19970429006969A

Accident · Substantial damage

FAA accident report · Beech 35-C33 · Carrollton, GA · April 29, 1997

Date
April 29, 1997 · 11:30 local
Place
Carrollton, GA
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N5863S
NTSB investigation
NTSBATL97LA069
Reported as
Beech 35C33
Reported engine
Continental IO520*
People aboard
2
Fatal injuries
0
Pilot’s flight hours
847 total453 in this make and model10 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.

Lost partial powr. Stall landed ctj. Prop pitch control arm seperated. Recent annual. Service bulletin not done. (-23) pilot lost control of propeller pitch due to physical disconnect at governor control. High pitch angle resulting from that disconnect did not provide desired power and pilot requested ATC assist to nearest airport. Descent through clouds and alignment with runway was highly successful, but power was insufficent on final and stretching glide caused full stall, hard landing. Wing (left) struck pavement hard enough to create 1-inch wrinkles in top surface extending diagonally from tip to trail edge.

As the FAA filed it

LOST PARTIAL POWR. STALL LANDED CTJ. PROP PITCH CONTROL ARM SEPERATED. RECENT ANNUAL. SERVICE BULLETIN NOT DONE. (-23) PILOT LOST CONTROL OF PROPELLER PITCH DUE TO PHYSICAL DISCONNECT AT GOVERNOR CONTROL. HIGH PITCH ANGLE RESULTING FROM THAT DISCONNECT DID NOT PROVIDE DESIRED POWER AND PILOT REQUESTED ATC ASSIST TO NEAREST AIRPORT. DESCENT THROUGH CLOUDS AND ALIGNMENT WITH RUNWAY WAS HIGHLY SUCCESSFUL, BUT POWER WAS INSUFFICENT ON FINAL AND STRETCHING GLIDE CAUSED FULL STALL, HARD LANDING. WING (LEFT) STRUCK PAVEMENT HARD ENOUGH TO CREATE 1-INCH WRINKLES IN TOP SURFACE EXTENDING DIAGONALLY FROM TIP TO TRAIL EDGE.

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 N5863S · 1

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