# N402UP: 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: 23724
- Year built: 1987
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 17, 1987
- Certificate issued: December 12, 1998
- Expires: February 28, 2029
- Mode S code: A4B5DF
- 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=402UP
- Page: https://openairdocs.org/aircraft/N402UP

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 (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB LAX07LA189](https://openairdocs.org/ntsb/LAX07LA189), Apr 24, 2007: Boeing 757-24APF (N402UP), Burbank, CA, no damage. Probable cause: The tow tractor driver's and mechanic's diverted attention resulting in the airplane rolling over the mechanic's foot. Also causal was the mechanic's failure to maintain clearance from the nose…

## 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.

- [Accident 20070424011229A](https://openairdocs.org/incident/20070424011229A), Apr 24, 2007: Boeing 75724APF (N402UP), Burbank, CA, No damage. (-23) During pushback, the towing supervisor stopped the towing operation due to a light aircraft taxiing behind the united postal service (ups) aircraft. As…

## Service difficulty reports (298, 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 IPXA2026101280317](https://openairdocs.org/sdr/IPXA2026101280317), Oct 3, 2026: SKIN. CORRODED. AFTER REMOVAL OF ADF ANTENNA FOUND UPPER FUSELAGE SKIN WITH DEEP PITTING CORROSION AND TOOLING MARKS.
- [SDR IPXA2026101718066](https://openairdocs.org/sdr/IPXA2026101718066), Sep 24, 2026: SUPPORT BRACKET. CORRODED. REMOVED SUPPORT BRACKET BETWEEN APU DOOR ACTUATOR AND DOOR HOUSING ASSY DIRTY WITH DETERIORATED CIC AND AREAS OF LITE CORROSION AROUND FASTENER HOLES. RL049 QCI
- [SDR IPXA2026101276017](https://openairdocs.org/sdr/IPXA2026101276017), Sep 22, 2026: FLOOR SKIN. CORRODED. DURING BUYBACK IN LH NOSE TUNNEL FOUND MAIN CABIN SUBFLOOR WITH EXFOLIATION ON LOWER SKIN STA 333.5 LBL 49 STR ATA 51-00.
- [SDR IPXA2026101355189](https://openairdocs.org/sdr/IPXA2026101355189), Sep 21, 2026: RETAINER. DAMAGED. BS 1963, LOWER RT SIDE SEAL RETAINER WAS DAMAGED. INSTALLED SEAL RETAINER AT STA 1963 LOWER R/H SIDE I.A.W B757-200 S.R.M 51-40-02-0G-0.
- [SDR IPXA2026101613332](https://openairdocs.org/sdr/IPXA2026101613332), Sep 18, 2026: PANEL. DELAMINATED. MAJOR REPAIR, LOWER AFT APU PANEL BETWEEN BS 1963 TO 1992 IS DELAMINATED VERIFIED STEP 14 IS ACCOMPLISHED AND HEAT CON. TAP TEST. NO DISBONDS OR DELAMINATIONS N
- [SDR IPXA2026101740890](https://openairdocs.org/sdr/IPXA2026101740890), Sep 14, 2026: CLOSEOUT PANEL. CORRODED. COCKPIT CLOSEOUT PANEL OVER SUPERNUMERARY AREA HAS CORROSION, FLL-096, C/W SRM 51-40-05-0G-0.
- [SDR IPXA2026101240869](https://openairdocs.org/sdr/IPXA2026101240869), Sep 14, 2026: CLOSEOUT PANEL. CORRODED. OFF A/C PARTS, COCKPIT CLOSEOUT OVER SUPERNUMERARY AREA HAS CORROSION. FABRICATED SPLICE I.A.W. DWG 141W6007/SAMPLE WORK ACCOMPLISHED ON TRAVELER 7003475011.
- [SDR IPXA2026102117121](https://openairdocs.org/sdr/IPXA2026102117121), Sep 12, 2026: STRAP. CORRODED. MAIN DECK CABIN FLOOR STRUCTURE BTW STA 1540 TO 1580 AND LBL 45.50 STABILIZATION STRAP HAS CORROSION, INSTALLED STABILIZATION STRAP AND 1EA STABILIZATION STRAP 
- [SDR IPXA2026102217366](https://openairdocs.org/sdr/IPXA2026102217366), Sep 12, 2026: SKIN. BULGED. AGING A/C INSPECTION A BULGE WAS NOTED BELOW THE LH FIXED COCKPIT WINDOW OF BS 255.
- [SDR IPXA2026102116974](https://openairdocs.org/sdr/IPXA2026102116974), Sep 12, 2026: STRAP. CORRODED. MAIN DECK CABIN FLOOR STRUCTURE BTW STA 1560 TO 1580 AND LBL 24.75 STABILIZATION STRAP HAS CORROSION, INSTALLED NEW STABILIZATION STRAP AND 2 EACH SPLICE PLATES
- [SDR IPXA2026101316528](https://openairdocs.org/sdr/IPXA2026101316528), Sep 12, 2026: FLOOR SUPPORT. DENTED. FWD CARGO COMP FLOOR SUPPORT LBL 2.90 AT STA. 662 HAS A DENT AT UPPER SURFACE. 83-043. ATA 53-30. INSTALLED NEW FLOOR SUPPORT ON FWD CARGO AT STA. 662 LBL 7.25 
- [SDR IPXA2026092217121](https://openairdocs.org/sdr/IPXA2026092217121), Sep 12, 2026: FLOOR SUPPORT. CORRODED. MAIN DECK CABIN FLOOR STRUCTURE BTW STA 1540 TO 1580 AND LBL 45.50 STABILIZATION STRAP HAS CORROSION, FLL-042, ATA 53. REQ. NDT (HFEC) CHECK FOR CRACK ON CUT OU
- [SDR IPXA2026091717519](https://openairdocs.org/sdr/IPXA2026091717519), Sep 12, 2026: FLOOR SUPPORT. CORRODED. MAIN DECK CABIN FLOOR STRUCTURE STA 800 TO 820 AND LBL 45.50 STABILIZATION STRAP HAS CORROSION, FLL-065, VERIFIED STEPS 14 AND 15
- [SDR IPXA2026101698760](https://openairdocs.org/sdr/IPXA2026101698760), Sep 11, 2026: SKIN. DELAMINATED. MAJOR REPAIR, APU COMPARTMENT SKIN PANEL HAS EVIDENCE OF DELAMINATION APPROX BTW BS 1885 AND BS 1896, STGR 17R AREA,
- [SDR IPXA2026101599728](https://openairdocs.org/sdr/IPXA2026101599728), Sep 11, 2026: RETAINER. BROKEN. RIGHT FUSELAGE SECTION 48 INTERIOR STRUCTURE RIB ASSY ANGLE SUPPORT HAS A SEAL RETAINER BROKEN APPROX AT BS 1963.80, BL 0 THRU RBL 10, LOCATED AND DRILLED SEAL 
- [SDR IPXA2026101203705](https://openairdocs.org/sdr/IPXA2026101203705), Sep 11, 2026: FLOOR SUPPORT. CORRODED. AFT CARGO FLOOR STGR SPLICE EXFOLIATED IN 2 PLACES STR 30L, BS 1460 REMOVED THE INCOMING REPAIR INSTALLED BY SB 757-53A0053 R1. IAW E.A 757-5360-01-B0851, REVIS
- [SDR IPXA2026100500255](https://openairdocs.org/sdr/IPXA2026100500255), Sep 11, 2026: DOOR FRAME. CHAFED. APU COMPARTMENT ACCESS DOOR 315 AL FRAME ASSY LOWER FLANGE HAS A CHAFING APPROX AT BS 1885.2, STGR 17L AREA. REMOVAL AND INSTALLATION ACCOMPLISHED. FRAME IAW DW
- [SDR IPXA2026100403755](https://openairdocs.org/sdr/IPXA2026100403755), Sep 11, 2026: SUPPORT WEB. CORRODED. AFT CARGO COMP ABOVE DOOR CUTOUT CEILING SUPPORT WEB CORRODED BS 1440.
- [SDR IPXA2026100603845](https://openairdocs.org/sdr/IPXA2026100603845), Sep 11, 2026: NUT PLATE. CORRODED. BULK CARGO MAIN CABIN FLOOR RH SIDE STA 1680 NUT PLATE RETAINER CORRODED STR ATA 51-00 GM014.
- [SDR IPXA2026093099320](https://openairdocs.org/sdr/IPXA2026093099320), Sep 11, 2026: DOUBLER. CORRODED. LEFT FUSELAGE SECTION 48 INTERIOR STRUCTURE RIB HAS EVIDENCE OF CORROSION ON LOWER AREA APPROX AT BS 1992.8,
- [SDR IPXA2026102188082](https://openairdocs.org/sdr/IPXA2026102188082), Sep 10, 2026: STRAP. CORRODED. AFT CARGO CEILING STABILIZATION STRAP 2ND FROM RH OTBD SIDE STA 1400-1420-1420 HAS CORROSION ON UPPER SURFACE. INSTALLED REPLACEMENT STABILIZATION STRAP BETWEEN
- [SDR IPXA2026101986516](https://openairdocs.org/sdr/IPXA2026101986516), Sep 10, 2026: PAD. CHAFED. NR 2 PYLON AFT FAIRING I/B ACCESS DOOR 445AL AFT LATCH AND PAD HAS DEEP CHAFE WEAR. 83-009. INSTALLED NEW PLATE (STOP PAD) ON #2 PYLON AFT FAIRING I/B ACCESS DO
- [SDR IPXA2026101876234](https://openairdocs.org/sdr/IPXA2026101876234), Sep 10, 2026: STIFFENER. WORN. APU COMPARTMENT BULKHEAD STA 1885 HORZ STIFFENER JUST BELOW LIGHT SWITCH ASSY DOOR SAFETY CATCH EDGE WORN. INSTALLED NEW RETAINER AT APU COMPARTMENT BULKHEAD ST
- [SDR IPXA2026100786152](https://openairdocs.org/sdr/IPXA2026100786152), Sep 10, 2026: SUPPORT ANGLE. CRACKED. NR 2 PYLON AFT FAIRING, ACCESS PANEL 445AR, FWD, LOWER CUTOUT AREA HAS A CRACKED SUPPORT CLIP.
- [SDR IPXA2026100574510](https://openairdocs.org/sdr/IPXA2026100574510), Sep 10, 2026: SKIN. CHAFED. APU DOOR 316AR OUTER SKIN AND INNER STRUCTURE OIL SOAKED, DIRTY AND DEBRIS WITH AREAS OF LOOSE, BLISTARD AND PEELING UP PAINT THAT REQUIRES REMOVAL THIS ALSO IN
- [SDR IPXA2026100675524](https://openairdocs.org/sdr/IPXA2026100675524), Sep 10, 2026: SUPPORT. GOUGED. APU DOOR 316AR FIRE-LOOP, SUPPORT RAIL AFT END GOUGED. REPLACED SUPPORT RAIL AT APU DOOR 316AR FIRE-LOOP, IAW SRM 51-40-02-0G-0.
- [SDR IPXA2026100276207](https://openairdocs.org/sdr/IPXA2026100276207), Sep 10, 2026: BULKHEAD. DENTED. MAJOR REPAIR, APU COMPARTMENT STA 1885 BULKHEAD REPAIR DOUBLE 10" INCHES RIGHT OF LIGHT SWITCH DENTED IN AND EDGES ROLLED UP. RL019 VERIFIED STEPS 22 AND 23 RII
- [SDR IPXA2026092288146](https://openairdocs.org/sdr/IPXA2026092288146), Sep 10, 2026: BRACKET. CRACKED. AFT CARGO APU DUCT BRACKET BROKEN LH OTBD TUNNEL BS 1220. REMOVED AND REPLACED 1EA BROKEN DUCT BRACKET REF. B75-200 SRM 51-40-02-0G-0.
- [SDR IPXA2026092286010](https://openairdocs.org/sdr/IPXA2026092286010), Sep 10, 2026: ANGLE. CRACKED. NR 2 PYLON PANEL LANDING O/B SIDE (ACCESS 445AR) LOWER SUPPORT CLIP IS CRACKED. INSTALLED 1 EA NEW ANGLE CLIP AT NR 2 PYLON PANEL LANDING O/B SIDE FOR ACCESS PA
- [SDR IPXA2026091476662](https://openairdocs.org/sdr/IPXA2026091476662), Sep 10, 2026: SUPPORT BRACKET. CORRODED. WIRE HARNESS CLAMP SUPPORT BRACKETS ATTACHED TO BS 1885 BULKHEAD HAVE LIGHT CORROSION AND MISSING PROTECTIVE FINISH.
- [SDR IPXA2026091488064](https://openairdocs.org/sdr/IPXA2026091488064), Sep 10, 2026: STRAP. CORRODED. AFT CARGO CEILING STABILIZATION STRAP RT OTBD SIDE BS 1420 HAS CORROSION ON UPPER SURFACE, VERIFIED STEP 5, 6, 7, AND 8.
- [SDR IPXA2026091488082](https://openairdocs.org/sdr/IPXA2026091488082), Sep 10, 2026: STRAP. CORRODED. AFT CARGO CEILING STABILIZATION STRAP 2ND FROM RT OTBD SIDE BS 1400-1420-1420 CORROED ON UPPER SURFACE. VERIFIED STEPS 6,7 AND 8
- [SDR IPXA2026091453424](https://openairdocs.org/sdr/IPXA2026091453424), Sep 9, 2026: CHANNEL. CORRODED. RIGHT PNEUMATIC GROUND SERVICE CONNECTION SUPPORT HAS CORROSION ON THE UPPER SURFACE. INSTALLED NEW RT PNEUMATIC GROUND SERVICE CONNECTION SUPPORT IAW SRM 51-40
- [SDR IPXA2026102135715](https://openairdocs.org/sdr/IPXA2026102135715), Sep 8, 2026: GUSSET. CRACKED. RIGHT WW GUSSET IS CRACKED.
- [SDR IPXA2026102136117](https://openairdocs.org/sdr/IPXA2026102136117), Sep 8, 2026: GUSSET. CRACKED. LH WW HAS A CRACKED GUSSET.
- [SDR IPXA2026101935723](https://openairdocs.org/sdr/IPXA2026101935723), Sep 8, 2026: GUSSET. CRACKED. RT WW GUSSET SUPPORT STRUCTURE IS CRACKED. INSTALLED GUSSET SUPPORT (BRACKET) ON RH W/W I.A.W B757-200 S.R.M 51-40-02-0G-0.
- [SDR IPXA2026101835885](https://openairdocs.org/sdr/IPXA2026101835885), Sep 8, 2026: RETAINER. CRACKED. RIGHT WW AFT SEAL RETAINER HAS A GOUGE.
- [SDR IPXA2026092236110](https://openairdocs.org/sdr/IPXA2026092236110), Sep 8, 2026: BRACKET. CRACKED. LEFT WW LT BRACKET CRACKED. INSTALLED NEW BRACKET AT LT WW PER SRM 51-40-02-0G-0
- [SDR IPXA2026101426713](https://openairdocs.org/sdr/IPXA2026101426713), Sep 7, 2026: SLAT TRACK. CRACKED. LT SLAT #4 OUTBD TRACK COVER CRACKED. INSTALLED REPLACEMENT COVER AT L/WING #4 SLAT O/B TRACK PER B757-200PF SRM 51-40-05-0G-0 & 51-40-02-0G-0.
- [SDR IPXA2026061806583](https://openairdocs.org/sdr/IPXA2026061806583), Jun 17, 2026: WINDOW. ARCED. L1 WINDOW ARCING IN LEFT TOP CORNER INSTALLED L1 WINDSHIELD REF MM 56-11€“01-424-015 UP TO AND INCLUDING STEP 3.E.(13). FIRST TORQUE ACCOMPLISHED AT 1400L. COM
- [SDR IPXA2026061706583](https://openairdocs.org/sdr/IPXA2026061706583), Jun 17, 2026: WINDSHIELD. ARCED. L1 WINDOW ARCING IN LEFT TOP CORNER INSTALLED L1 WINDSHIELD REF MM 56-11€“01-424-015 UP TO AND INCLUDING STEP 3.E.(13). FIRST TORQUE ACCOMPLISHED AT 1400L.
- [SDR IPXA2025111323417](https://openairdocs.org/sdr/IPXA2025111323417), Nov 11, 2025: DUCT. LEAKING. DURING LEFT ENGINE START, LEFT BLEED DUCT BLEED LEAK. ABORTED ENGINE START, RAN CHECKLIST SMOKE VISIBLE COCKPIT ON GROUND. RESULTED IN BTB. REPLACED 2 DAMAGED D
- [SDR IPXA2025111223417](https://openairdocs.org/sdr/IPXA2025111223417), Nov 11, 2025: DUCT. LEAKING. DURING LEFT ENGINE START, LEFT BLEED DUCT LEAK. ABORTED ENGINE START, RAN CHECKLIST SMOKE VISIBLE IN THE COCKPT AND ON THE GROUND. RESULTED IN BTB.
- [SDR IPXA2024091499980](https://openairdocs.org/sdr/IPXA2024091499980), Sep 3, 2024: TEE FITTING. CORRODED. T-CHORD AT AIR EXHAUST AREA BETWEEN STA 1037.67 - STA 1060 R/H SIDE WITH EXFOLIATION.REMOVED CORROSION IN T-CHORD AT AIR EXHAUST AREA BETWEEN STA 1037.67 - STA 
- [SDR IPXA2024092390936](https://openairdocs.org/sdr/IPXA2024092390936), Sep 2, 2024: STRAP. CORRODED. INSIDE AFT TAIL COMPARTMENT EXFOILATION CORROSION AT STA 1787.4 R/H INTERNAL UPPER AT APU AIR INLET DUCT. DOT 140-007 INSTALLED 5EA REPAIR PARTS, 1EA AFT STRAP,
- [SDR IPXA2024091850713](https://openairdocs.org/sdr/IPXA2024091850713), Aug 30, 2024: TEE ANGLE. CORRODED. UPPER T-CHORD BETWEEN STA 1180- STA 1200 L/H SIDE WITH EXFOLIATON. INSTALLED T-CHORD BETWEEN IN STA 1180- STA 1200 L/H, INSTALLED 2 EA HINGES IN STA 1140 - 1160
- [SDR IPXA2024091855209](https://openairdocs.org/sdr/IPXA2024091855209), Aug 30, 2024: TEE ANGLE. CORRODED. T-CHORD STA 1240 R/H RBL 59 WITH EXFOLIATION. INSTALLED NEW T-CHORD AT STA 1240 RH, I.A.W. SRM 51-40-02-0G.
- [SDR IPXA2024091249582](https://openairdocs.org/sdr/IPXA2024091249582), Aug 30, 2024: TEE ANGLE. CORRODED. LOWER T-CHORD BETWEEN STA 1180 - STA 1260 RH SIDE WITH EXFOLIATION.VERIFIED FOUND TO BE OUT OF LIMITS. REMOVED T-CHORD IAW SRM 51-40-02. VERIFIED AND DRILLED NE
- [SDR IPXA2024091047960](https://openairdocs.org/sdr/IPXA2024091047960), Aug 30, 2024: TEE ANGLE. CORRODED. T-CHORD STA 1220 R/H SIDE WITH EXFOLIATION. INSTALLED T-CHORD AT STA 1220 RH IAW SRM 51-40-02-0G.
- [SDR IPXA2024091050624](https://openairdocs.org/sdr/IPXA2024091050624), Aug 30, 2024: TEE ANGLE. CORRODED. LOWER T-CHORD BETWEEN STA 1180- STA 1240 L/H SIDE WITH CORROSION. INSTALLED NEW LOWER T-CHORD BETWEEN STA 1180 - STA 1240 LH I.A.W. SRM 51-40-02-0G.

All 298: https://openairdocs.org/aircraft/N402UP/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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