# N417UP: 1990 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: 23904
- Year built: 1990
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 26, 1990
- Certificate issued: August 3, 1998
- Expires: February 29, 2028
- Mode S code: A4EFF1
- 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=417UP
- Page: https://openairdocs.org/aircraft/N417UP

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 N417UP.

## FAA accident and incident reports

None matched to N417UP.

## Service difficulty reports (237, 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 IPXA2026061240613](https://openairdocs.org/sdr/IPXA2026061240613), Jun 12, 2026: STRAP. CORRODED. AFT CARGO COMPARTMENT CEILING STABILIZATION STRAP HAS CORROSION APPROX BTW BS 1560 AND BS 1580, LBL 45.50.
- [SDR IPXA2026061144531](https://openairdocs.org/sdr/IPXA2026061144531), May 12, 2026: FLOORBEAM. CORRODED. WHILE WORKING FAULT T3F18E008T21R FOUND CORROSION ON FLOORBEAM UPPER SURFACE AT STA. 1200 LBL 45.5 TO 62.2. ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH EO-
- [SDR IPXA2026052044531](https://openairdocs.org/sdr/IPXA2026052044531), May 12, 2026: FLOORBEAM. CORRODED. WHILE WORKING FAULT T3F18E008T21R FOUND CORROSION ON FLOORBEAM UPPER SURFACE AT STA. 1200 LBL 45.5 TO 62.2.
- [SDR IPXA2026061205245](https://openairdocs.org/sdr/IPXA2026061205245), May 9, 2026: SEAT TRACK. GOUGED. STR, MAIN DECK CARGO COMPARTMENT LOWER SILL AREA, SEAT TRACK HAS MULTIPLE GOUGES, APPROX BTW BS 520 AND BS 600, LBL 62.20, ID STICKER NUM. (085-063). ATA 53-10.
- [SDR IPXA2026061069790](https://openairdocs.org/sdr/IPXA2026061069790), May 7, 2026: FRAME. DENTED. AFT CARGO COMPARTMENT FRAME UPPER FLANGE HAS A DENT APPROX AT BS 1500, STGR 26R, ACCOMPLISHED REPAIR PER EO-97485-REQ1 AND EA 757-5360-01-B0741, REV. I/R.
- [SDR IPXA2026061070206](https://openairdocs.org/sdr/IPXA2026061070206), May 7, 2026: STRAP. CORRODED. AFT CARGO COMPARTMENT CEILING STABILIZATION STRAP HAS CORROSION APPROX BTW BS 1400 AND BS 1420, RBL 24.75, INSTALLED REPAIR SECTION CEILING STRAP STA 1380-1440 
- [SDR IPXA2026061069168](https://openairdocs.org/sdr/IPXA2026061069168), May 7, 2026: GUSSET. GOUGED. MAJOR REPAIR NR 2 PYLON LT SIDE AFT STRUT AREA FWD FRAME SUPPORT GOUGED IN 2 PLACES AT LOWER END. ACCOMPLISHED THE PERMANENT REPAIR PER EO-97464-REQ1 AND EA 757
- [SDR IPXA2026051570260](https://openairdocs.org/sdr/IPXA2026051570260), May 7, 2026: STRAP. CORRODED. AFT CARGO COMPARTMENT CEILING STABILIZATION STRAP HAS CORROSION APPROX BTW BS 1560 AND BS 1580, LBL 45.50, INSTALLED REPAIR PARTS. AT AFTÂ COMPARMENT CARGO CEIL
- [SDR IPXA2026060970356](https://openairdocs.org/sdr/IPXA2026060970356), May 7, 2026: STRAP. CORRODED. AFT CARGO COMPARTMENT CEILING STABILIZATION STRAP HAS CORROSION APPROX AT BS 1240, LBL 45.50, INSTALLED REPAIR PARTS AT AFT CARGO COMPARMENT CEILING STABILIZATI
- [SDR IPXA2026060970215](https://openairdocs.org/sdr/IPXA2026060970215), May 7, 2026: STRAP. CORRODED. AFT CARGO COMPARTMENT CEILING STABILIZATION STRAP HAS CORROSION APPROX BTW BS 1560 AND BS 1580, LBL 24.75 INSTALLED REPAIR PARTS (2EA SECTIONS AND 2 EA SPLICES)
- [SDR IPXA2026052045853](https://openairdocs.org/sdr/IPXA2026052045853), May 6, 2026: STRAP. CORRODED. WHILE EVALUATING CORROSION AT APU INLET SURROUND STRUCTURE FOUND CORROSION AT APU AREA AFT STRAP AT STA 1825 BETWEEN STR 3R-6R. REPAIR ACCOMPLISHED PER B757-200
- [SDR IPXA2026061051655](https://openairdocs.org/sdr/IPXA2026061051655), May 6, 2026: SEAT TRACK. CONTAMINATED. MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE SEAT TRACK ASSY HAS MULTIPLE NUT PLATE CORRODED APPROX BTW BS 1661 AND BS 1681, LBL 24.75, ACCOMPLISHED REPAIR PER B
- [SDR IPXA2026051551707](https://openairdocs.org/sdr/IPXA2026051551707), May 6, 2026: SEAT TRACK. CORRODED. MAIN DECK CARGO COMPARTMENT SEAT TRACK ASSY HAS MULTIPLE NUT PLATE CORRODED APPROX BTW BS 1661 AND BS 1681, LBL 45.50, ACCOMPLISHED REPAIR PER B757-200PF SRM 53
- [SDR IPXA2026061052459](https://openairdocs.org/sdr/IPXA2026061052459), May 6, 2026: FRAME. DENTED. AFT CARGO COMPARTMENT FRAME UPPER FLANGE HAS 2 EA DENT APPROX AT BS 1300, STGR 26L, ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-97545-REQ1 AND VT-SAA EA 757-5360-
- [SDR IPXA2026060952752](https://openairdocs.org/sdr/IPXA2026060952752), May 6, 2026: ANGLE. CRACKED. RT AFT WTB LOWER PANEL LANDING SUPPORT ANGLE HAS A CRACK AT FASTENER. INSTALLED NEW PART SUPPORT ANGLE ON RH AFT WTB LOWER PANEL LANDING IAW SRM 51-40-02-0G-0.
- [SDR IPXA2026060539830](https://openairdocs.org/sdr/IPXA2026060539830), May 6, 2026: BONDING CABLE. CORRODED. RH ELEV O/B BONDING HARNESS HAS A CORROSION - ATA 55 - LR-05. REMOVED AND REPLACED RH ELEV O/B BONDING IN REF. B757-200 SWPM 20-20-10. REVIEWED
- [SDR IPXA2026052651388](https://openairdocs.org/sdr/IPXA2026052651388), May 6, 2026: STRAP. CORRODED. MAIN DECK CARGO COMPARTMENT FLOOR BEAM ASSY HAS MULTIPLE NUT PLATE CORRODED AT APPROX BS1681.8, BTW BL 0 AND RBL 50. INSTALLED 5 EA NUTPLATES ASSY AT MAIN DECK 
- [SDR IPXA2026052039737](https://openairdocs.org/sdr/IPXA2026052039737), May 6, 2026: SKIN SPLICE. CORRODED. POWDERY CORROSION ON RT ELEV OTBD SKIN SPLICE PLATE. INSTALLED SPLICE PLATE AND FILLER ON RT ELEV OTBD SKIN IAW SRM 51-40-02-0G-0.
- [SDR IPXA2026052040562](https://openairdocs.org/sdr/IPXA2026052040562), May 6, 2026: SKIN SPLICE. CORRODED. POWDERY CORROSION ON LT ELEV OTBD SKIN SPLICE PLATE. LR-13 VERIFIED STEPS 7 & 8. OK TO INSTALL NEW CONDUCTIVE FRAME GIVEN. INSTALLED NEW FRAME CONDUCTIVE ON L/H
- [SDR IPXA2026051139830](https://openairdocs.org/sdr/IPXA2026051139830), May 6, 2026: BONDING STRAP. CORRODED. APG - RT ELEVATOR OTBD BONDING HARNESS HAS CORROSION.
- [SDR IPXA2026060932327](https://openairdocs.org/sdr/IPXA2026060932327), May 5, 2026: STRAP. CORRODED. AFT CARGO RH OTBD CEILING SUPPORT FRAME EXFOLIATED STA 1400-1420. INSTALLED 1 E/A STABILIZER STRAP SECTION AND 1 E/A SPLICE DOUBLER ON AFT CARGO RH OTBD STA 140
- [SDR IPXA2026051132327](https://openairdocs.org/sdr/IPXA2026051132327), May 5, 2026: SUPPORT FRAME. CORRODED. AFT CARGO RT OTBD CEILING SUPPORT FRAME EXFOLIATED BS 1400-1420.
- [SDR IPXA2026051908602](https://openairdocs.org/sdr/IPXA2026051908602), May 4, 2026: ANGLE. CORRODED. APU INLET DOOR SURROUND STRUCTURE FWD STRAP I/B END HAS CORROSION INSTALLED FWD STRAP, LOWER SUPPORT ANGLE, LOWER CORNER ANGLE, UPPER CORNER ANGLE AND UPPER SUP
- [SDR IPXA2026052014729](https://openairdocs.org/sdr/IPXA2026052014729), May 4, 2026: FLOOR SUPPORT. CORRODED. MAIN DECK CARGO COMPART. FLOOR SUPPORT ANGLE ASSY NUT PLATE STRAP HAS CORROSION, APPROX AT BS 1715 LBL 5, INSTALLED SUPPORT ANGLE AND ASSY NUT PLATE STRAP AT MA
- [SDR IPXA2026052014784](https://openairdocs.org/sdr/IPXA2026052014784), May 4, 2026: FLOOR SUPPORT. CORRODED. MAIN DECK CARGO COMPART. FLOOR SUPPORT ANGLE ASSY NUT PLATE STRAP HAS CORROSION, APPROX AT BS 1715 LBL 12, INSTALLED SUPPORT ANGLE AND ASSY NUT PLATE STRAP AT M
- [SDR IPXA2026052014767](https://openairdocs.org/sdr/IPXA2026052014767), May 4, 2026: STRAP. CORRODED. MAIN DECK CARGO COMPART. FLOOR STRUCT. SUPPORT ANGLE ASSY NUT PLATE STRAP HAS CORROSION, APPROX AT BS 1715 LBL 23, INSTALLED SUPPORT ANGLE AND ASSY NUT PLATE ST
- [SDR IPXA2026052014526](https://openairdocs.org/sdr/IPXA2026052014526), May 4, 2026: STRAP. CORRODED. MAIN DECK CARGO COMPART. FLOOR STRUCT. SUPPORT ANGLE ASSY NUT PLATE STRAP HAS CORROSION, APPROX AT BS 1715 RBL 5. INSTALLED SUPPORT ANGLE AND ASSY NUT PLATE STR
- [SDR IPXA2026052014600](https://openairdocs.org/sdr/IPXA2026052014600), May 4, 2026: STRAP. CORRODED. MAIN DECK CARGO COMPART. FLOOR STRUCT. SUPPORT ANGLE ASSY NUT PLATE STRAP HAS CORROSION, APPROX AT BS 1715 RBL 12. INSTALLED SUPPORT ANGLE AND ASSY NUT PLATE ST
- [SDR IPXA2026052014640](https://openairdocs.org/sdr/IPXA2026052014640), May 4, 2026: STRAP. CORRODED. MAIN DECK CARGO COMPART. FLOOR STRUCT. SUPPORT ANGLE ASSY NUT PLATE STRAP HAS CORROSION, APPROX AT BS 1715 RBL 23, INSTALLED SUPPORT ANGLE AND ASSY NUT PLATE ST
- [SDR IPXA2026052014704](https://openairdocs.org/sdr/IPXA2026052014704), May 4, 2026: STRAP. CORRODED. MAIN DECK CARGO BAY FLOOR STRUCTURE SUPPORT ANGLE ASSY NUT PLATE STRAP HAS CORROSION, APPROX AT BS 1715 RBL 36. INSTALLED SUPPORT ANGLE AND ASSY NUT PLATE STRAP
- [SDR IPXA2026052014818](https://openairdocs.org/sdr/IPXA2026052014818), May 4, 2026: STRAP. CORRODED. MAIN DECK CARGO COMPART. FLOOR STRUCT. SUPPORT ANGLE ASSY NUT PLATE STRAP HAS CORROSION, APPROX AT BS 1715 LBL 36, INSTALLED SUPPORT ANGLE AND ASSY NUT PLATE ST
- [SDR IPXA2026052015262](https://openairdocs.org/sdr/IPXA2026052015262), May 4, 2026: CASCADE. CORRODED. NR 2 ENG INBD T/R UPPER CASCADE HAD SURFACE CORROSION. CASCADE VANE REMOVED AND INSTALLED ON FAULT T3F18E008U9YH LINE 1162.
- [SDR IPXA2026051114526](https://openairdocs.org/sdr/IPXA2026051114526), May 4, 2026: FLOOR SUPPORT. CORRODED. MAIN DECK CARGO COMPART. FLOOR STRUCT. SUPPORT ANGLE ASSY NUT PLATE STRAP HAS CORROSION, APPROX AT BS 1715 RBL 5. VERIFIED STEP 8. OK TO INSTALL ITEM LISTED IN 
- [SDR IPXA2026051114600](https://openairdocs.org/sdr/IPXA2026051114600), May 4, 2026: FLOOR SUPPORT. CORRODED. MAIN DECK CARGO COMPART. FLOOR STRUCT. SUPPORT ANGLE ASSY NUT PLATE STRAP HAS CORROSION, APPROX AT BS 1715 RBL 12. VERIFIED STEP 8. OK TO INSTALL ITEM LISTED IN
- [SDR IPXA2026051114640](https://openairdocs.org/sdr/IPXA2026051114640), May 4, 2026: FLOOR SUPPORT. CORRODED. MAIN DECK CARGO COMPART. FLOOR STRUCT. SUPPORT ANGLE ASSY NUT PLATE STRAP HAS CORROSION, APPROX AT BS 1715 RBL 23. OK TO INSTALL ITEM LISTED IN STEP 8 IS GRANTE
- [SDR IPXA2026051114729](https://openairdocs.org/sdr/IPXA2026051114729), May 4, 2026: FLOOR SUPPORT. CORRODED. MAIN DECK CARGO COMPART. FLOOR STRUCT. SUPPORT ANGLE ASSY NUT PLATE STRAP HAS CORROSION, APPROX AT BS 1715 LBL 5. VERIFIED STEP 8. OK TO INSTALL ITEM LISTED IN 
- [SDR IPXA2026051114784](https://openairdocs.org/sdr/IPXA2026051114784), May 4, 2026: FLOOR SUPPORT. CORRODED. MAIN DECK CARGO COMPART. FLOOR STRUCT. SUPPORT ANGLE ASSY NUT PLATE STRAP HAS CORROSION, APPROX AT BS 1715 LBL 12. VERIFIED STEP 8. OK TO INSTALL ITEM LISTED IN
- [SDR IPXA2026051114767](https://openairdocs.org/sdr/IPXA2026051114767), May 4, 2026: FLOOR SUPPORT. CORRODED. MAIN DECK CARGO COMPART. FLOOR STRUCT. SUPPORT ANGLE ASSY NUT PLATE STRAP HAS CORROSION, APPROX AT BS 1715 LBL 23. VERIFIED STEP 8. OK TO INSTALL ITEM LISTED IN
- [SDR IPXA2026051114818](https://openairdocs.org/sdr/IPXA2026051114818), May 4, 2026: FLOOR SUPPORT. CORRODED. MAIN DECK CARGO COMPART. FLOOR STRUCT. SUPPORT ANGLE ASSY NUT PLATE STRAP HAS CORROSION, APPROX AT BS 1715 LBL 36, VERIFIED STEP 8. OK TO INSTALL ITEM LISTED IN
- [SDR IPXA2026050608602](https://openairdocs.org/sdr/IPXA2026050608602), May 4, 2026: STRAP. CORRODED. APU INLET DOOR SURROUND STRUCTURE FWD STRAP I/B END HAS CORROSION .
- [SDR IPXA2025102247232](https://openairdocs.org/sdr/IPXA2025102247232), Oct 14, 2025: WINDOW. WARNING MESSAGE. L SIDE WINDOW MSG (EICAS) QRH CHECKLIST DID NOT RETURN. OPS TO NORMAL. RESULTED IN BTB. FINISHED INSTALLATION OF #3L WINDSHIELD I/A/W B757 AMM 56-11-10. OPS CHE
- [SDR IPXA2025101447232](https://openairdocs.org/sdr/IPXA2025101447232), Oct 14, 2025: ANTI-ICE SYSTEM. INOPERATIVE. LEFT SIDE WINDOW MESSAGE, QRH CHECKLIST DID NOT RETURN OPS TO NORMAL RESULTED IN BTB T/S AND FOUND LT SIDE WINDOW NR 3 INOPERATIVE. DEFERED LEFT SIDE WINDOW PER
- [SDR IPXA2024062076533](https://openairdocs.org/sdr/IPXA2024062076533), Jun 3, 2024: FLOORBOARD. DAMAGED. R/H MCC FLOORBOARD 232XSF HAS SEVERAL INSERTS BLOWNOUT.REPAIRED R/H MCC FLOORBOARD 232XSF SEVERAL INSERTS IAW. EO B757-5320-9692-K, APPENDIX B, POINT 5
- [SDR IPXA2024061476069](https://openairdocs.org/sdr/IPXA2024061476069), Jun 3, 2024: FLOORBEAM. CORRODED. R/H MCC FLOOR BEAM AT 1200 RBL 0-25 HAS CORROSION. INSTALLED REPAIR PARTS I.A.W SRM 53-00-51-2R-6, DETAIL III STEP 4 O AND P AND SRM 51-40-02-0G.
- [SDR IPXA2024061175806](https://openairdocs.org/sdr/IPXA2024061175806), Jun 3, 2024: FLOOR PANEL. DELAMINATED. R/H MCC FLOORBOARD 252XUF FWD CORNER HAS DELAM . DOT 33-032. NSPECTED AND VERIFIED FABRICATED R/H M.D.C. FLOORBOARD 252XUG I.A.W. SREO B757-5320-9692.
- [SDR IPXA2024060442028](https://openairdocs.org/sdr/IPXA2024060442028), May 31, 2024: FRAME. DENTED. *SUPPLEMENTAL SDR* FAULT: FWD CARGO PIT - FRAME STA 720 RH SIDE HAS A DENT IN INNER CHORD BETWEEN STR 22R AND 23R INSTALLED SECTION "J" I.A.W SRM 53-00-07-2R-5,
- [SDR IPXA2024062441964](https://openairdocs.org/sdr/IPXA2024062441964), May 31, 2024: CAM. GOUGED. CREW ENTRY DOOR - UPPER AND LOWER CAM LATCHES HAVE GOUGES. COMPLETED SREO-14721-REQ001((APPX A). REVIEWED
- [SDR IPXA2024061442019](https://openairdocs.org/sdr/IPXA2024061442019), May 31, 2024: TIE DOWN. CORRODED. FWD CARGO PIT - STA 800 RH SIDE HAS A TIE DOWN WITH CORROSION. INSTALLED NEW TIE DOWN IAW SRM 51-40-02-0G-0, WITH RIVETS P/N: BACB30NX6K7 BATCH: 0004216299 P/N:
- [SDR IPXA2024061342173](https://openairdocs.org/sdr/IPXA2024061342173), May 31, 2024: STRUCTURE. CORRODED. WTB STRUCTURE FOR PANEL 195CL HAS SEVERAL CORRODED NUTPLATES. INSTALLED PANEL 195CL IAW AMM 53-66-01-404-005.
- [SDR IPXA2024060341964](https://openairdocs.org/sdr/IPXA2024060341964), May 31, 2024: LATCH. GOUGED. *SDR FILED OPEN* FAULT: CREW ENTRY DOOR - UPPER AND LOWER CAM LATCHES HAVE GOUGES VERIFIED BLEND ON UPPER AND LOWER CAM LATCHES AT CREW ENTRY DOOR

All 237: https://openairdocs.org/aircraft/N417UP/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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