# Service difficulty reports: N137UP

A list on [N137UP](https://openairdocs.org/aircraft/N137UP.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 6 · 253 reports

- [SDR IPXA2026071557741](https://openairdocs.org/sdr/IPXA2026071557741.md): Arming Lever · dislodged · Jul 14, 2026 · N137UP · Airbus A300F4622R · Passenger/Crew Doors
  > RED WARNING LIGHT ABOVE ARMING LEVER ON INSIDE OF CREW ENTRY DOOR POPPED IT OF THE SOCKET. REINSTALLED CREW ENTRY DOOR EMERGENCY ESCAPE-SLIDE-RELEASE WARNING LIGHT ASSEMBLY IAW AMM 52-73-00.
- [SDR IPXA2026020666273](https://openairdocs.org/sdr/IPXA2026020666273.md): Battery · inoperative · Feb 6, 2026 · N137UP · Airbus A300F4622R · Passenger/Crew Doors
  > RED INDICATION LIGHT ON L1 SLIDE ARMING PANEL INOP. REMOVED AND REPLACED ASPSU AND BOTH BATTERIES REF AMM 52-73-18 AND PERFORMED OPS CHECK REF AMM 52-73-00 ALL CHECKS SATISFACTORY AT THIS TIME OK FOR CONTINUED SERVICE THIS CLEARS MEL 52-73-01-1 PLACARD REMOVE
- [SDR IPXA2025111864709](https://openairdocs.org/sdr/IPXA2025111864709.md): Windshield · cracked · Nov 14, 2025 · N137UP · Airbus A300F4622R · Flight Compartment Windows
  > DURING DESCENT AT 8000 FT WINDOW ARCHING OBSERVED ON CAPTAIN`S SIDE WINDSCREEN, AFTER FOLLOWING QRH PROCEDURE TO TURN OFF WINDOW HEAT CAPTAIN`S WINDSHIELD CRACKED AND EXPANDED ACROSS WINDSHIELD. REMOVED AND REPLACED CAPTAIN'S FORWARD WINDSHIELD, OPS CHECK GOOD
- [SDR IPXA2025111764709](https://openairdocs.org/sdr/IPXA2025111764709.md): Window · arced · Nov 14, 2025 · N137UP · Airbus A300F4622R · Flight Compartment Windows
  > DURING DESCENT AT 8000 FT WINDOW ARCHING OBSERVED ON CAPTAIN€™S SIDE WINDSCREEN, AFTER FOLLOWING QRH PROCEDURE TO TURN OFF WINDOW HEAT CAPTAINS WINDSHIELD CRACKED AND EXPANDED ACROSS WINDSHIELD. ACCOMPLISHED RII ITEMS FOR R1 WINDOW INSTALL IAW AMM 56-11-11/40
- [SDR IPXA2025070928857](https://openairdocs.org/sdr/IPXA2025070928857.md): Door · no discrepancy · Jul 9, 2025 · N137UP · Airbus A300F4622R · Passenger/Crew Doors
  > SLIDE LEVER WAS EXTREMELY DIFFICULT TO DISARM AFTER SHUTDOWN PRIOR TO OPENING DOOR. PERFORMED OPERATIONAL TEST OF THE MAIN DOOR SLIDE LEVER REF. AMM 25-61-21/401. OPS CHECK GOOD. NO DEFECTS NOTED. BACK PRESSURE CAUSED DUE TO GROUND AC CART WAS CONNECTED BEFORE
- [SDR IPXA2025041617811](https://openairdocs.org/sdr/IPXA2025041617811.md): Girt Bar · out of adjust · Apr 15, 2025 · N137UP · Airbus A300F4622R · Emergency Equipment
  > UPON ARRIVAL FLT CREW COULD NOT OPEN CABIN DOOR FROM INSIDE ADJUSTED GIRT AND GIRT BAR W/R/T MM 25-61-21. VERIFIED DOOR LOCK IND FUNCTIONS. GOOD FOR SERVICE AT THIS TIME.
- [SDR IPXA2025022286750](https://openairdocs.org/sdr/IPXA2025022286750.md): Damper · failed · Feb 21, 2025 · N137UP · Airbus A300F4622R · Nose/Tail Landing Gear
  > LANDING GEAR RETRACTION FAULT UNABLE TO RETRACT.INSTALLED LOCKS ON MLG DOOR ACTUATORS IAW AMM 32-12-11/301 AND INSTALLED LOCKS ON NLG DOOR ACTUATORS IAW AMM 32-22-11/301.
- [SDR IPXA2025020995016](https://openairdocs.org/sdr/IPXA2025020995016.md): Pin · corroded · Jan 26, 2025 · N137UP · Airbus A300F4622R · Trailing Edge Flaps
  > FAULT: APG/ RH WING CENTER FLAP TRACK 3 PIN FLAP AND SLEEVE-LOCKING CORRODED REVIEWED
- [SDR IPXA2025020455060](https://openairdocs.org/sdr/IPXA2025020455060.md): Rib · cracked · Jan 17, 2025 · N137UP · Airbus A300F4622R · Trailing Edge Flaps
  > FAULT: LH CENTER FLAP CRACK FOUND IN RIB 13 AFT, AREA CIRCLED IN RED.ACCOMPLISHED REPAIR IN ACCORDANCE WITH VT-MAE EA 300-5750-27-A3777.
- [SDR IPXA2025020455143](https://openairdocs.org/sdr/IPXA2025020455143.md): Rib · cracked · Jan 17, 2025 · N137UP · Airbus A300F4622R · Trailing Edge Flaps
  > FAULT: RH CENTER FLAP - FOUND 2 CRACKS IN RIB 27 AFT, AREAS CIRCLED IN RED.ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH VT-MAE EA 300-5750-27-A3776.
- [SDR IPXA2025020455141](https://openairdocs.org/sdr/IPXA2025020455141.md): Rib · cracked · Jan 17, 2025 · N137UP · Airbus A300F4622R · Trailing Edge Flaps
  > FAULT: RH CENTER FLAP - FOUND 2 CRACKS IN RIB 26, AREA CIRCLED IN RED.ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH VT-MAE EA 300-5750-27-A3776
- [SDR IPXA2025021340099](https://openairdocs.org/sdr/IPXA2025021340099.md): Frame · cracked · Jan 16, 2025 · N137UP · Airbus A300F4622R · Fuselage Main, Frame
  > CRACKS FOUND ON RH FR 47 HORIZONTAL JUNCTION HOLES F, B AND Q REVIEWEDROTO PERFORMED ON HOLE B. NO DEFECTS FOUND IAW NTM 51-10-01. T96525 T91779. COMPLIED WITH EO# 300-5710-27-A3775 PRELIM 1 STEP #2
- [SDR IPXA2025021237849](https://openairdocs.org/sdr/IPXA2025021237849.md): Frame · cracked · Jan 16, 2025 · N137UP · Airbus A300F4622R · Fuselage Main, Frame
  > CRACK FOUND ON LH FR47 HORIZONTAL JUNCTION HOLE S. ACCOMPLISH THE REPAIR PER EA 300-5710-27-A3774 REV. -.
- [SDR IPXA2025020928236](https://openairdocs.org/sdr/IPXA2025020928236.md): Stringer · bent · Jan 16, 2025 · N137UP · Airbus A300F4622R · Fuselage Main, Longeron/Stringer
  > R/H T.H.S COMP BETWEEN FRAME 86-87, STRINGER AT THE 7*CLOCK POSITION IS BENT. DOT 33-002. INSTALLED NEW PARTS AT FRAME 86-87, STRINGER AT THE 7*CLOCK POSITION IAW A300-600 SRM 51-40-21 WITH SEALANT P/N: 04-001-010P BACTH#: 0004318644 AND FASTENERS MS20426AD4-6
- [SDR IPXA2025020928162](https://openairdocs.org/sdr/IPXA2025020928162.md): Stringer · bent · Jan 16, 2025 · N137UP · Airbus A300F4622R · Fuselage Main, Longeron/Stringer
  > R/H T.H.S COMP BETWEEN FRAME 86-87, STRINGER AT THE 8*CLOCK POSITION IS BENT. DOT 33-001. INSTALLED NEW PARTS AT FRAME 86-87, STRINGER AT THE 8*CLOCK POSITION IAW A300-600 SRM 51-40-21 WITH SEALANT P/N: 04-001-010P BACTH#: 0004318644 AND FASTENERS MS20426AD4-
- [SDR IPXA2025020521932](https://openairdocs.org/sdr/IPXA2025020521932.md): Rib · cracked · Jan 15, 2025 · N137UP · Airbus A300F4622R · Nacelle/Pylon, Frame/Spar/Rib
  > FAULT-STR-Z400-#2 ENG PYLON TOP AREA RIB 8 LH LATERAL PANEL CHANNEL CRACKED-DOT 139/21-MR/139. INSTALLED BLEED AIR PRECOOLER IAW AMM 36-11-15-0401. INSTALLED SPLICE BRACKET AT #2 ENG PYLON TOP AREA RIB 8 LH LATERAL PANEL IAW SRM 51-40-21. REVIEWED
- [SDR IPXA2025012821114](https://openairdocs.org/sdr/IPXA2025012821114.md): Plate · cracked · Jan 15, 2025 · N137UP · Airbus A300F4622R · Nacelle/Pylon Miscellaneous Structure
  > #2 ENG PYLON TOP AREA RH RIB 3 LATERAL PANEL SKIN CORNER CRACKED-DOT 139/18-MR/139. NSTALLED PLATE AT #2 ENG PYLON TOP AREA RH RIB 3 LATERAL PANEL SKIN CORNER IAW A300-600 SRM 51-40-21. FASTENER PN:NAS1200M4-7, BN:0004171072, PN:MS21060-3, BN:0004201914, PN:CC
- [SDR IPXA2025020957045](https://openairdocs.org/sdr/IPXA2025020957045.md): Bracket · broken · Jan 12, 2025 · N137UP · Airbus A300F4622R · Wing Main, Frame Structure
  > LH WING, CENTER FLAP, O/B EDGE HAS BRACKET BROKEN. DOT 103-62. REMOVERD AND REPLACE BRACKET AT L/H WING CENTER FLAP. FABRICATED BRACKET:P/N 2024-T3 0.32B BATCH 0004247650 P/N C3213-5-08 BATCH: 00044268033 IAW A300-600 SRM 51-40-21.
- [SDR IPXA2025020945882](https://openairdocs.org/sdr/IPXA2025020945882.md): Skin · dented · Jan 11, 2025 · N137UP · Airbus A300F4622R · Leading Edge Devices
  > R/H WING, AT O/B SLAT TIP, ON WING L/E SKIN WITH DENT. DOT 73-002. INSTALLED NEW PART SHOULD WING TIP ON RH WING WITH FASTENERS P/N# CR3212-4-2 BTCH#4349652, P/N# CR3212-6-7 BTCH#4262361, P/N# 04-001-0169 BTCH# 4263295 IAW A300-600 SRM 51-40-21.
- [SDR IPXA2025020939803](https://openairdocs.org/sdr/IPXA2025020939803.md): Bracket · cracked · Jan 11, 2025 · N137UP · Airbus A300F4622R · Fuselage Main, Frame
  > FR10 R/H SIDE HAS A CRACKED CEILING CORNER BRACKET. DOT 60-001. INSTALLED BRACKET IAW A300-600 SRM 51-40-21, HILOCK P/N: DAN5-6-4, BATCH # 0004128103.
- [SDR IPXA2025013140114](https://openairdocs.org/sdr/IPXA2025013140114.md): Skin · gouged · Jan 11, 2025 · N137UP · Airbus A300F4622R · Wing, Plate/Skin
  > LH WING, LOWER SURFACE, NEAR STA 0,(ROOT), UNDER I/B FLAP, NEXT TO I/B FLAP TRACK HAS GOUGE. DOT 103-35. FABRICATED NEW SKIN, TOP STUB IAW A300 57-51-12. PN: 2024-T3.050C, BN: 0004328497
- [SDR IPXA2025011462944](https://openairdocs.org/sdr/IPXA2025011462944.md): Floor Panel · damaged · Jan 7, 2025 · N137UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAIN DECK FLOOR PANEL 251ZG IS BROKEN DOT CL 1. FABRICATED FLOOR PANEL 251ZG.
- [SDR IPXA2025011463069](https://openairdocs.org/sdr/IPXA2025011463069.md): Floor Panel · damaged · Jan 7, 2025 · N137UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAIN DECK FLOOR PANEL 262DM IS BROKEN DOT CL 2. FABRICATED FLOOR PANEL 262DM USING PN: 5024N400001SS-G BATCH: 0004055277 PN: 04-001-0012 BATCH: 0004143182 PN: G2002B-3S BATCH: 0043483 PN: G2002B-3P BATCH: 000426239 IAW SREO-16407-REQ001. OSD: 1/27/2025
- [SDR IPXA2025012850124](https://openairdocs.org/sdr/IPXA2025012850124.md): Shear Tie · cracked · Jan 6, 2025 · N137UP · Airbus A300F4622R · Fuselage Internal Mounting Structure
  > BASE FRAME FITTING FR46 LH HAS SUSPECTED CRACK. NO DOT. INSTALLED NEW REPAIR PARTS AT FR46 LH SHIM, DOUBLER AND STIFENER WITH HARDWARE INCLUDED IN THE KIT P/N#536177A44R00 BATCH N#4357712, HRDW P/N# EN6115V3X9, EN6115V3X10, EN6115V3X11 ASNA2528-3 IAW SRM 51-4
- [SDR IPXA2025020514484](https://openairdocs.org/sdr/IPXA2025020514484.md): Bracket · cracked · Jan 3, 2025 · N137UP · Airbus A300F4622R · Fuselage Main, Structure
  > AVIONICS COMP. FLOORS, UNDER 121CF FLOOR PANEL, NEAR FR4, ELECTRICAL WIRE BRACKET SUPPORT IS BROKEN. DOT 103-01. INSTALLED NEW BRACKET UNDER PANEL 121CF NEAR FR4 IAW A300-600 SRM 51-40-21. JOB COMPLETE
- [SDR IPXA2025021200557](https://openairdocs.org/sdr/IPXA2025021200557.md): Adapter · corroded · Jan 2, 2025 · N137UP · Airbus A300F4622R · Fuselage Structure (General)
  > MAIN CABIN CLS ADAPTER FR61 Y0 RH HAS CORROSION NOTED. DOT 7628/09 INSTALLED CLS ADAPTER P/N A53275455200 ON FR61 RH Y0 IAW A300-600 SRM 51-40-21. REQUEST OK TO APPLY TOPCOAT. REVIEWED
- [SDR IPXA2025020900567](https://openairdocs.org/sdr/IPXA2025020900567.md): Adapter · corroded · Jan 2, 2025 · N137UP · Airbus A300F4622R · Fuselage Main, Structure
  > MAIN CABIN CLS ADAPTER FR60 Y0 RH HAS CORROSION NOTED. INSTALLED CLS ADAPTER P/N A53275455200 ON FR60 Y0 RH IAW A300-600 SRM 51-40-21. REQUEST OK TO APPLY TOPCOAT. ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH UPS EO-92457-REQ1.
- [SDR IPXA2025021200540](https://openairdocs.org/sdr/IPXA2025021200540.md): Adapter · corroded · Jan 2, 2025 · N137UP · Airbus A300F4622R · Fuselage Main, Structure
  > MAIN CABIN CLS ADAPTER FR63 Y0 RH HAS CORROSION NOTED. ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH UPS E0-92459-REQ1.
- [SDR IPXA2025021200505](https://openairdocs.org/sdr/IPXA2025021200505.md): Adapter · corroded · Jan 2, 2025 · N137UP · Airbus A300F4622R · Fuselage Main, Structure
  > MAIN CABIN CLS ADAPTER FR65 Y0 LH HAS CORROSION NOTED. INSTALLED CLS ADAPTER P/N A53275455200 ON FR65 Y0 IAW A300-600 SRM 51-40-21. REQUEST OK TO APPLY TOPCOAT. ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH UPS EO-92460-REQ1.
- [SDR IPXA2025012900371](https://openairdocs.org/sdr/IPXA2025012900371.md): Seat Track · corroded · Jan 2, 2025 · N137UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK FR80 Y794.3 HAS CORROSION NOTED. DOT 7628/05. INSTALLED NEW SEAT TRACK SECTION FR80 WTH FAST P/N: HL70-8 BATCH: 4353581, P/N: NAS1097DD6 BATCH: 4244840 IAW A300-600 SRM 51-40-21. REVIEWED
- [SDR IPXA2025021200494](https://openairdocs.org/sdr/IPXA2025021200494.md): Adapter · corroded · Jan 2, 2025 · N137UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN CABIN CLS ADAPTER FR66 Y0 RH HAS CORROSION NOTED. INSTALLED CLS ADAPTER P/N A53275455200 IAW A300-600 SRM 51-40-21. REQUEST OK TO APPLY TOPCOAT.
- [SDR IPXA2025020100557](https://openairdocs.org/sdr/IPXA2025020100557.md): Adapter · corroded · Jan 2, 2025 · N137UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN CABIN CLS ADAPTER FR61 Y0 RH HAS CORROSION NOTED. VERIFIED STEP #14, JOB COMPLETE.
- [SDR IPXA2025020100540](https://openairdocs.org/sdr/IPXA2025020100540.md): Adapter · corroded · Jan 2, 2025 · N137UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN CABIN CLS ADAPTER FR63 Y0 RH HAS CORROSION NOTED. VERIFIED STEP #14, JOB COMPLETE.
- [SDR IPXA2025020100567](https://openairdocs.org/sdr/IPXA2025020100567.md): Adapter · corroded · Jan 2, 2025 · N137UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN CABIN CLS ADAPTER FR60 Y0 RH HAS CORROSION NOTED. VERIFIED STEP #14, JOB COMPLETE.
- [SDR IPXA2025020100494](https://openairdocs.org/sdr/IPXA2025020100494.md): Adapter · corroded · Jan 2, 2025 · N137UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN CABIN CLS ADAPTER FR66 Y0 RH HAS CORROSION NOTED. VERIFIED STEP #14, JOB COMPLETE.
- [SDR IPXA2025020100505](https://openairdocs.org/sdr/IPXA2025020100505.md): Adapter · corroded · Jan 2, 2025 · N137UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN CABIN CLS ADAPTER FR65 Y0 LH HAS CORROSION NOTED. DOT 7628/07 VERIFIED STEP #15, JOB COMPLETE.
- [SDR IPXA2025012500371](https://openairdocs.org/sdr/IPXA2025012500371.md): Seat Track · corroded · Jan 2, 2025 · N137UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEATRACK FR80 Y794.3 HAS CORROSION NOTED.
- [SDR IPXA2024122018385](https://openairdocs.org/sdr/IPXA2024122018385.md): Warning Light · illuminated · Dec 20, 2024 · N137UP · Airbus A300F4622R · Cabin Pressure Control System
  > AFTER SHUTDOWN WITH PACKS OFF, RED EXCESSIVE CABIN PRESSURE LIGHT ILLUMINATED ON CARGO DOOR CONTROL PANEL CHECKED FOR CONTINIUITY AND NORMAL OPERATION OF 13WN (L1 DOOR ESCAPE SLIDE MICRO SWITCH) AND 9WN (L1 DOOR MICRO SWITCH) BOTH SWITCHES CHECKED GOOD IAW ASM
- [SDR IPXA2024121135934](https://openairdocs.org/sdr/IPXA2024121135934.md): Slide · faulted · Dec 11, 2024 · N137UP · Airbus A300F4622R · Escape Slide
  > SLIDE WARNING LIGHT DOES NOT ILLUMINATE WITH PRESS TO TEST PERFORMED ASPSU BITE TEST PER AMM 52-73-00/501, NO DISCREPANCIES NOTED, PERFORMED DOOR SLIDE WARNING LIGHT TEST PER AMM 52-73-00/401 AND OPERATION CHECKS GOOD, THIS CLEARS DMI,PLACARD REMOVED.
- [SDR IPXA2024120250868](https://openairdocs.org/sdr/IPXA2024120250868.md): Controller · faulted · Nov 29, 2024 · N137UP · Airbus A300F4622R · Pneumatic Distribution System
  > **EMERGENCY DECLARED** DURING DESCENT, BLEED #2 FAULT, RAN ECAM / AOM PROCEDURE ACCOMPLISHED #2 ENG RUN, AND ACCOMPLISHED BITE TEST OF #2 PNEUMATIC PRESSURE CONTROLLER, BLEED VALVE OPS CHECKED GOOD AT THIS TIME AND NO FAULTS DISPLAYED IAW AMM 71-00-00 TABLE 50
- [SDR IPXA2024112670522](https://openairdocs.org/sdr/IPXA2024112670522.md): Rod · broken · Nov 24, 2024 · N137UP · Airbus A300F4622R · Drag Control System
  > RH WING #1 SPOILER CONNECTING ROD BROKEN. INSTALLED/ADJUSTED RIGHT WING SPOILER #1 AND NEW CONNECTING ROD ASSY IAW AMM 27-61-54-401. OPS CHECK GOOD. COMPLIED WITH RII STEPS PER GMM 04.02.01.15.
- [SDR IPXA2024112570522](https://openairdocs.org/sdr/IPXA2024112570522.md): Rod · broken · Nov 24, 2024 · N137UP · Airbus A300F4622R · Drag Control System
  > RH WING #1 SPOILER CONNECTING ROD BROKEN REMOVED RIGHT WING #1 SPOILER IAW AMM 27-61-54-401. AWAITING PARTS.
- [SDR IPXA2024110482993](https://openairdocs.org/sdr/IPXA2024110482993.md): Hydraulic Line · leaking · Oct 31, 2024 · N137UP · Airbus A300F4622R · Hydraulic System, Main
  > LOST YELLOW HYD QUANTITY. ECAM YELLOW SYS LO PR. YELLOW LO PR LIGHT ON OVERHEAD FOLLOWED QRH/ECAM PROC DIVERTED BACK TO SDF. REPLACED THE YELLOW SYSTEM AILERON PRESSURE LINE REF AMM 20-23-11 AND EO A300-2910-60058-C. LEAKS CHECKS GOOD
- [SDR IPXA2024103182993](https://openairdocs.org/sdr/IPXA2024103182993.md): Hydraulic System · leaking · Oct 31, 2024 · N137UP · Airbus A300F4622R · Hydraulic System, Main
  > AIR TURN BACK, LOST YELLOW HYD QUANTITY. ECAM YELLOW SYS LO PR. YELLOW LO PR LIGHT ON OVERHEAD FOLLOWED QRH/ECAM PROC DIVERTED BACK TO SDF.
- [SDR IPXA202403130001](https://openairdocs.org/sdr/IPXA202403130001.md): Unknown · odor · Feb 27, 2024 · N137UP · Airbus A300F4622R · Air Distribution System
  > WHEN CLOSEING THE CARGO DOOR A PUNGENT SMELL STARTED BY THE CREW ENTRY DOOR. IT WAS HARD TO BREATHE WITHOUT COUGHING. SUSPECT SKYDROL (HYD FLUID). ACCOMPLISHED REPAIR OF HYD TUBING AT MCD SELECTOR VALVE. REF AMM 20-23-11 PARA.5, H RYNGLOK REPAIR. OPERATED MCD
- [SDR IPXA2024022780878](https://openairdocs.org/sdr/IPXA2024022780878.md): Unknown · odor · Feb 27, 2024 · N137UP · Airbus A300F4622R · Air Distribution System
  > WHEN CLOSEING THE CARGO DOOR A PUNGENT SMELL STARTED BY THE CREW ENTRY DOOR. IT WAS HARD TO BREATHE WITHOUT COUGHING. SUSPECT HYD FLUID. OPEN
- [SDR IPXA2023100243781](https://openairdocs.org/sdr/IPXA2023100243781.md): Relay · unknown · Oct 2, 2023 · N137UP · Airbus A300F4622R · Landing Gear System
  > *** ATB *** L/G RETRACTION INOP AFTER T/O LANDING GEAR LEVER WOULDN€™T MOVE TO THE UP POSITION.COMPLETED ECAM AND PERFORMED AN ATS, WHILE OPERATING IN SYSTEM 2 REPLACED NLG RELAY 14GB, AND MLG RELAYS 17GB AND 18GB IAW ESPM 20-46-50. PERFORMED GEAR SWING ION S
- [SDR IPXA2023092894289](https://openairdocs.org/sdr/IPXA2023092894289.md): Beam · cracked · Sep 23, 2023 · N137UP · Airbus A300F4622R · Cargo/Baggage Doors
  > INSPECTION TYPE:SVFR20A CRACKED AT BEAM 3REMOVED AND REPALCED FR20A IAW DWG A52370600,A52370610 AND A52370650
- [SDR IPXA2023092894288](https://openairdocs.org/sdr/IPXA2023092894288.md): Skin · cracked · Sep 23, 2023 · N137UP · Airbus A300F4622R · Cargo/Baggage Doors
  > INSPECTION TYPE:SV*MAJOR REPAIR* SKIN CRACKED ON C20A AT BEAM 3REPAIRED PER AIRBUS RDAF 81286150/03/2023#A AND UPS EO A300-5230-88313
- [SDR IPXA2023092294228](https://openairdocs.org/sdr/IPXA2023092294228.md): Door · cracked · Sep 22, 2023 · N137UP · Airbus A300F4622R · Cargo/Baggage Doors
  > INSPECTION TYPE:NA*SDR FILED OPEN* FOUND CRACK FWD LOWER CARGO DR LE BY DR LOCK HANDLE. ACCOMP A300-5230-88237-A FWD LOWER CRGO DR FWD EDGE DAMAGE AT FRAME 20A TO BEAM 3 FEF STEP 60A1 THRU 6 & TRANSFERRED ITEM TO DMI LOG REF D-812622 ASSIGNED FERRY PERMIT 9062

Next page: https://openairdocs.org/aircraft/N137UP/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 = 'N137UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N137UP/reports

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