# N406UP: 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: 23728
- Year built: 1988
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 2, 1988
- Certificate issued: June 3, 1999
- Expires: August 31, 2027
- Mode S code: A4C4BB
- 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=406UP
- Page: https://openairdocs.org/aircraft/N406UP

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 N406UP.

## FAA accident and incident reports

None matched to N406UP.

## Service difficulty reports (285, 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 IPXA2026081930589](https://openairdocs.org/sdr/IPXA2026081930589), Aug 18, 2026: FLAP SYSTEM. WARNING MESSAGE. EMD ON CLIMB OUT AT APPROX 3K' WE GOT A LE SLAT DISAGREE EICAS. MAINTAINED 230 KT OR LESS FOR ENTIRE FLIGHT. AFTER QRH PROCEDURE, MSG WENT OUT. PERFORMED BITE P
- [SDR IPXA2026042809227](https://openairdocs.org/sdr/IPXA2026042809227), Apr 27, 2026: LIGHT. INOPERATIVE. EMERGENCY LIGHT INOP FOUND THE EMERGENCY LIGHT WERE ON FOR MORE THAN 10 MINS. WHICH REQUIRES 16 HOURS OF CHARGING. R&R EMERGENCY BATTERY PACK REF. AMM. 33-51-07
- [SDR IPXA2025092269443](https://openairdocs.org/sdr/IPXA2025092269443), Sep 21, 2025: VALVE. FAULTED. ATB, CLIMB OUT PASSING 24000€™ L OIL TEMP WAS IN THE AMBER RANGE (165°) QRH COMPLETED ACCOMPLISHED AIR TURNBACK. REMOVED AND REPLACED L/H ENG AIR/OIL HEAT EXC
- [SDR IPXA2025091564404](https://openairdocs.org/sdr/IPXA2025091564404), Aug 20, 2025: TAIL CONE. DAMAGED. MAJOR REPAIR, DAMAGE ON TOP OF TAILCONE AREA BELOW RUDDER ALL STEPS OF EO-94785-REQ2 COMPLETED. THIS DEFERRAL IS NOW CLOSED.
- [SDR IPXA2025011359796](https://openairdocs.org/sdr/IPXA2025011359796), Jan 7, 2025: ANGLE. FAULTED. FAULT: REFERANCE FRAME REPAIR T3F18E005ERCC, CORRECTIVE ACTION 6 & 7 SURFACE HFEC PERFORMED ON CUTOUT ON FRAME 1500 IN AFT PIT REQUIRES RII AUTHERIZATION. ACCOM
- [SDR IPXA2025011349181](https://openairdocs.org/sdr/IPXA2025011349181), Jan 6, 2025: FRAME. DAMAGED. FAULT: Z100 STR OPEN UP FLOOR PANELS, MBA SYSTEM, SIDEWALLS, AND TRANSITION PANEL TO F.O.M FS 1500 FRAME REPAIR AT STR 26R. INSTALLED SIDEWALL PANELS 162BW, 154
- [SDR IPXA2025010522565](https://openairdocs.org/sdr/IPXA2025010522565), Jan 4, 2025: FRAME. NOT REPORTED. *SDR FILED OPEN* REF FRAME REPAIR T3F18E005ERBT, CORRECTIVE ACTION 7. - SURFACE HFEC PERFORMED ON CUTOUT ON FRAME 1460 RH SIDE IN AFT PIT REQUIRES RII AUTHORIZA
- [SDR IPXA2024112840807](https://openairdocs.org/sdr/IPXA2024112840807), Nov 7, 2024: TEE ANGLE. CORRODED. STA 1680 HAS CORROSION ON UPPER AND LOWER SURFACE OF UPPER T-CHORD
- [SDR IPXA2024120260414](https://openairdocs.org/sdr/IPXA2024120260414), Oct 30, 2024: TEE ANGLE. DAMAGED. WTB LOWER STRUCTURE, T-CHORD STA 1142, LBL 60 WITH CORROSION. INSTALLED T CHORD AT STA 1142, LBL 60 IAW SRM 51-40-02. REVIEWED
- [SDR IPXA2024120232048](https://openairdocs.org/sdr/IPXA2024120232048), Oct 29, 2024: SEAT TRACK. CORRODED. MAIN DECK FLOOR SUPPORT STRUCTURE, STA 1195 RBL 24 SEAT TRACK CORRODED. DOT 28-100 REVIEWED
- [SDR IPXA2024103131000](https://openairdocs.org/sdr/IPXA2024103131000), Oct 29, 2024: FLOOR PANEL. BROKEN. FLOOR PANEL 252XBF BROKEN STA 1200. FABRICATED FLOOR PANEL 252XBF USING MATERIAL P/N:5024N400001SS-G BATCH#:0000096292 I.A.W. SREO-B757-5320-9692-K.
- [SDR IPXA2024120240326](https://openairdocs.org/sdr/IPXA2024120240326), Oct 24, 2024: SKIN. DELAMINATED. LEFT INBOARD FLAP UPPER OUTBOARD SURFACE IS DELAMINATED IN TWO AREAS. DOT AA014. REVIEWED
- [SDR IPXA2025010310527](https://openairdocs.org/sdr/IPXA2025010310527), Oct 23, 2024: FLOORBEAM. CORRODED. FAULT-STR-100-AGING ACFT INSP.- FLOOR BEAM AT STA 1200, FORWARD SIDE, HAS EXFLOIATION CORROSIN AROUND NUT PLATE.. DOT AA10. ACCOMPLISHED REPAIR PER VT-MAE EA 75
- [SDR IPXA2024112010471](https://openairdocs.org/sdr/IPXA2024112010471), Oct 23, 2024: FRAME. DENTED. FRAME 1500 RIGHT SIDE IN AFT PIT IS DENTED. DOT AA007. REQUIRED SUPPLEMENTAL INSPECTIONS DEFERRED IAW B757-200PF, REV 121, 53-00-07-2R-5, TABLE #3 FOR ZONE #1.
- [SDR IPXA2024112510405](https://openairdocs.org/sdr/IPXA2024112510405), Oct 23, 2024: FRAME. DENTED. FRAME 1460 RIGHT SIDE BETWEEN S-25R AND S-27R, IN AFT PIT IS DENTED. DOT AA006. CORRECTION TO LAST STATEMENT REPAIR PER DETAIL #1
- [SDR IPXA2024120286460](https://openairdocs.org/sdr/IPXA2024120286460), Oct 22, 2024: SKIN. DELAMINATED. LEFT MLG STRUT MOUNTED DOOR LOWER AFT TRAILING EDGE IS DELAMINATED. DOT AA002. REVIEWED
- [SDR IPXA2024062459694](https://openairdocs.org/sdr/IPXA2024062459694), Jun 21, 2024: UNKNOWN. MISSING. FO'S EVAS TEST TOOL MISSING. INSTALLED FO'S EVAS TEST TOOL AS REQUIRED
- [SDR IPXA2024050811638](https://openairdocs.org/sdr/IPXA2024050811638), May 4, 2024: LANDING GEAR. WARNING MESSAGE. GEAR DISAGREE EICAS MESSAGE WHEN GEAR LOWERED ON APPROACH. ACCOMPANIED BY LDG GEAR MONITOR STATUS MESSAGE. QRH PROCEDURE RAN IN ENTIRETY FOUND LEFT SYSTEM RETUR
- [SDR IPXA2024050611638](https://openairdocs.org/sdr/IPXA2024050611638), May 4, 2024: WARNING MESSAGE. FALSE ACTIVATION. **SDR FILED OPEN** GEAR DISAGREE EICAS MESSAGE WHEN GEAR LOWERED ON APPROACH. ACCOMPANIED BY LDG GEAR MONITOR STATUS MESSAGE. QRH PROCEDURE RAN IN ENTIRETY VERI
- [SDR IPXA2023022191199](https://openairdocs.org/sdr/IPXA2023022191199), Feb 21, 2023: DOOR. WARNING MESSAGE. INSPECTION TYPE:N/AON LANDING WE RECIEVED A LEFT FORWARD ENTRY DOOR MESSAGEINSPECTED CREW ENTRY DOOR INDICATION PROXIMITY SWITCH AND FOUND LOWER PORTION OF SHIM
- [SDR IPXA2022102487481](https://openairdocs.org/sdr/IPXA2022102487481), Oct 24, 2022: BATTERY PACK. INOPERATIVE. FLT DECK INTERIOR EMERGENCY LIGHTS OVER ENTRY DOOR INOP. R & R EMERGENCY EXIT LIGHT BATTERY ENTRY DOOR. OPS CK GOOD IAW AMM 33-51-01-012-002, 33-51-01-402-003. 
- [SDR IPXA2022101587153](https://openairdocs.org/sdr/IPXA2022101587153), Oct 15, 2022: FRAME. DENTED. INSPECTION TYPE:SEG1LOWER AFT CARGO PIT FS FRAME 1360 STRINGER 26L NEEDS AN ALTERNATIVE METHOD TO INSPECT EXISTNG REPAIR PER EO# B757-5310-73926-A APPENDIX A ST
- [SDR IPXA2022101487137](https://openairdocs.org/sdr/IPXA2022101487137), Oct 14, 2022: SKIN. DENTED. INSPECTION TYPE:SEG1FUSELAGE SKIN AT STA 434 BETWEEN S23L AND 25L HAS 2 DENTS DENT 1 IS L-1.0" W=1.030" DEPTH=.046" AND DENT 2 L=.632" W=.621" AND DEPTH=.048" M
- [SDR IPXA2022100886960](https://openairdocs.org/sdr/IPXA2022100886960), Oct 8, 2022: FRAME. DENTED. INSPECTION TYPE:SEG1LOWER AFT CARGO PIT FS FRAME 1560 BETWEEN STRINGERS S25R AND S26R HAS TWO DENTS ON THE UPPER FLANGE OF FRAME 1560 NO DENTS ARE ALLOWED PER S
- [SDR IPXA2022100886958](https://openairdocs.org/sdr/IPXA2022100886958), Oct 8, 2022: FRAME. DENTED. INSPECTION TYPE:SEG1LOWER AFT CARGO PIT FS FRAME 1480 AT STRINGERS 26R THERE ARE TWO DENTS ON THE UPPER FLANGE OF FRAME NO DENTS ARE PERMITTED PER SRM 53-00-07-
- [SDR IPXA2022100886957](https://openairdocs.org/sdr/IPXA2022100886957), Oct 8, 2022: FRAME. DENTED. INSPECTION TYPE:SEG1LOWER AFT CARGO PIT FS FRAME 1520 BETWEEN STRINGERS 23R AND 26R THERE ARE TWO DENTS ON THE UPPER FLANGE OF FRAME NO DENTS ARE PERMITTED PER 
- [SDR IPXA2022100886956](https://openairdocs.org/sdr/IPXA2022100886956), Oct 8, 2022: FRAME. DENTED. INSPECTION TYPE:SEG1INCOMING REPAIR ACCOMPLISHED ON FS 1300 BETWEEN STRINGERS S23L AND S26L WAS DONE PER SRM 51-70-11. CUSTOMER REQUEST TO REMOVE REPAIR AND INS
- [SDR IPXA2022100886955](https://openairdocs.org/sdr/IPXA2022100886955), Oct 8, 2022: FRAME. DENTED. INSPECTION TYPE:SEG1LOWER AFT CARGO PIT FS FRAME 1460 BETWEEN STRINGERS S25L AND S26L THERE IS A .420" LONG BY .032" DEEP DENT ON THE UPPER FLANGE NO DENTS ARE 
- [SDR IPXA2022100886954](https://openairdocs.org/sdr/IPXA2022100886954), Oct 8, 2022: FRAME. DENTED. INSPECTION TYPE:SEG1LOWER AFT CARGO PIT FS FRAME 1540 1.2" O/B OF STRINGER S26R HAS A .70" LONG BY .45" WIDE BY .50" DEEP GOUGE ON THE UPPER PART OF WEB INTO TH
- [SDR IPXA2022090485888](https://openairdocs.org/sdr/IPXA2022090485888), Sep 4, 2022: SKIN. PUNCTURED. INSPECTION TYPE:N/ARIGHT ELEVATOR LOWER SKIN PUNCTUREDREPAIRED DAMAGED SKIN IAW EO B757-5520-84504-A
- [SDR IPXA2022051181990](https://openairdocs.org/sdr/IPXA2022051181990), May 11, 2022: NONE. BROKEN. INSPECTION TYPE:N/AEMERGENCY LIGHT SWITCH GUARD IS BROKENREPLACED SWITCH GROUND. OPS TEST GOOD IAW AMM CH 33-51-08
- [SDR IPXA2021060470179](https://openairdocs.org/sdr/IPXA2021060470179), Jun 4, 2021: RADOME. DAMAGED. EMERG DECLARED-NO EQUIP USED - LANDING UNEVENTFUL. DURING DESCENT THROUGH APPROX 15000 FT LOUD NOISE AND MULTIPLE EICAS MSG DISPLAYED DUE TO RADOME DAMAGE IAS D
- [SDR IPXA2021021265622](https://openairdocs.org/sdr/IPXA2021021265622), Feb 12, 2021: STRINGER. CORRODED. INSPECTION TYPE:SEG4AFT CARGO STRINGER 30 STA 1200 HAS CORROSIONREPAIRED IAW 53-00-03-2R-1 REMOVED DAMAGED SECTION SPLICED IN NEW SECTION
- [SDR IPXA2021020365305](https://openairdocs.org/sdr/IPXA2021020365305), Feb 3, 2021: FLOOR PANEL. DAMAGED. INSPECTION TYPE:SEG4MAIN CARGO COMPARTMENT FLOOR PANEL 242XCF DAMAGEDFABBED PANEL 242XCF FROM 5024N400001SS-G BATCH#3546253 PER SREO B757-5320-9692-K
- [SDR IPXA2021020365304](https://openairdocs.org/sdr/IPXA2021020365304), Feb 3, 2021: FLOOR PANEL. DAMAGED. INSPECTION TYPE:SEG4MAIN CARGO COMPARTMENT, FLOOR PANEL 242XDF DAMAGEDFABBED PANEL 242XDF FROM 5024M400001SS-G BATCH#3546253 PER SREO B757-5320-9692-K
- [SDR IPXA2021020365302](https://openairdocs.org/sdr/IPXA2021020365302), Feb 3, 2021: FLOOR PANEL. DAMAGED. INSPECTION TYPE:SEG4MAIN CARGO COMPARTMENT FLOOR PANEL 242XGF DAMAGEDFABBED PANEL 242XGF FROM 5024N400001SS-G BATCH#3546253 PER SREO B757-5320-9692-K
- [SDR IPXA2020020551852](https://openairdocs.org/sdr/IPXA2020020551852), Feb 5, 2020: FRAME. BENT. INSPECTION TYPE:SPVCHORD ON RIGHT SIDE PRESSURE BULKHEAD HAS SLIGHT BENT AT STA200 RBL37 WL200REMOVED DAMAGED AREA AND INSTALLED NEW SECTION AND REPAIRED SPLICE
- [SDR IPXA2020020551851](https://openairdocs.org/sdr/IPXA2020020551851), Feb 5, 2020: BULKHEAD WEB. DENTED. INSPECTION TYPE:SPVFWD PRESSURE BULKHEAD WEB PART #141N2800-164 DENTED BLKHD STA199 RBL30 WL200REMOVED DAMAGE, INSTALLED FILLER AND REPAIR DOUBLER
- [SDR IPXA2019041941214](https://openairdocs.org/sdr/IPXA2019041941214), Apr 19, 2019: GUARD. BROKEN. EMERGENCY LIGHT GUARD HAD A BLACK PIECE BREAK OFF. R&R THE SWITCH GUARD IAW SWPM 20-83-11, OPS CHECKED GOOD.
- [SDR IPXA2019041214957](https://openairdocs.org/sdr/IPXA2019041214957), Apr 10, 2019: SHUTOFF VALVE. FAILED. DIVERSION - L ENG BLEED OFF ILLUMINATED AFTER EAI WAS SELECTED ON DURING FLIGHT AT CRUISE FL 300. L ENG WAS FOLLOWED BY R ENG. L AND R PACK OFF. ACCOMPLISHED CH
- [SDR IPXA2019022539412](https://openairdocs.org/sdr/IPXA2019022539412), Feb 25, 2019: SKIN. DENTED. INSPECTION TYPE:C1, DENT STA 520 S-22L DOT18-13FOUND TO BE OUT OF LIMITS DUE TO LOCATION, DENT MUST BE MORE THAN 0.5" REPAIRED PER EA #B757-5330-27-A2331
- [SDR IPXA2019022099223](https://openairdocs.org/sdr/IPXA2019022099223), Feb 19, 2019: FLOOR PANEL. DELAMINATED. INSPECTION TYPE:C1MCD FLOOR PNL 252 XTF DELAMINATEDFABBED PNL 252 XTF FROM 5024N400001SS-G, BATCH # 0003384848 PER SREO B757-5320-9692-K
- [SDR IPXA2019022099210](https://openairdocs.org/sdr/IPXA2019022099210), Feb 19, 2019: FLOOR PANEL. DELAMINATED. INSPECTION TYPE:C1MCD FLOOR PANEL 231XFJ DELAMINATEDFABRICATED NEW FLOOR PANEL 231XJF FROM 5024N400001SS-G, BATCH #3350636 PER SREO B757-5320-9692-K
- [SDR IPXA2019022099209](https://openairdocs.org/sdr/IPXA2019022099209), Feb 19, 2019: FLOOR PANEL. DELAMINATED. INSPECTION TYPE:C1MCD FLOOR PNL 232 XJF DELAMINATEDFABRICATED NEW PNL 232XJF FROM 502N400001SS-G BATCH#0002379150 & 0003418355
- [SDR IPXA2019022099208](https://openairdocs.org/sdr/IPXA2019022099208), Feb 19, 2019: FLOOR PANEL. DELAMINATED. INSPECTION TYPE:C1MCD FLOOR PNL 221XBF DELAMINATEDFABRICATED NEW PNL FROM 5024N400001SS-G, BATCH#33550626 PER SREO B757-5320-9692 K
- [SDR IPXA2019022099207](https://openairdocs.org/sdr/IPXA2019022099207), Feb 19, 2019: FLOOR PANEL. DELAMINATED. INSPECTION TYPE:C1MCD FLOOR PANEL 231XFF DELAMINATEDFABRICATED NEW FLOOR PANEL 231XFF FROM 5024N400001SS-G BATCH# 3350636 PER SREO B757-5320-9692-K
- [SDR IPXA2019021839166](https://openairdocs.org/sdr/IPXA2019021839166), Feb 18, 2019: FLOOR PANEL. DAMAGED. INSPECTION TYPE:C1, PANEL 232XCF REQUIRES FAB. FABBED PANEL 232XCF FROM 5024N40000-G BATCH# 33550636 AND STEP CUT PER SREO B757-5320-9692-K.
- [SDR IPXA2019021839164](https://openairdocs.org/sdr/IPXA2019021839164), Feb 18, 2019: FLOOR PANEL. DAMAGED. INSPECTION TYPE:C1, PANEL 252XSF REQUIRES FAB. FABBED PANEL 252XSF FROM 5024N40000-G BATCH 33550636 PER SREO B757-5320-9692-K
- [SDR IPXA2019021839163](https://openairdocs.org/sdr/IPXA2019021839163), Feb 18, 2019: FLOOR PANEL. DAMAGED. INSPECTION TYPE:C1, PANEL 231XCF REQUIRES FAB. FABBED PANEL 231XCF FROM 5024N40000-G BATCH 33550636 AND STEP CUT PER SREO B757-5320-9692-K
- [SDR IPXA2019021839162](https://openairdocs.org/sdr/IPXA2019021839162), Feb 18, 2019: FLOOR PANEL. DAMAGED. INSPECTION TYPE:C1, MAIN CABIN FLOOR PANEL 211XAF REQUIRES FAB. FABBED PANEL 211XAF FROM 5024N40000-SS-G BATCH 33550636 PER SREO B757-5320-9692-K.

All 285: https://openairdocs.org/aircraft/N406UP/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

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.