Aircraft information PA-28RT-201T-IV

(Document nr.: 125) Aircraft information PA-28RT-201T-IV COPYRIGHT Avion Training BV No part of this manual or its extracts may be reproduced in any form, by print, photo print, microfilm or any other means, without written permission from Avion Training BV issue 1.1 Page 1-20

ISSUE RECORD Issue Number Issue Date 01 18-09-2014 1.1 23-06-2017 Issue 1.1 Page 2-20

TABLE OF CONTENTS 1. Introduction... 4 1.1 General... 4 1.2 Sources... 4 1.3 Abbreviations... 5 2. Aircraft information... 6 2.1 Power settings and speeds... 6 2.2 Expanded normal checklist PH-STY... 7 Issue 1.1 Page 3-20

1. INTRODUCTION 1.1 GENERAL This book contains speed, power settings and expanded checklists of aircraft and simulators used within Avion Training. This book is coupled to the SOP document of Avion Training. For the mentioned expanded checklists this book is coupled to the Avion Training checklists, which are mainly an extract out of the POH/AOM. The amendment system used for this book is conform the procedure described in the OM of Avion Training. 1.2 SOURCES Material used from: a) POH / AOM b) SOP`s c) Avion Training checklists Issue 1.1 Page 4-20

1.3 ABBREVIATIONS AGL AOM/POH ATC ATPL FIR ICAO FIO IFR NOTAM OM OPS POH PIC RT SE SCD SOP UTC VFR Above Ground Level Aircraft Operating Manual/ Pilots Operating Handbook Air Traffic Control Air Transport Pilot License Flight Information Region International Civil Aviation Organization Flight Information Office Instrument Flight Rules Notices to Airmen (part of Aeronautical Information Publication) Operating Manual Operations department of Avion Training Pilot Operating Handbook Pilot In Command Radiotelephony Single Engine Subject to Captains Discretion Standard Operating Procedure Universal Time Coordination Visual Flight Rules Speeds: Vr Vclimb Vcruise Vdescent Vglide Vstall Vs1 Vs0 Vslow Vhigh Vx Vy Rotation speed Climb speed Cruise speed Descent speed Glide speed Stall speed Stall speed, clean configuration Stall speed, landing configuration Slow speed High speed Maximum angle of climb Maximum rate of climb Issue 1.1 Page 5-20

2. AIRCRAFT INFORMATION 2.1 POWER SETTINGS AND SPEEDS initial taxi power static take-off power take-off power 1200 RPM 41 /2575 RPM 41 /2575 RPM normal take-off flaps up Vr 75 KIAS climb speed 105 KIAS short field take-off flaps 25º Vr (see POH) climb speed 105 KIAS obstacle take-off flaps 25º Vr (see POH) climb speed 79 KIAS normal/cruise climb 105 KIAS 33 /2450 RPM best angle of climb/gear up 79 KIAS 41 /2550 RPM best rate of climb/gear up 97 KIAS 41 /2550 RPM cruise flight (navigation flights). KIAS power setting table airwork 120 KIAS 18 /2400 RPM steep turn less than Va slow flight (flaps 10, gear up) 70 KIAS 16 /full fine turn in landing configuration minimum Vstall +10kts initial stall power 15 /2400 RPM holding speed 105 KIAS 16 /2400 RPM cruise descent 120 KIAS 13 /2400 RPM approach speed flaps 10º, gear down 100 KIAS 18 /full fine circle to land speed, gear down 95 KIAS 15 /full fine threshold speed flaps up 80 KIAS 12 /full fine threshold speed flaps 10 80 KIAS 12 /full fine threshold speed flaps 25 75 KIAS 13 /full fine threshold speed flaps 40 75 KIAS 14 /full fine best glide speed 79 KIAS CIRCUIT s Normal landing crosswind leg flaps up 95 KIAS 17 /2400 RPM downwind flaps 0/10 95-90 KIAS 17 /2400 RPM base leg flaps 25 80 KIAS 14 /full fine final flaps 40 75 KIAS 14 /full fine Flapless landing base leg flaps up 85 KIAS 13 / full fine final flaps up 80 KIAS 12 / full fine Precautionary landing final leg flaps 40 70 KIAS 15 / full fine Emergency landing glide speed 79 KIAS final flaps 40 72 KIAS (when the field can easily be reached) Issue 1.1 Page 6-20

2.2 EXPANDED NORMAL CHECKLIST PH-STY This expanded normal checklist is an explanation of the PH-STY checklist. BEFORE STARTING ENGINE (This checklist shall be performed after checking the weather and the crew briefing and before start up.) Crew briefing... COMPLETED See SOP s for format of briefing. Avionics switch... OFF Parking brake... SET Check Parking Brake off and on again. Make sure that the parking brake is set properly. Propeller... FULL INCREASE RPM Fuel selector... DESIRED TANK Alternate air... OFF Emergency equipment... CHECK Check hand microphone is on board. Check ELT Check fire extinguisher is on board, fully charged and readu to use Check first aid kit is on board Check life vests are on board if necessary according OM. Luggage... STOWED No heavy objects shall be left loose to avoid risk of injuries to the occupants or damage to the aircraft in turbulence or G-conditions. Papers... CHECK See OM for mandatory papers on board. Check existing deficiencies with the Minimum Equipment List before executing the flight Preflight inspection... COMPLETE Seats and Safety Belts...ADJUST Always fly with your seats and pedals in the same locked position. Check if seatbelts are fastened of all occupants. Make sure that passengers know how to close, adjust and open the seatbelts. Issue 1.1 Page 7-20

Controls... FREE AND CORRECT Check elevator and ailerons for complete and correct freedom of movement. Sequence: 1.yoke fully forward and left. check left aileron up and right aileron down. check elevator down. 2.yoke fully forward and right. check right aileron up and left aileron down, 3.return yoke to neutral 4. pull yoke fully aft. check elevator up. Flaps... CHECK Select flaps 40 and check visual. Select flaps 25 and check visual. Select flaps 10 and check visual. Select flaps up and check visual. Gear switch... DOWN Master switch... ON Fuel quantity indication... CHECKED Check if indication is in accordance with visual fuel check. Gear lights... 3 GREENS Annunciators... ON Test the lights by pushing the ANNUN TEST button on the left side of the pilots sub panel. When the button is pushed, all annunciators should illuminate. After releasing the button only the annunciators which are legible for the current condition shall remain on. Beacon Light... ON Set beacon light to warn for imminent engine start. Circuit Breakers... CHECKED Check circuit breaker panel located to the right of the panel. Circuit breakers may not be reset. Start up (if applicable)...received Avionics master switch...off STARTING ENGINE (This checklist shall be performed just before engine start.) Fuel selector... ON Mixture... FULL RICH Throttle...... FULL FORWARD Prop control... FULL FORWARD Master Switch... ON Issue 1.1 Page 8-20

Auxialiary Fuel pump... OFF Primer...... ON See POH chapter 4 for priming time (Figure 4-3). Throttle...CLOSE Starter... ENGAGE IMMEDIATLY At temperatures below +20ºF continue priming while cranking until engine starts. When engine starts firing open the throttle very slowly to raise engine speed to 1000 RPM. As engine speed accelerates through 500 RPM, release starter. Primer... RELEASE Auxialiary Fuel Pump LOW ONLY AS NECESSARY TO OBTAIN SMOOTH ENGINE OPERATION (1-3 minutes will be required when temp. Is below 20ºF) Oil pressure... CHECK Alternator... CHECK Gyro vacuum... CHECK STARTING ENGINE WHEN FLOODED (This checklist shall be performed just before engine start.) Mixture... IDLE CUT-OFF Throttle... FULL FORWARD Propeller... FORWARD Master Switch... ON Auxiliary Fuel Pump... OFF Propeller... CLEAR Starter... ENGAGE When engine fires: Throttle... RETARD Mixture... ADVANCE SLOWLY Issue 1.1 Page 9-20

STARTING ENGINE WITH EXTERNAL POWER SOURCE (This checklist shall be performed just before engine start.) Master Switch... OFF All Electrical Equipment... OFF Terminals... CONNECT External power plug... INSERT IN FUSELAGE PROCEED WITH NORMAL START Throttle... LOWEST POSSIBLE RPM External power plug... DISCONNECT FROM FUSELAGE Master Switch... ON CHECK AMMETER Oil pressure... CHECK WARM-UP (This checklist shall be performed when engine needs warm up.) Throttle... 900 TO 1200 RPM BEFORE TAXI (This checklist shall be performed after engine start en before taxi.) Alternator output... CHECK The alternator output should indicate that battery is charging Flight instruments... CHECK 1. Check OAT indicator (must be in accordance with ATIS) 2. Check ASI. 3. Check ADI. 4. Set QNH in the altimeter and check altitude pointer within 60 ft from field elevation. 5. Check HSI. 6. Check VSI. 7. Check Turn coordinator. 8. Check Clock set to UTC Avionics... CHECK and SET Avionics SET UP is performed by student DME - set Nav 1, Intercom - set required mode and adjust volume, Audio panel - set microphone selector Com 1, Marker beacon - hold function selector in TEST and check lights. COM 1 - select required COM station, - pull volume knob to TEST, to disable squelch circuit to allow audible verification of receiver operation, adjust volume control for desired audio level, push volume knob in to normal operation, - select required standby COM station. Issue 1.1 Page 10-20

COM 2 - select required COM station, - pull volume knob to TEST, adjust volume control for desired audio level, push volume knob in to normal operation, - select required standby COM station. NAV 1/2 - select simultaneously a suitable ILS freq. on NAV 1 & 2, - select NAV 1 at audio panel to PHONE, pull volume control to IDENT and adjust for desired audio level. Set NAV 1 on audio panel off. Repeat procedure for NAV 2. - check if the localizer and glide slope indication correspond with the aircraft s position in relation to the ILS, both on HSI and/or OBS, - select simultaneously a suitable VOR freq. on Nav. 1 & Nav. 2. - select NAV 1 at the audio panel to PHONE, pull the volume control to IDENT, set NAV 1 on audio panel OFF. Repeat the procedure for nav. 2. - perform OBS check: - check, if applicable, current radial on RMI and call out the radial, - centre HSI/OBS on radial by course selector, - check OBS radial with RMI radial if applicable, - turn course selector 10 degrees to the left of the centered radial and check a 5 dot deflection to the left, - turn course selector 10 degrees to the right of the centered radial and check a 5 dot deflection to the right, - turn course selector 90 degrees to the right of the centered radial and check a TO / FROM change. Repeat procedure for NAV 2 with OBS - set and identify the VOR and select the correct radials for the expected departure (both in NAV 1 and NAV 2) NOTE 1. NOTE 2. NOTE 3. Usually the aircraft position will prevent reception of an adequate GS signal. In case a VOT is selected a VOR signal conform radial 360 will be received, regardless of the actual position of the airplane. Usually the aircraft position will prevent reception of an adequate DME signal. Transponder - turn function selector to TST and hold. Reply light will illuminate, - turn function selector back to STBY. - Select squawk code, if no code received set standard VFR/IFR code. ADF - select a suitable NDB, - select ADF at audio panel to PHONE and adjust volume control to desired audio level, - check correct ident, - set ADF in audio panel off, - set ADF in ANT mode. The ADF pointer will go to the 90 degrees parked position), - set ADF in ADF mode (the ADF needle should return to the QDM through the shortest way.), - set NDB frequency for expected departure. Prior to subsequent flights of the day: DME - set NAV 1, Intercom - set required mode and adjust volume, Audio panel - set microphone selector COM 1 or 2 as required Issue 1.1 Page 11-20

COM 1 - select required COM station, - pull volume knob to TEST, to disable squelch circuit to allow audible verification of receiver operation, adjust volume control for desired audio level, push volume knob in to normal operation, - select required standby COM station. COM 2 - select required COM station, - pull volume knob to TEST, adjust volume control for desired audio level, push volume knob in to normal operation, - select required standby COM station. NAV 1 - set VOR frequency and radial for expected departure, - select NAV 1 at audio panel to PHONE, pull volume control to IDENT and adjust for desired audio level and check; - correct ident. signal, - correct DME indication, - set NAV 1 on audio panel off. NAV 2 - set VOR frequency and radial for expected departure, - select NAV 2 at audio panel to PHONE, pull volume control to IDENT and adjust for desired audio level and check; - correct ident. signal, - set NAV 2 on audio panel off. Transponder - check function selector set STBY, Test Transponder if possible, - Select squawk code, if no code received set standard VFR/IFR code. ADF - select required NDB, - check function selector in ADF, - select ADF at audio panel to PHONE and adjust volume control to desired audio level, - check correct ident, - set ADF on audio panel off. GPS - Set GPS if available. Autopilot.CHECK AND OFF Electrical trim... CHECK Manual trim... CHECK AND SET Time... NOTE Check Clock and note time on Nav-log TAXIING (This checklist items shall be performed during taxi. The checklist at the holding position before the run up.) Chocks... REMOVED Taxi Area... CLEAR Parking Brake... RELEASE Throttle... APPLY SLOWLY Prop... HIGH RPM Issue 1.1 Page 12-20

Brakes... CHECK Check both brake pedals as smooth as possible (the aim is to check the brakes and NOT to stop the aircraft). Check all four pedals during the first flight of the day. Steering... CHECKED Gyro instruments and Compass... CHECKED Left turn - turn indicator left - ball right - DI decreasing - AI steady, compass decreasing. Right turn - turn coordinator right - ball left - DI increasing - AI steady, compass increasing. Try to use the turns in the taxi-route; avoid unnecessary manoeuvring). GROUND CHECK (This checklist shall be performed at the holding position, preferably into the wind just before departure. If possible leave room for other aircraft to pass.) Parking Brake... SET Propeller control... FULL INCREASE Throttle... 1800 to 2000 RPM Magnetos... MAX. DROP 150 RPM MAX. DIFF. 50 RPM Check left/right magneto. Maximum drop 150 RPM, maximum difference between left and right magneto 50 RPM. Vacuum... 4.8 HG. TO 5.1 HG Oil Temp... CHECK Oil Pressure... CHECK Air Conditioner (if applicable)... CHECK Annunciator Panel... PRESS-TO-TEST Propeller... EXERCISE THEN FULL INCREASE Pull propeller control to low RPM to obtain a drop of 200 300 RPM and return to high RPM Repeat 3 times during first flight of the day. For subsequent flights 1 time is sufficient. Select 1900 RPM with propeller control, increase throttle 2 inch manifold pressure, check RPM stays at 1900, return throttle, return propeller to full forward. If necessary reset throttle to 2000 RPM. Alternate air... CHECK ENGINE IS WARM FOR TAKE-OFF WHEN OIL TEMPERATURE IS AT LEAST 100 F Auxiliary Fuel Pump... OFF Fuel pressure... CHECK Throttle... RETARD Issue 1.1 Page 13-20

Manifold pressure line... DRAIN BEFORE TAKEOFF (This checklist shall be performed at the holding position, preferably into the wind just before departure. If possible leave room for other aircraft to pass.) Master switch... ON Flight Instruments... CHECK Fuel Selector... PROPER TANK Auxiliary Fuel Pump... LO-if required Engine Gauges... CHECK Alternate Air... CLOSED Seat Backs... ERECT Mixture... SET Propeller... SET Belts/Harness... FASTENED/ADJUST Empty Seats... SEAT BELTS SNUGLY FASTENED Flaps... SET Trim tab... SET Controls... FREE Doors... LATCHED Make sure that the storm window and the doors are locked (baggage door included). Air conditioner (if applicable)... OFF Parking brake... RELEASED RUNWAY ITEMS (These checklist items shall be performed by memory. In case of single pilot operation these items shall be performed standing still. Line up clearance(if applicable) must be received.) Lights..... SET Transponder... SET Check if proper code is set and turn on ALT. If there are no instructions by the exit publications or ATC, select 2000 on IFR flights and 7000 on VFR flights. Fuel pump... LO-if required Pitot heat... ON Runway Heading... CHECK Airborne Time... CHECK Issue 1.1 Page 14-20

NOTE: Particularly at night, reflections from lights on clouds, dense haze or dust can produce optical illusions and intense vertigo. Such lights should be turned off before entering overcast. Their use may not be advisable under IMC or limited VMC. Take-off Clearance(if applicable)... RECEIVED TAKE OFF (This checklist shall be performed by memory during take-off.) NORMAL Flaps..... SET Tab.... SET Accelerate to... 70 to 75 KIAS Control wheelback PRESSURE TO ROTATE TO CLIMB ATTITUDE SHORT FIELD, OBSTACLE CLEARANCE Flaps..... 25 (SECOND NOTCH) Accelerate to 53 to 64 KIAS (depending on aircraft weight) Control wheelback PRESSURE TOROTATE TO CLIMB ATTITUDE After breaking ground, accelerate to 59 to 68 KIAS (depending on aircraft weight) Gear (OVERRIDE ENGAGED on aircraft equipped with the backup gear extender) UP Accelerate to best flaps up rate of climb speed 79 KIAS. Flaps..... RETRACT SLOWLY SOFT FIELD Flaps..... 25 (SECOND NOTCH) Accelerate to 53 to 64 KIAS (depending on aircraft weight) Control wheelback PRESSURE TOROTATE TO CLIMB ATTITUDE After breaking ground, accelerate to 59 to 68 KIAS (depending on aircraft weight) Gear (OVERRIDE ENGAGED on aircraft equipped with the backup gear extender) Accelerate to best flaps up rate of climb speed 97KIAS. UP Flaps..... RETRACT SLOWLY TAKE-OFF CLIMB Gear... UP Apply the brakes before gear-up selection to stop the rotation of the main wheels. When a positive rate of climb is indicated, pulling the gear handle out and moving UP initiates the retraction cycle illuminating the red IN TRANS light. Check all lights are out indicating the gears are up and locked CAUTION: Do not change the position of the control switch to reverse the direction of the landing gear while the gear is in transit, as this could cause damage the gear retracting system. Issue 1.1 Page 15-20

Flaps... UP Refer to specific T/O procedure for flap-selection procedures. Mixture... FULL RICH Prop speed... 2575 RPM Manifold pressure... DO NOT EXCEED 41 in. HG. Climb speed Best angle... 79 KIAS Best rate... 97 KIAS Auxiliary fuel pump... LO-if required CRUISE CLIMB (This checklist shall be performed when passing transition altitude, leaving the CTR or continuing cruise below transition altitude whichever comes first.) Mixture... FULL RICH Prop speed... 2450 RPM Manifold pressure... 33 in. HG. Climb speed... 104 KIAS Auxiliary fuel pump... LO-if required Altimeter... SET Lights... SET Normally landing light off, but Subject Captains Discretion. Issue 1.1 Page 16-20

CRUISING (This checklist shall be performed after leveling off for cruise.) Reference performance charts, Teledyne Continental operator s Manual and power setting table. Normal Max Power... 75 % Power... SET PER POWER TABLE Mixture... ADJUST Lean according POH Auxiliary Fuel pump... LO-if required Fuel selector... PROPER TANK Directional Gyro..... CHECK Line up with compass DESCENT (This checklist shall be performed after starting a descent.) Terrain clearance... CHECK Check the MORA or MSA. Check position (in relation to radar vectors). Altimeter... SET Set QNH in both altimeters as soon as cleared down to an altitude and cross-check. Mixture... ADJUST Adjust the mixture with descent. APPROACH (This checklist shall be performed when cleared to an altitude (if applicable) and inbound for a landing.during circuit training this checklist has to be performed at downwind in which caseavion Training items must be omitted.) Altimeter... SET Directional Gyro...CHECK Avionics... Lights...SET Brakes... CHECK Fuel selector...proper TANK Seat Backs... ERECT o Set and/or check both altimeters with QNH setting. Compare with magnetic compass SET Check all avionics set for the intended approach. Use comm. panel as checklist for avionics setup Issue 1.1 Page 17-20

Belts/Harness... FASTEN/ADJUST Mixture... SET LANDING (This checklist shall be performed by memory at the 500 ft call or at final during circuit training) Mixture... SET Propeller... SET Gear... DOWN 133 KIAS MAX Flaps... SET 108 KIAS MAX Air conditioner (if applicable)... OFF Trim to 75 KTS TAXI IN (This checklist shall be performed by memory after vacating the runway. The checklist may be performed rolling during single pilot operations but on straight taxiways only. The checklist shall then be read when on the parking position.) Lights... SET Landing lights remains ON when taxi-in routing is via (non-active) rwy(s) or when operating by night. In all other circumstances switch landing light OFF. Anti collision lights can be switched off, except when taxiing over (non-active)runways Fuel pump... OFF Pitot heat... OFF Transponder... STANDBY Flaps... RETRACT STOPPING ENGINE (This checklist shall be performed when on parking position.) Air Conditioner (if applicable)... OFF Radios... OFF Propeller... FULL INCREASE Throttle... FULL AFT Mind Throttle 1200 RPM for 5 minutes for cooling down period. Mixture... IDLE CUT-OFF Magnetos... OFF Master Switch OFF Fans... OFF Issue 1.1 Page 18-20

All lights... OFF Time... NOTE PARKING (This checklist shall be performed when on parking position.) Parking brake... SET Normally when parking for a short period, the parking brake is used to prevent the airplane from moving. Control Wheel... SECURED WITH BELTS Use seatbelt to lock steering wheel in most after and full right or left position depending wind. Flaps... FULL UP Wheel Chocks... IN PLACE (if applicable) Tie Downs... SECURE (if applicable) PRE STALL (This checklist shall be performed after the stall briefing and just before the (stall) exercise.) Angle of bank Flaps 40 0 Flaps retracted 0 0 61 KIAS 66 KIAS 20 0 62 KIAS 67 KIAS 40 0 68 KIAS 73 KIAS 60 0 84 KIAS90 KIAS Briefing... COMPLETE Mixture... RICH Fuel pump... LO-if required Fuel selector... FULLEST TANK Engine gauges... CHECK Loose items... STOW Safety belts... FASTEN APOS... CHECK Issue 1.1 Page 19-20

AFTER STALL (This checklist shall be performed when stabilized on altitude/level after the (stall) exercise.) Gear... UP Flaps... Mixture... Fuel pump... Engine instruments... Gyro s... Orientation...... UP SET OFF CHECK CHECK CHECK Issue 1.1 Page 20-20