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March 21, 1993 · Christen Industries Pitts S1-T · N218MC

Naples, FL

Overview

Report Status
Probable Cause
Event Type
Accident
Date
March 21, 1993
Injury Outcomes
1 injury (1 minor injury)
Location
Naples, FL
Aircraft
Christen Industries Pitts S1-T
Tail Number
N218MC
Operator
Cutshaw Michael H
Injuries
Minor
Aircraft Damage
Substantial
NTSB Number
MIA93LA088

The pilot, who does not hold an airframe or powerplant mechanic's license, stated he installed a straight air intake tube on his aircraft. This tube did not have any means for alternate air or filtering of incoming air. He further modified the tube by installing a screen and a piece of air filtering material in the tube. During the first takeoff after the modification, the aircraft climbed to 200 feet, at which time the manifold pressure dropped and the engine lost power. He was unable to maintain altitude and the aircraft touched down hard on the runway and nosed over inverted. Postcrash examination and testing of the intake tube was performed by an FAA inspector. When a vacuum cleaner was attached to the engine side of the intake tube and turned on, the air flow through the tube was normal for several minutes. After this, moisture built up on the air filtering material and the filter collapsed. The vacuum cleaner then began to strain due to lack of air flow.

NTSB Probable Cause

THE INSTALLATION OF AN IMPROPER DESIGNED INTAKE TUBE AND AIR FILTER BY THE NONMECHANIC RATED PILOT-IN-COMMAND, WHICH RESULTED IN MOISTURE BUILD UP AND COLLAPSE OF THE AIR FILTER, WHICH RESULTED IN BLOCKAGE OF AIR FLOW TO THE ENGINE AND LOSS OF ENGINE POWER. CONTRIBUTING TO THE ACCIDENT WAS THE FAILURE OF THE PILOT-IN-COMMAND TO MAINTAIN AIRSPEED AND FLARE PROPERLY DURING A FORCED LANDING.

Full Narrative

THE PILOT, WHO DOES NOT HOLD AN AIRFRAME OR POWERPLANT MECHANIC'S LICENSE STATED HE INSTALLED A STRAIGHT AIR INTAKE TUBE ON HIS AIRCRAFT. THIS TUBE DID NOT HAVE ANY MEANS FOR ALTERNATE AIR OR FILTERING OF INCOMING AIR. HE FURTHER MODIFIED THE TUBE BY INSTALLING A SCREEN AND A PIECE OF AIR FILTERING MATERIAL IN THE TUBE. DURING THE FIRST TAKEOFF AFTER THE MODIFICATION THE AIRCRAFT CLIMBED TO 200 FEET, AT WHICH TIME THE MANIFOLD PRESSURE DROPPED AND THE ENGINE LOST POWER. HE WAS UNABLE TO MAINTAIN ALTITUDE AND THE AIRCRAFT TOUCHED DOWN HARD ON THE RUNWAY AND NOSED OVER INVERTED. POSTCRASH EXAMINATION AND TESTING OF THE INTAKE TUBE WAS PERFORMED BY AN FAA INSPECTOR. WHEN A VACUUM CLEANER WAS ATTACHED TO THE ENGINE SIDE OF THE INTAKE TUBE AND TURNED ON THE AIR FLOW THROUGH THE TUBE WAS NORMAL FOR SEVERAL MINUTES. AFTER THIS, MOISTURE BUILT UP ON THE AIR FILTERING MATERIAL AND THE FILTER COLLAPSED. THE VACUUM CLEANER THEN BEGAN TO STRAIN DUE TO LACK OF AIR FLOW.

Flight

Event TypeAccident
Event Time11:42 EST
Nearest AirportNaples Municipal (1nm NE)
Runway4
Runway Length5000 ft
Runway Width150 ft
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftChristen Industries Pitts S1-T
Tail NumberN218MC
Aircraft CategoryAir
DamageSubstantial
OperatorCutshaw Michael H
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · AEIO-360 · Reciprocating · 200
Seats1

People & Injuries

Injury Summary1 injury (1 minor injury)
Fatal0
Serious0
Minor1
Uninjured0
Total1
Crew 1Age 38 · First Class

Conditions

ConditionsVMC
LightDaylight
Wind100° @ 3 kt
Visibility10 sm
CeilingBroken clouds 4000 ft
Temperature / Dew Point66 F
Altimeter30.00 inHg
Observation Time16:42
Weather SourceWFAC

Appendix: Source Data