TEMPORARY REVISION N 0C702 TR 07 20131010

Temporary Revision N 0c702 Tr 07 20131010-Free PDF

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TIME LIMIT COMPONENTS,MAINTENANCE MANUAL EXTRA 300 SC. 05 10 03 Recommended Replacement Times, It is recommended to replace the items shown in the follow. ing schedule at the times indicated The times may be. modificated by the respective national authorities. Item Replace,Battery Concorde on condition, on the recommendation Batteries of the ELT Pointer 2 years. of the manufacturer,Batteries of the ELT Artex 5 years. Wheels Cleveland Parker on condition,Tires on condition.
Oil hoses rubber type on condition,MIL DTL 6000C34. Brake hoses sensing hoses on condition,Knapp Hoerbiger. Fuel oil sensing hoses on condition,PTFE Type MIL DTL 25579 but in engine comp at. the latest together with,engine removal,Wingtip strobe light If any one LED fails. the unit must be,Seat belts Hooker Rework or replace.
after a period of 6 years,in use service life limit. of national aviation,authority must be,considered,Brake and brake assembly on condition. Cleveland Parker,Rudder control cable on condition. Fairleads on condition,Shock mounts on condition,Barry Controls but at the latest at each. engine overhaul, if not stated otherwise Bolts and nuts on condition.
PAGE DATE 10 October 2013 TEMPORARY REVISION CHAPTER 05. N 0C702 TR 07 20131010 PAGE 5,SCHEDULED MAINTENANCE CHECKS. MAINTENANCE MANUAL EXTRA 300 SC Maintenance Checks Schedule. s rs Date Inspector,0 00 Serial No Mechanic,s pe h 5 h 1. c Inspections,Instruments, O 1 Inspect panel mounting for security and safety. O 2 Check operation mounting and wiring of switches for condi. tion and safety, O 3 Check automatic circuit breaker mounting and wiring for. condition and safety,4 Reserved,WARNING Risk of blinding due to LED radiation.
Do not stare into beam,Wear eye protection, O 5 Check wing tip strobe lights for security and operation If any. one LED fails the units must be replaced Inspect the lens. Replace the unit if there is excessive scratching discoloration. or cracking, O O 6 Inspect compass and compass deviation card for proper indi. cation and compensation,O 7 Magnetic compass compensation. O 8 Check pitot static air pressure lines for condition and leaks. perform operational check,Electrical system,O O 1 Check engine bonding. O O 2 Check tank bonding wing and center tank, O 3 Check system wiring free from fraying or cracks.
O 4 Inspect battery and attachment,O O 5 Charge battery. 1 Annual each twelve calendar month, PAGE DATE 10 October 2013 TEMPORARY REVISION CHAPTER 05. N 0C702 TR 07 20131010 PAGE 24,INSTRUMENT PANEL,MAINTENANCE MANUAL EXTRA 300 SC. Instrument Panel,ON ON ON ARM,2 10 15 10 5 5 3 1 3. WARNING OFF OFF OFF REFILL, MASTER BOOST STROBE SMOKE ALT SMOKE COM XPDR TRIM 12 V.
SWITCH PUMP LIGHTS SYSTEM OUTPUT SYS STARTER,1 2 3 4 5 6 7 8 9 10 11 12 13 14. Switches Light and Circuit breakers, PAGE DATE 10 October 2013 TEMPORARY REVISION CHAPTER 31. N 0C702 TR 07 20131010 PAGE 4,MAINTENANCE MANUAL EXTRA 300 SC. 1 12 Volt power source jack,3 Air speed indicator,5 Manifold pressure fuel flow. 6 Magn direction indicator,7 RPM indicator,9 Trim position indicator.
10 Trim position switch,11 Altimeter,13 ELT switch. 14 Ammeter,15 Oil pressure oil temperature,16 Fuel quantity Rear center tank. 17 Fuel quantity Front center tank,18 Fuel quantity Wing tanks. 19 EGT CHT indicator,20 Magneto selector switch starter. 21 Switches circuit breakers light as listed below. 1 Alternator warning light incl press to test feature. 2 Master switch,3 Boost pump circuit breaker switch.
4 Strobe lights circuit breaker switch,5 Smoke system switch. 6 Overvoltage protection system cicuit breaker,7 Alternator output circuit breaker. 8 Smoke system circuit breaker,9 Starter circuit breaker. 10 Instruments circuit breaker,11 COM circuit breaker. 12 XPDR circuit breaker,13 TRIM circuit breaker,14 12 V circuit breaker.
PAGE DATE 10 October 2013 TEMPORARY REVISION CHAPTER 31. N 0C702 TR 07 20131010 PAGE 5,MAINTENANCE MANUAL EXTRA 300 SC. Chapter 33,33 10 00 FLIGHT COMPARTMENT 3,33 40 00 EXTERIOR 4. 33 40 10 LED Strobe Light System 4,33 40 11 LED Strobe Light 5. PAGE DATE 10 October 2013 TEMPORARY REVISION CHAPTER 33. N 0C702 TR 07 20131010 PAGE 2,MAINTENANCE MANUAL EXTRA 300 SC. 33 40 00 EXTERIOR,33 40 10 LED Strobe Light System.
Refer to figure 1 The LED strobe lights are installed on both. The wiring is routed through an aluminium tube inside the. wing and along the left resp right upper longeron to the. instrument panel, The circuit breaker switch is located on the instrument panel. see figure 2 of chapter 31, PAGE DATE 10 October 2013 TEMPORARY REVISION CHAPTER 33. N 0C702 TR 07 20131010 PAGE 4,MAINTENANCE MANUAL EXTRA 300 SC. 33 40 11 LED Strobe Light,Removal Installation,Refer to figure 1. 1 Power down the LED strobe lights,2 Remove the wing tip cover attachment bolts 3.
3 Pull out the wing tip cover plate some centimeters. 4 Remove the LED strobe light attachment bolts 1,5 Disconnect the electrical wiring. 6 Remove the LED strobe light, 7 Install in reverse sequence of removal after applying Sili. con between the wing tip cover and the LED strobe light. PAGE DATE 10 October 2013 TEMPORARY REVISION CHAPTER 33. N 0C702 TR 07 20131010 PAGE 5,PAGE DATE 10 October 2013. MAINTENANCE MANUAL EXTRA 300 SC,TEMPORARY REVISION. N 0C702 TR 07 20131010,LED Strobe Lights Removal Installation.
1 LED Strobe light attachment bolts,NOTE 2 LED Strobe light. The electrical wiring 3 Wing tip cover attachment bolts. has been omitted 4 Wing tip cover,5 Wing tip,MAINTENANCE MANUAL EXTRA 300 SC. Table of Contents,Figure Title,EA 9C102D POWER GENERATION DISTRIBUTION. EA 9C102 2A Magneto System,EA 9C102 3A Strobe Light System. EA 9C102 4A Fuel Gages,EA 9C102 5A COM S E Ger t,EA 94102 6 Audio Switches Jacks.
EA 9C102 7A Alternator Warning,EA 9C102 8 Smoke System. EA 9C102 9C Battery Circuit,EA 9C102 10A Alternator System. EA 9C102 11 Fuel Boost Pump,EA 94102 14C Pedal Adjustment System. EA 9C102 15 Accelerometer,EA 9C102 16B External Power. EA 93102 18A Batterie Charger System,EA 93102 22 Transponder BXP6401.
EA 9C102 27B Ampere Indication,EA 93102 28 Fuel Flow EDM700. EA 93102 29 Fuel Flow EDM800,EA 9C102 30A RPM Indication. EA 96102 31 Starter Engaged Light,EA 93102 33 Fuel Flow FS 450. EA 9D102 34 Oil Press Temp Indication,EA 93102 41A ELT Pointer 3000. EA 9D102 42A ARTEX ME 406 ELT,EA 93102 43 Transponder BXP 6401 x Enc.
EA 9C102 44A Electric Trim System,EA 96102 49 RC Allen RCA2600. EA 9C102 58 EGT CHT Indication,EA 9D102 58 EGT CHT Indication. EA 93102 59 Flight Timer, PAGE DATE 10 October 2013 TEMPORARY REVISION CHAPTER 91. N 0C702 TR 07 20131010 PAGE 2,see ALTERNATOR WARNING STARTER. EA 9C102 7 START RELAY M1,see ALTERNATOR SYSTEM K2.
MAIN BUS EA 9C102 10 4,see BATTERY CIRCUIT,STARTER see BATTERY CIRCUIT. EA 9C102 9,10A 1 EA 9C102 9 F7,18 20 see STARTER ENGAGE LIGHT Option. EA 96102 31,MAGNETO SWITCH Holder,S5 R L BOTH,20 left Magn. L see RPM INDICATION,18 GRD LR EA 9C102 30,20 right Magn. MAGNETOS R 18,SLICK START,SS 1001 20 6350,1 MAGNETOS L 18.
X 8 WIRE 1 x AWG 18 SHIELDED MIL C 27500 18TG1 mtr 02199. X 7 WIRE AWG 18,MIL W 22759 16 18 mtr 00776,X 6 WIRE AWG 20. MIL W 22759 16 20 mtr,1 5 SLICK START SS 1001,1 4 MAGNETO LEFT 6393. 1 3 MAGNETO RIGHT 6350,1 2 MAGNETO SWITCH 10 357200 1 00185. 1 1 CIRCUIT BREAKER 10A 7277 2 10 31505, 04 03 02 01 Nr Benennung Teilekennzeichen ZF Werkstoff Abmessungen Menge Einheit Gewicht MaWi Nr. Die G ltigkeitszuordnung Letzte Bearbeitung Datum Name Ma stab auf Projektion. von Version zu Bearb 05 05 08 HW SI Klasse Freima toleranz. Flugzeugbaureihe Oberfl chenschutz Oberfl che,ist der Bauakte bzw Gepr.
dem jeweiligen Fertigungsauftrag Gepr EA 300 SC,zu entnehmen. Zuordnung links rechts wird mit MAGNETO SYSTEM,A in allen Feldern angegeben A. 03 EA 9C102 2,02 Schwarze Heide 21 A4 Blatt 1 von 1. 01 A ab SC006 11 07 2008 HW 46569 H nxe Germany, Ver Bezeichnung Nr nderung Mod Nr Datum Name Schutzvermerk nach DIN 34 beachten. EDV Kennung EA3C0907,RIGHT WING,4 6 3 5 4 6 3 5,20 20 yel VCCS.
20 blk GND,B 7 Strobe white B,4 6 3 5 1 4 6 3 5 2,20 blk GND. 20 20 yel VCCS,Strobe white,X 7 WIRE AWG 20 MIL W 22759 16 20 mtr 02199. 4 6 BUCHSEN GEH USE 2 POLIG 180923 0 Fa AMP 00099,4 5 PIN GEH USE 2 POLIG 180924 0 Fa AMP 00103. 8 4 FLACHSTECKER BUCHSE 6 3mm 0042282 2 Fa AMP 00093. 8 3 FLACHSTECKER PIN 6 3mm 42565 2 Fa AMP 00097,2 2 LAMP ASSY AVE POSW 54G AVEO Engineering 34217. 1 1 CIRCUIT BREAKER SWITCH 5A W31X2M1G 5 02700, 04 03 02 01 Nr Benennung Teilekennzeichen ZF Werkstoff Abmessungen Menge Einheit Gewicht MaWi Nr.
Die G ltigkeitszuordnung Letzte Bearbeitung Datum Name Ma stab auf Projektion. von Version zu Bearb 05 05 08 HW SI Klasse Freima toleranz. Flugzeugbaureihe Oberfl chenschutz Oberfl che,ist der Bauakte bzw Gepr. dem jeweiligen Fertigungsauftrag Gepr EA 300 SC,zu entnehmen. Zuordnung links rechts wird mit STROBE LIGHT SYSTEM. D in allen Feldern angegeben D,EA 9C102 3 A,02 Schwarze Heide 21 A4 Blatt 1 von 1. Refer to EA 1C109 5 01 A M 300 13 10 08 08 13 HW, 1 Nr nderung Mod Nr Datum Name 46569 H nxe Germany. Ver Bezeichnung Schutzvermerk nach DIN 34 beachten. EDV Kennung EA3C0910,22 see RPM INDICATION,13 EA 9C102 30.
22 see OIL TEMP PRESS,EA 93102 34,20 see STARTER ENGAGE LIGHT Option. EA 96102 31,22 22 22 22,13 9 13 13,G I I G I G,FUEL FUEL FUEL. WING REAR CENTER FRONT CENTER,B INDICATOR 7 INDICATOR INDICATOR B. 2 3 180Ohm 240 33 Ohm 3 240 33 Ohm 3, 10 9 10 9 1 Kabel 22 an Pos 9 12 doppelt umgeschlagen quetschen. 1 2 1 2 X X 14 KABEL AWG 22 MIL W 22759 16 22 4 mtr 01694. 11 12 11 12 11 14 13 RING SE ROT 4mm 031890 01417,4 4 12 FLACHSTECKER PIN 6 3mm 1 42565 2 00097.
2 2 11 PIN GEH USE 2 POLIG 180924 0 00103, 8 13 13 2 2 10 BUCHSEN GEH USE 2 POLIG 180923 0 00099. C 9 6 9 FLACHSTECKER BUCHSE 6 3mm 1 0042282 2 00093 C. 9 2 2 8 BUCHSEN GEH USE 1 POLIG 925324 2 00098, S G S G 1 7 BUCHSEN GEH USE 3 POLIG X39 000 000 002 00386. 1 1 6 FRONT CENTER SENSOR 02700 15 Fa DATCON 33410. 1 1 5 REAR CENTER SENSOR 02700 12 Fa DATCON 33409, 4 5 6 1 1 WING FUEL SENSOR 226 801 015 001G FM4006. R 2 2 3 FUSELAGE FUEL INDICATOR 100176 33411, C C 1 2 WING FUEL INDICATOR DATCON 100726 Fa DATCON 33412. 226 801 015 001G 02700 12 02700 15,1 2 WING FUEL INDICATOR VDO 301 030 001G 200171.
WING REAR CENTER FRONT CENTER 1 1 1 CIRCUIT BREAKER 5A 7277 2 5 31506. TANK TANK TANK, 04 03 02 01 Nr Benennung Teilekennzeichen ZF Werkstoff Abmessungen Menge Einheit Gewicht MaWi Nr. Die G ltigkeitszuordnung Letzte Bearbeitung Datum Name Ma stab auf Projektion. von Version zu Bearb 05 05 08 HW SI Klasse Freima toleranz. Flugzeugbaureihe Oberfl chenschutz Oberfl che,ist der Bauakte bzw Gepr. S G dem jeweiligen Fertigungsauftrag Gepr EA 300 SC. STUD 8 32 zu entnehmen,Zuordnung links rechts wird mit FUEL GAGES. D in allen Feldern angegeben D,02700 12 04,EA 9C102 4 A. 02 Schwarze Heide 21 A4 Blatt 1 von 1,01 A M 300 09 19 12 10 2010 HW.
OPTION 02 FUEL WING INDICATOR Fa VDO Nr nderung Mod Nr Datum Name 46569 H nxe Germany. Ver Bezeichnung Schutzvermerk nach DIN 34 beachten. OPTION 01 FUEL WING INDICATOR FA DATCON EDV Kennung EA3C0908. 2 14 VDC AVIONIC BUS,COM S E GER T xA 1,13 75 VDC 11. 13 75 VDC 12,Lighting 23 J4 P4,PTT 17 A8 2,bl 24 bl bl 24 bl 24. see AUDIO JACKS SWITCHES,IC Control 7,EA 94102 6,ws ws ws ws. Mic Hi 18 A4,bl 24 bl bl 24 bl,B Mic GND 14 A3 B,R1 PHONE JACK. Phone Hi 2 ws ws ws ws,Phone Lo 3 bl 24 bl bl 24 bl.
bl bl see ACCELEROMETER,ws ws EA 9C102 15,Lighting 10. 1 1 9 RESISTOR 330 OHM 0 25 W CFR16J330RJIT FE4286. C X X 8 WIRE RG 400 RG 400 mtr FE4111 C,X X 7 WIRE 2xAWG24 MIL C 27500 24TG2 mtr FE4006. X X 6 WIRE AWG 20 MIL W 22759 16 20 mtr 00775,A C GROUND. 1 1 5 VHF ANTENNA 3001 10 FE4254,2 2 4 BNC CONNECTOR 11BNC 50 3 52 133 30705. RG 400 1 1 3 CONNECTOR KIT in Pos 2,1 2 COM S E GREAT AR 6201 0894 011 07 00652.
1 2 COM S E GREAT AR 4201 0610 321 9xx 33041,8 1 CIRCUIT BREAKER 7 5A 7277 2 7 5 32112. 1 1 CIRCUIT BREAKER 5A 7277 2 5 31506, 05 04 03 02 01 Nr Benennung Teilekennzeichen ZF Werkstoff Abmessungen Menge Einheit Gewicht MaWi Nr. COM ANTENNA Letzte Bearbeitung Datum Name Ma stab auf Projektion. P3 Die G ltigkeitszuordnung, von Version zu Bearb 05 05 08 HW SI Klasse Freima toleranz. Flugzeugbaureihe Oberfl chenschutz Oberfl che,ist der Bauakte bzw Gepr. dem jeweiligen Fertigungsauftrag Gepr EA 300 SC,zu entnehmen.
Zuordnung links rechts wird mit COM S E GER T,D in allen Feldern angegeben D. EA 9C102 5 A,02 Schwarze Heide 21 A4 Blatt 1 von 1. 01 A M 300 11 08 14 04 11 HW, OPTION 02 BECKER COM AR 6201 Nr nderung Mod Nr Datum Name. 46569 H nxe Germany, Ver Bezeichnung Schutzvermerk nach DIN 34 beachten. OPTION 01 BECKER COM AR 4201 EDV Kennung EA3C0911a. MAINTENANCE MANUAL EXTRA 300 SC TEMPORARY REVISION N 0C702 TR 07 20131010 PAGE DATE 10 October 2013 Pos Item 1 12 Volt power source jack 2 COM 3 Air speed indicator 4 Blank 5 Manifold pressure fuel flow 6 Magn direction indicator 7 RPM indicator 8 G meter 9 Trim position indicator 10 Trim position switch 11 Altimeter 12 XPDR 13 ELT

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