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Aero Safe Corporation,
a Texas Corporation
5300B Airport Road
Mineral Wells Municipal
Mineral Wells, TX 76067
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Installation of electrically driven standby vacuum pump in accordance with Aero
Safe Corporation Drawing List 820500 dated November 15, 1983, or later FAA
approved revision.
rnAaw4a,z4/6,7,4hivz4,The installer must determine whether this design change is compatible with
previously approved modifications. If the holder agrees to permit another
person to use this certificate to alter a product, the holder must give the
other person written evidence of that permission.
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12 /11 / 0 0 Revision 1
,4 irk-eativb o/afe ....-ZeGm:ree;iirmees,"
(Signature)
S. Frances Cox, Manager
Special Certification Office,
Southwest Region
(Title)
Any alteration of this certificate Is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or bothPAA Form 8110-2(10-68)
Page 1 of 2
This certificate may be transferred in accordance with FAR 21.47.
1
29
820218
PLACARD ON-OFF
GRAVOPLY HERMES PLASTICS
-A/R
26
QS100-M1OH
CLAMP, HOSE
1
25
1K14-1O-10-10
TEE
2
24
1H37-1
VALVE, CHECK
1
23
MS535058-22
SWITCH, TOGGLE
AIR
22
MS21104-14
CLAMP, SUPPORT
1
21
MS21104-11
CLAMP, SUPPORT
6
20
MS21042-L3
NUT
19
12
18
AN 960-10
WASHER
A/R
17
AN737TW34
CLAMP, HOSE
6
16
AN 3-6A
BOLT
A/R
15
MIL-H-5593-10
HOSE
MIL. SPEC. MIL-H-5593
A/R
14
307010/307020
FUSE
LITTLE FUSE
1
13
155020
FUSE HOLDER
LITTLE FUSE
12
11
10
-6
1
5
820402-2
PUMP/MOTOR/PLATE
28 VOLT
4
820402-1
PUMP/MOTOR/PLATE
14 VOLT
3
2
1
EQ.# ITEM#
DATE
11-15-83
BY
D.SURSELY
PART NUMBER
CHANGE
PART
NAME
VACUUM SYSTEM
INSTALLATION
AERO SAFE CORPORATION
MATERIAL
SPEC.
DRAWING NUMBER
820501
PAGE:
1
OF
8
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ELECTRICAL SYSTEM SCHEMATIC
DRAWN BY:
D. SURSELY
DATE: 11/15/83
I
SHEET
3 OF 8
VACUUM SYSTEM INSTALLATION
I
I DRAWING NO.
820501
AERO SAYE CORPORATION
TYPICAL
BATTERY
'
•
ee
STARTER
SOLENOID
1
I
#
PRIMARY BUSS.
SI
BATTERY
RELAY
r:4k4
e
MOTO
STAR1
I.
J
EXISTING
ENGINE MOUNT
( REF. ONLY )
EXISTING
VACUUM PUMP
SA'
fre'
•
,
N*81
I
APT
1
EXISTING
TO REGULATOR
DRAWING NO.
820501
4
SHEET
OF 8
DRAWN BY:
D. SURSELY
FIREWALL - TYPICAL - LOOKING AFT
DATE: 11/15/83
VACUUM SYSTEM INSTALLATION
AERO SAFE CORPORATION
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AMP
.1.77 .
(MONS VA13 N0001 INg NO CILLASINI 112.N
NOTE:
UNLESS OTHER WISE INDICATED:
1. DO NOT SCALE THIS DRAWING FOR DIMENSIONS.
2. BREAK ALL SHARP EDGES .003-.015 AND REMOVE ALL BURRS AND SLIVERS.
3. DIMENSIONS ARE IN INCHES AND TOLERANCES AS SHOWN BELOW.
TOLERANCES:
DECIMALS
.XXX +/- .005
.XX +/- .03
.X
+/- .1
ANGLES
+/- 1/2 IN.
4. BOLT, SCREW, RIVET AND SPACER LENGTHS, AND CLAMP SIZES WITH ( ) OR
(XXX) ARE TO BE DETERMINED ON INSTALLATION. MAINTAIN 2D EDGE
DISTANCE AND 3D SPACING.
5. MACHINED SURFACES TO BE 63 PER ANSI B46.1-1962.
6. APPLY TWO COATS OF ZINC CHROMATE PRIMER PER FAA ADVISORY CIRCULAR
AC43.13-1A, CHAPTER 6, PARAGRAPHS 248 AND 250, TO ALL NEW AND
REWORKED METAL SURFACES.
7. INSTALL ALL FASTENERS IN ACCORDANCE WITH STANDARD PRACTICES OF FAA
ADVISORY CIRCULAR AC43.13-1A, CHAPTER 2, PARAGRAPH 99F OF SECTION
3 AND CHAPTER 5, PARAGRAPHS 227B, 227E, 230A(1), 230A(2) AND 231A
OF SECTION 1.
8. BOLT, SCREW AND RIVET HOLE SIZES SHALL BE THE NEXT NUMBERED OR
LETTERED DRILL SIZE LARGER THAN THE FASTENER DIAMETER.
9. DRILLED HOLE TOLERANCES ARE PER AND10387.
10. DRILL HOLES ON INSTALLATION TO MATCH HOLES IN MATING PARTS.
11. ALL WIRE TO BE 12 AWG PER MIL-W-22759/16 OR MIL-W-81044/9. WHEN
SHIELDED, IT MUST BE SHIELDED AND JACKETED PER MIL-C-27500. THE
JACKET MATERIAL MUST MEET THE FLAMMABILITY REQUIREMENTS OF THE
WIRE BEING SHIELDED AND JACKETED. ROUTE WIRE WITH EXISITNG WIRE
BUNDLES WHERE POSSIBLE. ALL WIRING FABRICATION MUST BE
ACCOMPLISHED IN ACCORDANCE WITH FAA ADVISORY CIRCULAR AC43.13-1A,
CHAPTER 11, PARAGRAPHS 445 THRU 452 OF SECTION 2, PARAGRAPHS 482 &
483 OF SECTION 5 AND PARAGRAPHS 514 THRU 519 OF SECTION 7. USE
M535489 GROMMETS, MS21104 CLAMPS, AN743-13 BRACKETS, MS35207
SCREWS (#10), AN3 BOLTS, M521042 NUTS, AN960 WASHERS, AND NAS43DD3
SPACERS AS REQUIRED TO SECURE THE WIRING. DO NOT ATTACH CLAMPS NOR
BRACKETS TO "LIFE LIMITED" PARTS. (CONSULT THE DATA SHEET, MAINTENANCE MANUAL AND FLIGHT MANUAL FOR INFORMATION.) WIRE TERMINALS,
SPLICES AND CAPS MUST MEET THE REQUIREMENTS OF MS25036, MS25181
AND MS25274 RESPECTIVELY.
DATE: 11-15-83
VACUUM SYSTEM INSTALLATION
DRAWN BY
PAGE: 6 OF 8
DRAWING NUMBER
AERO SAFE CORPORATION
D. SURSELY
820501
12. SECURE ITEM 13 FUSEHOLDER TO THE FIREWALL USING ITEM 21 CLAMP.
PICKUP EXISTING AVAILABLE THREADED FASTENER OR USE ITEM 16 BOLT,
ITEM 20 NUT AND ITEM 18 WASHER. CONNECT THE BODY TERMINAL OF THE
FUSEHOLDER TO THE STARTER CONTACTOR WITH A 6.0 MAXIMUM WIRE LENGTH.
13. THE ELECTRIC MOTOR WIRE LEAD SELECTED FOR GROUNDING ( 2RB14
CONNECTOR ATTACHED) MUST CAUSE COUNTERCLOCKWISE ROTATION (AIRBORNE
211CC VACUUM PUMP) OR CLOCKWISE ROTATION (AIRBORNE 212CW/SIGMA TEK
1U128-003 VACUUM PUMP) OR THE ELECTRIC MOTOR SHAFT WHEN LOOKING
TOWARD THE SHAFT END OF THE MOTOR. THE GROUND WIRE MUST BE
ATTACHED DIRECTLY TO THE AIRPLANE OR A JUMPER WIRE USED TO ASSURE
PROPER GOUNDING TO THE AIRPLANE.
14. ELECTRIC SCHEMATIC SHOWN: TYPICAL. FUSED ELECTRICAL TERMINAL
SHOULD BE CONNECTED TO POWER SOURCE NEAREST CONTROL SWITCH.
(PRIMARY BUS, STARTER SOLENOID, ETC.) SELECTION SHOULD ALLOW FOR
CONTINUED ELECTRICAL POWER IN THE EVENT OF LOSS OF GENERATOR.
15. THIS INSTALLATION ADDS AN ELECTRICAL LOAD OF 7.5 AMPS (28 VOLT
SYSTEM) 13.5 AMPS (14 VOLT SYSTEM) TO THE ELECTRICAL SYSTEM. THE
TOTAL CONTINUOUS CONNECTED LOAD SHALL BE LIMITED TO APPROXIMATELY
80 PERCENT OF THE TOTAL RATED GENERATOR/ALTERNATOR OUTPUT CAPACITY.
USE THE PROCEDURE OUTLINED BY AC 43.13 SECTION 2 PARAGRAPHS 424,
425 AND 426 TO ASSURE COMPLIANCE WITH THE 80 PERCENT LIMITATION.
16. INSTALL ITEM 23 SWITCH AND PLACARD ITEM 29 IN AVAILABLE LOCATION
WITHIN ARE SHOWN. PROVIDE .06 CLEARANCE WITH OTHER COMPONENTS.
(MANUFACTURER'S TYPE SWITCH MAY BE USED IN LIEU OF ITEM 23.
LOCATE IN EXISTING SWITCH BANK.)
17. LOCALLY MANUFACTURED LABEL/PLACARD OPTIONAL IN LIEU OF FURNISHED
ITEM 29. SIZE AND COLOR OF CHARACTERS TO BE .12 HIGH, BLACK ON
WHITE (WHITE ON BLACK) OR SIMILAR TO ADJACENT COMPONENT LABELING.
PLACARDS MAY BE MADE FROM GRAVOPLY (WITH PRESSURE SENSITIVE
BACKING)BY HERMES PLASTIC COMPANY OR 3-M COMPANY SCOTCHCAL PROCESS.
FILL ENGRAVED CHARACTERS WITH LUSTERLESS ENAMEL OR LACQUER.
18. INSTALL ALL SWITCHES AND FUSEHOLDERS IN ACCORDANCE WITH THE
MANUFACTURER'S INSTRUCTIONS USING ATTACHING HARDWARE FURNISHED
WITH EACH COMPONENT. APPLY ENAMEL AND LACQUER PAINTS AND FABRICATE
AND APPLY ALL PLACARDS IN ACCORDANCE WITH THE MANUFACTURER'S
INSTRUCTIONS.
19. APPLY TWO COATS OF ZINC CHROMATE PER NOTE 6 ABOVE TO ALL EXPOSED
STEEL AND ALUMINUM SURFACES OF FABRICATED PARTS NOT PREVIOUSLY
CADMIUM PLATED NOR ANODIZED, RESPECTIVELY
20. THE OPTIONAL WING AND TAIL DE-ICER BOOTS WHEN INSTALLED, GETS ITS
VACUUM SOURCE WITHIN THE EXISTING PORTIONS OF THE SCHEMATIC BUT IS
NOT SPECIFICALLY SHOWN IN THIS FIGURE.
CHANGE: A 7-18-86
DATE: 11-15-83
VACUUM SYSTEM INSTALLATION
DRAWN BY
PAGE: 7 OF 8
DRAWING NUMBER
AERO SAFE CORPORATION
D. SURSELY
820501
21. ROUTE AND LOCATE ADDED HOSE TO PREVENT INTERFERENCE AND CHAFING.
USE ITEMS 16, 18, 20 AND 22 AS NEEDED FOR PROPER SEPERATION AND
SECURITY.
22. ITEM 17 MAY BE USED IN PLACE OF ITEM 26.
23. MAINTAIN MINIMUM .50 CLEARANCE BETWEEN ASSEMBLY AND ADJACENT
STRUCTURE.
24. ITEM 25, TEE FITTING SHOWN ROTATED FOR CLARITY.
25. POSITION OF UNIT AND HOSE LENGTHS SHOWN ARE OPTIMUM CONDITION AND
MAY VARY DUE TO MODIFICATIONS AND OPTIONAL EQUIPMENT INSTALLED.
26. THIS SYSTEM CERTIFIED FOR NORMAL CONTINUOUS OPERATION.
CHANGES: A: 7-18-86
DATE: 11-15-83
VACUUM SYSTEM INSTALLATION
DRAWN BY
PAGE: 7A OF 8
DRAWING NUMBER
AERO SAFE CORPORATION
D. SURSELY
820501
REVISIONS
LETTER
DATE
A
DESCRIPTIONS
7-18-86
DELETE "MAX. ALT. 15,0001 " FROM DETAIL A SHEET AND
NOTE 23 SHEET 7A. CORRECT NOTE 13 TO REFLECT
THE USE OF ALTERNATE VACUUM PUMPS: (A) AIRBORNE
MFG. - 212CW AND (B) SIGMA TEK 1U128-003 . . . BOTH
ARE ACCEPTABLE SUBSTITUTIONS FOR THE AIRBORNE MFG.
211CC
REVISION EFFECTIVITY
SHEET
1
2
3
4
LETTER
A
CHANGES: A
DATE:
5
6
7
8
A
A
9 10 11 12 13 14 15 16 17
7A
A
7-18-86
7-18-86
VACUUM SYSTEM INSTALLATION
DRAWN BY
PAGE:
8
OF
DRAWING NUMBER
AERO SAFE CORPORATION
D. E. ALLISON
8
820501
AERO SAFE CORPORATION
P.O. BOX 10206
FT. WORTH, TEXAS 76114
ENGINEERING CHANGE ORDER
DRAWING TITLE:
AUX. INST. AIR INSTALLATION
DRAWING NO:
820501
REASON: ALTERNATIVE CHECKVALVE
ADD NOTE [27] AND FLAG TO ITEM 24 IN PARTS LIST PAGE 1 OF 8.
[27] THE SWEENEY ENGINEERING CORPORATION CHECKVALVE P/N
34-1300-1 IS AN ACCEPTABLE ALTERNATE FOR THE AIRBORNE
1H37-1 CHECKVALUE.
CHANGE:
DATE:
4-19-88
APPROVED BY: D. ALLISON 4-19-88
DRAWN BY
SHEET
1
OF
E.C.N. NUMBER
AERO SAFE CORPORATION
D. ALLISON
1
488-1
AERO SAFE CORPORATION
P.O. BOX 10206
FT. WORTH, TEXAS 76114
DRAWING TITLE:
AUX. INT. AIR INSTALLATION
ENGINEERING CHANGE ORDER
DRAWING NO: 820501
REASON: ALTERNATE TEE FITTING
ADD FLAG NOTE [ X ] AND FLAG TO PART NUMBER 1 K 14 10 10 10 IN PARTS
LIST. ( NOTE [ X] IS NEXT AVAILABLE NOTE NUMBER)
NOTE [ X ] :
[ X ] THE AERO SAFE CORPORATION TEE FITTING P/N A/S 1 K 14 10 10 10
IS AN ACCEPTABLE ALTERNATE FOR THE AIRBORNE P/N 1 K 14 10 10 10
TEE FITTING.
DRAWN BY:
D. ALLISON
DATE:
6/05
1995
APPROVED BY:
D. ALLISON
E.C.N.
695-2A
NO.
SHEET
1 OF 1
AERO SAFE CORPORATION
P.O. BOX 10206
FT. WORTH, TEXAS 76114
DRAWING TITLE:
AUX. INT. AIR INSTALLATION
ENGINEERING CHANGE ORDER
DRAWING NO: 820403
REASON: ALTERNATE 90 DEGREE ELBOW FITTING
ADD FLAG NOTE [ X ] AND FLAG TO PART NUMBER 1 K 1 6 10 IN PARTS
LIST.
NOTE [ X ] IS NEXT AVAILABLE NOTE NUMBER)
NOTE [ X ] :
[ X ] THE AERO SAFE CORPORATION 90 DEGREE ELBOW FITTING P/N
A/S 1 K 1 6 IS AN ACCEPTABLE ALTERNATE FOR THE AIRBORNE 90
DEGREE ELBOW FITTING P/N 1 K 1 6 10
DRAWN BY:
D. ALLISON
DATE:
6/05
1995
APPROVED BY:
D. ALLISON
E.C.N.
NO.
695-2B
SHEET
1 OF 1
AERO SAFE CORPORATION
P.O. BOX 10206
FT. WORTH, TEXAS 76114
DRAWING TITLE:
AUX. INT. AIR INSTALLATION
ENGINEERING CHANGE ORDER
DRAWING NO: 820501
REASON: ALTERNATE TEE FITTING
ADD FLAG NOTE [ X ] AND FLAG TO PART NUMBER 1 K 14 10 10 10 IN PARTS
LIST. ( NOTE [ X] IS NEXT AVAILABLE NOTE NUMBER)
NOTE [ X ] :
[ X ] THE AERO SAFE CORPORATION TEE FITTING P/N A/S 1 K 14 10 10 10
IS AN ACCEPTABLE ALTERNATE FOR THE AIRBORNE P/N 1 K 14 10 10 10
TEE FITTING.
DRAWN BY:
D. ALLISON
DATE:
6/05
1995
APPROVED BY:
D. ALLISON
E.C.N.
695-2A
NO.
SHEET
1 OF 1
AERO SAFE CORPORATION
P.O. BOX 10206
FT. WORTH, TEXAS 76114
DRAWING TITLE:
AUX. INT. AIR INSTALLATION
ENGINEERING CHANGE ORDER
DRAWING NO: 820403
REASON: ALTERNATE 90 DEGREE ELBOW FITTING
ADD FLAG NOTE [ X ] AND FLAG TO PART NUMBER 1 K 1 6 10 IN PARTS
LIST. ( NOTE [ X ] IS NEXT AVAILABLE NOTE NUMBER)
NOTE [ X ] :
[ X ] THE AERO SAFE CORPORATION 90 DEGREE ELBOW FITTING P/N
A/S 1 K 1 6 IS AN ACCEPTABLE ALTERNATE FOR THE AIRBORNE 90
DEGREE ELBOW FITTING P/N 1 K 1 6 10
DRAWN BY:
D. ALLISON
DATE:
6/05
1995
APPROVED BY:
D. ALLISON
E.C.N.
NO.
695-2B
SHEET
1 OF 1
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