ISOMETRIC VIEW

NO SCALE

33

44

55

66

77

88

A B C 

D 

E 

F 

G H 

PARAMETERS:->DIMENSIONS IN INCHES UNLE->LOCATION OF PARTING LINES PINS TOOLING REPAIRS & CHA APPROVED BY SEAMECH.-> SAMPLES FOR APPROVAL MU PRODUCTION CONDITIONS.PLASTIC: BURRS, FLASHING OR 

 PERMISSIBLE WITHIN PRINT TOMETAL: NO CUTTING CHIPS, RUS

 GOUGES OR ANY OTHER ABNO DAMAGE IS ACCEPTABLE. BUR 20% OF MATERIAL THICKNESS BE THICKNESS OF MATERIAL U NOTED.

NEXT

ASSEMBLY

PER PER

NUMBER

REQUIRED

QUANTITY

N/A A/C PART

USED

APPLICATION

ON

DRAWN

CHECK

DESIGN

QARELEASED

S

INTERN

BE

C. BOWENM. HARNESSD. NIXON

3/31/20103/31/2010

M. HARNESS 3/31/2010

3/31/2010

M. GOULD 3/31/2010

THIS DRAWING CONTAINS CONFIDENTIALINFORMATION AND IS THE SOLE PROPERTYOF SEAMECH INTERNATIONAL INC. THIS DRAWING AND ANY INFORMATIONHEREIN, MAY NOT BE COPIED, SHOWN,REPRODUCED OR DISCLOSED TO ANY THIRD PARTY ELECTRONICALLY OR OTHERWISEWITHOUT FIRST OBTAINING THE WRITTEN PERMISSION FROM SEAMECH INTERNATIONAL

2216155 1 1 - DA40

19 1 AN96018 1 11002417 8 AN96016 DELET15 1 AN7-4614 1 37FWS13 4 NAS1212 1 22163411 DELET10 DELET

9 1 2216298 1 9425 7 4 MS3536 4 MS2105 3 AN9604 2 AN7-123 1 AN7-132 1 2216291 1 221628

ITEM QTY 

REVISION 

ZONE REV DESCRIPTION 

 A INITIAL RELEASE, SUPERSEDES PART NUMBE B

ADDED ITEMS 15, 16, 17 AND 18. DELETED ITEM 11 

WITH ITEM 15. ITEMS 5 AND 7 AND 13 CHANGED QU

TO 7 AND ITEM 13 CHANGED QUANTITY FROM 4 TO 

NOTES 8 AND 11.

 C

THE FOLLOWING BOM CHANGES WERE M

ITEM 1: CHANGED P/N FROM 2216293 TO 2ITEM 2: CHANGED P/N FROM 2216295 TO 2

ITEM 3: CHANGED P/N FROM AN6-12A TO AITEM 4: CHANGED P/N FROM AN6-11A TO A

ITEM 5: CHANGED QTY FROM 7 TO QTITEM 7: CHANGED QTY FROM 7 TO QT

ITEM 9: CHANGED P/N FROM 2216361 TO 2

ITEM 12: CHANGED P/N FROM GS14-018-12 T

ITEM 13: CHANGED P/N FROM MS21042-6 TO NAS12

QTY FROM 3 TO QTY 4

ITEM 15: CHANGED P/N FROM 14089 TO A

ITEMS 15 AND 16 DELETED

ITEM 17: CHANGED P/N FROM 31CLNZP-C QTY 1 TO 

 ITEM 18: CHANGED P/N FROM 2216299 QTY 1 TO 1

ITEM 19: ADDED

ADDED NOTE 12, 13 AND CORRESPONDING FLA

CHANGED TORQUE SPEC FROM 9 TO 15-16 

 D

DELETED NOTES 7, 8, 11, 12 AND 13. RENUMBEREADDED NEW ADDITIONAL FLAG NOTES 9 THRU 16

TYPO ON NOTE 7. REPLACED ITEM 19 WITH AN960-

ITEM 12 TO NEW PART NUMBER. DELETED QTY 3 O

ADDED QTY 3 TO ITEM 6.

NOTES UNLESS OTHERWISE SPECIFIED,1. INTENDED TO OPERATE IN AN ENVIRONMENT WITH A TEMPERATURE  RANGE FROM -40 DEG F TO +160 DEG F.2 IDENTIFY PER SEAMECH INTERNATIONAL SPECIFICATION 99, SECTION 36.3. COMPONENT WILL MEET INTENDED FUNCTION AND PERFORMANCE WHEN STORED IN ITS ORIGINAL SHIPPING PACKAGE AND WITHIN TEMPERATURE RANGE OF -20 DEG. F TO +120 DEG. F. 4. INSPECTION METHODS CONDUCTED IN ACCORDANCE WITH DOC. NO. QM12301,  (SII 2001 QA/QC QUALITY ASSURANCE MANUAL). INSPECT ONLY DIMENSIONS SHOWN.  REFERENCED DIMENSIONS AND OUTSIDE PROFILE DOES NOT NEED TO BE SCANNED.5. MOUNTING HARDWARE BAGGED SEPARATELY. SEE BOM FOR REORDER PART NUMBER AND DESCRIPTION.6. PULLEY DRIVE BELT SUPPLIED WITH KIT, SEE BOM FOR REORDER PART NUMBER AND DESCRIPTION.7. BONDING STRAP IS FOR COMPRESSOR CLUTCH FIELD COIL ELECTRICAL GROUND. BONDING CHECK NEEDS TO BE 2.5 MILLIOHMS OR LESS BETWEEN COMPRESSOR  HOUSING AND AIRCRAFT GROUND. VERIFY RESISTANCE AT EACH INTERFACE  IS 2.5 MILLIOHMS OR LESS FOR ADEQUATE ELECTRICAL GROUND RETURN.8 USE 3/8" BREAKER BAR TO AID IN SETTING BELT TENSION.  CAUTION: DO NOT PRY BETWEEN COMPRESSOR HOUSING AND COMPRESSOR MOUNT. INSTALLED BELT TENSION TO BE 50 TO 70 LBS. USE AN APPROVED BELT TENSIONING  GAUGE TO VERIFY BELT TENSION ACCORDING TO LYCOMING SERVICE INSTRUCTIONS. INSTALL BRACKET AND COMPRESSOR USING THE FOLLOWING SEQUENCE: 9 INSTALL ITEM 9 BRACKET TO ENGINE AND TORQUE ITEM 6 NUTS TO 30 FT-LBS. REFERENCE LYCOMING SERVICE TABLE OF LIMITS AND TORQUE VALUE RECOMMENDATIONS, SSP-177610 APPLY A LIGHT FILM OF CLEAR LUBRICATING OIL TO THE SHANK OF ITEM 15 BOLT. DO NOT GET LUBRICATING OIL ON THREADS.11. AFTER ITEM 9 BRACKET HAS BEEN MOUNTED TO THE ENGINE AND THE APPLICABLE MOUTING HARDWARE TORQUED  PER NOTE 9, MOUNT COMPRESSOR TO THE ALUMINUM BRACKET USING HARDWARE AND STEEL BRACKETS AS NOTED.  LOOSELY ASSEMBLE NUTS TO THE APPLICABLE BOLTS.12 CHECK GAP BETWEEN THE FORWARD COMPRESSOR EAR AND THE MAIN ALUMINUM MOUNTING BRACKET WITH FEELER GAUGE.  IF GAP IS GREATER THAN 0.004", SHIM GAP USING ITEM 18 SHIMS AS REQUIRED TO ACHIEVE A FINAL GAP OF LESS THAN 0.004".  INSERT SHIMS AS NEEDED.13 TIGHTEN THE NUTS ON THE THREE SHORT 7/16" BOLTS TO 47 FT-LBS (41 FT-LBS PLUS 6 FT-LBS NUT FRICTION DRAG TORQUE,  REFERENCE AC 43.13-1B). IT IS PERMISSIBLE TO HOLD THE NUT WITH A BACK-UP WRENCH AND TORQUE THE BOLT HEAD. DO NOT  TORQUE THE PIVOT BOLT BEFORE TORQUEING THESE THREE BOLTS.14 SET BELT TENSION PER NOTE 8. TORQUE ITEM 6 NUT TO 20 FT-LBS (16 FT-LBS PLUS 4 FT-LBS NUT FRICTION DRAG TORQUE, REFERENCE AC43.13-1B).15 CHECK GAP BETWEEN ITEM 1 AND THE COMPRESSOR EAR. IF GAP EXISTS, INSTALL ONE ITEM ITEM 19 WASHER IN THE PIVOT BOLT CLAMP GROUP.16 VERIFY SHIMS, IF REQUIRED, ARE CORRECTLY LOCATED AND INSTALLED. TORQUE PIVOT BOLT ITEM 15 TO 47 FT-LBS  (41 FT-LBS PLUS 6 FT-LBS NUT FRICTION DRAG TORQUE, REFERENCE AC43.13-1B). IT IS PERMISSIBLE TO HOLD THE NUT WITH A  BACK-UP WRENCH AND TORQUE THE BOLT HEAD.

4

2

5

6

1

13

13

6

14

8

13

5 7

6

COMPRESSOR SHOWN AS REFERENCE ONLY

9

9 9

2

8

5 7

6

9

WEIGHT NOT

TO EXCEED 5.7 LBS

17

17

13

13

13

7

16 13

12

7

17

17

17

14

D

D

D D

D

D

D

D

D

D

D

D

D

D

D

D

D

D

D

D

15 19 D

18

AS REQUIRED

THIS RING TERMINAL SIZED FOR 7/16" BOLT

D

D