20040626016549A

Accident · Substantial damage

FAA accident report · Cessna 172S · Glendale, AZ · June 26, 2004

Date
June 26, 2004 · 12:32 local
Place
Glendale, AZ
Airport
Glendale Municipal Airport
Phase of flight
Roll-Out (Fixed Wing)
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N35389
NTSB investigation
NTSBLAX04CA250
Reported as
Cessna 172S
People aboard
1
Fatal injuries
0
Pilot’s certificate
Student
Pilot’s flight hours
27 total18 in this make and model27 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) Immediately after touch down during first solo landing the student encountered a gust for which he failed to properly correct. The aircraft drifted off runway and impacted two small hills adjacent to the runway. Aircraft received substantial damage to firewall, forward left, forward right, and lower fuselage skin, nose gear and both main landing gear, fuel header tank, interior cockpit floor, center console, rudder pedal and rudder bar assemblies, control yoke guides, lower tail cone skin, lower tail skin, and aft rudder skin. Student also stated that during the dual instructional flight immediately prior to his first solo he had difficulty on two of the four landings due to wind. privacy data omitted

As the FAA filed it

(-23) IMMEDIATELY AFTER TOUCH DOWN DURING FIRST SOLO LANDING THE STUDENT ENCOUNTERED A GUST FOR WHICH HE FAILED TO PROPERLY CORRECT. THE AIRCRAFT DRIFTED OFF RUNWAY AND IMPACTED TWO SMALL HILLS ADJACENT TO THE RUNWAY. AIRCRAFT RECEIVED SUBSTANTIAL DAMAGE TO FIREWALL, FORWARD LEFT, FORWARD RIGHT, AND LOWER FUSELAGE SKIN, NOSE GEAR AND BOTH MAIN LANDING GEAR, FUEL HEADER TANK, INTERIOR COCKPIT FLOOR, CENTER CONSOLE, RUDDER PEDAL AND RUDDER BAR ASSEMBLIES, CONTROL YOKE GUIDES, LOWER TAIL CONE SKIN, LOWER TAIL SKIN, AND AFT RUDDER SKIN. STUDENT ALSO STATED THAT DURING THE DUAL INSTRUCTIONAL FLIGHT IMMEDIATELY PRIOR TO HIS FIRST SOLO HE HAD DIFFICULTY ON TWO OF THE FOUR LANDINGS DUE TO WIND. ^PRIVACY DATA OMITTED^

NTSB investigation

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