# N410UP: 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: 23732
- Year built: 1988
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 1, 1988
- Certificate issued: May 21, 1999
- Expires: May 31, 2027
- Mode S code: A4D5F0
- 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=410UP
- Page: https://openairdocs.org/aircraft/N410UP

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 N410UP.

## 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 19920319009049I](https://openairdocs.org/incident/19920319009049I), Mar 19, 1992: Boeing 75724APF (N410UP), Omaha, NE. Aircraft departed taxiway while taxiing to runway. Had temporary taxiway signs. Apparently crew did not see them.

## Service difficulty reports (130, 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 IPXA2026061692797](https://openairdocs.org/sdr/IPXA2026061692797), Jun 16, 2026: FUEL TANK. WARNING MESSAGE. RIGHT CENTER FUEL TANK PRESS ICAS. CENTER TANK HAD 3.8K USABLE FUEL ACCOMPLISHED DMP PER MEL 28-22-2-0-1
- [SDR IPXA2026020246985](https://openairdocs.org/sdr/IPXA2026020246985), Jan 30, 2026: LAMP. INOPERATIVE. EMERGENCY EXIT LIGHT- MANY LAMPS INOP. RELAMPED ALL EMERGENCY EXIT LIGHT, OPS CHECKS NORMAL IAW AMM 33-51-00-501.
- [SDR IPXA2026012369147](https://openairdocs.org/sdr/IPXA2026012369147), Jan 12, 2026: TEE FITTING. CORRODED. RIGHT WW EXTERNAL STRUCTURE BETWEEN BS 1040 - 1060 INTERCOSTAL DELAMINATED. INSTALLED NEW T-FITTING, IAW SRM 51-40-02-0G-0.
- [SDR IPXA2026012769147](https://openairdocs.org/sdr/IPXA2026012769147), Jan 12, 2026: INTERCOSTAL. DELAMINATED. RIGHT W/W EXTERNAL STRUCTURE BETWEEN STA 1040 TO 1060 INTERCOSTAL WITH DELAMINATION DOT 07-060 REVIEWED
- [SDR IPXA2026012356310](https://openairdocs.org/sdr/IPXA2026012356310), Jan 11, 2026: TEE FITTING. CORRODED. LOWER FUSELAGE RT SIDE STA 1200 T-FITTING EXFOLIATED. INSTALLED A NEW T-FITTING IAW SRM 51-40-02-0G.
- [SDR IPXA2026012353616](https://openairdocs.org/sdr/IPXA2026012353616), Jan 11, 2026: TEE ANGLE. CORRODED. EXTERNAL FUSELAGE LT W/W BETWEEN STA 1060 TO 1080 INTERCOSTAL HAS CORROSION. INSTALLED NEW T-CHORD / INTERCOSTAL I.A.W. B757-200 SRM 51-40-02-0G-0.
- [SDR IPXA2026012314754](https://openairdocs.org/sdr/IPXA2026012314754), Jan 8, 2026: TEE FITTING. CORRODED. RT WING TO BODY FAIRING PANEL 196CR AREA, BTWN STA 1180 AND STA 1200, T-FITTING EXFOLIATED. INSTALLED NEW T-FITTING 1 EA RT WING TO BODY FAIRING PANEL 196CR BTW
- [SDR IPXA2026012314576](https://openairdocs.org/sdr/IPXA2026012314576), Jan 8, 2026: TEE FITTING. CORRODED. RIGHT RAM AIR EXHAUST, BTWN BS 1040 AND 1060, OTBD T-FITTING CORRODED. INSTALLED NEW T-CHORD/ INTERCOSTAL I.A.W. B757-200 SRM 51-40-02-0G-0
- [SDR IPXA2026012734754](https://openairdocs.org/sdr/IPXA2026012734754), Jan 8, 2026: TEE FITTING. CORRODED. RIGHT WING TO BODY FAIRING PANEL 196CR AREA, BTWN STA 1180 AND STA 1200, T-CHORD EXFOLIATED. DOT 90-018 REVIEWED
- [SDR IPXA2026012174949](https://openairdocs.org/sdr/IPXA2026012174949), Jan 6, 2026: SKIN. CRACKED. LEFT WING FIXED L/E COMPOSITE SKIN WAS CRACKED, 5 INCHES IN LENGTH, UNDER SLAT NR 2. ACCOMPLISHED THE PERMANENT REPAIR IAW EO 96311-REQ1 & EA 757-5741-27-A4276 
- [SDR IPXA2026011271869](https://openairdocs.org/sdr/IPXA2026011271869), Jan 6, 2026: ANGLE. CORRODED. APU INLET DOOR UPPER ANGLE FROM BS 1787.45 - 1825.00, S3R WAS CORRODED. INSTALLED A NEW UPPER ANGLE IAW SRM 51-40-02-0G-0.
- [SDR IPXA2026012174971](https://openairdocs.org/sdr/IPXA2026012174971), Jan 6, 2026: SKIN. CRACKED. RIGHT WING FIXED L/E COMPOSITE SKIN WAS CRACKED UNDER SLAT NR 7, ON OTBD END. WORK ACCOMPLISHED IAW EA 757-5741-27-4268, REV-, PRELIM 1 EO-96233 REQ 1, AND EA 7
- [SDR IPXA2026011572116](https://openairdocs.org/sdr/IPXA2026011572116), Jan 6, 2026: STRAP. CORRODED. MAJOR REPAIR. APU INLET DOOR AFT STRAP AT BS 1825.00 FROM S3 - 6R WAS CORROED (EXISTING REPAIR FOUND IN THE AREA) INSTALLED NEW FILLER MIDDLE STRAP IAW SRM 51-4
- [SDR IPXA2026011272419](https://openairdocs.org/sdr/IPXA2026011272419), Jan 6, 2026: ANGLE. CORRODED. APU INLET DOOR LOWER CORNER ANGLE AT STA 1787.45 AT S-6R HAS CORROSION. INSTALLED NEW LOWER CORNER ANGLE I.A.W. B757-200 SRM 51-40-02-0G-0.
- [SDR IPXA2026011271946](https://openairdocs.org/sdr/IPXA2026011271946), Jan 6, 2026: ANGLE. CORRODED. APU INLET DOOR LOWER ANGLE FROM STA 1787.45 TO STA 1825.00 S-6R HAS CORROSION. INSTALLED NEW LOWER ANGLE IAW SRM 51-40-02-0G-0. REVIEWED
- [SDR IPXA2026012644037](https://openairdocs.org/sdr/IPXA2026012644037), Jan 4, 2026: SKIN. DELAMINATED. MAJOR REPAIR. APU COMPARTMENT LT SIDEWALL INNER SKIN WAS DELAMINATED APPROX 8"X10" AREA BETWEEN BS 1918 AND 1941 17 INCHES ABOVE THE LWR FRAME. VERIFIED COMPLET
- [SDR IPXA2026012643865](https://openairdocs.org/sdr/IPXA2026012643865), Jan 4, 2026: SKIN. DENTED. MAJOR REPAIR, APU COMPARTMENT RT SIDEWALL INNER SKIN HAS DENTED & CRACKED BETWEEN BS 1918 AND 1941 APPROX 26 INCHES ABOVE THE LWR FRAME. VERIFIED REPAIR IS A CA
- [SDR IPXA2026012843933](https://openairdocs.org/sdr/IPXA2026012843933), Jan 4, 2026: SKIN. DELAMINATED. MAJOR REPAIR, COMPOSITE APU COMPARTMENT: APU COMPARTMENT INNER SKIN INCLUDING OUTER SKIN HAS DELAMINATION BETWEEN BS 1918 & 1941 17 INCHES ABOVE THE LWR FRAME A
- [SDR IPXA2026011240212](https://openairdocs.org/sdr/IPXA2026011240212), Jan 3, 2026: STRAP. CORRODED. BS 1787.45, CORROSION ON THE UNDERSIDE OF THE APU DOOR SURROUND STRUCTURE FROM S3 - 6R. INSTALLED A NEW FWD STRAP IAW SRM 51-40-02-0G-0.
- [SDR IPXA2026011740349](https://openairdocs.org/sdr/IPXA2026011740349), Jan 3, 2026: TEE FITTING. CORRODED. CORROSION FOUND AT WTB T-FITTING FROM BS 1180 TO 1240 RBL 63 INSTALLED NEW T-FITTING IAW SRM 51-40-02-0G.
- [SDR IPXA2024100790244](https://openairdocs.org/sdr/IPXA2024100790244), Aug 9, 2024: FLOORBOARD. CORRODED. MCD RT SIDE #2 PALLET LOCATION FLOOR BOARD CORRODED/MISSING SEALANT BETWEEN NEXT PANEL REMOVED FLOORBOARD FOR RII AND INSTALLED REF AMM 53-01-01-424-023.
- [SDR IPXA2024081291000](https://openairdocs.org/sdr/IPXA2024081291000), Aug 9, 2024: FLOORBOARD. DAMAGED. MCD FLOOR BOARD DAMAGED - 6TH AFT OF BULKHEAD ( AFT OF MAIN CARGO DOOR ) PANEL REMOVED AND ROUTED TO SHEET METAL SHOP REF B757 AMM 53-01-01. VERIFIED MATERIAL U
- [SDR IPXA2024030435420](https://openairdocs.org/sdr/IPXA2024030435420), Mar 1, 2024: METERING VALVE. FAULTED. DURING PREFLIGHT BRAKE PRESSURE ACCUMULATOR LOSES PRESSURE FROM 3000 PSI TO 2500 PSI IN 1 MINUTE. POSSIBLE PRESSURE LEAK IN ACCUMULATOR. PRESSURIZED TO RESET ST
- [SDR IPXA2024012989730](https://openairdocs.org/sdr/IPXA2024012989730), Jan 11, 2024: FAIRING. CRACKED. FAULT: L/H PYLON INBD STRUT AFT FAIRING HAS A SUPPORT CRACKED AT NAC STA 203.85 INSTALLED NEW CHORD IAW SRM 51-40-02.
- [SDR IPXA2024011289730](https://openairdocs.org/sdr/IPXA2024011289730), Jan 11, 2024: UNKNOWN. UNKNOWN. L/H PYLON INBD STRUT AFT FAIRING HAS A SUPPORT CRACKED AT NAC STA 203.85 APPROVED
- [SDR IPXA2024012945677](https://openairdocs.org/sdr/IPXA2024012945677), Jan 9, 2024: LATCH. WORN. *** SUPPLEMENTAL SDR *** FAULT CREW ENTRY DOOR UPPER AND LOWER LATCH CAMS HAVE WEAR MARKS DOT47-07 TREATED AND PRIMED LATCH CAM IAW SRM 51-20-01 STEP 5
- [SDR IPXA2024012943096](https://openairdocs.org/sdr/IPXA2024012943096), Jan 9, 2024: SKIN. DAMAGED. *** SUPPLEMENTAL SDR *** FAULT : # 8 SLAT NOSE SKIN EXISTING REPAIR HAS A VOID SEALANT REPAIRED SEALANT IAW SOPM 20-50-19 STEP 20.
- [SDR IPXA2024012935491](https://openairdocs.org/sdr/IPXA2024012935491), Jan 9, 2024: STRUCTURE. DELAMINATED. FAULT: L/H ELEVATOR O/B T/E TIP HAS DELAMINATED. DOT 33-002 FABRICATED SHIMS PER BMS7-335 STEP 5.2 ON MATERIAL 2024T30.040 BATCH#0003813619, INSTALL SHIM PER SO
- [SDR IPXA2024012435373](https://openairdocs.org/sdr/IPXA2024012435373), Jan 9, 2024: ROD END. CORRODED. FAULT: L/H HORIZONTAL STAB O/B POGO STICK ROD END HAS CORROSION. DOT 33-000. REMOVED AND INSTALLED LH HORIZONTAL STAB O/B POGO STICK ROD END IAW AMM 27-31-05-02
- [SDR IPXA2024011745677](https://openairdocs.org/sdr/IPXA2024011745677), Jan 9, 2024: LATCH. WORN. FAULT CREW ENTRY DOOR UPPER AND LOWER LATCH CAMS HAVE WEAR MARKS DOT47-07 CREW DOOR UPPER LATCH CAM WE WILL INSTALL ON N/R 6100412629 ; T3F18E003R8UZ
- [SDR IPXA2024011043096](https://openairdocs.org/sdr/IPXA2024011043096), Jan 9, 2024: UNKNOWN. UNKNOWN. *SDR FILED OPEN* FAULT : # 8 SLAT NOSE SKIN EXISTING REPAIR HAS A VOID SEALANT APPROVED
- [SDR IPXA2024010935491](https://openairdocs.org/sdr/IPXA2024010935491), Jan 9, 2024: UNKNOWN. UNKNOWN. *SDR FILED OPEN* FAULT: L/H ELEVATOR O/B T/E TIP HAS DELAMINATED. DOT 33-002
- [SDR IPXA2024012928961](https://openairdocs.org/sdr/IPXA2024012928961), Jan 8, 2024: EXHAUST CONE. GOUGED. FAULT#2 ENG EXHAUST CONE LOWER OUTBD AREA BETWEEN 4 AND 5'0' CLOCK POSITION HAS A GOUGE DOT 47-04 AFTER REVEIWING DAMAGED AREA THE DISCREPANCY WAS FOUND TO BE A
- [SDR IPXA2024010928961](https://openairdocs.org/sdr/IPXA2024010928961), Jan 8, 2024: UNKNOWN. UNKNOWN. *SDR FILED OPEN* FAULT#2 ENG EXHAUST CONE LOWER OUTBD AREA BETWEEN 4 AND 5'0' CLOCK POSITION HAS A GOUGE DOT 47-04 APPROVED
- [SDR IPXA2024012908224](https://openairdocs.org/sdr/IPXA2024012908224), Jan 6, 2024: SKIN. DAMAGED. *** SUPPLEMENTAL SDR *** FAULT- TWO SCRATCHES 0N THE RIGHT SIDE FUSELAGE SKIN AT STA 320, S-14R. DOT 8-001 AFTER FURTHER EVALUATION NO DAMAGE WAS FOUND. ONLY TO
- [SDR IPXA2024010808224](https://openairdocs.org/sdr/IPXA2024010808224), Jan 6, 2024: UNKNOWN. UNKNOWN. OPEN. TWO SCRATCHES 0N THE RIGHT SIDE FUSELAGE SKIN AT STA 320, S-14R. DOT 8-001 APPROVED
- [SDR IPXA2023122288826](https://openairdocs.org/sdr/IPXA2023122288826), Dec 21, 2023: OIL SYSTEM. ABNORMAL. *** DIVERSION *** *** IFSD *** IN CRUISE, RT OIL PRESSURE 0, OIL PRESS RED (APPROX 45) QRH PROCEDURE FOLLOWED, ENG SHUTDOWN PERFORMED WINDMILL INSPECTION, REF T
- [SDR IPXA2023122288097](https://openairdocs.org/sdr/IPXA2023122288097), Dec 21, 2023: ENGINE. SHUTDOWN. *** SUPPLEMENTAL SDR *** DUE TO RH ENGINE SHUTDOWN IN FLIGHT ENGINE WINDMILLING INSPECTION IAW AMM 72-00-216-499-P00 REQUIRED NO. 2 ENGINE: REMOVE ESN 717921 (T
- [SDR IPXA2023122188097](https://openairdocs.org/sdr/IPXA2023122188097), Dec 21, 2023: UNKNOWN. UNKNOWN. *** DIVERSION *** *** IFSD *** DUE TO RH ENGINE SHUTDOWN IN FLIGHT ENGINE WINDMILLING INSPECTION IAW AMM 72-00-216-499-P00 REQUIRED DUE TO FINDINGS ON ENGINE WI
- [SDR IPXA2022112388381](https://openairdocs.org/sdr/IPXA2022112388381), Nov 23, 2022: A/C PACK. NOISY. AT HIGH POWER SETTINGS (I.E TAKE OFF ROLL) RIGHT PACK MAKES A VERY LOUD HIGH PITCH NOISE. DEFERRED RT PACK SYS PER MEL 21-51-1. DMP C/W. PLACARD INSTALLED. THIS
- [SDR IPXA2022022079195](https://openairdocs.org/sdr/IPXA2022022079195), Jan 31, 2022: FRAME. NONE. INSPECTION TYPE:C** SUPPLEMENTAL SDR**PREVIOUS REPAIR AT FRAME STA 1240, FROM S-25R TO S-28RREPAIRED PER UPS EO B757-24237-C AND VT MAE EA 757-5360-A2812 REV-
- [SDR IPXA2022022079197](https://openairdocs.org/sdr/IPXA2022022079197), Jan 31, 2022: FRAME. NONE. INSPECTION TYPE:CPREVIOUS REPAIR AT FR STA 1300, BETWEEN STR 23L AND 28LREPAIRED PER UPS EO B757-5310-24249-C AND VT MAE EA 757-5360-27-A2816 REV-
- [SDR IPXA2022022079196](https://openairdocs.org/sdr/IPXA2022022079196), Jan 31, 2022: FRAME. NONE. INSPECTION TYPE:CPREVIOUS REPAIR AT FRAME STA 1280, FROM S-23R TO S-26RREPAIRED PER UPS EO B757-5310-82771-A AND VT MAE EA 757-5360-A2813 REV-
- [SDR IPXA2020112562770](https://openairdocs.org/sdr/IPXA2020112562770), Nov 23, 2020: WARNING MESSAGE. ILLUMINATED. INSPECTION TYPE: N/A ATB. TAT PROBE EICAS ON TAKEOFF, AIR TURN BACK. REMOVED AND REPLACED TAT PROBE, IAW MM 34-12-02-024-033. OPERATIONS CHECKS GOOD. IPC 34-12-
- [SDR IPXA2020022655502](https://openairdocs.org/sdr/IPXA2020022655502), Feb 25, 2020: FLOOR PANEL. DAMAGED. INSPECTION TYPE:C1FLOOR PANEL 211XAF IS DAMAGEDFABRICATED NEW PANEL 211XAF IAW SREO B757 5320-9692-K
- [SDR IPXA2020022645440](https://openairdocs.org/sdr/IPXA2020022645440), Feb 24, 2020: FLOOR PANEL. DAMAGED. INSPECTION TYPE:C1MAIN CARGO COMPARTMENT, FLOOR PANEL 251XRF DAMAGEDFABBED PANEL 146N5361-29 FROM 5024N400001SS-G, BATCH# 3525521 PER SREO B757-5320-9692-K
- [SDR IPXA2020022645435](https://openairdocs.org/sdr/IPXA2020022645435), Feb 24, 2020: FLOOR PANEL. DAMAGED. INSPECTION TYPE:C1MAIN CARGO COMPARTMENT, FLOOR PANEL 252XUF DAMAGEDFABBED PANEL 146N5361-45 FROM 5024N400001SS-G, BATCH 3525521 PER SREO B757-5320-9692-K
- [SDR IPXA2020022152333](https://openairdocs.org/sdr/IPXA2020022152333), Feb 21, 2020: FLOOR PANEL. DAMAGED. INSPECTION TYPE:SEG3MAIN CARGO COMPARTMENT FLOOR PANEL 252XRF DAMAGEDFABBED PANEL 146N5361-18 FROM 5024N400001SS-G BATCH# 3525521 PER SREO B757-5320-9692-K
- [SDR IPXA2020022152332](https://openairdocs.org/sdr/IPXA2020022152332), Feb 21, 2020: FLOOR PANEL. DAMAGED. INSPECTION TYPE:SEG3MAIN CARGO COMPARTMENT FLOOR PANEL 114N5410-6 DAMAGEDFABBED PANEL 114N5410-6 FROM 5024N400001SS-G BATCH# 3525521 PER SREO B757-5320-9692-K
- [SDR IPXA2020022152331](https://openairdocs.org/sdr/IPXA2020022152331), Feb 21, 2020: FLOOR PANEL. DAMAGED. INSPECTION TYPE:SEG3MAIN CARGO COMPARTMENT FLOOR PANEL 114N5410-5 DAMAGEDFABBED PANEL 114N5410-5 FROM 5024N400001SS-G BATCH# 3525521 PER SREO B757-5320-9692-K

All 130: https://openairdocs.org/aircraft/N410UP/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.