# Service difficulty reports: N407UP

A list on [N407UP](https://openairdocs.org/aircraft/N407UP.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 5 · 205 reports

- [SDR IPXA2026021697269](https://openairdocs.org/sdr/IPXA2026021697269.md): Windshield · failed · Feb 13, 2026 · N407UP · Boeing 75724APF · Flight Compartment Windows
  > DIVERSION, RT FWD WINDSHIELD STARTED ARCING THEN SHATTERED UPON REACHING TOP OF CLIMB. FL400. COMPLIED WITH QRH. DIVERTED TO SDF PER MOC & DISPATCH. REPLACED R1 WINDOW WITH REF TO MM 56-11-01-401. ACCOMPLISHED CONTINUITY CHECK OF R1 WINDOW HEAT SENSORS WI
- [SDR IPXA2026021397269](https://openairdocs.org/sdr/IPXA2026021397269.md): Windshield · arced · Feb 13, 2026 · N407UP · Boeing 75724APF · Flight Compartment Windows
  > RIGHT FWD WINDSHIELD STARTED ARCING THEN SHATTERED UPON REACHING TOP OF CLIMB. FL400. COMPLIED WITH QRH. DIVERTED TO SDF PER MOC & DISPATCH. ACCOMPLISHED SECOND TORQUE AT 1:27 LOCAL PER MM 56-11-01-401.
- [SDR IPXA2025071820838](https://openairdocs.org/sdr/IPXA2025071820838.md): Angle · corroded · Jul 8, 2025 · N407UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > AFTER REMOVING THE APU DOOR SURROUND FOUND THE ANGLE HAS SURFACE CORROSION. INSTALLED ANGLE IAW SRM 51-40-02.
- [SDR IPXA2025071821035](https://openairdocs.org/sdr/IPXA2025071821035.md): Angle · corroded · Jul 8, 2025 · N407UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > AFTER REMOVING THE APU DOOR SHROUD FOUND THE ANGLE HAS SURFACE CORROSION. INSTALLED ANGLE IAW SRM 51-40-02.
- [SDR IPXA2025071819525](https://openairdocs.org/sdr/IPXA2025071819525.md): Bracket · corroded · Jul 8, 2025 · N407UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > AFTER REMOVAL OF THE APU DOOR SHROUD FOUND THE 148N3141-6 BRACKET HAS SURFACE CORROSION. INSTALLED ANGLE 148N3141-6 IAW SRM 51-40-02.
- [SDR IPXA2025071820911](https://openairdocs.org/sdr/IPXA2025071820911.md): Angle · corroded · Jul 8, 2025 · N407UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > AFTER REMOVING APU DOOR SHROUD FOUND THE 148N3152-2 ANGLE HAS SURFACE CORROSION INSTALLED ANGLE 148N3152-2 IAW SRM 51-40-02.
- [SDR IPXA2025071891774](https://openairdocs.org/sdr/IPXA2025071891774.md): Channel · cracked · Jul 6, 2025 · N407UP · Boeing 75724APF · Nacelle/Pylon Miscellaneous Structure
  > FOUND ROD STRUCTURE CHANNEL (313N3022-102) HAS A.60 LONG CRACK ON PANEL 445BL RUNNING FROM EDGE OF FASTENER HOLE TO EDGE OF PART. INSTALLED 1 EA CHANNEL IAW B757-200-SRM-51-40-02.
- [SDR IPXA2025080177856](https://openairdocs.org/sdr/IPXA2025080177856.md): Tee Angle · corroded · Jul 5, 2025 · N407UP · Boeing 75724APF · Aerodynamic Fairings
  > *** SUPPLEMENTAL SDR *** FAULT- Z100- STR: RH WTB T-CHORD BETWEEN STA 1037 - STA 1060 RBL 65 HAS EXFOLIATION ON UPPER SURFACE. INSTALLED T-CHORD P/N UP-149N7553-28, BETWEEN STA 1037 - STA 1060 RBL 65IAW B757-200PF, SRM 51-40-02
- [SDR IPXA2025071179209](https://openairdocs.org/sdr/IPXA2025071179209.md): Stringer · corroded · Jul 5, 2025 · N407UP · Boeing 75724APF · Fuselage Main, Longeron/Stringer
  > MAJOR REPAIR, LOWER AFT FUSELAGE, BS 1460 HAS EXFOLIATION CORROSION BETWEEN SKIN INNER AREA AND STRINGERS 29 AND 30. INSTALLED STRINGER 23 CLIPS. INSTALLED 2 SUPPORT CHANNELS. INSTALLED 8 FLOOR SUPPORT BRACKETS. INSTALLED 6 STRINGER SPLICES. INSTALLED ONE ANT
- [SDR IPXA2025072377856](https://openairdocs.org/sdr/IPXA2025072377856.md): Tee Angle · corroded · Jul 5, 2025 · N407UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > STRINGER RT WTB TEE-CHORD BETWEEN BS 1037 - 1060, RBL 65, HAS EXFOLIATION ON UPPER SURFACE.
- [SDR IPXA2025070677817](https://openairdocs.org/sdr/IPXA2025070677817.md): Intercostal · corroded · Jul 5, 2025 · N407UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > RIGHT PACK EXHAUST INTERCOSTAL FRAME SUPPORT AT FWD AREA HAS CORROSION INSTALLED NEW INTERCOSTAL IAW SRM 51-40-02. VERIFIED INSTALLATION OF RT PACK EXHAUST INTERCOSTAL FRAME FWD SUPPORT.
- [SDR IPXA2025070677685](https://openairdocs.org/sdr/IPXA2025070677685.md): Tee Angle · corroded · Jul 5, 2025 · N407UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > LOWER FUSELAGE INTERCOSTAL T-CHORD BETWEEN STA 1037-STA 1060 RBL 7 HAS CORROSION. INSTALLED T-CHORD P/N: UP-144N8180-48, STA 1037-STA 1060 RBL 7 IAW B757-200PF, SRM 51-40-02
- [SDR IPXA2025070677526](https://openairdocs.org/sdr/IPXA2025070677526.md): Tee Angle · corroded · Jul 5, 2025 · N407UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > WTB T-CHORD BETWEEN STA 1037 - STA 1060 LBL 65 HAS EXFOLIATION ON UPPER SURFACE. INSTALLED NEW WTB T-CHORD BETWEEN STA 1037 - STA 1060 LBL 65 IAW B757-200PF, SRM 51-40-02.
- [SDR IPXA2025070770161](https://openairdocs.org/sdr/IPXA2025070770161.md): Panel · cracked · Jul 4, 2025 · N407UP · Boeing 75724APF · Leading Edge Devices
  > NUMBER 6 SLAT O/B END LWR LEADING EDGE LWR SURFACE CLOSING PLIE HAS A CRACK AS MARKED. INSTALLED CLOSING PLIE IAW SRM 51-40-02.
- [SDR IPXA2025071169520](https://openairdocs.org/sdr/IPXA2025071169520.md): Floor Panel · corroded · Jul 4, 2025 · N407UP · Boeing 75724APF · Fuselage Floor Panel
  > FWD CARGO COMPT FLOOR PANEL 121DF HAS SURFACE CORROSION. INSTALLATION OF ROLLER TRAY, PN- 81658-1. INSTALLED FWD CARGO PIT MBA SYSTEM IAW 757-200 SRM 51-40-02-0G-0 AND AMM 25-57-01-404-003-001.
- [SDR IPXA2025080155352](https://openairdocs.org/sdr/IPXA2025080155352.md): Intercostal · corroded · Jul 3, 2025 · N407UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > FS 1037 - FS 1060 LBL 37 THE PAX EXHAUST INTERCOSTAL 149N7559-1 HAS EXFOLIATION ON UPPER FWD SURFACE INSTALLED PAX EXHAUST INTERCOSTAL OF FS 1037-1060 LBL 37 IAW SRM 51-40-02.
- [SDR IPXA2025071644664](https://openairdocs.org/sdr/IPXA2025071644664.md): Strap · corroded · Jul 3, 2025 · N407UP · Boeing 75724APF · APU Core Engine
  > APU INLET FWD STRAP HAS CORROSION UNDERNEATH. INSTALLED NEW STRAP IAW SRM 51-40-02
- [SDR IPXA2025070751400](https://openairdocs.org/sdr/IPXA2025070751400.md): Strip · corroded · Jul 3, 2025 · N407UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > METAL STRIP AT BS 1180, BL 5.5 IS CORRODED. INSTALLED METAL TRIP IAW B757-200 SRM 51-40-02 USING SAME HARDWARE.
- [SDR IPXA2025072355352](https://openairdocs.org/sdr/IPXA2025072355352.md): Intercostal · corroded · Jul 3, 2025 · N407UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > FS 1037 - FS 1060 LBL 37 THE PAX EXHAUST INTERCOSTAL 149N7559-1 HAS EXFOLIATION ON UPPER FWD SURFACE
- [SDR IPXA2024092606717](https://openairdocs.org/sdr/IPXA2024092606717.md): Guard · wrong part · Sep 26, 2024 · N407UP · Boeing 75724APF · Emergency Lighting
  > EMERGENCY LIGHTS BLACK GUARDED SWITCH COVER SEEMS TO BE WRONG PART. DONT BELIEVE IT SHOULD HAVE SPLIT IN MIDDLE OF GAURD REMOVED AND REPLACED EMERGENCY LIGHTS SWITCH GUARD IAW SWPM 20-83-11.
- [SDR IPXA2024080614276](https://openairdocs.org/sdr/IPXA2024080614276.md): Switch · inoperative · Aug 6, 2024 · N407UP · Boeing 75724APF · Emergency Lighting
  > EMERGENCY LIGHTSA SW GUARD IS LOOSE R AND R SWITCH GUARD IAW SWPM 20-83-11. OPS CK OK
- [SDR IPXA2023091193551](https://openairdocs.org/sdr/IPXA2023091193551.md): Handle · worn · Sep 8, 2023 · N407UP · Boeing 75724APF · Passenger/Crew Doors
  > CREW ENTRY DOOR EXTERIOR HANDLE€™S STUD IS WORN BEYOND LIMIT R&R CREW ENTRY EXTERIOR HANDLE€™S STUD PER AM 52-12-01
- [SDR IPXA2023090651214](https://openairdocs.org/sdr/IPXA2023090651214.md): Cam · worn · Aug 10, 2023 · N407UP · Boeing 75724APF · Passenger/Crew Doors
  > MAJOR REPAIR, CREW ENTRY DOOR UPPER AND LOWER LATCH CAMS HAVE WEAR MARKS DOT 47-04 APPLIED FINISH RESTORATION IAW EO N B757-5210-14721 AND SRM 51-20-01-0G. REVIEWED
- [SDR IPXA202308110214](https://openairdocs.org/sdr/IPXA202308110214.md): Unknown · unknown · Aug 10, 2023 · N407UP · Boeing 75724APF · Passenger/Crew Doors
  > *SDR FILED OPEN* FAULT CREW ENTRY DOOR UPPER AND LOWER LATCH CAMS HAVE WEAR MARKS DOT 47-04 APPROVED
- [SDR IPXA2023012090070](https://openairdocs.org/sdr/IPXA2023012090070.md): Transmitter · faulted · Jan 19, 2023 · N407UP · Boeing 75724APF · Trailing Flap Position Indicating System
  > EMERGENCY DECLARED, LANDED UNEVENTFULLY, ON ARRIVAL EXTENDED THE FLAPS TO 1 RECEIVED A TE FLAP ASYM EICAS MESSAGE. RAN QRH. REMOVED AND REPLACED LT WING FLAP POSITION TRANSMITTER IAW 27-58-03-0401. OPS CHECKS NORMAL. NO FAULTS FOUND. ACFT OK FOR SVC.
- [SDR IPXA2021071671748](https://openairdocs.org/sdr/IPXA2021071671748.md): Flap System · out of adjust · Jul 15, 2021 · N407UP · Boeing 75724APF · Trailing Edge Flap Control System
  > ATB - NO EMERG DECL'D - NO EQUIP USED - LANDED UNEVENTFULLY - AC OOS. ATB DUE TO T/E FLAP DISAGREE. AFTER MOVING THE FLAP SELECTOR TO UP WE RECEIVED A TE FLAP DISAGREE EICAS. RAN CHECKLIST, THE HANDLE WAS UP SO WE RETURNED TO DFW.PER FIM 27-51-00-815-808 #1,
- [SDR IPXA2019093047391](https://openairdocs.org/sdr/IPXA2019093047391.md): Skin · delaminated · Sep 30, 2019 · N407UP · Boeing 75724APF · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C1WHILE INSPECTING CARD # 128347, UPPER SKIN BETWEEN STA. 1896.20 & STA 1918.9 REPAIR HAS A DENT IN THE MIDDLE THAT IS DELAMINATED DOT 8-055REMOVED OLD REPAIR AND MADE A NEW REPAIR PER UPS RCD 128358, IAW B757 SRM 53-80-01-2R FIG 201 SHEET 1, &
- [SDR IPXA2019092447201](https://openairdocs.org/sdr/IPXA2019092447201.md): Floor Panel · damaged · Sep 24, 2019 · N407UP · Boeing 75724APF · Fuselage Floor Panel
  > INSPECTION TYPE:C1 FLOOR PANEL 211XAF IS DAMAGED AND NEEDS REPLACE. FAB PANEL 211XAF FROM 5024N00001SS-G BATCH# 3525521 AND STEP CUT OUT PER SREO B757-5320-9692-K.
- [SDR IPXA2019092447200](https://openairdocs.org/sdr/IPXA2019092447200.md): Floor Panel · damaged · Sep 24, 2019 · N407UP · Boeing 75724APF · Fuselage Floor Panel
  > INSPECTION TYPE:C1 FLOOR PANEL 212XAF IS DAMAGED AND NEEDS REPLACE. FAB PANEL 212XAF FROM 5024N400001SS-G BATCH# 3525521 AND STEP CUT OUT PER SREO B757-5320-9692-K.
- [SDR IPXA2019091947000](https://openairdocs.org/sdr/IPXA2019091947000.md): Doubler · delaminated · Sep 19, 2019 · N407UP · Boeing 75724APF · Trailing Edge Flaps
  > INSPECTION TYPE:C1 LT O/B AFT FLAP LOWER SURFACE REPAIR LOCATED BETWEEN AFSTA 345.765 AND 353.065 AND 6.5" FROM T/E TO CENTER OF REPAIR FAILED ULTRASONIC LF BOND TEST 1. SEVERAL AREAS MARKED IN RED. REPAIRED IAW SRM 51-70-05 PER SRM 57-53-01-2R-1 FIGURE 201 TA
- [SDR IPXA2019022639487](https://openairdocs.org/sdr/IPXA2019022639487.md): Warning Message · false activation · Feb 26, 2019 · N407UP · Boeing 75724APF · AC Generator-Alternator
  > ON LANDING BLOCK IN LEFT BUS A13 FOUND IN OUT POSITIONPERFORMED BPCU BITE TEST WRT B757FRFIM 24-20-810-802 CODE 59 RECORDED R/R LT GCU WRT AMM 24-22-02--401 AS REQ IN FIM ALSO R/R CB A13 WRT BSWPM 20-30-00 AS PRECAUTIONARY PERFORMED IDLE RUN ON LT ENG WRT AMM
- [SDR IPXA2018121737003](https://openairdocs.org/sdr/IPXA2018121737003.md): Lamp · inoperative · Dec 15, 2018 · N407UP · Boeing 75724APF · Emergency Lighting
  > L1 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS IAW MM 33-10-00. OPS NORMAL.
- [SDR IPXA2018112106155](https://openairdocs.org/sdr/IPXA2018112106155.md): Warning Message · false activation · Nov 17, 2018 · N407UP · Boeing 75724APF · Landing Gear Position and Warning
  > AFTER TAKEOFF WITH GEAR RETRACTION, A GEAR LIGHT INDICATED & GEAR DISAGREE EICAS. RAN THE NON-NORMAL CHECKLIST WITH NO CHANGE. ALL 3 GREEN GEAR LIGHTS, REMAINED EXTINGUISHED.E MAINTAINED 14,000 FT. AT 210 KIAS. PERFORMED FIM 32-30-00-815, STEPS 1, 11, AN
- [SDR IPXA2018083193376](https://openairdocs.org/sdr/IPXA2018083193376.md): Mount · broken · Aug 29, 2018 · N407UP · Boeing 75724APF · Emergency Equipment
  > FOUND THE EVAS MODULE BROKEN. THE EVAS MOUNT WAS BROKEN. REPLACED THE CAPTAIN`S EVAS MOUNT IAW EO 757-2560-45127H. REINSTALLED THE EVAS UNIT.
- [SDR IPXA2018070631412](https://openairdocs.org/sdr/IPXA2018070631412.md): Door Seal · out of position · Jul 5, 2018 · N407UP · Boeing 75724APF · Passenger/Crew Doors
  > LOUD SQUEAL FROM CREW ENTRY DOOR. DID NOT BEGIN UNTIL AFTER WE LEVELED AT FLT LEVEL 360 CABIN ALTITUDE WAS 5600' DIF WAS 8.5 PSI SEEMS LIKE ITS COMING FROM BOTTOM OF DOOR. FOUND LOWER RIGHT SEAL OFF RETAINER CLEANED & RESECURED SEAL IAW AMM 52-09-02-401. NO LE
- [SDR IPXA2018070531394](https://openairdocs.org/sdr/IPXA2018070531394.md): Door Seal · dirty · Jul 3, 2018 · N407UP · Boeing 75724APF · Passenger/Crew Doors
  > LOUD SQUEAL FROM ENTRY DOOR AT CRUISE ALTITUDE. PRESSURIZED THE AIRCRAFT AN FOUND SMALL LEAK AT MAIN CARGO DOOR REPAIR PER MM 52 09 00. ALSO FOUND SMALL LEAK AT CREW ENTRY DOOR. CLEANED CREW ENTRY DOOR SEAL AND PRESSURIZED. NO LEAKS NOTED. OK PER MM 52 09 00
- [SDR IPXA2018032227725](https://openairdocs.org/sdr/IPXA2018032227725.md): Evas Unit · inoperative · Mar 20, 2018 · N407UP · Boeing 75724APF · Emergency Equipment
  > CAPTAIN`S EVAS INOPERATIVE. INSTALLED A NEW EVAS UNIT IAW AMM 25-69-00, OPS CHECKED GOOD.
- [SDR IPXA2017092321967](https://openairdocs.org/sdr/IPXA2017092321967.md): Support · corroded · Sep 19, 2017 · N407UP · Boeing 75724APF · Aerodynamic Fairings
  > INSPECTION TYPE: C-18, RIGHT AFT LOWER WING TO BODY SUPPORT, FIVE INCHES ABOVE RAT DOOR HAS CORROSION AT INTERSECTION OF BS 1220. REMOVED AND REPLACED THE SUPPORT.
- [SDR IPXA2017092321969](https://openairdocs.org/sdr/IPXA2017092321969.md): Support · corroded · Sep 17, 2017 · N407UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C-18, BS 1200 LOWER KEEL BEAM AREA, RT CHANNEL SUPPORT CORRODED. REMOVED AND REPLACED THE CHANNEL SUPPORT
- [SDR IPXA2017092221953](https://openairdocs.org/sdr/IPXA2017092221953.md): Skin · damaged · Sep 17, 2017 · N407UP · Boeing 75724APF · Fuselage Main, Plate/Skin
  > INSPECTION TYPE: C18, FUSELAGE SKIN EXTERIOR DENTED BS 239, STRINGERS 20 - 21R. REPAIRED IAW SRM 53-00-01-2R, REPAIR 3.
- [SDR IPXA2017092822123](https://openairdocs.org/sdr/IPXA2017092822123.md): Attach Angle · corroded · Sep 15, 2017 · N407UP · Boeing 75724APF · Fuselage Main, Attach Fittings
  > INSPECTION TYPE: C18, RIGHT AFT LOWER WING TO BODY FAIRING AREA, BS 1240 HAS AREAS OF CORROSION AFT LOWER CORNER RAT COMPARTMENT FAIRING ATTACH ANGLE. CUT AND REMOVED DAMAGED SECTION OF ANGLE, REPAIRED IAW SRM 53-60-71-2R, AND 51-70-12
- [SDR IPXA2017080720249](https://openairdocs.org/sdr/IPXA2017080720249.md): Floor Support · dented · Aug 7, 2017 · N407UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > AFT LOWER CARGO BAY FLOOR SUPPORT HAS DENT DAMAGE AT BS 1436, RBL 7. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02. DRILLED, PAINTED & INSTALLED NUTPLATES IAW SRM 51-40-02, & AMM 51-21-00.
- [SDR IPXA2016100709060](https://openairdocs.org/sdr/IPXA2016100709060.md): Terminal · melted · Oct 6, 2016 · N407UP · Boeing 75724APF · Instrument System Wiring
  > PUNGENT ODOR IN COCKPIT NOTICED DURING INITIAL CLIMB WITH GEAR DOWN. ODOR DISAPEARED WITH THE GEAR UP. ON APPROACH WITH GEAR DOWN ODOR RETURNED AND WAS VERY STRONG. FOUND TERMINAL ON RUNWAY TURNOFF MELTED. REPLACED LIGHT CONTROL PANEL IAW 32-12-02.
- [SDR IPXA2016091308226](https://openairdocs.org/sdr/IPXA2016091308226.md): Controller · malfunctioned · Sep 9, 2016 · N407UP · Boeing 75724APF · Cabin Pressure Controller
  > RAPID DECOMPRESSION. CREW DONNED OXYGEN MASKS. REPLACED THE NR 1 CABIN PRESSURE CONTROLLER IAW AMM 21-31-02.
- [SDR IPXA2016061604694](https://openairdocs.org/sdr/IPXA2016061604694.md): Unknown · odor · Jun 16, 2016 · N407UP · Boeing 75724APF · Air Distribution System
  > WITH LT PACK OFF, CLIMBING THRU 8000 FT, HAD AN ODOR OF SOMETHING GETTING HOT OR BURNING. NO SMOKE INDICATIONS WERE NOTED. TURNED LT PACK BACK ON. SMELL DISSIPATED. DURING DESCENT NOTICED THE SMELL AGAIN FOR ABOUT 30 SECONDS, THEN DISSIPATED. PERFORMED ST
- [SDR IPXA2015092393863](https://openairdocs.org/sdr/IPXA2015092393863.md): Skin · punctured · Sep 18, 2015 · N407UP · Boeing 75724APF · Horizontal Stabilizer, Plate/Skin
  > INSPECTION TYPE:C17, LT LOWER HORIZONTAL 185N4001-1 SKIN PANEL ASSY HAS A SMALL PUNCTURE ON THE INTERNAL SKIN. REPAIRED IAW EO B757-5510-58825-A AND REO-G19208, REV-A.
- [SDR IPXA2015092293837](https://openairdocs.org/sdr/IPXA2015092293837.md): Wedge · dented · Sep 8, 2015 · N407UP · Boeing 75724APF · Leading Edge Devices
  > INSPECTION TYPE:C17, NR 7 L/E SLAT DENTS NR 7 & NR 8 ON T/E WEDGE OUT OF SRM LIMITS. REPAIRED WEDGE WITH METAL HOT BOND REPAIR IAW REO-G19182, REV B & EO B757-5750-58805-A.
- [SDR IPXA2015091093350](https://openairdocs.org/sdr/IPXA2015091093350.md): Floor Skin · cracked · Sep 3, 2015 · N407UP · Boeing 75724APF · Fuselage Floor Panel
  > INSPECTION TYPE: C-17, FLIGHT DECK FLOOR HAS A CRACK AT THE EDGE OF WEB BS 284, LBL 19. REMOVED DAMAGE, REPAIRED IAW SRM 53-10-51-2R-4, FIG 201.
- [SDR IPXA2015092193741](https://openairdocs.org/sdr/IPXA2015092193741.md): Floor Support · dented · Sep 1, 2015 · N407UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C-17, AFT CARGO FLOOR SUPPORT DENTED BS 1290, LBL 16.10. REPAIRED IAW SRM 53-00-53-2R-1.
- [SDR IPXA2015091293425](https://openairdocs.org/sdr/IPXA2015091293425.md): Floor Support · dented · Sep 1, 2015 · N407UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C-17, AFT CARGO FLOOR SUPPORT DENTED BS 1280, LBL 10.45. REPAIRED IAW SRM 53-00-53-2R-1.

Next page: https://openairdocs.org/aircraft/N407UP/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 = 'N407UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N407UP/reports

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