# Service difficulty reports: N353UP

A list on [N353UP](https://openairdocs.org/aircraft/N353UP.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 · 52 reports

- [SDR IPXA2026100560445](https://openairdocs.org/sdr/IPXA2026100560445.md): Lens · missing · Oct 2, 2026 · N353UP · Boeing 76734AF · Emergency Lighting
  > COCKPIT EMERGENCY LIGHT PANEL -LIGHT INDICATION MISSING LENS, REPLACED LENS IN REF WITH AMM 33-16-02 OPS CK NORMAL
- [SDR IPXA2026091898870](https://openairdocs.org/sdr/IPXA2026091898870.md): Smoke Goggles · damaged · Sep 17, 2026 · N353UP · Boeing 76734AF · Emergency Equipment
  > CENTER SUPERNUMERARY SEAT SMOKE GOGGLES CRAZED AND BUBBLED REMOVED AND REPLACED CENTER SUPERNUMERARY SEAT SMOKE GOGGLES IAW MM 25-64-00
- [SDR IPXA2026071295408](https://openairdocs.org/sdr/IPXA2026071295408.md): Engine · stalled · Jul 10, 2026 · N353UP · Boeing 76734AF · Engine (Turbine/Turboprop)
  > DIVERTED, LEFT ENG COMPRESSOR STALL AND VIBRATION. REF. T3F18E0095NNN. NR 1 ENG WAS REPLACED IAW MXP-6002-INST-JIC.
- [SDR IPXA2026071095408](https://openairdocs.org/sdr/IPXA2026071095408.md): Compressor · stalled · Jul 10, 2026 · N353UP · Boeing 76734AF · Turbine Engine Compressor Section
  > EMERGENCY DECLARED, LEFT ENG COMPRESSOR STALLED AND VIBRATION.
- [SDR IPXA2026061846827](https://openairdocs.org/sdr/IPXA2026061846827.md): Bearing · worn · Jun 13, 2026 · N353UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > WORN BEARING, NR 2 PYLON R/H AFT FAIRING DOOR NR 4 HINGE FITTING. (REPLACE). INSTALL LOCK FASTENERS ON NEW HINGE IAW SRM 51-40-02-0G REV. 95 AND DWG 313T3340 SH. 56 REV. -. REVIEWED
- [SDR IPXA2026061746847](https://openairdocs.org/sdr/IPXA2026061746847.md): Hinge · worn · Jun 13, 2026 · N353UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > WORN OUT, BEARING, NR 1 PYLON LT FAIRING DOOR NO.4 HINGE. IAW BAC5117-18 REV. D PERFORMED BONDING RESISTANCE TEST BETWEEN THE FASTEREN HEAD AND THE STRUCTURE, THE TEST VALUE 0.634 MILLI OHM, PASSED. INSTALLED NEW HINGE I.A.W SRM 51-40-02-0G REV. 95 AND BOE
- [SDR IPXA2026061648693](https://openairdocs.org/sdr/IPXA2026061648693.md): Seal · broken · Jun 13, 2026 · N353UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > BROKEN SPRING SEAL, NR 1 PYLON 436CL PANEL. REMOVED DAMAGE SEAL IAW SRM 51-40-02-0G, REV. 95. INSTALLED NEW SEAL IAW SRM 51-40-02-0G REV. 95, AND DWG 311T2570 SH. 16 REV -.
- [SDR IPXA2026061646606](https://openairdocs.org/sdr/IPXA2026061646606.md): Seal · broken · Jun 13, 2026 · N353UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > BROKEN SEAL, NR 2 PYLON FAIRING PNL 446CL. REMOVED DAMAGE SEAL IAW SRM 51-40-02-0G REV. 95. INSTALLED NEW SEAL IAW SRM 51-40-02-0G REV. 95 AND DWG 311T2570 SH. 16 REV -.
- [SDR IPXA2026061549269](https://openairdocs.org/sdr/IPXA2026061549269.md): Rub Strip · chafed · Jun 13, 2026 · N353UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > CHAFED WEARSTRIP, NR 1 ENG RT CORE COWL OUTER L/E 1:00 TO 4:00 AREA. INSTALLED NEW WEARSTRIP I.A.W SRM 51-40-02-0G REV.95 AND GOODRICH AEROSTRUCTURES CMM IPL 71-13-24 REV.50
- [SDR IPXA2026061546619](https://openairdocs.org/sdr/IPXA2026061546619.md): Bracket · chafed · Jun 13, 2026 · N353UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > CHAFED BRACKET ASSY, NO.1 ENG L/H CORE COWL HOLD OPEN ROD STOWAGE. INSTALLED NEW BRACKET I.A.W SRM 51-40-02-0G REV. 95 AND GOODRICH CMM IPL 71-13-23 REV. 47.
- [SDR IPXA2026061648540](https://openairdocs.org/sdr/IPXA2026061648540.md): Rivet · sheared · Jun 13, 2026 · N353UP · Boeing 76734AF · Wing Main, Frame Structure
  > SHEARED RIVET, RT WING OTBD L/E UPPER SURFACE AT OSS 439.50, ADJACENT NO.8 SLAT INBD AUX TRACK. REMOVED DAMAGE FORMER IAW SRM 51-40-02-0G, REV 95. INSTALLED NEW FORMER IAW SRM 51-40-02-0G, REV. 95 AND DWG 114T2241 SHT 4, REV -. AND SREO-54290-REQ1, REV 3.
- [SDR IPXA2026061548246](https://openairdocs.org/sdr/IPXA2026061548246.md): Bracket · cracked · Jun 13, 2026 · N353UP · Boeing 76734AF · Wing Miscellaneous Structure
  > CRACKED BRACKET, LT WING INBD L/E NO.6 SLAT DRIVE TORQUE TUBE SUPPORT, LES 285. INSTALLED NEW BRACKET I.A.W SRM 51-40-02-0G REV. 95 AND DWG NO.114T1240 SH.6 REV. -.
- [SDR IPXA2026061548249](https://openairdocs.org/sdr/IPXA2026061548249.md): Bracket · cracked · Jun 13, 2026 · N353UP · Boeing 76734AF · Wing, Attach Fittings
  > CRACKED BRACKET, RT WING INBD SLAT TORQUE TUBE SUPPORT AT INBD L/E CAVITY, ISS 285.233. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G REV. 95 AND DWG NO. 114T1240 SH. 6 REV. -.
- [SDR IPXA2026061548351](https://openairdocs.org/sdr/IPXA2026061548351.md): Plate · cracked · Jun 13, 2026 · N353UP · Boeing 76734AF · Wing Miscellaneous Structure
  > CRACKED PLATE, LT WING INBD T/E CAVITY LOWER RIB SUPPORT, WS 293. INSTALLED NEW PLATE I.A.W SRM 51-40-02-0G REV. 95 AND BOEING DWG NO.113T1639 SH. 1 REV. G.
- [SDR IPXA2026061646643](https://openairdocs.org/sdr/IPXA2026061646643.md): Angle · cracked · Jun 13, 2026 · N353UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > CRACKED ANGLE, NR 1 PYLON LOWER FAIRING NAC STA 376 FRAME AFT OUTBOARD. REMOVED DAMAGE CLIP I.A.W SRM 51-40-02-0G REV. 95. INSTALLED NEW CLIP IAW SRM 51-40-02-0G REV. 95 AND DWG 313T2303 SH. 131 REV. -. AND DWG 313T2303 SH.136 REV.-.
- [SDR IPXA2026061729318](https://openairdocs.org/sdr/IPXA2026061729318.md): Seal Depressor · deformed · Jun 12, 2026 · N353UP · Boeing 76734AF · Fuselage Main, Structure
  > DEFORMED DEPRESSOR, MAIN DECK CGO DOOR CUTOUT UPPER AREA AFT SIDE STA 632. INSTALLED MAIN DECK SIDE CARGO DOOR AFT-UPPER SIDE DEPRESSOR SEAL I.A.W AMM 20-11-00-910-802 REV. 148, TORQUED THE BOLT TO 30 IN-LB AND 22 IN-LB.
- [SDR IPXA2026061731672](https://openairdocs.org/sdr/IPXA2026061731672.md): Former · cracked · Jun 12, 2026 · N353UP · Boeing 76734AF · Wing Miscellaneous Structure
  > CRACKED FORMER, FWD SIDE OF LT WING OUTBD L/E NOSE BEAM, OSS 441.6. 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 SREO-54290-REQ1 REV.3 AND BOEING DWG NO:114T2241 SH 4 REV-.
- [SDR IPXA2026061733397](https://openairdocs.org/sdr/IPXA2026061733397.md): Rub Strip · chafed · Jun 12, 2026 · N353UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > CHAFING - WEARSTRIP, NO.1 ENG L/H CORE COWL INNER FACE T/E UPPER SIDE. (REPLACE) IAW AMM 71-11-06-714-013-H00 REV.148. CORE COWL INSTALLED NEW WEAR STRIP IAW SRM 51-40-02-0G REV. 95 AND GOODRICH CMM IPL 71-13-23 REV. 47.
- [SDR IPXA2026061733279](https://openairdocs.org/sdr/IPXA2026061733279.md): Angle · cracked · Jun 12, 2026 · N353UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > MEC COMPARTMENT, MAIN DECK FLOOR ANGLE CRACK STA 246, LBL 49. INSTALLED FABRICATED BRACKET I.A.W SRM 51-40-02-0G REV. 95 AND BOEING DWG NO:141T5600 SHEET 4 REV -.
- [SDR IPXA2026061532808](https://openairdocs.org/sdr/IPXA2026061532808.md): Bracket · chafed · Jun 12, 2026 · N353UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > CHAFED BRACKET ASSY, NR 1 ENG R/H CORE COWL HOLD OPEN ROD STOWAGE. INSTALL NEW BRACKET I.A.W SRM 51-40-02-0G REV.95 AND CMM IPL 71-13-24 REV.50.
- [SDR IPXA2026061628887](https://openairdocs.org/sdr/IPXA2026061628887.md): Support Angle · cracked · Jun 12, 2026 · N353UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FOUND AFT CARGO DOORWAY CEILING PANEL SUPPORT ANGLE CRACK BETWEEN BS 1329 TO BS 1338 RBL 90. ACCOMPLISHED REPAIR I.A.W SRM 51-40-02-0G REV. 95, UPS SREO-12357-REQ2 REV.2, BOEING DWG NO. 146T8501 SH. 2 REV. B AND BOEING DWG NO. 146T8501 SH. 3 REV. A.
- [SDR IPXA2026061633263](https://openairdocs.org/sdr/IPXA2026061633263.md): Plate · missing · Jun 12, 2026 · N353UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > MISSING PLATE, NR 1 PYLON LT FAIRING DOOR HOLD OPEN ROD BRACKET. FABRICATED IAW DWG 69B90733, SHT 1, REV.A. PL REV A; PSDL REV- AND ORIGINAL PART AS A SAMPLE IAW GMM-MTX CH 9.08, REV 15.2. REQUIREMENT AND EGAT WORK SHEET 60482. INSTALLED FABRICATED PLATE
- [SDR IPXA2026061631589](https://openairdocs.org/sdr/IPXA2026061631589.md): Channel · cracked · Jun 12, 2026 · N353UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > CRACKED CHANNEL, NR 1 PYLON FAIRING DOOR HOLD OPEN ROD BRACKET INSIDE. REMOVED DAMAGE BRACKET I.A.W SRM 51-40-02-0G REV. 95. INSTALLED NEW BRACKET I.A.W SRM 51-40-02-0G REV. 95 AND DWG NR 313T2303 SH. 135 REV. -.
- [SDR IPXA2026061816181](https://openairdocs.org/sdr/IPXA2026061816181.md): Floor Panel · delaminated · Jun 11, 2026 · N353UP · Boeing 76734AF · Fuselage Floor Panel
  > THE FLOOR PANEL P/N: 453T1996-116 IN THE AFT CARGO COMPARTMENT IS DELAMINATED. I.A.W. 767-300F SRM 53-00-50-2R-0 REV. 95 PERFORM REPAIR AS BELOW STEP:1.1 REMOVE THE DELAMINATED MATERIAL AND CLEAN.1.2 MEASURE THE DAMAGE AREA ( L: 17", W: 4.5", AT AFT EDGE)
- [SDR IPXA2026061611571](https://openairdocs.org/sdr/IPXA2026061611571.md): Antenna · eroded · Jun 11, 2026 · N353UP · Boeing 76734AF · Communications System
  > FOUND V.S.T HF ANTENNA (321E) EROSION.
- [SDR IPXA2026061612251](https://openairdocs.org/sdr/IPXA2026061612251.md): Skin · dented · Jun 11, 2026 · N353UP · Boeing 76734AF · Trailing Edge Flaps
  > DENTED SKIN, LOWER FACE OF LT WING T/E OUTBD FLAP T/E LOWER SKIN, WBL 373. IAW AMM 51-21-10-307-020 REV.148, REPAINT REWORK AREA.. JOB COMPLETED AND CONDITION CHECK NORMAL.
- [SDR IPXA2026061312271](https://openairdocs.org/sdr/IPXA2026061312271.md): Angle · cracked · Jun 11, 2026 · N353UP · 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.95. INSTALL NEW ANGLE I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG 146T5650 SH 5 REV.C.
- [SDR IPXA2026061312281](https://openairdocs.org/sdr/IPXA2026061312281.md): Angle · cracked · Jun 11, 2026 · N353UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > THE BULK CARGO OUTBOARD ANGLE AT BS 1578 LBL 80 IS CRACKED. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G REV. 95. INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G REV. 95 AND DWG 146T5650 SH. 5 REV. C.
- [SDR IPXA2026061312429](https://openairdocs.org/sdr/IPXA2026061312429.md): Angle · cracked · Jun 11, 2026 · N353UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > THE BULK CARGO INBOARD ANGLE AT STA 1578 LBL 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 IPXA2026061312492](https://openairdocs.org/sdr/IPXA2026061312492.md): Angle · cracked · Jun 11, 2026 · N353UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > THE BULK CARGO INBOARD ANGLE AT STA 1578 RBL 80 IS CRACKED. INSTALL NEW ANGLE I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO:146T5650 SH 5 REV.C.
- [SDR IPXA2026061311987](https://openairdocs.org/sdr/IPXA2026061311987.md): Floor Panel · cracked · Jun 11, 2026 · N353UP · Boeing 76734AF · Fuselage Floor Panel
  > MAJOR REPAIR, FOUND MAIN DECK FLOOR PANEL WITH CRACK DAMAGE. REMOVED MAIN DECK CARGO FLOOR PANEL AND REMOVED SEALANT. PANEL 251XFF. INSTALLED FLOOR PANEL I.A.W AMM 53-01-06-400-801 REV. 148.
- [SDR IPXA2026061312018](https://openairdocs.org/sdr/IPXA2026061312018.md): Floor Panel · cracked · Jun 11, 2026 · N353UP · Boeing 76734AF · Fuselage Floor Panel
  > MAJOR REPAIR, FOUND MAIN DECK FLOOR PANEL WITH CRACK DAMAGE, REMOVED MAIN DECK CARGO FLOOR PANEL AND REMOVED SEALANT. PANEL NO:252UFF. INSTALLED FLOOR PANEL IAW AMM 53-01-06-400-801 REV 148.
- [SDR IPXA2028080700149](https://openairdocs.org/sdr/IPXA2028080700149.md): Strut · corroded · Aug 6, 2025 · N353UP · Boeing 76734AF · Main Landing Gear Strut/Axle/Truck
  > SUSPECTED CORROSION RH MLG UPPER STRUT BODY - APPROX 14€? X 0.75€? TOTAL AREA BLENDED CORROSION AREAS IAW CMM 20-10-01 STEP 2.F AND 2.H. PITTING STILL REMAINS. MAPPED AND SENT DAMAGE PHOTOS TO ENGINEERING OF PITTED AREAS AND ATTACHED TO FAULT. PITTED AREAS
- [SDR IPXA2024062589422](https://openairdocs.org/sdr/IPXA2024062589422.md): Strap · cracked · Jun 11, 2024 · N353UP · Boeing 76734AF · Engine Cooling System
  > STRAP, NR 1 ENGINE LT HPT COOLING DUCT REAR FRAME FLANGE SUPPORT BRACKET RETAINING. IAW AMM 70-50-00-912-001-H00, REV.142, REPLACED THE STRAP WITH NEW & TORQUED THE NUTS. 2. COMPLETED THIS JOB AND CONDITION CHECK SATISFACTORY. 3. ATTACHMENTS ARE UPLOADED.
- [SDR IPXA2024061191168](https://openairdocs.org/sdr/IPXA2024061191168.md): None · none · Jun 11, 2024 · N353UP · Boeing 76734AF · Standard Practices/Structures
  > FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R. PERFORMED MODIFICATION PER UPS E.O.82173-JIC001. CONDITION CHECK OK.
- [SDR IPXA2024061189422](https://openairdocs.org/sdr/IPXA2024061189422.md): Bracket · cracked · Jun 11, 2024 · N353UP · Boeing 76734AF · Engine Bleed Air System
  > CRACK - STRAP, NO.1 ENGINE LH HPT COOLING DUCT REAR FRAME FLANGE SUPPORT BRACKET RETAINING (REPLACE) OK TO WORK
- [SDR IPXA2024040866276](https://openairdocs.org/sdr/IPXA2024040866276.md): Skin · gouged · Apr 1, 2024 · N353UP · Boeing 76734AF · Fuselage Main, Plate/Skin
  > SKIN GOUGE RH FUSELAGE APPROX 26€? FORWARD OF LOWER FWD CARGO DOOR. (APPROX. FUSELAGE STATION 453 BETWEEN STRINGER 26R & 25R). MARKED WITH TAPE. REINSTALLED SAME SERVICEABLE FWD.LOWER CARGO COMPARTMENT SIDE WALL PANEL I/A/W B767 AMM 25-52-01
- [SDR IPXA2024040166276](https://openairdocs.org/sdr/IPXA2024040166276.md): Skin · gouged · Apr 1, 2024 · N353UP · Boeing 76734AF · Fuselage Main, Plate/Skin
  > SKIN GOUGE RH FUSELAGE APPROX 26€? FORWARD OF LOWER FWD CARGO DOOR. (APPROX. FUSELAGE STATION 453 BETWEEN STRINGER 26R & 25R). MARKED WITH TAPE. MATERIAL ID & TRACEABILITY AS FOLLOWS:<BR>2024-T3.071 PO# SP2730176<BR>2024-T3.080 PO# SP2668300<BR>2024-T3.040
- [SDR IPXA2023112854981](https://openairdocs.org/sdr/IPXA2023112854981.md): Floor Panel · damaged · Nov 26, 2023 · N353UP · Boeing 76734AF · Fuselage Floor Panel
  > FLOOR PANEL POSITION 4 CENTER HAS A HOLE IN IT (REMOVED FOR SHEET METAL) HOLE IS MARKED VERIFIED COMPLETION OF FLOORBOARD REPAIR PER SRM 53-00-50-2R. OK TO INSTALL REPAIRED FLOORBOARD
- [SDR IPXA2023111733479](https://openairdocs.org/sdr/IPXA2023111733479.md): Cover · inoperative · Nov 17, 2023 · N353UP · Boeing 76734AF · Passenger/Crew Doors
  > L-1 DOOR ARMING LEVER HINGED COVER INOP. DEFERRED THE L-1 DOOR ARMING LEVER HINGED COVER IAW MEL 52-11-2. INSTALLED ARMING LEVER HINGE COVER AND INSTALLED L1 DOOR LINING IAW AMM 52-12-02-401.
- [SDR IPXA2023021891100](https://openairdocs.org/sdr/IPXA2023021891100.md): Light · none · Feb 18, 2023 · N353UP · Boeing 76734AF · Emergency Lighting
  > INSPECTION TYPE:N/ACOCKPIT AFT LFT EMERGENCY LIGHT INOP.R & R'D COCKPIT AFT LFT EMERGENCY LIGHT IAW MM 33-51-11-201.
- [SDR IPXA2022041681217](https://openairdocs.org/sdr/IPXA2022041681217.md): Floor Panel · none · Apr 16, 2022 · N353UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:N/AMAIN CARGO COMPARTMENT FLOOR PANEL REPAIR POSITION 4 CENTERMANUFACTURED NEW PANEL IAW UPS EO B767-5320-9693-1
- [SDR IPXA2021041968342](https://openairdocs.org/sdr/IPXA2021041968342.md): Actuator · malfunctioned · Apr 18, 2021 · N353UP · Boeing 76734AF · Landing Gear Actuator
  > ATB - NO EMERG DECLARED. NO EQUIP USED. AFTER T/O AND AFTER RAISING THE LANDING GEAR EICAS MESSAGE GEAR DISAGREE MSG DISPLAYED RAN APPROPIATE CHECK LIST, LANDING GEAR WAS EXTENDED MANUALLY LANDING WEIGHT 323.3. DEF LANDING GEAR ACTUATION SYS PER MEL 32-30-1
- [SDR IPXA2021021565681](https://openairdocs.org/sdr/IPXA2021021565681.md): Warning Message · false indication · Feb 12, 2021 · N353UP · Boeing 76734AF · Cabin Pressure Control System
  > -RAPID DECOMPRESSION -NO EMERG DECLARED-O2 MASKS USED-NO OTHER EMERG EQUIP USED** CABIN ALTTITUDE WARNING AT FL 360 WITH BOTH PACKS ON. RECOVERED CABIN IN AUTO 1 WHEN SELECTED. DEFERRED PER MEL 21-31-1A. BITE TESTED PER FIM 21-31-00-815-803, NO FAULTS FOUND ON
- [SDR IPXA2019072945044](https://openairdocs.org/sdr/IPXA2019072945044.md): Tru · inoperative · Jul 27, 2019 · N353UP · Boeing 76734AF · DC Rectifier/Converter
  > INSPECTION TYPE:CK TRU (35 AMP) CIRCUIT BREAKER TRIPPED. FOUND DURING PS CHECK.REMOVED AND REPLACED APU TRU. SYSTEM OPS CHECK GOOD. REF AMM 24-32-04.
- [SDR IPXA2019052842568](https://openairdocs.org/sdr/IPXA2019052842568.md): Unknown · malfunctioned · May 28, 2019 · N353UP · Boeing 76734AF · Engine Thrust Reverser
  > INSPECTION TYPE:N/A LEFT THRUST REVERSER UNLOCKED BUT DID NOT DEPLOY ON LANDING REV REMAINED AMBER BOTH THRUST REVERSERS STOWED CORRECTLY HAS HIST LPG 110584 5/19 C/W DMP 78-31-1 COLLARED 11L6/11D18/11D5 OK TO CONTINUE ASSIGNED M671285 PLACARDS INSTALLED ETOPS
- [SDR IPXA2018021426536](https://openairdocs.org/sdr/IPXA2018021426536.md): Oxygen Mask · inoperative · Feb 13, 2018 · N353UP · Boeing 76734AF · Crew Oxygen System
  > FIRST OFFICER`S OXYGEN MASK INFLATION HARNESS SEPERATED. DOES NOT INFLATE. REPLACED THE OXYGEN MASK. OPS CHECKED GOOD IAW MM 35-11-51-401.
- [SDR IPXA2017080720237](https://openairdocs.org/sdr/IPXA2017080720237.md): Lamp · inoperative · Aug 5, 2017 · N353UP · Boeing 76734AF · Emergency Lighting
  > EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP AND OPS CHECKED GOOD IAW AMM 33-51-16.
- [SDR IPXA2016081707135](https://openairdocs.org/sdr/IPXA2016081707135.md): Shutoff Valve · inoperative · Aug 17, 2016 · N353UP · Boeing 76734AF · Pneumatic Distribution System
  > EICAS FOR RT ENGINE HPSOV, LIGHT ON STEADY DURING CLIMBOUT. RT ENG BLEED LIGHT ILLUMINATED, AND DUCT PRESSURE FLUCTUATED.
- [SDR IPXA2016070805557](https://openairdocs.org/sdr/IPXA2016070805557.md): Lamp · inoperative · Jul 8, 2016 · N353UP · Boeing 76734AF · Emergency Lighting
  > EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP, OPS TESTED GOOD IAW AMM 33-50-00.

Next page: https://openairdocs.org/aircraft/N353UP/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 = 'N353UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N353UP/reports

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