20080529835279I

Incident · Minor damage

FAA incident report · Cessna 441 · Anchorage, AK · May 29, 2008

Date
May 29, 2008 · 14:15 local
Place
Anchorage, AK
Airport
Ted Stevens Anchorage International
Phase of flight
Normal Cruise
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N441SA
Reported as
Cessna 441
Reported engine
Garrett TPE33110N
People aboard
1
Fatal injuries
0
Pilot’s flight hours
14,650 total6,100 in this make and model155 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) The following narrative information is provided by the carrier's personnel: maintenance personnel previously installed a 4 bladed propeller per supplemental type certificate SA00058T. The maintenacne check flight required the pilot to shut down each engine individually. Approximately 5-10 seconds after shutting down the left engine, smoke appeared from beneath the switch panel left of the pilot's seat. Partial electrical system failures that included landing gear and flaps extension being inop was expeerienced by the pilot. Emergency landing gear extension procedures were followed and an emergency was declared by the pilot to the ted Stevens international airport tower. Pilot attempted to restart the lt engine without success. A succesful single engine, no-flap landing was accomplished. Maintenance personnel later found that the installation instructions for STC SA00058AT were not followed correctly. This resulted in an overloaded electrical circuit that caused smoke in the cockpit with partial electrical system failure.

As the FAA filed it

(-23) THE FOLLOWING NARRATIVE INFORMATION IS PROVIDED BY THE CARRIER'S PERSONNEL: MAINTENANCE PERSONNEL PREVIOUSLY INSTALLED A 4 BLADED PROPELLER PER SUPPLEMENTAL TYPE CERTIFICATE SA00058T. THE MAINTENACNE CHECK FLIGHT REQUIRED THE PILOT TO SHUT DOWN EACH ENGINE INDIVIDUALLY. APPROXIMATELY 5-10 SECONDS AFTER SHUTTING DOWN THE LEFT ENGINE, SMOKE APPEARED FROM BENEATH THE SWITCH PANEL LEFT OF THE PILOT'S SEAT. PARTIAL ELECTRICAL SYSTEM FAILURES THAT INCLUDED LANDING GEAR AND FLAPS EXTENSION BEING INOP WAS EXPEERIENCED BY THE PILOT. EMERGENCY LANDING GEAR EXTENSION PROCEDURES WERE FOLLOWED AND AN EMERGENCY WAS DECLARED BY THE PILOT TO THE TED STEVENS INTERNATIONAL AIRPORT TOWER. PILOT ATTEMPTED TO RESTART THE LT ENGINE WITHOUT SUCCESS. A SUCCESFUL SINGLE ENGINE, NO-FLAP LANDING WAS ACCOMPLISHED. MAINTENANCE PERSONNEL LATER FOUND THAT THE INSTALLATION INSTRUCTIONS FOR STC SA00058AT WERE NOT FOLLOWED CORRECTLY. THIS RESULTED IN AN OVERLOADED ELECTRICAL CIRCUIT THAT CAUSED SMOKE IN THE COCKPIT WITH PARTIAL ELECTRICAL SYSTEM FAILURE.

Other reports on N441SA · 1

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