# N401UP: 1987 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: 23723
- Year built: 1987
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 6, 1987
- Certificate issued: December 12, 1998
- Expires: February 28, 2029
- Mode S code: A4B228
- 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=401UP
- Page: https://openairdocs.org/aircraft/N401UP

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 N401UP.

## FAA accident and incident reports (4)

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 19900220007049I](https://openairdocs.org/incident/19900220007049I), Feb 20, 1990: Boeing 75724APF (N401UP), Des Moines, IA. Rapid decrease in NR2 fuel quantity indicator. Secured NR2 engine. Found a faulty fuel indicator.
- [Incident 19881115062609I](https://openairdocs.org/incident/19881115062609I), Nov 15, 1988: Boeing 75724APF (N401UP), Portland, OR, Minor damage. Bird strike into engine on takeoff. Severe vibration, smoke and fire. Emergency landing. Engine being replaced.
- [Incident 19880203069479I](https://openairdocs.org/incident/19880203069479I), Feb 3, 1988: Boeing 75724APF (N401UP), Phoenix, AZ, Minor damage. Lost directional control. Veered off runway. Hydraulic system depleted. Steering and reversers inoperative.
- [Incident 19871006062929I](https://openairdocs.org/incident/19871006062929I), Oct 6, 1987: Boeing 75724APF (N401UP), Billings, MT. Aircraft made a precautionary landing due to low oil quantity. Packing found split on number 1 hydraulic pump.

## Service difficulty reports (299, 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 IPXA2026102139239](https://openairdocs.org/sdr/IPXA2026102139239), Oct 20, 2026: SMOKE GOGGLES. DETERIORATED. SECOND OBSERVERS SMOKE GOGGLES HAVE DETERIORATED FOAM SEAL. REMOVED AND REPLACED SECOND OBSERVERS SMOKE GOGGLES IAW AMM 25-64-00.
- [SDR IPXA2026102039239](https://openairdocs.org/sdr/IPXA2026102039239), Oct 20, 2026: SMOKE GOGGLES. DETERIORATED. SECOND OBSERVERS SMOKE GOGGLES HAVE DETERIORATED FOAM SEAL. REMOVED AND REPLACED SECOND OBSERVERS SMOKE GOGGLES IAW AMM 25-64-00.
- [SDR IPXA2026092926582](https://openairdocs.org/sdr/IPXA2026092926582), Sep 25, 2026: EVAS UNIT. INOPERATIVE. FOUND CAPT EVAS BAD. REMOVED AND REPLACED CAPT EVAS IAW AMM25-69.
- [SDR IPXA2026092526582](https://openairdocs.org/sdr/IPXA2026092526582), Sep 25, 2026: EVAS UNIT. FAILED. FOUND CAPT EVAS BAD
- [SDR IPXA2026042783998](https://openairdocs.org/sdr/IPXA2026042783998), Apr 25, 2026: MODULE. INOPERATIVE. EMERGENCY LIGHTS UNARMED WARNING LIGHT INOPERATIVE. REMOVED AND REPLACED MODULE AND LENS CAP FOR EMERGENCY LIGHT UNARMED LIGHT IAW AMM 33-13.
- [SDR IPXA2025020571335](https://openairdocs.org/sdr/IPXA2025020571335), Jan 24, 2025: ANGLE. CORRODED. APU DOOR SURROUND BETWEEN FS 1790 - FS 1810 STR 6R ANGLE HAS SURFACE CORROSION ALL NUTPLATES ARE CORRODED WITH SCREW SHANKS STILL INSIDE. INSTALLED ANGLE LOWER 
- [SDR IPXA2025020471181](https://openairdocs.org/sdr/IPXA2025020471181), Jan 24, 2025: ANGLE. CORRODED. APU DOOR SURROUND PN 148N3152-2 BETWEEN FS 1790 - 1810 STR 3R ANGLE HAS INTERGRANULAR CORROSION. INSTALLED ANGLE UPPER STR 3 RH SIDE PER B757 SRM 51-40-02. AUDI
- [SDR IPXA2025020495767](https://openairdocs.org/sdr/IPXA2025020495767), Jan 20, 2025: STRAP. CORRODED. CLEAN CORROSION OFF OF STRAP AT FS 1825 S3R - S6R. ACCOMPLISH REPAIR PER 757-200PF SRM REV 122 CHAPTER 53-80-15-2R-1, DETAIL I ON FIGURE 202 (SHEET 2).
- [SDR IPXA2025012994882](https://openairdocs.org/sdr/IPXA2025012994882), Jan 20, 2025: DOOR FRAME. CORRODED. SEVERE CORROSION FOUND ON APU AIR INLET DOOR FRAME. INSTALLED NEW STRAP IAW B757-200, SRM 51-40-02. REVIEWED
- [SDR IPXA2025013155554](https://openairdocs.org/sdr/IPXA2025013155554), Jan 12, 2025: BRACKET. CRACKED. NR 1 ENG PYLON NAC STA.149.5 FRAME I/B HAS ELONGATED HOLES AND 0,5 CRACK. EA-62. INSTALLED NEW FRAME ANGLE ON #1 PYLON. IAW SRM 51-40-02-0G. INSTALLED NEW BRACK
- [SDR IPXA2025013142659](https://openairdocs.org/sdr/IPXA2025013142659), Jan 11, 2025: SKIN. CRACKED. RH WING, FIXED L/E UPPER SKIN, UNDER SLAT #7 O/B, HAS 2,5 IN CRACK AFT PREVIOUS . EA-62. VERIFIED FINAL EA # 757-5741-27-A3772 REV WAS RECEIVED ACCOMPLISHED WIT
- [SDR IPXA2025020543514](https://openairdocs.org/sdr/IPXA2025020543514), Jan 11, 2025: TEE ANGLE. CORRODED. FAULT-STR-ZONE 100. LH MID WING TO BODY STRUCTURE, T-CHORD AT STA 1080-1200, LBL 60 HAS CORROSION. DOT 28-01. INSTALLED NEW T-CHORD AT STA 1080-1200, LBL 60 IAW
- [SDR IPXA2025020543758](https://openairdocs.org/sdr/IPXA2025020543758), Jan 11, 2025: TEE ANGLE. CORRODED. RH WING TO BODY STRUCTURE, T-CHORD AT STA 1260, RBL 10 HAS LIGHT CORROSION. DOT 28-05. NEW T-CHORD IT IS FOUND TO BE INSTALLED IAW B757-200 SRM 51-40-02-0G-0.
- [SDR IPXA2025020444461](https://openairdocs.org/sdr/IPXA2025020444461), Jan 11, 2025: BRACKET. CRACKED. FS 900 LBL12 BRACKET THAT ATTACHES TO INTERCOSTAL TO 900 T-CHORD IS CRACKED INSTALLED NEW BRACKET ON STR FS 900 LBL12 IAW SRM 51-40-02.
- [SDR IPXA2025020444699](https://openairdocs.org/sdr/IPXA2025020444699), Jan 11, 2025: TEE ANGLE. CORRODED. FS 1037-1060 RBL 65 T-CHORD IS EXFOLIATED ON NUTPLATE EDGE. INSTALLED T-CHORD IAW B757-200, SRM 51-40-02 ON STR FS 1037-1060 RBL 65. PERFORMED CPCP STEPS
- [SDR IPXA2025020443836](https://openairdocs.org/sdr/IPXA2025020443836), Jan 11, 2025: TEE ANGLE. CORRODED. .LH WING TO BODY STRUCTURE, T-CHORD AT STA 1020-1040, LBL 30 HAS LIGHT CORROSION. DOT 28-08. INSTALLED 8 NUTPLATE AND T-CHORD AT STA 1020-1040, LBL 30 IAW B757-
- [SDR IPXA2025020443736](https://openairdocs.org/sdr/IPXA2025020443736), Jan 11, 2025: ATTACH BRACKET. CRACKED. FS1180 LBL 13 ON BOTTOM OF FUSELAGE SKIN WTB STR ATTACH BRACKET HAS CRACK IB SIDE OF RADIUS. INSTALLED BRACKET AT FS 1180 LBL 13 OUTER FUSELAGE SKIN TO WTB STR 
- [SDR IPXA2025020444064](https://openairdocs.org/sdr/IPXA2025020444064), Jan 11, 2025: TEE FITTING. CORRODED. FAULT-STR-ZONE 100. RH WING TO BODY STRUCTURE, T-CHORD AT STA 900-920, RBL 60 HAS CORROSION. DOT 28-10. INSTALLED T-CHORD AT STA 900-920 RBL 60 IAW B757 SRM51-4
- [SDR IPXA2025020443668](https://openairdocs.org/sdr/IPXA2025020443668), Jan 11, 2025: TEE FITTING. CORRODED. LH WING TO BODY STRUCTURE, T-CHORD AT STA 1040-1060, LBL 57 HAS LIGHT CORROSION . DOT 28-04. INSTALLED T-CHORD AT STA 1040-1060, LBL 57 LH WING TO BODY STRUCTUR
- [SDR IPXA2025013043970](https://openairdocs.org/sdr/IPXA2025013043970), Jan 11, 2025: TEE FITTING. CORRODED. LH WING TO BODY STRUCTURE, T-CHORD AT STA 1020-1040, LBL 50 HAS 10 NUTPLATES CORRODED. DOT 28-09. INSTALLED T-CHORD AT STA 1020-1040, LBL 50 IAW B757-200, SRM 5
- [SDR IPXA2025020443088](https://openairdocs.org/sdr/IPXA2025020443088), Jan 11, 2025: BRACKET. CRACKED. FS 1180 RBL 13 OUTER FUSELAGE SKIN TO WTB STR BRACKET HAS CRACK ON IB RADIUS. INSTALLED BRACKET AT FS 1180 RBL 13 OUTER FUSELAGE SKIN TO WTB STR IAW B757-200, S
- [SDR IPXA2025020343798](https://openairdocs.org/sdr/IPXA2025020343798), Jan 11, 2025: TEE FITTING. CORRODED. LOWER FUSELAGE STRUCTURE, T-CHORD AT STA 1020-1040, LBL 0, HAS CORROSION. VERIFIED INSTALLATION OF NEW T-CHORD AT STA 1020-1040 RBL 0. P/N BACB30NX8K12, BATCH 0
- [SDR IPXA2025020431025](https://openairdocs.org/sdr/IPXA2025020431025), Jan 10, 2025: SKIN. DENTED. R/H WING, #8 SLAT, UPPER SKIN WITH 8 DENTS (RED CIRCLE). DOT 73-004. RH SLAT#8 P/N 114N4004-172SP SERIAL:A2-0388 , INSTALLED IAW AMM TASK 27-81-02-424-021.
- [SDR IPXA2025012012393](https://openairdocs.org/sdr/IPXA2025012012393), Jan 9, 2025: SKIN. DAMAGED. FUSELAJE ZONE 200 HAS EVIDENCE LIGHTNING STRIKE BETWEEN STA. 1320 TO 1440 (S11-S26). ACCOMPLISH REPAIR PER 757-200PF SRM REV 122 CHAPTER 53-00-01-2R, REPAIR 28 
- [SDR IPXA2025013059623](https://openairdocs.org/sdr/IPXA2025013059623), Jan 7, 2025: SKIN. DENTED. FUSELAGE BETWEEN STA.1896.20 AND STA 1918.9 LEFT UPPER SIDE SKIN HAS DENT (NOT MAPPED). DOT 62-06. EA-62.ACCOMPLISH PERMANENT REPAIR PER 757-200PF SRM REV 121 C
- [SDR IPXA2025020765831](https://openairdocs.org/sdr/IPXA2025020765831), Jan 7, 2025: CAM. GOUGED. *SUPPLEMENTAL SDR* FAULT: STR Z837 - CREW ENTRY DOOR, UPPER AND LOWER LATCH CAM HAVE GOUGES. DOT 62-08. EA-62. VERIFIED SREO-14721-REQ001 REV1 WAS ACCOMPLISHED.
- [SDR IPXA2025020465996](https://openairdocs.org/sdr/IPXA2025020465996), Jan 7, 2025: ANGLE. CRACKED. NR 2 ENG STRAP AT NAC STA. 149.5 HAS CRACK AT HI-LOCK.DOT 69-003. EL-69. INSTALLED FRAME ANGLE IAW SRM 51-40-02-0G. AUDIT COMPLETE.
- [SDR IPXA2025020465427](https://openairdocs.org/sdr/IPXA2025020465427), Jan 7, 2025: BRACKET. CRACKED. FAULT:STR-Z400 #1 ENG PYLON HYD LINE BRACKET DAMAGED AT STRAP.NAC STA 149.5. DOT 69-001. EL-69. INSTALLED NEW FRAME ANGLE ON #1 PYLON. IAW SRM 51-40-02-0G. INST
- [SDR IPXA2025010865831](https://openairdocs.org/sdr/IPXA2025010865831), Jan 7, 2025: CAM. GOUGED. *SDR FILED OPEN* FAULT: STR Z837 - CREW ENTRY DOOR, UPPER AND LOWER LATCH CAM HAVE GOUGES. DOT 62-08. EA-62. APPROVED.
- [SDR IPXA2025011351200](https://openairdocs.org/sdr/IPXA2025011351200), Jan 6, 2025: PANEL. CRACKED. RT WING #8 SLAT OUTBD TRACK GAP PANEL IS CRACKED. DOT 8-010. RH SLAT#8 P/N 114N4004-172SP SERIAL:A2-0388 , INSTALLED IAW AMM TASK 27-81-02-424-021.
- [SDR IPXA2024112636647](https://openairdocs.org/sdr/IPXA2024112636647), Nov 22, 2024: WINDOW. ARCED. R FWD WINDOW STARTED TO ARC. CHECK LIST SAID TO CONTINUE. WINDOW WAS NOT DEFORMED, AIR LEAK NOT OBSERVED. FL370. REMOVED AND REPLACED R1 WINDSHIELD REF MM 56-11
- [SDR IPXA2024112236647](https://openairdocs.org/sdr/IPXA2024112236647), Nov 22, 2024: WINDOW. ARCED. RT FWD WINDOW STARTED TO ARC. CHECK LIST SAID TO CONTINUE. WINDOW WAS NOT DEFORMED, AIR LEAK NOT OBSERVED. FL370 REMOVED AND REPLACED R1 WINDSHIELD REF MM 56-11
- [SDR IPXA2023030791651](https://openairdocs.org/sdr/IPXA2023030791651), Mar 1, 2023: FLAP. NONE. INSPECTION TYPE:N/A*A/C WAS OOS* *ATB* *EMER DECL* TE FLAPS DISAGREE EICAS MESSAGE WHEN SELECTING FLAPS UP AT APPROX 1500 FT.REPL TORQ TUBE FOR RT INBD FLP OUTB
- [SDR IPXA2023021190887](https://openairdocs.org/sdr/IPXA2023021190887), Feb 11, 2023: FRAME. NONE. INSPECTION TYPE:SEG1*MAJOR REPAIR* EXISTING REPAIR FOUND AT AFT CARGO COMPT FRAME STA 1360, S-26L.ACCOMPLISHED REPAIR PER UPS EO# B757-5310-85613-A AND EA# 757-
- [SDR IPXA2023021190870](https://openairdocs.org/sdr/IPXA2023021190870), Feb 10, 2023: FRAME. NONE. INSPECTION TYPE:SEG1*MAJOR REPAIR* EXISTING REPAIR FOUND FRAME 1320, STR 25R TO 26R.ACCOMPLISHED REPAIR IAW UPS EO B757-5310-85615-A
- [SDR IPXA2022062283383](https://openairdocs.org/sdr/IPXA2022062283383), Jun 22, 2022: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS INOP. EMERGENCY LIGHTS INOP.R/R BATTERY PACK PER AMM 33-51-07 OPS CHECK GOOD.
- [SDR IPXA2021032067038](https://openairdocs.org/sdr/IPXA2021032067038), Mar 20, 2021: TEE FITTING. CORRODED. INSPECTION TYPE:SEG4RH WTB FAIRING STRUCTURE TEE CHORD AT STA 1180-1186 RBL 30.75REMOVED AND REPLACED TEE CHORD IAW SRM 51-40-02-OG
- [SDR IPXA2021032067037](https://openairdocs.org/sdr/IPXA2021032067037), Mar 20, 2021: TEE FITTING. CORRODED. INSPECTION TYPE:SEG4RH WTB FAIRING STRUCTURE TEE CHORD AT STA 1180 RBL 20-30 HAS SEVERE CORROSIONREMOVED AND REPLACED TEE CHORD IAW SRM 51-40-02
- [SDR IPXA2021032067033](https://openairdocs.org/sdr/IPXA2021032067033), Mar 20, 2021: STRINGER. CORRODED. INSPECTION TYPE:SEG4S-29L AT STA 1664 IS CORRODED AND REQUIRES REPAIRREPAIR AREA IAW SRM 53-00-03-2R-1
- [SDR IPXA2021032067032](https://openairdocs.org/sdr/IPXA2021032067032), Mar 20, 2021: FRAME. DENTED. INSPECTION TYPE:SEG4FRAME LIP AT STA 660 STR24 RT LIP IS DELAMINATEDREPAIRED IAW SRM 53-00-07-2R-5 DETAIL II
- [SDR IPXA2019122750421](https://openairdocs.org/sdr/IPXA2019122750421), Dec 27, 2019: EVAS UNIT. LOOSE. CAPTAIN`S EVAS UNIT WAS LOOSE & NOT SECURED TO THE MANUAL BIN. REMOVED THE EVAS SYSTEM AND BRACKET DUE TO RIVETS PULLED THROUGH. PREPARED & INSTALLED THE ANCHOR
- [SDR IPXA2019122645354](https://openairdocs.org/sdr/IPXA2019122645354), Dec 22, 2019: ENGINE. SURGES. ATB - LT ENG SURGE AT 1300FT. TAKE OFF THRUST.RAN BOTH ENGINES AT EPR SETTING OF THE DAY AND PERFORMED FIM TASK 73-21-00-815-813-P00, NO DEFECTS NOTED, OK FOR S
- [SDR IPXA2019031239983](https://openairdocs.org/sdr/IPXA2019031239983), Mar 12, 2019: FLOOR PANEL. DAMAGED. INSPECTION TYPE:C1 MAIN CARGO FLOOR PANEL 232XDF REQUIRES FAB. FABBED PANEL 232XDF FROM 5024N0000155-G, BATCH # 3441868 PER SREO B757-5320-9692-K.
- [SDR IPXA2019031139952](https://openairdocs.org/sdr/IPXA2019031139952), Mar 11, 2019: FLOOR PANEL. DAMAGED. INSPECTION TYPE:C1 MAIN CARGO FLOOR PANEL 232XEF REQUIRES FAB. FABBED PANEL 232 XEF FROM 2024N0000155-G,BATCH # 3441868 PER SREO B757=5320-9692-K.
- [SDR IPXA2019031139951](https://openairdocs.org/sdr/IPXA2019031139951), Mar 11, 2019: FLOOR PANEL. DAMAGED. INSPECTION TYPE:C1 MAIN CARGO FLOOR PANEL 231XBF REQUIRES FAB. FABBED PANEL 231XBF FROM 5024N0000155-G, BATCH # 3441868 PER SREO B757-5320-9692-K.
- [SDR IPXA2019031139950](https://openairdocs.org/sdr/IPXA2019031139950), Mar 11, 2019: FLOOR PANEL. DAMAGED. INSPECTION TYPE:C1 MAIN CARGO FLOOR PANEL 231XCF REQUIRES FAB. FABBED PANEL 231XCF FROM 504N0000155-G, BATCH # 3441868 PER SREO B757-5320-9692-K.
- [SDR IPXA2019031139946](https://openairdocs.org/sdr/IPXA2019031139946), Mar 11, 2019: FLOOR PANEL. DAMAGED. INSPECTION TYPE:C1 MAIN CARGO FLOOR PANEL 231XDF REQUIRES FAB. FABBED PANEL 231XDF FROM 5024N0000155-G,BATCH# 3441868 PER SREO B757-5320-9692-K.
- [SDR IPXA2019031139945](https://openairdocs.org/sdr/IPXA2019031139945), Mar 11, 2019: FLOOR PANEL. DAMAGED. INSPECTION TYPE:C1 MAIN CARGO FLOOR PANEL 231XEF REQUIRES FAB. FABBED PANEL 231XEF FROM 5024N0000155-G, BATCH# 3441868 PER SREO B757-5320-9692-K.
- [SDR IPXA2019031139943](https://openairdocs.org/sdr/IPXA2019031139943), Mar 11, 2019: FLOOR PANEL. DAMAGED. INSPECTION TYPE:C1 MAIN CARGO FLOOR PANEL 231XEF REQUIRES FAB. FABBED PANEL 231XEF FROM 5024N0000155-G, BATCH # 3441868 PER SREO B757-5320-9692-K.
- [SDR IPXA2019031139942](https://openairdocs.org/sdr/IPXA2019031139942), Mar 11, 2019: FLOOR PANEL. DAMAGED. INSPECTION TYPE:C1 MAIN CARGO FLOOR PANEL 231XGF REQUIRES FAB. FABBED PANEL 231XGF FROM 50240000155-G, BATCH# 3441868 PER SREO B757-5320-9692.

All 299: https://openairdocs.org/aircraft/N401UP/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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