20121218027879I

Incident · Minor damage

FAA incident report · Stol UC-1 · Winter Haven, FL · December 18, 2012

Date
December 18, 2012 · 12:30 local
Place
Winter Haven, FL
Airport
Winter Haven
Phase of flight
Taxi
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N9508U
Reported as
Stol UC-1
Reported engine
Lycoming I0360 series
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Private pilot
Pilot’s flight hours
215 total7 in this make and model31 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.

While taxiing to the runway for takeoff, the applicant for a private pilot multiengine land practical test lost directional control of the "twin bee" amphibious aircraft due to loss of effective brake pressure on the left brake while making a right turn with a moderate crosswind from the right side of the aircraft. With no brakes installed on the right side of the cockpit, the pilot examiner conducting the practical test was unable to instantly intervene. Intervention with differential power by the pilot examiner prevented the aircraft from going into a ditch, but the right sponson sustained minor damage from contact with an embankment.a post incident inspection of the aircraft brake system revealed a low level of brake fluid in the left brake master cylinder and air in the left brake line.

As the FAA filed it

WHILE TAXIING TO THE RUNWAY FOR TAKEOFF, THE APPLICANT FOR A PRIVATE PILOT MULTIENGINE LAND PRACTICAL TEST LOST DIRECTIONAL CONTROL OF THE "TWIN BEE" AMPHIBIOUS AIRCRAFT DUE TO LOSS OF EFFECTIVE BRAKE PRESSURE ON THE LEFT BRAKE WHILE MAKING A RIGHT TURN WITH A MODERATE CROSSWIND FROM THE RIGHT SIDE OF THE AIRCRAFT. WITH NO BRAKES INSTALLED ON THE RIGHT SIDE OF THE COCKPIT, THE PILOT EXAMINER CONDUCTING THE PRACTICAL TEST WAS UNABLE TO INSTANTLY INTERVENE. INTERVENTION WITH DIFFERENTIAL POWER BY THE PILOT EXAMINER PREVENTED THE AIRCRAFT FROM GOING INTO A DITCH, BUT THE RIGHT SPONSON SUSTAINED MINOR DAMAGE FROM CONTACT WITH AN EMBANKMENT.A POST INCIDENT INSPECTION OF THE AIRCRAFT BRAKE SYSTEM REVEALED A LOW LEVEL OF BRAKE FLUID IN THE LEFT BRAKE MASTER CYLINDER AND AIR IN THE LEFT BRAKE LINE.