ATL84LA155

NTSB accident investigation · Cessna 210D · Shaw, MS · April 28, 1984

Accident · Minor injuriesLimited investigationFinal report
Date
April 28, 1984, 10:40 local (16:40 UTC)
Place
Shaw, MS
Injuries
1 minor, 2 uninjured
Damage
Substantial damage
Phase of flight
Approach
Aircraft
N3882YCessna 210D
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
FAA report
19840428014669A
Case key
6446

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.

Airframe/component/system failure/malfunctionApproach - vfr pattern - base leg/base to final
Flight control,flap attachment - previous damageFactor
Flight control,flap attachment - overloadFactor
Flight control,flap surface - asymmetricalFactor
Forced landingDescent - emergency
Control interference - inadvertentPassengerFactor
Anxiety/apprehensionPilot in commandFactor
In-flight planning/decision - improperPilot in commandCause
Pressure induced by othersOther personFactor
Precautionary landing - prematurePilot in commandCause
In flight collision with terrain/waterLanding - flare/touchdown
Wheels up landing - intentionalPilot in commandCause
Nose overLanding - roll
Terrain condition - rough/unevenFactor

Analysis

The acft was landed gear up in a precautionary landing after a control difficulty in flt. On base leg a loud bang was heard and the acft started to roll right. Control forces were heavy so the other plt in the front seat tried to help on the controls. They thought the ailerons had failed, then the plt noticed right flap was up so he started to raise the flaps. He said the other plts inputs confused and alarmed him so he gave in to the pleas of the passengers to 'put it onthe ground'. He raised the gear and touched down before the gear was fully up on plowed ground. The acft slid 200 ft andnosed over. Investigation revealed that the only control problem was the failed push-pull rod (Cessna p/n 120058-2) on the right flap. They failed in overload with a rusted fracture surface on one which indicated some previous damage. These rods were in service 2040 hours. The most recent inspection was an annual 19 tach hours prior to the accident.

Aircraft

Registration
N3882Y
Reported as
Cessna 210D
Category
Airplane
Serial number
21058382
Airframe hours
2,840
Engine
Continental IO-520-A5B, 285 horsepower, reciprocating
Damage
Substantial damage
Flight
Aerial observation · Part 91
Registered owner
Harold C. Tapley
Airworthiness certificate
Standard, Normal
Last inspection
Annual · September 28, 1983 · 19 hours before
Departed
Shaw, MS

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
56
Certificate
Commercial
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Left
Flight hours
13,250 total · 300 in this make and model · 13,250 as pilot in command · 30 in the last 90 days

Weather

Conditions
Visual (VMC) · Day
Wind
140° at 5 knots
Visibility
7 statute miles
Lowest ceiling
3,000 ft broken
Temperature
72 °F, dew point 64 °F
Altimeter
30.00 inHg
Observed at
GWO, 45 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.