BEFORE TAXIING (4.15)

CAUTION

Do not operate engine above 1200 RPM with cabin doors open.

Throttle ...1000 to 1200 RPM Radio Master Switch ...ON Environmental System ...AS DESIRED Supplemental Electric Heater ...AS DESIRED

4.5e Taxiing Checklist (4.17) TAXIING (4.17)

Taxi Area...CLEAR Chocks ...REMOVED Parking Brake ...RELEASED Propeller Control ...FULL INCREASE Throttle ...APPLY SLOWLY Brakes ...CHECK Steering...CHECK Flight Instruments...CHECK

NOTE: During taxi, if low voltage annunciator comes on, increase engine RPM if possible to retain adequate battery charging.

4.5f Ground Check Checklist (4.19) GROUND CHECK (4.19)

CAUTION

Alternate air is unfiltered. Use of alternate air during ground or flight operations, when dust or other contaminants are present, may result in engine damage from particle ingestion.

Parking Brake ...SET Propeller Control ...FULL INCREASE Throttle ...2000 RPM Magnetos ...max. drop 175 RPM - max. diff. 50 RPM Gyro Suction ...CHECK (within normal operating range)

ISSUED: FEBRUARY 23, 1999 REPORT: VB-1710 REVISED: JANUARY 20, 2004 4-11 4.5d Before Taxiing Checklist (4.15)

BEFORE TAXIING (4.15)

CAUTION

Do not operate engine above 1200 RPM with cabin doors open.

Throttle ...1000 to 1200 RPM Radio Master Switch ...ON Environmental System ...AS DESIRED Supplemental Electric Heater ...AS DESIRED

4.5e Taxiing Checklist (4.17) TAXIING (4.17)

Taxi Area...CLEAR Chocks ...REMOVED Parking Brake ...RELEASED Propeller Control ...FULL INCREASE Throttle ...APPLY SLOWLY Brakes ...CHECK Steering...CHECK Flight Instruments...CHECK

NOTE: During taxi, if low voltage annunciator comes on, increase engine RPM if possible to retain adequate battery charging.

4.5f Ground Check Checklist (4.19) GROUND CHECK (4.19)

CAUTION

Alternate air is unfiltered. Use of alternate air during ground or flight operations, when dust or other contaminants are present, may result in engine damage from particle ingestion.

Parking Brake ...SET Propeller Control ...FULL INCREASE Throttle ...2000 RPM Magnetos ...max. drop 175 RPM - max. diff. 50 RPM Gyro Suction ...CHECK (within normal operating range)

ISSUED: FEBRUARY 23, 1999 REPORT: VB-1710 REVISED: JANUARY 20, 2004 4-11

FOR REFERENCE ONLY

NOT FOR FLIGHT

REPORT: VB-1710 ISSUED: FEBRUARY 23, 1999 4-12 REVISED: JANUARY 20, 2004 4.5f Ground Check Checklist (4.19) (Continued)

GROUND CHECK (4.19) (Continued)

NOTE

Refer to paragraph 4.50, Icing Information, prior to any flight operations. (Takeoff, cruise, landing, etc.) If flight into icing conditions (in visible moisture below +5°C) is anticipated, conduct a preflight check of the ice protection systems per Supplement No. 3 - Ice Protection System.

Ice protection equipment...CHECK AS REQUIRED Voltmeter ...CHECK Ammeters ...CHECK Oil Temperature ...CHECK Oil Pressure ...CHECK Propeller Control ...EXERCISE - then FULL INCREASE Fuel Flow ...CHECK Throttle ...RETARD Annunciator Panel ...PRESS-TO-TEST Switch Panel ...PRESS-TO-TEST

4.5g Before Takeoff Checklist (4.21) BEFORE TAKEOFF (4.21)

Battery Master Switch ...ON Emergency (EMERG) Fuel Pump ...ON Alternators ...ON - CHECK AMMETERS Flight Instruments ...CHECK Engine Gauges ...CHECK Pressurization Controls ...SET Fuel Selector ...PROPER TANK Induction Air ...PRIMARY

WARNING

Refer to paragraph 4.50, Icing Information, prior to any flight operations. (Takeoff, cruise, landing, etc.) If flight into icing conditions (in visible moisture below +5°C) is anticipated or encountered during climb, cruise or descent, activate the aircraft ice protection system,including the pitot heat, as described in supplement no. 3 - Ice Protection System.

REPORT: VB-1710 ISSUED: FEBRUARY 23, 1999 4-12 REVISED: JANUARY 20, 2004

4.5f Ground Check Checklist (4.19) (Continued) GROUND CHECK (4.19) (Continued)

NOTE

Refer to paragraph 4.50, Icing Information, prior to any flight operations. (Takeoff, cruise, landing, etc.) If flight into icing conditions (in visible moisture below +5°C) is anticipated, conduct a preflight check of the ice protection systems per Supplement No. 3 - Ice Protection System.

Ice protection equipment...CHECK AS REQUIRED Voltmeter ...CHECK Ammeters ...CHECK Oil Temperature ...CHECK Oil Pressure ...CHECK Propeller Control ...EXERCISE - then FULL INCREASE Fuel Flow ...CHECK Throttle ...RETARD Annunciator Panel ...PRESS-TO-TEST Switch Panel ...PRESS-TO-TEST

4.5g Before Takeoff Checklist (4.21) BEFORE TAKEOFF (4.21)

Battery Master Switch ...ON Emergency (EMERG) Fuel Pump ...ON Alternators ...ON - CHECK AMMETERS Flight Instruments ...CHECK Engine Gauges ...CHECK Pressurization Controls ...SET Fuel Selector ...PROPER TANK Induction Air ...PRIMARY

WARNING

Refer to paragraph 4.50, Icing Information, prior to any flight operations. (Takeoff, cruise, landing, etc.) If flight into icing conditions (in visible moisture below +5°C) is anticipated or encountered during climb, cruise or descent, activate the aircraft ice protection system,including the pitot heat, as described in supplement no. 3 - Ice Protection System.

FOR REFERENCE ONLY

NOT FOR FLIGHT

4.5g Before Takeoff Checklist (4.21) (Continued) BEFORE TAKEOFF (4.21) (Continued)

Seat Backs ...ERECT Seats ...ADJUSTED& LOCKED IN POSITION Armrests ...STOWED Mixture ...FULL RICH Propeller Control ...FULL INCREASE Belts/Harness ...FASTENED/ADJUSTED Empty Seats ...SEAT BELTS SNUGLY FASTENED Flaps ...SET Trim ...SET Controls ...FREE Door ...LATCHED Air Conditioner ...OFF Parking Brake ...RELEASED

4.5h Takeoff Checklist (4.23) NORMAL TECHNIQUE (4.23a)

NOTE

Takeoffs are normally made with full throttle. However, under some off standard conditions, the manifold pressure indication can exceed its indicated limit at full throttle. Limit manifold pressure to 42 in. Hg maximum. (See Section 7.)

NOTE

During landing gear operation, it is normal for the HYDRAULIC PUMP annunciator light to illuminate until full system pressure is restored.

NORMAL TECHNIQUE (4.23a)

Flaps ...0

°

to 10

°

Trim...SET Power...SET TO MAXIMUM Liftoff ...80-85 KIAS Climb Speed ...90-95 KIAS Landing Gear (when straight ahead

landing on runway not possible) ...UP Flaps ...RETRACT

ISSUED: FEBRUARY 23, 1999 REPORT: VB-1710 REVISED: JANUARY 20, 2004 4-13

4.5g Before Takeoff Checklist (4.21) (Continued) BEFORE TAKEOFF (4.21) (Continued)

Seat Backs ...ERECT Seats ...ADJUSTED& LOCKED IN POSITION Armrests ...STOWED Mixture ...FULL RICH Propeller Control ...FULL INCREASE Belts/Harness ...FASTENED/ADJUSTED Empty Seats ...SEAT BELTS SNUGLY FASTENED Flaps ...SET Trim ...SET Controls ...FREE Door ...LATCHED Air Conditioner ...OFF Parking Brake ...RELEASED

4.5h Takeoff Checklist (4.23) NORMAL TECHNIQUE (4.23a)

NOTE

Takeoffs are normally made with full throttle. However, under some off standard conditions, the manifold pressure indication can exceed its indicated limit at full throttle. Limit manifold pressure to 42 in. Hg maximum. (See Section 7.)

NOTE

During landing gear operation, it is normal for the HYDRAULIC PUMP annunciator light to illuminate until full system pressure is restored.

NORMAL TECHNIQUE (4.23a)

Flaps ...0

°

to 10

°

Trim...SET Power...SET TO MAXIMUM Liftoff ...80-85 KIAS Climb Speed ...90-95 KIAS Landing Gear (when straight ahead

landing on runway not possible) ...UP Flaps ...RETRACT

ISSUED: FEBRUARY 23, 1999 REPORT: VB-1710 REVISED: JANUARY 20, 2004 4-13

FOR REFERENCE ONLY

NOT FOR FLIGHT

REPORT: VB-1710 ISSUED: FEBRUARY 23, 1999 4-14 REVISED: JANUARY 20, 2004 4.5h Takeoff Checklist (4.23) (Continued)

0

°

FLAP TAKEOFF PERFORMANCE (4.23b)

Flaps ...0

°

Trim...SET Brakes ...APPLY Power...SET TO MAXIMUM Brakes ...RELEASE Liftoff...78 KIAS Obstacle Clearance Speed...91 KIAS Landing Gear ...UP

SHORT FIELD TAKEOFF PERFORMANCE (4.23c)

NOTE

Gear warning will sound when the landing gear is retracted with the flaps extended more than 10°. Flaps ...20

°

Trim...SET Brakes ...APPLY Power...SET TO MAXIMUM Brakes ...RELEASE Liftoff...69 KIAS Obstacle Clearance Speed...80 KIAS Landing Gear ...UP Flaps...RETRACT as speed builds thru 90 KIAS

4.5i Climb Checklist

MAXIMUM CONTINUOUS POWER CLIMB (4.25a)

Mixture ...FULL RICH Propeller Speed...2500 RPM Manifold Pressure...MAXIMUM CONTINUOUS POWER Climb Speed

Best Angle (short duration only) ...81 KIAS Best Rate ...110 KIAS Pressurization Controls ...SET Emergency (EMERG) Fuel Pump ...OFF at safe altitude

REPORT: VB-1710 ISSUED: FEBRUARY 23, 1999 4-14 REVISED: JANUARY 20, 2004 4.5h Takeoff Checklist (4.23) (Continued)

0

°

FLAP TAKEOFF PERFORMANCE (4.23b)

Flaps ...0

°

Trim...SET Brakes ...APPLY Power...SET TO MAXIMUM Brakes ...RELEASE Liftoff...78 KIAS Obstacle Clearance Speed...91 KIAS Landing Gear ...UP

SHORT FIELD TAKEOFF PERFORMANCE (4.23c)

NOTE

Gear warning will sound when the landing gear is retracted with the flaps extended more than 10°. Flaps ...20

°

Trim...SET Brakes ...APPLY Power...SET TO MAXIMUM Brakes ...RELEASE Liftoff...69 KIAS Obstacle Clearance Speed...80 KIAS Landing Gear ...UP Flaps...RETRACT as speed builds thru 90 KIAS

4.5i Climb Checklist

MAXIMUM CONTINUOUS POWER CLIMB (4.25a)

Mixture ...FULL RICH Propeller Speed...2500 RPM Manifold Pressure...MAXIMUM CONTINUOUS POWER Climb Speed

Best Angle (short duration only) ...81 KIAS Best Rate ...110 KIAS Pressurization Controls ...SET Emergency (EMERG) Fuel Pump ...OFF at safe altitude

FOR REFERENCE ONLY

4.5i Climb Checklist (Continued) CRUISE CLIMB (4.25b)

Manifold Pressure ...35 IN. HG Propeller Speed...2500 RPM Mixture...32 GPH Climb Speed...125 KIAS Pressurization Controls ...SET Emergency (EMERG) Fuel Pump ...OFF at safe altitude

4.5j Cruise Checklist (4.27) CRUISE (4.27)

WARNING

Operation above 25,000 ft is not approved.

CAUTION

To maintain lateral balance, alternate between right and left fuel tanks. See paragraphs 2.23 and 7.17.

Reference Section 5 power setting table and performance charts.

Cruise Power ...SET per power table Mixture (Refer to para. 4.27) ...ADJUST Pressurization Controls...CHECK'

4.5k Descent Checklist (4.29) NORMAL DESCENT (4.29)

Power ...CRUISE Mixture ...CRUISE SETTING Airspeed...AS REQUIRED Pressurization Controls ...SET Altimeter ...SET Windshield Defrost ...AS REQUIRED

4.5i Climb Checklist (Continued) CRUISE CLIMB (4.25b)

Manifold Pressure ...35 IN. HG Propeller Speed...2500 RPM Mixture...32 GPH Climb Speed...125 KIAS Pressurization Controls ...SET Emergency (EMERG) Fuel Pump ...OFF at safe altitude

4.5j Cruise Checklist (4.27) CRUISE (4.27)

WARNING

Operation above 25,000 ft is not approved.

CAUTION

To maintain lateral balance, alternate between right and left fuel tanks. See paragraphs 2.23 and 7.17.

Reference Section 5 power setting table and performance charts.

Cruise Power ...SET per power table Mixture (Refer to para. 4.27) ...ADJUST Pressurization Controls...CHECK'

4.5k Descent Checklist (4.29) NORMAL DESCENT (4.29)

Power ...CRUISE Mixture ...CRUISE SETTING Airspeed...AS REQUIRED Pressurization Controls ...SET Altimeter ...SET Windshield Defrost ...AS REQUIRED

ISSUED: FEBRUARY 23, 1999 REPORT: VB-1710

4-15

ISSUED: FEBRUARY 23, 1999 REPORT: VB-1710

4-15

FOR REFERENCE ONLY

NOT FOR FLIGHT

REPORT: VB-1710 ISSUED: FEBRUARY 23, 1999

In document Piper PA-46-350 Malibu Mirage POH (Page 95-100)