Normal Procedures for the Beechcraft 1900C

Diameter is maximum 82 in., minimum 81.5 in. Pitch settings at 33 in. sta.: low 13.5°, high not under 30°. NOTE Other propellers are approved for the Bonanza K35 or M35 but not installed as original equipment. These are listed in the FAA Aircraft Specification 3A15 or approved by Supplemental Type Certificate. ENGINE INSTRUMENT MARKINGS OIL TEMPERATURE Caution (Yellow Radial) Operating Range (Green Arc) Maximum (Red Radial) Revised: June 1978 100°F/38°C 100° to 225°F/38° to 107°C 225°F/107°C 2-5 PERFORMANCE WT & BAL/EQUIP LIST NORMAL PROCEDURES GENERAL LIMITATIONS BEECHCRAFT Bonanza K35 and M35 Section II Limitations OIL PRESSURE Minimum Pressure (Red Radial) Operating Range (Green Arc) Maximum Pressure (Red Radial) TACHOMETER Operating Range (Green Arc) Maximum RPM (Red Radial} CYLINDER HEAD TEMPERATURE Operating Range BEECHCRAFT Bonanza K35 and M35 Section II Limitations 30 psi 30 to 60 psi 80 psi FUEL QUANTITY Yellow Band (44-gallon system). E to 1/2 full WEIGHT AND CENTER OF GRAVITY 1750 to 2600 rpm 2600 rpm Maximum Take-off Weight Maximum Ramp Weight Zero Fuel Weight 2950 lbs .2960 lbs No Structural Limitation Maximum Baggage Compartment (Green Arc) 200° to 460°F/93° to 238°C Maximum Temperature 460°F/238°C (Red Radial) MANIFOLD PRESSURE Operating Range (Green Arc) Maximum (Red Radial) INSTRUMENT VACUUM With Autopilot; 15 to 29.6 in. Hg 29.6 in. Hg Minimum (Red Radial) Operating Range (Green Arc) 3.75 in. Hg 3.75 to 4.25 in. Hg Maximum (Red Radial) 4.6 in. Hg Without Autopilot; Minimum (Red Radial) 4.4 in. Hg Operating Range (Green Arc) Maximum (Red Radial) …………… 4.8 to 5.2 in. Hg 5.5 in. Hg FUEL PRESSURE Minimum (Red Radial) 1.5 psi Operating Range (Green Arc) Maximum (Red Radial) 4 to 17 psi 17.5 psi 2-6 June 1975 Load.. Refer to Weight and Balance Section REFERENCE DATUM Datum is 83.1 inches forward of center line through forward jack points. MAC leading edge is 66.7 inches aft of datum. MAC length is 65.3 inches. CG LIMITS (Gear Down) Loading calculations shall be checked before each flight to ensure that the Weight and Center of Gravity remain within the approved limits during flight. Forward: 77.0 inches aft of datum to 2475 lbs with straight line variation to 82.1 inches at 2950 lbs. Aft: 85.7 inches aft of datum to 2525 lbs with straight line variation to 84.7 inches at 2950 lbs. MANEUVER LIMITS This is a utility category airplane. Spins are prohibited. No acrobatic maneuvers are approved except those listed below. Maximum slip duration is 30 seconds for airplanes with baffled main fuel cells in both wings and 20 seconds for airplanes with unbaffled main fuel cells in either wing. March, 1987 2-7 PERFORMANCE WT & BAL/EQUIP LIST NORMAL PROCEDURES LIMITATIONS GENERAL Section II Limitations BEECHCRAFT Bonanza K35 and M35 APPROVED MANEUVERS (2950 POUNDS) MANEUVER Chandelle Steep Turn Lazy Eight Stall (Except Whip) ENTRY SPEED (CAS) 123 knots/142 mph 123 knots/142 mph 123 knots/142 mph Use slow deceleration Minimum fuel for above maneuvers - 10 gallons each tank. Spins are prohibited. FLIGHT LOAD FACTORS (2950 POUNDS} Positive Maneuvering Load Factors BEECHCRAFT Bonanza K35 and M35 Section II Limitations the airplane such as galley equipment, entertainment systems, passenger convenience items, etc. However, it is important to note that ALL ITEMS WHICH ARE RELATED TO THE AIRWORTHINESS OF THE AIRPLANE AND NOT INCLUDED ON THE LIST ARE AUTOMATICALLY REQUIRED TO BE OPERATIVE. To enable the pilot to rapidly determine the FAA equipment requirements necessary for a flight into specific conditions, the following equipment requirements and exceptions are presented. It is the final responsibility of the pilot to determine whether the lack of, or inoperative status of a piece of equipment on his airplane, will limit the conditions under which he may operate the airplane. Flaps Up 4.4G 2.0G WARNING One (1) Pilot FLIGHT IN KNOWN PROHIBITED. ICING CONDITIONS Flaps Down MINIMUM FLIGHT CREW KINDS OF OPERATION LIMITS This airplane is approved for the following type operations when the required equipment is installed and operational as defined herein: 1. VFR day and night 2. IFR day and night 3. FAR 91 operations when all pertinent limitations and performance considerations are complied with. 2-8 WARNING FLIGHT IN ICING CONDITIONS IS PROHIBITED. NOTE Refer to "REQUIRED EQUIPMENT FOR VARIOUS CONDITIONS OF FLIGHT" at the end of this Section. August 1982 I I WT & BAL/EQUIP LIST PERFORMANCE NORMAL PROCEDURES LEGEND (-) Indicates that the item may be inoperative for the specified condition. (*) Refer to the REMARKS AND/OR EXCEPTIONS column for explicit information or reference. Revised: June 1978 2-9 LIMITATIONS GENERAL BEECHCRAFT Bonanza K35 and M35 SECTION III EMERGENCY PROCEDURES TABLE OF CONTENTS PERFORMANCE WT & BAL/EQUIP LIST SYSTEMS DESCRIPTION v NORMAL PROCEDURES SUBJECT PAGE Emergency Airspeeds 3-3 Engine Failure 3-4 During Take-Off Ground Roll After Liftoff and in Flight 3-4 3-4 Landing Emergencies Engine Discrepency Checks Rough Running Engine Loss of Engine Power Air Start Procedure Engine Fire In Flight On The Ground Maximum Glide Configuration Emergency Descent Landing Without Power 3-5 3-5 3-5 3-5 3-6 3-6 3-6 3-6 3-7 3-7 3-7 Landing Gear Retracted - With Power 3-7 Systems Emergencies 3-8 Propeller Overspeed 3-8 Generator-Out Procedure 3-8 Landing Gear Manual Extension 3-8 Landing Gear Retraction After Practice Manual Extension 3-9 Unlatched Door in Flight 3-10 Emergency Exits 3-10 Spins Emergency Speed Reduction Revised: March 1983 3-10 3-11 3-1 1 1 LIMITATIONS GENERAL Section III Emergency Procedures Section III Emergency Procedures EMERGENCY AIRSPEEDS BEECHCRAFT Bonanza K35 and M35 BEECHCRAFT Bonanza K35 and M35 INTENTIONALLY LEFT BLANK Emergency Descent Glide Emergency Landing Approach 123 Knots/142 MPH 105 Knots/122 MPH 78 Knots/90 MPH ...... All airspeeds quoted in this section are indicated airspeeds (IAS). The following information is presented to enable the pilot to form, in advance, a definite plan of action for coping with the most probable emergency situations which could occur in the operation of the airplane. Where practicable, the emergencies requiring immediate corrective action are treated in check list form for easy reference and familiari- zation. Other situations, in which more time is usually per- mitted to decide on and execute a plan of action, are discussed at some length. ENGINE FIRE (GROUND} 1. Mixture - IDLE CUT-OFF 2. Fuel Selector Valve - OFF 3. Battery, Generator and Magneto Switches - OFF 4. Extinguish with Fire Extinguisher. ENGINE FAILURE ON TAKE-OFF DURING GROUND ROLL 1. Throttle - CLOSED 2. Braking MAXIMUM - 3. Fuel Selector Valve - OFF 4. Battery and Generator Switches 3-2 August 1982 June 1975 PERFORMANCE WT & BAL/EQUIP LIST - OFF 3-3 SYSTEMS DESCRIPTION HANDLING BERMASAINT. NORMAL PROCEDURES GENERAL LIMITATIONS Section III Emergency Procedures BEECHCRAFT Bonanza K35 and M35 If airborne and insufficient runway remains for landing: 1. Fuel Selector Valve - SELECT OTHER MAIN TANK 2. Auxiliary Fuel Pump 3. Mixture ON FULL RICH I BEECHCRAFT Bonanza K35 and M35 3. Propeller Overspeed a. Section III Emergency Procedures Retard throttle to reduce RPM to red line. b. Check oil pressure. C. Reduce speed to assist in maintaining altitude. d. Select nearest landing site, follow emergency landing procedures. (If loss of oil pressure was cause of overspeed, the engine will seize after a short period of operation.) AIR START PROCEDURE a. Fuel Selector Valve - SELECT MAIN TANK MORE NEARLY FULL (check to feel detent) b. Throttle - RETARD 4. Magnetos - CHECK, ON BOTH IF NO RESTART 1. Select most favorable landing site. 2. The use of landing gear is dependent on the terrain where landing must be made. ENGINE MALFUNCTION IN FLIGHT ENGINE FAILURE The most probable cause of engine failure would be loss of fuel flow or improper functioning of the ignition system. DISCREPANCY CHECKS (Rough running engine, loss of engine power, loss of fuel flow, etc.) 1. Rough Running Engine a. Mixture FULL RICH, then lean as required b. Magneto Switch CHECK on BOTH position 2. Loss of Power a. - Fuel Pressure Gage - CHECK (fuel pressure ab- normally low) (1) Mixture FULL RICH - (2) Auxiliary Fuel Pump ON - (3) Auxiliary Fuel Pump - OFF if performance does not improve in a few moments b. Fuel Quantity Indicator used is empty) - CHECK (fuel tank being (1) Select other tank (check to feel detent) 11 C. Mixture FULL RICH - d. Auxiliary Fuel Pump - ON until power is regained, then off. (Leave on if engine driven fuel pump is inoperative.) Throttle ADVANCE to desired power Mixture - LEAN as required e. f. ENGINE FIRE (FLIGHT) The red VENT SHUTOFF control on the outboard side of the right lower subpanel is used to close off all heating system outlets so that smoke and fumes will not enter the cabin. In the event of engine fire, shut down the engine as follows and make a landing: 1. Vent Shutoff Control - PULL TO CLOSE 2. Mixture IDLE CUT-OFF 3. Fuel Selector Valve - OFF 4. Battery, Generator, and Magneto Switches - OFF (Ex- tending the landing gear can be accomplished manually if desired.) 5. Do not attempt to restart engine. 3-4 June 1975 June 1975 3-5 PERFORMANCE WT & BAL/EQUIP LIST SYSTEMS DESCRIPTION HANDERILO MAMIT. NORMAL PROCEDURES GENERAL Section ill Emergency Procedures EMERGENCY DESCENT BEECHCRAFT Bonanza K35 and M35 BEECHCRAFT Bonanza K35 and M35 Section III Emergency Procedures PERFORMANCE WT BAL/EQUIP LIST SYSTEMS DESCRIPTION HANDLING, SERV & MAINT 1. Power IDLE 2. Propeller - HIGH RPM 3. Landing Gear - DOWN 4. Airspeed - ESTABLISH 123 kts/142 mph MAXIMUM GLIDE CONFIGURATION - 1. Landing Gear UP 2. Flaps - UP 3. Cowl Flaps - CLOSED 4. Propeller PULL for LOW RPM 5. Airspeed 105 KTS/122 MPH Glide distance is approximately 1.7 nautical miles (2 statute miles) per 1000 feet of altitude above the terrain. LANDING GEAR MANUAL EXTENSION Manual extension of the landing gear can be facilitated by first reducing airspeed. Then proceed as follows: 1. LDG GEAR Circuit Breaker (Right Subpanel) OFF (PULL OUT) 2. Landing Gear Switch Handle - DOWN position 3. Remove Safety Boot or Cover from handcrank handle at rear of front seats. 4. Engage handcrank and turn counterclockwise as far as possible (approximately 50 turns). 5. If electrical system is operative, check landing gear position lights and warning horn (check LDG GEAR INDICATOR and LDG GEAR WARNING circuit breakers engaged). 6. Check mechanical landing gear indicator 7. Disengage handcrank. 3-6 - DOWN June 1975 1 1 EMERGENCY DESCENT 1. Power - IDLE 2. Propeller - HIGH RPM 3. Landing Gear - DOWN 4. Airspeed - ESTABLISH 123 kts/142 mph LANDING EMERGENCIES LANDING WITHOUT POWER The approach speed is higher than normal to assure the availability of control during flare without power. When as- sured of reaching the landing site selected, and on final approach: 1. Airpeed - 78 kts/90 mph 2. Fuel Selector Valve - OFF 3. Mixture IDLE CUT-OFF - 4. Flaps - AS REQUIRED 5. Landing Gear TERRAIN - DOWN OR UP, DEPENDING ON 6. Battery, Generator and Igniton Switches - OFF LANDING GEAR RETRACTED WITH POWER - If possible, choose firm sod or foamed runway. Make a normal approach, using flaps as necessary. When you are sure of making the selected landing spot: 1. Throttle - CLOSED 2. Mixture IDLE CUT-OFF - 3. Battery, Generator and Ignition Switches - OFF 4. Fuel Selector Valve - OFF 5. Keep wings level during touchdown. 6. Get clear of the airplane as soon as possible after it stops. Revised: March 1983 3-7 LIMITATIONS NORMAL PROCEDURES GENERAL LIMITATIONS Section III Emergency Procedures SYSTEMS EMERGENCIES PROPELLER OVERSPEED 1. Throttle BEECHCRAFT BEECHCRAFT Bonanza K35 and M35 Bonanza K35 and M35 RETARD TO RPM RED LINE 2. Airspeed - REDUCE - 3. Oil Pressure CHECK WARNING If loss of oil pressure was the cause of over- speed, the engine will seize after a short period of operation. 4. Land SELECT NEAREST SUITABLE SITE and follow LANDING EMERGENCIES procedure. GENERATOR-OUT PROCEDURE A failure of the generator will place the entire electrical operation of the aircraft on the battery. Generator failure may be indicated by the ammeter. When a generator failure occurs in flight, all non-essential electrical load should be discontinued to conserve the battery. LANDING GEAR MANUAL EXTENSION Manual extension of the landing gear can be facilitated by first reducing airspeed. Then proceed as follows: 1. LDG GEAR Circuit Breaker -OFF (PULL OUT) DOWN position 2. Landing Gear Switch Handle - 3. Handcrank Handle Cover (at rear of front seats) REMOVE 4. Handcrank ENGAGE and TURN COUNTERCLOCK- WISE AS FAR AS POSSIBLE (approximately 50 turns} 3-8 August 1982 + I I CAUTION Section III Emergency Procedures The manual extension system is designed to lower the landing gear only. DO NOT ATTEMPT TO RETRACT THE GEAR MANUALLY. 5. If electrical system is operative, check landing gear warning horn (check LDG GEAR WARNING circuit breaker engaged). 6. Check mechanical landing gear indicator - DOWN 7. Handcrank DISENGAGE. Always keep it stowed - when not in use. WARNING Do not operate the landing gear electrically with the handcrank engaged, as damage to the mechanism could occur. After emergency landing gear extension, do not move any landing gear controls or reset any switches or circuit breakers until airplane is on jacks as failure may have been in the gear up circuit and gear might retract on the ground. LANDING GEAR RETRACTION AFTER PRACTICE MANUAL EXTENSION After practice manual extension of the landing gear, the gear may be retracted electrically, as follows: 2. Landing Gear Motor Circuit Breaker 3. Handcrank - CHECK, STOWED 3. Landing Gear - August 1982 RETRACT - IN 3-9 PERFORMANCE WT & BAL/EQUIP LIST SYSTEMS DESCRIPTION HANDLING, SERV & MAINT NORMAL PROCEDURES GENERAL LIMITATIONS Section III Emergency Procedures UNLATCHED DOOR IN FLIGHT BEECHCRAFT Bonanza K35 and M35 If the cabin door is not locked it may come unlatched in flight. This may occur during or just after take-off. The door will trail in a position approximately 3 inches open, but the flight characteristics of the airplane will not be affected, except that rate of climb will be reduced. Return to the field in a normal manner. If practicable, during the landing flare-out have a passenger hold the door to prevent it from swinging open. EMERGENCY EXITS Emergency exits, provided by the openable window on each side of the cabin, may be used for egress in addition to the cabin door. An emergency exit placard is installed below the left and right openable windows. To open each emergency exit: 1. Lift the latch. 2. Pull out the emergency release pin and push the window out. SPINS Spins are prohibited. If a spin is entered inadvertently: Immediately move the control column full forward and simultaneously apply full rudder opposite to the direction of the spin; continue to hold this control position until rotation stops and then neutralize all controls and execute a smooth pullout. Ailerons should be neutral and throttle in idle position at all times during recovery. 3-10 Revised: March 1983 H WT & BAL/EQUIP LIST SYSTEMS DESCRIPTION PERFORMANCE NORMAL PROCEDURES HANDLING, SERV & MAINT GENERAL NORMAL PROCEDURES LIMITATIONS BEECHCRAFT Bonanza K35 and M35 SECTION IV NORMAL PROCEDURES TABLE OF CONTENTS PERFORMANCE WT & BAL/EQUIP LIST SYSTEMS DESCRIPTION HANDLING, SERV & MAINT SUBJECT PAGE Speeds For Safe Operation 4-3 Preflight Inspection 4-3 1. Cabin 2. Right Fuselage 4-3 4-3 3. Empennage 4-3 4. Left Fuselage 4-4 5. Left Wing Trailing Edge 4-4 6. Left Wing Leading Edge 4-4 7. Left Landing Gear 8. Nose Section 4-4 4-4 9. Right Landing Gear 4-5 10. Right Wing Leading Edge 4-5 11. Right Wing Trailing Edge Before Starting 4-5 4-6 June 1975 4-1 [ 1