20140810014459A

Accident · Substantial damage

FAA accident report · Dehavilland DHC-8-102 · Harrisburg, PA · August 10, 2014

Date
August 10, 2014 · 06:30 local
Place
Harrisburg, PA
Airport
Harrisburg International
Phase of flight
Takeoff: Departure Roll
Operating rules
Air carrier (Part 121)
Operator
HNAA
Damage
Substantial damage
Aircraft
N815EX
NTSB investigation
NTSBDCA14CA147
Reported as
Dehavilland DHC-8-102
Reported engine
Pratt & Whitney Canada PW120
People aboard
26
Fatal injuries
0
Other injuries
0
Pilot’s certificates
Airline transport, flight instructor
Pilot’s flight hours
36,000 total18,000 in this make and model205 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.

During take off roll at approx 40 knots IAS aircraft encountered a flock of geese striking several causing approx 17 inches of 1 propeller blade to separate striking the right of the fuselage at the cabin window at approx station 300, resulting in the failure of both the outer cabin window and center window. Also causing severe damage to the right side of the aircraft iceshield and fuselage between frames X291.4 and X312.35. Also caused the cracking of a second propeller blade.

As the FAA filed it

DURING TAKE OFF ROLL AT APPROX 40 KNOTS IAS AIRCRAFT ENCOUNTERED A FLOCK OF GEESE STRIKING SEVERAL CAUSING APPROX 17 INCHES OF 1 PROPELLER BLADE TO SEPARATE STRIKING THE RIGHT OF THE FUSELAGE AT THE CABIN WINDOW AT APPROX STATION 300, RESULTING IN THE FAILURE OF BOTH THE OUTER CABIN WINDOW AND CENTER WINDOW. ALSO CAUSING SEVERE DAMAGE TO THE RIGHT SIDE OF THE AIRCRAFT ICESHIELD AND FUSELAGE BETWEEN FRAMES X291.4 AND X312.35. ALSO CAUSED THE CRACKING OF A SECOND PROPELLER BLADE.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.

Other reports on N815EX · 3

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