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-   -   Different engines possible? (http://www.337skymaster.com/messages/showthread.php?t=2888)

Don Nieser 05-12-11 11:49 PM

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

Frank Benvin 05-15-11 02:52 PM

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.

hharney 05-15-11 05:14 PM

One report said that they used sheet metal screws to attach the boom and tail. Not the best practice.


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