NTSB Identification: LAX84LA312.
The docket is stored on NTSB microfiche number 24256.
Accident occurred Monday, May 21, 1984 in HAYWARD, CA
Aircraft: CESSNA 172N, registration: N734TH
Injuries: 2 Uninjured.

NTSB investigators may not have traveled in support of this investigation and used data provided by various sources to prepare this aircraft accident report.

THE ACFT LANDED HARD AND PORPOISED DOWN THE RWY. THE PLT MADE A GO-AROUND AND REPORTED TO THE TOWER THAT HE HAD CONTROL PROBLEMS. HE PERFORMED A TOWER FLY-BY AND NO DAMAGE WAS APPARENT TO THE CONTROLLERS. THE PLT WAS CLEARED FOR LANDING ANDDID SO WITHOUT FURTHER INCIDENT. UPON INSPECTION,THE FIRE WALL WAS FOUND TO BE BUCKLED,THE NOSE WHEEL STRUT CANTED THE FUSELAGE WAS WRINKLED AND THE FLOOR WAS CAVED IN SO THAT THE VERTICAL INSTRUMENT PANEL SUPPORT WAS PULLED DOWN ON THE PUSH-PULL ROD FOR THE AILERON AND ELEVATOR.

The National Transportation Safety Board determines the probable cause(s) of this accident to be:

FLARE..IMPROPER..PILOT IN COMMAND

The National Transportation Safety Board determines the probable cause(s) of this accident to be:

TOTAL..PILOT IN COMMAND

The National Transportation Safety Board determines the probable cause(s) of this accident to be:

RECOVERY FROM BOUNCED LANDING..IMPROPER..PILOT IN COMMAND

The National Transportation Safety Board determines the probable cause(s) of this accident to be:

LACK OF RECENT TOTAL EXPERIENCE..PILOT IN COMMAND

The National Transportation Safety Board determines the probable cause(s) of this accident to be:

GO-AROUND..DELAYED..PILOT IN COMMAND

The National Transportation Safety Board determines the probable cause(s) of this accident to be:

INADEQUATE TRANSITION/UPGRADE TRAINING..PILOT IN COMMAND

The National Transportation Safety Board determines the probable cause(s) of this accident to be:

FLIGHT CONTROLS..IMPROPER USE OF..PILOT IN COMMAND


Contributing Factors

FUSELAGE,INSTRUMENT/ELECTRICAL PANEL..DISTORTED


Contributing Factors

FLT CONTROL SYST,AILERON CONTROL..MOVEMENT RESTRICTED


Contributing Factors

FLT CONTROL SYST,ELEVATOR CONTROL..MOVEMENT RESTRICTED


Contributing Factors

FUSELAGE,FLOOR..BUCKLED


Contributing Factors

LANDING GEAR,NOSE GEAR ASSEMBLY..DISTORTED


Contributing Factors

FUSELAGE,BULKHEAD..BUCKLED


Contributing Factors

FUSELAGE,SKIN..INCORRECT

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