N402G

MINR
None

Beech 100 S/N: B-14

Accident Details

Date
Saturday, April 5, 1997
NTSB Number
MIA97IA151
Location
KENLY, NC
Event ID
20001208X07769
Coordinates
35.589851, -78.120384
Aircraft Damage
MINR
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

Inadequate inspection procedures by the airframe manufacturer for failure to require removal of the metal retaining ring to inspect the entire area of the window for cracks.

Aircraft Information

Registration
N402G
Make
BEECH
Serial Number
B-14
Engine Type
Turbo-shaft
Model / ICAO
100 BE10
Aircraft Type
Fixed Wing Multi Engine
No. of Engines
2

Registered Owner (Historical)

Name
I S O AERO SERVICE INC
Address
PO BOX 1294
Status
Deregistered
City
KINSTON
State / Zip Code
NC 28503-1294
Country
United States

Analysis

On April 5, 1997, about 1030 eastern standard time, a Beech 100, N402G, registered to and operated by ISO Aero Service, Inc., experienced failure of the pilot's "D" oversize window while climbing to cruise near Kenly, North Carolina. Visual meteorological conditions prevailed at the time and no flight plan was filed for the 14 CFR Part 91 positioning flight. The airplane sustained minor damage and the airline transport-rated pilot, the sole occupant, was not injured. The flight originated about 15 minutes earlier from the Kinston Regional Jetport at Stallings Field, Kinston, North Carolina.

The pilot stated that while climbing through 12,000 for 12,500 feet, at a cabin differential pressure of 4.3 psi, the pilot's flight compartment side "D" window separated. He diverted to his departure airport and landed uneventfully. At the time of the window separation the cabin altitude was about 2,000 feet.

The remaining portion of the failed window was sent to the NTSB Materials Laboratory in Washington, D.C. Examination of the window revealed evidence of preexisting cracks that originated at the external surface of the window at the transition radius between the window flange and the center portion of the window.

Review of the maintenance records for the airplane revealed that the failed window was installed on February 13, 1986, in accordance with an Airworthiness Directive. At the time of failure, the airplane had accumulated 4,008 hours since the window installation. Further review of the maintenance records revealed that it was last inspected on October 10, 1996. The airplane had accumulated about 240 hours since that inspection at the time of failure. The airframe manufacturer inspection requirements for the failed window does not require the removal of the metal retaining ring to examine the entire area of the window for cracks if none are visually observed on the outer surface of the window during the initial inspection. Additionally, a detailed inspection of the failed window is required by the manufacturer to be accomplished only every 600 hours.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# MIA97IA151