# Service difficulty reports: N337UP

A list on [N337UP](https://openairdocs.org/aircraft/N337UP.md).

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

- [SDR IPXA2026031657601](https://openairdocs.org/sdr/IPXA2026031657601.md): Window · delaminated · Mar 13, 2026 · N337UP · Boeing 76734AF · Flight Compartment Windows
  > R2 WINDOW DELAMINATION FO SIDE. BUBBLE IN WINDOW AS WELL, IN LINE OF SIGHT FOR VISION DEGRADATION. R&R R2 SLIDING WINDOW IAW AMM 56-11-02. LEAK AND OPS CHECK GOOD.
- [SDR IPXA2026031357601](https://openairdocs.org/sdr/IPXA2026031357601.md): Window · delaminated · Mar 13, 2026 · N337UP · Boeing 76734AF · Flight Compartment Windows
  > R2 WINDOW DELAMINATION FO SIDE. BUBBLE IN WINDOW AS WELL, IN LINE OF SIGHT FOR VISION DEGRADATION.
- [SDR IPXA2025090334054](https://openairdocs.org/sdr/IPXA2025090334054.md): Floor Panel · damaged · Aug 30, 2025 · N337UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 143T5876-83 PANEL NO: 231GFF. I.A.W AMM 53-01-06-000-801 REV.146 REMOVE MAIN DECK CARGO FLOOR PANEL AND SEALANT, G.V.I AND CONDITION CHECK NORMAL. FABRICATE A NEW FLOOR PANEL I.A.W. UPS SREO-9693-REQ001 REV.4. I.A.W
- [SDR IPXA2025090334048](https://openairdocs.org/sdr/IPXA2025090334048.md): Floor Panel · damaged · Aug 30, 2025 · N337UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 143T5876-82 PANEL NO: 232GFF. I.A.W AMM 53-01-06-000-801 REV.146 REMOVE MAIN DECK CARGO FLOOR PANEL AND SEALANT, G.V.I AND CONDITION CHECK NORMAL. FABRICATE A NEW FLOOR PANEL I.A.W. UPS SREO-9693-REQ001 REV.4. I.A.W
- [SDR IPXA2025090334158](https://openairdocs.org/sdr/IPXA2025090334158.md): Floor Panel · damaged · Aug 30, 2025 · N337UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND MAIN DECK FLOOR PANEL DAMAGE. I.A.W AMM 53-01-06-000-801 REV.146 REMOVE MAIN DECK CARGO FLOOR PANEL AND SEALANT, G.V.I AND CONDITION CHECK NORMAL. FABRICATE A NEW FLOOR PANEL I.A.W. UPS SREO-9693-REQ001 REV.4. I.A.W AMM 53-01-06-400-801 REV.146 INSTALL
- [SDR IPXA2025090334100](https://openairdocs.org/sdr/IPXA2025090334100.md): Floor Panel · damaged · Aug 30, 2025 · N337UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND MAIN DECK FLOOR PANEL DAMAGE, PANEL NO: 232FFF. IAW AMM 53-01-06-000-801 REV.146 REMOVE MAIN DECK CARGO FLOOR PANEL, G.V.I AND CONDITION CHECK NORMAL. IAW AMM 53-01-06-000-801 REV.146. REMOVE MAIN DECK CARGO FLOOR PANEL SEALANT AND CONDITION CHECK N
- [SDR IPXA2025090334225](https://openairdocs.org/sdr/IPXA2025090334225.md): Floor Panel · damaged · Aug 30, 2025 · N337UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND MAIN DECK FLOOR PANEL DAMAGE, 232AFF. I.A.W AMM 53-01-06-000-801 REV.146 REMOVED MAIN DECK CARGO FLOOR PANEL, G.V.I AND CONDITION CHECK NORMAL. IAW AMM 53-01-06-000-801 REV.146. REMOVED MAIN DECK CARGO FLOOR PANEL SEALANT AND CONDITION CHECK NORMAL.
- [SDR IPXA2025090334252](https://openairdocs.org/sdr/IPXA2025090334252.md): Floor Panel · damaged · Aug 30, 2025 · N337UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 143T5876-78 PANEL NO: 231AFF. I.A.W AMM 53-01-06-000-801 REV.146 REMOVE MAIN DECK CARGO FLOOR PANEL AND SEALANT, G.V.I AND CONDITION CHECK NORMAL. FABRICATE A NEW FLOOR PANEL I.A.W. UPS SREO-9693-REQ001 REV.4. I.A
- [SDR IPXA2025091013085](https://openairdocs.org/sdr/IPXA2025091013085.md): Angle · cracked · Aug 29, 2025 · N337UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FOUND CRACK -ANGLE, BULK CGO COMPT CEILING AREA, STA 1577 LBL 74 INBOARD SIDE. I.A.W AMM 53-01-06-000-801 REV.146 REMOVE MAIN DECK CARGO FLOOR PANEL AND SEALANT, G.V.I AND CONDITION CHECK NORMAL. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G REV.93. I.A.W AMM
- [SDR IPXA2024032926686](https://openairdocs.org/sdr/IPXA2024032926686.md): Warning Message · illuminated · Mar 29, 2024 · N337UP · Boeing 76734AF · Landing Gear Door Retract Section
  > GEAR DOOR LIGHT ILLUMINATED FOLLOWED BY GEAR DOOR EICAS MSG GEAR EXTENDED AT 170 KTS, SEE PREVIOUS LOGBOOK ENTRY TROUBLESHOT REF FIM 32-3- TREE 806.FOUND LAST FLIGHT CODE 242 & 264 €ŒRIGHT LATCH LOCKED SYS 1 & 2. CYCLED DOORS USING GEAR HANDLE AND SYSTEM OPER
- [SDR IPXA2024013037780](https://openairdocs.org/sdr/IPXA2024013037780.md): Cover · inoperative · Jan 15, 2024 · N337UP · Boeing 76734AF · Passenger/Crew Doors
  > **SUPPLEMENTAL SDR**COVER TO LOCK ON CABIN DOOR WILL NOT STOW TO DOWN POSITION REMOVED DEBRIS FROM HINGE REF IPC 52-11-02-10A ITEM 170. OPS CHK THE CREW ENTRY DOOR IAW AMM 52-12-00. DEFERRAL CLEARED PLACARD REMOVED
- [SDR IPXA2024011637780](https://openairdocs.org/sdr/IPXA2024011637780.md): Unknown · unknown · Jan 15, 2024 · N337UP · Boeing 76734AF · Passenger/Crew Doors
  > COVER TO LOCK ON CABIN DOOR WILL NOT STOW TO DOWN POSITION DEFERRED DOOR ARMING LEVER HINGE COVER REF MEL 52-11-2, PLACARDS INSTALLED.
- [SDR IPXA2023082549891](https://openairdocs.org/sdr/IPXA2023082549891.md): Floor Panel · deformed · Aug 19, 2023 · N337UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND MAIN DECK CARGO FLOOR PANEL DEFORM PANEL, P/N:146T5869-89 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 25-58-04-404-015 REV 139 RESTORED MAIN DECK CARGO HANDLING. JOB COMPLETED AND CONDITION CHECK NORMAL. REVIEWED
- [SDR IPXA2023041814430](https://openairdocs.org/sdr/IPXA2023041814430.md): Unknown · vibration · Apr 18, 2023 · N337UP · Boeing 76734AF · Engine Indicating System
  > *SUPPLEMENTAL SDR* *ATB* DURING CLIMB WITH THRUST AT N1 106.0 LEFT AND RIGHT VIBRATION FELT THRU AIRFRAME. VIB INDICATION PEAKED AT LEFT 2.8 FAN / RIGHT 2.5 FAN. MOST PRONOUNCED INITIATING CLIMB THRUST FROM 2 INTERMEDIATE VIBRATION WITHIN LIMITS PER PARA H VIB
- [SDR IPXA2021090373496](https://openairdocs.org/sdr/IPXA2021090373496.md): Stiffener · cracked · Aug 28, 2021 · N337UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C6CRACK ON CENTER WING TANK STIFFENER (P/N: 111T2011-6) ON STA 785.9, RBL 55.REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV.81.00 AND UPS EO B767-5740-58151-C AND B767-5720-76672-A.
- [SDR IPXA2021090373495](https://openairdocs.org/sdr/IPXA2021090373495.md): Stiffener · cracked · Aug 28, 2021 · N337UP · Boeing 76734AF · Fuselage Miscellaneous 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 57-10-10-2R-2 REPAIR 2 REV.81.00 AND UPS EO B767-5740-58151-C AND B767-5720-76672-A.
- [SDR IPXA2021080272322](https://openairdocs.org/sdr/IPXA2021080272322.md): Skin · damaged · Aug 1, 2021 · N337UP · Boeing 76734AF · Leading Edge Devices
  > INSPECTION TYPE:N/ADAMAGE AT UPPER SKINREPAIR IAW EO B767-5750-80271
- [SDR IPXA2021072572048](https://openairdocs.org/sdr/IPXA2021072572048.md): Floor Panel · damaged · Jul 25, 2021 · N337UP · Boeing 76734AF · Fuselage Floor Panel
  > INSPECTION TYPE:N/AMAIN CARGO DECK FLOOR PANEL DAMAGED ALONG CENTERLINE OF POSITIONMANUFACTURED NEW PANEL IAW UPS E.O. B767-5320-9693-I ON NRC 663732
- [SDR IPXA2020071755824](https://openairdocs.org/sdr/IPXA2020071755824.md): Light · inoperative · Jul 15, 2020 · N337UP · Boeing 76734AF · Emergency Lighting
  > EXTERIOR EMERGENCY EGRESS LIGHT WAS INOPERATIVE. REPLACED THE LAMPS FOR THE EXTERIOR EMERGENCY ESCAPE LIGHT IAW AMM 33 51 16. OPS CHECKED NORMAL.
- [SDR IPXA2019090246227](https://openairdocs.org/sdr/IPXA2019090246227.md): Fseu · faulted · Sep 1, 2019 · N337UP · Boeing 76734AF · Trailing Flap Position Indicating System
  > INSPECTION TYPE:N/AATB - EMERGENCY DECLARED -AT FL 350 AT MACH.80, 270 KIAS THE LEADING EDGE SLAT ASSYMETRY ANNUNCIATED. EICAS MESSAGE LE SLAT ASYM, LEADING WARNING LIGHT ANNUNCIATED. FLAP LEVER INDICATOR BETWEEN 0 TO 1.ADJUSTED GAP ON S304 PER MM 27-88-01.
- [SDR IPXA2018101835116](https://openairdocs.org/sdr/IPXA2018101835116.md): Skin Panel · eroded · Oct 17, 2018 · N337UP · Boeing 76734AF · Vertical Stabilizer, Plate/Skin
  > VERTICAL STAB RT L/E PANEL ABOVE HF ANTENNA ERODED. REMOVED ERODED COMPOSITE AND INSTALLED COMPOSITE REPAIR IAW SRM 55-30-01-2R-6 AND 51-70-17. (MINOR)
- [SDR IPXA2018082033021](https://openairdocs.org/sdr/IPXA2018082033021.md): Manifold · broken · Aug 19, 2018 · N337UP · Boeing 76734AF · Engine Bleed Air System
  > NUMBER 2 ENGINE, FROM APPROXIMATELY 5 - 6 O'CLOCK POSITIONS, TCC MANIFOLD WAS BROKEN, TWO 1/2 INCH DIAMETER TUBES HAVE SEPARATED FROM MAIN MANIFOLD. REPLACED TCC MANIFOLD IAW AMM 75-24-03-401.
- [SDR IPXA2018081032629](https://openairdocs.org/sdr/IPXA2018081032629.md): Pump · inoperative · Aug 10, 2018 · N337UP · Boeing 76734AF · Fuel Boost Pump
  > CENTER FUEL PUMP EICAS AND LOW PRESS LIGHT ON WITH 1000LBS OF FUEL REMAINING IN THE CENTER TANK. LEFT PUMP CONTINUED NORMAL OPS UNTIL CENTER TANK DEPLETED. AIRCRAFT IN LEVEL FLIGHT & WINGS LEVEL.
- [SDR IPXA2017090721461](https://openairdocs.org/sdr/IPXA2017090721461.md): Warning Message · illuminated · Sep 7, 2017 · N337UP · Boeing 76734AF · Smoke Detection
  > EICAS STATUS MESSAGE FOR THE RT ENGINE FIRE LOOP 2 DISPLAYED PRIOR TO BLOCK OUT. OPEN.
- [SDR IPXA2017080320093](https://openairdocs.org/sdr/IPXA2017080320093.md): Connector · unsecure · Aug 2, 2017 · N337UP · Boeing 76734AF · Light System Wiring
  > DURING DESCENT EMERGENCY EXIT LIGHTS CAME ON INTERMITTENTLY. RESET CONNECTOR ON EMERGENCY EXIT LIGHTS BATTERY PACK SYS. OPS. CHECK NORMAL IAW MM 33-51-00-715-039.
- [SDR IPXA2016100108822](https://openairdocs.org/sdr/IPXA2016100108822.md): Floor Panel · damaged · Oct 1, 2016 · N337UP · Boeing 76734AF · Fuselage Floor Panel
  > MCD FLOOR PANEL POS 4 CTR IS DAMAGED. FABRICATED A NEW PANEL REF EO B767-5320-9693-I.
- [SDR IPXA2015093094120](https://openairdocs.org/sdr/IPXA2015093094120.md): Skin · cracked · Sep 30, 2015 · N337UP · Boeing 76734AF · Wing, Plate/Skin
  > INSPECTION TYPE: C3, CRACK DAMAGE WAS FOUND ON FASTENER HOLE 1EA OF RT WING LOWER SKIN, PN: 112T4702-8 AT STR L-6.5, NEAR W STA 995. REPAIR IAW SR: 3-3412176606 WITH FAA APPROVED 8100-9 FORM DATED: 27SEP2015 AND EO B767-5730-58859-A
- [SDR IPXA2015092994077](https://openairdocs.org/sdr/IPXA2015092994077.md): Sleeve · damaged · Sep 29, 2015 · N337UP · Boeing 76734AF · Engine Collector/Tailpipe/Nozzle
  > INSPECTION TYPE:C, DURING MAJOR MAINTENANCE VISIT 6764, FOUND DAMAGE - NR 1 EXHAUST SLEEVE OUTER SKIN DAMAGE 6 TO 7 O'CLOCK POSITION NAC BS 321TO 339REF EGAT NRC DGU05028 EVALUATED DAMAGE IAW SRM 54-42-30-1A-1, REV 63.00 INFORMATION SUBMITTED FOR ADM DAMAGE W
- [SDR IPXA2015090493121](https://openairdocs.org/sdr/IPXA2015090493121.md): Cooling Fan · inoperative · Sep 4, 2015 · N337UP · Boeing 76734AF · Air Distribution Fan
  > INSPECTION TYPE:ETOP, FWD EXHAUST FAN STATUS MSG DISPLAYED. ITEM DEFERRED IAW MEL 21-58-4-2-1. C/W IAW DMP 21-58-4-2-1, DMI M559969. INSTALLED PLACARD. NR T2156 IAW FIM 21-58-00-815, R & R FWD EQPT COOLING EXHAUST FAN IAW AMM 21-58-06. OPS TEST SATISFACT
- [SDR IPXA2015013085508](https://openairdocs.org/sdr/IPXA2015013085508.md): Relay · inoperative · Jan 29, 2015 · N337UP · Boeing 76734AF · Landing Gear Retraction/Extension System
  > DURING NOSE GEAR EXTENSION, NUMERIOUS WARNING LIGHTS ILLUMINATED ON FWD INST PANEL ALONG WITH SW MODE CONTROL PANEL LIGHTS. NO ASSOCIATED WARNING HORNS OR EICAS MESSAGES NOTED WITH WARNING LIGHTS. FOUND RELAY K710 PROVIDING TEST GROUND TO ASSOCIATED WARNING
- [SDR IPXA2014092684424](https://openairdocs.org/sdr/IPXA2014092684424.md): Warning Message · false indication · Sep 24, 2014 · N337UP · Boeing 76734AF · Fire Detection
  > LEFT ENGINE FIRE LOOP 1 STATUS MESSAGE. OPS CHECKED IAW AMM TASK 26-00-00. NO FAULTS NOTED AT THIS TIME.
- [SDR IPXA201406043158](https://openairdocs.org/sdr/IPXA201406043158.md): Floor Panel · punctured · Jun 2, 2014 · N337UP · Boeing 76734AF · Fuselage Floor Panel
  > MAIN CARGO FLOOR PANEL 6 HAS A HOLE, REPAIRED IAW SRM 53-00-50-2R-4C.
- [SDR IPXA2014060283150](https://openairdocs.org/sdr/IPXA2014060283150.md): Floor Panel · damaged · Jun 1, 2014 · N337UP · Boeing 76734AF · Fuselage Floor Panel
  > MAIN CARGO FLOOR PANEL DAMAGED. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.
- [SDR IPXA2014060283149](https://openairdocs.org/sdr/IPXA2014060283149.md): Floor Panel · damaged · Jun 1, 2014 · N337UP · Boeing 76734AF · Fuselage Floor Panel
  > MAIN CARGO FLOOR PANEL DAMAGED. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.
- [SDR IPXA2014060283144](https://openairdocs.org/sdr/IPXA2014060283144.md): Floor Panel · damaged · Jun 1, 2014 · N337UP · Boeing 76734AF · Fuselage Floor Panel
  > MAIN CARGO FLOOR PANEL DAMAGED. FABRICATED NEW FLOOR PANEL IAW EO-B767-5320-9693-H.
- [SDR IPXA2014052783065](https://openairdocs.org/sdr/IPXA2014052783065.md): Floor Panel · damaged · May 26, 2014 · N337UP · Boeing 76734AF · Fuselage Floor Panel
  > MAIN CARGO DECK FLOOR PANEL HAS NUMEROUS AREAS OF DAMAGE. FABRICATED AND REPLACED THE FLOOR PANEL IAW EO B767-5320-9693-H.
- [SDR IPXA2014052783064](https://openairdocs.org/sdr/IPXA2014052783064.md): Floor Panel · damaged · May 26, 2014 · N337UP · Boeing 76734AF · Fuselage Floor Panel
  > MAIN CARGO DECK FLOOR PANEL HAS NUMEROUS DAMAGES, FABRICATED AND REPLACED IAW EO B767-5320-9693-H.
- [SDR IPXA2675534](https://openairdocs.org/sdr/IPXA2675534.md): D-Ring · missing · Sep 23, 2012 · N337UP · Boeing 76734AF · Emergency Equipment
  > COCKPIT EMERGENCY ESCAPE DESCENT HARNESS HAS ONE D-RING MISSING. R & R EMERGENCY ESCAPE DESCENT HARNESS ASSY IAW GMM 25-61-00.
- [SDR IPXA12673048](https://openairdocs.org/sdr/IPXA12673048.md): Indicator · failed · Apr 17, 2012 · N337UP · Boeing 76734AF · Airspeed/Mach Indicator
  > DUE TO CAPTAIN`S AIRSPEED INDICATION INOPERATIVE, ALTERNATE AIR DATA SELECTED, FAILED TO CORRECT PROBLEM. CHECKED CAPTAIN`S AIRSPEED INDICATOR CONDITION, POWER AND GROUNDS AT CONNECTOR D101, REF WDM 34-13-11. CHECKED OK. FIM FAULT CODE 34012030 AND 4 34-12-7
- [SDR IPXA2672594](https://openairdocs.org/sdr/IPXA2672594.md): Connector · loose · Mar 22, 2012 · N337UP · Boeing 76734AF · Flight Control System Wiring
  > T/E FLAP DISAGREE ON APPROACH, WHEN FLAPS SELECTED PAST 5. ACCOMPLISHED T/E DISAGREE AND LANDED FLAPS 20. EMERGENCY DECLARED. LANDED WITHOUT INCIDENT. FOUND NR 3 FLAP POSITION TRANSDUCER CONNECTOR LOOSE. SYS CHECKED NORMAL IAW FIM 27-51-00, FIG 105.
- [SDR IPXA12672517](https://openairdocs.org/sdr/IPXA12672517.md): Connector · loose · Mar 22, 2012 · N337UP · Boeing 76734AF · Flight Control System Wiring
  > T/E FLAP DISAGREE ON APP WHEN FLAPS SELECTED PAST 5, ACCOMPLISHED T/E DISAGREE AND LANDED FLAPS 20 EMERGENCY DECLARED. FOUND NR 3 FLAP POSITION TRANSDUCER CONNECTOR PLUG LOOSE. SYS CKS NORMAL IAW FIM 27-51-00, FIG 105.
- [SDR IPXA1668640](https://openairdocs.org/sdr/IPXA1668640.md): Shutoff Valve · dirty · Aug 15, 2011 · N337UP · Boeing 76734AF · Pneumatic Distribution System
  > INSPECTION TYPE: ETOP, LT ENGINE BLEED EICAS MSG AND SWITCH LIGHT ILLUMINATED. MANUALLY CYCLED PRSOV AND CLEANED C/P. ENG RAN BY CREW CHECK OK IAW AMM 36-11-00-5.
- [SDR IPXA1666288](https://openairdocs.org/sdr/IPXA1666288.md): Counterbalance · out of adjust · Apr 30, 2011 · N337UP · Boeing 76734AF · Passenger/Crew Doors
  > CREW ENTRY DOOR VERY DIFFICULT TO OPEN (DOOR ITSELF, NOT HANDLE). NO FEELING OF "ASSIST" IN RAISING DOOR TO OPEN POSITION. ADJUSTED COUNTER BALANCE IAW MM 52-12-16-5. NO HELP. LUBED CREW ENTRY DOOR IAW MM 12-21-18-3. DOOR OPS CKS GOOD IAW MM 52-12-16-5.
- [SDR IPXA1664029](https://openairdocs.org/sdr/IPXA1664029.md): Seal · damaged · Jan 5, 2011 · N337UP · Boeing 76734AF · Passenger/Crew Doors
  > MAIN CABIN DOOR VERY STIFF DURING OPERATION. EXCESSIVE FORCE REQUIRED TO OPEN AND CLOSE. FOUND FWD DOOR TRIM SEAL BUNCHING UP AT 30-35 IN FROM FLOOR REF IPC 52-11-02, FIG 10A ITEM 15. ACCOMPLISHED CREW ENTRY DOOR ADJUSTMENT/TEST WITH NO ADJUSTMENTS MADE FOU
- [SDR IPXA10663317](https://openairdocs.org/sdr/IPXA10663317.md): Floorboard · dented · Oct 24, 2010 · N337UP · Boeing 76734AF · Fuselage Floor Panel
  > REF DMI D429161, MAIN CARGO DECK POS NR 2 RT FLOORBOARD - 2ND BOARD IN FROM OTBD HAS A 1-INCH BY 1-INCH DENT. REPLACED FLOORBOARD WORKING WITH EO B767-5320-9693 AND M/M 53-01-06.
- [SDR IPXA10662386](https://openairdocs.org/sdr/IPXA10662386.md): Detector · inoperative · Sep 7, 2010 · N337UP · Boeing 76734AF · Detection System
  > INSPECTION TYPE:E, TOP ATB - RT DUCT LEAK LIGHT ILLUM AND ASSOCIATED EICAS MSG R BLD DUCT LEAK DISPLAYED. IAW FIM 26-18-00, FIG 104. R & R M691 CONDITION RECURS AFTER 5 MINUTES RT ENG OPERATION. R & R TS218 DUE TO BEING OUT OF LIMITS CORE TO CORE MAX RES CH
- [SDR IPXA10662140](https://openairdocs.org/sdr/IPXA10662140.md): Skin · gouged · Aug 25, 2010 · N337UP · Boeing 76734AF · Fuselage Main, Plate/Skin
  > RT SIDE FUSELAGE SKIN GOUGED AFT OF FWD LOWER CARGO DOOR AT STA 610R AND BETWEEN STRINGERS S30 & S29 RT. ACCOMPLISHED PERMANENT REPAIR OF SKIN DAMAGE AT STA 612 RT AND BETWEEN STRINGERS S30 AND S29 RT IAW SRM 53-00-15-1A-1, FIG 101, DETAIL II.
- [SDR IPXA10660753](https://openairdocs.org/sdr/IPXA10660753.md): Lamp · inoperative · Jun 26, 2010 · N337UP · Boeing 76734AF · Emergency Lighting
  > INSPECTION TYPE:PS, EMERGENCY LIGHT BELOW CREW ENTRANCE OUT. RELAMPED IAW AMM33-51-16-2.

## 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 = 'N337UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N337UP/reports

---
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