20040927035139A

Accident · Substantial damage

FAA accident report · Blanca 17-30A · Roanoke, TX · September 27, 2004

Date
September 27, 2004 · 11:20 local
Place
Roanoke, TX
Phase of flight
Forced/Precautionary Landing
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N28086
NTSB investigation
NTSBDFW05CA021
Reported as
Blanca 1730A
Reported engine
Continental IO520*
People aboard
1
Fatal injuries
0
Pilot’s flight hours
1,500 total475 in this make and model6 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) N28086 departed northwest regional airport (52F) northbound. During climbout the aircraft experienced a partial power loss. The pilot switched fuel tanks and turned on the electric boost pump. The pilot reported that the electric boost pump seemed to briefly gie a little more power but that he was unable to maintain altitude. The aircraft landed hard in a pasture resulting in minor damage to the aircraft. The pilot was the sole occupant and was not injured. An inspection of the aircraft revealed that the mixture control cable was not connected. The engine was run with no indication of any mechanical irregularity. (-23 amendment) aircraft has substantial damage to left wing forward spar and landing gear fittings, fuselage lower longerons damaged, aircraft is totaled.

As the FAA filed it

(-23) N28086 DEPARTED NORTHWEST REGIONAL AIRPORT (52F) NORTHBOUND. DURING CLIMBOUT THE AIRCRAFT EXPERIENCED A PARTIAL POWER LOSS. THE PILOT SWITCHED FUEL TANKS AND TURNED ON THE ELECTRIC BOOST PUMP. THE PILOT REPORTED THAT THE ELECTRIC BOOST PUMP SEEMED TO BRIEFLY GIE A LITTLE MORE POWER BUT THAT HE WAS UNABLE TO MAINTAIN ALTITUDE. THE AIRCRAFT LANDED HARD IN A PASTURE RESULTING IN MINOR DAMAGE TO THE AIRCRAFT. THE PILOT WAS THE SOLE OCCUPANT AND WAS NOT INJURED. AN INSPECTION OF THE AIRCRAFT REVEALED THAT THE MIXTURE CONTROL CABLE WAS NOT CONNECTED. THE ENGINE WAS RUN WITH NO INDICATION OF ANY MECHANICAL IRREGULARITY. (-23 AMENDMENT) AIRCRAFT HAS SUBSTANTIAL DAMAGE TO LEFT WING FORWARD SPAR AND LANDING GEAR FITTINGS, FUSELAGE LOWER LONGERONS DAMAGED, AIRCRAFT IS TOTALED.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.