Bob

Would you be interested in doing a memoir or reminiscence about your lawyerly years in aviation for an ABA publication?  Both your experiences and reflections would be a great read for younger lawyers. If so, please contact me at [email protected]

Scott Wilson


On Jan 19, 2026, at 12:52 PM, Randal Craft via Mifnet <[email protected]> wrote:



Mike, in response to your question, no, I am no longer practicing law.  At the end of 2020 I retired from my law firm, Holland & Knight.  Fifty-two years of practicing aviation law, product-liability law, and non-profit law were probably enough.  (I never had an uninteresting day, but there were some days I would certainly like to forget.)  As best I could tell, I still had my wits about me, but it was a propitious time to retire even though the pandemic precluded any parades, farewell tours, or festive get-togethers to mark the event.

 

I didn’t plan to stay at my firm that long; it just happened naturally (“organically” is the word people use these days).  The retirement also happened naturally and seemed less like a watershed because in 2020 I was, like everyone else, already chronologically disoriented.  Having been marooned in our home for so long, I found that retirement did not bring much of a lifestyle change.

 

In addition, I retired from decades-long positions as General Counsel (on a pro bono basis) of The Wings Club (where my law-partner Rich Furey replaced me) and the New York City Ballet (where I continue to be actively involved on the Board as a Director Emeritus). 

 

Despite retirement, I still don’t have enough time to keep up with, much less respond to, the Mifnet emails, so I submit comments only occasionally.

 

         Bob

 

Randal Craft

Email: randalrobertcraft@gmailcom

Mobile: 646-226-2299 (USA)

 

From: Mike Borfitz via Mifnet <[email protected]>
Sent: Saturday, January 17, 2026 4:03 PM
To: Mike Borfitz via Mifnet <[email protected]>
Cc: Mike Borfitz <[email protected]>
Subject: [Mifnet
đź›° 75154] Re: AA Flight 191 DC-10 Crash at ORD

 

 

My faith is restored: 

"...cracks in the engine pylon aft bulkhead (not a bearing)..." I thought the bearing comment was a little odd.

 

Still, Boeing is in trouble again. The public probably won't get spooled up, however. No less a tragedy but freighter accidents tend to fade.

 

My bet is that it was an error rather than a management push to cut corners. Small fleet with many many cycles & hours; "Shouldn't be a problem."

 

Are you still practicing?  My guess is no, ORD was a long time ago.

 

Mike Borfitz

Cell         206-714-8797

Kilroy Aviation LLC

 

Kilroy is available for aviation regulatory and safety issues

- Type & Production Certification, Continued Operational Safety

- International validation & safety matters

- Program & system management

- FAA STC ODA

 

On Sat, Jan 17, 2026, 12:16 PM Randal Craft via Mifnet <[email protected]> wrote:

I was lead counsel to American Airlines in the NTSB investigation of the 25 May 1979 DC-10 crash of Flight 191 at O’Hare and in the FAA investigation and subsequent grounding of all DC-10 aircraft.  In light of the latest articles and emails referring to that crash, I probably should repeat some points I’ve made previously.

 

The MDC manuals were not dispositive on the use of a fork-lift engine-replacement procedure, and there was some controversy about what had been orally said (and meant) by MDC personnel to AA about the proposed fork-lift procedure that was blamed for the cracks in the engine pylon aft bulkhead (not a bearing) that led to the loss of the engine and, in turn, the airplane.  AA was under the impression that MDC thought the procedure was acceptable, in part because, as reflected in the written record described in the NTSB report, MDC was aware of AA's proposed fork-lift procedure and, without objection, supplied requested C.G. data so AA could use this procedure.  MDC apparently also did not object to Continental's use of this procedure.

 

I tried three cases (one against lawyer/aviator F. Lee Bailey) in which some details of the flight were at issue.  The pilots followed the manual’s engine-out procedure; they had no way of knowing that not only had they lost power on the left engine but that they had also lost the nacelle, the pylon, and part of the leading edge of the wing.  All this damaged some hydraulic lines and caused a loss of hydraulic pressure and retraction of outboard leading-edge slats on the left wing, which increased the left wing’s stall speed to a speed above the speed called for in the engine-out procedure.

 

Seconds after lift-off, the left wing started entering into a stall, causing the airplane to begin rolling to the left.  Impact with the ground occurred eleven seconds or so after that roll began.

 

As for the DC-10 grounding, it should be noted that the grounding was based on the FAA’s mistaken conclusion that the cracks in the pylon aft bulkhead that were discovered in a series of post-accident AD-directed fleet inspections had actually grown during the inspection period.  Before the grounding, I spoke by telephone and met in person with the AA inspection team that found the pylon bulkhead cracks, and their view was that the bulkhead cracks had not developed or grown during the series of post-accident inspections of the fleet.  They pointed out that the cracks in question had not been found in the earlier inspections because the earlier ADs had not called for inspections in the area where these cracks were later found.  Indeed, a chief reason why there was a series of ADs was that the areas to be inspected kept being clarified and expanded.  It was a later AD in the series that called for inspections of the location where the cracks in question were found.  My understanding was that this information was passed on to the FAA but was discounted.  The grounding followed.

 

A pre-grounding internal FAA inspection report indicated that the local (SFO) FAA inspectors agreed with AA that the cracks in question were pre-existing and were in a location that was not to be inspected in the original rounds of post-accident inspections (and this was confirmed in subsequent testimony of FAA personnel).  I understand that AA's head of maintenance also argued to Craig Beard of the FAA that the cracks were pre-existing and not an appropriate basis for a grounding.  I believe there was even a much-later FAA report that concluded that the FAA's instructions in the initial ADs were not adequate to reveal the cracks found later in the pylon aft bulkhead.  Accordingly, in my view the grounding of the DC-10 was not justified.

 

Bob

 

Randal Craft

Email: randalrobertcraft@gmailcom

Mobile: 646-226-2299 (USA)

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