MIA83FA226

NTSB accident investigation · Cessna C-114A · Ft. Lauderdale, FL · September 10, 1983

Accident · Serious injuriesField investigationFinal report
Date
September 10, 1983, 07:59 local (11:59 UTC)
Place
Ft. Lauderdale, FL
Injuries
2 serious, 3 minor
Damage
Destroyed
Phase of flight
Initial climb
Aircraft
N256ELCessna C-114A
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
FAA report
19830910047979A
Case key
30806

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Loss of engine power(partial) - mech failure/malfTakeoff - initial climb
Fuel system,strainer - blocked(partial)Cause
Exhaust system,turbocharger - disconnectedCause
Loss of control - in flightTakeoff - initial climb
Flight controls - improper use ofPilot in commandCause
Throttle/power control - improper use ofPilot in commandCause
Abort - not performedPilot in commandCause
In flight collision with terrain/waterManeuvering

Analysis

The acft crashed while maneuvering at low airspeed and altitude right after takeoff. The plt said the left engine started losing power intermittently at 90 KTS. The plt had rotated the acft and tried to continue the takeoff. He was cleared to land on any rwy and in attempting a turn with landing gear and partial flaps extended control was lost and a crash occurred. The acft flt manual states that if an engine fails below 105 mph the takeoff should be aborted. An on scene examination revealed no evidence to suggest a pre-impact failure or malfunction. Both propellers showed evidence of torsional overload damage. When the engines were further examined the left engine fuel strainer was partially cloggedwith dirt. During a run-up test the left engine would not develope more than 23 inches hg. At 2750 RPM and magneto RPM drop was erratic. The engine would not run with the aux fuel boost pump off. The reason for the low power output was a disconnected pressure line for the turbocharger which appeared to have been disconnected for some time.

Aircraft

Registration
N256EL
Reported as
Cessna C-114A
Category
Airplane
Serial number
411-0242
Airframe hours
2,439
Engine
Continental GTSIO-520-C, 340 horsepower, reciprocating
Damage
Destroyed
Fire
On-Ground
Flight
Personal · Part 91
Operator
Martin Bilt
Registered owner
Bertram E. Weech
Airworthiness certificate
Standard, Normal
Last inspection
Annual · May 14, 1983 · 2 hours before
Departed
FXE · Ft.Lauderdale, FL
Destination
ATL · Atlantic, GA
Flight plan
IFR
Airport
FXE · Ft.Lauderdale Executive, runway 8, 6,000 × 100 ft, asphalt

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
57
Certificate
Commercial
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Left
Flight hours
7,200 total · 500 in this make and model · 90 in the last 90 days

Weather

Conditions
Visual (VMC) · Day
Wind
80° at 5 knots
Visibility
7 statute miles
Lowest ceiling
10,000 ft broken
Temperature
81 °F, dew point 73 °F
Altimeter
30.00 inHg
Observed at
FXE

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.

Other investigations on N256EL · 2

Matched to the same aircraft by N-number and date.