20090917049529A

Accident · Substantial damage

FAA accident report · Grumman G-44A · Anchorage, AK · September 17, 2009

Date
September 17, 2009 · 09:29 local
Place
Anchorage, AK
Phase of flight
Landing: Rollout
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N86627
NTSB investigation
NTSBANC09LA100
Reported as
Grumman G-44A
Reported engine
Continental I0-470 series
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Commercial pilot
Pilot’s flight hours
3,550 total780 in this make and model20 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.

On 9-16-09, the aircraft was flown for a maintenance test flight after maintenance on several items. The RH gear, outboard wheel half had been replaced. The brake cylinders had been rebuilt with new gaskets, and new brake pads. Repaired systems were ground tested and maintenance documented before the test flight. The aircraft was test flown by the pilot with the associated mechanic on board. The aircraft landed on runway 7, and during braking on rollout, the brake on the right side failed, the pedal to the floor. Loss of aircraft braking control (RH) resulted in a veering off the runway to the side grassy area and an aircraft 270 degree ground loop. The aircraft damaged the right wingtip area, the right wing pontoon and supporting struts, and the right wing aileron. Inspection of the failed right side brake system revealed a failed, broken brake hose attach fitting, an to pipe, 1/4 inch, an 823-4D, failed approx. 1 thread below the brake cylinder outer surface.

As the FAA filed it

ON 9-16-09, THE AIRCRAFT WAS FLOWN FOR A MAINTENANCE TEST FLIGHT AFTER MAINTENANCE ON SEVERAL ITEMS. THE RH GEAR, OUTBOARD WHEEL HALF HAD BEEN REPLACED. THE BRAKE CYLINDERS HAD BEEN REBUILT WITH NEW GASKETS, AND NEW BRAKE PADS. REPAIRED SYSTEMS WERE GROUND TESTED AND MAINTENANCE DOCUMENTED BEFORE THE TEST FLIGHT. THE AIRCRAFT WAS TEST FLOWN BY THE PILOT WITH THE ASSOCIATED MECHANIC ON BOARD. THE AIRCRAFT LANDED ON RUNWAY 7, AND DURING BRAKING ON ROLLOUT, THE BRAKE ON THE RIGHT SIDE FAILED, THE PEDAL TO THE FLOOR. LOSS OF AIRCRAFT BRAKING CONTROL (RH) RESULTED IN A VEERING OFF THE RUNWAY TO THE SIDE GRASSY AREA AND AN AIRCRAFT 270 DEGREE GROUND LOOP. THE AIRCRAFT DAMAGED THE RIGHT WINGTIP AREA, THE RIGHT WING PONTOON AND SUPPORTING STRUTS, AND THE RIGHT WING AILERON. INSPECTION OF THE FAILED RIGHT SIDE BRAKE SYSTEM REVEALED A FAILED, BROKEN BRAKE HOSE ATTACH FITTING, AN TO PIPE, 1/4 INCH, AN 823-4D, FAILED APPROX. 1 THREAD BELOW THE BRAKE CYLINDER OUTER SURFACE.

NTSB investigation

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

Other reports on N86627 · 1

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