# N432UP: 1993 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: 25463
- Year built: 1993
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 22, 2005
- Certificate issued: April 20, 2005
- Expires: February 28, 2030
- Mode S code: A52C5C
- 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=432UP
- Page: https://openairdocs.org/aircraft/N432UP

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 N432UP.

## FAA accident and incident reports

None matched to N432UP.

## Service difficulty reports (179, 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 IPXA2026042779827](https://openairdocs.org/sdr/IPXA2026042779827), Apr 25, 2026: ESCAPE ROPE. DAMAGED. FOUND CAPTAIN ESCAPE ROPE DAMAGED. REPLACED CAPTAINS ESCAPE ROPE REF AMM 25-61-00.
- [SDR IPXA2025052787473](https://openairdocs.org/sdr/IPXA2025052787473), May 26, 2025: TEE ANGLE. CORRODED. FS 1037 RBL 45 T CHORD HAS CORROSION INSTALLED T-CHORD AT STA 1037 RBL 45 IAW B757-200PF, SRM 51-40-02-0G-0.
- [SDR IPXA2025060364625](https://openairdocs.org/sdr/IPXA2025060364625), May 24, 2025: TEE ANGLE. CORRODED. T-CHORD 1060 LBL 15 WITH EVIDENCE OF CORROSION NO DOT NSTALLED T-CHORD AT STA 1060 LBL 15 IAW B757-200PF, SRM 51-40-02-0G-0.
- [SDR IPXA2025060328098](https://openairdocs.org/sdr/IPXA2025060328098), May 11, 2025: DOUBLER. CORRODED. RH AIR CONDITIONING PACK EXHAUST FRAME SUPPORT CORRODED. DOT 28-50 INSTALLED FRAME SUPPORT AT RH AIR CONDITIONING PACK EXHAUST IAW B757-200PF, SRM 51-40-02-0G-0
- [SDR IPXA2025060384921](https://openairdocs.org/sdr/IPXA2025060384921), May 8, 2025: TEE ANGLE. CORRODED. RIGHT W/W OUTBD T-CHORD AT STA 1045, SUPPORT FOR A/C EXHAUST ASSY, HAS INTERGRAINLUER CORROSION. DOT 8-006. INSTALLED T-CHORD AT OUTBD STA 1045, SUPPORT FOR A/C
- [SDR IPXA2025060385010](https://openairdocs.org/sdr/IPXA2025060385010), May 8, 2025: TEE ANGLE. CORRODED. RIGHT W/W INBD T-CHORD AT STA 1045, SUPPORT FOR THE A/C EXHAUST ASSY, HAS CORROSION. DOT 8-009. INSTALLED T-CHORD AT INBD STA 1045, SUPPORT FOR A/C EXHAUST ASSY
- [SDR IPXA2025060384983](https://openairdocs.org/sdr/IPXA2025060384983), May 8, 2025: TEE ANGLE. CORRODED. RIGHT W/W FWD T-CHORD AT STA 1045, SUPPORT FOR THE A/C EXHAUST ASSY, HAS CORROSION. DOT 8-008. INSTALLED T-CHORD AT FWD STA 1045 RH, SUPPORT FOR A/C EXHAUST ASS
- [SDR IPXA2024020727940](https://openairdocs.org/sdr/IPXA2024020727940), Feb 6, 2024: FAN. FAILED. *SUPPLEMENTAL SDR* *AIR TURN BACK* EQUIPMENT OVHT EICAS AND ANNUCIATOR RECEIVED AFTER T/O. THE CHECK LIST DID NOT FIX THE OVHT. RESULTED IN AIR TURNBACK. REMOVE
- [SDR IPXA2024020627940](https://openairdocs.org/sdr/IPXA2024020627940), Feb 6, 2024: WARNING MESSAGE. ILLUMINATED. *SDR FILED OPEN* *AIR TURN BACK* EQUIPMENT OVHT EICAS AND ANNUCIATOR RECEIVED AFTER T/O. THE CHECK LIST DID NOT FIX THE OVHT. RESULTED IN AIR TURNBACK
- [SDR IPXA2023120607477](https://openairdocs.org/sdr/IPXA2023120607477), Nov 29, 2023: FLAP. WARNING MESSAGE. TE FLAP DISAGREE ON FLAP RETRACTION FROM 5 TO 1. USED ALTERNATE SYSTEM, EICAS MESSAGE ERASED. WITH ALT SYSTEM C/W FIM 27-51-808 FIG 105 SH 4.NO OVERLOAD INDICAT
- [SDR IPXA2023112907477](https://openairdocs.org/sdr/IPXA2023112907477), Nov 29, 2023: UNKNOWN. UNKNOWN. *SDR FILED OPEN* *DIVERSION* TE FLAP DISAGREE ON FLAP RETRACTION FROM 5 TO 1. USED ALTERNATE SYSTEM, EICAS MESSAGE ERASED. WITH ALT SYSTEM FIM 27-51 FAULT TREE 
- [SDR IPXA2023051693253](https://openairdocs.org/sdr/IPXA2023051693253), Apr 26, 2023: FRAME. CORRODED. INSPECTION TYPE:SEG4AFT CARGO DOOR STA 1436 LOWERE INTERIOR ANGLE HAS CORROSIONREMOVED DAMAGED FRAME WEB. INSTALLED NEW FRAME WEB IAW BOEING DWG 146N6603 AND SR
- [SDR IPXA2023051393216](https://openairdocs.org/sdr/IPXA2023051393216), Apr 25, 2023: SKIN PANEL. DELAMINATED. INSPECTION TYPE:SEG4*MAJOR REPAIR* LARGE DENT ON TOP OF TAIL CONE. AFT RUDDER, APPROX. BETWEEN S1L AND S2LREPAIRED PANEL IAW B757 SRM 51-70-10-2R REPAIR PER EA 
- [SDR IPXA2023051193189](https://openairdocs.org/sdr/IPXA2023051193189), Apr 25, 2023: SEAT TRACK. CORRODED. INSPECTION TYPE:SEG4MAIN CARGO COMP. STA 1100, LBL 65.5 HAS CORROSION. REMOVED DAMAGE. FOUND TO BE OUT OF LIMITS PER SRM 53-00-52-1A-1REMOVED DAMAGED SEAT TRACK
- [SDR IPXA2023022091140](https://openairdocs.org/sdr/IPXA2023022091140), Feb 19, 2023: BUSS. NONE. DIVERSION & EMERGENCY DECLARED. L AC BUSS OFF LIGHT IN FLIGHT. FOLLOWED PROCEEDURE IN QRH. RESETTING GEN CONT SWITCH HAD NO EFFECT. UPON STARTING APU AND RUNNIN
- [SDR IPXA2023020290543](https://openairdocs.org/sdr/IPXA2023020290543), Feb 1, 2023: BUSS. INOPERATIVE. INSPECTION TYPE:NA*EMERGENCY DECLARED* *LANDED WITH NO FURTHER PROBLEMS* L AC BUSS OFF - RAN QRH PROCEDURE RETURNED A/C TO NORMAL STATUS LEFT BUS TIE REMAINED I
- [SDR IPXA2021071071495](https://openairdocs.org/sdr/IPXA2021071071495), Jul 10, 2021: PANEL. DELAMINATED. INSPECTION TYPE:SEG3RIH I/B LOWER HORIZONTAL STAB JUST AFT OF THE AUX SPAR HAS A DENT/ DELAMINATIONREPAIRED PANEL IAW B757 SRM 51-70-10, PROCEDURE 4, 250 DEG F 
- [SDR IPXA2021070971485](https://openairdocs.org/sdr/IPXA2021070971485), Jul 9, 2021: TEE FITTING. CORRODED. INSPECTION TYPE:SEG3RH AFT WTB FAIRING STRUCTURE TEE CHORD AT STA 1180, RBL 36 HAS EXFOLIDATED CORROSIONREMOVED AND REPLACED TEE CHORD IAW ARM 51-40-02-0G
- [SDR IPXA2021070771386](https://openairdocs.org/sdr/IPXA2021070771386), Jul 7, 2021: FLOOR PANEL. DAMAGED. INSPECTION TYPE:SEG3MAIN CARGO COMPARTMENT, FLOOR PANEL 232XCF IS DAMAGEDFABBED PANEL 232XCF FROM 5024N400001SS-G BATCH# 3605496 PER SREO B757-5320-9692-K
- [SDR IPXA2021070771381](https://openairdocs.org/sdr/IPXA2021070771381), Jul 7, 2021: FLOOR PANEL. DAMAGED. INSPECTION TYPE:SEG3MAIN CARGO COMPARTMENT, FLOOR PANEL 232XJF IS DAMAGEDFABBED PANEL 232XJF FROM 5024N400001SS-G BATCH# 3605469 PER SREO B757-5320-9692-K
- [SDR IPXA2021070271223](https://openairdocs.org/sdr/IPXA2021070271223), Jul 2, 2021: SEAT TRACK. WORN. INSPECTION TYPE:SEG3SEAT TRACK AT STA 787 RBL 24.5 HAS WEAR DAMAGE BEYOND ALLOWABLE LIMITS AND REQUIRES REPAIRREMOVED AND REPLACED SEAT TRACK AT STA 787 RBL 24.
- [SDR IPXA2021070271218](https://openairdocs.org/sdr/IPXA2021070271218), Jul 2, 2021: FLOOR PANEL. DAMAGED. INSPECTION TYPE:SEG3MAIN CARGO COMPARTMENT, FLOOR PANEL 211XAF IS WORNFABBED PANEL 211XAF FROM 5024N400001SS-G, BATCH# 3605469 PER SREO B757-5320-9692-K
- [SDR IPXA2021070171198](https://openairdocs.org/sdr/IPXA2021070171198), Jul 1, 2021: DOOR. DELAMINATED. INSPECTION TYPE:SEG3DRY BAY DOOR 632FZ HAS EDGE DAMAGE DOT 6833-14REPAIRED PANEL IAW B757 SRM 51-70-07-0G 250 DEG F CURE PER SRM 57-20-09-2R, TABLE I.
- [SDR IPXA2020041754308](https://openairdocs.org/sdr/IPXA2020041754308), Apr 15, 2020: BUTTON. STUCK. INSPECTION TYPE:N/A**DIVERSION** LANDED W/O INCIDENT **JUST AFTER REACHING CRUISE ALT L ENG OVHT EICAS MSG WITH MASTER CAUTION AND ASOC LIGHT ON CTR CONSOLE ILL
- [SDR IPXA2019103098453](https://openairdocs.org/sdr/IPXA2019103098453), Oct 29, 2019: RELAY. MALFUNCTIONED. INSPECTION TYPE:N/A** EMERGENCY DECLARED ** ON APPROACH WENT TO FLAPS 30 RECIEVED TRAILING EDGE FLAP DISAGREEPERFORMED BITE OF FSEU 1, 2, AND 3 IAW AMM 27-51-01
- [SDR IPXA2019071044277](https://openairdocs.org/sdr/IPXA2019071044277), Jun 21, 2019: SKIN. DENTED. INSPECTION TYPE:SEG3 LT HORIZONTAL STABILIZER HAS DENT AT UPPER INBOARD EXTERNAL SKIN BETWEEN LEADING EDGE(AUX-SPAR) AND FRONT SPAR NEAR INBOARD LOGO LIGHT. REP
- [SDR IPXA2019061974371](https://openairdocs.org/sdr/IPXA2019061974371), Jun 15, 2019: HANDLE. LOOSE. L1 DOOR INNER HANDLE MOUNTING HARDWARE LOOSESECURED HANDLE MOUNTING HARDWARE IN REF AMM 20-11-00-201
- [SDR IPXA2019010737593](https://openairdocs.org/sdr/IPXA2019010737593), Jan 4, 2019: WARNING SYSTEM. FALSE ACTIVATION. INSPECTION TYPE:N/A EICAS MSG L FWD ENT DOOR APPEARED ON TOUCH DOWN. PER MEL 52-71-1 CREW ENTRY DOOR INDICATION DEFERRED. PLACARD INSTALLED. DMP WILL BE ON LOGP
- [SDR IPXA2017103123128](https://openairdocs.org/sdr/IPXA2017103123128), Oct 31, 2017: SIGN. INOPERATIVE. EMERGENCY EXIT SIGN OVER CREW ENTRY DOOR REMARKED FOR MA. REINSTALLED SAME EMERGENCY EXIT SIGN OVER CREW ENTRY DOOR PER AMM 33-51-01-402-003 & OPS CHECKS NORMAL
- [SDR IPXA2017080920323](https://openairdocs.org/sdr/IPXA2017080920323), Aug 7, 2017: INDICATION SYS. MALFUNCTIONED. TE FLAP DISAGREE ON FLAPS 1 SELECTION. FLAP INDICATOR BETWEEN 0 AND 1. REF SPEED 165 UPON LANDING. EMERGENCY DECLARED, PERFORMED A BITE AND T/E FLAP SYSTEM OPER
- [SDR IPXA2016041402130](https://openairdocs.org/sdr/IPXA2016041402130), Apr 12, 2016: LEVER. MALFUNCTIONED. EMERGENCY DECLARED, T/E DISAGREE CAUTION MESSAGE DISPLAYED WHEN SELECTING FLAPS 1. RAN T/E FLAP DISAGREE CHECKLIST AND LANDED WITH FLAPS 20. ALTERNATE FLAP EXTE
- [SDR IPXA2016041102003](https://openairdocs.org/sdr/IPXA2016041102003), Apr 11, 2016: WIRE. BROKEN. EMERGENCY LIGHT GUARDED SWITCH ARMING DEVICE BROKEN. R & R EMERGENCY LIGHTS SWITCH GUARD. OK TO CONTINUE.
- [SDR IPXA2015081592369](https://openairdocs.org/sdr/IPXA2015081592369), Jul 31, 2015: FRAME. DENTED. INSPECTION TYPE:C, FWD CARGO FRAME AT SLOPING AREA RT BS 680 INNER CHORD HAS DENT REPAIRED DAMAGE IAW SRM 53-00-07-2R, REPAIR 5, TABLE 3.
- [SDR IPXA2015081392319](https://openairdocs.org/sdr/IPXA2015081392319), Jul 30, 2015: PANEL. CORRODED. INSPECTION TYPE :C, AFT CARGO BS 1200-1310, RT SIDE PANEL CORRODED. R & R AFT CARGO SIDE PANEL IAW SRM 51-40-02-0G.
- [SDR IPXA2015081192256](https://openairdocs.org/sdr/IPXA2015081192256), Jul 30, 2015: INTERCOSTAL. CORRODED. INSPECTION TYPE:C, AFT CARGO, BS 1400-1420, LBL 2.9 INTERCOSTAL CORRODED. R & R INTERCOASTAL, PN:146N5425U19 WITH BACR15FV6, BATCH 0001771118, BACR15FT6, BATCH 
- [SDR IPXA2015080792126](https://openairdocs.org/sdr/IPXA2015080792126), Jul 29, 2015: FLOOR PANEL. DELAMINATED. INSPECTION TYPE: C, MAIN DECK FLOOR PANEL 231XJFS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SR EO B757-5320-9692H.
- [SDR IPXA2015080792125](https://openairdocs.org/sdr/IPXA2015080792125), Jul 29, 2015: FLOOR PANEL. DELAMINATED. INSPECTION TYPE: C, MAIN DECK FLOOR PANEL 231XFF IS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SR EO B757-5320-9692H.
- [SDR IPXA2015081192271](https://openairdocs.org/sdr/IPXA2015081192271), Jul 28, 2015: FLOOR PANEL. CORRODED. INSPECTION TYPE:C, FWD CARGO FLOOR PANEL 121BF HAS CHAFE MARKS/CORROSION ALSO INCLUDING UNDER AND AROUND THE MBA SYSTEM. BLENDED CHAFE MARKS AND CORROSION ON FW
- [SDR IPXA2015080792127](https://openairdocs.org/sdr/IPXA2015080792127), Jul 27, 2015: FLOOR PANEL. DAMAGED. INSPECTION TYPE: C, ELECTRICAL EQUIPMENT CENTER FLOOR PANEL 119AF HAS TORN FASTENER HOLES. FABRICATED A NEW FLOOR PANEL.
- [SDR IPXA2015081892490](https://openairdocs.org/sdr/IPXA2015081892490), Jul 26, 2015: CASTING. CORRODED. INSPECTION TYPE:C, CORROSION ON LT ELEVATOR LOWER OTBD SKIN SURFACE AT TIP CAP. REMOVED DAMAGED TIP CASTING IAW SRM 51-40-02-0G, FABRICATED SPLICE PLATES IAW DW
- [SDR IPXA2015081892489](https://openairdocs.org/sdr/IPXA2015081892489), Jul 26, 2015: CASTING. CORRODED. INSPECTION TYPE:C, CORROSION ON RT ELEVATOR LOWER OTBD SKIN SURFACE AT TIP CAP. REMOVED DAMAGED TIP CASTING IAW SRM 51-40-02-0G FABRICATED SPLICE PLATES IAW DWG
- [SDR IPXA2014051982990](https://openairdocs.org/sdr/IPXA2014051982990), May 16, 2014: LAMP. INOPERATIVE. EMERGENCY EXIT LIGHT DOES NOT ILLUMINATE WITH SWITCH OFF. REPLACED LAMP IAW AMM 33-13-00. OPS CHECKED GOOD.
- [SDR IPXA3580297](https://openairdocs.org/sdr/IPXA3580297), Sep 18, 2013: BATTERY. INOPERATIVE. EMERGENCY EXIT LIGHT OVER DOOR WAY WILL NOT TEST. REPLACED EXIT LIGHT BATTERY IAW 33-51-07-902-001 & 33-51-01-402-003. TEST NORMAL. IPC REF 33-57-11-01-045. PN 
- [SDR IPXA13579684](https://openairdocs.org/sdr/IPXA13579684), Aug 6, 2013: FLOOR PANEL. DAMAGED. INSPECTION TYPE: C1S3, MAIN DECK FLOOR PANEL 221XCF HAS EDGE DAMAGE. FABRICATED NEW FLOOR PANEL IAW EO B757-5320-9692-H.
- [SDR IPXA13579683](https://openairdocs.org/sdr/IPXA13579683), Jul 30, 2013: SKIN. DAMAGED. INSPECTION TYPE: C1S3, LT INBD MAIN FLAP UPPER SKIN DAMAGED AT APPROX 44.75 FROM INBD END. REPAIRED IAW RCD 012190.
- [SDR IPXA13579661](https://openairdocs.org/sdr/IPXA13579661), Jul 27, 2013: FLOORBOARD. DAMAGED. INSPECTION TYPE: C1S3, MAIN DECK FLOORBOARD 232XTF AFT EDGE HAD DAMAGE. FABRICATED NEW FLOORBOARD IAW EO B757-5320-9692-H.
- [SDR IPXA13579651](https://openairdocs.org/sdr/IPXA13579651), Jul 27, 2013: FLOORBOARD. PUNCTURED. INSPECTION TYPE: C1S3, MAIN DECK FLOORBOARD 231XSF HAS NUMEROUS PUNCTURES. FABRICATED NEW FLOORBOARD IAW EO B757-5320-9692-H .
- [SDR IPXA13579659](https://openairdocs.org/sdr/IPXA13579659), Jul 26, 2013: FLOORBOARD. PUNCTURED. INSPECTION TYPE: C1S3, FLOORBOARD 231XNF IS PUNCTURED AT BOTTON SURFACE. FABRICATED NEW FLOORBOARD IAW EO B757-5320-9692-H.
- [SDR IPXA13579656](https://openairdocs.org/sdr/IPXA13579656), Jul 26, 2013: FLOORBOARD. PUNCTURED. INSPECTION TYPE: C1S3, FLOORBOARD 232XQF HAS PUNCTURES AT BOTTOM SURFACE. FABRICATED NEW FLOORBOARD IAW EO B757-5320-9693-H.
- [SDR IPXA13579654](https://openairdocs.org/sdr/IPXA13579654), Jul 26, 2013: FLOORBOARD. PUNCTURED. INSPECTION TYPE: C1S3, CABIN FLOORBOARD 232XMF BOTTOM SURFACE HAD MULTIPLE PUNCTURES. FABRICATED NEW FLOORBOARD IAW EO B757-5320-9692-H.

All 179: https://openairdocs.org/aircraft/N432UP/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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