KING AIR 200 Flashcards

Question

**ENHANCED GROUND PROXIMITY** **WARNING SYSTEM (EGPWS)** GPWS WARNING (RED [PULL UP] ON PFD AND CONTINUOUS “PULL UP, PULL UP” VOICE WARNING) EGPWS TERRAIN WARNING (RED [PULL UP] ON PFD AND “TERRAIN, TERRAIN, PULL UP” OR “OBSTACLE, OBSTACLE, PULL UP” VOICE WARNING)

Answer 1

**In IMC or at Night:** ## Footnote 1. Wings .......................... LEVEL 2. Power ........................ MAX ALLOWABLE 3. Pitch ............................INCREASE * Promptly and smoothly increase pitch towards an initial pitch attitude of 20°–25°. * Adjust as required to avoid continuous buffeting and/or stall warning. * Adjust to maintain 100 KIAS. 4. Gear and Flaps ................. UP

Answer 2

Engine Oil Limitations Oil Temp for Starting .................... **–40°C** (Min) Oil Press for Idle RPM ................... **60 PSI** (Min) Oil Press Maximum Transient .............. **200 PSI**

Answer 3

ENGINE LIMITS Oil (°C/PSI) Oil Temp Takeoff & Max Continuous Thrust ........... **0—99°** C (55° C Recommended) Oil Press Takeoff & Max Continuous Thrust ..... **100 - 135 PS**I

Answer 4

PROPELLER LIMITS Idle ......................... **1180 RPM** Takeoff & Max Continuous ..... **2000 RPM** Transient .................... **2200 RPM**

Answer 5

EXTERNAL POWER LIMITS ## Footnote Volts .................... **28.0 – 28.4** Amps ..................... **1000** (Momentarily) **300** (Continuous)

Answer 6

Maximum sustained generator load is limited as follows: In-Flight: Sea Level to 31,000 Feet Altitude ........... **100**% Above 31,000 Feet Altitude ................... **88**% Ground Operation ............................. **85**%

Answer 7

Starter Limitations Duration On/Off .............. 40 seconds ON, 60 seconds OFF 40 seconds ON, 60 seconds OFF 40 seconds ON, **30 minutes OFF**

Answer 8

FUEL LIMITS Approved Engine Fuels Commercial Grades Military Grades * Jet A • Jet A-1 • Jet B * JP-4 • JP-5 • JP-8 * Chinese Jet Fuel No. 3

Answer 9

FUEL LIMITS ## Footnote Emergency Engine Fuels ............. 80 Red (Formerly 80/87) 100 Green (Formerly 100/130) 100LL Blue (100L Green) 91/96 115/145 Purple

Answer 10

FUEL LIMITS Emergency Engine Fuels - Limitations on the Use of Aviation Gasoline: 1. Operation is limited to 150 hours between engine overhauls. 2. Operation is limited to 20,000 feet pressure altitude (FL 200) or below if either standby pump is inoperative. 3. Crossfeed capability is required for climbs above 20,000 feet pressure 4. Operation above 31,000 feet (FL 310) is prohibited.

Answer 11

FUEL MANAGEMENT Usable Fuel (Gallons x 6.7 = Pounds) Total Usable Fuel Quantity ........ **544** gallons (**3,645** lb) * Each Main Fuel Tank System ..**193** gallons (**1,293** lb) * Each Auxiliary Fuel Tank ...........**79** gallons (**529** lb)

Answer 12

FUEL MANAGEMENT ## Footnote Maximum Imbalance ........... **1000** LB Fuel Crossfeed ...... Permitted only when **one engine is inoperative.**

Answer 13

FUEL MANAGEMENT Takeoff is not allowed with: Indication ................ **IN THE YELLOW ARC** Amount of Fuel ............ **LESS THAN 265 LB ** in each main tank system

Answer 14

1. Maintain Airplane Control. 2. AP/TRIM Disconnect ...........DEPRESS TO 1ST LEVEL TO CANCEL HORN

Answer 15

VFE/VFO (Approach) .............200 KIAS VFE/VFO (Full Down) ............157 KIAS

Answer 16

AIRSPEED LIMITATIONS Maximum Landing Gear Speeds (VLO/VLE) (KIAS at 12,500 lb) VLO (Extension) ...............181 KIAS VLO (Retraction) ..............163 KIAS VLE ...........................181 KIAS

Answer 17

AIRSPEED LIMITATIONS Air Minimum Control Speed (VMCA) (Red Line) 86 KIAS

Answer 18

AIRSPEED LIMITATIONS Maximum Operating Speeds VMO ................. 259 KIAS MMO ................. Mach .52

Answer 19

AIRSPEED LIMITATIONS Top of Low Speed Cue (LSC) VS0 (Max weight with flaps down and idle power) .....75 KIAS VS1 (Max weight with flaps approach and idle power) 85 KIAS VS1 (Max weight with flaps up and idle power) ......... 99 KIAS

Answer 20

EMERGENCY AIRSPEEDS VXSE (One-Engine-Inoperative Best Angle-of-Climb) VXSE ** 115 KIAS** VYSE (One-Engine-Inoperative Best Rate-of-Climb)(Blue Line) VYSE ** 121 KIAS** One-Engine-Inoperative Enroute Climb **121 KIAS**

Answer 21

EMERGENCY AIRSPEEDS Emergency Descent ..................**181** KIAS Maximum Range Glide ................**135** KIAS

Answer 22

Do not lift power levers in flight. Lifting the power levers in flight, or moving the power levers in flight below the flight idle position, could result in a nose-down pitch and a descent rate leading to aircraft damage or injury to personnel.

Answer 23

ENGINE LIMITS Torque — Takeoff, Max Continuous ......**2230 FT Lbs** Torque — Transient ....................**2750 FT lbs**

Answer 24

ENGINE LIMITS N1 — Takeoff, Max Continuous .........**101.5 %** N1 — Transient .......................**102.6 %**

Answer 25

ENGINE LIMITS ITT Temp (°C) Start ............................. **1000°C** Takeoff / Max Continuous .......... **800°C** Cruise Climb / Normal Cruise ...... **770°C** Transient ......................... **850°C**

Answer 26

FUEL LIMITS Approved Engine Fuels Commercial Grades Military Grades **Jet A • Jet A-1** **JP-4 JP-5 Jet B JP-8** **Chinese Jet Fuel No. 3**

Answer 27

AUXILIARY FUEL Do not put any fuel into the auxiliary tanks unless the main tanks are full.

Answer 28

OPERATING WITH LOW FUEL PRESSURE OR Time until overhauling or replacement of the affected engine driven fuel pump ...............................**10 Hours**

Answer 29

PROPELLER ROTATIONAL SPEED LIMITS Transients not exceeding 5 seconds ...........**2200 rpm** Reverse .......................................**1900 rpm** All other conditions ..........................**2000 rpm** Minimum idle speed ............................**1180 rpm**

Answer 30

PROPELLER ROTATIONAL OVERSPEED LIMITS Sustained above 2000 RPM (Primary Governor Failure): Torque Limit ............................. **1800 ft lbs** Sustained above 2120 RPM (Not Approved) (Primary Governor & Overspeed Governor Failure): Maximum Overspeed .........................**2200 rpms** Time Limit ..............................................**5 seconds**

Answer 31

PROPELLER AUTOFEATHER ## Footnote The propeller autofeather system must be operable for all flights and must be armed for takeoff, climb, approach and landing.

Answer 32

WEIGHT LIMITS ## Footnote Maximum Ramp Weight ..........................**12,590 lbs** Maximum Takeoff Weight: All Except 14 CFR Part 135 Operations ........**12,500 lbs** Maximum Landing Weight .......................**12,500 lbs** Maximum Zero Fuel Weight .....................**11,000 lbs**

Answer 33

WEIGHT LIMITS Maximum Weight in Baggage Compartment: When Equipped With Fold-Up Seats ............. **510 lbs** When Not Equipped With Fold-Up Seats ......... **550 lbs**

Answer 34

MAXIMUM OPERATING PRESSURE-ALTITUDE LIMITS ## Footnote Normal Operation ............................ **35,000 ft** Operation with Yaw Damp System Inoperative .. **17,000 ft**

Answer 35

MAXIMUM OUTSIDE AIR TEMPERATURE LIMITS ## Footnote Sea Level to 25,000 Feet Pressure Altitude .....**ISA + 37°C** Above 25,000 Feet Pressure Altitude ............**ISA + 31°C**

Answer 36

CABIN PRESSURIZATION LIMIT Maximum Cabin Pressure Differential ..........**6.6 psi**

Answer 37

Landing Gear Cycle Limits ## Footnote Landing gear cycles (1 up–1 down) are limited to **one every 5 minutes for a total of 6 cycles** followed by a **15 minute** cool-down period.

Answer 38

Aft-Facing Seats ## Footnote The seat back of each occupied aft-facing seat must be in the upright position and the headrest fully extended for takeoff and landing.

Answer 39

SYSTEMS AND EQUIPMENT LIMITS Brake Deice (If Installed) Brake Deice system is not to be operated above **15°C.**

Answer 40

ICING LIMITATIONS Min Ambient Temperature for Operation of Deicing Boots **–40°C** Min Airspeed for Sustained Icing Flight .........**140 KIAS**

Answer 41

ICING LIMITATIONS - Flight with Flaps Extended ## Footnote Sustained flight in icing conditions with flaps extended is prohibited except for approach and landings.

Answer 42

ICING LIMITATIONS - Engine Anti-Ice When flight free of visible moisture cannot be assured: ON ..............................**+5°C** or below Takeoff and Flight Operations: OFF .............................Above **+15°C**

Answer 43

1. Operating in the composite mode is limited to training and display failure conditions. 2. The pilot’s and copilot’s Air Data Computers must be operative for takeoff. 3. AHRS 1 and 2 must be operative for takeoff. 4. The pilots PFD and MFD and copilot PFD must be installed and operational in the normal mode for takeoff. 5. The MFD must be operational prior to engine start.

Answer 44

AUTOPILOT - Pre Flight Check ## Footnote 1. An autopilot preflight check must be conducted and found satisfactory prior to each flight on which the autopilot is to be used.

Answer 45

AUTOPILOT ## Footnote The autopilot minimum engage height after takeoff is **400** feet AGL.

Answer 46

AUTOPILOT ## Footnote The autopilot minimum use height during cruise is **1000 feet AGL.**

Answer 47

AUTOPILOT ## Footnote The autopilot minimum use height during approach is **79 feet AGL.**

Answer 48

AUTOPILOT The maximum coupled intercept angles are: * Nav and Localizer — **Less than 90°** * Back Course — **70°**

Answer 49

VNAV - Limitations ## Footnote 1. VNAV altitudes must be displayed on the MFD map page or CDU legs page when utilizing VNAV for flight guidance. 2. VNAV approach guidance to a DA is not authorized if the reported surface temperature is below the Baro-VNAV minimum temperature limitation specified on the applicable RNAV approach procedure chart.

Answer 50

ENHANCED GROUND PROXIMITY WARNING SYSTEM (EGPWS) ## Footnote 1. Within 15 NM of an airport not listed in the database during: a. Takeoff b. Approach c. Landing 2. FMS is operating in the DR mode.