19970509026389I

Incident

FAA incident report · Boeing B-17G · Burbank, CA · May 9, 1997

Date
May 9, 1997 · 14:40 local
Place
Burbank, CA
Airport
Burbank-Glendale-Pasadena Airp
Phase of flight
Ground Taxi, Other Airplane
Operating rules
General operating rules (Part 91)
Aircraft
N93012
Reported as
Boeing B17G
People aboard
3
Fatal injuries
0
Pilot’s flight hours
12,000 total5 in this make and model150 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.

Narrative: aircraft was in a left turn when an intermitting hydraulic failure temporarily resulted in loss of brake's to the right wheel. Aircraft continued in a left turn with the tail striking a four foot taxiway sign, knocking it to the ground. No damage to the aircraft. Pilot stated this is a reoccurring problem with the hydraulic system. Ral-fsdo airworthiness responded to chino. Bed-fsdo advised. On 8-4-97 bob collings of the collings foundation was queried by a van nuys FSDO airworthiness inspector. Collings stated that the loss of hydraulic brake pressure on 5-9-97 was due to a popped circuit breaker. Collings also said that the aircraft had had a minimum of 45 flights since this incident with no duplication of this problem. This investigation is closed: yes. M or d no.

As the FAA filed it

NARRATIVE: AIRCRAFT WAS IN A LEFT TURN WHEN AN INTERMITTING HYDRAULIC FAILURE TEMPORARILY RESULTED IN LOSS OF BRAKE'S TO THE RIGHT WHEEL. AIRCRAFT CONTINUED IN A LEFT TURN WITH THE TAIL STRIKING A FOUR FOOT TAXIWAY SIGN, KNOCKING IT TO THE GROUND. NO DAMAGE TO THE AIRCRAFT. PILOT STATED THIS IS A REOCCURRING PROBLEM WITH THE HYDRAULIC SYSTEM. RAL-FSDO AIRWORTHINESS RESPONDED TO CHINO. BED-FSDO ADVISED. ON 8-4-97 BOB COLLINGS OF THE COLLINGS FOUNDATION WAS QUERIED BY A VAN NUYS FSDO AIRWORTHINESS INSPECTOR. COLLINGS STATED THAT THE LOSS OF HYDRAULIC BRAKE PRESSURE ON 5-9-97 WAS DUE TO A POPPED CIRCUIT BREAKER. COLLINGS ALSO SAID THAT THE AIRCRAFT HAD HAD A MINIMUM OF 45 FLIGHTS SINCE THIS INCIDENT WITH NO DUPLICATION OF THIS PROBLEM. THIS INVESTIGATION IS CLOSED: YES. M OR D NO.

Other reports on N93012 · 6

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