# Service difficulty reports: N125UP

A list on [N125UP](https://openairdocs.org/aircraft/N125UP.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 · 297 reports

- [SDR IPXA2026082508532](https://openairdocs.org/sdr/IPXA2026082508532.md): Slide · unwanted deploy · Aug 25, 2026 · N125UP · Airbus A300F4622R · Escape Slide
  > SLIDE DEPLOYED L1 DOOR SLIDE PLACED ON MEL 52-11-01-2-3, PLACARD INSTALLED, DI LOG UPDATED. DMP COMPLIED WIITH. (SLIDE REMOVED). VERIFIED SAFETY PIN REMOVED AND PRESSURE ON SLIDE IAW GMM 04-02.
- [SDR IPXA2026072435588](https://openairdocs.org/sdr/IPXA2026072435588.md): Bulb · inoperative · Jul 24, 2026 · N125UP · Airbus A300F4622R · Passenger Compartment Lighting
  > LAV AUX LIGHT INOP REMOVED AND REPLACED LAV AUX LIGHT BULB REF AMM 33-51-21, OPS CHECK GOOD.
- [SDR IPXA2026050399528](https://openairdocs.org/sdr/IPXA2026050399528.md): Stop · broken · May 3, 2026 · N125UP · Airbus A300F4622R · Passenger/Crew Doors
  > WHILE ATTEMPTING TO ROB THE MAIN ENTRY DOOR EXTERIOR DOOR HANDLE LEVER STOP, IT BROKE. INSTALLED L1 DOOR HANDLE STOP PER AMM 52-11-11. MATCH DRILLED NEW STOP REF SRM 51-40-20
- [SDR IPXA2026021024123](https://openairdocs.org/sdr/IPXA2026021024123.md): Switch · out of tolerance · Feb 10, 2026 · N125UP · Airbus A300F4622R · Door Warning System
  > ATB, FWD CARGO DOOR NOT CLOSED ON ECAM AFTER TAKEOFF. COULD NOT PRESSURIZE THE AIRCRAFT. FWD CARGO DOOR VERIFIED TO BE CLOSED AND LATCHED. DEFERRED FWD CARGO DOOR INDICATION REF: MEL 52-71-01-2. PLACARD INSTALLED, DMP C/W. PRESSURIZATION CHECKS NORMAL. ACCO
- [SDR IPXA2025121540049](https://openairdocs.org/sdr/IPXA2025121540049.md): Spcc · faulted · Dec 15, 2025 · N125UP · Airbus A300F4622R · Leading Edge Slat Control System
  > DURING APPROACH, RECEIVED SLAT SYS 1+2 FAULT. RAN QRH AND ECAM. INITIALLY PLANNED <15 SLAT WITH 40 FLAP LANDING. WHEN WE SELECTED FLAPS 30/40, SYS 1 SELF CORRECTED, SLATS DEPLOYED TO APPROX 30 THEN. REF T3F18E007Y8MD REMOVED AND REPLACED #2 SFCC PER AMM 27-51
- [SDR IPXA2025063082924](https://openairdocs.org/sdr/IPXA2025063082924.md): Light · detached · Jun 30, 2025 · N125UP · Airbus A300F4622R · Door Warning System
  > PASSENGER/CREW DOOR WARNING LIGHT ASSY HANGING OUT OF DOOR LINER. SECURED PASSENGER/CREW DOOR WARNING LIGHT HOUSING IAW AMM 52-73-11. OPS CHECK GOOD.
- [SDR IPXA2025060912703](https://openairdocs.org/sdr/IPXA2025060912703.md): Support Angle · deformed · May 5, 2025 · N125UP · Airbus A300F4622R · Nacelle/Pylon Miscellaneous Structure
  > NR 2 PYLON FWD FAIRING LH AND RH SIDE SUPPORT ANGLES DEFORMED FWD OF RIB 4A. DOT# 110-99 JP-110. ACCOMPLISHED E.A.#: 300-5452-27-A3926, PRELIMINARY 6, STEP #38: INSTALLED IAW DRAWING A54612175 AND SRM 51-40-21.
- [SDR IPXA2025050512703](https://openairdocs.org/sdr/IPXA2025050512703.md): Skin · deformed · May 5, 2025 · N125UP · Airbus A300F4622R · Nacelle/Pylon, Plate/Skin
  > NR 2 PYLON FWD FAIRING LH AND RH SIDE SUPPORT ANGLES (P/N A54612200200/201)DEFORMED FWD OF RIB J4. DOT# 110-99 JP-110
- [SDR IPXA2025061833324](https://openairdocs.org/sdr/IPXA2025061833324.md): Support Angle · deformed · Apr 30, 2025 · N125UP · Airbus A300F4622R · Nacelle/Pylon Miscellaneous Structure
  > NUMBER 2 PYLON FWD FAIRING LH AND RH SIDE SUPPORT ANGLES (P/N A54612232200/201)DEFORMED FWD OF RIB 4A. DOT# 110-99 JP-110 REFORMED AREA AT #2 PYLON FWD FAIRING L/H AND R/H SIDE SUPPORT ANGLES P/N A54612232200/201 FWD OF RIB 4A IAW SREO-41097-C. AND EA 3005452-
- [SDR IPXA2025050533324](https://openairdocs.org/sdr/IPXA2025050533324.md): Skin · deformed · Apr 30, 2025 · N125UP · Airbus A300F4622R · Nacelle/Pylon Structure
  > #2 PYLON FWD FAIRING LH AND RH SIDE SUPPORT ANGLES (P/N A54612232200/201)DEFORMED FWD OF RIB J4. DOT# 110-99 JP-110 VERIFIED REMOVAL OF 2 EA SUPPORT ANGLES IAW-A300-SRM-51-40-21
- [SDR IPXA2025061910294](https://openairdocs.org/sdr/IPXA2025061910294.md): Skin · wrinkled · Apr 29, 2025 · N125UP · Airbus A300F4622R · Nacelle/Pylon, Plate/Skin
  > NR 1 ENGINE NACELLE FORWARD SKIN PANEL WRINKLED AT RIB J1 ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-93897-REQ1 AND VT-MAE EA 300-5452-27-A3925 REV. -. CAUTION: THE WORK INSTRUCTIONS CONTAINED WITHIN (OR APPROVED BY) THIS EO CONTAIN RII INSPECTION REQU
- [SDR IPXA2025061810362](https://openairdocs.org/sdr/IPXA2025061810362.md): Skin · wrinkled · Apr 29, 2025 · N125UP · Airbus A300F4622R · Nacelle/Pylon, Plate/Skin
  > NUMBER 2 ENGINE NACELLE FORWARD SKIN PANEL WRINKLED THE CURRENT CONFIGURATION OF AIRCRAFT AND PYLON: ENGINE REMOVED, DAMAGED SKIN REMOVED,DAMAGED LH AND RH SIDE SUPPORT ANGLES REMOVED (ITEM 170 ON SRM 54-52-11 FIG 1)ACCOMPLISHED STEP 5 OF EA: 300-5452-27-A3926
- [SDR IPXA2025050510362](https://openairdocs.org/sdr/IPXA2025050510362.md): Skin · wrinkled · Apr 29, 2025 · N125UP · Airbus A300F4622R · Nacelle/Pylon, Plate/Skin
  > #2 ENGINE NACELLE FORWARD SKIN PANEL WRINKLED VERIFIED ACCOMPLISHMENT OF STEP 17 PER EA: 300-5452-27-A3926 PRELIMINARY 3.<BR>VALIDATED DVI INSPECTION ON PYLON PRIMARY STRUCTURE, NO DAMAGE FOUND.
- [SDR IPXA2025050510294](https://openairdocs.org/sdr/IPXA2025050510294.md): Skin · wrinkled · Apr 29, 2025 · N125UP · Airbus A300F4622R · Nacelle/Pylon, Plate/Skin
  > #1 ENGINE NACELLE FORWARD SKIN PANEL WRINKLED AT RIB J1 VERIFIED ACCOMPLISHMENT OF EA #300-5452-27-A3925 PRELIMINARY 3 STEPS 20, 21 AND 22<BR>NO DISCREPANCIES NOTED AT THIS TIME.
- [SDR IPXA2025052564732](https://openairdocs.org/sdr/IPXA2025052564732.md): Skin · cracked · Apr 21, 2025 · N125UP · Airbus A300F4622R · Fuselage Main, Plate/Skin
  > TWO CRACKS FOUND INSIDE HOLE T ON FR47 RH HORIZONTAL JUNCTION. ACCOMPLISH THE REPAIR PER EO-93655-REQ1 REV. 2 AND EA 300-5710-27-A3905 REV. A. CAUTION: THE WORK INSTRUCTIONS CONTAINED WITHIN (OR APPROVED BY) THIS EO CONTAIN RII INSPECTION REQUIREMENTS AND RII
- [SDR IPXA2025052534907](https://openairdocs.org/sdr/IPXA2025052534907.md): Skin · cracked · Apr 18, 2025 · N125UP · Airbus A300F4622R · Fuselage Main, Plate/Skin
  > CRACK FOUND IN FASTENER HOLE ON BULK CARGO DOOR SCUFF PLATE. AREA MARKED IN RED. ACCOMPLISHED E.A.#: 300-5317-27-A3915, PRELIMINARY 1, STEP# 2: "INCREMENTALLY REAM THE 1 EACH CRACKED HOLE IN STEPS OF 0.4 MM UNTIL DAMAGE FREE AND ROUND CONDITION ACHIEVED OR MAX
- [SDR IPXA2025052562688](https://openairdocs.org/sdr/IPXA2025052562688.md): Skin · cracked · Apr 17, 2025 · N125UP · Airbus A300F4622R · Fuselage Main, Frame
  > CRACK FOUND IN HOLE T ON FR47 LH HORIZONTAL JUNCTION. ACCOMPLISH THE REPAIR PER EO-93642-REQ1 AND EA 300-5710-27-A3893 REV. -. CAUTION: THE WORK INSTRUCTIONS CONTAINED WITHIN (OR APPROVED BY) THIS EO CONTAIN RII INSPECTION REQUIREMENTS AND RII BUY - OFF WHICH
- [SDR IPXA2025061837191](https://openairdocs.org/sdr/IPXA2025061837191.md): Door Frame · gouged · Apr 16, 2025 · N125UP · Airbus A300F4622R · Fuselage Main, Structure
  > CREW DOOR, AFT FRAME (FR16.1) MECHANISM LOCK FITTING HAS GOUGE. DOT 103-62 (ATTACHED PHOTO) REMOVED MINOR GOUGE AT LOCK FITTING IAW SRM A300-600 51-73-11 MATERIAL THIKNESS IS 1.100" AND MATERIAL LOSS 0.003 AND REMAINING THIKNESS IS 1.197" THERE IS WHTIN IN
- [SDR IPXA2025061837628](https://openairdocs.org/sdr/IPXA2025061837628.md): Lock · damaged · Apr 16, 2025 · N125UP · Airbus A300F4622R · Passenger/Crew Doors
  > CREW DOOR, INNER SURFACE, UPPER SIDE, BRACKET SUPPORT AT AFT LOCK HOLE HAS GOUGE. DOT 103-64 (ATTACHED PHOTO) REMOVED MINOR GAUGE IAW SRM A300-600 51-73-11 MATERIAL LOSS 0.002 WITHIN LIMITS IAW SRM 51-73-11. T988826 C18-C02 OK TO RESTORE SURFACE PROTECTION. AP
- [SDR IPXA2025052546455](https://openairdocs.org/sdr/IPXA2025052546455.md): Skin · cracked · Apr 16, 2025 · N125UP · Airbus A300F4622R · Fuselage Main, Plate/Skin
  > TWO CRACKS FOUND IN HOLE A ON RH FR47 HORIZONTAL JUNCTION. ACCOMPLISH THE REPAIR PER EO-93655-REQ1 REV. 2 AND EA 300-5710-27-A3905 REV. A. CAUTION: THE WORK INSTRUCTIONS CONTAINED WITHIN (OR APPROVED BY) THIS EO CONTAIN RII INSPECTION REQUIREMENTS AND RII BUY
- [SDR IPXA2025052546480](https://openairdocs.org/sdr/IPXA2025052546480.md): Skin · cracked · Apr 16, 2025 · N125UP · Airbus A300F4622R · Fuselage Main, Plate/Skin
  > CRACK FOUND IN HOLE C ON RH FR47 HORIZONTAL JUNCTION. ACCOMPLISH THE REPAIR PER EO-93655-REQ1 REV. 2 AND EA 300-5710-27-A3905 REV. A. CAUTION: THE WORK INSTRUCTIONS CONTAINED WITHIN (OR APPROVED BY) THIS EO CONTAIN RII INSPECTION REQUIREMENTS AND RII BUY - OFF
- [SDR IPXA2025052546594](https://openairdocs.org/sdr/IPXA2025052546594.md): Skin · cracked · Apr 16, 2025 · N125UP · Airbus A300F4622R · Fuselage Main, Frame
  > CRACK FOUND IN HOLE S ON RH FR47 HORIZONTAL JUNCTION. ACCOMPLISH THE REPAIR PER EO-93655-REQ1 REV. 2 AND EA 300-5710-27-A3905 REV. A. CAUTION: THE WORK INSTRUCTIONS CONTAINED WITHIN (OR APPROVED BY) THIS EO CONTAIN RII INSPECTION REQUIREMENTS AND RII BUY - OFF
- [SDR IPXA2025052546546](https://openairdocs.org/sdr/IPXA2025052546546.md): Skin · cracked · Apr 16, 2025 · N125UP · Airbus A300F4622R · Fuselage Main, Frame
  > CRACK FOUND IN HOLE E ON RH FR47 HORIZONTAL JUNCTION. ACCOMPLISH THE REPAIR PER EO-93655-REQ1 REV. 2 AND EA 300-5710-27-A3905 REV. A. CAUTION: THE WORK INSTRUCTIONS CONTAINED WITHIN (OR APPROVED BY) THIS EO CONTAIN RII INSPECTION REQUIREMENTS AND RII BUY - OFF
- [SDR IPXA2025052546559](https://openairdocs.org/sdr/IPXA2025052546559.md): Skin · cracked · Apr 16, 2025 · N125UP · Airbus A300F4622R · Fuselage Main, Frame
  > CRACK FOUND IN HOLE G ON RH FR47 HORIZONTAL JUNCTION. ACCOMPLISH THE REPAIR PER EO-93655-REQ1 REV. 2 AND EA 300-5710-27-A3905 REV. A. CAUTION: THE WORK INSTRUCTIONS CONTAINED WITHIN (OR APPROVED BY) THIS EO CONTAIN RII INSPECTION REQUIREMENTS AND RII BUY - OFF
- [SDR IPXA2025052344612](https://openairdocs.org/sdr/IPXA2025052344612.md): Bracket · cracked · Apr 16, 2025 · N125UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > LH HORIZONTAL STAB LEADING EDGE APRON SUPPORT BRACKET P/N: A5517155120451 BROKEN. INSTALLATION OF NEW BRACKET P/N: A5517155120451, B/N:0004388210 IAW A300-600F SRM 51-40-21. FASTENERS USED: FOUR HI-LOKS P/N HL10VF6-6, BATCH #0004358134 AND FOUR COLLARS P/N N
- [SDR IPXA2025041637628](https://openairdocs.org/sdr/IPXA2025041637628.md): Support Bracket · gouged · Apr 16, 2025 · N125UP · Airbus A300F4622R · Passenger/Crew Doors
  > CREW DOOR, INNER SURFACE, UPPER SIDE, BRACKET SUPPORT AT AFT LOCK HOLE HAS GOUGE.
- [SDR IPXA2025041637191](https://openairdocs.org/sdr/IPXA2025041637191.md): Door Frame · gouged · Apr 16, 2025 · N125UP · Airbus A300F4622R · Fuselage Main, Structure
  > CREW DOOR, AFT FRAME (FR16.1) MECHANISM LOCK FITTING HAS GOUGE.
- [SDR IPXA2025052507731](https://openairdocs.org/sdr/IPXA2025052507731.md): Frame · cracked · Apr 14, 2025 · N125UP · Airbus A300F4622R · Fuselage Main, Frame
  > CRACK FOUND IN HOLE G ON FR47 LH HORIZONTAL JUNCTION. COMPLIED WITH STEP 15 OF PRELIM 1 EA-300-5710-27-A3893.
- [SDR IPXA2025052508352](https://openairdocs.org/sdr/IPXA2025052508352.md): Floor Support · cracked · Apr 14, 2025 · N125UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MDC FLOOR STRUCTURE RH SIDE FR38.1 SUPPORT (DOG BONE) CRACKED. DOT 11-056 THE SPARE PART IS CONSUMABLE AND DOES NOT HAVE A UPS PARTS TAG. (SEE ATTACHMENT).
- [SDR IPXA2025060308262](https://openairdocs.org/sdr/IPXA2025060308262.md): Floor Support · cracked · Apr 14, 2025 · N125UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MDC FLOOR STRUCTURE RH SIDE FR38.2 SUPPORT (DOG BONE) CRACKED.
- [SDR IPXA2025052307518](https://openairdocs.org/sdr/IPXA2025052307518.md): Crossbeam · bent · Apr 14, 2025 · N125UP · Airbus A300F4622R · Fuselage Main, Structure
  > MAIN DECK CROSSBEAM AT FR 48 BETWEEN -Y450 AND -Y953 BENT.DOT# 110-61 JP-110. INSTALLED NEW CROSSBEM I.A.W A300-600 SREO 75878-REQ001.
- [SDR IPXA2025052395256](https://openairdocs.org/sdr/IPXA2025052395256.md): Bracket · gouged · Apr 14, 2025 · N125UP · Airbus A300F4622R · Wing Structure
  > LH WING, UPPER SURFACE, ATTACHMENT WTB FAIRIG AREA, BRACKET SUPPORT HAS GOUGE (2EA). DOT 103-34 (ATTACHED PHOTO). NSTALLED NEW BRACKET IAW A300-600 SRM 51-40-21. RIVET P/N: CR3213-6-03 BATCH: 0004194656, HI-LOCK P/N: DAN5-6-6 BATCH: 0004178101, COLLAR P/N: NS
- [SDR IPXA2025052307579](https://openairdocs.org/sdr/IPXA2025052307579.md): Crossbeam · bent · Apr 14, 2025 · N125UP · Airbus A300F4622R · Fuselage Main, Structure
  > MAIN DECK CROSSBEAM AT FR 49 BETWEEN -Y450 AND -Y953 BENT. DOT# 110-62 JP-110. INSTALLED NEW CROSSBEM I.A.W A300-600 SREO 75878-REQ001. REVIEWED
- [SDR IPXA2025042908379](https://openairdocs.org/sdr/IPXA2025042908379.md): Floor Panel · damaged · Apr 14, 2025 · N125UP · Airbus A300F4622R · Fuselage Floor Panel
  > MDC FLOOR PANEL 231KJ IS DAMAGED AND BROKEN. FABRICATED MAIN DECK FLOOR PANEL 231KJ IAW SREO-16407-REQ001.
- [SDR IPXA2025042788628](https://openairdocs.org/sdr/IPXA2025042788628.md): Seat Track · damaged · Apr 13, 2025 · N125UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MDC FLOOR STRUCTURE FR79/Y0 UNDER FLOOR PANEL 261EM SEAT TRACK CORRODED.
- [SDR IPXA2025050794051](https://openairdocs.org/sdr/IPXA2025050794051.md): Adapter · corroded · Apr 13, 2025 · N125UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MDC FLOOR PANEL 251WG FWD ADAPTER CLS WITH CORROSION.
- [SDR IPXA2025050793709](https://openairdocs.org/sdr/IPXA2025050793709.md): Adapter · corroded · Apr 13, 2025 · N125UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MDC FR57.1/Y-0 UNDER FLOOR PANEL 252LG CLS ADAPTER CORRODED.
- [SDR IPXA2025050793730](https://openairdocs.org/sdr/IPXA2025050793730.md): Adapter · corroded · Apr 13, 2025 · N125UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MDC ON PANEL 251 WG ADAPTER CLS WITH CORROSION.
- [SDR IPXA2025050793732](https://openairdocs.org/sdr/IPXA2025050793732.md): Adapter · corroded · Apr 13, 2025 · N125UP · Airbus A300F4622R · Fuselage Main, Attach Fittings
  > MDC FLOOR STRUCTURE FR58/Y-0 UNDER FLOOR PANEL 251FM CLS ADAPTER CORRODED. ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-93740-REQ1 AND VT-MAE EA 300-5316-27-A3909 REV. -.
- [SDR IPXA2025052389112](https://openairdocs.org/sdr/IPXA2025052389112.md): Floorbeam · cracked · Apr 13, 2025 · N125UP · Airbus A300F4622R · Fuselage Main, Floor Beam
  > MDC FLOOR STRUCTURE FR79 RH SIDE FLOOR PANEL 262AH PROFILE CRACKED. DOT 11-026. ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-93576-REQ1 AND VT-MAE EA 300-5318-27-A3917, REV. -.
- [SDR IPXA2025043093692](https://openairdocs.org/sdr/IPXA2025043093692.md): Floor Panel · broken · Apr 13, 2025 · N125UP · Airbus A300F4622R · Fuselage Floor Panel
  > MDC FLOOR PANEL 251FM BROKEN. DOT 11-040 REVIEWED
- [SDR IPXA2025050689112](https://openairdocs.org/sdr/IPXA2025050689112.md): Profile · cracked · Apr 13, 2025 · N125UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > **SDR FILED OPEN**FAULT: STR-Z200 MDC FLOOR STRUCTURE FR79 RH SIDE FLOOR PANEL 262AH PROFILE CRACKED. DOT 11-026 VERIFIED INSTALLATION OF MDC FLOOR IN FR79 RH Z PROFILE IAW A300-600F SRM 51-40-21. MATERIALS USED: SEALANT P/N 04-001-0109, BATCH #0004371367, SO
- [SDR IPXA2025050694089](https://openairdocs.org/sdr/IPXA2025050694089.md): Profile · cracked · Apr 13, 2025 · N125UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > **SDR FILED OPEN**FAULT-STR-Z200-MDC FLOOR IN C65 LH Z PROFILE HAVE A CRACK DOT 07-119 VERIFIED INSTALLATION OF MDC FLOOR IN C65 LH Z PROFILE IAW A300-600F SRM 51-40-21. MATERIALS USED: SEALANT P/N 04-001-0109, BATCH #0004371367, SOLID RIVETS 36 EACH P/N NAS1
- [SDR IPXA2025042989085](https://openairdocs.org/sdr/IPXA2025042989085.md): Seat Track · corroded · Apr 13, 2025 · N125UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > FAULT: STR-Z200 MDC FLOOR STRUCTURE UNDER FLOOR PANEL 262FM FR80/-Y794.3 SEAT TRACK CORRODED. DOT 11-024.REMOVED CORROSION ON SEAT TRACK AT FR 80/-Y953 IAW A300-600F SRM 51-74-10.REMOVED SEAT TRACK AT MDC FLOOR STRUCTURE UNDER FLOOR PANEL 262FM FR80/-Y794.3, I
- [SDR IPXA2025050289249](https://openairdocs.org/sdr/IPXA2025050289249.md): Support · cracked · Apr 13, 2025 · N125UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > FLOOR STRUCTURE RH SIDE BETWEEN FR73/74 WEB SUPPORT UNDER SURFACE CRACKED. DOT 11-030.REMOVED SUPPORT UNDER MDC FLOOR STRUCTURE RH SIDE BETWEEN FR73/74 IAW A300-600 SRM 51-40-21.TREATED AND PRIMED NEW PART SHEAR WED IAW A300-600 SRM 51-21-10. APPLIED TOPCOAT
- [SDR IPXA2025050193756](https://openairdocs.org/sdr/IPXA2025050193756.md): Seat Track · corroded · Apr 13, 2025 · N125UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MDC FLOOR, SEAT TRACK IN Y450 ON PANEL 251VF HAVE CORROSION DOT 07-116 VERIFIED INSTALLATION OF NEW SEAT TRACK SECTION IN Y450 BETWEEN FR63 AND FR66 IAW SRM 53-10-16 PARAGRAPH 4 FIGURE 201 PAGE 207/208 AND SRM 51-40-21. OPEN
- [SDR IPXA2025041588630](https://openairdocs.org/sdr/IPXA2025041588630.md): Seat Track · corroded · Apr 13, 2025 · N125UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MDC FLOOR STRUCTURE FR79/-Y450 UNDER FLOOR PANEL 262EM SEAT TRACK CORRODED. DOT 11-023. VERIFIED REMOVAL OF CORROSION ON SEAT TRACK IAW A300-600F SRM 51-74-10. ORIGINAL MATERIAL THICKNESS.535", MATERIAL LOSS.021", MATERIAL LEFT.514". THE LOSS IS IN LIMITS
- [SDR IPXA2025052383032](https://openairdocs.org/sdr/IPXA2025052383032.md): Floor Support · cracked · Apr 12, 2025 · N125UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MDC COMPARTMENT AFT AREA FLOOR PANEL 261HM HAS A SUPPORT CRACKED. DOT 11-020. REMOVED AND REPLACED FLOOR SUPPORT ANGLE (PROFILE) FRAME 80 RH PNL 261 HM IAW A300-600 SRM 51-40-21. ANGLE P/N: A5398140120000 BATCH:0004390460. RIVETS P/N: MS20470AD5-5.BATCH:00043
- [SDR IPXA2025052383131](https://openairdocs.org/sdr/IPXA2025052383131.md): Frame · cracked · Apr 12, 2025 · N125UP · Airbus A300F4622R · Fuselage Main, Frame
  > MDC, BETWEEN FR74 AND FR73, LH SIDE, UNDER FLOOR STRUCTURE FRAME HAS A CRACK BETWEEN 2 RIVETS. INSTALLED NEW SHEAR WEB I.A.W A300-600 SRM 51-40-21.
- [SDR IPXA2025052383072](https://openairdocs.org/sdr/IPXA2025052383072.md): Floor Support · cracked · Apr 12, 2025 · N125UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MDC, BETWEEN FR 78 AND FR 77, LH SIDE, FLOOR STRUCTURE FRAME HAS 2EA CRACKS. DOT 23-002. NEW WEB HAS BEEN INSTALLED IAW A300-600 SRM 51-40-21 AND ALSO THE INTERFAY SEALING HAVE BEEN RESTORED BETWEEN THE SURFACES IAW A300-600 SRM 51-76-10. MATERIALS USED: SEAL

Next page: https://openairdocs.org/aircraft/N125UP/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 = 'N125UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N125UP/reports

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