# Service difficulty reports: N356UP

A list on [N356UP](https://openairdocs.org/aircraft/N356UP.md).

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

- [SDR IPXA2026031113913](https://openairdocs.org/sdr/IPXA2026031113913.md): Engine · shutdown · Jan 21, 2026 · N356UP · Boeing 76734AF · Engine (Turbine/Turboprop)
  > R STARTER CUTOUT (MOMENTARY) ENG FLUX OUT OF LIMITS SHUTDOWN AT FL370 DEIVERT TO CYYT STATUS MSGS RENG REV POS, RENG CONTROL, R ENG EEC C1 #2 ENGINE WAS R&R'D. SEE TASK CODE T3F18E00851E7.
- [SDR IPXA2026012213913](https://openairdocs.org/sdr/IPXA2026012213913.md): Starter · faulted · Jan 21, 2026 · N356UP · Boeing 76734AF · Engine Cranking
  > DIVERTED RT STARTER CUTOUT (MOMENTARY) ENG FLUX OUT OF LIMITS SHUTDOWN AT FL370 DIVERT TO CYYT STATUS MSGS RENG REV POS, RENG CONTROL, R ENG EEC C1
- [SDR IPXA2025090263446](https://openairdocs.org/sdr/IPXA2025090263446.md): Angle · cracked · Sep 1, 2025 · N356UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > MEC BAY CEILING AREA LEFT HAND SIDE, BS 246, LBL40 ANGLE CRACK REPAIR CRACKED.
- [SDR IPXA2025012345579](https://openairdocs.org/sdr/IPXA2025012345579.md): Ceiling Panel · damaged · Jan 17, 2025 · N356UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FOUND THE CEILING PANEL WITH SCRATCH DAMAGE IN AFT CARGO COMPARTMENT, P/N: 453T1862-57. (REPAIR). I.A.W AMM 25-52-01-404-049-001 REV.144 INSTALL AFT CARGO CEILING PANEL AND CONDITION CHECK NORMAL.P/N:453T1862-57.
- [SDR IPXA2025012145579](https://openairdocs.org/sdr/IPXA2025012145579.md): Ceiling Panel · damaged · Jan 17, 2025 · N356UP · Boeing 76734AF · Passenger Compartment Equipment
  > FOUND THE CEILING PANEL WITH SCRATCH DAMAGE IN AFT CARGO COMPARTMENT, P/N: 453T1862-57. (REPAIR) I.A.W AMM 25-52-01-404-049-001 REV.144 INSTALL AFT CARGO CEILING PANEL AND CONDITION CHECK NORMAL.
- [SDR IPXA2025011728784](https://openairdocs.org/sdr/IPXA2025011728784.md): Angle · cracked · Jan 16, 2025 · N356UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FOUND THE ANGLE CRACK AT STA 1578 LBL 80 INBOARD IN BULK CARGO COMPARTMENT LEFT AREA (REPLACE). INSTALL NEW PART I.A.W SRM 51-40-02-0G REV.91 AND BOEING DWG NO: 146T5650 SHEET 5 REV:C.
- [SDR IPXA2025011626595](https://openairdocs.org/sdr/IPXA2025011626595.md): Floor Panel · dented · Jan 16, 2025 · N356UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND MAIN DECK FLOOR PANEL DENT, P/N: 143T5876-99 (REPAIR). REQUEST PERFORM MAIN DECK CARGO FLOOR PANEL OK TO INSTALL CHECK. P/N:143T5876-99. THIS REPAIR IS CONSIDERED MAJOR PER GMM 05.04.01.02 CLASSIFICATION OF REPAIRS. REPAIR PER SREO-9693.
- [SDR IPXA2025011626558](https://openairdocs.org/sdr/IPXA2025011626558.md): Floor Panel · dented · Jan 16, 2025 · N356UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND MAIN DECK FLOOR PANEL DENT, P/N: 143T5876-75 (REPAIR). REQUEST PERFORM MAIN DECK CARGO FLOOR PANEL OK TO INSTALL CHECK. P/N:143T5876-75. THIS REPAIR IS CONSIDERED MAJOR PER GMM 05.04.01.02 CLASSIFICATION OF REPAIRS. REPAIR PER SREO-9693.
- [SDR IPXA2025011626521](https://openairdocs.org/sdr/IPXA2025011626521.md): Floor Panel · broken · Jan 16, 2025 · N356UP · Boeing 76734AF · Fuselage Floor Panel
  > BROKEN - FND M/D CGO FLOOR PANEL BROKEN AT STA 890, RBL 3 P/N:145T5876-85 (REPAIR). REQUEST PERFORM MAIN DECK CARGO FLOOR PANEL OK TO INSTALL CHECK. P/N:145T5876-85. THIS REPAIR IS CONSIDERED MAJOR PER GMM 05.04.01.02 CLASSIFICATION OF REPAIRS. REPAIR PER S
- [SDR IPXA2025011728641](https://openairdocs.org/sdr/IPXA2025011728641.md): Sidewall Panel · cracked · Jan 16, 2025 · N356UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > CRACK - BOTTOM CHORDS, STA 1065, SUPPORT AFT CARGO COMPARTMENT FWD WALL PANEL, (RH) LOWER CORNER, ZONE: 152 (REPLACE). INSTALL NEW PARTS I.A.W SRM 51-40-02-0G REV.91 AND BOEING DWG NO. 140T0130 SHEET 50 REV:A.
- [SDR IPXA2025011728715](https://openairdocs.org/sdr/IPXA2025011728715.md): Sidewall Panel · cracked · Jan 16, 2025 · N356UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > BOTTOM CHORDS, STA 1065, SUPPORT AFT CARGO COMPARTMENT FWD WALL PANEL (LH) LOWER CORNER ZONE: 151 (REPLACE). INSTALL NEW PARTS I.A.W SRM 51-40-02-0G REV.91 AND BOEING DWG NO. 140T0130 SHEET 50 REV:A.
- [SDR IPXA2025011626627](https://openairdocs.org/sdr/IPXA2025011626627.md): Floor Panel · dented · Jan 16, 2025 · N356UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND MAIN DECK FLOOR PANEL DENT, P/N: 143T5876-109 (REPAIR). REQUEST PERFORM MAIN DECK CARGO FLOOR PANEL OK TO INSTALL CHECK. P/N:143T5876-109. THIS REPAIR IS CONSIDERED MAJOR PER GMM 05.04.01.02 CLASSIFICATION OF REPAIRS. REPAIR PER SREO-9693.
- [SDR IPXA2025011626563](https://openairdocs.org/sdr/IPXA2025011626563.md): Floor Panel · dented · Jan 16, 2025 · N356UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND MAIN DECK FLOOR PANEL DENT, P/N: 143T5876-110 (REPAIR). REQUEST PERFORM MAIN DECK CARGO FLOOR PANEL OK TO INSTALL CHECK. P/N:143T5876-110. THIS REPAIR IS CONSIDERED MAJOR PER GMM 05.04.01.02 CLASSIFICATION OF REPAIRS. REPAIR PER SREO-9693.
- [SDR IPXA2025011626509](https://openairdocs.org/sdr/IPXA2025011626509.md): Floor Panel · dented · Jan 16, 2025 · N356UP · Boeing 76734AF · Fuselage Floor Panel
  > FAULT - FOUND MAIN DECK FLOOR PANEL DENT, P/N:143T5876-114 (REPAIR). THIS REPAIR IS CONSIDERED MAJOR PER GMM 05.04.01.02 CLASSIFICATION OF REPAIRS. REPAIR PER SREO-9693. REVIEWED
- [SDR IPXA2025011626484](https://openairdocs.org/sdr/IPXA2025011626484.md): Floor Panel · dented · Jan 16, 2025 · N356UP · Boeing 76734AF · Fuselage Floor Panel
  > FAULT - FOUND MAIN DECK FLOOR PANEL DENT, P/N: 143T5876-102 (REPAIR). THIS REPAIR IS CONSIDERED MAJOR PER GMM 05.04.01.02 CLASSIFICATION OF REPAIRS. REPAIR PER SREO-9693. REVIEWED
- [SDR IPXA2025011626464](https://openairdocs.org/sdr/IPXA2025011626464.md): Floor Panel · dented · Jan 16, 2025 · N356UP · Boeing 76734AF · Fuselage Floor Panel
  > FAULT - FOUND MAIN DECK FLOOR PANEL DENT, P/N: 143T5876-104 (REPAIR). THIS REPAIR IS CONSIDERED MAJOR PER GMM 05.04.01.02 CLASSIFICATION OF REPAIRS. REPAIR PER SREO-9693. REVIEWED
- [SDR IPXA2025011626387](https://openairdocs.org/sdr/IPXA2025011626387.md): Floor Panel · dented · Jan 16, 2025 · N356UP · Boeing 76734AF · Fuselage Floor Panel
  > FAULT - FOUND MAIN DECK FLOOR PANEL DENT, P/N: 143T5876-103 (REPAIR). THIS REPAIR IS CONSIDERED MAJOR PER GMM 05.04.01.02 CLASSIFICATION OF REPAIRS. REPAIR PER SREO-9693. REVIEWED
- [SDR IPXA2025011626438](https://openairdocs.org/sdr/IPXA2025011626438.md): Floor Panel · dented · Jan 16, 2025 · N356UP · Boeing 76734AF · Fuselage Floor Panel
  > FAULT - FOUND MAIN DECK FLOOR PANEL DENT, P/N: 143T5876-106 (REPAIR). THIS REPAIR IS CONSIDERED MAJOR PER GMM 05.04.01.02 CLASSIFICATION OF REPAIRS. REPAIR PER SREO-9693. REVIEWED
- [SDR IPXA2025011626392](https://openairdocs.org/sdr/IPXA2025011626392.md): Floor Panel · cracked · Jan 16, 2025 · N356UP · Boeing 76734AF · Fuselage Floor Panel
  > FAULT - FOUND MAIN DECK FLOOR PANEL WITH CRACK DAMAGE, P/N: 146T5869-135 PANEL NO.251XFF (REPAIR). I.A.W AMM 25-57-02-404-016, AMM 25-57-05-404-006, AMM 25-58-04-404-015 AND AMM 25-58-01-404-005 REV.144 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK N
- [SDR IPXA2025011626505](https://openairdocs.org/sdr/IPXA2025011626505.md): Floor Panel · dented · Jan 16, 2025 · N356UP · Boeing 76734AF · Fuselage Floor Panel
  > FAULT - FOUND MAIN DECK FLOOR PANEL DENT, P/N: 143T5876-101 (REPAIR). THIS REPAIR IS CONSIDERED MAJOR PER GMM 05.04.01.02 CLASSIFICATION OF REPAIRS. REPAIR PER SREO-9693. REVIEWED
- [SDR IPXA2025011626513](https://openairdocs.org/sdr/IPXA2025011626513.md): Floor Panel · dented · Jan 16, 2025 · N356UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND MAIN DECK FLOOR PANEL DENT, P/N: 143T5876-111 (REPAIR) OK TO INSTALL (RII ITEM) CHECK OK. OPEN
- [SDR IPXA2025011779614](https://openairdocs.org/sdr/IPXA2025011779614.md): Angle · cracked · Jan 14, 2025 · N356UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FOUND THE ANGLE CRACK AT STA 1578 LBL 80 OUTBOARD IN BULK CARGO COMPARTMENT LEFT AREA. (REPLACE). INSTALL NEW PARTS I.A.W SRM 51-40-02-0G REV.91 AND BOEING DWG NO: 146T5650 SHEET 5 REV:C. I.A.W AMM 25-57-05-404-006 REV.144 INSTALLED MAIN DECK CARGO HANDLING
- [SDR IPXA2025011780088](https://openairdocs.org/sdr/IPXA2025011780088.md): Angle · cracked · Jan 14, 2025 · N356UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FOUND THE ANGLE CRACK AT STA 1578 RBL 80 OUTBOARD IN BULK CARGO COMPARTMENT RIGHT AREA. (REPLACE). INSTALL NEW PARTS I.A.W SRM 51-40-02-0G REV.91 AND BOEING DWG NO: 146T5650 SHEET 5 REV:C. I.A.W AMM 25-57-05-404-006 AND AMM 25-58-04-404-015 REV.144 INSTALLED
- [SDR IPXA2023082826833](https://openairdocs.org/sdr/IPXA2023082826833.md): Apu · unknown · Aug 25, 2023 · N356UP · Boeing 76734AF · Airborne Auxiliary Power Unit (APU) System
  > *** SUPPLEMENTAL SDR *** APU GEN INTERMITTENTLY CUTS ON AND OFF*OII 2* PERFORMED APU BITE PROCEDURE IAW FIM TASK 49-11 FAULT TREE 803. T/S TO FIGURE 103 SH 7 TABLE B 'NORMAL STOP SIG' MESSAGE. FURTHER T/S TP FIM49-11-00/101 FIG 133 FOUND SYS SATIS. APU OPS CK'
- [SDR IPXA2023082526833](https://openairdocs.org/sdr/IPXA2023082526833.md): Unknown · unknown · Aug 25, 2023 · N356UP · Boeing 76734AF · Electrical Power System
  > *** SDR FILED OPEN *** APU GEN INTERMITTENTLY CUTS ON AND OFF*OII 2* DEFERRED APU GEN IAW MEL 22-00-2A. NON ETOPS. PLACARD INSTALLED. DMP C/W
- [SDR IPXA2023110861537](https://openairdocs.org/sdr/IPXA2023110861537.md): Flap · dented · Aug 21, 2023 · N356UP · Boeing 76734AF · Trailing Edge Flaps
  > RIGHT WING OUTBOARD FLAP TRAILING EDGE WEDGE LOWER SKIN DENT. VERIFIED ALL LOTO HAS BEEN REVERSED I AM MM 27-51-00 AND 27-81-00
- [SDR IPXA2023082161537](https://openairdocs.org/sdr/IPXA2023082161537.md): Unknown · unknown · Aug 21, 2023 · N356UP · Boeing 76734AF · Flight Control System
  > RIGHT WING OUTBOARD FLAP TRAILING EDGE WEDGE LOWER SKIN DENT. APPLIED SKIM COAT AND EXTERIOR FINISH TO COMPLETE REPAIR. SRM 51-70-06. OPEN
- [SDR IPXA2023032992378](https://openairdocs.org/sdr/IPXA2023032992378.md): Stiffener · cracked · Mar 23, 2023 · N356UP · Boeing 76734AF · Fuselage Structure (General)
  > INSPECTION TYPE:C5CRACK ON THE STIFFENER (P/N:141T5146-65) OF THE FLOOR BEAM ASSEMBLY AT STA 246, LBL 40.REPAIR I.A.W 767-300F SRM 53-10-51-2R-4 REV 85.01.
- [SDR IPXA2023032992377](https://openairdocs.org/sdr/IPXA2023032992377.md): Support · cracked · Mar 22, 2023 · N356UP · Boeing 76734AF · Fuselage Structure (General)
  > INSPECTION TYPE:C5CRACK ON SUPPORT (P/N:141T5282-2) OF M/D CGO FLOOR BEAM SUPPORT AT STA 246, NEAR LBL 26.INSTALL NEW PARTS I.A.W 767-300F SRM 51-40-02-0G REV.85.01 AND BOEING DWG 141T5104 SH 45,REV.''-''.
- [SDR IPXA2023032992376](https://openairdocs.org/sdr/IPXA2023032992376.md): Unknown · cracked · Mar 22, 2023 · N356UP · Boeing 76734AF · Fuselage Structure (General)
  > INSPECTION TYPE:C5CRACK ON CLIP (P/N:141T5146-16) OF M/D CGO FLOOR BEAM SUPPORT AT STA 246,LBL 49.INSTALL NEW PARTS I.A.W 767-300F SRM 51-40-02-0G REV.85.01 AND BOEING DWG 141T5600 SH 4,REV.''-''.
- [SDR IPXA2023033092423](https://openairdocs.org/sdr/IPXA2023033092423.md): Bracket · cracked · Mar 21, 2023 · N356UP · Boeing 76734AF · Fuselage Structure (General)
  > INSPECTION TYPE:C5CRACK ON BRACKET (P/N:148T7312-43) OF STABILIZER SEAL SEAL FAIRING NEAR STA 1767.25.INSTALL NEW PART I.A.W 767-300F SRM 51-40-02-0G REV.85.01, BOEING DWG 148T7320 SH 4, REV. ''-'' AND BOEING DWG 148T9220 SH 10, REV.''-''.
- [SDR IPXA2023032892337](https://openairdocs.org/sdr/IPXA2023032892337.md): Skin · none · Mar 20, 2023 · N356UP · Boeing 76734AF · Fuselage Structure (General)
  > INSPECTION TYPE:C5FUSELAGE DRAIN HOLES ADDITION AND INSPECTION AFT OF STA 1725.5 BETWEEN S-36L AND S-36R.PERFORM UPS EO B767-2740-82173-C APPX B.
- [SDR IPXA2022041581183](https://openairdocs.org/sdr/IPXA2022041581183.md): Engine · none · Apr 14, 2022 · N356UP · Boeing 76734AF · Powerplant System
  > INSPECTION TYPE:NA**SUPPLEMENTAL SDR**IFSD** DIVERSION**EMERGENCY DECL'D**DURING CRUISE FL370, LH ENG SURGE & LOST THRUST. THRUST LEVER MOVEMENT RESULTED IN NO RESPONSE. AUDIBLE BANG SHUT DOWN ENG/ WITH FUEL CONTROL SWITCH. RAN ENG QRH.PERFORMED FIM TASK AMM 7
- [SDR IPXA2021052469785](https://openairdocs.org/sdr/IPXA2021052469785.md): Sensor · dirty · May 21, 2021 · N356UP · Boeing 76734AF · Door Warning System
  > INSPECTION TYPE:NAL FWD ENT DOOR EICAS CAME ON AFTER LANDING AND WENT OUT JUST PRIOR TO BLOCK IN. THIS CAUSED THE ACARS TO SHOW US BLOCKED IN AS SOON AS THE LIGHT CAME ON.L FWD ENTRY DOOR INSPECTED SENSORS CLEANED OPERATIONAL CHECK C/O IAW AMM 52-12-00-601 REV
- [SDR IPXA2021032467216](https://openairdocs.org/sdr/IPXA2021032467216.md): Floor Panel · damaged · Mar 24, 2021 · N356UP · Boeing 76734AF · Fuselage Floor Panel
  > INSPECTION TYPE:C4DAMAGE ON M/D FLOOR PANEL AT STA 412, RBL 11 - LBL 11.FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NO. B767-5320-9693-I.
- [SDR IPXA2021032467215](https://openairdocs.org/sdr/IPXA2021032467215.md): Floor Panel · damaged · Mar 23, 2021 · N356UP · Boeing 76734AF · Fuselage Floor Panel
  > INSPECTION TYPE:C4DAMAGE ON M/D FLOOR PANEL AT STA984, RBL 33 - RBL 54.FABRICATE THE REPLACEMENT PANEL PER EO NO. B767-5320-9693-I.
- [SDR IPXA2021032667283](https://openairdocs.org/sdr/IPXA2021032667283.md): Skin · cracked · Mar 17, 2021 · N356UP · Boeing 76734AF · Leading Edge Devices
  > INSPECTION TYPE:C4CRACK ON THE NO.5 SLAT SKIN (P/N:114T4105-23) NEAR OSS 492.95.REPAIR I.A.W. 767-300F SRM 57-43-01-2R-2 REV.79.01
- [SDR IPXA2020102661691](https://openairdocs.org/sdr/IPXA2020102661691.md): Skin · damaged · Oct 26, 2020 · N356UP · Boeing 76734AF · Fuselage Main, Plate/Skin
  > DENT AND GOUGE ON RH SIDE OF FUSELAGE. REPAIRED, IAW EO B767-5330-78150. REPAIRED IAW EO B767-5330-78150.
- [SDR IPXA2020021765173](https://openairdocs.org/sdr/IPXA2020021765173.md): Skin · punctured · Feb 16, 2020 · N356UP · Boeing 76734AF · Elevator, Plate/Skin
  > INSPECTION TYPE:N/ALH INBD EVELVATOR HAS A SKIN PUNCTURE ON UPPER SURFACEREPAIRED IAW UPS E.O. B767-5520-75204 ON NRC 655755
- [SDR IPXA2019111348952](https://openairdocs.org/sdr/IPXA2019111348952.md): Seal · leaking · Nov 13, 2019 · N356UP · Boeing 76734AF · Passenger/Crew Doors
  > INSPECTION TYPE:N/AMAIN ENTRY DOOR SIGNIFICANT SEAL LEAKING AT BOTTOM CABIN LEAKING AT BOTTOM CABIN ALTITUDE NORMAL AT FLY 200 LEAK STARTED GOING GOING THOUGH 8,000FTREMOVED AND REPLACED MAIN ENTRY DOOR SEAL UP TO STEP E (2) OF 767 M/M DMP 52-09-01-424-019{ 05
- [SDR IPXA201906243587](https://openairdocs.org/sdr/IPXA201906243587.md): Seal · out of position · Jun 21, 2019 · N356UP · Boeing 76734AF · Passenger/Crew Doors
  > LOUD AIR LEAK AT BOTTOM OF CREW ENTRY DOOR DURING CLIMB OUT. PRESSURIZATION WAS GOOD DOOR SEAL IS LOOSE AT BOTTOM. REINSTALLED SEAL INTO THE SEAL RETAINER ON THE CREW ENTRY DOOR. IAW AMM 52-09-61-424-019
- [SDR IPXA2019031740128](https://openairdocs.org/sdr/IPXA2019031740128.md): Floor Panel · damaged · Mar 5, 2019 · N356UP · Boeing 76734AF · Fuselage Floor Panel
  > INSPECTION TYPE:C3 DAMAGE ON M/D CARGO FLOOR PANEL AT STA 1114 - STA 1197 PLUS 22, LBL 55 - LBL 77, PNL NR 251DFF. FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NR B767-5320-9693-I
- [SDR IPXA2019031740127](https://openairdocs.org/sdr/IPXA2019031740127.md): Floor Panel · damaged · Mar 5, 2019 · N356UP · Boeing 76734AF · Fuselage Floor Panel
  > INSPECTION TYPE:C3 DAMAGE ON M/D CARGO FLOOR PANEL AT STA 1114-STA 1197 PLUS 22, LBL 33 - LBL 55, PNL NO.251CFF. FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NR B767-5320-9693-I.
- [SDR IPXA2019021549018](https://openairdocs.org/sdr/IPXA2019021549018.md): Seal · dislodged · Feb 14, 2019 · N356UP · Boeing 76734AF · Doors
  > AFT PART CREW ENTRY DOOR LEAKS.NOISE HEARD AT 5500.2 DIFFERENTIAL PRESSURE. ABOUT 1,000 CABIN ALTITUDEDOOR & FRAME INSPECTED. FOUND 3" SECTION OF LOWER DOOR SEALPARTIALLY DISLODGED FROM CHANNEL. DOOR SEAL INSTALLED IAW AMM TASK 52-09-01-424-019. NO FURTHER DE
- [SDR IPXA2017120524215](https://openairdocs.org/sdr/IPXA2017120524215.md): Fan · malfunctioned · Dec 4, 2017 · N356UP · Boeing 76734AF · Air Distribution Fan
  > INSPECTION TYPE:FWD EQUIP EXH FAN STATUS MSG ON. FWD EQUIP COOLING EXHT FAN - ONE SUPPLY FAN INSTALL. AUTHORIZED BY 0557835. PLACARD INSTALLED. MEL/CDL 21-58-04-02-01. DMP ACCOMPLISHED BY KOENIG 0555527. R/R FWD EQUIP COOLING EXHT FAN PER AMM 21-58-06-401.
- [SDR IPXA2017072119602](https://openairdocs.org/sdr/IPXA2017072119602.md): Sleeve · missing · Jul 21, 2017 · N356UP · Boeing 76734AF · Engine Thrust Reverser
  > RIGHT ENGINE INBD THRUST REVERSER COWL INNER TRANSLATING SLEEVE MISSING THE SURFACE FILLER MATERAL AT THE 9 O`CLOCK POSITION, TWO PLACES. REPAIRED IAW SREO M-7830-24149-E.
- [SDR IPXA2016062004800](https://openairdocs.org/sdr/IPXA2016062004800.md): Skin · damaged · Jun 20, 2016 · N356UP · Boeing 76734AF · Rudder, Plate/Skin
  > RUDDER UPPER T/E LIGHTNING STRIKE DAMAGED. REF LOG PAGE 238111, REPAIRED REF EO 5540-60426-B.
- [SDR IPXA2015072791637](https://openairdocs.org/sdr/IPXA2015072791637.md): Evas Unit · no test · Jul 27, 2015 · N356UP · Boeing 76734AF · Emergency Equipment
  > CAPTAIN`S EMERGENCY VISION ASSURANCE SYSTEM FAILED THE SYSTEM TEST IAW T/C 25-069-00, BLOWER DID NOT ACTUATE DURING TEST. REPLACED THE CAPTAIN'S EVAS UNIT IAW MM 25-69-00-400-801-3. OPS CHECKED GOOD.

## 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 = 'N356UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N356UP/reports

---
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