# N407UP: 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: 23729
- Year built: 1988
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 24, 1988
- Certificate issued: May 21, 1999
- Expires: May 31, 2027
- Mode S code: A4C872
- 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=407UP
- Page: https://openairdocs.org/aircraft/N407UP

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 N407UP.

## 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 19910726041139I](https://openairdocs.org/incident/19910726041139I), Jul 26, 1991: Boeing 75724APF (N407UP), Syracuse, NY. Aircraft struck a barricade on the displaced threshold while landing at airport.

## Service difficulty reports (205, 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 IPXA2026021697269](https://openairdocs.org/sdr/IPXA2026021697269), Feb 13, 2026: WINDSHIELD. FAILED. DIVERSION, RT FWD WINDSHIELD STARTED ARCING THEN SHATTERED UPON REACHING TOP OF CLIMB. FL400. COMPLIED WITH QRH. DIVERTED TO SDF PER MOC & DISPATCH. REPLACED R1
- [SDR IPXA2026021397269](https://openairdocs.org/sdr/IPXA2026021397269), Feb 13, 2026: WINDSHIELD. ARCED. RIGHT FWD WINDSHIELD STARTED ARCING THEN SHATTERED UPON REACHING TOP OF CLIMB. FL400. COMPLIED WITH QRH. DIVERTED TO SDF PER MOC & DISPATCH. ACCOMPLISHED SECOND
- [SDR IPXA2025071820838](https://openairdocs.org/sdr/IPXA2025071820838), Jul 8, 2025: ANGLE. CORRODED. AFTER REMOVING THE APU DOOR SURROUND FOUND THE ANGLE HAS SURFACE CORROSION. INSTALLED ANGLE IAW SRM 51-40-02.
- [SDR IPXA2025071821035](https://openairdocs.org/sdr/IPXA2025071821035), Jul 8, 2025: ANGLE. CORRODED. AFTER REMOVING THE APU DOOR SHROUD FOUND THE ANGLE HAS SURFACE CORROSION. INSTALLED ANGLE IAW SRM 51-40-02.
- [SDR IPXA2025071819525](https://openairdocs.org/sdr/IPXA2025071819525), Jul 8, 2025: BRACKET. CORRODED. AFTER REMOVAL OF THE APU DOOR SHROUD FOUND THE 148N3141-6 BRACKET HAS SURFACE CORROSION. INSTALLED ANGLE 148N3141-6 IAW SRM 51-40-02.
- [SDR IPXA2025071820911](https://openairdocs.org/sdr/IPXA2025071820911), Jul 8, 2025: ANGLE. CORRODED. AFTER REMOVING APU DOOR SHROUD FOUND THE 148N3152-2 ANGLE HAS SURFACE CORROSION INSTALLED ANGLE 148N3152-2 IAW SRM 51-40-02.
- [SDR IPXA2025071891774](https://openairdocs.org/sdr/IPXA2025071891774), Jul 6, 2025: CHANNEL. CRACKED. FOUND ROD STRUCTURE CHANNEL (313N3022-102) HAS A .60 LONG CRACK ON PANEL 445BL RUNNING FROM EDGE OF FASTENER HOLE TO EDGE OF PART. INSTALLED 1 EA CHANNEL IAW B7
- [SDR IPXA2025080177856](https://openairdocs.org/sdr/IPXA2025080177856), Jul 5, 2025: TEE ANGLE. CORRODED. *** SUPPLEMENTAL SDR *** FAULT- Z100- STR: RH WTB T-CHORD BETWEEN STA 1037 - STA 1060 RBL 65 HAS EXFOLIATION ON UPPER SURFACE. INSTALLED T-CHORD P/N UP-149N7553
- [SDR IPXA2025071179209](https://openairdocs.org/sdr/IPXA2025071179209), Jul 5, 2025: STRINGER. CORRODED. MAJOR REPAIR, LOWER AFT FUSELAGE, BS 1460 HAS EXFOLIATION CORROSION BETWEEN SKIN INNER AREA AND STRINGERS 29 AND 30. INSTALLED STRINGER 23 CLIPS. INSTALLED 2 SU
- [SDR IPXA2025072377856](https://openairdocs.org/sdr/IPXA2025072377856), Jul 5, 2025: TEE ANGLE. CORRODED. STRINGER RT WTB TEE-CHORD BETWEEN BS 1037 - 1060, RBL 65, HAS EXFOLIATION ON UPPER SURFACE.
- [SDR IPXA2025070677817](https://openairdocs.org/sdr/IPXA2025070677817), Jul 5, 2025: INTERCOSTAL. CORRODED. RIGHT PACK EXHAUST INTERCOSTAL FRAME SUPPORT AT FWD AREA HAS CORROSION INSTALLED NEW INTERCOSTAL IAW SRM 51-40-02. VERIFIED INSTALLATION OF RT PACK EXHAUST INTE
- [SDR IPXA2025070677685](https://openairdocs.org/sdr/IPXA2025070677685), Jul 5, 2025: TEE ANGLE. CORRODED. LOWER FUSELAGE INTERCOSTAL T-CHORD BETWEEN STA 1037-STA 1060 RBL 7 HAS CORROSION. INSTALLED T-CHORD P/N: UP-144N8180-48, STA 1037-STA 1060 RBL 7 IAW B757-200PF,
- [SDR IPXA2025070677526](https://openairdocs.org/sdr/IPXA2025070677526), Jul 5, 2025: TEE ANGLE. CORRODED. WTB T-CHORD BETWEEN STA 1037 - STA 1060 LBL 65 HAS EXFOLIATION ON UPPER SURFACE. INSTALLED NEW WTB T-CHORD BETWEEN STA 1037 - STA 1060 LBL 65 IAW B757-200PF, SR
- [SDR IPXA2025070770161](https://openairdocs.org/sdr/IPXA2025070770161), Jul 4, 2025: PANEL. CRACKED. NUMBER 6 SLAT O/B END LWR LEADING EDGE LWR SURFACE CLOSING PLIE HAS A CRACK AS MARKED. INSTALLED CLOSING PLIE IAW SRM 51-40-02.
- [SDR IPXA2025071169520](https://openairdocs.org/sdr/IPXA2025071169520), Jul 4, 2025: FLOOR PANEL. CORRODED. FWD CARGO COMPT FLOOR PANEL 121DF HAS SURFACE CORROSION. INSTALLATION OF ROLLER TRAY, PN- 81658-1. INSTALLED FWD CARGO PIT MBA SYSTEM IAW 757-200 SRM 51-40-02-0
- [SDR IPXA2025080155352](https://openairdocs.org/sdr/IPXA2025080155352), Jul 3, 2025: INTERCOSTAL. CORRODED. FS 1037 - FS 1060 LBL 37 THE PAX EXHAUST INTERCOSTAL 149N7559-1 HAS EXFOLIATION ON UPPER FWD SURFACE INSTALLED PAX EXHAUST INTERCOSTAL OF FS 1037-1060 LBL 37 IA
- [SDR IPXA2025071644664](https://openairdocs.org/sdr/IPXA2025071644664), Jul 3, 2025: STRAP. CORRODED. APU INLET FWD STRAP HAS CORROSION UNDERNEATH. INSTALLED NEW STRAP IAW SRM 51-40-02
- [SDR IPXA2025070751400](https://openairdocs.org/sdr/IPXA2025070751400), Jul 3, 2025: STRIP. CORRODED. METAL STRIP AT BS 1180, BL 5.5 IS CORRODED. INSTALLED METAL TRIP IAW B757-200 SRM 51-40-02 USING SAME HARDWARE.
- [SDR IPXA2025072355352](https://openairdocs.org/sdr/IPXA2025072355352), Jul 3, 2025: INTERCOSTAL. CORRODED. FS 1037 - FS 1060 LBL 37 THE PAX EXHAUST INTERCOSTAL 149N7559-1 HAS EXFOLIATION ON UPPER FWD SURFACE
- [SDR IPXA2024092606717](https://openairdocs.org/sdr/IPXA2024092606717), Sep 26, 2024: GUARD. WRONG PART. EMERGENCY LIGHTS BLACK GUARDED SWITCH COVER SEEMS TO BE WRONG PART. DONT BELIEVE IT SHOULD HAVE SPLIT IN MIDDLE OF GAURD REMOVED AND REPLACED EMERGENCY LIGHTS S
- [SDR IPXA2024080614276](https://openairdocs.org/sdr/IPXA2024080614276), Aug 6, 2024: SWITCH. INOPERATIVE. EMERGENCY LIGHTSA SW GUARD IS LOOSE R AND R SWITCH GUARD IAW SWPM 20-83-11. OPS CK OK
- [SDR IPXA2023091193551](https://openairdocs.org/sdr/IPXA2023091193551), Sep 8, 2023: HANDLE. WORN. CREW ENTRY DOOR EXTERIOR HANDLE€™S STUD IS WORN BEYOND LIMIT R&R CREW ENTRY EXTERIOR HANDLE€™S STUD PER AM 52-12-01
- [SDR IPXA2023090651214](https://openairdocs.org/sdr/IPXA2023090651214), Aug 10, 2023: CAM. WORN. MAJOR REPAIR, CREW ENTRY DOOR UPPER AND LOWER LATCH CAMS HAVE WEAR MARKS DOT 47-04 APPLIED FINISH RESTORATION IAW EO N B757-5210-14721 AND SRM 51-20-01-0G. REVI
- [SDR IPXA202308110214](https://openairdocs.org/sdr/IPXA202308110214), Aug 10, 2023: UNKNOWN. UNKNOWN. *SDR FILED OPEN* FAULT CREW ENTRY DOOR UPPER AND LOWER LATCH CAMS HAVE WEAR MARKS DOT 47-04 APPROVED
- [SDR IPXA2023012090070](https://openairdocs.org/sdr/IPXA2023012090070), Jan 19, 2023: TRANSMITTER. FAULTED. EMERGENCY DECLARED, LANDED UNEVENTFULLY, ON ARRIVAL EXTENDED THE FLAPS TO 1 RECEIVED A TE FLAP ASYM EICAS MESSAGE. RAN QRH. REMOVED AND REPLACED LT WING FLAP PO
- [SDR IPXA2021071671748](https://openairdocs.org/sdr/IPXA2021071671748), Jul 15, 2021: FLAP SYSTEM. OUT OF ADJUST. ATB - NO EMERG DECL'D - NO EQUIP USED - LANDED UNEVENTFULLY - AC OOS. ATB DUE TO T/E FLAP DISAGREE. AFTER MOVING THE FLAP SELECTOR TO UP WE RECEIVED A TE FLAP D
- [SDR IPXA2019093047391](https://openairdocs.org/sdr/IPXA2019093047391), Sep 30, 2019: SKIN. DELAMINATED. INSPECTION TYPE:C1WHILE INSPECTING CARD # 128347, UPPER SKIN BETWEEN STA. 1896.20 & STA 1918.9 REPAIR HAS A DENT IN THE MIDDLE THAT IS DELAMINATED DOT 8-055REMO
- [SDR IPXA2019092447201](https://openairdocs.org/sdr/IPXA2019092447201), Sep 24, 2019: FLOOR PANEL. DAMAGED. INSPECTION TYPE:C1 FLOOR PANEL 211XAF IS DAMAGED AND NEEDS REPLACE. FAB PANEL 211XAF FROM 5024N00001SS-G BATCH# 3525521 AND STEP CUT OUT PER SREO B757-5320-9692
- [SDR IPXA2019092447200](https://openairdocs.org/sdr/IPXA2019092447200), Sep 24, 2019: FLOOR PANEL. DAMAGED. INSPECTION TYPE:C1 FLOOR PANEL 212XAF IS DAMAGED AND NEEDS REPLACE. FAB PANEL 212XAF FROM 5024N400001SS-G BATCH# 3525521 AND STEP CUT OUT PER SREO B757-5320-969
- [SDR IPXA2019091947000](https://openairdocs.org/sdr/IPXA2019091947000), Sep 19, 2019: DOUBLER. DELAMINATED. INSPECTION TYPE:C1 LT O/B AFT FLAP LOWER SURFACE REPAIR LOCATED BETWEEN AFSTA 345.765 AND 353.065 AND 6.5" FROM T/E TO CENTER OF REPAIR FAILED ULTRASONIC LF BON
- [SDR IPXA2019022639487](https://openairdocs.org/sdr/IPXA2019022639487), Feb 26, 2019: WARNING MESSAGE. FALSE ACTIVATION. ON LANDING BLOCK IN LEFT BUS A13 FOUND IN OUT POSITIONPERFORMED BPCU BITE TEST WRT B757FRFIM 24-20-810-802 CODE 59 RECORDED R/R LT GCU WRT AMM 24-22-02--401 AS 
- [SDR IPXA2018121737003](https://openairdocs.org/sdr/IPXA2018121737003), Dec 15, 2018: LAMP. INOPERATIVE. L1 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS IAW MM 33-10-00. OPS NORMAL.
- [SDR IPXA2018112106155](https://openairdocs.org/sdr/IPXA2018112106155), Nov 17, 2018: WARNING MESSAGE. FALSE ACTIVATION. AFTER TAKEOFF WITH GEAR RETRACTION , A GEAR LIGHT INDICATED & GEAR DISAGREE EICAS. RAN THE NON-NORMAL CHECKLIST WITH NO CHANGE. ALL 3 GREEN GEAR LIGHTS, REMAINE
- [SDR IPXA2018083193376](https://openairdocs.org/sdr/IPXA2018083193376), Aug 29, 2018: MOUNT. BROKEN. FOUND THE EVAS MODULE BROKEN. THE EVAS MOUNT WAS BROKEN. REPLACED THE CAPTAIN`S EVAS MOUNT IAW EO 757-2560-45127H. REINSTALLED THE EVAS UNIT.
- [SDR IPXA2018070631412](https://openairdocs.org/sdr/IPXA2018070631412), Jul 5, 2018: DOOR SEAL. OUT OF POSITION. LOUD SQUEAL FROM CREW ENTRY DOOR. DID NOT BEGIN UNTIL AFTER WE LEVELED AT FLT LEVEL 360 CABIN ALTITUDE WAS 5600' DIF WAS 8.5 PSI SEEMS LIKE ITS COMING FROM BOTT
- [SDR IPXA2018070531394](https://openairdocs.org/sdr/IPXA2018070531394), Jul 3, 2018: DOOR SEAL. DIRTY. LOUD SQUEAL FROM ENTRY DOOR AT CRUISE ALTITUDE. PRESSURIZED THE AIRCRAFT AN FOUND SMALL LEAK AT MAIN CARGO DOOR REPAIR PER MM 52 09 00. ALSO FOUND SMALL LEAK AT
- [SDR IPXA2018032227725](https://openairdocs.org/sdr/IPXA2018032227725), Mar 20, 2018: EVAS UNIT. INOPERATIVE. CAPTAIN`S EVAS INOPERATIVE. INSTALLED A NEW EVAS UNIT IAW AMM 25-69-00, OPS CHECKED GOOD.
- [SDR IPXA2017092321967](https://openairdocs.org/sdr/IPXA2017092321967), Sep 19, 2017: SUPPORT. CORRODED. INSPECTION TYPE: C-18, RIGHT AFT LOWER WING TO BODY SUPPORT, FIVE INCHES ABOVE RAT DOOR HAS CORROSION AT INTERSECTION OF BS 1220. REMOVED AND REPLACED THE SUPPO
- [SDR IPXA2017092321969](https://openairdocs.org/sdr/IPXA2017092321969), Sep 17, 2017: SUPPORT. CORRODED. INSPECTION TYPE: C-18, BS 1200 LOWER KEEL BEAM AREA, RT CHANNEL SUPPORT CORRODED. REMOVED AND REPLACED THE CHANNEL SUPPORT
- [SDR IPXA2017092221953](https://openairdocs.org/sdr/IPXA2017092221953), Sep 17, 2017: SKIN. DAMAGED. INSPECTION TYPE: C18, FUSELAGE SKIN EXTERIOR DENTED BS 239, STRINGERS 20 - 21R. REPAIRED IAW SRM 53-00-01-2R, REPAIR 3.
- [SDR IPXA2017092822123](https://openairdocs.org/sdr/IPXA2017092822123), Sep 15, 2017: ATTACH ANGLE. CORRODED. INSPECTION TYPE: C18, RIGHT AFT LOWER WING TO BODY FAIRING AREA, BS 1240 HAS AREAS OF CORROSION AFT LOWER CORNER RAT COMPARTMENT FAIRING ATTACH ANGLE. CUT AND R
- [SDR IPXA2017080720249](https://openairdocs.org/sdr/IPXA2017080720249), Aug 7, 2017: FLOOR SUPPORT. DENTED. AFT LOWER CARGO BAY FLOOR SUPPORT HAS DENT DAMAGE AT BS 1436, RBL 7. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02. DRILLED, PAINTED & INSTALLED NUTPL
- [SDR IPXA2016100709060](https://openairdocs.org/sdr/IPXA2016100709060), Oct 6, 2016: TERMINAL. MELTED. PUNGENT ODOR IN COCKPIT NOTICED DURING INITIAL CLIMB WITH GEAR DOWN. ODOR DISAPEARED WITH THE GEAR UP. ON APPROACH WITH GEAR DOWN ODOR RETURNED AND WAS VERY STR
- [SDR IPXA2016091308226](https://openairdocs.org/sdr/IPXA2016091308226), Sep 9, 2016: CONTROLLER. MALFUNCTIONED. RAPID DECOMPRESSION. CREW DONNED OXYGEN MASKS. REPLACED THE NR 1 CABIN PRESSURE CONTROLLER IAW AMM 21-31-02.
- [SDR IPXA2016061604694](https://openairdocs.org/sdr/IPXA2016061604694), Jun 16, 2016: UNKNOWN. ODOR. WITH LT PACK OFF, CLIMBING THRU 8000 FT, HAD AN ODOR OF SOMETHING GETTING HOT OR BURNING. NO SMOKE INDICATIONS WERE NOTED. TURNED LT PACK BACK ON. SMELL DISSIPA
- [SDR IPXA2015092393863](https://openairdocs.org/sdr/IPXA2015092393863), Sep 18, 2015: SKIN. PUNCTURED. INSPECTION TYPE:C17, LT LOWER HORIZONTAL 185N4001-1 SKIN PANEL ASSY HAS A SMALL PUNCTURE ON THE INTERNAL SKIN. REPAIRED IAW EO B757-5510-58825-A AND REO-G19208,
- [SDR IPXA2015092293837](https://openairdocs.org/sdr/IPXA2015092293837), Sep 8, 2015: WEDGE. DENTED. INSPECTION TYPE:C17, NR 7 L/E SLAT DENTS NR 7 & NR 8 ON T/E WEDGE OUT OF SRM LIMITS. REPAIRED WEDGE WITH METAL HOT BOND REPAIR IAW REO-G19182, REV B & EO B757-5
- [SDR IPXA2015091093350](https://openairdocs.org/sdr/IPXA2015091093350), Sep 3, 2015: FLOOR SKIN. CRACKED. INSPECTION TYPE: C-17, FLIGHT DECK FLOOR HAS A CRACK AT THE EDGE OF WEB BS 284, LBL 19. REMOVED DAMAGE, REPAIRED IAW SRM 53-10-51-2R-4, FIG 201.
- [SDR IPXA2015092193741](https://openairdocs.org/sdr/IPXA2015092193741), Sep 1, 2015: FLOOR SUPPORT. DENTED. INSPECTION TYPE:C-17, AFT CARGO FLOOR SUPPORT DENTED BS 1290, LBL 16.10. REPAIRED IAW SRM 53-00-53-2R-1.
- [SDR IPXA2015091293425](https://openairdocs.org/sdr/IPXA2015091293425), Sep 1, 2015: FLOOR SUPPORT. DENTED. INSPECTION TYPE: C-17, AFT CARGO FLOOR SUPPORT DENTED BS 1280, LBL 10.45. REPAIRED IAW SRM 53-00-53-2R-1.

All 205: https://openairdocs.org/aircraft/N407UP/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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