# N428UP: 1992 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: 25459 - Year built: 1992 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: September 10, 1992 - Certificate issued: October 13, 1992 - Expires: August 31, 2028 - Mode S code: A51B27 - 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=428UP - Page: https://openairdocs.org/aircraft/N428UP 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 N428UP. ## FAA accident and incident reports None matched to N428UP. ## Service difficulty reports (163, 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 IPXA2026101440497](https://openairdocs.org/sdr/IPXA2026101440497), Oct 14, 2026: A/C PACK. NO DISCREPANCY. STRONG FUMES WHEN RUNNING RT PACK. RAN ENGINES AT POWER. NO ODOR NOTED IAW AMM 05-51-56. - [SDR IPXA2026061695676](https://openairdocs.org/sdr/IPXA2026061695676), Jun 16, 2026: NUT PLATE. CORRODED. AFT OF BULK CARGO COMPARTMENT SUPPORT ANGLE, NUT PLATE STRAP HAS CORROSION APPROX AT BS 1715, BTW BL 0 AND RBL 9. - [SDR IPXA2026070896552](https://openairdocs.org/sdr/IPXA2026070896552), May 3, 2026: FITTING. GOUGED. DURING RIG CHECK OF THE RH AFT INBD FLAP (MAIN FLAP IN EXTENDED POSTION), AFT FLAP INBD TRACK ROLLER ATTACH FITTING OUTBD FACE FOUND WITH GOUGE DAMAGE. INSTALLE - [SDR IPXA2026051415340](https://openairdocs.org/sdr/IPXA2026051415340), Apr 15, 2026: SKIN. GOUGED. RIGHT LOWER FUSELAGE EXTERNAL SKIN, EXIST. REPAIR DOUBLER HAS A TOOLING MARK APPROX BTW BS 480 AND BS 500, BTW STGR 22R AND STGR 23R, REMOVED AND REPLACED EXIST - [SDR IPXA2026051117931](https://openairdocs.org/sdr/IPXA2026051117931), Apr 15, 2026: PANEL. CORRODED. AFT CARGO COMPARTMENT FLOOR STRUCTURE SIDE PANEL HAS CORROSION AND MULTIPLE DENTS, APPROX BTW BS 1440 AND BS1480, RBL 24, INSTALLED PANEL-TRANSITION AT AFT CARG - [SDR IPXA2026051113328](https://openairdocs.org/sdr/IPXA2026051113328), Apr 15, 2026: FLOOR SUPPORT. CRACKED. FWD CARGO CENTER FLOOR STRINGER UPPER FLANGE BENT AT BS 820. REFORMED UPPER FLANGE FLOOR STRINGER AT FWD CARGO STA 820 LBL 2.90 IAW B757-200PF SRM 51-00-05-0G-0 - [SDR IPXA2026042119590](https://openairdocs.org/sdr/IPXA2026042119590), Apr 15, 2026: NUT PLATE. CORRODED. AFT OF BULK CARGO COMPARTMENT SUPPORT ANGLE, NUT PLATE STRAP HAS CORROSION APPROX AT BS 1715, BTW LBL 20 AND LBL 24. INSTALLED FARBRICATED - 14. NUTPLATE-ASSY A - [SDR IPXA2026042119036](https://openairdocs.org/sdr/IPXA2026042119036), Apr 15, 2026: SUPPORT ANGLE. CORRODED. AFT OF BULK CARGO COMPARTMENT SUPPORT ANGLE, NUT PLATE STRAP HAS CORROSION APPROX AT BS 1715, BTW BL 0 AND RBL 9, ID STICKER NUM. (085-033). ATA 53-20. INSTALLE - [SDR IPXA2026042517931](https://openairdocs.org/sdr/IPXA2026042517931), Apr 15, 2026: SIDEWALL PANEL. CORRODED. AFT CARGO COMPARTMENT FLOOR STRUCTURE SIDE PANEL HAS CORROSION AND MULTIPLE DENTS, APPROX BTW BS 1440 AND BS1480, RBL 24, - [SDR IPXA2026042313853](https://openairdocs.org/sdr/IPXA2026042313853), Apr 15, 2026: FLOOR SUPPORT. CORRODED. MAIN DECK CABIN FLOOR STRUCTURE, BS 900 - 1080, LBL 45.5 - 54.9 CORRODED, REMOVED CORROSION ON MAIN DECK CABIN FLOOR STRUCTURE FROM STA. 900-1080 AND LBL 45.5 T - [SDR IPXA2026061700388](https://openairdocs.org/sdr/IPXA2026061700388), Apr 14, 2026: ROD. CORRODED. RH HORIZONTAL STABILIZER O/B ELEVATOR PCU INPUT ROD AFT CLEVIS IS RUSTED AND HAS 1EA CORRODED NUT AND SAFETY WIRE ATA 55-10 MARKED 84-14 INSTALLED NEW RH-HORIZ- - [SDR IPXA2026070694500](https://openairdocs.org/sdr/IPXA2026070694500), Apr 14, 2026: SKIN. GOUGED. RIGHT APU DOOR 316AR SKIN HAS A MULTIPLE GOUGE AT LWR/AFT CORNER APPROX BTW BS 1941 AND BS 1963.8, INSTALLED FABRICATED PLATE (REPAIR DOUBLER) AT RT APU DOOR 31 - [SDR IPXA2026070694554](https://openairdocs.org/sdr/IPXA2026070694554), Apr 14, 2026: SKIN. DENTED. RIGHT APU DOOR 316AR SKIN HAS A MULTIPLE DENTS APPROX BTW BS 1918 AND BS 1941. INSTALLED -1,-2 & -3 REPAIR PARTS IAW SRM 52-40-01-2R-40FIG 201 AND SRM 51-20-01- - [SDR IPXA2026042300388](https://openairdocs.org/sdr/IPXA2026042300388), Apr 14, 2026: CLEVIS. CORRODED. RIGHT HORIZONTAL STAB OTBD ELEVATOR PCU INPUT ROD AFT CLEVIS IS RUSTED AND HAS ONE CORRODED NUT & SAFETY WIRE. - [SDR IPXA2026090479144](https://openairdocs.org/sdr/IPXA2026090479144), Apr 13, 2026: ACCESS PANEL. CORRODED. FWD, LT LOWER WTB PANEL LANDING INSIDE ACCESS PANEL 193AL HAS SURFACE CORROSION. - [SDR IPXA2026090479384](https://openairdocs.org/sdr/IPXA2026090479384), Apr 13, 2026: STRUCTURE. CORRODED. LEFT AFT WTB FAIRING STRUCTURE LOWER CHORD AT APRROX. BS 1200 - 1220 HAS EXFOLIATION CORROSION. - [SDR IPXA2026051179384](https://openairdocs.org/sdr/IPXA2026051179384), Apr 13, 2026: ANGLE. CORRODED. LH, AFT WTB FAIRING STRUCTURE LOWER CHORD AT APRROX. STA 1200 TO 1220 HAS EXFOLIATION CORROSION. INSTALLED LWR CHORD AT LH AFT WTB FAIRING STRUCTURE BEAM ASSY B - [SDR IPXA2026051179310](https://openairdocs.org/sdr/IPXA2026051179310), Apr 13, 2026: FRAME. CORRODED. LH, AFT WTB FAIRING STRUCTURE CHORD AT APRROX. STA 1220 HAS CORROSION. INSTALLED CHORD FRAME AT LH AFT WTB FAIRING STRUCTURE STA 1220, BL 57-50 I.A.W. B757-200P - [SDR IPXA2026051179144](https://openairdocs.org/sdr/IPXA2026051179144), Apr 13, 2026: FAIRING. CORRODED. FWD, LH LOWER WTB PANEL LANDING INSIDE ACCESS PNL 193AL HAS SURFACE CORROSION. STICKER #83-003. ATA 53-30. REMOVED 1EA CORRODED WEB FROM INTERCOSTAL ASSY. INSTA - [SDR IPXA2026051179388](https://openairdocs.org/sdr/IPXA2026051179388), Apr 13, 2026: FAIRING. CORRODED. LH, AFT WTB FAIRING STRUCTURE FRAME AT APRROX. STA 1200 TO 1220 HAS EXFOLIATION CORROSION. 83-005. ATA 53-30. INSTALLED WEB AND REINSTALLED (1EA) LIGHT SUPPORT - [SDR IPXA2026042579388](https://openairdocs.org/sdr/IPXA2026042579388), Apr 13, 2026: FRAME. CORRODED. LEF AFT WTB FAIRING STRUCTURE FRAME AT APRROX. BS 1200 - 1220 HAD EXFOLIATION CORROSION. - [SDR IPXA2026042579310](https://openairdocs.org/sdr/IPXA2026042579310), Apr 13, 2026: STRUCTURE. CORRODED. LEFT AFT WTB FAIRING STRUCTURE CHORD AT APRROX. BS 1220 WAS CORRODED. - [SDR IPXA2026042579144](https://openairdocs.org/sdr/IPXA2026042579144), Apr 13, 2026: ACCESS PANEL. CORRODED. FWD, LT LOWER WTB PANEL LANDING INSIDE ACCESS PANEL 193AL HAS SURFACE CORROSION. - [SDR IPXA2026042579384](https://openairdocs.org/sdr/IPXA2026042579384), Apr 13, 2026: STRUCTURE. CORRODED. LEFT AFT WTB FAIRING STRUCTURE LOWER CHORD AT APRROX. BS 1200 - 1220, HAS EXFOLIATION CORROSION. - [SDR IPXA2026051147252](https://openairdocs.org/sdr/IPXA2026051147252), Apr 11, 2026: ANGLE. CORRODED. R/H HORZ STAB TIP REAR SPAR AND ELEVATOR FRONT SPAR BONDING STRAP ATTACH BRACKETS INCLUDING BONDING STRAPS HAVE CORROSION. INSTALLED 1 EA NEW ANGLE P/N 183N1341 - [SDR IPXA2026051147230](https://openairdocs.org/sdr/IPXA2026051147230), Apr 11, 2026: ANGLE. CORRODED. L/H HORZ STAB TIP REAR SPAR AND ELEVATOR FRONT SPAR BONDING STRAP ATTACH BRACKETS INCLUDING BONDING STRAPS HAVE CORROSION. RL003 INSTALLED 1 EA NEW ANGLE 1 EA N - [SDR IPXA2026051147853](https://openairdocs.org/sdr/IPXA2026051147853), Apr 11, 2026: SKIN. CORRODED. RIGHT HORIZONTAL STAB UPPER SURFACE SKIN HAS LIGHT CORROSION UNDER BUBBLED UP PAINT AREAS NEXT TO UPPER SLIDING FAIRING. ACCOMPLISH REPAIR PER EO-97446-REQ1 AND - [SDR IPXA2026042547252](https://openairdocs.org/sdr/IPXA2026042547252), Apr 11, 2026: SPAR. CORRODED. RIGHT HORIZONTAL STAB TIP REAR SPAR AND ELEVATOR FRONT SPAR BONDING STRAP ATTACH BRACKETS INCLUDING BONDING STRAPS HAD CORROSION. - [SDR IPXA2026043047230](https://openairdocs.org/sdr/IPXA2026043047230), Apr 11, 2026: SPAR. CORRODED. LEFT HORIZONTAL STAB TIP REAR SPAR AND ELEVATOR FRONT SPAR BONDING STRAP ATTACH BRACKETS INCLUDING BONDING STRAPS HAVE CORROSION. - [SDR IPXA2026020247576](https://openairdocs.org/sdr/IPXA2026020247576), Jan 30, 2026: HANDLE. BROKEN. CREW ENTRY WAY ASSIST HANDLE BROKEN. REPLACED THE CREW ENTRYWAY ASSIST HANDLE IAW IPC 52-12-51-01. - [SDR IPXA2025061258372](https://openairdocs.org/sdr/IPXA2025061258372), Jun 11, 2025: EVAS UNIT. ABNORMAL. **SUPPLEMENTAL SDR** CAPTAINS EVAS TEST TOOL MISSING. INSTALLED EVAS TOOL FOR CAPTAIN'S EVAS IAW AMM 25-69-00. OPS CHECK GOOD. REMOVED FROM NEF. - [SDR IPXA2025061158372](https://openairdocs.org/sdr/IPXA2025061158372), Jun 11, 2025: EVAS UNIT. ABNORMAL. CAPTAINS EVAS TEST TOOL MISSING - [SDR IPXA2025022507366](https://openairdocs.org/sdr/IPXA2025022507366), Feb 18, 2025: LAMP. INOPERATIVE. **SUPPLEMENTAL SDR**EMERGENCY EXIT LIGHT DIM RELAMPED EMERGENCY EXIT SIGN PER AMM TASK 33-51-01-962-001. OPS COS NORMAL. THIS CLEARS AUTH:2837083. PLACARD REMOV - [SDR IPXA2025021907366](https://openairdocs.org/sdr/IPXA2025021907366), Feb 18, 2025: LIGHT. MALFUNCTIONED. EMERGENCY EXIT LIGHT DIM 11 LIGHT BULBS INOP. ORDERED PARTS, DEFERRED IAW MEL 33-51-1-1. PLACARD INSTALLED OPEN - [SDR IPXA2024052015249](https://openairdocs.org/sdr/IPXA2024052015249), May 4, 2024: CAM. OUT OF LIMITS. FAULT: FOUND LOWER CREW ENTRY DOOR LATCH CAM OUT OF LIMITS. LATCH CAM P/N: 141N6531-3 S/N: TAGEK3759A IT IS EFFECTIVE FOR A/C: N428UP I.A.W. B757 ICP: 52-12-01- - [SDR IPXA2024052030020](https://openairdocs.org/sdr/IPXA2024052030020), Apr 29, 2024: LATCH. WORN. LOWER CREW ENRTY DOOR LATECH WORN. DOT 140-012. FOUND 1 LATCH OUT OF LIMITS IAW SREO B757-SREO 14721 REQ 001 SRM 51-10-02. AND CONTINUE TO REQUEST A NEW ONE AND - [SDR IPXA2024043030020](https://openairdocs.org/sdr/IPXA2024043030020), Apr 29, 2024: LATCH. WORN. LOWER CREW ENRTY DOOR LATCH WORN. - [SDR IPXA2024011623818](https://openairdocs.org/sdr/IPXA2024011623818), Jan 13, 2024: LIGHT. DAMAGED. EMERGENCY LIGHT UNARMED IND LENS, BULB REAINER DAMAGED. R&R AMM33-16-02-002 - [SDR IPXA2023121930291](https://openairdocs.org/sdr/IPXA2023121930291), Dec 15, 2023: BOOT. DAMAGED. DAMAGE ON RADOME BOOT **10 FLT HOUR ** R&R RADOME I/A/W AMM 53-12-01-902-008. - [SDR IPXA2023121530291](https://openairdocs.org/sdr/IPXA2023121530291), Dec 15, 2023: UNKNOWN. UNKNOWN. *SDR FILED OPEN* DAMAGE ON RADOME BOOT **10 FLT HOUR ** DEFERRED RADOME BOOT DAMAGE PER SREO-12211-REQ002 ALTERNATE REPAIR. - [SDR IPXA2023112189904](https://openairdocs.org/sdr/IPXA2023112189904), Nov 8, 2023: SKIN. DAMAGED. FUSELAGE SKIN HAS A BURN HOLE AT B STA 462 APPROX 2" ABOVE S-8R MEASURING 0.011" DEEP AND 0.060" IN DIAMETER. UPON FURTHER INSPECTION FOUND DAMAGE TO WITHIN LIM - [SDR IPXA2023110889941](https://openairdocs.org/sdr/IPXA2023110889941), Nov 8, 2023: UNKNOWN. UNKNOWN. FUSELAGE SKIN HAS A BURN HOLE AT B STA 488 APPROX 4" ABOVE S-14R MEASURING 0.047" DEEP AND 0.084" IN DIAMETER. - [SDR IPXA2023110889904](https://openairdocs.org/sdr/IPXA2023110889904), Nov 8, 2023: UNKNOWN. UNKNOWN. *SDR FILED OPEN* FUSELAGE SKIN HAS A BURN HOLE AT B STA 462 APPROX 2" ABOVE S-14R MEASURING 0.011" DEEP AND 0.060" IN DIAMETER. - [SDR IPXA2023080932999](https://openairdocs.org/sdr/IPXA2023080932999), Aug 9, 2023: ANTI-SKID SYS. WARNING MESSAGE. *DIVERSION* THE ANTISKID SYSTEM IN OPERATION (NORMAL + ALTERNATE) HAS A FAILURE. ANTISKID EICAS ADVISORY MESSAGE ILLUMINATED DURING CRUISE. C/W FIM 32-42 FAULT - [SDR IPXA2022071584195](https://openairdocs.org/sdr/IPXA2022071584195), Jul 15, 2022: WINDOW. INOPERATIVE. INSPECTION TYPE:N/A**ATB**F/O SIDE WINDOW OPENED UP DURING T.O. TRIED TO CLOSE RAN QRC CLD NOT GET CLOSED. NOISE MADE COMAN VERY DIFFICUTT DECLARED EMERG RETURN - [SDR IPXA2022041981306](https://openairdocs.org/sdr/IPXA2022041981306), Apr 19, 2022: NONE. CORRODED. INSPECTION TYPE:SEG4MAIN CARGO DECK BS 1200 RBL 38, FLOORBEAM LOWER SIDE OF UPPER FLANGE CORRODEDREPAIR PER 757-200PF REV 113.00, 53-00-51-2R-6 DETAIL III PER S - [SDR IPXA2022042581457](https://openairdocs.org/sdr/IPXA2022042581457), Apr 18, 2022: STRAP. CORRODED. INSPECTION TYPE:CCORROSION FOUND AT APU INLET DOOR CUTOUT FRAME AT STA 1825-00REPAIRED PER 757-200PF REV 113.00 CHAPTER 53-80-15-2R-1 - [SDR IPXA2022041881275](https://openairdocs.org/sdr/IPXA2022041881275), Apr 10, 2022: SKIN. DEBONDED. INSPECTION TYPE:16/4PER EO B757-5350-20611-C PERFORMED TAP TEST OF PREVIOUS REPAIR AND FOUND DISBOND CONDITION L/H SIDE AT BW 1920-1935 INSIDE APU COMPARTMENTRE - [SDR IPXA2022041881273](https://openairdocs.org/sdr/IPXA2022041881273), Apr 10, 2022: SKIN. DELAMINATED. INSPECTION TYPE:16/4AFT TAIL UPPER SKIN AT STA 1945, BL-0 HAS A DENT IN THE SKIN. DENT DELAMINATEDREPAIRED PANEL IAW B757 SRM 51-70-10-2R REPAIR 2 - [SDR IPXA2022042581469](https://openairdocs.org/sdr/IPXA2022042581469), Apr 7, 2022: FRAME. DENTED. INSPECTION TYPE:SEG4AFT CARGO COMPARTMENT STA 1280 R/H FRAME HAS A DENT ON UPPER SURFACE BELLOW S-26RREPAIRED PER 757-200PF REV 113.00 53-00-07-2R6 DETAIL VI PE All 163: https://openairdocs.org/aircraft/N428UP/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.