Beechcraft 200 King Air POH Pilots operating handbook

ISSUED: April 29, 2009 Revision IR: April 29, 2009 Document No. 09EA-52-116 FAA-APPROVED PILOT’S OPERATING HANDBOOK and Airplane Flight Manual Supplement for the SUPER KING AIR MODELS 200/200C/B200/B200C Equipped with Enhanced Aero: • PT6A-52 Engines – STC SA10842SC -AND- Equipped with Raisbeck Engineering: • Quiet Turbofan Propellers – STC SA2698NM-S • Ram Air Recovery System – STC SA3366NM • Enhanced Performance Leading Edges – STC SA3831NM • Dual Aft Body Strakes – STC SA3519NM • Fully Enclosed MLG Doors (when HFG-Equipped) – STC SA4175NM OR • Quiet Turbofan Propellers – STC SA2698NM-S • MARK VI System – STC SA1783NM • Fully Enclosed MLG Doors (when HFG Equipped) – STC SA1668NM

BEECHCRAFT Super King Air 200/B200 Series Equipped with • Enhanced Aero -52 Engines • Quiet Turbofan Propellers • Ram Air Recovery System • Enhanced Performance Leading Edges • Dual Aft Body Strakes • Fully Enclosed MLG Doors (when HFG-equipped) Document No. 09EA-52-116 FAA-Approved : Revision IR: April 29, 2009 iii TABLE OF DIVISIONS SECTION I.......................................................................GENERAL SECTION II.................................................................LIMITATIONS SECTION III.....................................EMERGENCY PROCEDURES SECTION IV............................................NORMAL PROCEDURES SECTION V...........................................................PERFORMANCE SECTION VI.............................................WEIGHT AND BALANCE SECTION VII.............................................SYSTEM DESCRIPTION

Document No. 09EA-52-116 BEECHCRAFT Super King Air 200/B200 Series Equipped with: • Enhanced Aero -52 Engines • Quiet Turbofan Propellers • Ram Air Recovery System • Enhanced Performance Leading Edges • Dual Aft Body Strakes • Fully Enclosed MLG Doors (when HFG-equipped) iv FAA-Approved : Revision IR: April 29, 2009 This page intentionally left blank.

BEECHCRAFT Super King Air 200/B200 Series Equipped with • Enhanced Aero -52 Engines • Quiet Turbofan Propellers • Ram Air Recovery System • Enhanced Performance Leading Edges • Dual Aft Body Strakes • Fully Enclosed MLG Doors (when HFG-equipped) Document No. 09EA-52-116 Section I – General Reference Material : Revision IR: April 29, 2009 1-1 SECTION I – GENERAL INTRODUCTION Thank you… for displaying your confidence in selecting quality products from Raisbeck Engineering Inc. Our design engineers, craftsmen, and technicians have utilized their professional skills and years of experience to provide you with state-of-the-art systems to enhance the performance, safety, and productivity of your Super King Air. The information contained in this FAA-approved Pilot’s Operating Handbook and Airplane Flight Manual Supplement highlights the areas of performance improvements to the propeller, air induction system, engine compartment, wing, and external drag items that increase the performance and productivity of your Beechcraft Super King Air200/ B200 across a broad spectrum of flight conditions. Your Raisbeck-equipped Super King Air also has FAA-approved enhanced performance in those flight regimes involving safety of flight such as take-off, flight in icing conditions, flight with one engine inoperative, approach and landing. This supplement is designed to facilitate maintaining the documents necessary for the efficient operation of your airplane. It has been prepared in loose-leaf form for ease in maintenance, and incorporates quick reference tabs for each section. After you have operated your Raisbeck-Equipped Super King Air 200/ B200 for a period of time, we would like to hear your comments regarding our systems in service with your operation. Please feel free to contact us at any time by mail or telephone. Raisbeck Engineering Inc. 4411 South Ryan Way Seattle, Washington 98178 U.S. 800-537-7277 Intl. 1-206-723-2000 FAX 206-723-2884 www.raisbeck.com FAA-approved information, limitations, performance and data are on pages marked at the bottom “FAA-Approved: Revision Level and Date”

Document No. 09EA-52-116 Section I – General BEECHCRAFT Super King Air 200/B200 Series Equipped with: • Enhanced Aero -52 Engines • Quiet Turbofan Propellers • Ram Air Recovery System • Enhanced Performance Leading Edges • Dual Aft Body Strakes • Fully Enclosed MLG Doors (when HFG-equipped) 1-2 Reference Material : Revision IR: April 29, 2009 This page intentionally left blank.

BEECHCRAFT Super King Air 200/B200 Series Equipped with • Enhanced Aero -52 Engines • Quiet Turbofan Propellers • Ram Air Recovery System • Enhanced Performance Leading Edges • Dual Aft Body Strakes • Fully Enclosed MLG Doors (when HFG-equipped) Document No. 09EA-52-116 Section II – Limitations FAA-Approved : Revision IR: April 29, 2009 2-1 SECTION II – LIMITATIONS NOTE: For aircraft with temporary repair installed per Beechcraft Service Bulletin No. 2040, Beechcraft Pilot’s Operating Handbook must be used for all performance data in Section V until the aircraft has been permanently repaired per the Beech Service Bulletin. AIRSPEED LIMITATIONS Air Minimum Control Speed V MCA FLAPS KIAS KCAS Up 91 96 Approach 88 92 Down 78 83 This is the lowest airspeed at which the airplane is directionally controllable when one engine suddenly becomes inoperative and the other engine is at take-off power. V MCA was determined with a 5º bank into the operating engine and the propeller feathered on the inoperative engine. AIRSPEED INDICATOR MARKINGS: 200 series aircraft red radial at 96KCAS air minimum control speed (V MCA ). B200 series aircraft red radial at 91KCAS. AIRSPEED INDICATOR DISPLAY (Collins Pro Line 21 Equipped Aircraft Only): DISPLAY KIAS VALUE OR RANGE SIGNIFICANCE Red Line 91 Air Minimum Control Speed (V MCA ) Solid Red Bar (at bottom of airspeed scale) ISS LSC # Marker. The top of marker changes with flap position to reflect the following stall speeds. 71 Stalling Speed (V S0 ) at maximum weight with flaps down. 83 Stalling Speed (V S1 ) at maximum weight with flaps approach. 91 Stalling Speed (V S1 ) at maximum weight with flaps up.* # Impending Stall Speed Low Speed Cue * Values are conservative. See performance section for approved stall speed chart.

Document No. 09EA-52-116 Section II – Limitations BEECHCRAFT Super King Air 200/B200 Series Equipped with: • Enhanced Aero -52 Engines • Quiet Turbofan Propellers • Ram Air Recovery System • Enhanced Performance Leading Edges • Dual Aft Body Strakes • Fully Enclosed MLG Doors (when HFG-equipped) 2-2 FAA-Approved : Revision IR: April 29, 2009 POWER PLANT LIMITATIONS ENGINE OPERATING LIMITS: Operating Conditions………………………….. Low Idle Gas Generator RPM N 1………... 22,500 RPM 60% (min.) Prop RPM……………………………..…… 1,150 (min.) NUMBER OF PROPELLERS: Two (2) PROPELLER MANUFACTURER: Hartzell Propeller Inc. PROPELLER HUB AND BLADE MODEL NUMBERS: Hub: HC-D4N-3A Blades: D9383K PROPELLER DIAMETER: Maximum Diameter: 94.0 inches Minimum Diameter: 93.0 inches PROPELLER BLADE ANGLES AT 30-INCH STATION: Feathered: 86º ± 2º Reverse: 10.5º ± 1º PROPELLER ROTATIONAL SPEED LIMITS: Continuous Operation on Ground – 1150 RPM minimum CAUTION Stabilized ground operation between 400 and 1,150 propeller RPM is prohibited. Operation between 0 and 400 propeller RPM is permissible only with propeller feathered. WARNING STABILIZED GROUND OPERATION WITHIN THE PROPELLER RESTRICTED RPM RANGE CAN GENERATE HIGH PROPELLER STRESSES AND RESULT IN PROPELLER FAILURE AND LOSS OF CONTROL OF THE AIRCRAFT. PROPELLER DE-ICE AMMETER: Green Arc (normal operating range) – 18 to 24 amperes. AUTO FEATHERING SYSTEMS: The Beech Propeller Autofeathering System must be installed, operational, and armed for takeoff, climb and approach. CAUTION With one-engine either at idle or inoperative, flaps up and propeller windmilling, V MCA may be as high as 108 KIAS.

BEECHCRAFT Super King Air 200/B200 Series Equipped with • Enhanced Aero -52 Engines • Quiet Turbofan Propellers • Ram Air Recovery System • Enhanced Performance Leading Edges • Dual Aft Body Strakes • Fully Enclosed MLG Doors (when HFG-equipped) Document No. 09EA-52-116 Section II – Limitations FAA-Approved : Revision IR: April 29, 2009 2-3 MAXIMUM OPERATING PRESSURE – ALTITUDE LIMITS: Yaw Damper Inoperative The yaw damper is no longer a requirement for flight up to the ceiling capability of the airplane when it is equipped with the Raisbeck Engineering Dual Aft Body Strakes. Therefore, all altitude limitations presented in the basic Beechcraft Pilot’s Operating Handbook and Flight Manual for yaw damper inoperative are removed. ICE VANES (INERTIAL SEPERATOR SYSTEM) LIMITATIONS: The aircraft can be operated with the inertial separator ice vanes deployed during ground and flight operations, at ambient temperatures up to, and including ISA + 27 ºC, below 13,650 feet or + 15 ºC above 13,650 feet, provided: 1. All other engine limits are observed. 2. During ground operations, oil temperatures are monitored closely. If the oil temperature limits are reached, the ice vanes must b 3. e stowed until the oil temperatures return within limits.

Beechcraft 200 King Air POH Pilots operating handbook

You're Reading a Preview

Recently Viewed