20040903021759A

Accident · Substantial damage

FAA accident report · Beech F33A · Fresno, CA · September 3, 2004

Date
September 3, 2004 · 16:30 local
Place
Fresno, CA
Airport
Fresno Yosemite International Airport
Phase of flight
Level Off Touchdown
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N1854N
NTSB investigation
NTSBLAX04LA312
Reported as
Beech F33A
People aboard
2
Fatal injuries
0
Pilot’s flight hours
668 total28 in this make and model28 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) On 9/3/04, Mr. Rathgeber flew N1854N from ksna on a VFR flight to O68. While entering the pattern at O68 he detected a loss of pitch control after lowering the landing gear and selecting approach flaps. After retracting gear and flaps and initiating a climbout, all controls functioned normally. He diverted to kfat, a larger airport with more facilities and informed Fresno TRACON of his difficulty. With fire equipment standing by, N1854N was cleared to land on runway 29L. Mr. Rathberger reported flying his approach at approx 80-90 knots and selected gear down and landing flaps at 500'AGL. At approx 40' AGL, he reported that the nose dropped and the aircraft impacted the runway in a nose low attitude. Mr. Bob lawrence of Fresno jet center assisted the FAA and NTSB in the investigation and the following is a summary of the facts: at the accident site, Mr. Lawrence noted resistance to full up movement of the elevator controls. He stated that the elevator could only be moved to partial full up travel. After placing the pilot's control to full down elevator, then full up, the resistance was still there. Mr. Lawrence was able to overcome the up elevator control resistance by pullinghard on the controls. At that point he heard a popping noise originating from the rear of the fuselage, and then full up elevator travel was obtained. During further investigation, a failure of the autopilot pitch control servo was discovered. A malfunction-defect will be completed for the servo. The pilot stated that on the flight from ksna to O68 he engaged the autopilot and experienced an abnormality in elevator pitch control. He disconnected the autopilot and did not attempt to re-engage it. During further investigation, a malfunction of the autopilot pitch control servo was discovered. A malfunction defect report will be completed for the servo.

As the FAA filed it

(-23) ON 9/3/04, MR. RATHGEBER FLEW N1854N FROM KSNA ON A VFR FLIGHT TO O68. WHILE ENTERING THE PATTERN AT O68 HE DETECTED A LOSS OF PITCH CONTROL AFTER LOWERING THE LANDING GEAR AND SELECTING APPROACH FLAPS. AFTER RETRACTING GEAR AND FLAPS AND INITIATING A CLIMBOUT, ALL CONTROLS FUNCTIONED NORMALLY. HE DIVERTED TO KFAT, A LARGER AIRPORT WITH MORE FACILITIES AND INFORMED FRESNO TRACON OF HIS DIFFICULTY. WITH FIRE EQUIPMENT STANDING BY, N1854N WAS CLEARED TO LAND ON RUNWAY 29L. MR. RATHBERGER REPORTED FLYING HIS APPROACH AT APPROX 80-90 KNOTS AND SELECTED GEAR DOWN AND LANDING FLAPS AT 500'AGL. AT APPROX 40' AGL, HE REPORTED THAT THE NOSE DROPPED AND THE AIRCRAFT IMPACTED THE RUNWAY IN A NOSE LOW ATTITUDE. MR. BOB LAWRENCE OF FRESNO JET CENTER ASSISTED THE FAA AND NTSB IN THE INVESTIGATION AND THE FOLLOWING IS A SUMMARY OF THE FACTS: AT THE ACCIDENT SITE, MR. LAWRENCE NOTED RESISTANCE TO FULL UP MOVEMENT OF THE ELEVATOR CONTROLS. HE STATED THAT THE ELEVATOR COULD ONLY BE MOVED TO PARTIAL FULL UP TRAVEL. AFTER PLACING THE PILOT'S CONTROL TO FULL DOWN ELEVATOR, THEN FULL UP, THE RESISTANCE WAS STILL THERE. MR. LAWRENCE WAS ABLE TO OVERCOME THE UP ELEVATOR CONTROL RESISTANCE BY PULLINGHARD ON THE CONTROLS. AT THAT POINT HE HEARD A POPPING NOISE ORIGINATING FROM THE REAR OF THE FUSELAGE, AND THEN FULL UP ELEVATOR TRAVEL WAS OBTAINED. DURING FURTHER INVESTIGATION, A FAILURE OF THE AUTOPILOT PITCH CONTROL SERVO WAS DISCOVERED. A MALFUNCTION-DEFECT WILL BE COMPLETED FOR THE SERVO. THE PILOT STATED THAT ON THE FLIGHT FROM KSNA TO O68 HE ENGAGED THE AUTOPILOT AND EXPERIENCED AN ABNORMALITY IN ELEVATOR PITCH CONTROL. HE DISCONNECTED THE AUTOPILOT AND DID NOT ATTEMPT TO RE-ENGAGE IT. DURING FURTHER INVESTIGATION, A MALFUNCTION OF THE AUTOPILOT PITCH CONTROL SERVO WAS DISCOVERED. A MALFUNCTION DEFECT REPORT WILL BE COMPLETED FOR THE SERVO.

NTSB investigation

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