ASN logo
ASN Wikibase Occurrence # 201885
Last updated: 13 September 2019
This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information. If you feel this information is incomplete or incorrect, you can submit corrected information.

Date:06-JAN-1999
Time:11:30
Type:Silhouette image of generic PA22 model; specific model in this crash may look slightly different
Piper PA-22-108
Owner/operator:Private
Registration: N4542Z
C/n / msn: 22-8047
Fatalities:Fatalities: 0 / Occupants: 1
Other fatalities:0
Aircraft damage: Substantial
Category:Accident
Location:Perry, GA -   United States of America
Phase: Unknown
Nature:Private
Departure airport:68GA
Destination airport:
Investigating agency: NTSB
Narrative:
The pilot stated that shortly after takeoff while climbing through 200 feet, the engine rpm decreased to 1,500 rpm. He changed the throttle settings which had no effect and unable to maintain altitude, he maneuvered the airplane for a forced landing at a nearby sod farm. The airplane stalled, and landed hard just short of the intended touchdown location then nosed over. Examination of the airplane and engine by an FAA Airworthiness Inspector revealed that the fuel selector valve was improperly assembled; no detents could be felt. Also, cold differential compression readings for cylinder Nos. 1, 2, 3, and 4 were recorded to be 20, 19, 54, and 5 psi respectively. The No. 2 cylinder valves were adjusted and the cold compression reading increased to 50 plus psi. Fire damage was noted to the back side of the induction air filter assembly. The carburetor was found to contain a two-piece venturi when by an airworthiness directive, a one-piece venturi is required. The maintenance records indicated that a one-piece venturi was installed. The records also indicated that the rocker arms were adjusted on April 21, 1997. The airplane had accumulated approximately 85 hours since then at the time of the accident.
Probable Cause: The maintenance personnel incorrect adjustment of the intake and exhaust valves resulting in the induction system fire and subsequent loss of engine power.

Sources:

NTSB: https://www.ntsb.gov/_layouts/ntsb.aviation/brief.aspx?ev_id=20001204X00092&key=1


Revision history:

Date/timeContributorUpdates
26-Nov-2017 09:37 ASN Update Bot Added

Corrections or additions? ... Edit this accident description