sierra industries, inc. - AeroElectric

CLEAR START ADVANCE, slowly RELEASE when engine starts NOTE The engine should start in two to three revolutions. If it does not continue running, start again at Step 3. If the en- gine does not start, leave the Auxiliary Fuel Pump Switch OFF, Set Mixture to IDLE CUT-OFF, open Throttle and crank engine until it fires (or for approximately 15 seconds). If still unsuccessful, allow the starter motor to cool, then start again using the normal starting procedure. (11) Throttle (12) Oil Pressure BEFORE TAKEOFF - - RESET to desired idle speed CHECK (1) Parking Brake (2) Cowl Flaps (3) (4) Flight Controls Elevator and Rudder Trim (5) Mixture (6) Throttle - SET - FULL OPEN - FREE and CORRECT - TAKEOFF - RICH (below 3000 feet) - 1700 RPM (7) a. Magnetos b. Propeller c. Engine Instruments and Ammeter d. Suction Gauge Cabin Doors and Windows (8) Flight Instruments and Radios (9) Autopilot (if installed) (10) Flashing Beacon, Navigation Lights and/or Strobe Lights (11) Throttle Friction Lock Sierra Approved - - - CHECK (RPM drop should not exceed 150 RPM on either magneto or 50 RPM differ- ential between magnetos) - CYCLE from high to low RPM return to high RPM (full forward) CHECK CHECK in green arc CLOSED and LOCKED - SET OFF - ON as required ADJUST A/C 210 61040 THRU 210 61573 Rev. A 08-10-90 Page 4 SIERRA INDUSTRIES, INC. Cessna Model 210L 4. NORMAL PROCEDURES (Cont.) TAKEOFF (1) Wing Flaps Elevator Trim (2) (3) Rudder Trim (4) Cowl Flaps (5) Brakes (6) Power (7) Mixture (8) Brakes (9) - 20° TAKEOFF - 1/2 RIGHT OPEN - APPLY Elevator Control (10) Initial Climb (11) After Clearing Obstacles (12) Landing Gear (13) Flaps (14) Enroute Climb NORMAL CLIMB - - POHS 15-1 FLIGHT MANUAL SUPPLEMENT FULL THROTTLE and 2850 RPM LEAN for Field Elevation per Fuel Flow Indicator Placard RELEASE ROTATE at 52 KIAS 60 KIAS while clearing Obstacles ACCELERATE to 78 KIAS RETRACT in Climb Out RETRACT - STANDARD PROCEDURES (1) Airspeed (2) Power (3) Mixture (4) Cowl Flaps 104 to 113 KIAS 25 INCHES Hg and 2550 RPM LEAN to 108 Lbs./Hr Fuel Flow OPEN as required MAXIMUM PERFORMANCE CLIMB Sea Level to 19,000 Ft (1) Airspeed - - 97 KIAS at Sea Level to 90 KIAS at 10,000 Ft. FULL THROTTLE and 2700 RPM LEAN per Fuel Flow Indicator Placard FULL OPEN (2) Power (3) Mixture (4) Cowl Flaps CRUISING (1) Power - (2) Cowl Flaps - 15 to 25 INCHES Hg and 2200 to 2550 RPM OPEN as required (3) Elevator and Rudder Trim - ADJUST (4) Mixture - LEAN for Cruise Fuel Flow per the Cessna Power Computer or per the CRUISE PERFORMANCE in Section 5 LETDOWN (1) Power (2) Mixture (3) Cowl Flaps Sierra Approved Rev. A 08-10-90 - - AS DESIRED LEAN for smooth performance in Power Descents FULL RICH for Idle Power - CLOSED A/C 210 61040 THRU 210 61573 Page 5 SIERRA INDUSTRIES, INC. Cessna Model 210L 4. NORMAL PROCEDURES (Cont.) BEFORE LANDING POHS 15-1 FLIGHT MANUAL SUPPLEMENT (1) Fuel Selector - (2) Landing Gear Lever FULLEST TANK DOWN (below 140 KIAS) (3) Landing Gear Light - GREEN (4) Mixture RICH (5) Propeller - HIGH RPM (6) Wing Flaps (7) Initial Approach (8) Final Approach - (9) Elevator Trim - DOWN 0° to 10° (below 140 KIAS) 10° to 30° (below 85 KIAS) FLAPS 20° at 85 KIAS FLAPS 30° at 58 KIAS ADJUST BALKED LANDING (1) Power (2) Wing Flaps (3) Climb Past Obstacles at - FULL THROTTLE and 2850 RPM RETRACT IMMEDIATELY to 20° 60 KIAS AFTER CLEARING OBSTACLES (4) Accelerate to (5) Flaps (6) Cowl Flaps LANDING (1) Power (2) Elevator and Rudder Trim (3) Touchdown (4) Touchdown Speed (5) Deceleration AFTER LANDING (1) Cowl Flaps (2) Wing Flaps 78 KIAS RETRACT SLOWLY - OPEN AS REQUIRED for NORMAL RATE OF DESCENT AS REQUIRED - MAIN WHEELS FIRST - 46 KIAS - CLOSE THROTTLE RETRACT FLAPS APPLY - SECURING AIRCRAFT (1) Parking Brake - (2) Radios and Electrical Equipment (3) Mixture - (4) Ignition and Master Switch - (5) Control Lock - Sierra Approved Rev. A 08-10-90 BRAKES OPEN RETRACT SET -OFF IDLE CUT-OFF (pulled full out) OFF INSTALLED A/C 210 61040 THRU 210 61573 Page 6 SIERRA INDUSTRIES, INC. Cessna Model 210L 5. PERFORMANCE No change except: POHS 15-1 FLIGHT MANUAL SUPPLEMENT The minimum performance required by the applicable certification regulations has been demonstrated to the FAA. However, the precise performance information in the basic Pilot's Operating Handbook may or may not be affected by the modification. AIRSPEED CALIBRATION STALL SPEEDS TAKEOFF LANDING Figure 5-1 Figure 5-2 Figure 5-3 Figure 5-4 Flaps 0° AIRSPEED CORRECTION TABLE GROSS WEIGHT 3800 LBS. IAS - MPH 50 50 60 80 100 120 140 160 CAS - MPH 44 64 79 98 118 137 157 Flaps 20°& 30° IAS MPH 35 40 50 60 00 70 80 80 90 100 CAS - MPH 45 48 53 61 70 80 90 100 MAXIMUM FLAP SPEEDS FLAPS 0° TO 10° - 140 KIAS FLAPS 10° TO 30° - 85 KIAS Figure 5-1 STALL SPEEDS ZERO THRUST ANGLE OF BANK CONDITION 0° 20° 40° 60° 3800 LBS FLAPS UP 59 60 68 86 GROSS FLAPS 20° 53 54 60 74 WEIGHT FLAPS 30° 46 47 54 6046 Sierra Approved Rev. A 08-10-90 SPEEDS ARE KIAS Figure 5-2 A/C 210 61040 THRU 210 61573 Page 7 SIERRA INDUSTRIES, INC. Cessna Model 210L POHS 15-1 FLIGHT MANUAL SUPPLEMENT SIERRA TAKEOFF DATA - SIERRA R/STOL CESSNA 210L CENTURION Takeoff Distance With 20° Flaps From Hard Surfaced Runway (FT.) SEA LEVEL GROSS KIAS HEAD 59°F 2500 FT. 5000 FT. 50°F 41°F 7500 FT. 32°F WT. @ 50 WIND GRND TOTAL RUN TO 50 GRND RUN TOTAL GRND TO 50 RUN LBS FT. KTS FT. FT. TOTAL GRND TO 50 RUN FT. TOTAL TO 50 FT. 715 1232 3800 60 60 10 535 975 20 373 745 860 1495 650 1195 465 925 1040 790 1495 575 1175 1850 1270 2460 975 2020 720 1610 0 555 975 665 1155 795 1380 970 1725 3400 56 10 405 765 490 910 600 1100 730 1385 20 280 570 345 690 425 845 530 1080 0 415 775 500 895 595 1045 720 1260 3000 51 10 295 600 360 695 440 820 535 995 20 200 440 245 520 305 615 380 760 NOTES: 1. Sierra Approved Rev. A 2. 3. Increase Distances 10% for each 20°F above Standard Temperature for particular altitude. For takeoff on a dry, grassy runway, increase Distances (both "Ground Run" and "Total to 50 Ft.") by 5% of the "Total to 50 FT." Distance. For operations in severe or gusty crosswind conditions, increase speeds 4 KIAS for each 10 knots of wind increment. 08-10-90 Figure 5-3 A/C 210 61040 THRU 210 61573 Page 8 SIERRA INDUSTRIES, INC. Cessna Model 210L POHS 15-1 FLIGHT MANUAL SUPPLEMENT SIERRA LANDING DATA SIERRA R/STOL CESSNA 210L CENTURION Landing Distance With 30° Flaps On Hard Surfaced Runway (Feet) GROSS KIAS SEA LEVEL 59°F 2500 FT. 50°F 5000 FT. 41°F 7500FT. 32°F WT. @ 50 GRND TOTAL GRND то ROLL CLEAR ROLL LBS FT 50 FT TOTAL GRND TO CLEAR ROLL 50 FT TOTAL GRND TO CLEAR ROLL 50 FT TOTAL TO CLEAR 50 FT 3800 57 490 960 525 1020 555 1085 590 1155 3400 53 440 905 470 955 495 1010 530 1075 3000 49 390 845 415 890 440 940 470 995 NOTES: 1. Distances shown are based on zero wind, power off, and heavy braking. 2. Reduce Landing Distances 10% for each 5 knots headwind. 3. For operation on a dry, grassy runway, increase Distances (both "Ground Roll" and "Total to Clear 50 Ft") by 20% of the "Total to Clear 50 Ft" figure. 4. For operating in gusty or severe crosswind conditions, increase speeds 4 KIAS for each 10 knot wind increment. Sierra Approved Rev. A 08-10-90 Figure 5-4 A/C 210 61040 THRU 210 61573 Page 9 SIERRA INDUSTRIES, INC. Cessna Model 210L POHS 15-1 FLIGHT MANUAL SUPPLEMENT 6. SUPPLEMENTS No changes 7. WEIGHT AND BALANCE See FAA Form 337 in the airplane records for the weight and C.G. of the weight added for this modification. AIRPLANE SYSTEMS AND DESCRIPTIONS No change HANDLING, SERVICE AND MAINTENANCE No Change Sierra Approved A/C 210 61040 THRU 210 61573 Rev. A 08-10-90 Page 10