19950228011059I

Incident

FAA incident report · Skrsky S76C · Venice, LA · February 28, 1995

Date
February 28, 1995 · 12:40 local
Place
Venice, LA
Airport
Venice
Phase of flight
Pwr On Vertical Ldng/Rtrcrft
Operating rules
Air taxi and commuter (Part 135)
Operator
HEEA
Aircraft
N1545K
Reported as
Skrsky S76C
Reported engine
Allison 250C30
People aboard
9
Fatal injuries
0
Pilot’s flight hours
16,976 total6,657 in this make and model78 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: on short final to a customer's heliport in Venice, Louisiana aircraft N1545K experienced a large torque split which could not be corrected. Just before landing, the no. 2 engine would not develop full power. During the subsequent landing, the no. 1 engine went to 106% nr, 102% N1, and 110% torque, with a T5 of 805 degrees. Maintenance sprayed contact cleaner on the droop compensator amplifier (dca) and bias motor cannon plugs. A ground run was conducted and the dca check was completed in accordance with flight manual procedures. The check was good and the aircraft was returned to service. There was no damage and no injury. A malfunction or defect report has been submitted.

As the FAA filed it

NARRATIVE: ON SHORT FINAL TO A CUSTOMER'S HELIPORT IN VENICE, LOUISIANA AIRCRAFT N1545K EXPERIENCED A LARGE TORQUE SPLIT WHICH COULD NOT BE CORRECTED. JUST BEFORE LANDING, THE NO. 2 ENGINE WOULD NOT DEVELOP FULL POWER. DURING THE SUBSEQUENT LANDING, THE NO. 1 ENGINE WENT TO 106% NR, 102% N1, AND 110% TORQUE, WITH A T5 OF 805 DEGREES. MAINTENANCE SPRAYED CONTACT CLEANER ON THE DROOP COMPENSATOR AMPLIFIER (DCA) AND BIAS MOTOR CANNON PLUGS. A GROUND RUN WAS CONDUCTED AND THE DCA CHECK WAS COMPLETED IN ACCORDANCE WITH FLIGHT MANUAL PROCEDURES. THE CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. THERE WAS NO DAMAGE AND NO INJURY. A MALFUNCTION OR DEFECT REPORT HAS BEEN SUBMITTED.

Other reports on N1545K · 2

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