# N403UP: 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: 23725 - Year built: 1987 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: September 18, 1987 - Certificate issued: December 12, 1998 - Expires: February 28, 2029 - Mode S code: A4B996 - Registered owner: [United Parcel Service Oc](https://openairdocs.org/faa-owner/UNITED%20PARCEL%20SERVICE%20OC) - 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=403UP - Page: https://openairdocs.org/aircraft/N403UP 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 N403UP. ## FAA accident and incident reports None matched to N403UP. ## Service difficulty reports (223, 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 IPXA2026082381790](https://openairdocs.org/sdr/IPXA2026082381790), Aug 23, 2026: BRACKET. MISINSTALLED. CREW ENTRY DOOR WARNING SENSOR BRACKET IS INCORRECTLY INSTALLED CAUSING CONTACT WITH CREW ENTRY DOOR SEAL WHEN CLOSING DEFERRED PER EO-98420 FOR 90 DAYS. - [SDR IPXA2026072004760](https://openairdocs.org/sdr/IPXA2026072004760), Jul 17, 2026: STRUCTURE. FOD. EMERGENCY DECLARED, AIR TURN BACK, BIRD STRIKE RESULTED IN AIR TURN BACK C/W BIRD STRIKE CONDITIONAL INSPECTION IAW AMM 05-51-18-212-001. NO OTHER BIRD STRIKES - [SDR IPXA2026071704760](https://openairdocs.org/sdr/IPXA2026071704760), Jul 17, 2026: NOT REPORTED. NOT REPORTED. EMERGENCY DECLARED, AIR TURN BACK, BIRD STRIKE RESULTED IN AIR TURN BACK. - [SDR IPXA2026032684640](https://openairdocs.org/sdr/IPXA2026032684640), Mar 26, 2026: ALTIMETER. FAULTED. DURING DESCEND GEAR NOT DOWN CONFIG LIGHT ON AFTER EXTENDING FLAPS GEAR NOT DOWN WARNING SOUNDED RR LEFT RADIO ALTIMETER IAW B757AMM 33-01-404-005 OPS CHECK NOR - [SDR IPXA2026022322493](https://openairdocs.org/sdr/IPXA2026022322493), Feb 20, 2026: BULB. INOPERATIVE. ENTRY HATCH EMERGENCY EXIT LIGHT HAS MULTIPLE BULBS INOPERATIVE. RELAMPED ENTRY HATCH EMERGENCY EXIT SIGN IAW AMM 33-51-01-962-001. OP'S CHECKED GOOD. - [SDR IPXA2025061664053](https://openairdocs.org/sdr/IPXA2025061664053), May 24, 2025: STRINGER. CORRODED. AFT CARGO BILGE AREA AT STRG 28L HAS CORROSION AT STA 1466. FOUND DURING DVI ATA 53-05 ACCOMPLISHED REPAIR PER EO-94038-REQ1 AND VT-SAA EA 757-5360-01-B0497, RE - [SDR IPXA2025061264053](https://openairdocs.org/sdr/IPXA2025061264053), May 24, 2025: STRINGER. CORRODED. AFT CARGO BILGE AREA AT STRG 28L HAS CORROSION AT STA 1466. FOUND DURING DVI. - [SDR IPXA2025061030265](https://openairdocs.org/sdr/IPXA2025061030265), May 22, 2025: RETAINER. INOPERATIVE. FLIGHT DECK CEILING RUBBER CABLE RETAINER FOR DESCENT DEVICE IS DIS-BONDED ATA 25-61 MARKED 84-40. RE BONDED FLIGHT DECK CEILING RUBBER CABLE RETAINER IAW DWG N - [SDR IPXA2025052330265](https://openairdocs.org/sdr/IPXA2025052330265), May 22, 2025: ESCAPE REEL. DAMAGED. FLIGHT DECK CEILING RUBBER CABLE RETAINER FOR DESCENT DEVICE IS DIS-BONDED. - [SDR IPXA2025061664937](https://openairdocs.org/sdr/IPXA2025061664937), May 19, 2025: STRINGER. CORRODED. FUSELAGE STA 1473 SUSPECTED CORROSION ON SKIN REPAIRED AT CTR VHF ANTENNA AREA TRIPLER METAL PLATE HAS BULGING AND 01EA FASTENER HEAD IS OUT ON METAL PLATE HOLE - [SDR IPXA2025061365070](https://openairdocs.org/sdr/IPXA2025061365070), May 19, 2025: SKIN. CORRODED. MAJOR REPAIR, BOTTOM FUSELAGE STA 1600-1620 SUSPECTED CORROSION ON EXTERNAL SURFACE SKIN HAS BULGING AND FASTENER HEADS FULL THROUGH. - [SDR IPXA2025061264937](https://openairdocs.org/sdr/IPXA2025061264937), May 19, 2025: SKIN. CORRODED. SUSPECTED CORROSION ON SKIN REPAIRED AT CTR VHF ANTENNA AREA TRIPLER METAL PLATE HAS BULGING AND 01EA FASTENER HEAD IS OUT ON METAL PLATE HOLE AS MARKED. 74-002 - [SDR IPXA2023051393219](https://openairdocs.org/sdr/IPXA2023051393219), May 5, 2023: SHEAR TIE. DENTED. INSPECTION TYPE:CK21*MAJOR REPAIR* FRAME STA 1240 RH SIDE AT STR26R HAS A DENTFRAME WAS REPAIRED IAW 757-200PF SRM REV 116.0 CHAPTER 53-00-07-2R DETAIL V PER SR - [SDR IPXA2023030691583](https://openairdocs.org/sdr/IPXA2023030691583), Mar 5, 2023: NONE. INOPERATIVE. INSPECTION TYPE:NA*DIVERSION* APPROX 1 HR INTO THE FLT AT FL400, ENG FLUCTUATIONS WERE OBSRVD ON BTH ENG. LFT 1ST, THN RT, FLLWED BY RT AGAIN APPROX 30 MINS LTE - [SDR IPXA2021090733527](https://openairdocs.org/sdr/IPXA2021090733527), Sep 3, 2021: WARNING MESSAGE. FALSE ACTIVATION. ATB - VNAV AND AUTOPILOT RETURNED AT 6000FT, BUT NOTICED LE SLAT DISGREE ON EICAS. WENT THROUGH CHECKLIST AND GOT 20 DEGREES AND LANDED. AUTOPILOT WAS NORMALREF - [SDR IPXA2021052569806](https://openairdocs.org/sdr/IPXA2021052569806), May 25, 2021: FRAME. DENTED. INSPECTION TYPE:SEGTHE FRAME AT STA 780 L/H SODE STR 23 HAS A DENT ON THE UPPER SURFACE LOCATED IN THE FWD CARGO AREA NO DOTREPAIR ACCOMPLISHED PER SRM 53-00-07 - [SDR IPXA2021052269692](https://openairdocs.org/sdr/IPXA2021052269692), May 22, 2021: SKIN. DELAMINATED. INSPECTION TYPE:SEGDELAMINATION ON TAIL CONEREPAIRED PANEL IAW B757 SRM 51-70-10-2R-2 350 DEG F CURE PER SRM 53-80-01-2R, FIG 201 - [SDR IPXA2021052269691](https://openairdocs.org/sdr/IPXA2021052269691), May 22, 2021: SKIN. DELAMINATED. INSPECTION TYPE:SEGDELAMINATION ON TAIL CONEREPAIRED PANEL IAW B757 SRM 51-70-10-2R-2 350 DEG F PER SRM 53-80-01-2R, FIG 201 - [SDR IPXA2021051569407](https://openairdocs.org/sdr/IPXA2021051569407), May 15, 2021: FLOOR PANEL. DAMAGED. INSPECTION TYPE:SEGMAIN CARGO COMPARTMENT FLOOR PANEL 231XTF DELAMINATEDFABBED PANEL 231 XTF FROM 5024N400001SS-G, BATCH# PER SREO B757-5320-9692-K - [SDR IPXA2021020965502](https://openairdocs.org/sdr/IPXA2021020965502), Feb 7, 2021: SEAL. LEAKING. INSPECTION TYPE:N/ALOUD SQUEAL ENTRY DOOR OPERATING HANDLE FL360 CABIN ALTITUDE 6,000 DIFFENTIAL 8.4FOUND PRESSURE SEAL DAMAGE REPAIRED IAW MM 52-09-00 PG BLOCK - [SDR IPXA201906143238](https://openairdocs.org/sdr/IPXA201906143238), Jun 13, 2019: STRUCTURE. DAMAGED. INSPECTION TYPE:SEG3DURING REMOVAL OF DENT ON NR 115828 FOUND DAMAGE TO CHORD UNDERNEATH.REPAIRED PER RCD# 116143 UPS EO # B757-5310-72739-A AND VTMAE EA #757-5 - [SDR IPXA201906143241](https://openairdocs.org/sdr/IPXA201906143241), Jun 13, 2019: PANEL. CRACKED. INSPECTION TYPE:SEG3LH WING DRY BAY PNL 532DZ IS DAMAGED.REPAIRED PER RCD #116169. - [SDR IPXA201906143237](https://openairdocs.org/sdr/IPXA201906143237), Jun 13, 2019: SKIN. DENTED. INSPECTION TYPE:SEG3REF DI D607396 LH FUSELAGE NOSE SECTION STA 215 WK 210 SKIN GOUGE.REPAIRED PER RCD 115825 UPS EO B757-5330-72671-A & VT MAE EA 757-5310-27-A - [SDR IPXA2019061243080](https://openairdocs.org/sdr/IPXA2019061243080), Jun 10, 2019: PANEL. DELAMINATED. INSPECTION TYPE:1C PANEL DELAMINATED. REPAIRED PER SRM 57-20-09-2R, 51-70-07-OG. - [SDR IPXA2019061082988](https://openairdocs.org/sdr/IPXA2019061082988), Jun 8, 2019: FLOOR SKIN. DELAMINATED. INSPECTION TYPE:SEG3FLOOR PANEL 211X AF IS DELAMINATEDFABRICATED NEW PANEL FROM 5024N40000I55-G, BATCH#3489461 PER SREO B757-5320-9692-K - [SDR IPXA2019061082990](https://openairdocs.org/sdr/IPXA2019061082990), Jun 8, 2019: FLOOR PANEL. DELAMINATED. INSPECTION TYPE:SEG3MCD FLOOR PANEL 232XJF IS DELAMINATEDFABRICATED FROM5024N40000ISS-G PER SREO B757-5320-9692-K - [SDR IPXA2019061072964](https://openairdocs.org/sdr/IPXA2019061072964), Jun 7, 2019: FLOOR PANEL. DELAMINATED. INSPECTION TYPE:SEG3 MCD FLOOR PANEL 232XHF IS DELAMINATEDFABRICATED FROM 5024N40000ISS-G PER SREO B757-5320-9692-K - [SDR IPXA2019061072963](https://openairdocs.org/sdr/IPXA2019061072963), Jun 7, 2019: FLOOR PANEL. DELAMINATED. INSPECTION TYPE:SEG3 MCD FLOOR PANEL 232XDF IS DELAMINATEDFABRICATED FROM 5024N40000ISS-G PER SREO B757-5320-9692-K - [SDR IPXA2019061072962](https://openairdocs.org/sdr/IPXA2019061072962), Jun 7, 2019: FLOOR PANEL. DELAMINATED. INSPECTION TYPE:SEG3MCD FLOOR PANEL 231XDF IS DELAMINATEDFABRICATED FROM 5024N40000ISS-G PER SREO B757-5320-9692-K - [SDR IPXA2019061072961](https://openairdocs.org/sdr/IPXA2019061072961), Jun 7, 2019: FLOOR PANEL. DELAMINATED. INSPECTION TYPE:SEG3, MCD FLOOR PANEL 231XEF IS DELAMINATEDFABRICATED FROM 5024N40000ISSG IAW SREO B757-5320-9692-K - [SDR IPXA2019061072960](https://openairdocs.org/sdr/IPXA2019061072960), Jun 7, 2019: FLOOR PANEL. DELAMINATED. INSPECTION TYPE:SEG, 3MCD FLOOR PANEL 232XDF IS DELAMINATED. FABRICATED FROM 5024N40000ISS-G PER SREO B757-5320-9692-K - [SDR IPXA2019061072959](https://openairdocs.org/sdr/IPXA2019061072959), Jun 7, 2019: FLOOR PANEL. DELAMINATED. INSPECTION TYPE:SEG3MCD FLOOR PANEL 231XFF IS DELAMINATEDFABRICATED FROM 5024N40000ISS-G PER SREO B757-5320-9692-K - [SDR IPXA2019061072958](https://openairdocs.org/sdr/IPXA2019061072958), Jun 7, 2019: FLOOR PANEL. DELAMINATED. INSPECTION TYPE:SEG3, MCD FLOOR PANEL 212XAF IS DELAMINATED, FABRICATED FROM 5024N4000ISS-G PER SREO B757-5320-9692-K - [SDR IPXA2019061072957](https://openairdocs.org/sdr/IPXA2019061072957), Jun 7, 2019: FLOOR PANEL. DELAMINATED. INSPECTION TYPE:SEG3, MCD FLOOR PANEL 231XHF IS DELAMINATED. FABRICATED FROM 5024N40000ISS-G PER SREO B757-5320-9692-K. - [SDR IPXA2019061072955](https://openairdocs.org/sdr/IPXA2019061072955), Jun 7, 2019: FLOOR PANEL. DELAMINATED. INSPECTION TYPE:SEG3, MCD FLOOR PANEL 231XJF IS DELAMINATED. FABRICATED FROM 5024N40000ISS-G PER SREO B757-5320-9692-K. - [SDR IPXA2019060742954](https://openairdocs.org/sdr/IPXA2019060742954), Jun 7, 2019: FLOOR PANEL. DELAMINATED. INSPECTION TYPE:SEG3 MCD FLOOR PANEL 232XGF IS DELAMINATEDFABRICATED FROM 5024N40000ISS-G PER SREO B757-5320-9692-K - [SDR IPXA2019060752880](https://openairdocs.org/sdr/IPXA2019060752880), Jun 5, 2019: STRUCTURE. DELAMINATED. INSPECTION TYPE:SEG3, TRAILING EDGE DELAMINATION WITH VOIDS OF SEALANT. REMOVED RIVETS ALONG TRAILING EDGE APPLIED SEALANT IN VOIDED AREA AND REINSTALLED RIVETS - [SDR IPXA2019060752879](https://openairdocs.org/sdr/IPXA2019060752879), Jun 5, 2019: SHAFT. DEFORMED. INSPECTION TYPE:SEG3, ROLLER RAIL SHAFTS DEFORMED AND DAMAGEDREMOVED AND REPLACED IAW ANCRA MM 25-50-79 - [SDR IPXA2019060752878](https://openairdocs.org/sdr/IPXA2019060752878), Jun 5, 2019: ROLLER. BENT. INSPECTION TYPE:SEG3, LOCKS HAVE CORROSION AND BENT ROLLERS. REMOVED AND REPLACED IAW MM 25-50-79 AND IPC 25-56-00-01 - [SDR IPXA2019060752877](https://openairdocs.org/sdr/IPXA2019060752877), Jun 5, 2019: HEAT SHIELD. DELAMINATED. INSPECTION TYPE:SEG3DELAMINATION/DISBONDS ON MULTIPLE AREASREMOVED AND REPLACED - [SDR IPXA2019060752876](https://openairdocs.org/sdr/IPXA2019060752876), Jun 5, 2019: ANGLE. CRACKED. INSPECTION TYPE:SEG3, ANGLE CRACKED, REMOVED AND REPLACED IAW SRM 51-40-02 - [SDR IPXA2019060752875](https://openairdocs.org/sdr/IPXA2019060752875), Jun 5, 2019: THRESHOLD. CRACKED. INSPECTION TYPE:SEG3, THRESHOLD PLATE CRACKED IN SEVERAL PLACES WELDED AND INSPECTED PER EO B757-5320-35929-C - [SDR IPXA2019060542873](https://openairdocs.org/sdr/IPXA2019060542873), Jun 5, 2019: SKIN. CORRODED. INSPECTION TYPE: SEG3 LOWER SKIN CORRODED OUT OF MANUFACTURERS LIMITS. LOWER SKIN REPLACED BY FABRICATING NEW SKIN PER EO M-2550-11648-0. - [SDR IPXA2019060542872](https://openairdocs.org/sdr/IPXA2019060542872), Jun 5, 2019: SKIN. CORRODED. INSPECTION TYPE:SEG3LOWER SKIN CORRODED OUT OF MANUFACTURERS LIMITS.LOWER SKIN REPLACED BY FABRICATING A NEW SKIN PER EO M-2550-11648-0 - [SDR IPXA2019060542871](https://openairdocs.org/sdr/IPXA2019060542871), Jun 5, 2019: SKIN. CORRODED. INSPECTION TYPE: SEG3 LOWER SKIN CORRODED OUT OF MANUFACTURERS LIMITS. LOWER SKIN REPLACED BY FABRICATING NEW SKIN PER EO M-2550-11648-0 - [SDR IPXA2019060542870](https://openairdocs.org/sdr/IPXA2019060542870), Jun 5, 2019: SKIN. CORRODED. INSPECTION TYPE: SEG3 LOWER SKIN CORRODEDD OUT OF MANUFACTURERS LIMITS. LOWER SKIN REPLACED BY FABRICATING NEW SKIN PER EO M-2550-11648-0 - [SDR IPXA2019060542869](https://openairdocs.org/sdr/IPXA2019060542869), Jun 5, 2019: SKIN. CORRODED. INSPECTION TYPE:SEG3 LOWER SKIN CORRODED OUT OF MANUFACTURERS LIMITS. LOWER SKIN REPLACED BY FABRICATING NEW SKIN PER EO M-2550-11648-0 - [SDR IPXA2019060542866](https://openairdocs.org/sdr/IPXA2019060542866), Jun 5, 2019: SKIN. CORRODED. INSPECTION TYPE:SEG3 LOWER SKIN CORRODED OUT OF MANFACTURES LIMITS LOWER SKIN REPLACED BY FABRICATING A NEW SKIN PER EO M-2550-11648-0 - [SDR IPXA2019060542865](https://openairdocs.org/sdr/IPXA2019060542865), Jun 5, 2019: PIN. DEFORMED. INSPECTION TYPE: SEG3 PIN DAMAGED BEYOND MANUFACTURES LIMITS REPLACED WITH NEW PIN ASSY PER ANCRA MM 25-50-79 - [SDR IPXA201906052806](https://openairdocs.org/sdr/IPXA201906052806), Jun 4, 2019: SKIN. DENTED. INSPECTION TYPE:SEG3 - LH FUSELAGE NOSE SECTION SKIN AT STA 239, W.L. 210 REMOVED FASTNERS COMON TO DENT, ROTO PROBED HOLES REPLACED FASTNERS, RESTORED FINISHES All 223: https://openairdocs.org/aircraft/N403UP/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 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.