# N429UP: 1992 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: 25460
- Year built: 1992
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 8, 1992
- Certificate issued: October 20, 1992
- Expires: August 31, 2028
- Mode S code: A51EDE
- 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=429UP
- Page: https://openairdocs.org/aircraft/N429UP

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 N429UP.

## FAA accident and incident reports

None matched to N429UP.

## Service difficulty reports (247, 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 IPXA2026082841022](https://openairdocs.org/sdr/IPXA2026082841022), Jul 13, 2026: HOOK. CORRODED. MCD FWD DOOR HOOK HAS PITTING.INSTALLED MCD FWD DOOR HOOK, ADJUSTMENT AND OPS CHECK. IAW CMM 52-32-03, AMM 52-32-00-825-001 AND AMM 52-32-00-715-011. ADJUSTMENT
- [SDR IPXA2026071610141](https://openairdocs.org/sdr/IPXA2026071610141), Jul 11, 2026: LANDING. CORRODED. DURING DET INSP OF DRAIN HOLES, FOUND CORROSION ON PANEL LANDING IN THE AREA AROUND BS 1040 LT SIDE AFTER CLEANING WAS ACCOMPLISHED. INSTALLED PANEL LANDING SUP
- [SDR IPXA2026082316909](https://openairdocs.org/sdr/IPXA2026082316909), Jul 5, 2026: BRACKET. CRACKED. MAIN E&E BAY CENTER WALKWAY CONNECTING BRACKET CRACKED. INSTALLED NUTPLATE ON REPLACEMENT BRACKET AND INSTALLED BRACKET AT THE MAIN E&E BAY CENTER WALKWAY IAW S
- [SDR IPXA2026071468356](https://openairdocs.org/sdr/IPXA2026071468356), Jun 26, 2026: SUPPORT ANGLE. BROKEN. UPON INSPECTION OF REMOVED N/P STRAP ASSY. AFT OF BULK CARGO BAY AT BS 1715, RBL 36. FOUND MATTING SUPPORT ANGLE BROKEN AND EXFOLIATED, INSTALLED ONE SUPPORT AN
- [SDR IPXA2026071469373](https://openairdocs.org/sdr/IPXA2026071469373), Jun 26, 2026: SUPPORT ANGLE. BROKEN. UPON INSPECTION OF REMOVED N/P STRAP ASSY.,AFT OF BULKCARGO COMPARTMENT AT BS 1715. RBL 24, FOUND MATTING SUPPORT ANGLE BROKEN AND EXFOLIATED. INSTALLED ONE SUP
- [SDR IPXA2026062629173](https://openairdocs.org/sdr/IPXA2026062629173), Jun 24, 2026: SUPPORT FITTING. CORRODED. (APG) RT AFT TRUNNION SUPPORT FITTING BEARING ASSY INSIDE HOUSING HAS CORROSION. INSTALLED SERVICEABLE BEARING ASSY R/H AFT TRUNNION SUPPORT FITTING IAW AMM 57-
- [SDR IPXA2026062629263](https://openairdocs.org/sdr/IPXA2026062629263), Jun 24, 2026: BEARING. CORRODED. LEFT AFT TRUNNION SUPPORT FITTING BEARING ASSY INSIDE HOUSING HAS CORROSION INSTALLED SERVICIABLE BEARING ASSY AT LT AFT TRUNNION SUPPORT FITTING IAW AMM 57-54-
- [SDR IPXA2026062703497](https://openairdocs.org/sdr/IPXA2026062703497), Jun 23, 2026: STRAP. CORRODED. WHILE EVALUATING CORROSION AT APU INLET SURROUND STRUCTURE FOUND CORROSION AT APU INLET AFT STRAP AT STA 1825 BETWEEN STR 3R-6R. ATA 49-11 OKAY TO FABRICATE PER
- [SDR IPXA2026082091705](https://openairdocs.org/sdr/IPXA2026082091705), Jun 22, 2026: NUT PLATE. CORRODED. AFT OF BULK CARGO COMPARTMENT, DECK PLATE FLOOR STRUCTURE SUPPORT ANGLE ASSY HAS CORROSION ON NUT PLATE STRAP APPROX AT BS 1715, RBL 24. INSTALLED ONE NUT PLATE
- [SDR IPXA2026062791765](https://openairdocs.org/sdr/IPXA2026062791765), Jun 22, 2026: NUT PLATE. CORRODED. AFT OF BULK CARGO COMPARTMENT, DECK PLATE FLOOR STRUCTURE SUPPORT ANGLE ASSY HAS CORROSION ON NUT PLATE STRAP APPROX AT BS 1715, LBL 24. INSTALLED NUT PLATE STR
- [SDR IPXA2026062791791](https://openairdocs.org/sdr/IPXA2026062791791), Jun 22, 2026: NUT PLATE. CORRODED. AFT OF BULK CARGO COMPARTMENT, DECK PLATE FLOOR STRUCTURE SUPPORT ANGLE ASSY HAS CORROSION ON NUT PLATE STRAP APPROX AT BS 1715, LBL 36. INSTALLED NUT PLATE STR
- [SDR IPXA2026062791739](https://openairdocs.org/sdr/IPXA2026062791739), Jun 22, 2026: NUT PLATE. CORRODED. AFT OF BULK CARGO COMPARTMENT, DECK PLATE FLOOR SUPPORT ANGLE ASSY HAS CORROSION ON NUT PLATE STRAP APPROX AT BS 1715, LBL 12. INSTALLED NUT PLATE STRAP ASSY ON
- [SDR IPXA2026062578498](https://openairdocs.org/sdr/IPXA2026062578498), Jun 21, 2026: BRACKET. CORRODED. RIGHT WING TO BODY OVER WING BRACKET HAS SIGNS OF CORROSION. REMOVED BRACHET (1EA) AND ATTACHED NUTPLATES FOR ACCESS AT RT WING TO BODY OVER WING IAW SRM 51-40-
- [SDR IPXA2026062578491](https://openairdocs.org/sdr/IPXA2026062578491), Jun 21, 2026: BRACKET. CORRODED. RIGHT WING TO BODY OVER WING BRACKET HAS SIGNS OF CORROSION. REMOVED BRACKET (1EA) AND ATTACHED NUTPLATES FOR ACCESS AT RT WING TO BODY OVER IAW SRM 51-40-02-0G
- [SDR IPXA2026081558961](https://openairdocs.org/sdr/IPXA2026081558961), Jun 20, 2026: SKIN. CORRODED. UPON REMOVAL OF THE LT HORIZONTAL STAB UPPER SLIDING FAIRING FOUND CORRODED ON THE HORIZONTAL STAB UPPER SKIN ALONG RIB 3 BTWN FRONT & REAR SPAR. REMOVED THE CO
- [SDR IPXA2026062358961](https://openairdocs.org/sdr/IPXA2026062358961), Jun 20, 2026: FAIRING. CORRODED. UPON REMOVAL OF THE LT HORIZONAL STAB UPPER SLIDING FAIRING FOUND CORROSION ON THE HORIZONTAL STAB UPPER SKIN ALONG RIB 3 BETWEEN THE FRONT AND REAR SPAR (CT-A)
- [SDR IPXA2026082353773](https://openairdocs.org/sdr/IPXA2026082353773), Jun 19, 2026: ANGLE. CRACKED. LOWER MID FUSELAGE, RT SIDE ANGLE, JUST OTBD OF KEEL BEAM & BS 1180, RBL 11, HAS A CRACK. INSTALLED REPLACEMENT ANGLE IAW SRM 51-40-02-0G-0.
- [SDR IPXA2026081327919](https://openairdocs.org/sdr/IPXA2026081327919), Jun 18, 2026: INLET. CORRODED. *** SUPPLEMENTAL SDR *** HORZ STAB COMPT. APU INLET SURROUND STRUCTURE ANGLE IS CORRODED BETWN STA. 1787.45 TO 1825 STGR S-6R (059-07) ATA: 53-80 SKILL: STR APU
- [SDR IPXA2026061827919](https://openairdocs.org/sdr/IPXA2026061827919), Jun 18, 2026: ANGLE. CORRODED. HORZIZONAL STAB COMPT. APU INLET SURROUND STRUCTURE ANGLE IS CORRODED BETWN STA. 1787.45 TO 1825 STGR S-6R (059-07) ATA: 53-80 SKILL: STR
- [SDR IPXA2026062300366](https://openairdocs.org/sdr/IPXA2026062300366), Jun 16, 2026: DOOR FRAME. CORRODED. APU INLET DOOR FRAME HAS CORROSION. INSTALLED SUPPORT ANGLES AND ONE STRAP AT BELOW APU INLET DOOR FRAME APPROX BS 1787-1825, STRINGERS 3 - 6R IAW SRM 51-40-02-
- [SDR IPXA2026063088739](https://openairdocs.org/sdr/IPXA2026063088739), Jun 16, 2026: BONDING STRAP. CORRODED. RIGHT HORIZONAL STAB OTBD END TO ELEVATOR BONDING STRAP AND BOTH FWD AND AFT ATTACH BRACKETS HAVE CORROSION. RL025 VERIFIED ITEMS IN STEP 7 ARE INSTALLED PER DO
- [SDR IPXA2026062787236](https://openairdocs.org/sdr/IPXA2026062787236), Jun 16, 2026: BONDING JUMPER. CORRODED. L/H HORZ STAB OTBD END TO ELEVATOR BONDING STRAP AND BOTH FWD AND AFT ATTACH BRACKETS HAVE CORROSION. INSTALLED ONE ANGLE BRACKET STRAP JUMPER & REINSTALLED ONE
- [SDR IPXA2024062705848](https://openairdocs.org/sdr/IPXA2024062705848), Jun 18, 2024: TEE ANGLE. CORRODED. L/H LOWER FUSELAGE BETWEEN STA. 1200-1260 T-CORD HAS CORROSION INSTALLED T-CHORD L/H FUSELAGE BETEWEEN STA 1200- 1260 IAW SRM 51-40-02.
- [SDR IPXA2024062611207](https://openairdocs.org/sdr/IPXA2024062611207), Jun 18, 2024: TEE ANGLE. CORRODED. L/H LOWER FUSELAGE AT STA. 1240 VERTICAL T-CORD HAS CORROSION ISNTALLED T-CHORD L/H FUSELAGE AT STA 1240 VERTICAL. SRM 51-40-02.
- [SDR IPXA2024062405953](https://openairdocs.org/sdr/IPXA2024062405953), Jun 18, 2024: WEB. CORRODED. L/H LOWER FUSELAGE BETWEEN STA. 1200-1260 WEB HAS CORROSION INSTALLED NEW CHANNEL, FILLER AND ANGLE, IAW SRM 51-40-02-0G.
- [SDR IPXA2022060382788](https://openairdocs.org/sdr/IPXA2022060382788), Jun 3, 2022: SKIN SPLICE. CORRODED. INSPECTION TYPE:SEG4RH WTB, EXHAUST STRUCTURE AREA T-CHORD HAS SURFACE CORROSION AND NUTPLATE HOLES CORRODEDREMOVED AND REPLACED I.A.W. SRM 51-40-05, SRM 51-40-
- [SDR IPXA2022060482806](https://openairdocs.org/sdr/IPXA2022060482806), May 31, 2022: SUPPORT ANGLE. CORRODED. INSPECTION TYPE:SEG4RH WTB T-CHORD AT STA 1040-1060 JUST O/B OF ECS EXHAUST VENT PANEL IS CORRODED OUT OF LIMITS AND REQUIRES REPLACEMENTREMOVED AND REPLACED SU
- [SDR IPXA2022060482805](https://openairdocs.org/sdr/IPXA2022060482805), May 19, 2022: SUPPORT ANGLE. CORRODED. INSPECTION TYPE:SEG4AT THE AFT RIGHT RAT COMPARTMENT, STA 1185 OUTBD. SUPPORT CHORD HAS EXFOLIATION CORROSION AT INBD. CORNERREMOVED AND REPLACED SUPPORT CHORD 
- [SDR IPXA2022060482804](https://openairdocs.org/sdr/IPXA2022060482804), May 19, 2022: FRAME ANGLE. CORRODED. INSPECTION TYPE:SEG4AT STA 1240 IN RAT COMPARTMENT INTERIOR FRAME IS CORRODEDWORK PER UPS E.O. B757-5320-83795-A AND VT-MAE 757-5360-27-A2933REV-
- [SDR IPXA2022060382775](https://openairdocs.org/sdr/IPXA2022060382775), May 18, 2022: FRAME. CRACKED. INSPECTION TYPE:SEG4AT STA 1240 IN RAT COMPARTMENT INTERIOR FRAME IS CORRODEDWORK PER UPSS E.O. B757-5310-24700-C, UPS RCD 262046, AND VT MAE E.A. 757-5360-A293
- [SDR IPXA2022060182728](https://openairdocs.org/sdr/IPXA2022060182728), May 18, 2022: NONE. NONE. INSPECTION TYPE:SEG4, DURING ACCOMPLISHMENT OF E.O.# B757-5310-73926-A. FOUND EXISTING REPAIR AT STA 1480, S-25R TO S-27R REQUIRE ENGINEERING ASSISTANCE FOR ALT
- [SDR IPXA2022060282751](https://openairdocs.org/sdr/IPXA2022060282751), May 18, 2022: FRAME. DAMAGED. INSPECTION TYPE:16/4DURING ACCOMPLISHMENT OF E.O#B757-531073926-A. FOUND EXISTING REPAIR AT STA 1280, S2323R TO S27R REQUIRE ENGINEERING ASSISTANCE FOR ALTERNAT
- [SDR IPXA2020080548640](https://openairdocs.org/sdr/IPXA2020080548640), Aug 4, 2020: SKIN. DELAMINATED. INSPECTION TYPE:SEG3, THERE IS A SMALL DENT ON THE EXTERIOR RIGHT SIDE OF THE RAIL CONE APPROX 24" AFT 315 BL. REPAIRED IAW SRM 51-70-10-2R-2, AND SRM 53-80-01-
- [SDR IPXA2020080318512](https://openairdocs.org/sdr/IPXA2020080318512), Aug 1, 2020: SHEAR WEB. CORRODED. INSPECTION TYPE:SEG3, SHEAR WEB IN COCKPIT CORRODED. REAPAIRED WITH FILLER AND DOUBLER.
- [SDR IPXA2020080318511](https://openairdocs.org/sdr/IPXA2020080318511), Aug 1, 2020: SHEAR WEB. CORRODED. INSPECTION TYPE:SEG3, COCKPIT SHEAR WEB CORRODED. REPAIRED WITH PILLER AND DOUBLER.
- [SDR IPXA2020072755206](https://openairdocs.org/sdr/IPXA2020072755206), Jul 25, 2020: PANEL. GOUGED. INSPECTION TYPE:SEG, LEFT WING DRY BAY PANEL 532BZ HAD EDGE DAMAGE. REPAIRED THE DRY BAY PANEL IAW SRM 51-70-07-OG, AND SRM 57-20-09-2R-1, FIG 201 TABLE I.
- [SDR IPXA2020072748190](https://openairdocs.org/sdr/IPXA2020072748190), Jul 24, 2020: FLOOR PANEL. DAMAGED. INSPECTION TYPE:SEG, MAIN CARGO COMPARTMENT FLOOR PANEL 232XWF DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.
- [SDR IPXA2020072748189](https://openairdocs.org/sdr/IPXA2020072748189), Jul 24, 2020: FLOOR PANEL. DAMAGED. INSPECTION TYPE:SEG, MAIN CARGO COMPARTMENT FLOOR PANEL 251XBF DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692.
- [SDR IPXA2020072748188](https://openairdocs.org/sdr/IPXA2020072748188), Jul 24, 2020: FLOOR PANEL. DAMAGED. INSPECTION TYPE:SEG, MAIN CARGO COMPARTMENT FLOOR PANEL 232XVF WAS DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-53209692-K.
- [SDR IPXA2020072748187](https://openairdocs.org/sdr/IPXA2020072748187), Jul 24, 2020: FLOOR PANEL. DAMAGED. INSPECTION TYPE:SEG, MAIN CARGO COMPARTMENT, FLOOR PANEL 232XPF DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.
- [SDR IPXA2018072031897](https://openairdocs.org/sdr/IPXA2018072031897), Jul 16, 2018: FLOOR PANEL. DELAMINATED. INSPECTION TYPE:SEG2, MAIN DECK FLOOR PANEL 231XJF IS DELAMINATED. FABRICATED PNL 231XJF AND STEPCUT LOWER SURFACE PER SREO B757-5320-9692-K. APPLIED FIBERGLASS
- [SDR IPXA2018072031895](https://openairdocs.org/sdr/IPXA2018072031895), Jul 16, 2018: FLOOR PANEL. DELAMINATED. INSPECTION TYPE:SEG2, MAIN DECK FLOOR PANEL 231XFF IS DELAMINATED. FABRICATED PNL 231XFF AND STEP CUT LWR SURFACE PER B757-5320-9692-K APPLIED FIBERGLASS DOUBLE
- [SDR IPXA2017030114597](https://openairdocs.org/sdr/IPXA2017030114597), Mar 1, 2017: LAMP. INOPERATIVE. SEVERAL LAMPS INOPERATIVE IN FWD ENTRY DOOR EMERGENCY EXIT SIGN. REPLACED THE LAMPS IAW AMM 33 51 01. OPS CHECKED NORMAL.
- [SDR IPXA2016063005246](https://openairdocs.org/sdr/IPXA2016063005246), Jun 18, 2016: WEB. PUNCTURED. INSPECTION TYPE:C-13, FLIGHT DECK LT UNDER CAP SEAT FLOOR AREA HAS IMPACT DAMAGE. FABRICATED NEW WEB IAW DWG 141N5810, REMOVED AND REPLACED WEB IAW SRM 51-40-02
- [SDR IPXA2016063005237](https://openairdocs.org/sdr/IPXA2016063005237), Jun 16, 2016: SKIN. DENTED. INSPECTION TYPE: C13, LOWER SKIN EXTERNAL FUSLAGE BS 610 S25L DENTED. REPAIRED IAW SRM 53-00-01 REPAIR 3.
- [SDR IPXA2016062204917](https://openairdocs.org/sdr/IPXA2016062204917), Jun 16, 2016: FITTING. CRACKED. INSPECTION TYPE:C13, FWD ACCESSORY COMPARTMENT CLIP CRACKED AT BL0 ABOVE NLG WHEEL WELL. R & R IAW SRM 51-40-02.
- [SDR IPXA2016070605462](https://openairdocs.org/sdr/IPXA2016070605462), Jun 15, 2016: WIRE. SHORTED. INSPECTION TYPE: C-13, GEAR DOORS WON'T OPEN WITH GROUND SWITCH, GEAR DOOR CONTROL SWITCHES & LIGHT (P72 PM), GR DR OPEN DR SWITCHES. TROUBLESHOOT AND FOUND BAD
- [SDR IPXA2016063005263](https://openairdocs.org/sdr/IPXA2016063005263), Jun 15, 2016: PANEL. DELAMINATED. INSPECTION TYPE: C-13, FOUND MULTIPLE AREAS OF DELAMINATION ON THE VERTICAL STAB LT LOWER FORWARD TORQUE BOX PANEL. REMOVED AND REPLACED THE PANEL IAW SRM 51.40
- [SDR IPXA2015101294702](https://openairdocs.org/sdr/IPXA2015101294702), Oct 10, 2015: SENSOR. INOPERATIVE. EICAS MSG "LT FWD ENT DOOR" DISPLAYED INTERMITTENT AND ENTRY DOORS OPEN LIGHT ON INTERMITTENT WITH DOOR CLOSED. BLOCK TURN BACK. ADJUSTED DOOR SENSOR IAW AMM 52
- [SDR IPXA2015081892492](https://openairdocs.org/sdr/IPXA2015081892492), Aug 17, 2015: MODULE. MALFUNCTIONED. INSPECTION TYPE:IN, CREW REPORTED AFT CABIN TEMP CONTROL U/S. R & R V3 AFT CABIN TRIM AIR MODULATING VALVE IAW AMM 21-61-07-4, REV 113.01 08/03/15. EFF REF IPC 

All 247: https://openairdocs.org/aircraft/N429UP/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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