(9)  
30-31-00, Pitot-Static and Temperature Probe Anti-Icing

 (10)
 32-09-02, Ground Safety Relay

 (11)
 33-11-00, Pilots Panel Lights

 (12)
 34-11-00, Pitot-Static System

 (13)
 34-41-00, Inertial Navigation System.

 (14)
 34-55-00, DME System

 (15)
 36-00-00, Pneumatic

 (16)
 36-11-00, Engine Bleed Air Distribution System

 (17)
 71-00-00, Power Plant

 (18)
 73-31-00, Fuel Flow Indicating System

 D. Prepare for Test
 (1)  
Set the altitude selector on the autopilot flight director mode select panel (A/P-F/D MSP) to zero altitude.

 (2)  
On the A/P-F/D MSP, place the AUTOPILOT ENGAGE switch to the OFF position.

 (3)  
Ensure that the TURB/SPEED switch on the A/P-F/D MSP is not
 in the PMS position.

 (4)  
Ensure that the PMS components (control display unit, limit select panel, limit indicator, computer unit, engine interface unit and switching unit) are properly installed.

 (5)  
Provide electrical power. Refer to 24-22-00.

 (6)  
Check for proper operation of pilots' panel illumination, indicator lamps and annunciator lights using master test and dim control. Refer to 33-11-00.

 (7)  
Provide cooling air to electronic equipment. Refer to 21-58-00.

 CAUTION: ENSURE EQUIPMENT COOLING IS OPERATING BEFORE TURN ON OF
_______ ELECTRONIC SYSTEMS, OR DAMAGE TO EQUIPMENT MAY RESULT. EQUIPMENT COOLING SYSTEM MUST BE SET FOR NORMAL COOLING AS DESCRIBED IN 21-58-00.
 (8)  Provide cooling air to INS equipment. Refer to 21-58-00.
 CAUTION: ENSURE THAT COOLING AIR IS AVAILABLE TO INS NAVIGATION
_______ UNITS BEFORE OPERATING INS. FAILURE TO PROVIDE ADEQUATE AIR SUPPLY WILL RESULT IN FAILURE OF INS NAVIGATION UNITS.
 (9)  Ensure that present position latitude and longitude coordinates are entered into each INS (Refer to 34-41). Verify that the mode selector switch, on each INS MSU, is set to ALIGN.
 NOTE: If the INS has been in the NAV mode, cycle the INS through
____ STANDBY back to ALIGN and reload present position.
 EFFECTIVITY

 AIRPLANES WITH PMS    10 Page 517  Apr 25/89

34-62-00
 (10)
 On IB airplanes, ensure that the AUTO/MAN/RMT switch on each INS CDU is set to MAN.

 (11)
 Ensure that the following circuit breakers are closed.

 CIRCUIT BREAKER_______________  LOCATION________
 PMS CDU  P7
 PMS SU ALTN  P7
 PMS SU PRIM  P7
 PMS CMPTR  P7
 PMS LSP  P7
 PMS ADS REF  P7
 PMS LIMIT IND  P7
 CONT POS FLAP OUTBD  P6
 (12) On IB airplanes,

 also ensure that the following circuit breakers are closed.
 CIRCUIT BREAKER_______________  LOCATION
 PMS EPR-1 REF P6 PMS EPR-2 REF P6 PMS EPR-3 REF P6 PMS EPR-4 REF P6
 (13) Enter gross weight of airplane into the PMS as follows:
 (a)  
Press PLNG key on the PMS CDU. Push the CDU slew switch as required to advance the display to PLNG INIT.....2/6 page. Verify that the left part of data line 1 indicates:

 GWT _ _ _ . _

 (b)  
Press the PMS CDU line select 1 key. Verify the key illuminates.

 (c)  
Using the data keys on the PMS CDU, enter gross weight of airplane to nearest hundred pounds (or tenth of a metric ton). Gross weight appears in data line 1 of the CDU display and the CDU INSERT key illuminates.

 NOTE: A gross weight, for example, of 643200 pounds is
____ entered as 6432.
 (d)  Ensure correct gross weight is displayed then press INSERT key. INSERT key and line select 1 key extinguish.
 E. PMS Control Display Unit (CDU) Test
 (1)  
If required prepare for test as described in paragraph D.

 (2)  
Verify that the DIM knob on the CDU is set to approximately half position of its full travel.

 (3)  
Press and hold STS/TEST key on the CDU and verify that the following occurs on the CDU:

 EFFECTIVITY
 AIRPLANES WITH PMS    12 Page 518  Apr 25/89

34-62-00
 (a)  
Four display lines each with 24 rectangles of 5 by 7 dot matrices illuminate.

 (b)  
Line select switches 1, 2 and 3 illuminate white.

 (c)  
Mode annunciators (CLB, CRZ and DES) illuminate white.
　
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