# Service difficulty reports: N355UP

A list on [N355UP](https://openairdocs.org/aircraft/N355UP.md).

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

- [SDR IPXA2026092286713](https://openairdocs.org/sdr/IPXA2026092286713.md): Cowling · cracked · Sep 17, 2026 · N355UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > CRACKED SKIN, NR 1 ENG RT CORE COWL LOWER FWD SKIN NEAR NO.1 LATCH. PERFORM REPAIR I.A.W UPS EO-98690-REQ1 REV.1.
- [SDR IPXA2026092191640](https://openairdocs.org/sdr/IPXA2026092191640.md): Panel · eroded · Sep 17, 2026 · N355UP · Boeing 76734AF · Vertical Stabilizer, Plate/Skin
  > ERODED VERTICAL STAB LE PANEL 321E. REMOVED THE DAMAGE MATERIALS AND CLEAN. BONDED THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 260 F FOR 130 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG I.A.W. 767-300F SRM 55-30-01-2R-6 REFER TO SRM 51-70-07-0G-0 REV. 96.
- [SDR IPXA2026092289443](https://openairdocs.org/sdr/IPXA2026092289443.md): Nose Cowl · dented · Sep 17, 2026 · N355UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > DENTED NR 1 NOSE COWL INLET AT 7 O'CLOCK POSITION. BOND THE SPACER WITH FILM ADHESIVE CURED AT 250°F FOR 2 HOURS AND FILL THE CUT OUT WITH ADHESIVE CURED AT 200°F FOR 1 HOUR I.A.W. B767-300F SRM 54-15-01-2R-3 REV. 96. CONDITION CHECK IS SATISFACTORY.
- [SDR IPXA2026092290656](https://openairdocs.org/sdr/IPXA2026092290656.md): Nose Cowl · dented · Sep 17, 2026 · N355UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > DENTED NR 1 ENG NOSE COWL INLET AT 5 O'CLOCK POSITION. BOND THE SPACER WITH FILM ADHESIVE CURED AT 250°F FOR 2 HOURS AND FILL THE CUT OUT WITH ADHESIVE CURED AT 200°F FOR 1 HOUR I.A.W. B767-300F SRM 54-15-01-2R-3 REV. 96. CONDITION CHECK IS SATISFACTORY.
- [SDR IPXA2026092290813](https://openairdocs.org/sdr/IPXA2026092290813.md): Nose Cowl · dented · Sep 17, 2026 · N355UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > DENTED SKIN, NR 2 ENG NOSE COWL INNER BARREL NEAR 2:00 TO 6:00 POS. BOND THE SPACER WITH FILM ADHESIVE CURED AT 250°F FOR 2 HOURS AND FILL THE CUT OUT WITH ADHESIVE CURED AT 200°F FOR 1 HOUR I.A.W. B767-300F SRM 54-15-01-2R-3 REV. 96. CONDITION CHECK IS SAT
- [SDR IPXA2026092290842](https://openairdocs.org/sdr/IPXA2026092290842.md): Nose Cowl · dented · Sep 17, 2026 · N355UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > DENTED NR 1 ENGINE NOSE COWL INLET AT 6 O'CLOCK POSITION. UT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( ‘ DIA: 0.2", 27" FROM FWD EDGE, 31.5" FROM UPPER EDGE ‘¡ DIA: 0.4", 32.4" FROM FWD EDGE, 31" FROM UPPER EDGE, AT 6 O'CLOCK ON THE INNER BARREL OF
- [SDR IPXA2026092186627](https://openairdocs.org/sdr/IPXA2026092186627.md): Floor Panel · cracked · Sep 17, 2026 · N355UP · Boeing 76734AF · Fuselage Floor Panel
  > CRACKED PANEL, AFT CARGO FLOOR STRUCTURE, BS 1329, BL 0. REMOVED DAMAGE PANEL I.A.W SRM 51-40-02-0G REV. 96. INSTALLED FABRICATED PANEL I.A.W SRM 51-40-02-0G REV. 96 AND BOEING DWG NO: 451T2612 SHEET 2 REV. B.
- [SDR IPXA2026092267592](https://openairdocs.org/sdr/IPXA2026092267592.md): Fairing · debonded · Sep 16, 2026 · N355UP · Boeing 76734AF · Aerodynamic Fairings
  > DEBONDED SKIN, RT AFT WING TO BODY FAIRING LATCH PANEL 198 CR. REMOVE THE DISBOND MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH RESIN CURED AT 200°F FOR 220 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG. BOND THE FOIL WITH RESIN CURED AT 200°F FOR 220 MINUTES
- [SDR IPXA2026092166138](https://openairdocs.org/sdr/IPXA2026092166138.md): Skin · punctured · Sep 16, 2026 · N355UP · Boeing 76734AF · Landing Gear Doors
  > SKIN, RT MLG W/W DOOR MID PUNCTURED. PERFORMED NDT/UT FOR THE REWORKED AREA AND PLUS 6 INCHES AROUND HEATED AREA, IAW NDT MANUAL PART 1, 51-01-01, REV 144. REMOVE THE DELAMINATION MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH RESIN CURED AT 200°F FOR 220
- [SDR IPXA2026092172110](https://openairdocs.org/sdr/IPXA2026092172110.md): Bracket · cracked · Sep 16, 2026 · N355UP · Boeing 76734AF · Wing, Attach Fittings
  > CRACKED BRACKET, LT WING INBD SLAT TORQUE TUBE SUPPORT AT INBD L/E CAVITY AT ISS 285.233. REMOVED DAMAGE BRACKET I.A.W SRM 51-40-02-0G REV. 96. INSTALLED NEW BRACKET I.A.W SRM 51-40-02-0G REV. 96 AND BOEING DWG NO. 114T1240 SH. 6 REV. -.
- [SDR IPXA2026092172477](https://openairdocs.org/sdr/IPXA2026092172477.md): Angle · cracked · Sep 16, 2026 · N355UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > CRACKED ANGLE, NR 1 PYLON AFT BULKHEAD REAR LT ANGLE. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G REV. 96. INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G REV. 96 AND DWG 313T2303 SH. 141 REV. A AND BOEING DWG NO. 313T2303 SH. 146 REV. -.
- [SDR IPXA2026092150993](https://openairdocs.org/sdr/IPXA2026092150993.md): Former · cracked · Sep 15, 2026 · N355UP · Boeing 76734AF · Wing Main, Frame Structure
  > CRACKED FORMER, RT WING OTBD L/E CAVITY CURTAIN SUPPORT BRACKET, NEAR WS 441.596. REMOVED DAMAGE FORMER I.A.W SRM 51-40-02-0G REV.96. INSTALL NEW FORMER I.A.W SRM 51-40-02-0G REV.96 AND BOEING DWG NO:1142241 SH 4 REV: - AND UPS SREO-54290-REQ1 REV.3.
- [SDR IPXA2026091850925](https://openairdocs.org/sdr/IPXA2026091850925.md): Bracket · cracked · Sep 15, 2026 · N355UP · Boeing 76734AF · Wing Miscellaneous Structure
  > CRACKED BRACKET, RT WING INBD L/E CAVITY TORQUE TUBE SUPPORT BRACKET. REMOVED DAMAGE BRACKET I.A.W SRM 51-40-02-0G REV.96. INSTALL NEW BRACKET I.A.W SRM 51-40-02-0G REV.96 AND BOEING DWG NO:114T1240 SH 6 REV: -.
- [SDR IPXA2026091850918](https://openairdocs.org/sdr/IPXA2026091850918.md): Angle · cracked · Sep 15, 2026 · N355UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > THE BULK CARGO OUTBOARD ANGLE AT STA 1578 LBL 80 IS CRACKED. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G REV. 96. INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G REV. 96 AND BOEING DWG NO. 146T5650 SH. 5 REV. C.
- [SDR IPXA2026091850822](https://openairdocs.org/sdr/IPXA2026091850822.md): Angle · cracked · Sep 15, 2026 · N355UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > THE BULK CARGO OUTBOARD ANGLE AT STA 1578 RBL 80 IS CRACKED. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G REV. 96. INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G REV. 96 AND BOEING DWG NO. 146T5650 SH. 5 REV. C.
- [SDR IPXA2026091850792](https://openairdocs.org/sdr/IPXA2026091850792.md): Angle · cracked · Sep 15, 2026 · N355UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > THE BULK CARGO INBOARD ANGLE AT STA 1578 RBL 80 IS CRACKED. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G REV. 96. INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G REV. 96 AND BOEING DWG NO. 146T5650 SH. 5 REV. C.
- [SDR IPXA2026091850818](https://openairdocs.org/sdr/IPXA2026091850818.md): Angle · cracked · Sep 15, 2026 · N355UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > THE BULK CARGO INBOARD ANGLE AT STA 1578 LBL 80 IS CRACKED. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G REV. 96. <BR>2. INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G REV. 96 AND BOEING DWG NO. 146T5650 SH. 5 REV. C.
- [SDR IPXA2026070613325](https://openairdocs.org/sdr/IPXA2026070613325.md): Oxygen Mask · no test · Jul 5, 2026 · N355UP · Boeing 76734AF · Crew Oxygen System
  > OBSERVERS OXYGEN MASK DOES NOT FLOW WHEN EMERGENCY BUTTON IS PUSHED. REMOVED AND REPLACED OBSERVER`S OXYGEN MASK IAW AMM 35-11-51. OPS CHKD GOOD.
- [SDR IPXA2024092758398](https://openairdocs.org/sdr/IPXA2024092758398.md): Drain · none · Sep 18, 2024 · N355UP · Boeing 76734AF · Standard Practices/Structures
  > (FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) COMPLETED SDR.
- [SDR IPXA2024091858398](https://openairdocs.org/sdr/IPXA2024091858398.md): None · no discrepancy · Sep 18, 2024 · N355UP · 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)
- [SDR IPXA2024091811151](https://openairdocs.org/sdr/IPXA2024091811151.md): Floor Panel · broken · Sep 15, 2024 · N355UP · Boeing 76734AF · Fuselage Floor Panel
  > MAJOR REPAIR. FOUND MAIN DECK CARGO FLOOR PANEL BROKEN PART NUMBER: 146T5869-135 (REPAIR) I.A.W AMM 53-01-06-400-801 REV.142 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL.
- [SDR IPXA2024092710203](https://openairdocs.org/sdr/IPXA2024092710203.md): Cover · worn · Sep 15, 2024 · N355UP · Boeing 76734AF · Passenger/Crew Doors
  > FOUND CREW ENTRY DOOR FORWARD DOORWAY ARMING LEVER COVER SCREW WORN (REPLACE) REPLACED DOORWAY ARMING LEVER COVER I.A.W AMM 20-11-00-910-802 REV.142.
- [SDR IPXA2024091811112](https://openairdocs.org/sdr/IPXA2024091811112.md): Floor Panel · broken · Sep 15, 2024 · N355UP · Boeing 76734AF · Fuselage Floor Panel
  > MAJOR REPAIR. FOUND MAIN DECK CARGO FLOOR PANEL BROKEN PART NUMBER: 146T5869-134 (REPAIR) I.A.W AMM 53-01-06-400-801 REV.142 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL.
- [SDR IPXA2024091610203](https://openairdocs.org/sdr/IPXA2024091610203.md): Lever · worn · Sep 15, 2024 · N355UP · Boeing 76734AF · Passenger/Crew Doors
  > **SDR FILED OPEN** FAULT - FOUND CREW ENTRY DOOR FORWARD DOORWAY ARMING LEVER COVER SCREW WORN (REPLACE) OK TO WORK
- [SDR IPXA2024092052030](https://openairdocs.org/sdr/IPXA2024092052030.md): Skin · dented · Jul 28, 2024 · N355UP · Boeing 76734AF · Trailing Edge Flaps
  > **SDR FILED OPEN** LH INBD FLAP, TRAILING EDGE AND MID FLAP HAS DENT/DAMAGE INSTALLED L/H INBD MID FLAP LWR PNL I.A.W SRM 51-40-02-0G REV.90 AND BOEING DWG NO:113T2224 SH1 REV: B
- [SDR IPXA2023082171352](https://openairdocs.org/sdr/IPXA2023082171352.md): Battery · discharged · Aug 21, 2023 · N355UP · Boeing 76734AF · Emergency Lighting
  > EMERGENCY ESCAPE LIGHTING INOP. R&R'D EMERGENCY EXIT LIGHT BATTERY ASSY. OPS CK GOOD, REF AMM 33-51-07-201.
- [SDR IPXA2022111588129](https://openairdocs.org/sdr/IPXA2022111588129.md): Floor Panel · damaged · Nov 13, 2022 · N355UP · Boeing 76734AF · Fuselage Floor Panel
  > INSPECTION TYPE:C5, DAMAGE ON MAIN DECK CARGO FLOOR PANEL BETWEEN STA 930 AND STA 972, AND BETWEEN LBL 11.0 AND RBL 11.0FABRICATE REPLACEMENT FLOOR PANEL PER UPS EO NO.:B767-5320-9693-I
- [SDR IPXA2022111588126](https://openairdocs.org/sdr/IPXA2022111588126.md): Floor Panel · damaged · Nov 13, 2022 · N355UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C5, DAMAGE ON MAIN DECK CARGO FLOOR PANEL BETWEEN STA 1114.8 AND STA 1197+22, AND BETWEEN LBL 11.0 AND RBL 11.0FABRICATE REPLACEMENT FLOOR PANEL PER UPS EO NO.:B767-5320-9693-I
- [SDR IPXA2022111588123](https://openairdocs.org/sdr/IPXA2022111588123.md): Floor Panel · damaged · Nov 13, 2022 · N355UP · Boeing 76734AF · Fuselage Floor Panel
  > INSPECTION TYPE:C5DAMAGE ON MAIN DECK CARGO FLOOR PANEL BETWEEN STA 1351 AND STA 1480, AND BETWEEN LBL 11.0 AND RBL 11.0.FABRICATE REPLACEMENT FLOOR PANEL PER UPS EO NO.:B767-5320-9693-I
- [SDR IPXA2022111588128](https://openairdocs.org/sdr/IPXA2022111588128.md): Floor Panel · damaged · Nov 10, 2022 · N355UP · Boeing 76734AF · Fuselage Floor Panel
  > INSPECTION TYPE:C5, DAMAGE ON MAIN DECK CARGO FLOOR PANEL BETWEEN STA 972 AND STA 1114.8, AND BETWEEN LBL 11.0 AND RBL 11.0FABRICATE REPLACEMENT FLOOR PANEL PER UPS EO NO.:B767-5320-9693-I
- [SDR IPXA2022111588125](https://openairdocs.org/sdr/IPXA2022111588125.md): Floor Panel · damaged · Nov 10, 2022 · N355UP · Boeing 76734AF · Fuselage Floor Panel
  > INSPECTION TYPE:C5, DAMAGE ON MAIN DECK CARGO FLOOR PANEL BETWEEN STA 1197+22 AND STA 1208, AND BETWEEN LBL 11.0 AND RBL 11.0FABRICATE REPLACEMENT FLOOR PANEL PER UPS EO NO.:B767-5320-9693-I
- [SDR IPXA2022111588124](https://openairdocs.org/sdr/IPXA2022111588124.md): Floor Panel · damaged · Nov 10, 2022 · N355UP · Boeing 76734AF · Fuselage Floor Panel
  > INSPECTION TYPE:C5DAMAGE ON MAIN DECK CARGO FLOOR PANEL BETWEEN STA 1208 AND STA 1351, AND BETWEEN LBL 11.0 AND RBL 11.0FABRICATE REPLACEMENT FLOOR PANEL PER UPS EO NO.:B767-5320-9693-I
- [SDR IPXA2021082473122](https://openairdocs.org/sdr/IPXA2021082473122.md): Lamp · inoperative · Aug 24, 2021 · N355UP · Boeing 76734AF · Emergency Lighting
  > INSPECTION TYPE:N/AEXTERNAL EMERGENCY EXIT LIGHT INOPEXTERNAL EMERGENCY EXIT LIGHT RELAMPED AND TESTED SERVICEABLE IAW B767 AMM 33-51-16-962-001
- [SDR IPXA2020111462354](https://openairdocs.org/sdr/IPXA2020111462354.md): Skin · broken · Nov 9, 2020 · N355UP · Boeing 76734AF · Leading Edge Devices
  > INSPECTION TYPE: C4 BROKEN ON LOWER SKIN (P/N:114T4114-23) OF NR 8 SLAT TRAILING EDGE WEDGE NEAR OSS 432.15. REPAIR IAW B767-300F SRM 57-43-02-2R-1 SRM 51-70-10-2R REPAIR GENERAL SRM 51-70-10-2R-4, REV.78.00.
- [SDR IPXA2020111462352](https://openairdocs.org/sdr/IPXA2020111462352.md): Skin · broken · Nov 9, 2020 · N355UP · Boeing 76734AF · Leading Edge Devices
  > INSPECTION TYPE: C4 BROKEN ON LOWER SKIN (P/N:114T4114-23) OF NR 8 SLAT TRAILING EDGE WEDGE NEAR OSS 498. REPAIR IAW B767-300F SRM 57-43-02-2R-1, SRM 51-70-10-2R REPAIR GENERAL, SRM 51-70-10-2R-4 REV 78.00.
- [SDR IPXA2020083159644](https://openairdocs.org/sdr/IPXA2020083159644.md): Floor Panel · damaged · Aug 31, 2020 · N355UP · Boeing 76734AF · Fuselage Floor Panel
  > INSPECTION TYPE:N/A MAIN CARGO DECK POSITION 2L INTERIM REPAIR TO FLOOR PANEL DAMAGE 20IN FWD OF BALLMAT AND 15IN FROM CENTER LINE. FABRICATE NEW PANEL REF EO B767-5320-9693-I APPENDIX B.
- [SDR IPXA2020083159643](https://openairdocs.org/sdr/IPXA2020083159643.md): Floor Panel · cracked · Aug 30, 2020 · N355UP · Boeing 76734AF · Fuselage Floor Panel
  > INSPECTION TYPE:N/A MAIN CARGO DECK POSITION 2L INTERIM REPAIR TO FLOOR PANEL 26 INCH FWD OF BALL AMOUNT AND 20 INCH FROM LEFT SIDE WALL. FABRICATED NEW FLOOR PANEL 143T5876-63U REF: EO B767-5320-9693-I APPENDIX B.
- [SDR IPXA2020021051991](https://openairdocs.org/sdr/IPXA2020021051991.md): Seal · torn · Feb 8, 2020 · N355UP · Boeing 76734AF · Landing Gear Doors
  > ATB - HEAVY VIB CLIMBING OUT OF 7000 FT AND GOT WORSEW AS WE ACCELERATED ABOVE 10,000 FT, VIB WAS FELT IN BOTH CONTROL COLUMNS AND FLOOR. SLOWED TO 290 / 0.78 AND VIB DECREASED. APPEARS LESS VIB IN DESCENTC/W AIRFRAME CONDITIONAL INSP PER M/M 05-51-38-202-001
- [SDR IPXA2019072945020](https://openairdocs.org/sdr/IPXA2019072945020.md): Warning System · false activation · Jul 29, 2019 · N355UP · Boeing 76734AF · Door Warning System
  > INSPECTION TYPE:INSPL FWD ENTRY DOOR EICAS MESSAGE. T/S PER FIM 52-90-17-41, CKD SENSOR S194 & LATCHING MECHANISM, NO FAULTS NOTED. FWD ENTRY DOOR IND OPS CKD NORMAL PER AMM 52-12-00-501. THIS CLEARS M677817.
- [SDR IPXA2019011537866](https://openairdocs.org/sdr/IPXA2019011537866.md): Warning System · false activation · Jan 15, 2019 · N355UP · Boeing 76734AF · Fuel Quantity Indicator
  > INSPECTION TYPE:ETOP LEFT FUEL QUANTITY BLANK & EICAS STATUS MSG "FUEL QTY IND" CONDITION INTERMITTENT. FOUND AT BITE CHECK FUEL COMPUTER LM TANK UNIT 9 OPEN LOZ OR HIZ WIRE G IAW FIM 28-41-815-851-004 REV 125.04. A/C DISPATCH IAW MEL 28-41-1-1B REV 48. DMP PE
- [SDR IPXA2016121611787](https://openairdocs.org/sdr/IPXA2016121611787.md): Engine · malfunctioned · Dec 13, 2016 · N355UP · Boeing 76734AF · Engine (Turbine/Turboprop)
  > DURING DESCENT, THE RT ENGINE FAILED TO RESPOND TO ANY THROTTLE MOVEMENTS. EGT REMAINED HIGH AT 670'C WITH N1 & N2 BACK AT IDLE. LOST CONTROL OF ANY THRUST ON RT ENGINE, EMERGENCY DECLARED. R & R NR 2 ENGINE IAW TC6001 AND 6002.
- [SDR IPXA2016111810785](https://openairdocs.org/sdr/IPXA2016111810785.md): Counterbalance · failed · Nov 17, 2016 · N355UP · Boeing 76734AF · Passenger/Crew Doors
  > CREW ENTRY DOOR STUCK HALF WAY OPEN. REPLACED COUNTERBALANCE SYSTEM L1 DOOR IAW AMM 52-12-16.
- [SDR IPXA2016051103204](https://openairdocs.org/sdr/IPXA2016051103204.md): Floorboard · gouged · May 11, 2016 · N355UP · Boeing 76734AF · Fuselage Floor Panel
  > FLOORBOARD IS GOUGED BEYOND SRM LIMITS. FABRICATED NEW FLOORBOARD IAW REO B767-5320-9693-I.
- [SDR IPXA2016051103236](https://openairdocs.org/sdr/IPXA2016051103236.md): Floorboard · gouged · May 11, 2016 · N355UP · Boeing 76734AF · Fuselage Floor Panel
  > FLOORBOARD GOUGED BEYOND SRM LIMITS. FABRICATED NEW FLOOR PANEL IAW SREO B767-5320-9693-I.
- [SDR IPXA2014071683611](https://openairdocs.org/sdr/IPXA2014071683611.md): Stringer · damaged · Jul 14, 2014 · N355UP · Boeing 76734AF · Fuselage Main, Longeron/Stringer
  > STRINGER 31L DAMAGED 7 INCHES FWD OF BS 1285. REPAIRED IAW EO B767-5310-54925-A.
- [SDR IPXA2014071683610](https://openairdocs.org/sdr/IPXA2014071683610.md): Skin · damaged · Jul 14, 2014 · N355UP · Boeing 76734AF · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DAMAGE BS 1270-1285 BETWEEN S30L AND S32L. REPAIRED IAW EO B767-5330-54923-A.
- [SDR IPXA2014071683609](https://openairdocs.org/sdr/IPXA2014071683609.md): Skin · damaged · Jul 14, 2014 · N355UP · Boeing 76734AF · Fuselage Main, Plate/Skin
  > FOUND DAMAGE TO THE FUSELAGE SKIN, BS 1197-1222. REPAIRED IAW EO B767-5330-54924-A.
- [SDR IPXA13678924](https://openairdocs.org/sdr/IPXA13678924.md): Cdu · inoperative · Jun 18, 2013 · N355UP · Boeing 76734AF · Central Display
  > ALL KEYS ON CAPTAIN`S CDU INOPERATIVE WITH NORMAL AND ALTERNATE FMC SELECTED. R & R NR 1 CDU IAW AMM 34-61-02-022-195 AND IPC 34-61-02-02A.

## 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 = 'N355UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N355UP/reports

---
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