# N413UP: 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: 23853
- Year built: 1988
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 30, 1988
- Certificate issued: October 13, 1988
- Expires: August 31, 2028
- Mode S code: A4E115
- 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=413UP
- Page: https://openairdocs.org/aircraft/N413UP

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 (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB FTW95LA055](https://openairdocs.org/ntsb/FTW95LA055), Nov 25, 1994: Boeing 757-24APF (N413UP), Tulsa, OK, substantial damage. Probable cause: THE PILOT'S FAILURE TO MAINTAIN VREF DURING APPROACH AND HIS IMPROPER FLARE TOUCHDOWN THAT RESULTED IN AN EXCESSIVE PITCH UP ATTITUDE FOLLOWING TOUCHDOWN.

## 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.

- [Accident 19941125040459A](https://openairdocs.org/incident/19941125040459A), Nov 25, 1994: Boeing 75724APF (N413UP), Tulsa, OK, Substantial damage. Pitch up on landing too high. Tail struck runway on touchdown. Damaged aft fuselage. Pilot at the controls.

## Service difficulty reports (256, 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 IPXA2026061187755](https://openairdocs.org/sdr/IPXA2026061187755), Jun 3, 2026: BRACKET. CORRODED. DURING REMOVAL OF LWR SKIN PANEL AT SECTION 48 WHILE ACCOMPLISHMENT OF T.C T3F18E008WDGE. FOUND 2EA ANGLE BRACKETS CORRODED AT BS 1963.8 AND BS 1992.8. INSTALLE
- [SDR IPXA2026061648877](https://openairdocs.org/sdr/IPXA2026061648877), Jun 1, 2026: SUPPORT. CRACKED. RIGHT LOWER WING TO BODY FAIRING SUPPORT STRUCTURE, INTERCOSTAL IS CRACKED AT BS 990. INSTALLED INTERCOSTAL IAW SRM 51-40-02-0G-0.
- [SDR IPXA2026061148884](https://openairdocs.org/sdr/IPXA2026061148884), Jun 1, 2026: TEE ANGLE. CORRODED. RIGHT LOWER WING TO BODY FAIRING SUPPORT STRUCTURE, TEE ANGLE HAS EXFOLIATED CORROSION, BTWN BS 1040 AND BS 1060 AT RBL 68. INSTALLED NEW TEE ANGLE RT LOWER WIN
- [SDR IPXA2026061249095](https://openairdocs.org/sdr/IPXA2026061249095), Jun 1, 2026: FRAME. CORRODED. RIGHT LOWER WING TO BODY FAIRING SUPPORT STRUCTURE, FRAME-WEB HAS CORROSION AT BS 1200 RBL 60. INSTALLED 1 EA FRAME WEB IAW SRM 51-40-02.
- [SDR IPXA2026060648764](https://openairdocs.org/sdr/IPXA2026060648764), Jun 1, 2026: SUPPORT BRACKET. CRACKED. LEFT MLG WHEEL WELL, 1EA BRACKET SUPPORT IS CRACKED AT THE 1180 BULKHEAD LWR SECTION. INSTALLED WEB REMOVED FOR ACCESS IN STEP 1 AND NEW BRACKET SUPPORT P/N UP-
- [SDR IPXA2026060949184](https://openairdocs.org/sdr/IPXA2026060949184), Jun 1, 2026: SUPPORT ANGLE. CRACKED. FAULT-STR-Z100- R/H WING TO BODY FAIRING SUPPORT STRUCTURE AT BS 1300, UPPER T-CHORD BRACKET SUPPORT IS CRACKED. DOT 21-14 INSTALLED NEW ANGLE SUPPORT P/N UP-14
- [SDR IPXA2026060248829](https://openairdocs.org/sdr/IPXA2026060248829), Jun 1, 2026: SPLICE PLATE. CORRODED. RT LOWER WING TO BODY FAIRING SUPPORT STRUCTURE, SUPPORT WEB HAS CORROSION AT BS 860 BL0. SURFACE PROTECTION RESTORATION COMPLIED WITH IAW SRM 51-20-01-0G-0, AM
- [SDR IPXA2026060249026](https://openairdocs.org/sdr/IPXA2026060249026), Jun 1, 2026: ANGLE. CORRODED. R/H LOWER WING TO BODY FAIRING SUPPORT STRUCTURE, T-CHORD "L" ANGLE HAS CORROSION AT BS 1040 AT RBL 68. VERIFIED STEP 3.INSPECTED SURFACE PROTECTION RESTORATION
- [SDR IPXA2026061741991](https://openairdocs.org/sdr/IPXA2026061741991), May 31, 2026: FRAME. GOUGED. FRAME 1380 RT SIDE HAS MULTIPLE GOUGES TO THE FRAME INNER CHORD (EXTERIOR RADIUS) BETWEEN S-25R TO S-27R. ACCOMPLISHED THE CATEGORY B REPAIR PER EO-97741-REQ1 A
- [SDR IPXA2026061620751](https://openairdocs.org/sdr/IPXA2026061620751), May 29, 2026: SUPPORT BRACKET. CORRODED. RH WING LOWER SURFACE SIDE OF BODY SPLICE INTERNAL TRIANGULAR SHAPE PANEL 194CR MID SUPPORT BRACKET ANGLE CORRODED/ DOT.139.032. INSTALLED 1EA FRAME, 1EA BRACKE
- [SDR IPXA2026061201031](https://openairdocs.org/sdr/IPXA2026061201031), May 28, 2026: STRAP. CORRODED. APU INLET DOOR AFT STRAP HAS CORROSION STA1825.00,S-3R TO S6R. INSTALLED PARTS OF REPAIR (STRAP 1, STRAP 2, FILLER 3, FILLER 4 AND OUTER STRAP) I.A.W. B757-200 
- [SDR IPXA2026061202381](https://openairdocs.org/sdr/IPXA2026061202381), May 28, 2026: ANGLE. CORRODED. APU INLET DOOR UPPER ANGLE FROM STA 1787.45 TO STA 1825.00 S-3R HAS CORROSION. INSTALLED NEW UPPER ANGLE I.A.W. B757-200PF SRM 51-40-02-0G-0
- [SDR IPXA2026061303166](https://openairdocs.org/sdr/IPXA2026061303166), May 28, 2026: TEE ANGLE. CORRODED. BS 1060 LWR SURFACE, JUST BEHIND OF BEACON LIGHT, FRAME WITH EVIDENCE OF CORROSION. INSTALLED NEW TEE ANGLE AT BS 1060 LWR SURFACE, JUST BEHIND OF BEACON LIGHT 
- [SDR IPXA2026060903107](https://openairdocs.org/sdr/IPXA2026060903107), May 28, 2026: INTERCOSTAL. CORRODED. BS 1040 LWR SURFACE, AROUND OF RH A/C PACK HOT AIR EXHAUST, FRAME WITH EVIDENCE OF CORROSION. INSTALLED NEW INTERCOSTAL IAW B757-200PF SRM 51-40-02-0G-0
- [SDR IPXA2026060103232](https://openairdocs.org/sdr/IPXA2026060103232), May 28, 2026: TEE ANGLE. CORRODED. STA 900 APPROX, LWR SURFACE, JUST IN FRONT OF LH A/C PACK PANEL, FRAME WITH EVIDENCE OF CORROSION. VERIFIED RESTORATION OF SURFACE PROTECTION IAW B757-200PF SRM
- [SDR IPXA2026060584560](https://openairdocs.org/sdr/IPXA2026060584560), May 27, 2026: SEAL DEPRESSOR. CRACKED. CARGO DOOR UPPER AFT CORNER HAS A CRACK. INSTALLED NEW CORNER SEAL DECOMPRESSOR FROM CARGO DOOR IAW SRM 51-40-02-0G-0
- [SDR IPXA2026061366314](https://openairdocs.org/sdr/IPXA2026061366314), May 26, 2026: TEE ANGLE. CORRODED. RIGHT A/C PACK PANEL, AFT FRAME WITH EVIDENCE OF CORROSION IN DIFERRENT AREAS. INSTALLED NEW TEE ANGLE IAW SRM 51-40-02-0G-0.
- [SDR IPXA2026061366338](https://openairdocs.org/sdr/IPXA2026061366338), May 26, 2026: TEE ANGLE. CORRODED. LEFT A/C PACK PANEL, AFT FRAME WITH EVIDENCE OF CORROSION IN DIFERRENT AREAS. INSTALLED TEE ANGLE AND 2 EA CLIP SUPPORTS IAW SRM 51-40-02.
- [SDR IPXA2026060663496](https://openairdocs.org/sdr/IPXA2026060663496), May 26, 2026: BRACKET. CRACKED. CRACK ON PRESS/CD FILTER MOD R SYS BRACKET MLG RH WHEEL WELL. INSTALLED NEW BRACKET AT MLG RH WHEEL WELL IAW SRM 51-40-02-0G-0
- [SDR IPXA2026061244839](https://openairdocs.org/sdr/IPXA2026061244839), May 24, 2026: ANGLE. CORRODED. FAULT Z-300 STR: APU INLET DOOR FWD LOWER CORNER ANGLE AT STA 1787.45 S-6R HAS CORROSION INSTALLED NEW LOWER CORNER ANGLE I.A.W. B757-200PF SRM 51-40-02-0G-0
- [SDR IPXA2026061744578](https://openairdocs.org/sdr/IPXA2026061744578), May 24, 2026: TAIL CONE. CORRODED. APU EXTERNAL AREA NEXT TO TAIL CONE (STA. 1992) SHOWS EVIDENCE OF CORROSION. INSTALLED BOND ASSY SKIN LOWER PANEL 1 EA AT APU EXTERNAL AREA NEXT TO TAIL CONE BS
- [SDR IPXA2026061244983](https://openairdocs.org/sdr/IPXA2026061244983), May 24, 2026: STRAP. CORRODED. APU INLET DOOR FWD STRAP HAS CORROSION INSTALLED NEW FWD STRAP I.A.W SRM 51-40-02-0G-0.
- [SDR IPXA2026061344863](https://openairdocs.org/sdr/IPXA2026061344863), May 24, 2026: ANGLE. CORRODED. APU INLET DOOR BETWEEN BS 1787.45 TO BS 1825 S-6R, LOWER ANGLE HAS CORROSION. INSTALLED NEW LOWER ANGLE IAW SRM 51-40-02-0G-0.
- [SDR IPXA2026061634755](https://openairdocs.org/sdr/IPXA2026061634755), May 23, 2026: SKIN. CORRODED. LH RUDDER SURFACE CONDUCTIVE FRAME ABOVE STA. 380 SHOWS EVIDENCE OF CORROSION. DOT 65-001 INSTALLED FAIRING P/N 173N2603-3, FAIRING P/N 179N1000-7, BRACKET SUPP
- [SDR IPXA2026061768095](https://openairdocs.org/sdr/IPXA2026061768095), Apr 24, 2026: DOOR FRAME. DENTED. (MAIN CARGO DOOR FRAME INSTALLATION (STA 600+12.9 & 600+17.25) DAMAGE - TEMPORARY REPAIR) [T3F18E008QANF]
- [SDR IPXA2025123066036](https://openairdocs.org/sdr/IPXA2025123066036), Dec 29, 2025: BULB. INOPERATIVE. FLIGHT DECK EXIT LIGHT HAS 11 INOP BULBS. RE-LAMPED FLIGHT DECK EXIT SIGN 11 EACH BULBS IAW AMM 33-51-01-962-001
- [SDR IPXA2025102914495](https://openairdocs.org/sdr/IPXA2025102914495), Oct 29, 2025: DOOR. BINDING. CAPT REPORTS ISSUES WITH CREW ENTRY DOOR OPEN/CLOSE.
- [SDR IPXA2024122688367](https://openairdocs.org/sdr/IPXA2024122688367), Dec 24, 2024: CHANNEL. UNSECURE. RUBBER CABLE CHANNELS FOR DESCENT DEVICES HANGING FROM CEILING. RE SECURED GUIDE BLOCKS IAW MM 25-64-00 OPS CK GOOD
- [SDR IPXA2024081284700](https://openairdocs.org/sdr/IPXA2024081284700), Aug 9, 2024: STUD. INOPERATIVE. CREW ENTRY DOOR OUTER HANDLE, REQUIRES STUD REPLACEMENT. REMOVED AND REPLACED CREW ENTRY DOOR OUTER HANDLE STUD PER MM 52-12-01.
- [SDR IPXA2024061744408](https://openairdocs.org/sdr/IPXA2024061744408), Jun 13, 2024: LIGHT. INOPERATIVE. NTERIOR EMERGENCY LIGHT. R&R BATTERY PACK PER AMM 33-51-07 OPS CHECK GOOD THIS CLEARS MEL 33-51-1-1 PLACARD REMOVED
- [SDR IPXA2024061344408](https://openairdocs.org/sdr/IPXA2024061344408), Jun 13, 2024: LIGHT. UNKNOWN. INTERIOR EMERGENCY LIGHT DEFERRED PER MEL 33-51-1-1. OPEN
- [SDR IPXA2023091435148](https://openairdocs.org/sdr/IPXA2023091435148), Sep 13, 2023: BLEED AIR SYS. INOPERATIVE. R ENG BLEED OFF WITH R PACK OFF. RESULTED IN DIVERSION TO SDF REMOVED AND REPLACED FAN AIR VALVE PER AMM 36-11-16. REMOVED AND RPLACED FAN AIR TEMP SENSOR PER A
- [SDR IPXA2023091335148](https://openairdocs.org/sdr/IPXA2023091335148), Sep 13, 2023: UNKNOWN. UNKNOWN. *SDR FILED OPEN* *DIV* R ENG BLEED OFF WITH R PACK OFF. RESULTED IN DIVERSION TO SDF REMOVED AND REPLACED FAN AIR VALVE PER AMM 36-11-16 REMOVED AND REPLACED FA
- [SDR IPXA2023041392870](https://openairdocs.org/sdr/IPXA2023041392870), Apr 13, 2023: UNKNOWN. INOPERATIVE. INSPECTION TYPE:NA*EMERGENCY DECLARED* AIRSPEED UNRELIABLE ON CAPT SIDE AT FLT LVL 250. CHECKLIST RESTORED CAPT INSTS BY USE OF "AIR DATA" SWITCHMCDP FAULT 2104
- [SDR IPXA2022081485215](https://openairdocs.org/sdr/IPXA2022081485215), Aug 13, 2022: NONE. NONE. INSPECTION TYPE:DIRH LOWER FUSELAGE AT STA 700, S-24R HAS A TEMPORARY LIGHTINING STRIKE REPAIR. REQUIRES PERMANENT REPAIR. SKIN P/N: 143N3691-2, ORIGINAL MAT: S
- [SDR IPXA2022070983986](https://openairdocs.org/sdr/IPXA2022070983986), Jul 9, 2022: FLOORBEAM. CORRODED. INSPECTION TYPE:SEG4MCD STA 1600 FLOOR BEAM HAS CORROSION DAMAGE ON UPPER CHORD AFT FLANGE LOWER SURFACE AND WEB BETWEEN RBL 40 AND RBL 60.REPAIRED PER UPS EO B
- [SDR IPXA2022070783904](https://openairdocs.org/sdr/IPXA2022070783904), Jul 7, 2022: FLOOR PANEL. DAMAGED. INSPECTION TYPE:SEG4MCD FLOOR PANEL 241XHF HAS DELAMINATION AND SEPARATING.FABRICATED PANEL 241XHF FROM 5024N400001SS-G, BAT: 3855547, PER SREO B757-5320-9692-K
- [SDR IPXA2022070683860](https://openairdocs.org/sdr/IPXA2022070683860), Jul 6, 2022: SKIN. CORRODED. INSPECTION TYPE:SEG4LH WING UPPER SURFACE SHOWING SIGNS OF CORROSION BETWEEN WS 150.00 - WS 177.50 DOT 33-022UPPER SKIN BLENDED IS WITHIN LIMITS PER SRM 57-20-0
- [SDR IPXA2022070683859](https://openairdocs.org/sdr/IPXA2022070683859), Jul 6, 2022: TIE CLIP. CORRODED. INSPECTION TYPE:SEG4COCKPIT FLOOR HAS CORROSION IN NUMEROUS SPOTS ON 1ST OFFICERS SIDE TO INCLUDE UNDER 1ST OBERVERS SEAT.REMOVED CORROSION, PERFORMED HFEC INSP
- [SDR IPXA2022070683867](https://openairdocs.org/sdr/IPXA2022070683867), Jul 6, 2022: FRAME ANGLE. CRACKED. INSPECTION TYPE:SEG4AFT CARGO COMPARTMENT HAS AN EXISTING FRAME REPAIR AT STA 1560 R/H BETWEEN STR 23 TO STR 28WORKED PER UPS EO B757-5310-26178-C, UPC RCD 2711
- [SDR IPXA2022070283714](https://openairdocs.org/sdr/IPXA2022070283714), Jul 2, 2022: SEAT TRACK. CORRODED. INSPECTION TYPE:SEG4MAIN CARGO COMPARTMENT SEAT TRACK STA 1190 LBL 45 HAS CORROSIONAFTER TO REWORK AREA, FOUND TO BE OUT OF LIMITS PER SRM 53-00-52-1A-1 REMOVE 
- [SDR IPXA2022070283723](https://openairdocs.org/sdr/IPXA2022070283723), Jul 2, 2022: FLOOR SUPPORT. CORRODED. INSPECTION TYPE:SEG4EXFOLIATION CORROSION AROUND DOME NUT ON LOWER SIDE OF T CHORD AT STA 1200 LBL 47 AT MAIN CARGO COMPARTMENTFOUND TO BE OUT OF LIMITS. REPAIR
- [SDR IPXA2022070283710](https://openairdocs.org/sdr/IPXA2022070283710), Jul 2, 2022: FRAME SPLICE. DENTED. INSPECTION TYPE:SEG4AFT CARGO COMPARTMENT LOWER LEFT SIDEWALL STA 1320 HAS DENTDENTS ARE NOT ALLOWED AT THE UPPER FLANGE OF THE FRAME PER SRM 53-00-07-1A-1 FRAM
- [SDR IPXA2022070283709](https://openairdocs.org/sdr/IPXA2022070283709), Jul 2, 2022: FRAME ANGLE. DENTED. INSPECTION TYPE:SEG4AFT CARGO COMPARTMENT LOWER FRAME STA 1300 LH HAS A DENT ABOVE S-26LDENTS ARE NOT ALLOWED AT THE UPPER FLANGE OF THE FRAME PER SRM 53-00-07-
- [SDR IPXA2022062983615](https://openairdocs.org/sdr/IPXA2022062983615), Jun 29, 2022: SKIN. DAMAGED. INSPECTION TYPE:SEG4RIGHT SIDE LOWER FUSELAGE LIGHTNING STRIKE DAMAGED REPAIR AT STA 700 AND S-24 R PERMANENT REPAIRREMOVE TEMPORARY REPAIR DOUBLER PER SRM 51-4
- [SDR IPXA2022070583845](https://openairdocs.org/sdr/IPXA2022070583845), Jun 22, 2022: FRAME ANGLE. DENTED. INSPECTION TYPE:C20L/H AFT CARGO COMPARTMENT AT FRAME STA 1600 IS DENTED (S-26L)REPAIRED PER EA# 757-5360-27-A2960
- [SDR IPXA2022070883959](https://openairdocs.org/sdr/IPXA2022070883959), Jun 21, 2022: FRAME ANGLE. DAMAGED. INSPECTION TYPE:C20AFT CARGO FRAME AT STA 1520 R/H SIDE IS DENTED ON THE TOP OF THE FRAME FLANGE BY S-26RREPAIR PER SRM 53-00-07-2R-5 DETAIL I AND RCD 271205
- [SDR IPXA2022070583850](https://openairdocs.org/sdr/IPXA2022070583850), Jun 21, 2022: SKIN. CORRODED. INSPECTION TYPE:C20APU COMPARTMENT HAS CORROSION ON INTERIOR SKIN L/H SIDE AT LOWER WEB ABOVE CLAMSHELL DOOR, AFT OF FWD HINGE (2 SPOTS) DOT 46-06WORKED PER RCD
- [SDR IPXA2022070583831](https://openairdocs.org/sdr/IPXA2022070583831), Jun 21, 2022: SKIN. CORRODED. INSPECTION TYPE:CK20APU COMPARTMENT HAS CORROSION ON INTERIOR SKIN LH LOWER WEB AREA ABOVE CLAMSHELL DOOR, AFT OF AFT HINGE. DOT 46-06WORKED PER RCD 271220. 757
- [SDR IPXA2021081972919](https://openairdocs.org/sdr/IPXA2021081972919), Aug 17, 2021: CONTROLLER. INOPERATIVE. EMERGENCY DECLARED, IN MANUAL MODE (R) PACK ON (R) ENG BLEED OFF ! TURNED ON (L) PACK AND TURNER OFF (R) PACK. PRESSURIZATION REGAINEDPERFORMED BITE TEST ON BOT

All 256: https://openairdocs.org/aircraft/N413UP/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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