KING AIR 200 ANNUNCIATOR PANELS
MASTER MASTER WARNING CAUTION
PRESS TO RESET PRESS TO RESET MASTER MASTER CAUTION WARNING
* OPTIONAL EQUIPMENT BB-453 AND AFTER PRIOR TO BB-453 PRESS TO RESET PRESS TO RESET GND COMM WARNING ANNUNCIATOR PANEL—200 AIRCRAFT PWR
AUX DRIVE ALT R ENG FIRE ALERT PUSH TO EXT D OK
0 M ALT
L ENG FIRE INVERTER DOOR UNLOCKED ALT WARN R ENG FIRE
ES L FUEL PRESS R FUEL PRESS PR S ALERT
L OIL PRESS L GEN OVHT A/P TRIM FAIL R GEN OVHT R OIL PRESS T O TEST I DH L ENG FIRE L BL AIR FAIL A/P FAIL R BL AIR FAIL R ENG FIRE PUSH TO EXT PUSH TO EXT D OK D OK MASTER MASTER MASTER MASTER WARNING CAUTION CAUTION WARNING PRESS TO RESET PRESS TO RESET PRESS TO RESET PRESS TO RESET
START START 12 12 9 9 EFIS ITT ITT
AUX ALT 8 8 AUTO COMM NAV MKR BCN DME COMM NAV MKR BCN DME AUTO 0 M ALT GPS CRS GPSCPS APR GPS DRIVE 2 2 ALERT COMM 11221 2 1 2 ADF 112222A1 1 DFCOMM ALERT INTEG C X 100 4 C X 100 4 I DH OBS LEG ARM ACTV 7 7 6 5 6 5 COLLINS OFF PILOT AUDIO OFF COPILOT AUDIO OFF OFF COMM 2 AUDIO AUDIO PUSH HOT AUDIO COMM 2 SPKR EMER VOICE B PAGING ON/OFF INTPH VOICE B INTPH SPKR 0 COMM 1 CABIN O O COMM 1 CABIN HDG ALT 9 T T 300 40 0 H VOL GND VOL H 280 9 1 V L OFF NORM RANGE COMM RANGE OFF OFF VO L 60 O PWR 300 0 0 KNOTS 300 40 YD 26 TORQUE 26 TORQUE DME MKR BCN 260 20 821 , 2 2 8 ALT 280 200 24 24 12 1 & 2 80 2 60 AVIONICS BY BEECHCRAFT 4 4 10 10 3 KNOTS 22 22 HI 240 00 260 5 5 1 20 FTLB X 100 20 FTLB X 100 SIDE- INTPH VOL SIDE- INTPH 100 3 80 10 10 10 GPWS BELOW 7 3 18 9 18 9 TONE SENS VOL VOL TONE SENS 220 7 2992 16 10 16 10 ALTITUDE SET 20 20 GPWS BELOW 240 14 12 14 12 PUSH TO LO G/S ALT 2992. ENCD 200 120 AIR G/S 100 ALTM ANN 6 4 P/TEST P/CANCEL A ALT BEECHCRAFT 220 COMM 1 1 ALERT 00 PUSH BRT COMM 2 5 P/TEST P/CANCEL PUL 180 140 5 L 3,0 TEST BARO 160 120 Collins CANCEL PU Collins
200 1 S
0 H I N 0 DIM 10 0 0 180 140 2 COLLINS 160 23 5 23 5 XFR XFR 22 PROP 22 PROP LR * OPTIONAL EQUIPMENT 0 21 10 21 10 DH 500 MEM MEM MEM MEM 20 1 20 1 COLLINS DME2 2 TCAS TCAS 1 2 TCAS 3 3 CRS 1 19 RPM X 100 19 RPM X 100 OFF 14 14 SQ COM SQ COM 9.3 359 OFF 18 15 18 15 ON OFF ON OFF 0 3 4 .5 4 17 16 17 16 STO PWR MAG1 00 INT STO N 3 .5 OFF OFF N 134 OFF 33 6 115 6 VERT SPEED V V 33 VERT SPEED DC 0 3 RDR NAV LR COLLINS 30 9 TEST TEST E 33 6 0 0 6
0 6 ACT ACT 3 12
A 12 A 27
NAV 27 X1000 FPM 9
30 X1000 FPM D D 12
0 0 F F W
1
NAV 1 NAV 2 1
5 5 24
TURBINE TURBINE 24 .5 4 7
12 .5 110 110
A A 4 150 300 1 2 1 DIST ET 20 20 1
8 8 4 21 RMT 21
Collins Collins 5
D D 100 100 2
F F
S DC 15 00:00
3 21 1 2
GYRO 24 N 1 2
-+SLAVING XFR XFR 18 40 40 21 6 %RPM %RPM PGE A/B R 33 A/B R 80 80 NAV NAV 60 60 COLLINS GSP VOR2 WARNING ANNUNCIATOR PANEL—B200 AIRCRAFT SLEW MODE ñ ñ ñ E MEM MEM EMG VOR VRS 199 MEM MEM NAV NAV L 30 DG COLLINS O FMS 1 NAV NAV
12 ON ON
C 6 6 HLD HLD DH GYRO W DATA -+ COLLINS OFF STO OFF STO 9.3 ICT SLAYING 1 5 5
V V 2INM D 15 FUEL FLOW FUEL FLOW SLEW MODE
24 4 4 TEST RCL SKP CLR TEST 1
S CH SEL PWR 1 EFIS 2 ACT ACT x 00 AUX POWER COLLINS DG (PRIOR TO BB-1444, EXCEPT BB-1439) BRG CRS GPWS 3 PPH X 100 0 3 PPH X 100 0 2 ON HORN G/S GPWS BENDIX/KING TRANSPONDER GPS FMS1 FLAP KLN 90B TSO PUSH ADF OFF 013 1 1 DIS 34.5NM DATE/TIME COLLINS SEL PWR CANCLD INOP 2 2 BR ON OVRD ï ï ï ï ï ï ï ï ï ï 23 FEB 88 TEST SILENCE COLLINS Collins OBS IN - - -∞ 21 :29 :38SDT Collins 20 3 OUT 315∞ ALT 01300FT CRSR CRSR RAD ALT AUX ST RMI 130∞ BARO:29 .92" 15 FA 1 XFR ON A ANNUN ON C APPROVE? 10 4 T ENRñLEG CRSR NAV APT 5 AUX TEST OIL OIL NAV CALC D/T VOR 200 200 FPL STAT ACTV PULL NDB E 140 140 MODE SETUP SCAN RECT 2 REF INT MEM MEM TRIP OTHER CTR SUPL 100 150 100 150 MSG ALT B CLR ENT TEST Collins 60 100 60 100 ATC ADF ON ALT ADFTONE PROP SYN STBY IDENT ANT STO MIC AVIONICS INVERTER ENG AUTO 20 50 20 50 IGNITION OFF OFF GPWS BELOW NORMAL MASTER PWR NO 1 ON 0 0 ARM -20 0 -20 0 O o o OFF CPSI C PSI TEST TEST 15K F PRE ACT K F 35 MIC 10 OFF AVIONICS BY BEECHCRAFT 4 5 NORMAL OXYGEN OFF LEFT RIGHT 36 PSI MASK NO 2 CABIN ENVIRONMENTAL OFF ENGINE ANTI-ICE LIGHTS LIGHTS 020 G/S FURN START/ NO SMOKE MANUAL VENT INCR MAIN AUTO GYRO PNEUMATIC GEN LEFT RIGHT LANDING TAXI ICE NAV RECOG BEACON STROBE L DC GEN HYD FLUID LOWRVS NOT READY R DC GEN RESET ON BRIGHT & FSB TEMP BLOWER HEAT SUCTION PRESSURE ON LDG GEAR CONTROL C INCHES OF MERCURY ON MASTER SWITCH O INCR HIGH OXYGEN F O D O MASK L CHIP DETECT PROP SYNC ONDUCT OVERTEMP R CHIP DETECT F F I F LO Beechcraft Beechcraft ON F M F OFF E PILOT DEFROST L ENG ICE FAIL BATTERY CHARGE EXT PWR R ENG ICE FAIL E DECR AUTO MAIN AIR AIR LEFT RIGHT OFF UP COOL CABIN COPILOT OFF OFF OFF OFF FSB AIR AIR P/TEST P/CANCEL BATT GEN 1 GEN 2 ICE PROTECTION GEAR L AUTO FEATHER ELEC TRIM OFFAIR COND N LOW R AUTO FEATHER WSHLD ANTI-ICE PROP TAIL 1 CABIN TEMP MODE ACTUATOR DOWN FLOOD STANDBY NORMAL AUTO MANUAL FUEL VENT BLEED AIR VALVES DN L ENG ANTI-ICEBRAKE DEICE ONLDG/TAXI LIGHT PASS OXY ON ELEC HEAT ON R ENG ANTI-ICE OPEN O NOSE LEFT RIGHT CABIN TEMP F DOWN 1000 LOCK REL 500 1500 F HD LT 10 20 LR L IGNITION ON L BL AIR OFF FUEL CROSSFEED R BL AIR OFF R IGNITION ON ENVR 50 80 TEST FLIGHT 0 MAIN HI OFF 01∞F 00 2000 PILOT COPILOT OFF LEFT RIGHT PSI OFF HOURS 1/10 PULL PULL IGNITION AND AUTOFEATHER 0 INSTR & ENVIR OFF L L ENGINE START PROP GOV ON ON SURFACE PROP AMPS 30 PULL PULL TEST BRAKE DEICE STALL LANDING HYD FLUID EXT DET STALL AFT R R DECR ON CABIN AIR OXYGEN DEICE SINGLE WARN PITOT GEAR SENSOR ELEC SUPPLY PRESSURE LEFT RIGHT ARM WARN BLOWER MADE IN USA ON TEST ON HEAT IN O CAB ICE F 2 ALT OFF 0 00 OFF EMERGENCY F FT OFF EXTENSION UP 2 PSI TEST SWITCH OFF LEFT MANUAL LEFT RIGHT 20 1 4 5 ENG FIRE SYS STARTER ONLY TEST ENG RELAY TEST CABIN CLIMB 40 0 OFF TAKEOFF .5 THDS FT PER MIN 1 OFF FLAPS 35 AND 7 OFF OFF PARKING BRAKE APPROACH 2 OFF 0 6 30 6 PARKING BRAKE 60 3 .5 5 4 10 80 1 4 25 DOWN 2 20 15
NOSE
LR
*OPTIONAL EQUIPMENT
WARNING ANNUNCIATOR PANEL—B200 AIRCRAFT GPS CRS GPSCPS APR GPS G/S GPWS GPWS FLAP OBS LEG ARM ACTV INTEG (BB-1439, 1444 AND SUBSEQUENT) CANCLD INOP OVRD KING AIR 200 CAUTION-ADVISORY ANNUNCIATOR PANELS
(PRIOR TO BB-453) (BB-453 AND AFTER)
L ENG FIRE INVERTER DOOR UNLOCKED ALT WARN R ENG FIRE
ES L FUEL PRESS R FUEL PRESS PR S
L OIL PRESS L GEN OVHT A/P TRIM FAIL R GEN OVHT R OIL PRESS T O TEST L ENG FIRE L BL AIR FAIL A/P FAIL R BL AIR FAIL R ENG FIRE PUSH TO EXT PUSH TO EXT D OK D OK MASTER MASTER MASTER MASTER WARNING CAUTION CAUTION WARNING PRESS TO RESET PRESS TO RESET PRESS TO RESET PRESS TO RESET
START START 12 12 9 9 EFIS ITT ITT
AUX ALT 8 8 AUTO COMM NAV MKR BCN DME COMM NAV MKR BCN DME AUTO 0 M ALT GPS CRS GPSCPS APR GPS DRIVE 2 2 ALERT COMM 11221 22A1 DF 112222A1 1 DFCOMM ALERT INTEG C X 100 4 C X 100 4 I DH OBS LEG ARM ACTV 7 7 6 5 6 5 COLLINS OFF PILOT AUDIO OFF COPILOT AUDIO OFF OFF COMM 2 AUDIO AUDIO PUSH HOT AUDIO COMM 2 SPKR EMER VOICE B PAGING ON/OFF INTPH VOICE B INTPH SPKR 0 COMM 1 CABIN O O COMM 1 CABIN HDG ALT 9 T T 300 40 0 H VOL GND VOL H 280 9 1 V L OFF NORM RANGE COMM RANGE OFF OFF VO L 60 O PWR 300 0 0 KNOTS 300 40 YD 26 TORQUE 26 TORQUE DME MKR BCN 260 20 821 , 2 2 8 ALT 280 200 24 24 12 1 & 2 80 2 60 AVIONICS BY BEECHCRAFT 4 4 10 10 3 KNOTS 22 22 HI 240 00 260 5 5 1 20 FTLB X 100 20 FTLB X 100 SIDE- INTPH VOL SIDE- INTPH 100 3 80 10 10 10 GPWS BELOW 7 3 18 9 18 9 TONE SENS VOL VOL TONE SENS 220 7 2992 16 10 16 10 ALTITUDE SET 20 20 GPWS BELOW 240 14 12 14 12 PUSH TO LO G/S ALT 2992. ENCD 200 120 AIR G/S 100 ALTM ANN 6 4 P/TEST P/CANCEL A ALT BEECHCRAFT 220 COMM 1 1 ALERT 00 PUSH BRT COMM 2 5 P/TEST P/CANCEL PUL 180 140 5 L 3,0 TEST BAR 160 120 Collins CANCEL PU Collins
200 O 100 S
H I N DIM 10 0 0 180 140 2 COLLINS 160 23 5 23 5 XFR XFR 22 PROP 22 PROP LR 0 21 10 21 10 DH 500 MEM MEM MEM MEM 20 1 20 1 COLLINS DME2 2 TCAS TCAS 1 2 TCAS 3 3 CRS 1 19 RPM X 100 19 RPM X 100 OFF 14 14 SQ COM SQ COM 9.3 359 OFF 18 15 18 15 ON OFF ON OFF 0 3 4 .5 4 17 16 17 16 STO PWR MAG1 00 INT STO N 3 .5 OFF OFF N 134 OFF 33 6 115 6 VERT SPEED V V 33 VERT SPEED DC 0 3 RDR NAV LR COLLINS 30 9 33 6 TEST TEST E 0 6
0 6 ACT ACT 30 1
A 1 A 27 27 2 NAV 2 X1000 FPM 9
30 X1000 FPM D D 12
0 0 F F W
15
NAV 1 NAV 2 15
24
TURBINE TURBINE 24 .5 4
12 .5 110 110
A A 4 150 300 15 27 18 DIST ET 20 20 18 4 21 RMT 21
Collins Collins
D D 100 100 2
F F
S DC 15 00:00 3 21 1 2
-+GYRO 24 N 1 2
SLAVING 1 XFR XFR 18 40 40 2 6 %RPM %RPM PGE A/B R 33 A/B R 80 80 NAV NAV 60 60 COLLINS GSP VOR2 SLEW MODE ñ ñ ñ E MEM MEM EMG VOR VRS 199 MEM MEM NAV NAV L 30 DG COLLINS O FMS 1 NAV NAV
12 ON ON
C 6 6 HLD HLD DH GYRO W DATA -+ COLLINS OFF STO OFF STO 9.3 ICT SLAYING 1 5 5
V V 2INM D 15 FUEL FLOW FUEL FLOW SLEW MODE
24 4 4 TEST RCL SKP CLR TEST 1
S CH SEL PWR EFIS 21 ACT ACT x 00 AUX POWER COLLINS DG BRG CRS GPWS 3 PPH X 100 3 PPH X 100 2 ON HORN G/S GPWS 0 0 BENDIX/KING TRANSPONDER GPS FMS1 FLAP KLN 90B TSO PUSH ADF OFF 013 1 1 DIS 34.5NM DATE/TIME COLLINS SEL PWR CANCLD INOP 2 2 BR ON OVRD ï ï ï ï ï ï ï ï ï ï 23 FEB 88 TEST SILENCE COLLINS Collins OBS IN - - -∞ 21 :29 :38SDT Collins 20 3 OUT 315∞ ALT 01300FT CRSR CRSR RAD ALT AUX ST RMI 130∞ BARO:29 .92" 15 FA 1 XFR ON A ANNUN ON C APPROVE? 10 4 T ENRñLEG CRSR NAV APT 5 AUX TEST OIL OIL NAV CALC D/T VOR 200 200 FPL STAT ACTV PULL NDB E 140 140 MODE SETUP SCAN RECT 2 REF INT MEM MEM TRIP OTHER CTR SUPL 100 150 100 150 MSG ALT B CLR ENT TEST Collins 60 100 60 100 ATC ADF ON ALT ADFTONE IDENT ANT STO ENG AUTO PROP SYN 20 50 20 50 STBY MIC AVIONICS INVERTER OFF OFF NORMAL MASTER PWR NO 1 IGNITION ON 0 0 ARM -20 0 -20 0 O o o OFF C PSI C PSI TEST TEST 15K F PRE ACT K F 35 MIC 10 OFF AVIONICS BY BEECHCRAFT 4 5 NORMAL OXYGEN OFF LEFT RIGHT 36 PSI MASK NO 2 CABIN ENVIRONMENTAL OFF ENGINE ANTI-ICE LIGHTS LIGHTS 020 FURN START/ NO SMOKE MANUAL VENT INCR MAIN AUTO GYRO PNEUMATIC GEN LEFT RIGHT LANDING TAXI ICE NAV RECOG BEACON STROBE L DC GEN HYD FLUID LOWRVS NOT READY R DC GEN RESET ON BRIGHT & FSB TEMP BLOWER HEAT SUCTION PRESSURE ON LDG GEAR CONTROL C INCHES OF MERCURY ON MASTER SWITCH O INCR HIGH OXYGEN F O D O MASK L CHIP DETECT PROP SYNC ONDUCT OVERTEMP R CHIP DETECT F F I F LO Beechcraft Beechcraft ON F M F OFF E PILOT DEFROST L ENG ICE FAIL BATTERY CHARGE EXT PWR R ENG ICE FAIL E DECR AUTO MAIN AIR AIR LEFT RIGHT OFF UP COOL CABIN COPILOT OFF OFF OFF OFF FSB AIR AIR BATT GEN 1 GEN 2 ICE PROTECTION GEAR L AUTO FEATHER ELEC TRIM OFFAIR COND N LOW R AUTO FEATHER WSHLD ANTI-ICE PROP TAIL 1 CABIN TEMP MODE ACTUATOR DOWN FLOOD STANDBY NORMAL AUTO MANUAL FUEL VENT BLEED AIR VALVES DN L ENG ANTI-ICEBRAKE DEICE ONLDG/TAXI LIGHT PASS OXY ON ELEC HEAT ON R ENG ANTI-ICE OPEN O NOSE LEFT RIGHT CABIN TEMP F DOWN 1000 LOCK REL 500 1500 F HD LT 10 20 LR L IGNITION ON L BL AIR OFF FUEL CROSSFEED R BL AIR OFF R IGNITION ON ENVR 50 80 TEST FLIGHT 0 MAIN HI OFF 01∞F 00 2000 PILOT COPILOT OFF LEFT RIGHT PSI OFF HOURS 1/10 PULL PULL IGNITION AND AUTOFEATHER 0 INSTR & ENVIR OFF L L ENGINE START PROP GOV ON ON SURFACE PROP AMPS 30 PULL PULL TEST BRAKE DEICE STALL LANDING HYD FLUID EXT DET STALL AFT R R DECR ON CABIN AIR OXYGEN DEICE SINGLE WARN PITOT GEAR SENSOR ELEC SUPPLY PRESSURE LEFT RIGHT ARM WARN BLOWER MADE IN USA ON TEST ON HEAT IN O CAB ICE F 2 ALT OFF 0 00 OFF EMERGENCY F FT OFF EXTENSION UP 2 PSI TEST SWITCH OFF LEFT MANUAL LEFT RIGHT 20 1 4 5 ENG FIRE SYS STARTER ONLY TEST ENG RELAY TEST CABIN CLIMB 40 0 OFF TAKEOFF .5 THDS FT PER MIN 1 OFF FLAPS 35 AND 7 OFF OFF PARKING BRAKE APPROACH 2 OFF 0 6 30 6 PARKING BRAKE 60 3 .5 5 4 10 80 1 4 25 DOWN 2 20 15
*Optional Equipment
(BB-1439, 1444 AND SUBSEQUENT) (PRIOR TO BB-144, EXCEPT 1439)