19990815024639A

Accident · Substantial damage

FAA accident report · Cessna 337 · Edgewood, NM · August 15, 1999

Date
August 15, 1999 · 09:20 local
Place
Edgewood, NM
Airport
Sandia Airpark Estates Airport
Phase of flight
Forced/Precautionary Landing
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N99MH
NTSB investigation
NTSBDEN99LA145
Reported as
Cessna 337
Reported engine
Continental IO360C
People aboard
2
Fatal injuries
0
Pilot’s flight hours
1,437 total201 in this make and model5 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.

(.19) On August 15, 1999, approximately 0920 mountain daylight time, a Cessna 337, N99MH, was substantially damaged when it collided with terrain during a forced landing near Edgewood, new Mexico. The commercial pilot and his passenger were not injured. Visual meteorological conditions prevailed, and no flight plan had been filed for the personal flight being conducted under title 14 CFR part 91. The flight had originated just minutes before the accident with an intended destination of belen, new Mexico. According to the pilot, during climbout the rear engine lost partial power. The pilot turned around and tried to return to the airpark, but the airplane would not maintain altitude. (-23) pilot stated immediately after departure, lost power (partially) on rear engine. Pilot decided to return to airport and make a downwind landing. During this process, pilot believed he had "made the airport". Landing gear was then lowered. After lowering the gear, the pilot then decided he could not make the airport and, instead, would "crash under control". Aircraft impacted/skidded into terrain about .3 mile west/southwest of Sandia airpark. Substantial damage to aircraft. No injuries. Post accident investigation revealed safety wire on the rear prop control cable had broken, which allowed the prop control cable to "flex" when the RPM was reduced after t/off. (.4) during climbout after takeoff, the rear engine lost partial power (1,700 RPM). The pilot started to turn around and return to the airpark, but changed his mind and decided to maintain aircraft control by landing in a rough and uneven but open field. Postaccident examination disclosed the safety wire securing the propeller control cable to the support bracket had broken, allowing the cable housing to flex within the engine compartment. When the pilot reduced RPM to climb power, the safety wire broke. This prevented the pilot from feathering or changing the rear propeller pitch settings.

As the FAA filed it

(.19) ON AUGUST 15, 1999, APPROXIMATELY 0920 MOUNTAIN DAYLIGHT TIME, A CESSNA 337, N99MH, WAS SUBSTANTIALLY DAMAGED WHEN IT COLLIDED WITH TERRAIN DURING A FORCED LANDING NEAR EDGEWOOD, NEW MEXICO. THE COMMERCIAL PILOT AND HIS PASSENGER WERE NOT INJURED. VISUAL METEOROLOGICAL CONDITIONS PREVAILED, AND NO FLIGHT PLAN HAD BEEN FILED FOR THE PERSONAL FLIGHT BEING CONDUCTED UNDER TITLE 14 CFR PART 91. THE FLIGHT HAD ORIGINATED JUST MINUTES BEFORE THE ACCIDENT WITH AN INTENDED DESTINATION OF BELEN, NEW MEXICO. ACCORDING TO THE PILOT, DURING CLIMBOUT THE REAR ENGINE LOST PARTIAL POWER. THE PILOT TURNED AROUND AND TRIED TO RETURN TO THE AIRPARK, BUT THE AIRPLANE WOULD NOT MAINTAIN ALTITUDE. (-23) PILOT STATED IMMEDIATELY AFTER DEPARTURE, LOST POWER (PARTIALLY) ON REAR ENGINE. PILOT DECIDED TO RETURN TO AIRPORT AND MAKE A DOWNWIND LANDING. DURING THIS PROCESS, PILOT BELIEVED HE HAD "MADE THE AIRPORT". LANDING GEAR WAS THEN LOWERED. AFTER LOWERING THE GEAR, THE PILOT THEN DECIDED HE COULD NOT MAKE THE AIRPORT AND, INSTEAD, WOULD "CRASH UNDER CONTROL". AIRCRAFT IMPACTED/SKIDDED INTO TERRAIN ABOUT .3 MILE WEST/SOUTHWEST OF SANDIA AIRPARK. SUBSTANTIAL DAMAGE TO AIRCRAFT. NO INJURIES. POST ACCIDENT INVESTIGATION REVEALED SAFETY WIRE ON THE REAR PROP CONTROL CABLE HAD BROKEN, WHICH ALLOWED THE PROP CONTROL CABLE TO "FLEX" WHEN THE RPM WAS REDUCED AFTER T/OFF. (.4) DURING CLIMBOUT AFTER TAKEOFF, THE REAR ENGINE LOST PARTIAL POWER (1,700 RPM). THE PILOT STARTED TO TURN AROUND AND RETURN TO THE AIRPARK, BUT CHANGED HIS MIND AND DECIDED TO MAINTAIN AIRCRAFT CONTROL BY LANDING IN A ROUGH AND UNEVEN BUT OPEN FIELD. POSTACCIDENT EXAMINATION DISCLOSED THE SAFETY WIRE SECURING THE PROPELLER CONTROL CABLE TO THE SUPPORT BRACKET HAD BROKEN, ALLOWING THE CABLE HOUSING TO FLEX WITHIN THE ENGINE COMPARTMENT. WHEN THE PILOT REDUCED RPM TO CLIMB POWER, THE SAFETY WIRE BROKE. THIS PREVENTED THE PILOT FROM FEATHERING OR CHANGING THE REAR PROPELLER PITCH SETTINGS.

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 N99MH · 2

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