19990905028549A

Accident · Substantial damage

FAA accident report · Cessna 190 · Enterprise, AL · September 5, 1999

Date
September 5, 1999 · 11:00 local
Place
Enterprise, AL
Airport
Enterprise Municipal
Phase of flight
Roll-Out (Fixed Wing)
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N9872A
NTSB investigation
NTSBATL99LA124
Reported as
Cessna 190
People aboard
2
Fatal injuries
0
Pilot’s flight hours
15,500 total290 in this make and model65 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.

(.19) On September 5, 1999, at 1100 central daylight time, a Cessna 190, N987CA, left main landing gear collapsed during a normal landing at the Enterprise Municipal Airport in Enterprise, Alabama. The personal flight was operated by the pilot under the provisions of title 14 CFR part 91 with no flight plan filed. Visual weather conditions prevailed at the time of the accident. The airplane sustained substantial damage. The commercial pilot and pilot/passenger were not injured. The flight departed Enterprise, Alabama, at 1000. According to the pilot, after approx. one hour of pleasure flying in the local flying area, the two pilots returned to Enterprise. After touchdown, the airplane had rolled several hundred feet, when the pilot felt an unusual sensation in the airframe. At approx. the same time, the left spring leaf landing gear assembly separated from the airframe, and the airplane fell to the ground. The field examination of the fracture face disclosed evidence of a pre-existing fracture in the steel material. (.4)after approximately one hour of pleasure flying in the local flying area, the two pilots returned to the departure airport for a full-stop landing. After touchdown, the airplane had rolled several hundred feet, when the pilot felt an unusual sensation in the airframe. At approximately the same time, the left spring leaf landing gear assembly separated from the airframe, and the airplane fell to the ground. The field examination of the fracture face disclosed evidence of a preexisting fracture in the steel material. During the follow-up examination of the fracture face, with the aid of a bench binocular microscope, revealed the presence of at least three small fracture areas typical of fatigue cracking. The origin of the fatigue cracking was damaged during the ultimate separation. The examination also disclosed that the fatigue origin was located in an area that showed fretting damage.

As the FAA filed it

(.19) ON SEPTEMBER 5, 1999, AT 1100 CENTRAL DAYLIGHT TIME, A CESSNA 190, N987CA, LEFT MAIN LANDING GEAR COLLAPSED DURING A NORMAL LANDING AT THE ENTERPRISE MUNICIPAL AIRPORT IN ENTERPRISE, ALABAMA. THE PERSONAL FLIGHT WAS OPERATED BY THE PILOT UNDER THE PROVISIONS OF TITLE 14 CFR PART 91 WITH NO FLIGHT PLAN FILED. VISUAL WEATHER CONDITIONS PREVAILED AT THE TIME OF THE ACCIDENT. THE AIRPLANE SUSTAINED SUBSTANTIAL DAMAGE. THE COMMERCIAL PILOT AND PILOT/PASSENGER WERE NOT INJURED. THE FLIGHT DEPARTED ENTERPRISE, ALABAMA, AT 1000. ACCORDING TO THE PILOT, AFTER APPROX. ONE HOUR OF PLEASURE FLYING IN THE LOCAL FLYING AREA, THE TWO PILOTS RETURNED TO ENTERPRISE. AFTER TOUCHDOWN, THE AIRPLANE HAD ROLLED SEVERAL HUNDRED FEET, WHEN THE PILOT FELT AN UNUSUAL SENSATION IN THE AIRFRAME. AT APPROX. THE SAME TIME, THE LEFT SPRING LEAF LANDING GEAR ASSEMBLY SEPARATED FROM THE AIRFRAME, AND THE AIRPLANE FELL TO THE GROUND. THE FIELD EXAMINATION OF THE FRACTURE FACE DISCLOSED EVIDENCE OF A PRE-EXISTING FRACTURE IN THE STEEL MATERIAL. (.4)AFTER APPROXIMATELY ONE HOUR OF PLEASURE FLYING IN THE LOCAL FLYING AREA, THE TWO PILOTS RETURNED TO THE DEPARTURE AIRPORT FOR A FULL-STOP LANDING. AFTER TOUCHDOWN, THE AIRPLANE HAD ROLLED SEVERAL HUNDRED FEET, WHEN THE PILOT FELT AN UNUSUAL SENSATION IN THE AIRFRAME. AT APPROXIMATELY THE SAME TIME, THE LEFT SPRING LEAF LANDING GEAR ASSEMBLY SEPARATED FROM THE AIRFRAME, AND THE AIRPLANE FELL TO THE GROUND. THE FIELD EXAMINATION OF THE FRACTURE FACE DISCLOSED EVIDENCE OF A PREEXISTING FRACTURE IN THE STEEL MATERIAL. DURING THE FOLLOW-UP EXAMINATION OF THE FRACTURE FACE, WITH THE AID OF A BENCH BINOCULAR MICROSCOPE, REVEALED THE PRESENCE OF AT LEAST THREE SMALL FRACTURE AREAS TYPICAL OF FATIGUE CRACKING. THE ORIGIN OF THE FATIGUE CRACKING WAS DAMAGED DURING THE ULTIMATE SEPARATION. THE EXAMINATION ALSO DISCLOSED THAT THE FATIGUE ORIGIN WAS LOCATED IN AN AREA THAT SHOWED FRETTING DAMAGE.

NTSB investigation

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