Commission Regulation (EU) No 965/2012 of 5 October 2012 laying down technical requirements and administrative procedures related to air operations pursuant to Regulation (EC) No 216/2008 of the European Parliament and of the Council (c. 965)

ANNEX IV U.K. COMMERCIAL AIR TRANSPORT OPERATIONS[PART-CAT]

SUBPART C AIRCRAFT PERFORMANCE AND OPERATING LIMITATIONS U.K.

SECTION 1 U.K. Aeroplanes

CHAPTER 3 U.K. Performance class B

CAT.POL.A.340 Take-off and landing climb requirements U.K.

(b) Landing climb U.K.

(2) OEI U.K.

(i) The steady gradient of climb shall be not less than 0,75 % at an altitude of 1 500 ft above the landing surface with: U.K.

(A)

the critical engine inoperative and its propeller in the minimum drag position;

(B)

the remaining engine at not more than maximum continuous power;

(C)

the landing gear retracted;

(D)

the wing flaps retracted; and

(E)

a climb speed not less than 1,2 V_S1.