20050824020859A

Accident · Substantial damage

FAA accident report · Cessna 172S · Savannah, GA · August 24, 2005

Date
August 24, 2005 · 13:19 local
Place
Savannah, GA
Airport
Savannah International
Phase of flight
Roll-Out (Fixed Wing)
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N21670
NTSB investigation
NTSBATL05CA153
Reported as
Cessna 172S
Reported engine
Lycoming IO360L2A
People aboard
2
Fatal injuries
0
Pilot’s flight hours
562 total411 in this make and model109 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) During an instructional flight, the student pilot (sp) was conducting a landing. The instructor pilot (ip) said everything was normal on the approach. As the sp flared the aircraft to land, the aircraft drifted to the right of the centerline. The initial correction made by the sp was to make a left pedal input (rather than a left wing down and a right pedal input). The sp realized that the input was incorrect and then lowered the left wing to stop the right drift. The sp then applied the right pedal to land the aircraft parallel to the centerline. Once the aircraft was on the ground, the ip explained that the sp then made a left pedal input to get back to the centerline. When this occurred, the aircraft turned approximately 45 degrees to the left and quickly departed the runway. The ip took the controls of the aircraft to avoid all the runway lights and the precision approach path indicator light system adjacent to runway 36. The aircraft then traversed across the grass and into a ditch adjacent to taxiway A-4. The aircraft came to rest as it impacted the FAR side of a ditch. The aircraft sustained substantial damage, as the firewall was badly damaged (as the nose gear foldedrearward in the ditch) and the aft fuselage bulkhead was distorted where the tailboom was attached. The right landing gear was bent upward after impacting the ground in the ditch. Additional damage occurred to the right wing (outboard 1/4) and tip, one propeller blade was bent aft (no power applied to engine-no signs of curling/q-tipping of the blades) and some minor leading edge damage occurred to the left wing just outboard of the landing/taxiing lights.

As the FAA filed it

(-23) DURING AN INSTRUCTIONAL FLIGHT, THE STUDENT PILOT (SP) WAS CONDUCTING A LANDING. THE INSTRUCTOR PILOT (IP) SAID EVERYTHING WAS NORMAL ON THE APPROACH. AS THE SP FLARED THE AIRCRAFT TO LAND, THE AIRCRAFT DRIFTED TO THE RIGHT OF THE CENTERLINE. THE INITIAL CORRECTION MADE BY THE SP WAS TO MAKE A LEFT PEDAL INPUT (RATHER THAN A LEFT WING DOWN AND A RIGHT PEDAL INPUT). THE SP REALIZED THAT THE INPUT WAS INCORRECT AND THEN LOWERED THE LEFT WING TO STOP THE RIGHT DRIFT. THE SP THEN APPLIED THE RIGHT PEDAL TO LAND THE AIRCRAFT PARALLEL TO THE CENTERLINE. ONCE THE AIRCRAFT WAS ON THE GROUND, THE IP EXPLAINED THAT THE SP THEN MADE A LEFT PEDAL INPUT TO GET BACK TO THE CENTERLINE. WHEN THIS OCCURRED, THE AIRCRAFT TURNED APPROXIMATELY 45 DEGREES TO THE LEFT AND QUICKLY DEPARTED THE RUNWAY. THE IP TOOK THE CONTROLS OF THE AIRCRAFT TO AVOID ALL THE RUNWAY LIGHTS AND THE PRECISION APPROACH PATH INDICATOR LIGHT SYSTEM ADJACENT TO RUNWAY 36. THE AIRCRAFT THEN TRAVERSED ACROSS THE GRASS AND INTO A DITCH ADJACENT TO TAXIWAY A-4. THE AIRCRAFT CAME TO REST AS IT IMPACTED THE FAR SIDE OF A DITCH. THE AIRCRAFT SUSTAINED SUBSTANTIAL DAMAGE, AS THE FIREWALL WAS BADLY DAMAGED (AS THE NOSE GEAR FOLDEDREARWARD IN THE DITCH) AND THE AFT FUSELAGE BULKHEAD WAS DISTORTED WHERE THE TAILBOOM WAS ATTACHED. THE RIGHT LANDING GEAR WAS BENT UPWARD AFTER IMPACTING THE GROUND IN THE DITCH. ADDITIONAL DAMAGE OCCURRED TO THE RIGHT WING (OUTBOARD 1/4) AND TIP, ONE PROPELLER BLADE WAS BENT AFT (NO POWER APPLIED TO ENGINE-NO SIGNS OF CURLING/Q-TIPPING OF THE BLADES) AND SOME MINOR LEADING EDGE DAMAGE OCCURRED TO THE LEFT WING JUST OUTBOARD OF THE LANDING/TAXIING LIGHTS.

NTSB investigation

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

Other reports on N21670 · 2

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