# Service difficulty reports: N342UP

A list on [N342UP](https://openairdocs.org/aircraft/N342UP.md).

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

- [SDR IPXA2026091176660](https://openairdocs.org/sdr/IPXA2026091176660.md): Seal · leaking · Sep 10, 2026 · N342UP · Boeing 76734AF · Passenger/Crew Doors
  > ENTRY DOOR POTENTIAL SEAL LEAK, LEAKING NOISE MOST OF THE FLIGHT ALL ALTITUDES, SOUND APPEARS TO COME FROM BOTTOM OF DOOR FOUND SEALANT MISSING FROM SEAMS IN SILL PLATE. REPLACED SEALANT. PRESSURIZED A/C AND FOUND NO MORE LEAKAGE/NOISE FROM CREW ENTRY DOOR.
- [SDR IPXA2026091076660](https://openairdocs.org/sdr/IPXA2026091076660.md): Seal · leaking · Sep 10, 2026 · N342UP · Boeing 76734AF · Passenger/Crew Doors
  > ENTRY DOOR POTENTIAL SEAL LEAK, LEAKING NOISE MOST OF THE FLIGHT ALL ALTITUDES, SOUND APPEARS TO COME FROM BOTTOM OF DOOR PRESSURE CHECK ENTRY DOOR IAW AMM 05-51-24. FOUND LEAK COMING FROM THE BOTTOM OF THE DOOR.
- [SDR IPXA2026060872758](https://openairdocs.org/sdr/IPXA2026060872758.md): Test Button · inoperative · Jun 8, 2026 · N342UP · Boeing 76734AF · Detection System
  > WHEEL WELL FIRE DETECTION TEST DOESN'T WORK WHEN TEST BUTTON IN FLIGHTDECK PRESSED. T/S CARRIED OUT IAW FIM 26-17 FAULT TREE 803 REV. 148. FOUND WHEELWELL FIRE TEST BUTTON U/S. FIRE/OVERHEAT TEST PANEL REPLACED IAW AMM 26-11-01 PB. 401 REV. 148. POST INSTALLA
- [SDR IPXA2025102829407](https://openairdocs.org/sdr/IPXA2025102829407.md): Flap · damaged · Oct 24, 2025 · N342UP · Boeing 76734AF · Leading Edge Devices
  > BIRD STRIKE DAMAGE TO RIGHT WING OUTBOARD FLAP LEADING EDGE. COMPLETED REPAIR TO LEADING EDGE PANEL PER SRM 51-70-05-0G-0 ALL STEPS OF REPAIR COMPLETE. REPAIR PLIES INSTALLED AND CURED. REAPPLIED PROTECTIVE COATINGS AND PERFORM POST REPAIR REQUIREMENTS. INSTA
- [SDR IPXA2025102429407](https://openairdocs.org/sdr/IPXA2025102429407.md): Flap · damaged · Oct 24, 2025 · N342UP · Boeing 76734AF · Leading Edge Devices
  > BIRD STRIKE DAMAGE TO RIGHT WING OUTBOARD FLAP LEADING EDGE. REMOVED PANEL 666AT AND ROUTED TO SHEET METAL SHOP FOR REPAIR.
- [SDR IPXA2025062264991](https://openairdocs.org/sdr/IPXA2025062264991.md): Fmc · faulted · Jun 22, 2025 · N342UP · Boeing 76734AF · Flight Management Computing Hardware System
  > ATB FMC LOCKED UP WITH STBY ONE MSG PRESENT (FULL WRITEUP IN FAULT DESCRIPTION). + PERFORMED TROUBLE SHOOTING REF B767 FIM 34-61 FAULT TREE 854,NO FAULTS FOUND.REMOVED AND REPLACED L/H FMC REFB767AMM 34-61-01 9 (PRECAUTIONARY) OPS CHECK GOOD ATT.
- [SDR IPXA2025020716359](https://openairdocs.org/sdr/IPXA2025020716359.md): None · none · Feb 7, 2025 · N342UP · Boeing 76734AF · Standard Practices/Structures
  > ADD SDR FOR EO-82173-JIC001 (FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF STA 1725.5 BETWEEN S-36L AND S-36R) [T3F18E0013XJ0] ACCOMPLISHED SDR. REVIEWED.
- [SDR IPXA2025020220164](https://openairdocs.org/sdr/IPXA2025020220164.md): Skin · debonded · Feb 1, 2025 · N342UP · Boeing 76734AF · Leading Edge Devices
  > DISBOND PNL, RT WING NR 8 L/E SLAT INBD, SIDE INNER UPPER WEDGE. INST THE EXT DBLR WITH FILM ADHESIVE & CURE IAW SRM 51-70-10-2R-0 PARA 18 & 20. PERFORMED NDT/UT FOR REWORKED AREA & 8" FROM WHERE EDGES OF HEAT BLANKET, IAW NDT MANUAL PT1 51-01-01 & 51-04-00 R
- [SDR IPXA2025020491420](https://openairdocs.org/sdr/IPXA2025020491420.md): Angle · cracked · Jan 26, 2025 · N342UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FOUND THE ANGLE CRACK AT STA 1578 RBL 80 INBOARD IN BULK CARGO COMPARTMENT RIGHT AREA. (REPLACE). REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-0G REV.91. INSTALL NEW PARTS I.A.W SRM 51-40-02-0G REV.91 AND BOEING DWG NO. 146T5650 SHEET 5 REV:C. JOB COMPLETED.
- [SDR IPXA2025020491290](https://openairdocs.org/sdr/IPXA2025020491290.md): Angle · cracked · Jan 26, 2025 · N342UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FOUND THE ANGLE CRACK AT STA 1578 RBL 80 OUTBOARD IN BULK CARGO COMPARTMENT RIGHT AREA. (REPLACE). REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-0G REV.91. INSTALL NEW PARTS I.A.W SRM 51-40-02-0G REV.91 AND BOEING DWG NO. 146T5650 SHEET 5 REV:C. JOB COMPLETED. I.A.W
- [SDR IPXA2025020491462](https://openairdocs.org/sdr/IPXA2025020491462.md): Angle · cracked · Jan 26, 2025 · N342UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FOUND THE ANGLE CRACK AT STA 1578 LBL 80 OUTBOARD IN BULK CARGO COMPARTMENT LEFT AREA. (REPLACE). REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-0G REV.91 INSTALL NEW PARTS I.A.W SRM 51-40-02-0G REV.91 AND BOEING DWG NO. 146T5650 SHEET 5 REV:C. JOB COMPLETED. I.A.W A
- [SDR IPXA2025013192484](https://openairdocs.org/sdr/IPXA2025013192484.md): Floor Panel · damaged · Jan 26, 2025 · N342UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 146T5869-65 PANEL NO: 251JFF STA 1197+22~STA 1197+110 LBL 55~LBL 77. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 25-57-05-404-006 AND AMM 25-58-01-404-005 REV.144 INSTALLED M
- [SDR IPXA2025013192466](https://openairdocs.org/sdr/IPXA2025013192466.md): Floor Panel · damaged · Jan 26, 2025 · N342UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 146T5869-9 PANEL NO: 241KFF STA 1197+22~STA 1197+110 LBL 77~LBL 88. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 25-57-05-404-006, AMM 25-58-04-404-015 AND AMM 25-58-01-404-00
- [SDR IPXA2025013192454](https://openairdocs.org/sdr/IPXA2025013192454.md): Floor Panel · damaged · Jan 26, 2025 · N342UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 145T5876-68 PANEL NO: 241AFF STA 731~STA 834 LBL 11~RBL 11. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 25-57-05-404-006, AMM 25-58-01-404-005 AND AMM 25-58-03-404-004 REV.14
- [SDR IPXA2025013192451](https://openairdocs.org/sdr/IPXA2025013192451.md): Floor Panel · damaged · Jan 26, 2025 · N342UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 146T5869-135 PANEL NO: 251XFF STA 1440~STA 1540 LBL 77.5~LBL 54.75. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 25-57-05-404-006, AMM 25-58-04-404-015, AMM 25-58-01-404-005 A
- [SDR IPXA202403040049](https://openairdocs.org/sdr/IPXA202403040049.md): Pitot Head · damaged · Feb 21, 2024 · N342UP · Boeing 76734AF · Pitot/Static Anti-Ice System
  > LUZ DE CAPT PITOT ENCENDIDA DESPUES DEL ARRANQUE DE MOTORES, PROBETA DE TUBO PITOT DEL CAPITAN DAÑADA CAPT PITOT LIGHT ON AFTER STARTING, PITOT TUBE DAMAGED.
- [SDR IPXA2023012690278](https://openairdocs.org/sdr/IPXA2023012690278.md): Floorbeam · damaged · Jan 13, 2023 · N342UP · Boeing 76734AF · Fuselage Main, Floor Beam
  > INSPECTION TYPE:C6, DAMAGE ON M/D CARGO FLOORBEAM, BS 246, LBL 53. FABRICATED A REPLACEMENT IAW DWG 141T5146 SH 15 REV B, PL REV F AND PSDL REV-. REPLACED IAW SRM 51-40-02-0G-0 REV. 85.01.
- [SDR IPXA2022112888472](https://openairdocs.org/sdr/IPXA2022112888472.md): Seal · detached · Nov 28, 2022 · N342UP · Boeing 76734AF · Passenger/Crew Doors
  > INSPECTION TYPE:N/ACREW ENTRY DOOR SEAL MAKES VERY LOUD HISSING NOISE IN FLIGHT.PRESSURISATION OKAYFOUND CREW ENTRY DOOR BOTTOM SEAL DETACHED SECURED AND CLEANED DOOR SEAL PER AMM 52-09-01-424-019 FOUND SATIS
- [SDR IPXA2021121777022](https://openairdocs.org/sdr/IPXA2021121777022.md): Apu · faulted · Dec 16, 2021 · N342UP · Boeing 76734AF · APU Cowling/Containment
  > INSPECTION TYPE:N/ASUPPLEMENTAL SDR**DIVERSION**EMERG DECLARED**A/C LANDED W/OUT INCIDENT**APU FAULT AT FL 390 DIVERTED TO STL. DEFERRED PER MEL 49-11-1A ASSIGNED M766577REPLACED APU COOLING FAN AMM 49-51-03-401 AND APU OIL COOLER AMM 49-27-09-404-011. OPS & L
- [SDR IPXA2020051355257](https://openairdocs.org/sdr/IPXA2020051355257.md): Tire · damaged · May 12, 2020 · N342UP · Boeing 76734AF · Tire
  > INSPECTION TYPE:N/A** EMERGENCY DECLARED ** THE FIRE TRUCKS FOLOWED THE A/C TO THE RAMP & THE FIRE CHIEF DETERMINED IT WAS SAFE TO TAXI TO THE GATE & FOLLOWED THE AIRCRAFT TO THE GATE ** # 7 MLG TIRE HEATSHIELD DAMAGED.R & R'D # 7 MAIN WHEEL ASSY IAW MM 32-45
- [SDR IPXA2020051155077](https://openairdocs.org/sdr/IPXA2020051155077.md): Control Module · inoperative · May 7, 2020 · N342UP · Boeing 76734AF · Rudder Tab Control System
  > INSPECTION TYPE:N/AHYDRAULIC POWER CAME ON PRIOR TO ENGINE START ON PUSHBACK, BOTH YOKES WENT 3/4 FULL LEFT TURN FOR NO REASON. A/P OFF.R/R AILERON RUDDER TRIM AILERON CONTROL MODULE PER AMM 27-21-23-022-001 & 27-21-23-422-007 OPS TEST AILERON & AILERON TRIM C
- [SDR IPXA2019091046567](https://openairdocs.org/sdr/IPXA2019091046567.md): Battery Pack · discharged · Sep 10, 2019 · N342UP · Boeing 76734AF · Emergency Lighting
  > INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INOP. R&R BATT PACK PER AMM 33-51-07 OPS CHK GOOD. ESR: IPC 33-51-07-32.
- [SDR IPXA2019040864843](https://openairdocs.org/sdr/IPXA2019040864843.md): Bulb · inoperative · Apr 6, 2019 · N342UP · Boeing 76734AF · Emergency Lighting
  > EXTERIOR EMERGENCY LIGHT INOP. REPLACED THE BULB IAW AMM 33-51-16-962-001 OPS CKS OK
- [SDR IPXA2019012338207](https://openairdocs.org/sdr/IPXA2019012338207.md): Skin Panel · broken · Jan 13, 2019 · N342UP · Boeing 76734AF · Wing, Plate/Skin
  > INSPECTION TYPE:C4 BROKEN ON LOWER SKIN PANEL OF RT WING INBD AFT FLAP NEAR IFS 119.75. REPAIR IAW SRM 57-53-01 REPAIR 1, SRM 51-70-10 REPAIR 2, SRM 51-70-10 GENERAL, SRM 51-70-03 GENERAL, REV.73.01
- [SDR IPXA2019011837983](https://openairdocs.org/sdr/IPXA2019011837983.md): Floor Panel · damaged · Jan 13, 2019 · N342UP · Boeing 76734AF · Fuselage Floor Panel
  > INSPECTION TYPE:C4 DAMAGE ON M/D CARGO FLOOR PANEL AT STA 834-STA 930, LBL 11 - RBL 11, PNL NR 241FFF. FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NR B767-5320-9693-I.
- [SDR IPXA2019010737587](https://openairdocs.org/sdr/IPXA2019010737587.md): Light · inoperative · Dec 8, 2018 · N342UP · Boeing 76734AF · Emergency Lighting
  > INSPECTION TYPE:N/A EXTERIOR EMERGENCY LIGHT INOP. R&R LAMP W/ REF TO AMM. 33-51-16. LIGHT OPERATES NORMAL P/N ON/OFF 767.
- [SDR IPXA2016062605049](https://openairdocs.org/sdr/IPXA2016062605049.md): Floor Panel · punctured · Jun 26, 2016 · N342UP · Boeing 76734AF · Fuselage Floor Panel
  > MCD FLOOR PANEL PUNCTURED POSITION 2R, FABRICATED NEW PANEL IAW EO B767-5320-9693-I.
- [SDR IPXA2015120896506](https://openairdocs.org/sdr/IPXA2015120896506.md): Fire Loop · malfunctioned · Dec 7, 2015 · N342UP · Boeing 76734AF · Fire Detection
  > RIGHT ENGINE FIRE LOOP 1 STATUS MESSAGE. REPLACED THE RT FWD LOWER FIRE LOOP DETECTOR IAW AMM 26-11-02 AND TESTED NORMAL.
- [SDR IPXA2015032287255](https://openairdocs.org/sdr/IPXA2015032287255.md): Skin · damaged · Mar 21, 2015 · N342UP · Boeing 76734AF · Cargo/Baggage Doors
  > DURING MAJOR MAINTENANCE VISIT NR 6749, FOUND DENT ON SKIN, BULK CARGO DOOR OUTER SURFACE, STA 1447, BETWEEN S-23L AND S-24 L/E, EVALUATED DAMAGE IAW SRM 52-30-01-1A-1, FIG 101, REF: TAIL VI, REV 61.00 INFORMATION SUBMITTED FOR ADM, DENT WITHIN ALLOWABLE DAMAG
- [SDR IPXA2014011001250](https://openairdocs.org/sdr/IPXA2014011001250.md): Lamp · inoperative · Jan 7, 2014 · N342UP · Boeing 76734AF · Emergency Lighting
  > EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP.
- [SDR IPXA2014010201191](https://openairdocs.org/sdr/IPXA2014010201191.md): Latch · broken · Dec 29, 2013 · N342UP · Boeing 76734AF · Emergency Equipment
  > CAPTAIN'S OVERHEAD ESCAPE ROPE DOOR LATCH INOPERATIVE. OVERHEAD PANEL ASSY R & R IAW AMM TASK 25-1 4-02. ROPE INSTALLED IAW AMM TASK 25-61-02-682-001, REV 110, 02.
- [SDR IPXA3680327](https://openairdocs.org/sdr/IPXA3680327.md): Floor Panel · damaged · Sep 21, 2013 · N342UP · Boeing 76734AF · Fuselage Floor Panel
  > FLOOR PANEL DAMAGED. REPAIRED IAW SRM 53-00-50.
- [SDR IPXA3677437](https://openairdocs.org/sdr/IPXA3677437.md): Skin · dented · Mar 4, 2013 · N342UP · Boeing 76734AF · Leading Edge Devices
  > INSPECTION TYPE:C01, A DENT WAS FOUND ON LT WING NR 3 SLAT UPPER SURFACE OF WEDGE AREA. DAMAGE SIZE IS MEASURED AS 1.75"(LENGTH) X 1.5"(WIDTH) X 0.031"(DEPTH) AT OSS 807. REPAIRED IAW SRM 57-43-02, REPAIR 1 AND 51-70-10, REPAIR 4, FIG 201, REV 55.
- [SDR IPXA3677436](https://openairdocs.org/sdr/IPXA3677436.md): Skin · dented · Mar 4, 2013 · N342UP · Boeing 76734AF · Leading Edge Devices
  > INSPECTION TYPE:C01, A DENT WAS FOUND ON LT WING NR 3 SLAT UPPER SURFACE OF WEDGE AREA. DAMAGE SIZE MEASURED AS 0.88" (LENGTH) X 0.62"(WIDTH) X 0.025" (DEPTH) AT OS S 804.5 REPAIR IAW SRM 57-43-02, REPAIR 1 AND 51-70-10, REPAIR 4, FIG 201, REV 55.
- [SDR IPXA3677435](https://openairdocs.org/sdr/IPXA3677435.md): Skin · dented · Mar 4, 2013 · N342UP · Boeing 76734AF · Leading Edge Devices
  > INSPECTION TYPE:C01, A DENT WAS FOUND ON LT WING NR 3 SLAT UPPER SURFACE OF WEDGE AREA. DAMAGE SIZE MEASURED AS 0.62" (LENGTH) X 0.55" (WIDTH) X 0.012"(DEPTH) AT OSS 805.5 REPAIRED IAW SRM 57-43-02, REPAIR 1 AND 51-70-10, REPAIR 4, FIG 201, REV 55.
- [SDR IPXA3677434](https://openairdocs.org/sdr/IPXA3677434.md): Skin · dented · Mar 4, 2013 · N342UP · Boeing 76734AF · Leading Edge Devices
  > A DENT WAS FOUND ON LT WING NR 3 SLAT UPPER SURFACE OF WEDGE AREA. DAMAGE SIZE IS MEASURED AS 0.78" (LENGTH) X 0.55" (WIDTH) X 0.012" (DEPTH) AT OSS 801.5. REPAIR IAW 767-300F SRM 57-43-02, REPAIR 1 AND 51-70-10, REPAIR 4, FIG 201, REV 55.
- [SDR IPXA3677431](https://openairdocs.org/sdr/IPXA3677431.md): Wedge · dented · Mar 4, 2013 · N342UP · Boeing 76734AF · Leading Edge Devices
  > INSPECTION TYPE:C01, LT WING NR 3 SLAT T/E WEDGE ASSY UPPER SKIN DENTED AT OSS 819. DAMAGE SIZE IS MEASURED AS 1.0" (LENGTH) X 0.66"(WIDTH) X 0.013"(DEPTH) AND THE CUT OUT IS MEASURED AS 1" DIAMETER. REPAIR IAW SRM 57-43-02, REPAIR 1 AND 51-70-10, REPAIR 4 FI
- [SDR IPXA2676466](https://openairdocs.org/sdr/IPXA2676466.md): Floor Panel · dented · Dec 15, 2012 · N342UP · Boeing 76734AF · Fuselage Floor Panel
  > MAIN CARGO DECK FLOOR PANEL POS NR 12L OTBD HAS DENT CENTER OF PANEL. REPAIRED IAW SRM 53-00-50-2R.
- [SDR IPXA2672017](https://openairdocs.org/sdr/IPXA2672017.md): Floor Panel · damaged · Mar 4, 2012 · N342UP · Boeing 76734AF · Fuselage Floor Panel
  > MAIN CARGO FLOOR PANEL HAS A 3" BY 1" HOLE AT POS 6/7 PANEL CENTER, IDENTIFIED PANEL FROM POS 6/7 CENTER AS PN 145T5876-60 IAW EO B767-5320-9693H. FABRICATED A REPLACEMENT PANEL FROM A402H ACCOMPLISHED PARA B, STEP 5 & 6 REF EO B767-5320--9693-H.
- [SDR IPXA2672016](https://openairdocs.org/sdr/IPXA2672016.md): Floor Panel · damaged · Mar 4, 2012 · N342UP · Boeing 76734AF · Fuselage Floor Panel
  > MAIN CARGO COMPARTMENT FLOOR PANEL HAS A 3" BY 1" HOLE AT POSITION 4/5 CENTER PANEL 31" AFT OF POS 4. IDENTIFIED PANEL FROM POSITION 4/5 CENTER AS PN 143T5876-112 IAW EO B767-5320-9693 H. FABRICATED A REPLACEMENT PANEL FROM A402H ACCOMPLISHED PARA B, STEP 5 &
- [SDR IPXA2672015](https://openairdocs.org/sdr/IPXA2672015.md): Floor Panel · damaged · Mar 4, 2012 · N342UP · Boeing 76734AF · Fuselage Floor Panel
  > MAIN CARGO COMPARTMENT FLOOR PANEL HAS A.5" DIAMETER HOLE AT POSITION 4/5 CENTER PANEL, 59" FWD FROM POS 4. IDENTIFIED PANEL FROM POS 4/5 CENTER AS PN 143T5876-112 IAW EO B767-5320-9693H, FABRICATED A REPL PANEL FROM A402H ACCOMPLISHED PARA B STEP 5&6 REF EO

## 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 = 'N342UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N342UP/reports

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