# N435UP: 1993 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: 25466
- Year built: 1993
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 21, 1993
- Certificate issued: November 15, 1993
- Expires: November 30, 2028
- Mode S code: A53781
- 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=435UP
- Page: https://openairdocs.org/aircraft/N435UP

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 N435UP.

## FAA accident and incident reports

None matched to N435UP.

## Service difficulty reports (188, 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 IPXA2025091892090](https://openairdocs.org/sdr/IPXA2025091892090), Sep 9, 2025: ANGLE. CORRODED. AFT UPPER FUSELAGE AT APU INLET AREA, STA 1787.45-1825, STR 6R, AFT LOWER ANGLE DELAMINATED. INSTALLED NEW AFT LOWER ANGLE IAW SRM 51-40-02-0G.
- [SDR IPXA2025092198447](https://openairdocs.org/sdr/IPXA2025092198447), Sep 9, 2025: SUPPORT ANGLE. CRACKED. FWD CARGO COMPT BS 560 E5 EE RACK BULKHEAD DECOMPRESSION PANEL SUPPORT O/B ANGLE HAS A CRACK. INSTALLED NEW ANGLE FROM FWD CARGO COMPT BS 560 E5 EE RACK BULKHEA
- [SDR IPXA2025092190774](https://openairdocs.org/sdr/IPXA2025092190774), Sep 9, 2025: FLOOR SUPPORT. CORRODED. ANGLE CORRODED AT STA 1716 RBL 33 UNDER AFT FLOOR DECK. INSTALLED NEW ANGLE FROM AT STA 1716 RBL 33 UNDER AFT FLOOR DECK IAW B757-200 SRM 51-40-02-0G.
- [SDR IPXA2025092191420](https://openairdocs.org/sdr/IPXA2025092191420), Sep 9, 2025: COVER. CHAFED. NR 1 ENG UPPER PYLON GAP PANEL HAS LARGE CHAFE ON PREVIOUS METAL REPAIR DOT 55-104. INSTALLED NEW DOUBLER IAW B757-200 AMM 51-21-15. VERIFIED INSTALLATION OF DO
- [SDR IPXA2025091762364](https://openairdocs.org/sdr/IPXA2025091762364), Sep 7, 2025: INTERCOSTAL. CORRODED. RIGHT W/W STA 1040 - 1060, RBL 62 INTERCOSTAL T-CHORD CORRODED. INSTALLED NEW T-CHORD IAW B757-200PF SRM 51-40-02-0G-0.
- [SDR IPXA2025092164563](https://openairdocs.org/sdr/IPXA2025092164563), Sep 7, 2025: DOUBLER. CRACKED. RIGHT WING, PANEL 621PB, TRACK CUTOUT, BRACKET IS BENT AND HAS A CRACK. DOT 103-788. INSTALLED NEW DOUBLER (BRACKET) ON PANEL 621PB, IAW B757-200PF SRM 51-40-02
- [SDR IPXA2025092150063](https://openairdocs.org/sdr/IPXA2025092150063), Sep 6, 2025: SUPPORT ANGLE. DELAMINATED. AFT UPPER FUSELAGE AT APU INLET AREA, BS 1787.45, STR 6R, FWD LOWER ANGLE DELAMINATED. INSTALLED NEW FWD LOWER ANGLE IAW SRM 51-40-02-0G.
- [SDR IPXA2025092248757](https://openairdocs.org/sdr/IPXA2025092248757), Sep 6, 2025: SUPPORT CHANNEL. CRACKED. RIGHT WW FWD SEAL RETAINER SUPPORT FRAME O/B AREA HAS A CRACK. INSTALLED SUPPORT CHANNEL AT RT WW IAW SRM 51-40-02.
- [SDR IPXA2025092341988](https://openairdocs.org/sdr/IPXA2025092341988), Sep 6, 2025: CRANK ASSY. GOUGED. CREW ENTRY DOOR FWD EDGE LOWER ROLLR CRANK FITTING GOUGED. VERIFIED ACCOMPLISHED SREO 14721-REQ001 REV 1.
- [SDR IPXA2025092341857](https://openairdocs.org/sdr/IPXA2025092341857), Sep 6, 2025: CRANK ASSY. GOUGED. CREW ENTRY DOOR FWD EDGE UPPER ROLLER CRANK FITTING GOUGED AT BOTTOM SIDE. VERIFIED ACCOMPLISHED SREO 14721-REQ001 REV 1.
- [SDR IPXA2025090841988](https://openairdocs.org/sdr/IPXA2025090841988), Sep 6, 2025: ROLLER. GOUGED. CREW ENTRY DOOR FWD EDGE LOWER ROLLR CRANK FITTING GOUGED.
- [SDR IPXA2025090841857](https://openairdocs.org/sdr/IPXA2025090841857), Sep 6, 2025: FITTING. GOUGED. CREW ENTRY DOOR FWD EDGE UPPER ROLLER CRANK FITTING GOUGED AT BOTTOM SIDE.
- [SDR IPXA2024100923436](https://openairdocs.org/sdr/IPXA2024100923436), Oct 8, 2024: ESCAPE REEL. TWISTED. ALL 6 EMER DECENT REELS ATTACHMENT CABLES MIS-ROUTED AND TWISTED TOGETHER. RE-ROUTED / UNTANGLED DECENT REEL CABLES TO PROPER ROUTING PER B757 AMM 25-61-02-201 
- [SDR IPXA2023110561462](https://openairdocs.org/sdr/IPXA2023110561462), Nov 1, 2023: FRAME. DENTED. FAULT: AFT CARGO FRAME STA 1240 LH BETWEEN STR 25L AND STR 26L HAS A DENT ACCOMPLISHED REPAIR PER 757-200 PF SRM REV 118 CHAPTER 53-00-07-2R6 DETAIL I PERSRM 53
- [SDR IPXA2023111651813](https://openairdocs.org/sdr/IPXA2023111651813), Oct 31, 2023: SEAT TRACK. CORRODED. FAULT: MAIN CARGO CABIN SEAT TRACK BETWEEN FR. STA. 1180 AND FR. STA. 1200 AT RBL 45.5 HAS 4 EACH DAMAGED AND CORRODED FASTENER HOLES. REMOVED SEAT TRACK SECTIO
- [SDR IPXA2023111379564](https://openairdocs.org/sdr/IPXA2023111379564), Oct 26, 2023: FRAME. DENTED. AFT CARGO COMPT. FRAME STA 1340 LH, HAS A DENT, BETWEEN S-23L TO S-25L ACCOMPLISH EO-88596-REQ1 AND EA 757-5360-27-A3417. AUDIT COMPLETE.
- [SDR IPXA2023111379398](https://openairdocs.org/sdr/IPXA2023111379398), Oct 26, 2023: FRAME. DENTED. MAJOR REPAIR, AFT CARGO COMPT. FRAME STA 1620 LH, HAS A DENT, BETWEEN S-24L TO S-26L ACCOMPLISHED REINFORCIND ANGLE REPAIR, IAW PER 757-200PF SRM REV 118.00 CHA
- [SDR IPXA2023111380640](https://openairdocs.org/sdr/IPXA2023111380640), Oct 26, 2023: FRAME. DENTED. MAJOR REPAIR, DENT AT FRAME STA 1520 RH BETWEEN STR25 TO STR 26R. ACCOMPLISH 757-5360-27-A3418 AND EO-88667-REQ1.
- [SDR IPXA2023111079548](https://openairdocs.org/sdr/IPXA2023111079548), Oct 26, 2023: FRAME. DENTED. FWD CARGO STA 680 R/H, HAS DENT BETWEEN S-24R TO S-25R. ACCOMPLISHED REPAIR PER 757-200PF SRM REV 118 CHAPTER 53-00-07-2R-5, DETAIL I PER SRM 53-30-07-2R. REPAI
- [SDR IPXA2023111079532](https://openairdocs.org/sdr/IPXA2023111079532), Oct 26, 2023: FRAME. DENTED. MAJOR REPAIR. AFT CARGO COMPT. FRAME STA 1320LH HAS A DENT BETWEEN S-23L TO S-25L. INSPECTED AND VERIFIED REPAIR ACCOMPLISHED IAW EO-88597-REQ1 AND VTMAE EA#757
- [SDR IPXA2023110679480](https://openairdocs.org/sdr/IPXA2023110679480), Oct 26, 2023: FRAME. DENTED. FWD CARGO STA 660 R/H HAS A DENT BETWEEN S-24R TO S-25R. ACCOMPLISHED REPAIR PER 757-200PF SRM REV 118 CHAPTER 53-00-07-2R-5 DETAIL I PER SRM 53-30-07-2R. JOB C
- [SDR IPXA2023110680698](https://openairdocs.org/sdr/IPXA2023110680698), Oct 26, 2023: FRAME. DENTED. DENT AT FRAME STA 1580 RH BETWEEN STR 25R TO STR 26R. PERFORMED REPAIR PER 757-200PF S.R.M. REV 118 CHAPTER 53-00-07-2R-5 DETAIL III PER S.R.M. 53-60-07-2R. VER
- [SDR IPXA2023110580600](https://openairdocs.org/sdr/IPXA2023110580600), Oct 26, 2023: FRAME. DENTED. DENT AT FRAME STA 1500 R/H, STR 26R. PERFORMED REPAIR PER 757-200PF S.R.M. REV 118 CHAPTER 53-00-07-2R-5 DETAIL I PER S.R.M 53-60-07-2R. JOB COMPLETED
- [SDR IPXA2023111658006](https://openairdocs.org/sdr/IPXA2023111658006), Oct 25, 2023: TRANSITION PANEL. CORRODED. FAULT: AFT CARGO COMPT, R/H TRANSITION PANEL, FOUND EXFOLIATED CORROSION, BETWEEN STA 1310 TO STA 1380. INSTALLED TRANSITION PANEL IAW 51-40-02. RIVET SOLID P/N
- [SDR IPXA2023111049673](https://openairdocs.org/sdr/IPXA2023111049673), Oct 25, 2023: FRAME. DENTED. AFT CARGO FRAME STA 1500 LH BETWEEN STA 25 AND STA 24 HAS DENT NO DOT INSPECTED AND VERIFIED REPAIR ACCOMPLISHED IAW B757-200PF REV 118.00 SRM 53-00-07-2R-5 DET
- [SDR IPXA2023110757733](https://openairdocs.org/sdr/IPXA2023110757733), Oct 25, 2023: FRAME. DENTED. FAULT: AFT CARGO COMPT, FRAME STA 1620 R/H, HAS A DENT BETWEEN S-25R TO S-26R. ACCOMPLISHED REPAIR PER SRM 53-00-07-2R-5 DETAIL III. VERIFIED ACCOPMLLISHED PER 
- [SDR IPXA2023110649579](https://openairdocs.org/sdr/IPXA2023110649579), Oct 25, 2023: FRAME. DENTED. FAULT: AFT CARGO FRAME STA 1240 LH BETWEEN STR 23 AND 24 HAS DENT NO DOT. ACCOMPLISHED REPAIR PER 757-200PF SRM REV 118 CHAPTER 53-00-07-2R-6, DETAIL IV PER SRM
- [SDR IPXA2023110557897](https://openairdocs.org/sdr/IPXA2023110557897), Oct 25, 2023: FRAME. DENTED. FAUL: AFT CARGO COMPT, FRAME STA 1540 R/H, HAS A DENT, BETWEEN S-25R TO S-S6R ACCOMPLISHED REPAIR PER 757-200PF S.R.M. REV 118 CHAPTER 53-00-07-2R-5 DETAIL I PE
- [SDR IPXA2023042993040](https://openairdocs.org/sdr/IPXA2023042993040), Apr 29, 2023: SKIN. DAMAGED. INSPECTION TYPE:SPV*MAJOR REPAIR* LH FUSE STA 518 BELOW SCUFF PLATE HAS A DENTREPAIRED PER EO B757-5330-86739-A
- [SDR IPXA2023042993039](https://openairdocs.org/sdr/IPXA2023042993039), Apr 29, 2023: SKIN. DAMAGED. INSPECTION TYPE:SPV*MAJOR REPAIR* LH FUSE STA 550 BELOW SCUFF PLATE HAS DENT AND CRACKREPAIRED PER EO B757-5330-86711-A
- [SDR IPXA2023022191211](https://openairdocs.org/sdr/IPXA2023022191211), Feb 20, 2023: INDICATOR. NONE. INSPECTION TYPE:N/A**DIVERSION**THE ACCURACY OF ONE OR MORE FUEL TANK QUANTITY INDICATORS IS NOT KNOWN. BOTH MAIN TANK QUANTITYS BLANKED IN FLIGHT.UPON ARRIVAL 
- [SDR IPXA2021120276554](https://openairdocs.org/sdr/IPXA2021120276554), Dec 1, 2021: NONE. NONE. INSPECTION TYPE:N/A**ATB**NO EMERG ACTION** A/C LANDED W/OUT INCIDENT**AFTER TAKE-OFF THE FLIGHT CREW EXPERIENCED A LOSS OF THE RIGHT ENGINE BLEED SYSTEM. THE F
- [SDR IPXA2021111175874](https://openairdocs.org/sdr/IPXA2021111175874), Nov 11, 2021: NONE. NONE. INSPECTION TYPE:N/A**SUPPLEMENTAL SDR* DECLD EMERG/UNDECLD EMERG*A/C LANDED W/O INCIDENT* WHILE @ FLT LVL 280 SINGLE PACK OPERATION GOT CABIN ALT EICAS & WARNIN
- [SDR IPXA2021110175502](https://openairdocs.org/sdr/IPXA2021110175502), Nov 1, 2021: RIB. CRACKED. INSPECTION TYPE:SEG3RH VERT STAB RIB #1 CHORD FWD END HAS A CRACK.REPAIRED PER UPS EO B757-5530-82018-A AND VT MAE EA 757-5530-27-A2732 REV -
- [SDR IPXA2021110175500](https://openairdocs.org/sdr/IPXA2021110175500), Nov 1, 2021: BEAM. NONE. INSPECTION TYPE:SEG31 EA FASTENER HOLE AT STA 1681 LBL 39.5, COMMON TO DECK PLATE AND FLOOR BEAM HAS CORROSION.REPAIRED PER UPS EO B757-5310-82015-A AND VT MAE 
- [SDR IPXA2021102875414](https://openairdocs.org/sdr/IPXA2021102875414), Oct 28, 2021: SEAT TRACK. CORRODED. INSPECTION TYPE:SEG3MAIN CABIN SEAT TRACK AT BL 0 FROM STA 345-365 HAS CORROSION.REMOVED AND REPLACED SEAT TRACK FROM STA 324-430 AT BL 0 IAW SRM 51-40-02-0G AN
- [SDR IPXA2021102575299](https://openairdocs.org/sdr/IPXA2021102575299), Oct 25, 2021: FLOOR PANEL. DAMAGED. INSPECTION TYPE:SEG3MAIN CARGO COMPARTMENT, FLOOR PANEL 231XHF IS DAMAGED.FABBED PANEL 231XHF FROM 5024N400001SS-G, BATCH# 3855547 PER SREO B757-5320-9692-K
- [SDR IPXA2021102275212](https://openairdocs.org/sdr/IPXA2021102275212), Oct 22, 2021: NONE. NONE. INSPECTION TYPE:SEG3LEFT WING DRY BAY PANEL 432FZ HAS EDGE DAMAGE.REPAIRED PANEL IAW B757 SRM 51-70-07-0G PER SRM 57-20-09-2R, FIG. 201, TABLE 1.
- [SDR IPXA2021103175481](https://openairdocs.org/sdr/IPXA2021103175481), Oct 15, 2021: DRAG FITTING. NONE. INSPECTION TYPE:CTHE #1 PYLON FITTING AND WING SKIN HAVE CORROSION AND CRACK INDICATION FOR HOLES #1 -18. REQUEST FOR FINAL APPROVAL.WORKED PER EA# 757-5720-27-
- [SDR IPXA2021092274158](https://openairdocs.org/sdr/IPXA2021092274158), Sep 22, 2021: LIGHT. INOPERATIVE. INSPECTION TYPE:N/A**SUPPLEMENTAL SDR** EMERGENCY LIGHTS PANEL ON OVERHEAD BACKGROUND PANEL LIGHTS INOP. OVHD P-5 EMERGENCY LIGHT PANEL BACKGROUND LIGHT DEFERRE
- [SDR IPXA2021051669425](https://openairdocs.org/sdr/IPXA2021051669425), May 15, 2021: SPLICE ANGLE. BROKEN. INSPECTION TYPE:CSPLICE ANGLE BROKE AT STA 600 - 17.25 AFTER BELLCRANK ASSY IMPACTREMOVED AND REPLACED SPLICE ANGLE IAW SRM 51-40-02
- [SDR IPXA2021051669424](https://openairdocs.org/sdr/IPXA2021051669424), May 15, 2021: BELLCRANK. BROKEN. INSPECTION TYPE:CMCD DOOR AFT CAM BELLCRANK BROKE AFTER BELLCRANK IMPACTREMOVED AND REPLACED BELLCRANK USING PN #69-21498-1 IAW SRM 51-40-02
- [SDR IPXA2021051669426](https://openairdocs.org/sdr/IPXA2021051669426), May 15, 2021: FRAME. BROKEN. INSPECTION TYPE:CLOWER FRAME AT STA 600 - 17.25 DAMAGED FROM BELLCRANK ASSY IMPACTREMOVED AND REPLACED LOWER FRAME IAW SRM 51-40-02
- [SDR IPXA2021051669427](https://openairdocs.org/sdr/IPXA2021051669427), May 15, 2021: FILLER. BROKEN. INSPECTION TYPE:CREDIOUS FILLER BROKE AT STA 600 - 17.25 AFTER BELLCRANK ASSY IMPACTREMOVED AND REPLACED RADIOUS FILLER IAW SRM 51-40-02
- [SDR IPXA2021021265596](https://openairdocs.org/sdr/IPXA2021021265596), Feb 11, 2021: SEAL. DIRTY. INSPECTION TYPE:N/AEXTREMELY LOUD SQUEAL EMANATING FROM FORWARD ENTRY DOOR. IT BEGAN IN THE CLIMB PASSING 19,000 FEET (7 PSID) AND STOPPED AT 29,000 FEET (8 PSI
- [SDR IPXA2020080358583](https://openairdocs.org/sdr/IPXA2020080358583), Jul 31, 2020: TRANSDUCER. MALFUNCTIONED. INSPECTION TYPE:N/ANO LEFT N1, LEFT OIL PRESSURE 0, L FUEL VALVE MESSAGE, RESULTED IN BTBPREFORMED OVER TEMP HOT SECTION INSPECTION WRT 757 AMM 72-00-00-206-530
- [SDR IPXA2019103148512](https://openairdocs.org/sdr/IPXA2019103148512), Oct 31, 2019: SKIN. DENTED. INSPECTION TYPE:SEG2BARE METAL DENT IN TAIL CONE SKIN UPPER 18 INCHES BEHIND RUDDER APPROX FS 1900 DOT 30/020 DAMAGE BETWEEN STA 1918.9 AND STA 1941.0REPAIRED A
- [SDR IPXA2019062143574](https://openairdocs.org/sdr/IPXA2019062143574), Jun 20, 2019: INDICATOR. INOPERATIVE. CREW ENTRY DOOR INDICATOR INOPERATIVE. R&R CREW ENTRY DOOR SENSOR PER MM 52-71-0-400-802. OPS NORMAL.
- [SDR IPXA201906143224](https://openairdocs.org/sdr/IPXA201906143224), Jun 12, 2019: PROXIMITY SENSOR. OUT OF ADJUST. L FWD ENT DOOR EICAS MESSAGE DISPLAYED INTERMITTENT AND ENTRY DOORS OPEN LIGHT INTERMITTENT WITH DOOR CLOSE.ADJUSTED PROX SENSOR PER AMM 52-71-00-000-802. OPS C
- [SDR IPXA2019041240969](https://openairdocs.org/sdr/IPXA2019041240969), Apr 11, 2019: SENSOR. OUT OF ADJUST. DURING TAXI IN FWD ENT DOOR EICAS - DOOR WAS CLOSED AND LATCHED EICAS EXTINGUISHED AFTER SEVERAL SECONDS ACARS DATA AFFECTED. ISSUED DEFERRAL M667124 CREW ENTRY

All 188: https://openairdocs.org/aircraft/N435UP/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.