# N754CX: 1996 Boeing 757-2YO - Status: Valid registration - Airframe: [Boeing 757-2YO](https://openairdocs.org/model/boeing-757-2yo) (registry code 1384922, 178 seats) - Engine: [Amateur-built UNKNOWN ENG](https://openairdocs.org/engine/amateur-built-unknown-eng) (registry code 99999) - Serial number: 26154 - Year built: 1996 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: September 2, 2013 - Certificate issued: January 31, 2013 - Expires: January 31, 2029 - Mode S code: AA292D - 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=754CX - Page: https://openairdocs.org/aircraft/N754CX 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): 0 in force ### Matched by airframe (Boeing 757-2YO) None in force. ### Matched by engine (Amateur-built UNKNOWN ENG) None in force. ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N754CX. ## FAA accident and incident reports None matched to N754CX. ## Service difficulty reports (204, 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 IXXA20260329026](https://openairdocs.org/sdr/IXXA20260329026), Mar 29, 2026: BOTTLE. RUPTURED. L4 DOOR SLIDE DEPLOYED BY CREW. SLIDE DID NOT INFLATE. REMOVED AND REPLACED PAX DOOR RESERVOIR DIAPHRAGM AND SERVICED RESERVOIR IAW B757 AMM 12-15-10. REINSTALL - [SDR IXXA20251219086](https://openairdocs.org/sdr/IXXA20251219086), Dec 19, 2025: HOUSING. DIRTY. L1 ENTRY DOOR SLIDE LIGHT INOPERATIVE. PLACED ON DEFERRAL 69103 MNIMUM EQUIPMENT LIST ATI-25-66-05-01 CATEGORY C. DUE 30 DECEMBER 2025. REMOVED, CLEANED AND REI - [SDR IXXA202512109085](https://openairdocs.org/sdr/IXXA202512109085), Dec 9, 2025: BATTERY PACK. INOPERATIVE. DURING SERVICE CHECK FOUND EMERGENCY LIGHTS IN FORWARD GALLEY INOPERATIVE. REMOVED AND REPLACED BATTERY PACK IN FORWARD GALLEY AFT OF ENTRANCE LIGHT PANEL IN AC - [SDR IXXA20250809040](https://openairdocs.org/sdr/IXXA20250809040), Aug 9, 2025: GOVERNOR. INOPERATIVE. LEFT ENGINE TAKING APPROXIMATELY 30 SECONDS TO SHUTDOWN AFTER FUEL CONTROL SHUTOFF. IN ACCORDANCE WITH B767 FIM 73-21 FAULT TREE 807 REMOVED AND REPLACED FUEL F - [SDR IXXA20250722032](https://openairdocs.org/sdr/IXXA20250722032), Jul 22, 2025: SLIDE. LOW PRESSURE. MAINTENANCE FOUND R3 EMERGENCY SLIDE PRESSURE GAUGE BELOW SERVICABLE LIMITS. REMOVED AND REPLACED R3 EMERGENCY SLIDE IN ACCORDANCE WITH BOEING 757 MAINTENANCE M - [SDR IXXA20250709028](https://openairdocs.org/sdr/IXXA20250709028), Jul 9, 2025: LIGHT. NO TEST. CREW PRE-FLIGHT, SLIDE LIGHT AT R4 DOOR DOES NOT ILLUMINATE. CLEANED GIRT BAR SLIDER STOP. OPERATIONAL CHECK IAW B767 AMM 52-11-25 NOTED NO FAULTS. - [SDR IXXA20250707027](https://openairdocs.org/sdr/IXXA20250707027), Jul 7, 2025: ACCESS PANEL. DAMAGED. CREW REPORTED, CATERING DAMAGED ACCESS DOOR TO SLIDE ON R4 DOOR. REINSTALLED R4 DOOR SLIDE IAW B757 AMM 25-66-03. OPERATIONAL CHECK OF SLIDE HOOK UP GOOD. NO OT - [SDR IXXA202506200005](https://openairdocs.org/sdr/IXXA202506200005), Jun 20, 2025: LATCH. GOUGED. #2 ENG O/B T/R FWD LATCH CATCH RECEIVER IS GOUGED. - [SDR IXXA20250620004](https://openairdocs.org/sdr/IXXA20250620004), Jun 20, 2025: HINGE. BENT. I/B T/R FWD AHAD DOOR HINGE ATTACH POINT BENT AND GOUGED - [SDR IXXA20250620003](https://openairdocs.org/sdr/IXXA20250620003), Jun 20, 2025: PAN. CORRODED. DURING OKAY INSTALL OF HANDLE L-1 DOOR, FOUND EXTERIOR DOOR HANDLE PAN TO BE GOUGED AND HAS CORROSION. - [SDR IXXA20250620002](https://openairdocs.org/sdr/IXXA20250620002), Jun 20, 2025: FASTENER. INCORRECT. L1 DOOR HANDLE PAN HAS SEVERAL INCORRECT LENGTH BLIND FASTENERS INSTALLED. - [SDR IXXA20250620001](https://openairdocs.org/sdr/IXXA20250620001), Jun 20, 2025: RETAINER. CRACKED. UPPER I/B T/R SEAL RETAINER CRACKED/BENT AT THREE LOCATIONS - [SDR IXXA2025061701](https://openairdocs.org/sdr/IXXA2025061701), Jun 17, 2025: STIFFENER. CORRODED. STIFFENER CORRODED STA 1071, RB-44.5 - RB-70 - [SDR IXXA20250611502](https://openairdocs.org/sdr/IXXA20250611502), Jun 15, 2025: SUPPORT ANGLE. CORRODED. LEFT LANDING GEAR HYDRAULIC STSTEM HOSE CLAMPS SUPPORT ANGLES CORRODED - [SDR IXXA2025061501](https://openairdocs.org/sdr/IXXA2025061501), Jun 15, 2025: SUPPORT CHANNEL. CORRODED. MULTIPLE HYDRAULIC BLOCK CLAMPS AND ATTACHING HARDWARE ARE CORRODED - [SDR IXXA2025061202](https://openairdocs.org/sdr/IXXA2025061202), Jun 12, 2025: FLAP TRACK. CORRODED. LEFT WING O/B FLAP I/B SUPPORT UPPER AND LOWER SURFACES CORRODED MAIN TRACK - [SDR IXXA20250612001](https://openairdocs.org/sdr/IXXA20250612001), Jun 12, 2025: STRINGER. CRACKED. STRINGER CRACK AT TOP CENTER FWD AREA AS SEEN THROUGH PANEL 313BZ ABOVE APU COMPARTMENT ACCESS THROUGH PANEL 313AL TAG #47012. - [SDR IXX202506110012](https://openairdocs.org/sdr/IXX202506110012), Jun 11, 2025: FLOORBEAM. CORRODED. CORROSION ON THE UPPER CHORD OF THE CABIN FLOORBEAM, AROUND THE FASTENER HOLE AT STA 1640, LBL54 #79247. - [SDR IXXA2025061101](https://openairdocs.org/sdr/IXXA2025061101), Jun 11, 2025: SUBFRAME. CORRODED. CORROSION ON THE CABIN SUBFLOOR AT STA 1716 BLO TO LBL38 - [SDR IXXA2025060801](https://openairdocs.org/sdr/IXXA2025060801), Jun 8, 2025: ATTACH FITTING. CORRODED. RT WHEEL WELL STA 1120 RBL2 WIRE STANDOFF HAS CORROSION - [SDR IXXA20250606003](https://openairdocs.org/sdr/IXXA20250606003), Jun 6, 2025: STRINGER. CRACKED. STRINGER CRACK AT TOP CENTER FWD AREA AS SEEN THROUGH PANEL 313BZ ABOVE APU COMPARTMENT ACCESS THROUGH PANEL 313AL - [SDR IXXA202500606004](https://openairdocs.org/sdr/IXXA202500606004), Jun 6, 2025: PRESSURE DECK. CORRODED. LH WHEEL WELL STA1120 LBL20 LOWER SKIN PRESSURE DECK CORRODED - [SDR IXXA202500606003](https://openairdocs.org/sdr/IXXA202500606003), Jun 6, 2025: PRESSURE DECK. CORRODED. LH WHEEL WELL STA1120 LBL20 LOWER SKIN PRESSURE DECK CORRODED - [SDR IXXA202500606002](https://openairdocs.org/sdr/IXXA202500606002), Jun 6, 2025: PRESSURE DECK. CORRODED. RH WHEEL WELL STA1065 RBL28 HAS CORROSION ON LOWER SURFACE OF PRESSURE DECK - [SDR IXXA20250606001](https://openairdocs.org/sdr/IXXA20250606001), Jun 6, 2025: PRESSURE DECK. CORRODED. RH WHEEL WELL STA1079 RBL28 HAS CORROSION ON LOWER SURFACE OF PRESSURE DECK - [SDR IXXA20250605002](https://openairdocs.org/sdr/IXXA20250605002), Jun 5, 2025: ANGLE. CORRODED. L/H WHEEL WELL STA 1110 LBL25 STIFFENER CORRODED - [SDR IXXA2025060501](https://openairdocs.org/sdr/IXXA2025060501), Jun 5, 2025: SUPPORT. CORRODED. FOUND CORROSION COMMON TO RH FUSELAGE FAIRING PNL 198LR ON SUPPORT STRUCTURE - [SDR IXXA20250605001](https://openairdocs.org/sdr/IXXA20250605001), Jun 5, 2025: SKIN. CORRODED. CORROSION ON THE VHF ANTENNA ON THE TOP OF THE FUSELAGE - [SDR IXXA2025060412](https://openairdocs.org/sdr/IXXA2025060412), Jun 4, 2025: RETAINER. CORRODED. APU INLET DOOR CUTOUT INTERNAL RETAINER FWD, AFT I/B & O/B CORROSION AROUND NUT PLATES - [SDR IXXA20250604012](https://openairdocs.org/sdr/IXXA20250604012), Jun 4, 2025: PRESSURE DECK. CORRODED. RH WHEEL WELL STA1047 RBL28 HAS CORROSION ON LOWER SURFACE OF PRESSURE DECK - [SDR IXXA20250604011](https://openairdocs.org/sdr/IXXA20250604011), Jun 4, 2025: STIFFENER. CORRODED. LH WHEEL WELL STA1110 LBL4 STIFFNER CORRODED - [SDR IXXA2025060410](https://openairdocs.org/sdr/IXXA2025060410), Jun 4, 2025: SKIN. CORRODED. #2 PYLON I/B SIDE, SKIN HAS CORRROSION ON INTERIOR SIDE LOOKING THRU PNL 443JC - [SDR IXXA20250604009](https://openairdocs.org/sdr/IXXA20250604009), Jun 4, 2025: DOUBLER. DAMAGED. THIS NR FOR DOC. OF MAJOR REPAIR FOR AMES DOC. 47651FAB28. DOUBLER WAS REMOVED ON NR 177268-0400-0133 AND LOST. PART WAS UNAVAILABLE FOR PURCHASE AND A SMAL WAS - [SDR IXXA2025060407](https://openairdocs.org/sdr/IXXA2025060407), Jun 4, 2025: WEB. CORRODED. LH WHEEL WEB STA 1110 LBL0 KEEL WEB AT FITTING CORRODED - [SDR IXXA20250604008](https://openairdocs.org/sdr/IXXA20250604008), Jun 4, 2025: SKIN. CORRODED. CORROSION ON #1 PYLON O/B SIDE, ON INNER SKIN, SEEN THRU FORWARD 2 ACCESS PANEL (1 BEING D-DOOR) - [SDR IXXA20250604006](https://openairdocs.org/sdr/IXXA20250604006), Jun 4, 2025: SKIN. CORRODED. CORROSION ON LOWER SURFACE OF LEFT WING SKIN AT LONGERON L-8, WSTA. 208.5 - [SDR IXXA20250604005](https://openairdocs.org/sdr/IXXA20250604005), Jun 4, 2025: FRAME. CRACKED. CRACKED FRAME IN ALC L/H SIDE STA 1520 LBL 25 ABOVE STR 26L - [SDR IXXA20250604004](https://openairdocs.org/sdr/IXXA20250604004), Jun 4, 2025: PRESSURE DECK. CORRODED. WIDE SPREAD CORROSION IN LWW UPPER PRESSURE DECK WEB STA 1070 LBL 39 - [SDR IXXA20250604003](https://openairdocs.org/sdr/IXXA20250604003), Jun 4, 2025: PRESSURE DECK. CORRODED. LH WHEEL WELL STA1140 LBL2 LOWER SKIN PRESSURE DECK CORRODED - [SDR IXXA2025060401](https://openairdocs.org/sdr/IXXA2025060401), Jun 4, 2025: LINK. CORRODED. SUPPORT BEAMS CONNECTING LINKS PN 113N1908-2 WERE FABBED ON 47651FAB18. INSTALLED ON NR 177268-0100-00039 - [SDR IXXA20250604001](https://openairdocs.org/sdr/IXXA20250604001), Jun 4, 2025: PANEL. CORRODED. ALC (SIDE WALL TO FLOOR) SIDE PANEL ON L/H SIDE STA 1410-1530 HAS CORROSION FROM ONE END TO THE OTHER PRIMARILY ON BOTTOM AROUND NUTPLATES AND SLPICE POINTS - [SDR IXXA2025060303](https://openairdocs.org/sdr/IXXA2025060303), Jun 3, 2025: TEE FITTING. CORRODED. CORROSION IN SEVERAL AREAS IN RWW AFT BULKHEAD ON T CORD STA 1180 RBL 50 - [SDR IXXA2025060302](https://openairdocs.org/sdr/IXXA2025060302), Jun 3, 2025: PRESSURE DECK. CORRODED. RH WHEEL WELL STA 1076 RBL54 HAS CORROSION ON LOWER PRESSURE DECK - [SDR IXXA20250060301](https://openairdocs.org/sdr/IXXA20250060301), Jun 3, 2025: PRESSURE PANEL. CORRODED. RH WHEEL WELL STA 1100-RBL 4 HAS CORROSION ON LOWER PRESSURE PLATE - [SDR IXXA2025060413](https://openairdocs.org/sdr/IXXA2025060413), Jun 2, 2025: SUPPORT BEAM. CORRODED. UPPER T/E PANEL SUPPORT ANGLE IS CORRODED LOCATED FROM THE SIDE OF BODY TO #6 FLAP FITTING JUST AFT OF RMLG SUPPORT BEAM - [SDR IXXA20250605412](https://openairdocs.org/sdr/IXXA20250605412), Jun 2, 2025: BRACKET. CORRODED. RMLG DOOR LOCK RELEASE ACTUATOR CRANK ASSEMBLY ATTACH BRACKET IS CORRODED - [SDR IXXA202505310013](https://openairdocs.org/sdr/IXXA202505310013), May 31, 2025: FLOOR SUPPORT. CORRODED. CORROSION ON ALC LOWER FLOOR PANEL SUPPORT Z- CHANNEL AT FWD END AROUND NUTPLATE STA 1200 LBL 3. - [SDR IXXA202505310012](https://openairdocs.org/sdr/IXXA202505310012), May 31, 2025: PRESSURE DECK. CORRODED. LWW STA1125 LBL4 LOWER SKIN PRESSURE DECK CORRODED - [SDR IXXA202505310011](https://openairdocs.org/sdr/IXXA202505310011), May 31, 2025: SHROUD. CRACKED. MDCD FWD LOWER SHROUD FOUND CRACK ON INTERNAL WEB. - [SDR IXXA202505310010](https://openairdocs.org/sdr/IXXA202505310010), May 31, 2025: SEAT TRACK. CORRODED. LH OB SEAT TRACK HAS MULTIPLE EXCESSIVELY WORN SPOTS WITH CORROSION FROM STA 1350-1540 All 204: https://openairdocs.org/aircraft/N754CX/reports.md ## Service difficulty reports on N754CX not matched to an aircraft (2) They name N754CX, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR IXXA20150729107](https://openairdocs.org/sdr/IXXA20150729107), Jul 2, 2015: SKIN. DENTED. FUSELAGE SKIN DENTED & SCRATCHED IN BETWEEN STRINGERS 15 - 16L, BS 1714 SIX INCHES FORWARD OF PRESSURE DOME. REPAIRED THE SKIN IAW SRM 53-00-01 REPAIR 3 FIGURE - [SDR IXXA2015072900107](https://openairdocs.org/sdr/IXXA2015072900107), Jun 25, 2015: SKIN. CRACKED. R4 DOOR SKIN CRACKED ON UPPER FOLD DOWN SECTION FORWARD END. REMOVED & INSTALLED UPPER GATE ASSEMBLY IAW AMM 52-11-38-404-009. ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## Related - Other Boeing 757-2YO aircraft: https://openairdocs.org/model/boeing-757-2yo/aircraft.md - The Amateur-built UNKNOWN ENG engine: https://openairdocs.org/engine/amateur-built-unknown-eng.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.