19990312017989I

Incident · Minor damage

FAA incident report · Cessna 337D · Miami, FL · March 12, 1999

Date
March 12, 1999 · 12:30 local
Place
Miami, FL
Airport
Tamiami Airport
Phase of flight
Roll-Out (Fixed Wing)
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N86377
Reported as
Cessna 337D
Reported engine
Continental IO360*
People aboard
1
Fatal injuries
0
Pilot’s flight hours
100 total27 in this make and model20 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.

(-5) History of flight - on March 12, 1999, at 12:30 p.m., a Cessna 337D, aircraft N86377, serial number 337-1167, operated by ernesto martin, departed the north side of runway nine left at Tamiami, and had a nose gear failure. Mr. Martin was performing short filed landings in preparation for a multi engine flight check. Mr. Martin stated that when the nose wheel contactedthe runway surface of nine left, the nose wheel vibrated severely. Mr. Martin said applied nose up elevator to keep the weight off the nose wheel. The aircraft drifted to left side of the runway. He said that he was reluctant to utilize the brakes to correct the drift. The aircraft departed the runway resulting in the nose landing gear shearing at the yoke. The aircraft came to rest approximately on aircraft length forward of the point where the nose landing gear failed. The front propeller received damage, however the engine did not sustain sudden engine stoppage. Injures to persons - none damage to aircraft - the yoke assembly, left front portion, in the bend radius was bent outward. The tire received damage from rubbing on the inside surfaces of the arm areas. The bead area on both sides of the tire were broken. The valve stem hole was intact. The wheel was loose on the axle and no grease was observed. The axle was attached to the yoke assembly. The tire sidewalls showed evidence of heat damage. The inner tube was shredded and the valve stem was missing. The tread did not show any unusual wear. One area of the tire was scuffed from skidding. Pilot information - Mr. Martin had a total time of 100 hours, approximately 20 hours were logged in the 90 days preceding this incident. Mr. Martin had received 20 hours of dual instruction in the Cessna 337. Mr. Martin satisfactorily completed a private pilot flight check on November 10, 1999. Mr. Martin holds a private pilot certificate, single engine land. Meteorological information - VMC conditions prevailed. The weather reported at 12:37 p.m. was clear with ten miles visibility and the wind was 120 degrees at seven knots. The wather report also noted haze in the remarks section. Summary - there was no evidence of any failure of the wheel bearing or nose wheel yoke prior to the incident. privacy data omitted

As the FAA filed it

(-5) HISTORY OF FLIGHT - ON MARCH 12, 1999, AT 12:30 P.M., A CESSNA 337D, AIRCRAFT N86377, SERIAL NUMBER 337-1167, OPERATED BY ERNESTO MARTIN, DEPARTED THE NORTH SIDE OF RUNWAY NINE LEFT AT TAMIAMI, AND HAD A NOSE GEAR FAILURE. MR. MARTIN WAS PERFORMING SHORT FILED LANDINGS IN PREPARATION FOR A MULTI ENGINE FLIGHT CHECK. MR. MARTIN STATED THAT WHEN THE NOSE WHEEL CONTACTEDTHE RUNWAY SURFACE OF NINE LEFT, THE NOSE WHEEL VIBRATED SEVERELY. MR. MARTIN SAID APPLIED NOSE UP ELEVATOR TO KEEP THE WEIGHT OFF THE NOSE WHEEL. THE AIRCRAFT DRIFTED TO LEFT SIDE OF THE RUNWAY. HE SAID THAT HE WAS RELUCTANT TO UTILIZE THE BRAKES TO CORRECT THE DRIFT. THE AIRCRAFT DEPARTED THE RUNWAY RESULTING IN THE NOSE LANDING GEAR SHEARING AT THE YOKE. THE AIRCRAFT CAME TO REST APPROXIMATELY ON AIRCRAFT LENGTH FORWARD OF THE POINT WHERE THE NOSE LANDING GEAR FAILED. THE FRONT PROPELLER RECEIVED DAMAGE, HOWEVER THE ENGINE DID NOT SUSTAIN SUDDEN ENGINE STOPPAGE. INJURES TO PERSONS - NONE DAMAGE TO AIRCRAFT - THE YOKE ASSEMBLY, LEFT FRONT PORTION, IN THE BEND RADIUS WAS BENT OUTWARD. THE TIRE RECEIVED DAMAGE FROM RUBBING ON THE INSIDE SURFACES OF THE ARM AREAS. THE BEAD AREA ON BOTH SIDES OF THE TIRE WERE BROKEN. THE VALVE STEM HOLE WAS INTACT. THE WHEEL WAS LOOSE ON THE AXLE AND NO GREASE WAS OBSERVED. THE AXLE WAS ATTACHED TO THE YOKE ASSEMBLY. THE TIRE SIDEWALLS SHOWED EVIDENCE OF HEAT DAMAGE. THE INNER TUBE WAS SHREDDED AND THE VALVE STEM WAS MISSING. THE TREAD DID NOT SHOW ANY UNUSUAL WEAR. ONE AREA OF THE TIRE WAS SCUFFED FROM SKIDDING. PILOT INFORMATION - MR. MARTIN HAD A TOTAL TIME OF 100 HOURS, APPROXIMATELY 20 HOURS WERE LOGGED IN THE 90 DAYS PRECEDING THIS INCIDENT. MR. MARTIN HAD RECEIVED 20 HOURS OF DUAL INSTRUCTION IN THE CESSNA 337. MR. MARTIN SATISFACTORILY COMPLETED A PRIVATE PILOT FLIGHT CHECK ON NOVEMBER 10, 1999. MR. MARTIN HOLDS A PRIVATE PILOT CERTIFICATE, SINGLE ENGINE LAND. METEOROLOGICAL INFORMATION - VMC CONDITIONS PREVAILED. THE WEATHER REPORTED AT 12:37 P.M. WAS CLEAR WITH TEN MILES VISIBILITY AND THE WIND WAS 120 DEGREES AT SEVEN KNOTS. THE WATHER REPORT ALSO NOTED HAZE IN THE REMARKS SECTION. SUMMARY - THERE WAS NO EVIDENCE OF ANY FAILURE OF THE WHEEL BEARING OR NOSE WHEEL YOKE PRIOR TO THE INCIDENT. ^PRIVACY DATA OMITTED^