19990306035879A

Accident · Substantial damage

FAA accident report · Cessna 177 · West Palm Beach, FL · March 6, 1999

Date
March 6, 1999 · 19:00 local
Place
West Palm Beach, FL
Airport
Palm Beach County Park Airport
Phase of flight
Level Off Touchdown
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N2890X
NTSB investigation
NTSBMIA99LA101
Reported as
Cessna 177
Reported engine
Lycoming IO360A1B6
People aboard
1
Fatal injuries
0
Pilot’s flight hours
62 total31 in this make and model31 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 March 6, 1999, about 1430 eastern standard time, a Cessna 177, N2890X, registered to a private individual, crashed during landing at lantana airport, lantana, Florida, while on a title 14 CFR part 91 instructional flight. Visual meteorological conditions were reported, and no flight plan was filed. The airplane was substantially damaged. The student pilot reported no injuries. The flight had departed the lantana airport about 1330. The airplane landed on runway 15, bounced, and landed on the nose gear. The pilot taxied to the parking area and noted that the airplane was damaged. The pilot said his stbilator had jammed, but examination of the airplane after the accident revealed impact damage around the stabilator. (.4) the pilot was practicing landings on runway 15, and was on his fourth takeoff. He said, '...on the downwind I went to push the control forward and it would not go.' He attempt an approach to runway 15, but on final he was too high and decided to go around and try another approach. The pilot said, '...I was on final I was at 400 [feet] AGL, and cut the power back to idle and hit the runway about 100 mph. The plane went end to end several times and h it the runway several times...I ended up on the east side of the grass.' The pilot taxied the airplane to the parking area and noted that the airplane was damaged. Examination of the wreckage revealed a stop drilled crack in the tail cone fairing assembly adjacent to the elevator that appeared to interfere with the travel of the flight control surface. Further examination revealed that the tail cone had sustained impact damage in the area of the stop drill crack. According to the FAA inspector the impact damage caused the interference with the travel of the flight control, and that the crush occurred after the pilot had made a hard landing, causing the damage.

As the FAA filed it

(.19) ON MARCH 6, 1999, ABOUT 1430 EASTERN STANDARD TIME, A CESSNA 177, N2890X, REGISTERED TO A PRIVATE INDIVIDUAL, CRASHED DURING LANDING AT LANTANA AIRPORT, LANTANA, FLORIDA, WHILE ON A TITLE 14 CFR PART 91 INSTRUCTIONAL FLIGHT. VISUAL METEOROLOGICAL CONDITIONS WERE REPORTED, AND NO FLIGHT PLAN WAS FILED. THE AIRPLANE WAS SUBSTANTIALLY DAMAGED. THE STUDENT PILOT REPORTED NO INJURIES. THE FLIGHT HAD DEPARTED THE LANTANA AIRPORT ABOUT 1330. THE AIRPLANE LANDED ON RUNWAY 15, BOUNCED, AND LANDED ON THE NOSE GEAR. THE PILOT TAXIED TO THE PARKING AREA AND NOTED THAT THE AIRPLANE WAS DAMAGED. THE PILOT SAID HIS STBILATOR HAD JAMMED, BUT EXAMINATION OF THE AIRPLANE AFTER THE ACCIDENT REVEALED IMPACT DAMAGE AROUND THE STABILATOR. (.4) THE PILOT WAS PRACTICING LANDINGS ON RUNWAY 15, AND WAS ON HIS FOURTH TAKEOFF. HE SAID, '...ON THE DOWNWIND I WENT TO PUSH THE CONTROL FORWARD AND IT WOULD NOT GO.' HE ATTEMPT AN APPROACH TO RUNWAY 15, BUT ON FINAL HE WAS TOO HIGH AND DECIDED TO GO AROUND AND TRY ANOTHER APPROACH. THE PILOT SAID, '...I WAS ON FINAL I WAS AT 400 [FEET] AGL, AND CUT THE POWER BACK TO IDLE AND HIT THE RUNWAY ABOUT 100 MPH. THE PLANE WENT END TO END SEVERAL TIMES AND H IT THE RUNWAY SEVERAL TIMES...I ENDED UP ON THE EAST SIDE OF THE GRASS.' THE PILOT TAXIED THE AIRPLANE TO THE PARKING AREA AND NOTED THAT THE AIRPLANE WAS DAMAGED. EXAMINATION OF THE WRECKAGE REVEALED A STOP DRILLED CRACK IN THE TAIL CONE FAIRING ASSEMBLY ADJACENT TO THE ELEVATOR THAT APPEARED TO INTERFERE WITH THE TRAVEL OF THE FLIGHT CONTROL SURFACE. FURTHER EXAMINATION REVEALED THAT THE TAIL CONE HAD SUSTAINED IMPACT DAMAGE IN THE AREA OF THE STOP DRILL CRACK. ACCORDING TO THE FAA INSPECTOR THE IMPACT DAMAGE CAUSED THE INTERFERENCE WITH THE TRAVEL OF THE FLIGHT CONTROL, AND THAT THE CRUSH OCCURRED AFTER THE PILOT HAD MADE A HARD LANDING, CAUSING THE 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.

Other reports on N2890X · 1

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