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The Nimrod Review - Official Documents

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<strong>The</strong> <strong>Nimrod</strong> <strong>Review</strong><br />

42<br />

Addition of SCP duct to MR2 (c. 1979)<br />

4.4<br />

4.5<br />

4.6<br />

2 When 35 of the <strong>Nimrod</strong> MR1s were upgraded to MR2s (1975-1984), they were all fi tted with a Supplementary<br />

Conditioning Pack (SCP) to supply extra cooling air to the aircraft’s upgraded electronic equipment. <strong>The</strong> SCP<br />

increased the mass fl ow of conditioned air to the cabin by supplementing the original two conditioning packs<br />

located in the wings. <strong>The</strong> SCP incorporates a pre-cooler in a fairing aft of the bomb bay and a tail pack in the<br />

APU compartment, which includes a two-stage heat exchanger and a Cold Air Unit (CAU). Space did not allow<br />

the SCP expansion bellows to be covered by the type of shrouds used on the Cross-Feed duct and so fl exible<br />

muffs were used instead (see further below).<br />

To power the SCP, it was decided to off-take bleed-air from the Cross-Feed duct and run the bleed-air aft to<br />

the tail where the SCP was located. To do this, a fi ve-way junction was fi tted to the pre-existing Cross-Feed<br />

duct, immediately below the entrance from the bomb bay to the starboard side No. 7 Tank Dry Bay. Adjacent<br />

to this off-take, the new SCP bleed-air duct was routed through the very lowest section of the starboard No. 7<br />

Tank Dry Bay and then aft (see below). With the air supply to the SCP switched on, hot, high-pressure air bled<br />

from the Cross-Feed duct fed through the SCP duct to a combined Pressure Regulating and Shut-Off Valve<br />

(PRSOV), which reduced the extracted bleed-air from up to 280psi (the maximum working pressure of the Cross<br />

Feed duct) to approximately 56psi (the normal operating pressure of the SCP duct) and through a fl ow-limiting<br />

venturi to the pre-cooler. Bleed-air for the SCP was routed along the outside of the starboard fuselage from the<br />

PRSOV to the pre-cooler and along the outside of the port fuselage from the pre-cooler to the tail pack itself. 3<br />

4 This combined duct now to be found in MR2s is referred to collectively in this Report as the “Cross-Feed/SCP<br />

duct” (see Figure 4.2 – a cross section shown with the bomb bay doors open).<br />

Figure 4.2: <strong>Nimrod</strong> MR2 Cross Feed Ducts<br />

2 <strong>The</strong> RAF took delivery of 35 upgraded MR2s between 1978 and 1984. XV230 was one of those upgraded.<br />

3 See also BOI paragraph 38 [2-27].<br />

4 And the BOI.<br />

Hot air from<br />

starboard<br />

engines<br />

Original Cross-Feed Duct<br />

SCP duct<br />

Forward<br />

Viewing Angle

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