20021019030019I

Incident · Minor damage

FAA incident report · Beech 1900D · Little Rock, AR · October 19, 2002

Date
October 19, 2002 · 08:58 local
Place
Little Rock, AR
Phase of flight
Normal Cruise
Operating rules
Air carrier (Part 121)
Operator
AMWA
Damage
Minor damage
Aircraft
N127ZV
Reported as
Beech 1900D
Reported engine
Pratt & Whitney PT6A67D
People aboard
16
Fatal injuries
0

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) On October 19, 2002 at 0858 central daylight time a Beechcraft 1900D reported sheet metal peeling off the right engine. The aircraft made an uneventful landing at Little Rock adams field. The airplane was registered to mesa airlines inc. of phoenix Arizona. The flight crew of 2 and 14 passengers were not injured during the incident. Subsequent investigation and maintenance revealed that a lightning strike blew off a rivet head and put a hole in the leading edge of the panel, causing the panel to lift up into the air stream further damaging the panel. A new panel was installed and the aircraft was approved for return to service.

As the FAA filed it

(-23) ON OCTOBER 19, 2002 AT 0858 CENTRAL DAYLIGHT TIME A BEECHCRAFT 1900D REPORTED SHEET METAL PEELING OFF THE RIGHT ENGINE. THE AIRCRAFT MADE AN UNEVENTFUL LANDING AT LITTLE ROCK ADAMS FIELD. THE AIRPLANE WAS REGISTERED TO MESA AIRLINES INC. OF PHOENIX ARIZONA. THE FLIGHT CREW OF 2 AND 14 PASSENGERS WERE NOT INJURED DURING THE INCIDENT. SUBSEQUENT INVESTIGATION AND MAINTENANCE REVEALED THAT A LIGHTNING STRIKE BLEW OFF A RIVET HEAD AND PUT A HOLE IN THE LEADING EDGE OF THE PANEL, CAUSING THE PANEL TO LIFT UP INTO THE AIR STREAM FURTHER DAMAGING THE PANEL. A NEW PANEL WAS INSTALLED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.