20231104018449A

Accident · Substantial damage

FAA accident report · Piper PA-18-150 · Wasilla, AK · November 4, 2023

Date
November 4, 2023 · 15:00 local
Place
Wasilla, AK
Airport
Wasilla
Phase of flight
Landing: Rollout
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N3994Z
NTSB investigation
NTSBANC24LA002
Reported as
Piper PA-18-150
Reported engine
Lycoming 0-320 series
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificates
Airline transport, flight instructor
Pilot’s flight hours
8,395 total89 in this make and model13 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.

Instructional flight for tail wheel endorsement practicing conventional wheel landings in PA-18 aircraft with flight instructor sitting in rear seat and student pilot sitting in front seat. Initial plan to conduct training flights at goose bay airport due to wider runway and larger margin for error, but fog layer prevented safe operations in the planned flight area. With increased traffic congestion at palmer airport, decision made by flight instructor to practice landings at a narrower nearby gravel strip at Wasilla Airport. During third and final practice landing of the day, student pilot instructed to touch down as close to the touchdown marker as possible for increased accuracy. Upon touchdown on runway centerline, aircraft began veering right toward runway edge. With restricted forward visibility from rear seat, flight instructor stated having difficulty clearly monitoring the landing looking over student pilot's shoulders and slow reaction to correct deviation. As the airplane got closer to the runway edge, flight instructor pulled back on control stick and began to apply brake pressure to keep aircraft on runway surface without applying aggressive rudder correction and prevent a ground loop. Slow reaction time during landing rollout and increased brake pressure being applied by flight instructor caused aircraft to nose over and invert at runway edge. Damage to tail and rudder, upper fuselage near tail, cockpit v-brace, wing strut, engine firewall, and propeller.

As the FAA filed it

INSTRUCTIONAL FLIGHT FOR TAIL WHEEL ENDORSEMENT PRACTICING CONVENTIONAL WHEEL LANDINGS IN PA-18 AIRCRAFT WITH FLIGHT INSTRUCTOR SITTING IN REAR SEAT AND STUDENT PILOT SITTING IN FRONT SEAT. INITIAL PLAN TO CONDUCT TRAINING FLIGHTS AT GOOSE BAY AIRPORT DUE TO WIDER RUNWAY AND LARGER MARGIN FOR ERROR, BUT FOG LAYER PREVENTED SAFE OPERATIONS IN THE PLANNED FLIGHT AREA. WITH INCREASED TRAFFIC CONGESTION AT PALMER AIRPORT, DECISION MADE BY FLIGHT INSTRUCTOR TO PRACTICE LANDINGS AT A NARROWER NEARBY GRAVEL STRIP AT WASILLA AIRPORT. DURING THIRD AND FINAL PRACTICE LANDING OF THE DAY, STUDENT PILOT INSTRUCTED TO TOUCH DOWN AS CLOSE TO THE TOUCHDOWN MARKER AS POSSIBLE FOR INCREASED ACCURACY. UPON TOUCHDOWN ON RUNWAY CENTERLINE, AIRCRAFT BEGAN VEERING RIGHT TOWARD RUNWAY EDGE. WITH RESTRICTED FORWARD VISIBILITY FROM REAR SEAT, FLIGHT INSTRUCTOR STATED HAVING DIFFICULTY CLEARLY MONITORING THE LANDING LOOKING OVER STUDENT PILOT'S SHOULDERS AND SLOW REACTION TO CORRECT DEVIATION. AS THE AIRPLANE GOT CLOSER TO THE RUNWAY EDGE, FLIGHT INSTRUCTOR PULLED BACK ON CONTROL STICK AND BEGAN TO APPLY BRAKE PRESSURE TO KEEP AIRCRAFT ON RUNWAY SURFACE WITHOUT APPLYING AGGRESSIVE RUDDER CORRECTION AND PREVENT A GROUND LOOP. SLOW REACTION TIME DURING LANDING ROLLOUT AND INCREASED BRAKE PRESSURE BEING APPLIED BY FLIGHT INSTRUCTOR CAUSED AIRCRAFT TO NOSE OVER AND INVERT AT RUNWAY EDGE. DAMAGE TO TAIL AND RUDDER, UPPER FUSELAGE NEAR TAIL, COCKPIT V-BRACE, WING STRUT, ENGINE FIREWALL, AND PROPELLER.

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 N3994Z · 1

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