# N405UP: 1987 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: 23727
- Year built: 1987
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 29, 1987
- Certificate issued: December 12, 1998
- Expires: February 28, 2029
- Mode S code: A4C104
- 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=405UP
- Page: https://openairdocs.org/aircraft/N405UP

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 N405UP.

## FAA accident and incident reports

None matched to N405UP.

## Service difficulty reports (189, 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 IPXA2025091690459](https://openairdocs.org/sdr/IPXA2025091690459), Sep 3, 2025: STRAP. CORRODED. APU INLET SUPPORT STRUCTURE AFT STRAP SHOWS SIGNS OF CORROSION. INSTALLED 1EA REPAIR DOUBLER (1), 1EA STRAP (2), 1EA FILLER (3), 1EA FILLER (4) AND 9EA NUTPLATE
- [SDR IPXA2025091653930](https://openairdocs.org/sdr/IPXA2025091653930), Aug 31, 2025: SUPPORT ANGLE. CORRODED. APU INLET SUPPORT STRUCTURE FWD STRAP O/B END SHOWS SIGNS OF CORROSION , HAS 3 EA NUT PLATES PULLED THROUGH STRAP WHITH A LAYER OF WHITE POWDER. REMOVED AND REP
- [SDR IPXA2025042577738](https://openairdocs.org/sdr/IPXA2025042577738), Apr 22, 2025: FLAP SYSTEM. WARNING MESSAGE. ON APPROACH FLAP SELECTOR TO 25 TE FLAP DISAGREE EICAS, FLAPS REMAIN 20, USED CHECKLIST ALT.REMOVED & REINSTALLED #1 FWD TE FLAP TRACK FAIRING. IAW AMM 27-51-31
- [SDR IPXA2025042377738](https://openairdocs.org/sdr/IPXA2025042377738), Apr 22, 2025: TRANSMISSION. TRIPPED. EMERGENCY DECLARED, ON APPROACH FLAP SELECTOR TO 25 TE FLAP DISAGREE EICAS, FLAPS REMAIN 20, USED CHECKLIST ALT. FLAPS TO 25 T/S REF FIM 27-51 FAULT TREE 808, F
- [SDR IPXA2024100791720](https://openairdocs.org/sdr/IPXA2024100791720), Oct 1, 2024: HEATER. WARNING MESSAGE. ON PREFLIGHT AFTER ALL WINDOW HEAT SWITCHED SELECTED ON L SIDE WINDOW EICAS AND OVERHEAD INOP LIGHT ILLUMINATED REVERSED DMP. REMOVED AND REPLACED L2 WINDOW IRW
- [SDR IPXA2024100191720](https://openairdocs.org/sdr/IPXA2024100191720), Oct 1, 2024: HEATER. FAULTED. *** SDR FILED OPEN *** ON PREFLIGHT AFTER ALL WINDOW HEAT SWITCHED SELECTED ON L SIDE WINDOW EICAS AND OVERHEAD INOP LIGHT ILLUMINATED ITEM PLACED ON DEFERRAL P
- [SDR IPXA2024052294935](https://openairdocs.org/sdr/IPXA2024052294935), May 22, 2024: OUTFLOW VALVE. MALFUNCTIONED. **EMERG DECLARED**CABIN ALT WARNING CAME ON & DESCENDED TO 25000 FT. RAN THE QRH & WARNING WENT OUT THEN OVERBOARD EX VLV OPEN ON STAT MSG. PILOTS REPORTED OUTF
- [SDR IPXA2023112660660](https://openairdocs.org/sdr/IPXA2023112660660), Nov 12, 2023: TEE ANGLE. CORRODED. FAULT: WTB T-CHORD STRUCTURE AT STA 900, BL 0 HAS EXFOLIATED CORROSION. INSTALLED T-CHORD AND 8 (EA) SPLICE PLATES AT STA 900 I.A.W SRM 51-70-12-OG-O DETAIL VII
- [SDR IPXA2023112621920](https://openairdocs.org/sdr/IPXA2023112621920), Nov 9, 2023: SPAR. CORRODED. FAULT-RIGHT WING UPPER EXTEIOR SURFACE STA 150 TO STA 204 SHOWS SPOTS WITH CORROSION. NO DOT. INSTALLED PANEL 196AR IAW SRM 51-40-02. REVIEWED
- [SDR IPXA2023112621836](https://openairdocs.org/sdr/IPXA2023112621836), Nov 9, 2023: SPAR. CORRODED. FAULT-LEFT WING UPPER EXTEIOR SURFACE STA 150 TO STA 204 SHOWS SPOTS WITH CORROSION. DOT 68-01. INSTALLED PANEL 195AL PER SRM 51-40-02. REVIEWED
- [SDR IPXA2023113099488](https://openairdocs.org/sdr/IPXA2023113099488), Nov 8, 2023: ACCESS DOOR. UNKNOWN. FWD EXTERNAL ACCESS DOOR 113 AL ( AREA FWD OF NLG W/W ) BOTH IB AND OB HINGES HAS WEAR BUSHINGS . 89-096. UPON FURTHER INVESTIGATION DOOR HINGES FOUND TO BE IN 
- [SDR IPXA2023113099411](https://openairdocs.org/sdr/IPXA2023113099411), Nov 8, 2023: DOOR LATCH. GOUGED. CREW ENTRY DOOR LATCHES UPPER AND LOWER 2EA APPEAR TO HAVE GOUGES . 89-095. BLENDED OUT GOUGES ON UPPER AND LOWER LATCHES OF CREW ENTRY DOOR. PER STEP 1 OF SREO
- [SDR IPXA2023110999411](https://openairdocs.org/sdr/IPXA2023110999411), Nov 8, 2023: UNKNOWN. UNKNOWN. CREW ENTRY DOOR LATCHES UPPER AND LOWER 2EA APPEAR TO HAVE GOUGES . OPEN
- [SDR IPXA2023110999488](https://openairdocs.org/sdr/IPXA2023110999488), Nov 8, 2023: UNKNOWN. UNKNOWN. FWD EXTERNAL ACCESS DOOR 113 AL ( AREA FWD OF NLG W/W ) BOTH IB AND OB HINGES HAS WEAR BUSHINGS . OPEN
- [SDR IPXA2023112475686](https://openairdocs.org/sdr/IPXA2023112475686), Nov 7, 2023: FRAME. NONE. *MAJOR REPAIR* FAULT : EXISTING FRAME REPAIR FOUND AT AFT CARGO COMPARTMENT STA 1240 R/H. VERIFIED ALL WORK ACCOMPLISHED IAW EO-87166-REQ1 AND VTMAE EA 757-5360
- [SDR IPXA2023111979160](https://openairdocs.org/sdr/IPXA2023111979160), Nov 7, 2023: SKIN. OUT OF LIMITS. *SDR FILED OPEN* FAULT: PUNCTURE BETWEEN STA 1400- 1420. STR 24-25 L/H. GIVEN THE OK TO APPLY TOP COAT. SUPPLEMENTAL INSPECTIONS DEFERRED IAW B757-200PF REV 118
- [SDR IPXA2022012178121](https://openairdocs.org/sdr/IPXA2022012178121), Jan 19, 2022: FLAP SYSTEM. FAULT MESSAGE. INSPECTION TYPE: A, EMERGENCY DECL'D* NO EQUIP USED*LANDED UNEVENTFULLY ON APPROACH WHEN SLECTING FLAPS 25 RECIEVED TE FLAP DISAGREE EICAS MESSAGE. COMPLETED QR
- [SDR IPXA2022011077696](https://openairdocs.org/sdr/IPXA2022011077696), Jan 9, 2022: NONE. UNRELIABLE. INSPECTION TYPE:NA**ATB** AIRSPEED UNRELIABLE ON DEPARTURE. RAN QRH PROCEDURE. RETURN TO SDFREPLACED CAPT / L/H ADC & FOUND LEAK IN PITOT STATIC PORT SEE THIS P
- [SDR IPXA2021111676025](https://openairdocs.org/sdr/IPXA2021111676025), Nov 16, 2021: NONE. NONE. INSPECTION TYPE:SEG4LEFT WING O/B FLAP TOP SURFACE REPAIR IS DELAMINATED. DOT 18-10REPAIRED PANEL IAW B757 SRM 51-70-07-0G PER SRM 57-53-01-2R-1.
- [SDR IPXA2021111676024](https://openairdocs.org/sdr/IPXA2021111676024), Nov 16, 2021: NONE. NONE. INSPECTION TYPE:SEG4FOUND A DELAMINATED AREA ON THE UPPER SURFACE OF THE L/H O/B MAIN FLAP. LOCATED 31" IN FROM THE O/B SIDE OF THE PART, AND 8.5" UP FROM THE T
- [SDR IPXA2021111575994](https://openairdocs.org/sdr/IPXA2021111575994), Nov 7, 2021: NONE. NONE. INSPECTION TYPE:CTHE VERT. STAB. UPR FWD TORQUE BOX PANEL HAS A DISBONDED DENT AT FSS 321.046 ON THE L/H SIDE.REPAIRED PANEL IAW B757 SRM 51-70-07-0G PER SRM 55
- [SDR IPXA2021111575993](https://openairdocs.org/sdr/IPXA2021111575993), Nov 7, 2021: NONE. NONE. INSPECTION TYPE:CTHE VERT. STAB. R/H LWR FWD TORQUE BOX HAS MULTIPLE DENTS FROM HAIL DAMAGE. AFTER CLEAN UP AND PAINT REMOVAL, ONE DISBOND FOUNDREPAIRED PANEL I
- [SDR IPXA2021031566817](https://openairdocs.org/sdr/IPXA2021031566817), Mar 14, 2021: SEAT TRACK. DAMAGED. INSPECTION TYPE:N/APOS 11/12 SEAT TRACK DAMAGE.REPAIRED SEAT TRACK IAW EO B757-5310-79593.
- [SDR IPXA2019120659733](https://openairdocs.org/sdr/IPXA2019120659733), Dec 3, 2019: TUBE. DAMAGED. AT 27,000 FT, CABIN ALTITUDE RED WARNING EICAS, CREW PERFORMED AN EMERGENCY, DESCENDED TO 10,000 FT, APPROACHING 10,000 FT, THE CABIN ALTITUDE AUTO STATUS MESSA
- [SDR IPXA2019113049525](https://openairdocs.org/sdr/IPXA2019113049525), Nov 30, 2019: WARNING MESSAGE. FALSE ACTIVATION. CLIMBING THRU 28,000' THE CABIN ALT WARNING EICAS WAS RECEIVED. NO OTHER INDICATIONS LEFT PACK WAS OFF AND WE TURNED IT BACK ON. CABIN ALT WAS ACCEPTABLE BELOW 
- [SDR IPXA2019111859042](https://openairdocs.org/sdr/IPXA2019111859042), Nov 15, 2019: ANGLE. CRACKED. INSPECTION TYPE:A300#2 PYLON AFT FAIRING FWD END RH SIDE FWD CORNER ANGLE PLATE CRACKEDREMOVED AND REPLACED IAW SRM 51-40-02
- [SDR IPXA2019112049213](https://openairdocs.org/sdr/IPXA2019112049213), Nov 14, 2019: FLOOR PANEL. DAMAGED. INSPECTION TYPE:SEGFLOOR BOARD PANBEL #252XTF HAS DAMAGED CORNERFABBED PNL 252XTF FROM 5024N00001SS-G BTCH#3546253 PER SREO B757-5320-9692-K
- [SDR IPXA2019112769454](https://openairdocs.org/sdr/IPXA2019112769454), Nov 12, 2019: STRINGER CLIP. BROKEN. INSPECTION TYPE:C1STATION 297,STRINGER 17L CLIP BROKENFABRICATED NEW BRACKET PER DRAWING #232N1504
- [SDR IPXA2019112769453](https://openairdocs.org/sdr/IPXA2019112769453), Nov 12, 2019: STRINGER CLIP. BROKEN. INSPECTION TYPE:C1STATION 297,STRINGER 17L CLIP BROKENFABRICATED NEW BRACKET PER DRAWING #232N1504
- [SDR IPXA2019112769449](https://openairdocs.org/sdr/IPXA2019112769449), Nov 9, 2019: SEAT TRACK. WORN. INSPECTION TYPE:SEGMAIN DECK SEAT TRACK SCALLOP LBL 45.5 DAMAGED BETWEEN STA 610-620WORK PER 757-200 PF SRM 53-30-52-2-R PROCEDURE 1
- [SDR IPXA2019111869055](https://openairdocs.org/sdr/IPXA2019111869055), Nov 8, 2019: FLOOR PANEL. DELAMINATED. INSPECTION TYPE:SEGFLIGHT DECK FLOOR PANEL 212XAF DELAMINATEFABBED PNL 212XAF FROM 5024N400001SS-G BTH# 0003546253 PER SREO B757-5320-9692-K
- [SDR IPXA2019111549013](https://openairdocs.org/sdr/IPXA2019111549013), Nov 7, 2019: ANGLE. CRACKED. INSPECTION TYPE:C1#1 PYLON AFT FAIRING FWD END RH SIDE HAVE CRACKED ANGLEREMOVED AND REPLACED IAW SRM 51-40-2
- [SDR IPXA2019112769458](https://openairdocs.org/sdr/IPXA2019112769458), Nov 6, 2019: PANEL. DELAMINATED. INSPECTION TYPE:C1LH VERTICAL STAB LOWER FWD TORQUE BOX PANEL DELAMINATED STARTING AT TOP EDGE EXTENDING DOWN APPROX 2.0 FEET AND SPANNING THE ENTIRE WIDTH OF P
- [SDR IPXA2018091984133](https://openairdocs.org/sdr/IPXA2018091984133), Sep 18, 2018: BULB. INOPERATIVE. EMERGENCY LIGHT HAS FIVE BULBS INOPERATIVE. REPLACED THE FIVE BULBS IAW AMM 33-51-01-2.
- [SDR IPXA2017111523600](https://openairdocs.org/sdr/IPXA2017111523600), Nov 12, 2017: FLOOR SUPPORT. CRACKED. INSPECTION TYPE: C-13, E & E BAY FLOOR SUPPORT IS CRACKED BS 460. REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR IPXA2017111623634](https://openairdocs.org/sdr/IPXA2017111623634), Nov 1, 2017: SKIN. DENTED. INSPECTION TYPE: C-18, AFT CARGO DOOR EXTERNAL SKIN FOUND DENTED JUST BELOW LATCH HANDLE. REPAIRED THE DOOR SKIN IAW SRM 52-30-01, REPAIR 4.
- [SDR IPXA2017110723358](https://openairdocs.org/sdr/IPXA2017110723358), Nov 1, 2017: FLOOR PANEL. PUNCTURED. E&E FLOOR PANEL 119BF HAS PUNCTURE. FAB NEW PANEL 119BF IAW GMM 09-10 AND DWG 284N1033.
- [SDR IPXA2017111523601](https://openairdocs.org/sdr/IPXA2017111523601), Oct 29, 2017: SKIN. DENTED. DENT 41 INCHES LEFT OF RUDDER, 1.3 INCHES IN DIAMETER. REPAIRED IAW SRM 51-70-10, REPAIR 2.
- [SDR IPXA2017111323496](https://openairdocs.org/sdr/IPXA2017111323496), Oct 29, 2017: PANEL. DENTED. DENT 16" LEFT OF RUDDER, 4.2" FORWARD OF AFT RIVET ROW 1.4" IN DIAMETER. PERMANENT REPAIR. INSTALLED INTERIM REPAIR IAW SRM 51-70-10 REPAIR 2.
- [SDR IPXA2017111323497](https://openairdocs.org/sdr/IPXA2017111323497), Oct 29, 2016: PANEL. DENTED. DENT 41" LEFT OF RUDDER 1.3" IN DIAMETER. PERMANENT REPAIR. INSTALLED INTERIM IAW SRM 51-70-10 REPAIR 2.
- [SDR IPXA2015091893686](https://openairdocs.org/sdr/IPXA2015091893686), Sep 18, 2015: CONTAINER. DAMAGED. F/O'S LIFE VEST BAG TORN. R & R F/O'S LIFE VEST IAW MM 25-11-00.
- [SDR IPXA2015051589114](https://openairdocs.org/sdr/IPXA2015051589114), May 15, 2015: BULB. INOPERATIVE. EMERGENCY LIGHT HAS SIX INOPERATIVE BULBS. REPLACED THE INOPERATIVE BULBS IAW AMM 33-51-01-2.
- [SDR IPXA2014080483860](https://openairdocs.org/sdr/IPXA2014080483860), Aug 4, 2014: SKIN. DAMAGED. LEFT OTBD T/E FLAP LOWER SKIN DAMAGED. REPAIRED IAW EO B757-5750-55118-A.
- [SDR IPXA2014021281899](https://openairdocs.org/sdr/IPXA2014021281899), Feb 11, 2014: FRAME. DENTED. DURING INSPECTION 4C16, AFT CARGO BAY FRAME, BS 1600 ABOVE S26L DENTED. CHECK LIMITS NO DENTS ALLOWED IAW SRM 53-00-07-1A-1, FIG 101 (SHEET 1) TRIMMED OUT DENT 
- [SDR IPXA2014021481914](https://openairdocs.org/sdr/IPXA2014021481914), Feb 3, 2014: FRAME. DENTED. DURING INSPECTION 4C16, AFT CARGO BAY, FRAME BS 1340 ABOVE S26R DENTED. ACCOMPLISHED FRAME REPAIR IAW SRM 53-00-07, REPAIR 5, DETAIL-1.
- [SDR IPXA2014021481913](https://openairdocs.org/sdr/IPXA2014021481913), Feb 3, 2014: FRAME. DENTED. DURING INSPECTION 4C16, AFT CARGO BAY FRAME BS 1320 ABOVE STINGER 26R DENTED. ACCOMPLISHED FRAME REPAIR, IAW SRM 53-00-07. REPAIR 5, DETAIL 1.
- [SDR IPXA2014021281898](https://openairdocs.org/sdr/IPXA2014021281898), Feb 3, 2014: FRAME. DENTED. DURING INSPECTION 4C16, AFT CARGO BAY FRAME, BS 1240 ABOVE S26L DENTED. TRIMMED OUT DENT IAW SRM 53-00-07-2R-6, STEP 4C. HFEC CUTOUT IAW PT6 NTM 51-00-19. NO DE
- [SDR IPXA2014021081832](https://openairdocs.org/sdr/IPXA2014021081832), Feb 2, 2014: FLOOR PANEL. DAMAGED. C16 INSPECTION, MAIN DECK FLOOR PANEL 242XMF HAS TWO DAMAGED HOLES. FABRICATED NEW FLOOR PANE IAW SREO EO B757-5320-9692-H.
- [SDR IPXA12575334](https://openairdocs.org/sdr/IPXA12575334), Sep 16, 2012: WEDGE. DENTED. NR 5 SLAT T/E WEDGE DENTED WITH DELAMINATION. REPAIRED IAW EO B757-5750-48255B.
- [SDR IPXA12571808](https://openairdocs.org/sdr/IPXA12571808), Feb 20, 2012: FLOOR PANEL. CRACKED. INSPECTION TYPE:C-CK, MAIN CARGO FLOOR PANEL 252XTF IS CRACKED, DELAMINATED AND MISSING INSERTS. FABRICATED MAIN CARGO FLOOR PANEL 252XTF IAW EO B757-5320-9692-

All 189: https://openairdocs.org/aircraft/N405UP/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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