# N418UP: 1990 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: 23905
- Year built: 1990
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 14, 1990
- Certificate issued: July 31, 1998
- Expires: November 30, 2027
- Mode S code: A4F3A8
- 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=418UP
- Page: https://openairdocs.org/aircraft/N418UP

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 N418UP.

## 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.

- [Incident 19960727026939I](https://openairdocs.org/incident/19960727026939I), Jul 27, 1996: Boeing 75724APF (N418UP), Richmond, VA, Minor damage. Narrative: on July 7, 1996, at 0630 local time, a B757-24, N418UP, landed at Richmond international airport, Richmond, Virginia. After landing, and while being…

## Service difficulty reports (239, 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 IPXA2026071148660](https://openairdocs.org/sdr/IPXA2026071148660), Jun 25, 2026: BRACKET. CRACKED. CREW ENTRY DOOR PROXIMITY SENSOR BRACKET IS CRACKED. REMOVED SENSOR BRACKET (SUPPORT ASSY) AT CREW ENTRY DOOR IAW SRM 51-40-02-0G-0. INSTALLED CREW ENTRY DOOR W
- [SDR IPXA2026071878612](https://openairdocs.org/sdr/IPXA2026071878612), Jun 21, 2026: FLOOR SUPPORT. DENTED. AFT CARGO COMPARTMENT FLOOR STRINGER HAS 2 EA DENTS, APPROX BTW BS 1240 AND BS 1260, LBL 7.55, INSTALLED NEW FLOOR STRINGER AT CARGO COMPARTMENT LBL 7.55 AND BE
- [SDR IPXA2026070271202](https://openairdocs.org/sdr/IPXA2026070271202), Jun 21, 2026: RETAINER. CORRODED. RIGHT MLG WW, AT AFT OTBD DOOR-CUTOUT, UPON THE REMOVAL OF BULB SEAL, FOUND THE RETAINER WITH CORROSION END TO END. REMOVED DAMAGED SEAL RETAINER AT AFT OTBD DO
- [SDR IPXA2026063078648](https://openairdocs.org/sdr/IPXA2026063078648), Jun 21, 2026: FLOOR SUPPORT. CORRODED. AFT CARGO COMPARTMENT FLOOR STRINGER HAS CORROSION AT NUT PLATE BOTTOM AREA, APPROX AT BS 1200, LBL 2.90. REMOVED CORROSION AT AFT CARGO COMP. FLOOR STRINGER AT
- [SDR IPXA2026062778873](https://openairdocs.org/sdr/IPXA2026062778873), Jun 21, 2026: SIDEWALL PANEL. CORRODED. AFT CARGO COMPARTMENT FLOOR STRUCTURE SIDE PANEL HAS CORROSION ON MULTIPLE AREAS, APPROX BTW BS 1410 AND BS 1530, LBL 16.10 THRU LBL 25, REMOVED CORROSION AT AF
- [SDR IPXA2026063066478](https://openairdocs.org/sdr/IPXA2026063066478), Jun 20, 2026: FLOOR SUPPORT. CORRODED. AFT CARGO RH SIDE OTBD FLOOR STRINGER UPPER SURFACE HAS CORROSION STA 1510. INSTALLED REPAIR CHANNEL AT AFT CARGO RT SIDE OTBD FLOOR STRINGER AT BS 1510, RBL 10
- [SDR IPXA2026070154082](https://openairdocs.org/sdr/IPXA2026070154082), Jun 19, 2026: ISOLATION MOUNT. CRACKED. COCKPIT CEILING ABOVE OVERHEAD PANEL ISOLATOR BRACKET CRACKED. REMOVED DAMAGED BRACKET AT COCKPIT CEILING ABOVE OVERHEAD PANEL BS 297 IAW SRM 51-40-02-0G-0 PAR 
- [SDR IPXA2026062754538](https://openairdocs.org/sdr/IPXA2026062754538), Jun 19, 2026: PAD. CORRODED. NR 1 ENGINE O/B CORE COWL T/E RUB PAD, 3RD FROM BOTTOM, HAS AREA OF CORROSION. INSTALEED SERVICEABLE PART AT NR 1 ENGINE OTBD CORE COWL T/E STOP PAD, 3RD FROM B
- [SDR IPXA2026071737767](https://openairdocs.org/sdr/IPXA2026071737767), Jun 18, 2026: BRACKET. BROKEN. IAW TASK CARD T3F18E004V6MO LINE 267 STEP 10, LEFT STRUT STA 149.5 BRACKET WAS INSPECTED AND FOUND BROKEN, FLL-050, INSTALLED FRAME ANGLE AT #1 PYLON UPPER SIDE
- [SDR IPXA2026071426239](https://openairdocs.org/sdr/IPXA2026071426239), Jun 18, 2026: ATTACH ANGLE. WORN. VERTICAL STAB TRAILING EDGE PANEL 324AL LOWER AFT CORNER SUPPORT STRUCTURE SECTION MISSING AND FUSELAGE ATTACH ANGLE WORN THIN IN SEVERAL AREAS. DAMAGED WELL MA
- [SDR IPXA2026063033532](https://openairdocs.org/sdr/IPXA2026063033532), Jun 18, 2026: SKIN. CORRODED. LEFT WING INBD FLAP HAS CORROSION AT T/E OTBD UPPER SURFACE.
- [SDR IPXA2026070724890](https://openairdocs.org/sdr/IPXA2026070724890), Jun 18, 2026: SPLICE PLATE. CORRODED. RIGHT ELEVATOR T/E UPPER AND LOWER SPICE PLATES BETWEEN TIP AND CONDUCTOR FRAME HAVE CORROSION. INSTALLED NEW UPPER CONDUCTIVE FRAME, LOWER CONDUCTIVE FRAME, UP
- [SDR IPXA2026062431723](https://openairdocs.org/sdr/IPXA2026062431723), Jun 18, 2026: COVER. CORRODED. FUSELAGE INTERIOR CENTER SECTION FLOOR PANEL 241XAF PLATE SUPPORT FLOOR PANEL HAS CORROSION, INSTALLED FLOOR SUPPORT HAT CHANNEL AND SUPPORT COVER IN MAIN CABIN
- [SDR IPXA2026061925530](https://openairdocs.org/sdr/IPXA2026061925530), Jun 18, 2026: SKIN. DAMAGED. RIGHT ELEVATOR T/E UPPER AND LOWER SPICE PLATES BETWEEN TIP AND CONDUCTOR FRAME HAVE CORROSION. OKAY TO FABRICATE PER DOCUMENTS ON STEP 1.
- [SDR IPXA2026062032578](https://openairdocs.org/sdr/IPXA2026062032578), Jun 18, 2026: SKIN. DAMAGED. AFT LOWER EXTERNAL FUSELAGE SKIN AT SEAM AT STA. 1460 HAS SMALL AREAS OF BUBBLING PAINT, LIGHT CORROSION PRESENT. SRM 53-00-01-1A-1 DETAIL II FIG 101. OK TO TRE
- [SDR IPXA2026061936844](https://openairdocs.org/sdr/IPXA2026061936844), Jun 18, 2026: GUSSET. CORRODED. FOUND CORROSION ON 4EA GUSSETS, BS 1885.20 BETWEEN S25R AND S25L REMOVED FOUR CORRODED GUSSETS AT BS 1885.20 BETWEEN S-25R TO S-25L IAW SRM 51-40-02-0G-0 PAR 4 
- [SDR IPXA2026061936748](https://openairdocs.org/sdr/IPXA2026061936748), Jun 18, 2026: STRAP. CORRODED. FOUND CORROSION ON FRAME STRAP P/N 148N6613-2 STA 1885.20 S25R TO S25L. INSTALLED 1 EA NEW STRAP IAW SRM 51-40-02-0G-0 AND DWG 148N6613.
- [SDR IPXA2026071104567](https://openairdocs.org/sdr/IPXA2026071104567), Jun 17, 2026: RETAINER. CORRODED. LEFT ELEVATOR T/E COUNT FROM OTBD TO INBD NR 2 STATIC WICK BASE HAS CORROSION. REMOVED AND REPLACED NR 2 STATIC WICK BASE ( MOUNTING STATIC DISCHARGER) P/N 1633
- [SDR IPXA2026070219049](https://openairdocs.org/sdr/IPXA2026070219049), Jun 17, 2026: SUPPORT ANGLE. CRACKED. RIGHT AFT WTB PANEL LANDING UPPER SUPPORT ANGLE HAS A CRACK. REMOVED SUPPORT ANGLE AT RT WING TO BODY UPPER AFT PANEL LANDING SUPPORT IAW SRM 51-40-02-0G-0. INS
- [SDR IPXA2026071492921](https://openairdocs.org/sdr/IPXA2026071492921), Jun 16, 2026: SKIN. DAMAGED. FWD FUSELAGE BTW BS 540 - 560 AND S-29L TO S-29R HAVE LIGHTNING STRIKES 3 EA, FLL-006, INSTALLED 3 EA 7/32" DIAMETER PROTRUDING RIVETS ON FWD FUSELAGE BETWEEN B
- [SDR IPXA2026070198178](https://openairdocs.org/sdr/IPXA2026070198178), Jun 16, 2026: PAN. CRACKED. FLIGHT COMPT RT FIRST OBSERVERS SEAT BACK PAN IS CRACKED. REPLACED FIRST OBSERVERS SEAT IN FLIGHT COMPARTMENT IAW B757 AMM 25-11-01-000-802 AND B757 AMM 25-11-0
- [SDR IPXA2026070193398](https://openairdocs.org/sdr/IPXA2026070193398), Jun 16, 2026: DOOR. DAMAGED. AFT FUSELAGE RT APU DOOR ACCESS 316AL IS BENDED ON FWD CORNER AND HAS SEVERAL GOUGES ALONG OUTER EDGE, FLL-015, INSTALLED 2 EACH REPAIR DOUBLERS AND 2 EACH FILL
- [SDR IPXA2026062794337](https://openairdocs.org/sdr/IPXA2026062794337), Jun 16, 2026: SUPPORT. CORRODED. APU COMPARTMENT L/H LOWER FWD CORNER OF FUESELAGE SKIN ACCESS DOOR HINGE SUPPORT LONGERON HAS CORROSION, ACCOMPLISHED REPAIR PER EO-98077-REQ1 AND STE-SAA EA 75
- [SDR IPXA2026062794351](https://openairdocs.org/sdr/IPXA2026062794351), Jun 16, 2026: LONGERON. CORRODED. APU COMPARTMENT RT LOWER FWD CORNER OF FUESELAGE SKIN ACCESS DOOR HINGE SUPPORT LONGERON HAS CORROSION. ACCOMPLISHED REPAIR PER EO-98076-REQ1 AND STE-SAA EA 757
- [SDR IPXA2026062792720](https://openairdocs.org/sdr/IPXA2026062792720), Jun 16, 2026: FRAME. CORRODED. RIGHT FWD LOWER FUSELAGE WASTE DISPOSAL ACCESS PANEL 118AR HAS CORROSION ON INNER AND LOWER FRAME. INSTALLED PANEL 118AR IN FWD FUSELAGE LAVATORY DISPOSAL IAW S
- [SDR IPXA2026061994597](https://openairdocs.org/sdr/IPXA2026061994597), Jun 16, 2026: ACCESS PANEL. CORRODED. AFT FUSELAGE INSIDE ACCESS PANEL 313AL STA 1885.20 AND FROM S-25L TO S-25R HAS CORROSION, FLL-030, REMOVED CORRODED CHORD AT BS 1885.20 BETWEEN S-23L TO S-23R I
- [SDR IPXA2026070666531](https://openairdocs.org/sdr/IPXA2026070666531), Jun 14, 2026: PITOT TUBE. DAMAGED. AUX 1 PITOT PROBE ON RT SIDE SHOWS SIGNS OF OVERHEATING
- [SDR IPXA2026070666517](https://openairdocs.org/sdr/IPXA2026070666517), Jun 14, 2026: PITOT TUBE. OVERHEATED. CAPTAIN PITOT PROBE ON LH SIDE SHOWS SIGNS OF OVERHEATING. INSTALLED NEW CAPTAIN PITOT PROBE ON LH SIDE IN REF TO B757 AMM 34-11-01-024-041
- [SDR IPXA2025011826274](https://openairdocs.org/sdr/IPXA2025011826274), Jan 16, 2025: FRAME. NO DISCREPANCY. REF HEAVY CHECK REPAIR T3F18E004SYHW, HFEC AFTER TRIM OUT REQUIRES RII VERIFICATION. COMPLIED WITH EO-92551. REVIEWED.
- [SDR IPXA2024083095805](https://openairdocs.org/sdr/IPXA2024083095805), Aug 28, 2024: TORQUE TUBE. UNSERVICEABLE. FLAP ASSYMMETRY TRAILING EDGE DURING APPROACH WHEN FLAPS 20 SELECTED. ACCOMPANIED WITH CORRESPONDING EICAS MSG AND LIGHT. REPLACED TORQUE TUBES 251N4281-16,-17,
- [SDR IPXA2024082995805](https://openairdocs.org/sdr/IPXA2024082995805), Aug 28, 2024: FLAP SYSTEM. FAULTED. EMERGENCY DECLARED, FLAP ASSYMMETRY TRAILING EDGE DURING APPROACH WHEN FLAPS 20 SELECTED. ACCOMPANIED WITH CORRESPONDING EICAS MSG AND LIGHT PER THE FIM 27-51 T
- [SDR IPXA2024073089425](https://openairdocs.org/sdr/IPXA2024073089425), Jul 24, 2024: BATTERY PACK. INOPERATIVE. FAULT EMERGENCY EXIT LIGHT INOP.REMOVED EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-07-902-001.INSTALLED NEW EMERGENCY LIGHT BATTERY PACK AND PERFORMED OPS CHECK
- [SDR IPXA2024072589425](https://openairdocs.org/sdr/IPXA2024072589425), Jul 24, 2024: LIGHT. INOPERATIVE. EMERGENCY EXIT LIGHT INOPERATIVE.
- [SDR IPXA2024072345670](https://openairdocs.org/sdr/IPXA2024072345670), Jul 10, 2024: SEAT TRACK. CORRODED. MCD, AT STA 1671, LBL 24.5 SEAT TRACK FLANGE, SHOWS EVIDENCE OF CORROSION. DOT 72-033.REMOVED DAMAGE SEAT TRACK SECTION BETWEEN STA 1640+9.45 IN TO STA 1681.8, 
- [SDR IPXA2024072631238](https://openairdocs.org/sdr/IPXA2024072631238), Jul 9, 2024: DOUBLER. CORRODED. MCD, AFT DECK AREA (ON DOUBLER REPAIR) AT STA 1681.8 BTW BL 0/RBL 24.75 IS CORRODED. REMOVED AND REPLACED DOUBLER REPAIR ON AFT DECK AREA AT STA 1681.8 BTW BL 0
- [SDR IPXA2024072331663](https://openairdocs.org/sdr/IPXA2024072331663), Jul 9, 2024: SEAT TRACK. CORRODED. FAULT: STR Z200 MCD, AFT AREA STA. 1681.8 SEAT TRACK LBL 45.5 IS CORRODED. DOT 34-008. INSTALLED SEAT TRACK IN STA 1681.8 LBL 45.5 IAW SRM 53-00-52-2R-5,SRM 51-
- [SDR IPXA2024072214234](https://openairdocs.org/sdr/IPXA2024072214234), Jul 8, 2024: HANDLE. GOUGED. **SUPPLEMENTAL SDR** FAULT. FOUND GOUGE ON CREW DOOR HANDLE.RESTORED SURFACE IN AREA IAW SRM 51-20-01 AMM 51-21-15 P/N ALONINE 1132 BATCH 004253000 P/N 02-013-8
- [SDR IPXA2024071014234](https://openairdocs.org/sdr/IPXA2024071014234), Jul 8, 2024: HANDLE. GOUGED. OPEN. FOUND GOUGE ON CREW DOOR HANDLE.
- [SDR IPXA2024072301272](https://openairdocs.org/sdr/IPXA2024072301272), Jul 7, 2024: SEAT TRACK. CORRODED. CORROSION FOUND ON SEAT TRACKS AT STA 1680 BL 0.-REMOVED SEAT TRACK DAMAGED SECTION BETWEEN STA 1680-1650 BL PER SRM 53-00-52. ACCOMPLISHED REPAIR PER 757-200PF
- [SDR IPXA2024072202331](https://openairdocs.org/sdr/IPXA2024072202331), Jul 7, 2024: FRAME. DENTED. DENT ON FRAME IN STA 720 RH BETWEEN STR 23R AND 25R. INSTALLED FRAME REPAIR, IAW SRM 53-00-07-2R-5, DETAIL I, MAT.
- [SDR IPXA2024072695371](https://openairdocs.org/sdr/IPXA2024072695371), Jul 6, 2024: TEE ANGLE. CORRODED. TEE CHORD WITH CORROSION AT BS 900 RT, UNDER PANEL 194AR. INSPECTED & VERIFIED INSTALLATION OF NEW MATERIAL IAW SRM 51-70-12-0G-0 ON STA 900.
- [SDR IPXA2024072494273](https://openairdocs.org/sdr/IPXA2024072494273), Jul 6, 2024: TRANSITION PANEL. CORRODED. TRANSITION PANEL STA 1440-1520 RH WITH CORROSION. INSTALLED TRANSITION PANEL IAW SRM 51-40-02. INSTALLED PANELS 161BF,161AF IAW SRM 51-40-02. INSTALLED LOWER MB
- [SDR IPXA2024071994561](https://openairdocs.org/sdr/IPXA2024071994561), Jul 6, 2024: NUT PLATE. CORRODED. FAULT: NUTPLATES UNDER FLOOR PANEL IN STA 1720 WITH CORROSION INSTALLED 1 NUTPLATE IAW B757-200 SRM 51-40-02. NUTPLATE P/N BACN10KE3DCD BTCH 4278069 RIVET P/N N
- [SDR IPXA2024072394617](https://openairdocs.org/sdr/IPXA2024072394617), Jul 6, 2024: NUT PLATE. CORRODED. SUPPORT NUTPLATE UNDER FLOOR PANEL IN STA 1720 WITH CORROSION INSTALLED ANGLE AND SUPPORT NUTPLATE IAW B757 SRM 51-40-02 PARAGRAPH 4. RIVET P/N:MS20426AD6-10 BA
- [SDR IPXA2024072294617](https://openairdocs.org/sdr/IPXA2024072294617), Jul 6, 2024: NUT PLATE. CORRODED. SUPPORT NUTPLATE UNDER FLOOR PANEL IN STA 1720 WITH CORROSION.
- [SDR IPXA2024071682131](https://openairdocs.org/sdr/IPXA2024071682131), Jul 5, 2024: MOUNT. GOUGED. CREW ENTRY DOOR FWD CUTOUT DOORSTOP FITTING MOUNT #2 HAS DEEP GOUGE. VERRIFIED RESTORED SURFACE PROTECTION IAW AMM 51-21-15-370-81A. P/N ALODINE1132 BTCH 429739
- [SDR IPXA202407082131](https://openairdocs.org/sdr/IPXA202407082131), Jul 5, 2024: MOUNT. GOUGED. OPEN, CREW ENTRY DOOR FWD CUTOUT DOORSTOP FITTING MOUNT #2 HAS DEEP GOUGE. REMOVED MARK BY METHOD ABRASION BY HAND AT CREW ENTRY DOOR FWD CUTOUT DOORSTOP FITTIN
- [SDR IPXA2022072084380](https://openairdocs.org/sdr/IPXA2022072084380), Jul 5, 2022: SKIN. CRACKED. INSPECTION TYPE:C18UPON HFEC OF A 15: DENT AT FS 1380 - FS 1400 BETWEEN STRINGERS 28L AND 27R NDT FOUND A 15" CRACK RUNNING ALONG THE RECESS OF DENT 15", CRACK 
- [SDR IPXA2018122137128](https://openairdocs.org/sdr/IPXA2018122137128), Dec 20, 2018: CLAMP. LOOSE. CLIMBING THROUGH FL 280, AN EICAS MESSAGE & WARNING HORN FOR CABIN ALTITUDE WERE ANNUNCIATED AND SOUNDED. EMERGENCY DECLARED, PERFORMED AN EMERGENCY DESCENT. LE
- [SDR IPXA2018101835141](https://openairdocs.org/sdr/IPXA2018101835141), Oct 18, 2018: FLOOR PANEL. DAMAGED. MAIN CARGO COMPARTMENT FLOOR PANEL 241XKF DAMAGED. FABBED PANEL 241XKF PER SREO B757-5320-9692-K.

All 239: https://openairdocs.org/aircraft/N418UP/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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