20240731010469A

Accident · Substantial damage

FAA accident report · Cirrus Design SR20 · Egg Harbor Twp, NJ · July 31, 2024

Date
July 31, 2024 · 15:40 local
Place
Egg Harbor Twp, NJ
Phase of flight
Takeoff: Climb Out
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N124RR
NTSB investigation
NTSBERA24LA333
Reported as
Cirrus Design SR20
Reported engine
Lycoming IO-390-C3B6
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Unknown or foreign certificate
Pilot’s flight hours
198 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.

On climb out at 2500 feet, the aircraft experienced a partial loss of engine power, engine power was restored momentarily followed by loss of engine power again.

The pilot elected to deploy the ballistic parachute system for the emergency landing.

The aircraft impacted trees before landing causing substantial damage to the aircraft which included the empenage separated from the fuselage, damage to both leading edges of the wings and both propeller blades bent.

An amendment will follow once further information is identified.

As the FAA filed it

ON CLIMB OUT AT 2500 FEET, THE AIRCRAFT EXPERIENCED A PARTIAL LOSS OF ENGINE POWER, ENGINE POWER WAS RESTORED MOMENTARILY FOLLOWED BY LOSS OF ENGINE POWER AGAIN.

THE PILOT ELECTED TO DEPLOY THE BALLISTIC PARACHUTE SYSTEM FOR THE EMERGENCY LANDING.

THE AIRCRAFT IMPACTED TREES BEFORE LANDING CAUSING SUBSTANTIAL DAMAGE TO THE AIRCRAFT WHICH INCLUDED THE EMPENAGE SEPARATED FROM THE FUSELAGE, DAMAGE TO BOTH LEADING EDGES OF THE WINGS AND BOTH PROPELLER BLADES BENT.

AN AMENDMENT WILL FOLLOW ONCE FURTHER INFORMATION IS IDENTIFIED.

NTSB investigation

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