# Service difficulty reports: N430UP

A list on [N430UP](https://openairdocs.org/aircraft/N430UP.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 · 270 reports

- [SDR IPXA2026040487396](https://openairdocs.org/sdr/IPXA2026040487396.md): Support Bracket · corroded · Apr 1, 2026 · N430UP · Boeing 75724APF · Aerodynamic Fairings
  > WING TO BODY FAIRING STR, RH FWD UPPER WING, BTW STA 1080-1100, 1EA PANEL SUPPORT BRACKET HAS CORROSION. REMOVED CORROSION FROM WING TO BODY FAIRING STR, RH FWD UPPER WING, BTW STA 1080-1100. EVALUATED, TOTAL THICKNESS: 0.080, MATERIAL LOSS:0.003IN (4%), MATE
- [SDR IPXA2026041587231](https://openairdocs.org/sdr/IPXA2026041587231.md): Angle · corroded · Apr 1, 2026 · N430UP · Boeing 75724APF · Aerodynamic Fairings
  > WING TO BODY FAIRING RH, FWD UPPER WING, BTW STA 900-920, 2EA PANEL SUPPORTS CORRODED. DOT 23-077. INSTALLED 2 NEW BRACKETS I.A.W. B757-200PF SRM 51-40-02. REVIEWED
- [SDR IPXA2026041367944](https://openairdocs.org/sdr/IPXA2026041367944.md): Holder · cracked · Mar 31, 2026 · N430UP · Boeing 75724APF · Fuselage Main, Structure
  > ACCESS DOOR 435AL, HOLD OPEN ROD HOLDER IS CRACKED. INSTALLED 1EA NEW SPRING CLIP IAW SRM 51-40-02-0G-0.
- [SDR IPXA2026041765252](https://openairdocs.org/sdr/IPXA2026041765252.md): Tee Fitting · corroded · Mar 31, 2026 · N430UP · Boeing 75724APF · Fuselage Main, Structure
  > LOWER FUSELAGE THROUGH ACCESS PANEL 198BR STRUCTURE FAIRING SUPPORT BS 1040 RBL 0 TO RBL 65 TIEH CORROSION DOT 07-106. INSTALLED 1 TEE FITTINGIAW SRM 51-40-02.
- [SDR IPXA2026041565071](https://openairdocs.org/sdr/IPXA2026041565071.md): Intercostal · corroded · Mar 31, 2026 · N430UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > LOWER FUSELAGE AT STA 1045 RBL 45 INTERCOSTAL WITH CORROSION. INSTALLED NEW PART AT OWER FUSELAGE AT BS 1045 RBL 45 IAW SRM 51-40-02-0G-0.
- [SDR IPXA2026041454777](https://openairdocs.org/sdr/IPXA2026041454777.md): Angle · cracked · Mar 31, 2026 · N430UP · Boeing 75724APF · Engine Thrust Reverser
  > NR 1 ENG O/B T/R INNER TOP MIDDLE BRACKET NEXT TO HOLD-OPEN ACTUATOR ATTACHMENTS IS CRACKED. INSTALLED NEW BRACKET ON #1 ENG O/B T/R INNER TOP MIDDLE. IAW B757-200PF, SRM 51-40-02.
- [SDR IPXA2026041365276](https://openairdocs.org/sdr/IPXA2026041365276.md): Web · corroded · Mar 31, 2026 · N430UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > LOWER FUSELAGE STA 1180 TO 1240 RBL 59 WEB WITH CORROSION DOT 07-107. INSTALLED NEW WEB (1 EA) LOWER FUSELAGE STA 1180 TO 1240 RBL 59 IAW B757-200 SRM 51-20-01. REVIEWED.
- [SDR IPXA2026041365017](https://openairdocs.org/sdr/IPXA2026041365017.md): Floor Support · corroded · Mar 31, 2026 · N430UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > BULK CARGO COMP, FLOOR SUPPORT HAS 2EA SHIMS CORRODED, BTW BS 1701-1720, LBL 9.20. REMOVED 2EA NUTPLATES SUPPORT (SHIMS) AND 1EA ANGLE SUPPORT CORRODED IAW SRM 51-40-02-0G-0. INSTALLED NUTPLATE SUPPORT SHIM & 1EA ANGLE SUPPORT AT BULK CARGO COMP, FLOOR SUPPO
- [SDR IPXA2026040965063](https://openairdocs.org/sdr/IPXA2026040965063.md): Intercostal · corroded · Mar 31, 2026 · N430UP · Boeing 75724APF · Aerodynamic Fairings
  > THROUGH ACCESS PANEL 198BR FAIRING STRUCTURE AT STA 1040 TO 1060 RBL 65 WITH CORROSION. REMOVED FAIRING STRUCTURE AT STA 1040 TO 1060 RBL 65 OUT OF LIMITS IAW SRM 53-00-71-1A-1. INSTALLED NEW INTERCOSTAL AT BS 1040 - 1060, RBL 65, IAW SRM 51-40-02.
- [SDR IPXA2026041150506](https://openairdocs.org/sdr/IPXA2026041150506.md): Tee Fitting · corroded · Mar 30, 2026 · N430UP · Boeing 75724APF · Aerodynamic Fairings
  > CORROSION FOUND AT STA 1180 TO STA 1240 L/H TEE CHORD. WTB SUPPORT AFT FUSELAGE. INSTALLED NEW T-CHORD.IAW B757-200PF, SRM 51-40-02. REVIEWED
- [SDR IPXA2026041032501](https://openairdocs.org/sdr/IPXA2026041032501.md): Bracket · cracked · Mar 29, 2026 · N430UP · Boeing 75724APF · Fuselage Main, Attach Fittings
  > RIGHT WHEEL WELL FILTER SUPPORT BRACKET IS CRACKED AY AFT CORNER. REMOVED BRACKET ON RIGHT WHEEL WELL FILTER SUPPORT AFT CORNER IAW SRM 51-40-02. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G-0.
- [SDR IPXA2026041136020](https://openairdocs.org/sdr/IPXA2026041136020.md): Skin · punctured · Mar 29, 2026 · N430UP · Boeing 75724APF · APU Cowling/Containment
  > APU COMPARTMENT LT INERNAL SKIN AT BS 1918 HAVE HONEYCOMB WITH HOLE. REMOVED DAMAGE AND PREPARED AREA IAW SRM 51-70-10-2R-2. FILLED AREA, FABRICATED AND PREPARED REPAIR DOUBLER IAW SRM 51-70-10-2R-2. BONDED REPAIR DOUBLER IAW SRM 51-70-10-2R-2. MAJOR REPAIR.
- [SDR IPXA2026041135878](https://openairdocs.org/sdr/IPXA2026041135878.md): Angle · corroded · Mar 29, 2026 · N430UP · Boeing 75724APF · Elevator Structure
  > LEFT HORIZONAL STAB BETWEEN ELEVATOR AND HORIZONTAL REAR SPAR AT THE OTBD TIP BRACKET THAT ATTACH BONDING WIRE ARE EXFOLIATED. REMOVED CORRODED BRACKET IAW SRM 51-40-02. INSTALLED NEW BRACKED ON LEFT HORIZONAL STABILIZER BETWEEN ELEVATOR & HORIZONTAL REAR SPA
- [SDR IPXA2026040835942](https://openairdocs.org/sdr/IPXA2026040835942.md): Splice Plate · corroded · Mar 29, 2026 · N430UP · Boeing 75724APF · Elevator Structure
  > LEFT HORIZONAL STAB ELEVATOR AT THE O/B TIP HAVE CORROSION. REMOVED AFFECTED LT HORIZONAL STAB ELEVATOR OTBD TIP LOWER BONDING PLATE AND SHIMS IAW SRM 51-40-02. INSTALLED SPLICE PLATE AND SHIM IAW SRM 51-40-02-0G-0.
- [SDR IPXA2026040426186](https://openairdocs.org/sdr/IPXA2026040426186.md): Cover · cracked · Mar 28, 2026 · N430UP · Boeing 75724APF · Wing Miscellaneous Structure
  > LEFT WING L/E SLAT NR 4 INBD MAIN TRACK COVER CRACKED. INSTALLED A NEW TRACK COVER ON LT WING L/E SLAT IAW SRM 51-40-02.
- [SDR IPXA2026041526322](https://openairdocs.org/sdr/IPXA2026041526322.md): Bracket · corroded · Mar 28, 2026 · N430UP · Boeing 75724APF · Fuselage, Wing Attach Fittings
  > LH WING ROOT UPPER SIDE THROUGH ACCESS PANEL 191DL HAVE 4 BRACKETS WITH CORROSION. INSTALLED 2 NEW BRACKETS I.A.W. B757-200PF SRM 51-40-02. REVIEWED
- [SDR IPXA2026041621262](https://openairdocs.org/sdr/IPXA2026041621262.md): Support · corroded · Mar 28, 2026 · N430UP · Boeing 75724APF · Aerodynamic Fairings
  > WING TO BODY WEB SUPPORT FROM BS 1180 - 1240, LBL 63 CORRODED. INSTALLED NEW WEB SUPPORT IAW SRM 51-40-02.
- [SDR IPXA2026041010983](https://openairdocs.org/sdr/IPXA2026041010983.md): Tee Angle · corroded · Mar 27, 2026 · N430UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > TEE CHORD CORRODED FOUND AT STA 1180 FROM BL0 TO RBL 61. INSTALLED T-CHORD STA 1180 FROM BL 0 TO RBL 61 IAW SRM 51-40-02.
- [SDR IPXA2026040810930](https://openairdocs.org/sdr/IPXA2026040810930.md): Tee Angle · corroded · Mar 27, 2026 · N430UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > TEE CHORD CORRODED FOUND BETWEEN STA 1180 AND STA 1240 RBL 63 ABOVE R.A.T. DOOR. INSTALLED TCHORD & PLATE BETWEEN STA 1180 AND STA 1240 RBL 63 ABOVE R.A.T. DOOR IAW B757-200PF SRM 51-40-02-0G-0. REVIEWED.
- [SDR IPXA2026041610845](https://openairdocs.org/sdr/IPXA2026041610845.md): Tee Fitting · corroded · Mar 27, 2026 · N430UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > TEE CHORD CORRODED FOUND BETWEEN STA 1180 AND STA 1240 RBL 58 ABOVE RAT DOOR. INSTALLED BETWEEN BS 1180 AND 1240, RBL 58 ABOVE RAT DOOR IAW SRM 51-40-02-0G-0 - 1.
- [SDR IPXA2026041611851](https://openairdocs.org/sdr/IPXA2026041611851.md): Intercostal · corroded · Mar 27, 2026 · N430UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > INTERCOSTAL L/H SIDE STA 1045, LBL20 TO LBL 37 WITH CORRODED. NSTALLED NEW INTERCOSTAL FROM L/H SIDE STA 1045, LBL20 TO LBL 37 IAW B757-200 SRM 51-40-02.
- [SDR IPXA2026041811200](https://openairdocs.org/sdr/IPXA2026041811200.md): Bracket · corroded · Mar 27, 2026 · N430UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > BRACKET CORRODED FOUND AT STA 1234 R/H BETWEEN RBL 58 TO RBL 63. INSTALLED NEW BRACKET (1 EA) BETWEEN STA 1180 AND STA 1240 RBL 58 ABOVE R.A.T DOOR IAW SRM 51-40-02. REVIEWED.
- [SDR IPXA2026041311405](https://openairdocs.org/sdr/IPXA2026041311405.md): Tee Fitting · corroded · Mar 27, 2026 · N430UP · Boeing 75724APF · Aerodynamic Fairings
  > T-CHORD STA 1060 L/H SIDE WITH CORRODED. REMOVED T-CHORD STA 1060 L/H IAW B757-200PF, SRM 51-40-02. OUT OF LIMITS IAW B757-200PF, SRM 53-00-71-1A-1 DATAIL IX. INSTALLED TCHORD STA 1060 LBL 56 TO 75 IAW B757-200PF SRM 51-40-02-0G-0. INSTALLED NEW CENTER SECTIO
- [SDR IPXA2026041611830](https://openairdocs.org/sdr/IPXA2026041611830.md): Tee Fitting · corroded · Mar 27, 2026 · N430UP · Boeing 75724APF · Fuselage Main, Structure
  > FAULT Z-100 STR: WTB TEE CHORD SUPPORT AT STA 1200 LH HAS CORROSION. REMOVED CHORD SUPPORT AT STA 1220 L/H, OUT OF LIMITS IAW B757-200PF, SRM 51-00-71-1A-1 DATAIL VII, SRM 51-40-02. INSTALLED NEW T-CHORD.IAW B757-200PF, SRM 51-40-02.
- [SDR IPXA2026040911691](https://openairdocs.org/sdr/IPXA2026040911691.md): Intercostal · corroded · Mar 27, 2026 · N430UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > LEFT INTERCOSTAL BS 1040 - 1060 CORRODED. REMOVED DAMAGE IAW SRM 51-10-02. INSTALLED A NEW INTERCOSTAL IAW SRM 51-40-02.
- [SDR IPXA2026040811015](https://openairdocs.org/sdr/IPXA2026040811015.md): Tee Fitting · corroded · Mar 27, 2026 · N430UP · Boeing 75724APF · Fuselage Main, Attach Fittings
  > LT LOWER MIDDLE FUSELAGE STA 1040 TO STA 1060 LBL65 T-CHORD CORRODED. INSTALLED 1 EA TCHORD IAW SRM 51-40-02.
- [SDR IPXA2026040911700](https://openairdocs.org/sdr/IPXA2026040911700.md): Tee Fitting · corroded · Mar 27, 2026 · N430UP · Boeing 75724APF · Aerodynamic Fairings
  > WTB TEE CHORD SUPPORT AT STA 1220 R/H HAS CORROSION INSTALLED WTB TEE CHORD SUPPORT AT STA 1220 R/H IAS 757-200PF SRM 51-40-02.
- [SDR IPXA2026041392807](https://openairdocs.org/sdr/IPXA2026041392807.md): Strap · corroded · Mar 26, 2026 · N430UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > APU INLET DOOR AFT STRAP STA 1825.00 FROM STR S3R TO STR S-6R HAS EVIDENCE OF CORROSION. REMOVED CORROSION THE INNER STRAP I.A.W. B757-200PF SRM 51-40-02 AND EVALUATED I.A.W. B757-200PF SRM 53-80-15-1A-1. REMOVED INNER STRAP CORRODED I.A.W. B757-200PF SRM 51-4
- [SDR IPXA2026041393076](https://openairdocs.org/sdr/IPXA2026041393076.md): Angle · corroded · Mar 26, 2026 · N430UP · Boeing 75724APF · Auxiliary Power Unit (APU) Doors
  > APU INLET DOOR LOWER CORNER ANGLE AT STA 1787.45 AT STR S6R HAS EVIDENCE OF CORROSION. REMOVED LOWER CORNER ANGLE CORRODED FROM APU INLET DOOR AT STA 1787.45 AT STR S6R, IAW 757-200PF SRM 51-40-02. INSTALLED NEW LOWER CORNER ANGLE I.A.W. B757-200PF SRM 51-40-0
- [SDR IPXA2026041392680](https://openairdocs.org/sdr/IPXA2026041392680.md): Angle · corroded · Mar 26, 2026 · N430UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > APU INLET DOOR UPPER ANGLE FROM STA 1787.45 TO STA 1825.00 STR S-3R HAS CORROSION. REMOVED UPPER ANGLE CORRODED FROM APU INLET DOOR, STA 1787.45 TO STA 1825.00 AT STR S3R, IAW 757-200PF SRM 51-40-02. INSTALLED NEW UPPER ANGLE I.A.W. B757-200PF SRM 51-40-02-0
- [SDR IPXA2026041392712](https://openairdocs.org/sdr/IPXA2026041392712.md): Angle · corroded · Mar 26, 2026 · N430UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > APU INLET DOOR LOWER ANGLE FROM STA 1787.45 TO STA 1825.00 STR S-6R HAS CORROSION. REMOVED LOWER ANGLE CORRODED FROM APU INLET DOOR, STA 1787.45 TO STA 1825.00 AT STR S6R, IAW 757-200PF SRM 51-40-02. INSTALLED NEW LOWER ANGLE I.A.W. B757-200PF SRM 51-40-02-0
- [SDR IPXA2026041192753](https://openairdocs.org/sdr/IPXA2026041192753.md): Strap · corroded · Mar 26, 2026 · N430UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > FAULT Z-300 STR: APU INLET DOOR FWD STRAP AT STA 1787.45 FROM STR S-3R TO STR S-6R HAS CORROSION. REMOVED EXFOLIATED FWD STRAP I.A.W. B757-200PF SRM 51-40-02-0G-0. INSTALLED NEW FWD STRAP I.A.W. B757-200PF SRM 51-40-02-0G-0.
- [SDR IPXA2026041392940](https://openairdocs.org/sdr/IPXA2026041392940.md): Angle · corroded · Mar 26, 2026 · N430UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > APU INLET DOOR UPPER CORNER ANGLE AT STA 1787.45 AT STR S3R HAS EVIDENCE OF CORROSION. REMOVED UPPER CORNER ANGLE CORRODED FROM APU INLET DOOR AT STA 1787.45 AT STR S3R, IAW 757-200PF SRM 51-40-02. INSTALLED NEW UPPER CORNER ANGLE I.A.W. B757-200PF SRM 51-40-0
- [SDR IPXA2025041625107](https://openairdocs.org/sdr/IPXA2025041625107.md): Channel · debonded · Apr 15, 2025 · N430UP · Boeing 75724APF · Emergency Equipment
  > FOUR EACH EMER DESCENT REELS ATTTACH CABLE RETAINING CHANNELS BECOMING DISBONDED FROM CEILING PANEL. *<BR>CHANNELS SECURED AND IN-TACT, DEFERRED PER EO-93451-REQ1, PARTS ORDERED FOR REPAIR.<BR><BR>DEFERED PER EO-93451-REQ1, REPAIR WITHIN 90 DAYS, ACP REPEAT
- [SDR IPXA2025031875481](https://openairdocs.org/sdr/IPXA2025031875481.md): Window · delaminated · Mar 15, 2025 · N430UP · Boeing 75724APF · Flight Compartment Windows
  > R1 WINDOW HAS WATER INTRUSION AND DELAMINATION. REMOVED AND REPLACED R1 WINDOW IAW 757 AMM 56-11-01-424-015.
- [SDR IPXA2025031775481](https://openairdocs.org/sdr/IPXA2025031775481.md): Window · delaminated · Mar 15, 2025 · N430UP · Boeing 75724APF · Flight Compartment Windows
  > R1 WINDOW HAS WATER INTRUSION AND DELAMINATION.
- [SDR IPXA2024102378232](https://openairdocs.org/sdr/IPXA2024102378232.md): Bumper · missing · Oct 22, 2024 · N430UP · Boeing 75724APF · Passenger/Crew Doors
  > CREW ENTRY DOOR DAMPER MISSING BUMPER REPLACED MISSING CREW ENTRY DOOR DAMPER BUMPER W/REF TO BOEING DRAWING PL 141N6541
- [SDR IPXA2024091333751](https://openairdocs.org/sdr/IPXA2024091333751.md): Torque Tube · faulted · Sep 11, 2024 · N430UP · Boeing 75724APF · Trailing Edge Flap Control System
  > ON APPROACH SELECTED FLAP 20 AND RECEIVED TE FLAP ASYM. EICAS PLUS TRAILING EDGE LIGHT. FLAPS ASYMETRY GREATHER THAN 5 AND LESS THAN 20. RII REMOVED AND REPLACED #3 TORQUE TUBE IAW AMM 27-51-25/201.
- [SDR IPXA2024091133751](https://openairdocs.org/sdr/IPXA2024091133751.md): Warning Light · illuminated · Sep 11, 2024 · N430UP · Boeing 75724APF · Trailing Flap Position Indicating System
  > ON APPROACH SELECTED FLAP 20 AND RECEIVED TE FLAP ASYM. EICAS PLUS TRAILING EDGE LIGHT. FLAPS ASYMETRY GREATHER THAN 5 AND LESS THAN 20.
- [SDR IPXA2024052187436](https://openairdocs.org/sdr/IPXA2024052187436.md): Frame · damaged · May 21, 2024 · N430UP · Boeing 75724APF · Fuselage Main, Frame
  > EO-83609-REQ001 (TIME LIMITED REPAIR: N430UP: FUSELAGE FRAME REPAIR AT STA 1280, BETWEEN STR 24R AND STR 28R, AMOC TO AD 2020-05-25) [T3F18E001KRM4] REQUIRES A SDR SDR. ACCOMPLISHED PERMANENT REPAIR EO-83609-REQ3TO IN ACCORDANCE WITH EA757-5360-01-B0184 IR.
- [SDR IPXA2024051724728](https://openairdocs.org/sdr/IPXA2024051724728.md): Seal · torn · May 5, 2024 · N430UP · Boeing 75724APF · Passenger/Crew Doors
  > L1 DOOR LINER SEAL TORN ON UPPER AFT CORNER ATA 52. REPAIRED L1 DOOR LINER SEAL ON UPPER AFT CORNER I.A.W. B757 AMM 52-09-00-108-024.
- [SDR IPXA2024050624728](https://openairdocs.org/sdr/IPXA2024050624728.md): Seal · torn · May 5, 2024 · N430UP · Boeing 75724APF · Passenger/Crew Doors
  > (APG) L1 DOOR LINER SEAL TORN ON UPPER AFT CORNER ATA 52
- [SDR IPXA2023080933780](https://openairdocs.org/sdr/IPXA2023080933780.md): Panel · bent · Aug 9, 2023 · N430UP · Boeing 75724APF · Nacelle/Pylon, Main Frame
  > PYLON PANEL ABOVE #2 ENGINE BENT, AND WONT CLOSE REPLACED FWD HINGE BOLT. OPS CHECK NORMAL OF DOOR PER 54-53-02
- [SDR IPXA2022122389246](https://openairdocs.org/sdr/IPXA2022122389246.md): Alternator · faulted · Dec 22, 2022 · N430UP · Boeing 75724APF · Fuel Controlling System
  > EMERGENCY DECLARED, DIVERTED, LANDED UNEVENTFUL. LEFT ENGINE FLAME OUT AFTER VNAV TRIED RESTART AT 10000 FT (UNSUCCESSFUL)R & R FUEL CONTROL IAW 73-21-01-401 R & R A STATOR EEC ALTENATOR IAW AMM 73-21-05-401 IPC 73-21-05-011015J IPC 73-21-03-045K
- [SDR IPXA2022060282736](https://openairdocs.org/sdr/IPXA2022060282736.md): Acm · inoperative · Jun 1, 2022 · N430UP · Boeing 75724APF · Cabin Cooling System
  > INSPECTION TYPE:NA***DIVERSION*** L PACK OFF AT FL 34K RAN PACK OFF CHECKLIST( BOTH PACKS OFF PER MEL 21-51-1) EMER DESCENT LAND KLCKTESTED AND OPS CK PACK TEMP CONTROLER AND FLOW CONT VALVE IAW AMM 21-51-00 AND 21-51-01 OPS CHECKED LT PACK OK IAW 21-51-00 UNA
- [SDR IPXA2022051782178](https://openairdocs.org/sdr/IPXA2022051782178.md): Repair · discovered · May 17, 2022 · N430UP · Boeing 75724APF · Fuselage Main, Structure
  > INSPECTION TYPE:SEG4 AFT CARGO COMPARTMENT HAS AN EXISTING REPAIR AT STA 1480 R/H. INBD SIDE OF S-26R. REF: B757-5310-25026-CREPAIRED PER EA# 757-5360-27-A2915
- [SDR IPXA2022051782186](https://openairdocs.org/sdr/IPXA2022051782186.md): Repair · discovered · May 17, 2022 · N430UP · Boeing 75724APF · Fuselage Main, Structure
  > INSPECTION TYPE:SEG4 AFT CARGO COMPARTMENT HAS AN EXISTING FRAME REPAIR AT STA 1280 R/H INBD SIDE OF THE S-26RREPAIRED PER EA # 757-5360-27-A2916 REV - AND EO B757-5310-83609-A
- [SDR IPXA2022051782187](https://openairdocs.org/sdr/IPXA2022051782187.md): Repair · discovered · May 17, 2022 · N430UP · Boeing 75724APF · Fuselage Main, Structure
  > INSPECTION TYPE:SEG4 AFT CARGO COMPARTMENT HAS AN EXISTING FRAME REPAIR AT STA 1360 R/H INBD SIDE OF THE S-26R.REPAIRED PER EA # 757-5360-27-A2917 AND EO B757-5310-83614-A
- [SDR IPXA2022051181992](https://openairdocs.org/sdr/IPXA2022051181992.md): Shear Plate · corroded · May 11, 2022 · N430UP · Boeing 75724APF · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:SEG4SURFACE CORROSION FOUND AT AFT DECK PLATE STA 1692, LBL 20.5REMOVED CORROSION AND CHECK LIMITS PER SRM 53-60-51-1A. IN LIMITS AFTER REWORK. NDT PERFORMED HFEC SURFACE INSPECTION AND ROTO INSPECTION ON AFFECTED AREA. NO REJECTABLE INDICATION
- [SDR IPXA2022051181991](https://openairdocs.org/sdr/IPXA2022051181991.md): Shear Plate · corroded · May 11, 2022 · N430UP · Boeing 75724APF · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:SEG4SURFACE CORROSION FOUND AT AFT DECK PLATE STA 1680, RBL 18.5REMOVED CORROSION AND CHECK LIMITS PER SRM 53-60-51-1A. IN LIMITS AFTER REWORK. NDT PERFORMED HFEC SURFACE INSPECTION AND ROTO INSPECTION ON AFFECTED AREA. NO REJECTABLE INDICATION

Next page: https://openairdocs.org/aircraft/N430UP/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 = 'N430UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N430UP/reports

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