# Service difficulty reports: N348UP

A list on [N348UP](https://openairdocs.org/aircraft/N348UP.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 · 58 reports

- [SDR IPXA2026031363475](https://openairdocs.org/sdr/IPXA2026031363475.md): Receiver · missing · Mar 7, 2026 · N348UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > MISSING BUSHING, NR 2 ENGINE LT FAN COWL, LWR MID BRACKET. INSTALLED A NEW RECEIVER ASSY IAW SRM 51-40-02-0G, REV 94, AND CMM IPL 71-13-21 REV.47.
- [SDR IPXA2026031047781](https://openairdocs.org/sdr/IPXA2026031047781.md): Bracket · chafed · Mar 6, 2026 · N348UP · Boeing 76734AF · Engine Thrust Reverser
  > CHAFED BRACKET, NR 2 ENG RT THRUST REVERSER LWR FAIRING T/E AREA. INSTALL A NEW BRACKET IAW SRM 51-40-02-0G, REV 94, AND ST ENGINEERING IPC 78-32-22 REV.94.
- [SDR IPXA2026031047970](https://openairdocs.org/sdr/IPXA2026031047970.md): Door · chafed · Mar 6, 2026 · N348UP · Boeing 76734AF · Engine Thrust Reverser
  > CHAFED DOOR, NR 2 ENG RT THRUST REVERSER BLOW OUT DOOR L/E AREA. INSTALL NEW BLOWOUT DOOR IAW SRM 51-40-02-0G REV.94 AND ST ENGINEERING IPC 78-32-22 REV.94 AND AIPC 78-31-51-03 REV.141. REVIEW COMPLETE
- [SDR IPXA2026031246369](https://openairdocs.org/sdr/IPXA2026031246369.md): Former · cracked · Mar 6, 2026 · N348UP · Boeing 76734AF · Wing Main, Frame Structure
  > CRACKED FORMER, LEFT WING LEADING EDGE CAVITY STRUCTURE LES 565. INSTALLED A NEW FORMER IAW SRM 51-40-02-0G, REV 94, AND DWG 114T2162, SHT 6, REV -, AND SREO-50900-REQ001, REV 2.
- [SDR IPXA2026031247725](https://openairdocs.org/sdr/IPXA2026031247725.md): Plate · worn · Mar 6, 2026 · N348UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > WORN PLATE, NR 1 ENG LT CORE COWL INNER AFT FRAME LOWER PLATE. INSTALLED A NEW PLATE IAW SRM 51-40-02-0G, REV 94, & CMM IPL 71-13-23 REV 47.
- [SDR IPXA2026031247676](https://openairdocs.org/sdr/IPXA2026031247676.md): Hinge · worn · Mar 6, 2026 · N348UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > WORN HINGE, NR 1 PYLON STRUT PRESSURE RELIEF DOOR 434AR UPPER HINGE. INSTALLED NEW HINGE IAW SRM 51-40-02-0G, REV 94, DWG 311T1064, SHT 1, REV G, & DWG 311T1064, SHT 2, REV E.
- [SDR IPXA2026031347798](https://openairdocs.org/sdr/IPXA2026031347798.md): Bracket · chafed · Mar 6, 2026 · N348UP · Boeing 76734AF · Engine Thrust Reverser
  > CHAFED BRACKET, NR 1 ENG LT THRUST REVERSER LOWER CLOSURE PANEL AFT SIDE BRACKET. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 94 AND ST ENGINEERING IPC 78-32-21 REV.94.
- [SDR IPXA2026031145649](https://openairdocs.org/sdr/IPXA2026031145649.md): Bracket · chafed · Mar 6, 2026 · N348UP · Boeing 76734AF · Engine Thrust Reverser
  > CHAFED BRACKET, NR 1 ENG RT THRUST REVERSER AFT ACCESS DOOR FWD EDGE (REPLACE). INSTALL NEW BRACKET I.A.W SRM 51-40-02-0G REV.94 AND ST ENGINEERING IPC 78-32-22 REV.94. REVIEW COMPLETE
- [SDR IPXA2026030943700](https://openairdocs.org/sdr/IPXA2026030943700.md): Former · cracked · Mar 6, 2026 · N348UP · Boeing 76734AF · Wing Main, Frame Structure
  > CRACKED FORMER, LEFT WING LEADING EDGE CAVITY STRUCTURE OSS 499. INSTALL NEW FORMER IAW SRM 51-40-02-0G REV.94 AND DWG 114T2161 SH 6 REV: - AND SREO-50900-REQ001 REV2.
- [SDR IPXA2026031245725](https://openairdocs.org/sdr/IPXA2026031245725.md): Longeron · chafed · Mar 6, 2026 · N348UP · Boeing 76734AF · Nacelle/Pylon, Longeron/Stringer
  > CHAFED LONGERON, NR 1 ENG LT CORE COWL LOWER LONGERON. INSTALLED NEW LONGERON IAW SRM 51-40-02-0G REV. 94 AND CMM IPL 71-13-23 REV. 47.
- [SDR IPXA2026031348628](https://openairdocs.org/sdr/IPXA2026031348628.md): Bracket · cracked · Mar 6, 2026 · N348UP · Boeing 76734AF · Wing, Attach Fittings
  > CRACKED BRACKET, LEFT WING NR 4 SLAT INBOARD SIDE ROTARY ACTUATOR ROD LOWER SEAL DOOR FORWARD SUPPORT BRACKET. IAW AMM 20-11-00-910-802 REV.147 REPLACE BRACKET.
- [SDR IPXA2026031349916](https://openairdocs.org/sdr/IPXA2026031349916.md): Door · cracked · Mar 6, 2026 · N348UP · Boeing 76734AF · Wing Main, Frame Structure
  > CRACKED DOOR, LOWER SURFACE OF LEFT WING LEADING EDGE LOWER 521ABB PANEL. IAW AMM 20-11-00-910-802 REV.147 REPLACED DOOR ASSEMBLY.
- [SDR IPXA2026031346226](https://openairdocs.org/sdr/IPXA2026031346226.md): Bracket · cracked · Mar 6, 2026 · N348UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > CRACKED BRACKET, NR 1 PYLON AFT FAIRING INTERNAL HYD SYS VENT TUBE SUPPORT BRACKET NAC STA 350. INSTALL FABRICATE BRACKET I.A.W SRM 51-40-02-0G REV.94 AND DWG NO: 313T2380 SHEET 184 REV-.
- [SDR IPXA2026031246244](https://openairdocs.org/sdr/IPXA2026031246244.md): Bracket · cracked · Mar 6, 2026 · N348UP · Boeing 76734AF · Auxiliary Power Unit (APU) Doors
  > CRACKED BRACKET, LT APU DOOR NR1 SUPPORT FROM FORWARD EDGE. REPLACED, CHECKED OK. INSTALLED NEW BRACKET I.A.W SRM 51-40-02-0G REV. 94 AND BOEING DWG NO. 355T5200 SH. 1 REV. A.
- [SDR IPXA2026031246143](https://openairdocs.org/sdr/IPXA2026031246143.md): Bracket · worn · Mar 6, 2026 · N348UP · Boeing 76734AF · Auxiliary Power Unit (APU) Doors
  > WORN BRACKET, LT APU DOOR NR 2 SUPPORT FROM FORWARD EDGE. CHECKED OK. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G REV. 94 AND DWG 355T5200 SH. 1 REV. A.
- [SDR IPXA2026031329791](https://openairdocs.org/sdr/IPXA2026031329791.md): Rod · worn · Mar 5, 2026 · N348UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > WORN RECEIVER, NR 1 ENG LT CORE COWL HOLD OPEN ROD. REMOVED DAMAGE RECEIVER IAW SRM 51-40-02-0G REV.94 2.INSTALL NEW RECEIVER IAW SRM 51-40-02-0G REV.94 AND AEROSTRUCTURES CMM IPL 71-13-23 REV.47 3.
- [SDR IPXA2026031229860](https://openairdocs.org/sdr/IPXA2026031229860.md): Bracket · worn · Mar 5, 2026 · N348UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > WORN BRACKET, NR 2 ENG LT CORE COWL WELD ASSY. REMOVED DAMAGE BRACKET I.A.W SRM 51-40-02-0G REV.94. INSTALL NEW BRACKET IAW SRM 51-40-02-0G REV.94 AND CMM IPL 71-13-23 REV.47.
- [SDR IPXA2026031327022](https://openairdocs.org/sdr/IPXA2026031327022.md): Bracket · worn · Mar 5, 2026 · N348UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > WORN BRACKET, NR 1 PYLON AFT FAIRING HOLD OPEN ROD UNIVERSAL JOINT AREA. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G REV.94 AND DWG 313T2303 SHT 135 REV-.
- [SDR IPXA2026031128598](https://openairdocs.org/sdr/IPXA2026031128598.md): Angle · cracked · Mar 5, 2026 · N348UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > CRACKED ANGLE, NR 1 PYLON AFT FAIRING INTERNAL BULKHEAD NAC STA 376 INBD SIDE. INSTALLED NEW ANGLE IAW SRM 51-40-02-0G REV. 94, DWG 313T2303, SHT 136, REV -, & DWG 313T2303, SHT 131, REV -.
- [SDR IPXA2026031028599](https://openairdocs.org/sdr/IPXA2026031028599.md): Angle · cracked · Mar 5, 2026 · N348UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > CRACKED ANGLE, NR 1 PYLON AF FAIRING INTERNAL BULKHEAD NAC STA 376 OTBD SIDE. INSTALLED A NEW ANGLE IAW SRM 51-40-02-0G, REV 94, & DWG 313T2303, SHT 136, REV-, & DWG 313T2303, SHT 131, REV.
- [SDR IPXA2026030906568](https://openairdocs.org/sdr/IPXA2026030906568.md): Support Bracket · cracked · Mar 4, 2026 · N348UP · Boeing 76734AF · Wing, Attach Fittings
  > CRACKED TORQUE TUBE SUPPORT BRACKET OF THE LT WING LEADING EDGE COMPARTMENT. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 94, & DWG 114T1240, SHT 6, REV -.
- [SDR IPXA2026031289808](https://openairdocs.org/sdr/IPXA2026031289808.md): Bracket · cracked · Mar 3, 2026 · N348UP · Boeing 76734AF · Engine Thrust Reverser
  > CRACKED BRACKET, NR 2 ENG LT THRUST REVERSER FWD TORQUE BOX SUPPORT BRACKET NEAR 11:00 POSITION. INSTALLED A NEW STIFFENR IAW SRM 51-40-02-0G, REV 94, AND AIPC 78-31-00-55, REV 141.
- [SDR IPXA2026031289779](https://openairdocs.org/sdr/IPXA2026031289779.md): Stiffener · cracked · Mar 3, 2026 · N348UP · Boeing 76734AF · Engine Thrust Reverser
  > CRACKED BRACKET, NR 2 ENG RT THRUST REVERSER FWD TORQUE BOX SUPPORT BRACKET NEAR 3:00 POSITION. INSTALLED A NEW STIFFENR IAW SRM 51-40-02-0G, REV 94, AND AIPC 78-31-00-60, REV 141.
- [SDR IPXA2026031089949](https://openairdocs.org/sdr/IPXA2026031089949.md): Angle · cracked · Mar 3, 2026 · N348UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > CRACKED ANGLE, NR 2 PYLON AFT FAIRING INNER AFT FRAME INBD SIDE SUPPORT CLIP. INSTALLED A NEW CLIP I.A.W SRM 51-40-02-0G REV.94 AND DWG 313T2303, SH 136, REV -, & DWG 313T2303, SH 131, REV -.
- [SDR IPXA2026030973683](https://openairdocs.org/sdr/IPXA2026030973683.md): Battery · inoperative · Mar 2, 2026 · N348UP · Boeing 76734AF · Emergency Lighting
  > **SUPPLEMENTAL SDR** FAULT - FOUND EMERGENCY LIGHT DID NOT STAY ON FOR 15 MINUTES (REPLACE). I.A.W AMM 33-51-07-022-001, 33-51-07-422-012 REV. 147 REPLACED THE BATTERY PACK, AND CONDITION CHECK NORMAL. REVIEW COMPLETE
- [SDR IPXA2026030874565](https://openairdocs.org/sdr/IPXA2026030874565.md): Seat Track · worn · Mar 2, 2026 · N348UP · Boeing 76734AF · Fuselage, Seat/Cargo Attach Fittings
  > FOUND SEAT TRACK ASSY INBOARD AFT OF FIRST OFFICER SEAT WORN, POSITION (REPLACE) 1. I.A.W AMM 25-11-01-822-095-001 REV.147, REPLACED TRACK ASSY. JOB COMPLETED AND CONDITION CHECK NORMAL.
- [SDR IPXA2026030273683](https://openairdocs.org/sdr/IPXA2026030273683.md): Light · no test · Mar 2, 2026 · N348UP · Boeing 76734AF · Emergency Lighting
  > FOUND EMERGENCY DID NOT STAY ON FOR 15 MINUTES.
- [SDR IPXA2025041809621](https://openairdocs.org/sdr/IPXA2025041809621.md): Floor Panel · cracked · Mar 18, 2025 · N348UP · Boeing 76734AF · Fuselage Floor Panel
  > *** SUPPLEMENTAL SDR *** LOAD CREW REPORTS MCD FLOOR AT POS 14R CRACKED INSTALLED AFFECTED CARGO LOCK BETWEEN POS 12 AND 14 RIGHT PER AMM 25-58-01. INSTALLED AFFECTED ROLLER RAILS AT POS 12 AND 14 RIGHT PER AMM 25-57-05. INSTALLED AFFECTED BALL TRAYS AT POS 12
- [SDR IPXA2025031809621](https://openairdocs.org/sdr/IPXA2025031809621.md): Floor Panel · cracked · Mar 18, 2025 · N348UP · Boeing 76734AF · Fuselage Floor Panel
  > LOAD CREW REPORTS MCD FLOOR AT POS 14R CRACKED INSTALLED NEW FABRICATED FLOOR PANEL AT POS 14R PER AMM 53-01-06 UP TO AND INCLUDING STEP F. (21). WAITING ON SEALANT TO CURE, WILL REQ MOISTURE BARRIER TAPE AND LOCK/ROLLER INSTALL ONCE CURED. OPEN
- [SDR IPXA2024122675823](https://openairdocs.org/sdr/IPXA2024122675823.md): Window · damaged · Dec 24, 2024 · N348UP · Boeing 76734AF · Flight Compartment Windows
  > CAPTAINS SIDE WINDOW L2 HAD FLICKERING LIGHT ON BOTTOM EDGE MIDDLE. SHUT OFF LEFT SIDE WINDOW HEAT AND IT STOPPED AND COOLED. WAS TOO HOT TO TOUCH WHEN FLICKERING. COMPLETED REMOVAL AND REPLACEMENT OF L3 WINDOWS WITH REF TO MM 56-11-10-401. VERIFIED TORQUES AN
- [SDR IPXA2024122475823](https://openairdocs.org/sdr/IPXA2024122475823.md): Heater · faulted · Dec 24, 2024 · N348UP · Boeing 76734AF · Windshield/Door Rain/Ice Removal
  > *SDR FILED OPEN* CAPTAINS SIDE WINDOW L2 HAD FLICKERING LIGHT ON BOTTOM EDGE MIDDLE. SHUT OFF LEFT SIDE WINDOW HEAT AND IT STOPPED AND COOLED. WAS TOO HOT TO TOUCH WHEN FLICKERING.€? COMPLIED WITH STEPS D-1 THROUGH D-4 OF 767 AMM 56-11-10 FOR L3 WINDOW REMOVA
- [SDR IPXA2024020284515](https://openairdocs.org/sdr/IPXA2024020284515.md): Skin Panel · dented · Jan 29, 2024 · N348UP · Boeing 76734AF · Fuselage Main, Plate/Skin
  > MAJOR REPAIR, DENT, FUSELAGE SKIN BETWEEN STA 360 - STA 384, S-16L - S-17L (REPAIR). ACCOMPLISHED REPAIR IAW SRM 53-00-01-2R-12 REV.88 AND EO-89370-REQ 1 REV. 1. JOB COMPLISHED. REVIEW COMPLETE
- [SDR IPXA2024020571729](https://openairdocs.org/sdr/IPXA2024020571729.md): None · none · Jan 28, 2024 · N348UP · Boeing 76734AF · Standard Practices/Structures
  > FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R. ACCOMPLISHED SDR.
- [SDR IPXA2024012971729](https://openairdocs.org/sdr/IPXA2024012971729.md): None · none · Jan 28, 2024 · N348UP · Boeing 76734AF · Standard Practices/Structures
  > **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) ACCOMPLISHED SDR.
- [SDR IPXA2024020523240](https://openairdocs.org/sdr/IPXA2024020523240.md): Adapter · broken · Jan 25, 2024 · N348UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FOUND MAIN DECK CARGO RESTRAINT FLOOR ADAPTER FITTING BROKEN AT STA 676, LBL 47.5 (REPLACE) I.A.W AMM 25-57-02-404-016, AMM 25-57-05-404-006 AND AMM 25-58-01-404-005 REV.141 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL
- [SDR IPXA2024020512998](https://openairdocs.org/sdr/IPXA2024020512998.md): Angle · cracked · Jan 25, 2024 · N348UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > CRACKED ANGLE IN BULK CARGO COMPARTMENT LEFT AREA STA 1578 LBL 60 (REPLACE) I.A.W AMM 25-57-05-404-006 AND AMM 25-58-04-404-015 REV.141 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL
- [SDR IPXA2024012522998](https://openairdocs.org/sdr/IPXA2024012522998.md): Angle · cracked · Jan 25, 2024 · N348UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FAULT - CRACK - ANGLE BULK CARGO COMPARTMENT LEFT AREA STA 1578 LBL 60 (REPLACE) I.A.W AMM 25-57-05-004-001 AND AMM 25-58-04-004-010 REV.141 REMOVED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL
- [SDR IPXA2024012523240](https://openairdocs.org/sdr/IPXA2024012523240.md): Fitting · broken · Jan 25, 2024 · N348UP · Boeing 76734AF · Fuselage Main, Attach Fittings
  > FAULT - FOUND MAIN DECK CARGO RESTRAINT FLOOR ADAPTER FITTING BROKEN AT STA 676, LBL 47.5 (REPLACE) 1. I.A.W AMM 25-57-02-004-029, AMM 25-57-05-004-001 AND AMM 25-58-01-004-001 REV.141 REMOVED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL
- [SDR IPXA2024020506229](https://openairdocs.org/sdr/IPXA2024020506229.md): Fire Detector · cracked · Jan 24, 2024 · N348UP · Boeing 76734AF · Fire Detection
  > CRACKED BULK CARGO FIRE DETECTION LOOP FASTENER STRIP CRACK AT STA 1562 LBL 66 (REPLACE) I.A.W AMM 26-18-01-424-014-001 REV.141 INSTALLED DUCT LEAK DETECTOR CLAMPS AT STA 1562 LBL 66 & CONDITION CHECK NORMAL.
- [SDR IPXA2024012406229](https://openairdocs.org/sdr/IPXA2024012406229.md): Strip · cracked · Jan 24, 2024 · N348UP · Boeing 76734AF · Fuselage Main, Attach Fittings
  > FAULT - CRACK - BULK CARGO FIRE DETECTION LOOP FASTENER STRIP CRACK AT STA 1562 LBL 66 (REPLACE) OK TO WORK
- [SDR IPXA2024010204861](https://openairdocs.org/sdr/IPXA2024010204861.md): Light · inoperative · Dec 29, 2023 · N348UP · Boeing 76734AF · Emergency Lighting
  > EMERGENCY LIGHTS DO NOT ILLUM WHEN SWITCH SELECTED TO "ON" REPLACED BATTERY PACK IAW AMM 33-51-07-422-012, OPS GOOD.
- [SDR IPXA2023082545816](https://openairdocs.org/sdr/IPXA2023082545816.md): Door · unknown · Aug 24, 2023 · N348UP · Boeing 76734AF · Passenger/Crew Doors
  > CREW ENTRY DOOR BINDING WHEN OPENING AND CLOSING ACCOMPLISHED DOOR LUBRICATION OF CREW ENTRY DOOR IAW AMM 12-21-18. OPS CK OK
- [SDR IPXA2023052395167](https://openairdocs.org/sdr/IPXA2023052395167.md): Flap System · warning message · May 23, 2023 · N348UP · Boeing 76734AF · Leading Edge Slat Position Indicating System
  > ON FINAL FLAPS 25 AND CONFIGURED LE SLAT ASYM EICAS BEFORE RUNNING QRH PROCEDURE EICAS CLEARED. RAN QRH LANDED UNEVENTFULLY. C/W FIM TC 27-81-00-815-809
- [SDR IPXA2022111088024](https://openairdocs.org/sdr/IPXA2022111088024.md): Sign · inoperative · Nov 9, 2022 · N348UP · Boeing 76734AF · Emergency Lighting
  > INSPECTION TYPE:NAEMERGENCY EXIT SIGN BY ENTRY DOOR MISSING BOTTOM 3 BULB SEGMENTR & R EMERGENCY EXIT SIGN ASSY PER MM 33 41 01 OPS CKS OK ESR 52 11 02 10A ITEM 075
- [SDR IPXA2023051319370](https://openairdocs.org/sdr/IPXA2023051319370.md): Floorboard · damaged · Jul 1, 2022 · N348UP · Boeing 76734AF · Fuselage Floor Panel
  > MAIN CARGO COMPARTMENT FLOOR PANEL REPAIR (SREO) 2 DENTS, 1WX 2.25LX.5D, AND.7***SM13/LMX8*** INSTALLED NEW FLOOR PANEL IAW AMM 53-01-06
- [SDR IPXA2021090173403](https://openairdocs.org/sdr/IPXA2021090173403.md): Escape Rope · faulted · Aug 31, 2021 · N348UP · Boeing 76734AF · Emergency Equipment
  > INSPECTION TYPE:N/ACAPT ESCAPE ROPE DOOR KEEPS FALLING OPENRESTORED CAPT. ROPE PER AMM 25-61-13 OPS CK GOOD
- [SDR IPXA2020030352723](https://openairdocs.org/sdr/IPXA2020030352723.md): Warning System · false activation · Mar 3, 2020 · N348UP · Boeing 76734AF · Door Warning System
  > INSPECTION TYPE:NA**AIR TURN BACK - SDR FILED OPEN** DURING INITIAL CLIMB OUT FROM MAD AT APPROX 7000' MSL THE FWD CARGO DOOR EICAS MSG AND CARGO DOORS OVERHEAD LT ILLUMINATED. FWD CARGO DOOR INDICATION DEFERRED INOP IAW MEL 52-71-1-1 CAT "C". MAINT PROCED
- [SDR IPXA2019100447543](https://openairdocs.org/sdr/IPXA2019100447543.md): Blade · nicked · Oct 3, 2019 · N348UP · Boeing 76734AF · Turbine Engine Compressor Section
  > LEFT ENGINE, 1 X FAN BLADE LEADING EDGE NICK DAMAGE AT 564 MM FROM ROOT. BLEND REPAIR C/O IAW AMM 72-31-02. C/W INSPECTION OF THE LT ENGINE ONE FAN BLADE IAW AMM 72-31-02. NO CRACK NOTED. OK FOR CONTINUED SERVICE.
- [SDR IPXA2018100634752](https://openairdocs.org/sdr/IPXA2018100634752.md): Connector · dirty · Oct 5, 2018 · N348UP · Boeing 76734AF · Engine Oil System Wiring
  > REV INTERLOCK STATUS MESSAGE DURING CLIMB OUT. T/S PERFORMED IAW FIM 78-36-815-805-H00. EXAMINED CONNECTOR D71990, CONNECTOR CLEANED. TESTED T/R IAW AMM 78-31-00 PB 201 REV 124.05, FOUND SATIS.
- [SDR IPXA2018053030154](https://openairdocs.org/sdr/IPXA2018053030154.md): Skin · gouged · May 29, 2018 · N348UP · Boeing 76734AF · Fuselage Main, Plate/Skin
  > GOUGE IN SKIN AT FR 1197 S26R. APPLIED DOUBLER PER EO B767-5330-68408-D.

Next page: https://openairdocs.org/aircraft/N348UP/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 = 'N348UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N348UP/reports

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