# N412UP: 1988 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: 23852
- Year built: 1988
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 30, 1988
- Certificate issued: October 13, 1988
- Expires: August 31, 2028
- Mode S code: A4DD5E
- 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=412UP
- Page: https://openairdocs.org/aircraft/N412UP

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 N412UP.

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20010105002739I](https://openairdocs.org/incident/20010105002739I), Jan 5, 2001: Boeing 75724APF (N412UP), Newburgh, NY. (-23) Flight 132 departed phl in route to buf, as the aircraft was climbingout of the trailing edge flap asymmetrical warning illuminated. The crew then…

## Service difficulty reports (248, 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 IPXA2026092882672](https://openairdocs.org/sdr/IPXA2026092882672), Sep 23, 2026: EVAS UNIT. DISLODGED. CAPTAIN (LEFT) SIDE EVAS CONTAINER LID DISLODGED AND EVAS EXPOSED. INSTALLED CAPTAIN (LEFT) SIDE EVAS PER AMM 25-60-00.
- [SDR IPXA2026092382672](https://openairdocs.org/sdr/IPXA2026092382672), Sep 23, 2026: EVAS UNIT. DISLODGED. CAPTAIN (LEFT) SIDE EVAS CONTAINER LID DISLODGED AND EVAS EXPOSED, DEFERRAL REMAINS
- [SDR IPXA2026060280694](https://openairdocs.org/sdr/IPXA2026060280694), May 20, 2026: SKIN. DAMAGED. AFTER REMOVAL OF DME ANTENNA, FOUND SIGNS OF CORROSION. CHECKED LIMITS AT FUSELAGE SKIN AREA ORIGINAL THICKNESS .080 IAW DWG# 143N3471 BLENDED DIMENSIONS L=5.50
- [SDR IPXA2026052180694](https://openairdocs.org/sdr/IPXA2026052180694), May 20, 2026: SKIN. CORRODED. AFTER REMOVAL OF DME ANTENNA,, FOUND SIGNS OF CORROSION.
- [SDR IPXA2026053022584](https://openairdocs.org/sdr/IPXA2026053022584), May 16, 2026: ATTACH FITTING. CORRODED. UPON REMOVAL OF UPPER AND LOWER SPLICE PLATE AT LH ELEVATOR T/E, TIP AREA, FOUND TRAILING EDGE TIP FAIRING ASSEMBLY WITH EVIDENCE OF CORROSION, INSTALLED ELEVAT
- [SDR IPXA2026052622502](https://openairdocs.org/sdr/IPXA2026052622502), May 16, 2026: FRAME. CORRODED. UPON REMOVAL OF UPPER SPLICE PLATE AT LH ELEVATOR T/E, TIP AREA, FOUND UPPER CONDUCTIVE FRAME CORRODED. INSTALLED NEW UPPER CONDUCTIVE FRAME P/N:183N2007Y8 BATC
- [SDR IPXA2026052622562](https://openairdocs.org/sdr/IPXA2026052622562), May 16, 2026: FRAME. CORRODED. UPON REMOVAL OF LOWER SPLICE PLATE AT LH ELEVATOR T/E, TIP AREA, FOUND LOWER CONDUCTIVE FRAME CORRODED, INSTALLED NEW LOWER CONDUCTIVE FRAME IAW SRM 51-40-02-0G
- [SDR IPXA2026060328065](https://openairdocs.org/sdr/IPXA2026060328065), May 11, 2026: SUPPORT ANGLE. DAMAGED. AFT CARGO COMPARTMENT AFT BULKHEAD ACCESS PANEL UPPER SUPPORT ANGLE HAS CORROSION AND 2 EA ELONGATED HOLE APPROX AT BS 1640 BTW RBL 50 AND LBL 50, INSTALLED UPP
- [SDR IPXA2026060226363](https://openairdocs.org/sdr/IPXA2026060226363), May 11, 2026: SKIN. CRACKED. NR 2 PYLON UPPER SKIN 12 HOLE HAS CRACK AT 12 O'CLOCK POSITION AT LOWER LAYER. ACCOMPLISHED REPAIR PER EO-97524-REQ1 AND VT-SAA EA 757-5700-01-B0750, REV I/R.
- [SDR IPXA2026052629850](https://openairdocs.org/sdr/IPXA2026052629850), May 11, 2026: STRAP. CORRODED. UPON REMOVAL OF CEILING DECOMPRESSION PANEL FOUND STABILIZATION STRAP CORRODED, APPROX BTW BS 1560 AND BS 1580, LBL 45.50, INSTALLED FABRICATED STABILIZATION ST
- [SDR IPXA2026052629952](https://openairdocs.org/sdr/IPXA2026052629952), May 11, 2026: STRAP. CORRODED. UPON REMOVAL OF CEILING DECOMPRESSION PANEL FOUND STABILIZATION STRAP CORRODED, APPROX BTW BS 1400 AND BS 1420, RBL 24.75, INSTALLED 01EA STABILIZATION STRAP CE
- [SDR IPXA2026052629852](https://openairdocs.org/sdr/IPXA2026052629852), May 11, 2026: STRAP. CORRODED. UPON REMOVAL OF CEILING DECOMPRESSION PANEL FOUND STABILIZATION STRAP CORRODED, APPROX BTW BS 1560 AND BS 1580, LBL 24.75, INSTALLED FABRICATED STABILIZATION ST
- [SDR IPXA2026052629933](https://openairdocs.org/sdr/IPXA2026052629933), May 11, 2026: STRAP. CORRODED. UPON REMOVAL OF CEILING DECOMPRESSION PANEL FOUND STABILIZATION STRAP CORRODED, APPROX BTW BS 1400 AND BS 1420, RBL 45.50, INSTALLED 01EA SECTION OF STABILIZATI
- [SDR IPXA2026060232065](https://openairdocs.org/sdr/IPXA2026060232065), May 11, 2026: MOUNT. GOUGED. NR 2 ENG AFT MOUNT HAS CHIPPED MATERIAL ON UPPER SURFACE, FLL-0035, ATA 71. ACCOMPLISHED REPAIR PER EO-97541-REQ1 AND VT-SAA EA 757-7121-01-B0744 REV I/R.
- [SDR IPXA2026052627817](https://openairdocs.org/sdr/IPXA2026052627817), May 11, 2026: FLOORBEAM. CORRODED. AFT OF BULK CARGO COMPARTMENT FLOOR BEAM ASSY UPPER FLANGE HAS 4 EA NUT PLATE CORRODED APPROX AT BS 1681.8, BTW BL 0 AND RBL 50, ID STICKER NUM. (085-015) ATA 5
- [SDR IPXA2026052129933](https://openairdocs.org/sdr/IPXA2026052129933), May 11, 2026: STRAP. CORRODED. UPON REMOVAL OF CEILING DECOMPRESSION PANEL FOUND STABILIZATION STRAP CORRODED, APPROX BTW BS 1400 AND BS 1420, RBL 45.50,
- [SDR IPXA2026052129850](https://openairdocs.org/sdr/IPXA2026052129850), May 11, 2026: STRAP. CORRODED. UPON REMOVAL OF CEILING DECOMPRESSION PANEL FOUND STABILIZATION STRAP CORRODED, BTW BS 1560 AND BS 1580, LBL 45.50,
- [SDR IPXA2026052129952](https://openairdocs.org/sdr/IPXA2026052129952), May 11, 2026: STRAP. CORRODED. UPON REMOVAL OF CEILING DECOMPRESSION PANEL FOUND STABILIZATION STRAP CORRODED, APPROX BTW BS 1400 AND BS 1420, RBL 24.75,
- [SDR IPXA2026052129852](https://openairdocs.org/sdr/IPXA2026052129852), May 11, 2026: STRAP. CORRODED. UPON REMOVAL OF CEILING DECOMPRESSION PANEL FOUND STABILIZATION STRAP CORRODED, APPROX BTW BS 1560 AND BS 1580, LBL 24.75,
- [SDR IPXA2026051619006](https://openairdocs.org/sdr/IPXA2026051619006), May 10, 2026: NUT PLATE. CORRODED. AFT OF BULK CARGO COMPARTMENT FLOOR DECK PLATE, SUPPORT ANGLE ASSY NUT PLATE STRAP HAS CORROSION APPROX AT BS 1715, RBL 12.50, ID STICKER NUM. (085-005) ATA 53-
- [SDR IPXA2026051619025](https://openairdocs.org/sdr/IPXA2026051619025), May 10, 2026: NUT PLATE. CORRODED. STR, AFT OF BULK CARGO COMPARTMENT FLOOR DECK PLATE, SUPPORT ANGLE ASSY NUT PLATE STRAP HAS CORROSION APPROX AT BS 1715, RBL 5, ID STICKER NUM. (085-006) ATA 53
- [SDR IPXA2026052419140](https://openairdocs.org/sdr/IPXA2026052419140), May 10, 2026: NUT PLATE. CORRODED. AFT OF BULK CARGO COMPARTMENT FLOOR DECK PLATE, SUPPORT ANGLE ASSY NUT PLATE STRAP HAS CORROSION APPROX AT BS 1715, LBL 23, ID STICKER NUM. (085-009) ATA 53-20 
- [SDR IPXA2026051619223](https://openairdocs.org/sdr/IPXA2026051619223), May 10, 2026: NUT PLATE. CORRODED. AFT OF BULK CARGO COMPARTMENT FLOOR DECK PLATE, SUPPORT ANGLE ASSY NUT PLATE STRAP HAS CORROSION APPROX AT BS 1710, RBL 51, ID STICKER NUM. (085-011) ATA 53-20 
- [SDR IPXA2026052414678](https://openairdocs.org/sdr/IPXA2026052414678), May 10, 2026: BRACKET. CORRODED. RIGHT WING TO BODY FARING BRACKET FOUND LIGHT CORRISION AT B.S. 906.5 ES-046. INSTALLED 2 EA WTB FAIRING BRACKETS, P/N: 149N7210-70SAAU AND P/N: 149N7210-76SAAU
- [SDR IPXA2026052418871](https://openairdocs.org/sdr/IPXA2026052418871), May 10, 2026: DECK PLATE. CORRODED. AFT OF BULK CARGO COMPARTMENT FLOOR DECK PLATE, SUPPORT ANGLE ASSY NUT PLATE STRAP HAS CORROSION APPROX AT BS 1715, RBL 23, I INSTALLED NUT PLATE STRAP AT FLOOR
- [SDR IPXA2026060214234](https://openairdocs.org/sdr/IPXA2026060214234), May 10, 2026: CROSSBEAM. DAMAGED. MAIN DECK WING CENTER SECTION FLOOR PANEL 241XBF STA 900 BTW LBL 24.75 AND LBL 45.5 HAS FLOOR PANEL FRAME SUPPORT BROKEN, FLL-003, ATA 53. INSTALLED 01 EA NEW S
- [SDR IPXA2026052419117](https://openairdocs.org/sdr/IPXA2026052419117), May 10, 2026: STRAP. CORRODED. AFT OF BULK CARGO COMPARTMENT FLOOR DECK PLATE, SUPPORT ANGLE ASSY NUT PLATE STRAP HAS CORROSION APPROX AT BS 1715, LBL 12.50. INSTALLED NUT PLATE STRAP AT FLOO
- [SDR IPXA2026060219107](https://openairdocs.org/sdr/IPXA2026060219107), May 10, 2026: NUT PLATE. DAMAGED. AFT OF BULK CARGO COMPARTMENT FLOOR DECK PLATE, SUPPORT ANGLE ASSY NUT PLATE STRAP HAS CORROSION APPROX AT BS 1715, LBL 36.50, INSTALLED NUT PLATE STRAP AT FLOO
- [SDR IPXA2026060219038](https://openairdocs.org/sdr/IPXA2026060219038), May 10, 2026: NUT PLATE. DAMAGED. AFT OF BULK CARGO COMPARTMENT FLOOR DECK PLATE, SUPPORT ANGLE ASSY NUT PLATE STRAP HAS CORROSION APPROX AT BS 1715, LBL 5, ID STICKER NUM. (085-007) ATA 53-20. 
- [SDR IPXA2026052118868](https://openairdocs.org/sdr/IPXA2026052118868), May 10, 2026: SUPPORT ANGLE. CORRODED. AFT OF BULK CARGO COMPARTMENT FLOOR DECK PLATE, SUPPORT ANGLE ASSY HAS CORROSION APPROX AT BS 1715, RBL 36.50. INSTALLED NEW SUPPORT ANGLE AND NUTPLATE STRAP AS
- [SDR IPXA2026052114678](https://openairdocs.org/sdr/IPXA2026052114678), May 10, 2026: BRACKET. CORRODED. RIGHT WING TO BODY FARING BRACKET FOUND LIGHT CORRISION AT B.S. 906.5 OUT OF LIMITS
- [SDR IPXA2026052114234](https://openairdocs.org/sdr/IPXA2026052114234), May 10, 2026: FLOOR SUPPORT. BROKEN. MAIN DECK WING CENTER SECTION FLOOR PANEL 241XBF STA 900 BTW LBL 24.75 AND LBL 45.5 HAS FLOOR PANEL FRAME SUPPORT BROKEN, C/W SRM 51-20-01-0G-0.
- [SDR IPXA2026051619038](https://openairdocs.org/sdr/IPXA2026051619038), May 10, 2026: SUPPORT ANGLE. CORRODED. AFT OF BULK CARGO COMPARTMENT FLOOR DECK PLATE, SUPPORT ANGLE ASSY NUT PLATE STRAP HAS CORROSION APPROX AT BS 1715, LBL 5,
- [SDR IPXA2026051618871](https://openairdocs.org/sdr/IPXA2026051618871), May 10, 2026: DECK PLATE. CORRODED. AFT OF BULK CARGO COMPARTMENT FLOOR DECK PLATE, SUPPORT ANGLE ASSY NUT PLATE STRAP HAS CORROSION APPROX AT BS 1715, RBL 23. QC AUDIT C/W.
- [SDR IPXA2026051619107](https://openairdocs.org/sdr/IPXA2026051619107), May 10, 2026: NUT PLATE. DAMAGED. AFT OF BULK CARGO COMPARTMENT FLOOR DECK PLATE, SUPPORT ANGLE ASSY NUT PLATE STRAP HAS CORROSION APPROX AT BS 1715, LBL 36.50.
- [SDR IPXA2026051619117](https://openairdocs.org/sdr/IPXA2026051619117), May 10, 2026: PLATE. CORRODED. AFT OF BULK CARGO COMPARTMENT FLOOR DECK PLATE, SUPPORT ANGLE ASSY NUT PLATE STRAP HAS CORROSION APPROX AT BS 1715, LBL 12.50.
- [SDR IPXA2026052405432](https://openairdocs.org/sdr/IPXA2026052405432), May 9, 2026: CONTROL WHEEL. CORRODED. COPILOTS CONTROL WHEEL OUTER SKIN CORRRODED RH SIDE. INSTALLED SERVICEABLE COPILOTS AILERON CONTROL WHEEL AND ADAPTER IAW AMM 27-11-02-424-010 TW ID:19-983 DD:0
- [SDR IPXA2026060205494](https://openairdocs.org/sdr/IPXA2026060205494), May 9, 2026: SKIN. CRACKED. NR 2 ENG FIRE LOOP ACCESS PANEL L/E SKIN CRACKED . INSTALLED EXTERNAL REPAIR DOUBLER AT #2 ENG FIRE LOOP ACCESS PANEL IAW E.A.# 757-5741-01-B0742 REV P1 STEP 7.
- [SDR IPXA2026060178921](https://openairdocs.org/sdr/IPXA2026060178921), May 8, 2026: ANGLE. CORRODED. L/H HORZ STAB TO ELEVATOR OTBD END BONDING STRAP ATTACH BRACKETS APPEARS TO HAVE LIGHT CORROSION. INSTALLED WEB, NEW ANGLE (BRACKET) AND NEW BONDING JUMPER (STR
- [SDR IPXA2026060378913](https://openairdocs.org/sdr/IPXA2026060378913), May 8, 2026: BRACKET. DAMAGED. R/H HORZ STAB TO ELEVATOR OTBD END BONDING STRAP ATTACH BRACKETS APPEARS TO HAVE LIGHT CORROSION. INSTALLED WEB, NEW ANGLE (BRACKET) AND NEW BONDING JUMPER (STR
- [SDR IPXA2026052478794](https://openairdocs.org/sdr/IPXA2026052478794), May 8, 2026: FRAME. CORRODED. RT ELEVATOR OTBD END UPPER CONDUCTIVE FRAME DISBONDED AT AREA UNDER CORRODED STATIC WICK BASE. RL003. INSTALLED CONDUCTIVE FRAME , AND INSTALLED STATIC WICK BAS
- [SDR IPXA2026052478671](https://openairdocs.org/sdr/IPXA2026052478671), May 8, 2026: SKIN. CORRODED. L/H ELEVATOR TO TIP (UPPER AND LOWER) SPLICE PLATE HAVE CORROSION WITH POPPED RIVET. RL013. INSTALLED UPPER SPLICE PLATE P/N 183N2007-5SAAU AND LOWER SPLICE PLA
- [SDR IPXA2026052793693](https://openairdocs.org/sdr/IPXA2026052793693), May 8, 2026: SUPPORT ANGLE. CRACKED. NR 1 PYLON HYD BAY O/B SIDE ACCESS PNL CUT-OUT HAS LOWER, FWD SUPPORT ANGLE WITH CRACKS. 83-017. ATA 54-40. INSTALLED ANGLE (SPRING CLIP) AT NR 1 PYLON HYD BAY 
- [SDR IPXA2026052793074](https://openairdocs.org/sdr/IPXA2026052793074), May 8, 2026: SUPPORT ANGLE. CRACKED. NR 1 PYLON HYD BAY FWD, UPPER SUPPORT ANGLE HAS A CRACK AT OTBD END. PRODUCTION AUDIT C/W. INSTALLED SUPORT ANGLE (BEAM) AT #1 PYLON HYD BAY FWD UPPER IAW B757-
- [SDR IPXA2026052178671](https://openairdocs.org/sdr/IPXA2026052178671), May 8, 2026: STRUCTURE. CORRODED. LEFT ELEVATOR TO TIP (UPPER AND LOWER) SPLICE PLATE HAVE CORROSION WITH POPPED RIVET. C/W SRM 51-40-02-0G-0.
- [SDR IPXA2026052178794](https://openairdocs.org/sdr/IPXA2026052178794), May 8, 2026: FRAME. DEBONDED. RIGHT ELEVATOR OTBD END UPPER CONDUCTIVE FRAME DISBONDED AT AREA UNDER CORRODED STATIC WICK BASE.
- [SDR IPXA2026051678913](https://openairdocs.org/sdr/IPXA2026051678913), May 8, 2026: BRACKET. CORRODED. R/H HORZ STAB TO ELEVATOR OTBD END BONDING STRAP ATTACH BRACKETS APPEARS TO HAVE LIGHT CORROSION. INSTALLED WEB, NEW ANGLE (BRACKET) AND NEW BONDING JUMPER (STR
- [SDR IPXA2026051678921](https://openairdocs.org/sdr/IPXA2026051678921), May 8, 2026: ATTACH ANGLE. CORRODED. L/H HORZ STAB TO ELEVATOR OTBD END BONDING STRAP ATTACH BRACKETS APPEARS TO HAVE LIGHT CORROSION. RL014 VERIFIED STEP 1 AND 2.
- [SDR IPXA2025022013683](https://openairdocs.org/sdr/IPXA2025022013683), Feb 18, 2025: PROXIMITY SWITCH. OUT OF ADJUST. ON APPROACH AT APPROX 2000€™ WE RECEIVED A L FWD ENT DOOR EICAS AS WELL AS AN OVERHEAD DISCREET ENTRY DOORS LIGHT. EXTINGUISHED AFTER LANDING. FOUND PROXIMITY 
- [SDR IPXA2025021913683](https://openairdocs.org/sdr/IPXA2025021913683), Feb 18, 2025: PROXIMITY SWITCH. OUT OF ADJUST. ON APPROACH AT APPROX 2000€™ WE RECEIVED A L FWD ENT DOOR EICAS AS WELL AS AN OVERHEAD DISCREET ENTRY DOORS LIGHT. EXTINGUISHED AFTER LANDING. FOUND PROXIMITY 

All 248: https://openairdocs.org/aircraft/N412UP/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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