20000906029429I

Incident · Minor damage

FAA incident report · Amtr GLASAIR · Lubbock, TX · September 6, 2000

Date
September 6, 2000 · 11:50 local
Place
Lubbock, TX
Airport
Lubbock International Airport
Phase of flight
To Init Climb(1st Pwr Reduct)
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N456RB
Reported as
Amtr Glasair
People aboard
1
Fatal injuries
0
Pilot’s flight hours
1,750 total730 in this make and model100 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

(-23)During this personal flight of an experimental (amatuer built) aircraft, under VFR conditions the commerical pilot experienced engine failure after rotation. The flight ended in a cotton field outside of the airport perimeter with the gear up. The pilot who was the sole occupant suffered no injuries and the aircraft sustained only minor damage. Post incident inspection revealed that a clamp that holds the mixture cable had not been properly secured after having been removed during the recent condition inspection. This allowed the mixture cable to move into the path of the nose gear retraction mechanisim. When the nose gear was retracted on takeoff it made contact with the mixture cable and moved it to the idle cut off position which shut doen the engine. This investigation is closed.

As the FAA filed it

(-23)DURING THIS PERSONAL FLIGHT OF AN EXPERIMENTAL (AMATUER BUILT) AIRCRAFT, UNDER VFR CONDITIONS THE COMMERICAL PILOT EXPERIENCED ENGINE FAILURE AFTER ROTATION. THE FLIGHT ENDED IN A COTTON FIELD OUTSIDE OF THE AIRPORT PERIMETER WITH THE GEAR UP. THE PILOT WHO WAS THE SOLE OCCUPANT SUFFERED NO INJURIES AND THE AIRCRAFT SUSTAINED ONLY MINOR DAMAGE. POST INCIDENT INSPECTION REVEALED THAT A CLAMP THAT HOLDS THE MIXTURE CABLE HAD NOT BEEN PROPERLY SECURED AFTER HAVING BEEN REMOVED DURING THE RECENT CONDITION INSPECTION. THIS ALLOWED THE MIXTURE CABLE TO MOVE INTO THE PATH OF THE NOSE GEAR RETRACTION MECHANISIM. WHEN THE NOSE GEAR WAS RETRACTED ON TAKEOFF IT MADE CONTACT WITH THE MIXTURE CABLE AND MOVED IT TO THE IDLE CUT OFF POSITION WHICH SHUT DOEN THE ENGINE. THIS INVESTIGATION IS CLOSED.