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Different Engines Possible
I agree with Ernie Martin and Roger.
I have a degree in Aerospace Engineering and an MBA. I own and operate Commodore Aerospace Corp where we specialize exclusively in Skymaster 337 and 0-2 aircraft. I spent 15 yrs in the aerospace industry at GE, LTV, McDonald Douglas, Bell Aerospace and my last 25 yrs working for the USAF at Tinker AFB depot. In my carreer I worked advanced aircraft designs, testing and analysis, aircraft accident investigations, aircraft stuctures, and aging aircraft corrosion research. With my background and experiece I can appreciate the extensive "slide rule era" engineering Cessna people did in designing the safest small twin aircraft, the 337 and 0-2 Skymasters. At Commodore Aerospace we try very hard to not quickly change the original Cessna design unless we have done a very careful and extensive analysis. Ernie is right, any change or mod must be analyzed using a "Systems Engineering" approach because everything is interrelated. See our company profile on page 43. Cessna Pilots Association magazine Aug 2010. We are in business to serve all you Skymaster owners with original Cessna parts and equipment. www.02337parts.com Don Nieser 405-503-4686 nieser.02.337parts@juno.com |
Guess the skymaster-pinto wasn't a good idea
NTSB Identification: LAX74FUQ18 14 CFR Part 91 General Aviation Aircraft: A.V.E.MIZAR 210, registration: N68X ---------------------------------------------------------------------------------------------------------------------------- FILE DATE LOCATION AIRCRAFT DATA INJURIES FLIGHT PILOT DATA F S M/N PURPOSE ---------------------------------------------------------------------------------------------------------------------------- 3-3128 73/9/11 OXNARD,CALIF A.V.E.MIZAR 210 CR- 2 0 0 MISCELLANEOUS PRIVATE, AGE 40, 2758 TIME - 1605 N68X PX- 0 0 0 TEST TOTAL HOURS, UNK/NR IN DAMAGE-DESTROYED OT- 0 0 0 TYPE, NOT INSTRUMENT RATED. NAME OF AIRPORT - VENTURA COUNTY DEPARTURE POINT INTENDED DESTINATION OXNARD,CALIF LOCAL TYPE OF ACCIDENT PHASE OF OPERATION AIRFRAME FAILURE: IN FLIGHT LANDING: TRAFFIC PATTERN-CIRCLING PROBABLE CAUSE(S) AIRFRAME - WINGS: BRACING WIRES,STRUTS MISCELLANEOUS ACTS,CONDITIONS - LOOSE,PART/FITTING MISCELLANEOUS ACTS,CONDITIONS - POOR WELD PERSONNEL - PRODUCTION-DESIGN-PERSONNEL: POOR/INADEQUATE DESIGN FIRE AFTER IMPACT REMARKS- ACFT/PINTO CAR COMB.R WG STRUT ATTACH FITTING FAILED AT AUTO BODY PANEL.DMGD OTR CAR & TRAILER. |
One report said that they used sheet metal screws to attach the boom and tail. Not the best practice.
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