# Service difficulty reports: N363UP

A list on [N363UP](https://openairdocs.org/aircraft/N363UP.md).

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

- [SDR IPXA2026072237604](https://openairdocs.org/sdr/IPXA2026072237604.md): Adapter · chafed · Jul 19, 2026 · N363UP · Boeing 737300 · Nacelle/Pylon Miscellaneous Structure
  > CHAFED BRACKET, NR 2 ENG LT CORE COWL OPEN ROD HOLD BRACKET. REMOVED DAMAGE BRACKETS IAW SRM 51-40-02-0G, REV 55. INSTALLED NEW BRACKETS IAW SRM 51-40-02-0G, REV 55, AND CMM IPL 71-13-23, REV 47.
- [SDR IPXA2026072237841](https://openairdocs.org/sdr/IPXA2026072237841.md): Bracket · chafed · Jul 19, 2026 · N363UP · Boeing 767346 · Nacelle/Pylon Miscellaneous Structure
  > CHAFED BRACKET, NR 2 ENG RT CORE COWL OPEN ROD HOLD BRACKET. REMOVED DAMAGE BRACKETS IAW SRM 51-40-02-0G, REV 55. INSTALLED NEW BRACKETS IAW SRM 51-40-02-0G, REV 55, AND CMM IPL 71-13-24, REV 51.
- [SDR IPXA2026072835996](https://openairdocs.org/sdr/IPXA2026072835996.md): Drain Mast · cracked · Jul 19, 2026 · N363UP · Boeing 767346 · Nacelle/Pylon, Main Frame
  > CRACKED MAST, NR 1 ENG LWR DRAIN MAST. IAW AMM 71-71-01-024-001-H00, REV 148, AND AMM 71-71-01-424-005-H00, REV.148, REPLACED THE DRAIN MAST OF NR 1 ENGINE.
- [SDR IPXA2026072035996](https://openairdocs.org/sdr/IPXA2026072035996.md): Drain Mast · cracked · Jul 19, 2026 · N363UP · Boeing 767346 · Engine (Turbine/Turboprop)
  > CRACKED MAST, NR1 ENG LWR DRAIN MAST. (REPLACE)
- [SDR IPXA2026072422572](https://openairdocs.org/sdr/IPXA2026072422572.md): Skin · cracked · Jul 18, 2026 · N363UP · Boeing 767346 · Nacelle/Pylon, Plate/Skin
  > CRACKED NR 2 PYLON FAIRING PANEL 447 ELX. ACCOMPLISH THE REPAIR IAW SRM 54-52-70-2R-4, REV 55, AND EGAT WORK SHEET 60557.
- [SDR IPXA2026072223130](https://openairdocs.org/sdr/IPXA2026072223130.md): Support · cracked · Jul 18, 2026 · N363UP · Boeing 767346 · Horizontal Stabilizer Miscellaneous Structure
  > CRACKED SUPPORT, LEFT HORIZONTAL STAB BODY SEAL 313CLX LAST ONE FITTING. INSTALLED NEW SUPPORT IAW SRM 51-40-02-0G, REV 55, AND DWG 182T7119, SHT 1, REV D.
- [SDR IPXA2026072223167](https://openairdocs.org/sdr/IPXA2026072223167.md): Support · cracked · Jul 18, 2026 · N363UP · Boeing 767346 · Horizontal Stabilizer Miscellaneous Structure
  > CRACK SUPPORT, RIGHT HORIZONTAL STABILIZER BODY SEAL NO.314CRX LAST ONE FITTING. INSTALLED NEW SUPPORT IAW SRM 51-40-02-0G, REV 55, AND DWG 182T7119 SH 1, REV D.
- [SDR IPXA2026072223255](https://openairdocs.org/sdr/IPXA2026072223255.md): Seal · cracked · Jul 18, 2026 · N363UP · Boeing 767346 · Nacelle/Pylon, Main Frame
  > CRACKED ZEE SEAL, NR 1 PYLON LT AFT FAIRING DOOR CUTOUT LWR, AFT SEAL AREA. INSTALLED FABRICATED ZEE SEAL IAW SRM 51-40-02-0G, REV 55, AND DWG 313T2380, SHT 68, REV A, & DWG 313T2303, SH 90, REV C, & SB 767-54-0109, REV 2.
- [SDR IPXA2026072707922](https://openairdocs.org/sdr/IPXA2026072707922.md): Floor Panel · delaminated · Jul 17, 2026 · N363UP · Boeing 767346 · Fuselage Floor Panel
  > THE FLOOR PANEL IN THE AFT CARGO COMPARTMENT IS DELAMINATED. IAW AMM 53-01-05-404-004, REV 148, INSTALLED THE FLOOR PANEL. CONDITION CHKD NORMAL.
- [SDR IPXA2026072204865](https://openairdocs.org/sdr/IPXA2026072204865.md): Retainer · broken · Jul 17, 2026 · N363UP · Boeing 767346 · Nacelle/Pylon Miscellaneous Structure
  > MISSING ZEE SEAL, NR 2 ENG RT AFT FAIRING LOWER AFT AREA. INSTALLED NEW ZEE SEAL IAW SRM 51-40-02-0G, REV 55, AND DWG NR 313T2380 SH. 68 REV. A.
- [SDR IPXA2026071803780](https://openairdocs.org/sdr/IPXA2026071803780.md): Angle · cracked · Jul 17, 2026 · N363UP · Boeing 767346 · Fuselage Miscellaneous Structure
  > THE BULK CARGO INBD ANGLE AT BS 1578, LBL 80 CRACKED. REMOVED DAMAGE ANGLE IAW SRM 51-40-02-0G, REV 55. INSTALLED FABRICATED ANGLE IAW SRM 51-40-02-0G, REV 55, AND DWG 657T1332, SHEET 5, REV A.
- [SDR IPXA2026071807167](https://openairdocs.org/sdr/IPXA2026071807167.md): Angle · cracked · Jul 17, 2026 · N363UP · Boeing 767346 · Fuselage Miscellaneous Structure
  > THE BULK CARGO OUTBOARD ANGLE AT BS 1578 LBL 80 IS CRACKED. INSTALLED NEW ANGLE IAW SRM 51-40-02-0G, REV 55, AND DWG 657T1332, SHT 5, REV A.
- [SDR IPXA2026072889610](https://openairdocs.org/sdr/IPXA2026072889610.md): Splice Plate · broken · Jul 16, 2026 · N363UP · Boeing 767346 · Wing Main, Frame Structure
  > BROKEN SPLICE PLATE, UPPER FACE OF LT WING INBD T/E UPPER FIXED PANEL, WBL 127. INSTALLED NEW SPLICE PLATE IAW SRM 51-40-02-0G, REV 55, AND DWG 113T1900, SHT 1, REV C, AND DWG 113T1603, SHT 1. REV B.
- [SDR IPXA2026072889321](https://openairdocs.org/sdr/IPXA2026072889321.md): Channel · corroded · Jul 16, 2026 · N363UP · Boeing 767346 · Auxiliary Power Unit (APU) Doors
  > LEFT APU DOOR HAS LIGHT CORROSION AT INBD INTERNAL SIDE. ACCOMPLISHED CORROSION DAMAGE REPAIR IAW EO-98128-REQ1, REV1, AND DWG 148T6551, SHEET 3, REV B. JOB COMPLETED.
- [SDR IPXA2026072485434](https://openairdocs.org/sdr/IPXA2026072485434.md): Fitting · cracked · Jul 16, 2026 · N363UP · Boeing 767346 · Engine Thrust Reverser
  > CRACKED FITTING, NR 1 ENG LT T/R FWD TORQUE BOX UPR ACTUATOR FITTING CRACK. INSTALLED NEW FITTING IAW SRM 51-40-02-0G, REV 55, AND IPC 78-32-21, REV 96.
- [SDR IPXA2026072289584](https://openairdocs.org/sdr/IPXA2026072289584.md): Beam · cracked · Jul 16, 2026 · N363UP · Boeing 767346 · Nacelle/Pylon Miscellaneous Structure
  > CRACKED BEAM, NR 2 ENG RT AFT FAIRING LOWER BEAM AFT AREA. NSTALLED NEW BEAM IAW SRM 51-40-02-0G, REV 55, SB 767-54-0109, REV 1, DWG 313T2380, SHT 88, REV A, DWG 313T2303, SHT 90, REV C, DWG 313T2303, SHT 94, REV C, & DWG 313T2303, SHT 95, REV C.
- [SDR IPXA2026072051088](https://openairdocs.org/sdr/IPXA2026072051088.md): Battery Pack · no test · Jul 14, 2026 · N363UP · Boeing 767346 · Emergency Lighting
  > FOUND EMERGENCY BATTERY PACK FAILED TO ILLUMINATE FOR 15 MINUTES. IAW AMM 33-51-07-022-001, AND 33-51-07-422-012, REV 148. REPLACED EMERGENCY LIGHT BATTERY PACK.
- [SDR IPXA2026071551088](https://openairdocs.org/sdr/IPXA2026071551088.md): Battery Pack · inoperative · Jul 14, 2026 · N363UP · Boeing 767346 · Emergency Lighting
  > FOUND EMERGENCY BATTERY PACK FAILS TO ILLUMINATE FOR 15 MINUTES. (REPLACE).
- [SDR 2025FA0000792](https://openairdocs.org/sdr/2025FA0000792.md): Rudder Pedal · obstructed · Nov 30, 2025 · N363UP · Boeing 767346 · Rudder Control System
  > FIRST OFFICER’S RUDDER PEDALS STIFF AND REQUIRE EXTRA FORCE. IAW AMM 27-21-05-214-033. RUDDER PEDALS OPERATED THROUGH FULL TRAVEL RANGE, NO OBVIOUS STIFFNESS NOTED. PEDALS MOVED FREELY THROUGH THEIR FULL RANGE WITH RUDDER OPERATING CORRECTLY WITH THE POSITIO
- [SDR IPXA2025102909684](https://openairdocs.org/sdr/IPXA2025102909684.md): Window · cracked · Oct 29, 2025 · N363UP · Boeing 767346 · Flight Compartment Windows
  > AIR TURN BACK PRESSURIZATION LEAK AFTER APPROXIMATELY 60 MINUTES ENROUTE-INCREDIBLY LOUD SQUEAL MADE COMM DIFFICULT/ATC+ BETWEEN FLT CREW. NOISE STOPPED BELOW 17000 FEET. ACCOMPLISHED T/S AND INSPECTION IAW AMM 56-11-00-210-016 REV 146. FOUND CRACK APP 3 INCH
- [SDR IPXA2025092946537](https://openairdocs.org/sdr/IPXA2025092946537.md): Apu · odor · Sep 25, 2025 · N363UP · Boeing 767346 · Airborne Auxiliary Power Unit (APU) System
  > WITH APU ON - TURNING ON FIRST PACK WE ARE HAVING HEAVY OIL SMELL FUMES IN COCKPIT. TS PERFORMED FOR OIL SMELL FUMES IN THE COCKPIT IAW FIM 21-00-21/201 REV 146. OIL SMELL FUMES NOT OBSERVED. AIR CONDITIONING SYSTEM OPERATIONAL TEST PERFORMED WITH APU BLEED IA
- [SDR IPXA2025092546537](https://openairdocs.org/sdr/IPXA2025092546537.md): A/C Pack · odor · Sep 25, 2025 · N363UP · Boeing 767346 · Cabin Cooling System
  > WITH APU ON, TURNING ON FIRST PACK WE ARE HAVING HEAVY OIL SMELL FUMES IN COCKPIT.
- [SDR IPXA2025062778700](https://openairdocs.org/sdr/IPXA2025062778700.md): Cover · damaged · Apr 22, 2025 · N363UP · Boeing 767346 · Fuselage, Door Hinge
  > MAIN ENTRY DOOR ARMING LEVER HINGED DOOR COVER DAMAGED REPLACED CREW ENTRY DOOR HINGE COVER IAW. AMM 52-12-02 PB 401 REV. 145. THIS CLOSES DMI. PLACARD REMOVED.
- [SDR IPXA2025042278700](https://openairdocs.org/sdr/IPXA2025042278700.md): Cover · damaged · Apr 22, 2025 · N363UP · Boeing 767346 · Passenger/Crew Doors
  > MAIN ENTRY DOOR ARMING LEVER HINGED DOOR COVER DAMAGED DEFERRED PER MEL 52-11-2. DI LOG UPDATED. PLACARD INSTALLED. BROKEN COVER PUT IN PFM WITH HARDWARE ATTACHED.
- [SDR IPXA2025020393810](https://openairdocs.org/sdr/IPXA2025020393810.md): Windshield · haze · Jan 30, 2025 · N363UP · Boeing 767346 · Flight Compartment Windows
  > ENTIRE RIGHT (FO) WINDSHIELD APPEARS FOGGY/HAZY IE DELAMINATION. ACCOMPLISHED RII FOR WINDOW HEAT CONTROL TERMINAL CONNECTION IAW. GMM 04.02.01 REV. 10.
- [SDR IPXA2024120409724](https://openairdocs.org/sdr/IPXA2024120409724.md): Slat System · malfunctioned · Dec 3, 2024 · N363UP · Boeing 767346 · Leading Edge Slat Control System
  > LE SLAT ASYM PSEU BITE PERFORMED SATIS IAW FIM 32-09 FT 803 AND OPS CHECKED SATIS IAW AMM 27-81-00/501. NO FAULTS FOUND. PLEASE MONITOR
- [SDR IPXA2024120243168](https://openairdocs.org/sdr/IPXA2024120243168.md): Slat System · warning message · Nov 28, 2024 · N363UP · Boeing 767346 · Leading Edge Slat Control System
  > AFTER TAKEOFF RECEIVED €ŒLE SLAT ASYM EICAS€? T/S C/O IAW FIM 32-09-00/101 FAULT TREE 803 REV 143, PSEU BITE TEST SATIS NO FAULT FOUND. CONNECTOR D4434 CLEANED IAW SWPM 20-10-04 REV 87 & SENSOR S279 MEASURED BETWEEN PIN 9 & 10 GOT 18 OHM, CONNECTOR D4486 CLE
- [SDR IPXA2024081995256](https://openairdocs.org/sdr/IPXA2024081995256.md): Channel · cracked · Aug 10, 2024 · N363UP · Boeing 767346 · Fuselage Miscellaneous Structure
  > FAULT - CRACK - SUPPORT AND ANGLE, AFT CGO L/H STA 1153-1175 LBL 77.5 (REPLACE) FABRICATE P/N: 212T3416-4 PER BOEING DWG NO: 212T3416 SH 2 REV."-"; PL REV."B"; PSDL REV."-" AND P/N: 212T3418-1 PER BOEING DWG NO: 212T3418 SH 2 REV."-"; PL REV."C"; PSDL REV."-"
- [SDR IPXA2024081754222](https://openairdocs.org/sdr/IPXA2024081754222.md): Floor Panel · damaged · Aug 8, 2024 · N363UP · Boeing 767346 · Fuselage Floor Panel
  > FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 814T3538-20. (REPAIR) I.A.W. UPS EO-91096-REQ1 REV.1 COMPLETE THE FAULT.
- [SDR IPXA2024081754196](https://openairdocs.org/sdr/IPXA2024081754196.md): Floor Panel · damaged · Aug 8, 2024 · N363UP · Boeing 767346 · Fuselage Floor Panel
  > FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 814T3538-68. (REPAIR) I.A.W. UPS EO-91096-REQ1 REV.1 COMPLETE THE FAULT.
- [SDR IPXA2024081431948](https://openairdocs.org/sdr/IPXA2024081431948.md): Drain · none · Aug 7, 2024 · N363UP · Boeing 767346 · Standard Practices/Structures
  > *** SUPPLEMENTAL SDR *** MAJOR REPAIR *** ADD SDR FOR EO-82173-JIC001 (FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) COMPLETED SDR.
- [SDR IPXA2024080731948](https://openairdocs.org/sdr/IPXA2024080731948.md): Drain · none · Aug 7, 2024 · N363UP · Boeing 767346 · Standard Practices/Structures
  > FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R. OPEN
- [SDR IPXA2023101060108](https://openairdocs.org/sdr/IPXA2023101060108.md): Flap System · warning message · Oct 7, 2023 · N363UP · Boeing 767346 · Trailing Edge Flaps
  > "FLAP ASYM" LIGHT AND EICAS MSG DURING CLIMB OUT SENSOR 279, TARGET CLEARANCE ADJUSTED, AMM SUBTASK 27-88-01-822-160, REV NO. / DATE: 140 / 11 SEP 2023, OUTBOARD AND INBOARD SLAT AUXILIARY TRACK ROLLERS AND SIDE BRACE LINKS LUBRICATED, REFERENCE: AMM TASK 12-
- [SDR IPXA2018071331627](https://openairdocs.org/sdr/IPXA2018071331627.md): Frame · cracked · Jul 13, 2018 · N363UP · Boeing 767346 · Fuselage Main, Frame
  > INSPECTION TYPE:C, CRACK FOUND APPROX 0.2" LENGTH DURING HFEC INSPECTION ON RT STA 903.5 BL 89 BELOW WL 200 AT FRAME INNER CHORD TRANSITION RADIUS. FRAME INNER CHORD TRANSITION RADIUS AT STA 903 RBL 89 CARRIED OUT REPAIR AS PER EO B767-5310-68072-A APPENDIX B.
- [SDR IPXA2018070931455](https://openairdocs.org/sdr/IPXA2018070931455.md): Doubler · corroded · Jul 7, 2018 · N363UP · Boeing 767346 · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C1, FUSELAGE KEELBEAM MANHOLE DOUBLER FROM STA 810-840 FOUND CORROSION. REMOVED DOUBLER AND ANGLE NUT PN: BACN10JN3 FOR ACCESS CORROSION BLENDED OUT REWORK AREA SMOOTHEN SIZE OF RWK L=1.0"X W=0'5" ORIGINAL THK =0'080" MATERIAL REMOVED =0'003"
- [SDR IPXA201804309058](https://openairdocs.org/sdr/IPXA201804309058.md): Skin · corroded · Apr 25, 2018 · N363UP · Boeing 767346 · Fuselage Main, Plate/Skin
  > INSPECTION TYPE: C4, SURFACE CORROSION FOUND ON THE LOWER FASTENER HOLE OF THE SKIN AT BS 955 TEE FITTING. REMOVED THE SURFACE CORROSION.

## 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 = 'N363UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N363UP/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.