# N416UP: 1990 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 PW2037](https://openairdocs.org/engine/pratt-whitney-pw2037) (registry code 52117)
- Data sheets: [TCDS E17NE](https://openairdocs.org/tcds/E17NE) (Pratt & Whitney) (OpenAirDocs)
- Serial number: 23903
- Year built: 1990
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 11, 1990
- Certificate issued: July 31, 1998
- Expires: November 30, 2027
- Mode S code: A4EC3A
- 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=416UP
- Page: https://openairdocs.org/aircraft/N416UP

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 PW2037)

- [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 N416UP.

## FAA accident and incident reports

None matched to N416UP.

## Service difficulty reports (261, 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 IPXA2026032266402](https://openairdocs.org/sdr/IPXA2026032266402), Mar 19, 2026: FLOOR SUPPORT. CRACKED. FAULT Z-100 STR: FLOOR STRINGER CRACKED FOUND AT AFT CARGO COMPARTMENT AT STA 1342 RBL 2.90 INSTALLED NEW STRINGER AT AFT CARGO COMPARTMENT AT STA 1342 RBL 2.90
- [SDR IPXA2026031153938](https://openairdocs.org/sdr/IPXA2026031153938), Mar 6, 2026: ANGLE. CRACKED. NUMBER 2 ENG PYLON FWD LOWER PLATE CRACKED INBD-OTBD SIDE. INSTALLED ANGLE AT NR 2 ENG PYLON FWD LOWER IAW SRM 51-40-02.
- [SDR IPXA2026031939735](https://openairdocs.org/sdr/IPXA2026031939735), Mar 5, 2026: TEE ANGLE. CORRODED. FAULT-STR-ZONE 100. RH LOWER MIDDLE FUSELAGE STA 1040-1060 RBL 65 T-CHORD CORRODED. DOT 28-05 INSTALLED NEW T-CHORD AT RH LOWER MIDDLE FUSELAGE STA 1040-1060 RB
- [SDR IPXA2026031919295](https://openairdocs.org/sdr/IPXA2026031919295), Mar 4, 2026: TEE ANGLE. CORRODED. LOWER HALF OF FUSELAGE TEE ANGLE BETWEEN BS 1040 & 1060, AROUND STRINGER 25R HAD CORROSION. INSTALLED A NEW TEE ANGLE BTWN BS 1040 - 1060, STRINGER 25R IAW SRM 
- [SDR IPXA2026032119365](https://openairdocs.org/sdr/IPXA2026032119365), Mar 4, 2026: ANGLE. CORRODED. LOWER HALF OF FUSELAGE RH PACK HOT AIR EXHAUST FRONT STRUCTURE ANGLE BETWEEN STR 1040 AND STR 1060 HAS CORROSION DOT 115-004. INSTALLED NEW INTERCOSTAL AND REIN
- [SDR IPXA2026031600239](https://openairdocs.org/sdr/IPXA2026031600239), Mar 3, 2026: SUPPORT ANGLE. CORRODED. AFT CARGO COMPT RIGHT LOWER BULKHEAD SUPPORT AT STA.1640 SHOWS EVIDENCE OF CORROSION AND A CRACK DOT 47-11 INSTALLED 2 ANGLES IAW SRM 51-40-02.
- [SDR IPXA2026030974670](https://openairdocs.org/sdr/IPXA2026030974670), Mar 2, 2026: FLOORBOARD. BROKEN. MAJOR REPAIR, MCD FLOORBOARD 241XCF AFT CORNER IS BROKEN. THE FLOORBOARD FABRICATED IAW SREO-9692-REQ001, VERIFIED RII REQUIREMENT COMPLETED, IAW UPS GMM 04.02.
- [SDR IPXA2026031579385](https://openairdocs.org/sdr/IPXA2026031579385), Mar 2, 2026: TRANSITION PANEL. CORRODED. TRANSITION PANEL FROM AFT CARGO COMPARTMENT STA1310 TO STA 1360 R/H CORROSION AND HOLES DAMAGED. INSTALLED NEW TRANSITION PANEL AFT CARGO COMPARTMENT STA 1310 T
- [SDR IPXA2026031784226](https://openairdocs.org/sdr/IPXA2026031784226), Mar 2, 2026: ANGLE. CRACKED. NR 1 ENG AFT PYLON FARING SUPPORT ANGLE L BRACKET ON INBD SIDE IS CRACKED. REMOVED BRACKET ON NR 1 ENGINE AFT PYLON FARING IAW SRM 51-40-02. INSTALLED A NEW L A
- [SDR IPXA2026032470530](https://openairdocs.org/sdr/IPXA2026032470530), Mar 1, 2026: FILLER. CORRODED. AFT CARGO, BS 1480 BILDGE AREA, NEAR ANTENNA LOWER SURFACE HAS CORRODED. INSTALLED NEW FILLER RADIUS IAW SRM 51-40-02-0G.
- [SDR IPXA2026030970913](https://openairdocs.org/sdr/IPXA2026030970913), Mar 1, 2026: FLOOR PANEL. DAMAGED. MAJOR REPAIR, FLOOR PANEL 241XDF IS DAMAGED IN A CORNER. DOT 23-027 INSPECTION FABRICATION OF FLOOR PANEL,VERIFIED RII REQUIREMENT COMPLETED, IAW UPS GMM 04.02.
- [SDR IPXA2026031770646](https://openairdocs.org/sdr/IPXA2026031770646), Mar 1, 2026: PANEL. CORRODED. AFT CARGO STA 1540 ON LH SIDE FLOOR ANCHOR POINT HAS CORROSION AROUND FASTENER. INSTALLED NEW REPAIR DOUBLER, NEW SIDE PANEL IAW B757-200PF, SRM 51-40-02.
- [SDR IPXA2026031763179](https://openairdocs.org/sdr/IPXA2026031763179), Mar 1, 2026: SUPPORT CHANNEL. CRACKED. LEFT MLG WW, TANG DOOR FWD CUTOUT, BRACKET SUPPORT AT LOWER SIDE HAS A CRACK. REMOVED DAMAGED BRACKET SUPPORT IAW SRM 51-40-02. INSTALLED PANEL 197DL, IAW AMM 5
- [SDR IPXA2026032658517](https://openairdocs.org/sdr/IPXA2026032658517), Feb 28, 2026: SKIN. DAMAGED. MAJOR REPAIR, TAIL EXTERNAL FUSELAGE, BTWN BS 1896.2 - 1992.8, 11 O'CLOCK POSITION, HAS 11EA POINTS WITH LIGHTNING STRIKE DAMAGE. BONDED REPAIR DOUBLER IAW SRM 
- [SDR IPXA2026032458260](https://openairdocs.org/sdr/IPXA2026032458260), Feb 28, 2026: RIVET. SHEARED. MAJOR REPAIR. EXTERNAL LOWER FUSELAGE, BS 1460, S29R HAD A SHEAR RIVET, EVIDENCE OF CORROSION INSIDE. VERIFIED REPAIR ACCOMPLISHED PER EO-96803-REQ1 AND VT-MAE 
- [SDR IPXA2026032153766](https://openairdocs.org/sdr/IPXA2026032153766), Feb 28, 2026: STRAP. CORRODED. MAJOR REPAIR, APU INLET DOOR CUTOUT AFT STRAP HAS EVIDENCE OF CORROSION INSTALLED ALL PARTS OF REPAIR: FILLER MIDDLE STRAP [3], FILLER SHEAR TIE [4], STRAP [2],
- [SDR IPXA2026032054456](https://openairdocs.org/sdr/IPXA2026032054456), Feb 28, 2026: TEE FITTING. CORRODED. LOWER FUSELAGE, STA 1040 T-CHORD RBL 6 TO RBL 25 HAS EVIDENCE OF CORROSION AND BARE METAL INSTALLED NEW T-CHORD ON, LOWER FUSELAGE, STA 1040, IAW B757-200PF, SR
- [SDR IPXA2026032453721](https://openairdocs.org/sdr/IPXA2026032453721), Feb 28, 2026: STRAP. CORRODED. APU INLET DOOR CUTOUT FWD STRAP HAS EVIDENCE OF CORROSION INSTALLED FWD STRAP IAW SRM 51-40-02-0G-0.
- [SDR IPXA2026031653968](https://openairdocs.org/sdr/IPXA2026031653968), Feb 28, 2026: SUPPORT ANGLE. CORRODED. APU INLET DOOR CUTOUT LOWER CORNER ANGLE BRACKET HAS EVIDENCE OF CORROSION INSTALLED LOWER CORNER ANGLE I.A.W. B757-200 SRM 51-40-02-0G-0
- [SDR IPXA2026031753310](https://openairdocs.org/sdr/IPXA2026031753310), Feb 28, 2026: SUPPORT ANGLE. CORRODED. APU INLET DOOR CUTOUT LOWER ANGLE SUPPORT HAS CORROSION INSTALLED 1EA NEW ANGLE IAW SRM 51-40-02-0G-0
- [SDR IPXA2026031753605](https://openairdocs.org/sdr/IPXA2026031753605), Feb 28, 2026: SUPPORT ANGLE. CORRODED. APU INLET DOOR CUTOUT UPPER ANGLE SUPPORT HAS EVIDENCE OF CORROSION INSTALLED 1EA NEW UPPER ANGLE I.A.W. B757-200PF SRM 51-40-02-0G-0
- [SDR IPXA2026031653872](https://openairdocs.org/sdr/IPXA2026031653872), Feb 28, 2026: SUPPORT ANGLE. CORRODED. APU INLET DOOR CUTOUT UPPER CORNER ANGLE BRACKET HAS EVIDENCE OF CORROSION INSTALLED ANGLE SUPPORT IAW SRM 51-40-02-0G-0.
- [SDR IPXA2026032144661](https://openairdocs.org/sdr/IPXA2026032144661), Feb 27, 2026: RIB. CORRODED. LH WING THROUGH ACCESS PANEL 561HB AILERON SUPPORT WITH CORROSION, INSTALLED NEW RIB IAW B757-200PF SRM 51-40-02.
- [SDR IPXA2026031844220](https://openairdocs.org/sdr/IPXA2026031844220), Feb 27, 2026: FLOOR PANEL. DAMAGED. MAJOR REPAIR, TAIL COMPARTMENT WORK PLATFORM STA 1743-1768 ANTI-SKID MATERIAL DEGRADED/DISBONDING. INSTALLED NEW FLOOBOARD IAW B757-200 SRM 51-40-02.
- [SDR IPXA2026031344908](https://openairdocs.org/sdr/IPXA2026031344908), Feb 27, 2026: PLATE. CRACKED. LH WING REAR SPAR AT PYLON #1 HAVE RIVETS CUT AND BRACKET BROKEN. REMOVED 2 EA BROKEN BRACKETS FROM LH WING REAR SPAR AT PYLON #1 IAW B757-200PF SRM-51-40-02-0G
- [SDR IPXA2024050453307](https://openairdocs.org/sdr/IPXA2024050453307), Apr 24, 2024: DECK PLATE. CORRODED. AFT DECK PLATE STA 1681 HAS CORROSION BETWEEN LBL 10 AND LBL 15. VERIFIED INSTALLED DOUBLER AND FILLER OK TO APPLY CIC INSP ONLY. APPLIED CIC I.A.W AMM 51-00-59
- [SDR IPXA2024050353295](https://openairdocs.org/sdr/IPXA2024050353295), Apr 24, 2024: DECK PLATE. CORRODED. AFT DECK PLATE STA 1681 HAS CORROSION BETWEEN RBL 10 AND RBL 15. INSTALLED DOUBLER AND FILLER I.A.W SRM 53-60-51-2R-8 PARAGRAPH 4. M TO O.VERIFIED INSTALLED DOU
- [SDR IPXA2024042453307](https://openairdocs.org/sdr/IPXA2024042453307), Apr 24, 2024: DECK PLATE. CORRODED. AFT DECK PLATE STA 1681 HAS CORROSION BETWEEN LBL 10 AND LBL 15. OPEN
- [SDR IPXA2024042453295](https://openairdocs.org/sdr/IPXA2024042453295), Apr 24, 2024: DECK PLATE. CORRODED. AFT DECK PLATE STA 1681 HAS CORROSION BETWEEN RBL 10 AND RBL 15. OPEN
- [SDR IPXA2024051089534](https://openairdocs.org/sdr/IPXA2024051089534), Apr 19, 2024: NUT PLATE. CORRODED. ONE EA NUTPLATE STRAP WITH CORROSION AT STA 1720 BETWEEN LBL 33.10 AND LBL 39.50 VERIFIED: INSTALLED AFT DRAIN PAN IAW B757 SRM 51-40-02-0G. VERIFIED JOB COMPLE
- [SDR IPXA2024050289556](https://openairdocs.org/sdr/IPXA2024050289556), Apr 19, 2024: FLOORBEAM. CORRODED. MAIN CARGO DECK - FLOOR BEAM WITH CORROSION AT STA 1200 RBL 5. INSTALLED 4EA REPAIR PARTS IAW SRM 53-00-51-2R-6 AND SRM 51-40-02-0G-0. REVIEWED.
- [SDR IPXA2024042289534](https://openairdocs.org/sdr/IPXA2024042289534), Apr 19, 2024: NUT PLATE. CORRODED. **SDR FILED OPEN** FAULT: 1 EA NUTPLATE STRAP WITH CORROSION AT STA 1720 BETWEEN LBL 33.10 AND LBL 39.50 APPROVED.
- [SDR IPXA2024042289556](https://openairdocs.org/sdr/IPXA2024042289556), Apr 19, 2024: FLOORBEAM. CORRODED. **SDR FILED OPEN** FAULT: MAIN CARGO DECK - FLOOR BEAM WITH CORROSION AT STA 1200 RBL 5 VERIFIED OUT OF LIMITS
- [SDR IPXA2024041966153](https://openairdocs.org/sdr/IPXA2024041966153), Apr 18, 2024: FRAME. DENTED. FWD CARGO PIT FRAME STA 720 RH HAS A DENT ON INBOARD CHORD BETWEEN STR 24R/25R APPROVED. OPEN
- [SDR IPXA2024041966275](https://openairdocs.org/sdr/IPXA2024041966275), Apr 18, 2024: FRAME. DENTED. **SDR FILED OPEN**FAULT: FWD CARGO PIT FRAME STA 820 LH HAS A DENT ON INBOARD CHORD BETWEEN STR 24L/25L APPROVED.
- [SDR IPXA2024041966665](https://openairdocs.org/sdr/IPXA2024041966665), Apr 18, 2024: FRAME. DENTED. FWD CARGO PIT FRAME STA 800 LH HAS A DENT ON INBOARD CHORD BETWEEN STR 24/25L APPROVED. OPEN
- [SDR IPXA2024041966254](https://openairdocs.org/sdr/IPXA2024041966254), Apr 18, 2024: FRAME. DENTED. FWD CARGO PIT FRAME STA 780 RH HAS A DENT ON INBOARD CHORD AT STR 24R APPROVED. OPEN
- [SDR IPXA2024050429715](https://openairdocs.org/sdr/IPXA2024050429715), Apr 16, 2024: FRAME. DENTED. AFT CARGO PIT - FRAME STA 1500 RH SIDE HAS A DENT ON TOP OF AN EXISTING REPAIR. REF STEP 65. INSPECTED AND VERIFIED ACCOMPLISHED EA# 757-5360-27-A3576 STEP 24 P
- [SDR IPXA2023111605008](https://openairdocs.org/sdr/IPXA2023111605008), Nov 15, 2023: LIGHT. INOPERATIVE. FAULT: MXP-5067-JIC--L1 DOOR EMERGENCY LIGHT INOP INSTALLED L1 DOOR BATTERY IAW MM 33-51-01. OPS CHECKED GOOD IAW MM 33-51-01-962-001. AUDIT COMPLETE
- [SDR IPXA2022042381417](https://openairdocs.org/sdr/IPXA2022042381417), Apr 23, 2022: STRUCTURE. CORRODED. INSPECTION TYPE:SEG2WING TO BODY STRUCTURE AT FS 1180-1240 RBL 57.5 HAS INTERGRANULAR CORROSION.REMOVED CORRODED T CHORD SECTION AND INSTALLED REPLACEMENT T CHO
- [SDR IPXA2022042681493](https://openairdocs.org/sdr/IPXA2022042681493), Apr 18, 2022: BRACKET. CRACKED. INSPECTION TYPE:C#1 ENGINE L/H PYLON O/B MID SPAR LOWER ATTACHMENT BRACKET IS CRACKED IN THE RADIUS CORNER 2.35" LONGREMOVED CRACKED BRACKET AND INSTALLED REPLA
- [SDR IPXA2022042681494](https://openairdocs.org/sdr/IPXA2022042681494), Apr 14, 2022: STRUCTURE. CORRODED. INSPECTION TYPE:CWING TO BODY SUPPORT STRUCTURE AT FS 1200 FROM WL 208 TO 133 RBL 70 HAS EXFOLIATED CORROSIONREMOVED AND REPLACED WITH TO BODY LOWER T CHORD SEG
- [SDR IPXA2022042681497](https://openairdocs.org/sdr/IPXA2022042681497), Apr 13, 2022: STRUCTURE. CORRODED. INSPECTION TYPE:CWING TO BODY SUPPORT STRUCTURE LOWER T CHORD AT FS 1180-1240 LBL 57.5 IS EXFOLIATEDREMOVED AND REPLACED WING TO BODY LOWER T CHORD SEGMENT PER 
- [SDR IPXA2022042881539](https://openairdocs.org/sdr/IPXA2022042881539), Apr 12, 2022: STRUCTURE. CORRODED. INSPECTION TYPE:CWING TO BODY STRUCTURE LOWER T CHORD AT FS 1180 TO FS 1240 RBL 50 LOWER FLANGE WAS EXFOLIATEDREMOVED AND REPLACED LOWER T CHORD PER SRM 51-40-0
- [SDR IPXA2022042881538](https://openairdocs.org/sdr/IPXA2022042881538), Apr 11, 2022: STRUCTURE. CORRODED. INSPECTION TYPE:CWING TO BODY STRUCTURE LOWER T CHORD AT FS 1180 FROM BL 0 TO RBL 70 IS EXFOLIATED ON UPPER FLANGE.REMOVED AND REPLACED LOWER T CHORD PER SRM 51
- [SDR IPXA2022042681498](https://openairdocs.org/sdr/IPXA2022042681498), Apr 11, 2022: BRACKET. CRACKED. INSPECTION TYPE:C#2 ENGINE PYLON AFT FAIRING FWD LOWER CORNER THE 313N3052-17 BRACKET IS CRACKEDREMOVED AND REPLACED BRACKET PER SRM 51-40-02-0G
- [SDR IPXA2022042581448](https://openairdocs.org/sdr/IPXA2022042581448), Apr 11, 2022: FRAME. DENTED. INSPECTION TYPE:CAFT LOWER CARGO PIT FRAME AT FS 1520 BETWEEN STR 25R TO 26R HAS A DENT ON UPPER FLANGE OF FRAMEREPAIRED FRAME 1520 PER SRM 53-00-07-2R-5
- [SDR IPXA2022050581792](https://openairdocs.org/sdr/IPXA2022050581792), Apr 9, 2022: FRAME. DAMAGED. INSPECTION TYPE:CNEEDED ALTERNATIVE METHOD TO INSPECT FRAME 1600 RH PER EO# B757-5310-73926-AMODIFIED REPAIR AT FR 1600 RH STR 26R PER EA# 757-5360-27-A2897
- [SDR IPXA2022050581791](https://openairdocs.org/sdr/IPXA2022050581791), Apr 9, 2022: FRAME. DAMAGED. INSPECTION TYPE:CNEEDED ALTERNATIVE METHOD TO INSPECT FRAME 1560 LH PER EO# B757-5310-73926-AMODIFIED REPAIR AT FR 1560 STR 26L PER EA# 757-5360-27-A2892
- [SDR IPXA2022050581790](https://openairdocs.org/sdr/IPXA2022050581790), Apr 9, 2022: FRAME. DAMAGED. INSPECTION TYPE:CNEEDED ALTERNATIVE METHOD TO INSPECT FRAME 1300 LH PER EO# B757-5310-73926-AMODIFIED REPAIR AT FR 1300 STR 26L PER EA# 757-5360-27-A2901-A

All 261: https://openairdocs.org/aircraft/N416UP/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 PW2037 engine: https://openairdocs.org/engine/pratt-whitney-pw2037.md

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