# Service difficulty reports: N341UP

A list on [N341UP](https://openairdocs.org/aircraft/N341UP.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 2 · 91 reports

- [SDR IPXA2026060273867](https://openairdocs.org/sdr/IPXA2026060273867.md): Seal Depressor · deformed · May 27, 2026 · N341UP · Boeing 76734AF · Fuselage Main, Structure
  > FOUND MAIN DECK SIDE CARGO DOOR UPPER - AFT SIDE DEPRESSOR SEAL DEFORM AND SCRATCH. INSTALLED THE DEPRESSOR SEAL. IAW AMM I.A.W AMM 20-11-00-910-802 REV.148.TORQUED THE SCREW TO 35 IN-LB. CONDITION CHECK NORMAL.
- [SDR IPXA2026060256189](https://openairdocs.org/sdr/IPXA2026060256189.md): Stiffener · cracked · May 26, 2026 · N341UP · Boeing 76734AF · Engine Thrust Reverser
  > CRACKED BRACKET, NR.2 ENG LT T/R FWD TORQUE BOX SUPPORT FITTING NEAR 9:30 AND 10:00 POS. REMOVED DAMAGE BRACKET I.A.W SRM 51-40-02-0G REV. 95. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G REV. 95 AND IPC 78-32-21 REV. 96.
- [SDR IPXA2026060257012](https://openairdocs.org/sdr/IPXA2026060257012.md): Former · cracked · May 26, 2026 · N341UP · Boeing 76734AF · Wing Main, Frame Structure
  > RIGHT WING OTBD L/E, NOSE FORMER CRACK, OSS 499.60. REMOVED DAMAGE FORMER IAW SRM 51-40-02-0G REV.95. INSTALL NEW FORMER I.A.W SRM 51-40-02-0G REV.95 AND DWG 114T2161 SH 4 REV.- AND SREO-50900-REQ001 REV.
- [SDR IPXA2026053056047](https://openairdocs.org/sdr/IPXA2026053056047.md): Attach Bracket · cracked · May 26, 2026 · N341UP · Boeing 76734AF · Wing, Attach Fittings
  > CRACK - BRACKET, L/H WING INBOARD L/E COMPARTMENT. (REPLACE) INSTALLED NEW BRACKET I.A.W SRM 51-40-02-0G REV. 95 AND BOEING DWG NO. 114T1240 SH. 6 REV. -.
- [SDR IPXA2026053056997](https://openairdocs.org/sdr/IPXA2026053056997.md): Attach Bracket · cracked · May 26, 2026 · N341UP · Boeing 76734AF · Wing, Attach Fittings
  > RIGHT WING INBOARD L/E CAVITY, PANEL RIB ATTACH BRACKET CRACK, ISS 285. (REPLACE) INSTALLED NEW BRACKET I.A.W SRM 51-40-02-0G REV. 95 AND BOEING DWG NO. 114T1240 SH. 6 REV. -.
- [SDR IPXA2026060158500](https://openairdocs.org/sdr/IPXA2026060158500.md): Skin · cracked · May 26, 2026 · N341UP · Boeing 76734AF · Trailing Edge Flaps
  > RIGHT WING OUTBOARD FLAP, INBOARD T/E END CAP SKIN, UPPER AND LOWER FOUND SKIN DAMAGE. I.A.W UPS SREO-70175-REQ001 REV. 1 PERFORM REPAIR.
- [SDR IPXA2026052956860](https://openairdocs.org/sdr/IPXA2026052956860.md): Support Angle · cracked · May 26, 2026 · N341UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > CRACKED ANGLE, NR 2 PYLON AFT FAIRING INNER AFT FRAME OTBD SIDE SUPPORT ANGLE.
- [SDR IPXA2026052957094](https://openairdocs.org/sdr/IPXA2026052957094.md): Angle · cracked · May 26, 2026 · N341UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > CRACKED ANGLE, NR 1 PYLON AFT FAIRING AFT INNER CAVITY INBD ANGLE CRACK. INSTALL NEW CLIP I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO:313T2303 SH 131 REV.- AND BOEING DWG NO: 313T2303 SH. 136 REV. -.
- [SDR IPXA2026052946995](https://openairdocs.org/sdr/IPXA2026052946995.md): Angle · cracked · May 25, 2026 · N341UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > THE BULK CARGO INBOARD ANGLE AT STA 1578 RBL 80 IS CRACKED. INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G REV. 95 AND BOEING DWG NO. 146T5650 SH. 5 REV. C
- [SDR IPXA2026052947168](https://openairdocs.org/sdr/IPXA2026052947168.md): Angle · unknown · May 25, 2026 · N341UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > THE BULK CARGO OUTBOARD ANGLE AT STA 1578 LBL 80 IS CRACKED. CONDITION CHECK NORMAL. INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G REV. 95 AND BOEING DWG NO. 146T5650 SH. 5 REV. C
- [SDR IPXA2026052947183](https://openairdocs.org/sdr/IPXA2026052947183.md): Angle · unknown · May 25, 2026 · N341UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > THE BULK CARGO INBOARD ANGLE AT BS 1578 LBL 80 IS CRACKED. CONDITION CHECK NORMAL. INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G REV. 95 AND BOEING DWG NO. 146T5650 SH. 5 REV. C
- [SDR IPXA2026060536086](https://openairdocs.org/sdr/IPXA2026060536086.md): Angle · cracked · May 24, 2026 · N341UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FOUND THE FIRE DETECTION LOOP FASTENER ANGLE CRACK AT STA 1562 LBL 76 IN BULK CARGO COMPARTMENT. INSTALLED FABRICATED ANGLE I.A.W SRM 51-40-02-0G REV. 95 AND BOEING DWG NO: 218T4100 SHEET 3 REV. B AND 218T4004 SH 23 REV F.
- [SDR IPXA2026052424821](https://openairdocs.org/sdr/IPXA2026052424821.md): Stiffener · cracked · May 23, 2026 · N341UP · Boeing 76734AF · Wing Miscellaneous Structure
  > CRACKED STIFFENER, FLOOR SUPPORT STRUCTURE STA 785.9 RBL 11. ACCOMPLISH THE REPAIR I.A.W SRM 57-10-10-2R-2 REV. 95 AND EGAT WORK SHEET NO: 60431 AND EO-58151-REQ001 REV1.
- [SDR IPXA2026052425094](https://openairdocs.org/sdr/IPXA2026052425094.md): Stiffener · cracked · May 23, 2026 · N341UP · Boeing 767300 · Fuselage Miscellaneous Structure
  > CRACKED STIFFENER, FLOOR SUPPORT STRUCTURE STA 785.9 LBL 55. ACCOMPLISH THE REPAIR I.A.W SRM 57-10-10-2R-2 REV. 95 AND EGAT WORK SHEET NO: 60432 AND EO-58151-REQ001 REV1.
- [SDR IPXA2026052425098](https://openairdocs.org/sdr/IPXA2026052425098.md): Stiffener · cracked · May 23, 2026 · N341UP · Boeing 767300 · Fuselage Miscellaneous Structure
  > CRACKED STIFFENER, FLOOR SUPPORT STRUCTURE STA 785.9 RBL 55. ACCOMPLISH THE REPAIR I.A.W SRM 57-10-10-2R-2 REV. 95 AND EGAT WORK SHEET NO: 60430 AND EO-58151-REQ001 REV1.
- [SDR IPXA2026052841073](https://openairdocs.org/sdr/IPXA2026052841073.md): Floor Panel · damaged · May 12, 2026 · N341UP · Boeing 76734AF · Fuselage Floor Panel
  > LOADER REPORT LOWER AFT CARGO R/H SIDE NEAR DOORWAY FLOOR PANEL EDGE DAMAGE 1. I.A.W. 767-300F SRM 53-00-50-2R-0 REV. 95 PERFORM REPAIR AS BELOW STEP.:CUT OUT THE DAMAGE AND CLEAN. MEASURE THE CUT OUT ( L: 3.7", W: 0.9", AT AFT EDGE, 3.5" FROM R/H EDGE).
- [SDR IPXA2024062474860](https://openairdocs.org/sdr/IPXA2024062474860.md): Housing · missing · Jun 22, 2024 · N341UP · Boeing 76734AF · Emergency Lighting
  > INTERIOR EMG LT. COVER PLATE MISSING LIGHT HOUSING, FWD MAIN ENT DOOR. R/R EMG. EXIT SIGN IAW AMM 33-51-01-022 AND -402. OPS CKS GOOD.
- [SDR IPXA2024052960336](https://openairdocs.org/sdr/IPXA2024052960336.md): Angle · cracked · May 26, 2024 · N341UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > CRACK - ANGLE BULK CARGO COMPARTMENT LEFT AREA STA 1578 LBL 60. I.A.W AMM 25-57-05-404-006 AND AMM 25-58-04-404-015 REV.142 RESTORED MAIN DECK CARGO HANDLING. JOB COMPLETED AND CONDITION CHECK NORMAL. REVIEW COMPLETED
- [SDR IPXA2024052960326](https://openairdocs.org/sdr/IPXA2024052960326.md): Angle · cracked · May 26, 2024 · N341UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > CRACK - ANGLE BULK CARGO COMPARTMENT RIGHT AREA STA 1578 RBL 60. I.A.W AMM 25-57-05-404-006 AND AMM 25-58-04-404-015 REV 142 RESTORED MAIN DECK CARGO HANDLING. JOB COMPLETED AND CONDITION CHECK NORMAL.
- [SDR IPXA2024052552655](https://openairdocs.org/sdr/IPXA2024052552655.md): None · none · May 25, 2024 · N341UP · Boeing 76734AF · Standard Practices/Structures
  > FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R.
- [SDR IPXA2024020712214](https://openairdocs.org/sdr/IPXA2024020712214.md): Skin · damaged · Oct 28, 2023 · N341UP · Boeing 76734AF · Leading Edge Devices
  > NR 6 SLAT DAMAGED- BROKEN SKIN SLAT CHANGE INSTALLED INBD SLAT #6 UP TO AND INCLUDING STEP H(15) PER AMM 27-81-01-424-143. C/W REMAINDER OF #6 L/E SLAT INSTALLATION REF AMM 27-81-01-424-143 ITEMS I-K(8). THIS COMPLETES SLAT INSTALL.
- [SDR IPXA2023103012214](https://openairdocs.org/sdr/IPXA2023103012214.md): Unknown · unknown · Oct 28, 2023 · N341UP · Boeing 76734AF · Leading Edge Devices
  > MAJOR REPAIR* #6 SLAT DAMAGED- BROKEN SKIN ASSIGNED EO-88575-PRELIM1 FOR TEMPORARY REPAIR INSTRUCTIONS. OPEN
- [SDR IPXA2023091872638](https://openairdocs.org/sdr/IPXA2023091872638.md): Light · inoperative · Sep 15, 2023 · N341UP · Boeing 76734AF · Emergency Lighting
  > EMERGENCY LIGHTS INOP R&R EMER SUPPLY BATTERY PACK IAW 767 AMM 33-51-07-002-006. OPS CHECK GOOD. IPC 33-51-07-32
- [SDR IPXA2022050681809](https://openairdocs.org/sdr/IPXA2022050681809.md): Stiffener · cracked · May 6, 2022 · N341UP · Boeing 76734AF · Wing Structure
  > INSPECTION TYPE:C6CRACK ON CENTER WING TANK STIFFENER(P/N:111T2008-12)ON STA 785.9, RBL 33.REPAIR I.A.W 767-300F SRM. 83.01, UPS EO B767-5740-58151-C.
- [SDR IPXA2022050881846](https://openairdocs.org/sdr/IPXA2022050881846.md): Floor Panel · damaged · May 2, 2022 · N341UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C6DAMAGE ON M/D CARGO FLOOR PANEL AT STA 287-412, LBL 11-RBL11.FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NO. B767-5320-9693-I
- [SDR IPXA2022041281120](https://openairdocs.org/sdr/IPXA2022041281120.md): Light · inoperative · Apr 12, 2022 · N341UP · Boeing 76734AF · Emergency Lighting
  > INSPECTION TYPE:NAEXTERIOR EMERGENCY LIGHT INOPRELAMPED EXTERIOR EMERGENCY LIGHT PER 767 MM 33-51-16-962-001. OPS CHECK NORMAL
- [SDR IPXA2020073108417](https://openairdocs.org/sdr/IPXA2020073108417.md): Seal · damaged · Jul 28, 2020 · N341UP · Boeing 76734AF · Passenger/Crew Doors
  > A LOUD HUMMING NOISE ORIGINATING CLOSE TO CREW ENTRY DOOR. STARTED AT 10000' ON CLIMB OUT AND EDED ABOUT 10000' ON DESCENT.CREW ENTRY DOOR SEALS INSPECTED AND CLEANED AMM 52-09-00. FOUND SMALL CUT IN AFT ACOUSTIC SEAL. SEAL REPAIRED IAW AMM 52-09-00-801. TASK
- [SDR IPXA2020072978304](https://openairdocs.org/sdr/IPXA2020072978304.md): Seal · cut · Jul 27, 2020 · N341UP · Boeing 76734AF · Passenger/Crew Doors
  > INSPECTION TYPE:N/AA LOUD HUMMING NOISE ORIGINATING CLOSE TO CREW ENTRY DOOR. STARTED AT 10000' ON CLIMB OUT AND EDED ABOUT 10000' ON DESCENT.CREW ENTRY DOOR SEALS INSPECTED AND CLEANED AMM 52-09-00. FOUND SMALL CUT IN AFT ACOUSTIC SEAL. SEAL REPAIRED IAW AMM
- [SDR IPXA2020080328554](https://openairdocs.org/sdr/IPXA2020080328554.md): Seal · not seated · Jul 25, 2020 · N341UP · Boeing 76734AF · Landing Gear Doors
  > GEAR DOOR VIBRATION ON CLIMB ACCELERATING TO 310KTS LOUD HUMMING AND VIBRATION OCCURS. SLOWED CLIMB SPEED TO 280KTS AND NOISE-VIBRATION WENT AWAY. ON DESCENT AT 310 KTS NOISE - VIBRATION RETURNEDINSPECTED DROOP OF THE FWD NOSE GEAR DOORS IAW AMM 32-22-02, NO D
- [SDR IPXA2019070744175](https://openairdocs.org/sdr/IPXA2019070744175.md): Skin · dented · Jul 7, 2019 · N341UP · Boeing 76734AF · Trailing Edge Flaps
  > INSPECTION TYPE:N/A RIGHT WING INBOARD AFT FLAP LOWER SURFACE DENT REPAIR 58 FROM INBOARD EDGE AND 2" FROM TRAILING EDGE. 1/2" DIAMETER AND.043 DEPTH. REPAIRED PER EO B767-5750-72225B. TRANS TO NRC 620420 **SUPPLEMENTAL SDR**REMOVED DAMAGED ON AFT INBOARD FLA
- [SDR IPXA2018083133417](https://openairdocs.org/sdr/IPXA2018083133417.md): Unknown · odor · Aug 31, 2018 · N341UP · Boeing 76734AF · Air Distribution System
  > MUSTY ODOR FROM AIR CONDTIONING IN COCKPIT, WHEN PACKS WERE ON, AND CONDENSATION IN OUTLETS BOTH PACKS, BITE CHECKED IAW AMM 21.51.00.5 NO LEAKS, THEN PACKS OPERATED AND CYCLED FROM HOT TO COLD CONDENSATION REMOVED AS ACFT WAS IN STORMY WEATHER FOR A COUPL
- [SDR IPXA2018030727224](https://openairdocs.org/sdr/IPXA2018030727224.md): Sensor · out of limits · Mar 6, 2018 · N341UP · Boeing 76734AF · Door Warning System
  > AIR TURNBACK DUE TO A FWD CARGO DOOR INDICATION. ACCOMPLISHED DMP 52-71-01-01 BY VERIFYING FWD LWR CARGO DOOR CLOSED, LATCHED, AND LOCKED. TROUBLESHOT IAW FIM 52-71-00-815-807, AND TC 52-000-101, FOUND S214 OUT OF SPECS. ADJUSTED, PRESSURIZED AIRCRAFT IA
- [SDR IPXA2017101622651](https://openairdocs.org/sdr/IPXA2017101622651.md): Blower · inoperative · Oct 15, 2017 · N341UP · Boeing 76734AF · Emergency Equipment
  > LEFT EVAS UNIT BLOWER INOPERATIVE. R & R THE EVAS UNIT IAW 25-69-00-401, OPS CHECKED GOOD.
- [SDR IPXA2017092121941](https://openairdocs.org/sdr/IPXA2017092121941.md): Escape Rope · loose · Sep 21, 2017 · N341UP · Boeing 76734AF · Emergency Equipment
  > WHEN OPENING THE CREW DOOR, THE EMERGENCY ROPE CAME OFF. THE DOOR WAS STUCK. INGRESS ROPE WAS PROPERLY FIXED AT CREW ENTRY DOOR LOCATION IAW AMM 25-61-04-402-013.
- [SDR IPXA2016021699491](https://openairdocs.org/sdr/IPXA2016021699491.md): Pawl · broken · Feb 15, 2016 · N341UP · Boeing 76734AF · Passenger/Crew Doors
  > CREW ENTRY DOOR HANDLE DIFFICULT TO MOVE, OPEN AND CLOSE, DOOR CLOSED IMPROPERLY, OUT OF SEQUENCE.REPOSITIONED UPPER PAWL AND UPPER CEILING PANEL. OPERATIONALLY CHECKED DOOR INSIDE AND OUT IAW AMM 52-12-00-201. OK FOR SERVICE.
- [SDR IPXA2015101094628](https://openairdocs.org/sdr/IPXA2015101094628.md): Shield · missing · Oct 10, 2015 · N341UP · Boeing 76734AF · Indicating/Recording System
  > CAPT'S EVAS CONTAINER IS MISSING DRIP SHIELD. INSTALLED NEW EVAS SPLASH GUARD REF AMM 25-69-00.
- [SDR IPXA2015061490136](https://openairdocs.org/sdr/IPXA2015061490136.md): Floor Panel · damaged · Jun 14, 2015 · N341UP · Boeing 76734AF · Fuselage Floor Panel
  > TWO DENTS, ONE INCH IN DIAMETER ON MCD FLOOR PANEL. FABRICATED A NEW FLOOR PANEL IAW EO B767-5320-9693H.
- [SDR IPXA2015061490140](https://openairdocs.org/sdr/IPXA2015061490140.md): Floor Panel · damaged · Jun 14, 2015 · N341UP · Boeing 76734AF · Fuselage Floor Panel
  > MAIN CARGO DECK FLOOR PANEL, HAS A ONE INCH IN DIAMETER HOLE. FABRICATED A NEW FLOOR PANEL IAW EO B767-5320-9693-H.
- [SDR IPXA2015060889951](https://openairdocs.org/sdr/IPXA2015060889951.md): Floor Panel · dented · Jun 8, 2015 · N341UP · Boeing 76734AF · Fuselage Floor Panel
  > MAIN CARGO DECK NR 2 AFT CENTER FLOOR PANEL HAS A ONE INCH SQUARE DENT. FABRICATED A NEW FLOOR PANEL IAW EO B767-5320-9693-H.
- [SDR IPXA2015060789909](https://openairdocs.org/sdr/IPXA2015060789909.md): Floor Panel · dented · Jun 7, 2015 · N341UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > MAIN CARGO DECK NR 2R AFT OTBD FLOOR PANEL DENTED 14.5". FABRICATED A NEW FLOOR PANEL IAW EO B767-5320-9693-H.
- [SDR IPXA2015060789901](https://openairdocs.org/sdr/IPXA2015060789901.md): Floor Panel · damaged · Jun 7, 2015 · N341UP · Boeing 76734AF · Fuselage Floor Panel
  > MAIN CARGO DECK 2R AFT OTBD FLOOR PANEL DENTED 14.5" LONG BY 1" DEEP, FABRICATED A NEW FLOOR PANEL IAW EO B767-5320-9693H.
- [SDR IPXA2015051989231](https://openairdocs.org/sdr/IPXA2015051989231.md): Control Panel · inoperative · May 19, 2015 · N341UP · Boeing 76734AF · Emergency Lighting
  > EMERGENCY LIGHTS INOPERATIVE, REF M33-51-1-1. REPLACED EMERGENCY LIGHT PANEL ASSY. OPS OK, REF AMM 33-51-08.
- [SDR IPXA2014031482250](https://openairdocs.org/sdr/IPXA2014031482250.md): Channel · damaged · Mar 12, 2014 · N341UP · Boeing 76734AF · Emergency Equipment
  > CREW ENTRANCE DOOR "SLIDE TAPE" RETENTION SLEEVE DAMAGED. R & R CREW DOOR INGRESS ROPE CHANNEL IAW AMM 25-61-04.
- [SDR IPXA3679981](https://openairdocs.org/sdr/IPXA3679981.md): Skin · damaged · Aug 25, 2013 · N341UP · Boeing 76734AF · Leading Edge Devices
  > .8 INCH HOLE IN NR 8 SLAT T/E WEDGE UPPER SKIN 45.8" FROM OTBD END AND 7.5" FWD OF T/E. REPAIRED IAW EO B767-5750-51892-A.
- [SDR IPXA2676481](https://openairdocs.org/sdr/IPXA2676481.md): Controller · inoperative · Dec 16, 2012 · N341UP · Boeing 76734AF · Cabin Pressure Controller
  > NO CABIN PRESSURIZATION AFTER DEPARTURE. COMPLETED CHECKLIST. FOUND NR 1 AUTO CABIN PRESSURE INOPERATIVE, WOULD NOT SELF TEST. R & R NR 1 AUTO PRESSURE CONTROLLER IAW AMM 21-31-02 AND IPC 21-31-02-01C. SYS CHECKS NORMAL.
- [SDR IPXA12674288](https://openairdocs.org/sdr/IPXA12674288.md): Skin · dented · Jul 6, 2012 · N341UP · Boeing 76734AF · Fuselage Main, Plate/Skin
  > INSPECTION TYPE: 1C, FUSELAGE AT BS 1916 LBL 3" AREA DENT IS FOUND DURING DMI D478160 RECTIFICATION. REPAIRED IAW RS R53-81-37375 REV A & EO B767-5330-47814-A, ORIG MATL: 2024T3-0016" 2 LAYERS BONDED SKIN ASSY. FINAL CUTOUT SIZE: 2" X 2.625", CLASSIFIED AS
- [SDR IPXA12674324](https://openairdocs.org/sdr/IPXA12674324.md): Wedge · dented · Jul 5, 2012 · N341UP · Boeing 76734AF · Trailing Edge Flaps
  > INSPECTION TYPE: 1C, LT WING OTBD T/E FLAP, T/E WEDGE, LOWER SURFACE DENTED. COMPOSITE PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A (1), FIG 9, REV 52.
- [SDR IPXA12674322](https://openairdocs.org/sdr/IPXA12674322.md): Wedge · dented · Jul 5, 2012 · N341UP · Boeing 76734AF · Trailing Edge Flaps
  > INSPECTION TYPE:1C LT WING OTBD T/E WEDGE UPPER SURFACE DENTED. COMPOSITE PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A(1), FIG 9, REV 52.
- [SDR IPXA12674318](https://openairdocs.org/sdr/IPXA12674318.md): Wedge · dented · Jul 5, 2012 · N341UP · Boeing 76734AF · Trailing Edge Flaps
  > INSPECTION TYPE: 1C, LT WING OTBD T/E FLAP, T/E WEDGE, UPPER SURFACE DENTED. COMPOSITE PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A(1), FIG 9, REV 52.
- [SDR IPXA12674316](https://openairdocs.org/sdr/IPXA12674316.md): Skin · dented · Jul 5, 2012 · N341UP · Boeing 76734AF · Trailing Edge Flaps
  > INSPECTION TYPE: 1C, LT WING OTBD T/E FLAP, T/E WEDGE UPPER SURFACE DENTED. COMPOSITE PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A(1), FIG 9, REV 52.

Next page: https://openairdocs.org/aircraft/N341UP/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 = 'N341UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N341UP/reports

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