CHI98LA328

NTSB accident investigation · Beech B35 · Iowa City, IA · August 23, 1998

Accident · No injuriesLimited investigationFinal report
Date
August 23, 1998, 12:40 local (17:40 UTC)
Place
Iowa City, IA
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Initial climb
Aircraft
N5210CBeech B35
Weather
Visual (VMC) · Dawn
Status
Completed · report February 16, 2001
Report
Approved by Office Director
FAA report
19980823021569A
Case key
43757

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

The fuel starvation due to improper fuel management by the pilot-in-command. Also, the aircraft procedures and directives which were not followed by the pilot-in-command is an additional cause. The rough and uneven terrain in addition to the low altitude of the aircraft were contributing factors.

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 powerTakeoff - initial climb
Fluid,fuel - starvationCause
Fuel management - improperPilot in commandCause
Procedures/directives - not followedPilot in commandCause
Forced landingEmergency landing after takeoff
Airport facilities,runway/landing area condition - rough/unevenFactor
Altitude - lowFactor
On ground/water encounter with terrain/waterEmergency landing

Analysis

Examination of the aircraft found the fuel selector was selected to the left main fuel tank and the left main fuel tank was 3/4 full of a light blue colored fuel. The right tank was empty and the 20 gallon auxiliary fuel tank was estimated to be 1/2-3/4 full of fuel. The engine, Teledyne Continental E185-11, serial number 26643-D-8-11, was shipped to Teledyne Continental Motors for examination and testing under the supervision of the National Transportation Safety Board. The testing and examination revealed no anomalies. The limitations section of the Beechcraft B35 Pilot's Operating Handbook (POH) states, 'Do not take off when the Fuel Quantity Gages indicate in the Yellow Band or with less than 10 gallons in each main tank.'. Furthermore, the systems description of fuel tank selection in the POH states, 'In no case should a take-off be made ... with less than 10 gallons of fuel in each main tank.

Factual narrative

On August 23, 1998, at 1240 central daylight time, a Beech B35, N5210C, piloted by an airline transport pilot, received substantial damage during impact with terrain following a forced landing into a corn field. The aircraft experienced a total loss of engine power after take off from Runway 24 (4,355 feet by 150 feet, concrete/dry) at Iowa City Municipal Airport near Iowa City, Iowa. Visual meteorological conditions prevailed at the time of the accident. The 14 CFR Part 91 local proficiency flight was not operating on a flight plan. The pilot and pilot-rated passenger reported no injuries. The flight originated at Iowa City Municipal Airport at 1210.

The pilot stated that he had performed two take off and landings and taxied for approximately 5 minutes prior to performing the third take off attempt. On the initial climb during the third takeoff, at approximately 350 feet above ground level, the pilot reported that the engine sputtered and quit. He selected the right tank and pumped the wobble pump but the engine gave an additional sputter and quit again. The pilot further described that he then switched back to the left tank but was so low that he had to direct his full attention to executing a safe landing. The aircraft landed in a corn field and reported that the aircraft received substantial damage. In a written statement by the pilot, he reported that there was 38 gallons of 100 Low Lead fuel aboard at last takeoff and that there were no unusual vibrations of noises from the engine.

Examination of the aircraft by a Federal Aviation Administration maintenance inspector found the fuel selector was selected to the left main fuel tank and the left main fuel tank was 3/4 full of a light blue colored fuel. The right tank was empty and the 20 gallon auxiliary fuel tank was estimated to be 1/2-3/4 full of fuel.

The engine, Teledyne Continental E185-11, serial number 26643-D-8-11, was shipped to Teledyne Continental Motors for examination and testing under the supervision of the National Transportation Safety Board. The testing and examination revealed no anomalies.

The Beechcraft B35 standard fuel system has two 20 gallon tanks in the wings, of which 34 gallons is usable. Additionally, the optional 20 gallon auxiliary tank has a usable fuel of 19 gallons. The limitations section of the Beechcraft B35 Pilot's Operating Handbook (POH) states, "Do not take off when the Fuel Quantity Gages indicate in the Yellow Band or with less than 10 gallons in each main tank.". Furthermore, the systems description of fuel tank selection in the POH states, "In no case should a take-off be made ... with less than 10 gallons of fuel in each main tank.

Aircraft

Registration
N5210C
Reported as
Beech B35
Category
Airplane
Serial number
2555
Airframe hours
4,200
Engine
Continental E-185-11, 185 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Gordon Aircraft Inc
Airworthiness certificate
Standard, Normal
Departed
IOW
Airport
IOW · Iowa City Municipal, runway 24, 4,355 × 150 ft, concrete

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
52
Certificates
Airline transport, Commercial
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Left
Flight hours
11,800 total · 75 in this make and model · 11,000 as pilot in command · 50 in the last 90 days · 20 in the last 30 days · 2 in the last 24 hours

Weather

Conditions
Visual (VMC) · Dawn
Wind
200° at 10 knots
Visibility
6 statute miles
Lowest ceiling
None
Temperature
84 °F, dew point 72 °F
Altimeter
29.00 inHg
Observed at
IOW, 1 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.