# N408UP: 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: 23730
- Year built: 1988
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 15, 1988
- Certificate issued: May 21, 1999
- Expires: May 31, 2027
- Mode S code: A4CC29
- 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=408UP
- Page: https://openairdocs.org/aircraft/N408UP

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 N408UP.

## FAA accident and incident reports

None matched to N408UP.

## Service difficulty reports (254, 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 IPXA2026021096944](https://openairdocs.org/sdr/IPXA2026021096944), Jan 27, 2026: STIFFENER. CRACKED. # 2 PYLON ANGLE IS CRACKED INSIDE PANEL 445AL , ATA 54 STR. INSTALLED (1EA) NEW SPAR STIFFENER, (1EA) WEB CHANNEL (INBD) AND (1EA) WEB CHANNEL (OUTB) PREVIOUSLY
- [SDR IPXA2026020125876](https://openairdocs.org/sdr/IPXA2026020125876), Jan 22, 2026: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK IN CABIN AT STA 1066 LBL 47", 4-003 ATA 53 STR AUDITED<BR>CPCP AND SDR SUBMITTED
- [SDR IPXA2026020184023](https://openairdocs.org/sdr/IPXA2026020184023), Jan 20, 2026: BRACKET. CORRODED. RH HORZ STAB REAR SPAR BEHIND HORZ TIP FAIRING, BONDING WIRE ATTACHED BRACKET IS CORRODED (059-07) INSTALLED BONDING WIRE ATTACHED BRACKET P/N 183N1341-2 ON RH 
- [SDR IPXA2026021193646](https://openairdocs.org/sdr/IPXA2026021193646), Jan 20, 2026: ANGLE. CORRODED. STR- BROKEN NUT PLATE ON RH AFT WING TO BODY JUST ABOVE RAM AIR TURBINE MARKED JK200-25 ATA 53-40. INSTALLED 01 EA TEE CHORD LOWER BEAM P/N 149N7630-38 BATCH 00
- [SDR IPXA2024020886935](https://openairdocs.org/sdr/IPXA2024020886935), Feb 3, 2024: WEB. DAMAGED. MAJOR REPAIR* ADDITIONAL DAMAGE FOUND ON LWR DOOR FRAME WEB UPON REMOVAL OF WEB CUP REF (T3F18E003BPRL) C/W EO-89397 FOR FRAME REPAIR.
- [SDR IPXA2024020586935](https://openairdocs.org/sdr/IPXA2024020586935), Feb 3, 2024: CUP. DAMAGED. *SDR FILED OPEN* *MAJOR REPAIR* ADDITIONAL DAMAGE FOUND ON LWR DOOR FRAME WEB UPON REMOVAL OF WEB CUP REF (T3F18E003BPRL) PROVIDED EO-89397-PRELIM1 FOR ADDITION
- [SDR IPXA2024020913291](https://openairdocs.org/sdr/IPXA2024020913291), Jan 12, 2024: SKIN. GOUGED. LEFT FIXED WING UPPER STRUCTURE BETWEEN SLAT NR 2 & SLAT NR 3 IS GOUGED. FOUND THAT DAMAGE IS ACTUALLY ON PANEL 114N2105. DAMAGE WAS FROM TO LONG OF A SCREW INS
- [SDR IPXA2024011413291](https://openairdocs.org/sdr/IPXA2024011413291), Jan 12, 2024: SKIN. GOUGED. *SDR FILED OPEN* LEFT FIXED WING UPPER STRUCTURE BETWEEN SLAT NO.2 & SLAT NO.3 IS GOUGED REF PICS AND DIMENSIONS***SM39/LMX6*** FOUND THAT DAMAGE IS ACTUALLY ON
- [SDR IPXA2025022621372](https://openairdocs.org/sdr/IPXA2025022621372), Nov 16, 2023: PAN. DAMAGED. MAIN CARGO DOOR LOWER FRAME HAS STRUCTURE DAMAGE BETWEEN STATION 600-620. REPLACED DAMAGED SILL WEB PAN IAW SRM 51-40-02.
- [SDR IPXA2023111721372](https://openairdocs.org/sdr/IPXA2023111721372), Nov 16, 2023: UNKNOWN. UNKNOWN. *SDR FILED OPEN* MAIN CARGO DOOR LOWER FRAME HAS STRUCTURE DAMAGE BETWEEN STATION 600-620.***SM EVAL REQ*** DEFERRING MCD LOWER WEB DAMAGE PER EO-88738
- [SDR IPXA2023050393109](https://openairdocs.org/sdr/IPXA2023050393109), May 3, 2023: HARNESS. INOPERATIVE. INSPECTION TYPE:NA*SDR FILED OPEN* 1 ESCAPE HARNESS MOVED TO DEMO POS IN LAV CABINET. ESCAPE HARNESS DEFERRED IAW EO B757-2560-12312-E, & MEL 25-61-1-2. PLACARD
- [SDR IPXA2023050393108](https://openairdocs.org/sdr/IPXA2023050393108), May 3, 2023: HARNESS. CONTAMINATED. INSPECTION TYPE:NADEMO ESCAPE HARNESS CONTAMINATED W/ LAV FLUID.INSTALLED NEW HARNESS IAW EO B757-2560-12312-E.
- [SDR IPXA2023011689934](https://openairdocs.org/sdr/IPXA2023011689934), Jan 16, 2023: FLOOR PANEL. DAMAGED. MAJOR REPAIR, LEFT FWD FLOOR PANEL, MCD HAS WATER DAMAGE. MANUFACTURED A NEW PANEL IAW EO B757-5320-9692-K ON NRC 684243.
- [SDR IPXA2022120688750](https://openairdocs.org/sdr/IPXA2022120688750), Dec 6, 2022: INDICATOR. TRIPPED. EMERGENCY DECLARED, ATB, DURING CLIMBOUT TE FLAP DISAGREE EICAS DECLARED EMERGENCY ATB KRFD INTERROGATED FSEU 1. FOUND MESSAGE 305 TE FLAP DISAGREE IAW FIM 27-5
- [SDR IPXA2022031179971](https://openairdocs.org/sdr/IPXA2022031179971), Mar 10, 2022: NONE. NONE. INSPECTION TYPE:N/AEMERGENCY EXIT SIGN LIGHTS DIMREPLACED 8 LAMPS IN EMERGENCY EXIT LT ASSY AMM 33-51-01-201 CKS NORMAL
- [SDR IPXA2022022879511](https://openairdocs.org/sdr/IPXA2022022879511), Feb 27, 2022: NONE. NONE. INSPECTION TYPE:NA**EMERGENCY DECLARED** TE FLAP ASYM WHEN FLAPS WERE SELECTEDTO 20 DURING APPROACH. COMPLETED QRH CHECKLIST FOR TE FLAPS. ASYM AND LANDED WITH 
- [SDR IPXA2022022279316](https://openairdocs.org/sdr/IPXA2022022279316), Feb 6, 2022: STRINGER. NONE. INSPECTION TYPE:CLOWER AFT CARGO PIT SKIN AT FS 1459 STRINGER 29R HAS INTERGRANULAR CORROSION AND A .870" LONG CRACK ON THE I/B SIDE OF STRINGER WEB DEEMING STR
- [SDR IPXA2022021579021](https://openairdocs.org/sdr/IPXA2022021579021), Feb 6, 2022: CHANNEL. CRACKED. INSPECTION TYPE:CAFT PIT STA 1600 STR26R FRAME SUPPORT ANGLE HAS DENT AND POSSIBLE CRACK IN THE BOTTOMFOUND CHANNEL TO BE CRACKED REMOVED CRACKED CHANNEL INSTAL
- [SDR IPXA2022022279307](https://openairdocs.org/sdr/IPXA2022022279307), Feb 5, 2022: NONE. NONE. INSPECTION TYPE:CLH WING UPPER SKIN SURFACE AT WS 150-240 AFT SPAR BEAM PANEL IS BUBBLING UP DUE TO CORROSION. REMOVED CORROSION FOUND REAR SPAR UPPER CHOR OUT 
- [SDR IPXA2022021779121](https://openairdocs.org/sdr/IPXA2022021779121), Feb 5, 2022: FRAME. CORRODED. INSPECTION TYPE:CR/H SIDE WING TO BODY FRAME AT FS 1180 LOWER AREA HAS CORROSION. BLENDED OUT OF LIMITS PER SRM 53-00-71-1A-1REMOVED DEAMAGED SECTION AND SPLICE
- [SDR IPXA2022021779115](https://openairdocs.org/sdr/IPXA2022021779115), Feb 4, 2022: FRAME. CORRODED. INSPECTION TYPE:CL/H SIDE FWD WING TO BODY @ STA 900 SUPPORT FRAME HAS CORROSION. DEEMED OUT OF LIMITS PER SRM 53-00-71-1A-A DETAIL I NOTE D.REMOVED DAMAGED SEC
- [SDR IPXA2022022379339](https://openairdocs.org/sdr/IPXA2022022379339), Feb 2, 2022: NONE. NONE. INSPECTION TYPE:CLOWER AFT CARGO PIT BELLY SKIN AT FS 1459 STINGER 30 BL 0 WAS CORRODED 1.5" FROM EDGE REMOVED CORROSION REMAINING MATERIAL .067" FOUND TO BE OU
- [SDR IPXA2022022379335](https://openairdocs.org/sdr/IPXA2022022379335), Feb 1, 2022: NONE. DENTED. INSPECTION TYPE:C#2 AFT CARGO DOOR AFT LOWER SKIN IS DENTED 1.00" WIDE BY 1.50" LONG BY .850" DEEPREPAIRED #2 AFT CARGO PER SRM 52-30-01-2R-1 REPAIR 1
- [SDR IPXA2022022079194](https://openairdocs.org/sdr/IPXA2022022079194), Feb 1, 2022: NONE. NONE. INSPECTION TYPE:CRH ENGINE I/B COWL THRUST REVERSER FAN DUCT INNER SKIN TRAILING EDGE IS DISBONDEDREPARIED INNER SKIN PER SREO B757-7830-59393-A
- [SDR IPXA2021090573584](https://openairdocs.org/sdr/IPXA2021090573584), Sep 5, 2021: POWER SUPPLY. NO TEST. INSPECTION TYPE:N/AEMERG EXIT INOP L1 DOOR. R&R POWER SUPPLY, OPS CK GOOD AT THIS TIME AMM 33-51-07
- [SDR IPXA2021081872880](https://openairdocs.org/sdr/IPXA2021081872880), Aug 16, 2021: A/C PACK. ODOR. INSPECTION TYPE:N/AUPON ARRIVING AIRCRAFT, VERY STRONG ODOR COMING FROM PACKS WITH EITHER OR BOTH PACKS SELECTED ON. ALMOST UNBEARABLE WITHOUT ENTRY DOOR OPEN.R
- [SDR IPXA2021021965850](https://openairdocs.org/sdr/IPXA2021021965850), Feb 18, 2021: WARNING MESSAGE. FALSE ACTIVATION. INSPECTION TYPE: NAON TAKEOFF ROTATION, THE L FWD ENT DOOR EICAS MSG CAME ON FOR 3 SECONDS THEN WENT OFF. PERFORMED ENTRY DOOR CK LIST IN QRH. PRESS WAS OK AND 
- [SDR IPXA2021010564145](https://openairdocs.org/sdr/IPXA2021010564145), Jan 4, 2021: BATTERY PACK. INOPERATIVE. INSPECTION TYPE: NA EMERGENCY FLIGHT DECK WILL NOT COME ON. R & R BATTERY PACK, PER AMM 33-51-01. OPERATIONS CHECK GOOD IPC 33-51-11-01 #45S.
- [SDR IPXA2020081959247](https://openairdocs.org/sdr/IPXA2020081959247), Aug 17, 2020: OIL FILTER. WARNING MESSAGE. DIVERTED, EMERGENCY DECLARED, AND LANDED WITHOUT INCIDENT, RIGHT OIL FILTER EICAS RAN CHECKLIST. EICAS REMAINED ILLUMINATED. SHUTDOWN RT. ENGINE PER CHECKLIST.R
- [SDR IPXA2020080768698](https://openairdocs.org/sdr/IPXA2020080768698), Aug 5, 2020: OIL FILTER. WARNING MESSAGE. DIVERTED, EMERGENCY DECLARED, RIGHT ENG OIL FILTER EICAS. RAN QRH SHUTDOWN ENGINE. ACCOMPLISHED ALERT INSPECTION IAW POWER PLANT ENGINEERING IAW MM 79-21-05, AN
- [SDR IPXA2020041054100](https://openairdocs.org/sdr/IPXA2020041054100), Apr 9, 2020: FIRE BOTTLE. DISCHARGED. INSPECTION TYPE:N/A**SUPPLEMENTAL SDR** DIVERTED ** EMERGENCY DECLARED ** APU FIRE BOTTLE HAS BEEN DISCHARGED. NO EVIDENCE OF FIRE IN APU BAY OR TAILPIPE. DEFER
- [SDR IPXA2020030452750](https://openairdocs.org/sdr/IPXA2020030452750), Mar 3, 2020: SEAT TRACK. CORRODED. INSPECTION TYPE:SEG3MAIN CARGO AFT SEAT TRACK STA 1681 HAS CORROSIONREPAIRED IAW SRM 53-00-52-2R-7
- [SDR IPXA2020030352704](https://openairdocs.org/sdr/IPXA2020030352704), Mar 2, 2020: SLAT. DELAMINATED. INSPECTION TYPE:SEG3ROBBED NO 8 SLAT FROM A/C N410UP HAS DELAMINATION REQUIRES REPAIRREPAIRED IAW SRM B757-51-70-10-2R-4
- [SDR IPXA2020030252617](https://openairdocs.org/sdr/IPXA2020030252617), Feb 29, 2020: SLAT. DELAMINATED. INSPECTION TYPE:SEG#3 SLAT HAS 1EA DELAMINATION DENT REQUIRING REPAIRREPAIR PER SRM B757-51-70-10-2R-2 AND 57-43-02-2R-1
- [SDR IPXA2020030252592](https://openairdocs.org/sdr/IPXA2020030252592), Feb 28, 2020: FLOOR PANEL. DAMAGED. INSPECTION TYPE:SEGMAIN CARGO COMPARTMENT, FLOOR PANEL 251XMF DAMAGEDFABBED PANEL 251XMF FROM 5024N400001SS-G, BATCH# 3489461 PER SREO B757-5320-9692-K
- [SDR IPXA2020010650679](https://openairdocs.org/sdr/IPXA2020010650679), Jan 4, 2020: UNKNOWN. ODOR. INSPECTION TYPE:N/ASTRONG OILY SMELL WHEN LEFT PACK IS ONC/W AMM TASK 21-00-01-002-001 NO OIL CONTAMINATION SMELL AT THIS TIME
- [SDR IPXA2019060762901](https://openairdocs.org/sdr/IPXA2019060762901), Jun 5, 2019: WARNING MESSAGE. ILLUMINATED. EMERGENCY DECLARED - TRAILING EDGE DISAGREETRAILING EDGE FLAP OPERATION CHECK AND (GVI) VISIUAL INSP C/O NO DAMAGE FOUND, LH/RH FSEU FLAP/SLAT ELECT UNIT BITE T
- [SDR IPXA2019051442121](https://openairdocs.org/sdr/IPXA2019051442121), May 13, 2019: PCA. MALFUNCTIONED. INSPECTION TYPE:SDR DIVERSION - SPOILERS EICAS AFTER REACHING CRUISE. TRANSFERRED TO M669906 IAW MEL 27-61-1-2, DMP C/W AND PLACARD INSTALLED. FOUND PCA FAULT O
- [SDR IPXA2019012338210](https://openairdocs.org/sdr/IPXA2019012338210), Jan 22, 2019: LIGHT. MISSING. INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT MISSING 1 BULB. RELAMPED PER AMM 33 51 01 CHECKS GOOD.
- [SDR IPXA2018010825230](https://openairdocs.org/sdr/IPXA2018010825230), Jan 6, 2018: IDG. INOPERATIVE. EICAS MESSAGE FOR THE LT GENERATOR OFF, GEN OFF LIGHT ON LT BUSS, OFF LIGHT ON LT BUS ISOLATION LIGHT ON GEN RESET DID NOT CORRECT THE PROBLEM. DIVERTED, EMERGE
- [SDR IPXA2017071419283](https://openairdocs.org/sdr/IPXA2017071419283), Jul 13, 2017: BULB. INOPERATIVE. EMERGENCY LIGHT HAS THREE INOPERATIVE BULBS. INSTALLED NEW BULBS IAW AMM 33-51-01-2
- [SDR IPXA2016031400710](https://openairdocs.org/sdr/IPXA2016031400710), Mar 1, 2016: FRAME. GOUGED. INSPECTION TYPE:C17, FWD CARGO DOOR AFT FRAME GOUGED AT LOWER END. REPAIRED IAW REO-G19684 AND EO B757-5230-60192-A.
- [SDR IPXA2016031200657](https://openairdocs.org/sdr/IPXA2016031200657), Feb 27, 2016: SKIN. DELAMINATED. INSPECTION TYPE:C-17, RT WING NR 10 SLAT, UPPER SURFACE HAS DENT THAT WAS FOUND TO BE DELAMINATED. REMOVED DAMAGE ON UPPER SURFACE OF THE NR 10 SLAT THAT IS LOC
- [SDR IPXA2016031400709](https://openairdocs.org/sdr/IPXA2016031400709), Feb 24, 2016: SUPPORT. CORRODED. INSPECTION TYPE:C17, AFT CARGO PANEL CEILING SUPPORT STRUCTURE IS CORRODED. RT BS 1400, RT BS 1420 STREAMER ATTACHED REPAIRED IAW REO-G19681, REV A AND EO B757-
- [SDR IPXA2016031400736](https://openairdocs.org/sdr/IPXA2016031400736), Feb 24, 2016: NUT PLATE. CORRODED. INSPECTION TYPE:SERVICE, AFT CARGO BS 1720, RT OVERHEAD SUPPORT BRACKET CORRODED NEXT TO RT DRAIN LINE. R & R CORRODED NUTPLATE ASSY IAW SRM 51-40-02.
- [SDR IPXA2016031400734](https://openairdocs.org/sdr/IPXA2016031400734), Feb 24, 2016: NUT PLATE. CORRODED. INSPECTION TYPE:SERVICE, AFT CARGO BS 1720 RT OVERHEAD SUPPORT BRACKET CORRODED INBD OF RT DRAIN LINE. R & R CORRODED NUTPLATE ASSY IAW SRM 51-40-02.
- [SDR IPXA2016031400733](https://openairdocs.org/sdr/IPXA2016031400733), Feb 24, 2016: SKIN. DENTED. INSPECTION TYPE: C-17, RT WING NR 7 SLAT LOWER SURFACE HAS A DENT AT INBD END. REPAIRED THE SLAT IAW REO-G19670, REV A AND SRM 51-70-10.
- [SDR IPXA2016031400730](https://openairdocs.org/sdr/IPXA2016031400730), Feb 24, 2016: SKIN. DENTED. INSPECTION TYPE:C-17, RT WING NR 7 SLAT UPPER SURFACE HAS A DENT FOUND TO BE DELAMINATED. REPAIRED SLAT WITH METAL BOND REPAIR IAW REO G19670, REV A AND SRM 51-
- [SDR IPXA2016031400729](https://openairdocs.org/sdr/IPXA2016031400729), Feb 24, 2016: SKIN. DENTED. INSPECTION TYPE:C-17, RT WING NR 7 SLAT UPPER SURFACE HAS DENT FOUND TO BE DELAMINATED REPAIRED SLAT WITH METAL BOND REPAIR IAW REO-G19670, REV A AND SRM 51-70-
- [SDR IPXA2016030300300](https://openairdocs.org/sdr/IPXA2016030300300), Feb 24, 2016: NUT PLATE. CORRODED. INSPECTION TYPE:SV, AFT CARGO BS 1720, RT OVERHEAD SUPPORT BRACKET CORRODED NEXT TO RT DRAIN LINE R & R CORRODED NUTPLATE ASSY IAW SRM 51-40-02.

All 254: https://openairdocs.org/aircraft/N408UP/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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