Catalogue description Bristol Siddeley: Olympus 320 TSR.2 engine & reheat unit flight specification. MoA Contract Ref.KG/M/090/CB(a) Issue 14

Development A Department. Development history Volume 2. Section 2: Olympus 22R to functional 320 conversion specification. Section 3: Fuel system specification. Section 4: Schemes cleared since Issue 1 of Conversion specification. Section 5: Development features required for 150-hour development type test (fighter) schedule. Engine 22213 June 1965 Build. Section 6: List of additionalschemes since the re-issue of OL.320 flight specification to Issue 14. Section 7: Olympus 320X master flight clearance note. Section 8: Olympus 320 master flight clearance note. Section 9: Mechanical condition report on Olympus 320 engine 2209 Build 4. Section 10: Development plan 11/11. Section 11: Specification No.D.Eng.RD.2437. Issue 4. Section 12: BSE Mk.320 supplement to D.Eng.RD.2437 (TRM.44).