20190926018289I

Incident · Minor damage

FAA incident report · Cessna 172S · Daytona, FL · September 26, 2019

Date
September 26, 2019 · 15:29 local
Place
Daytona, FL
Airport
Daytona Beach
Phase of flight
Unknown
Operating rules
Pilot school (Part 141)
Operator
NX4S
Damage
Minor damage
Aircraft
N479ER
Reported as
Cessna 172S
Reported engine
Lycoming IO-360-L2A
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Commercial pilot
Pilot’s flight hours
581 total

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.

RDDL479 struck a bird on the fuselage and landed without further incident 09/26/2019 1929Z.

Investigation in progress: bird strike: dents on left wing, pilot door, nose gear. It was corescted as follows: complied with Cessna modification kit MK172-57-03 by installing jack pad point on left wing. Removed inboard left wing leading edge, left wing strut, pitot tube assy, left wing tip, stall horn scoop and inspected ribs and spar in affected area and no damage noted. Installed new inboard leading edge skin(0523028-28) and ribs (0523027-1 X2 & 0523027-2 X1. Iaw Cessna maintenance manual and srm manual chapter 57-10, 57-25 and 57-40. Reinstalled left wing strut, (torqued bolts to 55 ft. lbs, pitot tube assy. Performed leak check. No leaks noted, left wing tip, stall horn scoop and adjusted, operational check of pitotheat and lt wing light good. Returned to service.

As the FAA filed it

RDDL479 STRUCK A BIRD ON THE FUSELAGE AND LANDED WITHOUT FURTHER INCIDENT 09/26/2019 1929Z.

INVESTIGATION IN PROGRESS: BIRD STRIKE: DENTS ON LEFT WING, PILOT DOOR, NOSE GEAR. IT WAS CORESCTED AS FOLLOWS: COMPLIED WITH CESSNA MODIFICATION KIT MK172-57-03 BY INSTALLING JACK PAD POINT ON LEFT WING. REMOVED INBOARD LEFT WING LEADING EDGE, LEFT WING STRUT, PITOT TUBE ASSY, LEFT WING TIP, STALL HORN SCOOP AND INSPECTED RIBS AND SPAR IN AFFECTED AREA AND NO DAMAGE NOTED. INSTALLED NEW INBOARD LEADING EDGE SKIN(0523028-28) AND RIBS (0523027-1 X2 & 0523027-2 X1. IAW CESSNA MAINTENANCE MANUAL AND SRM MANUAL CHAPTER 57-10, 57-25 AND 57-40. REINSTALLED LEFT WING STRUT, (TORQUED BOLTS TO 55 FT. LBS, PITOT TUBE ASSY. PERFORMED LEAK CHECK. NO LEAKS NOTED, LEFT WING TIP, STALL HORN SCOOP AND ADJUSTED, OPERATIONAL CHECK OF PITOTHEAT AND LT WING LIGHT GOOD. RETURNED TO SERVICE.