Grumman American Cougar NORMAL PROCEDURES
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- Job Lawrence
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1 Grumman American Cougar NORMAL PROCEDURES AIRSPEED LIMITATIONS At 3800 lbs 1. V NE.188 Kts 2. V NO.160 Kts 3. V A..120 Kts 4. V FE Kts FULL..110 Kts 5. V LE..145 Kts 6. V MCA.61 Kts 7. V SO 63 Kts 8. V S1 71 Kts 9. V X.70 Kts 10.V XSE.85 Kts 11.V Y Kts 12.V YSE.85 Kts COCKPIT INSPECTION 1. Publications...Check 2. Baggage...Stowed 3. Weight & C.G... Within Envelope 4. Avionics... OFF 5. Magnetos... OFF 6. Landing Gear Handle...DOWN 7. Propellers...Clear 8. Master switch... ON 9. Gear lights...3 Green 10. Rotating Beacon...Check 1 N
2 11. Fuel Quanity...Check 12. Lighting Systems...Check 13. Pitot Heat...Check 14. Alternator Warning Lights...Check 15. Landing Gear Intransit Light..Check 15. Master switch... OFF 16. Cowl Flaps... OPEN 17. Controls... Unlocked 18. Trim Tabs...NEUTRAL 19. Fuel Selectors... ON 20. Take-Off Briefing... Available EXTERIOR CHECK RIGHT FUSELAGE 1. Cargo...Secure 2. Door...Secure 3. Static Port.. Check 4. Fuselage.Check EMPENNAGE 1. Control Surfaces..Check 2. Trim Tabs.. Check 3. Tailcone.Check 4. Tiedown...Remove 5. Position Light & Beacon..Check LEFT FUSELAGE 1. Static Port. Check 2 N
3 2. Fuselage.Check 3. Antennas.. Check LEFT WING 1. Skin condition...check 2. Aileron & Flap...Check 4. Wing Tip & Position Lights...Check 5. Fuel Tank Vent...Check 6. Tiedown Remove 6. Fuel Tanks Vent...Check 7. Fuel...Check 8. Bottom of Wing Check 9. Chocks. Remove 10. Fuel Tank Drain Drain 11. Main Landing Gear & Wheel Well..Check 12. Brake Linings.Check 13. Heater Fresh Air Scoop..Check 14. Engine Cowling.Check LEFT ENGINE & PROPELLER 1. Cowling...Check 2. Oil quantity & Cap...Check (6-8 qt) 3. Engine Air Intakes..Check 4. Propeller...Check 5. Fuel drain... Drain 6. Cowl Flap...Check NOSE SECTION 3 N
4 1. Left Air Inlet...Check 2. Nose Access Panel...Secure 3. Pitot Tube...Check 4. Nose Gear and Well...Check 5. Baggage Door...Secure 6. Battery Vent...Check 7. Right Air Vent...Check 8. Taxi Light...Check 9. Chocks...Remove RIGHT ENGINE & PROPELLER 1.. Fuel Sump Drain...Check 2.. Propeller...Check 3.. Engine Air Intakes.Check 4.. Cowling...Check 5.. Oil quantity & cap...check (6-8 qt) 6.. Cowl Flap. Check RIGHT WING 1. Skin condition...check 2. Main Landing Gear & Wheel Well...Check 3. Brake Linings...Check 4. Fuel Drains...Check 5. Chocks...Remove 6. Heater Fresh Air Scoop.Check 7. Fuel Tank...Check 8. Bottom of Wing Check 9. Chocks.. Remove 4 N
5 10. Fuel Tank Vent.Check 11. Stall Warning Vanes (2)...Check 13. Tiedown...Remove 14. Wing tip & position light...check 15. Flap & Aileron...Check ELECTRICAL SYSTEMS PREFLIGHT NOTE Complete electrical checks as quickly as possible to decrease drain on battery. Cockpit: 1. Master Switch ON 2. Instrument Lights Check Rheostat,OFF 3. Navigation Lights ON 4. Strobe Lights.ON 5. Pitot Heat.. ON 6. Landing Light ON Exterior: 1. All lights ILLUMINATED 2. Pitot Heat.Check Cockpit: 1. Master Switch OFF 2. Navigation Lights OFF 3. Strobe Lights.OFF 4. Pitot Heat.. OFF 5. Landing Light OFF 5 N
6 INTERIOR CHECK 1. Crew/Passenger Briefing:... As required 2. Entrance door... Locked BEFORE STARTING ENGINES 1. Seats, pedals, belts & harness...adjust 2. Circuit breakers...check 3. Auxiliary Fuel Pumps... OFF 4. Fuel Selectors... ON 5. Cowl Flaps... Open 6. Carburetor Heat... OFF 7. Mixtures... FULL RICH 8. Propellors...FULL FORWARD 9. Throttles...OPEN ½ Inch 10.Landing Gear Handle...DOWN 11.Emergency Gear Extend Knob... IN 12.Electrical Switches... OFF 13.Light Rheostats... AS DESIRED 14. Cabin Heat... AS DESIRED 15. Parking Brake SET 16. Master & Alternator Switches.. OFF 17. Magneto Switches.OFF 18. Primer CENTER 19. Flight & Engine Instruments Check 20. Master Switch.ON 21. Radios...SET 22. ATIS...RECEIVED 23. Engine Start..GRANTED 24. Radios.OFF 6 N
7 STARTING ENGINES AIRPLANE POWER LEFT ENGINE START 1. External Lights AS REQUIRED 2. Fuel Pump... ON, Check Pressure, OFF 3. Propeller.. Clear 4. Left Magneto ON 5. Starter Engage 6. Primer.AS NECESSARY NOTE In the event of a balked start or overprimed condition, place the mixture control in idle cut-off and open the throttle. Operate the starter to remove excess fuel. As the engine starts, reduce the throttle to idle rpm and place the mixture control in FULL RICH. 7. Right Magneto ON after start 8. Throttle..Adjust ( RPM) 9. Oil Pressure.. Check 10. Alternator..ON 11. Engine Instruments CHECK 12. Gyro Pressure Gauge.Check 13. Alternator.Check 7 N
8 RIGHT ENGINE START 1. Fuel Pump.. ON, Check Pressure, OFF 2. Mixture..RICH until fuel flow, then OFF 3. Propeller.. Clear 4. Left Magneto ON 5. Starter Engage 6. Primer.AS NECESSARY 7. Right Magneto ON after start 8. Throttle.Adjust ( RPM) 9. Oil Pressure.. Check 10. Alternator..ON 11. Engine Instruments CHECK EXTERNAL POWER 1. Master Switch... OFF 2. External Power...Set for 12 Volts, CONNECTED 3. Master Switch... ON 4. External Lights...AS REQUIRED 5. Fuel Pump... ON, Check Pressure, OFF 6. Propeller.. Clear 7. Left Engine, Left Magneto.. ON NOTE In the event of a balked start or overprimed condition, place the mixture control in idle cut-off and open the throttle. Operate the starter to remove excess fuel. As the engine starts, reduce the throttle 8 N
9 to idle rpm and place the mixture control in FULL RICH. 8. Propeller.. Clear 9. Left Starter... Engage 10. Right Magneto.. ON after start 11. Throttle....Adjust ( RPM) 12. Oil Pressure...Check 13. Left Alternator..ON 14. Left Ammeter.. Check 15. Gyro Pressure Gauge Check 16. Left Alternator Switch.OFF 17. Master Switch OFF 18. External Power DISCONNECTED 19. Master Switch.ON 20. Left Alternator Switch..ON CAUTION IF THE LEFT ALTERNATOR IS OPERATING PROPERLY AND THE RIGHT ENGINE WILL NOT START USING AIRPLANE POWER, REMOVE THE BATTERY FROM THE AIRPLANE AND SERVICE OR REPLACE BEFORE FURTHER FLIGHT. 21. Using the AIRPLANE POWER procedure above, start the right engine. NOTE Starting one engine with airplane power will ensure that the battery system is charged and operating. If it is necessary due to extreme cold conditions, use 9 N
10 EXTERNAL POWER procedure to start both engines. Allow sufficient time for warm-up, then shut down right engine only. Restart right engine using AIRPLANE POWER procedure. BEFORE TAXIING 1. Avionics....ON 2. Altimeter/Gyros/Clock..SET 3. Autopilot...Checked,OFF 4. Electric Trim...Checked, SET 5. Exterior Lights..AS REQUIRED 6. Parking Brake...Release TAXIING 1. Brakes.Check 2. Flight Instruments.. Check ENGINE RUNUP 1. Nose Gear... Straight 2. Parking Brake... As required 3. Fuel Selectors... BOTH ON 4. Engine Instruments... GREEN 5. Propeller Feathering...Check (1500 RPM) 6. Magnetos...Check (1800 RPM) 7. Alternators..Check 8. Carburetor Heat Check 10 N
11 9. Gyro Pressure Gauge.Check 10. Propeller Governors.Check (2200 RPM) 11. Throttles... Set 1000 RPM 12. Flaps....Check BEFORE TAKEOFF 1. Seats and Belts....Secure 2. Shoulder Harnesses...Secure 3. Avionics...Checked and set 4. Fuel Selectors... ON 5. Fuel Pumps... ON 6. Engine Gauges... GREEN 7. Alternators... ON 8. Autopilot... Checked and OFF 9. Gyros, clock, altimeter...set 10. Carburetor Heat...OFF 11. Cowl Flaps... OPEN 12. Mixtures and Propellers...FULL FORWARD 13. Quadrant Friction... Set 14. Flight Controls... FREE and CORRECT 15. Trim...SET 16. Flaps... Visually check to Door & Window...Secure 18. Takeoff Briefing... Accomplished LINEUP CHECK 1 Gyro Heading... Set 2. Transponder... ALT 3. Landing Lights... As required 11 N
12 4. Pitot Heat... As required 5. Strobes... ON TAKEOFF 1. Throttles.. ADVANCE 2. Power and airspeed Check 3. Rotate.... at KIAS 4. Gear...UP CLIMB 1. Climb Power... Set 2. Engine Instruments...Check 3. Cowl Flaps... As required 4. Fuel Pumps... OFF 5. Best Rate of Climb airspeed...95 KIAS 6. Cruise Climb airspeed KIAS CRUISE CHECKS 1.. Cowl Flaps....Closed 2.. Cruise Power......Set 3.. Mixtures Set 4.. Fuel Selectors....As Required 5.. Engine Guages.. Monitor WARNING Improper Leaning Techniques Can Reduce Endurance 12 N
13 DESCENT 1.. Mixtures...Set 2.. Power As Required 3.. Defroster.As Required 4.. Altimeter.. Set BEFORE LANDING 1. Seats and Belts Secure 2. Shoulder Harnesses..Secure 3.. Fuel Pumps.. ON 4.. Carburetor Heat..Check 5.. Mixtures..RICH 6.. Propellers...FULL FORWARD 7. Landing/Taxi Lights...ON 8. Cowl Flaps As Required 9.. Wing Flaps KIAS to FULL 110 KIAS 10.Gear DOWN (below 145 KIAS) & Checked 11.Autopilot OFF LANDING CHECK SHORT FINAL 1.. Gear..Recheck DOWN 2.. Propellers...FULL FORWARD 13 N
14 GO-AROUND 1. Throttles...FULL FORWARD 2. Carburetor Heat..OFF 3. Airspeed..80 KIAS 4. Flaps..Reduce in steps 5. Gear..UP 6. Cowl Flaps..As Required AFTER LANDING CLEAR OF RUNWAY 1. Landing/Taxi Lights.... As Required 2. Cowl Flaps..As Required 3. Flaps....UP 4. Radios/transponder/radar...As Required 5. Strobe Lights...OFF 6. Fuel Pumps..OFF 7. Carburetor Heat.OFF 8. Trim.Neutral ENGINE SHUTDOWN 1. Nose Wheel Centered 2. Avionics...OFF 3. Pitot Heat... OFF 4. Throttle RPM 5. Mixtures.IDLE CUT-OFF 6. Magnetos...OFF - when props stopped 10.Rotating Beacon......OFF 11.Lighting systems..off 14 N
15 12. Alternator Switches...OFF 13.Master Switch OFF 15 N
16 Wright-Patterson Aero Club Grumman American COUGAR EMERGENCY PROCEDURES NOTE: The urgency of certain emergencies require immediate & instinctive action by the pilot. The most important single consideration is aircraft control. All procedures are subordinate to this requirement. SPEEDS Minimum Control. 61 KIAS Best Single Engine Angle of Climb.. 85 KIAS Best Single Engine Rate of Climb KIAS Maneuvering Speed (MGW)..120 KIAS Maneuvering Speed (3200 lbs) KIAS Never Exceed KIAS ENGINE INOPERATIVE PROCEDURES ENGINE SECURING PROCEDURE (FEATHERING PROCEDURE) Inoperative Engine IDENTIFY Throttle Closed Propeller.FEATHER Mixture IDLE CUT-OFF Cowl Flap...Closed Magneto Switches OFF - 1 E
17 Wright-Patterson Aero Club Fuel Pump..OFF Fuel Selector..OFF Alternator Switch.OFF Electrical Load. Reduce Crossfeed.Considered ENGINE MALFUNCTION DURING TAKEOFF RUN (ABORT) Throttles... Throttles..CLOSE Brakes APPLY... As Required Mixture.IDLE CUT-OFF Master Switch.OFF Magneto Switches..OFF Fuel Selectors.OFF Apply brakes maintaining directional control and maneuver to avoid any obstacles. ENGINE MALFUNCTION IMMEDIATELY AFTER TAKEOFF (SUFFICENT RUNWAY REMAINING) Throttles..CLOSE Brakes APPLY WARNING Certain combinations of aircraft weight, configuration, ambient conditions and speeds will not permit a positive climb. - 2 E
18 Wright-Patterson Aero Club ENGINE MALFUNCTION AFTER TAKEOFF (TAKEOFF CONTINUED) Airspeed...85 KIAS minimum Directional Control.Maintain Power.. SET MAXIMUM Flaps.. UP Gear UP Inoperative Engine..IDENTIFY Throttle (Inop. Eng.)....VERIFY Propeller (Inop. Eng.)...FEATHER Cowl Flaps.CLOSED Airspeed.85 KIS after obstacles cleared Trim.bank 5 0 towards operative engine Climb..straight ahead (avoiding obstacles and attain sufficient altitude to execute a single engine landing approach) Operative Engine MONITOR Inoperative Engine.Complete Engine Inop. Securing Procedure Land as soon as practical at the nearest suitable airport. ENGINE MALFUNCTION DURING CLIMB Airspeed Maintain 85 KIAS Directional Control.Maintain Inop Engine IDENTIFY Inop Engine...Complete Engine Inop Securing Procedure - 3 E
19 Wright-Patterson Aero Club Land as soon as practical at the nearest suitable airport. ENGINE MALFUNCTION DURING FLIGHT Inoperative Engine.. IDENTIFY Power.As Required Mixture.As Required Flaps.UP Gear..UP Fuel Pumps..ON If altitude permits, a restart may be attempted. If engine does not start, complete engine inop securing procedure. Power (operative engine).as required Mixture (operative engine) Adjust Fuel Quanity (operative engine side) Sufficient Fuel Pump (operative engine). As required Cowl Flap (operative engine)...as required Engine Instruments (operative engine) Monitor Electrical Load Adjust Land as soon as practical at the nearest suitable airport. SINGLE ENGINE LANDING - 4 E
20 Wright-Patterson Aero Club Inoperative Engine. SECURE Airspeed maintain 90 KIAS until landing is assured Gear...DOW Seat Belts.Secure Fuel Pump..ON Fuel Quantity....CHECK Cowl Flap (operative engine)...as Required ENGINE RESTART DURING FLIGHT (UNFEATHERING) Fuel Selector.. ON Fuel Pump.....ON Throttle Open ½ inch Mixture RICH Propeller.. Full Forward Right Magneto Switch..ON Starter.Engage until prop unfeathers Throttle..15 in MAP, 2000 RPM until warm Left Magneto Switch..ON Engine Instruments.Check Alternator..ON Fuel Pump......OFF - 5 E
21 Wright-Patterson Aero Club OVERSPEEDING PROPELLER Throttle.. RETARD Airspeed.REDUCE Throttle..add slowly after RPM under control Airspeed.maintain below airspeed at which overspeed occurred. (Select lower RPM if higher airspeed is required.) Descend at 2200 RPM Land with prop set at 2400 RPM Note: Prop will not feather while overspeeding, therefore while in overspeed condition, do not select feather position and do not shut down the engine. Propeller will feather normally if not overspeeding. FIRE ENGINE FIRE DURING START Starter..ENGAG E Throttle..OPE N Mixture. IDLE CUT- Radio call for assistance - 6 E
22 Wright-Patterson Aero Club Master, Alternator & Magneto Switches.OFF Abandon aircraft & use fire extinguisher ENGINE/NACELLE FIRE IN FLIGHT Fuel Selector.OFF Mixture...IDLE CUT- OFF Fuel Pump..OFF Inoperative Engine FEATHER before 1000 RPM Operative Engine..Power as Required Drag.Reduce Alternator (Inop Eng)... OFF Magneto Switches (Inop Eng)... OFF Electrical load...reduce If fire persists, increase airspeed as much as possible in an attempt to blow out the fire. Land at the nearest suitable airport. FUSELAGE FIRE Vents.Closed Heater OF F Fire Extinguisher..Use When fire is out, ventilate the cabin. Land at the nearest suitable airport. - 7 E
23 Wright-Patterson Aero Club CABIN VENTILATION PROCEDURE Fresh Air Vents..OPEN Direct Vision Window..OPEN Cabin Heat Selectors COLD Floor Heat Shutoffs..OPEN Defrosters.ON ELECTRICAL FIRE Master S it h OFF Alternator Switches....OFF Circuit Breakers.Check, then pull all Electrical Switches.all OFF Avionics OFF Heater OFF Vents...Close Fire Extinguisher...Use When fire is out: Master Switch...ON Vents..OPEN Circuit Breakers...ON, one at a time Electrical Switches.. ON, one at a time Land at the nearest suitable airport. - 8 E
24 Wright-Patterson Aero Club ELECTRICAL SYSTEM FAILURE SINGLE ALTERNATOR FAILURE Reduce electrical load to minimum required. If Alternator circuit breaker tripped: Turn Off affected alternator. Reset tripped circuit breaker. Turn ON affected alternator switch. If circuit breaker reopens, turn off alternator. If circuit breaker not tripped: Monitor output. If output normal and failure light remains on, disregard failure indication and have indicator checked after landing. If complete loss of alternator output occurs, check field circuit breaker and reset if necessary. BOTH ALTERNATORS FAIL Turn OFF all electrical loads. Repeat above procedure for each alternator. Reset circuit breakers, one at a time. Left Alternator switch... ON Monitor output. If alternator still inoperative, turn it off. Right Alternator Switch.ON Monitor output. If alternator still inoperative, turn it off. - 9 E
25 Wright-Patterson Aero Club Terminate flight as soon as possible. Note: Since battery is furnishing all the current, keep the load low. FUEL SYSTEM EMERGENCIES FLUCTUATING FUEL PRESSURE Mixture Lever... FULL RICH Fuel Pump... ON Mixture Lever... As Required GOING INTO CROSSFEED To use fuel from side opposite operating engine: Fuel Selector Operating Engine..CROSSFEED Fuel Selector Inoperative Engine.OFF Fuel Pump Operating Engine..OFF unless needed When fuel from same side as operating engine. Fuel Selector - Operating Engine.. ON Fuel Pump Operating Engine OFF, unless needed Landing: Fuel Selector Operating Engine.FULLEST TANK Fuel Selector Inoperative Engine..OFF Fuel Pump Selected Tank..ON - 10 E
26 Wright-Patterson Aero Club ENGINE ROUGHNESS Fuel Pump... ON Engine Instruments...scan for cause Mixture...adjust as required Carburetor Heat...Check Cowl Flaps... adjust for proper CHT Magnetos...check INFLIGHT EMERGENCIES EMERGENCY DESCENT Throttles. retard slowly to idle Propellers...FORWAR D Gear and Flaps.UP Moderate Bank INITIATE SPIN RECOVERY Throttle. IDLE (both) Rudder full opposite to spin until rotation stops Control Wheel neutral and forward if necessary - 11 E
27 Wright-Patterson Aero Club Note: In as much as FAA Regulations do not require spin demonstrations of airplane with this weight, no spin test were conducted. The recovery technique is based on available information. LANDING EMERGENCIES LANDING GEAR EMERGENCIES -- GENERAL If the gear cannot be lowered successfully, proceed with the emergency procedures for the appropriate gear malfunction. CAUTION If an unsafe gear indication existed and the gear has been successfully lowered, do not attempt to raise the gear. EMERGENCY LANDING GEAR EXTENSION Master Switch..ON NAV LTS Switch...OFF Landing Gear Selector..DOWN Circuit Breaker.. Check LG breaker IN If Landing Gear fails to extend: GEAR-UP LANDING - 12 E
28 Wright-Patterson Aero Club Normal check list...complete (except for gear selector) Gear Selector...UP All Switches except Master & Magnetos..OFF Flaps...FULL DOWN Make a normal approach with power.75 KIAS Cabin Door.. UNLATCH Close throttles before touchdown. Master and Magneto Switches... OFF Touch down at minimum speed (If time permits, use starter to position props parallel with wings.) - 13 E
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