19980421009839I

Incident · Minor damage

FAA incident report · Amtr GLASAIR III · Carlsbad, CA · April 21, 1998

Date
April 21, 1998 · 07:20 local
Place
Carlsbad, CA
Airport
Mcclellan-Palomar
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N17S
Reported as
Amtr Glasairiii
Reported engine
Lycoming IO540K1B5
People aboard
1
Fatal injuries
0
Pilot’s flight hours
5,886 total

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.

Narrative: on April 21, 1998, Mr. Craig w. williams, pilot in command of glassair hombuilt N17S, departed crq on a repositioning flight. Following take off the PIC stated that engine throttle commands failed to respond. N17S returned to crq, for landing. During the ensuing high speed landing roll-out, side load forces collapsed N17S nose gear, causing minor damage to the aircraft and no injuries to the PIC. Investigation revealed throttle cable end attachment hardware had separated from the throttle body. Malfunction or defect form 8010-4 submitted. This incident did not involve a pilot deviation or NMAC.

As the FAA filed it

NARRATIVE: ON APRIL 21, 1998, MR. CRAIG W. WILLIAMS, PILOT IN COMMAND OF GLASSAIR HOMBUILT N17S, DEPARTED CRQ ON A REPOSITIONING FLIGHT. FOLLOWING TAKE OFF THE PIC STATED THAT ENGINE THROTTLE COMMANDS FAILED TO RESPOND. N17S RETURNED TO CRQ, FOR LANDING. DURING THE ENSUING HIGH SPEED LANDING ROLL-OUT, SIDE LOAD FORCES COLLAPSED N17S NOSE GEAR, CAUSING MINOR DAMAGE TO THE AIRCRAFT AND NO INJURIES TO THE PIC. INVESTIGATION REVEALED THROTTLE CABLE END ATTACHMENT HARDWARE HAD SEPARATED FROM THE THROTTLE BODY. MALFUNCTION OR DEFECT FORM 8010-4 SUBMITTED. THIS INCIDENT DID NOT INVOLVE A PILOT DEVIATION OR NMAC.

Other reports on N17S · 2

Matched to the same aircraft by N-number and date.