20080430847369I

Incident · Minor damage

FAA incident report · Cessna 177RG · Griffith, IN · April 30, 2008

Date
April 30, 2008 · 13:00 local
Place
Griffith, IN
Airport
Griffith-Merrillville
Phase of flight
Level Off Touchdown
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N8208G
Reported as
Cessna 177RG
Reported engine
Lycoming IO360LYC*
People aboard
1
Fatal injuries
0
Pilot’s flight hours
3,000 total2,200 in this make and model36 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) Pilot stated he flew a normal traffic pattern and final approach with flaps at 20 degrees. Pilot stated he performed a gump check and check the landing gear position 3 times. At about 4', over the numbers, he felt the aircraft sink. He added power and flew further down the ruway. About the time he expected to touch down he felt a severe shaking of the aircraft. He pulled back on the control wheel thinking he may have lost a wheel. He then heard and felt a "bam, bam bam" and the prop stopped vertical. The aircraft slid to stop, on its belly, slightly off the right side of the runway at 45 degree angle to the runway heading. Propeller marks on the runway are consistent with the pilot's statement regarding a "severe shaking" and then pulling back on the control wheel and then hearing the "bam, bam, bam." The propeller marks start approximately 2000' from the approach end of the runway and continue for approximately 100' then cease for approximately 20', a reappear and continue, gradually growing fainter. There are no scuff marks on the tires or skid marks on the runway that would indicate an intransient, partially extended (retracted) landing gear. Landing gear was cycled several times. The landing gear operated smoothly, without hesitation and locked into the selected position. Initially the landing gear warning horn did not operate with the landing gear in the up and locked position and the throttle retarded to idle. A mechanic manipulted the mechanism at the throttle body and the warning horn sounded each time the throttle was retarded to idle.

As the FAA filed it

(-23) PILOT STATED HE FLEW A NORMAL TRAFFIC PATTERN AND FINAL APPROACH WITH FLAPS AT 20 DEGREES. PILOT STATED HE PERFORMED A GUMP CHECK AND CHECK THE LANDING GEAR POSITION 3 TIMES. AT ABOUT 4', OVER THE NUMBERS, HE FELT THE AIRCRAFT SINK. HE ADDED POWER AND FLEW FURTHER DOWN THE RUWAY. ABOUT THE TIME HE EXPECTED TO TOUCH DOWN HE FELT A SEVERE SHAKING OF THE AIRCRAFT. HE PULLED BACK ON THE CONTROL WHEEL THINKING HE MAY HAVE LOST A WHEEL. HE THEN HEARD AND FELT A "BAM, BAM BAM" AND THE PROP STOPPED VERTICAL. THE AIRCRAFT SLID TO STOP, ON ITS BELLY, SLIGHTLY OFF THE RIGHT SIDE OF THE RUNWAY AT 45 DEGREE ANGLE TO THE RUNWAY HEADING. PROPELLER MARKS ON THE RUNWAY ARE CONSISTENT WITH THE PILOT'S STATEMENT REGARDING A "SEVERE SHAKING" AND THEN PULLING BACK ON THE CONTROL WHEEL AND THEN HEARING THE "BAM, BAM, BAM." THE PROPELLER MARKS START APPROXIMATELY 2000' FROM THE APPROACH END OF THE RUNWAY AND CONTINUE FOR APPROXIMATELY 100' THEN CEASE FOR APPROXIMATELY 20', A REAPPEAR AND CONTINUE, GRADUALLY GROWING FAINTER. THERE ARE NO SCUFF MARKS ON THE TIRES OR SKID MARKS ON THE RUNWAY THAT WOULD INDICATE AN INTRANSIENT, PARTIALLY EXTENDED (RETRACTED) LANDING GEAR. LANDING GEAR WAS CYCLED SEVERAL TIMES. THE LANDING GEAR OPERATED SMOOTHLY, WITHOUT HESITATION AND LOCKED INTO THE SELECTED POSITION. INITIALLY THE LANDING GEAR WARNING HORN DID NOT OPERATE WITH THE LANDING GEAR IN THE UP AND LOCKED POSITION AND THE THROTTLE RETARDED TO IDLE. A MECHANIC MANIPULTED THE MECHANISM AT THE THROTTLE BODY AND THE WARNING HORN SOUNDED EACH TIME THE THROTTLE WAS RETARDED TO IDLE.

Other reports on N8208G · 2

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