20041015028919A

Accident · Substantial damage

FAA accident report · Beech C24R · Hyannis Port, MA · October 15, 2004

Date
October 15, 2004 · 19:45 local
Place
Hyannis Port, MA
Phase of flight
Climb
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N6598C
NTSB investigation
NTSBIAD05LA005
Reported as
Beech C24R
Reported engine
Continental IO360*
People aboard
1
Fatal injuries
0
Pilot’s flight hours
3,190 total40 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) N6598C a BE-23-C24R made a gear up forced landing at the Hyannis Port gulf club due to an engine failure preceded by the odor of smoke being detected in the cockpit by the pilot mark alexander on October 15, 2004 at 1852Z. An inspection of the engine compartment by the FAA revealed that severe fire damage had occurred in the engine compartment aft of the engine accessory baffle up to and including the fire wall. The fuel pressure indicator line from the fuel distribution spider to the fuel pressure indicator was disconnected, allowing fuel to spray from the 45DEG elbow attached to the baffle into the accessory compartment. Note the heavy soot deposits on the fitting and the complete absence of deposits on the hose connector indicating that were not connected. Other damage includes buckled and heat distorted fire wall.

As the FAA filed it

(-23) N6598C A BE-23-C24R MADE A GEAR UP FORCED LANDING AT THE HYANNIS PORT GULF CLUB DUE TO AN ENGINE FAILURE PRECEDED BY THE ODOR OF SMOKE BEING DETECTED IN THE COCKPIT BY THE PILOT MARK ALEXANDER ON OCTOBER 15, 2004 AT 1852Z. AN INSPECTION OF THE ENGINE COMPARTMENT BY THE FAA REVEALED THAT SEVERE FIRE DAMAGE HAD OCCURRED IN THE ENGINE COMPARTMENT AFT OF THE ENGINE ACCESSORY BAFFLE UP TO AND INCLUDING THE FIRE WALL. THE FUEL PRESSURE INDICATOR LINE FROM THE FUEL DISTRIBUTION SPIDER TO THE FUEL PRESSURE INDICATOR WAS DISCONNECTED, ALLOWING FUEL TO SPRAY FROM THE 45DEG ELBOW ATTACHED TO THE BAFFLE INTO THE ACCESSORY COMPARTMENT. NOTE THE HEAVY SOOT DEPOSITS ON THE FITTING AND THE COMPLETE ABSENCE OF DEPOSITS ON THE HOSE CONNECTOR INDICATING THAT WERE NOT CONNECTED. OTHER DAMAGE INCLUDES BUCKLED AND HEAT DISTORTED FIRE WALL.

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 N6598C · 1

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