LAX04LA308

NTSB accident investigation · Rockwell 112TCA · San Rafael, CA · August 31, 2004

Accident · Minor injuriesLimited investigationFinal report
Date
August 30, 2004, 17:35 local (Aug 31, 2004, 00:35 UTC)
Place
San Rafael, CA
Injuries
1 minor
Damage
Substantial damage
Phase of flight
Initial climb
Aircraft
N44MHRockwell 112TCA
Weather
Visual (VMC) · Day
Status
Completed · report March 28, 2006
Report
Approved by Office Director
Parties
Federal Aviation Administration
FAA report
20040830021819A
Case key
60036

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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Probable cause

A total loss of engine power during initial climb due to fuel starvation, which was caused by the pilot's failure to turn on the electric boost pump and an undetermined failure of the engine driven pump to supply sufficient fuel to the carburetor.

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(total) - nonmechanicalTakeoff - initial climb
Fluid,fuel - starvationCause
Checklist - not followedPilot in commandFactor
Fuel boost pump selector position - improperPilot in commandCause
Fuel system,pump - output low
Forced landingEmergency landing after takeoff
On ground/water encounter with terrain/waterEmergency landing
Terrain condition - swampyFactor
Nose overEmergency landing

Analysis

During initial climb between 100 and 200 feet above ground level, the airplane's engine lost all power due to fuel starvation. The pilot made a forced landing in a marsh about 1/4-mile beyond the runway's departure end. After the airplane came to rest upside down in the 2- to 4-foot-deep marsh, the pilot extricated himself and waded to the shore. The pilot had refueled his airplane just before takeoff. During takeoff, full engine power was initially developed with the fuel selector positioned to the "Both" tanks position. Following the accident when the airplane was examined, no evidence of any preimpact mechanical malfunction was noted. The engine's electric fuel pump switch was observed in the "OFF" position. The pump switch was required to be "ON" during takeoff. During the initial climb, the engine driven fuel pump likely had not pumped sufficient fuel to the engine to maintain power, which resulted in fuel starvation.

Factual narrative

On August 30, 2004, about 1735 Pacific daylight time, a Rockwell International 112TCA, N44MH, experienced a total loss of engine power during initial climb from a private airstrip about 3 miles north of San Rafael, California. The pilot made a forced landing in a marshy area of the Mcinnis Park. The airplane nosed over upon touchdown and was substantially damaged. The private pilot, who owned and operated the airplane, sustained minor shoulder harness-related restraint type injuries. Visual meteorological conditions prevailed, and no flight plan had been filed. The personal flight was performed under the provisions of 14 CFR Part 91. The flight originated from San Rafael about 1734.

The pilot reported to the National Transportation Safety Board investigator that he had just refueled his airplane at the San Rafael private airstrip, his home base. Thereafter, he performed a normal preflight inspection and checked the engine's magnetos. No discrepancies were noted. Full engine power was applied during the takeoff roll, with the fuel selector positioned to the "Both" tanks position. Upon climbing between 100 and 200 feet above ground level, the engine suddenly lost all power. The pilot stated that, to the best of his recollection, the power loss was not preceded by any unusual sound.

The pilot made a forced landing about 1/4-mile beyond the runway's departure end. After the airplane came to rest upside down in the 2- to 4-foot-deep marsh, the pilot extricated himself and waded to the shore.

The airplane was recovered from the accident site and was examined by a Federal Aviation Administration (FAA) aviation safety inspector. The FAA inspector reported finding no evidence of any preimpact mechanical malfunction. He indicated that only about 1 teaspoon of fuel was drained out of the gascolator. The engine's electric fuel pump switch was observed in the "OFF" position. The FAA inspector additionally reported that the pump was required to be "ON" during takeoff.

The FAA inspector opined that during the initial climb, the engine driven fuel pump had not pumped sufficient fuel to the engine to maintain power. This resulted in fuel starvation.

Aircraft

Registration
N44MH
Reported as
Rockwell 112TCA
Category
Airplane
Serial number
13308
Airframe hours
1,820
Engine
Lycoming TO-360-C1A6D, 210 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
James L. Thomas, III
Airworthiness certificate
Standard, Utility; Standard, Normal
Last inspection
Annual · August 1, 2003 · 83 hours before
Departed
CA35 · San Rafael, CA
Destination
0Q9 · Sonoma, CA
Airport
CA35 · San Rafael

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
43
Injuries
Minor
Certificate
Private
Airplane ratings
Single-engine land
Instrument ratings
Airplane
Medical
Class 3, Valid Medical--w/ waivers/lim
Last flight review
September 1, 2003
Seat
Left
Flight hours
988 total · 791 in this make and model · 938 as pilot in command · 21 in the last 90 days · 7 in the last 30 days · 0 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
290° at 18 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
66 °F, dew point 57 °F
Altimeter
29.90 inHg
Observed at
SFO, 20 nm away

FAA reports on this event · 1

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