20191202022139I

Incident · Minor damage

FAA incident report · Beech F90 · Myrtle Beach, SC · December 2, 2019

Date
December 2, 2019 · 09:31 local
Place
Myrtle Beach, SC
Airport
Myrtle Beach International
Phase of flight
Cruise/Level Flight
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N960V
Reported as
Beech F90
Reported engine
Pratt & Whitney Canada PT6A-135
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Commercial pilot
Pilot’s flight hours
6,127 total

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 cruise at FL230, the copilot side windshield suddenly cracked (as shown in picture above). Windshield heat was on normal as per the checklist and recommended procedures for high altitude flight. Pilot requested lower altitude from center and stated that the aircraft had broken a windshield. Pilot later clarified that it was cracked. Pilot made a controlled descent down to 11,000 MSL and then further descent to final landing at planned destination of myr. Checklist states no other action is necessary other than a descent if it is the inner panel. Pilot wanted to stay below 12,500 due to oxygen requirements in case the windshield completely blew out or cabin pressurization was lost. The cabin pressure slowly rose to actual flight level due to a small hole in the windshield but not until 11,000 MSL. Descent and landing were uneventful.

As the FAA filed it

DURING CRUISE AT FL230, THE COPILOT SIDE WINDSHIELD SUDDENLY CRACKED (AS SHOWN IN PICTURE ABOVE). WINDSHIELD HEAT WAS ON NORMAL AS PER THE CHECKLIST AND RECOMMENDED PROCEDURES FOR HIGH ALTITUDE FLIGHT. PILOT REQUESTED LOWER ALTITUDE FROM CENTER AND STATED THAT THE AIRCRAFT HAD BROKEN A WINDSHIELD. PILOT LATER CLARIFIED THAT IT WAS CRACKED. PILOT MADE A CONTROLLED DESCENT DOWN TO 11,000 MSL AND THEN FURTHER DESCENT TO FINAL LANDING AT PLANNED DESTINATION OF MYR. CHECKLIST STATES NO OTHER ACTION IS NECESSARY OTHER THAN A DESCENT IF IT IS THE INNER PANEL. PILOT WANTED TO STAY BELOW 12,500 DUE TO OXYGEN REQUIREMENTS IN CASE THE WINDSHIELD COMPLETELY BLEW OUT OR CABIN PRESSURIZATION WAS LOST. THE CABIN PRESSURE SLOWLY ROSE TO ACTUAL FLIGHT LEVEL DUE TO A SMALL HOLE IN THE WINDSHIELD BUT NOT UNTIL 11,000 MSL. DESCENT AND LANDING WERE UNEVENTFUL.

Other reports on N960V · 2

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