background image

Summary of Contents for Hawk XP

Page 1: ...r PILOT S OPERATING HANOBOO 1 Hawk XP CESSNA MODEL R172K I l NORTHEAST REGION CAP...

Page 2: ...Roll Total Distance Over 50 Ft Obstacle STALL SPEED CAS Flaps Up Power Off Flaps Down Power Off MAXIMUM WEIGHT STANDARD EMPTY WEIGHT Hawk XP Hawk XP II MAXIMUM USEFUL LOAD Hawk XP Hawk XP ff o t BAGGA...

Page 3: ...6 85 Full Flap Operating Range Lower White Arc limit is maximum weight Vs in landing configuration Uppe limit is maximum speed permissible with flaps extended 54 129 Normal Operating Range Lower limit...

Page 4: ...ar seat must not be occupied CENTER OF GRAVITY LIMITS NORMAL CATEGORY Center of Gravity Range Forward 35 0 inches aft of datum at 1950 lbs or less with straight line variation to 41 0 inches aft of d...

Page 5: ...ign load factors are 150 of the above and in all cases the structure meets or exceeds design loads UTILITY CATEGORY Flight Load Factors Gross Weight 2200 lbs Flaps Up 4 4g 1 76g Flaps Down 3 0g The de...

Page 6: ...oad factors are 150 of the above and in all cases the structure meets or exceeds design loads JTILITY CATEGORY light Load Factors Gross Weight 2200 lbs Flaps Up 4 4g 1 76g Flaps Down 3 0g The design l...

Page 7: ...m Entry Speed Maneuver Reem Entry Speed Chandelles 110 knots Lazy Eights 110 k nots Steep Turns 105 knots Spins Slow Deceleration Stalls except whip stalls Slow Deceleration 2 10 Altitude loss in stal...

Page 8: ...ds For Emergency Operation OPERATIONAL CHECKLISTS Engine Failures Engine Failure During Takeoff Run Engine Failure Immediately After Takeoff Engine Failure During Flight Forced Landings Emergency Land...

Page 9: ...ting terrain and obstruct d ions then retract flaps upon reaching a safe J ltitu e nd airspeed 5 All Switches except master and igmt10n switches __ OF F l I CESSNA MODEL R172K SECTION 3 EMERGENCY PROC...

Page 10: ...OFF 3 6 CESSNA MODEL R172K SECTION 3 EMERGENCY PROCEDURES 2 Vents Cabin Air Heat CLOSED to avoid drafts 3 Fire Extinguisher ACTIVATE if available WARNING After discharging an extinguisher within a clo...

Page 11: ...ILURE If an engine failure occurs during the takeoff run the most impor tant thing to do is stop the airplane on the remaining runway Those extra items on the checklist will provide added safety durin...

Page 12: ...om the tailpipe and po ur i g 1 1 n en the fuel puddle on the pavement In the event th t this ssi ly igniting in accordance with the Fire During Start On Ground choccklu s proceed ec ist 3 10 I ll 1 1...

Page 13: ...ng conditions is prohibited airplane Durmg mstrument flights however icing conditions in this encountered inadve rtently and therefor so e corrective action m_ay be required as shown m the checklists...

Page 14: ...iven fuel pump will be evidenced by a sud den reduction in the fuel flow indication prior to a loss of power while operating with adequate fuel in either or both fuel tanks In the event of an engine d...

Page 15: ...stem To do this turn both sides of the master switch off and then on again If the problem no longer exists normal alternator charging will resume and the warning light will go off If the light comes o...

Page 16: ...ems can be found in Section 9 SPEEDS FOR NORMAL OPERATION Unless otherwise noted the following speeds are based on a maxi mum weight of 2550 pounds and may be used for any lesser weight However to ach...

Page 17: ...during a stall recovery may be as much as 160 feet 2 KI AS values are approximate MOST REARWARD CENTER OF GRAVITY ANGLE OF BANK WEIGHT FLAP LBS DEFLECTION oo 30 45 60 KIAS KCAS KIAS KCAS KIAS KCAS KIA...

Page 18: ...ELD I 50 FT OBS 1510 1655 1820 2005 2220 2470 2765 3115 3545 REFER TO SHEET 1 FOR APPROPRIATE CONDITIONS AND NOTES o0 c 10 c 20 c 3o0 c PRESS ALT TOTAL TOTAL TOTAL TOTAL FT GRND TO CLEAR GRND TO CLEAR...

Page 19: ...le Mixture Set at Placard Fuel Flow Cowl Flap Open Standard Temperature NOTES MIXTURE SETTING PRESS ALT GPH S L 16 4000 14 8000 12 12 000 10 1 Add 1 4 gallons of fuel for engine st art taxi and takeof...

Page 20: ...nded Lean Mixture Cowl Flap Closed 20 c BELOW STANDARD TEMP _9oc RPM MP KTAS GPH BHP 2600 24 23 78 122 11 1 22 73 118 10 3 21 68 114 9 6 2500 25 24 80 122 11 2 r j 75 J19 10 6 22 70 16 9 9 2400 25 79...

Page 21: ...20 il 98 7 3 49 97 7 1 47 19 46 92 6 8 45 91 6 6 43 Figure 5 7 C rnise Performance Sheet 2 of 6 Fig f 101 7 4 95 6 9 89 6 4 C SSNA MODEL R172K CRUISE PERFORMANCE PRESSURE ALTITUDE 6000 FEET CONDITION...

Page 22: ...7 0 47 96 6 8 57 110 8 2 55 109 7 9 53 105 7 7 51 103 7 4 49 g9 7 1 47 97 6 9 45 93 6 6 43 91 6 4 Figure 5 7 Cruise Performance Sheet 4 of 6 I rl l CESSNA MODEL R172K PERFO _ v 5 CRUISE PERFORMANCE PR...

Page 23: ...2 45 95 6 7 44 93 6 5 i i 111 8 0 54 109 7 8 52 104 7 5 50 103 7 2 47 98 6 9 46 96 6 7 43 90 6 4 41 88 6 2 53 1llh 7 6 1 51 104 7 4 48 100 7 1 47 98 6 8 44 93 6 5 43 90 6 3 7 1 Lil 101 47 99 6 9 45 94...

Page 24: ...ry grass runway increase distances by 40 of the ground roll figure SPEED o0 c 10 c 20 c 30 c WEIGHT AT PRESS 0 I Cl Ul 0 Ul z 2 Q 30_ Cl c l i i 0 3 fS iJi O Q Ol c i iil s x c Cl Q Q c c Cl LBS 50 FT...

Reviews: