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Aircraft Maintenance Manual

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Содержание Beechraft Starship 2000

Страница 1: ...Aircraft Maintenance Manual Illustrated Parts Catalog Printed Circuit Board Manual Structural Repair Manual Wiring Diagram Manual...

Страница 2: ...ke hoses entry to retraction and extension hoses 5 20 00 New style and format Revised Item 25 page 5 Revised item 10 b on page 6 Revised items 12 and 13 on page 15 21 30 00 New style and format Revise...

Страница 3: ...includes the maintenance information required to be available by 14 CFR Part 23 Note This manual was formerly called the Beechcraft Starship Maintenance Manual Copyright 2006 Raytheon Aircraft Company...

Страница 4: ...dministration Regulations Diversion contrary to US law is prohibited For guidance on export control requirements contact the Commerce Department s Bureau of Export Administration at 202 482 4811 or vi...

Страница 5: ...ual give the basic number and the reissue code when applicable if a complete up to date publication is desired Should only revision pages be required give the basic number and revision code for the pa...

Страница 6: ...Effective Pages Section PAGE DATE Title Page Vol 1 Oct 31 06 Logo Page Title Page Vol 2 Oct 31 06 Logo Page A Page B10 B Page B10 Introduction 1 thru 13 Oct 31 06 NOTE The chapter List of Effective Pa...

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Страница 9: ...rvicing information is required Additional publications are listed in the current Publications Price List P N 118556 Contact your nearest Raytheon Aircraft Service Center for information on these publ...

Страница 10: ...disclaims any responsibility for malfunctions failures damage or injury caused by use of parts not approved by the Raytheon Aircraft Company Any maintenance requiring the disconnection and reconnectio...

Страница 11: ...ions are printed on yellow paper and are to be inserted in the maintenance manual in accordance with the instructions provided and adjacent to applicable chapter section and subject matter in the manu...

Страница 12: ...sion is inserted into the manual and the initials of the person s inserting the revision should be recorded on this page D Log of Temporary Revisions Page The printed manual will have a Log of Tempora...

Страница 13: ...is assigned at the option of the manufacturer and may or may not be used B Application Any publication conforming to the GAMA or ATA format will use the same basic numbering system Thus whether the m...

Страница 14: ...A Specification No 100 for use with Maintenance Manuals Parts Catalogs and Wiring Diagram Manuals The following chapters are not applicable to this Maintenance Manual 29 37 49 60 70 81 83 91 and 95 Ta...

Страница 15: ...eral 10 Exterior Color Schemes and Markings 20 Exterior Placards and Markings 12 SERVICING 00 Servicing 10 Replenishing 20 Scheduled Servicing 30 Unscheduled Servicing 20 STANDARD PRACTICES AIRFRAME 0...

Страница 16: ...oling 60 Temperature Control 22 AUTO FLIGHT 10 Autopilot 23 COMMUNICATIONS 00 General 10 Speech Communications 11 VHF Communications 12 Radiophone System 40 Ground Interphone System 50 Audio Intergati...

Страница 17: ...tem 20 Engine Fire Extinguishing 21 Portable Fire Extinguishing 27 FLIGHT CONTROLS 00 General 20 Rudder and Tabs 30 Elevators Elevons and Tabs 31 Stall Warning System 50 Flap Forward Wings 70 Control...

Страница 18: ...10 Main Gear and Doors 20 Nose Gear and Doors 30 Extension and Retraction 40 Wheels and Brakes 50 Nose Landing Gear Steering 60 Landing Gear Position and Warning 33 LIGHTS 00 General 10 Cockpit Light...

Страница 19: ...9 ELECTRICAL PANELS 10 Instrument And Control Panels 20 Electrical Electronic Equipment Panels 30 Printed Circuit Boards 51 STRUCTURES 00 General 52 DOORS 00 General 10 Passenger Crew 20 Emergency Exi...

Страница 20: ...TABILIZERS 00 General 10 Forward Wing 20 Elevator 30 Tipsails 40 Rudder 60 Ventral Stabilizer 56 WINDOWS 00 General 10 Cockpit 20 Cabin 57 WINGS 00 General 50 Eleven 61 PROPELLERS 00 General 10 Propel...

Страница 21: ...Air Intakes 70 Engine 72 ENGINE 00 General 73 ENGINE FUEL SYSTEMS 00 General 10 Fuel Distribution 74 IGNITION 00 General 76 ENGINE CONTROLS 00 General 77 ENGINE INDICATING 00 General 40 Intergrated En...

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Страница 28: ...TARSHIP 1 MAINTENANCE MANUAL List of Effective Pages CH SE SU PAGE DATE 5 LOEP 1 Oct 31 06 5 CONTENTS 1 and 2 Oct 31 06 5 10 00 1 thru 4 Oct 31 06 5 11 00 1 thru 3 Oct 31 06 5 20 00 1 thru 18 Oct 31 0...

Страница 29: ...Limited 2 Inspection Timetable 3 Starship 1 Inspection Form 4 A Left Power Plant Zone 411 4 B Right Power Plant Zone 421 6 C Environmental Systems 8 D Nose Section F S 0 to F S 95 8 E Cockpit F S 95...

Страница 30: ...TABLE OF CONTENTS Continued Log Book Entry After Hard Landing 6 Inspection After Encountering Turbulent Air 7 Repair of Damage After Encountering Turbulent Air 9 Log Book Entry After Encountering Tur...

Страница 31: ...ION REQUIREMENTS This section consists of components that are subject to a thorough inspection based on calendar time operating hours or cycles The inspections should be done with reference to this ma...

Страница 32: ...the Pratt Whitney PT6A 67A Engine Maintenance Manual Engine Perform hot section inspection as required Refer to the Pratt Whitney PT6A 67A Engine Maintenance Manual Pedestal Throttle Lever Stop Pin R...

Страница 33: ...ator and Hydraulic Lock Solenoid Valve Every 200 hours check the control actuator for no backs and the hydraulic lock solenoid valve for proper operation as detailed in Chapter 27 50 00 Flap Flexible...

Страница 34: ...AIR VALVES switch to L ENG or R ENG C Press SURF DEICE MAIN test switch make sure minimum engine N1 speed of 85 is maintained System is OK if no failure annunciations are present Pitot Static Masts Ev...

Страница 35: ...noted in this manual are based on average usage and average environmental conditions NOTE The recommended periods do not constitute a guarantee the item will reach the period without malfunction as th...

Страница 36: ...an one cumulative hour Underwater Locator Device ULD Replace at date marked on the device approx every 6 years Power Plant Engine TBO Refer to Pratt Whitney Service Bulletin Number 14603 or subsequent...

Страница 37: ...t Pump Ref Chapter 73 Refer to the applicable manual in the Starship Component Maintenance Manual 9 Utility Systems Windshield Wiper Blade Assembly Ref Chapter 30 When the blade does not clear wipe ar...

Страница 38: ...th all applicable Airworthiness Directives as specified in Part 39 of the Federal Aviation Regulations It is further the responsibility of the owner or operator to ensure that the airplane is inspecte...

Страница 39: ...INSPECTION GENERAL INFORMATION INSPECTION INTERVAL TOLERANCE To facilitate scheduling inspections Raytheon Aircraft Company authorizes the following inspection interval tolerances LETTER INSPECTIONS...

Страница 40: ...STARSHIP 1 MAINTENANCE MANUAL Page 3 B10 Oct 31 06 5 20 00...

Страница 41: ...o the Pratt Whitney PT6A 67A Engine Maintenance Manual for corrective action Ref Chapter 78 X 7 INDUCTION SYSTEM Check air intake duct and engine inlet screen for obstruction and damage Ref Chapter 71...

Страница 42: ...linkage for condition and attachment X 20 AUTOFEATHER RELAYS DUMP SOLENOIDS AND AUTOFEATHER AUTO IGNITION PRESSURE SWITCHES Check for condition security of attachment and proper electrical connection...

Страница 43: ...y Ref Chapter 74 X 6 ENGINE EXHAUST SYSTEM Examine the exhaust system and visible portions of the power turbine for burning distortion damage and cracks If any are found refer to the Pratt Whitney PT6...

Страница 44: ...nd security of attachment Check for proper operation of all pedestal controls and switches X 18 PROPELLER Dynamically balance as instructed in Chapter 61 10 00 X 19 INERTIAL ANTI ICER Check the inerti...

Страница 45: ...the evaporator filters Check filter in return air inlet of the forward and aft vent blowers for blockage and replace as necessary Ref Chapter 21 X 3 FLOW CONTROL UNIT Inspect unit and associated equi...

Страница 46: ...UATOR INSPECTION procedure Ref Chapter 27 50 00 X 12 DEICE BOOTS Visually inspect boots for cracks tears or delamination from the wing Visually inspect leading edge of boots for erosion of surface coa...

Страница 47: ...r and control wheel switches Ref Chapter 27 30 00 X 5 COLUMN SHAKER PUSHER SYSTEM Check G switch Ref Chapter 27 X 6 ELECTRICAL EQUIPMENT Check operation of all lights Check switches knobs and circuit...

Страница 48: ...lement Ref Chapter 30 70 00 X 8 WINDOWS Inspect windows and window seals for general condition Chips excessive crazing or other damage is basis for replacement of outer windows Ref Chapter 56 X 9 CABI...

Страница 49: ...BILIZER Check the drain holes in the stabilizer for obstructions condition and attachment X 7 SIGNIFICANT STRUCTURAL ITEMS Inspect for condition as outlined in Chapter 51 X H AFT WING A B C D E MECH I...

Страница 50: ...condition and attachment X 13 FLAP ROLLERS Check for condition and operation X 14 LIGHTS Check navigation recognition and landing lights for broken lenses and replace bulbs as necessary Ref Chapter 3...

Страница 51: ...including hook and springs for visible damage leakage and condition X 5 LANDING GEAR STRUT Inspect shock strut and components for condition attachment proper inflation and leakage Deflate and check fl...

Страница 52: ...Check actuator and support brackets for visible damage leakage and condition X 7 STEERING LINKAGE Check nose steering mechanism for condition attachment and correct adjustment X 8 NOSE GEAR STRUT Insp...

Страница 53: ...rity and adjustment of switches loose wires and proper indication X 4 WARNING HORN Check for proper operation X 5 LOCK LINKS Check over center mechanism for positive positioning in extended position C...

Страница 54: ...hapter 61 22 00 X 11 PROPELLER GOVERNOR Check for proper governor operation and feathering X 12 POWER CHECK Without Jetcal Refer to Chapter 77 00 00 for the procedure covering this check X 13 IDLE RPM...

Страница 55: ...nd ensure ELT is ARMED before returning airplane to service X 29 CABIN ENTRANCE LIGHT Check for proper operation with battery switch OFF if unit fails to operate check the circuit breaker Ref Chapter...

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Страница 331: ...PAGE DATE 21 LOEP 1 Oct 31 06 21 CONTENTS 1 and 2 Oct 31 06 21 00 00 1 thru 5 Feb 25 94 21 20 00 1 thru 11 Feb 25 94 21 21 00 1 thru 7 Feb 25 94 21 30 00 1 thru 28 Oct 31 06 21 40 00 1 thru 4 Feb 25 9...

Страница 332: ...ation Blower Speed Controller Removal Effectivity NC 4 8 Aft Ventilation Blower Speed Controller Installation Effectivity NC 4 8 Aft Ventilation Blower Speed Controller Removal Effectivity NC 5 and Af...

Страница 333: ...abin Altitude Warning Pressure Switch Installation 11 Cabin Altitude Warning Pressure Switch Check 11 Method One 12 Method Two 12 Auxiliary Volume Tank Removal 13 Auxiliary Volume Tank Installation 13...

Страница 334: ...Diverter Valve Installation 11 Environmental Dome Thermal Isolator Removal Effectivity NC 4 13 Environmental Dome Thermal Isolator Installation Effectivity NC 4 13 Environmental Dome Thermal Isolator...

Страница 335: ...Installation 21 Air Conditioner Service Valve Union and Service Valve Removal 21 Air Conditioner Service Valve Union and Service Valve Installation 23 Air Conditioner Sight Glass Removal 24 Air Condit...

Страница 336: ...d After 51 Aft Evaporator Condensation Drain Assembly Installation Effectivity NC 5 and After 52 Air Conditioning Refrigeration Plumbing 53 21 60 00 Temperature Control Description and Operation 1 Coc...

Страница 337: ...ower Pressure Switch Installation Effectivity NC 4 21 Aft Ventilation Blower Pressure Switch Removal Effectivity NC 5 and after 21 Aft Ventilation Blower Pressure Switch Installation Effectivity NC 5...

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Страница 361: ...lly controlled according to crew selected settings Full rotation of the manual rate control valve clockwise selects the DUMP position and will depressurize the cabin The cabin pressurization controlle...

Страница 362: ...cabin pressure The outflow valve poppets are held open and pressurization of the cabin is prevented while the airplane is on the ground Before takeoff when the power levers are advanced far enough to...

Страница 363: ...TCH CABIN PRESSURE 1 MODULE N SPEED CONTROL 1 90 GREATER THAN L R N LEFT SQUAT SWITCH AIRPLANE ON THE GROUND SWITCH CB L SQUAT TRIPLE FED BUS 5 SYSTEM CB PRESSURE FED BUS TRIPLE 5 ATMOSPHERE AIR ATMOS...

Страница 364: ...Oct 31 06 B10 This Page Intentionally Left Blank 21 30 00 STARSHIP 1 MAINTENANCE MANUAL Page 4...

Страница 365: ...on control module assembly 221 Solenoid Valves B and C Part of the pressurization control module assembly 221 Volume Tank Mounted on top of the pressurization control module assembly 221 Continuous Fl...

Страница 366: ...g Remove the nuts securing the outflow valves and seals to the outflow valve access door and remove the outflow valves and seals h Carefully remove the reducer and packing from the outflow valve altit...

Страница 367: ...ough to access the pneumatic lines CAUTION Do not remove the outflow valve access door until the pneumatic lines are disconnected from the outflow valves d Tag and disconnect the pneumatic lines from...

Страница 368: ...and disconnect the pressurization control system plumbing from all three jet pump ejector ports and remove the ejector h Remove the reducer from the CONTROL PORT of the jet pump ejector Remove and di...

Страница 369: ...r 10 Chart 1 21 00 00 and sealant 24 Chart 1 21 00 00 to the adapter threads to be installed in the manual shutoff valve and install the adapters in the manual shutoff valve b Connect the pneumatic pl...

Страница 370: ...ght of center d Disconnect the static air hose from the pressure switch e Remove the screws lock washers and washers securing the pressure switch to the mounting bracket and remove the pressure switch...

Страница 371: ...ring harness g Align the cabin altitude warning pressure switch with the mounting bracket and secure with washers and screws h Connect wiring to the cabin altitude warning pressure switch according to...

Страница 372: ...n a position so that it can be clearly read c Increase the vacuum in the chamber and check for onset of continuity at an increasing altitude of 9 500 to 10 000 feet d After continuity is acquired slow...

Страница 373: ...lation a Remove all electrical power from the airplane b Remove the pilot s seat c Disconnect the pneumatic line from the auxiliary volume tank d Remove the two screws and washers securing the auxilia...

Страница 374: ...to be replaced remove the elbow jam nut washer and packing from the filter housing boss Discard the packing PRESSURIZATION CONTROL SYSTEM CONTINUOUS FLOW AIR FILTER INSTALLATION CAUTION The air filte...

Страница 375: ...N CAUTION The pressurization control module assembly must be electrically bonded to the forward pressure bulkhead and LH cockpit floorboard panel Electrical bonding requirements are specified in Chapt...

Страница 376: ...tion b Position the pneumatic relay in the control module assembly and connect the pneumatic lines according to tags CAUTION Ensure that the pneumatic lines are connected to the proper fittings and po...

Страница 377: ...er from the airplane b Refer to PRESSURIZATION CONTROL MODULE ASSEMBLY REMOVAL in this chapter and remove the control module assembly CAUTION When working around the control module assembly extra care...

Страница 378: ...e union in the inflow port of the C solenoid valve e Carefully remove the C solenoid valve from the restrictor assembly Remove and discard the packing from the restrictor assembly f Remove the union f...

Страница 379: ...s specified in Chapter 20 00 03 a Install the adapters in the cabin pressurization controller pneumatic ports b Align the cabin pressurization controller with the cabin pressurization control panel an...

Страница 380: ...llation a Remove all electrical power from the airplane b Remove the copilot s seat c Remove the copilot s inboard subpanel electroluminescent panel Ref Chapter 31 10 00 d Remove the screws securing t...

Страница 381: ...20 00 03 a Align the cabin altitude differential pressure indicator with the copilot s inboard subpanel and secure with screws b Connect the static air plumbing to the pressure indicator according to...

Страница 382: ...r is secure i Exit all personnel from the airplane j Close and latch the cabin door and any access panels that contribute to pressurization NOTE Secure heavy strength nylon safety straps to the cabin...

Страница 383: ...s As the cabin pressure reaches 8 0 0 1 psi the cabin will begin to peak and the cabin climb indicator will show a climb NOTE If the rated pressure cannot be reached determine the source of excess lea...

Страница 384: ...vessel 1 Nose wheel well 2 Hoses plumbing and wire bundles piercing the pressure vessel 3 Windshield seal and attachment hardware 4 Seal around emergency exit door 5 Seal around the cabin door 6 Acces...

Страница 385: ...of the tee f Connect a pitot static tester 6 Chart 1 21 00 00 or equivalent to the atmospheric sense line port 1 on the left outflow valve dome g Set the pitot static tester altitude to 29 92 in hg Re...

Страница 386: ...21 30 00 STARSHIP 1 MAINTENANCE MANUAL Page 26 Oct 31 06 B10 Outflow Valve Functional Test Diagram Figure 3...

Страница 387: ...STARSHIP 1 MAINTENANCE MANUAL Page 27 B10 Oct 31 06 21 30 00 ALTITUDE TO PRESSURE CROSS REFERENCE Chart 2...

Страница 388: ...he valve or may leave a residue which will interfere with the valve action d Refer to OUTFLOW VALVE INSTALLATION in this chapter and install the outflow valves CABIN PRESSURIZATION CONTROLLER FILTER C...

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Страница 777: ...ANCE MANUAL List of Effective Pages CH SE SU PAGE DATE 26 LOEP 1 Oct 31 06 26 CONTENTS 1 and 2 Oct 31 06 26 00 00 1 and 2 Feb 25 94 26 10 00 1 thru 10 Feb 25 94 26 11 00 1 thru 10 Feb 25 94 26 20 00 1...

Страница 778: ...onal Test 10 26 11 00 Engine Bleed Air Warning System Description and Operation 1 Engine Bleed Air Warning System Troubleshooting 2 Engine Bleed Air Warning System Maintenance Practices 6 Bleed Air Wa...

Страница 779: ...ng Description and Operation 1 Portable Fire Extinguishing Effectivity NC 4 thru NC 7 1 Portable Fire Extinguishing Effectivity NC 8 and After 1 Portable Fire Extinguishing Maintenance Practice 3 Port...

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Страница 802: ...OSED light switches and the EXTINGUISHER PUSH light switches The electrical power for the light switches originates from 5 ampere circuit breakers identified as CB1 left and CB2 right located on the r...

Страница 803: ...of extinguishing agent is discharged from the fire extinguisher bottle A fill and safety relief valve is located on the fire extinguisher bottle The safety relief valve releases pressure from 1520 to...

Страница 804: ...B10 Oct 31 06 26 20 00 STARSHIP 1 MAINTENANCE MANUAL Engine Fire Extinguishing System Figure 1 Page 3...

Страница 805: ...26 20 00 STARSHIP 1 MAINTENANCE MANUAL Page 4 Oct 31 06 B10 This Page Intentionally Left Blank...

Страница 806: ...STARSHIP 1 MAINTENANCE MANUAL Page 5 B10 Oct 31 06 26 20 00 Left Engine Fire Extinguishing System Electrical Schematic Figure 2...

Страница 807: ...26 20 00 STARSHIP 1 MAINTENANCE MANUAL Page 6 Oct 31 06 B10 Right Engine Fire Extinguishing System Electrical Schematic Figure 3...

Страница 808: ...hield electrical connector P310 pin 8 If pin 2 does not check to ground repair ground circuit At completion of troubleshooting and or repair remove the plastic protection cap from the cartridge electr...

Страница 809: ...d to Step 4 NO Repair electrical wiring as necessary Step 4 Is there continuity between the OK light and relay K16 left or K18 right YES Proceed to Step 5 NO Repair electrical wiring as necessary Step...

Страница 810: ...epair electrical wiring as necessary Step 4 Is there continuity between relay K16 left K18 right and printed circuit board A130 YES Proceed to Step 5 NO Repair electrical wiring as necessary Step 5 Is...

Страница 811: ...Perform system operational test Refer to FIRE EXTINGUISHING SYSTEM OPERATIONAL TEST NO If there is no continuity through the pressure switch a defective pressure switch is probable or the pressure ha...

Страница 812: ...trical connector from the fire extinguisher bottle cartridge squib d Install a plastic protection cap on the electrical connector of the cartridge to prevent accidental firing of the explosive cartrid...

Страница 813: ...ccess panel 581AT left 681AT right assembly Ref Chapter 54 00 00 FIRE EXTINGUISHER BOTTLE INSPECTION NOTE The fire extinguisher bottles must be replaced at the interval specified in Chapter 4 a Inspec...

Страница 814: ...B10 Oct 31 06 26 20 00 STARSHIP 1 MAINTENANCE MANUAL Engine Fire Extinguishing System Installation Figure 4 Page 13...

Страница 815: ...Oct 31 06 B10 This Page Intentionally Left Blank 26 20 00 STARSHIP 1 MAINTENANCE MANUAL Page 14...

Страница 816: ...nt tube between the fire extinguisher bottle outlet port fitting and the special bulkhead fitting on the forward side of the engine firewall Ref Figure 4 d Disconnect the forward nozzles and bracket a...

Страница 817: ...A130 Refer to Figures 2 or 3 and or the BEECHCRAFT Starship 1 Wiring Diagram Manual to trace the electrical circuits The Left and Right FIRE EXT test switches located on the pilot s outboard subpanel...

Страница 818: ...itch to OFF Set the BATT switch to OFF NOTE Two individuals are required to perform Steps i and j i Left Extinguisher Voltage Check 1 Connect the negative lead of a dc voltmeter to wire W174C22 2 Conn...

Страница 819: ...by the operator in the cockpit 2 Set the BATT switch to ON Set the EXT PWR switch to the on position 3 Press and hold the RIGHT ENG FIRE PUSH TO EXT switch The test lamp should illuminate 4 Release t...

Страница 820: ...e on the right engine fire extinguish switch Set the RIGHT ENG FIRE TEST EXT switch to OFF the D or DISCH and OK indicators go out u Set the RIGHT ENG FIRE TEST EXT switch to TEST B The OK indicator s...

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Страница 938: ...HIP 1 MAINTENANCE MANUAL List of Effective Pages CH SE SU PAGE DATE 28 LOEP 1 Oct 31 06 28 CONTENTS 1 thru 5 Oct 31 06 28 00 00 1 thru 12 Oct 31 06 28 10 00 1 thru 52 Feb 25 94 28 20 00 1 thru 29 Feb...

Страница 939: ...and Operation 1 Forward Fuel Tanks 1 Fuel Tank Access Openings 1 Tank Baffles 3 Wing Fuel Filler 3 Refueling Grounding Recepticale 3 Hopper Compartment 3 Hopper Compartment Manifold 4 Gravity Feed Li...

Страница 940: ...l 27 Gravity Feed Line and In Line Check Valve Installation 28 Hopper Compartment Manifold Removal 28 Hopper Compartment Manifold Installation 30 Forward Tank Fuel Drain Valves Removal Effectivity NC...

Страница 941: ...r Check Valve Assembly Installation 50 Aft Fuel Tank Vent Removal 50 Aft Fuel Tank Vent Installation 51 28 20 00 Fuel Distribution Description and Operation 1 Fuel Distribution Components Description...

Страница 942: ...l Check Purge Valve With Fuel Flow 29 28 40 00 Fuel Indicating Description and Operation 1 Fuel Quantity Indicating 1 Fuel Quantity Probes 1 Fuel System Concentrator 6 Digital Fuel Quantity Indicators...

Страница 943: ...OF CONTENTS Continued Oct 31 06 B10 28 CONTENTS Fuel Temperature Sensor Removal 22 Fuel Temperature Sensor Installation 22 Fuel Low Level Sensor Removal 22 Fuel Low Level Sensor Installation 22 Low F...

Страница 944: ...of each specification is listed No attempt has been made to update the listing to the latest revision It is the responsibility of the technican or mechanic to determine the current revision of the app...

Страница 945: ...cludes the fuel quantity indicating systems fuel temperature indicating systems fuel low level indicating systems and the fuel pressure warning systems NOTE For continuation of the engine fuel supply...

Страница 946: ...ection to the adjacent conductive structure f The airplane must be grounded to an approved ground at all times with a proper and serviceable grounding cable s Ground cables should always be connected...

Страница 947: ...losive proof lights and air driven power tools j Close all tank openings when work is not in progress to prevent entry of dirt dust and foreign matter Fuel tanks requiring extensive work should be vac...

Страница 948: ...in the fuel filters When contamination is discovered it must be removed a Completely defuel the airplane Ref Chapter 12 10 00 CAUTION When performing open fuel tank maintenance refer to General Preca...

Страница 949: ...o classified as to immediate repair required and leaks not considered a potential flight hazard Fuel leaks that are classified as a stain seep or heavy seep in an open area require repair when the air...

Страница 950: ...STARSHIP 1 MAINTENANCE MANUAL Page 7 B10 Oct 31 06 28 00 00 Fuel Leak Classification Figure 1...

Страница 951: ...ing must be completed within the work life application time of the sealant Marking on sealing surface is permitted only with felt tip ink markers or stamps with ink No grease pencils or any other cont...

Страница 952: ...in capacity A third container may be hooked into the test setup to provide an optional overflow collector if desired The two containers should be provided with rubber stoppers that have holes for the...

Страница 953: ...ect against skin irritation when handling the cloth As a further protection against possible penetration of the phenolphthalein solution through the gloves wash your hands thoroughly after finishing t...

Страница 954: ...STARSHIP 1 MAINTENANCE MANUAL Page 11 B10 Oct 31 06 28 00 00 Bladder Fuel Cell Leakage Test Figure 2...

Страница 955: ...hipped to the cell manufacturer for repair which have foreign material applied to the fittings or fuel cell walls either inside or outside will not be repaired and all warranty is null and void Foreig...

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