20050405005519A

Accident · Substantial damage

FAA accident report · Cessna 152 · Jacksonville, NC · April 5, 2005

Date
April 5, 2005 · 11:05 local
Place
Jacksonville, NC
Airport
Albert J Ellis
Phase of flight
Forced/Precautionary Landing
Operating rules
General operating rules (Part 91)
Operator
JQWS
Damage
Substantial damage
Aircraft
N48820
NTSB investigation
NTSBATL05LA071
Reported as
Cessna 152
Reported engine
Lycoming O235L2C
People aboard
2
Fatal injuries
0
Pilot’s flight hours
5,000 total30 in this make and model120 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.

(-23) Aircraft was departing rwy 23 at oaj on an instructional flight when at approx. 150' engine lost power and PIC elected to shut down engine and land straight ahead. Aircraft came to rest in the grass over-run area adjacent to the runway approach lighting system. Damage to airframe included a bent prop, collapsed NLG, bent r/s wing tip, buckled wing near rear spar attach point, and damaged firewall. Further investigation revealed a broken carburetor mixture control cable. Engine timing, induction, exhaust, valve train and accys were inspected and found to be installed properly and functioning as designed

As the FAA filed it

(-23) AIRCRAFT WAS DEPARTING RWY 23 AT OAJ ON AN INSTRUCTIONAL FLIGHT WHEN AT APPROX. 150' ENGINE LOST POWER AND PIC ELECTED TO SHUT DOWN ENGINE AND LAND STRAIGHT AHEAD. AIRCRAFT CAME TO REST IN THE GRASS OVER-RUN AREA ADJACENT TO THE RUNWAY APPROACH LIGHTING SYSTEM. DAMAGE TO AIRFRAME INCLUDED A BENT PROP, COLLAPSED NLG, BENT R/S WING TIP, BUCKLED WING NEAR REAR SPAR ATTACH POINT, AND DAMAGED FIREWALL. FURTHER INVESTIGATION REVEALED A BROKEN CARBURETOR MIXTURE CONTROL CABLE. ENGINE TIMING, INDUCTION, EXHAUST, VALVE TRAIN AND ACCYS WERE INSPECTED AND FOUND TO BE INSTALLED PROPERLY AND FUNCTIONING AS DESIGNED

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 N48820 · 1

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