Thread: Cessna C337 SID
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Unread 08-29-09, 12:11 PM
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Ernie Martin Ernie Martin is offline
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Wichita Meeting

We had a productive meeting with Cessna yesterday. There were 9 people from Cessna and these 7 guests/users: 3 owners (Steve Keller, Steve Walz and me, all very familiar with the aircraft), 2 from Commodore Aerospace (Don Nieser and his structures person, Larry Good) and 2 from AirScan (which operates 23 late-model Skymasters).

For context let me mention that this SID exercise is FAA driven and is expected to be followed by similar exercises for other Cessna aircraft models.

Here, in brief, are my impressions:

1. Cessna has been working on this for roughly 6 months or more. Some of the documents date to March and some of the Cessna people at the meeting visited Steve Keller about 6 months ago to get a first-hand look at his airplane (most of these people were unfamiliar with Skymasters because they were not around when they were designed, built and tested, and Cessna does not have a significant database of experience with the aircraft).

2. Unlike the 400-series SID program, this is an experience-based, not analytically-based program. No finite-element structural analysis of the aircraft is planned. Instead, the Cessna people went to the FAA's Service Difficulty Reports (SDRS) database and used that as the basis for the proposed SIDs. At the time of the meeting, Cessna had written draft SIDs and the meeting was in part intended to get the users’ inputs on these proposed SIDs.

3. Approximately 23 proposed SIDs were reviewed, some in more detail than others.

4. For some, the guests were surprised by, and expressed disagreement with, the area in question and/or the initial compliance requirement (for instance, 7,500 hrs or 20 years).

a) As an example, one may call for an inspection for cracks in a wing area where none of the users have ever seen a crack, either on very-high-time aircraft or aircraft that have seen high-load accidents, yet there were no SIDs for other areas of the wing which are susceptible to damage due to fatigue or excessive loads.

b) Or one may call for inspection at 20 years (from manufacture) when it’s a fatigue (not corrosion) issue, so that an aircraft which has sat in a hangar since manufacture and never flown would be subject to this SID looking for fatigue cracks. Or the SID may call for an inspection requiring massive aircraft disassembly even if there is no corrosion evident in easy-to-inspect adjacent/comparable areas.


5. As a result of these user comments, Cessna agreed to look more closely at the SDRS data (some of which are 15 – 20 years old) to try to determine whether they may have come from questionable aircraft or sources (e.g., an aircraft which may have had an earlier accident and/or improper repair) or misidentified the aircraft or part. Inquiries I performed after the meeting suggest that FAA SDRS data is generally considered suspect in the aircraft maintenance business. If true, then Cessna’s re-examination may bear fruit.

6. Moreover, Don (a retired Air Force Lt. Col. who has over 20 yrs experience with our aircraft, worked for years on aging aircraft and corrosion research for the Air Force, has disassembled and restored dozens of Skymasters, and has many Skymaster aircraft and parts which Cessna can examine) invited Cessna to visit him and see first-hand why he believes that some of the proposed SIDs need re-examination. Roughly, his words were “When you see this item, especially one removed from a high-load, high-fatigue aircraft, you’ll see right away that this item can’t fail that way, that other parts will fail first, that the SDRS data must be from a suspect aircraft or refer to a different part”.

7. Cessna also agreed to re-examine the initial compliance requirements, including the possible removal of years-since-manufacture requirement.

8. We were asked to estimate the manpower requirement for each SID.

9. I don’t have at this point a schedule of future activities. There wasn't enough time to review all of the proposed SIDs, so we are continuing their review. We talked about the next meeting of this group perhaps held both in person and as a WebEx Internet meeting. With the caveat that all of these points are my impressions, I believe that such a meeting will likely come after we have submitted our views on the unreviewed SIDs and after points 4 – 6 above are addressed. I’m hoping that Cessna goes to Don’s shop (it’s a 3 hour drive) and that Don (and perhaps AirScan and others) can furnish point 7 after that. I expect to contact Cessna and hope to get a better feel for future activities.

In summary, there are some issues that we’re all working through, but I found the Cessna people competent, professional and receptive to considering our points. The attendance of Don and Larry was crucial and I hope that they can continue contributing.

Ernie
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