# N430UP: 1992 Boeing 757-24APF

- Status: Valid registration
- Airframe: [Boeing 757-24APF](https://openairdocs.org/model/boeing-757-24apf) (registry code 1384969, 178 seats)
- Engine: [Pratt & Whitney PW2040](https://openairdocs.org/engine/pratt-whitney-pw2040) (registry code 52121)
- Data sheets: [TCDS E17NE](https://openairdocs.org/tcds/E17NE) (Pratt & Whitney) (OpenAirDocs)
- Serial number: 25461
- Year built: 1992
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 22, 1992
- Certificate issued: November 20, 1992
- Expires: November 30, 2028
- Mode S code: A524EE
- Registered owner: [United Parcel Service Co](https://openairdocs.org/faa-owner/UNITED%20PARCEL%20SERVICE%20CO)
- Location: [Louisville, KY](https://openairdocs.org/faa-place/KY/Louisville)
- Owner type: Corporation
- Owner's area on the map: 38.2585° N, 85.5398° W: Placed by OpenAirDocs at the center of ZIP code 40223, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=430UP
- Page: https://openairdocs.org/aircraft/N430UP

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 15 in force

### Matched by airframe (Boeing 757-24APF)

None in force.

### Matched by engine (Pratt & Whitney PW2040)

- [AD 2026-07-06](https://openairdocs.org/ad/2026-07-06): Turbine Section · Pratt & Whitney F117-PW-100, PW2037, PW2037D and 3 more. Effective May 29, 2026
- [AD 2024-12-04](https://openairdocs.org/ad/2024-12-04): Turbine Section · Pratt & Whitney PW2037, PW2037M and PW2040. Effective Aug 13, 2024
- [AD 2021-14-13](https://openairdocs.org/ad/2021-14-13): Turbine Section · Pratt & Whitney F117-PW-100, PW2037, PW2037M and 1 more. Effective Sep 1, 2021
- [AD 2019-05-01](https://openairdocs.org/ad/2019-05-01): Turbine/Turboprop Engine · Pratt & Whitney F117-PW-100, PW2037, PW2037D and 6 more. Effective Apr 16, 2019
- [AD 2018-22-06](https://openairdocs.org/ad/2018-22-06): Fuel Control/Turbine Engines · Pratt & Whitney PW2037, PW2037M and PW2040. Effective Dec 3, 2018
- [AD 2018-14-10](https://openairdocs.org/ad/2018-14-10): Fuel Control Turbine Engines · Pratt & Whitney PW2037, PW2037M and PW2040. Effective Sep 28, 2018
- [AD 2012-02-01](https://openairdocs.org/ad/2012-02-01): Fan blades · Pratt & Whitney Division PW2037, PW2037M and PW2040. Effective Apr 24, 2012
- [AD 2009-14-05](https://openairdocs.org/ad/2009-14-05): High-pressure compressor (HPC) · Pratt & Whitney Division PW2037, PW2037M and PW2040. Effective Jul 23, 2009
- [AD 2009-10-08](https://openairdocs.org/ad/2009-10-08): High-pressure turbine 2nd stage hubs that have previously been exposed to Pratt & Whitney cleaning procedure SPOP 10 or SPOP 9 or equivalent procedure. · Pratt & Whitney Division PW2037, PW2037M and PW2040. Effective Jun 17, 2009
- [AD 2007-02-06](https://openairdocs.org/ad/2007-02-06): High pressure compressor (HPC) drum rotor disk assemblies · Pratt & Whitney Division PW2037, PW2037M and PW2040. Effective Feb 28, 2007
- [AD 2005-18-03](https://openairdocs.org/ad/2005-18-03): Engine manufacturer's time limits section (TLS) · Pratt & Whitney Division PW2037, PW2037D, PW2037M and 5 more. Effective Feb 28, 2006
- [AD 99-20-03](https://openairdocs.org/ad/99-20-03): High Pressure Turbine Disks · Pratt & Whitney Division PW2037, PW2037M, PW2040 and 2 more. Effective Nov 23, 1999
- [AD 96-18-08 R1](https://openairdocs.org/ad/96-18-08-R1): (HPT) High Pressure or (LPT) Low Pressure Turbine · Pratt & Whitney Division PW2037, PW2037M, PW2040 and 2 more. Effective Nov 10, 1998
- [AD 97-11-51 R1](https://openairdocs.org/ad/97-11-51-R1): First Stage High Pressure Turbine (HPT) Disk Assembly · Pratt & Whitney Division PW2037, PW2037M, PW2040 and 5 more. Effective Aug 7, 1997
- [AD 88-03-52](https://openairdocs.org/ad/88-03-52): Fuel Quantity Indication System · Pratt & Whitney Division PW2037 and PW2040. Effective Jul 13, 1988

### Historical (superseded or no longer in force)

- [AD 2017-12-03](https://openairdocs.org/ad/2017-12-03) (historical): Fuel Control Turbine Engines · Pratt & Whitney PW2037, PW2037M and PW2040. Effective Jul 20, 2017
- [AD 2017-11-06](https://openairdocs.org/ad/2017-11-06) (historical): Turbine/ Turboprop Engine · Pratt & Whitney F117-PW-100, PW2037, PW2037D and 6 more. Effective Jul 18, 2017
- [AD 2014-05-32](https://openairdocs.org/ad/2014-05-32) (historical): Diffuser-to-high-pressure turbine (HPT) case flange · Pratt & Whitney F117-PW-100, PW2037, PW2037D and 8 more. Effective May 5, 2014
- [AD 2002-12-06](https://openairdocs.org/ad/2002-12-06) (historical): Time Limits Section (TLS) · Pratt & Whitney Division PW2037, PW2037M, PW2040 and 5 more. Effective Jul 17, 2002
- [AD 2000-21-09](https://openairdocs.org/ad/2000-21-09) (historical): Critical Life-limited Parts · Pratt & Whitney Division PW2037, PW2037M, PW2040 and 5 more. Effective Jan 22, 2001
- [AD 99-08-14](https://openairdocs.org/ad/99-08-14) (historical): Maintenance Program, Mandatory Inspections · Pratt & Whitney Division PW2037, PW2037M, PW2040 and 5 more. Effective May 13, 1999

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N430UP.

## FAA accident and incident reports

None matched to N430UP.

## Service difficulty reports (270, newest 50)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR IPXA2026040487396](https://openairdocs.org/sdr/IPXA2026040487396), Apr 1, 2026: SUPPORT BRACKET. CORRODED. 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
- [SDR IPXA2026041587231](https://openairdocs.org/sdr/IPXA2026041587231), Apr 1, 2026: ANGLE. CORRODED. 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. REVI
- [SDR IPXA2026041367944](https://openairdocs.org/sdr/IPXA2026041367944), Mar 31, 2026: HOLDER. CRACKED. 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), Mar 31, 2026: TEE FITTING. CORRODED. 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), Mar 31, 2026: INTERCOSTAL. CORRODED. 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), Mar 31, 2026: ANGLE. CRACKED. 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-
- [SDR IPXA2026041365276](https://openairdocs.org/sdr/IPXA2026041365276), Mar 31, 2026: WEB. CORRODED. 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.
- [SDR IPXA2026041365017](https://openairdocs.org/sdr/IPXA2026041365017), Mar 31, 2026: FLOOR SUPPORT. CORRODED. 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 
- [SDR IPXA2026040965063](https://openairdocs.org/sdr/IPXA2026040965063), Mar 31, 2026: INTERCOSTAL. CORRODED. 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 S
- [SDR IPXA2026041150506](https://openairdocs.org/sdr/IPXA2026041150506), Mar 30, 2026: TEE FITTING. CORRODED. 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), Mar 29, 2026: BRACKET. CRACKED. 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 
- [SDR IPXA2026041136020](https://openairdocs.org/sdr/IPXA2026041136020), Mar 29, 2026: SKIN. PUNCTURED. 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 PREPARE
- [SDR IPXA2026041135878](https://openairdocs.org/sdr/IPXA2026041135878), Mar 29, 2026: ANGLE. CORRODED. 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 
- [SDR IPXA2026040835942](https://openairdocs.org/sdr/IPXA2026040835942), Mar 29, 2026: SPLICE PLATE. CORRODED. 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.
- [SDR IPXA2026040426186](https://openairdocs.org/sdr/IPXA2026040426186), Mar 28, 2026: COVER. CRACKED. 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), Mar 28, 2026: BRACKET. CORRODED. 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), Mar 28, 2026: SUPPORT. CORRODED. 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), Mar 27, 2026: TEE ANGLE. CORRODED. 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), Mar 27, 2026: TEE ANGLE. CORRODED. 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
- [SDR IPXA2026041610845](https://openairdocs.org/sdr/IPXA2026041610845), Mar 27, 2026: TEE FITTING. CORRODED. 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 - 
- [SDR IPXA2026041611851](https://openairdocs.org/sdr/IPXA2026041611851), Mar 27, 2026: INTERCOSTAL. CORRODED. 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), Mar 27, 2026: BRACKET. CORRODED. 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 51-4
- [SDR IPXA2026041311405](https://openairdocs.org/sdr/IPXA2026041311405), Mar 27, 2026: TEE FITTING. CORRODED. 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. I
- [SDR IPXA2026041611830](https://openairdocs.org/sdr/IPXA2026041611830), Mar 27, 2026: TEE FITTING. CORRODED. 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 DATA
- [SDR IPXA2026040911691](https://openairdocs.org/sdr/IPXA2026040911691), Mar 27, 2026: INTERCOSTAL. CORRODED. 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), Mar 27, 2026: TEE FITTING. CORRODED. 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), Mar 27, 2026: TEE FITTING. CORRODED. 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), Mar 26, 2026: STRAP. CORRODED. 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 EV
- [SDR IPXA2026041393076](https://openairdocs.org/sdr/IPXA2026041393076), Mar 26, 2026: ANGLE. CORRODED. 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
- [SDR IPXA2026041392680](https://openairdocs.org/sdr/IPXA2026041392680), Mar 26, 2026: ANGLE. CORRODED. 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 
- [SDR IPXA2026041392712](https://openairdocs.org/sdr/IPXA2026041392712), Mar 26, 2026: ANGLE. CORRODED. 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 
- [SDR IPXA2026041192753](https://openairdocs.org/sdr/IPXA2026041192753), Mar 26, 2026: STRAP. CORRODED. 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
- [SDR IPXA2026041392940](https://openairdocs.org/sdr/IPXA2026041392940), Mar 26, 2026: ANGLE. CORRODED. 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
- [SDR IPXA2025041625107](https://openairdocs.org/sdr/IPXA2025041625107), Apr 15, 2025: CHANNEL. DEBONDED. FOUR EACH EMER DESCENT REELS ATTTACH CABLE RETAINING CHANNELS BECOMING DISBONDED FROM CEILING PANEL. *<BR>CHANNELS SECURED AND IN-TACT, DEFERRED PER EO-93451-RE
- [SDR IPXA2025031875481](https://openairdocs.org/sdr/IPXA2025031875481), Mar 15, 2025: WINDOW. DELAMINATED. 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), Mar 15, 2025: WINDOW. DELAMINATED. R1 WINDOW HAS WATER INTRUSION AND DELAMINATION.
- [SDR IPXA2024102378232](https://openairdocs.org/sdr/IPXA2024102378232), Oct 22, 2024: BUMPER. MISSING. 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), Sep 11, 2024: TORQUE TUBE. FAULTED. 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 REPLACE
- [SDR IPXA2024091133751](https://openairdocs.org/sdr/IPXA2024091133751), Sep 11, 2024: WARNING LIGHT. ILLUMINATED. 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), May 21, 2024: FRAME. DAMAGED. 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 IPXA2024051724728](https://openairdocs.org/sdr/IPXA2024051724728), May 5, 2024: SEAL. TORN. 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), May 5, 2024: SEAL. TORN. (APG) L1 DOOR LINER SEAL TORN ON UPPER AFT CORNER ATA 52
- [SDR IPXA2023080933780](https://openairdocs.org/sdr/IPXA2023080933780), Aug 9, 2023: PANEL. BENT. 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), Dec 22, 2022: ALTERNATOR. FAULTED. 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 
- [SDR IPXA2022060282736](https://openairdocs.org/sdr/IPXA2022060282736), Jun 1, 2022: ACM. INOPERATIVE. 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
- [SDR IPXA2022051782178](https://openairdocs.org/sdr/IPXA2022051782178), May 17, 2022: REPAIR. DISCOVERED. 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), May 17, 2022: REPAIR. DISCOVERED. 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 B
- [SDR IPXA2022051782187](https://openairdocs.org/sdr/IPXA2022051782187), May 17, 2022: REPAIR. DISCOVERED. 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 B757-5
- [SDR IPXA2022051181992](https://openairdocs.org/sdr/IPXA2022051181992), May 11, 2022: SHEAR PLATE. CORRODED. 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. 
- [SDR IPXA2022051181991](https://openairdocs.org/sdr/IPXA2022051181991), May 11, 2022: SHEAR PLATE. CORRODED. 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. 

All 270: https://openairdocs.org/aircraft/N430UP/reports.md

## STCs that may be installed (OpenAirDocs)

None matched to this aircraft's models.

## Related

- Other Boeing 757-24APF aircraft: https://openairdocs.org/model/boeing-757-24apf/aircraft.md
- The Pratt & Whitney PW2040 engine: https://openairdocs.org/engine/pratt-whitney-pw2040.md

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