20160507007769A

Accident · Destroyed

FAA accident report · Beech G35 · Surprise, AZ · May 7, 2016

Date
May 7, 2016 · 16:56 local
Place
Surprise, AZ
Phase of flight
Cruise/Level Flight
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N4401D
NTSB investigation
NTSBWPR16FA102
Reported as
Beech G35
Reported engine
Continental E225 series
People aboard
2
Fatal injuries
1
Other injuries
1
Pilot’s certificates
Commercial pilot, flight instructor

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.

At 2330, the acft departed kgeu, performed a touch and go back to kgeu at 2337 and crashed at 2354 with the beginning of the event occurring around 2347 at 3,800 MSL (aprx 2,600 AGL).

Post-accident investigation revealed the attaching hardware connecting the linkage between the carburetor and the throttle control was not intact. Hardware consistent with the required linkage attaching hardware (bolt and castellated nut, no cotter pin) was found in the engine cowling during post-crash investigation. No other technical or operational factors were identified during the post-crash investigation.

During an interview with the certificated airman that returned the acft to service, post carburetor installation, the airmen stated that while he has assistance from a non-certificated person, he had visually confirmed that carburetor attachments, including the cotter pin were installed/connected as part of the carburetor installation.

As the FAA filed it

AT 2330, THE ACFT DEPARTED KGEU, PERFORMED A TOUCH AND GO BACK TO KGEU AT 2337 AND CRASHED AT 2354 WITH THE BEGINNING OF THE EVENT OCCURRING AROUND 2347 AT 3,800 MSL (APRX 2,600 AGL).

POST-ACCIDENT INVESTIGATION REVEALED THE ATTACHING HARDWARE CONNECTING THE LINKAGE BETWEEN THE CARBURETOR AND THE THROTTLE CONTROL WAS NOT INTACT. HARDWARE CONSISTENT WITH THE REQUIRED LINKAGE ATTACHING HARDWARE (BOLT AND CASTELLATED NUT, NO COTTER PIN) WAS FOUND IN THE ENGINE COWLING DURING POST-CRASH INVESTIGATION. NO OTHER TECHNICAL OR OPERATIONAL FACTORS WERE IDENTIFIED DURING THE POST-CRASH INVESTIGATION.

DURING AN INTERVIEW WITH THE CERTIFICATED AIRMAN THAT RETURNED THE ACFT TO SERVICE, POST CARBURETOR INSTALLATION, THE AIRMEN STATED THAT WHILE HE HAS ASSISTANCE FROM A NON-CERTIFICATED PERSON, HE HAD VISUALLY CONFIRMED THAT CARBURETOR ATTACHMENTS, INCLUDING THE COTTER PIN WERE INSTALLED/CONNECTED AS PART OF THE CARBURETOR INSTALLATION.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.