' SLICK Service Letter - Champion...

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Service Letter TO:

Aircraft Manufacturers, Distributors, Dealers, Engine Overhaul Facilities, Owners and Operators of Champion Aerospace Slick Aircraft Products aircraft magnetos.

SUBJECT:

Airframe Supplemental Type Certificate Installation Instructions for SlickSTART'" magneto booster systems.

BACKGROUND INFORMATION:

Piston aircraft engines typically use impulse coupled or retard breaker systems to augment magneto output during the engine start sequence. While these systems generally provide adequate spark energy, they do not provide optimum starting performance under severe conditions where higher spark energy is needed.

The FAA-PMA approved SlickSTART'" magneto booster system integrates solid state electronics with conventional ignition hardware to deliver optimum spark energy for improved engine starting under all operating conditions. SlickSTART'" delivers up to 340% more spark energy during start than conventional impulse coupled or retard breaker systems. This added energy enables the magnetos to fire partially fouled spark plugs, ignite less than optimum fuel mixtures, improve hot engine restarts, and improve starting performance during extreme cold weather operations.

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SlickSTART'" is designed to replace all BendixlTCM starting vibrators used in conjunction with Champion Aerospace Slick Aircraft Products magnetos. SlickSTART'" is also approved for use with Slick impulse coupled magnetos to enhance engine starting performance. See Table 1.

CAUTION: INSTALLATION OF SlickSTART'" PART NUMBER SS1001 WITH BENDIX/TCM MAGNETOS MAY RESULT IN MAGNETO DAMAGE AND ENGINE STOPPAGE.

CAUTION: ELECTRONIC TACHOMETERS UTILIZING A MAGNETO PICKUP ARE NOT COMPATIBLE WITH SlickSTART"'. THE TACHOMETER SENSOR SHOULD BE RELOCATED TO THE RIGHT HAND MAGNETO.

CAUTION: IT IS THE RESPONSIBILITY OF THE INSTALLERTO DETERMINE THE COMPATABILITY OF OTHER SUPPLIER'S STC PRODUCTS WHEN INSTALLED IN CONJUNCTION WITH STC APPROVED CHAMPION PRODUCTS.

CAUTION: SlickSTART'" MODEL SS1001 IS NOT INTENDEDTO REPLACE EXISTING STARTING VIBRATORS WHICH INCLUDE A RELAY, UNLESS IT IS VERIFIED THE NON-BOOSTED MAGNETO IS GROUNDED WHEN THE IGNITION SWITCH IS IN THE START POSITION.

Table 1

SlickSTART'" PIN Application

SS1001 Must Be Used With Slick 4200,6200,4300,6300 Series Magnetos


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Champion authorizes the installer to use the STC and detailed instructions contained in this document to accomplish the installation of the products described within the STC.

This Service Letter provides step-by-step instructions for converting airframes noted on STC No. SA593CH to the SlickSTART'"' system. The instructions are written to install SlickSTART'"' in aircraft equipped with key or push button type ignition switches which engage the starter motor through a separate, dedicated solenoid. Alternate procedures to use SlickSTART'"' with starter motors engaged by a pull cable must be developed and approved by the installer SlickSTART'"' should receive input power only when the starter motor is engaged.

COMPLIANCE:

As required.

PROOF OF COMPLIANCE:

Appropriate logbook entries.

MODELS AFFECTED:

All Slick impulse coupled, retard breaker, and direct drive 4200/6200 Series and 4300/6300 Series magnetos.

MAINTENANCE PARTS AFFECTED

None.

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REQUIRED SERVICE LITERATURE:

Refer to the following literature for instructions on installation, continued airworthiness, maintenance and overhaul:

. Champion Aerospace Slick Master Service Manual F-ll 00 • L-1492 SlickSTART"" Installation, Operation, Maintenance, and Troubleshooting Manual

CHECK WITH CHAMPION AEROSPACETO BE SURE THAT YOU HAVE THE MOST CURRENT REVISIONS OFTHE APPROPRIATE MANUALS, PERTINENT SERVICE BULLETINS, AND SERVICE LEHERS BEFORE PERFORMING MAINTENANCE.

PARTS REQUIRED PER BULLETIN:

Part number SSl 001 SlickSTART"" is approved for use in all airframes listed in STC No. SA593CH.

SlickSTART"" can be installed with either impulse coupled or retard breaker magnetos and can be used with either 12 volt or 24 volt electrical systems. If SlickSTART"" is installed with retard breaker magnetos, then the existing ignition vibrator must be removed from the airframe and replaced with SlickSTART"".

Each SlickSTART"" Magneto Start Booster includes installation kit part number Kl00l which provides all the electrical hardware needed to complete the installation. Kl00l consists of one 5 ampere fuse, one fuse holder, two crimp splice connectors, six 1/ inch spade terminals, one

4 5/'6 inch ring terminal, one 3/8inch ring terminal, one package of tie wraps, one 6 foot shielded wire bundle (pre-terminated at one end), and one 6 foot red wire.


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TOOLS REQUIRED PER BULLETIN:

Standard shop tools.

WEIGHT CHANGE:

No weight change when SlickSTART"" is replacing starting vibrators. An increase ofapproximately 0.6 lb. for each SlickSTART"" is added to impulse coupled systems.

DETAILED INSTRUCTIONS:

I. Disconnect Aircraft Battery And Ignition Harness

A. Disconnect the negative lead from the aircraft battery.

B. Secure the negative lead away from the negative terminal of the battery to prevent inadvertent contact.

C. To prevent accidental firing of magnetos and possible engine operation, disconnect the ignition harness from the spark plugs.

II. Remove starting vibrator

A. If SlickSTART"" is installed to replace a conventional starting vibrator, disconnect the wires from the vibrator and ignition switch, and deactivate them by capping with an end connector Consult Airframe manufacturers manuals for correct wiring schematics to ensure only the vibrator wiring is deactivated.

B. Unbolt and remove the starting Vibrator. The SlickSTART"" mounting hole diameters and spacing are identical to typical starting vibrators.

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III. Install SlickSTARr'" (Refer to Figure 1.)

WARNING: THE MAGNETO IS "0N'WHEN THE IGNITION SWITCH WIRE (P-LEAD) IS DETACHED FROM THE MAGNETO. NORMAL PRECAUTIONS MUST BE TAKEN TO PREVENT ACCIDENTAL ENGINE IGNITION.

A. Select a suitable location to mount the SlickSTARr'". Be sure the mounting bracket will not interfere with or affect the aircraft structure. Minor rerouting of wiring or relocation ofthe accessories may be required. The SlickSTARr'" and associated wiring should be mounted away from heat sources, clear of the exhaust, engine control linkages, and any other systems critical to the airworthiness ofthe aircraft.

JIMates With 5 in.

.2'8 Dia.

'/4 in. Female JSpade Terminal

0'"\' ~

SlickSTART

I I

DANGER HIGH VOLTAGE

'. ::) \1...----_~>-EJ ~ -r ~ ,'l8in.

'n.in~ 0in.H,.938 ~ 210-1 Figure 1

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B. SlickSTART"" should be mounted vertically with the terminals facing downward. The two mounting holes will accommodate 3/16 inch bolts.

IV. Connect SlickSTART"" according to the following appropriate section. (Refer to Table 2.)

Table 2

If EXisting System Includes ... Go To Paragraph ...

Starting Vibrator Without Relay A BendixlTCM PIN:

10-176487-121 10-176487-122 10-176487-241 10-176487-242

I When Converting from an Impulse Coupled A to a Retard Breaker Magneto Single Impulse Coupled Magneto B

Dual Impulse Coupled Magneto B

Twin Engine Impulse Coupled Magnetos B

CDual Retard Breaker Applications

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A. To replace starting vibrators, which do not include a relay, or when converting from impulse coupled to retard breaker magnetos, when the engine will be started using only the left magneto on single engine applications only (refer to Figure 2):

1. Connect the SlickSTARr" terminal marked "VIN" to the switched positive terminal of the starter solenoid on the starter side, as close to the starter solenoid as possible, or equivalent electrical point. The SlickSTART™ should only receive power when the starter is engaged. Use the unshielded red wire, 5 ampere fuse, fuse holder, crimp splice connectors, appropriate ring terminal and 1/4 inch spade terminals supplied with each SlickSTARr".

/"

SlickSTART

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/1Connect to Ground on Left Magneto.

Connect to Left Magneto Capacitor -D-AN-G-ER-HI-GH-Y-Ol-TA-G-E'1

Terminal Stud. ~ Y G Connect to Positive Switched 1 2 3 I N (Starter) Side of Starter Solenoid.

SF=~~N~D~fJr / Include a 5.0 Amp Inline Fuse as '~o ~ P,rto'W"'"g'"P"'

Connect to Magneto Retard ~ BreakerTerminal.

Figure 2


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2. Connect the terminal marked "GND" to the left magneto ground.

a. Using the shielded wire bundle supplied with each SlickSTART"', connect the pre-crimped ring terminal of the black wire to the ground screw on Slick magneto.

b. After routing the wire bundle to the SlickSTART"', cut and trim to the appropriate length.

c. Using 1/4 inch spade terminals provided, connect the black wire to the SlickSTART™ terminals"GNDf~ The foil shielding and the bare silver wire in the wire bundle should be trimmed back to the cable jacket and left unconnected.

3. Use the red wire in the wire bundle to connect the SlickSTART™ terminal marked "l"to the left magneto capacitor stud terminal (P-lead),leaving the existing "P" lead wire attached.

4.

5.

6.

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Disconnect the "LR" wire at the ignition switch, and cap, or remove.

Disconnect the "BO" wire at the ignition switch, and cap, or remove.

Connect the SlickSTART'" terminal marked "3" to the left magneto retard breaker terminal using locally sourced 18 gauge wire and ring terminal.

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WARNING: DURING STEP 7, ENSURE THAT THE ELECTRICAL POWER SOURCE HAS BEEN REMOVED FROM ·rHE STARTER MOTOR AND INSULATED PRIORTO ENGAGING THE START SWITCH. FAILURE TO DO SO MAY RESULT IN SERIOUS INJURY OR DEATH.

7. Verify that the right magneto is grounded when the start switch is in the start position. Most start switches automatically ground the right magneto P-Iead while starting. If the right magneto is not grounded with the start switch in the start position, verify that the jumper shown in Figure 3 is installed. If your aircraft is not equipped with this type of switch, it may be necessary to replace the existing switch(s) with areM or equivalent combination ignition and starter switch in order to ground the right magneto during start.

VerifyThatThis Jumper Is Installed If Your Aircraft Is Equipped With This

Type Of Switch.

These Diagrams Show The Most Common Switches. Refer To The

Switch Manufacturer's Installation Instructions For Your Switch.

~T ~'1d> s

R

GRD

lQJ LR CO (6?~

o 8 f9PR 80

TCM/Bendix 10-357000 Series ACS/Gerdes

Figure 3

8. Proceed to Section V.

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B. To connect SlickSTART'"" with an impulse coupled magneto when the engine will be started using only one SlickSTART'"" boosted magneto per engine (refer to Figure 4):

NOTE: For dual impulse coupled applications, it is preferred to attach SlickSTART™ to the left magneto. If required for ease of installation or convenience, SlickSTART™ can be attached to the right magneto without any further modification.

NOTE: Twin engine impulse coupling applications require two SlickSTART'"" units; one per engine.

1. Connect the SlickSTART'"" terminal marked "VIN" to the switched positive terminal of the starter solenoid on the starter side, as close to the starter solenoid as possible, or equivalent electrical point. The SlickSTART™ should only receive power when the starter is engaged. Use the red wire,S ampere fuse, fuse holder, crimp splice connectors, appropriate ring terminal and 1/4 inch spade terminals supplied with each SlickSTART'"".

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SlickSTART

1__1

viConnectTo Ground On Left Magneto.

1.....---------..,. DANGER HIGH VOLTAGEconnectTo Left

V G ConnectTo Positive Switched Magneto Capacitor

1 , 3 I N (Starter) Side Of Starter Solenoid. Terminal Stud. I _~JiF=~~N~D~~~ / Include A S.O Amp Inline -- "C.0 ~ Fuse As Part OfWiring Input

Leave Unconnected.

Figure 4

2. Connect the terminal marked "GND"to the boosted magneto ground and the terminal marked "1" to the boosted magneto capacitor stud.

a. Using the shielded wire bundle supplied with each SlickSTAR"P", connect the pre-crimped ring terminal of the black wire to the ground screw on Slick magneto. Connect the pre-crimped ring terminal of the red wire to the capacitor stud terminal, leaving the existing "P" lead wire attached.

b. After routing the wire bundle to the SlickSTAR"P", cut and trim to the appropriate length.


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c. Using 1/4 inch spade terminals provided, connect the black and red wires to the SlickSTART"" terminals "GND" and "1" respectively. The foil shielding and the bare silver wire in the wire bundle should be trimmed back to the cable jacket and left unconnected.

3. Install insulated terminals, without attached wires, on remaining SlickSTART™ terminal "3':

4. For installations where the non-boosted magneto is not impulse-coupled and, therefore, not used for engine starting, verify that the non-boosted magneto is grounded when the start switch is in the start position. Most start switches automatically ground the non-boosted magneto P-Iead while starting. If the non-boosted magneto is not grounded with the start switch in the start position, verify that the jumper shown in Figure 3 is installed. If your aircraft is not equipped with this type of switch, it may be necessary to replace the existing switch(s) with aTeM or equivalent combination ignition and starter switch in order to ground the non-boosted magneto during start.


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C. To replace starting vibrators when the engine will be started using two boosted retard breaker magnetos with two SlickSTARTs™ (refer to Figure 5):

1. Connect the SlickSTARrm terminal marked "VII'J"to the switched positive terminal of the starter solenoid on the starter side, as close to the starter solenoid as possible, or equivalent electrical point. The SlickSTART™ should only receive power when the starter is engaged. Use the red wire, 5 ampere fuse, fuse holder, crimp splice connectors, appropriate ring terminal and 1/4 inch spade terminals supplied with each SlickSTARrm.

Connect To Ground On Magneto Being Boosted

Connect To Magneto CapacitorTerminal Connect To Positive Switched

SlickSTART

1'--__1

'...-O-A-NG-E.-H-,GH-V-OC-TA-GE......1 v G

'" /1Stud Of Magneto I'-....... I N (Starter) Side Of Starter Solenoid. Being Boosted I ~_ ~JiF==iF=lFN=*°trfJ / Include A 5.0 Amp Inline

L..---=:. -' .... ~0 ~ Fuse As Part OfWiring Input

~ ConnectTo Magneto Retard BreakerTerminal Of Magneto Being Boosted.

Figure 5

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2. Connect the terminal marked IGND"to the left magneto ground and the terminal marked "1" to the left magneto capacitor stud.

a. Using the shielded wire bundle supplied with each SlickSTART"', connect the pre-crimped ring terminal of the black wire to the ground screw on Slick magneto. Connect the pre-crimped ring terminal of the red wire to the capacitor stud terminal (P-Iead), leaVing the existing "P" lead wire attached.

b. After routing the wire bundle to the SlickSTART"', cut and trim to the appropriate length.

3. Disconnect the "LR" wire at the ignition switch, and tape or cap.

4. Disconnect the "BO" wire at the ignition switch, and tape or cap.

5. Connect the SlickSTART'" terminal marked "3" to the magneto retard breaker terminal of the magneto being boosted. The existing wire can be used if serviceable and a new 1/4 inch spade terminal is installed.


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V. Reconnect the Ignition HarnessTo the Spark Plugs.

VI. Check SlickSTART'"'" Installation.

A. Inspect all wiring connections for proper termination.

B. Check all wiring for proper routing away from heat generating sources, mechanical stresses and abrasion.

C. Check for removal of all installation tools.

VII. Reconnect Aircraft Battery.

A. Confirm that the aircraft ignition and master switches are in the off position.

B. Reconnect the negative lead of the aircraft electrical system to the negative battery terminal.

DOCUMENTATION:

Make all appropriate logbook entries. SlickSTART'"'" is approved by STC.


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Q!lnit.rh §tnt.rz nf Am.rrirn

1Hrp-artmrnt of CITranzp-ortation- -lJi'rllrral Aviation Allminiztration

§upp12m2utal crryp2 QJ2rtifirat2 f'~ 5A593CH

~t:el&~ ~.0 Champion Aerospace LLC 1230 Old Norris Road Liberty, 5C 29657

ud~c/t'kt' t'~ "k~" en t'~ ~ ~~n.4~ t'~~t!ZU'??z;?'/!~"t' 'wet'£'t',,{; d'mit'at'ePn and""na'!:t'ePno t'k,~ ao Ff/d,,{;za,n nuet3 t'k aiUO';~e4:J",,?uizenu=t3 t}/!9fat' *,yt',,{; * ~udt&>no,

&~ma/g~ --~ ~~ ~~l,' * * See Attached FAA Approved Model List (AML) No.

~~. * 5A593CH for list of approved engine models and

Jtd!,f.' * applicable airworthiness regulations

Install Champion 5IickSTART'" magneto booster system in accordance with Slick Installation Instructions as listed on AML No. 5A593CH or later FAA Approved revision.

1. Compatibility of this design change with previously approved modifications must be determined by the installer. 2. A copy of this Certificate and FAA Approved Model List (AML) No. 5A593CH, or later FAA approved revision, must be

maintained as part of the permanent records for the modified aircraft. 3. 51ickSTART'" Model 551001 may only be used with Slick 4200,6200,4300,6300 series magnetos. 4. 51ickSTART'" Model 551002 may only be used with TCM/Bendix 5-20, 5-200, 5-1200 series magnetos.


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5. Do not install 5IickSTART'" Model 551001 with Teledyne Continental Motors/Bendix 5-20, 5-200, and 5-1200 series magnetos.

6. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

§.u:,~~..

§.u:,~~ce ..

December 18, 1995

January 24, 1997

§.u:, ~ February 10,2009

§.u:, ~ May 2,1997; March 9,1998, April 20, 2000; March 12, 2004

~d~,y;k~dJaah~

Signed originalon file at Champion

~n~J Thaddeus D. Krolicki, Jr. Manager, Propulsion Branch Chicago Aircraft Certification Office

tI1iis certijUate may 6e tratuje"ea in accoraance witli '1'}f.~21.47

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FAA APPROVED MODEL LIST (AML) NO. SAS93CH CHAMPION AEROSPACE LLC

FOR INSTALLING SlickSTART'" MAGNETO BOOSTER SYSTEM

Date of Issuance January 24, 1997

AIRCRAFTLINE AIRCRAFT MAK< MODEL

1 AD Aerospace Inc. T-11,T-211

AERMACCHIS.p.A. 5.205-1 B/F, S.20S-l8/R, S.20S-20/F, S.20S-20/R, S.205-22/R, 5.208, S.208A

3

2

AERMACCHIS.p.A. F.260, F.260B, F.26OC, F.260D

Aero Resources J-2 (McCUlloch)

5

4

Aeracar Inc. I

Aerodifusion,S.L. Jodel 0-11905 6

Aeromere 5.A. Falco F.8.L7

AMT-l00, AMT-2008 Aeromot

Aeronautica Macchi AL 60, AL 60-B S.PA

10

9

6S-TC (Army L-3J), 6S-TAC (Army L-3E),

YO-58 (Army L-3) 11

Aeronca

Aeronca 6S-CA(L-3F),S-6S-CA

Aerostar Aircraft12 360,400

Aerostar Aircraft PA-60-6oo (Aerostar 600), PA-60-601 (Aerostar 601),

PA-60-601 P(Aerostar 601 P), PA-60-602P (Aerostar 602P), PA-60-700P (Aerostar 700P)

14

13

Air & Space America 18A

A, A-2, A-3, A-4, A-5, A-ST, A-6, A-7, 15 Aircraft Parts & A-7T, A-9, A-9BDevelopment

ORIGINAL TYPE

CERTIFICATION BASIS

INSTALLATION INSTRUalONS 'AFM

SUPP NO/OATF

AML AMEND

OATF CERTIFICATE

N"MR

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FAA APPROVED MODEL LIST (AMLl NO. SA593CH CHAMPION AEROSPACE LLC

FOR INSTALLING SlickSTART"" MAGNETO BOOSTER SYSTEM

Date of Issuance January 24. 1997

AIRCRAFT MA

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LINE AIRCRAFT AIRCRAFT MAKE MODEL

31 Anderson, 14 Greenwood

32 Anderson, Sl,SlA Greenwood

33 S-lA INTERSTATE

34

STOL Aviation LLC

STOL Aviation LLC S-lB2 INTERSTATE

3S 21S0, 21 SOA, 2180 VARGA

36

Augustair Inc.

D-140-BAvionJodel

lS0Avions Jodel 37

DR-l0S038 Avions Jodel

D-l19039 AVionJodel

CAP lOBAPEX Aircraft40

APEX Aircraft R216041

R3OO0/16042 APEX Aircraft

HoneyBee (HB)Beecraft Associates43

47, 47B, 47B3, 47D, 47Dl, 47E, 47G,Bell Helicopter44 47G-2,47H-l

4S Textron

47G-3, 47G-2A, 47G-38, 47G-3B-l,Bell Helicopter 47G-2A-1, 47G-4, 47G-4A, 47G-S,

47G-3B-2, 47G-SA, 47G-3B-2A 46

Textron

47J, 47K, 47J-2,47J-2ABell Helicopter Textron

ORIGINAL TYPE

CERTIFICATION BASIS

INSfALLATION INSTRUCTIONS "AFM

SUPP NOJDATE

AML AMEND

DATE CERTIFICATE

NUMBER FOR

ALTERATION NUMBER "REV.

NOJDATE 4Al CAR 3 SL2-96 Rev.D

1/01/00 N/A 3/12/04

A11SW FAR 23 SL2-96 Rev.D 1/01/00

N/A 3/12/04

A-737 CAR 4 SL2-96 Rev.D 1/01/00

N/A 3/12/04

A-7S4 CAR4a SL2-96 Rev.D 1/01/00

N/A 3/12/04

4A19 CAR 3 SL2-96 Rev.D 1/01/00

N/A 3/12/04

A31N CARlO SL2-96 Rev.D 1/01/00

N/A 3/12/04

A141N CARlO SL2-96 Rev.D 1/01/00

N/A 3/12/04

MIN CARlO SL2-96 Rev.D 1/01/00

N/A 3/12/04

AlOIN CAR 10 SL2-96 Rev.D 1/01/00

N/A 3/12/04

A36EU FAR 21.29 SL2-96 Rev.D 1/01/00

N/A 3/12/04

M8EU FAR 23 SL2-96 Rev.D 1/01/00

N/A 3/12/04

A66EU FAR 23,36 SL2-96 Rev.D 1/01/00

N/A 3/12/04

4All CAR 3 SL2-96 Rev.D 1/01/00

N/A 3/12/04

H-l CAR 6 SL2-96 Rev.D 1/01/00

N/A 3/12/04

2H3 CAR 6 SL2-96 Rev.D 1/01/00

N/A 3/12/04

2H1 CAR 6 SL2-96 Rev.D 1/01/00

N/A 3/12/04


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47 Seastar Corp.

4B DaimlerChrysler Aerospace AG

49 Brantly International

50 Brantly International

51 British Aerospace Scottish Division

52 B-N Group Ltd

53 B-N Group Ltd

54 C.ltoh

55 Cessna Aircraft

56 Cessna Aircraft

57 Cessna Aircraft

58 Cessna Aircraft

59 Cessna Aircraft

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AIRCRAFT MODE

TsC-1A,T5C-1A1, T5C-1A2

BolkowJr.

B-2, B-2A, B-2B

305

Beagle B.206 Series 1 &2

BN-2A MK.lII, BN-2A MK.l1I2, BN-2AMKJII3

BN-2, BN-2A, BN-2A 2, BN-2A 3, BN-2A 6, BN-2A 8, BN-2A 9, BN-2A 20,

BN-2A 21, BN-2A 26, BN-2A 27, BN-2B 20, BN-2B 21, BN-2B 26,

BN-2B 27, BN-2T, BN-2T-4R N-62

120,140

140A

150, 150A, 150B, 15OC, 150D, 150E, 150F, 150G, 150H, 15QJ, 150K, A150K, 150L,A150L,150M,A150M,152,A152

170, 170A, 170B

172, 172A 172B, 172C, 172D, 172E, 172F (T-41 A), 172G, 172H (1041 A),

1721, 172K, 172L,172M, 172N, 172P, 1720. 172R, 1725

ORIGINAL TYPE

CERTIFICATION BASIS

INSTALLATION INSTRUCTIONS ·AFM

SUPP NOJDATE

AML AMEND

DATE CERTIFICATE

NUMB"R FOR

ALTERATION NUMO"R • REV.

NOJDATE AlSEA FAR 23 5L2-96 Rev.D

1/01/00 N/A 3/12104

A1EU CARlO 5L2-96 Rev.D 1/01/00

N/A 3/12/04

2H2 CAR 6 5L2-96 Rev.D 1/01/00

N/A 3112/04

H35W CAR 6 5L2-96 Rev.D 1/01/00

N/A 3112/04

A11EU CAR 3 5L2-96 Rev.D 1/01/00

NlA 3112/04

A29EU FAR 21.29, 23 5L2-96 Rev.D 1/01/00

N/A 3/12/04

A17EU FAR 21.29, 23 5L2-96 Rev.D 1/01/00

N/A 3112/04

A3PC CAR 10 5L2-96 Rev.D 1/01/00

N/A 3112/04

A-768 CAR4a 5L2-96 Rev.D 1/01/00

N/A 3112/04

5A2 CAR 3 (CAR 4a) 5L2-96 Rev.D 1/01/00

N/A 3/12/04

3A19 CAR 3 5L2-96 Rev.D 1/01/00

N/A 3112/04

A-799 CAR3 5L2-96 Rev.D 1/01/00

N/A 3/12/04

3A12 CAR3 5L2-96 Rev.D 1/01/00

N/A 3/12/04

CHAMPION AEROSPACE LLC 1230 Old Norris Road

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SL2-96 "


PAGE NO. REVISION

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AIRCRAFT MAKE

LINE AIRCRAFT MnDFI

60 172RG, Pl72D, Rl72E (T-41B, T-41C, T-41 D), Rl72F, Rl72G, Rl72H, R172J,

Rl72K, 175, 17SA. 17sB, 17SC 61

Cessna Aircraft

Cessna Aircraft 177, 177A, 177B

Cessna Aircraft 177RG62

Cessna Aircraft 180, 180A, 180B, 18OC, 180D, 180E, 180F, 18OG, 180H, 180J, 180K

64

63

Cessna Aircraft 182, 182A, 182B, 182C, 182D, 182E, 182F, 182G, 182H, 182J, 1821

/' ......SL2-96


FOR INSTALLING SlickSTART"' MAGNETO BOOSTER SYSTEM


LINE AIRCRAFT MAK.

71 Cessna Aircraft

Cessna Aircraft72

Cessna Aircraft73

74 Cessna Aircraft

75 Great Lake Aircraft

76 Cirrus Design Corp

77 CPAC, Inc.

Commonwealth Aircraft

78

79 Composite Aircraft Corp

80 Diamond Aircraft

Diamond Aircraft81

Domier-Werke G.M.b.H.82

83 Domler-Werke G.M.b.H.

84 Dynac Aerospace Aero Commander

ORIGINAL CERTIFICATION INSTALLATION

AIRCRAFT TYPE

CERTIFICATE BASIS FOR

INSTRUCTIONS *AFM SUPP

AML AMEND* REV.

Mon., NUM··R A T.RATlnN I NUMBER NOJDATE NOJDATE DATE 310, 310A, 310B, 31OC, 3100, 310E, 3Al0 CAR3 SL2-96 Rev. 0 N/A 3112104

310F, 31OG, 310H, Bl0H, 3101,31OJ, 1/01/00 310J-1, E310J, 310K, 310L, 310N, 310P,

3100. T310Q310R,T310R 320A, B, C, 0, E, F, 320-1, 335, 340,

340A 3A25 CAR 3 SL2-95 Rev. 0

1/01/00 N/A 3/12/04

337, 337A(02B), 337B, 337C, 3370, A6CE FAR 23 SL2-95 Rev. 0 N/A 3112/04 337E, 337F, 337G, 337H, M337B (02A), 1/01/00 P337H, T337B, T337C, T337D, T337E,

T337F, T337G, T337H, T337H-SP "'01,401 A, 401 B, 402, 402A, 402B, 402C A7CE CAR3,FAR23 SL2-96 Rev. 0 N/A 3112104 411, 411A,414, 414A,421,421A, 421B, 1/01/00

421C 2T-1A, 2T-1A-l, 2T-1A-2 A18EA AB-7A, FAR 23 SL2-96 Rev. 0

1/01/00 N/A 3/12104

SR20,SR22 AOOOO9CH FAR 23,36 SL2-96 Rev. 0 1/01/00

N/A 3/12/04

112,112B,114B,114TC A12S0 FAR 23, 36 SL2-96 Rev. 0 1/01/00

N/A 3112/04

175, 180, 185 A-729 CAR4a SL2-95 Rev. 0 1/01/00

N/A 3/12/04

AC-7 A7SW FAR 23 SL2-95 Rev. 0 1/01/00

N/A 3112/04

DA2o-A1, DA2o-C 1 TMCH FAR 21.29, 23, 36,JAR-VLA

SL2-96 Rev. 0 1/01/00

N/A 3112/04

DA-40 M7CE 14 CFR 21, 23, 36,JAR23

SL2-95 Rev. 0 1/01/00

N/A 3/12/04

Do 27 Q-jj A81N CARlO SL2-96 Rev. 0 1/01/00

N/A 3/12/04

D028A-1,D028 B-1 7A13 CARlO SL-2-95 Rev. 0 1/01/00

N/A 3/12/04

(Volaire) 10, lOA (Aero Commander) 100, l00A, 100-180

1A21 Car 3 SL2-96 Rev. 0 1/01/00

N/A 3/12104


DAY YEAR YEARMO MO DAY Liberty, South Carolina, U.S.A. 29657 24 of 34 Ge 2009 Champion Aerospace

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LINE AIRCRAFT MAKE

BS Edward Scott Kearns

Elzie Wright, Jr.B6 Falcon Enstrom HelicopterB7 Corp.

88 Micco Aircraft Co.

King's Engineering89 Fellowship (TKEF)

90 Extra

FFT-GmbH91

92 FFA

Found Aircraft Development

94

93

Found Brothers

Frontier-Aerospace95 Fletcher

96 Fuji Heavy Industries

97 GENERAL AVIA

GENERAL AVIA98

Gippsland99 Aeronautics Goodyear A 100

AIRCRAFT Mnn

F SL2-96 '\




LINE AIRCRAFT AIRCRAFT MAKE MODEL

101 Goodyear Aircraft GA-22A

2T-1A,2T-1A 1,2T-1A2102 Great Lake Aircraft

103 GROBG 109, Luft-und Raumfahrt Burkhart GROB

GROBG 109B Gmbh

104 GllS, G1 lSA,GllSB,GllSC,GllSC2, G1 lSD, G11SD2,Gl 1SEG

GROB-WERKE

lOS Gulfstream 111 Aerospace Corp.

106 Helio Aircraft Corp. lSA,20 (Taylorcraft)

107 H-391 (YL-24), H-391 B, H-39S (L-2BA or Ul0B), H-39SA

lOB

Helio Aircraft Corp.

UH-12,UH-12AHiller Aviation

Hiller Aviation UH-12B, UH-12C109

UH-12DHiller Aviation110

UH-12E, UH-12E-LHiller Aircraft 111

UH-12L, UH-12L4Hiller Aviation 112

11 OO(OH-SA), FH-11 00 Manufacturing Corp

114

FH-11oo113

LC40-SS0FG, LC42-SS0FGCessna Aircraft

TZ-123OO0, GZ-19A, GZ-19, GZ-20, GZ-20A

116

Lockheed Martin11S

11A Aerospace Inc. Quartz Mountain

ORIGINAL TYPE

CERTIFICATION BASIS

INSTALLATION INSTRUCTIONS "AFM

SUPP NO/DATE

AML AMEND

DATE CERTIFICATE

NUMBER FOR

ALTFRATION NIJMRER "'REV.

NO/DATE lA12 CAR3 SL2-96 Rev.D

1/01/00 N/A 3/12/04

AlBEA Aero Bul.7A (FAR 23)

SL2-96 Rev.D 1/01100

N/A 3/12/04

G43EU FAR 21.23, 21.29, 21.50

SL2-96 Rev.D 1/01/00

N/A 3/12/04

AS7EU FAR 21.23, 21.29 SL2-96 Rev.D 1/01/00

N/A 3/12/04

A11S0 FAR 23, 21 SL2-96 Rev.D 1/01/00

N/A 3/12104

3A3 CAR4a SL2-96 Rev.D 1/01/00

N/A 3/12/04

lAB CAR3 SL2-96 Rev.D 1/01/00

N/A 3/12/04

6Hl CAR6 SL2-96 Rev.D 1/01/00

N/A 3/12/04

6H2 CAR6 SL2-96 Rev.D 1/01/00

N/A 3/12/04

4H10 CAR6 SL2-96 Rev.D 1/01100

N/A 3/12/04

4H11 CAR6 SL2-96 Rev.D 1/01/00

N/A 3/12104

H1WE CAR6 SL2-96 Rev.D 1/01/00

N/A 3/12/04

H2WE CAR6 SL2-96 Rev.D 1/01/00

N/A 3/12/04

Aoo003SE FAR 23,36 SL2-96 Rev.D 1/01/00

N/A 3/12/04

T.C.l Navy Approval 1935

SL2-96 Rev.D 1/01/00

N/A 3/12/04

A-B04 CAR 3 SL2-96 Rev.D 1/01/00

N/A 3/12/04


YEARMO DAY YEAR MO DAY Liberty, South Carolina, U.S.A. 29657 26 of 34 G02009 Champion Aerospace

\.. 2410 31 0996 09

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CHAMPION AEROSPACE LLC FOR INSTALLING SlickSTART'" MAGNETO BOOSTER SYSTEM


LINE AIRCRAFT AIRCRAFT MAKE MOOFI

117 The Don Luscombe 8, 8A, 8B, 8C, 8D, 8E, 8F, T-8F Aviation History Foundation Inc. Mael Aircraft BA-42118

Maule Aerospace Bee Dee M-4, M-4, M-4C, M-4S, M-4T, M-4-18OC, M-4-180S, M-4-180T, M-4-210, M-4-210C, M-4-21 OS, M-4-210T, M-4-220, M-4-220C,

M-4-220S, M-4-220T, M-5-18OC, M-5-200, M-5-210C, M-5-210TC,

M-5-220C, M-5-235C, M-li-180, M-li-235 M-7-235, MX-7-235, MX-7-180,

MX-7-420, MXT-71S0, MT-7-235, M-8-235, MX-7-160, MXT-7-160,

MX-7-180A, MXT-7-180A, MX-7-180B, M-7-235B, M-7-235A, M-7-235C, MX-7-18OC, M-7-260, MT-7-260,

M-7-260C, M-7-420AC, MX-7-16OC, MX-7-180AC, M-7-420A

120

119

BO-209-150 FV & RV Aerospace AG DaimlerChrysler

BO-209 160 FV & RV BO-209-150 FF

121 Thomas H. McClish (Funk) B, B75L(UC-92), BS5C

G-21C, G-21D Seaplanes LLC

123

Atlantic Coast122

90AL-115MonocQupe Corp.

M20, M20A, M20B, M2OC, M20D, Company

124 Mooney Airplane M20E, M20F, M2OG, M20J, M20K,

M20L,M20M

ORIGINAL TYPE

CERTIFICATION BASIS

INSTALLATION INSTRUCTIONS 'AFM

SUPP NO/DATE

AML AMEND

DATF CERTIFICATE

NUMBER FOR

ALTERATION NUMBER 'REV.

NOJDATF A-li94 CAR4a SL2-96 Rev.D N/A 3/12104

1/01/00

A6S0 FAR21, FAR23 SL2-96 Rev.D N/A 3/12104 1/01/00

3A23 CAR 3 SL2-96 Rev.D N/A 3/12104 1/01/00

A27EU FAR 21.29, 23 SL2-96 Rev.D N/A 3/12104 1/01/00

A-715 CAR4a SL2-96 Rev.D N/A 3/12104 1/1/00

4A24 CAR3 SL2-96 Rev.D N/A 3/12104 1/01/00

A-306 Aeronautics SL2-96 Rev.D N/A 3/12/04 Bulletin 7-A 1/01/00

CAR4a 2A3 CAR3 5L2-96 Rev.D N/A 3/12/04

1/01/00


YEAR MO DAY YEARMO DAY Liberty, South Carolina, U.S.A. 29657 27 of 34 Ge 2009 Champion Aerospace

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CHAMPION AEROSPACE LLC FOR INSTALLING SlickSTARr'" MAGNETO BOOSTER SYSTEM


LINE AIRCRAFT MAK<

AIRCRAFT MODEL

125 Mooney Mite Aircraft M-18C Corp.

126 Moravan ZLIN S26L

Moravan a.s.127 Z-242L

128 Morrisey Aviation 2000C

FN-333129 NARDIS.A.

Navion (L-17A), Navion A (L-17B, Inc. (Navion)

130 Sierra Hotel Aero, L-17C), Navion B, Navion D, Navion E,

Navion F, Navion G, Navion H EADS-PZL PZL-Koliber lS0A 131 "Warszawa~Okecie"

P68, P68B, P68C, P68 ·Observer 2·

133

132 Vulcanair S.p.A.

Piper Aircraft Inc. HC-40, J3C-SO, J3C-SOS, HC-65, J3C-6SS, PA-ll, PA-llS

134 Piper Aircraft Inc. J4, J4A, J4A-S

JSA (L-4F), J5A-80, JS8 (L-4G), J5C, AE-l,HE-l

136

FS 2001 Corp.135

L-14FS 2000 Corp.

PA-12,PA-12S137 FS 2003 Corp.

PA-14138 FS 2002 Corp.

PA-15139 Piper Aircraft Inc.

PA-16,PA-16SPiper Aircraft Inc.140

ORIGINAL TYPE

CERTIFICATION BASIS

INSTALLATION INSTRUCTIONS 'AFM

SUPP NOJDATF

AML AMEND

DATF CERTIFICATE

N MR

/" '\SL2-96




LINE AIRCRAFT AIRCRAFT MAKE MOOFI

141 Piper Aircraft Inc. PA-17

142 Piper Aircraft Inc. PA·18, PA·18s, PA·18 "105", PA·18 "125" (L·21 A),

PA·18AS "125", PA·18s"12s", PA·18 "135" (L-21 B),

PA·18A "135", PA·l8As "13S~ PA·18s "135", PA-18 "150",

PA·18A "ls0",PA·18As "lS0~ PA 185 "150", PA·19(L·18C), PA-19s

143 Piper Aircraft Inc. PA-18A (Restricted), PA·18A "135" (Restricted), PA-18A "1 SO" (Restricted)

144 Piper Aircraft Inc. PA·20, PA-20s, PA-20 "11 5", PA-20s "115", PA·20 "135",

PA-20s "135" 145 PA'22, PA·22·1 08, PA·22·13S,

PA·22s·13s, PA·22·1 SO, PA-22s-1 SO, PA·22·160, PA·22s·160

146

Piper Aircraft Inc.

PA-23, PA·23·160, PA·23·23s, PA·23·2s0, PA·E23-2s0

147

Piper Aircraft Inc.

Piper Aircraft Inc. PA-24, PA·24·2s0, PA·24·260, PA·24-400

148 PA-2s, PA·2s·23s, PA·2S·260 (Normal Category)

149

LAVIAs.A.

PA·2s, PA-2S-23S, PA·2s·260 (Restricted Category)

150

LAViA SA

PA·28·140, PA-28-1S0, PA·28-ls1, PA·28·160, PA·28·161, PA-28-180,

PA·28-23S, PA-28s-160, PA·28R·180, PA·28s·180, PA·28·181, PA-28R·200,

PA-28R-201, PA·28R·20lT, PA-28RT-201, PA·28RT·20lT,

PA·28·20lT

Piper Aircraft Inc.

ORIGINAL TYPE

CERTIFICATION BASIS


SUPP NOtOATF

AML AMEND

OATF CERTIFICATE

NUMBER FOR

ALTERATION NUMRFR • REV.

NOtOATF A-80s CAR 3 sL2·96 Rev.D

1/01/00 N/A 3/12/04

lA2 CAR 3 sL2·96 Rev.D 1/01/00

N/A 3/12/04

AR-7 CAR8.10b sL2·96 Rev.D 1/01/00

N/A 3/12/04

lA4 CAR 3 sL2·96 Rev.D 1/01/00

N/A 3/12/04

lA6 CAR 3 sL2-96 Rev.D 1/01/00

N/A 3/12/04

lAl0 CAR 3 sL2-96 Rev.D 1/01/00

N/A 3/12/04

lAls CAR 3 sL2-96 Rev.D 1/01/00

N/A 3/12/04

2A8 CAR 3 sL2·96 Rev.D 1/01/00

N/A 3/12/04

2Al0 CAR8.10b sL2·96 Rev.D 1/01/00

N/A 3/12/04

2A13 CAR 3 sL2·96 Rev.D 1/01/00

N/A 3/12/04

REVISIONISSUED

YEAR MO

96 09

REVISED CHAMPION AEROSPACE LLC 1230 Old Norris Road

Liberty, South Carolina, U.S.A. 29657

" 2009 Champion Aerospace


YEAR

09

PAGE NO"

DAYMO DAY

29 of 34 G10 31 24 ~\...

/

\.



AIRCRAFT MODCI

PA-30, PA-39, PA-40

PA-31, PA-31-3oo, PA-31-3S0, PA-31-32S

PA-31P, PA-3lT, PA-3lTl, PA-3lT2, PA-3lT3, PA-31 P-3S0

PA-32-260, PA-32-300, PA-32S-3oo, PA-32R-301(HP), PA-32-301,

PA-32-30lT PA-34-200, PA-34-200T,

PA-34-220T PA-36-2BS, PA-36-3oo, PA-36-37S

(Normal Category) PA 36-2BS, PA-36-300, PA-36-37S

(Restricted Category) PA-38-112

PA-44-180, PA-44-180T

PA-46-310P, PA-46-3S0P

Pirtle (Johnson) Rocket 18S

200, 2ooA, 200B, 20OC, 200D, 400

CP-6S

19A, B19, M19A, 23, A23, A23A, A23 19, A23 24,823, C23, A24, A24R,

824R,C24R 3S, A3S, 83S, OS, D3S, E3S, F3S, G3S,

3SR

SL2-96 '"


ORIGINAL TYPE

CERTIFICATION BASIS

INSTALLATION INSTRUCTIONS *AFM

SUPP NO DATE

AML AMEND

DATC CERTIFICATE

NUMRCR FOR

AITCRATION NUMRCR "'REV.

NO JnATc A1EA CAR 3, FAR 23 SL2-96 Rev.D

1/01/00 N/A 3/12/04

A20S0 FAR 23 SL2-96 Rev.D 1/01/00

N/A 3/12/04

ABEA FAR 23 SL2-96 Rev.D 1/01/00

N/A 3112/04

A3S0 CAR 3 SL2-96 Rev.D 1/01100

N/A 3/12/04

A7S0 FAR 23 SL2-96 Rev.D 1/01/00

N/A 3/12/04

A9S0 FAR 23 SL2-96 Rev.D 1/01/00

N/A 3112/04

AlOS0 FAR 23 SL2-96 Rev.D 1/01100

N/A 3/12/04

A18S0 FAR 23 SL2-96 Rev.D 1/01/00

N/A 3/12/04

A19S0 FAR 23 SL2-96 Rev.D 1/01/00

N/A 3112/04

A2SS0 FAR 23 SL2-96 Rev.D 1/01/00

N/A 3112/04

n6 CAR4a SL2-96 Rev.D 1/01/00

N/A 3112/04

3A18 CAR 3 SL2-96 Rev.D 1/01/00

N/A 3/12/04

A-nO CAR4a SL2-96 Rev.D 1/01/00

N/A 3/12/04

A1CE CAR3 SL2-96 Rev.D 1/01/00

N/A 3/12/04

A-777 CAR 3 SL2-96 Rev.D 1/01/00

N/A 3112/04

MO

LINE

lSl

lS2

lS3

lS4

lSS

lS6

lS7

lS8

lS9

160

161

162

163

164

16S

AIRCRAFT MAKE

Piper Aircraft Inc.

Piper Aircraft Inc.

Piper Aircraft Inc.

Piper Aircraft Inc.

Piper Aircraft Inc.

Piper Aircraft Inc.

Piper Aircraft Inc.

Piper Aircraft Inc.

Piper Aircraft Inc.

Piper Aircraft Inc.

Pirtle, J.e.

Interceptor Aircraft

Joe Rankin

Hawker Beechcraft

Hawker 8eechcraft

ISSUED

DAY

31

REVISED CHAMPION AEROSPACE LLC 1230 Old Norris Road

YEAR MO DAY YEAR Liberty, South Carolina, U.S.A. 29657 96 09 24 09 e 2009 Champion Aerospace


PAGE NO. REVISION

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AIRCRAFT MODEL

166 5-33, 35-A33, 3S-B33, 35-C33, 35-C33A E33, E33A, E33C, F33, F33A, F33C, G33, H35, J35, K35, M3S, N3S, P35, 535, V35,

V35A, V35B, 36, A36, A36TC, B36TC 167

Hawker Beechcraft

45(YT-34j, A45(T-34A, B-45), D4S(T-34B)

168

Hawker Beechcraft

Hawker Beechcraft 50, B50, C50, D50, D50A, D50B, D50C, D50E, D50E-5990,

ESO, FSO, G50, H50, J50 169 58P, 58PA, S8TC, S8TCAHawker Beechcraft

Hawker Beechcraft 60,A60, B60170

65,6S-80,6S-88,65-A80, 65-ABO-88oo, 65-B8O

172

171 Hawker Beechcraft

Hawker Beechcraft 76

95, B95, B95A, D95A, E95, 95 55, -ASS, -B55, -B55A, -BS5B (T-42Aj, -CS5, -C5SA, D55, D55A, E55, E55A, 56TC, 58,

58A 174

Hawker Beechcraft 173

77Hawker Beechcraft

F172D, F172E, Fl72F, Fl72G, Fl72H, F172K, Fl72L, Fl72M, Fl72N, Fl72P

176

Cessna Aircraft175

F15OG, F150H, F150J, F150K, FA150K, F150L, FA150L, FRA150L, Fl 50M,

FRA150M, F152, FA152 177

Cessna Aircraft

FRl72E, FRl72F, FRl 72G, FRl 72H, FR172J, FRl72K

178

Cessna Aircraft

Cessna Aircraft F182p, F182Q FR182

Cessna Aircraft F177RG179

ORIGINAL TYPE

CERTIFICATION BASIS


SUPP NOJDATE

AML AMEND

DATE CERTIFICATE

NUMBER FOR

ALTERATION NUMBER "REV.

NO.lDATE 3A1S CAR 3 SL2-96 Rev.D

1/01/00 N/A 3/12/04

5A3 CAR3 SL2-96 Rev.D 1/01/00

N/A 3/12/04

5A4 CAR3 SL2-96 Rev.D 1/01/00

N/A 3/12/04

A23CE FAR 23 SL2-96 Rev.D 1/01/00

N/A 3/12/04

A12CE FAR 23 SL2-96 Rev.D 1/01/00

N/A 3/12/04

3A20 CAR 3 SL2-96 Rev.D 1/01/00

N/A 3/12/04

A29CE FAR 23 5L2-96 Rev.D 1/01/00

N/A 3'12/04

3A16 CAR 3 5L2-96 Rev.D 1/01/00

N/A 3/12/04

A30CE FAR 23 SL2-96 Rev.D 1/01/00

N/A 3/12/04

A4EU CARlO 5L2-96 Rev.D 1/01/00

N/A 3/12/04

A13EU CAR 3 SL2-96 Rev.D 1/01/00

N/A 3/12/04

A18EU FAR21.29 CAR 3

SL2-96 Rev.D 1/01/00

N/A 3/12/04

A42EU CAR 3 5L2-96 Rev.D 1/01/00

N/A 3/12/04

A26EU FAR 23 5L2-96 Rev.D 1/01/00

N/A 3/12/04


YEARYEAR MO DAYMO DAY liberty, South Carolina, U.s.A. 29657 31 of 34 Ge 2009 Champion Aerospace

\. 24 0910 31 96 09

./www.chamnionaerosoace.com

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AIRCRAFT MAKF

LINE AIRCRAFT MODFL

lBO Revo, Inc. Colonial C-1, Colonial C-2 Lake LA-4, Lake LA-4A, Lake LA-4P,

Lake LA-4-200, Lake Model 250 181 R22, R22 ALPHA, R22 BETA,

R22MARINER 182

Robinson

Robinson R44,R44 II

Ruschmeyer R9O-230RG Luftfahrttechnik GmbH

184

lB3

Ryson Aviation Corp ST-100

ST-100Ryson Aviation Corp1BS

Texas Bullet 205Richard P.Schutze186

269A, 269A-1, 269B, 269C, 269C-l, 269D,

188

187 Schweizer Aircraft

RC-3Sky Enterprises Inc.

Sky Internationallne. 5-15, S-lT, 5-2, S-2A, 5-25, S-2B, S-2C189

A-l,A-1A,A-1B190 Sky Internationallne.

T67M260, T67M260-T3A Ltd.

192

191 Slingsby Aviation

MD3-160SME Aero Inc.

TB9, TB 200 AEROSPATIALE

194

SOCATA-Groupe193

MS 892E-1 SO, Rallye 23SC, AEROSPATIALE SOCATA-Groupe

MS893E, Rallye 23SE

ORIGINAL TYPE

CERTIFICATION BASIS


SUPP NOInATE

AML AMEND

DATF CERTIFICATE

NUMBER FOR

AITFRATION NLJMRFR "REV.

No/nATF lAB CAR 3

FAR 23,36 SL2-96 Rev.D

1/01/00 N/A 3/12/04

Hl0WE 14 CFR 27 SL2-96 Rev.D 1/01/00

N/A 3/12/04

HllNM 14CFR 27,36 SL2-96 Rev.D 1/01/00

N/A 3/12/04

A77EU 14CFR21,23,36 SL2-96 Rev.D 1/01/00

N/A 3/12/04

G1NM AC21.231 SL2-96 Rev.D 1/01/00

N/A 3/12/04

A7NM FAR 23, 36 SL2-96 Rev.D 1/01/00

N/A 3/12/04

4A2 CAR 3 SL2-96 Rev.D 1/01/00

N/A 3/12/04

4H12 CAR6 SL2-96 Rev.D 1/01/00

N/A 3/12/04

A-769 CAR3 SL2-96 Rev,D 1/01/00

N/A 3/12/04

A8SO FAR 23,36 SL2-96 Rev.D 1/01/00

N/A 3/12/04

A22NM FAR 23 SL2-96 Rev.D 1/01/00

N/A 3/12/04

A73EU FAR 21.29, 23 SL2-96 Rev.D 1/01/00

N/A 3/12/04

A6SEU Part 23 SL2-96 Rev.D 1/01/00

N/A 3/12/04

AS1EU FAR 21.29 SL2-96 Rev.D 1/01/00

N/A 3/12/04

7A14 CAR 10, 3 SL2-96 Rev.D 1/01/00

N/A 3/12/04

CHAMPION AEROSPACE LLC PAGE NO. REVISIONISSUED REVISED 1230 Old Norris Road

DAY YEAR MO DAY YEARMO Liberty, South Carolina, U.s.A. 29657 32 of 34 Ge 2009 Champion Aerospace

\.. 09 24 0910 31 96

./www.chamoionaerosoace.com

/ SL2-96

'\




LINE AIRCRAFT MAK"

AIRCRAFT MODE

195 HW-75,10 Consolidated Vuitee Stinson Division,

Aircraft Corp 196 5tits Aircraft Inc. 5A-9A

(Twin-Bee) UC-l197 5TOL Aircraft Corp.

Sud-Aviation Gardan GY.80 150, GY.80-160 GY.80-180

199

198

Superior Aircraft LCA,LFA

200 Superior Aircraft V,V-2

Swift Museum GC-1A,GC-1B201 Foundation Taylorcraft 2000, 19, F19, F21, F21A, F21 B, F22, F22A, LLC

202 F22B, F22C

203 Taylorcraft 2000, BC, BC5, BC-65, BC12-65, BC512-65, BC12-D, BC512-D, BC12-D 1, BC512-01,

BC12D-85, BC512D-85, BC12D-4-B5, BC512D-4-85

204 T-35 (TE-18)William E. Quinn

44205 King's Engineering Fellowship (TKEF)

206 PL-12fT-300Transfield Ply Ltd.

500, 500-A, 500-B, 5ao-U, 500-5, 520, Aircraft Corp.

207 Twin Commander 560, 560A, 560E

208 560-F,680FL(P) Aircraft Corp.

209

Twin Commander

Twin Commander 700 Aircraft Corp.

ORIGINAL TYPE

CERTIFICATION BASIS

INSTALLATION IN5TRUalON5 'AFM

5UPP Ntl InAT"

AML AMEND

"AT< CERTIFICATE

NUMR"R FOR

A J"RATIClN N MR"R • REV.

NCllnAT" A-709 CAR4a 5L2-96 Rev.D

1/01/00 N/A 3/12/04

4A31 CAR 3 5L2-96 Rev.D 1/01/00

N/A 3112/04

MEA CAR 3 5L2-96 Rev.D 1/01/00

N/A 3/12/04

A12IN CARlO 5L2-96 Rev.D 1/01/00

N/A 3/12/04

A-730 CAR4a 5L2-96 Rev.D 1/01/00

N/A 3112/04

A-778 CAR 3 5L2-96 Rev. D 1/01/00

N/A 3/12/04

A-766 CAR4a 5L2-96 Rev.D 1/01/00

N/A 3/12/04

lA9 CAR 3 5L2-96 Rev. D 1/01/00

N/A 3/12/04

A-696 CAR 4 5L2-96 Rev.D 1/01/00

N/A 3112/04

AR20 CAR 8.30 5L2-96 Rev.D 1/01/00

N/A 3112/04

A2Wi FAR 23 FAR 36

5L2-96 Rev.D 1/01/00

N/A 3112/04

Al7NM FAR 23 5L2-96 Rev.D 1/01/00

N/A 3112/04

6Al CAR 3 5L2-96 Rev.D 1/01/00

N/A 3/12/04

2M CAR 3 5L2-96 Rev.D 1/01/00

N/A 3/12/04

A125W FAR 23, 25 5L2-96 Rev.D 1/01/00

N/A 3112/04


DAY YEARMO DAY YEAR MO liberty, South Carolina, U.s.A. 29657 33 of 34 Ge 2009 Champion Aerospace 24 0910 31 96 09

\.. www.chamoionaerosoace.com ./

AIRCRAFT MAKf'

Univair Aircraft Corp

Univair Aircraft Corp

Univalr Aircraft Corp

Emerald Enterprises LTD. WSK PZL Mielec and OBR SK Mielec Zenair Ltd.

/"

LINE

210

211

212

213

214

215

• Or later FAA approved revision

CHAMPION AEROSPACE LLC

96 09 09

REVISIONPAGE NO.REVISEDISSUED 1230 Old Norris Road

MO DAY YEAR MO DAY YEAR Liberty, South Carolina, U.S.A. 29657 ~ 2009 Champion Aerospace 34 of 34 G2410 31

www.championaerospace.com ..)\..

SL2-96 "' FAA APPROVED MODEL LIST (AML) NO. SA593CH

CHAMPION AEROSPACE LLC FOR INSTALLING SlickSTARTTM MAGNETO BOOSTER SYSTEM

Dale of Issuance January 24, 1997

AIRCRAFT Mnnf'1

108,108-1,-2,-3

(ERCDl 41 SoC, (ERCDl 415-CD

A 2,A2-A,G, E,415D F-1,F-1A,M10

Model 0-1

PZLM2003

CH2000

ORIGINAL TYPE

CERTIFICATION BASIS


SUPP NO.lDATE

AML AMEND

DATE CERTIFICATE

NIIMRf'R FOR

AI Tf'RATlnN NIIMBf'R • REV.

Nn.lnATE A-767 CAR3 SL2-96 Rev. 0

1/01/00 N/A 3112104

A-718 CAR4a SL2-96 Rev. 0 1/01/00

N/A 3112/04

A-787 CAR 3 SL2-96 Rev. 0 1/01/00

N/A 3112/04

A9WE CAR 3, FAR 23 SL2-96 Rev. 0 1/01/00

N/A 3112/04

A68EU FAR 23,36 SL2-96 Rev. 0 1/01/00

N/A 3/12/04

TASCH FAR21.29,23 SL2-96 Rev. 0 1/01/00

N/A 3/12/04

FAA Approved: Signed original on file at Champion Aerospace LLC Thaddeus D. Krolicki, Jr. Manager, Propulsion Branch Chicago Aircraft Certification Office

Date Reissued: February 10, 2009 Date Amended: May 12, 1997, March 9,1998, April 20, 2000

March 12, 2004

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