AIR-ESPACE HB-GHG SN TC-1616 CHECK - LIST BARON BE95 B55 EXPANDED PROCEDURES PREFLIGHT INSPECTION AIRCRAFT DOCUMENTS EMERGENCY EQUIPMENT
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1 AIR-ESPACE HB-GHG SN TC-1616 CHECK - LIST BARON BE95 B55 EXPANDED PROCEDURES Change vers 2.7 : paging, A/C type, pitch/power, short finale speed, weighing, fuel qty. AIR-ESPACE - Expanded Procedures BE95-B55 / HB GHG For training purpose only PREFLIGHT INSPECTION WALKAROUND according the POH/AFM (Prior to each flight) 01) Maintenance A/C Book / HIL CHECK 02) Refueling Fuel Quantity NOTE 03) Engines OIL Quantity NOTE 04) Propellers A/I Quantity CHECK 05) ELT/ELBA RH panel ARMED 06) Windshield Pilot / Copilot CLEAN 07) Headset (2) ON-BOARD CHECK AIRCRAFT DOCUMENTS 01) A/C Log Book/HIL CHECK ON-BOARD 02) FOCA-Documents VALID ON-BOARD 03) Pilot Handbook POH / AFM ON-BOARD 04) Route Manual CURRENT ON-BOARD 05) SOP - OM Manual AIR-ESPACE ON-BOARD 06) Checklist AIRCRAFT ON-BOARD EMERGENCY EQUIPMENT 01) Flashlights (2) CHECK (NIT) ON-BOARD 02) Hand-Mike (1) CHECK ON-BOARD 03) Fire extinguisher SECURED CHECK 04) Emergency Exits SECURED CHECK 05) Emergency VHF If on board Checked 06) Emergency CHECKLIST ON-BOARD GHG_expanded_IFR3 (vers 2.7) Page X-1
2 AFCS AP/FD S-TEC S55-X CHECK PREFLIGHT (*) Check prior to each flight 01) Turn and Bank indicator CHECK / No FLAG 02) Autopilot Master switch ON (FD/AP) and observe : all annunciators 5 sec ON, then 03) "READY" annunciator CHECK / ON 04) Trim master switch ON 05) HDG and VS buttons PRESS / RELEASE and monitor :"HDG"; "VS" Annunciators ON 06) CWS button PRESS / HOLD and check : servos Disengaged and controls FREE 07) CWS button RELEASE and check : servos REENGAGED 08) VS knob ROTATE CW and check : pitch control MOVE slowly OUT 09) VS knob ROTATE CCW and check : pitch control MOVE slowly IN 10) Autopilot disconnect button PRESS and verify : autopilot DISCONNECTED 11) HDG mode ENGAGE 12) HSI HDG BUG MOVE LH / RH and check roll control FOLLOW BUG 13) "ALT" button PUSH, then a) Pitch control PULL slowly and check AUTOTRIM RUNS NOSE DOWN TRIM annunciator (after 3 sec) FLASHES b) Pitch control PUSH slowly and check AUTOTRIM RUNS NOSE UP TRIM annunciator (after 3 sec) FLASHES 14) TRIM Master Switch OFF GHG_expanded_IFR3 (vers 2.7) Page X-2 15) HSI CRS UNDER LUBBERLINE 16) NAV Mode ENGAGE 17) CRS LH / RH MOVE LH /RH 18) and check roll control FOLLOW CRS Select a valid VOR and CENTER NEEDLE 19) CRS LH / RH MOVE 1 dot -> LH /RH and check roll control FOLLOW DEV BAR 20) REV button PRESS 21) CRS LH / RH MOVE 1 dot -> LH /RH and check roll control GOES OPPOSITE DEV BAR 22) Autopilot Master switch ON (FD only) and check for all servos DISENGAGED 23) HDG Mode ENGAGE 24) HDG bug MOVE 45 OFF LUBBERLINE and check steering bars FOLOWS HDG BUG 25) VS Mode ENGAGE 26) VS Knob SELECT 1500 FT/MIN ROC and check pitch steering bar MOVES UP 27) Autopilot Master switch ON (FD/AP) and check for all servos REENGAGED 28) TRIM Master Switch ON 29) Manual Trim Switch (yoke) MOVE EITHER SIDE and check autopilot DISCONNECTS AP-LIMITATIONS : 1000 ft (EN-ROUTE) ft (ILS-APCH) GHG_expanded_IFR3 (vers 2.7) Page X-3
3 MANUAL ELECTRIC PITCH-TRIM TEST MFD (MAP + Radar) Bendix MFD ) TRIM Master Switch ON 02) Each segment (one at a time) MOVE UP /DOWN and check Trim servo NOT RUNNING 03) Both segments MOVE FORWARD and check Trim servo RUNNING NOSE DOWN 04) Both segments MOVE AFT and check Trim servo RUNNING NOSE UP 05) AP/ Trim Disconnect switch PRESS AND HOLD Both segments MOVE AFT / FORWARD and check Trim servo NOT RUNNING 06) AIRCRAFT TRIM SET FOR TAKE-OFF GPSS MODE TEST RMK : To be performed during auto-test of GNS430 01) Avionics Master switch ON 02) GNS430 ON Check its auto-test until date of validity and when "OK?" appears : "ENTER" Button PRESS check the page for DEV TEST 03) Autopilot "NAV" PRESS TWICE Check A/P annunciator shows GPSS 04) GNS 430 "Enter" Button PRESS Check A/P annunciator shows GPSS FAILED 05) Autopilot DISCONNECT Functions TRFC (Traffic Alert) Not available TERR (Terrain Alert) Not available EGPWS Not available Stormescope Not installed Flight Plan information icons on left part of display Icon Colors Description Black symbol with a magenta Flight plan information being received and displayed line below and white line above on a cyan background Black on gray background Flight plan information being received but not displayed f Radar information icons on left part of display on MAP MODE Icon Colors Description Black on Cyan background Weather radar in standby mode being displayed. Note that since the OVLY key is never enabled on the WX page when the radar is in standby mode, "hold to Help" text is not available Black on Cyan background Weather radar in active mode being displayed Black on gray background Black on gray background Black on gray background with a red slash Weather radar is in standby mode not being displayed Weather radar is in active mode not being displayed Weather radar data invalid / not being received. Previously in standby Black on gray background with a red slash Weather radar data invalid / not being received. Previously active GHG_expanded_IFR3 (vers 2.7) Page X-4 GHG_expanded_IFR3 (vers 2.7) Page X-5
4 IFR PROCEDURES TAXI CHECK SOP Flight - INSTRUMENTS 01) VG HORIZON (# 1 AIR) STABLE NORMAL 02) VG HORIZON (# 2 Elect) STABLE NO FLAG 03) HSI (2) DIR GYRO CHECK NO FLAG 04) TB TURN & BANK CHECK NO FLAG 05) STBY COMPASS CHECK NORMAL 06) BA ALTIMETER(2) CHECK SET/QNH 07) ASI AIRSPEED CHECK ZERO 08) VSI VERTICAL (VARIO) CHECK ZERO INSTRUMENTS - Setting DEP/ATC Clearance 01) DG HSI HDG/BUG SET RWY-HDG 02) NAV-1 HSI FREQ/CRS SET ATC/SID 03) NAV-2 VOR FREQ/CRS SET ATC/SID LH + RH IND + RMI (Sandel) 04) DME DME NAV1/NAV2 SET ATC/SID 05) ADF RMI (Sandel) FREQ/NDB SET ATC/SID 06) ATC XPDR STBY SET CODE/SID 07) GPS (IFR) FPL SET FPL/DCT 08) COM-1 FREQ/SBY SET ATC/SID 09) COM-2 FREQ/SBY SET ATC/SID TAKEOFF BRIEFING DEP : VFR/IFR 01) WEATHER/PERFO:VMC/IMC, RWY condit., Wind, Obstacles, Climb 02) SPEEDS: Vr/Decision = 90 KIAS Vy = 107 KIAS Vmca= 78 KIAS Vyse = 100 KIAS 03) IF MAJOR MALFUNCTION : Below Vr/Décision Throttle Idle, Brakes, Maintain centerline, Advise ATC 04) IF MAJOR MALFUNCTION: Above Vr/Décision VMC: R/H or L/H to downwind, Circling Alt, Vyse, secure dead engine IMC: Fly SID/Clearance, Climb MSA, Vyse, ATC, Vectors to RWY Emergency Circling, climb MSA, alternate, GHG_expanded_IFR3 (vers 2.7) Page X-6 IFR PROCEDURES Landing DATA SOP ATIS - WEATHER 01) VHF COM-2 Select ATIS / WX (FREQ) 02) VHF COM 1 Request to Leave ATC (2 MIN) 03) VHF COM 2 Landing Data (COPY) 04) VHF COM 1 Advise ATC / Back ON (FREQ) RMK : On first contact with Destination, advise ATC for ETA Destination VFR / IFR Approach BRIEFING 01) TOD NM = (Act FL minus desired FL) x 3/10 02) MSA Safe Altitude within 25 NM in case of Emergency 03) AIRPORT Elevation / APP + Runway Lights / Taxiway 04) TYPE of Approach (Precision or Non Precision, Circling) 05) FINAL TRACK (Inbound) Position of OM or equivalent 06) ALTITUDE for Initial, Intermediate APP and Outer Marker 07) MINIMUM DA /MDA and RVR (Visibility for circling) 08) MAP Missed Approach Procedure Initial HDG/ALT VFR / IFR Approach INSTRUMENT setting 01) HSI NAV-01 ILS VOR Inbound CRS 02) VOR NAV-02 VOR LOC Inbound CRS 03) DME DME ILS VOR NAV1 ILS/DME 04) RMI (sandel) ADF OM LCTR ADF Bearing 05) RMI VOR ARP NAV2 VOR Bearing (sandel) 06) IFR GPS OM (OR) AS REQUESTED HSI MODE SELECTOR SHOULD BE : ON V/LOC MODE FOR ILS APP GHG_expanded_IFR3 (vers 2.7) Page X-7
5 PITCH / POWER SOP PHASE MP / RPM KIAS ROD ATT TAKEOFF FT / CLIMB (Vx..) FT (MAX) / CLIMB (Vy..) 25" (MAX) / CLIMB (cruise) 25" (MAX) / CRUISE 23" (MAX) / DESCENT -1 20" / ft/min - 1 DESCENT 2 17" / ft/min - 2 DESCENT 3 15" / ft/min - 3 HOLDING 17" (clean) / FLAPS KIAS GEAR DN 130 KIAS GEAR UP not specified FLAPS KIAS FULL FLAPS 110 KIAS APPROACH 17" / KIAS CLEAN FINAL APP 15" / KIAS FLAPS 20 SHORT FINAL 15" / KIAS FULL FLAPS HIGH SPEED 15 / KIAS CLEAN VMCA = 78 KIAS VNO = 183 KIAS VA = 157 KIAS AIRCRAFT GENERAL Usable Fuel = 136 USG FAR/JAR 23 (Class B) S/N = TC-1616 Special Equipment : 2 x GPS/Garmin 430 (B-RNAV!) Weather Radar Bendix/King RDR 2000 AP = S-TEC S55X(with GPSS) MFD Bendix/ King KMD 850 (Radar) FD = Bendix King KI-256 Modes S Transponder Garmin GTX330 GHG_expanded_IFR3 (vers 2.7) Page X-8 AIRSPEED LIMITATIONS Vr/V1 90 KIAS Vmca 78 KIAS Vsse 84 KIAS Vxse 91 KIAS Vyse 100 KIAS Vs0 (Landing) 69 KIAS Vs1 (Clean) 79 KIAS Vx 84 KIAS Vy 107 KIAS Vfe (Full Flaps) 122 KIAS Vlo /Vle 153 KIAS Va (Max TOW) 157 KIAS Vne 224 KIAS Vno 183 KIAS Max Glide 120 KIAS Approach Speed 110 KIAS Threshold Speed 90 KIAS Emergency Descent 153 KIAS Max Cross Wind 22 Kts OPERATIONAL INFORMATIONS HB-GHG Serial Number # TC-1616 Useable Fuel 136 USG Total Fuel 142 USG Oil 9-12 Qts (min 9 Qts) X-feed only approved for Emergency (Level Flight) M&B Max Ramp 5121 lbs / 2325 Kg Max TO 5100 lbs / 2316 Kg Max Landing 5100 lbs / 2316 Kg Weighing Empty mass lbs Empty moment in.lbs GHG_expanded_IFR3 (vers 2.7) Page X-9
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