FA-18ABCD US Navy Flight Manual

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The twin vertical stabilizers are angled outboard 20°from the vertical. The wings have hydraulically actuated leading edge and trailing edge flaps and ailerons. The twin rudders and differential stabilators are also hydraulically actuated. The speed brake is mounted on the top side of the aft fuselage between the vertical stabilizers. The pressurized cockpit is enclosed by an electrically operated clam shell canopy. An aircraft mounted auxiliary power unit (APU) is used to start the engines. On the ground, the APU may be used to supply air conditioning or electrical and hydraulic power to the aircraft systems.

Should’’ has been used only when application of a procedure is recommended. ‘‘May’’ and ‘‘need not’’ have been used only when application of a procedure is optional. CHANGE SYMBOLS Revised text is indicated by a black vertical line in either margin of the page, adjacent to the affected text, like the one printed next to this paragraph. The change symbol identifies the addition of either new information, a changed procedure, the correction of an error, or a rephrasing of the previous material.

G. ON PAGE III-7-5, CHANGE THE SJU-17 CALLOUT UNDER THE CAUTION TO READ: "SJU-17 AND SJU-17A" H. ON PAGE III-7-5, CHANGE PARAGRAPH P TO READ AS FOLLOWS: "P. SJU-17(V)1/A, 2/A, AND 9/A ONLY-NEGATIVE G STRAP SECURE IN SEAT BUCKET. " I. G, ABOVE) AS FOLLOWS: "T. " J. ON PAGE V-17-1, CHANGE THE LAST SENTENCE OF THE LAST PARAGRAPH BEFORE THE WARNING TO READ AS FOLLOWS: "DURING EJECTION SEAT DEVELOPMENT AND TESTING, THE FOLLOWING SEATS WERE QUALIFIED FOR THE RESPECTIVE MINIMUM AND MAXIMUM (NUDE) WEIGHT RANGES FOR AVIATORS LISTED HERE: SJU-5/A, 6/A, AND SJU-17(V)1/A, 2/A, AND 9/A - 136 LB TO 213 LB.

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