SUPER KING AIR 200 SERIES MAINTENANCE MANUAL SCHEDULED INSPECTION PROGRAM (PHASE 1)-MAINTENANCE PRACTICES A. NOSE SECTION ATA/GAMA REFERENCE

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1 SCHEDULED ECTION PROGRAM (PHASE 1)-MAINTENANCE PRACTICES Owner W /O Num ber Date In Date Out SerialNo. Reg.No. LastInspection Phase LastInspection Date LastInspection Hours Hourm eter TotalTim e TotalCycles Researched By LH Eng.S/N TotalTim e TotalCycles TSOH Cycles SOH TSHSI Cycles SHSI RH Eng.S/N TotalTim e TotalCycles TSOH Cycles SOH TSHSI Cycles SHSI LH Prop S/N LH Prop TotalTim e TSOH RH Prop S/N RH Prop TotalTim e TSOH A. NOSE SECTION ATA/GAMA NOTE There are no inspections required in this section during this phase. B. NOSE AVIONICS COMPARTMENT 1. VACUUM REGULATOR VALVE FILTER -Inspectfor blockage C. NOSE LANDING GEAR AREA 1. ELECTRICAL W IRING and EQUIPMENT -Inspectal exposed electricalwiring and equipmentforchafing,damage and security ofatachment. D. NOSE GEAR 1. W HEEL a. Inspectwheelforwear,damage and corrosion b. Inspectwheelbearings and races forwear,piting,cracks, discoloration,rustorotherindications ofdamage Page 201 Jul29/05

2 D. NOSE GEAR (Continued) ATA/GAMA 2. TIRE a. Inspect for wear and deterioration b. Check for correct inflation SHIMMY DAMPER - Inspect for leaks, security and 4. NOSE GEAR DRAG BRACE STOP LUGS - Inspect for cracks, damage or distortion. 5. NOSE GEAR STEERING STOP - Inspect steering stop for damage or distortion. 6. LANDING and TAXI LIGHTS - Inspect for broken lenses or bulbs. 7. STEERING LINKAGE - Inspect nose gear steering mechanism and attaching hardware for wear, damage and corrosion. 8. NOSE LANDING GEAR STRUT - Check strut for leakage and correct extension. 9. NOSE GEAR RETRACT and EMERGENCY EXTENSION CHAINS (Mechanical Gear)- Inspect, clean and lubricate chains. 10. ELECTRICAL WIRING and EQUIPMENT - Inspect for chafing, damage, proper routing of wire bundles and security of E. PILOT S COMPARTMENT 1. RETURN AIR INLET FILTERS - Inspect filters in return air inlet of the forward vent blower WINDSHIELD a. Inspect windshield for cracks and visibility impairment b. Inspect windshield weather seal (Silicone)for debonding, cracks or wear. c. Inspect windshield weather hump seal (Polysulfide)for debonding, cracks or wear Page 202 Jul 29/05

3 E. PILOT S COMPARTMENT (Continued) ATA/GAMA 3. WINDOWS - Inspect exterior surface of cockpit side windows for deep scratches, cracks, chips or excess crazing or other damage ALTERNATE AIR VALVE - Drain off all moisture SEAT TRACKS - Inspect seat tracks for damage and wear PORTABLE FIRE EXTINGUISHER - Inspect the bottle for signs of damage and mount for security of 7. SEATS, SEAT BELTS and SHOULDER HARNESSES - Inspect seats, seat belts and shoulder harnesses for deterioration. 8. BRAKE FLUID RESERVOIR PRESSURE EQUALIZATION ORIFICE - Inspect for blockage UPHOLSTERY PANELS - Inspect for security of 10. FLIGHT CONTROL CABLE TENSION - Check aileron control cable tension. 27 F. CABIN SECTION 1. WINDOWS - Inspect exterior surface of windows for deep scratches, cracks, chips and excessive crazing or other damage. 2. ROTATING or FLASHING BEACON - Inspect for cracked or broken lenses ACCESS DOORS - Inspect for fit and 4. OUTFLOW and SAFETY VALVES - Drain outflow valve control line SEAT TRACKS - Inspect seat tracks for damage and wear AFT EVAPORATOR FILTER - Inspect aft evaporator filter SEATS, SEAT BELTS and SHOULDER HARNESSES a. Inspect seats, seat belts and shoulder harnesses for deterioration or missing components. b. Inspect shoulder harness attachment post for cracked, worn, brittle or missing grommet OXYGEN SYSTEM a. Inspect oxygen system installation for damage and security of Page 203 Jul 29/05

4 F. CABIN SECTION (Continued) ATA/GAMA b. Perform the appropriate OXYGEN SYSTEM FUNCTIONAL TEST TOILET - Inspect for spillage and leakage below the toilet CABIN ENTRANCE DOOR (BB-2 and After;BT-1 and After) a. Inspect the door seal for cuts, abrasions and security of b. Inspect the cabin door support cables for wear, damage and security. 11. CABIN CARGO DOOR and CABIN ENTRANCE DOOR (BL-1 and After;BN-1 and After) - Inspect door seals for cuts, abrasions, deterioration and security of LANDING GEAR HYDRAULIC LINES - Inspect for leaks, damage and security of 13. PORTABLE FIRE EXTINGUISHER - Inspect bottle for damage and security. 26 G. REAR FUSELAGE AND EMPENNAGE 1. REAR FUSELAGE DRAINS - Inspect rear fuselage drains ELT BATTERY a. Inspect for leakage, corrosion or loose leads b. Determine remaining useful life NAVIGATION LIGHTS and ROTATING or FLASHING BEACONS - Inspect for broken or cracked lenses ACCESS DOORS - Inspect for fit and security of 5. VENTRAL FIN DRAIN HOLES - Inspect the drain holes in the bottom of the ventral fin for obstructions DEICER BOOTS - Inspect for deterioration, damage and 7. RUDDER and TRIM TAB DRAIN HOLES - Inspect the drain holes for obstructions. 8. STATIC WICKS - Inspect for damage and security of RUDDER BOOST FILTER (With Autopilot) - Replace Filter Page 204 Jul 29/05

5 G. REAR FUSELAGE and EMPENNAGE (Continued) ATA/GAMA 10. FLIGHT CONTROL CABLE TENSION - Inspect elevator, elevator tab, rudder and rudder tab control cable tensions. 27 H. LEFT-HAND OUTBOARD WING 1. FUEL PROBES - Inspect for leaks at points of WING ATTACH FITTING DRAIN HOLES - Determine that the drain holes are open in the wing center section and outboard wing upper attachment fittings LIGHTS a. Inspect the navigation and recognition lights for broken or cracked lenses b. Inspect the strobe light for broken or cracked lenses FUEL TANKS and VENTS a. Inspect the exterior of the wing for leaks b. Inspect fuel cap and antisiphon valve for damage and c. Inspect exterior openings of vents for obstructions INTEGRAL FUEL TANK - Inspect the exterior surface of the integral tank access doors for leaks. 6. DEICER BOOTS - Inspect exterior surface for deterioration, damage and 7. ACCESS DOORS (ECTION PANELS) - Inspect for fit and STATIC WICKS a. Inspect for damage and security of b. Check the static wick for proper bonding to the airplane AILERON and TRIM TAB - Check trim tab free play LEFT-HAND OUTBOARD WING AREA - Inspect skin, structure, all components and attaching hardware for general condition and security of If damage is found, check the adjacent area. Page 205 Jul 29/05

6 H. LEFT-HAND OUTBOARD WING (Continued) ATA/GAMA 11. AILERON and OUTBOARD FLAP - Inspect skin, structure and attaching hardware for wear, damage and corrosion. If damage or corrosion is found in a given area, check the adjacent area. 12. ELECTRICAL WIRING and EQUIPMENT - Inspect for chafing, damage, proper routing of wire bundles and security of 13. FLIGHT CONTROL COMPONENTS, CABLES and PULLEYS a. Inspect control system components (pushrods, turnbuckles, end fittings, castings, etc.) for bulges, splits, bends or cracks which are conditions for replacement. b. Inspect control system cables, pulleys and associated equipment for wear, cracks, breaks, attachment, alignment, clearance and proper operation. Replace cables that have more than three broken wires in any given three-foot cable length or have evidence of corrosion c. Inspect aileron control cable tensions. 27 d. Inspect aileron tab control cable tensions FLAPS and ACTUATORS a. Inspect flap 90 drive, cable and actuator for b. Inspect flap tracks for wear c. Perform flap safety mechanism functional test FUEL PLUMBING - Inspect for leaks, chafing or damage and 16. HINGED ACCESS DOORS ABOVE DOORS NO. 13 and 14 - Inspect for cracks or damage to hinge and fasteners I. LEFT-HAND WING CENTER SECTION 1. FUEL PROBES - Inspect for leaks at points of FUEL TANKS and VENTS a. Inspect the exterior of the center section for leaks b. Inspect fuel cap and antisiphon valve for damage and c. Inspect the exterior openings of the vents for obstructions Page 206 Jul 29/05

7 I. LEFT-HAND WING CENTER SECTION (Continued) ATA/GAMA 3. ACCESS DOORS (ECTION PANELS) - Inspect for fit and ENGINE FIRE EXTINGUISHER (If Installed) a. Inspect plumbing for security of b. Check fire bottle pressure gage FUEL PUMPS - Inspect the pumps for leaks and security of LANDING GEAR HYDRAULIC POWER PACK and MOTOR (If Installed) a. Inspect the hydraulic power pack gear-up and gear-down port screens. b. Inspect the landing gear hydraulic system bleed air pressure overboard relief orifice screen for blockage c. Inspect the hydraulic power pack fill reservoir screen d. Inspect all plumbing attach points for leaks and security of 7. LEFT-HAND WING CENTER SECTION AREA - Inspect skin, structure, all components and attaching hardware for general condition and security of If damage is found in a given area, check the adjacent area SIRM 8. FLAPS and ACTUATORS a. Inspect flap 90 drive, cable and actuator for b. Inspect flap tracks for wear LEADING EDGE and NACELLE FUEL PLUMBING - Inspect fuel plumbing for leaks, damage and security of FLIGHT CONTROL COMPONENTS, CABLES and PULLEYS a. Inspect control system components (pushrods, turnbuckles, end fittings, castings, etc.) for bulges, splits, bends or cracks which are conditions for replacement. b. Inspect control cables, pulleys and associated equipment for wear, cracks, breaks, attachment, alignment, clearance and proper operation. Replace cables that have more than three broken wires in any given three-foot cable length or have evidence of corrosion Page 207 Jul 29/05

8 I. LEFT-HAND WING CENTER SECTION (Continued) ATA/GAMA 11. ELECTRICAL WIRING and EQUIPMENT - Inspect for chafing, damage and proper routing of wire bundles and security of 12. BLEED AIR BYPASS VALVE - Check bleed air valve at heat exchanger for operation of linkage to butterfly valve and operation of actuator motor. 13. ANICAL LANDING GEAR TORQUE TUBE AND ASSOCIATED COMPONENTS - Inspect torque tube, bearings, supports, universal joints, and hardware for security of attachment, wear, cracks, breaks, bends, splits, chaffing, alignment, and clearance from associated structures and their components J. LEFT-HAND MAIN LANDING GEAR AREA WHEELS a. Inspect wheels for wear, damage and corrosion. b. Inspect wheel bearings and races for wear, pitting, cracks, discoloration, rust or other indications of damage. 2. BRAKES - Inspect brake discs, linings and plumbing for wear damage, leaks, corrosion and security of all components BRAKE DEICING (If Installed) a. Inspect manifold for blocked orifices b. Inspect exterior of lines, hoses and connections for leakage and 4. TIRES - Inspect tires for wear, deterioration and correct inflation. 5. LEFT-HAND MAIN LANDING GEAR STRUT - Check strut for leaks and proper extension. 6. ELECTRICAL WIRING and EQUIPMENT - Inspect exposed wiring and equipment for chafing, damage and proper routing and security of MAIN GEAR ACTUATOR a. ACTUATOR (Mechanical Gear) 1) Inspect actuator support brackets for visible damage, wear and loose and missing fasteners ) Inspect brackets for loose or missing rivets Page 208 Jul 29/05

9 J. LEFT-HAND MAIN LANDING GEAR AREA (Continued) ATA/GAMA 3) Inspect actuator for significant leakage of internal lubricant b. ACTUATOR (Hydraulic Gear) 1) Inspect actuator support brackets for visible damage, wear and loose and missing fasteners ) Inspect actuator and plumbing for leakage DRAG BRACE a. Inspect for security of attach fittings b. Inspect downlock bolts for proper torque (finger-tight and safety-wired). 9. LEFT-HAND MAIN LANDING GEAR AREA - Inspect wheel well and gear door structure, all components and attaching hardware for general condition and security of If damage is found, check the adjacent area. K. LEFT-HAND ENGINE 1. PROPELLER DEICER - Inspect propeller deice system (spinner removal required) P3 AIR FILTER - Inspect the filter for cleanliness. P&W 3. FIREWALL FUEL FILTERS and SCREENS - Inspect the firewall filter for evidence of foreign matter, corrosion or microbiological growth in the fuel system. If any microbiological growth is found, use BIOBOR JF additive. 4. PROPELLERS - Inspect for damage and attachment (spinner removal required) ENGINE OIL FILTER - Inspect for metal particles. P&W 6. LEFT-HAND ENGINE - Inspect all systems, all components and attaching hardware for general condition and security of Check all tubes and hoses for general condition, leaks and security of L. RIGHT-HAND OUTBOARD WING 1. FUEL PROBES - Inspect for leaks at points of WING ATTACH FITTING DRAIN HOLES - Determine that the drain holes are open in the wing center section and outboard wing upper attachment fittings Page 209 Jul 29/05

10 L. RIGHT-HAND OUTBOARD WING (Continued) ATA/GAMA 3. LIGHTS a. Inspect the navigation and recognition lights for broken or cracked lenses b. Inspect the strobe light for broken or cracked lenses FUEL TANKS and VENTS a. Inspect the exterior of the wing for leaks b. Inspect fuel cap and antisiphon valve for damage and c. Inspect exterior openings of vents for obstructions INTEGRAL FUEL TANK - Inspect the exterior surface of the integral tank access doors for leaks. 6. DEICER BOOTS - Inspect exterior surface for deterioration, damage and 7. ACCESS DOORS (ECTION PANELS) - Inspect for fit and STATIC WICKS a. Inspect for damage and security of b. Check the static wick for proper bonding to the airplane AILERON and TRIM TAB - Check trim tab free play RIGHT-HAND OUTBOARD WING AREA - Inspect skin, structure and attaching hardware for wear, damage and corrosion. If damage or corrosion is found in a given area, check the adjacent area. 11. AILERON and OUTBOARD FLAP - Inspect skin, structure and attaching hardware for wear, damage and corrosion. If damage or corrosion is found in a given area, check the adjacent area. 12. ELECTRICAL WIRING and EQUIPMENT - Inspect for chafing, damage, proper routing of wire bundles and security of 13. FLIGHT CONTROL COMPONENTS, CABLES and PULLEYS a. Inspect control system components (pushrods, turnbuckles, end fittings, castings, etc.) for bulges, splits, bends or cracks which are conditions for replacement. 27 Page 210 Jul 29/05

11 L. RIGHT-HAND OUTBOARD WING (Continued) ATA/GAMA b. Inspect control system cables, pulleys and associated equipment for wear, cracks, breaks, attachment, alignment, clearance and proper operation. Replace cables that have more than three broken wires in any given three-foot cable length or have evidence of corrosion. 27 c. Check aileron control cable tension FLAPS and ACTUATORS a. Inspect flap 90 drive, cable and actuator for b. Inspect flap tracks for wear c. c. Perform flap safety mechanism functional test FUEL PLUMBING - Inspect for leaks, chafing or damage and 16. HINGED ACCESS DOORS ABOVE DOORS NO. 13 and 14 - Inspect for cracks or damage to hinge and fasteners M. RIGHT-HAND WING CENTER SECTION 1. FUEL PROBES - Inspect for leaks at points of FUEL TANKS and VENTS a. Inspect the exterior of the center section for leaks b. Inspect fuel cap and antisiphon valve for damage and c. Inspect the exterior openings of the vents for obstructions ACCESS DOORS (ECTION PANELS) - Inspect for fit and BATTERY a. Service battery as required b. Remove battery and inspect the battery box, cables and vent tubes for deterioration or obstructions. (BB-2 thru BB- 1631; BT-1 thru BT-38; BL-1 thru BL-140; BN-1 thru BN-4) c. Remove battery and inspect the battery box and cables for deterioration or obstructions. (BB-1632 and After; BT-39 and After; BL-141 and After; BN-5 and After) ENGINE FIRE EXTINGUISHER (If Installed) Page 211 Jul 29/05

12 M. RIGHT-HAND WING CENTER SECTION (Continued) ATA/GAMA a. Inspect plumbing for security and b. Check fire bottle pressure gage FUEL PUMPS - Inspect for leaks and security of RIGHT-HAND WING CENTER SECTION AREA - Inspect skin, structure, all components and attaching hardware for general condition and security of If damage is found in a given area, check the adjacent area. 57 SIRM 8. FLAPS and ACTUATORS a. Inspect flap 90 drive, cable and actuator for b. Inspect flap tracks for wear LEADING EDGE and NACELLE FUEL PLUMBING - Inspect fuel plumbing for leaks, damage and security of FLIGHT CONTROL COMPONENTS, CABLES and PULLEYS a. Inspect control system components (pushrods, turnbuckles, end fittings, castings, etc.) for bulges, splits, bends or cracks which are conditions for replacement. b. Inspect control cables, pulleys and associated equipment for wear, cracks, breaks, attachment, alignment, clearance and proper operation. Replace cables that have more than three broken wires in any given three-foot cable length or have evidence of corrosion. 11. ELECTRICAL WIRING and EQUIPMENT - Inspect for chafing, damage and proper routing of wire bundles and security of 12. BLEED AIR BYPASS VALVE - Check bleed air valve at heat exchanger for operation of linkage to butterfly valve and operation of actuator motor. 13. REFRIGERANT LINES and PRESSURE SWITCHES - Inspect lines and switches for leakage, damage and 14. ANICAL LANDING GEAR TORQUE TUBE AND ASSOCIATED COMPONENTS - Inspect torque tube, bearings, supports, universal joints, and hardware for security of attachment, wear, cracks, breaks, bends, splits, chaffing, alignment, and clearance from associated structures and their components Page 212 Jul 29/05

13 N. RIGHT-HAND MAIN LANDING GEAR AREA ATA/GAMA 1. WHEELS a. Inspect wheels for wear, damage and corrosion. b. Inspect wheel bearings and races for wear, pitting, cracks, discoloration, rust or other indications of damage. 2. BRAKES - Inspect brake discs, linings and plumbing for wear, damage, leaks, corrosion and security of all components BRAKE DEICING (If Installed) a. Inspect manifold for blocked orifices b. Inspect exterior of lines, hoses and connections for leakage and 4. TIRES - Inspect tires for wear, deterioration and correct inflation. 5. RIGHT-HAND MAIN LANDING GEAR STRUT - Check strut for leaks and proper extension. 6. ELECTRICAL WIRING and EQUIPMENT - Inspect exposed wiring and equipment for chafing, damage and proper routing and security of MAIN GEAR ACTUATOR a. ACTUATOR (Mechanical Gear) 1) Inspect actuator support brackets for visible damage, wear and loose and missing fasteners ) Inspect brackets for loose or missing rivets ) Inspect actuator for significant leakage of internal lubricant b. ACTUATOR (Hydraulic Gear) 1) Inspect actuator support brackets for visible damage, wear and loose and missing fasteners ) Inspect actuator and plumbing for leakage DRAG BRACE a. Inspect for security of attach fittings b. Inspect downlock bolts for proper torque (finger-tight and safety-wired). Page 213 Jul 29/05

14 N. RIGHT-HAND MAIN LANDING GEAR AREA (Continued) ATA/GAMA 9. RIGHT-HAND MAIN LANDING GEAR AREA - Inspect wheel well and gear door structure, all components and attaching hardware for wear, damage and corrosion. If damage or corrosion is found, check the adjacent area. O. RIGHT-HAND ENGINE 1. PROPELLER DEICER - Inspect propeller deice system (spinner removal required) P3 AIR FILTER - Inspect the filter for cleanliness. P&W 3. FUEL FILTERS and SCREENS - Inspect the firewall filter for evidence of foreign matter, corrosion or microbiological growth in the fuel system. If any microbiological growth is found, use BIOBOR JF additive. 4. PROPELLERS - Inspect for damage and attachment (spinner removal required) ENGINE OIL FILTER - Inspect for metal particles. P&W 6. RIGHT-HAND ENGINE - Inspect all systems, all components and attaching hardware for general condition and security of Check all tubes and hoses for general condition, leaks and security of P. LANDING GEAR RETRACTION NOTE Mechanical and Hydraulic Landing Gear Systems - Since battery voltage is not sufficient to properly cycle the landing gear, use only an external power source capable of delivering and maintaining ±0.25 volts throughout the extension and retraction cycles when performing the landing gear retraction inspection. Hydraulic Landing Gear System - The hydraulic landing gear system pump may cavitate and not operate properly during ground use of the hydraulic power pack for retraction and/or extension of the landing gear. To prevent this, an exterior supply of dry air at 18 to 20 psi must be applied to the power pack reservoir to prevent cavitation. If an exterior air supply is not available, use an exterior hydraulic pressure source. Refer to OPERATING THE LANDING GEAR USING THE POWER PACK in Chapter of the Super King Air 200 Series Maintenance Manual. 1. RETRACT ANISM - Check retraction system for proper operation of all components through at least two complete cycles. 32 Page 214 Jul 29/05

15 P. LANDING GEAR RETRACTION (Continued) ATA/GAMA 2. DOORS and LINKAGE a. Check door for damage, operation and fit. 32 b. Check door linkage for wear, damage and rigging DOWNLOCK INDICATOR SWITCHES a. Check for security and proper operation of switches b. Clean terminals and connectors as required c. Check wiring for damage and security of connection UPLOCK INDICATOR SWITCHES a. Check for security and proper operation of switches b. Clean terminals and connectors as required c. Check wiring for damage and security of connection WARNING HORN - Check operation MAIN GEAR DOWNLOCKS - Check locking mechanism for positive engagement in extended position SAFETY SWITCH - Check for proper operation ACTUATORS - Check for noise, binding and proper rigging LIMIT SWITCHES - (Mechanical Gear) a. Check for correct adjustment b. Check for security of EMERGENCY EXTENSION (Mechanical Gear) - Check system for freedom of operation and positive engagement of downlocks. CAUTION Do not continue operation after receiving a gear-down indication on a l gears.further movement of the handle could damage the drive mechanism and prevent subsequent electricalgear retraction.the landing gear cannot be retracted manua ly. 11. EMERGENCY EXTENSION (Hydraulic Gear) - Check system for freedom of operation and positive engagement of downlocks NOSE GEAR RETRACT CHAIN (Mechanical Gear) Page 215 Jul 29/05

16 P. LANDING GEAR RETRACTION (Continued) ATA/GAMA a. Inspect chains for broken links, excessive pin and link wear, misalignment, rust, corrosion and dirt. b. Check sprockets for excessive wear and hook-shaped teeth c. Check for proper chain tension d. Check nose gear and nose gear linkage clearance from electrical wires and obstructions. 13. PLACARDS - Check that all placards are in place and are legible. 14. LANDING GEAR RETRACTION - Inspect all landing gear components and attaching hardware, structure and hydraulic lines for general condition and security of 15. LANDING GEAR MOTOR CONTROLLER (Mechanical Gear) - Inspect controller for pitted or damaged contacts. Repair as necessary Q. OPERATIONAL ECTION NOTE The following Operational Inspection procedures are to be applied during start and run of the engine. Refer to the Super King Air 200 and B200 Pilot s Operating Handbook and FAA Approved Airplane Flight Manual for the engine start and run procedures. 1. FIREWALL SHUTOFF FUEL VALVES - Check for proper operation. 2. CROSSFEED FUEL VALVE - Check for proper operation. 3. STANDBY PUMPS - Check for proper operation. 4. STARTER-GENERATOR a. Check starter for operation. b. Check generator for output. 5. IGNITION a. Check for proper operation. b. Check for annunciator panel light illumination. 6. ENGINE OIL - Check for proper pressure and temperature limits. Page 216 Jul 29/05

17 Q. OPERATIONAL ECTION (Continued) ATA/GAMA 7. FUEL QUANTITY GAGES - Check operation. 8. INTERSTAGE TURBINE TEMPERATURE - Check for correct limits on engine start. 9. VACUUM SYSTEM - Check for correct limits. 10. PNEUMATIC PRESSURE GAGE - Check for correct pressure. 11. PNEUMATIC SYSTEM SHUTOFF VALVES - Check for proper operation. 12. GYRO INSTRUMENTS - Check for erratic or noisy operation. 13. PROPELLERS - Perform flight idle torque check. 14. AUTOFEATHERING CHECK - Refer to AUTOFEATHER SYSTEM OPERATIONAL CHECK. 15. PROPELLER SYNCHROPHASER - Refer to SYNCHROPHASER SYSTEM FUNCTIONAL TEST and confirm proper synchronization PROPELLER GOVERNOR - Check governor operation (including feathering and reversing). 17. IDLE RPM - Check for correct rpm (both high and low rpm). 18. AC INVERTERS (If Installed) - Check for proper operation. 19. RUDDER BOOST - Check for proper operation. 20. AUTO-IGNITION a. Check for proper operation. b. Check for annunciator panel illumination. 21. PROPELLER DEICER - Check for proper operation and cycling. Refer to Chapter 30 of the King Air Series Component Maintenance Manual. 22. ENGINE INERTIAL ANTI-ICER - Check for proper operation and rigging. 23. SURFACE DEICE SYSTEM - Check for proper operation and cycling. 24. BRAKE DEICE SYSTEM (If Installed) - Check for proper operation with engines running. 25. ELECTRICAL SYSTEM - Perform functional checks Page 217 Jul 29/05

18 Q. OPERATIONAL ECTION (Continued) ATA/GAMA 26. ENVIRONMENTAL SYSTEM - Check for proper operation in: a. Manual heat mode. b. Manual cool mode. c. Automatic mode. 27. REFRIGERANT LEVEL - Check for proper level. 28. AUTOPILOT - Check for proper operation as outlined by the applicable Super King Air 200 and B200 Pilot's Operating Handbook and FAA Approved Airplane Flight Manual Supplement. 29. STALL WARNING - Check for proper operation. 30. ENGINE FIRE DETECTORS - Perform system test according to instructions found in the Super King Air 200 and B200 Pilot's Operating Handbook and FAA Approved Airplane Flight Manual. 31. ENGINE FIRE EXTINGUISHERS (If Installed) - Perform system test according to instructions found in the Super King Air 200 and B200 Pilot's Operating Handbook and FAA Approved Airplane Flight Manual. 32. PRESSURIZATION SYSTEM - Check for proper operation. NOTE Refer to the Super King Air 200 and B200 Pilot s Operating Handbook and FAA Approved Airplane Flight Manual and perform system test. 33. AUXILIARY FUEL TRANSFER JET PUMPS - Check for proper operation. 34. CONDITION LEVER - Check for clean shutdown at IDLE-CUT-OFF. 35. PITOT TUBE - Check for proper heating at the unit and for obstructions. 36. LANDING and TAXI LIGHTS - Check operation of all lights. 37. OUTBOARD WING LIGHTS (RIGHT and LEFT) - Check operation of all navigation and strobe lights. 38. COCKPIT LIGHTS - Check operation of all cockpit lights. 39. EFIS COOLING BLOWERS (If Installed) - Check operation Page 218 Jul 29/05

19 Q. OPERATIONAL ECTION (Continued) ATA/GAMA 40. ELECTRIC ELEVATOR TRIM - Check for proper operation. 41. ENGINE and PROPELLER CONTROLS - Check for freedom of movement, full travel and friction-lock operation. 42. STATIC SYSTEM - Inspect alternate air valve for operation. 43. WINDSHIELD - Perform heated operational check. 44. THRESHOLD LIGHT - Check for proper operation. 45. AUXILIARY ELECTRIC HEAT (If Installed) - Check for proper operation of the Electric Heat System. 46. CABIN and COMPARTMENT LIGHTS - Check for proper operation. 47. PILOT'S and COPILOT'S SEATS, SEAT BELTS and SHOULDER HARNESSES - Check seat adjustment mechanism, seat belts and shoulder harness inertia reel for operation. 48. CABIN SEATS, SEAT BELTS and SHOULDER HARNESSES - Check seat adjustment mechanism, seat belts and shoulder harness inertia reel for operation. 49. CABIN ENTRANCE DOOR (BB-2 and After; BT-1 and After) a. Check that folding steps do not fold too soon and that they fold properly without interference. b. Check cabin DOOR UNLOCK annunciator for proper operation. c. Inspect cabin door damper for leakage and proper operation. 50. CABIN CARGO DOOR and CABIN ENTRANCE DOOR (BL-1 and After; BN-1 and After) a. Inspect door latching mechanism for operation and security of b. Check latching mechanism, folding steps and gas springs for proper operation. 51. EMERGENCY EXIT (WITH DOOR INSTALLED) a. Check emergency release handles (inside and outside) and latch mechanism for operation. b. Check that latches open and close freely. Page 219 Jul 29/05

20 Q. OPERATIONAL ECTION (Continued) ATA/GAMA 52. EMPENNAGE CONTROL SURFACES a. Check for freedom of movement. b. Check optional trim actuators and motors for smoothness of operation. 53. REAR FUSELAGE and EMPENNAGE LIGHTS - Check operation of all lights. 54. AILERON (LH and RH) - Check for freedom of movement. 55. AILERON TRIM TAB - Check trim tab actuator for smoothness of operation and 56. FUEL TANK HEATED VENTS (LH and RH) - Check the operation of the heated vents. They should be warm to the touch. 57. STALL WARNING HEAT - Check for proper operation. 58. FLAPS and ACTUATORS (Inboard, Outboard, LH and RH) - Check flaps for noisy or erratic operation. 59. WING CENTER SECTION LIGHTS - Check operation of all lights. 60. ENGINE INDUCTION SYSTEM (LH and RH) (BB-2 THRU BB-1439, BB-1440 THRU BB-1443; BT-1 THRU BT-34; BL-1 THRU BL-138; BN-1 THRU BN-4) - Check the inertial vane and bypass door for movement with the main and manual system. 61. ENGINE INDUCTION SYSTEM (LH and RH) (BB-1439, BB-1444 AND AFTER; BT-35 AND AFTER; BL-139 AND AFTER; BN-5 AND AFTER) - Check the inertial vane and bypass door for movement with the main and standby actuator motors EXTERNAL POWER RELAY - Check for proper operation. R. POST ECTION ITEMS 1. AIRPLANE CLEANED and SERVICED AS REQUIRED LUBRICATE AS NECESSARY ENGINES ECTED AFTER GROUND RUN-UP or FLIGHT TEST - Check for oil leaks, security and attachment of all components. Page 220 Jul 29/05

21 R. POST ECTION ITEMS (Continued) ATA/GAMA 4. AIRWORTHINESS DIRECTIVES and SERVICE BULLETINS - Must be reviewed and complied with as required. 5. ADDITIONAL ECTION REQUIREMENTS - Ensure Chapter 5, Special Inspection, and Airworthiness Limitations Manual (P/N ) requirements are complied with at the appropriate intervals. 6. IN-FLIGHT WORKSHEETS - All discrepancies noted by the pilot must be checked and corrected as required. 7. EMERGENCY LOCATOR TRANSMITTER - Check for proper operation and ensure ELT is ARMED before returning airplane to service OXYGEN SYSTEM PRESSURE - Check for proper pressure EMERGENCY and SURVIVAL EQUIPMENT - (If Installed) Ensure all necessary emergency and survival equipment is installed in the airplane and is serviceable. 10. PLACARDS - Determine that all required placards are in place and legible and POH 11. LOGBOOK ENTRY - Ensure that log books are filled out properly. ECTION COMPLETED I certify that Phase 1 Inspection was performed in accordance with the 200 Series Inspection Program and that the airplane is approved for return to service: DATE: ANIC: CREW CHIEF: QUALITY CONTROL ECTOR: Page 221 Jul 29/05