AVEO ENGINEERING 300 Beechcraft King Air Instruction Manual
- June 1, 2024
- AVEO ENGINEERING
Table of Contents
AVEO ENGINEERING 300 Beechcraft King Air
Document approval
This document has been established in accordance with an alternative procedure
to DOA approved under EASA AP429.
This installation Instruction is applicable for the Beechcraft models B200,
B200C, B200GT, B200CGT, B300 and B300C.
Amendment Record procedure
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 amendments to this manual will initiate a raise of Issue
ALL raises of issue will be given a sequential Alphabetic Issue Ident
sequentially from 01 to 99 in Table 01 – Issue No: Column– Initial Issue of
Document will be “01”
ALL Issues of this document will be approved by Head of DO
| Issue No. | Details | Date | Effected Pages |
|---|---|---|---|
| 01 | Initial Issue | 15.Dec.2016 | ALL |
02
| Add statement
Add removal of high-voltage unit Correct typo
| | 8
9-10
14
03| Landing and TAXI Light P/N changed| 20. – Mar. –
2018
| 16
04| Precise statement
Add step for corrosion protection
| 5.Apr.2018| 5
8
05| Adding Lights,connectors Replacing Rear Position Light| | 7, 11-14
9-10
Table 01: Document Amendment Record Table
Effected Pages Procedure
ALL pages affected by ANY raise of issue of this manual will be listed in
Table 01 – 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 01 – 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)
Distribution List
As stated in 0.3 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 02
– Distribution List.
Copy holders listed will be issued a copy of this document with sequential
copy number as shown in Table 02 – Distribution List
| Copy No. | Holder |
|---|---|
| MASTER | Aveo Engineering Group, s.r.o. |
Table 02: Distribution List
Installation Instruction
This installation is to be performed in accordance to common practice as
described in FAR AC 43.13-2B Chapter 4 and in FAR AC 43.13 1B Chapter 11
Section 15 (Bonding) as published by FAA.
The installer is responsible to follow the installation instructions in the
latest revision of:
• FAR AC 43.13-2B Chapter 4
• FAR AC 43.13 1B Chapter 11 Section 15
• AVE-WPS-64G-IM
• AVE-POSW-54G-IM
• AVE-PSPSYW-IM
• AVE-RBXP-001-IM
• AVE-N09PANSNT-0HA-IM
• AVE-H30-001-IM
All drawings applicable for this change are listed in the Drawing List:
AVE-MOD-008-DL, issue 01
The following appliances carry an ETSO authorization:
• AVE-WPSR-64G & AVE-WPSG-64G – ETSOA 210.10053936
• AVE-RBXPR-001 – ETSOA 210.10055069
• AVE-POSW-54G – ETSOA.210.10053449
• AVE-PSPSYW-T01 – ETSOA. 210.10068603
The change is to be performed using the document AVE-MOD-008-MCS in the latest
issue.
The aircraft modified according to this instruction may not be released back
to service without the EASA design approval certificate being provided.
Continued Airworthiness
The aircraft manuals remain fully valid. The inspection intervals and the
procedures of the aircraft override the general statements in the component
manuals as listed under §1.1.
For inspection of the new lights themselves follow the procedure of the Aveo
Installation Manuals referenced above.
Description
This modification is the replacement of position lights (type I, II & III),
anti-collision lights, strobe lights, taxi lights and the landing lights by
LED type lights.
In general the lights are direct replacements and do not require any
structural change on the A/C side. Only exemption may be additional attachment
holes and installation of anchor nuts in the secondary bracket of the wingtip
light installation. The changes in wiring are very minor and are to be done
according to referenced standard practice.
Wing Position Lights Installation
Figure and Index
Number
|
Part Number
|
Description
| Parts Avail.| QTY.
Per assy.
---|---|---|---|---
1
|
AVS-P000100175-A6C
|
Ultra NG Adapter M5
|
|
2
2| AVS-93615A216| Screw#6-32 x1/2″ LPSHS| 6
3| AVS-P001290550-A1A| Gasket| 2
4| AVE-WPSR-64G Mod(4)| Ultra Galactica Embedded Red| 1
| AVE-WPSG-64G Mod(4)| Ultra Galactica Embedded Green| 1
5| AVS-OR00480190N70-D0A| O-ring 4,8×1,9, NBR 70| 2
6| AVS-79840905045| Mounting Screw M5 x 45| 2
7| 03-09-1041| 4-Pole Connector – Male| 2
7a| 02-09-2116| Pin| 8
8| 03-09-2041| 4-Pole Connector – Female| 2
8a| 02-09-1117| Socket| 8
| Original parts| |
170| 130-170033-19| Bracket-LH| 1
(175)| 130-170033-35| Bracket-LH| 1
(180)| 130-170033-20| Bracket-RH| 1
(185)| 130-170033-36| Bracket-RH| 1
(200)| 130-170033-23| Bracket-LH| 1
(205)| 130-170033-24| Bracket-RH| 1
220| MS35206-245| Screw| 8
225| NAS1149F0332P| Washer| 8
230| 100-384118-19| Power supply-wingtip| 2
255| 130909B12| Bolt| 8
260| NAS1149F0332P| Washer| 8
265| 101-361163-5| Bracket – wing tip power supply| 2
275| 130909N29| Nut| | 2
---|---|---|---|---
280| MS35338-43| Washer lock| 2
285| NAS1149F0332P| Washer| 2
340| MS35207-263| Screw| 3
| NAS1096-3-8| Screw| 3
350| MS35207-264| Screw| 1
| NAS1096-3-9| Screw| 1
360| MS35338-43| Washer lock| 4
365| NAS1149F0332P| Washer| 4
370| NAS1149D0316H| Washer| 1
375| 130909N29| Nut| 1
380| MS35338-43| Washer lock| 1
385| NAS1149F0332P| Washer| 1
390| MS205832BB12| Jumper assy bonding| 1
415| 130909N29| Nut| 2
420| MS35338-43| Washer lock| 2
425| NAS1149F0332P| Washer| 2
620| 130-381000-1| Light assy – LH, position and strobe| 1
625| 130-381000-2| Light assy – RH, position and strobe| 1
670| A6177| Retainer-Lens| 1
675| NAS388-6-16| Screw| 1
680| MS35336-9| Washer lock| 1
685| A1280-2| Lens – LH red| 1
690| A1280-3| Lens – RH green| 1
700| A7512-24| Lamp – navigation light| 1
705| A1825| Lamp holder assembly| 1
710| A1811| Base – navigation light| 1
715| MS21042L04| Nut| 1
720| NAS1149FN416P| Washer| 4
725| MS35206-216| Screw| 4
740| 131270-3| Stud – Ground| 2
NOTES
1. Remove both position and the strobe lights (View C) in accordance to the aircraft maintenance manual.
2. Disconnect the wire bundle from the position and the strobe light
3. Inspect the installation area for corrosion and correct according to AMM if required
4. Install item 1 to 5 as described. Holes on bracket items 170 to 205 are to be drilled on installation and anchor nuts installed as required. Items 170 to 205 may be trimmed as necessary. After trimming remove sharp edges and apply primer.
5. Apply corrosion protection to all unused holes as per AMM.
6. Wiring for forward position light is to be capped and stowed.
7. Splice the new light’s wires into the bundle according to the referenced installation manuals and the common practice FAR AC 43.13-2B Chapter 4
8. Remove strobe box (View B) according to the aircraft maintenance manual and remove connectors on both sides. Splice the wires in accordance to common practice FAR AC 43.13-2B Chapter 4as follows:
a. 28VDC to ANODE
b. SYNC to TRIGGER
c. GND to CATHODE
Rear Position Light Installation
Kit Number: KNG-02
Figure and Index
Number
|
Part Number
|
Description
| Parts Avail.| QTY.
Per assy.
---|---|---|---|---
1
|
AVE-PSPSYW-T01
|
PosiStrobe Titania
|
|
1
1a| AVS-P000105638-A10| Gasket| 1
2| AVS-92196A152| Screw UNC#6-32 Thread, 7/8″ LSHS| 2
3| AVS-90295A359| Flat Washer – Nylon| 2
4| 03-09-1041| 4-Pole Connector – Male| 1
4a| 02-09-2116| Pin| 4
5| 03-09-2041| 4-Pole Connector – Female| 1
5a| 02-09-1117| Socket| 4
| View A| |
105| MS3456L10SL3S| Connector| 1
120| 207573-1| Housing Pin| 1
135| 101-361159-9| Strap| 1
140| MS35206-245| Screw| 5
190| 100-384118-9
100-384118-21
| Power Supply – Strobe Light| 1
NOTES
1. Remove position light in accordance to the aircraft maintenance manual.
2. Disconnect the wire bundle from the position light
3. Inspect the installation area for corrosion and correct according to AMM if required
4. Splice the new light’s wires into the bundle according to the referenced installation manuals and the common practice FAR AC 43.13-2B Chapter 4
5. Install item 1 to 3 as described.
6. Remove strobe box (View A) according to the aircraft maintenance manual and remove connectors on both sides. Splice the wires in accordance to common practice FAR AC 43.13-2B Chapter 4as follows:
a. 28VDC to ANODE
b. SYNC to TRIGGER
c. GND to CATHODE
Anti-colllision Lights Installation
Figure and Index
Number
|
Part Number
|
Description
| Parts Avail.| QTY.
Per assy.
---|---|---|---|---
A
|
View A
|
BOTTOM ANTI-COLLISION LIGHT
|
|
| | INSTALLATION|
1| AVS-79840905050| Screw M5x50mm| 1
1a| AVS-170299005| Flat Washer – Nylon| 1
1b| AVS-OR05300200N70-D0A| O-Ring| 1
2A| AVE-RBXPR-001| RedBaron XP Galactica Red| 1
2B| AVE-RBXPW-001| RedBaron XP Galactica White| 1
3| | Original Fasteners| 5
4| AVS-P000600093-A60| RedBaron XP Light Replacement Adapter 2| 1
5| 03-09-1031| 3-Pole Connector – Male| 1
5a| 02-09-2116| Pin| 3
6| 03-09-2031| 3-Pole Connector – Female| 1
6a| 02-09-1117| Socket| 3
B| View B| UPPER ANTI-COLLISION LIGHT|
| | INSTALLATION|
1| AVS-79840905050| Screw M5x50mm| 1
1a| AVS-170299005| Flat Washer – Nylon| 1
1b| AVS-OR05300200N70-D0A| O-Ring| 1
2A| AVE-RBXPR-001| RedBaron XP Galactica Red| 1
2B| AVE-RBXPW-001| RedBaron XP Galactica White| 1
3| | Original Fasteners| 5
4| AVS-P000600092-A60| RedBaron XP Light Replacement Adapter 1| 1
5| 03-09-1031| 3-Pole Connector – Male| 1
5a| 02-09-2116| Pin| 3
6| 03-09-2031| 3-Pole Connector – Female| 1
6a| 02-09-1117| Socket| 3
|
Original parts
| |
3| AVS-94023A117| Original Fasteners| 10
NOTES
1. Remove A523 lower flashing beacon in accordance to the aircraft maintenance manual.
2. Disconnect the wire bundle from the flashing beacon
3. Inspect the installation area for corrosion and correct according to AMM if required
4. Splice the new light’s wires into the bundle according to the referenced installation manuals and the common practice FAR AC 43.13-2B Chapter 4
5. Install item A1 to 5 as described in view A. Drill hole to substructure for anti- rotation pin as required.
6. Remove A524 upper flashing beacon in accordance to the aircraft maintenance manual.
7. Disconnect the wire bundle from the flashing beacon
8. Splice the new light’s wires into the bundle according to the referenced installation manuals and the common practice FAR AC 43.13-2B Chapter 4
9. Install item B1 to 5 as described in view B. Drill hole to substructure for anti- rotation pin as required.
Recognition Lights Installation – Wingtip
Figure and Index
Number
|
Part Number
|
Description
| Parts Avail.| QTY.
Per assy.
---|---|---|---|---
1
|
AVE-N09PANSNT-3WAMod(2)
AVS-91400A191 AVS-92146A545 03-09-1031
02-09-2116
03-09-2031
02-09-1117
|
Nubion Taxi
| |
2
2| Screw #8-32 x 5/16” PHPS| 2
3| #8 Self-Retaining Washer| 2
4| 3-Pole Connector – Male| 2
4a| Pin| 6
5| 3-Pole Connector – Female| 2
5a| Socket| 6
NOTES-
1. Remove recognition light in accordance to the aircraft maintenance manual.
2. Disconnect the wire bundle from the recognition light
3. Inspect the installation area for corrosion and correct according to AMM if required
4. Splice the new light’s wires into the bundle according to the referenced installation manuals and the common practice FAR AC 43.13-2B Chapter 4
5. Install item 1 to 3 as described.
Taxi and Landing Lights Installation – Nose Gear
Figure and Index
Number
|
Part Number
|
Description
| Parts Avail.| QTY.
Per assy.
---|---|---|---|---
1
|
AVE-H30-W-112 Mod(1)
|
Hercules LLP Landing
|
|
2
2| AVE-H30-W-111 Mod(1)| Hercules LLP Taxi| 1
| Original parts| |
10| 130909B46| Bolt| 2
15| 130909B44| Bolt| 1
20| NAS1149F0432P| Washer| 4
25| NAS1149F0463P| Washer| 1
30| MS35333-40| Washer| 4
35| NAS43DD4-48| Spacer| 1
40| 130909N32| Nut| 3
60| 90-360010-1| Bracket assy-LH| 1
60| 90-360010-17| Bracket assy-LH| 1
| | For spares order:90-360042-0001|
60| 90-360042-0001| Bracket assy-LH| 1
| | Spares replacement for|
| | 90-360010-17|
65| 90-360010-2| Bracket assy-RH| 1
65| 90-360010-18| Bracket assy-RH| 1
| | For spares order: 90-360042-0002|
65| 90-360042-0002| Bracket assy-RH| 1
| | Spares Replacement for|
| | 90-360010-18|
70| 130909B19| Bolt| 4
75| NAS1149F0332P| Washer| 8
80| 130909N29| Nut| 4
NOTES
1. Remove landing and taxi light in accordance to the aircraft maintenance manual.
2. Disconnect the wire bundle from the landing and taxi lights.
3. Inspect the installation area for corrosion and correct according to AMM if required
4. Install connector item 3 in accordance with referenced installation manual
5. Install item 1 and 2 using the original hardware as described and in accordance to the aircraft maintenance manual.
Compliance demonstration
This document is in relation to the certification program AVE-MOD-007-PFC. The compliance is demonstrated for the following certification specification:
| Requirements | MoC | Statement of Compliance |
|---|---|---|
| CS 23.609 Protection of structure | 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
CS 23.1301 Function and installation| MoC 0| (a) All navigation and anti- collision lights are ETSO certified. All landing lights are qualified according to RTCA DO160 as per AVE-H30-001-CCL.
(b) Only one optional switch may be installed an label is defined herein.
(c) All equipment is installed within their limits.
CS 23.1529
Instructions for Continued Airworthiness
| MoC 0| The modification does not require any changes to the aircraft maintenance procedure which is clearly stated in §1.1 General.