KAPF - Naples Florida - Challenger crash on highway
The truck would be acting more like an out-of-control roller skate. I would have mentioned the truck driver as an agent in the steering if that was what I intended to convey.
Kudos to cabin attendant
We’ve been briefing pax and F/A on the baggage door as a third means of egress for years, but it was put there to load bags. Most bizjets use a baggage door, it’s not an airliner.
A question for our erudite 601/604/605 drivers: if this scenario occurred, is there any plausible way to recover an engine in sufficient time (~1000 ft AGL, landing configuration, dropping like a stone) to avoid contact with terra firma?
But I would also add, that the chance of this happening to BOTH thrust levers is extremely remote. I say this having flown as PM from the LHS of a 604 (and actuated the flaps) on many occasions.
The CVR would likely reveal much more - was it recovered/useable?
Preliminary report noted “FDR revealed” L/R engine oil warnings. Thus assume good FDR data. This crash far more forgiving to FDR/CVR than N605TR (Truckee) crash and latter yielded good FDR/CVR data. If N823KD FDR same type as N605TR, then thrust lever (TL) position not FDR parameter. For N605TR, TL position was estimated from N1. However, N605TR FDR did record engine fuel flow as a direct parameter. If same for N823KD, then FDR should make clear if TLs were pulled over gate to shutdown.
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I wouldn’t say “never”, I know of at least a few ex-UA cabin crew who are now doing charters instead. It’s definitely rare, but not necessarily unheard of.
Which is awesome but they are bringing their own knowledge and experience with them.. they are likely not being trained nor qualified in the legal sense to act as crew. Thats why its “easy” to pick up work as contract cabin servers on both 91 and 135 gigs..
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Not arguing that there shouldn’t likely be some additional training requirements. Just observing that there are examples of trained people working in that side of the industry too.
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Not total failure but serious problems with both engines in flight:
AAIB Formal Report: G-POWN, Engine malfunction after takeoff from London Gatwick Airport
[I can't make it a link, not enough posts on here]
Edit to add - I assume fuel quantity, if recorded, would be a clue.
Despite the Gulstream having larger than most cabin windows including over-wing exits, we always doubted due the size of most of our passengers hat they could egress that way and if tried would block the remaining persons!
Thoroughly enjoyable experience as we got away with it
Again assuming similarity with N605TR, the FDR collects data for Fuel Qty-Aux and Fuel Qty-L/R/Tail.
In this case the engines failed within 1 sec of each other.. so simultanous as you can get.. no way in heck that tallies with BOTH collector tanks empty at almost exactly same time…
How did this fuel shut off design ever get certified if it is so vulnerable to inadvertent activation when aircraft is flown from the right seat? Is this design weakness emphasized when converting to type?