# N753CX: 1992 Boeing 757-2Y0

- Status: Valid registration
- Airframe: [Boeing 757-2Y0](https://openairdocs.org/model/boeing-757-2y0) (registry code 138492A, 178 seats)
- Engine: [Rolls-Royce RB211-535E4 series](https://openairdocs.org/engine/rolls-royce-rb211-535e4-series) (registry code 54223)
- Data sheets: [TCDS E12EU](https://openairdocs.org/tcds/E12EU) (Rolls-Royce Deutschland Ltd & Co KG) (OpenAirDocs)
- Serial number: 26152
- Year built: 1992
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 7, 2013
- Certificate issued: January 31, 2013
- Expires: January 31, 2029
- Mode S code: AA2576
- Registered owner: [Cargo Aircraft Management Inc](https://openairdocs.org/faa-owner/CARGO%20AIRCRAFT%20MANAGEMENT%20INC)
- Location: [Wilmington, OH](https://openairdocs.org/faa-place/OH/Wilmington)
- Owner type: Corporation
- Owner's area on the map: 39.4607° N, 83.8443° W: Placed by OpenAirDocs at the center of ZIP code 45177, within about 7 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=753CX
- Page: https://openairdocs.org/aircraft/N753CX

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. The registry lists only the engine series, so ADs for every Rolls-Royce RB211-535E4 model are included.

## ADs that may apply (OpenAirDocs): 20 in force

### Matched by airframe (Boeing 757-2Y0)

None in force.

### Matched by engine (Rolls-Royce RB211-535E4 series)

- [AD 2024-10-06](https://openairdocs.org/ad/2024-10-06): Engine (Turbine/Turboprop) · Rolls-Royce Deutschland RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-C-37. Effective Jun 27, 2024
- [AD 2020-08-03](https://openairdocs.org/ad/2020-08-03): Turbine Engine Compressor Section · Rolls-Royce Deutschland RB211-535E4-37, RB211-535E4-B-37, RB211-535E4-B-75 and 1 more. Effective May 18, 2020
- [AD 2017-24-08](https://openairdocs.org/ad/2017-24-08): Fuel control/Turbine engines · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-C-37. Effective Jan 16, 2018
- [AD 2016-03-04](https://openairdocs.org/ad/2016-03-04): Life-limited rotating parts · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-C-37. Effective Mar 15, 2016
- [AD 2013-23-17](https://openairdocs.org/ad/2013-23-17): High-pressure (HP) and intermediate-pressure (IP) turbine discs · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37, RB211-535E4-C-37 and 3 more. Effective Dec 11, 2013
- [AD 2013-16-23](https://openairdocs.org/ad/2013-16-23): Cracked and distorted FCL metering panel · Rolls-Royce RB211-524B-02, RB211-524B2-19, RB211-524B3-02 and 13 more. Effective Oct 8, 2013
- [AD 2012-25-09](https://openairdocs.org/ad/2012-25-09): Intermediate-pressure (IP) turbine discs · Rolls-Royce RB211-524G2-19, RB211-524G2-T-19, RB211-524G3-19 and 10 more. Effective Feb 6, 2013
- [AD 2012-02-11](https://openairdocs.org/ad/2012-02-11): LP turbine stage 1, 2, and 3 discs · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37, RB211-535E4-B-75 and 1 more. Effective Mar 6, 2012
- [AD 2009-20-14](https://openairdocs.org/ad/2009-20-14): Eddy current inspection (ECI) · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Nov 17, 2009
- [AD 2008-20-04](https://openairdocs.org/ad/2008-20-04): HP turbine discs · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 26 more. Effective Nov 3, 2008
- [AD 2006-11-05 R2](https://openairdocs.org/ad/2006-11-05-R2): High pressure compressor (HPC) · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 27 more. Effective Feb 21, 2008
- [AD 2007-14-07](https://openairdocs.org/ad/2007-14-07): Fluorescent penetrant inspections (FPI) · Rolls-Royce RB211-524B-02, RB211-524B-B-02, RB211-524B2-19 and 21 more. Effective Aug 16, 2007
- [AD 2006-17-12](https://openairdocs.org/ad/2006-17-12): High pressure (HP) turbine discs · Rolls-Royce RB211-22B-02, RB211-535C-37, RB211-535E4-37 and 3 more. Effective Sep 27, 2006
- [AD 2004-19-04](https://openairdocs.org/ad/2004-19-04): Critical Life-Limited Rotating Engine Parts · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 27 more. Effective Nov 1, 2004
- [AD 2004-01-21](https://openairdocs.org/ad/2004-01-21): Frount engine mount housing · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 27 more. Effective Feb 27, 2004
- [AD 2003-10-03 R1](https://openairdocs.org/ad/2003-10-03-R1): High pressure (HP) turbine discs · Rolls-Royce RB211-535E4-B-37 and RB211-535E4-B-75. Effective Jun 20, 2003
- [AD 2001-19-05](https://openairdocs.org/ad/2001-19-05): High Speed Gearbox Drive · Rolls-Royce RB211-535C-37, RB211-535E4-37, RB211-535E4-B-37 and 1 more. Effective Oct 11, 2001
- [AD 2000-09-14](https://openairdocs.org/ad/2000-09-14): Radial Drive Steady Bearings · Rolls-Royce RB211-535C-37, RB211-535E4-37, RB211-535E4-B-37 and 1 more. Effective Jul 11, 2000
- [AD 97-02-12](https://openairdocs.org/ad/97-02-12): Fuel Flow Governor (FFG) · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Apr 4, 1997
- [AD 87-25-04](https://openairdocs.org/ad/87-25-04): Fuel Quantity Indication System · Rolls-Royce RB211-535C-37, RB211-535E4-37, RB211-535E4-B-37 and 1 more. Effective Dec 8, 1987

### Historical (superseded or no longer in force)

- [AD 2015-17-21](https://openairdocs.org/ad/2015-17-21) (historical): High-pressure turbine (HPT) disks · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-C-37. Effective Dec 2, 2015
- [AD 2014-24-08](https://openairdocs.org/ad/2014-24-08) (historical): Fuel leaks · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-C-37. Effective Jan 6, 2015
- [AD 2013-19-18](https://openairdocs.org/ad/2013-19-18) (historical): LPT stage 2 disc failure · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37, RB211-535E4-B-75 and 1 more. Effective Nov 7, 2013
- [AD 2013-19-17](https://openairdocs.org/ad/2013-19-17) (historical): Failure of rotating life limited parts · Rolls-Royce RB211-535E4-B-37. Effective Nov 7, 2013
- [AD 2011-11-08](https://openairdocs.org/ad/2011-11-08) (historical): LP Turbine discs · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37, RB211-535E4-B-75 and 1 more. Effective Jun 30, 2011
- [AD 2008-22-24](https://openairdocs.org/ad/2008-22-24) (historical): Low pressure compressor (LPC) fan blade · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Dec 9, 2008
- [AD 2006-11-05 R1](https://openairdocs.org/ad/2006-11-05-R1) (historical): Disc assemblies · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 27 more. Effective May 1, 2007
- [AD 2006-11-05](https://openairdocs.org/ad/2006-11-05) (historical): High pressure compressor (HPC) stage 3 disc assemblies · Rolls-Royce RB211-22B-02, RB211-524B-02, RB211-524B-B-02 and 24 more. Effective Jun 27, 2006
- [AD 2005-02-05](https://openairdocs.org/ad/2005-02-05) (historical): Low Pressure Compressor (LPC) Fan Blade Roots · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Feb 11, 2005
- [AD 2004-26-03](https://openairdocs.org/ad/2004-26-03) (historical): High pressure (HP) turbine discs · Rolls-Royce RB211-22B-02, RB211-535C-37, RB211-535E4-37 and 3 more. Effective Jan 13, 2005
- [AD 2004-01-20](https://openairdocs.org/ad/2004-01-20) (historical): High pressure compressor (HPC) · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 27 more. Effective Feb 24, 2004
- [AD 2003-17-15](https://openairdocs.org/ad/2003-17-15) (historical): Low pressure (LP) turbine stage 2 discs · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Oct 2, 2003
- [AD 2003-12-15](https://openairdocs.org/ad/2003-12-15) (historical): LPC fan blade roots · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Jul 30, 2003
- [AD 2003-10-03](https://openairdocs.org/ad/2003-10-03) (historical): High Pressure (HP) turbine discs · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Jun 20, 2003
- [AD 2002-23-08](https://openairdocs.org/ad/2002-23-08) (historical): Low Pressure (LP) Turbine Stage 2 Discs · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Dec 30, 2002
- [AD 2001-23-02](https://openairdocs.org/ad/2001-23-02) (historical): High Pressure Turbine Disks · Rolls-Royce RB211-22B-02, RB211-535C-37, RB211-535E4-37 and 2 more. Effective Dec 24, 2001
- [AD 98-07-07](https://openairdocs.org/ad/98-07-07) (historical): Fuel System Tube Assembly · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Apr 29, 1998
- [AD 86-07-01](https://openairdocs.org/ad/86-07-01) (historical): Outer Combustion Case Inspection · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective May 16, 1986

## Information bulletins (advisory) (1 in force)

- [SAIB 2026-11](https://openairdocs.org/saib/2026-11): Theft of Turbofan Engine Parts before Mutilation. Issued Jun 8, 2026

## NTSB investigations

None matched to N753CX.

## FAA accident and incident reports

None matched to N753CX.

## Service difficulty reports (104, 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 IXXA20251105002](https://openairdocs.org/sdr/IXXA20251105002), Nov 5, 2025: SKIN. CORRODED. RIGHT WING LOWER SURFACE SKIN PANEL NO 1, WSTA 95.0-177.5 CORROSION GRID NR 2.
- [SDR IXXA20251105001](https://openairdocs.org/sdr/IXXA20251105001), Nov 5, 2025: SKIN. CORRODED. RIGHT WING LOWER INBD SURFACE, AFT OUTBD OF FUSELAGE HAS AREA OF CORROSION WSTA, 95.0-177.5
- [SDR IXXA20251030004](https://openairdocs.org/sdr/IXXA20251030004), Oct 30, 2025: SKIN. CORRODED. RIGHT WING I/B LOWER LEADING EDGE WING SKIN IS CORRORED AT RIGHT WING I.B SLAT STA 284
- [SDR IXXA20251030003](https://openairdocs.org/sdr/IXXA20251030003), Oct 30, 2025: SKIN. CORRODED. RIGHT WING LOWER SKIN APPROX 18 INCHES FWD OF FUEL PANEL 631BB CORRODED AT SKIN BUTT SPLICE
- [SDR IXXA20251030002](https://openairdocs.org/sdr/IXXA20251030002), Oct 30, 2025: SKIN. CORRODED. RW LOWER SKIN 37" AFT OF SKIN SPLICE 5"- 46" OUTBD OF FUSELAGE HAS AREA OF CORROSION PN112N4101-34, AND 112N4102-42
- [SDR IXXA20251030001](https://openairdocs.org/sdr/IXXA20251030001), Oct 30, 2025: SKIN. CORRODED. RW LOWER SKIN 37" AFT OF SKIN SPLICE, 5"- 46 "OUTBD OF FUSELAGE HAS AREA OF CORROSION PN 112N4101-34 AND 112N4102-42
- [SDR IXXA20280925055](https://openairdocs.org/sdr/IXXA20280925055), Sep 25, 2025: BULB. INOPERATIVE. FORWARD FLIGHT ATTENDANT'S EMERGENCY CALL LIGHT IS INOPERATIVE. PLACED ON DEFERRAL 66475 MINIMUM EQUIPMENT LIST 23-41-01-04 CATEGORY B. DUE 28 SEPTEMBER 2025. R
- [SDR IXXA20250304010](https://openairdocs.org/sdr/IXXA20250304010), Feb 28, 2025: BOLT. DISLODGED. WHILE OPENING L1 DOOR TO TROUBLESHOOT POPPED CIRCUIT BREAKER, BOLTS FOR LOWER DOOR HINGE SERATION PLATE DISLODGED. AIRCRAFT GROUNDED FOR REPAIRS. 4 EACH BOLTS F
- [SDR IXXA20241102075](https://openairdocs.org/sdr/IXXA20241102075), Oct 31, 2024: BULB. INOPERATIVE. 1 EACH EMERGENCY EXIT BULB INOPERATIVE ABOVE SEAT 6E. 1 EACH EMERGENCY EXIT BULB ABOVE SEAT 6E REMOVED AND REPLACED. OPERATIONAL CHECK GOOD PER BOEING 757 AIRCR
- [SDR IXXA20241102074](https://openairdocs.org/sdr/IXXA20241102074), Oct 31, 2024: BULB. INOPERATIVE. 1 EACH EMERGENCY EXTERNAL ILLUM LIGHT @4R DOOR INOPERATIVE. 1 EACH EXTERNAL EMERGENCY BULB AT 4R DOOR POSITION REMOVED AND REPLACED. OPERATIONAL CHECK GOOD PER 
- [SDR IXXA20240923001](https://openairdocs.org/sdr/IXXA20240923001), Sep 23, 2024: FLOORBOARD. DAMAGED. MAIN DECK CARGO FLOOR PANELS AT STA 485 DAMAGE OUT OF LIMITS ON THE UPPER FACE OF 6 PANELS.
- [SDR IXXA20240921001](https://openairdocs.org/sdr/IXXA20240921001), Sep 21, 2024: SKIN. DENTED. RIGHT WING, ON #9 SLAT FOUND SMALL GOUGE.
- [SDR IXXA20240916002](https://openairdocs.org/sdr/IXXA20240916002), Sep 16, 2024: WEB. CORRODED. CORROSION NOTED AT WHEEL WELL CEILING STA 1160 LBL 12
- [SDR IXXA20240916001](https://openairdocs.org/sdr/IXXA20240916001), Sep 16, 2024: WEB. CORRODED. CORROSION NOTED AT MLG WHEEL WELL CENTER WEB. L/H SIDE STA. 1134 AND 15 TO 24 INCHES UP FROM TOP SIDE OF KEEL BEAM.
- [SDR IXXA20240914002](https://openairdocs.org/sdr/IXXA20240914002), Sep 14, 2024: SKIN. CORRODED. RIGHT WONG LOWER SKIN HAS SURFACE CORROSION AT WS 743.5
- [SDR IXXA202409140008](https://openairdocs.org/sdr/IXXA202409140008), Sep 14, 2024: SKIN. CORRODED. LEFT WING LOWER SKIN HAS SURFACE CORROSION AT WS 743.5
- [SDR IXXA20240606037](https://openairdocs.org/sdr/IXXA20240606037), Jun 3, 2024: FLASHLIGHT. NO TEST. FOLLOWING SCHEDULED MAINTENANCE, SUPERNUMERARY FLASHLIGHT DOES NOT TEST. FAULT TRANSFERRED TO DEFERRAL MAINTENANCE ITEM-52249 PER ATI MINIMUM EQUIPMENT LIST 25-
- [SDR IXXA20230915063](https://openairdocs.org/sdr/IXXA20230915063), Sep 13, 2023: UNKNOWN. UNKNOWN. AT FL360 CREW REPORTED LEFT ENGINE N1 FAN HIGH VIBE WITH ENGINE ANTI-ICE ON. IN LIGHT RIME ICING NOTED. AFTER DESCENDING TO FL240 VIBE STILL PRESENT. AFTER 15 M
- [SDR IXXA20221009139](https://openairdocs.org/sdr/IXXA20221009139), Oct 5, 2022: SWITCH. BROKEN. R 3 EMERGENCY LIGHT TEST SWITCH BROKEN. REMOVED AND REPLACED R-3 EMERGENCY LIGHT TEST SWITCH PER PEMCO 757-200 AMM 25-21-06. OPERATIONAL CHECK GOOD. NO ADDITION
- [SDR IXXA2022073001001](https://openairdocs.org/sdr/IXXA2022073001001), Jul 30, 2022: SEAL DEPRESSOR. BROKEN. RIGHT MLG DOOR LOWER SEAL DEPRESSOR BROKEN
- [SDR IXXA2022072910001](https://openairdocs.org/sdr/IXXA2022072910001), Jul 29, 2022: BRACKET. CORRODED. RAT ACTUATOR CONTROL BRACKET CORRODED
- [SDR IXXA202272812](https://openairdocs.org/sdr/IXXA202272812), Jul 28, 2022: BEAR STRAP. CORRODED. LEFT WING UPPER SURFACE T/E PANEL EXTRUSION ATTACHMENT ANGLE FROM WHEEL WELL TO INBD FLAP HINGE HAS NUMEROUS AREAS OF CORROSION UNDER NUTPLATES.
- [SDR IXXA2022728200011](https://openairdocs.org/sdr/IXXA2022728200011), Jul 28, 2022: SUPPORT BEAM. CORRODED. LEFT WING UPPER SURFACE T/E PANEL EXTRUSION ATTACHMENT ANGLE FROM WHEEL TO INBD FLAP HINGE HAS NUMEROUS AREAS OF CORROSION UNDER NUTPLATES.
- [SDR IXXA2022728000011](https://openairdocs.org/sdr/IXXA2022728000011), Jul 28, 2022: TEE FITTING. CORRODED. LEFT WING LOWER T/E PNL FROM WHEEL WELL TO LANDING GEAR STRUT 3 EA ATTACK T ANGLES CORRODED.
- [SDR IXXA202272810](https://openairdocs.org/sdr/IXXA202272810), Jul 28, 2022: WING ROOT. CORRODED. LEFT WING ABOVE MAIN LANDING GEAR ACTUATOR ATTACHMENT POINT SS267 CORROSION UNDER NUTPLATES.
- [SDR IXXA202272809](https://openairdocs.org/sdr/IXXA202272809), Jul 28, 2022: SHIM. WORN. O/B FLAP IB SUPPORT LINK FWD LINK ATTACH POINT HAS SHIM MIGRATING.
- [SDR IXXA202272807](https://openairdocs.org/sdr/IXXA202272807), Jul 28, 2022: FLANGE. CORRODED. LWW FILLET PANEL 197BL AFT SUPPORT/ATTACH FLANGE HAS CORROSION AROUND O/B NUTPLATE.
- [SDR IXXA202272805](https://openairdocs.org/sdr/IXXA202272805), Jul 28, 2022: SKIN SPLICE. CORRODED. EARLY SIGNS OF CORROSION ON EXTERIOR LOWER FUSELAGE SKIN. LOCATED AFT ACCESSOR AREA RIGHT LOWER SKIN SPLICE.
- [SDR IXXA202272804](https://openairdocs.org/sdr/IXXA202272804), Jul 28, 2022: SUPPORT ANGLE. CORRODED. APU INLET DOOR SURROUND FWD LOWER BULGED AND 2 FASTENERS MISSING.
- [SDR IXXA202272802](https://openairdocs.org/sdr/IXXA202272802), Jul 28, 2022: BRACKET. CORRODED. BLO FLAP MOTOR CROSSOVER CABLE PULLY HAS EVIDENCE OF CORROSION.
- [SDR IXXA2022072803](https://openairdocs.org/sdr/IXXA2022072803), Jul 28, 2022: STRAP. CORRODED. APU INLET DOOR SURROUND STRAP CORRODED
- [SDR IXXA2022072801](https://openairdocs.org/sdr/IXXA2022072801), Jul 28, 2022: DOOR FRAME. GOUGED. L2 DOOR SURROUND GOUGED ON WEB FRAME
- [SDR IXXA2022072020001](https://openairdocs.org/sdr/IXXA2022072020001), Jul 20, 2022: SKIN. CRACKED. RW LE UPPER SURFACE CRACKED
- [SDR IXXA2022072808](https://openairdocs.org/sdr/IXXA2022072808), Jul 12, 2022: DOOR. CORRODED. L2 ENTRY DOOR LOWER GATE CORRODED
- [SDR IXXA20220529116](https://openairdocs.org/sdr/IXXA20220529116), May 28, 2022: EICAS. FAULT MESSAGE. ENROUTE FROM PHIK TO PKWA, RIGHT ENGINE BLEED OFF EICAS MESSAGE DISPLAYED. CREW DECLARED EMERGENCY AND DESCENDED TO FL100. 9 EACH OXGEN GENERATORS DEPLOYED. FLI
- [SDR IXXA](https://openairdocs.org/sdr/IXXA), May 16, 2022: EICAS. FAULT MESSAGE. APPROXIMATELY FL 310 CABIN PRESSURE EICAS MESSAGE DISPLAYED. MASTER CAUTION OUTFLOW VALVE SHOWED CLOSED. NO CHANGE WHEN SWITCHED FROM AUTO 1 TO AUTO 2. AIR TURN
- [SDR IXXA202201317005](https://openairdocs.org/sdr/IXXA202201317005), Jan 27, 2022: NONE. NONE. PRE-DEPARTURE, L1 DOOR WILL NOT CLOSE. AIRCRAFT GROUNDED FOR UNSCHEDULED MAINTENANCE. WORK IN PROGRESS
- [SDR IXXA20201216041](https://openairdocs.org/sdr/IXXA20201216041), Dec 13, 2020: BATTERY PACK. INOPERATIVE. POST LANDING: EMERGENCY EXIT SIGN AT 3R DOOR INOPERATIVE. REMOVED AND REPLACED POWER PACK BATTERY AT R3 DOOR, IAW B757 AMM 33-51-07. OPERATIONAL CHECK SATISFACT
- [SDR 6PMR202009150409](https://openairdocs.org/sdr/6PMR202009150409), Sep 11, 2020: FLANGE. CORRODED. AIRBORNE/PEMCO NON-ROUTINE 3024.0021 DISCREPANCY: NR 2 ENGINE INLET DUCT ATTACHMENT FLANGE HAS CORROSION AROUND MATING HOLES. CORRECTIVE ACTION: EVALUATED AND R
- [SDR 6PMR2020090500013](https://openairdocs.org/sdr/6PMR2020090500013), Sep 5, 2020: PRESSURE WEB. CORRODED. AIRBORNE/PEMCO NON-ROUTINE 2867N702 DISCREPANCY: (EO20355-6) REPAIR RT HORIZONTAL PRESSURE DECK WEB (SECTION 44) STATION 1174 AND RBL 45.27 AND RBL 16.5 (LOCATI
- [SDR 6PMR202009050012](https://openairdocs.org/sdr/6PMR202009050012), Sep 5, 2020: PRESSURE WEB. CORRODED. AIRBORNE/PEMCO NON-ROUTINE 2867N701 DISCREPANCY: (EO 20355-8) REPAIR RT HORIZONTAL PRESSURE DECK WEB (SECTION 44) STATION 1160 BETWEEN RBL 8.2 AND RBL 16.5 (LOC
- [SDR 6PMR2020090500011](https://openairdocs.org/sdr/6PMR2020090500011), Sep 5, 2020: PRESSURE WEB. CORRODED. AIRBORNE/PEMCO NON-ROUTINE 2867N700 DISCREPANCY: (EO 20355-11) REPAIR RT HORIZONTAL PRESSURE DECK WEB (SECTION 44) STATION 1153 AND RBL 60 (LOCATIONS 29 & 38). 
- [SDR 6PMR202009050010](https://openairdocs.org/sdr/6PMR202009050010), Sep 5, 2020: PRESSURE WEB. CORRODED. AIRBORNE/PEMCO NON-ROUTINE 2867N675 DISCREPANCY: (EO 20366-7) REPAIR RT KEEL BEAM WEB (SECTION 44), STATION 1125.00 AND WL 183.00 (LOCATION 14) MIRROR EO. CORRE
- [SDR 6PMR2020082900393](https://openairdocs.org/sdr/6PMR2020082900393), Aug 19, 2020: PRESSURE WEB. CORRODED. AIRBORNE/PEMCO NON-ROUTINE 2867N684 DISCREPANCY: (722409) EO CONTROL NR 20355-9 REPAIR RIGHT HORIZONTAL PRESSURE DECK WEB (SECTION 44), STATION 1147 AND RBL 53.
- [SDR 6PMR2020082600387](https://openairdocs.org/sdr/6PMR2020082600387), Aug 13, 2020: GROUND WIRE. DAMAGED. AIRBORNE/PEMCO NON-ROUTINE 2867N127 DISCREPANCY: P/R 722290-OPERATIONAL TEST OF EMERGENCY LIGHTS IS WORKING, BUT SEVERAL INTERIOR AND EXTERIOR LIGHTS ARE OUT. C
- [SDR 6PMR2020082800392](https://openairdocs.org/sdr/6PMR2020082800392), Aug 12, 2020: WEB. CORRODED. AIRBORNE/PEMCO NON-ROUTINE 2867N674 DISCREPANCY: EO CONTROL NR 20366-5 REPAIR-RIGHT KEEL BEAM WEB (SECTION 44), STATION 1125.500 AND WL 153 (LOCATION 12), B757 
- [SDR 6PMR2020082800391](https://openairdocs.org/sdr/6PMR2020082800391), Aug 12, 2020: WEB. CORRODED. AIRBORNE/PEMCO NON-ROUTINE 2867N673 DISCREPANCY: EO CONTROL NR 20366-4 REPAIR-RIGHT KEEL BEAM WEB (SECTION 44), STATION, STATION 1140.00 AND WL 183.00 (LOCATION
- [SDR 6PMR202008280390](https://openairdocs.org/sdr/6PMR202008280390), Aug 12, 2020: WEB. CORRODED. AIRBORNE/PEMCO NON-ROUTINE 2867N672 DISCREPANCY: EO CONTROL NR 20366-1 REPAIR- RIGHT KEEL BEAM WEB (SECTION 44), STATION, BETWEEN STATION 1120 AND STATION 1180,
- [SDR 6PMR2020F00389](https://openairdocs.org/sdr/6PMR2020F00389), Aug 12, 2020: WEB. CORRODED. AIRBORNE/PEMCO NON-ROUTINE 2867N671 DISCREPANCY: EO CONTROL NR 20366-3 REPAIR-RIGHT KEEL BEAM WEB (SECTION 44), STATION 1146.30 AND WL 163.00 (LOCATION NR 9) B7
- [SDR 6PMR202008280388](https://openairdocs.org/sdr/6PMR202008280388), Aug 12, 2020: WEB. CORRODED. AIRBORNE/PEMCO NON-ROUTINE 2867N670 DISCREPANCY: EO CONTROL NR 20366-2 REPAIR-RIGHT KEEL BEAM WEB (SECTION 44), STATION 1165.00 AND WL 153-WL 183 (LOCATION NR 1

All 104: https://openairdocs.org/aircraft/N753CX/reports.md

## STCs that may be installed (OpenAirDocs) (1)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the engine (Rolls-Royce RB211-535E4 series)

- [STC SA4005NM](https://openairdocs.org/stc/SA4005NM): Precise Flight Inc. Pulselite Control System. Precise Flight Inc. Lists RB211-535E4-37

## Related

- Other Boeing 757-2Y0 aircraft: https://openairdocs.org/model/boeing-757-2y0/aircraft.md
- The Rolls-Royce RB211-535E4 series engine: https://openairdocs.org/engine/rolls-royce-rb211-535e4-series.md

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