20000306023079I

Incident · Minor damage

FAA incident report · Piper PA-31-350 · Adrian, MI · March 6, 2000

Date
March 6, 2000 · 09:18 local
Place
Adrian, MI
Airport
Lenawee County Airport
Phase of flight
Roll-Out (Fixed Wing)
Operating rules
Air taxi and commuter (Part 135)
Operator
H8BA
Damage
Minor damage
Aircraft
N628HA
Reported as
Piper PA31350
People aboard
1
Fatal injuries
0
Pilot’s flight hours
1,528 total152 in this make and model87 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.

(-23)After elveling the acft @ 3000 ft following a t/o, pilot noticed that the landing gear selector was not in the correct position following the landing gear retraction (also a yaw to the right). Landing gear was recycled several times with only (2) green lts (LH main & nose) indication. Emergency gear extension was used then with the same results. After several low passes to verify with ground personnel gear position (appreas to them that it was locked), pilot landed the acft on rwy 5. Shortly after touchdown the acft veered to the right (no brakes applied), came off the rwy, RH MLG collapsed and came to a stop. Damage to the RH side prop, flap and MLG inboard door was sustained. Investigation reveals that the rod end (p/n 762554) of the hyd actuator (wiebel, model 2115-1, p/n 451 825) failed after unlocking the RH gear on retraction at a point in which gear would not fall back inot a lock position.

As the FAA filed it

(-23)AFTER ELVELING THE ACFT @ 3000 FT FOLLOWING A T/O, PILOT NOTICED THAT THE LANDING GEAR SELECTOR WAS NOT IN THE CORRECT POSITION FOLLOWING THE LANDING GEAR RETRACTION (ALSO A YAW TO THE RIGHT). LANDING GEAR WAS RECYCLED SEVERAL TIMES WITH ONLY (2) GREEN LTS (LH MAIN & NOSE) INDICATION. EMERGENCY GEAR EXTENSION WAS USED THEN WITH THE SAME RESULTS. AFTER SEVERAL LOW PASSES TO VERIFY WITH GROUND PERSONNEL GEAR POSITION (APPREAS TO THEM THAT IT WAS LOCKED), PILOT LANDED THE ACFT ON RWY 5. SHORTLY AFTER TOUCHDOWN THE ACFT VEERED TO THE RIGHT (NO BRAKES APPLIED), CAME OFF THE RWY, RH MLG COLLAPSED AND CAME TO A STOP. DAMAGE TO THE RH SIDE PROP, FLAP AND MLG INBOARD DOOR WAS SUSTAINED. INVESTIGATION REVEALS THAT THE ROD END (P/N 762554) OF THE HYD ACTUATOR (WIEBEL, MODEL 2115-1, P/N 451 825) FAILED AFTER UNLOCKING THE RH GEAR ON RETRACTION AT A POINT IN WHICH GEAR WOULD NOT FALL BACK INOT A LOCK POSITION.

Other reports on N628HA · 2

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