# N453UP: 1995 Boeing 757-24APF

- Status: Valid registration
- Airframe: [Boeing 757-24APF](https://openairdocs.org/model/boeing-757-24apf) (registry code 1384969, 178 seats)
- Engine: [Rolls-Royce RB211-535E4 series](https://openairdocs.org/engine/rolls-royce-rb211-535e4-series) (registry code 54223)
- Data sheets: [TCDS E12EU](https://openairdocs.org/tcds/E12EU) (Rolls-Royce Deutschland Ltd & Co KG) (OpenAirDocs)
- Serial number: 25474
- Year built: 1995
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 31, 2007
- Certificate issued: August 11, 1995
- Expires: February 29, 2028
- Mode S code: A57F11
- 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=453UP
- Page: https://openairdocs.org/aircraft/N453UP

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. The registry lists only the engine series, so ADs for every Rolls-Royce RB211-535E4 model are included.

## ADs that may apply (OpenAirDocs): 20 in force

### Matched by airframe (Boeing 757-24APF)

None in force.

### Matched by engine (Rolls-Royce RB211-535E4 series)

- [AD 2024-10-06](https://openairdocs.org/ad/2024-10-06): Engine (Turbine/Turboprop) · Rolls-Royce Deutschland RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-C-37. Effective Jun 27, 2024
- [AD 2020-08-03](https://openairdocs.org/ad/2020-08-03): Turbine Engine Compressor Section · Rolls-Royce Deutschland RB211-535E4-37, RB211-535E4-B-37, RB211-535E4-B-75 and 1 more. Effective May 18, 2020
- [AD 2017-24-08](https://openairdocs.org/ad/2017-24-08): Fuel control/Turbine engines · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-C-37. Effective Jan 16, 2018
- [AD 2016-03-04](https://openairdocs.org/ad/2016-03-04): Life-limited rotating parts · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-C-37. Effective Mar 15, 2016
- [AD 2013-23-17](https://openairdocs.org/ad/2013-23-17): High-pressure (HP) and intermediate-pressure (IP) turbine discs · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37, RB211-535E4-C-37 and 3 more. Effective Dec 11, 2013
- [AD 2013-16-23](https://openairdocs.org/ad/2013-16-23): Cracked and distorted FCL metering panel · Rolls-Royce RB211-524B-02, RB211-524B2-19, RB211-524B3-02 and 13 more. Effective Oct 8, 2013
- [AD 2012-25-09](https://openairdocs.org/ad/2012-25-09): Intermediate-pressure (IP) turbine discs · Rolls-Royce RB211-524G2-19, RB211-524G2-T-19, RB211-524G3-19 and 10 more. Effective Feb 6, 2013
- [AD 2012-02-11](https://openairdocs.org/ad/2012-02-11): LP turbine stage 1, 2, and 3 discs · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37, RB211-535E4-B-75 and 1 more. Effective Mar 6, 2012
- [AD 2009-20-14](https://openairdocs.org/ad/2009-20-14): Eddy current inspection (ECI) · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Nov 17, 2009
- [AD 2008-20-04](https://openairdocs.org/ad/2008-20-04): HP turbine discs · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 26 more. Effective Nov 3, 2008
- [AD 2006-11-05 R2](https://openairdocs.org/ad/2006-11-05-R2): High pressure compressor (HPC) · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 27 more. Effective Feb 21, 2008
- [AD 2007-14-07](https://openairdocs.org/ad/2007-14-07): Fluorescent penetrant inspections (FPI) · Rolls-Royce RB211-524B-02, RB211-524B-B-02, RB211-524B2-19 and 21 more. Effective Aug 16, 2007
- [AD 2006-17-12](https://openairdocs.org/ad/2006-17-12): High pressure (HP) turbine discs · Rolls-Royce RB211-22B-02, RB211-535C-37, RB211-535E4-37 and 3 more. Effective Sep 27, 2006
- [AD 2004-19-04](https://openairdocs.org/ad/2004-19-04): Critical Life-Limited Rotating Engine Parts · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 27 more. Effective Nov 1, 2004
- [AD 2004-01-21](https://openairdocs.org/ad/2004-01-21): Frount engine mount housing · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 27 more. Effective Feb 27, 2004
- [AD 2003-10-03 R1](https://openairdocs.org/ad/2003-10-03-R1): High pressure (HP) turbine discs · Rolls-Royce RB211-535E4-B-37 and RB211-535E4-B-75. Effective Jun 20, 2003
- [AD 2001-19-05](https://openairdocs.org/ad/2001-19-05): High Speed Gearbox Drive · Rolls-Royce RB211-535C-37, RB211-535E4-37, RB211-535E4-B-37 and 1 more. Effective Oct 11, 2001
- [AD 2000-09-14](https://openairdocs.org/ad/2000-09-14): Radial Drive Steady Bearings · Rolls-Royce RB211-535C-37, RB211-535E4-37, RB211-535E4-B-37 and 1 more. Effective Jul 11, 2000
- [AD 97-02-12](https://openairdocs.org/ad/97-02-12): Fuel Flow Governor (FFG) · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Apr 4, 1997
- [AD 87-25-04](https://openairdocs.org/ad/87-25-04): Fuel Quantity Indication System · Rolls-Royce RB211-535C-37, RB211-535E4-37, RB211-535E4-B-37 and 1 more. Effective Dec 8, 1987

### Historical (superseded or no longer in force)

- [AD 2015-17-21](https://openairdocs.org/ad/2015-17-21) (historical): High-pressure turbine (HPT) disks · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-C-37. Effective Dec 2, 2015
- [AD 2014-24-08](https://openairdocs.org/ad/2014-24-08) (historical): Fuel leaks · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-C-37. Effective Jan 6, 2015
- [AD 2013-19-18](https://openairdocs.org/ad/2013-19-18) (historical): LPT stage 2 disc failure · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37, RB211-535E4-B-75 and 1 more. Effective Nov 7, 2013
- [AD 2013-19-17](https://openairdocs.org/ad/2013-19-17) (historical): Failure of rotating life limited parts · Rolls-Royce RB211-535E4-B-37. Effective Nov 7, 2013
- [AD 2011-11-08](https://openairdocs.org/ad/2011-11-08) (historical): LP Turbine discs · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37, RB211-535E4-B-75 and 1 more. Effective Jun 30, 2011
- [AD 2008-22-24](https://openairdocs.org/ad/2008-22-24) (historical): Low pressure compressor (LPC) fan blade · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Dec 9, 2008
- [AD 2006-11-05 R1](https://openairdocs.org/ad/2006-11-05-R1) (historical): Disc assemblies · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 27 more. Effective May 1, 2007
- [AD 2006-11-05](https://openairdocs.org/ad/2006-11-05) (historical): High pressure compressor (HPC) stage 3 disc assemblies · Rolls-Royce RB211-22B-02, RB211-524B-02, RB211-524B-B-02 and 24 more. Effective Jun 27, 2006
- [AD 2005-02-05](https://openairdocs.org/ad/2005-02-05) (historical): Low Pressure Compressor (LPC) Fan Blade Roots · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Feb 11, 2005
- [AD 2004-26-03](https://openairdocs.org/ad/2004-26-03) (historical): High pressure (HP) turbine discs · Rolls-Royce RB211-22B-02, RB211-535C-37, RB211-535E4-37 and 3 more. Effective Jan 13, 2005
- [AD 2004-01-20](https://openairdocs.org/ad/2004-01-20) (historical): High pressure compressor (HPC) · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 27 more. Effective Feb 24, 2004
- [AD 2003-17-15](https://openairdocs.org/ad/2003-17-15) (historical): Low pressure (LP) turbine stage 2 discs · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Oct 2, 2003
- [AD 2003-12-15](https://openairdocs.org/ad/2003-12-15) (historical): LPC fan blade roots · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Jul 30, 2003
- [AD 2003-10-03](https://openairdocs.org/ad/2003-10-03) (historical): High Pressure (HP) turbine discs · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Jun 20, 2003
- [AD 2002-23-08](https://openairdocs.org/ad/2002-23-08) (historical): Low Pressure (LP) Turbine Stage 2 Discs · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Dec 30, 2002
- [AD 2001-23-02](https://openairdocs.org/ad/2001-23-02) (historical): High Pressure Turbine Disks · Rolls-Royce RB211-22B-02, RB211-535C-37, RB211-535E4-37 and 2 more. Effective Dec 24, 2001
- [AD 98-07-07](https://openairdocs.org/ad/98-07-07) (historical): Fuel System Tube Assembly · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Apr 29, 1998
- [AD 86-07-01](https://openairdocs.org/ad/86-07-01) (historical): Outer Combustion Case Inspection · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective May 16, 1986

## Information bulletins (advisory) (1 in force)

- [SAIB 2026-11](https://openairdocs.org/saib/2026-11): Theft of Turbofan Engine Parts before Mutilation. Issued Jun 8, 2026

## NTSB investigations

None matched to N453UP.

## FAA accident and incident reports

None matched to N453UP.

## Service difficulty reports (415, 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 IPXA2026072080748](https://openairdocs.org/sdr/IPXA2026072080748), Jul 15, 2026: FLOORBEAM. CORRODED. MAJOR REPAIR. N453UP: FUSELAGE MAIN CABIN FLOORBEAM UPPER TEE AT STA 1681.8 AND LBL 24.75 - CORROSION REPAIR (CATEGORY C REPAIR)) [T3F18E005PVTD] REQUIRE PERMAN
- [SDR IPXA2026071314904](https://openairdocs.org/sdr/IPXA2026071314904), Jul 5, 2026: BRACKET. CRACKED. PYLON NR 2 INTERNAL BRACKET NEAR PPS 174.30 RT SIDE SHOWS INDICATION OF A CRACK. REMOVED BRACKET BROKEN AT PYLON NR 2 INTERNAL NEAR PPS 174.30 RT SIDE IAW SRM 5
- [SDR IPXA2026082672737](https://openairdocs.org/sdr/IPXA2026082672737), Jul 2, 2026: BONDING STRAP. CORRODED. AGING AIRCRAFT INSP: STR Z-300: RIGHT ELEVATOR BONDED STRIP ON OUTBOARD LOWER SURFACE HAS EVIDENCE OF CORROSION AND IS DISBONDED - AA014 INSTALLED 1EA SPLICE PL
- [SDR IPXA2026071516833](https://openairdocs.org/sdr/IPXA2026071516833), Jun 29, 2026: STIFFENER. CORRODED. LEFT WING TRAILING EDGE UPPER COMPOSITE PANEL FWD OF LEFT AILERON IS BULGING, NUT PLATE CHANNEL SEEN FROM THE BOTTOM IS DISFIGURED POSSIBLY BY CORROSION - AA003
- [SDR IPXA2026070706484](https://openairdocs.org/sdr/IPXA2026070706484), Jun 29, 2026: PANEL. CRACKED. NR 2 ENG OTBD SPRING PANEL IS CRACKED 115-072. INSTALLED NEW SPRING PANEL NR 2 ENG OTBD IAW SRM 51- 40-02.
- [SDR IPXA2026071089100](https://openairdocs.org/sdr/IPXA2026071089100), Jun 27, 2026: SUPPORT BRACKET. CRACKED. APU INLET DUCT WITH BRACKET BROKEN. REMOVED BRACKET IAW B757-200 SRM 51-40-02. INSTALLED NEW PARTS (BRACKET SUPPORT) AT APU INLET DUCT IAW SRM 51-40-02-0G.
- [SDR IPXA2026071191237](https://openairdocs.org/sdr/IPXA2026071191237), Jun 27, 2026: RETAINER. CORRODED. DURING REMOVAL ACCESS FOR BEAM REPAIR AT BS 1681 FOUND A RETAINER CORRODED FROM BS 1600 - 1681, RBL 65. RETAINER FOUND TO BE CORRODED, DELAMINATED AND CRACKED, 
- [SDR IPXA2026070179170](https://openairdocs.org/sdr/IPXA2026070179170), Jun 26, 2026: ANGLE. CRACKED. FWD CARGO COMPARTMENT BRACKET CRACKED. INSTALLED NEW PART IAW SRM 51-40-02
- [SDR IPXA2026070762443](https://openairdocs.org/sdr/IPXA2026070762443), Jun 25, 2026: INTERCOSTAL. CORRODED. INTECOSTAL BETWEEN BS 1040 AND STA 1060 LT SIDE OF THE LT ACFT EXHAUST WITH EVIDENCE OF CORROSION. INSTALLED NEW INTERCOSTAL BETWEEN BS 1040 AND 1060 LT SIDE OF
- [SDR IPXA2026070361984](https://openairdocs.org/sdr/IPXA2026070361984), Jun 25, 2026: PROFILE. CORRODED. C-PROFILE WITH CRACK AT RH W/W STA 1180 NEXT TO RH MLG DOOR. INSTALLED NEW C-PROFILE IAW SRM 51-40-02.
- [SDR IPXA2026071031580](https://openairdocs.org/sdr/IPXA2026071031580), Jun 24, 2026: STRAP. CORRODED. MAJOR REPAIR, APU INLET DOOR AFT STRAP HAS CORROSION. INSTALLED REPAIR PARTS IAW SRM 51-40-02 AND SRM 53-80-15-2R-1.
- [SDR IPXA2026071030906](https://openairdocs.org/sdr/IPXA2026071030906), Jun 24, 2026: ANGLE. CORRODED. APU INLET DOOR FWD LOWER CORNER ANGE AT STA 1787.45 S-6R CORRODED. REMOVED CORROED ANGLE AT APU INLET DOOR FWD LOWER CORNER ANGLE AT STA 1787.45 S-6R, ANGLE PRE
- [SDR IPXA2026071436610](https://openairdocs.org/sdr/IPXA2026071436610), Jun 24, 2026: FLOOR SUPPORT. CORRODED. AFT CARGO AREA FLOOR PANEL STRUCTURE BTWN BS 1500-1520, LBL2 HAS EXFOLIATION CORROSION. REMOVED CORROSION ON STRINGER STA 1500-1520 LBL2 IAW SRM 53-00-53-1A-1 D
- [SDR IPXA2026071436647](https://openairdocs.org/sdr/IPXA2026071436647), Jun 24, 2026: FLOOR SUPPORT. CORRODED. AFT CARGO AREA FLOOR PANEL STRUCTURE BTWN STA 1500-1520 LBL7 HAS EXFOLIATION CORROSION. REMOVED CORROSION ON STRINGER STA 1500-1520 LBL7, ORIGINAL MATERIAL 0.06
- [SDR IPXA2026071030999](https://openairdocs.org/sdr/IPXA2026071030999), Jun 24, 2026: ANGLE. CORRODED. FAULT: ZONE300 STR APU INLET DOOR BETWEEN BS 1787.45 STA 1825.00 S-6R LOWER ANGLE HAS CORROSION. REMOVED CORRODED ANGLE LOCATED BTW 1787.45 STA 1825.00 S-6R.IAW
- [SDR IPXA2026071136245](https://openairdocs.org/sdr/IPXA2026071136245), Jun 24, 2026: TRANSITION PANEL. CORRODED. AFT CARGO AREA RH TRANSITION PANEL STA 1440-1530 HAS CORROSION ON MARKED LOCATIONS REMOVED DAMAGED TRANSITION PANEL AT AFT CARGO R/H STA 1440-1530 ORIG.MAT 0.06
- [SDR IPXA2026071336554](https://openairdocs.org/sdr/IPXA2026071336554), Jun 24, 2026: FLOOR SUPPORT. CORRODED. AFT CARGO AREA FLOOR PANEL STRUCTURE BTWN STA 1500-1520 RBL12 HAS CORROSION. REMOVED STRINGER IAW B757-200 SRM 51-40-02-0G. INSTALLED REPAIR CHANNEL ON FLOOR ST
- [SDR IPXA2026071336616](https://openairdocs.org/sdr/IPXA2026071336616), Jun 24, 2026: FLOOR SUPPORT. CORRODED. AFT CARGO AREA FLOOR PANEL STRUCTURE BTWN STA 1500-1520 RBL7 HAS CORROSION. CUT AND REMOVED DAMAGED PART OF THE CARGO COMPARTMENT FLOOR STRINGER IAW B757-200PF 
- [SDR IPXA2026071336620](https://openairdocs.org/sdr/IPXA2026071336620), Jun 24, 2026: FLOOR SUPPORT. CORRODED. AFT CARGO AREA FLOOR PANEL STRUCTURE BTWN BS 1500-1520 RBL2 HAS EXFOLIATION CORROSION. CUT AND REMOVED DAMAGED PART OF THE CARGO COMPARTMENT FLOOR STRINGER IAW 
- [SDR IPXA2026071031007](https://openairdocs.org/sdr/IPXA2026071031007), Jun 24, 2026: STRAP. CORRODED. APU INLET DOOR FWD STRAP HAS CORROSION. INSTALLED FWD STRAP, APU INLET DOOR. IAW SRM 51-40-02-0G-0. INSTALLED REPAIR PARTS IAW SRM 51-40-02 AND SRM 53-80-15-2R-
- [SDR IPXA2026071136249](https://openairdocs.org/sdr/IPXA2026071136249), Jun 24, 2026: FLOOR SUPPORT. CORRODED. AFT CARGO AREA FLOOR PANEL STRUCTURE BTWN BS 1460-1480, RBL 15 HAS EXFOLIATION. INSTALLED NEW FLOOR SUPPORT IAW SRM 51-40-02.
- [SDR IPXA2026071136513](https://openairdocs.org/sdr/IPXA2026071136513), Jun 24, 2026: FLOOR SUPPORT. CORRODED. AFT CARGO AREA FLOOR PANEL STRUCTURE BTWN BS 1460-1480, LBL 15 HAS EXFOLIATION CORROSION. INSTALLED NEW STRINGER AT AFT CARGO AREA FLOOR PANEL STRUCTURE LBL15 I
- [SDR IPXA2026071336673](https://openairdocs.org/sdr/IPXA2026071336673), Jun 24, 2026: FLOOR SUPPORT. CORRODED. AFT CARGO AREA FLOOR PANEL STRUCTURE BTWN BS 1500 - 1520, LBL 12 HAS EXFOLIATION CORROSION. REMOVED CORROSION ON STRINGER BS 1500 - 1520, LBL12, ORIGINAL MATERI
- [SDR IPXA2026070624712](https://openairdocs.org/sdr/IPXA2026070624712), Jun 24, 2026: ANGLE. CORRODED. AFT CARGO AREA AFT BULKHEAD UPPER STRUCTURE HAS EXFOLIATION CORROSION. INSTALLED NEW ANGLE IAW SRM 51-40-02.
- [SDR IPXA2026070936418](https://openairdocs.org/sdr/IPXA2026070936418), Jun 24, 2026: FLOOR SUPPORT. CORRODED. AFT CARGO AREA FLOOR PANEL STRUCTURE BTWN STA 1460-1480 RBL7 HAS EXFOLIATION CORROSION. INSTALLED NEW PART (STRINGER) AT AFT CARGO AREA FLOOR PANEL STRUCTURE BT
- [SDR IPXA2026070535982](https://openairdocs.org/sdr/IPXA2026070535982), Jun 24, 2026: TEE FITTING. CORRODED. RT FUSELAGE AT STA 1300 TEE FITTING IS CORRODED. INSTALLED A NEW TEE FITTING IAW SRM 51-40-02.
- [SDR IPXA2026071415726](https://openairdocs.org/sdr/IPXA2026071415726), Jun 23, 2026: BRACKET. CRACKED. NR 1 ENG INTERNAL OUTBD T/R, T/R TO ENGINE EXHAUST BRACKET IS CRACKET. DOT 93-020. REMOVED #1 ENG INTERNAL OUTBD T/R, T/R TO ENGINE EXHAUST BRACKET IAW B757-200
- [SDR IPXA2026070315968](https://openairdocs.org/sdr/IPXA2026070315968), Jun 23, 2026: TEE ANGLE. CORRODED. BS 1220 LT SIDE, LBL 65 HAD CORROSION ON TEE ANGLE UNDER PANEL 195 CL. INSTALLED A NEW PART IAW SRM 51-40-02-0G.
- [SDR IPXA2026070116210](https://openairdocs.org/sdr/IPXA2026070116210), Jun 23, 2026: CHANNEL. CORRODED. FWD CARGO COMPARTMENT BS 520 UPPER SUPPORT CEILING CRACKED. INSTALLED NEW SUPPORT CHANNEL IAW SRM 51-40-02-0G
- [SDR IPXA2026071686426](https://openairdocs.org/sdr/IPXA2026071686426), Jun 22, 2026: BRACKET. CRACKED. SLAT #3 I/B ND O/B SLAT DRIVE ARM GAP PANELS ARE LOOSE. . REMOVED 2EA GAP PANEL AND 2EA BRACKETS FROM #3 SLAT I/B AND O/B IAW B757-200PF SRM 51-40-02-0G-0. DURI
- [SDR IPXA2026071690929](https://openairdocs.org/sdr/IPXA2026071690929), Jun 22, 2026: WEB. CRACKED. NR 2 ENGINE O/B TR UPPER FLANGE CRACKED WERE CASCADE IS REMOVED. REMOVED DAMAGE IN TR Z420 #2 ENGINE O/B TR UPPER FLANGE.IAW.SRM 51-10-02-06 AND AMM 78-31-20-30
- [SDR IPXA2026071586789](https://openairdocs.org/sdr/IPXA2026071586789), Jun 22, 2026: COVER PLATE. CRACKED. SLAT NR 9, OUTBD TRACK GAP PANEL COVER IS CRACKED. REMOVED COVER SLAT #9, OUTBD TRACK GAP IAW SRM 51-40-02-0G. VERIFIED INSTALLED SKIRT EXTENSION PANEL ON #9 SL
- [SDR IPXA2026071586820](https://openairdocs.org/sdr/IPXA2026071586820), Jun 22, 2026: COVER PLATE. CRACKED. SLAT NR 8, INBD TRACK GAP PANEL COVER IS CRACKED. REMOVED COVER ON SLAT NR 8, INBD TRACK GAP I.A.W B757-200 SRM 51-40-02-0G. INSTALLED IAW SRM 51-40-02. VERIFIE
- [SDR IPXA2026071682132](https://openairdocs.org/sdr/IPXA2026071682132), Jun 22, 2026: LATCH. GOUGED. LEFT UPPER FWD FUSELAGE CREW ENTERANCE DOOR FWD EDGE UPPER LATCH GOUGED AT INNER SIDE. VERIFIED THIS TASK WILL BE PERFORMED ON TASK CARD (T3F18E00950C3) SRO-147
- [SDR IPXA2026071087519](https://openairdocs.org/sdr/IPXA2026071087519), Jun 22, 2026: ANGLE. CORRODED. APU INLET DOOR UPPER ANGE FROM STA 1787.45 TO STA 1825.00 S-3R CORROSION. REMOVED ANGLE.APU INLET DOOR UPPER ANGE FROM STA 1787.45 TO STA 1825.00 S-3R. IAW 757-
- [SDR IPXA2026070292708](https://openairdocs.org/sdr/IPXA2026070292708), Jun 22, 2026: BRACKET. CORRODED. RH MLG W/W FWD SEAL RETAINER HAS (3EA) CRACKED BRACKETS. REMOVAL OF CORNER SEAL RETAINER AND REMOVED SEAL RETAINER SEAL AND SUPPORT CHANNEL "(BRAKETS 3EA)" IAW 
- [SDR IPXA2026070391033](https://openairdocs.org/sdr/IPXA2026070391033), Jun 22, 2026: SUPPORT BRACKET. CORRODED. LEFT MLG WHEEL WELL, ACMP CD/PRESSURE FILTER MODULE SUPPORT BRACKET CRACKED. INSTALLED BRACKET FRAME NEW WITH IAW SRM 51-40-05.
- [SDR IPXA2026070290181](https://openairdocs.org/sdr/IPXA2026070290181), Jun 22, 2026: SUPPORT. CORRODED. NLG WHEEL WELL CUT-OUT AT BS 324 RT SIDE, GUSSET REINFORCEMENT PLATE IS CRACKED. INSTALLED NEW SUPPORT AT NLG WHEEL WELL CUT-OUT AT BS 324 RT SIDE, IAW SRM 51-4
- [SDR IPXA2026070591072](https://openairdocs.org/sdr/IPXA2026070591072), Jun 22, 2026: SUPPORT BRACKET. CRACKED. LEFT MLG WHEEL WELL, FWD CUT-OUT SEAL HAS 3EA RETAINERS CRACKED AT BS 1060. INSTALLED CHANNEL AND SUPPORT BRACKET AT LT MLG WHEEL WELL, FWD CUT-OUT SEAL HAS 3EA
- [SDR IPXA2026070693040](https://openairdocs.org/sdr/IPXA2026070693040), Jun 22, 2026: ANGLE. CORRODED. RIGHT WTB BS 1300 WTB SUPPORT BRACKET AT LWR SIDE IS CRACKED. INSTALLED ANGLE AT RT WTB BS 1300 IAW SRM 51-470-02-0G.
- [SDR IPXA2026070782144](https://openairdocs.org/sdr/IPXA2026070782144), Jun 22, 2026: SEAL. TORN. LH FWD UPPER FUSELAGE CREW DOOR CUTOUT AFT EDGE BULB SEAL TORN. REPAIRED LH FWD UPPER FUSELAGE CREW DOOR CUTOUT AFT EDGE BULB SEAL IAW AMM 52-09-00-308-001.
- [SDR IPXA2026062982144](https://openairdocs.org/sdr/IPXA2026062982144), Jun 22, 2026: SEAL. TORN. LH FWD UPPER FUSELAGE CREW DOOR CUTOUT AFT EDGE BULB SEAL TORN.
- [SDR IPXA2026062282121](https://openairdocs.org/sdr/IPXA2026062282121), Jun 22, 2026: LATCH. WORN. CREW ENTRANCE DOOR FWD EDGE UPPER AND LOWER LATCHES BARE METAL EXPOSED.
- [SDR IPXA2026062282132](https://openairdocs.org/sdr/IPXA2026062282132), Jun 22, 2026: LATCH. GOUGED. LEFT UPPER FWD FUSELAGE CREW ENTRANCE DOOR FWD EDGE UPPER LATCH GOUGED AT INNER SIDE.
- [SDR IPXA2026060192736](https://openairdocs.org/sdr/IPXA2026060192736), May 21, 2026: WINDOW. FAILED. LEFT WINDOW (L1) STARTED ARCING AT PC360 THEN SHATTERED. QRH COMPLETED. REMOVED AND REPLACE L1 WINDOW PER AMM56-11-01. OPS CK GOOD. TORQUED WINDSHIELD POWER TER
- [SDR IPXA2026052292736](https://openairdocs.org/sdr/IPXA2026052292736), May 21, 2026: WINDOW. FAILED. LEFT WINDOW (L1) STARTED ARCING AT PC360 THEN SHATTERED. QRH COMPLETED. APPLIED AERODYNAMIC SEALANT TO COMPLETE THE WINDOW INSTALLATION IAW AMM 56-11-01-424-015
- [SDR IPXA2026042127320](https://openairdocs.org/sdr/IPXA2026042127320), Apr 9, 2026: ACTUATOR. FAULTED. UPON LANDING RECEIVED A RIGHT REVERSER YELLOW CAS UPON EXITING THE RUNWAY TOWER INFORMED HAD SMOKE OUT OF THE RIGHT ENG. COMPLETED QRH EVACUATION CHECKLIST AND 
- [SDR IPXA2026041027320](https://openairdocs.org/sdr/IPXA2026041027320), Apr 9, 2026: ACTUATOR. FAULTED. UPON LANDING WE GOT A RIGHT REVERSER YELLOW CAS UPON EXITING THE RUNWAY TOWER INFORMED US WE HAD SMOKE OUT OF THE RIGHT ENG WE COMPLETED QRH EVACUATION CHECKLIS
- [SDR IPXA2025010289404](https://openairdocs.org/sdr/IPXA2025010289404), Jan 2, 2025: LAMP. INOPERATIVE. DURING PS1 CHECK FOUND MULTIPLE LIGHTS OUT IN INTERIOR EMERGENCY EXIT SIGN. RELAMPED ALL INOPERATIVE LIGHTS IN THE INTERIOR EMERGENCY EXIT LIGHTED SIGN IAW AMM 
- [SDR IPXA2024102406920](https://openairdocs.org/sdr/IPXA2024102406920), Oct 7, 2024: LONGERON. CRACKED. REMOVED #1 ENG. EXHAUST NOZZLE FAIRING FOR ACCESS.FOUND UPPER AFT. I/B ANGLE CRACKED ATA 78-00. ACCOMPLISHED EO-91831-REQ1 (VT-SAA EA 757-7811-01-B0298, REV IR)

All 415: https://openairdocs.org/aircraft/N453UP/reports.md

## STCs that may be installed (OpenAirDocs) (1)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the engine (Rolls-Royce RB211-535E4 series)

- [STC SA4005NM](https://openairdocs.org/stc/SA4005NM): Precise Flight Inc. Pulselite Control System. Precise Flight Inc. Lists RB211-535E4-37

## Related

- Other Boeing 757-24APF aircraft: https://openairdocs.org/model/boeing-757-24apf/aircraft.md
- The Rolls-Royce RB211-535E4 series engine: https://openairdocs.org/engine/rolls-royce-rb211-535e4-series.md

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