By Department of the NAVY USA.

Книга F-18 Flight handbook F-18 Flight guide Книги Вооружение Автор: division of the military united states. Формат: pdf Размер: 36,2 Язык: Русский0 (голосов: zero) Оценка:Летная инструкция самолета F-18 (военно-морская модель).

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Fuel System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Environmental Control System . . . . . . . . . . . . . . . . . . . FO-3 FO-7 FO-11 FO-13 FO-17 FO-21 FOLDOUTS Figure Figure Figure Figure Figure Figure FO-1 FO-2 FO-3 FO-4 FO-5 FO-6 30 CHANGE 1 A1-F18EA-NFM-000 RECORD OF CHANGES Change No. and Date of Change Date of Entry 31 (Reverse Blank) Page Count Verified by (Signature) ORIGINAL A1-F18EA-NFM-000 INTERIM CHANGE SUMMARY The following Interim Changes have been cancelled or previously incorporated in this manual: INTERIM CHANGE NUMBER REMARKS/PURPOSE The following Interim Changes have been incorporated in this Change/Revision: INTERIM CHANGE NUMBER REMARKS/PURPOSE Interim Changes Outstanding - To be maintained by the custodian of this manual: INTERIM CHANGE NUMBER ORIGINATOR/DATE (or DATE/TIME GROUP) PAGES AFFECTED 33 (Reverse Blank) REMARKS/PURPOSE ORIGINAL A1-F18EA-NFM-000 SUMMARY OF APPLICABLE TECHNICAL DIRECTIVES Information relating to the following technical directives has been incorporated in this manual Change Number ECP Number (R) Retrofit Description Visual Identification Effectivity (P) Production Information relating to the following recent technical directives will be incorporated in the future change.

A speed brake function is provided by differential deflection of the primary flight control surfaces. The pressurized cockpit is enclosed by an electrically operated clamshell canopy. An aircraft mounted auxiliary power unit (APU) provides self-contained start capability for the engines. 2 Aircraft Gross Weight. Basic weight is approximately 31,500 pounds for the F/A-18E and 32,000 pounds for the F/A-18F. Refer to applicable DD 365-3 for accurate aircraft weight. 3 F/A-18F. The F/A-18F is the two seat model of the Super Hornet and is configured with tandem cockpits.

RATS logic also senses WonW, wheel speed (less than 20 knots), and THA to prevent the engines from spooling back to MIL power at the end of cable pullout. RATS operation is canceled when the throttles are reduced to IDLE (THA less than 10°). RATS operation is inhibited during single engine operation. RATS operation can be overridden by advancing the throttles to full afterburner (THA within 2° of the MAX stop). With RATS enabled, afterburner operation is inhibited if the throttles are subsequently advanced to afterburner (below the MAX stop).

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