SURFACE
FLAPS
GROUP/LIBRARY
TEST NUMBER
11.08
11.09
11.13
11.14
11.50
11.52
11.53
11.54
11.55
11.56
11.57
11.58
11.60
11.61
11.62
11.30
11.31
11.32
11.33
11.34
11.35
GROUP/LIBRARY
TEST NUMBER
12.08
12.11
12.13
12.50
12.51
12.52
12.53
12.54
12.55
12.56
12.57
12.34
DFCS BITE - Current Status (Test Group and Library Numbers)
Figure 502 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS ú
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500
MAINTENANCE MANUAL
3. MACH TRIM TESTS - GROUP NUMBER 13_________________________________ TEST NUMBER GROUP/LIBRARY
INTERACTIVE
NONE --
SURFACE
MACH TRIM 13.33
4. SPEED TRIM TESTS - GROUP NUMBER 14__________________________________ TEST NUMBER GROUP/LIBRARY
INTERACTIVE
SPEED TRIM 14.36
SURFACE
STAB TRIM 14.32 1
5. ALTITUDE ALERT TESTS - GROUP NUMBER 15______________________________________ TEST NUMBER GROUP/LIBRARY
INTERACTIVE
FMA 15.13
MCP PUSHBUTTON 15.50
MCP F/D SW MCP C/O SW MCP BNK LMT 15.51 15.52 15.53
MCP SPD KNB 15.54
MCP ALT KNB 15.55
MCP V/S KNB MCP DISPLAY 15.56 15.57
INTERLOCK 15.58
ILS DEV WARN 15.60 2
ALT ALERT 15.61
SURFACE
NONE --
DFCS BITE - Current Status (Test Group and Library Numbers)
Figure 502 (Sheet 2)
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A 737-300/400/500MAINTENANCE MANUAL
IF LIBRARY TEST 32 (STABILIZER TRIM) FAILS, PUT THE CODE 100 INTO THE CDU SCRATCHPAD THEN PUSH LSK ADJACENT TO RERUN>. IF SUBTESTS 32.S.5 THRU
32.S.8 FAIL, GO TO THE ELEVATOR RIGGING TEST 51.01 AND SET THE STABILIZER TRIM AT A = +2.88 |0.07 (IGNORE THE UL AND LL LIMITS SHOWN ON THE SCREEN). DO THE LIBRARY TEST 32 AGAIN BUT DO NOT MOVE THE STABILIZER TRIM.
IGNORE THE QUESTION "ARE CPT AND F/O EADI G/S AND LOC SCALES WHITE?" SHOWN ON
THE CDU. PUSH THE LSK ADJACENT TO <YES. IGNORE THE QUESTION "ARE CPT AND F/O EADI G/S AND LOC SCALES YELLOW?" SHOWN ON THE CDU. PUSH THE LSK ADJACENT TO <YES.
3 IF LIBRARY TEST 30 (ELEVATOR) FAILS, PUT THE CODE 100 INTO THE CDU SCRATCHPAD THEN PUSH LSK ADJACENT TO RERUN>. IF THE RESULT OF SUBTESTS 30.S.19/20 AND 30.S.21/22 IS GREATER THAN OR EQUAL TO 1.40, THEN IGNORE THE FAILURE OF THESE SUBTESTS. IF THE RESULT OF THESE SUBTESTS IS LESS THAN 1.40, DO THE RIGGING CHECK OF THE PITCH CWS SENSOR.
4IF LIBRARY TEST 35 (DUAL TEST) FAILS, PUT THE CODE 100 INTO THE CDU SCRATCHPAD THEN PUSH LSK ADJACENT TO RERUN>. IF THE RESULT OF THE SUBTESTS 35.S.18 AND
35.S.38 IS 1.0 PLUS OR MINUS 0.25, THEN IGNORE THE FAILURE OF THEST SUBTESTS.
DFCS BITE - Current Status (Test Group and Library Numbers)
Figure 502 (Sheet 3)
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
E02927
A
737-300/400/500MAINTENANCE MANUAL
WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF ALL
_______ CONTROL SURFACES BEFORE YOU SUPPLY HYDRAULIC POWER. AILERONS, RUDDER, ELEVATORS, FLAPS, SLATS, SPOILERS, LANDING GEAR, AND THRUST REVERSERS CAN MOVE QUICKLY WHEN YOU SUPPLY HYDRAULIC POWER. THIS CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
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