A10_-_1C-10(K)A-6WC-2.pdf

TO 1C-10(K)A-6WC-2

ONE SET

USAF KC-10 AIRCRAFT

“A” CHECK INSPECTION WORK CARDS

Prepared by Rockwell Collins

FA8106-09-R-0007

F34601-95-C-0945

SPECIAL RIGHTS LEGEND - This data and/or computer software, furnished under Government Contract No. F33700-78-C-0001, shall be used only for satisfying U.S. Government requirements on U.S. Government-owned DC-10 type aircraft, and shall not be used, released, or disclosed in whole or in part, for any other purpose without the express written permission of the aircraft manufacturer. Such data and/or computer software shall not be used for the manufacture of spare parts. This legend shall have precedence over all other McDonnell Douglas Aerospace Transport Aircraft (division of McDonnell Douglas Corporation) data rights legends contained hereon.

DISTRIBUTION STATEMENT D - Distribution authorized to the Department of Defense and U.S. DoD contractors only, Administrative or Operational Use, 1 July 2003. Other requests shall be referred to AFLCMC/WKDBC, Tinker AFB, OK 73145-3018.

Special Rights Legend, Special Rights Notice, Disclosure Notice and Handling and Destruction Notice are located on page T-2.

PUBLISHED UNDER AUTHORITY OF THE SECRETARY OF THE UNITED STATES

1 JULY 2003

CHANGE 42 - 1 NOVEMBER 2013

T.O. 1C-10(K)A-6WC-2

WARNING - This document contains technical data whose export is restricted by the Arms Export Control Act (Title 22, U.S.C., Sec. 2751 et seq.) or the Export Administration Act of 1979 as amended (Title 50, U.S.C., App. 2401 et seq.). Violations of these export laws are subject to severe criminal penalties. Disseminate in accordance with provisions of DoD Directive 5230.25.

NOTICE - THIS SPECIAL RIGHTS LEGEND IS APPLICABLE TO ALL TECHNICAL DATA EXCEPT THOSE SYSTEMS AND COMPONENTS LISTED INSUPPLEMENTAL AGREEMENT P00075 OF THE U.S. GOVERNMENT CONTRACT F33700-78-C-0001.

DISCLOSURE NOTICE - This information is furnished upon the condition that it will not be released to another nation without the specific authority of the Department of the Air Force of the United States, that it will be used for military purposes only, that individual or corporate rights originating in the information, whether patented or not will be respected, that the recipient will report promptly to the United States, any known or suspected compromise, and that the information will be provided substantially the same degree of security afforded it by the Department of Defense of the United States. Also, regardless of any other markings on the document, it will not be downgraded or declassified without written approval of the originating United States agency.

HANDLING AND DESTRUCTION NOTICE - Comply with distribution statement and destroy by any method that will prevent disclosure of the contents or reconstruction of the document.

PUBLISHED UNDER AUTHORITY OF THE SECRETARY OF THE UNITED STATES

T-2 1 JULY 2003

CHANGE 42 – 1 NOVEMBER 2013

LIST OF EFFECTIVE CARDS

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DATE OF ISSUE FOR ORIGINAL AND CHANGED PAGES ARE:

ORIGINAL ..................... 0 .............................................. 1 JUL 03 CHANGE ...................... 1 .............................................1 MAR 04 CHANGE ...................... 2 ........................................... 15 MAR 04 CHANGE ...................... 3 ..............................................1 JUN 04 CHANGE ...................... 4 ........................................... 15 AUG 04 CHANGE ...................... 5 ............................................. 1 NOV 04 CHANGE ...................... 6 ............................................ 15 JAN 05 CHANGE ...................... 7 .............................................1 MAR 05 CHANGE ...................... 8 ........................................... 15 MAY 05 CHANGE ...................... 9 ........................................... 15 AUG 05 CHANGE ...................... 10 ......................................... 15 OCT 05 CHANGE ...................... 11 ...........................................1 MAR 06 CHANGE ...................... 12 .......................................... 15 JUL 06 CHANGE ...................... 13 ......................................... 15 OCT 06 CHANGE ...................... 14 ......................................... 15 DEC 06 CHANGE ...................... 15 ......................................... 15 MAR 07 CHANGE ...................... 16 ........................................... 1 MAY 07 CHANGE ...................... 17 .......................................... 15 JUL 07 CHANGE ...................... 18 ......................................... 15 AUG 07 CHANGE ...................... 19 ......................................... 15 OCT 07 CHANGE ...................... 20 .......................................... 15 JAN 08 CHANE ......................... 21 ............................................1 FEB 08

CHANGE ...................... 22 .............................................. MAR 08 CHANGE ...................... 23 .......................................... 15 APR 08 CHANGE ...................... 24 ............................................1 DEC 08 CHANGE ...................... 25 ......................................... 15 MAR 09 CHANGE ...................... 26 ............................................ 1 JUN 09 CHANGE ...................... 27 ........................................... 1 AUG 09 CHANGE ...................... 28 ............................................ 1 SEP 09 CHANGE ...................... 29 ............................................ 1 JAN 10 CHANGE ...................... 30 .......................................... 15 FEB 10 CHANGE ...................... 31 ............................................ 1 APR 10 CHANGE ...................... 32 ............................................ 1 JUN 10 CHANGE ...................... 33 ............................................ 1 SEP 10 CHANGE ...................... 34 ............................................1 OCT 10 CHANGE ...................... 35 ............................................ 1 APR 11 CHANGE ...................... 36 ......................................... 15 AUG 11 CHANGE ...................... 37 ......................................... 30 NOV 11 CHANGE ...................... 38 .......................................... 15 JAN 12 CHANGE ...................... 39 .......................................... 15 FEB 12 CHANGE ...................... 40 ........................................... 15 JUL 12 CHANGE ...................... 41 ............................................1 DEC 12 CHANGE ...................... 42 ........................................... 1 NOV 13

TOTAL NUMBER OF CARDS IN THIS PUBLICATION IS 1043 CONSISTING OF THE FOLLOWING.

CARD NO. *CHANGE NO. CARD NO. *CHANGE NO.

TITLE

T-2

A THRU J

INTRO (I-001)

INTRO (I-002)

INTRO (I-003) (1)

INTRO (I-003) (2 THRU 3) ADDED

*Zero in this column indicates an original card.

(ISSUE 5-34) CHANGE 42 A

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CARD NO. *CHANGE NO. CARD NO. *CHANGE NO.

1A GENERAL VISUAL INSPECTION (GVI)

101A-021 (1) 101A-023 (1) 101A-067 (1) 101A-080 (1)

101A-218 (1 THRU 2)

101A-219 (1) 101A-219 (2) 101A-219 (3)

101A-246 (1) DELETED

101A-247 (1) DELETED

101A-248 (1) DELETED

101A-267 (1) 101A-267 (2)

101A-268 (1 THRU 2)

101A-274 (1) DELETED

101A-500 (1) 101A-501 (1) 101A-503 (1) 101A-504 (1) 101A-506 (1)

101A-506 (2) ADDED

101A-507 (1 THRU 2)

101A-508 (1 THRU 2)

101A-509 (1)

101A-509 (2) ADDED

101A-510 (1)

101A-519 (1 THRU 2)

101A-520 (1) 101A-521 (1) 101A-523 (1)

1A DETAILED INSPECTION (DI)

101A-002 (1 THRU 3)

101A-006 (1 THRU 2) DELETED

101A-007 (1 THRU 2)

101A-008 (1 THRU 3)

101A-017 (1 THRU 3)

101A-019 (1) 101A-019 (2)

101A-019 (3 THRU 4)

101A-019 (5)

101A-028 (1 THRU 2)

101A-069 (1 THRU 3)

101A-069 (4) ADDED

101A-081 (1) 101A-108 (1)

101A-111 (1 THRU 4)

101A-112 (1 THRU 3)

101A-112 (4) DELETED

101A-113 (1 THRU 4)

101A-116 (1 THRU 3)

101A-117 (1 THRU 3)

101A-118 (1 THRU 3)

101A-202 (1)

B CHANGE 42

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ILLUSTRATIONS ARE INDICATED BY MINIATURE POINTING HANDS.

CARD NO. *CHANGE NO. CARD NO. *CHANGE NO.

1A DETAILED INSPECTION (DI)

(CONTINUED)

101A-224 (1 THRU 5)

101A-241 (1 THRU 2)

101A-241 (3) 101A-241 (4) 101A-241 (5) 101A-241 (6)

101A-241 (7 THRU 8)

101A-241 (8A) ADDED

101A-241 (9 THRU 13)

101A-242 (1 THRU 2)

101A-242 (3) 101A-242 (4) 101A-242 (5) 101A-242 (6)

101A-242 (7 THRU 8)

101A-242 (8A) ADDED

101A-242 (9)

101A-242 (10 THRU 13)

101A-243 (1 THRU 2)

101A-243 (3) 101A-243 (4) 101A-243 (5) 101A-243 (6)

101A-243 (7 THRU 8)

101A-243 (8A) ADDED

101A-243 (9)

101A-243 (10 THRU 13)

101A-250 (1 THRU 2)

101A-264 (1 THRU 4)

101A-265 (1 THRU 3)

101A-265 (4 THRU 5)

101A-269 (1) ADDED

101A-271 (1)

101A-273 (1 THRU 2) DELETED

101A-275 (1) ADDED

101A-276 (1) ADDED

101A-277 (1) ADDED

101A-278 (1) ADDED

101A-279 (1) ADDED

101A-280 (1) ADDED

101A-281 (1 THRU 3) ADDED

101A-283 (1) ADDED

101A-285 (1)

101A-290 (1 THRU 7) ADDED

101A-511 (1 THRU 2)

101A-511 (3)

101A-511 (4 THRU 5)

101A-511 (6) 101A-511 (7) 101A-512 (1) 101A-512 (2) 101A-512 (3) 101A-512 (4)

CHANGE 42 C

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CARD NO. *CHANGE NO. CARD NO. *CHANGE NO.

1A DETAILED INSPECTION (DI)

(CONTINUED)

101A-512 (5 THRU 7)

101A-513 (1 THRU 2)

101A-513 (3)

101A-513 (4 THRU 5)

101A-513 (6) 101A-513 (7)

101A-518 (1 THRU 2)

101A-522 DELETED

101A-525 (1) ADDED

101A-526 (1) ADDED

101A-527 (1) ADDED

101A-528 (1) ADDED

101A-529 (1 THRU 3)

1A LUBRICATION (LU) AND SERVICING (SV)

101A-003 (1)

101A-009 (1 THRU 9)

101A-022 (1 THRU 2)

101A-058 (1 THRU 3)

101A-073 (1 THRU 7)

101A-074 (1 THRU 3)

101A-075 (1 THRU 3)

101A-076 (1)

101A-076 (2 THRU 6)

101A-076 (6A) ADDED

101A-076 (7)

101A-076 (8 THRU 11)

101A-207 (1)

101A-207 (2 THRU 3)

101A-208 (1)

101A-208 (2 THRU 3)

101A-209 (1)

101A-209 (2 THRU 3)

101A-217 (1 THRU 2)

101A-233 (1 THRU 2)

101A-233 (3)

101A-254 (1 THRU 4)

101A-255 (1) 101A-255 (2)

101A-256 (1 THRU 5)

101A-257 (1 THRU 4)

101A-258 (1 THRU 2)

101A-259 (1 THRU 7)

101A-260 (1 THRU 3)

101A-261 (1 THRU 5)

101A-262 (1)

101A-262 (2 THRU 3)

1A RESTORATION (RS)

101A-047 (1 THRU 9) DELETED

101A-201 (1) DELETED

101A-223 (1 THRU 5)

D CHANGE 42

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ILLUSTRATIONS ARE INDICATED BY MINIATURE POINTING HANDS.

CARD NO. *CHANGE NO. CARD NO. *CHANGE NO.

1A RESTORATION (RS)

(CONTINUED)

101A-225 (1)

101A-225 (2 THRU 5)

101A-240 (1 THRU 7)

101A-245 (1)

101A-245 (2 THRU 9) DELETED

101A-249 (1) 101A-249 (2) 101A-249 (3)

101A-251 (1 THRU 3)

101A-251 (4)

101A-252 (1 THRU 2)

101A-253 (1 THRU 2)

101A-263 (1 THRU 14)

101A-263 (15)

101A-282 (1 THRU 2) ADDED

OPERATIONAL CHECK (OP)

101A-001 (1)

101A-001 (2) DELETED

101A-005 (1)

101A-011 (1 THRU 2)

101A-011 (3) 101A-011 (4)

101A-016 (1 THRU 2)

101A-016 (3)

101A-066 (1 THRU 4)

101A-086 (1)

101A-086 (2)

101A-086 (2A) ADDED

101A-086 (3) 101A-086 (4) 101A-086 (5) 101A-086 (6) 101A-086 (7) 101A-120 (1) 101A-214 (1)

101A-215 (1 THRU 5) DELETED

101A-231 (1 THRU 2)

101A-231 (3 THRU 6)

101A-231 (7)

101A-231 (8 THRU 11)

101A-231 (12) 101A-231 (13-15)

101A-270 (1 THRU 2)

101C-272 DELETED

1A FUNCTIONAL CHECK (FC)

101A-004 (1)

101A-107 (1 THRU 6)

101A-109 (1) DELETED

101A-109 (1 THRU 1)

101A-109 (2 THRU 9) DELETED

101A-110 (1)

101A-110 (2 THRU 3)

101A-110 (4) 101A-110 (5) 101A-012 (1)

CHANGE 42 E

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CARD NO. *CHANGE NO. CARD NO. *CHANGE NO.

1A FUNCTIONAL CHECK (FC)

(CONTINUED)

101A-226 (1 THRU 5)

101A-237 (1 THRU 2)

101A-244 (1) DELETED

101A-284 (1)

101A-284 (2 THRU 3)

101A-284 (4 THRU 5)

101A-284 (6 THRU 8) ADDED

1A DISCARD (DS)

2A GENERAL VISUAL INSPECTION (GVI)

102A-201 (1) 102A-202 (1)

102A-225 (1) DELETED

102A-300 (1 THRU 2) ADDED

102A-302 (1 THRU 2) ADDED

102A-306 (1) ADDED

2A DETAILED INSPECTION (DI)

102A-016 (1) 102A-016 (2)

102A-016 (3 THRU 14)

102A-029 (1 THRU 8)

102A-048 (1 THRU 2)

102A-048 (3) 102A-048 (4) 102A-050 (1) 102A-050 (2)

102A-058 (1 THRU 10) DELETED

102A-075 (1) DELETED

102A-205 (1 THRU 4)

102A-205 (5 THRU 10)

102A-206 (1 THRU 4)

102A-206 (5 THRU 10)

102A-207 (1 THRU 4)

102A-207 (5 THRU 10)

102A-211 (1 THRU 2)

102A-213 (1)

102A-215 (1) DELETED

102A-216 (1) DELETED

102A-218 (1) DELETED

102A-219 (1)

102A-220 (1 THRU 12) DELETED

102A-221 (1 THRU 4)

102A-221 (5) ADDED

102A-222 (1) 102A-223 (1) 102A-223 (2) 102A-223 (3) 102A-301 (1)

102A-301 (2 THRU 4) ADDED

102A-303 (1)

F CHANGE 42

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CARD NO. *CHANGE NO. CARD NO. *CHANGE NO.

2A DETAILED INSPECTION (DI)

(CONTINUED)

102A-303 (2 THRU 6)

102A-303 (7)

102A-303 (8 THRU 17)

102A-311 (1) ADDED

102A-312 (1 THRU 2)

102A-312 (3)

102A-313 (1 THRU 2) ADDED

102A-314 (1 THRU 2) ADDED

102A-315 (1 THRU 2) ADDED

102A-316 (1) ADDED

102A-317 (1) DELETED

2A LUBRICATION (LU) AND SERVICING (SV)

102A-020 (1 THRU 7)

102A-028 (1) DELETED

102A-031 (1 THRU 2)

102A-031 (3) 102A-031 (4) 102A-031 (5)

102A-043 (1) DELETED

102A-052 (1) 102A-052 (2)

102A-052 (3 THRU 5)

102A-052 (6 THRU 22) DELETED

102A-073 (1 THRU 2)

2A RESTORATION (RS)

102A-032 (1)

102A-032 (2) ADDED

102A-047 (1 THRU 6)

102A-047 (7)

102A-047 (8 THRU 9)

102A-060 (1)

102A-200 (1 THRU 8)

2A OPERATIONAL CHECK (OP)

102A-002 (1 THRU 3)

102A-009 (1 THRU 4)

102A-010 (1 THRU 2) DELETED

102A-037 (1 THRU 3)

102A-041 (1 THRU 4) DELETED

102A-042 (1)

102A-043 (1) DELETED

102A-045 (1)

102A-045 (2 THRU 5)

102A-208 (1 THRU 15) DELETED

102A-209 (1 THRU 15) DELETED

102A-212 (1 THRU 4)

102A-217 (1 THRU 4)

102A-308 (1 THRU 2) ADDED

102A-309 (1 THRU 2) ADDED

CHANGE 42 G

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CARD NO. *CHANGE NO. CARD NO. *CHANGE NO.

2A FUNCTIONAL CHECK (FC)

102A-210 (1)

2A DISCARD (DS)

3A GENERAL VISUAL INSPECTION (GVI)

103A-007 (1 THRU 2) ADDED

103A-200 (1 THRU 2) DELETED

103A-201 (1 THRU 2) DELETED

103A-212 (1) 103A-217 (1) 103A-219 (1)

103A-223 (1) ADDED

3A DETAILED INSPECTION (DI)

103A-001 (1 THRU 2)

103A-002 (1) 103A-004 (1)

103A-208 (1 THRU 10)

103A-213 (1 THRU 6)

103A-218 (1 THRU 6)

103A-220 (1 THRU 2)

103A-222 (1 THRU 8)

103A-223 (1) DELETED

103A-224 (1) 103A-224 (2)

103A-224 (2A) ADDED

103A-224 (3 THRU 4) ADDED

103A-224 (5)

103A-224 (6 THRU 7)

103A-224 (8 THRU 12) ADDED

103A-224A (1) ADDED

103A-226 (1 THRU 5)

103A-226 (6 THRU 8)

103A-227 (1 THRU 3)

3A LUBRICATION (LU) AND SERVICING (SV)

103A-009 (1)

3A RESTORATION (RS)

103A-005 (1 THRU 3)

103A-007 (1 THRU 2) DELETED

103A-008 (1 THRU 2)

103A-203 (1 THRU 3)

3A OPERATIONAL CHECK (OP)

103A-207 (1)

103A-010 (1 THRU 2)

103A-228 (1 THRU 53) DELETED

103A-231 (1)

103A-231 (2 THRU 77) DELETED

H CHANGE 42

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ILLUSTRATIONS ARE INDICATED BY MINIATURE POINTING HANDS.

CARD NO. *CHANGE NO. CARD NO. *CHANGE NO.

3A FUNCTIONAL CHECK (FC)

103A-204 (1 THRU 4)

103A-211 (1 THRU 2) DELETED

103A-229 (1)

103A-229 (2) ADDED

4A GENERAL VISUAL INSPECTION (GVI)

104A-034 (1)

4A DETAILED INSPECTION (DI)

4A LUBRICATION (LU) AND SERVICING (SV)

104A-006 (1)

104A-006 (2 THRU 3)

104A-006 (4) 104A-006 (5)

104A-011 (1 THRU 4)

4A RESTORATION (RS)

104A-001 (1 THRU 6)

104A-044 (1)

104A-045 (1) DELETED

4A OPERATIONAL CHECK (OP)

104A-002 (1 THRU 5)

104A-010 (1 THRU 6)

4A FUNCTIONAL CHECK (FC)

104A-039 (1)

4A DISCARD (DS)

CHANGE 42 J

PUBLICATION

CHANGE NO.

CHANGE DATE

NOV 1/13

PAGE NO.

INSP CHK

1A

CARD NO.

101A-251

ATA CHAP

AREA ZONE

INSP DATE

A/C NO.

INSTRUCTION SIGN OFF

BEFORE TCTO 1C-10(K)A-1291 MECH INSP

INS BATTERY RS

CAUTION: ENSURE MODE SELECTOR ON OVERHEAD SWITCH PANEL IS TURNED TO OFF BEFORE

REMOVING/INSTALLING BATTERY UNIT.

1. REMOVE BATTERIES FOR CHECK.

A. OPEN AVIONICS COMPARTMENT ACCESS DOOR 110BB (SEE FIGURE 1).

B. OPEN CIRCUIT BREAKER ON BATTERY UNIT.

C. RELEASE LEVER LATCH SECURING BATTERY UNIT (REF. 34-43-01) TO MOUNTING RACK BY

SQUEEZING TRIGGER PORTION OF HANDLES.

D. PULL LEVER LATCH FORWARD AND DOWN.

E. SLIDE BATTERY UNIT FORWARD UNTIL DISCONNECTED FROM MOUNT CONNECTORS AND

GUIDE PINS.

F. REMOVE BATTERIES AND REPLACE WITH NEW BATTERIES.

2. INSTALL NEW BATTERY UNIT

CHANGE NO.

CHANGE DATE

NOV 1/13

PAGE NO.

INSP CHK

1A

CARD NO.

101A-251

ATA CHAP

AREA ZONE

CAUTION: ENSURE MODE SELECTOR ON OVERHEAD SWITCH PANEL IS TURNED TO OFF BEFORE

REMOVING/INSTALLING BATTERY UNIT.

MECH INSP

A. ENSURE CIRCUIT BREAKER ON BATTERY UNIT (REF. 34-43-01) IS OPEN.

B. CAREFULLY POSITION BATTERY UNIT ONTO MOUNTING RACK AND ENSURE GUIDE PINS ARE

LINED UP.

C. SLIDE BATTERY UNIT (REF. MM 34-34-01) CAREFULLY INTO RACK UNIT UNTIL FRONT LEVER

LATCHES CAN BE ENGAGED.

D. ENGAGE LEVER LATCHES AND TIGHTEN BY LIFTING LEVER HANDLE FORWARD AND UPWARD.

E. CONTINUE LIFTING LEVER HANDLE UNTIL REAR CONNECTORS ARE SECURELY ENGAGED AND

HANDLE IS LATCHED.

F. CLOSE CIRCUIT BREAKER ON BATTERY UNIT.

G. VISUALLY INSPECT MOUNTING RACK AND AREA FOR CLEANLINESS AND GENERAL CONDITION.

H. CLOSE ACCESS DOOR 110BB.

3. TEST BATTERY UNIT.

A. ENERGIZE AIRCRAFT ELECTRICAL BUSES.

CHANGE NO.

CHANGE DATE

NOV 1/13

PAGE NO.

INSP CHK

1A

CARD NO.

101A-251

ATA CHAP

AREA ZONE

B. PLACE MODE SELECTOR ON MODE SELECTOR UNIT (MSU) (REF. 34-43-05) TO STBY. MECH INSP

C. PLACE DISPLAY SELECTOR ON CONTROL/DISPLAY UNIT (CDU) TO POS. OBSERVE DISPLAYS ON

CDU LIGHT TO INDICATE EQUIPMENT IS WORKING. OBSERVE BATT ANNUNCIATOR ON MSU

DOES NOT COME ON.

D. PLACE MODE SELECTOR ON MSU TO OFF AND DE-ENERGIZE ELECTRICAL BUSES.

CAUTION: ENSURE MODE SELECTOR IS TURNED TO OFF BEFORE REMOVING SYSTEM POWER TO

PREVENT BATTERY POWER DEPLETION. ◄

CHANGE NO.

CHANGE DATE

NOV 1/13

PAGE NO.

INSP CHK

1A

CARD NO.

101A-231

ATA CHAP

AREA ZONE

OP MECH INSP

OPERATIONAL CHECK SECTION

1. ATTITUDE MONITOR/SWITCHING UNIT (AM/SU) FUNCTION (REF. MS 34.23.04).

A. PERFORM ATTITUDE SYSTEM SWITCHING FUNCTION AS FOLLOWS:

(1) ENERGIZE AIRCRAFT ELECTRICAL BUSES; ALLOW 5 MINUTES FOR SYSTEM WARMUP.

(2) ON OVERHEAD SWITCH PANEL, SET INS SWITCH TO NORM POSITION.

(3) BEFORE TCTO 1C-10(K)A-1291 ON OVERHEAD SWITCH PANEL, SET INS-1, INS-2 AND INS-3

MODE SELECTORS FROM OFF TO ATT REF POSITION.

CAUTION: IF INS FLOW OFF LIGHT ON OVERHEAD ANNUNCIATOR PANEL COMES ON AND

STAYS ON, OPERATION OF INS SYSTEM MUST BE DISCONTINUED TO AVOID

DAMAGE TO EQUIPMENT FROM OVERHEATING. ◄

(4) AFTER TCTO 1C-10(K)A-1291 ON OVERHEAD SWITCH PANEL, SET ALL IRS-1 MODE

SELECTORS FROM OFF TO ATT POSITION.

NOTE: INS FLOW # OFF INDICATES A MALFUNCTION OF THE COOLING FAN IN THE IRU

COMPARTMENT. THE IRU DOES NOT NEED TO BE SHUTDOWN. MAINTENANCE MAY

BE REQUIRED FOR THE FAN. ◄

CHANGE NO.

CHANGE DATE

NOV 1/13

PAGE NO.

INSP CHK

1A

CARD NO.

101A-231

ATA CHAP

AREA ZONE

(5) ON FRONT PANEL OF AMSU, DEPRESS PUSH TO TEST BUTTON. THE RED LIGHT

(PLACARDED TEST IN PROGRESS) SHOULD COME ON, MOMENTARILY. IF THERE IS A

FAILURE DETECTED IN THE IN-LINE MONITORING, THE MONITOR VALID ANNUNCIATOR

WILL DISPLAY BRIGHT YELLOW. IF THERE IS NO FAILURE THE ANNUNCIATOR WILL

DISPLAY BLACK

NOTE: DO NOT RELY ON THE MONITOR VALID ANNUNCIATOR FAULT INIDCATION FOR

FAILURE OF AM/SU. CONTINUE TEST FOR FURTHER DETERMINATION OF UNIT

FAILURE.

(6) ON OVERHEAD SWITCH PANEL, SET INS SWITCH TO CAPT ON AUX POSITION. ON AMSU,

THE CAPT ANNUNCIATOR SHOULD DISPLAY THE NUMBER 3.

(7) ON OVERHEAD SWITCH PANEL, SET INS SWITCH TO F/O ON AUX POSITION. ON AMSU, THE

F/O ANNUNCIATOR SHOULD DISPLAY THE NUMBER 3.

(8) ON OVERHEAD SWITCH PANEL, SET INS SWITCH TO NORM POSITION. ON AMSU, THE

CAPT, AND F/O ANNUNCIATORS SHOULD DISPLAY BLACK.

(9) BEFORE TCTO 1C-10(K)A-1291 ON OVERHEAD SWITCH PANEL, SET INS-1, INS-2, AND INS-3

MODE SELECTORS TO OFF POSITION.

NOTE: THE INS MODE SELECTORS MUST BE IN OFF POSITION WHEN ELECTRICAL

BUSES ARE DE-ENERGIZED TO AVOID DRAINING BATTERIES.◄

(8) AFTER TCTO 1C-10(K)A-1291 ON OVERHEAD SWITCH PANEL, SET ALL IRS-1, MODE

SELECTORS TO OFF POSITION.

NOTE: THE IRS MODE SELECTORS MUST BE IN OFF POSITION WHEN ELECTRICAL

BUSES ARE DE-ENERGIZED TO AVOID DRAINING BATTERIES.◄

CHANGE NO.

CHANGE DATE

NOV 1/13

PAGE NO.

INSP CHK

1A

CARD NO.

101A-231

ATA CHAP

AREA ZONE

(9) DE-ENERGIZE AIRCRAFT ELECTRICAL BUSES, TEST COMPLETE. MECH INSP

(10) REMOVE EXTERNAL ELECTRICAL POWER FROM BUSES.

(11) ENSURE DC AMP INDICATOR INDICATES BETWEEN 26 AND 29 VDC.

NOTE: IF BATTERY WAS FULLY CHARGED IN STEP 4A(9), ABOUT 2 MINUTES MAY BE

REQUIRED FOR VOLTAGE TO DROP WITHIN RANGE.

(12) PLACE BATTERY SWITCH IN OFF POSITION.

(13) ENSURE DC VOLT INDICATOR INDICATES BETWEEN 26 AND 29 VDC.

5. STALL WARNING SYSTEM OPERATION CHECK (REF. MS 22.33.01).

A. TEST STALL WARNING SYSTEM (REF. MM 22.33.01) USING “BITE” CHECK PROCEDURES AS

FOLLOWS:

NOTE: BEFORE TCTO 1C-10(K)A-1291 PLACE INS MODE SWITCH IN ATT REF, BOTH SYSTEM

NO. 1 AND NO. 2 INS MUST BE IN ATTITUDE REFERENCE FOR PROPER SYSTEM

CHECKOUT. ◄

NOTE: AFTER TCTO 1C-10(K)A-1291 PLACE IRS MODE SWITCH IN ATT, BOTH SYSTEM NO. 1

AND NO. 2 IRS MUST BE IN ATTITUDE FOR PROPER SYSTEM CHECKOUT.◄

(1) THE FOLLOWING CIRCUIT BREAKERS AFFECT THE OPERATION OF STALL WARNING

SYSTEM (REF. MM 22-33-00) AND SHOULD REMAIN CLOSED FOR THE DURATION OF TEST

PROCEDURES UNLESS SPECIFICALLY INSTRUCTED OTHERWISE.

CHANGE NO.

CHANGE DATE

NOV 1/13

PAGE NO.

INSP CHK

1A

CARD NO.

101A-231

ATA CHAP

AREA ZONE

7. COMPUTER, ENHANCED GROUND PROXIMITY WARNING OPERATIONAL CHECK (REF MS 34.45.01).

CHECK ENHNACED GROUND PROXIMITY WARNING AS FOLLOWS:

A. ENSURE THE FOLLOWING CIRCUIT BREAKERS ARE CLOSED:

CIRCUIT BREAKER PANEL LOCATION PANEL AREA

GND PROXIMITY WARN CMPTR AVIONICS AC BUS 1

RADIO ALTIMETER -1 AVIONICS AC BUS 1

RADIO ALTIMETER-2 AVIONICS AC BUS 1

ACCEL-1 AVIONICS AC BUS 1

GND PROXIMITY WARN LT AVIONICS 28 VDC

B. SELF TEST LEVEL 1.

OPERATION DESIRED RESULTS

(1) ENERGIZE AIRCRAFT ELECTRICAL BUSES

AND ALLOW 5 MINUTE WARMUP.

(2) ENSURE FMS IS ON AND OBTAIN GPS

POSITION.

(3) BEFORE TCTO 1C-10(K)A-1291 ALIGNED

INS TO NAV MODE (REF. 34-43-00). ◄

(3) AFTER TCTO 1C-10(K)A-1291 ALIGNED IRS

TO NAV MODE (REF. 34-43-00). ◄

CHANGE NO.

CHANGE DATE

NOV 1/13

PAGE NO.

INSP CHK

2A

CARD NO.

102A-045

ATA CHAP

AREA ZONE

AUTO THROTTLE MAXIMUM AUTHORITY SWITCH MECH INSP

NOTE: GYROS, RADIO ALTIMETER AND FLIGHT DIRECTORS SHOULD BE PREVIOUSLY CHECKED OUT

AND FUNCTIONING PROPERLY.

NOTE: FLAPS MUST REMAIN ABOVE 22 DEGREES.

NOTE: AT CONCLUSION OF FUNCTIONAL CHECK, BITE SHOULD BE USED TO RESET ANY FAULT

INDICATORS.

NOTE: BEFORE TCTO 1C-10(K)A-1291 APPROPRIATE INS(S) REQUIRED TO BE ON AND TIMED-IN FOR

ATS ENGAGEMENT. ◄

NOTE: AFTER TCTO 1C-10(K)A-1291 APPROPRIATE IRS(S) REQUIRED TO BE ON AND TIMED-IN FOR

ATS ENGAGEMENT. ◄

1. TEST AUTO THROTTLE MAXIMUM AUTHORITY SWITCH (REF. MM 22-30-00) AS FOLLOWS:

ACTION LOCATION DESIRED RESULT

A. ENERGIZE 115 VAC AND 28 VDC

BUSSES.

B. ADJUST SPEED CONTROL SELECT

KNOB ON ATS CONTROL PANEL

TO 200 KNOTS.

FGS SPEED BUG IN MACH

AIRSPEED INDICATOR

200 (±4) KNOTS.

C. MOVE THROTTLE LEVERS (3) TO

APPROXIMATELY MID RANGE.

THROTTLE QUADRANT NO TEST.