Noha307 wrote:
Since you are familiar with the accident record of the airplane, I'm going to copy-paste a couple of accidents, as written on the Wikipedia article for the aircraft, below as I would like to hear your thoughts on them:
Wikipedia wrote:
- 11 December 1954 during an air demonstration at the christening of aircraft carrier USS Forrestal, pilot Lt J.W. Hood was killed when his F7U-3 had a malfunction with the wing locking mechanism and the aircraft crashed into the sea.
- 30 May 1955 pilot Lt Cmdr Paul Harwell's Cutlass suffered an engine fire upon takeoff on his first flight in the aircraft. Harwell ejected and never flew another Cutlass again. By the time he had landed on the ground, he had spent more airborne time in the parachute than the aircraft.
Pilot Tom Quillin's Cutlass took off as part of a flight of four Cutlasses. Quillin's aircraft had an electrical failure which forced him to abort his training mission and return to base. At the airbase he had to wait in a landing pattern because two other aircraft in the flight also had aborted due to malfunctions in the aircraft. - 14 July 1955 pilot LCDR Jay T. Alkire was killed in a ramp strike on USS Hancock.
- 4 November 1955, pilot Lt George Millard was killed when his Cutlass went into the cable barrier at the end of the flight deck landing area of USS Hancock. The nosegear malfunctioned and drove a strut into the cockpit which triggered the ejection seat and dislodged the canopy. Millard was launched 200 feet (61 m) forward and hit the tail of a parked A-1 Skyraider and later died of his injuries. The captain of Hancock ordered every Cutlass off the ship.
(Source:
Wikipedia)
I am particularly interested in these because they all
sound like pretty clear cut cases of design faults. If this was indeed not the case, what were the actual causes? (Keep in mind, I don't know the answer here and I'm not trying to be accusatory.)
My apologies for the delay - was flying last night until late.
So, allow me to address these accidents highlighted on Wikipedia in reverse order, as the first listed accident differs from the rest.
This said, a lot of things in these listed accidents will serve to highlight my consternation with Wikipedia and their "verifiability versus truth or fact" campaign. Frankly, I find it funny to even be engaged in a conversation that condone's that the truth is not the first and foremost desired outcome, but so be it! For my part, what I offer here are the checked and triple-checked "facts", "verifiable" by Wiki or not....
MILLIARD ACCIDENT
Regarding the Milliard accident: First off, the accident occurred on 01 November 1955, not 04 November. The fourth is when he succumbed to his injuries. Secondly, the pilot was a LTJG, not a Lieutenant. To follow up in this vein, the Wiki review indicates that the "nose gear
malfunctioned and
drove a strut into the cockpit which triggered the ejection seat" Although "verifiable" since this tripe has been repeated in print so many times its better known than the words to
Happy Birthday, its still a bunch of bunk. The facts of this accident are these: George Milliard, who went by "Barry", held off after receiving the cut from the LSO and bypassed all the cross-deck pendants (arresting wires). That was
human error #1. As he proceeded up the antiquated axial deck of the USS Hancock (which allowed no bolter capability due to aircraft spotted on the foredeck) his arresting hook engaged the #2 Davis Barrier cable (which is meant to assist in stopping an errant aircraft by engaging it's landing gear, not its arresting hook). This cable, to exacerbate matters, was mis-rigged by the Hancock's ship personnel for the possible engagement of an AJ Savage heavy bomber/tanker aircraft. This meant that the payout of the cable would be far more firm than that required for a much lighter fighter aircraft.
Human error #2. As a result, the aircraft pitched forward causing the aircraft's nose gear to then engage the #5 Davis Barrier cable and its associated straps, (but again, due to the mis-set tension, was subjected to forces far in excess of design specifications set by BuAer and met completely within contract parameters by Vought in the aircrafts construction).
Human error #2.5 The aircraft, still proceeding forward engaged the Barricade, (designed to arrest the forward motion of the aircraft by engaging its wings in a last ditch effort to avoid incursion into the pack of aircraft spotted forward), and straddled one of the vertical barricade straps. The F7U had a "Barricade Strap Cutter" mounted on its lower nose gear to cut the vertical barricade straps to preclude the full force of the barricade's impediment forces from acting upon the nose gear and not the airframe. This cutter was unfortunately fouled by the Davis barrier strap and was not cut, instead taking the full force of the barreling aircraft on the bottom of the nose gear. The force subjected to the nose gear, which was far in excess of ANY designed or specified requirement, caused the upper trunnion that supported the nose-gear's actuation cylinder to shear from the back of the cockpits armor plate. This trunnion, which has a portion that protrudes through the aft canopy turtle-deck to provide an attach point for the canopy actuation cylinder, sheared through the turtle deck vertically, allowing the nose gear to collapse. Important point: All this occurred BEHIND the cockpit.....No nose gear EVER breached an F7U's cockpit, nor was ANY pilot ever "speared" as is often written by all those "verifiable" source authors. In a freak circumstance, the canopy, which was now dislodged from the aircraft due to its actuator being displaced, departed the machine, arming the ejection seat as designed (when the ejection sequence is normally initiated, the jettisoned canopy pulls the arming pin from the seat allowing it to be fired). The canopy actuator, now broken from its mount point, swung forward and struck the left hand firing cam of the ejection seat as well as knocking out the safety pin of the firing cap, which fired the seat. The pilot was propelled forward into the pack of AD's and struct the vertical tail of one of the parked aircraft, resulting in soon-to-be mortal injury.
The result of this accident, as with lessons learned from all accidents, resulted in modifications and guard placement to prevent another such freak occurrence. It must be emphasized, that this accident was precipitated by multiple human errors, which caused structural stresses above and beyond any design limitations and would have resulted in catastrophe no matter the aircraft type. The shore-basing of the squadron (VF-124) was undertaken in an effort to facilitate investigation of the accident prior to further carrier operations, which was normal protocol for incidents affecting new aircraft on initial deployments.
ALKIRE ACCIDENT
The most famous ramp strike in history is also one of the least understood. I have heard everything from slow spool-up time for the engines, to no visibility from the cockpit as causes for this incident. To diverge from the accident a bit, a few " facts"..... the F7U's J46 engines were not slow to spool in the approach. One would say, "all those old engines were slow to spool!!" But the J46 operates completely different from all other engines.....it is 100% "spooled" in all regimes past a percentage above idle (which varies engine-to-engine ). Thrust is changed by the modulation of the afterburner's petals (or eyelids, if you so prefer). This means that during the approach, you are always fully spooled (insert foot-stomping here!) What was cumbersome, was that if you so desired to use afterburner to dig yourself out of a hole you flew yourself into, the selection of burner initially resulted in the opening, or dilation of the petals to unload the burner allowing it to light-off. This resulted in a momentary LOSS of thrust just when you needed more thrust, until the burner lit and then became effective. As much as this was always a factor in carrier approaches, it really wasn't the cause of the Alkire ramp strike.
Alkires ramp strike was due to one thing and one thing only: attitude. Im not talking about the aircraft's attitude either, although one begets the other.
LCDR Jay Alkire was a land-based patrol pilot who in BuAer's infinite wisdom of the day, transitioned to fighters through the ubiquitous F7U training program.....one week ground school, blindfold cockpit checkout, and a tap on the helmet with the words "good luck son". After joining VF-124 as it's executive officer, he amassed a sizable amount of time (146 hours) in the F7U, but was known to "push" things. When advised by the junior officers in the squadron when he arrived about the advisability of taking the wave off, or aborting an approach if things got low and slow, he admonished them "I've never taken a wave-off in my life, and I never will!" Well, that "attitude" didn't work so well in the end. Alkire launched during work-ups for the deployment over 1000 pounds in excess of maximum landing weight, (human error #1) and to his credit completed one circuit to a successful arrested landing. Following the second launch, still over weight, he turned final long in the groove and began to settle. The LSO, Tom Reilly saw the excessive deviance from the glide path and issued a wave-off signal, which was ignored. As the aircraft began to settle farther and farther, Reilly's wave-offs continued.....all ignored. Afterburner was initiated, and became effective just prior to impact with the ramp, but was precipitated by continued aft-stick forces resulting in an exponential increase in drag versus lift (See the excerpt of the manual so kindly posted which addresses this). Of course, only Alkire can speak to what he was thinking or dealing with, but an analysis of the accident by BuAer found no reason other than pilot error to blame for this horrific accident.
For the record, again in defiance of all oft-repeated "verifiable" sources, NO other personnel were killed in this accident. And this comes directly from the ships logs, gentlemen.
TOM QUILLAN INCIDENT
Oft repeated for comedic effect, the "Number Five (or pick a "verifiable" number) in the Emergency pattern" story is used to disparage the F7U and make it out to be a mechanical disaster waiting to happen. What the magazine and Wikipedia reviewers fail to mention, is the reason why these aircraft all suffered electrical failures after launching. The investigation into the incidents revealed that the starter power cables on the NC-5 "self-propelled electric power plant" being used to start the squadron's alert-line aircraft were reversed following routine maintenance. This caused a reversal in the field of both aircraft's generators in each aircraft, causing complete electrical loss following takeoff. Ironically, this same scenario played out aboard USS Intrepid during the same squadron's (VA-83) deployment, when a similar mistake was accomplished by ship's personnel. Not the F7U's fault.
LCDR HARWELL
More time in a parachute than the airplane....haha ha, ooooh-wee! An oft-chortled knee-slapper to be sure!
First off, details.....His name wasn't Paul Harwell in spite of being referred to as that in Wally Schirra's book "Schirra's Space". He was LCDR Payton O. Harwell, commonly referred to as "Po". Secondly, the accident occurred on 30 March 1955, not 30 May 1955, but hell, who cares about such things, as long as its repeated in multiple Wiki-Friendly sources! Anyway, Harwell was primarily a land-based multi-engine pilot (who eventually attended test pilot school) based at Moffett Field with Fleet Air Service Squadron Ten (FASRON-10). The Transitional Training Unit Pacific (TRANSTUPAC) of VC-3, tasked with checking out the senior officers of prospective F7U squadrons was also based across the field at Hangar 1 at Moffett, and Harwell was a constant visitor, wanting a crack at the Cutlass. His pestering, especially of then LT Walter Schirra, was such that finally VC-3's commander, CDR "Jig Dog" Ramage, gave in and issued the go-ahead to check Harwell out in the Cutlass.... if for no other reason than to stop the constant badgering. Po attended the VC-3 check-out program and was ready for his first (and intended to be ONLY) flight to satisfy his desire to fly the hottest jet in the Navy. Schirra was his wingman instructor pilot. The scenario plays out as reported, they took off and Harwell's aircraft started streaming flames, followed by an explosion which blew off the entire tailcone. Harwell ejected, and did in fact have more time in the chute than airborne in F7U-3 BuNo 128474. But what happened? Nobody seems to care after the chuckles subside and they saunter off to the next amusing anecdote. But what occurred, and actually occurred quite often, was that Harwell's aircraft was brought to the flight line following an engine change. The fuel line to the afterburner (sized like a small fire-hose) was left unconnected following installation of the burner. This resulted in raw fuel spraying all over the aft burner compartment following application of after-burning thrust for takeoff. The spraying fuel pooled in the compartment and lit off, eventually exploding when subjected to the normal high temperatures rushing through the burner at maximum military power. Quite a few F7U engine fire accidents occurred for this reason. I suppose a case can be made that the design of the aircraft precipitated the accident(s) by having the fuel line in a not-easy-to-be-seen location following engine change, but I would opine that perhaps the use of a CHECKLIST, or the employment of a pre-release INSPECTOR might just nip this issue in the bud. Naval aviation in the pre-NATOPS days was just as lax in the maintenance realm as it was in the cockpit, and the F7U bore a sizable brunt of this apathy for checking and double-checking one's work.
Finally.....
LTJG (Not LT) J.W. HOOD
Sad is the case of LTJG John Wylie "Foggy" Hood, USNR. I've left this for last because it is one of the
very few cases that a Cutlass pilot was let down by his aircraft and not the other way around. Hood was a pilot for VF-81, the first squadron to receive the F7U-3. He was taking part in the pre-launch ceremonies for the USS Forrestal at Newport News, VA on 11 Deember 1954. Flying BuNo 129659, he along with a squadron mate, and two pilots from VF-83 were conducting high-speed formation fly-bys of the crowd during the launch and performing a very well rehearsed show for the public. He crashed at 450 knots, ejecting just prior to the impact, but not at a sufficient height to avoid a failure to separate from the seat prior to impacting the bay. The aircraft impacted just short of a tanker ship, the SS Pocahontas Fuel which was being actively loaded with bunker oil at the dock. The cause of the accident was revealed to be the engagement of the wing-fold centering unit, which was a system designed to center and hold firm the ailavator (elevon in non Vought-speak) when the wings were folded in order to prevent impingement on the vertical fins during the folding process. This system engaged in flight, either through mechanical breakage or detachment of fasteners, and locked his ailavators precluding any pitch adjustment. He was in a nose low attitude when the unfortunate engagement occurred and was unable to alter his course into the bay. The system was redesigned to preclude a repeat of this accident. So.....that one I'll give you - that was a bad design of that system, but it was rectified and never occurred again.
Hope this helps, despite my inability to not take the easy shots at Wikipedia!
Al