CRUISE PERFORMANCE – 2,500’2500 lbs, lean best power, 45 min (0.8 hrs) reserve

PRESS ALT RPM MP 10

49 Gal(45min resv.)

% BHP KTAS GPH Hours NM

2500 2500

24 79 121 10.6 3.8 46323 74 118 10.0 4.1 48422 70 115 9.3 4.5 51421 66 111 8.7 4.8 536

2400

24 77 119 10.3 4.0 47123 73 116 9.7 4.3 49322 68 113 9.1 4.6 51821 64 110 8.5 5.0 546

2300

24 75 119 10.0 4.1 48823 71 115 9.4 4.4 50722 66 111 8.8 4.8 52921 62 108 8.2 5.2 559

2200

24 72 116 9.6 4.3 49923 68 113 9.0 4.6 52522 64 110 8.4 5.0 55421 60 105 7.9 5.4 567

2100

24 69 114 9.1 4.6 52323 65 110 8.6 4.9 53922 61 107 8.1 5.2 56221 57 103 7.6 5.6 58220 53 98 7.2 6.0 58919 50 92 6.7 6.5 599

CRUISE PERFORMANCE – 5,000’

2500 lbs, lean best power, 45 min (0.8 hrs) reserve

PRESS ALT RPM MP 5

49 Gal(45min resv.)

% BHP KTAS GPH Hours NM

5000 2500

24 82 125 11.1 3.6 45223 77 123 10.4 3.9 48122 73 119 9.7 4.3 50621 68 116 9.0 4.6 539

2400

24 79 123 10.7 3.8 46523 75 121 10.1 4.1 49022 71 117 9.4 4.4 51621 67 114 8.8 4.8 544

2300

24 77 123 10.4 3.9 48123 73 119 9.7 4.3 50622 69 116 9.1 4.6 53221 65 112 8.5 5.0 556

2200

24 74 120 10.0 4.1 49223 70 117 9.4 4.4 51622 66 114 8.8 4.8 54421 62 110 8.2 5.2 569

2100

24 71 118 9.5 4.4 51423 68 115 8.9 4.7 54122 64 111 8.4 5.0 55921 60 107 7.9 5.4 57820 56 103 7.4 5.8 60019 52 96 7.0 6.2 595

CRUISE PERFORMANCE – 7,500’2500 lbs, lean best power, 45 min (0.8 hrs) reserve

PRESS ALT RPM MP

49 Gal(45min resv.)

% BHP KTAS GPH Hours NM

7500

2500

22 75 123 10.1 4.1 49821 71 120 9.4 4.4 53020 66 116 8.7 4.8 56119 61 110 8.1 5.2 577

2400

22 73 122 9.8 4.2 51221 69 118 9.2 4.5 53420 65 114 8.6 4.9 55819 61 109 8.0 5.3 580

2300

22 71 120 9.5 4.4 52321 67 116 8.9 4.7 54620 63 112 8.3 5.1 57219 59 107 7.8 5.5 587

2200

22 69 118 9.1 4.6 54121 65 114 8.5 5.0 56620 61 109 8.0 5.3 58019 56 104 7.5 5.7 596

2100

22 66 116 8.7 4.8 56121 62 111 8.2 5.2 57420 58 106 7.7 5.6 59019 54 101 7.2 6.0 60718 50 94 6.8 6.4 602

CRUISE PERFORMANCE 10,000’ & 12,500’2500 lbs, lean best power, 45 min (0.8 hrs) reserve

PRESS RPM MP -5 49 Gal (45 min)

ALT % BHP KTAS GPH Hours NM

10,000

2500

20 68 120 9.0 4.6 55719 64 115 8.4 5.0 57918 59 109 7.8 5.5 59817 54 102 7.3 5.9 603

2400

20 67 118 8.9 4.7 55519 63 114 8.3 5.1 58218 59 109 7.7 5.6 60617 54 101 7.2 6.0 607

2300

20 65 116 8.6 4.9 56819 61 111 8.0 5.3 59118 57 105 7.5 5.7 60217 52 97 7.0 6.2 601

220020 63 114 8.3 5.1 58219 59 109 7.8 5.5 59818 55 102 7.3 5.9 603

210020 61 110 8.0 5.3 58619 56 105 7.5 5.7 60218 52 98 7.0 6.2 608

PRESS ALT RPM MP 49 Gal (45min)

% BHP KTAS GPH Hours NM

12,5002500

18 61 113 8.1 5.2 59317 57 105 7.5 5.7 60216 52 96 7.0 6.2 595

240018 61 113 8.0 5.3 60217 56 105 7.5 5.7 60216 52 95 7.0 6.2 589

2300 18 59 109 7.8 5.5 59817 54 102 7.3 5.9 603

2200 18 57 106 7.5 5.7 60817 53 96 7.1 6.1 586

2100 18 55 102 7.3 5.9 60317 50 91 6.8 6.4 583

SHORT FIELD TAKE-OFF DATA Hard dry surface, cowl flaps open, 15° flaps, full power, climb speed 70 MPH

GROSS WEIGH

T

PRES

ALT

HEAD WINDTEMP °C0 KTS 10 KTS 20 KTS

GRN ROL

L

CLEAR 50' OBST

GRN ROL

L

CLEAR 50' OBST

GRN ROL

L

CLEAR 50' OBST

2500

SL 750 1400 525 1060 335 760 152500 900 1675 635 1280 415 935 105000 1090 2050 780 1585 520 1175 57500 1335 2640 970 2070 660 1565 0

2200

SL 555 1085 380 810 230 565 152500 665 1265 460 950 290 675 105000 800 1500 560 1140 360 820 57500 975 1835 685 1410 455 1035 0

1900

SL 400 840 260 615 150 420 152500 475 955 315 710 190 490 105000 570 1105 385 825 235 580 57500 690 1310 475 985 300 700 0

1. Increase distance by 10% for each 10° C above standard.2. For operation on a dry, grass runway, increase distances (both "ground roll" and

"total to clear 50 ft. obstacle") by 7% of the "total to clear 50 ft. obstacle" figure.

MAXIMUM RATE OF CLIMBFull throttle, 2700 RPM, cowl flaps open, flaps up, leaned above 3000'

GROSS WEIGHT

PRES ALT

TEMP C

CLIMB SPEED

MPH

RATE OF

CLIMB

FUEL from SL

2500SL 15 92 840 1.5

5000 5 88 585 3.410 000 -5 83 330 5.615 000 -15 79 80 10.4

2200SL 15 89 1020 1.5

5000 5 84 735 3.010 000 -5 80 450 4.815 000 -15 76 165 7.7

1900SL 15 86 1205 1.5

5000 5 81 890 2.810 000 -5 77 575 4.215 000 -15 73 260 6.3

1. Decrease rate of climb 30 ft/min for each 5° C above standard

LANDING DISTANCEHard dry surface, 30° flaps, power off, approach speed 72 MPH

GROSS WEIGHT

PRES ALT

GRND ROLL

CLEAR 50’

TEMP °C

OBST

2500

SL 600 1220 152500 635 1290 105000 675 1370 57500 715 1450 0

1. Reduce landing distance 10% for each 4 knots of headwind.2. For operation on a dry, grass runway, increase distances (both "ground roll" and

"total to clear 50 ft. obstacle") by 20% of the "total to clear 50 ft. obstacle" figure.

AIRSPEED LIMITATIONS

Climb Speeds Flaps (Vfe)Vx flaps Up 77 MPH 0° - 10° 130 MPHVx flaps 15° 69 MPH 10° - 30° 105 MPH

Vy 92 MPHCruise Climb 100 MPH

Best Glide Stall SpeedsFlaps up 85 MPH Vs 63 MPH

Vso 53 MPH

Manoeuvring (Va)2500 lbs 117 MPH2200 lbs 110 MPH

JPI EDM 700 ENGINE MONITOR

DisplayP (%) view: displays EGT as a percent of redline. Full height is 100%, 1 segment only is 50% of redline.

Use during: 1. Power changes2. Decent

 N (normalize) view: displays EGT normalized with all column peaks are set to same half level height. Any changes are shown as increase/decrease of column height. Each segment = 10°F change. Use during:

1. Runup (fouled plug will be higher temp)2. Cruise Flight

 Hold LF button 5 seconds to toggle between views. CHT is displayed by missing segment, in 25°F increments starting at 300°F ModesAutomatic (default 2 min after start up): Each cylinder and each parameter value is automatically sequenced and shown in the digital display for a few seconds. Press LF then STEP to change to Automatic mode Manual (default at start up): Tap STEP button to enter manual mode. Each parameter is displayed until you manually STEP to the next parameter (press STEP button). If no button is depressed for 15 minutes, the Automatic Mode will resume. Tap LF button to record data in memory (SNAP will display)

…/2

JPI EDM 700 ENGINE MONITOR (cont.)

Lean Find

Establish cruise @ ~ 65-75% power In Manual Mode, lean until any cylinder reaches peak & then enrich ~

50°F Wait 1 minute Tap LF button. Confirm display indicates LEAN R. If shows LEAN L hold STEP & LF buttons simultaneously for 5

seconds to change unit to LEAN R Continue leaning at ~ 10°F/second (¼ turn of vernier/sec). Flashing DOT indicates hottest cylinder & that unit is in Lean Find

mode. Stop leaning when a column begin flashing & display flashes

LEANEST for 2 seconds (not necessarily the hottest cylinder). Hold LF button to display PEAK EGT. Due to thermal inertia this will

typically be -15°F lean of peak. Slowly enrich mixture, EGTs will continue to rise, to:

 Peak EGT for best economy100°F rich of peak for best power

 Hold LF button after peak EGT is found to display peak EGT AlarmsTap STEP button to terminate alarm for 10 minutesHold STEP button to terminate alarm for remainder of flight EGT in Cruise 1350°F & should drop 200°F with full throttle.

EGT span (DIF) 120 to 150°F

CHT 350°F (OAT 60°F)

CHT span 50 to 70°F

Shock cooling CHT drop of 40°/minute or more

S-Tec 40 AUTO PILOT

NAV Modes: APR, NAV & REV

ROLL Modes: HDG & STB On/Off button puts unit into STB mode: command roll left or right using Turn KnobPre Flight

Turn A/P master switch to Test position: all lights & annunciators should illuminate.

When TC is up to speed, set A/P master switch to On: Green Ready light should remain lit.

Press On/Off switch to place unit in STB mode. Command roll left and right using Turn Knob & observe control wheel movement.

Set DG bug to current heading and press HDG mode button. Confirm HDG is illuminated. Move DG bug left & right of heading and observe control wheel movement.

Using control wheel, gently override roll servo to both left and right.

Tune nav radio to VOR, press NAV mode button. Adjust OBS to deflect CDI and observe control wheel following.

Repeat in APR and REV modes. Confirm REV mode reverse sensing.

Disengage A/P using control wheel AP disconnect switch. Turn AP OFF using Master AP switch

In Flight Turn AP master switch ON. Confirm RDY light illuminates. Trim A/C in both yaw & pitch. Centre Turn Knob & press On/Off switch. Confirm STB mode

light illuminates. Set heading bug on DG & press Turn Knob to engage.

Confirm HDG mode light illuminates. Must be within a needle width and 10° of heading to

engage NAV, APR or REV modes. Use APR mode when tracking GPS is when cross country.

…/2

S-Tec 40 AUTO PILOT (cont.)

Emergency Procedures

In the event of an un-commanded autopilot control input1. Override autopilot with firm use of the aircraft control

column and disengage autopilot using the control wheel AP disconnect switch.

2. Switch the A/P master switch off.3. Do not use auto pilot until it has been repaired.

Monroy Traffic-Watch ADT-300

The ATD-300 is a PASSIVE receiver capable of detecting transponder replies from nearby aircraft. It WILL NOT detect

aircraft that do not have an operating transponder or when not being interrogated by Secondary Surveillance Radar. Ground CheckSet to NEAR or FAR & turn on (BRT or DIM)May be set To MUTE while taxing but ensure is set to NEAR or FAR prior to moving onto departure runway. Normal setting is FAR in order to offer the earliest possible detection though may be set to NEAR when operating in the vicinity of a busy airport.  ModesNear Within 1NM & 500': "TRAFFIC NEARBY"Far Within 3 NM & 1000': "TRAFFIC"

Within 1 NM & 1000': "TRAFFIC NEARBY"Mute No audio alerting & displays traffic in MSL vs. relative

altitude. 

 

If traffic has no Mode C, will display range only:

STRIKE FINDER

Pre Flight: On power up, 3 sunburst patterns followed by Test Status

Annunciator or “Walking Dot” rotates clockwise in the four Cardinal positions.

Default range is 200 NM. Avoid take-off or landing when Strike Finder displays a cluster within

20 NM of air field.

In Flight: At 100 - 200 range, each dot represents 1 strike At 25-50 range, 4 dots represents 1 strike Dots remain illuminated for 5 minutes Use Clear button to clear display

Assess cluster size, accumulation rate, adjacent activity, persistence & fragmentation.

…/2

STRIKE FINDER (cont.)

Displaying History Press Time button to replay history (last 4000 strikes). Compresses

up to 1 hr. into 1 min. Test Status Annunciator rotates counter clockwise to indicate displaying history.

Max age of history is briefly displayed in lower left corner. Press Time button again during playback to display age of current

playback. Display returns to normal operation once history has been

displayed (may take up to 1 min.) To end playback immediately, press Time & Clear buttons simultaneously.

Error CodesX0 - Intermittently Displayed: Sometimes a high level of storm activity may cause a momentary X0 error to appear. This is an acceptable condition, requiring no operator action. All other error codes indicate display or sensor malfunctions. Do not rely on Strike Finder until corrected. Whenever an error is detected the "Walking Dot” Test Status Annunciator disappears from the display.