20110905018739A

Accident · Substantial damage

FAA accident report · Cessna 170A · Anchorage, AK · September 5, 2011

Date
September 5, 2011 · 12:40 local
Place
Anchorage, AK
Airport
Lake Hood Strip
Phase of flight
Landing: Rollout
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N5406C
NTSB investigation
NTSBANC11CA095
Reported as
Cessna 170A
Reported engine
Continental C145 series
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Private pilot
Pilot’s flight hours
92 total75 in this make and model75 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.

privacy data omitted Lost the use of his left brake during landing at Lake Hood Strip. As the airplane slowed the rudder became ineffective for steering and only the right brake was operational. The airplane went past the end of the runway at a slow speed, the wheels hit a soft, marshy area causing the airplane to tip over on its back causing damage to the top of the rudder, the left wing tip and bending both propeller blades. It was discovered that the left brakeline flare cracked at the upper fuselage hydraulic fitting causing the hydraulic fluid to leak out. Brake pressure was then unavailable.privacy data omitted Stated that the brakes were fully operational when he completed his run-up checks prior to take-off. He then flew 3.8 hours before landing back at Lake Hood Strip where this event occured.

As the FAA filed it

^PRIVACY DATA OMITTED^ LOST THE USE OF HIS LEFT BRAKE DURING LANDING AT LAKE HOOD STRIP. AS THE AIRPLANE SLOWED THE RUDDER BECAME INEFFECTIVE FOR STEERING AND ONLY THE RIGHT BRAKE WAS OPERATIONAL. THE AIRPLANE WENT PAST THE END OF THE RUNWAY AT A SLOW SPEED, THE WHEELS HIT A SOFT, MARSHY AREA CAUSING THE AIRPLANE TO TIP OVER ON ITS BACK CAUSING DAMAGE TO THE TOP OF THE RUDDER, THE LEFT WING TIP AND BENDING BOTH PROPELLER BLADES.IT WAS DISCOVERED THAT THE LEFT BRAKELINE FLARE CRACKED AT THE UPPER FUSELAGE HYDRAULIC FITTING CAUSING THE HYDRAULIC FLUID TO LEAK OUT. BRAKE PRESSURE WAS THEN UNAVAILABLE.^PRIVACY DATA OMITTED^ STATED THAT THE BRAKES WERE FULLY OPERATIONAL WHEN HE COMPLETED HIS RUN-UP CHECKS PRIOR TO TAKE-OFF. HE THEN FLEW 3.8 HOURS BEFORE LANDING BACK AT LAKE HOOD STRIP WHERE THIS EVENT OCCURED.

NTSB investigation

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