King Air C90A. Speeds (KIAS)



Similar documents
Super King Air 200. Speeds (KIAS)

BOMBARDIER CRJ700. Bombardier CRJ700 Aircraft Reference

Multi Engine Oral Exam Questions

MULTI-ENGINE TURBO-PROP AEROPLANE ENDORSEMENT

MULTI-ENGINE TURBO-PROP AEROLANE ENDORSEMENT

SINGLE ENGINE TURBO-PROP AEROPLANE ENDORSEMENT

Cessna Grand Caravan Pilot s Technical Examination

General Characteristics

This is the fourth of a series of Atlantic Sun Airways CAT B pilot procedures and checklists for our fleet. Use them with good judgment.

This is the third of a series of Atlantic Sun Airways CAT B pilot procedures and checklists for our fleet. Use them with good judgment.

MULTI-ENGINE PISTON AEROPLANE ENDORSEMENT ENGINEERING, DATA AND PERFORMANCE QUESTIONNAIRE

PILOT OPERATING HANDBOOK FOR ROCKWELL TURBO COMMANDER 690B

Compiled by Matt Zagoren

MULTI-ENGINE PISTON AEROPLANE ENDORSEMENT

CESSNA 172 CHECKLIST TAXI PRE-EXTERNAL CHECKS. 1. Lights - As required 2. Brakes - CHECK 3. Rolling Instruments Check - L/R

LANDING GEAR & BRAKES GTM CONTENTS INTRODUCTION

Lancair Legacy Annual Condition Inspection Checklist

MEMO AIRBUS A319/A320/A321. SOP / Flow Pattern

FLIGHT CONTROLS 1. GENERAL 2. MAIN COMPONENTS AND SUBSYSTEMS ROLL CONTROL. Smartcockpit.com BOEING 737 SYSTEMS REVIEW Page 1

Cessna Citation 500/501 Pilot s Technical Examination

SINGLE ENGINE PISTON AEROPLANE ENDORSEMENT

Electro-Mechanical Landing Gear System. Landing Gear and Brakes

FLYBLOCKTIME PA /160 Aircraft Type Checkout and Currency Quiz. NOTE: There may be one or more correct answers to each question.

ELECTRICAL. Primary electrical power is provided by two engine driven generators which supply three-phase, 115 volt 400 cycle alternating current.

S-Tec System Thirty Autopilot

AIR - PNEUMATIC, AIR CONDITIONING, PRESSURIZATION

AIR CONDITIONING & PRESSURIZATION

OPERATING LIMITATIONS

B777. Landing Gear DO NOT USE FOR FLIGHT

Municipal Airport 1410 Arizona Place S.W. Orange City, IA

Hydraulic Landing Gear System

PROPELLER OPERATION AND MALFUNCTIONS BASIC FAMILIARIZATION FOR FLIGHT CREWS

CUB CRAFTERS, INC. CC PILOT S OPERATING HANDBOOK AND FLIGHT TRAINING SUPPLEMENT

SERIOUS INCIDENT. Aircraft Type and Registration: No & Type of Engines: 2 SNECMA CFM 56-7B turbofan engines. Year of Manufacture: 1999

FLIGHT REFERENCE CARDS

Multi-Engine Training And The PTS

Section 9. Pitot Static System. 1 of 6

B777. Automatic Flight DO NOT USE FOR FLIGHT

Bombardier Challenger Air Conditioning & Pressurization

Nomad WINGS FLAP OPERATING LIMITATIONS

VFR Day Emergencies - C172R

File Number MDRA C20 MANUAL of PROCEDURES for INSPECTION of COMPOSITE AMATEUR-BUILT AIRCRAFT, INSPECTION AND TECHNICAL INFORMATION RECORD

TYPE CERTIFICATE DATA SHEET Nº EA-2011T03 Type Certificate Holder: COSTRUZIONI AERONAUTICHE TECNAM S.r.l. Via Tasso, Napoli Italy

MODULE 11B. PISTON AEROPLANE AERODYNAMICS, STRUCTURES AND SYSTEMS

Pneumatic Air Conditioning Pressurization

This section includes performance data on the King Air B200. Information consists of:

DA Katana 4X Manual. This Chapter provides description and operation of the airplane and its systems.

2013 Airborne Aviation Pty Ltd

FUEL. Fuel is contained in three tanks located within the wings and wing center section.

AIRCRAFT GENERAL GTM CONTENTS

McCAULEY FULL FEATHERING CONSTANT SPEED PROPELLER GOVERNING SYSTEM. Professor Von Kliptip Answers Your Questions About The

CIRRUS AIRPLANE MAINTENANCE MANUAL

Chapter 21 Air Conditioning

B 737 NG El ectrical

06 HYDRAULICS, FLIGHT CONTROLS, LANDING GEAR, BRAKES

Cessna 172SP & NAV III Maneuvers Checklist

BE76 Beechcraft Duchess Maneuvers Checklist

Cherokee Archer II Pilot s Operating Handbook

FLIGHT TRAINING (AEROPLANE) BASED ON JAR FCL - PPL(A) FLIGHT INSTRUCTION Syllabus

This file contains the full script of the corresponding video, published on YouTube. November 2014:

Light Sport West Standard Flight Training Procedures for N110GX (Remos GX, 100 H.P.)

Multi-information Display (see MID )

CHAPTER 10 PARKING AND STORAGE. Section Title Page

2014 NIFA CRM Contestant Briefing Guide San Diego, California

Introduction to Aircraft Design and Aviation Systems (ENG3005)

Aerosoft HUEY X 1.00 manual

Operational Overview and Controls Guide. Two or Three Pump IronHeart Lite with Variable Frequency Drives

Operating Instructions Display, graphic. Numeric language

Airbus A319/320/321 Notes

EDUCATION IS THE KEY TO SUCCESS Aviation Maintenance Training School (AMT School)

The following information is an exert from THE CESSNA 182 TRAINING MANUAL, Oleg Roud and Danielle Bruckert

MCR-01 Ultralight. AFS-design. Andreas Meyer

SPECIFICATIONS & PRICE LIST 2016

Automation at Odds. A 737 stalled when a radio altimeter malfunction caused the autothrottle and autopilot to diverge during an approach to Schiphol.

09 FLIGHT MANAGEMENT, NAVIGATION

NOTICE. Dec 2/96 CESSNA AIRCRAFT COMPANY ORIGINAL ISSUE - 2 DECEMBER 1996

Electrical Systems - IQAN Digital Control System. IQAN Control System Components

The SeaRey - An Introduction

Alarm and Detection/Suppression

Multi-Engine Class Rating

Phoenixtech Brushless Motor Speed Controller Programming Guide

ENGINE FIRE / SEVERE DAMAGE / SEPARATION ON TAKEOFF

For Information Only-Not approved for cockpit use.

Introduction. The Normal Takeoff. The Critical Engine. Flying Light Twins Safely

Mathematically Modeling Aircraft Fuel Consumption

THERMO KING TRUCK & TRAILER UNIT ALARM CODES THIS DOCUMENT SHOWS ALL CURRENT ALARM CODES FOR THERMO KING TRUCK AND TRAILER UNITS.

AIRCRAFT SYSTEMS EQUIPMENT

Signature and ISX CM870 Electronics

ACCUMULATOR INSTALLATION

Revision Number Revision Date Insertion Date/Initials 1 st Ed. Feb 01, 00 2 nd Ed. Jun 24, 02 3rd Ed. Feb 15, 07

737 NG Comm unications

TECNAM P2002JF. Specification & Description INTRODUCTION

GROUND OPERATIONS MANUAL

SUPPLEMENTARY INFORMATION FOR FLIGHT STUDENTS

FLIGHT TEST SCHEDULE. Pagina 1 of 5. Examiner(s): TRAINING/SKILL TEST/PROFICIENCY CHECK. single pilot aeroplanes (except HPA complex aeroplanes)

CHAPTER 11 MARKING AND PLACARDS

FFS A340 - MALFUNCTION LIST BY A/C SUB-SYSTEMS

Transcription:

King Air C90A Speeds (KIAS) V MCA 90 V SSE 97 V X 101 V Y 111 V XSE 100 V YSE 107 V A 169 V REF 100 V MO 208 V FE 178 35% 137 100% V LE 156 129 Retraction only Other 95 Balked landing climb 125 Glide 161 Turbulent air Cruise climb 150 To 10 000 130 10 000 to 20 000 120 20 000 to 25 000 110 25 000 to 30 000 Note: V MCA and V Y are not indicated on ASI. Take-off Speeds Weight (lbs) Take-off speeds (KIAS) Rotate At 50 9650 97 106 9500 96 105 9000 95 104 8500 94 103 8000 92 102 BE90 (C90A) Checklist V 1.2 1

King Air C90A Normal Checklist Before starting engines Cabin door: Locked Load and baggage: Secure Weight and CG: Checked * Emergency exit: Latched Cabin seats: Positioned (outboard), backs upright Control locks: Remove Seat belts and harnesses: Fastened Parking brake: Set Pedestal circuit breakers: In Overhead panel: Check Oxygen control: Pull on, check mask flow, push off R sidepanel CBs: Check * Oxygen system pressure: Check (see manual) * Emergency static source: Normal R subpanel CBs: Check Cabin Temp Mode: Off Landing gear handle: Down Condition levers: Cut off Propeller levers: High RPM Power levers: Idle L subpanel switches: Off Fuel panel: Check * CBs: In * Firewall valves: Closed * Crossfeed: Open Boost pumps: On (check sound) Battery switch: On FUEL PRESS ann.: Check on Firewall valves: Open FUEL PRESS ann.: Check off Transfer pumps: On (check sound), Off If no Xfer pump: Xfer test, no annunciator Fire detectors: Check Voltmeters: Check Cabin signs: FSB or NS&FSB BE90 (C90A) Checklist V 1.2 2

Engine Start (Battery) R ign/start: On R IGN ON: Check illuminated Stable N 1 > 12%: Wait R condition lever: Low idle ITT and N 1 : Monitor (1090 C max., rise in 10 s) R oil pressure: Check R condition lever: High idle Wait: N 1 = 51% R ign/start: Off R generator: Reset, On Charge battery: Load = 0,5, max. 5 min. (R generator: Off) L ign/start: On L IGN ON: Check illuminated Stable N 1 > 12%: Wait (R generator: On) L condition lever: Low idle ITT and N 1 : Monitor (1090 C max., rise in 10 s) L oil pressure: Check L ign/start: Off L generator: Reset, On R condition lever: Low idle After start Transfer pumps: On Crossfeed: Auto DC Voltage/Load: Check Inverter: Check both, select Avionics master: On Lights: As required Fuel control heat: Heat Cabin temp/mode: As required (Check N 1 /ITT/load) Annunciators: Test, clear Instruments: Check BE90 (C90A) Checklist V 1.2 3

Taxi Brakes: Check Gyros: Check Before takeoff (Runup) Boost pumps and auto crossfeed: Test L Boost: Off (L FUEL PRESS off, XFEED on) L Boost: On Crossfeed: Closed, then Auto R Boost: Off (R FUEL PRESS off, XFEED on) R Boost: On Crossfeed: Closed, then Auto Avionics and Radar: Check Pressurisation: Check, set (alt.+500/cabin 500agl, rate) * Autopilot: Check, then off Electric trim: Check (tab control, wheel switch) Trim: Set Engine frictions: Set Flaps: Check, set Flight controls: Full, free, correct * Autofeather: Check Power: 500 ft-lbs Autofeather: Hold to test Power levers: Retard each (400: ann. 260: fthr) Power: Retard (both ann. out, no feather) Autofeather: Arm * Overspeed governors: Test Propellers: Full forward Power levers: Below 1900 rpm Overspeed governor test: Hold to test Power: Increase to limit, watch ITT/Tq Power: Reduce to 1900 rpm Overspeed governor test: Release * Primary governors: Exercise at 1900 rpm * Engine ice protection: Pull, push; check Tq Gyro suction, pneumatic pressure: Check Power: Idle Propeller: Check feathering Fuel, flight engine instruments: Check (oil temp!) BE90 (C90A) Checklist V 1.2 4

Before takeoff (ready to go) Bleed air valves: Open Annunciators: Out/considered Transponder: On Prop synchrophaser: As required Strobes: On Ice protection: As required Auto-ignition: Armed During takeoff run Autofeather annunciators: Check illuminated Ignition On annunciators: Check extinguished Engines: Check ITT/Tq in limits After takeoff Landing gear: Up Flaps: Up Engines: Climb power set, check limits Props: Set Synchrophaser: On Autofeather: Off Engine instruments: Monitor Cabin sign: As required Cabin pressurisation: Check Descent Pressurisation: Set cabin altitude (table), Rate Altimeter: Set Cabin sign: As required Windshield anti-ice: As required Power: As required Pressurisation Settings: QNH 970 980 990 1000 1010 1020 1030 1040 1050 Above 1800 1500 1200 900 600 300 0-300 -600 Interpolate or use next lower QNH. Default 500. BE90 (C90A) Checklist V 1.2 5

Before landing Pressurisation: Check Cabin sign: FSB or NS/FSB Prop autofeather: Arm Prop synchrophaser: As desired Flaps: Approach Landing gear: Down Lights: As required Radar: Standby or off Short final: Props: High rpm Power: Beta or reverse Remove reverse at 40 kts Balked landing Power: Maximum Props: Full forward Airspeed: 95 kts until clear of obstacles Flaps: Up Gear: Up After landing Landing and taxi lights: As required Ice protection: Off Auto-ignition: Off Electrics: Observe load limits Trim: Set Flaps: Up Transponder and radar: Off Strobes: Off BE90 (C90A) Checklist V 1.2 6

Shutdown Parking brake: Set Transfer pumps: Off Crossfeed: Closed Inverter: Off Avionics master: Off Autofeather: Off Cabin mode: Off Blower: Auto Subpanel and avionics: Off Oxygen supply: Off Battery: Charged ITT: Below 585 C for 1 min Condition levers: Cut-off Props: Feather Wait: N 1 < 10% Boost pumps: Off DC Volt/Load: Check voltage Overhead panel switches: Off Battery/Gen bar: Off Control locks: Install Park brake: Off External covers: Install BE90 (C90A) Checklist V 1.2 7

C90A Abnormal Checklist Air start (Starter) Cabin temp: Off, Blower: Auto Radar: Standby or Off Windshield heat: Off Power lever: Idle Condition lever: Cut-off Fuel panel: Check Fuel firewall valve: Open Boost pump: On Transfer pump: On Crossfeed: Auto Ign./engine start: On, check IGN annunciator Wait: 8 s Condition lever: Low idle Fuel control heat: On Electrical equipment: As required Air start (windmilling) Cabin temp: Off, Blower: Auto Radar: Standby or Off Windshield heat: Off Power lever: Idle Propeller: 2200 rpm Condition lever: Cut-off Fuel panel: Check Fuel firewall valve: Open Boost pump: On Transfer pump: On Crossfeed: Auto Generator (inop. engine): Off Airspeed: 140 kts minimum Altitude: Below 20 000 ft Auto-ignition switch: On Wait: 8 s Condition lever: Low idle Wait: ITT peaks Auto-ignition switch: Off Fuel control heat: On Electrical equipment: As required BE90 (C90A) Checklist V 1.2 8

Landing gear manual extension Airspeed: 120 KIAS Ldg Gr circuit breaker (copilot panel): Pull Landing gear handle: Down Emergency engage handle: Lift, clockwise Extension lever: Release clip, pump until 3 greens Landing gear up after manual ext. Emergency engage handle: CCW, push down Extension lever: Stow Ldg Gr circuit breaker: Push in Landing gear: Up Zero thrust Propeller: 1800 rpm Power lever: Set Tq = 100 ft-lbs BE90 (C90A) Checklist V 1.2 9

C90A Emergency Checklist Engine shutdown Condition lever: Cut-off Prop lever: Feather Fuel firewall valve: Closed Fire extinguisher: Actuate if required Clean up (inop. engine): Bleed air valve: As required Engine auto ignition: Off Boost pump: Off Fuel transfer pump: Off Crossfeed: Closed Generator: Off Fuel control heat: Off Autofeather: Off Synchrophaser: Off Electrical load: Monitor Engine fire on ground Condition lever: Cut-off Fuel firewall valve: Closed Starter switch: Starter only Boost pump: Off Fuel transfer pump: Off Crossfeed: Closed Fire extinguisher: Actuate (if required) Engine failure during ground roll Power levers: Idle Brakes: As required If insufficient runway for stopping: Condition levers: Cut-off Fuel firewall valves: Closed Master switch: Off with gang bar Boost pumps: Off BE90 (C90A) Checklist V 1.2 10

Engine failure after lift-off (can t land) Power: Max. allowable Prop RPM: Full increase Airspeed: Maintain (takeoff speed or above) Landing gear: Up Power lever (inop. engine): Idle after autofeather Propeller (inop. engine): Feather Airspeed: VYSE (after obstacles cleared) Clean-up (inop. engine): Condition lever: Cut-off Bleed air valve: As required Engine auto ignition: Off Fuel firewall valve: Closed Boost pump: Off Fuel transfer pump: Off Crossfeed: Closed Generator: Off Fuel control heat: Off Autofeather switch: Off Synchrophaser: Off Electrical load: Monitor 2nd engine flame-out Power lever: Idle Propeller: Do not feather Condition lever: Cut-off Conduct air start BE90 (C90A) Checklist V 1.2 11

Smoke and fumes: Electrical Oxygen: Handle On, Connect/don masks Cabin temp mode: Off Vent blower: Auto Avionics master: Off Nonessential electrical equipment: Off If fire or smoke ceases: Individually turn on equipment to isolate If fire or smoke persists: Cabin pressure switch: Dump Land as soon as practical Smoke and fumes: Environmental Oxygen: Handle On, Connect/don masks Cabin temp mode: Off Vent blower: Auto Left bleed valve: Closed If smoke decreases: Continue operation If smoke does not decrease: Left bleed valve: Open Right bleed valve: Closed If smoke decreases: Continue operation Emergency descent Power levers: Idle Prop controls: Full high RPM Wing flaps: Approach Landing gear: Down Airspeed: 156 KIAS (V LE ) Glide Landing gear: Up Wing flaps: Up Try restart before feathering both Propellers: Feather Airspeed: 125 KIAS BE90 (C90A) Checklist V 1.2 12

Boost pump failure Identified by CROSSFEED On Crossfeed: Momentarily off Identify failed pump Inoperative pump: Off Consider continued flight: Lower power setting Lower altitude Cool fuel 10 h maximum Crossfeed Fuel boost pumps: On Transfer pumps: On Crossfeed: Open, check CROSSFEED ann. on Boost pump (non-feeding side): Off, check ann. Crossfeed Off Fuel boost pumps: Both on Crossfeed switch: Closed Fuel boost pump (inop. eng.): Off Circuit breaker tripped Nonessential circuit: Do not reset in flight Essential circuit: Push to reset, once only Subpanel feeder circuits: Do not reset in flight Pressurisation differential in red Cabin altitude selector: Select higher setting If condition persists: Bleed air valves: Closed Cabin pressure switch: Dump Bleed air valves: Open Cracked windshield Outer panel: No action required Inner panel: Descend or < 3 PSI differential in 10 mins. BE90 (C90A) Checklist V 1.2 13