# N411UP: 1988 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: 23851
- Year built: 1988
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 1, 1988
- Certificate issued: September 12, 1988
- Expires: May 31, 2028
- Mode S code: A4D9A7
- 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=411UP
- Page: https://openairdocs.org/aircraft/N411UP

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 N411UP.

## FAA accident and incident reports

None matched to N411UP.

## Service difficulty reports (199, 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 IPXA2026080363542](https://openairdocs.org/sdr/IPXA2026080363542), Aug 1, 2026: DUCT. WARNING MESSAGE. LEFT BLD DUCT LEAK EICAS MSG AT F340. QRH CHECKLIST COMPLETED AND L BLD DUCT LEAK MESSAGE WENT AWAY. PERFORMED FIM 26-90-15-00 SHEET 1 FIG 103 STEPS 1,10,2, SHE
- [SDR IPXA2026012304472](https://openairdocs.org/sdr/IPXA2026012304472), Jan 14, 2026: WEB. DAMAGED. STA 1200 UPPER WEB HAS A DAMAGED HOLE. AFTER FURTHER EVALUATION FOUND 4 DOUBLE HOLE AT THE TOP OF THE WEB. FOUND OUT OF LIMITS IAW B757-200 SRM 53-00-71-1A-1 AD
- [SDR IPXA2026011963930](https://openairdocs.org/sdr/IPXA2026011963930), Jan 12, 2026: SEAT TRACK. CORRODED. CAP SEAT TRACKS HAVE EVIDENCE OF CORROSION (AFT I/B EXFOLIATED) MARKED AREAS. REMOVED CORROSION LOCATED ON MAIN DECK FLOOR SHEAR UNDER SEAT TRACK. LBL13.0 AND 2
- [SDR IPXA2026020462981](https://openairdocs.org/sdr/IPXA2026020462981), Jan 12, 2026: STRINGER. CORRODED. FUSELAGE SKIN IS BULDGING AROUND TWO FASTNER HEADS, JUST FORWARD OF THE AFT LOWER FUSELAGE MAJOR REPAIR AT AFT VHF ANTENNA. REMOVED 3 BULDGING RIVETS FORWARD OF
- [SDR IPXA2026013069167](https://openairdocs.org/sdr/IPXA2026013069167), Jan 12, 2026: TEE ANGLE. CORRODED. WING TO BODY FAIRING STRUCTURE LOWER T-CHORD EXFOLIATED AND WITH MULTIPLE SPOTS OF HEAVY CORROSION FROM BS 1180 TO 1240 AT RBL 57.50. DOT 21-40. EVALUATED TEE F
- [SDR IPXA2026012869037](https://openairdocs.org/sdr/IPXA2026012869037), Jan 12, 2026: TEE FITTING. CORRODED. WING TO BODY FAIRING STRUCTURE UPPER TEE FITTING EXFOLIATED AND WITH MULTIPLE SPOTS OF HEAVY CORROSION FROM BS 1180 TO BS 1240, RBL 57.50. REMOVED AFT WTB PANEL
- [SDR IPXA2026012868936](https://openairdocs.org/sdr/IPXA2026012868936), Jan 12, 2026: CHANNEL. CORRODED. WING TO BODY FAIRING SUPPORT STRUCTURE WITH EXFOLIATED CORROSION AT BS 1219 RBL 6. INSTALLED NEW CHANNEL, 2EA SUPPORT PLATES, 1EA ANGLE, IN WING TO BODY, BS 121
- [SDR IPXA2026012869140](https://openairdocs.org/sdr/IPXA2026012869140), Jan 12, 2026: TEE FITTING. CORRODED. WING TO BODY FAIRING STRUCTURE, VERTICAL T-FITTING EXFOLIATED AT LWR END AT BS 1200 RBL 57.50. INSTALLED T-FITTING IAW SRM 51-40-02.
- [SDR IPXA2026011955833](https://openairdocs.org/sdr/IPXA2026011955833), Jan 11, 2026: SKIN PANEL. CORRODED. APU BAY, INTERNAL STRUCTURE RT SIDE, BTWN BS 1885.2 & 1918.9, ALUMINUM HONEYCOMB SKIN HAD CORROSION. TRIMMED OUT LOWER FWD SECTION OF HONEYCOMB ONLY ON SKIN BON
- [SDR IPXA2026013056128](https://openairdocs.org/sdr/IPXA2026013056128), Jan 11, 2026: LONGERON. CORRODED. APU BAY, INTERNAL STRUCTURE RT LONGERON, BS 1885.2 CORRODED. REMOVED CORROSION ON THE RT APU LONGERON, ORIGINAL THICKNESS 0.050", MATERIAL REMOVED 0.008". INSTA
- [SDR IPXA2026013056154](https://openairdocs.org/sdr/IPXA2026013056154), Jan 11, 2026: INTERCOSTAL. CRACKED. MDC DOOR INTERNAL STRUCTURE, AN INTERCOSTAL FOUND CRACKED AT FWD LWR SECTION. REMOVED THE INTERCOSTAL IAW SRM 51-40-02-0G-0, AFTER EVALUATION FOUND CRACK TO BE 
- [SDR IPXA2026012234008](https://openairdocs.org/sdr/IPXA2026012234008), Jan 9, 2026: SKIN. CRACKED. LEFT WING FIXED LEADING EDGE SKIN UPPER SURFACE HAS A GOUGE, AREA BY SLAT NR 1 OTBD END. PERFORMED CUT OUT OF THE AFFECTED PANEL FROM THE CENTER LINE OF THE MAI
- [SDR IPXA2026012833721](https://openairdocs.org/sdr/IPXA2026012833721), Jan 9, 2026: TEE FITTING. CORRODED. LEFT WING TO BODY FAIRING STRUCTURE WITH TEE FITTINGBEAM EXFOLIATED BTWN STA 1200 AND 1220 AT BL 57.50. INSTALLED NEW T-FITTING P/N: UP-149N7630-37 BETWEEN STA 
- [SDR IPXA2026011209109](https://openairdocs.org/sdr/IPXA2026011209109), Jan 8, 2026: FLOORBEAM. CORRODED. STR Z100 FAULT: FRETTING CORROSION ON T-ANGLE AT STA 1037, LBL 5 TO LBL 15 INSTALLED T-CHORD. IAW B757-200 SRM 51-40-02.
- [SDR IPXA2026012709232](https://openairdocs.org/sdr/IPXA2026012709232), Jan 8, 2026: FLOORBEAM. CORRODED. FRETTING CORROSION ON FLOORBEAM T-ANGLE AT BS 900 BETWEEN LBL 7 TO LBL 12. REVIEWED.
- [SDR IPXA2026012110991](https://openairdocs.org/sdr/IPXA2026012110991), Jan 8, 2026: ANGLE. CORRODED. ANGLE AT BS 1037, LBL 60 HAD CORROSION. INSTALLED NEW ANGLES 2EA IAW SRM 51-40-02.
- [SDR IPXA2026013096567](https://openairdocs.org/sdr/IPXA2026013096567), Jan 7, 2026: TEE FITTING. CORRODED. TEE FITTING AT BS 1147, RBL 65 SHOWS SIGNS OF LIGHT CORROSION. REMOVED THE DAMAGED TEE FITTING IAW SRM 51-40-02. INSTALLED NEW TEE FITTING P/N: UP-149N7222-69 B
- [SDR IPXA2026013096671](https://openairdocs.org/sdr/IPXA2026013096671), Jan 7, 2026: TEE FITTING. CORRODED. TEE FITTING, BS 1037 - 1060, LBL 37, HAD EXFOLIATING CORROSION. REMOVED FLOOR PANEL 198CR AT EXHAUST AREA BTWN BS 1037 TO 1060, RBL 65 TO FACILITATE THE EVALUAT
- [SDR IPXA2026012896589](https://openairdocs.org/sdr/IPXA2026012896589), Jan 7, 2026: TEE FITTING. CORRODED. THE OTBD T-FITTING FOR ECS EXHAUST, STA 1037-1060, RBL 60 HAS CORROSION. INSTALLED T-FITTING IN STA 1037-1060, RBL 60 PER B757-200 SRM 51-40-02.
- [SDR IPXA2026010996688](https://openairdocs.org/sdr/IPXA2026010996688), Jan 7, 2026: TEE FITTING. CORRODED. TEE FITTING, BS 1037 - 1060, LBL 60, EXFOLIATING CORROSION. REMOVED THE TEE FITTING IAW SRM 51-40-02. INSTALLED A NEW TEE FITTING IAW SRM 51-40-02.
- [SDR IPXA2025032894505](https://openairdocs.org/sdr/IPXA2025032894505), Mar 27, 2025: BLEED AIR SYS. OSCILLATES. RIGHT BLEED AIR OSCILLATING RAPIDLY AT FL 390. THIS WAS CAUSING ENG TO SURGE FROM 1.17 TO 1.34 EPR ALONG WITH A YAWING MOTION TO AIRCRAFT. AFTER BLEED VALVE SHU
- [SDR IPXA2025032794505](https://openairdocs.org/sdr/IPXA2025032794505), Mar 27, 2025: BLEED VALVE. FAULTED. **SDR FILED OPEN** **DIVERSION**RIGHT BLEED AIR OSCILLATING RAPIDLY AT FL 390. THIS WAS CAUSING ENG TO SURGE FROM 1.17 TO 1.34 EPR ALONG WITH A YAWING MOTION TO
- [SDR IPXA2024020680118](https://openairdocs.org/sdr/IPXA2024020680118), Feb 2, 2024: SKIN. DAMAGED. R/H ELEVATO AFT TIP HAS EXFOILATION ON TO AND BOTTOM MARKED IN RED. DOT 140-1 INSTALLED R/H ELEVATOR IAW AMM 27-31-01-424-028. REPLACED ROD END OF POSITION TRAN
- [SDR IPXA2024021625858](https://openairdocs.org/sdr/IPXA2024021625858), Jan 31, 2024: SKIN. CORRODED. FAULT: #2 ENG O/B CORE COWL HAS CORROSION I/B UP TOP IN THE MIDDLE. DOT 33-010 INSTALLED #2 ENG O/B CORE COWL IAW AMM 71-11-06-404-036-P00 UNTILL STEP G (4).
- [SDR IPXA2024020936216](https://openairdocs.org/sdr/IPXA2024020936216), Jan 31, 2024: ANGLE. CORRODED. ANGLE WITH CORROSION IN LH RUDDER PEDAL ASSY. DOT 07308-001 INSTALLED NEW ANGLE I.A.W. SRM 51-40-02-0G.
- [SDR IPXA2023101658163](https://openairdocs.org/sdr/IPXA2023101658163), Oct 12, 2023: BULKHEAD. CRACKED. *SUPPLEMENTAL SDR* R\H PYLON, HYD BAY, AFT SIDE OF PYLON BULKHEAD, UPPER SUPPORT ANGLE, I\B SIDE, HAS AN 1 1\2 INCH CRACK. VERIFIED HEAT TREATMENT PER NDTM, PAR
- [SDR IPXA2023101358163](https://openairdocs.org/sdr/IPXA2023101358163), Oct 12, 2023: UNKNOWN. UNKNOWN. *SDR FILED OPEN* R\H PYLON, HYD BAY, AFT SIDE OF PYLON BULKHEAD, UPPER SUPPORT ANGLE, I\B SIDE, HAS AN 1 1\2 INCH CRACK
- [SDR IPXA2022090185804](https://openairdocs.org/sdr/IPXA2022090185804), Sep 1, 2022: NONE. NONE. INSPECTION TYPE:**SDR FILED OPEN** L FWD ENTRY DOOR EICAS AFTER LANDING \, DURING TAXI, ILLUMINATED. WENT OUT AFTER 1 MINUTE. DEFERRED LEFT FWD ENTRY DOOR INDIC
- [SDR IPXA2020052255632](https://openairdocs.org/sdr/IPXA2020052255632), May 22, 2020: FITTING. CRACKED. INSPECTION TYPE:SEG3UPPER SKIN FITTING RH PYLON #3 HOLE HAD REJECTABLE CRACK INDICATIONS AT BOTTOM OF HOLEREAMED HOLE TO REMOVED INDICATION PER E.O. B757-5720-7
- [SDR IPXA2020052255631](https://openairdocs.org/sdr/IPXA2020052255631), May 22, 2020: FITTING. DAMAGED. INSPECTION TYPE:SEG3UPPER SKIN DRAG FITTING RH PYLON #1 HOLE HAS VISUAL DAMAGEREAMED HOLE TO REMOVED DAMAGE PER E.O. B757-5720-76605-A.
- [SDR IPXA2020052255627](https://openairdocs.org/sdr/IPXA2020052255627), May 22, 2020: SKIN. CRACKED. INSPECTION TYPE:SEG3UPPER SKIN RH PYLON #8 HOLE HAS CRACK INDICATIONSREPAIRED PER EO BY REMAINING HOLE TO REMOVED DAMAGE B757-5720-76605-A
- [SDR IPXA2020052055527](https://openairdocs.org/sdr/IPXA2020052055527), May 19, 2020: ANGLE. CORRODED. INSPECTION TYPE:SEG3ANGLE SUPPORT FWD RAT CUTOUT BEAM HAS CORROSION ON THE IB SIDE STA 1180REPLACED ANGLE IAW DWG 149N7734
- [SDR IPXA2020022875537](https://openairdocs.org/sdr/IPXA2020022875537), Feb 26, 2020: WARNING MESSAGE. FALSE ACTIVATION. INSPECTION TYPE:N/AEMERGENCY DECLARED - TRAILING EDGE FLAP DISAGREE MESSAGE AFTER T/O. ASSOCIATED TRAILING EDGE LIGHT ILLUMINATED. ACCOMPLISHED QRH TRAILING EDG
- [SDR IPXA2020011350866](https://openairdocs.org/sdr/IPXA2020011350866), Jan 10, 2020: ROTARY ACTUATOR. FAULTY. INSPECTION TYPE:N/A**EMERGENCY DECLARED** IN PATTERN AT SDF @ 3000FT AND 210 KNOTS WE SELECTED FLAPS 1 AND GOT LE SLAT DISAGREE EICAS AND LEADING EDGE ANNEMERAT
- [SDR IPXA2018051409532](https://openairdocs.org/sdr/IPXA2018051409532), May 2, 2018: FLOOR PANEL. TORN. INSPECTION TYPE: SEG2, MAIN DECK FLOOR PANEL 231XJF FOUND TORN. FABRICATED A NEW FLOOR PANEL, AND INSTALLED IAW SREO B757-5320-9692-K.
- [SDR IPXA2018051409531](https://openairdocs.org/sdr/IPXA2018051409531), May 2, 2018: FLOOR PANEL. DELAMINATED. INSPECTION TYPE: SEG2, MAIN DECK FLOOR PANEL 231XFF FOUND DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K, AND INSTALLED.
- [SDR IPXA2018052189757](https://openairdocs.org/sdr/IPXA2018052189757), Apr 30, 2018: SKIN. DENTED. INSPECTION TYPE: SEG2,M UPPER MID FUSELAGE EXTERNAL SKIN HAD ONE DENT AT BS 1180 STRINGER 7R. REPAIRED IAW EA 757-5361-27-A2298.
- [SDR IPXA2017053117742](https://openairdocs.org/sdr/IPXA2017053117742), May 25, 2017: SMOKE GOGGLES. CRACKED. SUPERNUMERARY SEAT SMOKE GOGGLES CRACKED. REPLACED THE SMOKE GOGGLES.
- [SDR IPXA2016102709939](https://openairdocs.org/sdr/IPXA2016102709939), Oct 26, 2016: CABLE. MISROUTED. INSPECTION TYPE: N/A, EMER DECENT REELS CABLES IMPROPERLY ROUTED BACKWARDS. REROUTED CABLES PER AMM 25-61-02-201.
- [SDR IPXA2016052303769](https://openairdocs.org/sdr/IPXA2016052303769), May 23, 2016: SKIN. CORRODED. INSPECTION TYPE:C-17, EXTERNAL FUSELAGE BS 1473 VHF ANTENNA SUPPORT HAS SURFACE CORROSION, MATERIAL THICKNESS DOES NOT MATCH S/O 757-53A0053 REQUIREMENTS, SHOUL
- [SDR IPXA2016052203664](https://openairdocs.org/sdr/IPXA2016052203664), May 17, 2016: SHEAR TIE. CRACKED. INSPECTION TYPE:C-17, AFT PIT BS 1480, SHEAR TIE CRACKED BETWEEN S-25L AND S-26L. R & R SHEAR TIE IAW SRM 51-40-02.
- [SDR IPXA2016052203673](https://openairdocs.org/sdr/IPXA2016052203673), May 1, 2016: SKIN. DENTED. INSPECTION TYPE:C-17, FUSELAGE SKIN DENT AT BS 1475, BETWEEN STR 25L- 26L. REPAIRED IAW REO-G19910.
- [SDR IPXA2015101694858](https://openairdocs.org/sdr/IPXA2015101694858), Oct 14, 2015: SHAFT. LOOSE. ON LANDING MAIN ENTRY DOOR EICAS MESS AND OVERHEAD LT, CAME ON AND STAYED ON DOOR WAS CLOSED AND LATCHED. TIGHTENED ATTACHING HARDWARE ON HANDLE SHAFT IAW MM 52
- [SDR IPXA2015082892818](https://openairdocs.org/sdr/IPXA2015082892818), Aug 27, 2015: BULB. INOPERATIVE. INSPECTION TYPE:IN, EMERGENCY LIGHTS "UNARMED" AND HAS ONE BULB OUT. REPLACED THE ANNUNCIATOR. , OK FOR SERVICE.
- [SDR IPXA2015020985675](https://openairdocs.org/sdr/IPXA2015020985675), Feb 6, 2015: BULB. INOPERATIVE. EMERGENCY LIGHT HAS SIX INOPERATIVE BULBS. REPLACED THE BULBS IAW AMM 33-51-01-2.
- [SDR IPXA2014061183260](https://openairdocs.org/sdr/IPXA2014061183260), May 16, 2014: FRAME. DENTED. C16 INSPECTION, AFT CARGO BAY BS 1560, S26L FRAME DENTED. REPAIRED IAW SRM 53-00-07-2R REPAIR 5, DETAIL II.
- [SDR IPXA2014060683213](https://openairdocs.org/sdr/IPXA2014060683213), May 16, 2014: FRAME. DENTED. C16 INSPECTION, AFT CARGO BAY FRAME BS 1540, STR 25L DENTED. REPAIRED IAW SRM 53-00-07-2R, REPAIR 5, DETAIL II.
- [SDR IPXA2014060683212](https://openairdocs.org/sdr/IPXA2014060683212), May 16, 2014: STRINGER. CORRODED. C16 INSPECTION, AFT CARGO BAY STRINGER 25L BS 1460 IS CORRODED. REPAIRED IAW SRM 53-00-03-2R, REPAIR 1, DETAIL II.
- [SDR IPXA2014060683200](https://openairdocs.org/sdr/IPXA2014060683200), May 16, 2014: FRAME. DENTED. C16 INSPECTION, AFT CARGO BAY FRAME BS 1280, S26L DENTED. INSTALLED REPAIR IAW SRM 53-00-07-2R, REPAIR 6, DETAIL IV.
- [SDR IPXA2014060483199](https://openairdocs.org/sdr/IPXA2014060483199), May 16, 2014: FRAME. DENTED. C16 INSPECTION, AFT CARGO BAY BS 1460, S26L FRAME DENTED. REPAIRED IAW SRM 53-00-07-2R-5 FIG 201, DETAIL I.

All 199: https://openairdocs.org/aircraft/N411UP/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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