19970429011039A

Accident · Substantial damage

FAA accident report · Beech D35 · Lexington, KY · April 29, 1997

Date
April 29, 1997 · 13:30 local
Place
Lexington, KY
Airport
Blue Grass
Phase of flight
Normal Cruise
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N5985C
NTSB investigation
NTSBCHI97LA119
Reported as
Beech D35
Reported engine
Continental E2258
People aboard
2
Fatal injuries
0
Pilot’s flight hours
2,000 total25 in this make and model25 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.

Tail flutter enroute. Reduced power landed lex. To check. Tail inspecttion plated came loose. Tail skin lonerons bent. (-23) while in cruise flight, owner/pilot encountered occasional light turbulence. Two occasions initiated severe airframe vibrations, which ceased when power and speed were reduced. Aircraft diverted to lex with normal landing and no injuries. Damage was found in aft fuselage, vicinity of sta 250 to sta 272: creasing and wrinkling of skin, loss of retaining screws on an inspection plate, distortion of stringers, bending, distortion and cracks in bulkheads at sta 256.9 and 272, and skin on lower surface torn loose at sta 272. Aircraft was operated within limitations, and aircraft logbook indicates aircraft was maintained in accordance with FARS, including compliance with applicable airworthiness directives. Control flutter at the ruddervators occured. Cause is undetermined.

As the FAA filed it

TAIL FLUTTER ENROUTE. REDUCED POWER LANDED LEX. TO CHECK. TAIL INSPECTTION PLATED CAME LOOSE. TAIL SKIN LONERONS BENT. (-23) WHILE IN CRUISE FLIGHT, OWNER/PILOT ENCOUNTERED OCCASIONAL LIGHT TURBULENCE. TWO OCCASIONS INITIATED SEVERE AIRFRAME VIBRATIONS, WHICH CEASED WHEN POWER AND SPEED WERE REDUCED. AIRCRAFT DIVERTED TO LEX WITH NORMAL LANDING AND NO INJURIES. DAMAGE WAS FOUND IN AFT FUSELAGE, VICINITY OF STA 250 TO STA 272: CREASING AND WRINKLING OF SKIN, LOSS OF RETAINING SCREWS ON AN INSPECTION PLATE, DISTORTION OF STRINGERS, BENDING, DISTORTION AND CRACKS IN BULKHEADS AT STA 256.9 AND 272, AND SKIN ON LOWER SURFACE TORN LOOSE AT STA 272. AIRCRAFT WAS OPERATED WITHIN LIMITATIONS, AND AIRCRAFT LOGBOOK INDICATES AIRCRAFT WAS MAINTAINED IN ACCORDANCE WITH FARS, INCLUDING COMPLIANCE WITH APPLICABLE AIRWORTHINESS DIRECTIVES. CONTROL FLUTTER AT THE RUDDERVATORS OCCURED. CAUSE IS UNDETERMINED.

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 N5985C · 1

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