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Commander

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2013

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Содержание Commander 112

Страница 1: ...referred to as Model 112A At the time of issue of this Maintenance Manual the contents were to the best of Rockwell International s knowledge adaquate to maintain the aircraft in a continued airworthy...

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Страница 6: ...4 16 Revision 1 4 17 Change 1 Page Issue 4 18 thru 4 24 Revision 1 4 25 Change 3 4 26 thru 4 28 Revision 1 4 29 Change 3 4 30 thru 4 34 Change 2 5 1 Change 2 5 2 thru 5 4 Revision 1 5 5 thru 5 6 Chang...

Страница 7: ...6A Change 2 10 66B Blank Change 2 10 67 thru 10 68 Change 1 10 68A Change 1 10 68B Blank Change 1 10 69 thru 10 70 Change 2 10 70A Change 3 10 70B Blank Change 2 10 71 thru 10 72 Revision 1 10 73 Chan...

Страница 8: ...ll manuals delivered from the factory All recommended changes will be reviewed by Cus tomer Service Engineering etc before incorpora tion or rejection Additional forms may be requested from Rockwell I...

Страница 9: ...lowing definitions apply to WARNINGS CAUTIONS and NOTES found throughout the manual ii IWARNING I An operating procedure practice or condition etc which may result in injury or death if not carefully...

Страница 10: ...G INSPECTION AIRFRAME MAINTENANCE LUBRICATION AND STORAGE 2 1 III HYDRAULICS 3 1 IV POWER PLANT AND PROPELLER 4 1 V FUEL SYSTEM 5 1 VI LANDING GEAR WHEELS AND BRAKES 6 1 VII FLIGHT CONTROLS 7 1 VIII I...

Страница 12: ...er Inlet Screen 5 9 Fuel Selector 5 9 Trouble Shooting Fuel System 5 10 Figure 6 1 6 2 6 3 6 4 6 5 6 6 6 7 6 8 6 9 6 10 6 11 6 12 7 1 7 2 7 3 7 4 7 5 7 6 7 7 7 8 7 9 7 10 7 12 7 11 7 13 7 14 7 15 7 16...

Страница 13: ...thru 10 38 See Wiring Diagrams Index Part II 10 33 10 39 Connector and T Strip Locator 10 46 10 40 thru 10 49 See Wiring Diagrams Index Part III 10 47 10 50 thru 10 57 See Wiring Diagrams Index Part...

Страница 14: ...ine cowling provide easy access to aircraft and engine systems components The retractable tricycle landing gear is operated hy draulically during normal operation Passenger and pilot comfort are assur...

Страница 15: ...NANCE MANUAL 1 25 O 50 1 32 9 ft 35 7 20 112 10 8 44 112B TC TCA 10 11 40 Figure 1 1 General Dimensions 1 2 1 8 r ROCKWELL COMMANDER 112 B TC TCA X161A7 Change 1 Copyright Commander Owners Group 2013...

Страница 16: ...18 00 sq ft 33 64 sq ft 18 00 sq ft 17 00 sq ft 22 36 sq ft 5 00 sq ft 5 75 sq ft FUSELAGE AND WING STATIONS The station diagram shown in Figure 1 2 provides a convenient method for identifying and lo...

Страница 17: ...47 16 1 I 58 95 70 50 I I 275 122 286 08 LEFT HORIZONTAL STABILIZER N 0 275 12 298 50 I Z 120 50 Z 82 75 Z 83 80 Z 63 41 Z 28 58 I I J o 22 00 27 50 62 50 85 00 123 00 168 32 178 00 205 00 230 50 263...

Страница 18: ...L PI l N l til l 0 N z l 0 Lt 0 r 0 Lt N t N 0 LI 0 N o o 0 0 r N C CI I N LI r N 00 N Figure 1 2 Station Diagram Sheet 2 of 2 Change 3 SECTION I GENERAL INFORMATION M C N o o M C N o Lt l I 0 M N o o...

Страница 19: ...ize stressed and beaded skin construction to provide maximum strength with minimum structural components The horizontal surface is of single unit constructions with a fixed for ward surface and a hing...

Страница 20: ...extension knob in the DOWN position to release hydraulic fluid trapped in the uplock portion of actu ators This bypasses hydraulic fluid directly to the Change 1 hydraulic power pack reservoir allowi...

Страница 21: ...ilation system utilizes the fresh air intake openings in the leading edge of the wing to supply fresh air to the floor level outlets 1 8 ELECTRICAL SYSTEM The 14 volt dc electrical system obtains powe...

Страница 22: ...be accom plished by the following methods Hydraulic System Engine Oil System Engine Induction Air Filter Cleaning Fuel System Landing Gear Wheels and Brakes Battery INSPECTION Inspection Checklist AIR...

Страница 23: ...ure may freeze in brakes or if brakes are overheated Close cowl flaps install internal control 2 2 lock Figure 2 1 and pitot covers and place chocks under wheels MOORING Park aircraft as previously ou...

Страница 24: ...pera tures Whenever possible shelter aircraft in a heated hangar to prevent frost ice and snow accumu lation which requires added maintenance time to remove These weather elements if allowed to ac cum...

Страница 25: ...erated in cold weather POST FLIGHT MAINTENANCE Cold weather opera tion demands procedures that are in addition to normal post flight maintenance procedures The engine should be allowed to run dry by c...

Страница 26: ...or valve LEFT or RIGHT fullest tank STARTING COLD ENGINE a Mixture control lever full RICH b Propeller control lever High RPM c Throttle control lever forward approximately one fourth inch d Induction...

Страница 27: ...control lever full for ward ill RPM and note any indication of sluggish or erratic operation Refer to Section IV if propeller does not operate properly Do not allow cylinder head and oil temp peratur...

Страница 28: ...S 13 INDUCTION AIR FILTER 5 FUEL TANK FILLER VALVES AND CAPS 14 NOSE GEAR STRUT INFLATING VALVE 6 FUEL SELECTOR VALVE DRAIN 112 TC 15 NOSE TIRE iNFLATING VALVE 7 BATTERY 16 NOSE GEAR SHIMMY DAMPENER 8...

Страница 29: ...close drain valve pUll down and remove hose e Clean oil suction screen as outlined in this section f Remove and replac e full flow oil filter g Add eight quarts of oil and check level with dip stick...

Страница 30: ...f time accomplish the following steps a Install new or cleaned oil sc reen and filter element and fill sump with new oil b Operate engine until cylinder head temperature is within green range Operate...

Страница 31: ...L SYSTEM RE FUELING Refuel aircraft with fueling facilities that contain filters for removing the moisture content from the fuel If fueling faCilities with filters are not available filter fuel throug...

Страница 32: ...nless improper fuel circulation requires immediate service to the system See Section V for removal and cleaning instructions DE FUELING Gasoline fumes are present during de fueling operation therefore...

Страница 33: ...r belt tension Lycoming Service In struction 1129 6 Engine oil Lycoming Service Instruction 1014 7 Oil screens Lycoming Service Instruction 1023 8 Magneto timing Lycoming Service Instruction 1132 1080...

Страница 34: ...y be balanced on automotive type balanCing equipment Clean tires with soap and water If air craft is out of service rotate tires every seven days to prevent flat spots from developing BRAKE BLEEDING B...

Страница 35: ...Repair Sealant 5000 White Sealer Dow Corning Corp RTV 732 24 hour Coast Pro Seal 700 72 hour MIL S 38249 Type 1 NOTE Class A indicates brushable material Class B indicates filleting or injection mate...

Страница 36: ...e Windshield and Window Removal and Installation REPAIR OF SEALANTS Should the sealant become damaged during its work life it may be repaired by remOving the damaged filler and applying new sealant or...

Страница 37: ...two of cloth may be used to strengthen area i Place patch on the inside of structure over the hole Cover with cellophane and squeegee from center to edges to remove all air bubbles and assure adhesion...

Страница 38: ...NDOW UPPER RETAINERS 5 CABIN WINDOW FORWARD RETAINERS r 6 CR 12 SFR SINGLE FACED RUBBER FOAM 7 PRODUCTS RESEARCH CO NUMBER 5000 WHITE SEALER 8 PRODUCTS RESEARCH CO 1221 SEALER 9 WINDSHIELD RETAINER 10...

Страница 39: ...ENANCE MANUAL 1 INTERIOR DOOR HANDLE 2 DOOR HANDLE ADJUSTMENT CABLE 3 PIVOT PIN 4 COTTER PIN 5 EXTERIOR DOOR HANDLE 6 DOOR LOCK 7 VENT WINDOW Figure 2 10 Cabin Door Sheet 1 of 3 2 18 ROCKWELL COMMANDE...

Страница 40: ...ENANCE MANUAL 1 INTERIOR DOOR HANDLE 2 LATCH ASSEMBLE 3 PIVOT PIN 4 COTTER PIN 5 EXTERIOR DOOR HANDLE 6 DOOR LOCK 7 VENT WINDOW Figure 2 10 Cabin Door Sheet 2 of 3 Change 2 SECTION IT SERVICING AND IN...

Страница 42: ...ay soften the plastic and produce visual distortion REPAIR OF WINDSHIELD AND WINDOWS Windows that are extensively damaged should be replaced rather than repaired since even a carefully patched area wi...

Страница 43: ...ign and press window into frame channel d Apply Products Research Co number 5000 white sealer to inside of window e Install retainers and secure with mounting screws f Clean window area of excess whit...

Страница 44: ...use lage skin To adjust striker hook remove striker plate and spacer then rotate hook to desired position Change 2 Replace spacer and striker plate The weather strip around the perimeter of the interi...

Страница 46: ...n the door edges to permit a smooth tight fit Install the door by reversing the above procedure SEATS FRONT SEATS Standard individual front seats are equipped with manually operated reclining seat bac...

Страница 47: ...IEW 0 0 X2212 CENTER LINE FORGING AN174 12A BOLT AN960 416 WASHER MS20365 428 NUT TORQUE 50 70 IN LBS c f NASI106 13 BOLT AN960 616 WASHER MS20364 624 NUT TORQUE 95 110 IN LBS X22 13 AFT ATTACH MOUNT...

Страница 48: ...ileron balance cable support bracket and pulley from spar web attach point q Remove bolts securing truss assembly to main spar and aft cabin mounts and remove assembly Use extreme care to prevent notc...

Страница 49: ...rtical stub spar i Remove upper portion of vertical stabilizer VERTICAL STABILIZER INSTALLATION To install the vertical stabilizer reverse the preceding steps and check rudder control rigging in accor...

Страница 50: ...ESS COVER MOUNT ELEVATOR TRIM ACCESS TYPICAL BOTH SIDES SPAR MOUNT ACCESS OVHD VENTILATION ELECTRIC WffiING HARNESS ACCESS BATTERY HYD POWER PACK FLOOR LEVEL ACCESS PLATES 3 EACH SIDE ACCESS PANEL Fig...

Страница 51: ...OF LUBRICATION MIL G 81322 AIRCRAFT GREASE ROCKWELL COMMANDER 112 B TC TCA X2224 MIL G 23827 AIRCRAFT GREASE Top of nose gear trunnion only MIL G 81322 AIRCRAFT GREASE MIL L 5606 HYDRAULIC FLUID MIL L...

Страница 52: ...NISM B CABIN DOOR r50 HOURS rr 50 HOURS SECTION II SERVICING AND INSPECTION X22 20 X22 21 C ELEVATOR AND TRIM TAB ASSEMBLY II 50 HOURS X2225 Figure 2 15 Lubrication Chart Sheet 2 of 4 2 27 Copyright C...

Страница 53: ...100 HOURS MAINTENANCE MANUAL E FLAP AND AILERON ASSEMBLY 50 HOURS X2222 G MAIN GEAR DOORS ROCKWELL COMMANDER 112 B TC TCA X22 23 1 50 HOURS 50 HOURS XI67 XI68 Figure 2 15 Lubrication Chart Sheet 3 of...

Страница 54: ...DDER TRIM AND NOSE WHEEL STEERING l _ HF HF DAILY f 100 HOURS 50 HOURS 100 HOURS J NOSE GEAR DOOR MODEL 112 TC 50 HOURS f XI65A rl HOURS As Required X2238 MODEL 112B TCA XI66 X2239 Figure 2 15 Lubrica...

Страница 55: ...freezing Emulsion type cleaners usually contain solvents which are injurious to rubber if al lowed to remain in contact for any length of time therefore rinse affected area immediately with water Aft...

Страница 56: ...In addi tion the engine must be prepared and stored in ac cordance with installation and storage details contained Change 3 RETURNING AIRCRAFT TO SERVICE If proper procedures have been observed during...

Страница 57: ...AN320 12 15 30 40 60 85 95 110 270 300 290 410 480 600 660 780 1300 1500 1500 1800 2200 3300 3000 4200 5400 6600 See Note 4 12 19 30 48 60 106 95 240 270 390 290 500 480 750 660 1060 1300 2200 1500 2...

Страница 58: ...the piston locks on each actuating cylinder and the overtravel in the drag brace assisted by emergency extension springs The system is protected from Change 2 Page Hydraulic Power Pack 3 9 Emergency...

Страница 59: ...ing fluid Federal SpeCification P D 680 and dry with moisture free air d Inspect component parts for cracks nicks burrs scratches scoring and condition of threads on com ponent parts and fittings e Cl...

Страница 60: ...NGS THERMAL RELIEF VALVE 2025 2425 PSI I N OlE PRESSURE CONTROL VALVES AND THERMAL RE LIE F VALVE REMAIN IN POSITION SHOWN UNLESS PRESSURE LIMITS ARE EXCEEDED GEAR UP CHECK VALVE OPENS AT BEGINNING OF...

Страница 61: ...P PILOT CHECK VALVE MODEL 112 437 AND SUBS ALL MODELS 112B TC TCA i VALVE THERMAL RELIEF VALVE 2025 2425 PSI NOI PRESSURE CONTROL VALVES AND THERMAL RELIEF VALVE REMAIN IN POSITION SHOWN UNLESS PRESSU...

Страница 62: ...ENSION VALVE o SEE FIGURE 3 3 FOR EFFECTIVITIES AND PRESSURE SETTINGS HYDRAULIC POWER PACK ASSE MBLY t o RIGHT MAIN GEAR t 1 ACTUATOR o c J D i FREE FALL I g NOSE GEAR EXTEND ACTUATOR ASSISTED BY SPRI...

Страница 63: ...rational check as outlined be low Functional test procedures applicable to speCific components of the hydraulic system are also incorpo rated in this section Procedures contained in the pre ceding Gen...

Страница 64: ...NTENANCE MANUAL COVER PLATE MODEL 112 1 THRU 380 SECTION III HYDRAULICS SNAP RING I z _ SPRING PISTON DETENT LOCKNUT SET SCREW X239A END PLUG X239A Figure 3 4 Landing Gear Actuating Cylinders Sheet 1...

Страница 65: ...CYLINDER ROD SETSCREW MODEL 112 381 AND SUBSEQUENT MODEL 112B TC TCA PLUG PISTON Figure 3 4 Landing Gear Actuating Cylinders Sheet 2 of 2 3 8 ROCKWELL COMMANDER 112 B TC TCA X23 IDA X23 IDA Change 2...

Страница 66: ...to rotate c Connect hydraulic lines to actuators d Operate hydraulic power pack to purge system of air as necessary and check fluid level in reservoir e Fill reservoir as needed f Pressurize actuator...

Страница 67: ...m pletion of psi check During pre ceding checks there should be no external leakage Place gear selector switch in UP position Check for following 1 Gear shall retract in 14 seconds maximum 2 Pressure...

Страница 68: ...sengaged EMERGENCY EXTENSION FREE FALL TEST With the aircraft on jacks retract the landing gear and place the throttle in midposition Apply a five and Change 4 one half pound weight to the axle of the...

Страница 69: ...k tained in Section VI TROUBLE SHOOTING The trouble shooting figure in this section discusses 3 12 symptoms which can be diagnosed and interprets the results in terms of probable causes and the appro...

Страница 70: ...lve Check visually Reset circuit breaker Check visually Reset circuit breaker Check wiring Replace defective wiring To check switches and wiring refer to Section X Check wiring Replace defective wirin...

Страница 71: ...eakage in system Hydraulic power pack pump high pres sure relief valve out of adjustment Leakage in system Hydraulic power pack vent port restricted REMEDY ROCKWELL COMMANDER 112 B TC TCA Check visual...

Страница 72: ...propeller A separate manual prepared by the engine manufac turer provides complete information concerning en Change 2 Page Throttle 4 17 Mixture Control 4 18 Propeller Control 4 18 Alternate Air Cont...

Страница 73: ...O J J PROPELLER FUEL PUMP INLET MODELS 112 B THROTTLE LEVER OIL DRAIN BREATHER OIL FROM COOLER VENT LINE CONNECTION MODELS 112TC TCA MIXTURE CONTROL LEVER OIL SUCTION SCREEN X246 TACHOMETER CONNECTION...

Страница 74: ...transformer coil and a distributor A two lobe cam is secured to the breaker end of the rotating magnet shaft The distri butor gear is driven at one third magneto shaft speed High tension current gene...

Страница 75: ...e marked at 20 and 25 degrees Con sult engine nameplate for correct advance timing mark to use Continue rotating the crankshaft until the tim ing pointer and the parting flange of the crankcase align...

Страница 76: ...ion in the center of the housing Rotate mag net drive shaft in normal direction of rotation until the painted tooth on large distributor gear is centered in the timing hole The shaft on the impulse co...

Страница 77: ...ntake air is di rected through an oil impregnated filter element and flexible ducts for delivery to the induction air box The air box then directs the filtered air to the fuel 4 6 injector unit for th...

Страница 78: ...ANUAL MODEL 112B SECTION IV POWER PLANT AND PROPELLER AIR FILTER HOUSING I AIR FILTER MODEL 112 AIR FILTER HOUSING AIR FILTER t lll AIR FILTER AIR FILTER HOUSING Figure 4 4 Induction Air System X244 X...

Страница 79: ...o valve This provides regulated servo pressure for operation of the fuel flow divider valve which schedules a fuel flow that is correctly proportioned to the engine inlet airflow A balanced fuel flow...

Страница 80: ...CUT OFF AIR INLET 10 FUEL AIR BLEED NOZZLE 9 FLOW DIVIDER VALVE 10 NOZZLE ONE PER CYLINDER 11 THROTTLE VALVE 12 IMPACT TUBE 13 BALL SERVO VALVE 14 FUEL DIAPHRAGM 6 FUEL FLOW GAGE RT HALF OF DUAL GAGE...

Страница 81: ...r fuel flow port and a fuel flow gage located in the instrument panel to provide an accurate indication of metered fuel flow to the engine AIR BLEED NOZZLES MODELS 112 B An air bleed nozzle installed...

Страница 82: ...ger adapter and torque as required c Uncap and install all fuel lines Change 1 When replacing AI0 5200 carburetor with another carburetor of the same number assure needle valve assembly retainer is se...

Страница 83: ...rward side of engine firewall and receives its cooling air from the engine nacelle external scoop Oil under pressure from the engine enters the inboard side of the cooler passes through the cooler and...

Страница 84: ...ating of engine BAFFLE REMOVAL REPAIR AND INSTALLATION Removal and installation on the various baffles can be made with the engine cowling removed Insure that any replaced baffles and seals are instal...

Страница 85: ...T AND PROPELLER MODELS 112 B MODELS 112TC TCA 4 14 MAINTENANCE MANUAL MUFFLER Figure 4 7 Exhaust Stack ROCKWELL COMMANDER 112 B TC TCA X249A6 X2433 Copyright Commander Owners Group 2013 All Rights Res...

Страница 86: ...T FRONT BAFFLE MODELS 112 B MAINTENANCE MANUAL RIGHT AFT BAFFLE LEFT SIDE FORWARD BAFFLE LEFT FRONT BAFFLE Figure 4 8 Engine Baffle Assembly Sheet 1 of 2 SECTION IV POWER PLANT AND PROPELLER LEFT SIDE...

Страница 87: ...16 MAINTENANCE MANUAL RIGHT FORWARD BAFFLE ASSEMBLY BOTTOM BAFFLE ASSEMBLY LEFT FORWARD BAFFLE ASSEMBLY Figure 4 8 Engine Baffle Assembly Sheet 2 of 2 ROCKWELL COMMANDER 112 B TC TCA LEFT REAR BAFFLE...

Страница 88: ...t to activate the warning bell circuit when the engine manifold pressure is ap proximately 14 inches Hg Procedures for adjusting the micro switch is provided in Section VI Change 1 MODELS 112TC TCA Th...

Страница 89: ...ntrols engine rpm and propeller pitch by altering the propeller governor setting Forward movement of the control lever decreases propeller pitch and 4 18 increases engine rpm and aft movement increase...

Страница 90: ...ator belt tension should be maintained to provide satisfactory service see Lycoming Service Instructions Number 1129A For additional informa tion concerning the alternator system refer to Sec tion X R...

Страница 91: ...ER 4 RUBBER SHOCK PAD 5 DAMPER 6 RUBBER SHOCK PAD 7 BOLT 8 NUT 9 WASHER 10 BOLT 11 ENGINE MOUNT 4 20 MAINTENANCE MANUAL 10 Figure 4 10 Engine Mount Sheet 1 of 2 ROCKWELL COMMANDER 1t2 B TC TCA X248 Co...

Страница 92: ...4 RUBBER SHOCK PAD 5 DAMPER 6 RUBBER SHOCK PAD 7 BOLT 8 NUT 9 WASHER 10 BOLT 11 ENGINE MOUNT MAINTENANCE MANUAL Figure 4 10 Engine Mount Sheet 2 of 2 SECTION IV POWER PLANT AND PROPELLER X242 4 21 Co...

Страница 93: ...trol cables from servo regulator 1 Disconnect electrical wiring from engine m Disconnect engine ground wire n Disconnect propeller control cable from prop governor o Secure control cables at firewall...

Страница 94: ...as received from the manufacturer requires the addition of certain ac cessories wiring ducting and lines prior to instal lation This is accomplished during engine buildup It is recommended that the ol...

Страница 95: ...tle and mixture control cables to servo regulator h Connect electrical wiring to engine 4 24 i Attach engine ground wire j Connect propeller control cable to propeller governor k Install oil cooler oi...

Страница 96: ...ure OF Using SAE 50 Oil Desired Maximum Cylinder Head Temperature OF Maximum Recommended Dry Weight Lbs Approx w accessories Turbocharger Direction of rotation as viewed facing drive pad IO 360 C1D6 l...

Страница 97: ...d screens cleaned installed and safetied 4 26 t 10 Fuel cells for sufficient fuel and fuel sumps drained Install cowling A new engine has been carefully run in and has passed a rigid final test at the...

Страница 98: ...how to correct ignition problems to eliminate the adverse effect on operating economy and flight safety Spark plugs cause the majority of ignition problems Normal erosion of the plug electrodes caused...

Страница 99: ...REMOVAL a Remove screws and washers attaching propeller spinner to spinner wlkheads see Figure 4 13 b Remove upper and lower engine cowling to gain access to propeller attaching nuts c Break safety wi...

Страница 100: ...NGLE DIFFERENCE CHECK a Remove spinner from propeller See proce dures under propeller removal Change 3 b Measure 30 inches out from center of propeller hub and mark each blade c Set propeller protract...

Страница 101: ...peed stop screw jam nut c Turn stop screw in to decrease maximum rpm and out to increase maximum rpm One full revolu tion of stop screw causes a change of approximately 25 rpm d Tighten stop screw jam...

Страница 102: ...DY Review starting procedure Refer to Section V Clear excess fuel Remove and check Clean test and regap Check by rotating propeller ignition switch OFF Repair or replace magneto Check continuity Repai...

Страница 103: ...de propeller or exces sive blade friction ROCKWELL COMMANDER 112 B TC TCA REMEDY Refer to Section V Remove and check Clean and re gap Replace if defective Refer to Section X Check compression Listen f...

Страница 104: ...mechanism inside propeller or exces sive blade friction Defective prop governor Damage 0 ring seal between engine and propeller Foreign material between engine and propeller mating surfaces or nuts no...

Страница 105: ...or binding frozen or fouling housing Exhaust bypass valve sticking REMEDY ROCKWELL COMMANDER 112 B TC rCA Supply required oil pressure Clean or replace oil line clean oil strainer If trouble persists...

Страница 106: ...the engine for Models 112 B and at the carburetor inlet fitting on the engine for Models 112TC TCA The fuel tanks are vented to atmosphere through vents at the lower outboard wing surfaces and under...

Страница 107: ...MECHANICAL ELECTRICAL MAINTENANCE MANUAL FUEL VENT FUEL DRAIN 112 ONLY ENGINE DRIVEN FUEL PUMP _ CHECK VALVE 112B ONLY Figure 5 1 Fuel System Sheet 1 of 2 5 2 RIGHT FUEL TANK ROCKWELL COMMANDER 112 B...

Страница 108: ...L PRESSURE GAGE ENGINE DRIVEN PRIMER FUEL PUMP THROTTLE MIXTURE O lr O I I I I I I I I I I I I I I I I I I I I I I I I I SOLENOID CARBURETOR J FUEL PRIMER SWITCH FUEL Am MIXTURE t l FUEL SUPPLY I Z l...

Страница 109: ...ansmitter is gained by removing the inboard access cover The transmitter contains a movable contact arm that is mechanically linked to the trans mitter liquid level float arm As the fuel level changes...

Страница 110: ...n be removed by removing the attaching bolt and clamp Maintenance and disassembly of this valve is not authorized therefore servicing of this valve is limited to removal and replacement AUXILIARY FUEL...

Страница 111: ...ghten sup port nut d Safety wire support nut to wire retainer eo Operate engine turn fuel selector on and check for leaks MODEL 112 Serial numbers 221 and subsequent MODELS 112B TC TCA a o Replace cle...

Страница 112: ...eads of finger inlet screen with Parker Sealube or equivalent sealube conforming to requirements of MIL L 6032 Change 2 b c d e 1101 If sealant around the fitting of the fuel tank wall is damaged or d...

Страница 114: ...ting of Product Research base compound and accelerator should be carefully mixed in accordance with the instructions printed on their containers Thoroughly clean all surfaces to which sealing compound...

Страница 115: ...r should be checked for air bubbles or thin spots Applyaddi tional sealer as necessary e Reseal access covers with PR 1403 G B2 and fuel quantity transmitter mounting with PRC 1422 A2 sealers and bolt...

Страница 116: ...probable causes and the appropri ate corrective remedy to be taken Review all prob able causes given and check other listings of troubles with similar symptoms Items are presented in se quence but not...

Страница 117: ...an screens and flush out tanks Disconnect inlet and outlet lines from valve If fuel flows from in let line but not through valve it is defective Remove and repair or replace selector valve Inspect scr...

Страница 118: ...ually if not open check continuity Reset Replace if de fective Disconnect wire from transmitter at indicator not registering and attach it to the opposite indicator that is registering If indicator do...

Страница 120: ...ut and then pushed down to operate The main landing Page LANDING GEAR POSITION INDICATORS AND WARNING SySTEM 6 13 Position Indicator Lights 6 13 WHEELS AND BRAKES 6 16 General Description 6 16 Main Wh...

Страница 121: ...re set limits and retain the gear in the full up position When the landing gear selector switch is placed in the DOWN pOSition the hydraulic fluid lock is released hydrauliC fluid directed to the down...

Страница 122: ...to Lubrication Chart Section II To prevent abrasive material damage to a rings seals trunnion piston Change 2 and actuating cylinder piston rod clean them fre quently using a suitable dry type cleanin...

Страница 123: ...NG ASSEMBLY FORWARD FITTING ASSEMBLY 0 00 CLEARANCE 0 060 0 090 CLEARANCE MODEL 1 THRU 380 Figure 6 1 Main Landing Gear ROCKWELL COMMANDER 112 B TC TCA h EMERGENCY EXTENSION SPruNG WHEEL AND BRAKE ASS...

Страница 124: ...REASSEMBLY OF MAIN GEAR OLEO a If orifice plate was removed first install the plate with countersunk side exposed facing down and then install retaining ring holding plate in place b Ascertain that p...

Страница 125: ...ENANCE BEA l ROCKWELL COMMANDER 112 B TC TCA BACK UP RINGS O RING 4 RETAINER RING SCRAPER l I RmG J mER PffiTON RETA ROD RING Gear Main Landing Figure 6 2 Strut ss A embly Change 3 Copyright Commander...

Страница 126: ...en connecting door retraction rod to door attach point it is necessary that the same amount of washers be installed on both sides of rod as were removed to obtain proper clearance DOOR RIGGING a Jack...

Страница 127: ...DEL 112 1 THRU 380 WITH CYLINDER LOCK ENGAGED AND DRAG BRACE RESTING ON OVER CENTER STOP IN RELAXED CONDITION PUSH UP ON PIVOT POINT OF DRAG BRACE ASSEMBLY CLEARANCE AT KNUCKLE AREA SHOULD BE 0 40 TO...

Страница 128: ...Remove bolts washers and nuts attaching Change 3 upper and lower torque links to strut and remove torque links c To drain fluid from strut remove bolt washers and nut from collar above fork remove plu...

Страница 129: ...TORQUE TUBE _ BEARINGS BODY WASHER l RETAINER RING 8_UPPERBEARING If I ORIFICE PLATE COLLAR 0 DRAG BRACE J X ASSEMBLY IS RETAINER RING 6 10 i 8 LOWER BEARING I m O RING I BACKVP RING PISTON TUBE AXLE...

Страница 130: ...ain 0 250 t 03 inches cushion as actuating cylinder is installed f Tighten jam nut on rod end Drag stay of drag brace assembly should be resting on stop STRUT SERVICING a After strut is assembled with...

Страница 131: ...eversing removal procedure LANDING GEAR ACTUATING CYLINDERS The hydraulically operated actuating cylinders are 6 12 attached to the drag brace and trunnion on the nose gear and side brace and trunnion...

Страница 132: ...rd against tube end of bungee then give one additional full turn on turnbuckle LANDING GEAR POSITION INDICATORS AND WARNING SYSTEM POSITION INDICATOR LIGHTS MODEL 112 Serial numbers thru 380 The landi...

Страница 133: ...ts respective green gear safe light SWITCH ADJUSTMENTS MODEL 112 Serial num bers thru 380 All adjustments of position switches should be made with the aircraft on jacks See Section II for Jacking Proc...

Страница 134: ...switch so switch is activated d Appropriate green gear safe light will illuminate red unsafe light will go out e f 110 11 Do not bend or distort switch lever Repeat steps a thru d for each gear Cycle...

Страница 135: ...r and lift cover up enough to gain access to throttle switch f With a small screwdriver loosen screws attaching switch to bracket g Adjust switch tighten screws press metal console cover down and move...

Страница 136: ...Remove axle cups and axle and drop wheel out from fork Axle spacers are now free for removal d Wheel halves may be separated by first com pletely deflating tire With tire completely deflated remove wh...

Страница 137: ...RING 6 INNER WHEEL HALF 7 INNER TUBE 8 TffiE 9 OUTER WHEEL HALF 10 BRAKE DISC 11 WHEEL THROUGH BOLT 12 CONE BEARING 13 GREASE SEAL 14 FELT GREASE SEAL 15 GREASE SEAL 16 SNAP RING 1 SNAP RING 2 GREASE...

Страница 138: ...CYLINDERS a Release parking brake b Reduce brake system pressure to zero c Disconnect brake cylinders from top and bottom attaching points and remove cylinders d Disconnect hydraulic hoses from cylind...

Страница 139: ...arent line to brake assembly bleed port e Connect a manual hydraulic pump to transparent line and force bleed brake assembly up to bleed tee in wing wheel well NOTE Use MIL H 5606 hydraulic fluid in h...

Страница 140: ...LATION MODEL 112 PILOT S BRAKE MASTER CYLINDER PILOT COPILOT BRAKE CYLINDER MODEL 112B TC TCA 1 CLEVIS 2 LOCKNUT 3 FILLER PLUG MODEL 112 ONLY 4 SNAP RING RETAINER 5 SQUARE CUT SEAL 6 O RINGS 7 THRUST...

Страница 141: ...Connect a manual hydraulic pump to transparent line and force bleed brake assembly up to bleed tee in wing wheel well f After all air bubbles have been removed from brake assembly and brake line up t...

Страница 142: ...IVET 561 112B TC TCA MAINTENANCE MANUAL 6 PRESSURE PLATE 7 7 LININGS 8 BACK PLATE 9 ANCHOR BOLT 10 TORQUE PLATE 6 PRESSURE PLATE 7 LININGS 8 BACK PLATE 9 ANCHOR BOLT 10 TORQUE PLATE Figure 6 11 Brake...

Страница 143: ...e supply line and cap bleed tee at W S 66 00 left side i Repeat steps b thru h for right side 6 24 TROUBLE SHOOTING The best method of trouble shooting is to decide on the various causes of a given tr...

Страница 144: ...Rebalance Check for play overcenter tolerance Replace worn bolts or bushings Remove assembly and test Service or replace if necessary Check tire pressure Inflate to proper PSI see Figure 6 9 Inspect s...

Страница 145: ...te freely loosen brake line at brake housing to re lieve any pressure trapped in the line If wheel now turns freely the brake line is restricted or there is a restriction in the brake master cylinder...

Страница 146: ...d at any setting between UP and DOWN by intermittent operation of the flap switch Page Aileron and Flap Rigging Alternate Method 7 10 Rudder 7 11 Elevators 7 14 Elevator Trim Tabs 7 17 Aileron Rudder...

Страница 147: ...1 ELEVATOR ARM ROCKWELL COMMANDER 112 B TC TCA 4 FLANGE BEARING 12 CONTROL YOKE PIVOT BUSHING 5 UNIVERSAL JOINT 13 AILERON CABLE PULLEY 6 O RING 14 CONTROL YOKE 7 CONTROL WHEEL SHAFT 15 CENTER SPROCKE...

Страница 148: ...sion is taken FLIGHT CONTROL SYSTEMS CONTROL COLUMN The control column which is supported by bushings and bearings is attached to the mounting yoke plate located at the forward end of the console tunn...

Страница 149: ...ccess REMOVAL AND INSTALLATION OF AILERON BELL CRANK a Remove aileron bellcrank access plate furthest 7 4 outboard from wing b Remove screws attaching aileron stop bracket and remove bracket Model 112...

Страница 150: ...2 l THRU 50 ALIGNMENT TOOL RF 42003 MAINTENANCE MANUAL PUSH PULL ROD SECTION vn FLIGHT CONTROLS TURNBUCKLE CONTROL X27 12 Figure 7 2 Aileron Controls Sheet 1 of 3 7 5 Copyright Commander Owners Group...

Страница 151: ...NTROLS MODEL 112 51 THRU 470 7 6 MAINTENANCE MANUAL Figure 7 2 Aileron Controls Sheet 2 of 3 TURNBUCKLE ROCKWELL COMMANDER 112 B TC TCA X27 12 AS Copyright Commander Owners Group 2013 All Rights Reser...

Страница 152: ...2 471 AND SUBSEQUENT MODELS 112B TC TCA MAINTENANCE MANUAL t CONTROL YOKE Figure 7 2 Aileron Controls Sheet 3 of 3 SECTION vn FLIGHT CONTROLS TURNBUCKLE X27 1285 7 7 Copyright Commander Owners Group 2...

Страница 153: ...APS An all metal wing flap installed on each wing is at tached to the aft wing spar and extends outboard from the fuselage to the ailerons These wing flaps are electrically operated and controlled by...

Страница 154: ...TORQ EULL ROD 3 SUPPOR TUBE FLIGHi COTION vn iNTROLS 4 LIMIT S T BEARING 5 LIMIT s iCH NUMBER 3 6 LIMIT SWITCH NUMBER 2 7 FLAP MOTO H NUMBER 1 Figure 7 4 FI ap Controls Inst II a atlon 7 9 Copyright C...

Страница 155: ...rotractor 12 inches aft of firewall on bottom surface of aircraft at centerline see Figure 7 11 Adjust protractor to zero degrees Be certain protractor is not rotated 180 degrees b Set flaps in fully...

Страница 156: ...ce all parts removed for access Change 2 REMOVAL AND INSTALLATION OF CONTROL CABLES a Remove rear seat and floorboard assembly front seats Royalite and metal console covers and stinger assembly from a...

Страница 157: ...r RIGGING AND ADJUSTMENT OF RUDDER TRIM MODEL 112 Serial numbers thru 380 The rudder control system must be rigged before rigging the trim The aircraft must be on jacks gear clear of the ground and no...

Страница 158: ...orque tube arm Aircraft must be on jacks gear extended and clear of ground a Clamp all left and right rudder pedals in neu tral position Lower forward surface of pedal will accommodate a metal straigh...

Страница 159: ...ted through a series of pulleys to the elevator bellcrank The bellcrank is connected to the elevator horn with a push pull rod When the control wheel is moved forward or aft the cables move in opposit...

Страница 160: ...ft and right elevator in position If both elevator balance horns do not align with the hori zontal stabilizer clamp both elevators in average position This average position shall be the zero rigging p...

Страница 161: ...TRIM TURNBUCKLES 6 LEFT ELEVATOR TRIM CABLE 7 RIGHT ELEVATOR TRIM CABLE 3 STA 262 75 STA 179 98 8 COTTER PIN 9 SPRING 10 ELEVATOR TRIM INDICATOR STRIP 110 TRIM WHEEL SUPPORT 12 ELEVATOR TRIM WHEEL 13...

Страница 162: ...round cables to temporarily hold in place e Install trim wheel and insert cotter pins through supports f Route cables around trim cable pulleys as depicted in Figure 7 10 and back through console g Fe...

Страница 163: ...able guards are properly installed then replace all parts removed for access k Remove clamps from control surfaces 1 Turn elevator trim wheel aft until elevator trim tab is 26 1 degrees down relative...

Страница 164: ...OP ADJUSTMENT ct RUDDER VERT STAB 0 FIREWALL I I I PANEL I I 12 OO PROPELLER PROTRACTOR ______________ ______ t WRP 11_1 2 10 t FLAP 0 POSITION Figure 7 11 Control Surfaces Rigging Sheet 1 of 2 X27 13...

Страница 165: ...m its leading edge and apply new primer and paint evenly to all surfaces When sheet metal repairs are re quired weigh the material removed from the surface in preparation for repair The weight of mate...

Страница 166: ...r at inboard edge of tip f Slip wire hook under trailing edge of elevator Vertical distance between trailing edge and balance beam should be 1 25 inches go Hang a I pound weight 12 5 inches forward of...

Страница 167: ...A CABLE TENSION 30 t 5 POUNDS c f ELEVATOR TRIM TAB UP 15 2 DOWN 260 1 E I CABLE TENSION 15 POUNDS MAXIMUM 12 POUNDS MINIMUM CABLE TENSION 65 1 5 POUNDS AIRCRAFT L LIFT CABLE TENSION 45 5 POUNDS X2711...

Страница 168: ...M WIRE HOOK ELEVATOR BALANCING X27 lOA5 Figure 7 14 Control Surface Balancing V V O V vy V V O V LPf 1 V O V V V V V V V V CABLES TO BE RIGGED _ V V RUDDER 5 0 LBS ELEVATOR 5 0 LBS _ AILERON 5 0LBS I...

Страница 169: ...ve flap motor Defective electrical circuit Stripped or broken jackscrew on flap motor REMEDY ROCKWELL COMMANDER 112 B TC TCA Adjust cable tension as shown in Figure 7 13 Replace pulley Install cables...

Страница 170: ...ed by faulty bushing or bent rudder arm assembly Rudder pedal bushings misaligned or needs lubrication Cables not in place on pulleys Bent rudder Rudder cables incorrectly rigged Rudder horn assembly...

Страница 171: ...rectly rigged ELEVATOR TRIM CONTROL SYSTEM I Trim control wheel moves with excessive resistance Cable tension too high Pulleys binding or rubbing REMEDY ROCKWELL COMMANDER 112 B TC TCA Check rigging o...

Страница 172: ...actuator Indicator incorrectly attached to the trim wheel shaft SECTION vn FLIGHT CONTROLS REMEDY Install cables correctly Lubricate hinge If necessary replace hinge Repair or replace jackscrew actua...

Страница 174: ...and heating ventilation con trol knobs The manifold pressure and tachometer gages and the flap indicator and directional gyro are individually lighted by post lights and visible from Change 1 Engine...

Страница 175: ...ging an instrument In cases where dual instru ments are installed it may be expedient to exchange instruments or instrument signal sources as a means of determining if the malfunction is in the instru...

Страница 176: ...ction d Slowly apply suction until altimeter indicates a 1000 foot increase in altitude When applying or releasing suction do not exceed the range of the vertical speed indicator or airspeed indicator...

Страница 177: ...COMMANDER 112 B TC TCA AFT FUSELAGE 2 OVERHEAD TEE COUPLING 7 ALTERNATE STATIC SOURCE VALVE 3 MAIN SPAR CARRY THROUGH AREA 8 VERTICAL SPEED INDICATOR 4 PITOT MAST MOUNTING COVER 9 ALTIMETER 10 SUMP T...

Страница 178: ...E 6 AIRSPEED INDICATOR SECTION vm INSTRUMENTS 2 OVERHEAD TEE COUPLING 7 ALTERNATE STATIC SOURCE VALVE 3 MAIN SPAR CARRY THROUGH AREA 8 VERTICAL SPEED INDICATOR 4 PITOT MAST MOUNTING COVER 9 ALTIMETER...

Страница 180: ...Dow Silicone Number 30 Dow Corning Co Midland Mich VACUUM REGULATOR VALVE A vacuum regulator valve is installed in the line between the instruments and the pump Since the pump is capable of creating m...

Страница 181: ...NDER 112 B TC TCA 4 ENGINE DRIVEN VACUUM PUMP 5 VACUUM PUMP EXHAUST 6 FIREWALL 7 VACUUM REGULATOR AND FILTER 8 ARTIFICIAL HORIZON 9 DIRECTIONAL GYRO 10 SUCTION GAGE 11 VACUUM FILTER CARTRIDGE 12 WASHE...

Страница 182: ...ain ing a ball Gravitational and centrifugal forces posi tion the ball within the tube to indicate correct lateral attitude for the rate of turn ALTIMETER The altimeter is an absolute pressure instrum...

Страница 183: ...ed with the following a Set adjustment screw s on compensating magnets to zero Zero position is when dot on screw is lined up with dot on compass frame b Position aircraft in a magnetically north dire...

Страница 184: ...fuel flow divider and a vent line sensing ambient pressure in the engine compartment TACHOMETER INDICATOR The tachometer is a mechanical indicator driven at half crankshaft speed by a flexible shaft...

Страница 185: ...g 15 To SO PSrD 30 PSID Red Line Green Arc Red Line MAXIMUM NORMAL MAXIMUM MODELS 112TC TCA AIRSPEED 54 VSO To 109 KTS 61 VSL To 143 KTS 143 To 180 KTS 180 KTS White Arc FLAP EXTENSION oDeg 35 Deg Gre...

Страница 186: ...ELS 112B TC AIRSPEED 52 VSO To 109 KTS White Arc FLAP EXTENSION oDeg 35 Deg 57 VSL To 143 KTS Green Arc NORMAL OPERATION 143 To 180 KTS Yellow Arc CAUTION Smooth Air Only 180 KTS Red Line NEVER EXCEED...

Страница 187: ...0 90 PSI 90 PSI OIL PRESSU RE Red Line Yellow Arc Green Arc Red Line MODEL 112 OIL PRESSURE Red Line Yellow Arc Green Arc Red Line MODEL 112B 500 THRU 544 OIL PRESSU RE MINIMUM CAUTION NORMAL MAXIMUM...

Страница 188: ...E Green Arc Red Line NORMAL MAXIMUM MODEL 112 AND 112B 500 THRU 544 CYLINDER HEAD TEMPERATURE Green Arc Red Line NORMAL MAXIMUM MODEL 112B 545 AND SUBS AND 112TCA VOLTMETER 10 0 11 3 Volts 11 3 12 0 V...

Страница 189: ...mperes from the alternator to the battery or from the battery to the electrical system Figure 8 5 With the engine operating and both halves of the split master switch ON the ammeter indicates the rate...

Страница 190: ...ting screws located on each side of the switch cutout enables the lift detector switch Change 1 to be adjusted Loosening the lift detector switch mounting screws allows slight fore and aft movement of...

Страница 192: ...nnections for leaks Repair or replace damaged lines tighten connections Substitute known good instrument and check reading Replace instru ment Substitute known good instrument and check reading Replac...

Страница 193: ...ng screws Substitute known good indicator and check for vibration Replace instru ment Check line for obstructions Check static source Blowout lines Clean static source Substitute known good altimeter...

Страница 194: ...l screw or glass Leak in pressure line REMEDY SECTION vm INSTRUMENTS Check filter clean or replace Adjust or replace relief valve Substitute known good suction gage and check gyro response Replace suc...

Страница 195: ...maged bellows or mechanism Damaged or dirty mechanism Pointer bent rubbing on dial or glass Leak or partial obstruction in pressure line REMEDY ROCKWELL COMMANDER 112 B TC TCA Check line for obstructi...

Страница 196: ...grade and amount of fuel Check circuit breaker inspect for open circuit Reset breaker re pair or replace defective wire or component Check for partial ground between transmitter and indicator Repair...

Страница 197: ...restriction in pump discharge line Central air filter dirty Defective gage or stiCking relief valve ROCKWELL COMMANDER 112 B TC TCA REMEDY Replace instrument Check voltage to instrument Cor rect volt...

Страница 198: ...e vacuum pump Replace safety valve Substitute known good pump and check pump pressure Replace vacuum pump Test generator for output Over haul or replace as necessary Replace flexible shaft Replace ins...

Страница 200: ...T or RIGHT CABIN HEAT control the amount of heated air de livered to the right and left cabin floor heater outlets Page Trouble Shooting The Systems 9 5 Repair and Replacement of Components 9 5 These...

Страница 201: ...SEMBLIES 5 LE FT DE FROSTER OUTLET 6 DISTRIBUTION BOX AND TAKEOFF VALVE PULL ON II 9 00 LEFT RIGHT DEFROSTER _ _ CABIN z __ 7 10 8 7 Q DEFROSTER 7 7 CABIN FLOOR SIDE DUCT 8 AMBIENT AIR INTAKE FROM WIN...

Страница 202: ...VIRONMENTAL 1 AMBIENT AIR INTAKE FWD COWL 5 DEFROSTER CONTROL GATE ASSEMBLY 2 EXHAUST SHROUD 6 LEFT DEFROSTER OUTLET 3 RIGHT CABIN HEAT VALVE 7 LEFT CABIN HEAT VALVE 4 RIGHT DEFROSTER OUTLET 8 CONTROL...

Страница 203: ...AFFLES DEFROSTER 6 TAKEOFF ASSEMBLY 7 RIGHT DEFROSTER OUTLET ASSEMBLY 8 LEFT DEFROSTER OUTLET ASSEMBLY 9 GATE ASSEMBLY DEFROSTER 10 GATE ASSEMBLY DEFROSTER 11 LEFT CABIN HEAT OUTLET ASSEMBLY RIGHT SID...

Страница 204: ...repaired or replaced When check ing rigging of controls be sure valves respond free ly to control movement and that they move through Change 1 their full range of travel and seal properly Check that...

Страница 205: ...T 3 DORSAL FIN INTAKE 4 PLATE 5 SLIDE ASSEMBLY 6 SPACER 7 PLATE 10 8 SEAL 9 WING AIR INTAKE OPENING 10 CABIN AIR VALVE 11 HEAT AND VENTILATION DUCT 12 HEATER AND CABIN AIR INTERCONNECTING CABLE 13 AIR...

Страница 206: ...DE ASSEMBLY 6 SPACER 7 PLATE 8 SEAL 9 WING AIR INTAKE OPENING 10 CABIN AIR VALVE 11 HEAT AND VENTILATION DUCT 12 VENTILATION CONTROL CABLE 13 HEATER CONTROL CABLE 14 AIR VENTS Figure 9 3 Cabin Ventila...

Страница 207: ...ASSEMBLY 6 SPACER 7 PLATE S SEAL 9 WING AIR INTAKE OPENING 10 CABIN AIR VALVE 11 HEAT AND VENTILATION DUCT 12 VENTILATION CONTROL CABLE 13 HEATER CONTROL CABLE 14 AIR VENTS Figure 9 3 Cabin Ventilati...

Страница 208: ...ems and other electri cal component circuits are protected by trip free push to reset circuit breakers Each electrical system component circuit is wired so a failure within a partic ular circuit will...

Страница 209: ...ure of 70 to 80 degrees F Battery voltage should be 14 4 v olts with zero load on battery Check security of terminal connections and battery charger output voltage if hydrometer check indicates a leve...

Страница 210: ...from the ram air pick up on the forward engine baffling see Figure 10 4 MODELS 112TC TCA ALTERNATOR A 14 volt 70 ampere belt driven alternator is mounted on the forward lower right side of the engine...

Страница 211: ...ge reads 14 1 1 volts The adjustment screw is located under the plastic plug on the regulator If the regulator can not be adjusted to the above setting check the alternator overvoltage relay master sw...

Страница 212: ...Capacity 1 70 00 Battery Capacity 1 25 00 hr Figure 10 5 Electrical Load Chart LOCATION MANUFACTURER LAMP NUMBER NOTES I Glove Compartment Light Wing Tip Navigation Lights Tail Cone Navigation Light...

Страница 213: ...3 AMMETER OIL TEMPERATURE IND FUEL QUANTITY IND CYL HEAD TEMPERATURE ALT LANDING GEAR FLAPS MODEL 112 188 THRU 380 OPTIONAL EQUIPMENT FUEL PHOT NAY PUMP HfAT BEACON LITES Ii AYJONICS XIS 12 INST LANO...

Страница 214: ...AULIC POWER PACK 13 ALTERNATOR FIELD 14 ALTERNATOR OUTPUT MODELS 112B TCA OPTIONAL EQUIPMENT FUEL PITOT ANTI COL NAV INST LOG STROBE PUMP HEAT LlTES iifli ii 5 6 t t 7 1 Fli 00000 i DME GIS fWD AUDIO...

Страница 216: ...UMBERS 6 THRU 187 SCHEMATIC ABBREVIATION CODES BW C NC NO GL OVHD RL SW TS 109 Light Blue White Common Normally Closed Normally Open Indicator Light green Overhead Light Light red Switch Terminal Stri...

Страница 217: ...ng Light 10 16 Strobe Lights 10 17 Exterior Courtesy Lights 10 18 Interior Courtesy Lights 10 19 Instrument Lights 10 20 10 18 Auxiliary Fuel Pump 10 21 LANDING GEAR 10 19 Landing Gear Actuation and W...

Страница 218: ...T FIELD REGULATOR F 1 MAINTENANCE MANUAL 239 OVERVOLTAGE RELAY REG 0 1 111 19 ALTERNATOR 1 TS 1 20 18 Figure 10 8 Alternator 17 SECTION X ELECTRICAL ALT E 10 11 Copyright Commander Owners Group 2013 A...

Страница 219: ...TRICAL 10 12 MAINTENANCE MANUAL r OUTPUT AUX I r L _ _ _ r_ GROUND Figure 10 9 Alternator Internal Wiring ROCKWELL COMMANDER 112 B TC TCA E Copyright Commander Owners Group 2013 All Rights Reserved un...

Страница 220: ...STARTER RELAY 3 MAINTENANCE MANUAL 2 166 271 10 BAT MASTER SWITCH SECTION X ELECTRICAL O l TO CABIN AND BAGGAGE LIGHT E Figure 10 10 External Power Receptacle Optional 10 13 Copyright Commander Owner...

Страница 221: ...10 14 LEFT MAG START SW 13 2S 10 TOALT FLD TO OVER VOLTAGE RELAY_ I C J III RIGHI THRU TS l l MAG MASTER SWITCH Figure 10 11 Starter ROCKWELL COMMANDER 112 B TC TCA 2 166 TO COURTESY LIGHTS BATTERY t...

Страница 222: ...ROCKWELL COMMANDER 112 B TC TCA MAINTENANCE MANUAL NAV LIGHTS Figure 10 12 Navigation Lights SECTION X ELECTRICAL E 10 15 Copyright Commander Owners Group 2013 All Rights Reserved unofficial copy...

Страница 223: ...SECTION X ELECTRICAL 10 16 MAINTENANCE MANUAL LAND LIGHT Figure 10 13 Landing Light ROCKWELL COMMANDER 112 B TC TCA E Copyright Commander Owners Group 2013 All Rights Reserved unofficial copy...

Страница 224: ...AERO FLASH CKT 363 MAINTENANCE MANUAL WHE LEN CKT POW SUPPLY 350 349 Figure 10 14 Strobe Lights 363 359 SECTION X ELECTRICAL POW SUPPLY 343 345 344 E 10 17 Copyright Commander Owners Group 2013 All R...

Страница 225: ...RCUIT 166 l ATTERY SA BAGGAGE LIGHT 283 86 I TO INTERIOR COURTESY LIGHTS CIRCUIT I J 8 286 I HOLDING RELAY _ _ 1 307 118 TIME DELAY CIRCUIT 112 trim t ItrI trI O Z t I s z I m Z z m s z c I I I 0 trI...

Страница 226: ...00 MAINTENANCE MANUAL START ACC 335 _ _ _ 14 ref 1 01 I TO EXTERIOR COURTESY LIGHTS CIRCUIT Figure 10 16 Interior Courtesy Lights 29 SECTION X ELECTRICAL E 10 19 Copyright Commander Owners Group 2013...

Страница 227: ...MER CKT RELAY r Ju I I L 368 372 MAINTENANCE MANUAL 83 91 374 213 INST DIM TO LANDING GEAR CIRCUIT Figure 10 17 Instrument Lights ROCKWELL COMMANDER 112 B TC TCA E Copyright Commander Owners Group 201...

Страница 228: ...ROCKWELL COMMANDER 112 B TC TCA MAINTENANCE MANUAL FUEL PUMP Figure 10 18 Auxiliary Fuel Pump SECTION X ELECTRICAL E 10 21 Copyright Commander Owners Group 2013 All Rights Reserved unofficial copy...

Страница 229: ...82 I L_ JL J 257 145 63 250 155 10 130 125 GEAR POSITION SW 140 144 145 257 124 1154 TO INST DIMMER CONTROL 214 GEA GEAR ACT SEL TO TLAPS IIOHN CmClll1 BREAK EH 63 I T T T T T S S 4 154 DOWN LOCK MIC...

Страница 230: ...MANDER 112 B TC TCA FLAPS MAINTENANCE MANUAL Figure 10 20 Wing Flap Actuation 24 FLAP MOTOR SECTION X ELECTRICAL NC c LIMIT SWITCH E 10 23 Copyright Commander Owners Group 2013 All Rights Reserved uno...

Страница 231: ...SECTION X ELECTRICAL 10 24 MAINTENANCE MANUAL Figure 10 21 Elevator Trim Actuation ROCKWELL COMMANDER 112 B TC TCA E Copyright Commander Owners Group 2013 All Rights Reserved unofficial copy...

Страница 232: ...P MAINTENANCE MANUAL SECTION X ELECTRICAL TS l t 48 FUEL QUANTITY TRANSMITTERS 36 eYL HD TEMP SENDER UNIT Figure 10 22 Engine and Fuel Gages OIL TEMP SENDER UNIT E 10 25 Copyright Commander Owners Gro...

Страница 233: ...CTION X ELECTRlCAL 10 26 MAINTENANCE MANUAL TURN COORD Figure 10 23 Turn Coordinator Indicator ROCKWELL COMMANDER 112 B TC TCA E Copyright Commander Owners Group 2013 All Rights Reserved unofficial co...

Страница 234: ...TART ACC EXTERNAL 4 SHUNT TO STARTER 13 B S START SW TO ALT FLD l l r rE 277 10 TO OVER VOLTAGE RELAY I II THRU TS l L MASTER SWITCH Figure 10 24 Ammeter SECTION X ELECTRICAL 166 TO EXTERIOR LIGHTS CI...

Страница 235: ...X ELECTRICAL 10 28 MAINTENANCE MANUAL STALL WARN _17_ 3 i 1I Figure 10 25 Stall Warning Transmitter ROCKWELL COMMANDER 112 B TC TCA E Copyright Commander Owners Group 2013 All Rights Reserved unoffici...

Страница 236: ...LL COMMANDER 112 B TC TCA MAINTENANCE MANUAL START StACe 56 r I I I I I I 1 Figure 10 26 Cigar Lighter SECTION X ELECTRICAL E 10 29 Copyright Commander Owners Group 2013 All Rights Reserved unofficial...

Страница 237: ...SECTION X ELECTRICAL 10 30 MAINTENANCE MANUAL PITOT HEAT Figure 10 27 Pitot Heater ROCKWELL COMMANDER 112 B TC TCA E Copyright Commander Owners Group 2013 All Rights Reserved unofficial copy...

Страница 238: ...R 112 B TC TCA MAINTENANCE MANUAL PART II DIAGRAMS APPLICABLE TO MODEL 112 AIRCRAFT WITH SERIAL NUMBERS 188 THRU 380 SECTION X ELECTRICAL 10 31 Copyright Commander Owners Group 2013 All Rights Reserve...

Страница 239: ...WING 6 MAIN HARNESS LEFT WING 7 STEP LIGHT RELAY 8 MAIN HARNESS BATTERY COVER 9 AFT T STRIP B 10 SUB PANEL INSTR PANEL 11 SUB PANEL AFT WING FUS 12 INSTR PANEL AFT 13 INSTR PANEL FWD Figure 10 28 Conn...

Страница 240: ...LIGHTING 10 31 Interior Lighting 10 37 10 32 Exterior Lighting 10 38 FUEL SYSTEM 10 33 Auxiliary Fuel Pump 10 39 LANDING GEAR 10 34 Landing Gear Actuation Position Indication and Warning System 10 40...

Страница 241: ...RCUIT Figure 10 29 Electrical Symbols ROCKWELL COMMANDER 112 B TC TCA CODE DESCR LTR BUTT SPLCE BC CIRCUIT BREAKER CB CtRCUI T BREAKER SWITCH CBS CONNECTOR PLUG P RECPTACLE J FUSE F T BOARD T GENERAL...

Страница 242: ...E 20VND S7RAP fiREWALL JII n I T CA 4 I I f C CJ r Y 1 PEL s tfOl h MAINTENANCE MANUAL Figure 10 30 Power Distribution Sheet 1 of 2 SECTION X ELECTRICAL TO NTEII R l I6HTIN6 CKT V 6 10 35 Copyright Co...

Страница 243: ...G NE tIC N GROUND STRAP MAINTENANCE MANUAL 5 Figure 10 30 Power Distribution Sheet 2 of 2 ROCKWELL COMMANDER 112 B TC TCA TO INTERIDR LfGHTIN6 CKT TO INTEIlIOR Ll6 1T1NG CKT Y 6 1 Copyright Commander...

Страница 244: ...A _t 7EZii _ hI C iii 4 7 I L L22 GAllJ GAIl l22 LZft LJr 22 L 1 2 22 i198 i 2 C f1llV REAt j l T I A _ 1 1 l LLlZ E l2 B22 lI A22 _ _ y LVA22 f 2 _ I ll __ 12 V OPT Oil Ai 3 4 eOPILor T L lOA 6 AlD...

Страница 245: ...T f 15 f F L34 414_ 1 L 1MI II 70 7 04 C OJ IP5 l L 91114 H t 4fNEk BE 4COIIJ Pt JWEk S UPPLY L 9D14 L29t 14 k U35 8f8 I I L 3 4 8 IIL y RED WHT 1 k PED I NT e IWIIIG polI R S UPPLY L WIAtG T I rTRD8...

Страница 246: ...MMANDER 112 B TC TCA MAINTENANCE MANUAL LLijr c U R PURl t PS t J1 A CJ Figure 10 33 Auxiliary Fuel Pump SECTION X ELECTRICAL U 11 10 39 Copyright Commander Owners Group 2013 All Rights Reserved unoff...

Страница 247: ...3 L 2D4BlO ID6fl20 D9C2D Ot20 3 4 P2 D D P3 91l20 OlOR2D Dle O i7fBi O t I 2 cJ 5 Z I I i 2 BCL SA LJ CL A S W 1 1 I C7t9 O S5CC LJ I l __ S CCL CBB o i_ trlUl t trl trl f 3 f 3 g t 3 z I m Z z o m 3...

Страница 248: ...S TC TCA MAINTENANCE MANUAL LjrRd r lJ t 8 9 P t7 B 2l t7B 4 CAlb 6 Y 16 YO b l Vc 3S I ll C Figure 10 35 Wing Flap SECTION X ELECTRICAL U 8 10 41 Copyright Commander Owners Group 2013 All Rights Res...

Страница 249: ...SECTION X ELECTRICAL 10 42 MAINTENANCE MANUAL Figure 10 36 Turn Coordinator Indicator ROCKWELL COMMANDER 112 B TC TCA U 8 Copyright Commander Owners Group 2013 All Rights Reserved unofficial copy...

Страница 250: ...320 SECTION X ELECTRICAL W2A 20 STALL WARNING SWITCH W2D20 NQIIMW2 20 NORM OPEN b CLOSED COMMON GND 20 7 I W2A20 WZ B2 0 Q ND I 203_20 3 W2 EZO l l AIR Z 20 GND coII TAcr Sill WZM20 W2L20 TFST 5W mr N...

Страница 251: ...Y JV __________________________ J 1 J rr A C 9 5 t 11 9 07 2 ROCKWELL COMMANDER 112 B TC TCA L oJ r sU t t O r WA f 1V 8 N I J 0 MZA22 U 11 Figure 10 38 Cigar Lighter Pitot Heater Hourmeter and Avioni...

Страница 252: ...CA MAINTENANCE MANUAL PART III DIAGRAMS APPLICABLE TO MODEL 112 AIRCRAFT WITH SERIAL NUMBERS 381 AND SUBSEQUENT AND MODEL 112TC SECTION X ELECTRICAL 10 45 Copyright Commander Owners Group 2013 All Rig...

Страница 253: ...IGHT WING 6 MAIN HARNESS LEFT WING 7 STEP LIGHT RELAY 8 MAIN HARNESS BATTERY COVER 90 AFT T STRIP B 10 SUB PANEL INSTR PANEL 11 SUB PANEL AFT WING FUS 12 INSTR PANEL AFT 13 INSTR PANEL FWD Figure 10 3...

Страница 254: ...10 49 LIGHTING 10 42 Interior Lighting 10 51 10 43 Exterior Lighting 10 52 FUEL SYSTEM 10 44 Auxiliary Fuel Pump 10 53 LAN DING GEAR 10 45 Landing Gear Actuation Position Indication and Warning System...

Страница 255: ...0 40 Electrical Symbols ROCKWELL COMMANDER 112 B TC TCA CODE DESCR LTR BUTT SPLICE Be CIRCUIT BREAKER CB CIRCUI T BREAKER SWITCH CBS CONNECTOR PLUG P RECPTACLE J FUSE F T BOARD T GENERAL NOTES E Y MPL...

Страница 256: ...1 7 8 T 7 20 EBAcO r r OA M CM H T J YJY Ef I 2 t J EJA LJ j J car K K 4 K K I 4 M 2 RrtlELfot s_ F E u v C LW4 b E9 l T 4 I TD mE n I LlQNT H lKeUIT B ff A o Er I Wf flU a 9 l1j 1 1 N w 0 tI c Hl l...

Страница 257: ...AND SUBSEQUENT MODEL 112TC MODEL 112B 477 ONLY C 4 MAINTENANCE MANUAL I Figure 10 41 Power Distribution Sheet 2 of 2 10 50 ROCKWELL COMMANDER 112 B TC TCA Y 6 3 Copyright Commander Owners Group 2013 A...

Страница 258: ...L2 8 L2 41122 r SiY 3 __ J 2 B22 LI _ Ql tJ LIt LI9A 7 I n n W8P2 r l ll ff Sf Sf m e A22 V L Z2 P OT aP o v _ V m822 p n f I COM A GE I BF2 EN e J PT LT ILI AZZ I E SW 2LlliAZZ R TEPLT i STEP LT_ f...

Страница 259: ...RED I lIr R 1 1111 6 PtJWER S LlPPLY RE m l lIr Rio I R r m lrl WilT u WilT TIP e ft III G TIP L OBE L T IL STR J8E L T FLASPER BE AlC t J t ERTIC IU ST AlEJIt li ER L37 18 P4 37818 LAII DI S LlGPT 6...

Страница 260: ...MANDER 112 B TC TCA MAINTENANCE MANUAL MODEL 112 B MODEL 112TC PR ME rw Figure 10 44 Auxiliary Fuel Pump SECTION X ELECTmCAL U 11 1 10 53 Copyright Commander Owners Group 2013 All Rights Reserved unof...

Страница 261: ...R Pt S 7CW LJ Ch 7tJR SIYOW 1 A LJA L 7CK A 5 7 v o u tW pfIf C aY LJUC O 413 I SW j r c v 7 rO I DIBC2tJ t DIJS 7 _ _ _ _ Y 7 r J7 P A L7 I BLU L k _I GJPN 7 L FA tr1cn t 4tr1 tr1 Ci CiI 3 1 30 Z Ci...

Страница 262: ...NDER 112 B TC TCA MAINTENANCE MANUAL y y C l 6 C Y J 6 YO 1 35 f N C GND h GNO WIRE Figure 10 46 Wing Flap SECTION X ELECTRICAL Y 8 1 10 55 Copyright Commander Owners Group 2013 All Rights Reserved un...

Страница 263: ...SECTION X ELECTRICAL 10 56 MAINTENANCE MANUAL Figure 10 47 Turn Coordinator Indicator ROCKWELL COMMANDER 112 B TC TCA V 8 1 Copyright Commander Owners Group 2013 All Rights Reserved unofficial copy...

Страница 264: ...AINTENANCE MANUAL STALL WARNING HORN TEST i W2L2 rW2M20 SU TE r NOI tM Figure 10 48 Stall Warning P7 STALL WAPltmlG 5WI TC If SECTION X ELECTRICAL Y 8 1 10 57 Copyright Commander Owners Group 2013 All...

Страница 265: ...CS P TOT I IE 4TER it SINGJ E TU8E NEIITIik V 410 Z2 t OILPRESS I S WITChl 443 422 M2 4R2 MaDEL 112 38 nODEL IJ2rc f MODf L 112 47b TII lJ 4 99 110DEL JIlT _ 1304Z TJliU J3 f9 MODEL IllB 477 ONLY V G...

Страница 266: ...MAINTENANCE MANUAL PART IV DIAGRAMS APPLICABLE TO MODEL 112B AIRCRAFT WITH SERIAL NUMBERS 477 500 AND SUBSEQUENT AND MODEL 112TCA SECTION X ELECTRICAL 10 59 Copyright Commander Owners Group 2013 All...

Страница 267: ...ARNESS LE FT WING 8 MAIN HARNESS BATTERY COVER 9 CABIN T STRIP A 10 SUB PANEL INSTR PANEL 11 SUB PANEL AFT WING FUS 12 INSTR PANEL AFT 13 INSTR PANEL FWD ROCKWELL COMMANDER 112 B TC TCA 7 STEP UGHT RE...

Страница 268: ...Circuit 10 73 Fuel Pump see Figure 10 57 Fuel Pump and Primer see Figure 10 57 10 55 Landing Gear Actuation Position Indication and Warning System 10 69 FLIGHT CONTROLS 10 56 Flight Control Circuits...

Страница 269: ...H TO MAKE PUSH TO BREAK PUSH BUTTON 2 CI RCUIT Figure 10 51 Electrical Symbols ROCKWELL COMMANDER 112 B TC TCA CODE OESCR LTR BUTT SPL E Be CIRCUIT BREAKER CB CIRCUI T BREAKER SWITCH CBS CONNECTOR PLU...

Страница 270: ...IN GeOLIND STR 4P FlR n LL MIi t7 1 Y T P 7 E I JI f V 6 6 n TO INTERltJR 8__JIT P A L l c LIGHTJN J A i ze ACJ m N J 00 tJj 8 JZt tj st ll trjl J O trj Z t m Z z m z c r t trjOO Jtrj J E9 j t t Copyr...

Страница 271: ...j tc r pC B 1 8 r 7 rll tflSu r P L C z2 STAJ T T A r A 8 p JA I Q2AI8 n P aD e III r lO n L 2 iaAT I I F3 _ rL2 A 2__t NTE D LlC HTlltlG Ll7AAI6 5 LI7A20 t INTER DR LlGHTlN G Af D23AI6 D22A22 f ELEC...

Страница 272: ...IOC22 L GlIbit O I _ STA J 1 C Z I l 8 6 STAi T 5jqTY 5 qTY s 1 TEMP 5 C812 70 C139 5 1 0 C1Ui 1 C S o 1 01 Ll_ _ _ _ I _ MAIIII BUS IPS P108 2 P 10 1C81 o SMA AI Bl JS P AI2 c P588 RIIDIO MJlSTliR 35...

Страница 274: ...12 V 1 5 LMm 1420 lI OOIM UI r _ _ G AlOM mw 1 _ 3 P1 _ 20 l r u U L20A Z 1 4420 J PI b 1 1 G 1 1IA1 1 If flf TIle N NUl IM PO i T UG o TS _ lfIrT PIIII EL H XlA MHER POST LI T L39A20 L 9B20 1lf iINST...

Страница 275: ...66 2 L25C22 Z2 r r 2 Ljn LT I f L L L f I G I AI flf r t rnAPI O porr A rTR P l l tFL I10UA METER POST LlGI IT L39A22 L 95Z 2 RW IN5TR _ _ __ aUSTER LH INSTR CLUSTER Ill 5 22 2L fll5B Ii 12L II J _ IJ...

Страница 276: ...__ Pll t IIl r ED lP 22 PILDT MIIpLT MAPLT 2lJ 7 N012 REF Tc r S t k T 0 It V 1 U A2Z RE f I H Jt WVI cA cAIP n U 511 D A f A R J l mm I SN t fr IJ U6 LI L A I J OUAfIL 4 J 1 2 GSA 2ff C f D G IJO L22...

Страница 278: ...11111 r IJ CCIII HtJ l r KGO 1 6lK U T It t L lfillll I II lJfi AIB IIL I yELl 1 0 TAIl S TIt I r L WIM i TIP J OI IF t T It1M PIiIt PI HES III J1l CAl III U 9CIII OOW Jl1 J n i l m r n LV 1 8LtHi K...

Страница 279: ...t J VI i ty r m GJ1 D U CI8 J n J UJ 1 lIiHE eV IIlED 1 lI Z M m J ru rLASNli MACDA II K VEL TICAl rrAlJltJ EL I D 1fT L MMS PON I l VPPtY N m l L RioII n m l4 WHf MIT I III Aft TIP L If If li TIP J r...

Страница 280: ...112TCA 13190 AND SUBS Change 1 MAINTENANCE MANUAL 3 ci3 8 l 011 SECTION X ELECTRICAL C ______ S I f ___________ i o V AS 10 1 1I Figure 10 54 Exterior Lighting Sheet 3 of 3 10 68A l0 68B Copyright Co...

Страница 282: ...J 719 0 fOC20 b96 t1 7 DlIA20 2U4BlO 3 4 P2 O P3 D9A20 OIOAlO 1 PJ B O P l LJIC 70 e I DIBC O t Df6C 20 fty m I Th eOTTlE SN P31DI7A I I D TiI RJL4 o fh d DI7B O 5 0 PRt SS 8LU ni u c J 7020 1 6 LJ se...

Страница 283: ...OTn SIY Pi P lu 20462 0 Glm 4880 A N r ID j1l2O ___I r 6 J aJ 7 t N tIC Nt 1 vl J W Ur lOCK OCK Err _ C fl R I S 7QV A O C fl7l7 R SHOWN A LM L4 C A I T a v 3 i QQ CICI mm NN C 1 _U I Wl 2 g C en cc a...

Страница 284: ...r C c n II j 3 Vi r D w 2 w a z S is_I 5 z C r f f f f r f LJ 0 Tlt l OTTZe SJIY 00 00 m m r r NN Ie n en Wl NZ mo l Ct ZC oe Ct I C CII I I OO b rsZ trl Ot 4 t 3trlt 4 It Z I m Z It Z o m It Z C It...

Страница 286: ...1 QND I 3 20 3 We E lO 1 2 20 2 W2I20 GND C NTAcr S i W2L2 14121 12 0 rEST SUI TE N MAINTENANCE MANUAL STALL WA NllfG 5WITCff Figure 10 56 Flight Control Circuits Sheet 1 of 2 SECTION X ELECTRICAL Y...

Страница 287: ...AINTENANCE MANUAL P7 sTALL WAP NfNG sWITCff y t 6 rrIU l r1 tWYJM I t 0 L J A f 3S J N C C O S H A Figure 10 56 Flight Control Circuits Sheet 2 of 2 ROCKWELL COMMANDER 112 B TC TCA V 8 II Copyright Co...

Страница 288: ...K C RCt T V tfWiN 2 t OIL PRES S I S WITC 1 tl1 1 t MR LISHTER M2AI I f SIJl6U TUSE NEAT k y GAI Z2 t J1i PREfr I J W TC M tlZI fMU22 M2AZZ AI Olll CS 3l 20 AO m r Nt CCI 0 00 b3 r5 ttj t lt 4 tl lt 4...

Страница 289: ...RIMER CKT 4400EL I TC40I1 LY 13 5Q TH IJ 131 SS POWB OlsrR FiEe CiOCk ClReOIT MOLlE 11213 M2 A 2 IfOURME TER CIRCL IT HOI3I3S METEe r MZq ___ MODEL 112B 500THRU 531 MODEL 112TCA 13160 THRU 13166 lD RB...

Страница 290: ...Iti III M I C oil VIi j l f 2 3 c 11 mo z c AtOT l A t lli mcf 6117 b n U 31111 ll NllIlII II o II E E Figure 10 57 Miscellaneous Circuits Sheet 3 of 3 SECTION X ELECTRICAL AG 12 1I lO 74A IO 74B Copy...

Страница 292: ...TG MODEL 1128 538 AND SUBS MODEL 112TCA 13167 AND SUBS STOW t SEcUIiE IN CENTEI WING AREA FLUX XMTR MODEL 112B 545 AND SUBS MODEL 112TCA 13190 AND SUBS Figure 10 57 Miscellaneous Circuits Sheet 3 of...

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