# N422UP: 1991 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: 25324
- Year built: 1991
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 25, 1991
- Certificate issued: November 19, 1991
- Expires: November 30, 2028
- Mode S code: A504DD
- 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=422UP
- Page: https://openairdocs.org/aircraft/N422UP

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 N422UP.

## FAA accident and incident reports

None matched to N422UP.

## Service difficulty reports (271, 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 IPXA2026040685799](https://openairdocs.org/sdr/IPXA2026040685799), Mar 15, 2026: SUPPORT STRAP. CORRODED. CORROISION FOUND ON FWD CARGO CEILING GILL LINER SUPPORT STRAP UNDER NUT PLATE STA 820 LBL 45. FOUND WHILE WORKING EO.89712-REQ007 DECOMPRESSION PANEL.ATA 25. I
- [SDR IPXA2026031475944](https://openairdocs.org/sdr/IPXA2026031475944), Mar 14, 2026: WEB. CORRODED. CORROSION ON FLOOR FORWARD OF PILOTS CONTROL COLUMN.
- [SDR IPXA2026031425145](https://openairdocs.org/sdr/IPXA2026031425145), Feb 26, 2026: FLOORBEAM. CORRODED. MAJOR REPAIR, AGING A/C INSP DOT AA024 STR ATA 53-00 MAIN CABIN FLOORBEAM CORRODED STA 1420 RH OTBD LOWER SIDE ABOVE AFT LOWER CARGO DOOR INSTALLED FABRICATED -
- [SDR IPXA2026032324391](https://openairdocs.org/sdr/IPXA2026032324391), Feb 26, 2026: SPLICE STRAP. CORRODED. WORKING FAULT T3F18E008B4MR FOUND CORROSION ON NUT PLATES AND DOUBLER DRILL HOLE ON FLOOR PANEL SPLICE STRAP STA.1510. SPLICE STRAP P/N 453N1611-23 TO BE INSTAL
- [SDR IPXA2026032324635](https://openairdocs.org/sdr/IPXA2026032324635), Feb 26, 2026: SPLICE STRAP. CORRODED. WORKING FAULT T3F18E008B4LL AFT CARGO FOUND CORROSION ON NUT PLATES AND DOUBLER DRILL HOLE ON FLOOR PANEL SPLICE STRAP BS 1470. FABRICATED 01 EA SPLICE STRAP P/
- [SDR IPXA2026031424391](https://openairdocs.org/sdr/IPXA2026031424391), Feb 26, 2026: SPLICE STRAP. CORRODED. WORKING FAULT T3F18E008B4MR FOUND CORROSION ON NUT PLATES AND DOUBLER DRILL HOLE ON FLOOR PANEL SPLICE STRAP STA.1510 ATA 53-60 PRODUCTION AUDIT C/W
- [SDR IPXA2026031424635](https://openairdocs.org/sdr/IPXA2026031424635), Feb 26, 2026: SPLICE STRAP. CORRODED. WORKING FAULT T3F18E008B4LL AFT CARGO FOUND CORROSION ON NUT PLATES AND DOUBLER DRILL HOLE ON FLOOR PANEL SPLICE STRAP STA.1470 PRODUCTION AUDDIT C/W
- [SDR IPXA2026022825145](https://openairdocs.org/sdr/IPXA2026022825145), Feb 26, 2026: FLOORBEAM. CORRODED. MAIN CABIN FLOORBEAM CORRODED BS 1420 RT OTBD LOWER SIDE ABOVE AFT LOWER CARGO DOOR VERIFIED STEP 17. FORMED TWO REPAIR ANGLES IAW SRM 53-00-51-2R-6.
- [SDR IPXA2026022845547](https://openairdocs.org/sdr/IPXA2026022845547), Feb 22, 2026: FLOOR SKIN. CORRODED. CORROSION ON FLOOR FORWARD OF PILOTS CONTROL COLUMN. REMOVED CORROSION FROM 2EA. FLOOR WEB PANELS IAW B757-200PF SRM 51-10-02-0G-0. INSTALLED 2EA. FLOOR WEB PAN
- [SDR IPXA2026031635090](https://openairdocs.org/sdr/IPXA2026031635090), Feb 21, 2026: FLOORBEAM. CORRODED. MAJOR REPAIR. UPON REMOVAL OF DAMAGED ON DECK PLATE, FOUND FLOORBEAM UPER FLANGE EXFOLIATED BS 1681, LBL 28 - 33. REMOVED THE DAMAGE. CUT OUT THE FLOORBEAM UPPE
- [SDR IPXA2026032038490](https://openairdocs.org/sdr/IPXA2026032038490), Feb 21, 2026: FLOOR SUPPORT. CORRODED. AFT CARGO COMP. FLOOR STRUCT. FLOOR STRINGER HAS EVIDENCE OF CORROSION AROUND MULTIPLE NUT PLATE HOLE BTW STA 1440 AND STA 1480 APPROX LBL/RBL 16.10, ID STICKER
- [SDR IPXA2026030838490](https://openairdocs.org/sdr/IPXA2026030838490), Feb 21, 2026: FLOOR SUPPORT. CORRODED. AFT CARGO COMP. FLOOR STRUCT. FLOOR STRINGER HAS EVIDENCE OF CORROSION AROUND MULTIPLE NUT PLATE HOLE BTW STA 1440 AND STA 1480 APPROX LBL/RBL 16.10, INSTALLED 
- [SDR IPXA2026031138732](https://openairdocs.org/sdr/IPXA2026031138732), Feb 21, 2026: FLOOR SUPPORT. CORRODED. AFT CARGO COMP. FLOOR STRUCT. FLOOR STRINGER HAS EVIDENCE OF CORROSION AROUND MULTIPLE NUT PLATE HOLE BTW STA 1440 AND STA 1480 APPROX LBL/RBL 7.55, ID STICKER 
- [SDR IPXA2026031810473](https://openairdocs.org/sdr/IPXA2026031810473), Feb 20, 2026: FLOOR PANEL. GOUGED. APPROX. 1 INCH LINE GOUGE, DIRT/ DEBRIS ON AFT CARGO FLOOR PANEL TAGGED, FROM BS 1460 - 1500. BLENDED DAMAGE. ORIGINAL MATERIAL THICKNESS IS .071, MATERIAL REMO
- [SDR IPXA2026031499164](https://openairdocs.org/sdr/IPXA2026031499164), Feb 19, 2026: FLOORBEAM. CORRODED. MAJOR REPAIR, MAIN DECK FLOOR AREA STA 1600 LBL 49 FLOORBEAM UNDERNEATH SURFACE HAS CORROSION. REMOVED CORROSION AT MAIN DECK FLOOR AREA STA 1600 LBL 49 FLOOR B
- [SDR IPXA2026032299492](https://openairdocs.org/sdr/IPXA2026032299492), Feb 19, 2026: STRINGER SPLICE. CORRODED. AFT CARGO COMP FLOOR STGR AT STA. 1460, RBL 15 HAS CORROSION AT BOTTOM SIDE. INSTALLED 1 EA NEW FLOOR STRINGER AT AFT CARGO COMPARTMENT STA. 1460, RBL 15 IAW B7
- [SDR IPXA2026031493675](https://openairdocs.org/sdr/IPXA2026031493675), Feb 19, 2026: SUPPORT ANGLE. CORRODED. APU INLET SUPPORT STRUCTURE UPPER SUPPORT ANGLE HAS CORROSION. LOWER SUPPORT ANGLE APU INLET P/N 148N3152-2 WILL BE INSTALLED ON JOB CARD T3F18E008AL0N LINE # 6
- [SDR IPXA2026031699642](https://openairdocs.org/sdr/IPXA2026031699642), Feb 19, 2026: STRAP. CORRODED. AFT CARGO COMP LH SIDE CEILING DECOMPRESSION PANEL STRAP BETWEEN BS 1560 & 1580 IS CORRODED. INSTALLED NEW CEILING DECOMPRESSION PANEL STABILIZATION STRAP, AND 
- [SDR IPXA2026031393618](https://openairdocs.org/sdr/IPXA2026031393618), Feb 19, 2026: STRAP. CORRODED. APU INLET SUPPORT STRUCTURE AFT STRAP IS CORRODED ATA 53-80 INSTALLED, 1EA REPAIR STRAP, 2EA REPAIR FILLER, 1EA STRAP AND 1EA EXISTING STRAP AT APU INLET SUPPOR
- [SDR IPXA2026031499075](https://openairdocs.org/sdr/IPXA2026031499075), Feb 19, 2026: FLOORBEAM. CORRODED. MAIN DECK FLOOR AREA STA 1681 LBL 31 METAL PLATE PANEL SURFACE BULGING SIGN OF CORROSION. ACCOMPLISHED REPAIR PER SRM 53-60-51-2R-6 REPAIR 6.
- [SDR IPXA2026031499159](https://openairdocs.org/sdr/IPXA2026031499159), Feb 19, 2026: RETAINER. CORRODED. MAIN DECK FLOOR AREA STA 1620-1640 LBL 62 ANGLE BAR SURFACE BULGING AND FASTENER HEAD FULL THROUGH SIGN OF CORROSION. INSTALLED NEW ANGLE BAR FASTENER RETAINER 
- [SDR IPXA2026031499642](https://openairdocs.org/sdr/IPXA2026031499642), Feb 19, 2026: STRAP. CORRODED. AFT CARGO COMP LT SIDE CEILING DECOMPRESSION PANEL STRAP BETWEEN STA 1560 AND 1580 IS CORRODED. 83-015. ATA 53-00 QC AUDIT C/W
- [SDR IPXA2026031499696](https://openairdocs.org/sdr/IPXA2026031499696), Feb 19, 2026: STRAP. CORRODED. AFT CARGO COMP RT SIDE CEILING DECOMPRESSION PANEL STRAP BETWEEN STA 1400 AND 1420 HAS CORROSION. 83-018. INSTALLED DECOMPRESSION PANEL LANDING ON AFT CARGO COM
- [SDR IPXA2026031499056](https://openairdocs.org/sdr/IPXA2026031499056), Feb 19, 2026: SEAT TRACK. CORRODED. MAIN DECK FLOOR AREA STA 1661-1681 RBL 45 SEAT TRACK SPLICE PLATE HAS CORROSION. INSTALLED FABRICATED FILLER AT MAIN DECK RBL45 SEAT TRACK P/N 146N5337-1SAAU IA
- [SDR IPXA2026031693647](https://openairdocs.org/sdr/IPXA2026031693647), Feb 19, 2026: SUPPORT ANGLE. CORRODED. APU INLET SUPPORT STRUCTURE LOWER SUPPORT ANGLE HAS CORROSION.
- [SDR IPXA2026031693675](https://openairdocs.org/sdr/IPXA2026031693675), Feb 19, 2026: SUPPORT ANGLE. CORRODED. APU INLET SUPPORT STRUCTURE UPPER SUPPORT ANGLE HAS CORROSION ATA 53-80 PRODUCTION AUDIT C/W
- [SDR IPXA2026031493686](https://openairdocs.org/sdr/IPXA2026031493686), Feb 19, 2026: SUPPORT ANGLE. CORRODED. APU INLET SUPPORT STRUCTURE FWD SIDE SMALL UPPER SUPPORT ANGLE HAS CORROSION. FABRICATED LOWEER SUPPORT ANGLE APU INLET IAW DWG 148N3141/ SAMPLE, WORK ACCOMPLIS
- [SDR IPXA2026031498924](https://openairdocs.org/sdr/IPXA2026031498924), Feb 19, 2026: SUPPORT ANGLE. CORRODED. APU INLET SUPPORT STRUCTURE LOWER SUPPORT ANGLE HAS CORROSION ATA 53-80 UPPER SUPPORT ANGLE APU INLET P/N 148N3152-1 WILL BE INSTALLED ON JOB CARD T3F18E008AL0N
- [SDR IPXA2026022399164](https://openairdocs.org/sdr/IPXA2026022399164), Feb 19, 2026: FLOORBEAM. CORRODED. MAIN DECK FLOOR AREA STA 1600 LBL 49 FLOORBEAM UNDERNEATH SURFACE HAS CORROSION.
- [SDR IPXA2026022899492](https://openairdocs.org/sdr/IPXA2026022899492), Feb 19, 2026: FLOOR SUPPORT. CORRODED. AFT CARGO COMP FLOOR SUPPORT AT STA. 1460, RBL 15 HAS CORROSION AT BOTTOM SIDE. 83-010. VERIFIED REMOVAL OF FLOOR SUPPORT ON STEP 7.
- [SDR IPXA2026022399056](https://openairdocs.org/sdr/IPXA2026022399056), Feb 19, 2026: SEAT TRACK. CORRODED. MAIN DECK FLOOR AREA STA 1661-1681 RBL 45 SEAT TRACK SPLICE PLATE HAS CORRODED. 7VERIFIED STEP 6 HAS BEEN ACCOMPLISHED.
- [SDR IPXA2026031355302](https://openairdocs.org/sdr/IPXA2026031355302), Feb 17, 2026: SUPPORT STRAP. CORRODED. APU INTAKE SUPPORT STRUCTURE FWD STRAP CORRODED FWD O/B SIDE. 61-016 ATA 53-80 INSTALLED 1EA UPPER SUPPORT ANGLE P/N: 148N3152-2, 1EA LOWER SUPPORT ANGLE P/N: 1
- [SDR IPXA2026022355337](https://openairdocs.org/sdr/IPXA2026022355337), Feb 17, 2026: NUT PLATE. CORRODED. CORROSION AROUND NUT PLATE 5 INCHES FWD OF STATION 1720 BTWN 24.75LB AND 0 LB AFT CARGO COMP. INSTALLED REPLACEMENT NUT PLATE ASSY AT AFT CARGO COMP. STA. 1715 
- [SDR IPXA2026030956993](https://openairdocs.org/sdr/IPXA2026030956993), Feb 17, 2026: DRAIN MAST. CORRODED. RIGHT AFT FUSELAGE RT APU EXHAUST CONE DRAIN MAST BASE EXFOLIATED. REMOVED CORROSION AT RT AFT FUSELAGE AT APU EXHAUST DRAIN MAST BASE IAW SRM 51-10-02-0G-0. IN
- [SDR IPXA2026030855388](https://openairdocs.org/sdr/IPXA2026030855388), Feb 17, 2026: NUT PLATE. CORRODED. CORROSION AROUND NUT PLATE 6 INCHES AFT OF STA 1701 BTWN LBL 45.5 AND 62. AFT CARGO COMP. INSTALLED REPLACEMENT NUT PLATE ASSY AT AFT CARGO COMP. STA. 1707 BTWN
- [SDR IPXA2025121057370](https://openairdocs.org/sdr/IPXA2025121057370), Dec 10, 2025: BRAKE. INOPERATIVE. UPON BLOCK IN AT DF THE PARKING BRAKE WAS SET THE BRAKES WERE RELEASED AND I FELT THE A\C MOVING . LOOKED UP AND QUICKLY SET THE FOOT BRAKES. ATTEMPTED TO SET T
- [SDR IPXA2025071881182](https://openairdocs.org/sdr/IPXA2025071881182), Jul 17, 2025: SIGN. INOPERATIVE. EMERGENCY EXIT SIGN HAS 7 EACH LIGHTS INOP. ++REPLACED 7 EACH BULBS IN EMERGENCY EXIT SIGN IAW AMM 33-51-01 OPS CHECK GOOD
- [SDR IPXA2025012126292](https://openairdocs.org/sdr/IPXA2025012126292), Jan 16, 2025: NONE. NONE. REF HEAVY CHECK REPAIR T3F18E004J5QK, HFEC AFTER TRIM OUT REQUIRES RII VERIFICATION. VERIFIED ACCOMPLISHMENT OF REPAIR PER EA 757-5360-27-A3771, REV- COMPLETED.
- [SDR IPXA2025012222873](https://openairdocs.org/sdr/IPXA2025012222873), Jan 15, 2025: WINDOW. SCRATCHED. **SUPPLEMENTAL SDR**FIRST OFFICERS #2 WINDOW SCRATCHED TO THE POINT THAT VISIBILITY IS COMPROMISED OUT THAT WINDOW. VERIFIED PROPER INSTALLATION AND TORQUE OF E
- [SDR IPXA2025011622873](https://openairdocs.org/sdr/IPXA2025011622873), Jan 15, 2025: WINDOW. SCRATCHED. FIRST OFFICERS #2 WINDOW SCRATCHED TO THE POINT THAT VISIBILITY IS COMPROMISED OUT THAT WINDOW. VERIFIED PROPER INSTALLATION AND TORQUE OF ELECTRICAL CONNECTION
- [SDR IPXA2024102987439](https://openairdocs.org/sdr/IPXA2024102987439), Oct 27, 2024: WINDSHIELD. CRACKED. LEFT FORWARD WINDSHIELD CRACKED IN FLIGHT @FL380 AFTER ARCING. COMPLETED #1 WINDSHIELD INSTALL IAW AMM 56-11-01. WITNESSED TERMINAL HARDWARE TORQUE OF THE #1 WI
- [SDR IPXA2024102887439](https://openairdocs.org/sdr/IPXA2024102887439), Oct 27, 2024: WINDSHIELD. CRACKED. LEFT FORWARD WINDSHIELD CRACKED IN FLIGHT @FL380 AFTER ARCING REMOVED AND REPLACED #1 WINDSHIELD REF AMM 56-11-01 UP TO STEP 13 (A) FIRST TORQUE. INITIAL TORQUE
- [SDR IPXA2024061824985](https://openairdocs.org/sdr/IPXA2024061824985), May 23, 2024: FLOOR SUPPORT. CORRODED. R/H T-CHORD FROM STA 1040-1060 RBL 0-68 HAS CORROSION. VERIFIED INSTALLED NUT PLATE IN T-CHORD STA 1040 -1060 RBL 0-68 IAW SRM 51-40-02. REVIEWED
- [SDR IPXA2024061428155](https://openairdocs.org/sdr/IPXA2024061428155), May 23, 2024: FLOOR SUPPORT. CORRODED. FAULT FLIGHT DECK ENTRANCE STA 297 SECTION 41 LOWER FLOOR BRACKET CORROSION DOT 44-44 INSTALLED ANGLE FROMFLIGHT DECK ENTRANCE STA 297, SECC 41, I.A.W. SRM 51-4
- [SDR IPXA2024061425327](https://openairdocs.org/sdr/IPXA2024061425327), May 23, 2024: TEE ANGLE. CORRODED. L/H T-CHORD FROM STA 1040-1060 LBL 0-37 HAS EXFOLIATED CORROSION (NEXT TO RAM EXHAUST) INSTALLED NEW LH T-CHORD ON STA 1040-1060 LBL0-37IAW B757 SRM 51-40-02 RE
- [SDR IPXA2024061225283](https://openairdocs.org/sdr/IPXA2024061225283), May 23, 2024: TEE ANGLE. CORRODED. *** SUPPLEMENTAL SDR *** FAULT: L/H T-CHORD AT STA 1045 HAS EXFOLIATED CORROSION. (NEXT TO RAM EXHAUST) INSTALLED NEW T-CHORD AT STA 1045 L/H. FASTENER P/N NAS6
- [SDR IPXA2024060924985](https://openairdocs.org/sdr/IPXA2024060924985), May 23, 2024: TEE ANGLE. CORRODED. *SDR FILED OPEN* FAULT: R/H T-CHORD FROM STA 1040-1060 RBL 0-68 HAS CORROSION JOP COMPLETE.
- [SDR IPXA2024060725283](https://openairdocs.org/sdr/IPXA2024060725283), May 23, 2024: TEE ANGLE. CORRODED. **SDR FILED OPEN**FAULT: L/H T-CHORD AT STA 1045 HAS EXFOLIATED CORROSION. (NEXT TO RAM EXHAUST) VERIFIED INSTALL
- [SDR IPXA2024061899986](https://openairdocs.org/sdr/IPXA2024061899986), May 22, 2024: FLOOR SUPPORT. CORRODED. **SUPPLEMENTAL SDR** FAULT: R/H T-CHORD 1180-1240 RBL 0-30 HAS CORROSION.INSTALLED NEW T-CHORD IAW SRM 51-40-02. INSTALLED NUT PLATES IAW SRM 51-40-02. REVIEWED
- [SDR IPXA2024060899986](https://openairdocs.org/sdr/IPXA2024060899986), May 22, 2024: TEE ANGLE. CORRODED. *SDR FILED OPEN* FAULT: R/H T-CHORD 1180-1240 RBL 0-30 HAS CORROSION VERIFIED INSTALL.

All 271: https://openairdocs.org/aircraft/N422UP/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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