Normal Procedures for Cessna 210

Auxiliary Fuel Pump OFF. Lack of a flow indication with the HIGH portion in the ON position may indicate a broken fuel line that can lead to a fire hazard. Page 7 of 10 Date: April 28, 2000 15393101, Rev. A Revised: June 01, 2001 FAA APPROVED r Έ 63 a ATLANTIC AERO Serving the World through Aviation DAS 7 SO Pilot's Operating Handbook and FAA Approved Airplane Flight Manual Supplement For Cessna 210N SECTION 4 NORMAL PROCEDURES STARTING ENGINE SECTION Use the Auxiliary Fuel Pump Switch HI portion for priming the engine. Turn Switch OFF after priming. NORMAL AND SHORT FIELD TAKEOFF Power:...... NORMAL CLIMB Power:. ture: FULL THROTTLE AND 2700 RPM 25 inches Hg. and 2550 RPM Lean to 120 LBS/HR BALKED LANDING Power:... FULL THROTTLE and 2700 RPM FAA APPROVED Date: April 28, 2000 Revised: June 01, 2001 Page 8 of 10 15393101, Rev. A == ΓΕ 16 ≈ (V a FR A ATLANTIC AERO Serving the World through Aviation DAS 7 SO Pilot's Operating Handbook and FAA Approved Airplane Flight Manual Supplement For Cessna 210N SECTION 5 DESC PERFORMANCE MS Performance is either unchanged or improved with installation of the IO-550-P engine and PHC-J3YF-1RF/F7691() propeller. SECTION 6 WEIGHT AND BALANCE The weight and moment of added items is as follows: ITEM WEIGHT (LBS) ARM (IN) MOMENT (IN-LB) IO-550-P ENGINE 465 -17.5 7945 PHC-J3YF-1RF/F7691() 77.3 -44 -3401 PROPELLER NOTE: The weight and moment of the removed engine and propeller must be accounted for when changing the overall aircraft weight and balance. FAA APPROVED Date: April 28, 2000 Revised: June 01, 2001 1000. 0 Page 9 of 10 15393101, Rev. A ATLANTIC AERO Serving the World through Aviation DAS 7 SO Pilot's Operating Handbook and FAA Approved Airplane Flight Manual Supplement SECTION 7 For Cessna 210N DESCRIPTION OF SYSTEMS FUEL SYSTEM AUXILIARY FUEL PUMP OPERATION The auxiliary fuel pump is a dual speed, dual pressure pump activated by a yellow and red split-rocker type switch located on the left side of the instrument panel. The yellow right half of the switch is labeled LOW, and its ON position is used for increasing fuel flow and minor vapor purging. The red left half of the switch is labeled HIGH, and its ON position is used in the event of an engine-driven fuel pump failure. The HIGH pump position is also used for priming during normal starting and for extreme vapor purging. Maximum fuel flow is produced when the HIGH side of the switch is placed in the ON position. In this position, an interlock within the switch also trips the LOW side of the switch to the ON position. When the HIGH side of the switch is turned OFF, the LOW side will remain in the ON position until manually returned to the OFF position. WARNING Continued used of the HIGH side will cause an overly rich mixture if the engine-driven fuel pump is so operating. Manual leaning will be required to prevent engine roughness and possible engine stoppage due to excessive richness. FAA APPROVED Date: April 28, 2000 Revised: June 01 2001 =7 ar th ua Page 10 of 10 15393101, Rev. A 17 v. IF