Modificatie Mod.: 43. Jetpipe cooling shroud, clearance between front and rearshroud increased (see also modification 34) Tekening DH-82a, nr. U2755 Mk. I /Mk. II Assembly of front fuselage Tek. nr. B.205401; electrical equipment in front fuselage, loading chart and circuit index. Hawker Aircraft Limited, Kingston-on-Thames Tek. nr. C.222094; Hydraulics in front fuselage, piping diagram. Hawker Aircraft Limited, Kingston-on-Thames Tek. nr. C.187563; G.A. pitot installation in front fuselage. Hawker Aircraft Limited, Kingston-on-Thames Tek. nr. Hydraulics in front fuselage, piping diagram. Hawker Aircraft Limited, Kingston-on-Thames Tek. nr. D.204500; Electricla equipment in front fuselage, loading chart and circuit index. Hawker Aircraft Limited, Kingston-on-Thames Tek. nr. D.2099/2; Lubrication flying controls in front fuselage, centre fuselage, rear fuselage & wings. Hawker Aircraft Limited, Kingston-on-Thames Tek. nr. D.209916; Lubrication gearbox & engine controls in front fuselage, centre fuselage. Hawker Aircraft Limited, Kingston-on-Thames Tek. nr. E.179358; G.A. of nose spar (frame 19) front face. Hawker Aircraft Limited, Kingston-on-Thames Tek. nr. D.218009; Piping diagram hydraulic installation front fuselage. Hawker Aircraft Limited, Kingston-on-Thames TD-1142 Fokekr C.X Kopie van tekening C13354: support for front fuselage welding jig; ref WUC 11A00
