Meridian PA-46-500TP Pilot Operating Handbook Download

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Summary of Contents for PA-46-500TP

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Page 205: ... 2 Aircraft Configuration SECTIONS PERFORMANCE Page No 5 3 5 5 5 7 Introduction Performance and Flight Planning 5 1 5 1 5 1 5 3 5 9 5 9 5 13 flight Planning Example Performance Graphs List of Figures List of Figures Metric ISSL ED November 12 2008 REPORT VB 1993 5 i ...

Page 206: ...SECTIOJ i 5 PERFORMANCE PA 46 SOOTP nm PAGE INTENTIONALLY LEFT BLk K REPORT VB 1993 5 ii ISSUED November 12 2008 ...

Page 207: ...only 5 2 AIRCRAFT CONFIGURATION Performance depicted in Section 5 is applicable to aircraft equipped with a weather radar pod main landing gear fairings 2 communications antennas 2 GPS antennas l dual purpose navigation antenna l radar altitude antenna 2 transponder antennas 1 marker beacon antenna 1 storrr1scope antenna 1 ADF antenna 1 DME antenna and I A MIFM radio antenna 5 3 INTRODUCTION PERFO...

Page 208: ...REMEMBER To get chart performance follow the chart procedures The information provided by paragraph 5 5 Flight Planning Example outlines a detailed t11ght plan using performance charts in this section Each charl includes it own example to show how it is used WARNING Performance information derived by extrapolation beyond the limits shown on the charts should not be used for t1ight planning purpose...

Page 209: ...e total weight of the airplane and the center of gravity position After proper utilization of the information provided the following Veights have been determined for consideration in the lljght planning example The landing weight cannot be determined until the weight of the fuel to be used has been established Refer to item g I I Basie Empty Weight 3380 lb 2 Occupants 520 lb 3 Baggage and Cargo 80...

Page 210: ...takeoff and or obstacle clearance The landing distance calculations are performed ln the same manner using the existing conditions at the destination airport and when established the landing weight The conditions and calculations for the example flight are listed below The takeoff and landing distances required for the flight have fallen well below the available runway lengths l Pressure Altitude ...

Page 211: ...utside air te1nperature values have been established apply the existing conditions at the departure field to graph figures 5 55 5 57 5 59 Now subtract the values obtained from the graph for the field of departure conditions from those for the cruise pressure altitnde The retnaining values are the true fuel titne and distance components for the climb segment of the night plan corrected for field pr...

Page 212: ...ues needed for the descent segment of the flight plan The values obtained by proper utilization of the graphs for the descent segment of the example are shown below I Fuel to Descend 50 1 lb minus 10 7 lb 39 4 lb 2 Time to Descend 16 6 min minus 2 6 min 14 min 3 Distance to Descend 60 2 nautical miles minus 8 2 nautical miles 52 nautical miles e Cruise Using the total distance to be traveled durin...

Page 213: ...istance e l minus c 5 minus d 3 188 nautical miles 1ninus 52 6 nautical miles mmus 52 nautical miles 3 Cruise Torque 4 Cruise Speed 5 Cruise Fuel Consumption 6 Cruise Time e 2 divided by e 4 83 4 nautical miles divided by 259 KTS 7 Cruise Fuel e 5 multiplied by eJ 6 255 pph multiplied by 0 32 hrs f Total Flight Time 83 4 nautical miles 1174 FT LB maximum speed cruise 259 KTS TAS 255 pph 032 hrs 8L...

Page 214: ...uired 0 87 hrs Determine the total fuel required by adding the fuel to climb includes fuel to start taxi and runup the fuel to descend and the cruise fuel When the total fuel in pounds is determined divide this value by 6 7 lb gal to determine the total fuel in gallons used for the flight The total fuel calculations for the example Hight plan are shown below l Total Fuel Required c 3 plus d I plus...

Page 215: ...31 5 17 Airspeed Calibration Primary Static Flaps 36 Gear Down 5 32 5 19 Airspeed Calibration Alternate Static Flaps 0 and 10 5 33 5 2 Airspeed Calibration Alternate Static Flaps 20 Gear Down 5 34 5 23 Airspeed Calibration Alternate Static Flaps 36 Gear Down 5 35 5 25 Altitude Calibration Primary Static Flaps 0 and 10 5 36 5 27 Altitude Calibration Primary Static Flaps 20 Gear Down 5 37 5 29 Altit...

Page 216: ...55 5 63 Cruise Climb Fuel 5 56 5 65 Cruise Climb Distance 5 57 5 67 Maximum Speed Cruise ISA ISA 10 ISA 20 5 58 5 69 Maximum Speed Cruise ISA 10 ISA 20 ISA 35 5 59 5 75 Low Power Cruise 500 FT LB ISA ISA 10 ISA 20 5 60 5 77 Low Power Cruise 500 FT LB ISA 10 ISA 20 ISA 35 5 61 5 79 Intermediate Cruise Power 600 FT LB ISA ISA 10 ISA 20 5 62 5 81 Intermediate Cruise Power 600 FT LB ISA 10 ISA 20 ISA ...

Page 217: ...ise Power 1100 FT LB ISA SA 10 ISA 20 5 72 5 101 Intermediate Cruise Power 1100 FT LB ISA 10 ISA 20 ISA 35 5 73 5 103 Intermediate Cruise Power 1200 FT LB ISA ISA I0 SA 20 5 74 5 J05 Intermediate Cruise Power 200 FT LB ISA 10 ISA 20 ISA 35 5 75 5 111 SpecificAirRange 5 76 5 113 Holding Time vs Fuel on Board 5 77 5 115 1ime to Descend 5 78 5 117 Fuel to Descend 5 79 5 J19 Distance to Descend 5 30 5...

Page 218: ...SECTIONS PERFO VIANCE PA 46 SOOTP THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 1993 5 12 ISSUED November 12 2008 ...

Page 219: ...ation Primary Static Flaps 20 Gear Down 5 95 5 163 Altitude Calibration Primary Static Flaps 36 Gear Down 5 96 5 165 Altitude Calibration Alternate Static Flaps 0 and 10 5 97 5 167 Altitude Calibration Alternate Static Flaps 20 Gear Down 5 98 5 169 Altitude Calibration Alternate Static Flaps 36 Gear Down 5 99 5 173 Angle of Bank vs Stall Speed 5 101 5 175 Normal Takeoff Ground Roll 0 Flaps 5 102 5...

Page 220: ...118 5 211 Low Power Cruise 500 FT LB ISA 10 ISA 20 ISA 35 5 119 5 213 Intermediate Cruise Power 600 FT LB ISA ISA JO ISA 20 5 120 5 215 Intermediate Cruise Power 600FT LB ISA IO ISA 20 ISA 35 5 121 5 217 Intermediate Cruise Power 700 FT LB ISA ISA 10 ISA 20 5 122 5 219 Intermediate Cruise Power 700 FT LB ISA 10 ISA 20 ISA 35 5 123 5 221 Intermediate Cruise Power 800 FT LB ISA ISA JO ISA 20 5 124 5...

Page 221: ...0 ISA 20 ISA 35 5 131 5 237 Intermediate Cruise Power 1200 FT LB ISA ISA 10 ISA 20 5 132 5 239 Intermediate Cruise Power 1200 FT LB ISA 10 ISA 20 ISA 35 5 133 5 245 Specific Air Range 5 134 5 247 Holding Time vs Fuel on Board 5 135 5 249 TimetoDescend 5 136 5 251 Fuel to Descend 5 137 5 253 Distance to Descend 5 138 5 255 Glide Endurance 5 139 5 257 Glide Distance 5 140 5 259 Balked Landing Climb ...

Page 222: ...SECTIONS PERFORMANCE PA 46 SOOTP THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 1993 5 16 ISSUED November 12 2008 ...

Page 223: ...SECTIONS PERFORMANCE THIS PAGE INTENTIONALLY LEFT BLANK ISSUED November 12 2008 REPORT VB 1993 5 17 ...

Page 224: ... BY 0 3048 3 2808 3 7854 0 2642 0 4536 2 2046 33 8639 0 02953 PA 46 500TP TO OBTAIN Meters Feet Liters Gallons Kilograms Pounds Millibars Inches of Mercury Example 50 feet 50 x 0 3048 meters 15 24 meters 100 liters 100 x 0 2642 gallons 26 42 gallons REPORT VB 1993 5 18 Conversion Table Figure 5 1 ISSUED November 12 2008 ...

Page 225: ...3 80 70 60 50 FAHRENHEIT 40 DEGREES 30 20 F 9 5 C 32 10 0 10 20 30 40 40 30 20 10 0 10 20 30 40 Temperature Conversion Figure 5 2 ISSUED November 12 2008 SECTIONS PERFORMANCE Sea Level ISA Standard Day 59 F 15 C CELSIUS DEGREES C 5 9 F 32 REPORT VB 1993 5 19 ...

Page 226: ...ECTIONS PERFORMANCE VOLUME U S GALLONS REPORT VB 1993 5 20 1 8 0 1 6 0 600 1 4 0 500 1 2 0 400 1 0 0 80 300 60 4 0 100 20 0 Volume Conversion Figure 5 3 PA 46 SOOTP VOLUME LITERS ISSUED November 12 2008 ...

Page 227: ...00 LENGTH 15000 FEET 10000 5000 0 9000 8000 7000 6000 5000 4000 3000 2000 1 0 0 0 0 SECTIONS PERFORMANCE LENGTH METERS Feet to Meters Conversion 0 to 30 000 feet Figure 5 4 ISSUED November 12 2008 REPORT VB 1993 5 21 ...

Page 228: ...ECTIONS PERFORMANCE LENGTH FEET 1 0 0 90 80 70 6 0 50 40 3 0 20 1 0 0 PA 46 SOOTP 30 20 LENGTH METERS 1 0 0 Feet to Meters Conversion 0 to 100 feet Figure 5 5 REPORT VB 1993 5 22 ISSUED November 12 2008 ...

Page 229: ...00 W EIGHT POUNDS 4400 4300 4200 4100 4000 3900 3800 2300 2200 21 0 0 2 0 0 0 1900 1 8 0 0 SECTIONS PERFORMANCE MASS KILOGRAMS Pounds to Kilograms Conversion 3 800 to 5 100 pounds Figure 5 6 ISSUED November 12 2008 REPORT VB 1993 5 23 ...

Page 230: ...EIGHT POUNDS 300 250 200 1 5 0 1 a a 50 0 PA 46 SOOTP 1 3 0 1 2 0 1 1 0 1 0 0 90 80 70 MASS KILOGRAMS 60 50 40 30 20 1 0 0 Pounds to Kilograms Conversion 0 to 300 pounds Figure 5 7 REPORT VB 1993 5 24 ISSUED November 12 2008 ...

Page 231: ...tandard Day 950 28 1013 25 Mb 29 92 lnHg 27 900 26 850 25 800 24 23 750 22 700 21 20 PRESSURE 650 PRESSURE MILLIBARS 19 IN HG 600 18 17 550 16 500 15 14 450 13 400 12 11 350 10 9 Inches of Mercury to Millibars Conversion Figure 5 8 ISSUED November 12 2008 REPORT VB 1993 5 25 ...

Page 232: ...0 ui N REPORT VB 1993 5 26 0 0 0 c i N 0 0 0 c i I 3Cn l 1 13 nSS3 d ISA Temperature Conversion Figure 5 9 0 0 0 ui PA 46 SOOTP 1 li BIIEBIIII K JW 1teniiffid 0 0 0 0 N 0 0 0 w ct 0 i w 0 0 N w I 0 7 0 I 0 0 0 I 0 ISSUED November 12 2008 ...

Page 233: ... w 0 0 Ill w J 1 z N 1 0 0 0 0 0 1 1 r i fv o s 0 0 N 1 1 1 LN INOdlNO l ONIMO cf IH Wind Components Figure 5 10 ISSUED November 12 2008 SECTION 5 PERFORMANCE 0 1 0 0 0 z w z 0 0 IL I 0 0 C z 0 3 N rn rn 0 0 0 0 REPORT VB 1993 5 27 ...

Page 234: ...ATE ALTITUDE 1 000 930 2 000 1 930 3 000 2 930 4 000 3 930 5 000 4 930 6 000 5 930 7 000 6 930 8 000 7 930 9 000 8 930 10 000 9 930 11 000 10 930 12 000 11 930 13 000 12 930 AIRSPEED 125 CLIMB 122 175 CRUISE 172 85 APPROACH 83 Alternate Static System Correction Figure 5 11 ISSUED November 12 2008 ...

Page 235: ... fl f l i lO ii 1 _ _ jl 1 1 1 w I _ 1 1 1 L 1 1 l ll 1 1 J 1 1 1 1 l l f l f l 1 lf l l l l l l o 1 11 1 1 1 1 1 1 1 1 1 rt 1 1 l 1 1 l l t 1 1 l l I 1 I 1 i I 1 l 1 1 l l l I i I I I I I I i 0 0 I I I I T I I 0 0 N O O O 1 1 0 s nis1 1HDl3M l ll 3dS 13n i Aviation Fuel Specific Weight Figure 5 12 ISSUED November 12 2008 I I ri REPORT VB 1993 5 29 ...

Page 236: ...I Ii I f I I ll I Ii I 11 f J f l f 1 L fJ l l I I fr TI u u 1 a J U l 444 H li I l_ ri I I 1 TT I I IlJ 11T 111 IP ill t 1 i 1 fl 1 1 i f1 r fJi Tf 4 fiJ h1 I I I I t l 1 1 I I I L l I H s i i I I I I I I I I I I I li 1 I I I I l I I I I I 11 I l I 1 I I I r I f I 1 1i 1 I 1 1 ITf H 1 i y 0 N I I I S J ON f 033dS flt 031 81llf Airspeed Calibration Primary Static Flaps 0 and 10 Figure 5 13 I I I I...

Page 237: ...1 H f H H 1t 1 H t r 1 tt t ilrrr 1tt 1 H1 t rr t 1 H1 t H1 tt H 1 I I j L f1 I I ji_t I II 11 1 11 rT o g O SlON l 033dS tlllf 03llll l811 10 Airspeed Calibration Primary Static Flaps 20 Gear DOWN Figure 5 15 ISSUED November 12 2008 REPORT VB 1993 5 31 ...

Page 238: ...P 0 zW 00 E Ox Zw 0 0 i 0 I 0 0 J Q H t i i L 1 I i I l L i I I I I i I i 0 I S lON I 033dSHl lf 03 l IIH811 110 Airspeed Calibration Primary Static Flaps 36 Gear DOWN Figure 5 17 H 0 O 0 O REPORT VB 1993 5 32 ISSUED November 12 2008 ...

Page 239: ... P 4 1 1_ 1 P 4 P 1 _t1 t 4 P J 1 _Pf 1 I I i I I l i t I t j J j i l T T 1 l l IJ J 0 L ti I 11 r h ii i I L 1 t I J d 1 1 L 11 1 1H r ii 1 1 t 1f J f i T1 1 Yr r 1 Y i t t f r 1 H r H H trt H t1d t ti tt tt1 t twtt 1t i t tlttwtt11t t d t1t H t ttttHtt d t n TtLM 4 t t tt dr g 1 I i I I II 1 _ lJ I II I I I 0 0 0 12 Q J co 0 S LON I 033dS 1 03 L ln Slllt Airspeed Calibration Alternate Static Fla...

Page 240: ...i g I I I t I i 1 I I I 1 J f l ll 1 H l ll i ll l l l H 1 I j i I i l i I 1 1 i JI I 1 L 1 11 I j o I I I I I a H 1 l I J H H I I 1 t j 1 H t I H t rn H l H I 111 I I I 1 tr H h tr 0 S LONJ t 033dSlll o 03 L fll8111f0 Airspeed Calibration Alternate Static Flaps 20 Gear DOWN Figure 5 21 REPORT VB 1993 5 34 ISSUED November 12 2008 ...

Page 241: ... t l l 1 1 I 16 5 1 1 1 r 1 lI c yt t tl rl J i ltt 1 1 Jt L 1 rL__ 1 1 l iu L L 1 1 j t r 1 1 q f I ii l 1 t 1 i l I r H 1 i t t H t t t t t Hg 1 j1 J I l I J J J I jl i I i f l t c i i c 1 1 1 I ttl 1 1 i t i I 1 i 11 1 ii l Ii TTJf t I g S LON 033dS l lf 03 L Sll lf Airspeed Calibration Alternate Static Flaps 36 Gear DOWN Figure 5 23 ISSUED November 12 2008 REPORT VB 1993 5 35 ...

Page 242: ...PLE Indicated Airspeed 170 KT Pressure Altitude 25 000 FT Altitude Correction 22 FT Add Correction to Press Alt 24 978 FT I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I INDICATED ALTiTUDE _ r 130 140 150 160 170 180 INDICATED AIRSPEED KNOTS Assumes zero instrument error Sea Le ve1 1 I IL s oo0 1 11L_ 10 opo_ I I 1s 00 1 I I I 21 g 1 1 00 1 f ooo 1 I I I I I I I I I ao ooo I I I I ...

Page 243: ...n m u C II SECTION 5 PERFORMANCE J J J J J j 0 0 j I J I II 0 I J gl J cJ J I Q j I j J J J I 0 0 f 133 1 NOl 103HHOO 3an 11 1w V Altitude Calibration Primary Static Flaps 20 Gear DOWN Figure 5 27 _ _ 0 0 0 0 ISSUED November 12 2008 REPORT VB 1993 5 37 ...

Page 244: ...I Q C C z 0 c 0 z w 0 C z C w WO I D w ti i i 0 C E Cl 0 1 1 Ill PA 46 SOOTP I I I I 0 c l i i 0 t t 2 _ Ii 2 f rJ s 0 0 0 33 1 N01 03 ll IOO 3anllll lf 7 Altitude Calibration N 0 N 0 0 0 0 0 0 0 0 0 t z le c C E w w 0 1ii 5 0 C ii w ill E 0 Cw Primary Static Flaps 36 Gear DOWN Figure 5 29 REPORT VB 1993 5 38 ISSUED November 12 2008 ...

Page 245: ...o I _ 00 i3 0 ui C it 0 C 1 SECTIONS PERFORMANCE I I iif cL od f Jd cj 9 s i n rv _ _ _ u _ I 2 J _ g Q i 0 0 N 0 a 0 X 0 r 0 0 0 0 0 N 0 0 0 0 a N 0 N 0 133 NOl103l ll IOO 3an1111v V Altitude Calibration Alternate Static Flaps 0 and 10 Figure 5 31 U C e 0 z c C E w w Cl en U i 0 i e C w en _ E u en C en a ISSUED November 12 2008 REPORT VB 1993 5 39 ...

Page 246: ...c C z w 0 C t z 0 w WO w ti 0 u mm u LL 0 Ill YI 1 1 I 0 1 __ AC J ff I I v v L I 0 I _ PA 46 SOOTP I fil0 ijI tcs V CS CS If r L C L 0 u C 0 0 I z C o E w w D II u C 0 I w II 0 0 m E t Cm i 133 1 No1103 00 3an111111 v Altitude Calibration Alternate Static Flaps 20 Gear DOWN Figure 5 33 REPORT VB 1993 5 40 ISSUED November 12 2008 ...

Page 247: ... w WO f w u q_ L 0 g I ii SECTION 5 PERFORMANCE I I I I J 1jj1 IJJ I _J s z IJJ Vr i 1 C J Q fl tJttt I 0 0 0 7 1 133 1 NOIJ 03HHOO 3GnJ IJ 1 f V Altitude Calibration Alternate Static Flaps 36 Gear DOWN Figure 5 35 0 N 0 0 0 0 0 1 C e 0 z C C E w W ll JI U C a 0 C w E u 5 JI z JI ISSUED November 12 2008 REPORT VB 1993 5 41 ...

Page 248: ...SECTIONS PERFORMANCE PA 46 SOOTP THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 1993 5 42 ISSUED November 12 2008 ...

Page 249: ...E i I 1 l l H i lrt t t 1 j i l g 1 i 0 I l 0 0 Hl 1 1 il H 1 11 i HH W 1 i L C Ll Ll LI l 0 0 0 0 0 0 0 0 CX SJ ON Q33dS 11 tJ S 03J lt IONI Angle of Bank vs Stall Speed Figure 5 39 0 0 ci w C w I z c z c co ISSUED November 12 2008 REPORT VB 1993 5 43 ...

Page 250: ... 1 1 L 1 f 1 ai O r 1 t ff j 0 f J L f i li Juf i I j i a _ _ dJ I _L a5l4 1 1_i_l I I I r r i 0 I iii J t 1 e I _ f c QJ a 1 l t i _Q __ Down g _ i L I _ _ _ l O Cll C 7 4 000 f t _f J t lo Ul Q qQ L t I r Cl e Ji r I I _ _ I J I i b l 1 1 1 i l Q N I 1 clJ 1 w i r I __ _ r I 7r k 1 i i L I 1 1 I _ FJ I t I i 1 r J j I _ cl e J0 r I _ _ J _____ o 1 1 1 see __ _ 1 _ __ _ _ j 1 I i _ r 1 1 I l 1 i ...

Page 251: ...i j 1 1 I 1 H i c 1 t i 1 1 t 1 1 t J t L __i_ s u J __j_ c g C 1 r I 1 1 1 i 1 0fi k 1 1 f I a I J Down c s __ r 1 1 t rR of l 3 r fJ 1 1 e _ l 1 r i j I _ I Si L L_ 7 _ j E f i t i I Cf J 1 Ql tly b 0 N j J Jt J I a l i 2 b __ a 1 1 L 1 t h n 7 ie 1 i t _0_ t i b sea tt o J I I I i I i h i I rl 1 y r 1 f t f 1 J 1 f t 1 1 I 1 1 1 J s J Ff 11 l t 1 4 i L 1 1 I 2 905 FT t f 8 000 u 7 000 6 000 gj ...

Page 252: ...1 727FT m TTR ___ r T T J D T __ J l ru t f H_j_ J J 1 c 1 _j_ _ c I T I al J I i w P m i J _J 1 i 0 s __ _ J 1 J 1 __ _ I fl m o w J Wn wc l S 1 Jl Ll a I 5 u 17rr _ J S I I J 2 __ ___ s s 0 iii i 11 N I l f N J tE B i 1 I _ _ L 7e L I h I O _ _I 1 k r I I I T I 1 k I i T I I 1 1 LL c I l _ r rr 1 I l _ I J i c 5 000 l j 4 000 J C 3 000 z i u u 2 000 fil i5 30 20 10 0 10 20 30 40 50 OUTSIDE AIR T...

Page 253: ...ponent Takeoff Distance ru _j__J 5 0 1 J H 1 J L L U t 1 09 N 1 W Li 1 I t I r i Down t ______ o w qjt 1 if 0 et j E t 1 1 1 tlt I l l l I 1 1 l 1 a t i H b e R u 1 1 1 H ____ E E 29 C 2o o UP 1 000 FT 4 841 LB 10 KT 2 488 FT 7 000 u UJ 6 000 3 i 8 5 000 O t 0 4 000 a 3 000 z i C J 2 000 i5 u u l l j _J 1 t t 30 20 10 0 10 20 30 40 50 0 1 2 I I I 11 1 1 i I I I i I i I 1 crn 1 000 38 0 10 20 lf 1 ...

Page 254: ...Weight Climb Performance 7 C 12 000 FT 4 800 LB 1 459 FPM _j otffl i I ff I 1 TT l_l tJfJ i 1 __ 1 1 _ e Sea leverT 1 sooo L t 1 l c1 0 i 20 OOo J u L I i 1 _ c r _ s c l II v Hrt1f1J J _ C 1 t c mB r i 1 t i t Jtcti Sl i fV I i fl F 5f s 21 J I J H T 1 ut i i l l_l j J J 44 t 1 1 1 l l l J p 2 500 2 000 ii 1 500 ca E 1 000 w i 500 70 60 50 40 30 20 10 0 10 20 30 40 50 OUTSIDE AIR TEMP c tE Htltl ...

Page 255: ...de Aircraft Weight Climb Performance CJ i l r I amTi J t E I 1 __ 4 __ _ _ J_J_5 o o 10 000 _ i 1 1 j i itwJ R l 1s ooo ov 7 C 12 000 FT 4 800 LB 572 FT NM H t _ I i J Jf 1 __g J 1 tf t slc f i J j q_ J st 1 nl I ff 1 000 500 70 60 50 40 30 20 10 0 10 20 30 40 50 OUTSIDE AIR TEMP C 50 48 46 44 42 40 WEIGHT LBx100 0 38 z j LL i z w I co l u 111 I ffil I liJ u J j ol g i 1l 0 Q t l l Z 0 l z t l ...

Page 256: ...g 4 t t1 IWi ff f ft i 1 tttt j 1 J JZ g1 r t 1 2r1 I I I f I I I 1 I l I i i i i i V I I I I I l ffi r ttt J tjz 1 i r t J Il i er r t t E fzt cb I I 1 l _J r f I _ O set t j t r t 3 _ _ t_ _jz EE I t s n Ooo a Level i 8 ooo_ _ i I 1 r il i j Do i _ D i r I _ r 1 r L_ r L I I I 10 1 OOOF S 1 i f t t f I p L 1 i 1 c f T4 1_ _ t j tF t r I i 1 jj t t l l f 30 20 10 0 10 20 30 OUTSIDE AIR TEMP C 40 ...

Page 257: ... zO 0 j 0 _ CZ 1 UJ ZO e zc t oo w O Q t CC S 00 w z w 0 0 z U ld 1 SUiin 10 3 1 _ 1 I j I l i 1fK i 1 l I I l I i I H H e 1 t i T I I I I I Takeoff Climb Performance 20 Flaps Figure 5 54 I I I 0 0 O i _ I c w s g 0 ISSUED November 12 2008 REPORT VB 1993 5 51 ...

Page 258: ...Alt 25 000 FT Flaps Time To Departure Alt 0 7 Min Time To Cruise Alt 20 Min Gear Time During Climb 20 w 0 7 19 3 Min Climb Speed 125 KIAS __ _s J l 1 45 r 40 r t 1 1 1 i_ 1 l 1 _ _ 35 1 I _l o J Zf lo i ___ __ l C l t s J 5 ooo 1 1 I I I 1 I 1 CRUISE Jc I I 30 z ii 25 cc 20 U f 4 1 _ 1 X f2 15 ij F f r f r1ff1 1 c s oo 1 70 J 60 50 40 i t f c ea Lev 30 20 10 0 10 OUTSIDE AIR TEMP C 10 5 0 20 30 40...

Page 259: ...ing Climb 152 48 104 LB 1 i H 1 J 1 1 E l Y w y t 1 Fuel to start taxi and takeoff included 1 1 i L 5 I i fl_ o OOIJ c l t 10 i I 1 I I I I f 1 I r S T T 240 220 200 180 i 1 I _ 1 160 l X RUISE al s o00 140 5 _ r f _ 9 F _t t_ _ 20 000 1 r o I s_ 0 1 120 t 15 00D J _ _____ x __ __ t 1 t C I i l 100 U s v oo s i 4 00 __ _ _ D c o 80 L __j __ _ __ l 5 000 l _ _ a 60 t 1 OEPARTURE k t _ __ S sea Leve...

Page 260: ...limb 54 1 3 52 7 NM f ffl r __ 1 L r 1 t t b 1 IW j 1 1 140 120 i I _trt p __ff _t 1 t l E j L _ f fft f L l l 100 iE ooO j l 2 f Jt t j __ 1 1 0 __l i 1 I I 1 i 1 I 1 I Jc ____ c C L 4 j __ _ 1 r _ f OOG 1 H4 J 1 i 80 _ V _ I u CRUISE 1 cd l 1 I _ u l 1 EJ i r J oolt 4 r i 40 I S 1 20 _ 0 f t 1 l 60 r _ _ i 1s 0001 i __ 1___ __ 1 I _j____ H10 ooo l 1 1 _hJ _ 1 J 1 1 70 60 50 40 f 1 30 fs EALEVEL ...

Page 261: ...Min Time To Cruise Alt 23 3 Min Flaps RETRACTED Time During Climb 23 3 1 3 22 Min Gear RETRACTED Climb Speed 140 KIAS to 20 000 FT 125 KIAS to 30 000 FT r 1 tu f _ 0 r l 1 t z t t t t i MJ t1 z_ _ t 1 I ___ 1 1 1 i fo t i f 10 0oo I I s 1 j ___ r 4 r 1 r i l f l 1 I t t T r i 000 SeaLevCW DEPARTURE 1 i t 70 60 50 40 30 20 10 0 10 20 30 40 50 OUTSIDE AIR TEMP C 45 40 35 z E 30 co 25 u 20 w 15 10 5 ...

Page 262: ... TO 20 000 FT 125 KIAS TO 30 000 FT _ ______ ___ __ __ 1 1 _ r r i 1 1 1 1 l l tl i 1 I Fueltostart taxi I i t lb y l t and takeoff rnc uded 1 1 I 0 00 I f l l I I _ __j i r l l 1 _J I I L__ ____ _ J _ _ _ f__ 1 I 1 1 CRUISE I t 0i _ _ r i t t t I l f 1 k L 1 I __ 15000 1 1 4 I _ r 1 t l 5 L 1 J L o 10 0001 a6 t E I E__ i r 1 O I c _ x r L L t J 1 5 000 _ J 1 _____ _ r t 1 t t l l i t f l s _t s L...

Page 263: ...parture OAT 29 c Cruise OAT 2o c Departure Press Alt 1 000 FT Cruise Press Alt 25 000 FT Dist to Departure Alt 1 8 NM Dist to Cruise Alt 67 5 NM Distance during Climb 67 5 1 8 65 7 NM 1 t 160 I 1 140 f _ ___ 120 i 1 E r z I 100 ca 80 C J CRU 0 71 i t 1 t i r iwt_4_ i t 60 I 40 en i5 t1 t 1i t t t trt j I r 1 o oool i 20 t 1 1 1 1 I 5 00 ltj _ 1 s 2 ioEMR URE 0 70 60 50 40 30 20 10 0 10 20 30 40 50...

Page 264: ... 177 998 318 190 1066 293 205 1153 280 222 1255 281 241 C 13 13 ii 1112 ISA 10 QC Torque Fuel Flow TAS FT LB PPH KT 956 353 180 1014 322 194 1088 297 209 1177 285 226 1285 286 246 1298 278 260 1077 230 256 ISA C Torque Fuel Flow TAS FT LB PPH KT 969 355 183 1030 325 197 1106 301 213 1201 290 231 1313 291 251 1250 269 260 1040 222 255 NOTE Shaded areas are beyond aircraft OAT limit See paragraph 2 ...

Page 265: ... 7 5000 40 1088 10000 30 1177 15000 20 1285 20000 10 1201 25000 0 1071 30000 9 890 Fuel Flow PPH 360 330 305 295 292 260 214 Fuel Flow PPH 363 334 310 299 292 250 207 Fuel Flow PPH 3El8 339 317 307 274 237 195 SECTIONS PERFORMANCE TAS KT 186 201 217 235 254 259 254 TAS KT 189 204 221 240 257 258 253 TAS KT 194 209 227 246 253 255 250 NOTE Shaded areas are beyond aircraft OAT limit See paragraph 2 ...

Page 266: ...5 161 164 55 I LI J 14 ti 17l i qli t _ 129 173 ISA 10 C OAT Torque Fuel Flow TAS OC FT LB PPH KT 5 292 131 5 252 140 15 214 149 25 500 185 157 35 161 166 45 143 173 54 129 180 ISA C OAT Torque Fuel Flow TAS OC FT LB PPH KT 15 292 133 5 253 142 5 215 151 15 500 185 159 25 162 167 35 143 175 44 129 182 NOTE Shaded areas are beyond aircraft OAT l1m1t See paragraph 2 28 ECS NORMAL REPORT VB 1993 5 60...

Page 267: ...85 162 143 130 Fuel Flow PPH 293 254 216 186 162 143 130 Fuel Flow PPH SECTIONS PERFORMANCE TAS KT 136 144 153 161 169 177 183 TAS KT 137 146 155 163 171 178 184 TAS KT II o L 50 i 2S4 t4f c 5000 40 255 149 10000 30 217 157 15000 20 500 187 165 20000 10 164 173 25000 0 145 180 30000 9 131 185 NOTE Shaded areas are beyond aircraft OAT limit See paragraph 2 28 ECS NORMAL Low Power Cruise 500 FT LB I...

Page 268: ...179 c55 57 i i 18ff f4t 64 197 ISA 10 QC OAT Torque Fuel Flow TAS QC FT LB PPH KT 5 306 146 5 265 155 15 227 164 25 600 198 173 35 175 182 45 157 191 54 145 199 ISA QC OAT Torque Fuel Flow TAS QCl FT LB PPH KT 15 307 148 5 266 157 5 227 166 15 600 199 175 25 176 184 35 158 193 44 145 202 NOTE Shaded areas are beyond aircraft OAT limit See paragraph 2 28 ECS NORMAL Intermediate Cruise Power 600 FT ...

Page 269: ...LB 600 ISA 35 C Torque FT LB 1 _ 600 Fuel Flow PPH 308 267 228 199 176 158 145 Fuel Flow PPH 308 268 228 200 177 159 146 Fuel Flow PPH 309 269 230 201 178 159 146 SECTIONS PERFORMANCE TAS KT 150 159 168 177 186 195 204 TAS KT 152 161 170 179 188 197 205 TAS KT 156 164 173 182 191 200 208 NOTE Shaded areas are beyond aircraft OAT lrm1t See paragraph 2 28 ECS NORMAL Intermediate Cruise Power 600 FT ...

Page 270: ...Fuel Flow TAS FT LB PPH KT 318 156 277 165 240 174 700 211 183 189 192 I H2 202 I 161 212 ISA 10 QC Torque Fuel Flow TAS FT LB PPH KT 319 158 278 167 240 176 700 212 185 190 195 172 205 161 215 ISA QC Torque Fuel Flow TAS FT LB PPH KT 320 160 278 169 241 178 700 212 187 190 197 172 207 161 217 NOTE Shaded areas are beyond aircraft OAT limit See paragraph 2 28 ECS NORMAL Intermediate Cruise Power 7...

Page 271: ...FT LB 700 ISA 35 C Torque FT LB 700 Fuel Flow PPH 321 279 242 213 191 173 162 Fuel Flow PPH 322 280 243 214 191 174 162 Fuel Flow PPH 324 282 244 215 192 175 163 SECTIONS PERFORMANCE TAS KT 162 171 180 190 199 210 220 TAS KT 164 173 182 192 202 212 222 TAS KT 1 167 176 185 195 205 215 225 NOTE Shaded areas are beyond aircraft OAT limit See paragraph 2 28 ECS NORMAL Intermediate Cruise Power 700 FT...

Page 272: ...e Fuel Flow TAS FT LB PPH KT 331 165 291 174 254 184 800 225 193 204 203 Cri 1 8 214 17il I 220 ISA 10 C Torque Fuel Flow TAS FT LB PPH KT 332 168 292 177 255 186 800 226 196 204 206 188 217 178 228 ISA C Torque Fuel Flow TAS FT LB PPH KT 333 170 293 179 255 188 800 227 198 205 209 189 219 178 230 NOTE Shaded areas are beyond aircraft OAT limit See paragraph 2 28 ECS NORMAL Intermediate Cruise Pow...

Page 273: ...H 334 294 256 228 205 189 178 Fuel Flow PPH 335 295 257 228 206 190 179 Fuel Flow PPH ff 5 1 I 337 5000 40 296 10000 30 259 15000 20 800 230 20000 10 208 25000 0 191 30000 9 179 SECTIONS PERFORMANCE TAS KT 172 181 191 201 211 222 233 TAS KT 174 183 193 203 213 224 235 TAS KT 177 186 196 206 217 228 239 NOTE Shaded areas are beyond aircraft OAT lim1t See paragraph 2 28 ECS NORMAL Intermediate Cruis...

Page 274: ...que Fuel Flow TAS FT LB PPH KT 344 174 305 183 268 193 900 241 203 220 213 205 224 9e Z l6 ISA 10 C Torque Fuel Flow TAS FT LB PPH KT 345 176 306 185 269 195 900 241 205 220 216 205 227 196 239 ISA C Torque Fuel Flow TAS FT LB PPH KT 346 178 307 188 270 198 900 242 208 220 219 206 230 196 242 NOTE Shaded areas are beyond aircraft OAT limit See paragraph 2 28 ECS NORMAL Intermediate Cruise Power 90...

Page 275: ...25 206 233 34 196 245 OAT r0 e 35 25 15 5 5 15 24 ISA 20 0 e Torque Fuel Flow FT LB PPH 349 309 272 900 243 ISA 35 0 e 222 207 196 TAS KT 182 192 202 213 224 235 247 OAT Torque Fuel Flow TAS 0 e FT LB PPH KT 50 i 40 30 20 900 10 0 t 351 311 274 245 223 207 197 i 185 195 205 216 227 239 251 NOTE Shaded areas are beyond aircraft OAT limit See paragraph 2 28 EeS NORMAL Intermediate Cruise Power 900 F...

Page 276: ...1 iQc FT LB PPH KT 0 5 360 184 5000 5 320 193 10000 15 284 203 15000 25 1000 256 214 20000 35 237 225 25000 45 222 237 30000 54 215 249 ISA QC Altitude OAT Torque Fuel Flow TAS FT 1 C FT LB IPPH KT 0 15 361 186 5000 5 321 196 10000 5 285 206 15000 15 1000 257 216 20000 25 237 228 25000 35 223 240 30000 44 214 252 NOTE Shaded areas are beyond aircraft OAT limit See paragraph 2 28 ECS NORMAL Interme...

Page 277: ...000 ISA 35 QC Torque FT LB I 1000 Fuel Flow PPH 362 323 286 258 238 223 215 Fuel Flow PPH 364 324 287 259 239 223 212 Fuel Flow PPH 366 327 288 261 239 224 199 SECTION 5 PERFORMANCE TAS KT 188 198 208 219 230 242 255 TAS KT 190 200 210 221 233 245 258 TAS KT 1Jl3 203 214 225 237 249 262 NOTE Shaded areas are beyond aircraft OAT limit See paragraph 2 28 ECS NORMAL Intermediate Cruise Power 1000 FT ...

Page 278: ... SOOTP ISA 20 C Torque Fuel Flow TAS FT LB PPH KT 298 208 1100 271 219 253 230 iccl Ji r r e I ISA 10 C Torque Fuel Flow TAS FT LB PPH KT 299 211 1100 271 221 254 233 241 245 234 258 ISA C Torque Fuel Flow TAS FT LB PPH KT 300 213 1100 273 224 254 236 241 248 229 261 NOTE Shaded areas are beyond aircraft OAT limit See paragraph 2 28 ECS NORMAL Intermediate Cruise Power 1100 FT LB ISA ISA 10 ISA 20...

Page 279: ...Fuel Flow 1 C FT LB PPHl 35 25 339 15 302 5 1100 275 5 256 15 241 24 ISA 35 1 C OAT Torque Fuel Flow OC FT LB PPH c c 5 0 40 341 30 304 20 1100 276 10 256 0 238 9 SECTION 5 PERFORMANCE TAS KT 216 227 239 251 264 TAS KT 207 218 229 241 254 TAS KT Ii 211 222 233 245 258 NOTE Shaded areas are beyond aircraft OAT l1m1t See paragraph 2 28 ECS NORMAL Intermediate Cruise Power 1100 FT LB ISA 10 ISA 20 IS...

Page 280: ...5 5 5 15 25 35 44 PA 46 SOOTP ISA 20 QC Torque Fuel Flow TAS FT LB PPH KT 1200 270 237 fl i 250 1 ISA 10 QC Torque Fuel Flow TAS FT LB PPH KT 1200 289 229 271 240 259 253 239 266 ISA QC Torque Fuel Flow TAS FT LB PPH KT 1200 290 231 271 243 259 256 NOTE Shaded areas are beyond aircraft OAT hm1t See paragraph 2 28 ECS NORMAL Intermediate Cruise Power 1200 FT LB ISA ISA 10 ISA 20 REPORT VB 1993 5 74...

Page 281: ...5 C Torque FT LB Fuel Flow PPH 290 272 260 Fuel Flow PPH 291 272 254 Fuel Flow PPH SECTIONS PERFORMANCE TAS KT 234 246 259 TAS KT 237 249 262 TAS KT re o I 50 I I 5000 40 10000 30 321 229 15000 20 1200 292 241 20000 10 273 253 25000 0 238 267 30000 9 NOTE Shaded areas are beyond aircraft OAT hm1t See paragraph 2 28 ECS NORMAL Intermediate Cruise Power 1200 FT LB ISA 10 ISA 20 ISA 35 Figure 5 105 I...

Page 282: ...25000 104 9 106 4 107 6 108 6 109 7 30000 1144 116 1 117 6 118 9 121 9 LOW POWER CRUISE 500 FT LB Altitude Cruise Nautical Miles 100 Lbs Fuel FT ISA 20 C ISA 10 C ISA ISA 10 C ISA 20 C 0 44 3 44 9 45 6 46 4 46 9 5000 54 9 55 6 56 3 56 8 57 4 10000 68 9 69 7 70 4 71 0 71 6 15000 84 1 85 1 86 1 87 0 87 7 20000 101 8 102 8 103 6 104 3 105 4 25000 119 9 121 2 122 3 123 1 124 2 30000 138 5 139 4 140 3 ...

Page 283: ... 5 0 a E i 0 I l i I I I I I I I 0 0 0 rt a 0 LI f 1 1 H H 1 H1 1 _ _ t t t 1 l t t tl _ i 1 I w w I 0 r J e 0 Q wiii s s e 0 0 ll r r j _ I i i 11 1 I 1 1 1 1 g 8 N N Holding Time vs Fuel On Board Figure 5 113 0 0 ISSUED November 12 2008 REPORT VB 1993 5 77 ...

Page 284: ... 4 400 LB 179 KIAS at 5 092 LB Time During Descent 16 6 2 6 14 0 Min t __ t tT T r Li 1 EE Cf i_ I 61 1 I l t o 25 ooo f 1 _ Fr f 1 l t 1 1 i r r 120 000 _ 1 f __ 1 _t t f I r ___ r r r ___j___ r i 1 t tr J 5 0oot r 1 t J 1 t I 1 I L ____ _ c__ 10 occ oo 25 20 2 15 0 2 UJ 0 ff l 0 10 0 t UJ 2 I ___ _ ____ tl C 1 1 1 J r f l s ooo t J f i t l i J I T i t t 1 t I ___ C 5 i t t i 1 i i i t 40 Sea Lev...

Page 285: ...Used During Descent 50 1 10 7 39 4 LB tfi l i lj60 F i c l f j i J l J c pi Oot j rr2_j f I I 1 r t l ft nnn I i t I 15 000 i 1 1 i I 1 r I i i stb 1 1 ft t t 1 0 1 0 0 F I f3 Ec r f s r _ r I 1 l I 1 1 f t t t r r I I I 1 t 1 ir 1 n oool l 1 1 I 1 t 50 40 C 2 w 30 w C f2 20 u J u 1 I __ ______L___ L __t ___1 DESTlNATION J I v I _ 10 3 t l t t 3 f f t f f f L 1 I r 1 I 1 I l c __ __ y r l 1 __ __ ...

Page 286: ... Dist to Descend 8 2 NM Descent Speed 170 KIAS AT 3 800 LB 174 KIAS AT 4 400 LB 179 KIAS AT 5 092 LB Distance during Climb 60 2 8 2 52 NM t1 e so oo5R fltrJ t a F j1 t J0f7 t 1 I I d Ud t Ifflt1 i 000 0tf M t1 1 t 1 L 1 3 l 3 3 t l J lc i H E f t t 1 l l r f 1 oocil r r I H I I I I t t t l r lJ Effl 70 60 50 40 30 20 10 0 10 OUTSIDE AIR TEMP c 1 J µJ t 1 1 4 QESTINATION I 20 30 40 50 60 z 0 50 Z w...

Page 287: ...2 Min Destination Press Alt 3 500 FT Glide Time 5 92 Min Glide Endurance 36 6 30 Min 50 H 1 1 1 1 LJ tt l I Ll 4 0 z 1 I l z 30 W t z l 1 i l 1 1 I 1 I I I l 1 1 l r 2 0DO j_ I Ii r 5 092 LB 4 850 LB 4 300 LB 3 800 LB l MH i f 4 i I i I F 108 KIAS I i I 105 KIAS 0 oESTINATJON 1 100 KIAS 95 KIAS i J 20 w w 0 10 CJ 70 60 50 40 30 20 10 0 10 20 30 40 50 OUTSIDE AIR TEMP C 50 48 I 0 40 38 46 44 42 WEI...

Page 288: ... 000 WEIGHT f 5 092LB 20 000 4 300LB f 3 800LB 15 000 10 000 5 000 DESTINATION_ I 0 0 10 20 EXAMPLE Cruise Press Alt 25 000 Ft Dest Press Alt 3 500 Ft Cruise Glide Range 72 4 N M Dest Glide Range 9 8 N M Glide Range 72 4 9 8 62 6 N M GRUIS I AIRSPEED 108 KIAS 100 KIAS 95KIAS I I I I I I 30 40 50 60 70 80 GLIDE RANGE N M 90 ti trj trj l rj 0 l z l l 1 Ill Ira JIii Its t I s s ...

Page 289: ...00 LB Climb Performance 1 113FPM 7 J Lc 1 600 i l l I c r t 1 i f t 1 Y T7 1 500 4 I 1 T _ __ l ll ___ t 1 t m f t 1 i 1 0 g c 1 Fko S ve f_ 6 000 1 o cl t J 1 c 7 E lf t l f 1 i Ti i I 1 30 20 10 0 10 20 30 40 50 OUTSIDE Al R TEMP c l J r A 1 400 r 1 g a er LY 1 300 ll 1 200 IC 1 100 0 u 1 000 O 900 800 700 1 1 r 1 r11 r r 1 1 J 600 48 46 44 42 40 38 WEIGHT LBx100 1m lliffl II r u a g i 0 t R l l...

Page 290: ...__ __ 8 j f 1 1 1 r r g i ___ _l_ o i 1 l i l 1 ___ j_____ oc i I l r i ov 111 i r 1 Jfc _J p eSS p 1 1 1 1 l 1 o oo oft _ i 1 coo 1 1 1 e ooo _l___ l J6 r 4 00 j _ I 1 l I 2 t JO 1 4 j t I I o i SeaLevel i 1 c J EId 1 r T I r l f f I _ t_ t t L 1 r r I r j i r t 1 f Up__ I 1 25C0 2 o UP 3 500 FT 5KT 1 042 FT 20 10 0 10 20 30 40 OUTSIDE AIR TEMP c 50 0 1 RWY GRADIENT 2 0 10 WIND KT 2 500 2 000 _ u...

Page 291: ...a lNICN 11 0 0 0 0 0 m 0 0 m 0 0 0 IJ I 0 0 m IJ 0 N I Cl 2 1 2 w i Cl g a t t 1 t i l 0 i l l l t t t 1 w Cl 1 f t l l C o f l t 1 l O 11 J 0 I H H Landing Distance Flaps 36 without Reverse Figure 5 131 ISSUED November 12 2008 REPORT VB 1993 5 85 ...

Page 292: ...SECTIONS PERFORMANCE THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 1993 5 86 ISSUED November 12 2008 ...

Page 293: ...t J I g I O I I I I b a I I i J i 1 l _ f it 0 J l 1 l 1 i q I 1 o C T l u u I w1m I 1 I C t Il l I r 1 lt t tc l i 0 I 1 1 1 C 1 j 0 d I I I i I I 0 12 co _ d d 0 1 6 1 1H l3M ll ll l3dS 13n I Aviation Fuel Specific Weight Figure 5 145 ISSUED Novernber 12 2008 I 0 0 ct 0 REPORT VB 1993 5 87 ...

Page 294: ...3 iii z C 2 0 Q u 0 w o Oil 00 0 I u I Q l l i I L I 1 L I lt 1 1 L T I H fr h 1 T 1 SJ ON t 033dS llt 03J 8111t l Airspeed Calibration Primary Static Flaps 0 and 10 Figure 5 147 PA 46 SOOTP REPORT VB 1993 5 88 ISSUED November 12 2008 ...

Page 295: ...hl H l l i l t1 r H l H il 4 1 41 4 g i l 1 1 i 1 II Ii I I Jt P 1 1 1 1 11 I l I i l g SlON I a33dSl llll a31lllil811 10 Airspeed Calibration Primary Static Flaps 20 Gear DOWN Figure 5 149 ISSUED November 12 2008 REPORT VB 1993 5 89 ...

Page 296: ... ro 2 El ro f u a w 00 E a i5 w 0 a ill I c o 0 f J u 0 i l i I I i S lON t 033dSHllt 03 llfH81lltO Airspeed Calibration Primary Static Flaps 36 Gear DOWN Figure 5 151 I e 0 2 c CE w w Q vi C a 0 c c w I ci E 0 15 REPORT VB 1993 5 90 ISSUED November 12 2008 ...

Page 297: ... I Ill _ 1 l j I Ltf L T r i I l i 1 t 1 I I p I 1 ta I ti LI_ l I I II _ l 1 i1 l1 1At 1t t tl r r l f 0 I I I 1 I I l 1 I L ri L fi i I F t J L I LJ I l 11 1 IP ti I m rm mm r a r aH f E J1 LE 1E 1 1 m a i ll 11 l I 1 1 0 l r t r rH R II II 0 0 CD IO 0 0 l i II S ON I Q33dS llf 03 81111 Airspeed Calibration Alternate Static Flaps 0 and 10 Figure 5 153 0 0 g R g 0 IO f f e 0 z OE 0 w w 1n gi s 0 ...

Page 298: ... r I t i i r S O E I 1 I l 1 1 1 l 1 i I i i i fH 2 l I H 81 f l IH I H l l i 1 Q I II 1 i I CC i ill i Jij 1 i i J_ N 1 i f 11 1 t M I r1 1 ti i j T TT o c3 i I i 1 1 l l l i i i m C l I 1 i I I i i i S 5 l I f l i l I l i ii l j I J I I I I t I I rrl In r trr tt 1 T 1 1 1 1 II iffill1 I i FI H i t1t l 1 t t rrr t ixt 1 1 1 tt t 1 1 0 1 1 1 I r t 11T 1Yi 1 I I I I I I l I 11 I i I ti l 0 0 0 0 0 ...

Page 299: ... zW ca I ili C Zw 0 CJ C i l I D 0 C i I I I I I I I I i 11 I I 1 l I I 1 1 I I 1 i I I I W L i l J J L l l W L l l J L W L lc L J l g 0 N 0 0 0 0 a R g S LON t 033dSHll103 L lnl811110 Airspeed Calibration Alternate Static Flaps 36 Gear DOWN Figure 5 157 ISSUED November 12 2008 REPORT VB 1993 5 93 ...

Page 300: ...o w r I rf t t _o r 0 t _z 0 I I I I I Jg J lo it l 0 o o g g t i 1 i o 0 o ro r t flft o t 1 0 r r r r c J I T t Ni N l t t r i 1 0 133 1 NOll 3 l JQ 3an11111t V Altitude Calibration Primary Static Flaps 0 and 10 Figure 5 159 PA 46 SOOTP r r 0 0 0 0 0 0 0 0 0 0 0 REPORT VB 1993 5 94 ISSUED November 12 2008 ...

Page 301: ...TRIC PERFORMANCE El I I C C it J _ g _ 2 I J J ff 2 J ij c a J I 0 g J j I J J J j I I I I I J I J 0 0 0 0 0 7 f 133 1 NOl 03HHOO 3an1111V V Altitude Calibration Primary Static Flaps 20 Gear DOWN Figure 5 161 0 1 0 0 0 0 0 a ISSUED November 12 2008 REPORT VB 1993 5 95 ...

Page 302: ...l C z 0 E C C z w 0 C u z C w WO I I D w 0 in 0 C i l Li 0 II II 0 7 I I I I iii s CZ Q r t 9 r 2 J If 2 fi J cJ iS it I 0 0 7 33 NOl 3 o 3an111w v Altitude Calibration Primary Static Flaps 36 Gear DOWN Figure 5 163 N 0 N 0 0 0 0 a 0 a 0 0 i f e 0 z C 0 E w w Q 1ii II C 0 0 C ill w E u c z REPORT VB 1993 5 96 ISSUED November 12 2008 ...

Page 303: ...l 1 1 l i Jl l l l ol l l l l lCl 1 1 U Cl l a H f l l _f Jl l l l fl l 11 jf l 1 11 1 1 1 l l f l fjJH l f 11 _ _ l l l l H 1 4 1 _ l l l H4 l l ll 1 ill I I l l l cf_ _ l 1 l l l l JJ l lC I Jcl l l l f l i 5 l lle 1 1 Jl l f l l f 1 l U f l U l t l Jl l l Cl l lJ LIL l l l 0 U N 0 N I 133 l N01103 00 300111111 7 Altitude Calibration Alternate Static Flaps 0 and 10 Figure 5 165 ISSUED November 1...

Page 304: ... iU O E a z 0 i3 0 z w 0 0 u z 0 w WO I o X w ti in 0 Q iI 0 I I I 0 t J cJ iJ l l i I 0 PA 46 SOOTP l l i 1 _ rs df 1 t t V II H I 0 0 C _ 0 0 I z s 1 c E w w Q 1n 5 0 Ci w 0 _ 0 0 C E u Cm 133 1 NOl 3 00 3an111l lt V Altitude Calibration Alternate Static Flaps 20 Gear DOWN Figure 5 167 REPORT VB 1993 5 98 ISSUED November 12 2008 ...

Page 305: ...WO I w 13 iii 0 C en Cl en ii SECTION 5 METRIC PERFORMANCE II II 0 J __ J J rJ iS I I I fi 1 M l 0 r J 0 33 1 NOl 03l ll IOO 3an J 111 7 Altitude Calibration Alternate Static Flaps 36 Gear DOWN Figure 5 169 N 0 N 0 0 0 0 0 0 0 0 e 0 z I II c I C E w w n C cc 0 C i l w I I E C n ISSUED November 12 2008 REPORT VB 1993 5 99 ...

Page 306: ...SECTION 5 METRIC PERFORMANCE PA 46 SOOTP THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 1993 5 100 ISSUED November 12 2008 ...

Page 307: ...E I I i 1 1 I J l f 1 l f 1 4 l 1 lctl 1 I u i I L L J LJ L l L LL Ll LL L Jc L LL L Lll Ll LJ o 0 g g f2 g SJ ON I 033dS 11 1fJ S 03J lf llONI Angle of Bank vs Stall Speed Figure 5 173 ISSUED November 12 2008 REPORT VB 1993 5 101 ...

Page 308: ... 1 L r g 1 o L I I _ T w I I J LJ 1 l 1 9 c I I g I rT r n a w ii5 I c i I p p _ I _r U f t j 6 ii a I 1 r l T ii ro c 1 b s I L o 1 c t _ O o I W I 0 T 1 e Yi QQ w I N I 1 I I l I _ l _ _ N I I i i i l 1 t E f 71 0 1 I I 2 000 L 1 ill u I I I I I I I ii l t t 1 500 1 400 1 300 ffi 1 200 tu 1100 J 1 000 5 a 900 C z 800 700 L 1 _ _ LI I r f f 1 L r I b 1 t RB I L f L Q I _ I T _ L i _ _ tr I u Ll 1...

Page 309: ...n PTl l t l l j i H t 1 J 1 i tttti tttttttl C I i I i I I LLJ_i 30 20 10 0 10 20 30 40 50 OUTSIDE AIR TEMP C Takeoff Weight 2 196 Kg Headwind Component 1OKT Takeoff Distance 885 FT r I ID _I G c J I I 1 ll O i 111 T 11 gr i l EttfEErri N J w W C 0 i r C 1 __ 1 l i 1 1 ci 1 i 1 1 i u w 1 i tt r ro DoWn I i c 5 t r f l J _ _ 0 E 1 J L 1 1 r r r I h j 1 1 I fWrfffffi i 0 1 2 23 RWY GRAD 22 21 20 19 ...

Page 310: ...ftoff Speed I 1 11 Li j 1 Ll J i r t n 11 1 1 I I I r t I 1 I H r 1 0 _ e 1 i 1 1 t 1 f 30 20 10 0 10 20 30 40 50 OUTSIDE AIR TEMP C Ground Roll Distance t r ll L g 0 0 11 4 i t t l lJJ fil _UQ S 11 i er t_ L i 1 1 Down _ 1 8 f i l CJ Q r 4 t I 7i 1 j __ l o u i j N __ i i N m H ttlirdffiJ 1 r 1 0 1 2 23 22 21 20 19 18 RWY GRAD WT KGx100 1 _S I l r I l _ 1 r i I 1 500 1 400 1 300 ffi 1 200 ti 1 10...

Page 311: ... Nlfl SIO 1 103 11fl g _ N 0 0 0 o 0 0 N Q 2 3 0 I 1 c I L t Tl i1 ii j I I I 0 0 0 x 0 N I I I I I I I i I I I I N N I I I I I I 1 i i I I I 1 I N I I I I Maximum Effort Takeoff Performance over 50 ft Obstacle 20 Flaps Figure 5 181 ISSUED November 12 2008 REPORT VB 1993 5 105 ...

Page 312: ...t 1 4 _ t f 1 l g s j t li i 5 00 ea Leve1 t i t f _ 10 oo 1 1 H q f l t i f b l l l __ _ _ ___ _ 1s 001 0 L J J t t _ _ 1 500 u 1 t i O QO J I 1 t i l L l 1 i 1 3 E f 1 I 11 _ v U t1 o T r N i1 f i l i o f j t L l J r R k f s f _______ t 1 1 r J r1 f 1 fC4 cl J f f sf Y C J 30n i 6 0 1 _____ ___ 1 i V0 J J 1 vu I r 1 1 I pres t t 1 rrr I I l I I 1 s JJt j rJT I 1 11 I I l I l 1 j I I l r 1 t c t ...

Page 313: ...ar RETRACTED Climb Speed 125 KIAS i I I I I I H 30 40 50 EXAMPLE I OAT 7 C Pressure Altitude 12 000 FT Aircraft Weight 2 177 KG Climb Performance 572 FT NM 1 500 1 r iE 1 000 i t f i l 1 1 i 1 e b tt rr I I I I I I I I 11 O 23 22 21 20 19 18 WEIGHT KGx100 z UJ i5 ffi al iE Iii mr 1 u i i t i I t i 0 I z I 0 s t i z l el t i ...

Page 314: ...1 1 1 r 1 l ____ J ___ g I J l l 1 1 r I L n i H t t f 1ZC i dl J_lf f t l t t t2t t C I t i 1 i J r r t fi J 1 _ _ j 0 L r f 1 T t I j _ I r I I tr l __ _ 2 00o _Sea Leve 4 0oo 1 _ r 6 000_ 1 i l i 1 800 1 600 lE C 1 400 Ill lE i 1 200 0 t 1 000 ii oon _ i ____J_L l t ____ y e V r 1 t di 1 I o l 800 10oooF I Lr I 1 t ress A It I 11 II_ __ r HI I 1 t 1 I 30 20 10 0 10 20 30 OUTSIDE AIR TEMP C 40 5...

Page 315: ...i 2 i i t I I 111 S Qi ll H _LL i J I X 3 a i i I I I I i 111 J J 1 sss 1 E s s ai1c a11 all a e a 1 g 8 L 60 lJ aun e u u iJa J oa o II l I ll j I rr r t t 1 1 1 1 H H H f ff Hi _ 0 Pp 1 I I I i I I I I I 1 1 i I i I I r 0 i i 1 1 i i I 1 1 rt r1 T 1 g u IJ i ll II I l I oci I f L 1 J Nin i C il11 J fro o O Z J w rn t 1 t f l I I kl 1 l 1 z S w I I I I I Jr I I o g 1 1 i 1 J I J t 1 r 1 o s U fl ...

Page 316: ... Lf tt ti l ttttiJ t tt ti1i t lt t1 i 1tj fJ1 l I l t Ht 1 1 JJtiLptiW ll l rHc J l rrclNrillQ H t µ 1 4 1 i µ11 µ11Jµ 1 41 IH I H i jl 0 J 11 I r u I I I 1 1 1 I ii 1 II I w I I I 1 11 1 i O 1 N 1 1 111 I uI I I i I I O t H t H i i I l i I I i I II 111 5 I t I i 1 f i r1 11 nlrn1 v j fI 1 1 g I 1 1 11 I I 1 1 i 1 I f _ J I 1 l j 1 l I 1 l rt ll 1i I 11 t1 VJ1itl t i I I l Ki i II iI l t 11 Ii ll...

Page 317: ...KG Fuel Used During Climb 69 22 47 KG 110 L t I __J i I Ti r i 1 l 1 _ _ 1 i Fuel to start 1 S I aod axi t 7 S y i T takeoffiocluded 000 r l O lf i T 90 cl t L I _ oo C I r 1 1 1 T r __ CRU1s E I 0 000 _ _ 1 70 J _j 1 1 I t i 1 60 j 100 l 50 m iE u g J UJ 40 15 0UU 6 1 __ Ll I I _ i_ s t t 1 _ __ o 1 10 00 I I 1 o c i 1 I I r 1 i t 5 000 30 ___l___ 1 1 i k l 1 l 1 l 1 1 20 1 i I 1 i l r DEPARTURE_...

Page 318: ...T Cruise Press Alt 25 000 FT Gear RETRACTED Dist to Departure Alt 1 3NM Dist to Cruise Alt 54 NM Climb Speed 125 KIAS Distance during Climb 54 1 3 52 7 NM 140 1 f 1 1 j r _j_ f l 120 I I I 1 1 J J 1 l j m i t I l_f 11 I I I I r t t 1 l i 1 J r l 1 1 f t t f t _ i p 1T1 t 100 z Ill 80 0 t 60 UJ z 40 i5 1 I I 10 000 20 1 l l 1 t sEA LEVEL 1 g 0 70 60 50 40 30 20 10 0 10 20 30 40 50 OUTSIDE AIR TEMP ...

Page 319: ...140 KIAS to 20 000 FT 125 KIAS to 30 000 FT Time To Departure Alt 1 3 Min Time To Cruise Alt 23 3 Min Time During Climb 23 3 1 3 22 Min 1 1 11 1 1 1 1 1 1 1 l t _ t L 1 J _ _ _ J _ 0 ___ j__ R a f f I t 0 1 _ _ _ _ _ _ t tz c 1 i r oOO r r CRL1 t 1 i tj 1 r1 f ff f t l j EI 10 ooo H Z 1 oOo 50 45 40 35 z E 30 m 25 0 20 UJ 15 10 5 1 t ealt t DE ARilJR a 1 t t 0 70 60 50 40 30 20 10 0 10 20 30 40 50...

Page 320: ...23 KG Fuel To Cruise Alt 78 KG Fuel Used During Climb 78 23 55 KG 125 KIAS TO 30 000 FT r 1 F i _ r t 1 1 1 Fuel to start taxi and takeoff included 120 110 _____ J Jggj 3 e _ r c cc J 3 c _ r i I 70 _ 1 _ flii 5 ocr r 1 1 1 i 1 1 1 c I 1 1 100 90 le __ I 20 000 1 i 1 t ooo 70 f 1 r 60 1 1 i 60 i c 1 l _ __ i 1 1 i l j C a r i Bm 40 _ c l c 1 t r 1 50 1 wi ea Level i 1 r 13e _ 3 _ ET 50 40 30 20 10...

Page 321: ... FT Cruise Press Alt 25 000 FT Dist to Departure Alt 1 8 NM Dist to Cruise AH 67 5 NM Distance during Climb 67 5 1 8 65 7 NM 160 1 I J 1 J 1 1 J F I l t t t s i 1 J t 140 120 2 z Ill _ 2 l f Cf 00 _ O uv _J I i f I 1 0 cf _ sl oi __ oo I o I 1 f 20 000 le c I 1 1 1 1 1 J I f s Vo 1 LIJ 1Voc j i L 60 15 oo s tz L I 1 f L I _ r i 4 f 1 10 000 O C i 1 r s ooo _ 20 a f J I SEA LEVEL k l l 1 DEPARTURE ...

Page 322: ... 132 9 205 1153 126 8 222 1255 127 5 241 1313 1y ji7 9 257 111 Z 10T3 255 ISA 10 QC Torque Fuel Flow TAS FT LB Kg Hr KT 956 160 1 180 1014 146 1 194 1088 134 7 209 1177 129 3 226 1285 129 7 246 1298 126 1 260 1077 104 3 256 ISA C Torque Fuel Flow TAS FT LB Kg Hr KT 969 161 0 183 1030 147 4 197 1106 136 5 213 1201 131 5 231 1313 132 0 251 1250 122 0 260 1040 100 7 255 NOTE Shaded areas are beyond a...

Page 323: ...955 ISA 35 DC Torque FT LB J Ofil 1088 1177 1285 1201 1071 890 SECTION 5 METRIC PERFORMANCE Fuel Flow TAS Kg Hr KT 163 3 186 149 7 201 138 3 217 133 8 235 132 4 254 117 9 259 97 1 254 Fuel Flow TAS Kg Hr KT 164 7 189 151 5 204 140 6 221 135 6 240 132 4 257 113 4 258 93 9 253 Fuel Flow TAS Kg Hr KT 16 6 ll _ 1 94 1 53 8 209 143 8 227 139 3 246 124 3 253 107 5 255 88 5 250 NOTE Shaded areas are beyo...

Page 324: ... Flow TAS FT LB Kg Hr KT 132 2 129 114 2 138 96 8 147 500 83 8 155 72 8 164 6 4 8 171 58 4 178 ISA 10 C Torque Fuel Flow TAS FT LB Kg Hr KT 132 4 131 114 5 140 97 0 149 500 83 8 157 73 0 166 64 8 173 58 6 180 ISA C Torque Fuel Flow TAS FT LB Kg Hr KT 132 6 133 114 8 142 97 3 151 500 83 9 159 73 3 167 64 9 175 58 7 182 NOTE Shaded areas are beyond aircraft OAT limit See paragraph 2 28 ECS NORMAL RE...

Page 325: ...Hr KT 0 35 133 1 137 5000 25 115 4 146 10000 15 97 9 155 15000 5 500 84 3 163 20000 5 73 5 171 25000 15 65 1 178 30000 24 59 1 184 ISA 35 C Altitude OAT Torque Fuel Flow TAS FT C FT LB Kg Hr KT O _ 50 P 1 133 fr 14 1 5000 40 115 7 149 10000 30 98 4 157 15000 20 500 84 7 165 20000 10 74 2 173 25000 0 65 7 180 30000 9 59 4 185 NOTE Shaded areas are beyond aircraft OAT limit See paragraph 2 28 ECS NO...

Page 326: ...5 139 0 146 5000 5 120 2 155 10000 15 102 9 164 15000 25 600 89 7 173 20000 35 79 5 182 25000 45 71 3 191 30000 54 65 6 199 ISA QC Altitude OAT Torque Fuel Flow TAS FT 1Qc FT LB Kg Hr KT 0 15 139 4 148 5000 5 120 6 157 10000 5 103 0 166 15000 15 600 90 1 175 20000 25 79 6 184 25000 35 71 5 193 30000 44 65 6 202 NOTE Shaded areas are beyond aircraft OAT limit See paragraph 2 28 ECS NORMAL Intermedi...

Page 327: ...600 20000 10 25000 0 30000 9 SECTION 5 METRIC PERFORMANCE Fuel Flow TAS Kg Hr KT 139 7 150 121 0 159 103 2 168 90 4 177 79 8 186 71 7 195 65 8 204 Fuel Flow TAS Kg Hr KT 139 9 152 121 4 161 103 6 170 90 7 179 80 1 188 71 9 197 66 0 205 Fuel Flow TAS Kg Hr KT 140 r 1 122 0 164 104 3 173 91 2 182 80 6 191 72 3 200 66 3 208 NOTE Shaded areas are beyond aircraft OAT limit See paragraph 2 28 ECS NORMAL...

Page 328: ... Kg Hr KT 0 5 144 9 158 5000 5 125 9 167 10000 15 109 1 176 15000 25 700 96 0 185 20000 35 86 0 195 25000 45 78 1 205 30000 54 73 0 215 ISA QC Altitude OAT Torque Fuel Flow TAS FT QC FT LB Kg Hr KT 0 15 145 3 160 5000 5 126 2 169 10000 5 109 5 178 15000 15 700 96 3 187 20000 25 86 3 197 25000 35 78 1 207 30000 44 73 1 217 NOTE Shaded areas are beyond aircraft OAT limit See paragraph 2 28 ECS NORMA...

Page 329: ...000 0 30000 9 SECTION 5 METRIC PERFORMANCE Fuel Flow TAS Kg Hr KT 145 8 162 126 5 171 109 9 180 96 6 190 86 6 199 78 4 210 73 3 220 Fuel Flow TAS Kg Hr KT 146 3 164 127 1 173 110 3 182 97 0 192 86 8 202 78 7 212 73 5 222 Fuel Flow TAS Kg Hr KTl 147 0 167 128 0 176 110 9 185 97 7 195 87 2 205 79 2 215 73 8 225 NOTE Shaded areas are beyond aircraft OAT limit See paragraph 2 28 ECS NORMAL Intermediat...

Page 330: ... KT 0 5 150 4 168 5000 5 132 3 177 10000 15 115 4 186 15000 25 800 102 6 196 20000 35 92 7 206 25000 45 85 5 217 30000 54 80 8 228 ISA C Altitude OAT Torque Fuel Flow TAS FT oc FT LB Kg Hr KT 0 15 150 8 170 5000 5 132 7 179 10000 5 115 8 188 15000 15 800 103 0 198 20000 25 92 9 209 25000 35 85 7 219 30000 44 80 8 230 NOTE Shaded areas are beyond aircraft OAT hm1t See paragraph 2 28 ECS NORMAL Inte...

Page 331: ...74 5000 25 133 7 183 10000 15 116 7 193 15000 5 800 103 6 203 20000 5 93 6 213 25000 15 86 1 224 30000 24 81 0 235 ISA 35 QC Altitude OAT Torque Fuel Flow TAS FT QC FT LB Kg Hr KT o 50 153 I 177 5000 40 134 4 186 10000 30 117 5 196 15000 20 800 104 2 206 20000 10 94 2 217 25000 0 86 5 228 30000 9 81 2 239 NOTE Shaded areas are beyond aircraft OAT limit See paragraph 2 28 ECS NORMAL Intermediate Cr...

Page 332: ... Ka Hr KT 156 0 174 138 3 183 121 5 193 900 109 1 203 99 6 213 r J Q2 Qti 8Q T 224 F 236 ISA 10 C Torque Fuel Flow TAS FT LB Kg Hr KT 156 4 176 138 8 185 121 8 195 900 109 4 205 99 6 216 93 1 227 89 1 239 ISA C Torque Fuel Flow TAS FT LB Kg Hr KT 157 0 178 139 3 188 122 3 198 900 109 7 208 99 9 219 93 3 230 89 0 242 NOTE Shaded areas are beyond aircraft OAT limit See paragraph 2 28 ECS NORMAL Inte...

Page 333: ...r KT 157 7 180 139 8 190 122 7 200 110 0 210 100 3 221 93 5 233 89 1 245 Fuel Flow TAS Ksi Hr KT 158 3 182 140 3 192 123 3 202 110 4 213 100 7 224 93 8 235 89 1 247 Fuel Flow TAS KQ Hr KT J 50I J59A 18 5 1 5000 40 141 3 195 10000 30 124 2 205 15000 20 900 111 1 216 20000 10 101 2 227 25000 0 94 1 239 30000 89 2 251 NOTE Shaded areas are beyond aircraft OAT limit See paragraph 2 28 ECS NORMAL Inter...

Page 334: ...Ka Hr KT 144 6 191 128 4 201 1000 115 8 211 107 1 222 I I Ifft 233 J _ 1 2 i1W ISA 10 C Torque Fuel Flow TAS FT LB Kg Hr KT 163 2 184 145 1 193 128 8 203 1000 116 1 214 107 4 225 100 9 237 97 3 249 ISA C Torque Fuel Flow TAS FT LB Kg Hr KT 163 8 186 145 7 196 129 2 206 1000 116 4 216 107 7 228 101 0 240 97 2 252 NOTE Shaded areas are beyond aircraft OAT limit See paragraph 2 28 ECS NORMAL Intermed...

Page 335: ... FT LB 10 1000 SECTION 5 METRIC PERFORMANCE Fuel Flow TAS Kg Hr KT 164 3 188 146 4 198 129 7 208 116 9 219 107 8 230 101 2 242 97 3 255 Fuel Flow TAS Ka Hr KT 165 0 190 147 1 200 130 1 210 117 5 221 108 2 233 101 3 245 96 0 258 Fuel Flow TAS Kg Hr KT 16 9 19 l_ 148 1 203 130 8 214 118 2 225 108 6 237 101 7 249 90 2 262 NOTE Shaded areas are beyond aircraft OAT limit See paragraph 2 28 ECS NORMAL I...

Page 336: ...LB Kg Hr KT 0 5 5000 5 10000 15 135 7 211 15000 25 1100 123 1 221 20000 35 115 2 233 25000 45 109 3 245 30000 54 106 3 258 ISA C Altitude OAT Torque Fuel Flow TAS FT roe IFT LB Kg Hr KT 0 15 5000 5 10000 5 136 1 213 15000 15 1100 123 6 224 20000 25 115 4 236 25000 35 109 3 248 30000 44 103 8 261 NOTE Shaded areas are beyond aircraft OAT l1m1t See paragraph 2 28 ECS NORMAL Intermediate Cruise Power...

Page 337: ...0 10000 30 15000 20 1100 20000 10 25000 0 30000 9 SECTION 5 METRIC PERFORMANCE Fuel Flow TAS K11 Hrl KT 136 5 216 124 1 227 115 7 239 109 2 251 100 0 264 Fuel Flow TAS Kg Hrl KT 153 7 207 137 1 218 124 6 229 115 9 241 109 3 254 Fuel Flow TAS Kg Hr KT 1 154 8 211 138 0 222 125 3 233 116 3 245 107 9 258 NOTE Shaded areas are beyond aircraft OAT l1m1t See paragraph 2 28 ECS NORMAL Intermediate Cruise...

Page 338: ... 35 30000 44 ISA 20 QC Torque Fuel Flow TAS FT LB Kq Hr KT 1200 122 7 237 11J fC 50 ISA 10 QC Torque Fuel Flow TAS FT LB Kg Hr KT 1200 131 0 229 122 9 240 117 5 253 108 2 266 ISA QC Torque Fuel Flow TAS FT LB Kg Hr KT 1200 131 3 231 123 1 243 117 6 256 NOTE Shaded areas are beyond aircraft OAT hm t See paragraph 2 28 ECS NORMAL Intermediate Cruise Power 1200 FT LB ISA ISA 10 ISA 20 REPORT VB 1993 ...

Page 339: ...e FT LB 1200 ISA 20 C Torque FT LB 1200 ISA 35 C Torque FT LB SECTION 5 METRIC PERFORMANCE Fuel Flow TAS Ka Hr KT 131 6 234 123 3 246 117 7 259 Fuel Flow TAS Kq Hr KT 132 0 237 123 5 249 115 3 262 Fuel Flow TAS Kg Hr KT 1 _ c 145 4 229 1200 132 5 241 123 9 253 108 1 267 NOTE Shaded areas are beyond aircraft OAT l1m1t See paragraph 2 28 ECS NORMAL Intermediate Cruise Power 1200 FT LB ISA 10 ISA 20 ...

Page 340: ...5 213 5 215 3 25000 231 3 234 5 237 2 239 5 241 9 30000 252 2 255 8 259 2 262 1 268 7 LOW POWER CRUISE 500 FT LB Altitude Cruise Nautical Miles 100 Ka Fuel FT SA 20 C ISA 10 C ISA ISA 10 C lSA 20 C 0 97 6 99 1 100 6 102 2 103 3 5000 121 1 122 6 124 1 125 3 126 6 10000 151 8 153 6 155 2 156 6 158 0 15000 185 5 187 7 189 9 191 9 193 4 20000 224 5 226 6 228 3 229 9 232 4 25000 264 4 267 3 269 7 271 4...

Page 341: ...IC PERFORMANCE I I I I I 1 1 I 1 h l t I I I i _ l 1 i l 4 1 44 1 4 4 i c w 1 _ I I lI j_ _L I i I C l l l 4 j 4 l 1 _ lH I 1 r l l ll 0 I 0 0 co 0 Holding Time vs Fuel On Board Figure 5 247 0 C 0 E j 0 0 0 ISSUED November 12 2008 REPORT VB 1993 5 135 ...

Page 342: ...at 2309 7 KG Time During Descent 16 6 2 6 14 0 Min 1 25 I Ill__ _ I l 1 t t l I l 1 I l 1 r 1 I t t I I ___ I___ l l l 1 r I Fl o 30 ooo FT PRESS ALT i I I 1 Kl i t 1 i I o 25 000 1 _ 1 as _ C UISE _ i 1 I C I r f i l l I i 0 000 1 1 c i j f 1 FFISiJ YJ f i 1 1_ _j__ _ ____ __j _ i t_ j o o 3 j 1 r f rs t 1 1 j I I I I ___J____ _ ____ _s o o_ 1 I I I 20 z 15 C z UJ 0 10 0 1 UJ i 5 t 1 i foE 1 STl ...

Page 343: ...tination OAT 25 c Cruise Press Alt 25 000 FT Destination Press Alt 3 500 FT Fuel To Descend 22 7 KG Fuel To Descend 4 8 KG Fuel Used During Descent 22 7 4 8 17 9 KG i f r i 1 1f i F tJ1 ft l t 30 ooo Fr PRESS ALT s i 1 cRUISE t 30 25 13 bi 1 c t 1 1 _ l i l F fJ Effi5 l _ 1 t S J L _ I___ Sea Levei 0 50 70 60 50 40 30 20 10 0 10 20 30 40 OUTSIDE AIR TEMP c 11 E ffilll ltll u J a g i J 0 i t 1 J i ...

Page 344: ...scend 60 2 NM Dist to Descend 8 2 NM Distance during Climb 60 2 8 2 52 NM t t t 30 000 FT PRESS ALT 80 1 r J 70 i _i CRUISEJ _J 60 2 1 _ C 50 2 UJ t Cl f r f f pf 1d El t 1 1 l P t l l t 1 _ F i 1 1 1 i 40 f F F r i s 000 t l E 1 s r 1 1 t Ff i l N f l fsJ I 1 l t s r _ r Jr 1 I l 1 1 i 1 f l ___ j _10 00 _ t Is I 70 _ _ 1 r X s ocio l t 1 1 1 1 r l t I 60 50 40 30 l X t c K c 1 r SEI LEVEL j 20 1...

Page 345: ... C I r 1 I r i f JJ I I l L l 1 f 1 1 J 1 x CRUISE 4 ooo _u16 1 1 l t 1 _ j 1 t b2ci a _ __ 1 1 1 CJ 16 ooo f 1 g 1 1 1 1 I I _12 000 t ___ t g l __ ct WEIGHT AIRSPEED a oo Tl 11 t tJ t t t 1 j 2309 7 KG 108 KIAS _ t I 2199 9 KG 105 KIAS i c1 1 i 1 4 ooo j i er DESTIN TION i t 1950A KG 100 KIAS J r 1 _ lf l l l t i tr t1i t 1 50 40 z 30 w l 1 0 20 1 w w 0 10 9 1723 6 KG 95 KIAS I t J LLJ 1 1 _ 1 I...

Page 346: ...ide Range 72 4 9 8 62 6 N M I 3 500 Ft 9 SN M l 1 ___J_____ __ I I i __ _______ _ r __1I lcRu 1 t 1 1 L I l 25 000 m20 000 r 1 r 1 f t 1 F 3 tT I _i 1 J___ WEIGHT AIRSPEED 1 r i _ 1 1 2309 7 KG 108 KIAS w Q 1950 4 KG 100 KIAS 1723 6 KG 95 KIAS 15 000 ijij I I i lff 1 1 I I l L 1 1Q QQQ 2 1 t 1 I ffl It k I I I 8 r 1 r _ 1 5 000 DESTINATION 11 i l 1 j i 1 t 1 r r 1 f 0 a 10 20 30 40 50 60 GLIDE RAN...

Page 347: ... KG 1 113 FPM __ 1 J i 1 600 1 F J g z t l rl J 1 500 1 t 1 400 Cl 4 r r 1 300 2 Y J t 1 J ti EE E3 v1 _ 1 1 r T 19 __ _ i c1 1 l j 1 r t rur 0 g 1 LL t 1200 v a i ll J L 7 2 i 1 100 J 2 ooo Sea L 00 0 er i ooo 1 0 t i 10 Q7 rrt 001F SS Af _L___t_ r c t_ 1 _ _ l i l I f 1 E f i i l f I U I s 10000 I l J cV H l 1 f 1 t 1 i 1 i 900 i 800 1 l 1 700 I 600 30 20 10 0 10 20 30 40 50 22 21 20 19 18 OUTSI...

Page 348: ...E WITH BETA Landing Ground Roll lti f Hf1 1 t l l I i e 1 100 I C O I ID rr 1 i t J r I l t 1 1 1 1 l l 1 t r ti J t l 1 4 rr g _ S r 1 t _ i 91 n _ ur l 600 0 1 1 I I I I I i r t t J i i i l r l I r 1 l__ 500 v 1 0ooof i _ 5 ooo 1 Qoo l 1 r A ooo _ Eer r 400 sea l e le1 l I 1300 V __ __j I _j ___ j OOWN 200 20 10 0 10 20 30 40 500 1 20 10 WIND KT 20 OUTSIDE AIR TEMP C RWY GRADIENT 111 IJ i5 g 0 z...

Page 349: ...80 H OS l l3AO LSIO NION 11 rlj III 1 e i l r r 1 r lll 1 1 11 1 I l_o r 1J J N H 1 11rJ_ I111 I I I 8 I I 1 I_ 11 1 ii i 1 i II j I i 11 1 j I 1 Landing Distance Flaps 36 without Reverse Figure 5 265 ISSUED November 12 2008 REPORT VB 1993 5 143 ...

Page 350: ...SECTIONS METRIC PERFORMANCE THIS PAGE INTENTIONALLY LEFT BLANK REPORT VB 1993 5 144 ISSUED November 12 2008 ...

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Meridian PA-46-500TP, Pilot Operating Handbook

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