Crash of a Rockwell Aero Commander 720 in Alcoa: 2 killed

Date & Time: Dec 9, 1988 at 0600 LT
Operator:
Registration:
N120G
Flight Type:
Survivors:
No
Schedule:
Fort Lauderdale – Alcoa
MSN:
720-630-3
YOM:
1958
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
4103
Circumstances:
After encountering icing conditions in flight and experiencing problems maintaining altitudes and headings, the pilot elected to divert from his planned destination of Dayton, OH to Knoxville, TN. While on final approach after descending 1,300 feet below minimum procedure turn altitude followed by being told the aircraft was well above the glideslope, ATC instructed the pilot to maintain 3,000 feet. Shortly thereafter, ATC reported the mode C indicated 1,900. The pilot responded with 'engine quit'. The aircraft crashed in a pasture about 1 mile from the airport. The investigation revealed that the aircraft was not equipped to operate in icing conditions. The evidence indicated that the flaps and landing gear were extended. Approximately 40 lbs of cocaine were found onboard the aircraft. The tox report for the pilot disclosed .05 mg/l benzoylecognite (cocaine metabolite) in his blood. The pilot had received a weather briefing which included a freezing level at 7,000 feet and filed a flight plan requesting a cruising altitude of 14,000 feet. Both occupants were killed.
Probable cause:
Occurrence #1: loss of engine power (total) - nonmechanical
Phase of operation: approach - iaf to faf/outer marker (ifr)
Findings
1. (f) weather condition - icing conditions
2. (f) weather evaluation - poor - pilot in command
3. 1 engine
4. (c) induction air control/system - ice
5. (c) in-flight planning/decision - poor - pilot in command
6. (f) impairment (drugs) - pilot in command
----------
Occurrence #2: loss of control - in flight
Phase of operation: missed approach (ifr)
Findings
7. (c) emergency procedure - improper - pilot in command
8. (f) gear retraction - not performed - pilot in command
9. (f) raising of flaps - not performed - pilot in command
----------
Occurrence #3: in flight collision with terrain/water
Phase of operation: descent - uncontrolled
Final Report:

Crash of a Rockwell Aero Commander 720 in Wausau: 3 killed

Date & Time: Aug 4, 1977 at 1157 LT
Registration:
N688R
Flight Type:
Survivors:
No
Schedule:
Rhinelander - Wausau
MSN:
720-790-11
YOM:
1959
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
197
Captain / Total hours on type:
146.00
Circumstances:
While on approach to Wausau-Waukesha Airport, one of the engine failed. The pilot lost control of the airplane that stalled, entered a spin and crashed few miles from the airport. The aircraft was destroyed and all three occupants were killed.
Probable cause:
Stall and spin on approach following an engine failure for undetermined reasons. The following contributing factors were reported:
- Poorly planned approach,
- Delayed in initiating go-around,
- Failed to follow approved procedures,
- Improper emergency procedures,
- Failed to maintain flying speed,
- Complete engine failure on one engine,
- Forced landing off airport on land,
- Improper single-engine procedures.
Final Report:

Crash of a Rockwell Aero Commander 720 Alti Cruiser in Klamath River: 1 killed

Date & Time: Jan 18, 1969 at 1805 LT
Registration:
N4831C
Flight Phase:
Survivors:
No
Schedule:
Fresno - Eugene
MSN:
720-760-10
YOM:
1959
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
695
Captain / Total hours on type:
154.00
Circumstances:
While cruising by night in marginal weather conditions (rain and fog), the pilot informed ATC about an engine failure. Shortly later, the airplane went out of control, entered a dive and crashed near Klamath River, north of California. The wreckage was found a day later and the pilot, sole on board, was killed.
Probable cause:
It was determined that the probable cause of the accident was that the carburetor on one engine failed after encountering icing conditions. It was reported that the aircraft was not equipped with de-icing equipments.