19971127035739A

Accident · Destroyed

FAA accident report · Beech S35 · Chatham, MA · November 27, 1997

Date
November 27, 1997 · 11:40 local
Place
Chatham, MA
Airport
Chatham Municipal Airport
Phase of flight
To Init Climb(1st Pwr Reduct)
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N5667K
NTSB investigation
NTSBNYC98FA034
Reported as
Beech S35
Reported engine
Continental IO520*
People aboard
2
Fatal injuries
2
Pilot’s flight hours
2,400 total1,400 in this make and model

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.

(Tty) acft crashed und unk circ while landing, pilot suffer fatal inj, pass serious inj, Chatham, MA. (.4)according to the passengers, the airplane landed on runway 24. The wind 'affected the airplane,' and the pilot aborted the landing. The initial climb was normal, and the engine produced maximum power. Then, an 'unknown force slam[med] the left wing down,' and the airplane rolled approximately 90 degrees. The airplane descended toward a pond and impacted trees. One of the passengers heard the stall warning horn after the upset, but said she did not feel a stall; it was 'more of a violent down draft forcing the left wing down.' Several witnesses reported observing the airplane at the departure end of runway 24 in a climb, just above the trees, when it banked 90 degrees left and descended into the trees. The witnesses also reported hearing the engine, and stated that it sounded loud. The reported winds at the time of the accident were from 290 degrees at 17 knots, gusting to 33 knots, with a peak gust of 42 knots. Examination of the airplane and engine did not reveal any evidence of a mechanical malfunction. (-23) see narrative # NYC98FA034.

As the FAA filed it

(TTY) ACFT CRASHED UND UNK CIRC WHILE LANDING, PILOT SUFFER FATAL INJ, PASS SERIOUS INJ, CHATHAM, MA. (.4)ACCORDING TO THE PASSENGERS, THE AIRPLANE LANDED ON RUNWAY 24. THE WIND 'AFFECTED THE AIRPLANE,' AND THE PILOT ABORTED THE LANDING. THE INITIAL CLIMB WAS NORMAL, AND THE ENGINE PRODUCED MAXIMUM POWER. THEN, AN 'UNKNOWN FORCE SLAM[MED] THE LEFT WING DOWN,' AND THE AIRPLANE ROLLED APPROXIMATELY 90 DEGREES. THE AIRPLANE DESCENDED TOWARD A POND AND IMPACTED TREES. ONE OF THE PASSENGERS HEARD THE STALL WARNING HORN AFTER THE UPSET, BUT SAID SHE DID NOT FEEL A STALL; IT WAS 'MORE OF A VIOLENT DOWN DRAFT FORCING THE LEFT WING DOWN.' SEVERAL WITNESSES REPORTED OBSERVING THE AIRPLANE AT THE DEPARTURE END OF RUNWAY 24 IN A CLIMB, JUST ABOVE THE TREES, WHEN IT BANKED 90 DEGREES LEFT AND DESCENDED INTO THE TREES. THE WITNESSES ALSO REPORTED HEARING THE ENGINE, AND STATED THAT IT SOUNDED LOUD. THE REPORTED WINDS AT THE TIME OF THE ACCIDENT WERE FROM 290 DEGREES AT 17 KNOTS, GUSTING TO 33 KNOTS, WITH A PEAK GUST OF 42 KNOTS. EXAMINATION OF THE AIRPLANE AND ENGINE DID NOT REVEAL ANY EVIDENCE OF A MECHANICAL MALFUNCTION. (-23) SEE NARRATIVE # NYC98FA034.

NTSB investigation

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