20010320005529A

Accident · Substantial damage

FAA accident report · Piper PA-28-181 · Gila Bend, AZ · March 20, 2001

Date
March 20, 2001 · 09:30 local
Place
Gila Bend, AZ
Airport
Gila Bend Municipal Airport
Phase of flight
Sfl Final Approach
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N4188E
NTSB investigation
NTSBLAX01LA122
Reported as
Piper PA28181
Reported engine
Lycoming O360*
People aboard
3
Fatal injuries
0
Pilot’s flight hours
725 total253 in this make and model118 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 20, 2001, at 1000 hrs. MST, a Piper PA-28-181, N4188E, landed short of runway 4 at the Gila Bend Municipal Airport, Gila Bend, Arizona. The airplane was operated by sabena airline training center as an instructional flight under the provisions of 14 CFR part 91, and was substantially damaged. The CFI and two students were not injured. Visual meteorological conditions prevailed for the local area flight. The flight was originating at the time and was scheduled to terminate at the scottsdale, AZ, airport. No flight plan was filed. The purpose of the flight was to practice engine out approaches and landings. On short final, the CFI saw that the airspeed was too slow. The airplane stalled and landed about 100 yards short of the runway. During the landing rollout the stabilizer struck a tree and the airplane came to rest in a ditch. (-23) see attached pilot statement (.4) during a simulated engine out procedure the airplane landed short of the runway in desert terrain colliding with brush and coming to rest in a ditch. The purpose of the flight was to conduct simulated engine out landings . Both pilots estimated the wind as coming down the runway about 5-10 knots. The student had landed two previous times with no problems noted by him or the CFI. On the third landing the CFI simulated an engine out. When the student entered onto the final leg of the approach he noted that the winds had increased, or were stronger than expected. He informed the CFI that he was not going to add the second notch of flaps because of the increased drag. On short final he estimated that at his current altitude and airspeed, with the given wind condition, he would not be able to make the landing. He called out a go-around, and was instructed to continue the approach. The CFI then added the second notch of flaps. He adjusted his airspeed to compensate for the increased drag and noted that the airplane was rapidly losing altitude. He called out for a go-around and advanced the throttle full forward; however, the airplane continued to sink. The CFI thought they had encountered a wind shear event, from a straight headwind to no wind at all.

As the FAA filed it

(.19) ON MARCH 20, 2001, AT 1000 HRS. MST, A PIPER PA-28-181, N4188E, LANDED SHORT OF RUNWAY 4 AT THE GILA BEND MUNICIPAL AIRPORT, GILA BEND, ARIZONA. THE AIRPLANE WAS OPERATED BY SABENA AIRLINE TRAINING CENTER AS AN INSTRUCTIONAL FLIGHT UNDER THE PROVISIONS OF 14 CFR PART 91, AND WAS SUBSTANTIALLY DAMAGED. THE CFI AND TWO STUDENTS WERE NOT INJURED. VISUAL METEOROLOGICAL CONDITIONS PREVAILED FOR THE LOCAL AREA FLIGHT. THE FLIGHT WAS ORIGINATING AT THE TIME AND WAS SCHEDULED TO TERMINATE AT THE SCOTTSDALE, AZ, AIRPORT. NO FLIGHT PLAN WAS FILED. THE PURPOSE OF THE FLIGHT WAS TO PRACTICE ENGINE OUT APPROACHES AND LANDINGS. ON SHORT FINAL, THE CFI SAW THAT THE AIRSPEED WAS TOO SLOW. THE AIRPLANE STALLED AND LANDED ABOUT 100 YARDS SHORT OF THE RUNWAY. DURING THE LANDING ROLLOUT THE STABILIZER STRUCK A TREE AND THE AIRPLANE CAME TO REST IN A DITCH. (-23) SEE ATTACHED PILOT STATEMENT (.4) DURING A SIMULATED ENGINE OUT PROCEDURE THE AIRPLANE LANDED SHORT OF THE RUNWAY IN DESERT TERRAIN COLLIDING WITH BRUSH AND COMING TO REST IN A DITCH. THE PURPOSE OF THE FLIGHT WAS TO CONDUCT SIMULATED ENGINE OUT LANDINGS . BOTH PILOTS ESTIMATED THE WIND AS COMING DOWN THE RUNWAY ABOUT 5-10 KNOTS. THE STUDENT HAD LANDED TWO PREVIOUS TIMES WITH NO PROBLEMS NOTED BY HIM OR THE CFI. ON THE THIRD LANDING THE CFI SIMULATED AN ENGINE OUT. WHEN THE STUDENT ENTERED ONTO THE FINAL LEG OF THE APPROACH HE NOTED THAT THE WINDS HAD INCREASED, OR WERE STRONGER THAN EXPECTED. HE INFORMED THE CFI THAT HE WAS NOT GOING TO ADD THE SECOND NOTCH OF FLAPS BECAUSE OF THE INCREASED DRAG. ON SHORT FINAL HE ESTIMATED THAT AT HIS CURRENT ALTITUDE AND AIRSPEED, WITH THE GIVEN WIND CONDITION, HE WOULD NOT BE ABLE TO MAKE THE LANDING. HE CALLED OUT A GO-AROUND, AND WAS INSTRUCTED TO CONTINUE THE APPROACH. THE CFI THEN ADDED THE SECOND NOTCH OF FLAPS. HE ADJUSTED HIS AIRSPEED TO COMPENSATE FOR THE INCREASED DRAG AND NOTED THAT THE AIRPLANE WAS RAPIDLY LOSING ALTITUDE. HE CALLED OUT FOR A GO-AROUND AND ADVANCED THE THROTTLE FULL FORWARD; HOWEVER, THE AIRPLANE CONTINUED TO SINK. THE CFI THOUGHT THEY HAD ENCOUNTERED A WIND SHEAR EVENT, FROM A STRAIGHT HEADWIND TO NO WIND AT ALL.

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 N4188E · 2

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