bnt83
Final Approach
Try to get an R model.
R model was just inflicted with more frequent eddy current inspection of lower wing spar caps than older cantilevers.
Try to get an R model.
P210 and practical. Two things one rarely hears in a GA conversation.
I'd make sure they have the 800 # for SWA in their phone contacts....
I agree. One owner right now is budgeting a FWF overhaul and looking at roughly $60k-70k. I'm pretty sure they have a 1600 hr or 1800 hr TBO. (I'm aware TBO isn't required but still.)
60-70k!
Seems quite high for a 520/550.
R model was just inflicted with more frequent eddy current inspection of lower wing spar caps than older cantilevers.
Great... What was the basis? Are they starting to see more problems? Did they put a life limit on the airframe like a P-Baron?
I'm unfamiliar with the P Barron.
They (Cessna) has been very busy writing SIDS for every model from 100 series to 400 series. The 210 (cantilevers) were issued a new, never-been-seen-before on a legacy Cessna, Airworthiness Limitation section that was approved by the FAA (FAA signature of the cover), which is the eddy current inspection requirements. The early spars were made from a different series of alloy than the later ones and the inspection intervals reflect that (it says right in there which alloys they were made from but I can't remember and being lazy).
Each SID list a "theoretical" life limit or 13,000 hrs with no calendar life limit believe.
Interesting, thanks. The P-Baron has a 10,000hr life limit on the airframe IIRC, at that point it turns into a pumpkin, I don't believe there is any inspection for extension. Is that 13,000hr number a suggestion or a deadline?
Interesting, thanks. The P-Baron has a 10,000hr life limit on the airframe IIRC, at that point it turns into a pumpkin, I don't believe there is any inspection for extension. Is that 13,000hr number a suggestion or a deadline?
You'll be happy to know that the SIDs go EFFING crazy with eddy current. Beechcraft was happy to use dye penetrant on the carry thru spar cracking, but not Cessna - we're too good for that.
For instance
D637-1TR9 (100 Series 1963-1968)
Model 150 Serial Numbers 644, 649, 15059701 thru 15069308,Model F150 Serial Numbers F150-0001 thru F150-0389,Model 172 Serial Numbers 639, 17249545 thru 17257161,Model F172 Serial Numbers F172-0001 thru F172-0559,Model P172 Serial Numbers P17257120 thru P17257188,Model FP172 Serial Numbers FP172-0001 thru FP172-0003,Model 182 Serial Numbers 18254424 thru 18259305,Model A182 Serial Numbers A182-0001 thru A182-0116
Requires Eddy Current on the nose gear torque links every 3000 hrs or 5 years, whichever is first.
D. Inspect the nose gear upper torque link for cracks in the area of the stop block and the flanges of the “I”
section of the link, using surface eddy current inspection. Refer to Section 2A-13-01 Non-destructiveInspection Methods and Requirements, Eddy Current Inspection - Surface Inspection, for additionalinstructions.
Interesting. I wonder how many of these SIDs are driven by the insurance companies?
60-70k!
Seems quite high for a 520/550.
FWF would include the engine, the turbo, the exhaust system and all accessories as well as the prop, plus labor.
60-70k would be about right.
The basis for all of the Cessna SIDS are very simple, liability, sales and lawyers.
Cessna never intended these airplanes to have an unlimited life. With the legal culture of the US they are flying lawsuits, no matter what causes the accident. Also, by people keeping old models flying it lessens the market for newer models.
Yep. He wants a fresh start, probably the cheapest way to go. Doing stuff one thing at a time wastes a lot of downtime, access, R&R etc.
All those planes are far older than 14 years, so it's not particularly their liability that is the concern.
BS. Anytime one crashes, the lawyers will sue the manufacturer, the engine manufacturer, the prop manufacturer, the avionics manufacturer, anyone who serviced the airplane, etc, etc, etc.
Even if it doesn't see a court, it's still expensive to settle.
An aging airframe with outstanding inspections is a lawyers dream. If Cessna stacks enough intrusive and expensive inspections on an airframe, then eventually the plane is not viable and goes away.
BS. Anytime one crashes, the lawyers will sue the manufacturer, the engine manufacturer, the prop manufacturer, the avionics manufacturer, anyone who serviced the airplane, etc, etc, etc.
Even if it doesn't see a court, it's still expensive to settle.
An aging airframe with outstanding inspections is a lawyers dream. If Cessna stacks enough intrusive and expensive inspections on an airframe, then eventually the plane is not viable and goes away.
The manufactures do not self insure to the best of my knowledge.
Well, duh!:
Do you think their insurance providers provide free policies?
What happens to premiums every time they have to pay out in a lawsuit? Think those premiums remain the same?
The premiums on the old stuff are already paid and done. The current premiums are set by current production and therefor are limited by market competition.
Its like the courts are the managers of a day care center...
http://www.nbcnews.com/business/consumer/red-bull-drinkers-can-claim-10-over-gives-you-wings-n221901
That's the typical reaction when people finally understand how the insurance industry works.
I have a good understanding of insurance and how litigation works.....
You, however....