# Service difficulty reports: N395UP

A list on [N395UP](https://openairdocs.org/aircraft/N395UP.md).

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

- [SDR IPXA2026042684022](https://openairdocs.org/sdr/IPXA2026042684022.md): Timer · faulted · Apr 25, 2026 · N395UP · Boeing 767316 · Fuel Boost Pump
  > FOUND FAULTY TIME DELAY K5 FOR R FWD BOOST PUMP REPLACED THE TIME DELAY K5 RELAY IAW SWPM:20-81-11 REV.38 AND FOUND OPS TEST OF RT FWD FUEL PUMP SATISFACTORY IAW AMM:28-22-00/501 REV.148 CONFIRMED ALL PARTS AND TOOLS REMOVED FROM ACFT.
- [SDR IPXA2026022511384](https://openairdocs.org/sdr/IPXA2026022511384.md): Flap · none · Feb 14, 2026 · N395UP · Boeing 767316 · Trailing Edge Flaps
  > DOUBLER, REPAIR DOUBLER NOT EXIST ON MAPPING, RIGHT WING INBD FLAP AFT FLAP UPPER SURFACE, WBL 265 (AGING INSPECTION (NO.4734) (EVALUATE). ACCOMPLISH REPAIR PER 767-300 SRM 57-53-01-2R-1, 51-70-10-2R-0 AND 51-70-10-2R-4 REV. 130, WITHOUT DEVIATION. REVIEW CO
- [SDR IPXA2026022411434](https://openairdocs.org/sdr/IPXA2026022411434.md): Floorbeam · cracked · Feb 14, 2026 · N395UP · Boeing 767316 · Fuselage Main, Floor Beam
  > CRACKED BRACKET, MAIN DECK FLOOR BEAM TO FUSELAGE BRACKET, STA 917 S-21L (AGING INSPECTION) (NO.4736) (REPLACE). INSTALL REPAIR PART -T01 STRINGER CLIP AS SHOWN IN FIGURE 2 AND PER IAI DWG 371-53-00-C4181-001 REQUIREMENTS. ACCOMPLISHED REPAIR I.A.W EO-96668-R
- [SDR IPXA2026022470882](https://openairdocs.org/sdr/IPXA2026022470882.md): Rib · cracked · Feb 12, 2026 · N395UP · Boeing 767316 · Wing, Rib/Bulkhead
  > CRACKED FITTING, RT WING OTBD L/E RIB LES 600, NOSE INTERIOR. INSTALLED A FABRICATED RIB IAW SRM 51-40-02-0G, REV 130, AND DWG 114T2606, SHEET 1, REV E, DWG 114T2601, SHEET 1, REV B, DWG 114T2301, SHEET 3, REV C, DWG 114T2250, SHEET 1, REV A, DWG 114T224
- [SDR IPXA2026022546988](https://openairdocs.org/sdr/IPXA2026022546988.md): Splice · corroded · Feb 11, 2026 · N395UP · Boeing 767316 · Fuselage Main, Keel
  > CORROSION-SPLICE TEE, SEC45 LOWER FUSELAGE KEEL AREA BS 910, RBL 9.5 INNER SURFACE (AGING INSPECTION) (NO.4701). INSTALLED NEW SPLICE TEE I.A.W SRM 51-40-02-0G REV. 130 AND DWG 145T8629 SH. 2 REV. A.
- [SDR IPXA2026022024931](https://openairdocs.org/sdr/IPXA2026022024931.md): Skin · cracked · Feb 10, 2026 · N395UP · Boeing 767316 · Passenger/Crew Doors
  > MAJOR REPAIR, CRACKED FWD ENTRY DOOR LT AFT LOWER CORNER SKIN. INSTALLED THE DOORWAY LINING IAW AMM 52-11-02-404-025, REV. 80.
- [SDR IPXA2026022024904](https://openairdocs.org/sdr/IPXA2026022024904.md): Skin Panel · cracked · Feb 10, 2026 · N395UP · Boeing 767316 · Fuselage Main, Plate/Skin
  > CRACK, FWD ENTRY DOOR RH AFT LOWER CORNER SKIN. (REPAIR). ACCOMPLISH THE REPAIR I.A.W EO-87307-REQ8 REV2 AND SRM 53-10-01-2R-1 REV.130 AND EGAT WORK SHEET NO.60098. REVIEW COMPLETE.
- [SDR IPXA2026030322790](https://openairdocs.org/sdr/IPXA2026030322790.md): Depressor · deformed · Feb 10, 2026 · N395UP · Boeing 767316 · Fuselage Main, Structure
  > DEFORMED SILL, MAIN DECK CARGO DOOR CUTOUT AFT EDGE. FABRICATE IAW DWG 368-53-00-95379, SH 2, REV F, PL REV M, & GMM-MTX, 9.08, REV 14. INSTALLED THE FABRICATED PART IAW SRM 51-40-02-0G, REV 130, AND DWG 368-53-00-95301, SH 6, ISSUE AV.
- [SDR IPXA2026030223168](https://openairdocs.org/sdr/IPXA2026030223168.md): Channel · cracked · Feb 10, 2026 · N395UP · Boeing 767316 · Nacelle/Pylon Miscellaneous Structure
  > CRACKED CHANNEL, NR 1 PYLON AFT FAIRING PANEL 437DB INNER OTBD SIDE CHANNEL. INSTALLED A NEW BULKHEAD ANGLE IAW SRM 51-40-02-0G, REV 130 AND DWG 313T2362, SHT 4, REV B.
- [SDR IPXA2026022523383](https://openairdocs.org/sdr/IPXA2026022523383.md): Bracket · cracked · Feb 10, 2026 · N395UP · Boeing 767316 · Nacelle/Pylon Miscellaneous Structure
  > CRACKED BRACKET, NR 2 PYLON INTERNAL RESERVOIR HYD TUBE SUPPORT BRACKET AT R/H SIDE UPPER HINGE BEAM AREA. (REPLACE). IAW SRM 51-40-02-0G REV. 130 AND AIPC 54-51-53-18 REV. 36 INSTALLED NEW BRACKET.
- [SDR IPXA2026022410668](https://openairdocs.org/sdr/IPXA2026022410668.md): Channel · cracked · Feb 9, 2026 · N395UP · Boeing 767316 · Nacelle/Pylon Miscellaneous Structure
  > CRACKED CHANNEL, NR 1 PYLON AFT FAIRING INNER AFT BULKHEAD INBD SIDE CHANNEL. (REPLACE). INSTALLED NEW CHANNEL I.A.W SRM 51-40-02-0G REV. 130 AND BOEING DWG NO. 313T3380 SH. 5 REV. H AND 313T2362 SH. 4 REV. B. REVIEW COMPLETE.
- [SDR IPXA2026022510717](https://openairdocs.org/sdr/IPXA2026022510717.md): Channel · cracked · Feb 9, 2026 · N395UP · Boeing 767316 · Nacelle/Pylon Miscellaneous Structure
  > CRACKED CHANNEL, NR 2 PYLON AFTER FAIRING PANEL 447DB INNER OUTBOARD CHANNEL CRACK. (REPLACE). INSTALLED NEW CHANNEL I.A.W SRM 51-40-02-0G REV. 130 AND BOEING DWG NO. 313T2362 SH. 4 REV. B. REVIEW COMPLETE.
- [SDR IPXA2026020900534](https://openairdocs.org/sdr/IPXA2026020900534.md): Wedge · debonded · Feb 8, 2026 · N395UP · Boeing 767316 · Trailing Edge Flaps
  > FAULT - RIGHT WING INBOARD AFT FLAP WEDGE, INBOARD SIDE UPPER SKIN DISBOND (REPAIR). ACCOMPLISH REPAIR PER 767-300 SRM 57-53-01-2R-1, 51-70-10-2R-0 AND 51-70-10-2R-4 REV. 130, WITHOUT DEVIATION. REVIEW COMPLETE.
- [SDR IPXA2026022899828](https://openairdocs.org/sdr/IPXA2026022899828.md): Beam · cracked · Feb 8, 2026 · N395UP · Boeing 767316 · Nacelle/Pylon, Main Frame
  > CRACKED BEAM, NR 1 PYLON AFT FAIRING INNER INBD SIDE LWR BEAM. INSTALLED A NEW BEAM IAW SRM 51-40-02-0G, REV 130, SB 767-54-0109, REV 1, DWG 313T2303, SHT 25, REV A, DWG 313T2303, SHT 27, REV A, DWG 313T2303, SHT 28, REV A, DWG 313T2303, SHT 29, REV A,
- [SDR IPXA2026022400346](https://openairdocs.org/sdr/IPXA2026022400346.md): Support Bracket · cracked · Feb 8, 2026 · N395UP · Boeing 767316 · Nacelle/Pylon Miscellaneous Structure
  > CRACKED SUPPORT BRACKET, NR 2 PYLON AFTER FAIRING INNER VANE TUBE SUPPORT NR 1 SUPPORT BRACKET (REPLACE). INSTALLED NEW BRACKET IAW SRM 51-40-02-0G REV. 130 AND DWG 272T0182 SH. 1 REV. A.
- [SDR IPXA2026022400341](https://openairdocs.org/sdr/IPXA2026022400341.md): Support Bracket · cracked · Feb 8, 2026 · N395UP · Boeing 767316 · Nacelle/Pylon Miscellaneous Structure
  > CRACKED BRACKET, NR 2 PYLON AFTER FAIRING INNER VANE TUBE SUPPORT NR 2 SUPPORT BRACKET (REPLACE). INSTALL NEW BRACKET IAW SRM 51-40-02-0G REV. 130 AND DWG 272T0182 SH. 1 REV. A.
- [SDR IPXA2026022099584](https://openairdocs.org/sdr/IPXA2026022099584.md): Former · cracked · Feb 8, 2026 · N395UP · Boeing 767316 · Leading Edge Devices
  > CRACKED FORMER, LT WING L/E NR 4 SLAT INBD DOOR LINK INBD CURTAIN SUPPORT WS 564 (REPLACE) REVIEW COMPLETE.
- [SDR IPXA2026022099451](https://openairdocs.org/sdr/IPXA2026022099451.md): Former · cracked · Feb 8, 2026 · N395UP · Boeing 767316 · Leading Edge Devices
  > CRACKED SUPPORT, LT WING L/E NO.5 SLAT OUTBD DOOR LINK CURTAIN OUTBD SUPPORT, OSS 499 (REPLACE) REVIEW COMPLETE.
- [SDR IPXA2025081828045](https://openairdocs.org/sdr/IPXA2025081828045.md): Battery Pack · inoperative · Aug 18, 2025 · N395UP · Boeing 767316 · Emergency Lighting
  > EMERGENCY DOOR LIGHTS AND R/H DOME EMERGENCY LIGHT INOP. REPLACED M735 EMERGENCY BATTERY PACK AND TESTED LIGHT SATIS IAW AMM 33-51-07-401 REV 145.
- [SDR IPXA2025072131163](https://openairdocs.org/sdr/IPXA2025072131163.md): Power Supply · inoperative · Jul 21, 2025 · N395UP · Boeing 767316 · Emergency Lighting
  > EXTERIOR EMERGENCY LIGHT AND L9801 DOME EMERGENCY LIGHT INOP T/S ACCOMPLISHED IAW IAI WDM 33-51-13 AND FOUND M736 PWR SUPPLY INOP. R & R M736 IAW AMM 33-51-07-401 REV 145.
- [SDR IPXA2024112569479](https://openairdocs.org/sdr/IPXA2024112569479.md): Smoke Detector · false activation · Nov 24, 2024 · N395UP · Boeing 767316 · Smoke Detection
  > MAIN DECK SMOKE DETECTOR LED A2 REMAINED AMBER (ILLUMINATED) ONCE AIRBORNE WITHOUT EICAS OR STATUS MESSAGE. NO FAULTS AFTER POWER RESET. MAIN DECK SMOKE DETECTOR SYSTEM TEST C/O IAW AMM 26-16-00-715-001 REV. 143. TEST SATIS.
- [SDR IPXA2024070917370](https://openairdocs.org/sdr/IPXA2024070917370.md): Door · leaking · Jul 9, 2024 · N395UP · Boeing 767316 · Passenger/Crew Doors
  > LOUD SQUEAL FROM ENTRY DOOR AREA AS AIRCRAFT BEGINS TO PRESSURIZE PERFORMED ENTRY DOOR INSPECTION AND SEAL INSPECTION IAW AMM 52-11-00/601 REV142<BR><BR>NO DAMAGE ON THE DOOR, NO BROKEN OR MISSING PARTS FOUND. SEAL WITHOUT CUTS OR DAMAGE.
- [SDR IPXA2024062187942](https://openairdocs.org/sdr/IPXA2024062187942.md): Adc · inoperative · Jun 17, 2024 · N395UP · Boeing 767316 · Air Data Computer
  > AIR TURNBACK. AFTER TAKE OFF ABOVE 2000 CAPTAINS AIRSPEED UNRELIABLE THEN BLANKED OUT. IT CAME BACK THEN WENT AWAY. AFTER 3 MINUTES IT CAME TO NORMAL. THESE WERE ACCOMPANIED WITH AILERON LOCKOUT AND RUDDER RATIO AIRDATA SWITCHING TEST PERFORMED IAW AMM 34-12-
- [SDR IPXA2024061787942](https://openairdocs.org/sdr/IPXA2024061787942.md): Indicator · unreliable · Jun 17, 2024 · N395UP · Boeing 767316 · Airspeed/Mach Indicator
  > AIR TURNBACK AFTER TAKE OFF ABOVE 2000 CAPTAINS AIRSPEED UNRELIABLE THEN BLANKED OUT. IT CAME BACK THEN WENT AWAY. AFTER 3 MINUTES IT CAME TO NORMAL. THESE WERE ACCOMPANIED WITH AILERON LOCKOUT AND RUDDER RATIO AIRDATA SWITCHING TEST PERFORMED IAW AMM 34-12-00
- [SDR IPXA2024030465268](https://openairdocs.org/sdr/IPXA2024030465268.md): Sign · damaged · Feb 8, 2024 · N395UP · Boeing 767316 · Emergency Lighting
  > *** SUPPLEMENTAL SDR *** FAULT - THE SELF LUMINOUS EXIT SIGN INSTALLED ON LIFE RAFT CONTAINER WITH PARTIAL MISSING OF THE COATING. (REPLACE) I.A.W AMM 33-51-02-702-001 REV.141 DO A LIGHTING INTENSITY TEST, RESULT WAS SATISFIED. REFERENCED TO IAI SUPPLEMENT IPC
- [SDR IPXA2024020965268](https://openairdocs.org/sdr/IPXA2024020965268.md): Sign · unsecure · Feb 8, 2024 · N395UP · Boeing 767316 · Emergency Lighting
  > *** SDR FILED OPEN *** FAULT - FOUND MAIN DECK CARGO EXIT SIGN PEEL OFF (REPLACE) OK TO WORK
- [SDR IPXA2023030691575](https://openairdocs.org/sdr/IPXA2023030691575.md): Handle · inoperative · Mar 6, 2023 · N395UP · Boeing 767316 · Passenger/Crew Doors
  > INSPECTION TYPE:NAEXIT HANDLE AT L1 WILL NOT RELAESE ON THE OUTSIDE OF THE A/C. UNABLE TO CLOSE L1 DOOR FOM THE OUTSIDE.REMOVED INTERIOR DOOR LINING PARTIALLY. DOOR INTERIOR HANDLE WAS NOT REMOVED AMM TASK 52-12-02-004-001, REV 138.02. FOUND SCREW FOR SECONDAR
- [SDR IPXA2023012990372](https://openairdocs.org/sdr/IPXA2023012990372.md): Tube · cracked · Jan 29, 2023 · N395UP · Boeing 767316 · Turbine Section
  > ENG #1, TURBINE CASE COOLING TUBES, LEFT UPPER TUBE, STRAP CRACKED. STRAP REMOVED, NO PART ON HAND. P/N 9358M66P33 ORDERED, REQUEST #432499.STRAP REPLACED, AMM 70-50-00 PB 201 REV. 138.01.
- [SDR IPXA2022102187359](https://openairdocs.org/sdr/IPXA2022102187359.md): Skin · cracked · Oct 7, 2022 · N395UP · Boeing 767316 · Wing, Plate/Skin
  > INSPECTION TYPE:SVCRACK FASTENER HOLE ON L/H WING LOWER SURFACE WHEN PERFORM APB SB AP767-57-013 NEAR WSTA 898.4.REPAIR IAW BOEING SR:4-5635772766, EO B767-5710-84921 AND EO B767-5710-85045-A.
- [SDR IPXA2022102187358](https://openairdocs.org/sdr/IPXA2022102187358.md): Skin · cracked · Oct 7, 2022 · N395UP · Boeing 767316 · Wing, Plate/Skin
  > INSPECTION TYPE:SV, CRACK FASTENER HOLE ON L/H WING LOWER SURFACE WHEN PERFORM APB SB AP767-57-013 NEAR WSTA 952(FOR HOLE 3)REPAIR IAW BOEING SR:4-5635772766, EO B767-5710-84921 AND EO B767-5710-85045-A.
- [SDR IPXA2022102187357](https://openairdocs.org/sdr/IPXA2022102187357.md): Skin · cracked · Oct 7, 2022 · N395UP · Boeing 767316 · Wing, Plate/Skin
  > INSPECTION TYPE:SV, CRACK FASTENER HOLE ON L/H WING LOWER SURFACE WHEN PERFORM APB SB AP767-57-013 NEAR WSTA 926.(FOR HOLE 2). REPAIR IAW BOEING SR:4-563577276, EO B767-5710-84921 AND EO B767-5710-85045-A
- [SDR IPXA2022102287362](https://openairdocs.org/sdr/IPXA2022102287362.md): Stringer · cracked · Oct 7, 2022 · N395UP · Boeing 767316 · Wing, Longeron/Stringer
  > INSPECTION TYPE:SV, CRACK FASTENER HOLE ON L/H WING LOWER SURFACE WHEN PERFORM APB SB AP767-57-013 BETWEEN WSTA 962.2 AND WSTA 1018.2. REPAIR IAW BOEING SR:4-5635772766, EO B767-5710-84921 AND EO B767-5710-85030-A.
- [SDR IPXA2022102287361](https://openairdocs.org/sdr/IPXA2022102287361.md): Skin · cracked · Oct 7, 2022 · N395UP · Boeing 767316 · Wing, Plate/Skin
  > INSPECTION TYPE:SV, CRACK FASTENER HOLE ON L/H WING LOWER SURFACE WHEN PERFORM APB SB AP767-57-013 BETWEEN WSTA 962.2 AND WSTA 1018.2REPAIR IAW BOEING SR:4-5635772766, EO B767-5710-84921 AND EO B767-5710-85030-A.
- [SDR IPXA2022100386824](https://openairdocs.org/sdr/IPXA2022100386824.md): Skin · cracked · Oct 3, 2022 · N395UP · Boeing 767316 · Wing, Plate/Skin
  > INSPECTION TYPE:NA*SUPPLEMENTAL SDR* L/H WING, LOWER SKIN AROUND FASTENER COMMON TO STGR: L-9.5 BETWEEN RIB: 27 (WS 879.2) AND RIB 31 (WS 990.2): CRACK INDICATION > 40%, CRACK LENGTH: 1,0 MM. ACCOMPLISHED EO: B767-5730-84911-A STEP 6A REV. DATE 10/02/2022 AND
- [SDR IPXA2022100436824](https://openairdocs.org/sdr/IPXA2022100436824.md): Skin · cracked · Oct 3, 2022 · N395UP · Boeing 767316 · Wing, Plate/Skin
  > L/H WING, LOWER SKIN AROUND FASTENER COMMON TO STGR: L-9.5 BETWEEN RIB: 27 (WS 879.2) AND RIB 31 (WS 990.2): CRACK INDICATION > 40%, CRACK LENGTH: 1,0 MM. ACCOMPLISHED EO: B767-5730-84911-A STEP 6A REV. DATE 10/02/2022 AND OPENED DMI: D792434 ON LOG PAGE 42736
- [SDR IPXA2022021378912](https://openairdocs.org/sdr/IPXA2022021378912.md): None · none · Jan 30, 2022 · N395UP · Boeing 767316 · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C12CRACK ON FUSELAGE SKIN (P/N:148T3121-2) ON STA 1725.5,NEAR S-7R.REPAIR I.A.W UPS EO B767-5330-24301-K AND 767-300 SRM 53-80-01-2R REPAIR 5,REV 118.01.
- [SDR IPXA2021071671755](https://openairdocs.org/sdr/IPXA2021071671755.md): Pump · inoperative · Jul 16, 2021 · N395UP · Boeing 767316 · Fuel Boost Pump
  > INSPECTION TYPE:ETOP** ETOPS FILED OPEN ** WITH APU RUNNING, WITH AC PWR PROVIDED, L FWD FUEL PUMP IS NOT IN THE COMMANDED ON FUNCTION. PRESS LIGHT IS ILLUMINATED. A/C REL IAW MEL 28-22-1-1, CAÏ¿½T C REFV 57.
- [SDR IPXA2021012965058](https://openairdocs.org/sdr/IPXA2021012965058.md): Duct · cracked · Jan 29, 2021 · N395UP · Boeing 767316 · Pneumatic Distribution System
  > INSPECTION TYPE: NA NO EMERGENCY WAS DECLARED OR EQUIPMENT USED. MOMENTARY WHEEL WELL FIRE ON APPROACH TO VLC. QRH CHECKLIST COMPLETED. LIGHT WENT OUT WITHIN 1 MIN, SUSPECT HOT BRAKE WHEEL WELL FIRE DETECTION SYSTEM BITE C/O, IAW FIM 26-17-TASK 815.803, NO

## 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 = 'N395UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N395UP/reports

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