T33652
EFFECTIVITY
CONFIG 2 AT ALL; MD ALL; VM ALL;
799 Page 103IB 406-499
Apr 25/86
34-15-00
OK
NOT OK
OK
TEST TAT EPR LIMIT MODE______________________
(| 0.5`C) (| 0.005)
FULL RTG _____________________________RTG I
*[1] *[2] *[3] *[4] *[1] *[2] *[3] *[4] TOW +10`C ___ 1.505 ___ ___ ___ 1.000 ___ ___ TOD +10`C 1.5051.463 1.5821.6321.5181.505 1.4951.531GA +10`C 1.475 1.439 1.549 1.596 1.488 1.484 1.429 1.455 CON +10`C 1.468 1.431 1.526 1.526 1.405 1.423 1.526 1.526 CLB +10`C 1.468 1.426 1.526 1.526 1.405 1.423 1.441 1.441 CRZ +10`C 1.398 1.391 1.390 1.390 1.373 1.382 1.390 1.390
RTG II
*[1]*[2]*[3] *[4]TOW +10`C ___ 1.000 ___ ___ TOD +10`C 1.458 1.494 1.411 1.436 GA +10`C 1.457 1.463 1.398 1.420 CON +10`C 1.397 1.351 1.526 1.526 CLB +10`C 1.397 1.351 1.422 1.442 CRZ +10`C 1.365 1.308 1.390 1.390
TABLE 101
*[1] MD 501-599 *[2] AT 701-799 *[3] IB 406-410 LESS APLS INCORP SB 34-2266; VM ALL *[4] IB 411-499 PLUS APLS INCORP SB 34-2266
T33662
EFFECTIVITY
CONFIG 2
AT ALL; MD ALL; VM ALL;
799 Page 104
IB 406-499
Apr 25/86
34-15-00
TOTAL AIR TEMPERATURE/N1 LIMIT INDICATING SYSTEM -
__________________________________________________ MAINTENANCE PRACTICES
_____________________
1. General
_______
A. This section covers the removal and installation of the TAT/N1 limit computer, control panel and indicator. Procedures for the computer control panel and indicator are obvious and only safety related steps are given.
2. Referenced Procedures
_____________________
A. 20-11-13, Cam-Lock Lever Latch Fork Adjustment, Type V
B. 24-22-00, Maintenance Practices (Apply Power)
C. 33-11-09, Lighted Pushbutton Switches
3. Removal of TAT/N1 Limit Computer
________________________________
A. Before removing unit, open TAT/N1-COMP and TAT/N1 IND circuit breakers on P7 panel; and N1 TACH 1, 2, 3 and 4 circuit breakers on P6 panel.
4. Removal of TAT/N1 Limit Control Panel
_____________________________________
A. Before removing panel, open the following circuit breakers:
(1)
TAT/N1 - COMP on P7 panel
(2)
SEC PROTECTION on pilots' control stand P8 for control stand panel lights dimmer T144
(3)
IND LTS-PILOTS and SW LTS on P12 panel
B. After removing panel, remove RTG I and RTG II switch caps from panel (Ref 33-11-09). Retain in airplane to install on new panel.
5. Removal of TAT/N1 Limit Indicator
_________________________________
A. Before removing indicator, open the following circuit breakers:
(1)
TAT/N1-COMP and TAT/N1-IND on P7 panel
(2)
SEC PROTECTION on pilots' control stand P8 for center instrument panel lights dimmer T137
6. Installation of TAT/N1 Limit Computer
_____________________________________
A. Before installing unit, ensure that circuit breakers listed in par.
3.A. are open.
B. Install computer (Ref 20-11-13).
CAUTION: IMPROPER ADJUSTMENT OF CAM LOCK LATCH ON EQUIPMENT SHELF
_______ MAY CAUSE CIRCUIT MALFUNCTION OR EQUIPMENT DAMAGE.
C. Close TAT/N1-COMP, TAT/N1-IND, CADC 1 and CADC 1 - SYNC EXCIT circuit breakers on panel P7; and N1 TACH 1, 2, 3 and 4 circuit breakers on panel P6.
D. Press TEST LAMPS switch on computer; three failure lights should come on. Release switch; lights should go out.
E. Remove electrical power if no longer required (Ref 24-22-00).
7. Installation of TAT/N1 Limit Control Panel
__________________________________________
A. Install RTG I and RTG II switch caps (Ref 33-11-09) on panel.
B. Before installing panel, ensure that circuit breakers listed in par. 4.A.(1), (2) and (3) are open.
C. Install control panel and close circuit breakers opened in par. 4.A.(1), (2) and (3).
D. Check that panel lights are on.
E. Remove electrical power if no longer required (Ref 24-22-00).
EFFECTIVITY
LH 011-030,051-070,082-099
AF 121-199; AZ 221-299; AND GN 601-699 AIRPLANES CONFIG 1 WITHOUT PMS 17 Page 201
Sep 25/94
34-15-00
8. Installation of TAT/N1 Limit Indicator
______________________________________
A. Before installing indicator, ensure that circuit breakers listed in par. 5.A.(1) and (2) are open.
B. Install indicator and close circuit breakers opened in 5.A.(1) and (2).
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