20050730018139I

Incident · Substantial damage

FAA incident report · Beech B36TC · Scottsdale, AZ · July 30, 2005

Date
July 30, 2005 · 09:15 local
Place
Scottsdale, AZ
Airport
Scottsdale Municipal Airport
Phase of flight
Roll-Out (Fixed Wing)
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N136BF
Reported as
Beech B36TC
Reported engine
Continental TSIO520*
People aboard
2
Fatal injuries
0
Pilot’s flight hours
1,221 total100 in this make and model4 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) The pilot (and one passenger) had taken off from sdl heading in a northerly direction and set the auto-pilot for 4,500 ft (AGL). At approx. 4000 ft (AGL) the oil pressure indication was noticed to be near the bottom of the "green" arc. The pilot immediately reversed his course, gained some alt, throttled back, and headed back to sdl since he was only approx. fifteen (15) minutes into his flight. The pilot claims the oil pressure eventually went to zero, the engine "coughed" once but continued to develop power. The pilot contacted sdl tower and notified them of his problem. He received clearance to rwy 3 and established a long final when he began to lose electrical power. He began "cranking" the l/gear down but claims some carpeting "interfered slightly" with the process. Upon rolling out on touch down the pilot stopped "cranking" the l/gear down. The l/h main l/g remained dn + locked, as did the nose l/g. however the r/h main was not dn + locked and collapsed and the a/c slid to a stop on the RH wingtip. The pilot (and passenger) did not sustain any injuries. There was no post-event fire. The propeller was severely damaged. The engine remained operating @ low RPM until it (prop) contacted the ground on ldg.

As the FAA filed it

(-23) THE PILOT (AND ONE PASSENGER) HAD TAKEN OFF FROM SDL HEADING IN A NORTHERLY DIRECTION AND SET THE AUTO-PILOT FOR 4,500 FT (AGL). AT APPROX. 4000 FT (AGL) THE OIL PRESSURE INDICATION WAS NOTICED TO BE NEAR THE BOTTOM OF THE "GREEN" ARC. THE PILOT IMMEDIATELY REVERSED HIS COURSE, GAINED SOME ALT, THROTTLED BACK, AND HEADED BACK TO SDL SINCE HE WAS ONLY APPROX. FIFTEEN (15) MINUTES INTO HIS FLIGHT. THE PILOT CLAIMS THE OIL PRESSURE EVENTUALLY WENT TO ZERO, THE ENGINE "COUGHED" ONCE BUT CONTINUED TO DEVELOP POWER. THE PILOT CONTACTED SDL TOWER AND NOTIFIED THEM OF HIS PROBLEM. HE RECEIVED CLEARANCE TO RWY 3 AND ESTABLISHED A LONG FINAL WHEN HE BEGAN TO LOSE ELECTRICAL POWER. HE BEGAN "CRANKING" THE L/GEAR DOWN BUT CLAIMS SOME CARPETING "INTERFERED SLIGHTLY" WITH THE PROCESS. UPON ROLLING OUT ON TOUCH DOWN THE PILOT STOPPED "CRANKING" THE L/GEAR DOWN. THE L/H MAIN L/G REMAINED DN + LOCKED, AS DID THE NOSE L/G. HOWEVER THE R/H MAIN WAS NOT DN + LOCKED AND COLLAPSED AND THE A/C SLID TO A STOP ON THE RH WINGTIP. THE PILOT (AND PASSENGER) DID NOT SUSTAIN ANY INJURIES. THERE WAS NO POST-EVENT FIRE. THE PROPELLER WAS SEVERELY DAMAGED. THE ENGINE REMAINED OPERATING @ LOW RPM UNTIL IT (PROP) CONTACTED THE GROUND ON LDG.

Other reports on N136BF · 1

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