Installation Instruction 150 & 172 SERIES.

Transcription

1 Installation Instruction 0 & SERIES

2 Part 0 Manual Administration 0. Table of Contents PART 0 MANUAL ADMINISTRATION 0. TABLE OF CONTENTS 0. DOCUMENT APPROVAL 0. AMENDMENT RECORD PROCEDURE 0. EFFECTED PAGES PROCEDURE 0. DISTRIBUTION LIST PART INSTALLATION INSTRUCTION. GENERAL. DESCRIPTION.. Position and anti-collision lights.. Taxi- and landing lights.. Energy consumtion. WINGTIP INSTALLATION CONVENTIONAL LIGHTS.. Wingtip Installation Left.. Wingtip Installation RIGHT 0. WINGTIP INSTALLATION CONFORMAL SOLUTION.. Wingtip Installation LEFT.. Wingtip Installation RIGHT. NAVIGATION LIGHTS INSTALLATION TAIL POSITION. ANTICOLLISION LIGHT INSTALLATION. LANDING / TAXI LIGHT INSTALLATION 0. LANDING LIGHT INSTALLATION 0. LANDING / TAXI LIGHT INSTALLATION.0 ADDITION OF STROBE FUNCTION PART COMPLIANCE DEMONSTRATION Issue of form 0 Drasov 0, 0 Drasov Page of

3 0. Document approval This document has been established in accordance with an alternative procedure to DOA approved under EASA AP. This installation Instruction is applicable for all Cessna 0 and. Compiled by: Dec - 0 Petr Jaros Engineer, Approved by: Dec - 0 Georg Hartl Head of DO, 0. Amendment Record procedure The master copy of this document shall be kept electronically as a read only document under the control of as Master Copy. ALL amendments to this manual will initiate a raise of Issue ALL raises of issue will be given a sequential Alphabetic Issue Ident sequentially from 0 to in Table 0 - Issue No: Column Initial Issue of Document will be 0 ALL Issues of this document will be approved by Head of DO Issue No. Details 0 Initial Issue 0 Corrections as marked addition of Conformal Solution. addition of two light anticollision light solution Date 0 Nov 0 Dec 0 Effected Pages ALL ALL - - Table 0: Document Amendment Record Table 0. Effected Pages Procedure ALL pages affected by ANY raise of issue of this manual will be listed in Table 0 - Effected Pages Column. The reason(s) for ALL raise of issue and description of change due to raise of issue will be provided for ALL raises of issue in Table 0 - Details Column. Changes from the previous issue are highlighted by YELLOW HIGHLIGHTING over new content. AND YELLOW HIGHLIGHTING AND CROSSING OUT of deleted content. Example (CROSSING OUT) Issue of form 0 Drasov 0, 0 Drasov Page of

4 0. Distribution List As stated in 0. above; the master copy of this document shall be kept electronically as a read only document under the control of Aveo Engineering Group, s.r.o. as Master Copy. All holders of copies of this Document will be recorded by listing in Table 0 Distribution List. Copy holders listed will be issued a copy of this document with sequential copy number as shown in Table 0 Distribution List Copy No. MASTER Holder Table 0: Distribution List Issue of form 0 Drasov 0, 0 Drasov Page of

5 Part Installation Instruction. General This installation is to be performed in accordance to common practice as described in FAR AC.-B Chapter and in FAR AC. B Chapter Section (Bonding) as published by FAA. The installer is responsible to follow the installation instructions in the latest revision of: FAR AC.-B Chapter FAR AC. B Chapter Section AVE-H0-00-IM AVE-WPS-G-IM AVE-POSW-G-IM AVE-RBXP-00-IM AVE-CCPS-IM_0 All drawings applicable for this change are listed in the Drawing List: AVE-MOD-00-DL, issue 0 The following appliances carry an ETSO authorization: AVE-POSW-G ETSOA O.00 AVE-WPSR-G & AVE-WPSG-G ETSOA O.00 AVE-WPSR-G & AVE-WPSG-G ETSOA O.00 AVE-RBXPR-00 ETSOA O.000 AVE-RBXPR-00 ETSOA O.000 AVE-CCPSR-D & CCPSG-D EASA Account Number: 0 The change is to be performed using the document AVE-MOD-00-MCS in the latest issue. The aircraft manuals remain fully valid. For maintenance of the new lights follow the Aveo Installation Manuals referenced above.. Description This modification is the replacement of the composite wingtip segment and of position, anti-collision, taxi- and landing lights by LED type lights... Position and anti-collision lights The new position lights all also include the strobe function. Also two options for the anti-collision lights can be installed. The RedBaron XP Galactica offers the red or white anti-collision light or two units of RedBaron Mini Galactica. As not all C0 and are already equipped with the strobe function (white strobe) Issue of form 0 Drasov 0, 0 Drasov Page of

6 in addition to the red beacon, this function may be added with this modification. Hence the following optional installations can be done with this modification: For aircraft with strobe function already installed: Position lights including strobe + Beacon red (RedBaron XP) Position lights including strobe + Beacon red including strobe (RedBaron Mini) For aircraft without strobe: Position lights without strobe + Beacon red (RedBaron XP) Additional switch and wiring change + Position lights including strobe + Beacon red (RedBaron XP or two RedBaron Mini) Additional switch and wiring change + Position lights including strobe + Beacon red including strobe (RedBaron XP or two RedBaron Mini) Synchronization: The strobe lights may be synchronized but the frequency of the strobes is so low that synchronization of the lights is not required. For the synchronization function the blue wires of each light to be synchronized have to be connected. If for this function additional wires are to be installed then these must be installed along the wire bundle in which the lights power wires run. If the function is not used the blue wire at each light is to be capped and stowed... Taxi- and landing lights The C0 and can be equipped with a taxi light (wide angle lens) and a landing light (narrow angle). This modification allows replacing all installed taxi and landing lights with the same configuration as installed before the modification. A configuration change is not allowed... Energy consumtion The analysis (I= IB a IL) showed that after installation of LED lights, in case of Position/Strobe lights, the total energy consumption dropped by.% when Ultra Galactica Embedded lights or by.0 % when Crystal Conforma lights were installed. In case of Landing/Taxi lights, the energy consumption dropped by. %. On the contrary, in case of Anti-collision lights, the energy consumption increased by.% when RedBaron XP Galactica or by. % when two RedBaron Mini Galactica lights were installed. It was caused by higher power drain of our AVEO lights. Issue of form 0 Drasov 0, 0 Drasov Page of

7 Lights Input Current Input Current Lights I BUBL (A) I LED (A) Position light/strobe.0 /. Ultra Galactica 0. /. Position light/strobe.0 /. Ultra Galactica Embedded 0. /. Position light/strobe.0 /. Crystal Conforma 0. /. Tail position light.0 PosiStrobe CP 0. /. Anti-collision.0 RedBaron XP Galactica. Anti-collision.0 RedBaron Mini Galactica.0 GE0. Hercules Drop-In Landing. GE. Hercules Drop-In Taxi. Table 0: Energy consumtion Note: GE0, GE original Cessna Langing and TAXI bulbs. Issue of form 0 Drasov 0, 0 Drasov Page of

8 . Wingtip Installation Conventional Lights.. Wingtip Installation Left 0,, STROBE Issue of form 0 Drasov 0, 0 Drasov Page of

9 Figure and Index Number Part Number Description Parts Avail. QTY. Per assy AVS-C0000-A0A AVS-C0000-A0A AVE-WPSTR-G AVE-WPSR-G AVS- P0000-A0 AVS- P0000-AA ANCR AN-R S CM-0 Wingtip Fiberglass subassembly Left Wingtip Carbon subassembly Left Ultra Galactica (RED) Ultra Galactica embedded (RED) Mx Gasket Original fasteners Connector Kit - Male Connector Kit - Female Nutplate Breaker LDG Light AWG0 Wire Yellow - Strobe AWG Wire Blue - Synchro STROBE Sticker NOTES Remove installed wing tip and verify that aircraft structure is not subject to substantial corrosion. In case of detected corrosion apply relevant AMM section or consult OEM before continuing with this installation. (#) Use original fasteners to mount wingtips to the wing. The lights are to be connected as described in manual AVE-WPS-G-IM or AVE-WPS- G-IM. If the strobe function is not used the blue and the yellow wires described in the component installation manual are not used and therefore have to be capped and stowed. If the aircraft (Cessna 0 only) is not already equipped with the strobe function this function can be installed through this change by following the instructions in.0. Additional cables for strobe (#) and synchronization (#) function and circuit breaker (#) and STROBE sticker (#) are to be installed according to.0. Issue of form 0 Drasov 0, 0 Drasov Page of

10 .. Wingtip Installation RIGHT 0,, STROBE Issue of form 0 Drasov 0, 0 Drasov Page 0 of

11 Figure and Index Number Part Number Description Parts Avail. QTY. Per assy AVS-C000-A0A AVS-C000-A0A AVE-WPSTG-G AVE-WPSG-G AVS- P0000-A0 AVS- P0000-AA ANCR AN-R S CM-0 Wingtip Fiberglass subassembly Right Wingtip Carbon subassembly Right Ultra Galactica (GREEN) Ultra Galctica embeded (GREEN) Mx Gasket Original fasteners Connector Kit - Male Connector Kit - Female Nutplate Breaker LDG Light AWG0 Wire Yellow - Strobe AWG Wire Blue Synchro STROBE Sticker NOTES Remove installed wing tip and verify that aircraft structure is not subject to substantial corrosion. In case of detected corrosion apply relevant AMM section or consult OEM before continuing with this installation. (#) Use original fasteners to mount wingtips to the wing. The lights are to be connected as described in manual AVE-WPS-G-IM or AVE-WPS- G-IM. If the strobe function is not used the blue and the yellow wires described in the component installation manual are not used and therefore have to be capped and stowed. If the aircraft (Cessna 0 only) is not already equipped with the strobe function this function can be installed through this change by following the instructions in.0. Additional cables for strobe (#) and synchronization (#) function and circuit breaker (#) and STROBE sticker (#) are to be installed according to.0. Issue of form 0 Drasov 0, 0 Drasov Page of

12 . Wingtip Installation Conformal Solution.. Wingtip Installation LEFT 0, STROBE Issue of form 0 Drasov 0, 0 Drasov Page of

13 Figure and Index Number Part Number Description Parts Avail. QTY. Per assy AVS-C00-A00 AVS-C00-A00 AVE-CCPSR-D0 AVS-C00-A00 AVS- SCM000FAS-D0A AVS- SCM000HAS-D0A AVS- WAM0DFS-D0A S- AN-R ANCR CM-0 Wingtip Fiberglass subassembly Left Wingtip Carbon subassembly Left Drooped Crystal Conforma Red Cessna Conforma Light Module Holder L Washer Connector Kit - Male Connector Kit - Female Nutplate Original fasteners Breaker LDG Light AWG0 Wire Yellow - Strobe AWG Wire Blue - Synchro STROBE Sticker NOTES Remove installed wing tip and verify that aircraft structure is not subject to substantial corrosion. In case of detected corrosion apply relevant AMM section or consult OEM before continuing with this installation. (#) Use original fasteners to mount wingtips to the wing. The lights are to be connected as described in manual AVE-CCPS-IM. If the strobe function is not used the blue and the yellow wires described in the component installation manual are not used and therefore have to be capped and stowed. If the aircraft (Cessna 0 only) is not already equipped with the strobe function this function can be installed through this change by following the instructions in.0. Additional cables for strobe (#) and synchronization (#) function and circuit breaker (#) and STROBE sticker (#) are to be installed according to.0. Issue of form 0 Drasov 0, 0 Drasov Page of

14 .. Wingtip Installation RIGHT 0, STROBE Issue of form 0 Drasov 0, 0 Drasov Page of

15 Figure and Index Number Part Number Description Parts Avail. QTY. Per assy AVS-C00-A00 AVS-C00-A00 AVE-CCPSG-D0 AVS-C00-A00 AVS- SCM000FAS-D0A AVS- SCM000HAS-D0A AVS- WAM0DFS-D0A S- AN-R ANCR CM-0 Wingtip Fiberglass subassembly Right Wingtip Carbon subassembly Right Drooped Crystal Conforma - Green Cessna Conforma Light Module Holder R Washer Connector Kit - Male Connector Kit - Female Nutplate Original fasteners Breaker LDG Light AWG0 Wire Yellow - Strobe AWG Wire Blue - Synchro STROBE Sticker NOTES Remove installed wing tip and verify that aircraft structure is not subject to substantial corrosion. In case of detected corrosion apply relevant AMM section or consult OEM before continuing with this installation. (#) Use original fasteners to mount wingtips to the wing. The lights are to be connected as described in manual AVE-CCPS-IM. If the strobe function is not used the blue and the yellow wires described in the component installation manual are not used and therefore have to be capped and stowed. If the aircraft (Cessna 0 only) is not already equipped with the strobe function this function can be installed through this change by following the instructions in.0. Additional cables for strobe (#) and synchronization (#) function and circuit breaker (#) and STROBE sticker (#) are to be installed according to.0. Issue of form 0 Drasov 0, 0 Drasov Page of

16 . Navigation Lights Installation Tail Position 0 Issue of form 0 Drasov 0, 0 Drasov Page of

17 Figure and Index Number Part Number Description Parts Avail. QTY. Per assy AVE-POSW-G S- MS AN-R S Mount PosiStrobe CP Rudder assembly Refer to figure 0 Nut Connector Kit - Male Connector Kit - Female Nutplate AWG Wire Blue Synchro AWG0 Wire Yellow - Strobe NOTES Remove installed navigation light and verify that aircraft structure is not subject to substantial corrosion. In case of detected corrosion apply relevant AMM section or consult OEM before continuing with this installation. The lights are to be connected as described in manual AVE-POSW-G-IM. If the strobe function is not used the blue and the yellow wires described in the component installation manual are not used and therefore have to be capped and stowed. If the aircraft is not already equipped with the strobe function this function can be installed through this change by following the instructions in.0. Additional cables for strobe (#) and synchronization (#0) function are to be installed according to.0. Issue of form 0 Drasov 0, 0 Drasov Page of

18 . Anti-collision Light Installation B STROBE A B TOP BOTTOM Issue of form 0 Drasov 0, 0 Drasov Page of

19 Figure and Index Number Part Number Option A AVS-P0000-AA AVE-RBXPR-00 AVE-LARBUHS-0B 00- NAS0A AN-R S- S0Z- MS- MS Option B TOP AVS-P00000-AA AVE- RBXPR-00 AVS-P00000-A0 00- NAS0A AN-R S- S0Z- MS- MS Option B BOTTOM AVS-P00000-AA AVE- RBXPR-00 AVS-LAM0Z-M00 MS0AD AN-R S Description Hex Socket Metric Assy RedBaron XP Galactica Original Fasteners RedBaron Legacy Light Replacement Adapter Plate assembly mounting Nutplate Tip Assembly- flashing beacon Tip Assembly- flashing beacon Connector Kit - Male Connector Kit - Female Nutplate Gromet Gromet AWG Wire Blue Synchro Hex Socket Metric Assy RedBaron Mini Galactica Original Fasteners RedBaron Mini Light Replacement Adapter Plate assembly mounting Nutplate Tip Assembly- flashing beacon Tip Assembly- flashing beacon Connector Kit - Male Connector Kit - Female Nutplate Gromet Gromet AWG Wire Blue Synchro Hex Socket Metric Assy RedBaron Mini Galactica M Two Lug Anchor Nut Rivet Connector Kit - Male Connector Kit - Female Nutplate AWG Wire Blue Synchro Parts Avail QTY. Per assy Issue of form 0 Drasov 0, 0 Drasov Page of

20 NOTES Remove installed anticollision light and verify that aircraft structure is not subject to substantial corrosion. In case of detected corrosion apply relevant AMM section or consult OEM before continuing with this installation. The lights are to be connected as described in manuals AVE-RBXP-00-IM depending on which option is to be installed. If the aircraft (Cessna 0 only) is not already equipped with the strobe function this function can be installed through this change by following the instructions in.0. Option A: Additional cable for synchronization function (#) is to be installed according to.0. Option B: Additional cable for synchronization function (#) is to be installed according to.0. Used drawing number 000 Fitting Modification for bottom light installation. Issue of form 0 Drasov 0, 0 Drasov Page 0 of

21 . Landing / Taxi Light Installation 0 Issue of form 0 Drasov 0, 0 Drasov Page of

22 Figure and Index Number Part Number Description Parts Avail. QTY. Per assy. 0 Option A - - S0Z- AVE-H0TATSNL-T0A AN R NASDD- AN0-0 AN0-0L NAS-- Support assembly landing light Bracket LH Bracket RH Hercules Drop-In Landing Gasket Plate assembly LH Plate assembly RH Spacer -----LH only Washer-----LH only Washer-----LH only NUT AR AR AR 0 Option B - - S0Z- AVE-H0TATSNL-T0A AVE-H0TATSNT-T0A AN R NASDD- AN0-0 AN0-0L NAS-- Support assembly landing light Bracket LH Bracket RH Hercules Drop-In Landing Hercules Drop-In Taxi Gasket Plate assembly LH Plate assembly RH Spacer -----LH only Washer-----LH only Washer-----LH only NUT AR AR AR NOTES It is to be checked by the installer before the modification whether Option A or B is installed on the aircraft. For a change in configuration e.g. landing lights into landing and taxi light requires an additional EASA change. Remove installed landing / taxi lights and verify that aircraft structure is not subject to substantial corrosion. In case of detected corrosion apply relevant AMM section or consult OEM before continuing with this installation. Remove existing connector and replace as indicated. Verify polarity of wires before connection (ref. to AVE-H0-00-IM). Issue of form 0 Drasov 0, 0 Drasov Page of

23 . Landing Light Installation 0 Issue of form 0 Drasov 0, 0 Drasov Page of

24 Figure and Index Number Part Number Description Parts Avail. QTY. Per assy. 0&0A Landing light AN-R AN0-L NAS0A0 00- S0Z- NAS AN-R 00- AVE-H0TATSNL-T0A 00- NAS0A0 Cower Cowl Light Washer Nutplate Bracket NUT Plate Spring Hercules Drop-In Landing Bracket assembly landing light support Nutplate NOTES Remove installed landing lights and verify that aircraft structure is not subject to substantial corrosion. In case of detected corrosion apply relevant AMM section or consult OEM before continuing with this installation. Remove existing connector and replace as indicated. Verify polarity of wires before connection (ref. to AVE-H0-00-IM). Issue of form 0 Drasov 0, 0 Drasov Page of

25 . Landing / Taxi Light Installation Figure and Part Number Description Issue of form 0 Drasov 0, 0 Drasov Parts Avail. Page of QTY. Per

26 Index Number assy. Option A, 0 0 AVE-H0TATSNL-T0A AN0-0R S- 0 NASDD-FC NASDD-FC NASF0P NASdd-FC 0- NASDD-FC NASF0P NASDD-FC S- 0- AN0-0R 0- S0Z- MS-S AN0-0R S0Z- NASF0P 0- C-0 Hercules Drop-In Landing Nut Plate Spacer Spacer Washer Spacer Baffle assembly refer to -0-00figure 0 Finish Channel Spacer Bracket assembly refer to figure 0 Washer Spacer Nut Plate Bracket Washer Lens assembly Ring alt C-0- AR RF RF AR AR 0 NP Option B 0 AVE-H0TATSNT-T0A AVE-H0TATSNL-T0A AN0-0R S- 0 NASDD-FC NASDD-FC NASF0P NASdd-FC 0- NASDD-FC NASF0P NASDD-FC S- 0- AN0-0R Hercules Drop-In Taxi Hercules Drop-In Landing Nut Plate Spacer Spacer Washer Spacer Baffle assembly refer to -0-00figure 0 Finish Channel Spacer Bracket assembly refer to figure 0 Washer Spacer Nut Plate AR RF RF AR 0 0- S0Z- MS-S AN0-0R Bracket Issue of form 0 Drasov 0, 0 Drasov Page of

27 S0Z- NASF0P 0- C-0 Washer Lens assembly Ring alt C-0- AR 0 NP NOTES It is to be checked by the installer before the modification whether Option A or B is installed on the aircraft. For a change in configuration e.g. landing lights into landing and taxi light requires an additional EASA change. Remove installed landing / taxi lights and verify that aircraft structure is not subject to substantial corrosion. In case of detected corrosion apply relevant AMM section or consult OEM before continuing with this installation. Remove existing connector and replace as indicated. Verify polarity of wires before connection (ref. to AVE-H0-00-IM). Issue of form 0 Drasov 0, 0 Drasov Page of

28 .0 Addition of strobe function For aircraft C0 which are not already equipped with the strobe function this function can be integrated using the following modification instruction. Wiring Diagram Option A Option B Issue of form 0 Drasov 0, 0 Drasov Page of

29 Instrument panel C0 (actual instrument panel to be taken from AMM) Use free location for strobe switch only is not already equipped with the strobe function. Label with STROBE sticker STROBE Issue of form 0 Drasov 0, 0 Drasov Page of

30 FIGURE AND INDEX NUMBER PART NUMBER DESCRIPTION PARTS AVAIL QTY PER ASSY STROBE FUNCTION INSTALLATION CM-0 Breaker LDG Light STROBE Sticker NOTES To install the strobe light function (Cessna 0 only): Install switches (item ) into a free location off the instrument panel according Aircraft Maintenance Manual. The switches are labeled Strobe and Anti-collision. Wiring is to be performed according the wiring diagram. If the strobes are to be synchronized then the blue wires of the position lights and the anti-collision light must be connected. If the lights shall not be synchronized the blue wires of the different lights are to be capped and stowed. The additional wires are to be installed along the wire bundle with the wires for the position and anti-collision lights. Issue of form 0 Drasov 0, 0 Drasov Page 0 of

31 Part Compliance demonstration This document is in relation to the certification program AVE-MOD-00-PFC. The compliance is demonstrated for the following certification specification: Requirements MoC Statement of Compliance CS.0 Protection of structure CS.0 Function and installation CS. Electric cables and equipment MoC 0 MoC 0 MoC 0 (a) All parts installed are verified to be suitable. The installation instruction requests the aircraft structure to be inspected for probable corrosion before installing the new lights. (b) Not applicable (a) All navigation and anti-collision lights are ETSO certified. All landing lights are qualified according to RTCA DO0 as per AVE-H0-00-CCL. (b) Only one optional switch may be installed an label is defined herein. (c) All equipment is installed within their limits. The installation instruction. requests to follow the FAR AC.-B Chapter and in FAR AC. B Chapter Section which implies that only aviation specified wiring is to be used CS. Switches MoC 0 (a) The only switch specified is the OEM type switch used for the same power rating. (b) Switch is next to the control column and evaluated to be accessible by the flight crew. (c) The switch is labelled for the appropriate function. CS. Taxi and landing lights CS. Instructions for Continued Airworthiness MoC 0 MoC 0 (a)the configuration of the original installation is not changed. (b) is not affected as the installation is not changed. (c) is improved as the new lights are brighter than the originally installed. (d) The landing light surface temperature is significantly lowered by this modification. The modification does not require any changes to the aircraft maintenance procedure which is clearly stated in. General. Issue of form 0 Drasov 0, 0 Drasov Page of