MISHAPs: 31 DEC 51 A/C: PBM-5 Location: 1/4mi.NW, Channel Rock,Hong Kong Strike: Yes BUNO: 84682 Cause: CRSHED Contributed by Terry firstname.lastname@example.org [17MAR98]
BA1 Mishap Photo's "...Salvage operation 2 JAN 52..." Contributed by Frank Breitenstein email@example.com [11AUG2000]
BA1 Mishap Crew Photo "...BA1 crew taken at NS Sangley Point, Philippines 10 October 1951. A. E. Baxter, is the third from the right in the bottom row of the smaller photo showing the nose of the plane and the middle person in the bottom row of the closeup photo ..." Contributed by Frank Breitenstein firstname.lastname@example.org [11AUG2000]
"...The top photo back row: Orville O. Seal, AOAN; Ens. R. H. Wilson; Ens, Fendorf; Cdr. W. T. Hardaker; Ens. Reynolds; Ens. Bentley; James E. Finau, AN -- front row: D. E. Tripp, AM3; W. G. Rabb,AN; Jolly W. Britton, AD1; A. O. Vickers, AL1; Alfred O. Baxter, AOAN; R. D. Brown, AT2; S. V. Neville, AN...The bottom photo is arranged slightly differently with the back row: Seal, Reynolds, Fendorf, Hardaker, Bentley, Wilson, Neville. Front row: Tripp, Britton, Vickers, Baxter. Brown, Raab, and Finau...The crew members that died in the Hong Kong crash were: Britton, Baxter, Finau, and Neville..." Contributed by Frank Breitenstein email@example.com [01DEC2000]
"...Rhonda Spruill: I saw your remarks in the VP Squadron page about the crash of BA1 in Hong Kong. It brought back memories. I've several photos of the salvage operation in Hong Kong and of BA1 and crew at Sangley Point prior to the crash. I was and aerial photographer with VP-47...Frank Breitenstein firstname.lastname@example.org..." [19JUL2000]
"...I'm the niece of AD3 Alfred Eugene Baxter of VP-47. Flight crew on BA1, during the Korean Conflict. He died when the plane went down. If anyone has more info please let me know...Rhonda Spruill email@example.com..." [12SEP99]
"...re: VP 47 wreck which occurred 13 Oct 43 Acft BUNO 84682. I have some doubts about the accuracy of this information. 1. VP 47 didn't exist until 1949...2. BUNO appears to be a fairly late BUNO which I question the production date of an aircraft with such a high BUNO, let alone being operational in WestPac in 1943...3.VP 47 Did in fact lose an aircraft in Hong Kong Kowloon Bay on 31 Dec 1951...4. The aircraft lost an engine the night before and went into HK for an emergency single engine landing...5. During the attempt to lighten ship a piece of engine stand being thrown overboard sailed upward and cut the fabric of the underside of one of the elevator control surfaces. The plane captain made emergency repairs the next morning using an extra locking pin to hold the elevator in place while he made repairs. Upon completion of the repairs, the Plane Captain failed to remove the spare locking pin...6. On takeoff, the lack of elevator control caused the aircraft to crash killing 4 enlisted crewmembers. The pilot, co-pilot and two crewmembers survived with injuries...7. The deceased crewmembers were: Jolly W. Britton AMM1, Alfred E. Baxter AMM3, James E. Finau AN and Shelby V. Neville AN..." Contributed by George Littlefield Stuart firstname.lastname@example.org [18AUG98]
MISHAPs: 26 DEC 52 A/C: PBM-5 Location: East Coast of Korea Strike: Yes BUNO: Unknown DEATHS: 10 Cause: Unknown. Lost: LT William Dale Anderson, ENS Wayne Eugene Bancroft, AN Ernest Newton Franklin, AEN John Alvin James, AD George Edward Haigh, AN Frederick Charles Lynch, AN Clinton Bernard Macklin and AD Willian D. Whynn. Injured: ENS Donald Eugene McKinney, AEN Max Earl Studer and AD Joseph O. Smith.
"...Post Korea Early 50s KIA Navy Pilot Group Chicago..." WebSite: EBay http://search.ebay.com/_W0QQsassZuniversallive [11DEC2007]
Newspaper Article Contributed by BREITENSTEIN, AF1 Frank email@example.com [13AUG2005]
MISHAPs: 09 JUN 54 A/C: PBM-5 LOCATION: Yaka Shima Island South of Japan TYPE: Hit a mountain on Yaku Shima Island SRIKE: Yes DEATHS: 18 BUNO: 4779 CAUSE: Unknown See In Memorial for lost friends...VP-47 June 9th, 1954
In Memorial for lost friends June 9th, 1954 [Updated 10JUN2010]
MISHAPs: 00 SEP 62 A/C: PBM-5 LOCATION: Unknown TYPE: Over sped the prop on the starboard engine and couldn't feather SRIKE: Yes DEATHS: 00 Cause: Mechanical [21JUN2010]
"...I served with VP-47 from 1962 to 1963. Our PBM when down while operating with the USS Seadragon (SSN-584) on a chilly evening in September 1962. We over sped the prop on the starboard engine and couldn't feather - we eventually lost the aircraft - we sustained no injuries. The USS Seadragon (SSN-584) had just surfaced and the Skipper made the conning tower seconds before we hit the water. They had us out of the water, in dry clothes, sitting in the galley with coffee in hand in less than an hour. Love those Sub Sailors..." Contributed by TABER, W. Doyle firstname.lastname@example.org [21JUN2010]
MISHAPs: 00 JUL 67 A/C: P3 LOCATION: NS Sangley Point, Philippines TYPE: Landing gear fell through runway SRIKE: No DEATHS: 00 BUNO: xxx425 CAUSE: Heat caused surface to "give in!" [31AUG99]
THE CRUNCH OF RD-B Contributed by Charlie Switzer CharlieGO@aol.com [25FEB2000]
18 JULY 1967
NS Sangley Point, Philippines
VP-47 was deployed to Naha, Okinawa, with a detachment at Utapo, Thailand. On this date a USAF F-105 pilot at 35,000 feet over Danang, Vietnam, made "positive visual confirmation" of a Whiskey Class submarine snorkel just outside of Danang harbor.
The Navy reacted by ordering VP-47 to place a P-3 at the site to localize and track the sub. Squadron resources were stretched very thin at the time: the only aircraft available was a new P-3B (RD-8, BUNO 153425) in the Naha hangar undergoing maintenance, and the only flight crew available was one hastily pieced together, led by PPC Lt. Charlie Switzer. Lt. Switzer and his crew were to proceed to NS Sangley Point, P.1., for briefing, arming and fueling, thence to just outside Danang to find the sub.
At NS Sangley Point, while the enlisted crew prepared the aircraft with a full fuel load, four depth charges in the bomb bay, and underwing racks of paraflares, the officer crewmembers were briefed by Intelligence. As the officers were leaving Intelligence to proceed to the aircraft, the briefing officer announced that the mission had just been canceled because ‘‘the aircraft had fallen through the ramp.
Rushing to the aircraft, the officers observed the aircraft in a nose-high, right-wing- down attitude, with the starboard wing paraflare rack and aft fuselage resting on the pavement, prop tips of both starboard engines dug into the pavement, the nose gear (still attached to a tug by a bent towbar) approx. one foot above the pavement, heavy fuel leaks from the starboard wing, and the starboard main gear settled into a large hole in the ramp. It had bee$n under tow by a tug.
Thankfully, no one was injured (fortunately the engines were not operating) but of immediate concern was the hazard of fire and explosion due to the crushed and bent paraflares on the right wing, the fuel leaks, and the depth charges in the bomb bay.
Fortunately, there was adequate clearance to open the bomb bay doors to allow removal of the depth charges. The salvage plan was to use a large air bag under the starboard wing and a crane sling around the aft fuselage to lift the starboard side of the aircraft high enough to allow a large steel plate to be placed over the hole in the ramp and then to lower the starboard main gear down upon the steel plate. With the starboard side lifted up but before the steel plate could be placed over the hole, the clutch on the crane sling slipped and the aircraft came crashing down once again, exacerbating the earlier damage.
The ensuing accident board determined that no person in the Navy aviation establishment was in any way at fault in this accident, but that the civil contractor who had built the ramp was at fault, allowing a sewer joint beneath the pavement to leak and filter away the underlying soil. A Lockheed crew ferried the aircraft, unpressurized and at 250 kts. max., to the Burbank factory for repair. The aircraft eventually returned to VP-47. What happened to the "USAF" submarine is not known. Contributed by Charlie Switzer CharlieGO@aol.com [25FEB2000]
MISHAPs: 12 APR 73 A/C: P3 LOCATION: NAS Moffett Field, California TYPE: Midair W/Con 990 SRIKE: Yes DEATHS: 05 BUNO: 157322 CAUSE: Hit Cabin
In Memorial for lost friends April 12, 1973 [Updated 16DEC2014]
MISHAPs: 18 MAY 79 A/C: P3 LOCATION: NAF Kadena, Okinawa, Japan TYPE: Eng Turb Explosion SRIKE: No DEATHS: 00 BUNO: 158574 CAUSE: Turbine Failure
MISHAPs: 25 MAR 95 A/C: P3 LOCATION: Masirah TYPE: Prop Lk/Separation SRIKE: Yes DEATHS: 00 BUNO: 158217 CAUSE: Prop Corrosion
"...I've received these pictures while serving with VP-30 in mid 1995...Bert de Jong http://www.centerseat.net/..." [07NOV2009]
"...If you could make a correction to this story, I would be delighted. The Flight Engineer in the seat was AE1 Richard Willhite. Me. Not AE1 White. Thanks..." Contributed by AE1 Richard Willhite email@example.com [29OCT2006]
VP-47 Mishap"...VP-47 Mishap - Naval Aviation News - May - June 1995.." WebSite: http://www.history.navy.mil/nan/backissues/1990s/1995/mj95.pdf [12NOV2004]
"...I didn't see a list of the entire crew on the ditch 25 MAR 95. Here it is: LT Harrison (Pilot), LCDR Radice (CoPilot), LT Abrams (Third Pilot), AE1 Richard Willhite (Flight Engineer), PO1 Davenport (Off-Duty Flight Engineer), LT Smith (TACCO), LT Knollmueller (NAV/COMM), PO1 Tart (Sensor 3), PO2 Poulson (Sensor 1), PO3 Hildebrand (Sensor 2), and PO2 Fulgium (In-Flight Technician/Ordnance..." Contributed by AT1 Michael D. Fulgium Fulgium_Michael%PAX6@mr.nawcad.navy.mil
"...They Said It Would Never Happen - A P-3C Ditches with Four Engines Out, All Survive! - 25 March 1995 - Foundation Volume 18 Number 1 - Spring 1997..."
"They Said It Would Never Happen:"
"A P-3C Ditches with Four Engines Out, All Survive!"
25 March 1995
Foundation Volume 18 Number 1 - Spring 1997
"The fallen hunter, a P-3C Orion is raised from the Gulf of Oman after a dramatic ditching on 25 March 1995. All 11 crewmembers survived. Photo courtesy LT J. Harrison."
While going through the P3 FRS, newly winged aviators have always asked the question: "Has a P-3 ever lost all four engines at the same time." The answer was always: "No, it will never happen." Well as Murphy's Law applies, it can - and we did.
While on deployment and after performing an anti-submarine warfare mission with the USS Constellation (CV-64) battle group, which was located 200 miles east of Oman, VP-47 combat aircrew nine was returning to Masirah, Oman. The flight station crew was composed of LCDR Mark Radice, a lieutenant commander and a former P-3 FRS instructor who had just checked into the squadron 19 days earlier for his second tour; AE1 Richard Willhite, the flight engineer; and me, a senior lieutenant in the squadron with about 273 aircraft commander hours.
Little did we know that we were about to experience the beginning of what would eventually be one of the worst P-3 mishap ever. We had just restarted the number one engine, which was loitered on station to conserve fuel, and climbed up to an altitude of 16,000 feet for our transit home. At about 130 miles east of the island of Masirah, Oman, the flight engineer noticed that the number one prop pump warning light on the number four engine was illuminated. I directed the flight engineer to increase the number four power lever, which was the first step of our emergency procedure, and it also ensured that we have a good blade angle.
We then pulled out our NATOPS flight manual commonly referred to as the "Big Blue Sleeping Pill," and read through the remaining steps of our procedure. Having a prop pump light in itself was not a big worry, but it could eventually lead to bigger problems. Approaching 80 miles east of Masirah, the situation worsened. The second prop pump light on the number four engine illuminated and the prop began to overspeed. The crew went through the overspeed procedures, and we determined that the prop was pitch locked. This malfunction does not occur on a regular basis in the P-3 Orion, so needless to say, the flight crew's concern and heart rate increased as to what would happen to the prop when we fuel chopped the engine during our descent to land.
"View of the P-3 as it is being pulled from the Gulf of Oman. Photo courtesy LT J. Harrison."
We flew back to the airfield at 16,000 feet and executed a slow, spiraling descent to maintain our number four engines rpm at 100 percent. Not knowing what would happen when we fuel chopped the number four engine, the flight station went through the descent, approach and three engine landing considerations checklists. Approaching 6,000 feet and nearing the engine's limit power setting, we decided to circle the field one last time, extend out fora good downwind leg and fuel chop the engine in anticipation for our landing. Unfortunately, we would not get to land at the airfield. Passing 5,600 feet, we heard and felt a tremendous explosion. My co-pilot, who was in the right seat, looked out and saw a huge cloud of black smoke. To his utter dismay, when the smoke cleared, he saw the number four prop missing and the reduction gear box on fire. LCDR Radice called out to shut down the number four engine and discharge the fire extinguisher.
I was in the left seat, so I was unable to see what was going on. Trusting his judgment, I concurred with the decision to shut the engine down. The flight engineer shut down the engine and discharged the fire extinguisher. LCDR Radice looked out at the engine and the fire was still raging. AE1 Richard Willhite then discharged the second fire bottle. Unfortunately, the fire kept burning. AE1 Richard Willhite then called out that the number three engine's rpm was winding down. LCDR Radice looked out at the number three prop and called out that the prop are looked bad. It made sense that during the explosion, the number four engine probably took out the number three engine. We then called out to shut down the number three engine. While the flight engineer was pulling the number three emergency shutdown handle, I simultaneously advanced the number one and number two engine power levers.
Expecting to hear or feel a pitch change in the prop and not getting one, you can imagine my reaction when I looked out and saw both props barely rotating. Upon seeing this, I looked back inside the flight station to let the rest of the crew in on the secret, but AE1 Richard Willhite beat me to it and called flameout on number one and two engines.
All of the sudden the flight station went dark due to a total electrical power loss. Shaking my head with dismay, "saying you've got to be kidding me," we directed AE1 Richard Willhite to pull the hydraulic boost handles and start the auxiliary power unit in order to get electrical power back. At this time we were gust locked, which is the same as when your car's steering column locks up and you can't move it. To say the least, it was not a good feeling. After the boost handles were pulled, the flight engineer made several attempts to start the APU, but it kept flaming out. At this point things were really looking bad for VP-47's crew. When the boost handles were pulled, the aircraft should have switched from a hydraulic to a mechanical advantage. For some reason, this didn't occur and we were unable to control the aircraft. The aircraft rolled right into a 45-50 degree angle of bank and our airspeed bled off from 260 to 210 knots.
On the flight station we thought that the aircraft was going to stall and roll inverted. What a horrible gut wrenching feeling it was to think that this was going to be the end for everyone. I was their aircraft commander and I as responsible for their well-being. I could not get control of the aircraft and we did not have time to put on our parachutes to bailout. Even if we would have had time to don our parachutes, the main cabin door was facing the sky, which made bailing out impossible.
Up to this point, the entire evolution from engine explosion had taken about 45 seconds. With my heart pounding from being afraid and wanting to save the rest of the crew, I said a quick prayer. My prayers were answered. The control column went boost out and unlocked. Finally at about 2,500 feet, we were able to control the aircraft. We leveled the wings, then continued in a left hand turn to acquire the airfield. When I saw the airfield 90 degrees off of our left wing, we were at 2,000 feet and 6-7 miles away from land. A harsh reality set in -- we were going to have to ditch the aircraft.
Having never heard of or seen NATOPS procedures for a no engine, no-flap, boost-out ditch, the we had to use gut instinct. We knew that if we flew too fast, it would be hard to pull the nose up upon water entry. If we flew to slow, the aircraft would stall soon after leveling off above the water. We maintained our airspeed between 175-180 knots, which gave us a 1,000 fpm rate of descent. At this time, as with all life threatening situations, each crew 7 member's adrenaline system kicked in to its maximum. Fortunately, I had a great set of parents and a high school football coach who was a former Oakland Raider all-pro football player who taught me to never quit and find ways to win. At about 1,200 feet, we told the rest of the crew to prepare for immediate ditching. At 200 feet approaching water entry, both LCDR Radice and I started pulling back on the yoke. The nose came up nicely. The two biggest items necessary to perform a successful ditch is to maintain wings level and have a shallow rate of descent. At first, we were able to keep our wings level and get our rate of descent to about 300 feet per minute. At 80 feet, the right wing started rolling as we slowed down. LCDR Radice recognized the problem, called for left full yoke and the right wing came back up. Upon water entry, we were wings level, had a 200 feet per minute rate of descent and were right at 135 knots. After several skips across the water and fighting to keep the nose of the aircraft up, the plane finally came to rest. A P-3 ditch can best be described as being similar to a log ride at an amusement park, but with more of a kick in the pants.
The amazement of still being alive with the Orion still afloat caught me off guard, but there was little time for celebration. The water traversed through the tube of the aircraft and shot into the flight station like someone pointing a fire hose at us. My co-pi lot and flight engineer evacuated the aircraft through the overhead escape hatch. I evacuated the aircraft through the side escape hatch located immediately behind the pilot seat on the left side. After jumping into the water, I soon realized that the plane was still drifting like a boat does without power.
To my chagrin, the number two prop was coming right for me and was going to plow right over me. All that 1 could do was to paddle backwards as fast as I could to avoid the prop, putting my hands on the prop to push me out of its way. Fortunately, the aircraft came to a stop and I was able to swim to the leading edge of the wing between the number one and number two engines. I called out to LCDR Radice to see if the whole crew made it out of the aircraft. I was covered from head to toe with aircraft fuel and my eyes were on fire. My flight gloves were slippery from the fuel and this made it difficult to climb on top of the wing. After three tries, I was finally able to climb on top of the wing and reach the my TACCO and in-flight technician. The rest of the crew evacuated out the starboard side escape hatch and entered their life rafts. My in-flight tech nician was pulling the ring to inflate the life raft, but the blasted thing would not inflate.
A pilot friend of mine and his crew were waiting to take off to pick up an admiral in Bahrain when we hit the water. Shortly after we got into the life rafts, my buddy flew over and the crew let out a big yell. Once things finally settled down, the crew looked each other over and checked for injuries. To my surprise, not a single crew member was injured. The only person with a problem was me.
Up to this point I had controlled my temper quite well, but this was too much. After a few choice words directed to the life raft, the only option left was to inflate our life vests and swim around to the other side. Realizing our predicament, the crew in the other life rafts began to paddle around the rear of the aircraft in order to meet us. The three of us joined the other crew members and climbed into the rafts.
I had fuel in my eyes and they were burning like crazy. My sensor one operator carried a little water bottle in his life vest. He pulled out the water bottle and began to pour it in my eyes to flush out the fuel. While he was taking care of me, my TACCO and second pilot were trying to contact the other P-3 crew on our PRC-90 radios to let them know of our status.
This day was true to form, because my TACCO went through three radios before he found one that worked. On the fourth radio, he was finally able to talk to the other crew to let them know that we were fine.
We were in the rafts for only 10 minutes before the SAR helicopter arrived. The rescue was uneventful. The helicopter took seven crew members on the first trip and four crew members on the second trip.
A month later, a barge and crane raised the aircraft and we discovered that the number four prop had thrown a blade. The imbalance of only three blades caused the engine to explode. The prop blade was thrown from right to left and cut through the body of the aircraft, severing 35 of 44 engine and flight control cables. Four of the cables cut went to the four engines. The cutting action caused a pulling action which shut down all four engine simultaneously. The hydraulic boost handle cables were cut and the APU fuel line was cut. The nine intact cables were two aileron cables, two elevator cables, two elevator trim tab cables and two rudder trim tab cables.The co-pilot's main flight control cable was cut. VP-47's crew nine flew under a lucky cloud that day.
For so many things to So wrong and everything to work out perfectly was a total surprise to me. I have never questioned the reason we were spared, but I am glad that we were.
"VP-47 Summary Page"