INSPECTION SCHEDULE

18 . Check the brakes for effectiveness and the parking brake for correct operation. LANDING GEAR (FLOA TPLANE) 1. z. 3. Inspect the support struts and spreader bars for damage, distortion, corrosion and security, Check the bracing wires for tautness and inspect for corrosion and security. Check the floats for leaks by applying a bilge pump to all stand pipes. Inspect for corrosion. 4. Check the water rudders for correct operation, corrosion and security. 5. Inspect the rudder control cables, pulleys and attachments for wear, fraying, cor- rosion and security. 6. Inspect the paddles for security of stowage, 7. · Inspect the canoe canvas covering for tears and deterioration, 8. Inspect the canoe attachment fittings and straps for security. 9. Inspect the strut steps for cracks, corrosion and security. l 0, Inspect the canoe for security of attachment to carrying gear. ~ANDING GEAR (AMPHIBIOUS FLOA TPLANE) In addition to the Landing Gear (Floatplane) checks, carry out the following: Inspect the nose wheel hydraulic shock struts for leaks and check for serviceabi: ,: , 4 It I l ''! IT.E LANI: I . 2. 3. 4. LANDI: 1. 2, 3. 4. 5, 6, 7. 8, utraJ ty ty. ,. I I . i 1 IiI Il 2. Inspect the main wheel forks for damage, security and corrosion. 3. Inspect the brake units for damage and corrosion. 4. Inspect the hydraulic lines, actuating jacks, and connections for leaks. D :i il y Powc~r Off Airframe 5. Inspect the retracting mechanisms for damage, security, corrosion and obstructions, 6. Inspect the electrical connections for security. 7. Check the brakes for operation. 8, Check the hydraulic reservoir for specified level. 9. Check motor pump assembly (if fitted) for leaks and security • LANDING GEAR (SKIPLANE) 1, Inspect the attachments and fittings for damage and security. 2, Inspect the skis for wear, damage, security and trim. 3. Inspect the springs for fractures, and the shackles for corrosion and security. 4. Inspect the trim cables for corrosion, fraying and security. LANDING GEAR (WHEEL - SKIPLANE) 1. Inspect the main ski trim unit for damage and security and rubbers for deterioration. 2, Inspect the tail ski for damage and security, 3, Check the main ski actuators £or specified extension. 4. Inspect the check cables for fraying and security of attachment, 5. Inspect the hydraulic lines and connections for leaks. 6. · Check the wheel-ski hydraulic reservoir £or specified level. 7. Check the tail ski £or freedom about the axle, by rocking the ski, 8. Check motor pump assembly (if fitted) for leaks and security. Revised · I September 1963 5 I Daily Power Off Power Plant ITEM NO. 1. 2.. 3. 4. s. 6. 7. 8. 9. POWER 'PLANT Inspect the cowlings for cracks and damaged or missing fasteners. Inspect the engine for obvious damage and leaks. Inspect the ~ngine controls for security. Inspect the exhaust brackets and flange bolts for security. Inspect the exhaust stacks and muffs for cracks and evidence o! leaks and security. Inspect the carburettor hot and cold air intakes duct openings for obstructions. Inspect the carburettor air filter for obstructions. Inspect the oil cooler for leaks and obstructions. Check the engine winter shutters for freedom of operation and control locked in the desired position. 1 O. Che~k the drain box by draining. 11. Inspect the oil tank, lines, hoses and connections for leaks, chafing and security. 12.. 13. Check the fuel tanks for water, ensure drain tap is properly closed after check. Inspect the !uel vents for any obstructions. 14. Inspect accessible fuel lines, hoses and connections for leaks, chafing and 3ecurity. 15, I 6. Check the fuel filter for water and other foreign matter by turning on the drain valve lever. Check the fuel selector valve for freedom of operation. 17. Check the wobble pump for _operation and security. 18. Inspect the emergency fuel and oil shut-off control handle for correct lockwiring ir. the "OPEN" position. 19. Check the engine controls (throttle, mixture and propeller) for full and free move· ment, spring back and operation o! friction dampers. 20. Inspect the propeller governor for external leaks. I l ITEll. I 2 1. 2. 3. 1. 2. 3. 4. s. 1. 2. 3, n 0 ins. [J 0d in the 0 [] [] 0.ring m 0 [1 u u i I I! rI ! ; .. '' f !. l ITEM NO. 1. 2. 1. z. 3. l. z. 3, 4. s. 1, z. 3. Daily l' u w, : r Off Utility SyslPrn::; Electrical 111.;trumcnts Power On Power Plant UTILITY SYSTEMS Check cabin heat control for freedom of operation. Inspect cabin ventilating duct openings for obstructions. ELECTRICAL Inspect the battery area for evidence of electrolyte spillage, Inspect the battery jumpers for security of attachment, inspect the circuit breaker panel for circuit breakers in the trir,ped position. INSTRUMENTS Inspect the pitot head and static port openings for obstructions. Inspect the instrument cover glasses for cleanliness and cracks and the limit mark- ings for adhesion. Inspect the rate of climb indicator for zero setting, Inspect the magnetic compass for discolouration of fluid and air bubbles. Inspect the compass correction cards for legibility. ELECTRICAL POWER ON POWER PLANT Inspect the fuel quantity gauges for correct reading against known tank quantities, Check the fuel booster pump for specified pressure, (Mixture control in "IDLE CUT-OFF"), Inspect all accessible fuel system components, lines, hoses, and connections for leaks. (Mixtu.re control in "IDLE CUT-OFF' 1 and booster pump "ON",) 7 n 0 [] 0 [J 0 [J g 0 0 0 0 0 L1 0 0 0 C l u 0 Daily Power On Electrical Instruments ITEM NO. ELECTRICAL 1. Check the landing light !or operation. z. Check the navigation lights for operation in "STEADY" and "FLASH" positions. 8 3. Check the instrument lights and intensity control rheostats for operation. 4. Check the cockpit and cabin lights for operation. s. 6. Check the anchor lights for operation, Check the battery voltage on the voltmeter. 7. Check rotating anti-collision light for operation, INSTRUMENTS 1. Check the pitot heater for operation. Revised 1 September 1 ·. INSl 4th Il PART 3 PERIODIC INSPECTION ELECTRICAL POWER OFF Periodi, Power OH Preparation Airframe INSP. DUE ITEM NO. PREPARATION 4th 1. Landplane - wheels chocked fore and aft. 2. Floatplane - secure on beaching gear. 3. 4. Maintenance stands provided, Aircraft covers and shields removed. s. Engine cowlings, access panels, strut fairings at landing gear attach- ments and fuselage panels under cockpit floor removed; reinstall on completion of inspection and inspect for security. 6. Battery disconnected and aircraft grounded, 7. External power source provided. AIRFRAME 1. Inspect the aircraft for cleanliness. 2. Inspect stencils and insignias for legibility. 3, Inspect drain holes for obstructions. 4, Inspect the aircraft fairings, panels, doors and engine cowls for . cracks, corrosion and distortion-, check hinges, latches and fasteners for serviceability. 5, Inspect the wings, fuselage and tail unit for loose or missing rivets, skin for buckles, wrinkles, abrasions, dents or cracks. 6, Inspect the wing front and rear attachment pins and wing struts upper and lower bolts for security; attachment fittings for cracks, corrosion and security. 7. Inspect all flying control ~urfaces. for cracks, wrinkles and abrasions; hinges and attachment fittings for cracks, corrosion and security. 8, Inspect the horizontal stabili.zer attaching bolts for security, 9 1 eriodic 'ower Of! .irframe NSP. DUE ITEM NO. 4th 4th · 4th 4th 4th 4th 4th 4th 4th 4th 9. Inspect the mass balance weights (ailerons, elevator and rudder) for security • . 10. Inspect the elevator torque tube for distortion, and evidence 0£ heavy contact with adjustable stops on front frame, bearings for wear and excessive play. 11. 12. 13. 14. 15. 16. 17. Check the rudder and trim tab cables for the correct tension. · Check the rudder and trim tab _for correct range 0£ travel. Check the elevators and trim tab cables for correct tension. Check th~ elevators and trim tabs for correct range of travel. Check the aileron cables for correct tension. Check the aileron cables for correct range of travel. Check the flaps for correct range of travel. 18. Check the wing flap position indicator for correct flap angle. · 19. Inspect all pulleys, pulley brackets, guides and fairleads for cracks, wear, alignment and security. 20. Inspect push rods and linkage for wear and security. 21. 22. 23. Inspect all rod end bearings, bellcrank bearings, control pulley bear• ings and cable fittings for wear, misalignment and corrosion. Inspect accessible control cables for corrosion and fraying; turn- buckles and attachment points for security, Inspect all control cables throughout their entire length for corrosion and fraying. Z4. Inspect engine control brackets for cracks, corrosion and security. 25. Check pilot's and co-pi+ot 1 s seats for ease of adjustment and security , 26. Inspect cabin seats for damage and security. 27. Inspect safety belts and shoulder harnesses for security of attachment, damaged and corroded metal parts; fabric and leather for cleanliness, cuts and fraying. Check latching · mechanism !or freedom of operation and positive locking. ZS. Inspect cabin floors for security. 29. Inspect the control column torque tube for distortion and check bear• ing for wear and excessive play. 30. Inspect fir s t aid kits for l eg ible identifi catio n markings and broken INSl 8tl Stl 8tl Stl LAND lNSP. DUE ITEM NO. Periodic Power Off Airframe )r seals, vy l ·- n 'f. 8th 8th 8th 8th 31. Check all doors for security in closed position. 32. Inspect windshield, cockpit and cabin windows for cleanliness, cracks, crazing, leaks and security, 33. Inspect the relief tube for cleanliness, deterioration and security. 34, Check the main hydraulic reservoir for correct level and inspect for leaks and security, 35, Inspect the wing flap components and lines for security and chafing and check for leaks while under pressure. 36. Inspect hand fire extinguishers for dents, operating mechanism for cleanliness, pressure within specified limits, seal intact and mounting brackets for cracks and security. 37. 38. 39. 40, 41. 42. Inspect the cabin heating and ·.rentilating ducts for dents, loose con~ nections and security, Check the cockpit and cabin heat and ventilator outlets for operation and inspect the opening for freedom from obstructions. Check the symmetry of the aircraft. Inspect the aircraft skin for buckling, rippling and check for oil can- ning. Inspect the aircraft for corrosion and paint for flaking or blistering. Inspect the aircraft for damaged, missing or loose rivets. LANDING GEAR (LANDPLANE) l. Inspect the · main landing gear assembly and attachment fittings for cracks, corrosion, distortion and security. z. Inspect the structure adjacent to the main attachment .fittings for buckling or damage. 3. Inspect aH strut assembly bolts for security. 4. Inspect the strut steps for cracks and security. S. Inspect the accessible brake lines, hoses and connections for leaks with parking brake ON, lines and hoses for chafing and security. 11 )criodic >ower Of£ 1.ir!rame NSP. DUE ITEM NO. Znd 4th 2nd 4th 4th 6. 7. 8. Inspect the wheels and brake units for cracks, corrosion and security, Inspect the main wheels (main wheels removed) for cleanliness, cor- rosion, cracks and distortion; bearings and bearing surfaces for wear and damage, relubricate bearings, felt grease retainers for cleanli- ness (replace if saturated with lubricant) brake discs and pucks for cracks, excessive or uneven wear, drive keys for cracks. excessive wear and security; brake cylinders for leaks and security. Check the main landing gear for proper track. 9. Inspect the main and tailwheel tires for cuts, deterioration. presence of oil, grease and creep marks for alignment. NOTE Reverse tires for increased wear life. 1 O. Check the tires for correct inflation. 11. Inspect the tailwheel shock strut assembly and surrounding area of fuselage structure for cracks, corrosion, distortion and security. lZ. Inspect the tailwheel (tailwheel removed) for cleanliness, corrosion, cracks and distortion; bearings and bearing surfaces for wear and damage,. felt grea-se• retainers for cleanliness (replace, if saturated - with lubricant). 13. Inspect the tailwheel shock strut for fluid leaks; check for correct inflation, and clean the polished surfaces. 14. Check the tailwheel shock strut for specified servicing. 15. Check the brakes for effectiveness and parking brake for operation. 16. Check the brake pedals and mechanical linkage for proper adjustment and lost motion, inspect for wear and security. ANDING GEAR (FLOATPLANE) 1, Inspect exterior and interior of floats for corrosion and check for leaks by applying the bilge pump to stand pipe of each compa.rtment. 2., Inspect vent holes for obstructions. 3. Inspect the floats for cracks, scratches, dents, oil canning and loolie rivets, nose bumpers for cuts and wear, handhole covers for distor- tion and security, j INSF 4t LANDI urity, :or- wear 1li- or ive nee ( n, nt Periodic Power Off Airframe INSP. DUE ITEM NO. 4. Inspect the support struts and spreader bars for cracks, dents,. dis- tortion, corrosion and fractures in welding; check the bolts for correct torque values and inspect for corrosion and security, 4th 5. 6, Check the bracing wires for tautness and inspect for corrosion and security of locknuts; inspect the fibre separators for wear and secur- ity. Check the rigging of t~e floats by ensuring that distances are equal between wires. Tension of wires must be sufficient to prevent slack- ness. 7. Inspect the water rudders for cracks, dents, distortion, corrosion and security, supporting structure for cracks, springs for fracture, cor- rosion and security, 8, Check the water rudders for correct steering operation, correct re- traction and full travel, inspect for security in the retracted position. 9. Inspect the water rudder retraction and steering cables for fraying, corrosion and security of attachments; inspect the cables from air rudder quadrant to water rudder for fraying, corrosion, tautness and security; pulleys and fairleads for cracks, wear and security; check pilot's operating handle for binding and lubricate all moving parts and cable guide tube. 10. Inspect the strut and float attachments and bolts for fractures, cor- rosion and security. 11. Inspect the strut steps for cracks, wear, corrosion and security, 1 Z. Inspect the paddles for security of installation. LANDING GEAR (AMPHIBIOUS FLOATPLANE) 1. Inspect the landing gear struts for damage and security. z. Inspect the landing gear and wheels (with aircraft hoisted, jacked or trestled clear of ground) for ·damage and security, and the adjacent structure for buckling or distortion. Check retraction of wheels. _ 3. Inspect the nose wheel shock struts for oil leaks, and the exposed sur- face of the inner cylinders for scoring, 4. Inspect the main wheel shock strut-a for serviceability. 5. Inspect the main and nose wheel actuating jacks !or leaks, and the ex- . posed surface of piston rod for scoring. 13 . Periodic Power Off Airframe INSP. DUE ITEM NO. 6. Inspect the sequence valves for leaks. 7. Inspect wheel axles for damage, scoring or flat spots. 8. Inspect the tires for wear, cuts, bruises, oil and grease, and creep marks for alignment. 9. Check the tires for correct inflation. 10. Inspect the main wheel shock strut boots for tears and excessive wear. 11. Check the nose wheel shock struts for correct servicing. 12. Inspect the wheels and brake units for damage and corrosion. 13. Inspect the brake lines and connections for damage, chafing and leaks. 14. Inspect nose wheel actuating cables for wear and fraying. 15. Inspect the front struts for corrosion and security of leg fairings; check torque value of bolts. 16. Inspect the float and fuselage attachment fittings, strut and tie•rod connections for security. 17. Check rudders for retraction, steering, full travel, sticking, rough or uneven action and lost motion. Check cables for tautness (not tight). 18. Inspect the float interior for damage, dents and loose rivets. Check for seepage between compartments and external leaks by flushing out each compartment, one at a time with fresh water. 19. Check the brakes for effectiveness. zo. Inspect the brake linings for we~r. 2.1. Check the nosewheel shock struts for correct air pressure. 22. Inspect all bare steel surfaces for specified anti•corrosive treatment. 23. Inspect all the electrical terminals for specified anti-corrosive treat· ment. 2.4. Inspect the floats and struts for corrosion. 25. Check the rigging of the floats by ensuring that distances between wires are equal and that the wires are tensioned to prevent slackness, INS. LA? LANl eaks, i i or ). nt. s. P 1• riu d 1, J>ow1• r 0 1f Ai rfra111«· INSP. DUE ITEM NO. LANDING GEAR (SKIPLANE) 1. Inspect the ski surfaces for loose rivets, damage, dents and cracks. 2. Inspect shackles for damage, corrosion and se c urity. 3. Inspect the spring leaves for fractures. 4. Inspect mountings for damage and security. 5. Inspect trim cables for fraying and security. LANDING GEAR (WHEEL-SKIPLANE) 1. 2. 3. Inspect ski attachments, fittings, pins and bolts fo .r cracks, wear, corrosion and security. Inspect main sk i pedestals and attachments for wear, damage and corrosion. Inspect ski shoes, runners and !airings for cracks , distort i on, cor- rosion and security. 4. Inspect ma i n ski trim unit for damage, bind i ng and security; check the plates and rubbers for correct tension and inspect for deter i oration. 5. Check air chamber o{ each main ski actuator for correct pressure. 6. Inspect checking cables for cuts, abrasions, fra y ing and loosening of binding at thimbles; end fittings for correct attachment and s ecurity. 7. Check skis for correct trim and angle; main skis for correct extension and retraction and pump gauge for correct position indicatio n. 8. Check ski handpump and handle for freedom of operation; inspect for cleanliness, damage and security. 9. Inspect ski hydraulic reservoir for damage, corrosion and security, overflow and vent line outlet for obstructions; check for correct fluid level, inspect the filler cap gasket for wear and distortion and filler cap and chain for damage and security. 10. Inspect hydz:aulic motor pump for damage, security and leaks at con- nections. 11. Inspect hydraulic lines, hose and connections on complete ~ystem for abra, i ons, dents, leaks and security, 15 Periodic Power Off Power Plant . :NSP. DUE ITEM NO. POWER PLANT 1. z. 3. Inspect the cowling for cracks and damaged or missing fasteners. Insp·ect the cowling supports for cracks, abrasions and security. Inspect the engine mounts for cracks, corrosion and security of at~ taching bolts. 4. Inspect the engine vibrat i on isolators for breaks in the bonding be- tween rubber and metal parts; metal parts for wear. cracks and security. s. Inspect the firewall for cracks and structural damage. 6. Inspect the cylinders for cracked or broken fins, hold down nuts for security, deflectors for cracks, chafing and security. 7. Inspect the cylinder heads and rocker box housings !or cracks, 8. Inspect the push rod housings !or dents and cracks, and packing nuts for leaks. 9. Inspect the engine for fuel and oil leaks, loose or missing nuts, bolts, studs and clamps, broken lockwiring. 10. Check the carburettor fuel filter for cleanliness and da~age. 11. Inspect the carburettor for leaks, Ii. Check the sump plugs for metal particles. 13. Check the pressure oil filter for cleanliness and damage. 14. Inspect the crankcase breather line for chafing and security. 15. Inspect the carburettor hot and cold air intake ducts and accessory air cooling ducts for cracks, foreign matter in openings and security. 16, Check the carburettor heat control for full free movement, 17. Check the carburettor air filter for free movement and cleanliness. 18. Inspect the exhaust collector r~ng for cracks and security (outer half of hot air muff removed) accessible portion of heater muff for crac}(. ~, tail pipe for cracks and security, 19. Check the engine winter shutter for free operation. 20. Check the engine controls (throttle, mixture and propeller) for lost motion and full, free travel with corresponding travel at engine and control quadrant; friction locks for proper operation. l l ' I iii Il F OILS R evise ir l t i t j I I Il Pc rio<lic Power Off Power Plant INSP. DUE ITEM NO. FUEL SYSTEM OIL SYSTEM 1. Check the fuel taX?,ks for quantity, Z, Check the fuel tank filler caps for security and gaskets for wear and deterioration. 3. 4. s. 6. Check the fuel tank filters for cleanlin~ss and damage. Inspect the fuel tank.drain cocks £or damage, leaks and positive shut- off. Chee~ the fuel line filter for cleanliness and damage_. Inspect the fuel selector valve for leaks and security of mounting: control cables for fraying and corrosion; check the linkage for free- dom of operation and the control cables for tautness. 7, Inspect the priming pump, lines and connections for leaks, damage and security, 8. Check the emergency fuel and oil shut-off control for operation, reset in the OPEN position and lockwire. ·9. "Inspect the fuel tank vents for obstructions. 11. 12. Inspect the exterior of the aircraft for fuel leaks. Check the booster pump for leaks and security . Check the wobble pump £or leaks and operation. 1, Inspect the oil tank system components, lines, hoses and connections for leaks, chafing and security, metal lines for dents and scratches, and hoses for cuts, cracks and deterioration. 2. Inspect the oil cooler for leaks and security, and the air passages for cleanliness. 3, Inspect the oil cooler regulating valve for leaks and security. 4. Drain and flush the oil system. refill with specified oil, and check filler cap for security. R.evia ed l September 1963 . -- 17 Periodic Power Off ?ower Plant Jtility Systems · NST. DUE ITEM N:O. :GNITION SYSTEM )ROPELLER l. Inspect the ignition harness for loose connections, chafing, deteriora- tion of rubber or plastic covering, and cracked brackets; conduits and spark plug leads for evidence of overheating. z. Inspect the magnetos, ventilation plugs and magneto ground connec- tions fqr security, drain holes for obstructions. 3. Inspect the boost coil and external electrical connections for security , 1. Inspect the hub and cylinder for oil leaks, 2. Inspect the propeller for cleanliness. 3. Inspect the propeller blades for cracks, nicks, dents and corrosion; blade tips for correct markings. 4. Inspect the exposed surface of the piston for scoring. 5. Check the clearance betweer. the counterweight brackets and the bronze thrust washer. 6. Check the track of the blades. 7. Check the piston for tightness. 8. Inspect the governor for leaks and security, UTILITY SYSTEMS 1. Check the actuating flap in the heater unit a nd control cable for fre e movement, Inspect ·co ntrol cable for wear, corrosion and spring for tension and corrosion, 2. Inspect hoses for se c urity and ducts for freedom from obstructions. 3. Inspect the air inlet and outlet for freedom from obstructions, Check the outlet shutter valve for free movement, f f jI INSP, 2nd 2nd 2nd INSP. DUE ITEM NO. l, l• 2. ld 3. 4. y. i i 5, 6. 7. 8. ' ·9. I I I 10. l i 11. I l 12. 2nd 13. 2nd 14. Znd 15. Periodic Power Off Power Plant Electrical ELECTRICAL Remove battery for capacity check. Inspect the battery area for evidence of electrolyte leakage or over- flow; terminals for pitting and corrosion. Check momentary toggle switches for sticking in the 11 0N11 position. Inspect the reverse current relay externally for cleanliness and security; electrical connections for security. Inspect the voltage regulator for cleanliness and security; electrical connections for security; shock mounts for deterioration. Inspect the generator for security, cracked or broken mounting flange and end housing; electrical connections for security. Inspect the starter motor for cracJ.ced or broken mounting flange and security; electrical connections for security. Inspect the tachometer generator for security. Inspect the exte·rnal power receptacle for cleanliness and contacts for cleanliness. Inspect all relays for security of mounting and connections and service- ability of wires. Inspect the navigation, landing, cockpit and cabin lights for broken lenses, corrosion and security. Inspect the anchor light for broken lens, corrosion and security. Check the starter brushes for specified minimum length, even wear and freedom of movement in brush holders; inspect the commutator for evidence of excessive arcing. Check the generator brushes for specified minimum length, even wear and freedom of movement in brush hblders; inspect the commutator for evidence of excessive arcing_, dirt, oil, grease or metal particles. Inspect all electrical systems for the following: a. Wiring for deterioration, chafing, fraying, evidence of overheat- ing and security of clipping. b. Connector plugs for corrosion, cracks, evidence of overheating and security, c. Wire shielding for fraying, crimping and corrosion., d, Junction boxes for cracks, cleanliness and corrosion. 19 Periodic Power Off Electrical Instrllments Power On Power Plant INSP. DUE ITEM NO. 2nd ;,UEL SYSTEM 0 e. Bonding for damage, corrosion and security. 16, Check the booster pump motor for worn or binding brushes. INSTRUMENTS 1. Check the pitot static system for leaks and accumulation of moisture. 2. Inspect the instrument lines for deterioration, chafing and security o! connections. 3, Inspect all instrument electrical connections for security. 4. Inspect the thermocouple lead connections for security. 5. Inspect the instruments for broken or deranged pointers, cracked or broken glass, broken bezels, correctly positioned operating limit markings and security. 6. Check the gyro and artificial horizon caging mechanism for. operati.o.n. 7. Inspect the temperature bulbs for security and check the connector plugs for tightness. 8, Check the outside air temperature gauge against a master thermome· ter. 9. Inspect all instrument wiring for deterioration, chafing, fraying, over· heating and proper support. Shielding for fraying, corrosion and dam- age. Terminal strips, connections and bonding for damage, corrosion and security. ELECTRICAL POWER ON POWER PLANT I, Check the fuel quantity in tanks. 2. Inspect the fuel system components. lines, hoses and connections for leaks, chafing and security; lines for dents and s c ratches; hoses for cuts, cracks and deterioration. (Mixture control in "IDLE CUT-OFF" I l I' INSF l lI !I ! OIL~ e. of e- n- m ,r INSP. DUE OIL SYSTEM ITEM NO. and booster pump or wobble pump "ON"). Periodic Puw c r On Pow1•r Plant Electrical Instruments Engine Operation 3. Inspect for specified fuel pressure (mixture control in "IDLE CUT- OFF" and booster pump "ON"). 4. Inspect the fuel pressure warning system for specified calibration. 1. 1. 2. Check the oil dilution system for proper operation by disconnecting the line on the discharge side of the valve and with the mixture con- trol in "IDLE CUT-OFF", and booster pump or wobble pump 11 0N11 • Inspect for leaks when oil dilution valve is "OFF" and full flow when valve is "ON". ELECTRICAL Check the landing light for operation. Check the navigation lights for operation in "STEADY" and "FLASH" positions. 3, Check the instrument lights and intensity control rheostats for opera- tion. 4. Check the cockpit and cabin lights for operation. s. 6. Check the anchor light for operation. Check battery voltage on voltmeter. INSTRUMENTS 1. Check the pitot h~d heating element for operation. ENGINE OPERATION The !allowing checks should be performed during an engine ground run: 1. IDLE SPEED CHECK a. Check that engine idles at 500.:. 50 r.p.m. Z 1 · :>eriodic >ower On :ngine Operation tNSP. DUE ITEM NO. 2. IGNITION SWITCH CHECK. a. Set throttle at 600 r.p.m. b. Momentarily turn ignition switch "OFF". c. Engine should stop firing. 3, PROPELLER PITCH CHANGE CHECK. a. Set throttle at 1600 r.p.m. with propeller in full increase r.p.m. position, b, Move propeller lever to full decrease r.p.m. position. c. The r.p.m. should drop smoothly and rapidly to approximately 1000 r.p.m. 4. IDLING MIXTURE CONTROL CHECK (MANUAL). a. Set throttle at 450-500 r.p.m. b. Pull mixture control lever back to "FULL LEAN" position. c. The r.p.m. should momentarily rise approximately 20 r.p.m. before the normal drop, 5. IGNITION CHECK. a. Set throttle to 1750 r.p.m. b. Turn ignition switch to "L" and then to "R". c, Drop in either position should not exceed 100 r.p.m. d. If drop does exceed 100 r.p.m., set throttle at 2200 r.p.m. and recheck. NOTE Return ignition switch to "BOTH" between "L" and "R" checks to allow the engine to regain normal r.p.m. 6, POWER CHECK. a. Open throttle until manifold pressure is equal to airfield pres- sure and check that tachometer reading is within 2100 _:t 20 r.p.m. range, b. Check that fuel pressure gauge_ registers 3-5 p.s.i. c, Check that oil temperature gauge registers 40° C and that oil pressure gauge registers 75-85 ·p,s.i, INS1 ,. 'f f If !NSF. DUE ITEM NO, 7. Periodi c Power On Engine Ope ration d, Pull propeller control lever slowly back to halfway, then return to increase r.p.m., tachometer r.p.m. should remain steady, indicating that the propeller governor is functioning correctly. CARBURETTOR HEAT CHECK, .· a. Move carburettor heat control to the "HOT" position, then re - turn to the "COLD" position. b. Check for increase and decrease of carburettor mixture tem- perature. 8. GENERA TOR OUTPUT CHECK. a, Check that generator cuts in at approximately 1400 r.p.m. b. Check voltmeter an~ ammeter readings; voltage should not ex- ceed 28.5 volts. 23 f. J [l [l Ll [J rJ [l D [J u u u u u LJ u u PART 4 Spt·c:i. ,i Ai rrr:, 111•· Power l'la11 l SPECIAL INSPECTIONS INSPECTION DUE After cleaning or repair of safety belts and harnesses, and every 12 months. After salt water landing. After any circumstance which might result in damage to the landing gear. After heavy one wheel landing. Overspeed in excess of specified limits. Overspeed not in excess of specified limits. 10_ flying hours after engine inspection due to overspeed. At engine change. AIRFRAME ITEM NO, l. 2 . 3. 4. Weight test safety .belts and harnesses . Thoroughly clean exterior of aircraft with fresh water. Remove the tires from the wheels . Inspect the tires for damage and the wheels £or cracks and distortion. Inspect the landing gear components and c-ttachments for cracks, distortion and security. Inspect windshield frames, with particular attention to area at base of windshield centre post, for loose or sheared rivets or other damage. POWER PLANT l. 2. 3. 4. (a) Change the engine, (b) Completely dismantle propeller and governor and magnetically inspe c t all steel parts; visually inspect all other parts for cracks and distortion. (a) Inspect the engine for cracked or broken cylinder heads and barrels. (b) Remove the sump plugs and oil filter and check for m .etal particles; drain the oil from the sump and check for metal particles. Remove the sump plugs and oil filter and check for metal particles; drain o il from the sump and check for metal particles. (a) Check the vibration isolator core as- sembly £or specified dimensions. (b) Drain, flush and refill the oil system. ( c) Carburettor heater intake duct for security and flap valve for full travel. Revised l September 1963 ZS Special Power Plant [NSPECTION DUE a..fter ground run following an engine :hange or cylinder change. ?rior to first and second flights fol- .owing an engine change, \.fter an engine change and the flight :est following. ~fter a fuel system component is ·eplaced. ,fter a fuel quantity transmitter is eplaced, .fter first oil dilution, if 50 flying ours have elapsed since last dilu- lon series. rithin l hour after last flight when round temperature is below freezing. very 7 days when ground temperature , abo:ve freezing, very daily inspection, or as conditions emand, when operating in dusty areas, 6 ITEM NO, s. 6. 7. 8. 9. 1 o. 11. 12. 13. Inspect the air ducts for cleanliness and damage. "(d) Flight test, (a) Check the cylinder hold down nuts for correct safetying. (b) Check the manifolds and oil lines for leaks and security. ( c) Remove the sump plugs and oil filters and check. for metal particles. Check the fuel and oil hose clamps for proper positioning, leaks and tightness . Inspect all fuel system components, lines, ·hoses and _connections for chafing and security; metal lines for dents and scratch. es; hose £or cuts, cracks and deterioration: check for leaks (mixture control at "IDLE CUT-OFF" and booster pump "ON" or wobble pump operated). ( a) Check fuel flow, (b) Check lines, hoses and connections adjacent to new component for chafing and leaks (mixture control IDLE CUT -OFF booster pump "ON" or wobble pump operated). Check the lines, hoses and connections ad• jacent to the new component for chafing and leaks. Conduct a calibration test by adjust• ing transmitter at empty position and filliL..! tank in 5 gallon increments. Indicator should be correct within l gallon throughout range. Check the oil filter for cleanliness; drain the oil from the sump and drain off any sludge from the oil drain cock. Drain any water from oil tank sump. Drain any water from oil tank sump. Remove and clean carburettor air filter. Revised I Septemher I' 1 l Il IN! Ev Ev, At of a Eve Eve: Ever After rnight After ing ai: Every ,s for or ers :h- on; lng i- nd t- 11g mt 3 INSPECTION DUE Every propeller change. Every governor change, At 10 flying hours after delivery of aircraft. Every 50 hours of flying. Every C of A. Every 7 days. After any equipment changes which might cause compass deviation. After a water landing and after wash- ing aircraft, . Every 24 hours in dusty conditions. Revised 1 September l 963 ITEM NO. 14. 15, 16. 17. 18. ( a) (b) ( a) (b) Special Puwc1· Plant F.Jcctrici"ll Instruments R etorque retaining nut after 15 min- utes engine operation. Flight test. Retorque retaining nuts after 15 min- utes engine operation. Flight test. Check, tighten all accessory hold down nuts, clips, clamps and connections, Remove exhaust heat exchanger tube from the exhaust tail pipe assembly. Inspect thoroughly both internally and externally for deterioration, cracks or porosity. Pressure test under water to 10 p. s, i. Remove exhaust heat exchanger tube from the exhaust tail pipe assembly, Inspect thoroughly both internally and externally for deterioration, cracks or porosity. Pressure test under water to 50 p. s. i. ELECTRICAL l. Check the battery cells for proper electro- lyte level and specific gravity. Inspect leads and connectors for corrosion and check the connectors for tightness. Inspect the drain for obstructions, and the battery, container and cover for security. INSTRUMENTS 1 • 2. 3. Conduct a compass swing and replace cor- rection cards. Check pitot static system for moisture. Check pitot static ports for accumulation of dust. 27 · ITEM PART 5 RECOMMENDED OVERHAUL OR REPLACEMENT SCHEDULE This replacement schedule has been compiled to assist the operator in planning the periodic replacement of certain items of equipment by new or overhauled items. The flying hours suggested for rep1acement are based on ideal conditions and will vary according to the conditions under which each air- craft operates. AIRFRAME RECOMMENDED OVERHAUL OR REPLACEMENT Flap Actuating Jack Ratchet Valve 1400 Hours 1400 Hours 1000 Hours Horizontal Stabilizer to Fuselage Attachment Bolts ,Landing Gear Compression and Rebound Rubbers Brake Master Cylinders 1000 Hours or 24 Months 1200 Hours Wing Struts C2W469A/70A } Wing Struts C2W545A/46A Engine Spark Plugs Propeller POWER PLANT Propeller (with modified counterweight shafts) Governor Tachometer Generator Revised l September 1963 In accordance wit h n Engineering Bulletin # 15 ~ 800 Hours 200 Hours (Nominal) 800 Hours 800 Hours 800 Hours 2000 Hours or 36 Months 29 ITEM Voltage Regulator Generator Reverse Current Relay Starter Starter.Solenoid Flasher Booster Pump Turn & Bank Indicator (Electrical} Turn & Bank Indicator (Air Driven) Artificial Horizon Indicator Altimeter Airspeed Indicator Rate of Climb Indicator Directional Gyro Fuel Contents Transmitter (TJ13) Fuel Contents Indicator Vacuum Gauge Clock Cylinder Head Temperature Gauge Engine Gauge Unit Manifold Pressure Gauge Tachometer Carburetor Mixture Temperature Gauge Voltam.meter Magnetic Compass 30 ELECTRICAL INSTRUMENTS RECOMMENDED OVERHAUL OR REPLACEMENT 800 Hours 800 Hours 1000 Hours 800 Hours 1000 Hours 1000 Hours 800 Hours .12.00 Hours or 36 Months 1200 Hours or 24 Months 1000 Hours or 2.4 Months 2000 Hours 2000 Hours,. 2.000 Hours 1000 Hours or 2.4 Months 1600 Hours or 36 Mc,nths 2000 Hours or 36 Months 2000 Hours 1600 Hours 1200 Hours ZOOO Hours ZOOO Hours 2000 Hours or 36 Months 2000 Hours 1600 Hours 36 Months Revi s ed 15 June l '} •-l Crc Am; Car ·, .' l ' '/ I ~ l~ ITEM INSTRUMENTS Course Selector Cross Pointer Indicator Wheel/Ski Position Indicator Amphibious Float Wheel Position Indicator ENGINE FIRE PROTECTION Cartridge Unit Revised 1 September 1963 RECOMMENDED OVERHAUL OR REPLACEMENT 2000 Hours 1200 Hours or 36 Months 2000 Hours 2000 Hours 5 years after date of manufacture or 2 years after removal from its sealed package 31