# N414UP: 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: 23854
- Year built: 1988
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 28, 1988
- Certificate issued: November 9, 1988
- Expires: November 30, 2028
- Mode S code: A4E4CC
- 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=414UP
- Page: https://openairdocs.org/aircraft/N414UP

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 N414UP.

## 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 19890201005939I](https://openairdocs.org/incident/19890201005939I), Feb 1, 1989: Boeing 75724APF (N414UP), San Antonio, TX, Minor damage. Had flap problem on approach. Made no flap landing. Due to high deck angle aft fuselage struck runway.

## Service difficulty reports (176, 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 IPXA2026061785122](https://openairdocs.org/sdr/IPXA2026061785122), Jun 16, 2026: FUSE. FAILED. WHEN WE PUT THE GEAR DOWN ON APPROAH, WE HAD THE GEAR DOORS EICAS MESSAGE AND DOORS LIGHT IS ON R & R RT MLG EXT/RET HYD FUSES PER AMM 32-32-19. OPS CHECKS AND 
- [SDR IPXA2026061685122](https://openairdocs.org/sdr/IPXA2026061685122), Jun 16, 2026: WARNING MESSAGE. ILLUMINATED. WHEN WE PUT THE GEAR DOWN ON APPROACH, WE HAD THE GEAR DOORS EICAS MESSAGE AND DOORS LIGHT IS ON INSTALLED ALL 3 EACH GEAR PINS. REMOVED RED FLAGS SECURE GEAR P
- [SDR IPXA2026052872646](https://openairdocs.org/sdr/IPXA2026052872646), May 27, 2026: UNKNOWN. ODOR. STRONG FUEL SMELL ON FLT DECK FROM PACK AIR SOURCE. RT. PACK WAS ON. REF 757 FIM 71-05€“00-811. OPERATED BOTH ENGINES FOR 5 MIN PER STEP 1 OF FIM. ACCOMPLISHED
- [SDR IPXA2026052772646](https://openairdocs.org/sdr/IPXA2026052772646), May 27, 2026: UNKNOWN. ODOR. STRONG FUEL SMELL ON FLT DECK FROM PACK AIR SOURCE. RT. PACK WAS ON. REF 757 FIM 71-05€“00-811. OPERATED BOTH ENGINES FOR 5 MIN PER STEP 1 OF FIM. ACCOMPLISHED
- [SDR IPXA2025122718415](https://openairdocs.org/sdr/IPXA2025122718415), Dec 18, 2025: SKIN. CRACKED. AFTER REMOVAL NR 2 ENG. PYLON LEADING EDGE FOUND OUTER SKIN CRACKED. ACCOMPLISHED REPAIR PER EO-96111-REQ1 AND VT-SAA EA 757-5741-01-B0649, REV. IR.
- [SDR IPXA2025122978415](https://openairdocs.org/sdr/IPXA2025122978415), Dec 18, 2025: SKIN. CRACKED. AFTER REMOVAL NR 2 ENG. PYLON LEADING EDGE FOUND OUTER SKIN CRACKED. INSTALLED REPAIR DOUBLER IAW EA 757-5741-01-B0649, REV, P3, STEP 2 & SRM 57-41-01-2R-3, REP
- [SDR IPXA2026010531066](https://openairdocs.org/sdr/IPXA2026010531066), Nov 18, 2025: TRANSITION PANEL. CORRODED. UPON REMOVAL OF ACCESS FOR STRINGER REPAIR, AFT CARGO RT SIDE TRANSITION PANEL UPPER SURFACE BETWEEN BS 1440-1530 HAS AREAS OF CORROSION. REMOVED AND REPLACED S
- [SDR IPXA2026010559590](https://openairdocs.org/sdr/IPXA2026010559590), Nov 13, 2025: STRINGER. CORRODED. DURING DVI INSPECTION ON EO-91261-REQ1 REV3 FOUND AFT CARGO COMPARTMENT. BILGE AREA WITH CORROSION ON STR-28R BETWEEN STA1420 AND 1440. REMOVED AND REPLACED STR
- [SDR IPXA2025122959619](https://openairdocs.org/sdr/IPXA2025122959619), Nov 13, 2025: INTERCOSTAL. CORRODED. DURING DVI INSPECTION ON EO-91261-REQ1 REV3 FOUND AFT CARGO COMPARTMENT. BILGE AREA WITH CORROSION ON WEB LOCATED APPROX STR 30 BETWEEN BS 1400 AND 1420. REMOVE
- [SDR IPXA2025121659590](https://openairdocs.org/sdr/IPXA2025121659590), Nov 13, 2025: STRINGER. DAMAGED. DURING DVI INSPECTION ON EO-91261-REQ1 REV3 FOUND AFT CARGO COMPARTMENT. BILGE AREA WITH CORROSION ON STR-28R BETWEEN STA1420 AND 1440. (015-005) VERIFIED INSTA
- [SDR IPXA2025120359619](https://openairdocs.org/sdr/IPXA2025120359619), Nov 13, 2025: WEB. CORRODED. DURING DVI INSPECTION ON EO-91261-REQ1 REV3 FOUND AFT CARGO COMPARTMENT. BILGE AREA WITH CORROSION ON WEB LOCATED APPROX STR30 BETWEEN BS 1400 AND 1420.
- [SDR IPXA2025120726859](https://openairdocs.org/sdr/IPXA2025120726859), Nov 5, 2025: SKIN. DAMAGED. LEFT WING SKIN FASTENER HOLE COMMON TO UPPER DRAG FITTING HOLE DIAMETER NOT CONSISTANT THROUGH PART STACK UP , IDENTIFIED AS HOLE NR 3 . VERIFIED STEP 57 IAW GM
- [SDR IPXA2026022096208](https://openairdocs.org/sdr/IPXA2026022096208), Nov 3, 2025: STRAP. CORRODED. MAJOR REPAIR, WHILE EVALUATING CORROSION AT APU INLET SURROUND STRUCTURE FOUND CORROSION AT APU INLET AFT STRAP AT STA 1825 BETWEEN STR 3R-6R.
- [SDR IPXA2025120896208](https://openairdocs.org/sdr/IPXA2025120896208), Nov 3, 2025: STRAP. CORRODED. WHILE EVALUATING CORROSION AT APU INLET SURROUND STRUCTURE FOUND CORROSION AT APU INLET AFT STRAP AT BS 1825 BETWEEN S3-6R. ACCOMPLISHED REPAIR IAW SRM 53-80-15
- [SDR IPXA2025112096208](https://openairdocs.org/sdr/IPXA2025112096208), Nov 3, 2025: STRAP. CORRODED. WHILE EVALUATING CORROSION AT APU INLET SURROUND STRUCTURE, FOUND CORROSION AT APU INLET AFT STRAP AT STA 1825 BETWEEN STR 3R-6R PRODUCTION AUDIT C/W
- [SDR IPXA2025120897297](https://openairdocs.org/sdr/IPXA2025120897297), Oct 28, 2025: STRAP. CORRODED. APU INLET DUCT HAS EVIDENCE OF CORROSION AROUND NUT PLATES. REMOVED AND REPLACED SUPPORT ANGLES AND STRAP IAW DWGS 148N3152, 148N3141, 148N3138, AND 148N3105 IA
- [SDR IPXA2025121485445](https://openairdocs.org/sdr/IPXA2025121485445), Oct 27, 2025: CHANNEL. CORRODED. RIGHT MLG WHEEL WELL DOOR CUT OUT OTBD, FWD EDGE SUPPORT CHANNEL HAD EVIDENCE OF CORROSION, APPROX BTW BS 1063 & 1097, LOCATED AND DRILLED RT MLG WW SUPPORT CHA
- [SDR IPXA2025111984916](https://openairdocs.org/sdr/IPXA2025111984916), Oct 27, 2025: SKIN. DELAMINATED. RIGHT WING. OTBD FLAP, CENTER UPPER PANEL HAS DELAMINATION. ACCOMPLISHED REPAIR PER SRM 57-53-01-2R-1 REPAIR 1 FIGURE 201 TABLE III REV 124 AND 250°F CURE IAW 
- [SDR IPXA2025111745555](https://openairdocs.org/sdr/IPXA2025111745555), Oct 25, 2025: HANDLE. DIRTY. CREW ENTRY DOOR, EXTERIOR DOOR HANDLE, LIFT HANDLE OUT, STUD CORRODED/WORN, MARKED, 107-009. CLEANED CREW ENTRY DOOR, ENTERIOR DOOR HANDLE, LIFT HANDLE OUT, STU
- [SDR IPXA2025103045555](https://openairdocs.org/sdr/IPXA2025103045555), Oct 25, 2025: HANDLE. CORRODED. CREW ENTRY DOOR, EXTERIOR DOOR HANDLE, LIFT HANDLE OUT, STUD CORRODED AND WORN. OPEN
- [SDR IPXA2024122340806](https://openairdocs.org/sdr/IPXA2024122340806), Dec 21, 2024: PBE. EXPIRED. ESSEX PBE EXPIRES THIS MONTH. REMOVED AND REPLACED PBE PER AMM 35-31-01. EXPIRES 06/2028
- [SDR IPXA2024010312831](https://openairdocs.org/sdr/IPXA2024010312831), Dec 30, 2023: RADAR. WARNING MESSAGE. STATUS MESS TERR SYS ON DECENT INTO ATL PERF GROUND PROX TEST PER AMM 34-00, UNABLE TO DUPLICATE, NO FAULTS FOUND.
- [SDR IPXA2023050193049](https://openairdocs.org/sdr/IPXA2023050193049), May 1, 2023: FLOOR PANEL. DAMAGED. INSPECTION TYPE:NA*MAJOR REPAIR* MAIN DECK FLOOR BOARD DAMAGED.MANUFACTURED NEW PANEL PER EO B757-5320-9692-K.
- [SDR IPXA2023021190886](https://openairdocs.org/sdr/IPXA2023021190886), Feb 11, 2023: FRAME. NONE. INSPECTION TYPE:SEG4*MAJOR REPAIR* UPON INSPECTION FOR EO (B757-5310-73926-A) FOUND AN EXISTING REPAIR AT STA 1240 RH STR 25R-27RREPLACED REPAIR PER UPS EO B757
- [SDR IPXA2023021190895](https://openairdocs.org/sdr/IPXA2023021190895), Feb 11, 2023: FRAME. DENTED. INSPECTION TYPE:SEG4*MAJOR REPAIR* STA 1360 RH STA 26R-25R FRAME HAS 2 DENTS OUT OF LIMITSACCOMPLISHED REPAIR ON FRAME PER UPS EO B757-5310-85838-A AND VT MAE E
- [SDR IPXA2023021090857](https://openairdocs.org/sdr/IPXA2023021090857), Feb 10, 2023: SKIN. CHAFED. INSPECTION TYPE:SEG4*MAJOR REPAIR* RH FUSELAGE SKIN AT STA 1862.70 AND WL 235.15 HAS CHAFFING DAMAGEACCOMPLISHED CUTOUT REPAIR IAW SRM 53-80-01-2R-2 DETAIL 2 AN
- [SDR IPXA2023020990834](https://openairdocs.org/sdr/IPXA2023020990834), Feb 9, 2023: FRAME. NONE. INSPECTION TYPE:SEG4*MAJOR REPAIR* UPON INSPECTION FOR EO (B757-5310-73926-A) FOUND AN EXISTING REPAIR AT STA 1560 LH S25L-S27LACCOMPLISHED ALTERNATE INSPECTION
- [SDR IPXA2023020990831](https://openairdocs.org/sdr/IPXA2023020990831), Feb 9, 2023: SKIN. NONE. INSPECTION TYPE:SEG4*MAJOR REPAIR* MAJOR REPAIR LOCATED AT LWR CENTER FUSELAGE IS NOT LISTED ON THE MAJOR REPAIR MAP. REPAIR EXTENDS FROM STA 1490-1520 STR 29R-
- [SDR IPXA2022070883939](https://openairdocs.org/sdr/IPXA2022070883939), Jul 7, 2022: COVER PLATE. BROKEN. INSPECTION TYPE:N/AEMERGENCY EQUIPMENT LIGHT SWITCH COVER WILL NOT CLOSER/R SWITCH GUARD ASSY FOR EMERGENCY EXIT LIGHT SWITCH. IAW AMM 33-51-0-501, AMM 33-51-08
- [SDR IPXA2022061083009](https://openairdocs.org/sdr/IPXA2022061083009), Jun 9, 2022: SLAT SYSTEM. MALFUNCTIONED. EMERGENCY DECLARED, A/C OOS, LE SLAT DISAG WHEN CONFIGURING TO FLAP 1. PROCEDED TO HOLD & WORK CHK LIST. CHK LIST LED US TO LE SLAT ASYM CK LIST. ENDED UP WITH 
- [SDR IPXA2022060682857](https://openairdocs.org/sdr/IPXA2022060682857), Jun 3, 2022: ACM. LEAKING. INSPECTION TYPE:NATHE SMELL OF BURNING RUBBER OCCURRED ONCE AGAIN DURING THE FLIGHTPEFORMED GVI OF BOTH PACKS/ENGS/&APU FOR LEAKS. FOUND HYD LEAK FROM L/H PDU M
- [SDR IPXA2022060182731](https://openairdocs.org/sdr/IPXA2022060182731), Jun 1, 2022: FLEX COUPLING. SHEARED. AFTER TAKEOFF THE SMELL OF BURNING RUBBER ENTERED THE FLIGHT DECK. WE CONTINUED THE CLIMB AND DECIDED TO DECLARE AN EMERGENCY AND DIVERT TO BHM. NO EICAS MSSGS,
- [SDR IPXA2022033080658](https://openairdocs.org/sdr/IPXA2022033080658), Mar 26, 2022: CABLE. BROKEN. INSPECTION TYPE:CON TAKE OFF RECEIVED PARKING BRAKE EICAS AND WARNING HORN AND REJECTED TAKE OFF FOUND PARKING CABLE FRAYED AND BROKE FROM THE HAND BRAKEREMOVED
- [SDR IPXA2021020165190](https://openairdocs.org/sdr/IPXA2021020165190), Feb 1, 2021: DRAG FITTING. CORRODED. INSPECTION TYPE: SEGOUTER WING - UPPER SKIN, DRAG FITTINGS, DIAGONAL BRACE AND SHIM MIGRATION INSPECTION HAS 6 EA HOLES WITH CI/DI INDICATIONS. REPAIRED IAW EA 
- [SDR IPXA2021020165187](https://openairdocs.org/sdr/IPXA2021020165187), Feb 1, 2021: DRAG FITTING. CORRODED. INSPECTION TYPE: SEGOUTER WING - UPPER SKIN, DRAG FITTINGS, DIAGONAL BRACE AND SHIM MIGRATION INSPECTION HAS 6 EA CRACK AND CORROSION INDICATIONS. REPAIRED IAW 
- [SDR IPXA2021012664893](https://openairdocs.org/sdr/IPXA2021012664893), Jan 26, 2021: INTERCOSTAL. CRACKED. INSPECTION TYPE: SEG INTERCOSTAL IN AFT CARGO FROM STA 1500-1520 AT S-30R HAS INDICATIONS OF CORROSION BETWEEN SKIN AND INTERCOSTAL. FOUND CRACK IN INTERCOSTAL 
- [SDR IPXA2021012164711](https://openairdocs.org/sdr/IPXA2021012164711), Jan 21, 2021: FLOOR PANEL. DAMAGED. INSPECTION TYPE: SEG MAIN CARGO COMPARTMENT, FLOOR PANEL 231XMF DAMAGED. FABBED PANEL 231XMF FROM 5024N400001SS-G, BATCH 3489461, PER SREO B757-5320-9692-K.
- [SDR IPXA2021011864576](https://openairdocs.org/sdr/IPXA2021011864576), Jan 18, 2021: FLOOR PANEL. DAMAGED. INSPECTION TYPE: SEG MAIN CARGO COMPARTMENT, FLOOR PANEL 221XCF DAMAGED. FABBED PANEL 221XCF FROM 5024N400001SS-G, BATCH NR 3489461 PER SREO B757-5320-9692-K.
- [SDR IPXA2021011564471](https://openairdocs.org/sdr/IPXA2021011564471), Jan 15, 2021: SKIN. DELAMINATED. INSPECTION TYPE: SEG DELAMINATION MARKED IN RED, .600" DIA CUTOUT, 20" FWD OF THE AFT EDGE AND 32" BELOW THE UPR EDGE OF PANEL. REPAIRED IAW B757 SRM 51-70-10-2
- [SDR IPXA2021011564470](https://openairdocs.org/sdr/IPXA2021011564470), Jan 15, 2021: SKIN. DELAMINATED. INSPECTION TYPE: SEG DELAMINATION MARKED IN RED, .700" CUTOUT, 32" FWD OF THE AFT EDGE AND 52" ABOVE THE LOWER EDGE OF PANEL. REPAIRED IAW B757 SRM 51-70-10-2R,
- [SDR IPXA2021011564469](https://openairdocs.org/sdr/IPXA2021011564469), Jan 15, 2021: SKIN. DELAMINATED. INSPECTION TYPE: SEG DELAMINATION MARKED IN RED .700" DIA CUTOUT, 7" FWD FROM THE AFT EDGE, AND 15.250" BELOW THE UPPER EDGE OF PANEL. REPAIRED IAW B757 SRM 51-
- [SDR IPXA2021011464452](https://openairdocs.org/sdr/IPXA2021011464452), Jan 14, 2021: FLOOR PANEL. DAMAGED. INSPECTION TYPE: N/A FLOOR PANEL 212XAF IS DAMAGED. FABRICATED FLOOR PANEL, IAW SREO B757-5320-9692K.
- [SDR IPXA2021011464451](https://openairdocs.org/sdr/IPXA2021011464451), Jan 14, 2021: FLOOR PANEL. DAMAGED. INSPECTION TYPE: SEG MAIN CARGO COMPARTMENT, FLOOR PANEL 211XAF IS DAMAGED. FABBED PANEL 211XAF FROM 5024N400001SS-G, BATCH 354653, PER SREO B 757-5320-9692-K.
- [SDR IPXA2019112759349](https://openairdocs.org/sdr/IPXA2019112759349), Nov 24, 2019: BATTERY PACK. INOPERATIVE. INSPECTION TYPE:N/AEMERGENCY LIGHTS "UNARMED" LIGHT SWITCH PARTIALLY ILLUMINATEDR&R EMERGENCY LIGHTS BATTERY PACK WITH REF. TO AMM 33-51-07 CKS SATISFACTORY. IP
- [SDR IPXA2019050141640](https://openairdocs.org/sdr/IPXA2019050141640), May 1, 2019: UNKNOWN. ODOR. INSPECTION TYPE:N/A LIGHT DIRTY SOCK SMELL FROM RIGHT PACK WITH ENGINES RUNNING. RAN LEFT AND RIGHT ENG SEPERATE WITH RT PACK ON ONLY, NO SMELLS NOTED, SMALL AP
- [SDR IPXA2018072031889](https://openairdocs.org/sdr/IPXA2018072031889), Jul 17, 2018: DOOR SEAL. TORN. SEAL TORN ON LOWER AFT QUADRANT OF L1 DOOR FRAME. R&R SEAL PER DRAWING 232041642.
- [SDR IPXA2018032127682](https://openairdocs.org/sdr/IPXA2018032127682), Mar 20, 2018: SENSOR. INOPERATIVE. ACFT PRESSURIZED SLOWLY, FAILED TO MAINTAIN CABIN ALTITUDE. R & R THE RT PACK COMPRESSOR OUTLET SENSOR NR 1 IAW AMM 21-51-06-401. PERFORMED PRESSURE LEAKAGE RAT
- [SDR IPXA2016091608299](https://openairdocs.org/sdr/IPXA2016091608299), Sep 15, 2016: DOOR. OUT OF ADJUST. COCKPIT ENTRY DOOR DIFFICULT TO OPEN AND CLOSE. PERFORMED VERTICAL ADJUSTMENT IAW AMM 52-12-00-5, OPS GOOD.
- [SDR IPXA2016072706393](https://openairdocs.org/sdr/IPXA2016072706393), Jul 27, 2016: LIGHT. INOPERATIVE. EMERGENCY LIGHT ASSY HAS 5 LAMPS INOPERATIVE. RELAMPED 5 LAMPS IN THE EMERGENCY LIGHT ASSY IAW AMM 33-51-01-2.
- [SDR IPXA2016050803042](https://openairdocs.org/sdr/IPXA2016050803042), May 8, 2016: SKIN. DENTED. LT WING I/E T/E FLAP UPPER SKIN DENTED 18.75" FROM OTBD EDGE AND 13.5" FROM T/E REPAIRED IAW EO B757-5750-60697-A.

All 176: https://openairdocs.org/aircraft/N414UP/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.