SM18/LMX8*** R&R LWR AFT CARGO DOOR FWD FRAME DOOR LATCH IAW SRM 51-40-1
- [SDR IPXA2023091450947](https://openairdocs.org/sdr/IPXA2023091450947.md): Unknown · unknown · Sep 14, 2023 · N331UP · Boeing 76734AF · Fuselage Main, Structure
  > *** SDR FILED OPEN *** LOWER AFT CARGO DOOR FORWARD FRAME DOOR LATCH GUARD BROKEN AND SEAL RETAINER BENT.***SM18/LMX8*** R&R LWR AFT CARGO DOOR FWD FRAME DOOR LATCH IAW SRM 51-40-1
- [SDR IPXA2023072180745](https://openairdocs.org/sdr/IPXA2023072180745.md): Spring · broken · Jun 16, 2023 · N331UP · Boeing 76734AF · Passenger/Crew Doors
  > *SUPPLEMENTAL SDR* MAIN ENTRY/DOOR ARMING LEVER HINGE COVER SPRING BROKEN. REPLACED MAIN ENTRY DOOR ARMING LEVER HINGE COVER SPRING PER MM 52-12-00-201. OPS CHK NML PER SAME THIS CLEARS AUTH # 2501580. REMOVED PLACARD
- [SDR IPXA2023061680745](https://openairdocs.org/sdr/IPXA2023061680745.md): Unknown · unknown · Jun 16, 2023 · N331UP · Boeing 76734AF · Doors
  > *SDR FILED OPEN* MAIN ENTRY/DOOR ARMING LEVER HINGE COVER SPRING BROKEN.
- [SDR IPXA2023033192468](https://openairdocs.org/sdr/IPXA2023033192468.md): Unknown · warning message · Mar 30, 2023 · N331UP · Boeing 76734AF · Trailing Edge Flap Control System
  > INSPECTION TYPE:N/A**EMERGENCY DECLARED**TRAILING EDGE FLAP DISAGREE EICAS MSG AND LIGHT APPEARD WHEN FLAPS 5 SELECTED LIGHT EXTINGUISHED WHEN ALT TRAILING EDGE SWITCH PUSHED ON APPROACHPERFORMED FSEU BITE PROCEDURE FOUND FLT 0 SEC 3 DATA MSG NO 27-51333 IAW F
- [SDR IPXA2023031791916](https://openairdocs.org/sdr/IPXA2023031791916.md): Door · inoperative · Mar 16, 2023 · N331UP · Boeing 76734AF · Passenger/Crew Doors
  > INSPECTION TYPE:N/ACREW ENTRY DOOR: RH TRIM SEAL LOOSE - FALLSOUT FROM THE TOP.REPOSITIONED DISLODGED TRIM SEALS ON THE FWD SIDE OF THE CREW ENTRY DOOR IAW B767 MM 52-09-01.
- [SDR IPXA2022072284431](https://openairdocs.org/sdr/IPXA2022072284431.md): Flap · cracked · Jul 15, 2022 · N331UP · Boeing 76734AF · Leading Edge Devices
  > INSPECTION TYPE:C12CRACK ON SEAL STRIP (P/N: 114T2800-165) OF RH WING FIXED LEADING EDGE SKIN AT OSS 514.17.REPLACE I.A.W. 767-300F SRM 51-40-02-0G REV.83.02 AND BOEING DRAWING 114T2800 SHEET 5, REV. G.
- [SDR IPXA2022030379667](https://openairdocs.org/sdr/IPXA2022030379667.md): Flap · none · Mar 2, 2022 · N331UP · Boeing 76734AF · Trailing Edge Flap Control System
  > INSPECTION TYPE:NA**EMERGENCY DECLARED** **LANDED WITHOUT INCIDENT** ON APPROACH TE FLAP DISAGREE RAN CK LIST LANDED USING ALT SYSTEMTROUBLE SHOT TE DISAGREE MSG IAW FIM27-51-00-815-810 FIG5 BLOCKS 1THRU6 ALL 3 FSPM CARFD BITE GOOD SYSTEM CHECK OK. PERFORMED O
- [SDR IPXA2021042068441](https://openairdocs.org/sdr/IPXA2021042068441.md): Switch · inoperative · Apr 20, 2021 · N331UP · Boeing 76734AF · Emergency Lighting
  > INSPECTION TYPE:N/ADURING FLIGHT EMER LIGHT SWITCH OFF OVERHEAD MOVED TO THE ON POSITION THE GUARD IS CAUSING THE SWITCH TO THE OFF POSITION (INSTEAD OF REMAINING ARMED WITH THE GUARD CLOSED)REPOSITION GUARD RING OPS TEST OK IAW B767 MM 33 50 00

Next page: https://openairdocs.org/aircraft/N331UP/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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 = 'N331UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N331UP/reports

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