19950327009029I

Incident · Minor damage

FAA incident report · Beech 1900D · Phoenix, AZ · March 27, 1995

Date
March 27, 1995 · 13:25 local
Place
Phoenix, AZ
Airport
Phoenix Sky Harbor International
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
Air taxi and commuter (Part 135)
Operator
MASA
Damage
Minor damage
Aircraft
N93ZV
Reported as
Beech 1900D
People aboard
18
Fatal injuries
0
Pilot’s flight hours
8,200 total6,000 in this make and model300 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 March 27, 1995, a BE-1900D, N93ZV, operated by mesa airlines as flight 5012, departed Phoenix sky Harbor at approximately 1318 MST. After departure a passenger noted the #2 engine upper cowling was loose and informed the crew, the aircraft returned to phx using rwy 26R. Upon landing and application of the propeller reverse pitch, the engine cowling was drawn into the propeller causing the separation of two (2) blades of the 4 bladed propeller. The aircraft received minor damage to the right wing leading edge and outboard winglet. The aircraft had undergone maintenance prior to departure on the #2 engine fire loop system by mechanics employed by dyn air tech of AZ, inc.

As the FAA filed it

NARRATIVE: ON MARCH 27, 1995, A BE-1900D, N93ZV, OPERATED BY MESA AIRLINES AS FLIGHT 5012, DEPARTED PHOENIX SKY HARBOR AT APPROXIMATELY 1318 MST. AFTER DEPARTURE A PASSENGER NOTED THE #2 ENGINE UPPER COWLING WAS LOOSE AND INFORMED THE CREW, THE AIRCRAFT RETURNED TO PHX USING RWY 26R. UPON LANDING AND APPLICATION OF THE PROPELLER REVERSE PITCH, THE ENGINE COWLING WAS DRAWN INTO THE PROPELLER CAUSING THE SEPARATION OF TWO (2) BLADES OF THE 4 BLADED PROPELLER. THE AIRCRAFT RECEIVED MINOR DAMAGE TO THE RIGHT WING LEADING EDGE AND OUTBOARD WINGLET. THE AIRCRAFT HAD UNDERGONE MAINTENANCE PRIOR TO DEPARTURE ON THE #2 ENGINE FIRE LOOP SYSTEM BY MECHANICS EMPLOYED BY DYN AIR TECH OF AZ, INC.