FTW95IA022 · Canadair CL 600
Affiliated Health Services Canadair CL 600 · Incident: total loss of engine power (non-mechanical) en route
From Tucson International Airport (TUS) to Shreveport Regional Airport (SHV)
Event
- NTSB case
- FTW95IA022
- Event typeAccident: someone killed or seriously injured, or the aircraft substantially damaged (NTSB definition). Incident: an occurrence that affected or could have affected safety, short of that. Glossary
- Incident
- InvestigationHow far the investigation had got when the record was published: preliminary, ongoing, final or completed. Unknown where the source does not say. Glossary
- Completed
- API-reported fatalities
- 0 · all aircraft and ground
- Ground fatalities
- 0
- OperationWhat kind of flying it was, grouped by the rules it flew under: airline (US Part 121), air taxi and commuter (Part 135), general aviation (Part 91 and similar), military or government. Glossary
- General aviation
- WeatherVisual meteorological conditions (VMC): good enough to fly by looking outside. Instrument conditions (IMC): cloud or low visibility, flying by instruments. Glossary
- Instrument Meteorological Cond
Canadair CL 600
- Aircraft type
- Canadair CL-600
- Category
- Airplane
- RegistrationThe aircraft's tail number, such as N12345 or G-ABCD. Registrations are reissued, so the same one years apart can be a different aircraft. Glossary
- N600RE
- Operator
- Affiliated Health Services
- Onboard fatalities
- Unknown
- Route
- From Tucson International Airport (TUS), Tucson, AZTo Shreveport Regional Airport (SHV), Shreveport, LA
- Aircraft age
- Not recorded
- Flight rulesThe regulations the flight operated under: in the US, Part 91 (general aviation), Part 121 (airlines), Part 135 (air taxi and commuter) and others; for flights abroad, the NTSB's coarser commercial or non-commercial code. Glossary
- Part 91: General Aviation
- Phase of flightThe stage of the flight when things started to go wrong: standing, taxi, takeoff, initial climb, en route, maneuvering, approach or landing. Glossary
- En route · descent
- First occurrenceThe single coded event the NTSB judges best describes what happened (records from 2008 on). Older records name the first occurrence in the sequence instead. Glossary
- Total loss of engine power (non-mechanical)
- DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
- Minor
Cause areas
- Flightcrew › Anti-ice/deice system, improper use of
- Miscellaneous, engine › Ice
- Miscellaneous, engine › Ice ingestion
Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.
NTSB narrative
DURING FLIGHT AT FL370, THE AIRPLANE ENTERED A CLOUD LAYER AND ENCOUNTERED TURBULENCE. A DESCENT WAS MADE TO FL330. AS POWER WAS BEING APPLIED FOR LEVEL OFF AT FL330, THE N1 INDICATION DID NOT RESPOND. AT FL310 THE #1 ENGINE FLAMED OUT. WEATHER INCLUDED ICE CRYSTALS, THUNDERSTORM OUTFLOW, AND TURBULENCE. DURING AN ATTEMPTED CROSS BLEED AIR START, THE #2 ENGINE FLAMED OUT. WITH THE AIR DRIVEN GENERATOR (ADG) DEPLOYED, THE CREW WAS SUCCESSFUL WITH AN APU ASSISTED START. BOTH ENGINES WERE STABILIZED BY 5000 FEET, AND THE FLIGHT LANDED SAFELY. INTERVIEWS AND INFORMATION FROM THE CVR REVEALED THAT THE CREW DID NOT CALL FOR THE EMERGENCY CHECKLIST AND THAT THEY LACKED KNOWLEDGE OF THE AIRPLANE SYSTEMS. AS THE CREW RECOGNIZED THE INITIAL POWER LOSS, THE CAPTAIN ASKED THE FIRST OFFICER IF HE HAD TURNED ON ENGINE ANTI-ICE. HE REPLIED THAT HE HAD NOT. THE CREW HAD NOT ATTENDED A FORMAL TRAINING COURSE FOR THE CL 600. THE CAPTAIN AND COPILOT RECEIVED TYPE RATINGS FROM A DESIGNATED PILOT EXAMINER (DPE) IN MAY AND MARCH 1994, RESPECTIVELY. TESTS OF THE FUEL CONTROL UNITS REVEALED DISCREPANCIES IN THE START AND ACCELERATION SCHEDULES; HOWEVER, NO DISCREPANCIES WERE FOUND THAT WOULD HAVE CONTRIBUTED TO THE FLAMEOUTS.
Probable cause
THE FLIGHT CREW'S IMPROPER USE OF THE ANTI-ICE SYSTEM, WHICH RESULTED IN ENGINE ICE, SUBSEQUENT ICE INGESTION, AND ENGINE FLAMEOUT. FACTORS RELATED TO THE ACCIDENT WERE: FAILURE OF THE FLIGHT CREW TO FOLLOW THE CHECKLIST PROCEDURES AFTER FLIGHT INTO ADVERSE WEATHER CONDITIONS, AND THE AIRCREW'S LACK OF FAMILIARITY WITH THE AIRCRAFT REGARDING FLIGHT IN ICING C0NDITIONS.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record FTW95IA022
- Event ID
- 20001206X02431
- Case number
- FTW95IA022
- Dataset
- historical-pre2008
- Source SHA-256
- 89e2df6d848e7ab3b42e7d7c7a03ff403303057a26ca04c95b3ea67201c3ce74
Source notes (4)
- Unreviewed is an editorial label, not an investigation status. API-sourced is not report-checked or human-reviewed. Explicit event totals are used without summing aircraft injury tables; onboard allocation is withheld. Unknown values remain unknown. The operation category is mapped from the NTSB-reported FAR part and has not been reviewed.
- Filled from the NTSB case API where the bulk record had no value: local date, investigation status. Values present in the bulk record are kept.
- The date is the local date; the NTSB stores the UTC date 1994-10-17.
- API snapshot SHA-256: 49b6fa473678a66e395e19a6040f639f3210fe2cc7f7a317df035187fa2feff8; retrieved 2026-09-23T00:31:48.418Z.