Air New Zealand gets first Boeing 787-9 Dreamliner. Also to feature at Farnborough

Air New Zealand takes Delivery of the first Boeing 787-9 Dreamliner, also to feature at Farnborough

 Air New Zealand has become the first airline to take delivery of the new 787-9, a stretched version of the revolutionary Dreamliner aircraft.

The plane was handed over in front of more than 1000 Boeing employees and guests at the aircraft manufacturer's facility in Everett, near Seattle in the US.

"It's a privilege to be the global launch customer for this aircraft and our team is looking forward to flying it home to New Zealand.  The 787-9 is a real game changer," Luxon said.

The fuselage for the 787-9 is stretched by 6 metres over the 787-8, and will fly up to 40 more passengers an additional 450 nautical miles (830 km).

Boeing's Dreamliners feature several major differences from other major passenger aircraft.

It is the first airliner to be made of carbon fibre, not aluminium, and promises airlines more fuel efficiency - a saving of 20 per cent. It also offers 20 per cent less carbon dioxide emissions than comparable aircraft.

The aircraft promises a better experience for passengers too. The cabin air is, unlike other aircraft, drawn directly from outside, rather than through the engines, meaning it is fresher. The air is also more humid, and pressurised at a lower level - the theory being that passengers will feel better at the end of their flights. There are also larger windows and a more spacious cabin.

Twenty-six customers from around the world have ordered 409 787-9s, accounting for 40 per cent of all 787 orders, Boeing said.

The Air New Zealand aircraft is scheduled to depart the US on Thursday morning, local time, and arrive in Auckland late afternoon on Friday.

This is the first of ten 787-9 Dreamliners to join Air New Zealand's fleet.  The aircraft will operate the Auckland-Perth route from 15 October 2014 and to Shanghai and Tokyo later this year.

Another of Air New Zealand's 787-9s will be displayed by Boeing at the Farnborough International Airshow later this month.

Delayed for several years, the Dreamliner has faced criticism over its reliability from some carriers. All active aircraft were grounded for three months last year after a battery fire on one Dreamliner. The incident forced Boeing to re-design the powerful lithium-ion battery and enclose it in a tough new steel containment box.

Boeing admitted in January it was not satisfied with the aircraft's performance. The Dreamliner's reliability rate was at about 98 per cent - this meant that two out of every 100 flights were delayed for mechanical problems.

The rate was higher than the 97 per cent recorded in October but was still short of Boeing's target. The company aims to have the aircraft's reliability up to the level of its long-range 777 model, which has a reliability rate of 99.4 per cent.

Plane spotters may think this is the same livery as the ‘All-Blacks’ livery that already graces some of the fleet, but you’ll actually be wrong. The fern, which now is the ‘New Zealand Way’ national fern rather than the all-blacks ‘Silver’ fern (above), is a sign of national pride, and symbolises New Zealand internationally.

Created by Designworks, the fern, now a part of the national carrier livery, was just one part of the job of bringing together all the ingredients needed to accelerate New Zealand’s brand on the world stage. “[we were] involved in a process of clarifying and articulating the strategic idea of New Zealand’s past, present and future purpose – engaging the country in a program of initiatives aimed at moving the whole population onto the same song sheet and collaborating with artists, designers and the wider community on a national attitude and vocabulary that is unique.”

Aussie Mirage III's: The Mirage III O

Being a long-time Mirage fan, I was (pleasantly) surprised to learn that Austalia, like South Africa had operated and built Mirages under licence from Dassault in France

A3 Dassault Mirage III

The search for a Sabre replacement began in the 1950s, and when a joint evaluation team from the Departments of Air and Supply visited Europe and North America in 1960, the Dassault Mirage III emerged as their selection over the Lockheed F-104 Starfighter.

Built by the French firm Generale Aeronautique Marcel Dassault (GAMD), the Mirage I flew on 25 June 1955, followed the following year by the prototype Mirage III. Having selected the Mirage, the RAAF then had to decide on the power plant, and with the Rolls Royce Avon already in service powering both the Sabre and the Canberra, this option was pursued for the Mirage. A French Mirage IIIA, known as 'City of Hobart', was fitted with an RB146 Avon 67 turbojet and flew on 13 February 1961. This was known as a Mirage IIIO, but did not receive a RAAF serial number as, although this modification delivered superior performance, its cost was prohibitive and this project was discontinued.

Having selected the French SNECMA Atar 9C engine, the first RAAF aircraft, numbered A3-1, flew at Bordeaux on 14 March 1963 and was handed over to the RAAF at Villaroche, near Paris, on 9 April. This definitive IIIO was similar to the French Air Force Mirage IIIE. While A3-1 was flown to Australia by Hercules, the second French-built aircraft, A3-2, remained in France until August 1965 to test the various RAAF modifications. Meanwhile, two further aircraft were shipped to Australia as fully-equipped major assemblies and completed at Avalon by the Government Aircraft Factories (GAF), the Australian prime contractor. The first of these, A3-3, was flown by Squadron Leader (later Air Vice Marshal) Bill Collings at Avalon on 16 November 1963.

Gradually the French content was reduced, with GAF subcontracting the wings, tail and engine to the Commonwealth Aircraft Corporation (CAC), and by aircraft A3-16 the first Australian-built primary parts were incorporated. The first order in December 1960 for 30 aircraft, A3-1 to A3-30, was followed in 1962 by an order for a further 30, A3-31 to A3-60. In 1963 the order was increased by another 40, A3-61 to A3-100, followed by 10 two-seat trainers, similar to the French Mirage IIIB, and designated IIID, A3-101 to A3-110.

Following the two French aircraft, the first 48 Australian-assembled aircraft (A3-3 to A3-50) were built as Mirage IIIO(F) interceptors and No 2 Operational Conversion Unit (2OCU) at Williamtown began receiving deliveries in 1964. No 75 Squadron became the first operational unit to equip in 1965 followed by No 76 Squadron in 1966. The next 50 aircraft (A3-51 to A3-100) were built as IIIO(A) ground attack variants with slightly different radar and the addition of doppler navigation and radar altimeters for low-level operation.

In 1967 No 75 Squadron deployed to Malaysia to replace No 3 Squadron. No 3 Squadron then became the first unit to equip with the ground-attack Mirage under Wing Commander Jake Newham, who was later to be Chief of Air Staff. When No 3 Squadron returned to Butterworth in 1969, No 77 Squadron re-equipped and became the fourth RAAF Mirage squadron.

The first two-seater Mirage IIID, A3-101, flew on 6 October 1966 and was accepted by the RAAF at Avalon on 10 November, followed by a further nine over the next year. The trainer version did not have the Cyrano II nose radar; a second cockpit was added behind the first and the avionics equipment previously stored there was relocated in the nose. The Mirage trainers were assembled by GAF from imported French-built fuselages and CAC-built wings and vertical tail surfaces.

In December 1970 the government approved the procurement of six additional Mirage IIID trainers at a cost of $11 million. These aircraft, A3-111 to A3-116, delivered from August 1973 to January 1974, enabled the retirement of the Sabre from operational fighter training.

An anomaly in Mirage deliveries occurred with A3-26. This aircraft was retained in France by Dassault from 1965 to 1968 as a trials installation for the IIIO(A) standard. The aircraft was finally delivered to 2OCU in November 1968 and the following June it was decided to convert the remaining IIIO(F) aircraft to the IIIO(A) standard for the ground-attack role.

With defence cuts under the Whitlam Government, No 76 Squadron was disbanded amongst much ill feeling in August 1973. The remaining three squadrons continued operating the Mirage in air defence and ground attack, based at Williamtown and Butterworth. Several Mirage aerobatic teams were also formed during its service with No 77 Squadron. Best known were the Deltas in 1971, followed by the Miracles in 1976 and a three-aircraft team of red, white and blue aircraft organised for the 1981 air shows. Basing of aircraft extended to Darwin in 1983 when No 75 Squadron relocated from Butterworth.

As 2OCU began to work up for the F/A-18 Hornet in 1984, all Williamtown-based Mirages were transferred to No 77 Squadron, with some 40 of the type on strength. This must have made No 77 Squadron the largest fighter squadron ever in the RAAF. No 77 Squadron finally relinquished their Mirages for Hornets in November 1987. In March 1986 No 79 Squadron reformed at Butterworth from No 3 Squadron, as the latter began conversion to the Hornet. No 79 Squadron operated the Mirage until disbanding in April 1988, leaving No 75 Squadron at Darwin and Aircraft Research and Development Unit (ARDU) at Edinburgh as the remaining operators. In early September 1988, No 75 Squadron flew a formation of Mirages over the east coast state capitals as a farewell gesture before the aircraft ceased squadron operations on 30 September. In October the remaining No 75 Squadron Mirages were ferried to Woomera and so, appropriately, this squadron, which was the first to equip with the Mirage in 1966, was the last to operate it.

The last RAAF Mirage flight was on 8 February 1989 when A3-101 was flown from ARDU at Edinburgh to Woomera to join 47 of the type in storage pending their disposal. In 1990 Pakistan purchased fifty RAAF Mirages, including two which had been stored at Point Cook, and these have now been delivered to the Pakistan Air Force, where some will undoubtedly fly for many years to come.

The Mirage saw longer service in the RAAF front line than any other fighter. Despite the original estimated design fatigue life of only 1500 hours, some Australian Mirages flew over 4000 hours. Over forty aircraft were lost in flying accidents, but those who flew it held the type in high regard. Although the 'Miracle' has left our skies, many examples remain on display at museums around Australia.

Like so many Mirage IIIs, now designated to the scrapyard:
Death in a Pakistani boneyard for one RAAF Mirage III

TECHNICAL DATA: Dassault/GAF Mirage IIIO

DESCRIPTION:
Single-seat interceptor/ground attack fighter.

POWER PLANT:
One 6200 kg (13 670 lb) thrust SNECMA Atar 9C turbojet with afterburner.

DIMENSIONS:
Length 15.03 m (49ft 4in); wingspan 8.22 m (27 ft); height 4.5 m (14ft 9in).

WEIGHTS:
Empty 7049kg (15 540 lb); max 13 699kg (30 200 lb).

PERFORMANCE:
Max speed Mach 2.2; Mach 1.14 (1390 km/h) at sea level: ferry range 3862 km (2085 nm).

ARMAMENT:
One Matra R530 and either two Sidewinder AIM-9B or two Matra R550 Magic air-to-air missiles and twin 30mm DEFA cannon. Ground attack weapons such as six Mk 82 227 kg (500 lb) bombs or three GBU-12 laser-guided bombs.

Dassault Mirage III A3-92

Selected to replace the Avon Sabre as the RAAF's fighter aircraft in 1960, the Mirage was the first aircraft in RAAF service capable of flying at twice the speed of sound. Entering operational service during 1965, the Mirage served as the front-line fighter until 1988, making the aircraft the longest-serving fighter in RAAF history. Built under licence in Australia by the Government Aircraft Factories (GAF), 100 single-seat and 16 two-seat Mirages were operated by seven RAAF units.

The first Australian-assembled Mirage flew at Avalon airfield in March 1963, and this and the following 48 aircraft were built as Mirage IIIO(F) interceptors. Following aircraft A3-50, production switched to the Mirage IIIO(A) ground attack aircraft with slightly different equipment for this role. In June 1969, the IIIO(F) aircraft were modified to the ground attack standard, to increase commonality within the Mirage fleet.

Now a gate guard at RAAF Wagga Wagga

             
In RAAF service, the Mirage operated with Nos 3, 75, 76, 77 and 79 Squadrons, as well as No 2 Operational Conversion Unit and the Aircraft Research and Development Unit, from bases across Australia and also at Butterworth in Malaysia. With the acquisition of the F/A-18 Hornet in 1985, the Mirage was phased out of service, and in October 1988 the last Mirages of No 75 Squadron were ferried to Woomera for eventual disposal.

After the cessation of Mirage operations, a number of aircraft were retained by the RAAF as training aids. This aircraft, A3-92, was one such aircraft and was used at the RAAF School of Technical Training at Wagga Wagga before transfer to the RAAF Museum for preservation.

Delivered from the GAF airfield at Avalon, Victoria, on 26 July 1968, A3-92 served with Nos 3 and 79 Squadrons at Butterworth, Malaysia, and No 77 Squadron at Williamtown, New South Wales. Withdrawn from service in May 1987, the total airframe time for the aircraft was 4037 hours.

Sources Wikipedia, Net, RAAF website. No copyright infringement intended, merely a fan blog. Happy to credit or remove content at request

Mirage III: More info and SAAF service (Click to follow links)

Mirage III in SAAF Service Part 1
Part 2: Progeny The Cheetah and Kfir

The Mirage F1 (click to follow links) 
Part 1 History of the F1
Part 2 The Border War: F1s in Combat
Part 3 Combat record and First Hand Account (Arthur Piercy)

Dakotas to Remember D-Day: The C-47 Dakota Part 1

D-Day Remembrance: C-47 Dakotas to drop Parachutists once more

On 6 June 2014 it is exactly 70 years ago that the largest invasion in history took place. 

On D-Day the beach landings saw almost 7 000 ships transport over 160 000 young men to the beaches of Normandy in France, to liberate Europe. This invasion was preceded by the landing of 13 000 paratroopers behind the enemy lines. Most of them jumped from the famous Douglas C-47 Dakota; the workhorse of the Allied troops.

The 70th anniversary of the D-day Invasion in June 2014 sees a “Dakota Fest” to bring as many of these aircraft that are still airworthy to Normandy again, and allow sky diving enthusiasts with the WW 2 style round parachutes to drop down to Normandy again !

For the first time since 1944 the skies over Normandy will be filled with Dakotas to drop paratroopers. Throughout Europe about 15 of these aircraft are still flying, and several will be joining from the US and Canada.

The only Airworthy Dakota in New Zealand

This has galvanised me to do a series of posts on the grand old Lady of the skies: 

The DC3/AC47 Skytrain or Dakota...watch this blog!

Junkers JU 87 Stuka Survivors and replicas (Stuka Part 1)

Airworthy Junkers JU 87 Stuka - 1940s Terror of the Skies

Survivors and Replicas

Steve Scheckter recently placed a photo of a replica/model Ju87 on Facebook, apparently flying over European  countryside. I guessed it was a Photoshop picture, as I'm reasonably sure there are no airworthy Ju 87 in the world. Well, then again, that was also said of the Mosquito, so I did a bit of research on the history and current facts, and came up with this:

History (Wiki) :

The Junkers Ju 87 or Stuka (from Sturzkampfflugzeug, "dive bomber") was a two-man (pilot and rear gunner) German dive bomber and ground-attack aircraft. Designed by Hermann Pohlmann, the Stuka first flew in 1935 and made its combat debut in 1936 as part of the Luftwaffe's Condor Legion during the Spanish Civil War.

The aircraft was easily recognisable by its inverted gull wings and fixed spatted undercarriage, upon the leading edges of its faired main gear legs were mounted the Jericho-Trompete ("Jericho Trumpet") wailing sirens, becoming the propaganda symbol of German air power and the blitzkrieg victories of 1939–1942. The Stuka's design included several innovative features, including automatic pull-up dive brakes under both wings to ensure that the aircraft recovered from its attack dive even if the pilot blacked out from the high acceleration.

Although sturdy, accurate, and very effective against ground targets, the Ju 87, like many other dive bombers of the war, was vulnerable to modern fighter aircraft. Its flaws became apparent during the Battle of Britain; poor manoeuvrability and a lack of both speed and defensive armament meant that the Stuka required heavy fighter escort to operate effectively.

The Stuka operated with further success after the Battle of Britain, and its potency as a precision ground-attack aircraft became valuable to German forces in the Balkans Campaign, the African and Mediterranean theaters and the early stages of the Eastern Front campaigns where Soviet fighter resistance was disorganised and in short supply.

Once the Luftwaffe lost air superiority on all fronts, the Ju 87 once again became an easy target for enemy fighter aircraft. In spite of this, because there was no better replacement, the type continued to be produced until 1944. By the end of the conflict, the Stuka had been largely replaced by ground-attack versions of the Focke-Wulf Fw 190, but was still in use until the last days of the war. An estimated 6,500 Ju 87s of all versions were built between 1936 and August 1944.

Some notable airmen flew the Ju 87. Oberst Hans-Ulrich Rudel was the most successful Stuka ace and the most highly decorated German serviceman of the Second World War. The vast majority of German ground attack aces flew this aircraft at some point in their careers.

See a separate post on the history: Ju 87 Stuka History Part 2

Survivors

Two intact Ju 87s survive:

Ju 87 R-2/Trop. Werk Nr. 5954

This aircraft is displayed in the Chicago Museum of Science and Industry. It was abandoned in North Africa and found by British forces in 1941. The Ju 87 was donated by the British government and sent to the USA during the war. It was fully restored in 1974 by the EAA of Wisconsin.

Ju 87 G-2, Werk Nr. 494083

A later, ground-attack variant, this is displayed at the Royal Air Force Museum in London; it was captured by British troops in Germany in 1945. It is thought to have been built in 1943–1944 as a D-5 before being rebuilt as a G-2 variant, possibly by fitting G-2 outer wings to a D-5 air frame. After the war, it was one of 12 captured German aircraft selected by the British for museum preservation.

 In 1967, permission was given to use the aircraft in the film Battle of Britain and it was repainted and modified to resemble a 1940 variant of the Ju 87. The engine was found to be in excellent condition and there was little difficulty in starting it, but returning the aircraft to airworthiness was considered too costly (and risky)  for the filmmakers, and ultimately, models were used in the film to represent Stukas. (see below)

 In 1998, the film modifications were removed, and the aircraft returned to the original G-2 configuration.

Junkers Ju 87 R-2 Werk Nr. 0875709 is owned by Paul Allen's Flying Heritage Collection (FHC) and is believed to be under a long-term restoration to fly. It served bearing the Stammkennzeichen of LI+KU with 1./St.G.5, and was recovered to the United Kingdom in 1998 before being sold to the FHC. It is likely to be the best candidate for an airworthy restoration.

Other aircraft survive as wreckage, recovered from crash sites.

1. The Deutsches Technikmuseum in Berlin has the wreckage of two complete aircraft that were recovered from separate crash sites near Murmansk in 1990 and 1994.

These wrecks were purchased from New Zealand collector Tim Wallis, who originally planned for the remains to be restored to airworthy, in 1996.

The Sinsheim Auto & Technik Museum displays the remains of an aircraft that crashed near Saint-Tropez in 1944 and was raised from the seabed in 1989.

2. In October 2006, a Ju 87 D-3/Trop. was recovered underwater, near Rhodes, Greece:

Markings still visible after almost 70 years under water

S7+GM

More on the history of this aircraft: 

According to a combination of available historical data, it appears that the aircraft is most probably S7+GM (100375), crewed by Lt. Rolf Metzger & Uffz. Hans Sopnemann - both MIA), which was shot down on 9 October 1943.

The Hellenic Air Force web-site tells us this about this aircraft:

"On that very day the II/St.G. 3 lost a total of nine Ju 87D-3/Trop when they were intercepted during their mission against Royal Navy and Hellenic Navy ships in the Aegean. Of these nine, seven crashed into the sea and two made emergency landings on Rodos. A week before, German troops had landed on the island of Kos, which fell the next day. On 9 October 1943, HMS cruiser "Carlisle" and other destroyers, returning from a sweep west of Kos, were dive-bombed SW of Rodos Island by a formation of Ju-87 Stukas. "Carlisle" was seriously damaged and HMS destroyer "Panther" was sunk. Most of her crew were saved by the RHN destroyer "Miaoulis", which has also claimed firing against the Ju-87 formation and probably hit a couple of them."

3.  Junkers Ju 87 B-2 9801 (serial number: 0406) is under reconstruction at Yugoslav Aeronautical Museum.

5. The fuseage of a Junkers Ju 88 was raised 6 miles off the coast of the German Island of Rügen in June 2012, the team of German Army researchers having thought it to be a Stuka. The two Junkers planes shared several parts, including the engines, and from the way it sat in the seabed it reportedly appeared to have been a Ju 87.

British Flying Replicas

 During the filming of 'The Battle of Britain' in 1968, serious thought was given to using the Hendon Stuka for the Ventnor radar bombing scenes. At the time the Stuka was part of the Air Historic Branch's collection of German aircraft, and it was decided by them that the Ju 87 was too valuble to risk (It was unique at that point).

The cost of getting the aircraft airworthy would have been prohibitive, but they did get the engine running, and this was recorded for use on the films soundtrack. Next they bought 4 Percival Procters for conversion to 'lookalikes'. The work was carried out by Viv Bellamy and entailed a major redesign of the cockpit glazing, new rectangular tail plane, rear fuselage cut down and new centre section built to pass for the distinctive Stuka cranked wing. 

The conversion was pretty convincing but, when flight tested by Bellamy, they did not fly well and were not used for filming. Their places were taken by large-scale radio controlled models which bombed the Ventnor film set constructed at The Mound near Dover.

New Zealand Static replica:

The full-size replica Stuka built by Lester Hope and his team of dedicated volunteers for Classic Fighters, was moved to its new location outside the Omaka Aviation Heritage Centrey. Here it joins its contemporary adversary, the replica Hawker Hurricane. 

Frankfurt Airport Static Replica:

Ukranian scaled down  flying replica, one of many in the world.

Link to more info on survivors

Avro Shackleton MR3 in SAAF service (Part 2)

Avro Shackleton MR3 in SAAF service (Part 2)

35 Squadron Emblem

(Shaya Amanzi - From the Zulu: "Hit the Water")

To replace the Short Sunderland, the SAAF ordered eight Avro Shackleton MR Mk3 in 1954, and delivery took place in 1957. The SAAF operated (1957 to 1984) a total of eight Avro Shackleton Mk.3's with tail numbers 1716-1723.

One Shackleton was lost on operations when it crashed in the Wemmershoek (Stettynsberg) range of mountains during poor weather conditions on 8th August 1963 with the loss of life of all 13 crew:

All aircraft were deployed by 35 Squadron at AFB Ysterplaat Cape Town , after initially flying out of Congela , close to Durban harbour.

The Shackleton served as a Maritime Patrol Aircraft with both the SAAF and RAF and was later replaced in the SAAF by the C-47TP and Nimrod in RAF service. The SAAF however used only the Mk.3 variant without the Viper upgrade.

Procuring the Shackleton was a major step up from the previous use of Sunderlands and Catalinas and according to Wiki , even Harvards and Spitfires were used! Shackletons were used extensively until 23 November 1984 when it was officially withdrawn from service.

 Shackleton 1716 was re-furbished to flying condition for the SAAF Museum, but had the unfortunate experience to crash land in the Sahara desert near the border with Mauritania on 13 July 1994 whilst on a flight to Great Britain to take part in a number of air shows. It suffered a number of engine failures and was forced to land in the dark, without any loss of life to the 19 crew on board. (See separate post on this)

Another Shackleton 1722 has been re-conditioned to flying status and flies as part of the SAAF Historical Flight in Cape Town.

 Armament consisted of two 20-mm cannon in the nose, plus up to 10,000lb (4 536kg) of weapons in the underfuselage bay.

 From the book Avro Shackleton by Barry Jones:

The SAAF's Shackleton strength was reduced by one in August 1963. 1718 had previously suffered a hydraulic failure,resulting in a wheels-up landing at D. F. Malan on 9 November 1959, but the
required repairs were carried out in record time, in order to get the aircraft back into service. On 8 August 1963 the aircraft had been engaged in joint exercises with the RAF and was on a return flight to Cape
Town. In gusting winds and severe icing conditions down to 3,000ft (l,000m), 1718 struck high ground before crashing into the Wemmershoek mountain range outside the town of Worcester, some 60
mile (96km) east of its destination. The crash occurred about 25.8 km (16 miles from the nearest town, Worcester, in the Stettynskloof valley between Paarl and Stellenbosch.

All thirteen crew members were killed in the tragedy, that was hard to accept by the squadron for some time. The aircraft had made a total of 777 flying hours during the six years since its acceptance by the SAAF

On the other side of the coin, two years later 1722 took part in an impressive display of search and rescue. Eight Buccaneer S.50s were in loose formation on their delivery flight to the SAAF when one, SAAF No.419, had a flame-out in both engines at high altitude, about 500 miles (800km) south of the Canary Islands. The two crew members,Captains Jooste and de Kerk, ejected while Major A. M. Muller, who was leading the formation, relayed their position. 1722 was scrambled, and only a couple of hours into the mission picked up the 'blips' from the downed airmen's SARAH beacons.

Coloured flares were fired by both the Shackleton crew and the survivors in the Atlantic, to verify visual contact by all concerned.Another MRJ, 1721, was drafted into what was no longer a search, but a rescue
operation and two sets of Lindholme Gear were dropped to the Buccaneer crew.
The Dutch liner Randfontein was in the area and 1722 guided it to the rescue location, where a successful transfer from life raft to luxury was made. 1722, captained by Major Pat Conway, had flown nearly eighteen
hours on the AR mission, which had been undertaken as a text-book operation.

In 1971, the treacherous currents around the Cape of Good Hope claimed another victim. The 70,000 ton oil tanker Wafra ran aground on rocks off Cape Agulhas, the most southerly tip of the African continent.
With its 60,000-ton cargo of crude oil threatening to cause an ecological disaster for the area's wildlife, not to mention the renowned holiday resorts that were located around that part of the country, an ocean-going tug was called in to tow the stricken vessel off the rocks. Good seamanship by the tug's crew got the Wafra
clear of the reef with very little oil spillage and the tanker was towed some 200 miles (300km) out to sea. As the vessel was unsalvageable in her existing state and there was no chance of transferring her cargo to another tanker, the SAAF was briefed to sink her, with the added instruction that, if possible, the ship's internal structure was not to be ruptured, so that she could take her cargo with her when she sank.
No. 24 Squadron's Buccaneer S.50s, armed with a pair of Nord AS-30 air-to ground missiles under each wing, carried out two sorties against the vessel, under the guidance of No. 35 Squadron, but the tanker remained intact. Consequently,MR.3s were called into action and a salvo of depth charges dropped alongside the Wafra had the desired effect. She sank onto the Agulhas Plateau, 2,300ft (700m) below the turbulent meeting place of the Atlantic and Indian Oceans, complete with her crude oil.

At least two SAAF MRJs are known to have returned to the UK. 1719 arrived on 25 February 1963 for a six-week training exercise with Coastal Command and it arrived back at D. F Malan on 1 April. The
following year, 1722 touched down at BalIykelly on 28 June, for a four-week course at the JASS, returning to Cape Town on 30 July 1964.

After the loss of 1718, the seven surviving MR.3s were all progressively modified to Phase III standard by Hawker Siddeley CWPs, except that the Armstrong Siddeley Viper jet boost (JATO) engines was never installed in any of the South African aircraft. The bases used by No. 35 squadron were deemed to be large
enough to get even a fully laden MRJ airborne. The Phase III modifications were implemented before the arms embargo and the full ECM suit was installed in all seven aircraft, so that they approximated to the
RAF's final MR.3 condition, apart from the Viper JATO.

Wing re-sparring was carried out on at least two aircraft, 1716 being out of service for the work between March 1973 and April 1976. Re-sparring on 1717 took a lot less time - no doubt the engineers had
learned from the work on 1716 - the squadron being without the aircraft from September 1975 to October 1977. At least two other aircraft, besides 1718 and 1723 already mentioned, had undercarriage
problems on landing. 1722's nose wheel refused to lock down on 7 June 1960 and the aircraft landed on a foam laid down at Langebaanweg, the nose-wheel assembly collapsing on contact with the runway. Two years later, on 10 September 1962, 1721 had to make a wheels-up landingat Ysterplaat, but the damage sustained was repaired in a comparatively short time.



One other mishap to the SAAF MRJ fleet occurred on 18 September 196 I, when 1720 was undertaking asymmetric landing practice. The pilot undershot the runway at D. F Malan and the aircraft was extensively
damaged. Rather than dismantling 1720 and taking it away for repair, a hangar was constructed around it for the work to be carried out where it was.

The arms embargo certainly had a detrimental affect on the SAAF's MR.3s, and the two re-sparrings already mentioned were quite an engineering accomplishment on the part of their maintenance engineers. Engine spares were impossible to obtain, as were new tyres and electronic replacements so, in November 1984, the Shackleton was officially withdrawn as an operational aircraft in the SAAF.

1723 had expended its fatigue life several years prior to this and had been grounded since 22 November 1977. It was stored in the open at Ysterplaat, until being purchased by Vic de Villiers, who acquired the aircraft via a triple deal involving both the South African Airways Museum and the SAAF Museum. De Villiers gave the airways museum Vickers Viking ZS-DKH, which he had held for many years, and
they let the SAAF Museum have a Lockheed Ventura. The SAAF completed the convoluted agreement by selling 1723 to de Villiers, who mounted it on the roof of his 'Vic's Viking Garage' on the Johannesburg
to Vereeniging road. For many years it remained in its service colours, but without national markings. However, by 1994,commercial advertising had taken over and the aircraft was repainted a vivid red,
over which' Coca Cola' logos were liberally displayed. A sign that is mounted beside the aircraft, incorrectly said 'World War Two Shackleton'; today this has been edited and the word 'Two' has gone, although
the legend is still inaccurate.

On 24 April 1978, five months after 1723 was grounded, 1719 followed suit and it too was stored in the open at Ysterplaat to begin with. Later the aircraft was moved on it own wheels to an airfield at Stellenbosch, in the South African wine region. Finally, in 1991, 1719 was moved, to the
Cape Town Waterfront complex, where it is displayed today.

1720 had reached the end of its fatigue life by 10 March 1983, so it was grounded.
It had been planned to mount the aircraft a the gate guardian at Ysterplaat, but someone 'pulled rank' and instead it was positioned outside the Warrant Officer's Club. For a reason that cannot be ascertained,
it was repainted to represent '1719', complete with the individual code 'L'. Maybe it was hoped to frustrate future aviation historians, but today the aircraft's proper identity has been restored.

In 1984,1717 too was grounded; it had only been kept flying to that date by courtesy of a technical team that ascended the Wemmershoek Mountains to where the wreckage of 1718 lay, in order to retrieve serviceable parts that could be used on 1717. After open-air storage at Ysterplaat, the aircraft was dismantled to be taken by sea to Durban. From there, in October 1987,it went by road to Midmar Dam and was reassembled for static display at the Natal Park Board Museum.

The nostalgia of the Shackleton' retirement was not lost on the SAAF and on 23 November 1984 the surviving trio of airworthy MRJ ,1716,1721 and 1722, took part in a ceremonial flypast at D. F. Malan
Airport. Twelve growling Griffons was quite a farewell note! Two weeks after the ceremony, 1716 and 1721 were flown to the AAF Museum at Swartkop, while 1722 was retained in ground-running condition
by No. 35 Squadron for the museum.

In November 1991, the aircraft was flown to Ysterplaat, which, by then, had developed into the second largest military aviation museum in South Africa.

1963 ACCIDENT SUMMARY ANALYSIS



Occurrence Date: 8 August 1963
Aircraft Involved: one Avro MR. Mk 3 Shackleton (serial 1718)
Aircrew & Aircraft Home Unit: 35 Squadron at DF Malan International Airport
Aircraft Damage Classification: Category IIIa
Accident Root Cause: human error (pilot error)
Total Human Involvement: 13
Total On-Board Human Involvement: 13
Total Human Attrition: 13 killed

Identity of Deceased:

Pilot, Capt Thomas Howard Silvertsen (P22051) attested in the SAAF 01/04/48
co-pilot, 2/Lt Charles Alwyn du Plooy (P1/48842/1) attested in the SAAF 25/01/61
3rd pilot, Capt Jaques Guillaume Labuchagne (P21805) attested in the SAAF 04/02/53
navigator, Lt Abraham Gert Willem Coetzee (P20965) attested in the SAAF 28/01/57
2nd navigator, 2/Lt George James Smith (P1/24862) attested in the SAAF 23/03/60
3rd navigator, CO Derek Ian Strauss (P50506) attested in the SAAF 07/01/63
flight engineer, WO2 Sydney Shields Scully (P4895) attested in the SAAF 01/09/36
2nd flight engineer, L/Cpl Marthienus Christoffel Vorster (P2/20554) attested in the SAAF 01/04/58
signals leader, Sgt David Hope Sheasby (P17877) attested in the SAAF 03/03/55
radio operator, L/Cpl Charl Paul Viljoen (P20356) attested in the SAAF 01/06/55
2nd radio operator, L/Cpl Matthys Johannes Taljaard (P17993) attested in the SAAF 06/03/57
3rd radio operator, L/Cpl Michel Adolf Brodreiss (P23845) attested in the SAAF 01/12/59
4th radio operator, A/M Johannes Chamberlain (P50083) attested in the SAAF 01/07/62

The tactical submarine phase of Operation CAPEX (Cape Exercise), a joint training exercise involving elements of Britain's Royal Navy and both the SA Navy and Air Force, commenced on August 7, 1963. During this phase, the Royal Navy submarine, HMS Alliance, would relocate from her existing position south of Port Elizabeth to a position further west, from where she would take part in further exercises with the SA Navy. During this transitional phase of the submarine, Shackleton 1718 was tasked by Maritime Group to conduct a CAPEX A exercise with the submarine.

Although 35 Squadron was based at the military section of DF Malan International Airport in Cape Town, the unit's headquarters was at nearby Air Force Station (AFS) Ysterplaat and it was at this latter facility that the flight crew of Shackleton 1718 received a full briefing at 12H30 on August 8, 1963. During this briefing, the Operations Officer on duty advised the Shackleton aircrew to head out over False Bay after take-off and to transit seawards towards the exercise area. He warned them that the direct overland route to Port Elizabeth should be avoided due to anticipated high icing levels on this route.

Forecast weather for the route over False Bay and then southwards was poor. Heavy icing conditions could be expected between 1 220 and 1 829 m ( 4,000 and 6,000 ft) above mean sea level (AMSL) and consequently the flight crew were further briefed that Maritime Group had granted them special clearance to transit to the exercise area under 915 m (3,000 ft) AMSL. A 244 m (800 ft) AMSL cloud base would exist with tops up to 6 707 m (22,000 ft). Heavy air turbulence could be expected with cumulonimbus clouds, hail and heavy rain throughout. Surface wind was 42 km/h (26 mph) at 340? and 92 km/h (57 mph) at 340? and 1 524 m (5,000 ft).
Even though the forecast weather over the eastern overland route was no better, at least the seaward route would eliminate the risk of the aircraft accidentally flying into high ground in the conditions of much reduced visibility. The aircraft commander, Captain (Capt) TH Silvertsen , when giving his own briefing, confirmed his route as south over False Bay and then seawards towards the exercise area. The flight had been authorised by Maritime Group to provide the Shackleton crew with training in the radar detection of a submarine. No special instructions were issued.

Shackleton 1718 was fully serviceable for flight even though the compasses had not been swung on their normal expiry date of July 19, 1963. Maritime Group gave authorisation for a month's extension provided that no major part of the aircraft was replaced. The compasses were therefore considered serviceable.

The Flight Office at Ysterplaat was uncomfortable about the weather conditions and telephoned the Maritime Group Operations Centre thrice prior to the departure of the Shackleton, in an effort to get the flight cancelled, but this request was not forthcoming.

Just minutes before take-off, Capt Silvertsen, notwithstanding his briefing instructions, informed Air Traffic Control (ATC) that he would climb to 2 896 m (9,500 ft) AMSL and head overland towards Port Elizabeth.

The aircraft lifted off Runway 34 at 15H06 and turned right on 350? for the climb out. Moments later, ATC informed the commander to come to 330? so as to safely avoid Tiger Mountain. Capt Silvertsen acknowledged this transmission and did accordingly. After the lapse of about a minute, he requested clearance to resume his original course of 350?. This was the last radio transmission received from Shackleton 1718.

At about 15H20 the radar technician at DF Malan requested permission to deactivate the radar for about ten minutes due to flooding of the radar installation on account of the heavy rain. This permission was granted, but before the radar was deactivated, 1718's location was given as a distance on the radar screen of about 40 km (25 miles) on a course of 100?. The ground course was about 145?.

Although the evidence suggested that the airplane had crashed, most likely in the Stettynskloof/Wemmershoek Mountains area, the adverse weather conditions, combined with the lateness of the hour, precluded any meaningful attempt at a search and rescue effort being mounted until the following day, August 9.

At 10H00 and again at 13H30 on August 9, helicopters were sent out to the Wemmershoek area to report on the weather, which remained completely adverse. Following a report of an aircraft having been heard, a further helicopter was despatched at 15H00 to search the mountains south of Simonstown. On August 10, another helicopter continued the search at Simonstown from 08H15, while a second aircraft was sent to report back on the weather in the Wemmershoek area. Here, the weather was still closed in, but hinted at the first signs of improvement. At 09H00 at aircraft was sent to fly high over the Wemmershoek Mountains to report on the cloud coverage. At 11H00 two aircraft continued a search in the same mountains and at 13H15 they were joined by a further pair of rotorcraft. The wreck was finally discovered from the air at 17H18 just over two days following the accident. It was evident from the almost complete destruction of the aircraft that nobody aboard could possibly have survived the crash.

The crash occurred about 25.8 km (16 miles from the nearest town, Worcester, in the Stettynskloof valley between Paarl and Stellenbosch. After inspecting the crash scene, the 35 Squadron Engineering Officer, Capt WJ Stiglingh decided to investigate the failures apparent on the port elevator and the upper section of the starboard rudder, both of which detached in flight, although the Board of Inquiry (BOI) officially convened to investigate the cause of the accident, was unable to establish which broke off first.

The section of the starboard rudder was found 1 620 m (5,314 ft) and the port elevator 1 250 m (4,100 ft) from the impact point. Following the disintegration of these two flight control surfaces, the aircraft would have been rendered uncontrollable. At this point (about 15H25) the pilot was heard to make his final radio transmission: “Mayday. Mayday,” but this was not recognised as such by the ATC. The timing of the transmission coincides exactly with the crash time.

At the same time that the starboard rudder and port elevator detached in flight, the port fuel tip tank also broke away removing a section of the port wing and both outer elevators. The outer most starboard elevator was found further forward than the impact point of the port tip tank. Clearly, it broke away shortly after the tip tank. The port elevator, which was complete, showed relatively little damage. Most of the damage sustained was consistent with it having fallen on to its inboard end and then on to some rocks. Signs were found, however, of excessive downward movement of this elevator to the extent that the hinges had damaged the steel spar, more so at the outboard hinge where the hinge arm had actually cut into the spar. It was official opinion that pilot applied force could not have caused this damage since the control column movement in restricted by stops strong enough to resist human force.

It is considered that at the time of the excessive downward movement of the elevator, the force, mainly due to leverage over the spar, was sufficient to cause failure of the hinge bolts in tension. Failure of the spar attachment upper lug clearly indicated that the outboard end of the elevator broke away first in a rearward direction. No evidence was found to suggest that this port elevator was attached to the airframe at the time of impact.

Examination of the starboard elevator indicated that its upward travel had been exceeded; this and other damage to this elevator being consistent with crash damage.

Regarding the section of the upper starboard rudder, the outboard skin at the break had failed in tension and the inboard skin was torn away from the front rearwards, this indicating that the broken off portion was first bent inwards and then backwards. Furthermore, apart from damage at the upper leading edge, which was inflicted when the rudder struck the ground, this portion of rudder was altogether undamaged. The rudder was probably detached from the aircraft before the point of impact.

As for the lower portion of the starboard rudder, failures on the outboard and inboard skins correspond to failure on the upper section. Damage on this section would appear to indicate that it did not strike the ground at the point of impact, but that it was flung forwards and carried further assisted by the strong winds prevailing at the time.

Considerable violence coupled with exceptionally strong winds and/or air turbulence was necessary to carry the port and starboard fin, port tailplane and several other pieces of empennage to their final positions. None of these parts, except the starboard fin, displayed any damage that could have occurred at the point if impact.

The port tailplane front spar had pulled out along its length, shearing all its rivets. Examination of the main impact zone indicated that the fuselage struck at right angles to the main mark down the slope and the sideways cartwheel or flick might have thrown empennage parts in to the air forward of, and to the right of, the impact area.

Examination of the point of impact of the port wingtip fuel tank indicated that the angle that the tank struck the ground was such that, had the tank been attached to the aircraft, the empennage should then have hit the ground. The tank was therefore most probably detached from the aircraft while still in the air. Positions of the No. 3 and 4 ailerons and part of the port wing support this reasoning.

The dump valves of both port and starboard tip tanks were found in the fully open position. As these valves are electro-mechanically driven, they were probably intentionally open and most likely before the port tip tank impact since this tank still had a considerable amount of fuel left over in it, judging by the flash fire area. The forward portion of the starboard tip tank, on the other hand, showed no signs of flash fire or explosion, indicating that its fuel content at the time of impact must have been low. The open dump valves appear to suggest that the pilot must have been busy dumping fuel in order to reduce the load on the airframe when it experienced the heavy turbulence and just before the aircraft began disintegrating. The aircraft weighed about 43 213 kg (95,242 lb) at the time of the accident.

In an attempt to reconstruct the events leading up to the crash, another Shackleton of the same weight and load as Shackleton 1718, took off from Runway 34 at DF Malan on August 22, 1963 to attempt to emulate as closely as possible the course and climb tempo of the stricken aircraft. Based on this emulation, it was ascertained that Shackleton 1718 was either at or very close to its intended cruise altitude of 2 896 m (9,500 ft) AMSL.

Instrument Flight Rules (IFR) flight had been authorised and the aircraft had been operating under IFR conditions at the time of its demise.

The Board was satisfied that the flight crew were under all circumstances both qualified and capable of performing the mission with which they had been tasked.

The accident occurred over State ground; property of the Department of Forestry. The terrain was unplanted, deforested and in its natural state. No claim could thus be made by the Department. There was no damage to private or other military property.

Shackleton 1718 was manufactured in August 1957. Although possessing a maximum take-off weight of 45 372 kg (100,000 lb), for its final flight it lifted off at 43 938 kg (96,840 lb). Since the aircraft was heavily laden with its maximum weight point close to the rearmost limit, the pilots would have experienced some instability in the yawing (left/right) plane.

The Board established that the impact speed of the aircraft was high and that this, combined with the resulting fire following the crash, caused almost complete destruction of the aircraft. There was no attempt by the crew to use parachutes and all aboard are assumed to have perished in the high G impact.

The Board established that the atrocious weather was a significant contributory factor in this accident. Wind was about 148 km/h (92 mph) due to the unstable air mass forming convection currents. Cloud cover extended from 305 m (1,000 ft) to 8 841 m (29,000 ft) AMSL with associated heavy precipitation. Due to the turbulence, the moist unstable air mass and low icing height resulted in unusually high icing conditions from 1 220 m to 1 829 m (4,000 ft-6,000 ft).

Air Force headquarters telephonically informed the Board that the maximum acceleration permitted on the Shackleton airframe was 2.4 G. It was thus theoretically possible to easily exceed this low limitation, especially under conditions of unusually high turbulence as in this case. Although it cannot be proved, it is not impossible that the pilot in control could have over controlled the aircraft on at least one occasion in response to the unusually heavy turbulence. This could have placed an additional load on the airframe.

It was considered a possibility that, due to the turbulence, the pilot found himself unwittingly between the mountain peaks and that either one wingtip or one of the tail surfaces skimmed the side of one of the mountains, the impact causing the aircraft to disintegrate in flight and causing the pilot to lose control. The Board, however, considered this scenario unlikely given the fact that the ATC heard the pilot's Mayday transmission clearly and the aircraft must have thus been flying above the mountain peaks under normal circumstances when the radio call was put out. Additionally, the fact that the dump valves were open does not correspond with a collision against a mountain.

The Board found Capt Silvertsen solely responsible for the accident. He displayed a complete lack of discipline by disobeying a direct order to rather route south over False Bay and instead routed over land, where the mountainous terrain exacerbated the already foul weather conditions. The aerodynamic effect of heavy icing, strong and turbulent winds, the heavy weight of the aircraft combined with the possible over control by the pilot in control, placed an unusually high loading on the airframe. This resulted in the airframe exceeding its design limits and initiated disintegration, leading to the loss of control and the consequent fatal crash. The accident was classed as an avoidable major flying accident.

All the evidence submitted by all the witnesses interviewed was considered credible by the Board.

Shackleton 1718 was delivered new to the SAAF valued at R 417 250.00. At the time of its demise it had completed 775.15 total airframe hours and, with depreciation, was valued with engines and propellers at R 266 109.45. The Rolls-Royce Griffon Mk 57A piston engines, like the airframe, were all classified as having sustained Category IIIa (write-off damage with no salvageable content). Engine numbers were 64411, 64412, 64416 and 64445.

This was the only Shackleton to be written off in 27 years of SAAF service from 1957 to 1984.

The Group Commander remarked that the ultimate load factor was 4 G. This figure suggests that the airframe was considerably stronger than the BOI was made to believe when they made their investigation. This information was, however, not available to the Board at the time.

The only flight crew member of the 13 that perished on board to have received any honours or awards was WO2 (Warrant Officer Class 2) Scully, recipient of the Africa Star with Clasp and the Union Medal (No. 285).

Individual Aircraft History:

1716 / J - c/n1526, first flight 29th March 1957, accepted at the Woodford Airfield by 35 Sqdn on the 16th May 1957, ferried to RAF St Mawgan for SAAF air-crew work-up exercises on the 21st May 1957, Departed for South Africa on the 13th August 1957, arrived Waterkloof on the 18th August 1957, Progressively modified up to Phase III standard. Wing re-sparring took place in South Africa, from March 1973 to April 1976. The aircraft took part in the retirement ceremony flypast at DF Malan airport, Cape Town, on the 23rd November 1984. 

She was ferried from Cape Town to the SAAF Museum Swartkops on the 4th December 1984, with Capt Louis van Wyk as aircraft Captain. Restored to airworthy status in 1994, for planned attendance at a series of airshows in the UK. 1716 departed Cape Town International RW01 on the 8th July 1994, for the United Kingdom, routing via Libreville, Gabon, - Abidjan, Ivory Coast, - Lisbon, Portugal for intended entry into the UK via Brize Norton. Crashed 13th July 1994, in the Western Sahara Desert (22.38N, 03.14W) en-route to the UK.

Shackleton 1720 - painted as 1717 - which was on static display in front of the NCO's mess at 

Ysterplaat AFB in Cape Town for many years, was sadly broken up on 12th March 2013.

Speculation has it that it was due to corrosion - it had been considered a safety hazard

1717 / O - c/n1527, first flight on the 6th May 1957, accepted at the Woodford Airfield by 35 Sqdn on the 16th May 1957, ferried to RAF St Mawgan for SAAF air-crew work-up exercises on the 21st May 1957, Departed for South Africa on the 13th August 1957, arrived Waterkloof on the 18th August 1957, from where 1716, 1717, & 1718 departed to Cape Town. The a/c was progressively modified up to Phase III standard. Wing re-sparring was done from September 1975 to October 1977. The aircraft was withdrawn from service & placed in storage at AFB Ysterplaat. During October 1987, she was dismantled & transported by sea to Durban, & then via road to the Midmar Dam, for static display at the Natal Parks Board transport museum. Financially the Natal Parks Board were unable to keep funding the museum, and all the exhibits were disposed of. With the subsequent closure of the Midlands Historic Village, where the aircraft was displayed, she was bought on auction by Mr Desai, a private businessman from Stanger in Kwazulu Natal. As of 2006, the airframe had been cut up for scrap, with only the engines remaining, potentially being sold to the UK.

1718 / K - c/n1528, first flight on the 13th May 1957, accepted at the Woodford Airfield by 35 Sqdn on the 16th May 1957, ferried to RAF St Mawgan for SAAF air-crew work-up exercises, Departed for South Africa on the 13th August 1957, and arrived Waterkloof on the 19th August 1957, from where 1716, 1717, & 1718 departed to Cape Town. The a/c had a wheels-up landing at DF Malan airport on the 9th November 1959, and was repaired during 1959-1960. She crashed in the Wemmershook mountains during poor weather, on the 8th August 1963. The aircraft was taking part in a CAPEX exercise, when severe icing caused loss of control, and the aircraft crashed inverted into a mountain valley, killing all 13 onboard. The crew were: Capt Thomas Howard Sivertsen , Capt Jaques Guillaume Labuchagne, Lt George James Smith, Lt Abraham Gert Willem Coetzee, CO Derek Ian Strauss, 2/Lt Charles Alwyn du Plooy, WOII Sydney Shields Scully, A/Cpl Charl Paul Viljoen, A/Cpl Marthienus Christoffel Vorster, T/A/Cpl Matthys Johannes Taljaard, A/Cpl Michel Adolf Brodreiss, F/Sgt David Hope Sheasby, Air Mech Johannes Chamberlain.

1719 / L - c/n1529, first flight on the 6th September 1957, accepted by 35 Sqdn in January 1958, departed for Cape Town on the 8th February 1958, arrived Cape Town on the 13th February 1958. Returned to the UK for training with Coastal Command on the 25th February 1963 and returned to South Africa on the 1st April 1963. Progressively modified up to Phase III standard. She was withdrawn from service on the 24th April 1978 & in storage at AFB Ysterplaat. Static display outside clubhouse at Stellenbosch airfield. Static display at the V&A Waterfront in Cape Town, cut up for scrap.

1720 / M - c/n1530, first flight on the 26th September 1957. Accepted by 35 Sqdn in January 1958. departed for Cape Town on the 8th February 1958, arrived Cape Town on the 13th February 1958. During asymmetric practice on the 18th September 1961, landed in undershoot at DF Malan airport, and was badly damaged. Repaired on site, with a hangar being constructed around the aircraft whilst repairs were carried out. Progressively modified over the years up to Phase III standard by March 1973. Tthe aircraft was withdrawn from service on the 10th March 1983, after reaching the end of its fatigue life. Initially allocated as a gate-guard at AFB Ysterplaat, she is displayed outside the WO's club, now having been sprayed in the1957 delivery colours & marked as 1717-O. Due to the airframe deteriorating & being a safety concern, she was cut up for scrap 2013. 

1721 / N - c/n1531, first flight 12th December 1957, accepted by 35 Sqdn on the 30th January 1958, departed for Cape Town on the 14th February 1958, and arrived cape Town on the 26th February 1958, damaged in a wheels-up landing at AFB Ysterplaat on the 10th September 1962. Progressively modified over the years up to Phase III standard, has the distiction of being the Shackleton which using depth charges, sunk the damaged tanker Wafra in March 1971. This after attempts by the Buccaneers of 24 Sqdn to sink the ship had failed. Took part in the retirement ceremony flypast at DF Malan airport on the 23rd November 1984. Ferried to SAAF Museum Swartkops for static display in December 1984. She was used as a parts donor for the restoration of 1716.

1722 / P - c/n 1532, First flown on the 7th February 1958. Departed for South Africa on the 14th February 1958, arriving Cape Town on the 26th February 1958. On the 7th June 1960 the aircraft nosewheel assembly refused to lock down, and she landed on a foam strip at Langebaanweg. The nose undercarriage collapsed on touchdown resulting in slight damage. The aircraft was repaired and progressively brought up to Phase III (non-Viper) standard. She returned to the UK on the 28th June 1964 for Joint Anti Submarine School (JASS) course, flying from RAF Ballykelly. Returning to Cape Town on the 30th July 1964. Took part in final retirement ceremony, overflying DF Malan in formation with 1716 and 1721 on the 23rd November 1984. Retained by 35 Sqn at DF Malan in ground running condition for the SAAF Museum. Her last public flight was on the 24th September 2006, at the Africa Aerospace & Defence airshow, after which the Chief of the Air Force, felt the value of Shackleton 1722 was too high to risk by continuing to fly the aircraft, and she was grounded. This ended the famous "Pelican22"'s flying career, which had spanned an impressive 48 years! Still not 100% sure of her final flight date though?

Quote:

So the last flying Shackleton in the world was certainly 'Pelican 22', whose final flight happened on March 29, 2008. This was a typical flight which took it over the city of Cape Town, and then out over the Atlantic Ocean, then back over Robben Island to Ysterplaat AFB. This final flight was piloted by Captain Peter Dagg. The crew included flight engineer Bronkhorst and ground engineer Potgieter.

1723 / Q - c/n1533, First flown on the 10th February 1958. Departed for South Africa on the 14th February 1958, and on arrival at AFB Ysterplaat on the 26th February 1958, the aircraft suffered a hydraulic failure. The undercarriage and flaps were lowered using emergency air, but the brakes were inoperative and the aircraft ran off the runway, colliding with a brick building. The damage to No. I engine was repaired. Progressively modified up to Phase III standard. The aircraft was retired on the 22nd November 1977, having expended her fatique life. Ironically she was the last aircraft delivered, but the first to be retired. She was stored in the open at AFB Ysterplaat until sold, and in March 1987, was put on display on top of Vic de Villiers 'Vic's Viking', garage in Johannesburg. This was a three way swop, with the Shackleton replacing a Vickers Viking, ZS-DKH, which went to the SAA Museum, and the SAA museum then gave the SAAF Museum three Ventura's. 1723 was initially kept displayed in her SAAF colours, but was subsequently over the years sprayed red/white in Coca Cola colours, then blue/white in SASOL colours.

Read more about this particular aircraft 1723 and Vick's Viking Garage (click on link)

No copyright infringement intended. Happy to credit you, link or delete images. Just contact me. Not my work, just collated.