N363CM Boeing 767-338
Timeline
- Current registration certificate issuedOwner type: Corporation
- NTSB incident record ENG21LA013Damage: Minor · Highest injury: Not recorded
- Latest FAA registry actionMost recent change recorded in the FAA registry
- Registration expiresValid
From FAA registry and NTSB records. Registration dates reflect paperwork, not flights.
The aircraft
- Make & model
- Boeing 767-338
- Category
- Fixed-wing airplane, multi-engine
- Year built
- Not listed
- Engine type
- Turbofan (jet) · 2 engines
- Max takeoff weight class
- 20,000 lb and over
- Serial number
- 24853
Registration
- Status
- Valid
- Expires
- Oct 31, 2027
- Certificate issued
- Oct 21, 2011
- Owner type
- Corporation
- Registered owner
- CARGO AIRCRAFT MANAGEMENT INC
The registered owner is often a bank, leasing company or trust, not necessarily the airline or person who flies it.
What kind of aircraft is this?
The Boeing 767 is a twin-engine, twin-aisle (wide-body) jet used for long-haul passenger and cargo flying since the early 1980s.
In plain terms, it's a jet (turbofan) multi-engine airplane. Certification: Type certificated (factory design approved by the FAA).
There are 13 aircraft of this exact model variant on the US register, and about 576 Boeing aircraft with closely related model designations, out of 317,717 registered aircraft in total.
An aircraft's age on its own says little about how safe it is: airliners are maintained on strict, regulator-approved schedules, and inspections become more detailed as aircraft get older. More about the Boeing 767 →
NTSB accident & incident history for N363CM
1 record found. An "incident" is a less serious event; an "accident" involves serious injury or substantial damage, as defined by the NTSB. Many records involve no injuries at all.
-
Jan 29, 2021 (18:49 UTC)Incident · Ontario, CANTSB #ENG21LA013Aircraft in report: BOEING 767-338Damage: MinorHighest injury: Not recorded
NTSB probable cause: The fatigue fracture and liberation of two airfoils from a low pressure turbine stage 5 nozzle segment that impacted and damaged the downstream low pressure stage 5 blades creating an initial imbalance load in the engine’s low pressure turbine rotor sufficient to allow all the low pressure turbine blades to lose radial blade clearance, contact static structure, and to fracture transversely across the airfoil. The progressive failure of the low pressure rotor caused an increasingly imbalanced load that eventually resulted in the fracture of the oil supply tube that allowed oil to contact hot engine parts and smolder and ignite resulting in the undercowl fire.
Look up full reports by NTSB number in CAROL, the NTSB's public database.
Data: FAA Releasable Aircraft Database (file dated 2026-10-16) and NTSB aviation accident database; refreshed 2026-10-17 20:47 UTC. SafelyAboard shows public records only and does not rate or score aircraft, airlines or operators.