AN CITATION II MODEL 550/551 PROCEDURES UNs 0002-0733 rBT Beovs , ot : PILOT CHECKLIST Copyright © 2000, Fightsafety Intemational, Inc, Unautiorized reproduction or distrioution is prohibited. All rights reserved.CITATION I PILOT CHECKLIST—MODEL 550/551 INSERT LATEST REVISED PAGES, DESTROY SUPERSEDED PAGES: LIST OF EFFECTIVE PAGES Original. ‘TOTAL NUMBER OF PAGES IN THIS PUBLICATION IS 55, CONSISTING OF THE FOLLOWING: Page “Revision No. No. Title 1-649. “Zero in this column indicates an original page. These are suggested procedures only and in no way supersede current procedures outined in the FAA-approved Flight Manual and any revisions thereto. In the case of conflict, the Fight Manual takes orecedence. IB TRAINING PURPOSES ONLYNUMBERLON FIGHT REFERS TO TAB NUMBER AND THE LETTER REFERS TO PROCEDURE OROER, ENGINE/FUEL, ENGINE FAIL OR FIRE DURING TAKEOFF. ENGINE FIRE (ENG FIRE SW ILLUMINATED)... ENGINE FAIL URE/PRECAUTIONARY SHUTDOWN, ENGINE FAILURE DURING COUPLED APPROACH ENGINE FIRE DURING GROUND SHUTDOWN....... ENGINE STARTER WILL NOT DISENGAGE AIRSTART ENVELOPE. “ ENGINE START MALFUNCTION EMERGENCY RESTART ~ TWO ENGINES, EMERGENCY RESTART — ONE ENGINE ... FIREWALL SHUTOFF VALVE CLOSED (FAV SHUTOFF LIGHT ON LOW OIL PRESSURE (OIL PRESS WARN LIGHT ON)... LOW OIL PRESSURE (OIL PRESS WARN LIGHT OFF) LOW FUEL PRESSURE (FUEL LOW PRESS LIGHT ON).. LOW FUEL QUANTITY (FUEL LOW LEVEL LIGHT ON) FUEL FILTER 8YPASS (FUEL FILTER BYPASS LIGHT ON). FUEL BOOST PUMP ON (FUEL BOOST PUMP LIGHT ON) . ELECTRICAL ELECTRICAL FIRE OR SMOKE, BATTERY OVERHEAT (BATT OTEMP LIGHT ON). i AG LOSS OF BOTH GENERATORS, 4D 4B SINGLE GENERATOR FAILURE (GEN OFF LIGHT ON). 5A ‘AC POWER FAILURE (BOTH INVERTERS + AND 2 AND AC FAIL LIGHTS ON)... oe 5B AC POWER AND/OR DISTRIBUTION FAILURE (AG FAIL UT ON AFTER MASTER WARN HAS BEEN RESET, INVERTER FAIL 1 AND 2 LIGHTS OUT) 5C SINGLE INVERTER FAILURE (INVERTER FAIL 1 AND 2 LIGHTS AND AC FAIL LIGHT ON)... eon eoe5D) EFIS SYMBOL GENERATOR FAILURE (RED X AND SG FAIL ON ADI OR BOTH DISPLAYS BLANK).....64. EFIS SYMBOL GENERATOR OVERHEAT (SG HOT LIGHT ON).sn6l EFIS ELECTRONIC DISPLAY INDICATOR FAILURE (EADI OR EHS))...6C EFIS HEADING FAILURE.. EFIS COOL FAN FAIL (DISP FAN LIGHT ON). EFIS ELECTRONIC DISPLAY INDICATOR ‘OVERTEMPERATURE (EAD! HOT OR EHS! HOT LIGHT ON).. PRESSURIZATION RAPID DECOMPRESSION (INDICATED BY CAB ALT 10,000 FEET LIGHT ON) 6G EMERGENCY DESCENT. : 6H CABIN ALTITUDE ABOVE SELECTED ALTITUDE. si OVERPRESSURIZATION.... EMERGENCY PRESSURIZATION ON (AUTOMATIC ACTUATION) (EMER PRESS LIGHT ON). BLEED AIR GROUND (BLO AIR GND LT ON)... AIR CYCLE MACHINE OVERPRESSURE (ACM O'PRESS LIGHT ON)...7E VACUUM SYSTEM FAILURE (INDICATED BY CABIN AT MAXIMUM PRESSURE DIFFERENTIAL WITH NO CONTROL) PRECOOLER FAILURE (LOR R PRECOOL FAIL LIGHT ON)... FORT (3 PURPOSES ONLY EMERGENCY/ABNORMALEMERGENCY/AGNORAIAL CITATION If PILOT CHECKL °—MODEL 550/551 THIS PAGE INTENTIONALLY LEFT BLANKFlightSafety NUNGER OW RIGHT REFERE To TABHUNGER AND TE LETTER ACFERS 1OPPOCEDUNE ORDER ENVIRONMENTAL ENVIRONMENTAL SYSTEM SMOKE OR ODOR 8A SMOKE REMOVAL (IF SMOKE INTENSE)... BB ENVIRONMENTAL SYSTEM AIR DUCT OVERHEAT (AIR DUCT OHEAT LIGHT ON). FLIGHT CONTROLS/TRIM BC AUTOPILOT HARDOVER roc 8D AUTOPILOT TORQUE FAILS TO HIGH TORQUE (AP TORQUE LIGHT ON). BE, ELECTRIC ELEVATOR RUNAWAY TRIIM.... ELECTRIG TRIM INOPERATIVE aF 8G JAMMED ELEVATOR TRIM TAB.. 8H HYDRAULIC THRUST REVERSER — INADVERTENT DEPLOYMENT DURING TAKEOFF - 9A THRUST REVERSER ~ INADVERTENT INFLIGHT DEPLOYMENT THRUST REVERSER UNLOCK LIGHT ON IN FLIGHT THRUST REVERSER ARM LIGHT ON IN FLIGHT .. LANDING GEAR WILL NOT EXTEND. LOW HYDRAULIC FLOW (HYD FLOW LOW LIGHT ON). LOW HYDRAULIC FLUID LEVEL (HYD LOW LEVEL LIGHT ON). HYDRAULIC SYSTEM REMAINS PRESSURIZED (HYD PRESS ON LIGHT REMAINS ON AFTER SYS CYCLE IS COMPLETED) 104 ANTISKID SYSTEM FAILURE (ANTISKID INOP LIGHT ON, PWR BRAKE LOW PRESS LIGHT OUT)... POWER BRAKE SYSTEM FAILURE (PWR BRAKE LOW PRESS AND ANTISKID INOP LIGHTS ON)....10C ANTIICE ENGINE ANTLICE FAILURE (ENG ANTIICE LIGHT ON) 2400 WINDSHIELD SLEED AIR FAILURE. 10E WINDSHIELD AIR OVERHEAT (WIS AIR OHEAT LIGHT ON).......10F PITOT-STATIC HEATER FAILURE (PIS HTR OFF, LH OR RH LIGHT MAY BE ON). SURFACE DEICE TIMER FAILURE. MISCELLANEOUS MASTER WARNING LIGHT ON STEADY ..... DOOR NOT LOCKED (DOOR NOT LOCKED LIGHT ON) NOSE AVIONICS OVERTEMPERATURE (NOSE COMP O-TEMP LIGHT ON) ABNORMAL LANDING WHEEL BRAKE FAILURE SINGLE ENGINE APPROACH AND LANDING SINGLE ENGINE GO AROUND .... SINGLE ENGINE REVERSING FLAPS INOPERATIVE APPROACH AND LANDING (NOT IN LANDING POSITION), _ MAXIMUM GLIDE ~ EMERGENCY LANDING EMERGENCY EVACUATION FOR TRAINING PURPOSES CNLYCITATION I PILOT CHECKLIST—MODEL 550/551 a6 V6 06 a6, ( ( ( C ¢ ( ( ( ( H3QUO SUNGIIOHd O1 SHIIIH H3L13T IHL ONY HIEWINN B¥L 01 SH349H IHOIH NO H3aVINN 30YONISIO UaLUYLS 401430 ‘TAWUON. wwnion | 401430 a6 v6 snd snd aol away away & 26 callLog Log a6 vi TRAINING PURPOS FORFlightSafety YOLVIONNNNY \ WSGHO SUNCIOOUd O1 SYBISY SY3LLF7 GNV YASWNN avL OL SY34IY UaSWAN eon) re) i Dl Pon Br pry fon wa) Ce rr Cou Qe ‘ans aNvo3s9 SN ho po ae (a) « vii on TRANG PURPOSES FORCITATION I PILOT CHECKLIST—MODEL 550/351 Anno ans any ‘Sev0 ‘caro SH ‘WQHO SUNGIOOUd O1 SH349H HALLITSHL CNY HS@WWNN av OL SH343H 1HOIH NO HaeWNN Sogo 2000 ¢Nn aianaixa mma | PALS | fa) vib 06 viii URPEEES GNLY RAINING aAFlightSafety THIS PAGE INTENTIONALLY LEFT BLANK ea 3 PURPOSES CNLYCITATION If PILOT CHECKLIST—MODEL 550/551 ENGINE FAIL OR FIRE DURING TAKEOFF SPEED BELOW V, - TAKEOFF SHOULD BE ABORTED Brakes ‘AS REQUIRED Threitles : IDLE Speed Brakes... nen : seve EXTEND Thrust Reverser.. DEPLOY ON UNAFFECTED ENGINE Aes IF ENGINE FIRE: 5. Accompish ENGINE FIRE Procedures; Tao 1, Procedure B. IF ENGINE FAILURE: 5. Accomplish ENGINE FAILURE/PRECAUTIONARY SHUTDOWN Procedure; Tab 1, Procedure C. SPEED ABOVE V, - TAKEOFF SHOULD NORMALLY BE CONTINUED 1. Gear. “UP (AFTER ESTABLISHING A POSITIVE RATE-OF-CLIMB) 2. Clear of obstacles, and Vo +10. FLAPS UP 3. Continue Climb enn! IF ENGINE FIRE: 3. Accomplish ENGINE FIRE Procedure; Tab 1, Procedure B. IF ENGINE FAILURE: 3, Accomplish ENGINE FAIL URE/PRECAUTIONARY SHUTDOWN Procedure; Tab 1, Procedure C. E2 FOR TRAN PURPOSES ONLYFlightSafety ENGINE FIRE (ENG FIRE SW ~ ILLUMINATED) 1. Throttle {Affected Engine) so DLE) IF LIGHT REMAINS ON: > 2. Engine Fire Sviteh....0.ce0:ssnnsneneaLIFT COVER AND PUSH 3. Either lluminated Bottle Armed Light. -PUSH 4. Ignition... = NORM me 5. Throttle (Affected Engine). oo OFF 6. Electrical Load. REDUCE (AS REQD) 7. Boost Pump (Affactad Engine) = OFF = 8. Land 2s soon as practical 9. Refer to SINGLE-ENGINE APPROACH AND LANDING Procedure; Tab 12, Procedure B. _.__ IFFIRE WARN LIGHT ON AFTER 30 SECONDS: 9, Remaining ltuminated Bottle Armed Light PUSH 10. Land as soon as possible. (Reter to SINGLE-ENGINE APPROACH AND LANDING Procedure: Tab 12, Procedure B.) —\ _ IFLIGHT GOES OUT & SECONDARY INDICATIONS NOT PRESENT: 2. Land as soon as practical. 9. Refer to SINGLE-ENGINE APPROACH AND LANDING Procedure: Tab 12, Procedure B. ~ Nera U EIS PRECAUTIONARY SHUTDOWN Throttle (Affected Engine)... Igrition (Affected Engine} . Engine Synchrorizor.. Generator (Atfoctod Engine) Electrical Load REDUCE (AS REQUIRED) Fuel Crossfeed.. AS REQUIRED IF No Fire, Firewall Shutoff.........OPEN AND BOOST PUMP ~ ON Refer to EMERGENCY RESTART — ONE ENGINE Procedure; Tab 2, Procedure F or SINGLE-ENGINE APPROACH AND LANDING Procedure; Tab 12, Procedure B, as conditon warrants. E-3 FOR TRANING PURPOSES otCITATION If PILOT CHECKLIST—MODEL 550/551 ENG FAIL DURING COUPLED APPROACH 7. Power (Operating Engine) INCREASE 2. Autopilot and Yaw Damper. OFF 8. Airspeed nen oseVREF +10 KIAS 4. Rudder Trim TRIM (TOWARD OPERATING ENG) 5. Flaps. 1.0. & APPR 6. Approach or Traffic Pattern, Before Landing, -COMPLETE 1. Throttle : 33 (CHECK OFF 2. Start Button... PRESS MOMENTARILY 2. Starter Disongage PRESS (AFTER 15 SEC) 4. Starter Disengage Button PRESS IF STARTER DOES NOT DISENGAGE AND START BUTTON LIGHT REMAINS ILLUMINATED (START RELAY STUCK): 2. Battery Switch. : . OFF 3. Battery Quick Disconnect Connector DISCONNECT (IN TAILCONE) 4. Throttie(s) : OFF ®) PRESSURE ALTITUDE FEET sca Levey E4 FOR TRAINING PURPOSES ONY1. Throttle 2, Starter Disengago EMERGENCY RESTART — TWO ENGINES . OFF -PRESS (15 SEC AFTER THROTTLE OFF) BOTHON lorition Boost Pumas .. Thoottles... It Altitude Autows. INCREASE AIRSPEED TO 200 KIAS. Firewall Shutoff... CHECK OPEN All Anti-ice Switches OFF lino star! in ten seconds; either start button, press momentarily. Ii no start, maximum glide ...... EMERGENCY LANDING; TAB 13 B EMERGENCY RESTART — ONE ENGINE FOLLOWING SHUTDOWN — WITH STARTER ASSIST: . Thiotle.. OFF 2. Generator.. seuss GEN 3. Firewall Shutof. CHECK OPEN i, ty option ON PE Eg OFT REIT ei ea 3 Thiet. DLE (AT 8 TO 10 PERCENT TURBINE RPM) 7. Engine instruments. so MONITOR 8. lgniion .NORM 8. If Start Does Not Occur..... PRESS STARTER DISENGAGE SWITCH FOLLOWING SHUTDOWN ~ WINDMILLING WITH AIRSPEED ABOVE 200 KIAS: 1. Thioitle. seeene OFF 2, Firewall Shuto CHECK OPEN 3. Ignition : cee ON 4. Boost Pump sa 5. Throttle : IDLE 6. Engine Instruments... MONITOR 7. After Engine Stabilzes.... SOOST PUMP AND IGNITION - NORM 8. Generator GEN ES FOR TRAINNG PURPOSES ONLYCITATION Hf PILOT CHECKLIST—MODEL 550/551 closed at applicable firewall LOW OIL PRESSURE (OIL PRESS WARN Advisory — Operated by LH/RH ENG FIRE Push Switch(es) all electrical, tuel and hydraulic system(s) are erie) ABOVE 70 PSI: 1. Land as soon as practical. BETWEEN 35 AND 70 PSI: 1. Throttio (Affacted Engine) REDUCE POWER 2. Land as soon as practical. BELOW 35 PSI: ™~ 1. Throttle (Affected Engine). se OFF 2. Accomplish ENGINE FAILURE/PRECAUTIONARY SHUTDOWN Procedures; Tab 1, Procedure C. ~ (©) —~ BETWEEN 35 AND 70 PSI: 1. Throttle (Affected Engine) .REDUCE POWER BELOW 35 PSI: ~ 1. Land as soon as practical ~ my E6 OR TRAINNG PURPOS 5 ¢FlightSafety .ON (BOOST PUMP CKT BKR(S) IN) CHECK ..IF REQUIRED Advisory ~ The illumination of this light serves notice to the pilot that 169 pounds or less of fuol romaing in the respective tank, 1. Fuel Boost. 1. Fuel Boost. 2, Fuel Quantity... 3, Fuel Crossieed ON (BOOST PUMP CKT BKR(S) IN) 2. Land as soon as practical Advisory — Consider possibility of partial or total loss of both engines. Inspect fters after landing E7CITATION II PILOT CHECKLIST—MODEL 550/551 Advisory — Indicates that the respective fuel boost pump Was either automaticaly or manually turned on. 4. Fuel Boost Switch (Affected Pump) .ONTHENNORM = —\ IF FUEL BOOST PUMP ON LIGHT REMAINS ILLUMINATED Advisory —If aifected FUEL LOW PRESS light does not extinguish, leave the fuel boost switch in NORM with pump running. ae ELECTRICAL FIRE OR SMOKE 1. Oxygen Masks. DON AND 100% OXYGEN > 2. Oxygen Microphone Switches... AS REQUIRED 3, Pressurzation Souroe SeISCtOF nn. NORM UNs 0001-0481, 0483, 0484 ‘BOTH HI KNOWN SOURCE: ~ 4. Isolate Faulty Circuit...... .---+-PULL CIRCUIT BREAKER(S) UNKNOWN SOURCE: 4, Flood Lights... FULBRIGHT 5. Battory Switch neuen EMER 6. Generators .OFF 7. Microphone Selector (UNS 0001-0626) ......ssn-2-EMER COMM WSEHEADSET) = 8. Receiver Selector (UNs 0001-0626). .GOMM 1 TO HDPH 9. Windshield Bleed Air Manual Valves ...esnsu:OFF OR MINIMUM 10. DC Power RH Bus No. 1, 2 and Cireuit Breakers. PULL 11. RH CB PANEL Circuit Breaker (on LH Panel) PULL ~ 12, AC INVERTER No. 1 Circuit Breaker (on LH Panel) -PULL 13. Land as soon as practical (within 20 minutos). IF SEVERITY WARRANTS: 18, Inttate SMOKE REMOVAL Procedure; Tab 8, Procedure 8, andior. = Emergency Descent Procedures (As Required): Tab 6, Procedure H. Land as soon as possible. WHEN LANDING ASSURED: 14. LH Generator. = ” ON ~ 18, Landing Gear. . OWN 16. Flaps. ss LAND 17. Airspeed --VREE IF SMOKE OR FIRE RESTARTS: 18. LH Generator...... 7 - - OFF ‘Advisory - Antikid system willbe inoperative. Mutiply landing distance by 1.6. Be prepared to use the emergency brake system. EB OR TRAINING APOSES ONLY~ FlightSafety PNB IOUS sie ORR i i 1. Note Amperage, Baltery Switch EMER 2. Amperage. iad NOTE DECREASE 3. Hbatiery voltage is 1 toll iese hay gonersier rola 40 Seconds 19 2 minutes, Moritor battery Overmeat aniunciator for possible change. IF VOLT/AMP DECREASE: 4. Battery Switch .........OFF (VOLTMETER WILL BE INOPERATIVE) IF BATTERY O'TEMP LIGHT GOES OUT: 8. Battery Switch BATT IF NO AMP DECREASE OR BATT O'TEMP LIGHT FLASHES: 4, Batiery Switch. sadEMER 5. Flood Lights ULL BRIGHT 6. Generators... 2 OFF IF NORMAL DC POWER IS LOST (BATTERY RELAY NOT sTUcig: 7. Generators. GEN 8. Battery Switch. _-OFF 9. Land as soon as practical IF NO DC POWER LOST (BATTERY RELAY STUCK): , 7, Microphone Selector (UNS 0001-0626) .vsesne R.COMM (ea) 8, Receiver Select (UNs 0001-0626) oenCOMM1 TO HDPH $. Windshield Bleed Air Manual ValVe8 ssn 10. DO Power LH & RH Bus No. 1,2 & 3 CKT BKRS- 11. Landas soon as practical Layyen LANDING ASSURED: G EW DC Power LH and RH Bus CKT BKR 13. Landing Gear... 14. Paps 15, Airspeed... LOSS OF BOTH GENERATORS IF ONLY ONE GENERATOR COMES O1 2, Electrical Load. IF NEITHER GENERATOR COMES ON: REDUCE (AS REQUIRED) 2, Flood Lights FULL BRIGHT 3, Battery Switch... i EMER 4. Microphone Selector (UNs 0001-0626). EMER COMM jSE HEADSET) 5. Receiver Select (UNs 0001-0626) .....n.....--COMM 1 TO MDPH 6. Windshield Bleed Air Manual Valves OFF OR MINIMUM. 7. Land as soon as practical. WHEN LANDING ASSURED: 8, Battery SWiCH anon BATT © Landing Gear ern eeeeeD OWN 10, Flaps... . LAND 11. Airspeed Maer E9 De TRAMIMG PUBPOSES ONLYCITATION I PILOT CHECKLIST—MODEL 550/551 @) 1. Electrical Lead.. 2. Failed Generater.. DECREASE (IF REQUIRED) + CHECK SW AND CB; RESET (AS REQUIRED) IF UNABLE TO RESET: OFF 3. Failed Generator... AC POWER FAILURE (BOTH INVERTERS 1 AND 2 FAIL AND AC FAIL LIGHTS ON) 1. Inverter Circuit Breakers (AC Inverter No. 1 on LH Panel and AC Inverter No. 2. on RH Panel)... CHECK & RESET IF ONE OR BOTH INVERTERS RESET: 2. Land as soon as practical IF BOTH INVERTERS WILL NOT RESET (UNS 0002-0505): 3. Battery Switch. EMER (Checklist Complete for UNS 0002-0550) UNS 0550 & ON 8. Ac Inverter No. 1 Circuit Breaker (LH Panel)... PULL 4. INVTR FAIL 2 Annunciator. .CHECK (NO ANNUNCIATION INDI RECOVERY OF INVERTER 2) NOTE If Inverter 2 recovers, do not reset Inverter No. + breaker. IF INVTR FAIL 2 ANNUNCIATOR REMAINS ILLUMINATED: 5. AG Inverter No. 1 Circuit Breaker (LH Panel) -RESET 6. AC Invertor No. 2 Circuit Breaker (RH Panel)... se PULL, 7. INVTR FAIL 4 Annuneiator... CHECK (NO ANNUNCIATION INDICATES RECOVERY OF INVERTER 1) NOTE Inverter 4 recovers, do not reset Inverter No. 2 breaker. IF INVERTER 1 OR 2 RECOVERS (INVTR FAIL 1 OR 2 ANNUNCI- ATOR EXTINGUISHED): 8. Land as soon as practical IF BOTH INVERTERS REMAIN FAILED: 9. Battery Switch... 10. Land as soon as acta (within 80 minutes). EMER E40 IG PURPOSES OFlightSafety Neq TOTP Pela) DISTRIBUTION FAILURE (AC FAIL LIGHT ON AFTER MASTER WARNING HAS BEEN RESET, INVERTER FAIL 1 AND 2 LIGHTS OUT) UNS 0002-0505 Ea 1. Avionics Power SELECT INV 1 OR INV 2 AS APPROPRIATE UNS 0550 & ON esitisy 4. Chock the right sub-circuit breaker panel for disencaged AC BUS ltcul breaker(s). If circuit breaker(s) is/are disengaged, operate with loss of bus as re-engagament may result in further damage to the electrical system. NOTE Depending on which bus(ses) has/have been lost, the fellowing equipment will be lost: a. 26 VAC Bus 1 — Filot's ADI: pilet’s RMI; pilots HSI (HDG and NAV flags in view); pilot's rate-o-tumn indicator; copilot’s RMI compass card and Nav 1 bearing pointer; and ADF 4 b. 115 VAC Bus 1 — Pilot's flight director; autopilot; yaw damper; radar and pilot's attitude gyro: and YNAV computericontroller. ©. 26 VAG Bus 2 ~ NAY 2 , copliot's ADI (optional dual fight director installation); and copilot's HSI; copilot's RMI; pilot's RMI compass card and NAY 2 ~ bearng pointer and ADF 2 (optional). Operation of the following equipment can be reinstated by plac- ing the BATT switch to EMER: NAV 2; copilot's RMI bearing pointer and DG of copilot’s HSI. 4. 115 VAG Bus 2 — Copilot's tight director (optional); air data computer and pilot's altimeter. Tho autopilt will only operate in the basic autopilot modes due to, loss of valid signal irom the air data computer. Advisory ~ Incicates ess of power from affected inverter. 1. AC Inverter No. 1 and No. 2 Circuit Breakers. HECK IN 2. Master Warning RESET AND CONTINUE FLIGHT ett FOR TRAINING PURPOSES OnUYCITATION If PILOT CHECKLIST—MODEL 550/551 EFIS SYMBOL GENERATOR FAILURE (RED X AND SG FAIL ON EADI (4) OR BOTH DISPLAYS BLANK) 1. This EFIS system is inoperative. Refer to the Copilot’s Attitude Indicator and HSI and Standby Gyro Horizon for compass and attitude information. or 1. Optional MFD Mode Selector .... oR: 1. Optional Dual EFIS SG REV Button PUSH EFIS SYMBOL GENERATOR OVERHEAT (SG HOT LIGHT ON) 4 Advisory ~ Indicating overheat of EFIS symiol generator. 1. DC Circuit Breakers PULL EFIS 1, EADI 1 & EHSI1 1. Dim Button (Affected Display) OFF ©) 4. HDG REV Button PUSH DISP FAN LIGHT ILLUMINATED ON GROUND: Advisory — Indicates failure of pilot's EFIS cooling fan. 1. DC CKT BKRS.. PULL EFIS 1, EADI 1 & EHS! 4 2, Ground Operating Time. ene 10 MINUTES 3. Prior 0 Takeott RESET EFIS 1, EAI 1 & EHS! 1 4. EADI Hot and EHS! Hot Lights MONITOR 5. Return to Normal Procedures. DISP FAN LIGHT ILLUMINATED IN FLIGHT: Advisory — Indicates failure ot pilct's cooling fan. 4. EAD] Hot and EHS! Hot Lights ...0. ore rain 2URPORES ONLY1. Cockpit Temp Select. MANUAL COLD ~ 2. Dim ard Raster Dim.. -REDUCE BRIGHTNESS 3. Affected EADI 1 or EHSI 1 CKT BKR(S) voPULL, 4. Dim Button (Affected Display)... OFF RAPID DECOMPRESSION (INDICATED BY CAB ALT 10,000 ESS FEET LIGHT ON) EE DON AND 100% OXYGEN 1. Oxygen Masks. 2. Emergency Descent. AS REQUIRED 8. Passenger OxYQEM o.snun--ue~--ENSURE PASSENGERS ARE RECEIVING OXYGEN 4. Oxygen MIC Switch(s) MIG OXY MASK 5. Transponder sn EMERGENCY i . (4) EMERGENCY DESCEN 1. Thvoitles 2, Speedbrakes ... 8. Iniate Moderate Bark 4. Airplane Pitch Atitude ... 15 DEGREES NOSE DOWN 5. Passongor Advisory Lights. eePASS SAFETY 6. Maximum Airspeed Vigo/Miuo (REDUCE SPEED IF STRUCTURAU'DAMAGE Has OCCURRED) 7. Transponder .. z EMERGENCY E13 FOR IRAININS PURPOSES CMUCITATION II PILOT CHEC @) 1. Cabin Altitude Selector 2. Rate Control 3, Press Source SeleCtOt con IF NOT ARRESTED BY 14,000 FT CABIN ALTITUDE: 4, Initiate EMERGENCY DESCENT Procedure; Tab 6, Procedure H. 5. Oxygen Control Valve. MANUAL DROP 6. Passenger Oxygen .... ENSURE PASS ARE RECEIVING OXYGEN ERPRESSURIZATION 1. Cabin Altitude Selector. .SET (HIGHER CABIN ALTITUDE) °KLISP—MODEL 550/551 SET (LOWER CABIN ALTITUDE) FULL INC EMER 2. Rate Control. - en tNC IF STILL OVERPRESSURIZED: 3. Press Source Selector. LH OR RH (CONTROL CABIN PRESSURE WITH THROTTLE) IF UNABLE TO CONTROL: 4. Oxygen Masks DON AND 100% OXYGEN 5, Oxygen Control Valve. -MANUAL DROP 6. UNS 0001-0505 Crew Oxygen Priority Valve... NORMAL 7. Passenger Oxygen .. ENSURE PASSENGERS ARE RECEIVING OXYGEN 8. Oxygen MIC Switches... z MIG OXY MASK PASS SAFETY 9. Passenger Advisory Light. 10. Pressurization Source Salector OFF 11, Descend. IF STILL OVERPRESSURIZED: 14. Emergency Dump Switch DUMP E14 UR TRAINING PURPOSES ONLYAdvisory — Air cycle mackine shutdown or failure. 1. Norm Pressurization CKT BKR..... CHECK IN 2. Temp Control snenenDJUST TO WARMER SETTING (MAY REQUIRE MANUAL MODE) 3. Press Source Select MER, WAIT 1 MIN After 1 Minute: 4, Press Source Select.. RH, LH OR NORM IF EMERGENCY PRESSURIZATION REMAINS, o 5. Pressurization Source SelectOt v.nuns 6. Control cabin temp with LH throttle, ©) Advisory ~ Light must be out betore takeott, 1. Press Source Soloctor Switoh rn ON THE GROUND: 1. Do not fly the airplane until the matfunetion has been repaired DURING FLIGHT: 1. Prossurization Source Selector -RH (REDUCE POWER ON RIGHT ENGINE TO 80 PERCENT TURBINE SPEED} 2. Emergency Pressurization Circuit Breaker PULL 3. Norm Pressurization Circuit Breaker . PULL AND RESET 4. Emergency Pressurization Circuit Breaker sos RESET 1. Pressurization Source Selector.......LH OF RH (REDUCE POWER BELOW 70 N, RPM) OFF BEFORE LANDING. 2. Prossurization Source Selector. (On AIC Unit -0002 thru -0481, -0483 and-04s4 1. Affected Engine....... REDUCE POWER (IF SITUATION PERMITS) IF LIGHT DOES NOT GO OUT OR SITUATION DOES NOT PERMIT POWER REDUCTION: 2. Pressurization Source Selector... LH OR RH (OPPOSITE OF EFFECTED ENGINE) E15 FOR TRAINING PURPOSES ONLYCITATION H PILOT CHECKLIST—MODEL 550/551 ENVIRONMENTAL SYS SMOKE OR ODOR 4. Oxygen Masks... DON AND 100% OXYGEN 2. Oxygen Microphone Switches. snes AS REQUIRED 3, Cabin (VHD) Fan... 3 oe FF 4. Defog Fan - : OFF 5, Pressurization Source Solector ...-..-----.LH (ALLOW TIME FOR SMOKE TO DISSIPATE) IF SMOKE CONTINUES: 6. Prescurization Source Selector... RH (ALLOW TIME FOR SMOKE TO DISSIPATE) IF SMOKE STILL CONTINUES (AIR CYCLE MACHINE SEAL MAY BF LEAKING): 7. Pressurization Source Selector ..-.-.0EMER (CONTROL CABIN PRESSURE WITH LH THROTTLE) SMOKE REMOVAL (IF SMOKE INTENSE) 1. Oxygen Masks DON AND 100% OXYGEN 2, UNs 0001~0505 Grew Oxygen Prionty Valve. NORMAL, 3, Passenger Oxygen ...u ENSURE PASS ARE RECEIVING OXYGEN 4. Oxygen MIC Suitches . .MIC OXY MASK 5. Passenger Adivsory Light PASS SAFETY 6. Cabin Altitude Selector........SET TO HIGHER GABIN ALTITUDE 7. Emergency Dump Switch DuMP IF SMOKE PERSISTS OR IT CANNOT BE VERIFIED THAT THERE IS NO FIRE: 8. Land as soon as possible. 1. Temperature Circuit Breaker... ESET 2. Auto Temperature Select... MANUAL 3. Manual HotManual Cold Switch... MANUAL COLD. (HOLD POSITION UNTIL OVERHEAT LIGHT GOES OUT) AFTER LIGHT GOES OUT: 4. Auto Temperature Select IF THE LIGHT ILLUMINATES AGAIN: 5. Auto Temperature Select MANUAL IF LIGHT DOES NOT GO OUT: 4. Pressurization Source Selector ....u.LH OR RH (REDUCE POWER ON SELECTED ENGINE, IF NECESSARY) AUTO. E16 For Tr ING PURPOSES UMLFlightSafety (0) AUTOPILOT HARDOVER 1. Autopilot’Trim Disengage Switch... PRESS: 1 1. Autopilov Trim DIsengage SWiCH wn... .a.PRESS AND HOLD] UNTIL PITCH TRIM CIRCUIT] BREAKER IS PULLED| \S REQUIRED] 2. Manual Elevator Trim... 1. Blecvi¢ Tim Circuit Breaker (Pitch Trim) IF STILL INOPERATIVE: 2. Manual Elevator Trim. CHECK CIRCUIT BREAKER AS REQUIRED NOTE Do not use autopilot. CRUISE: 1. Maintain trim speed as long as practical. Do not extend taps for approach or landing. Use FLAPS INOPERATIVE APPROACH AND LANDING Procedure; Tab 13, Procedure A. ‘TAKEOFF OR GO AROUNI 1, Reduce power as necessary to maintain 120 KIAS oF less. Do rot change flap position. Minimum speed is Vper for full flaps, Vape for flaps in T.O. & APPR, oF Vagr + 15 KIAS for flaps 0° or Unknown. Do not retract landing gear. Land as soon as practical NOTE Do notuse autorilet. FOR TRAINS PURPOSES ONYCITATION II PILOT CHECKLIST—MODEL 550/551 ESS (a) UN SUS RON SNp Romi DURING TAKEOFF SPEED BELOW Vj - TAKEOFF SHOULD BE ABORTED: 1. Brakes AS REQUIRED 2. Throttles 38. Speedbrakes .. 4. Thrust Reversers BOTH DEPLOY 5. Reverser indicator Lights HECK ILLUMINATION OF ARM, UNLOCK AND DEPLOY LIGHTS, REVERSE POWER ON BOTH ENGINES SPEED ABOVE V, ~ TAKEOFF SHOULD CONTINUE: 1, Emergency Stow Switch....... ACTUATE ON AFFECTED ENGINE 2. After establishing a positive rate-of-climb, retract landing gear. Do not exceed 125 KIAS until thrust reverser stows. 3. At MSA, retract flaps at V2 + 10 and accelerate. Do not exceed 200 KIAS after thrust reverser stows. 4. Land as soon as practical. IF THRUST REVERSER WILL NOT STOW: 5. Thrust Reversor CKT BKR .... 6. Throttle (Affected Engine)... CUTOFF 7. Airspeed MAINTAIN 180 KIA OR BELOW 8 Refer to SINGLE ENGINE APPROACH AND LANDING Procedure, Tab 12, Procedure ®. THRUST REVERSER — INADVERTENT INFLIGHT pS Rose 1. Reverser Indicator Lights (CHECK ILLUMINATION OF ARM, UNLOCK, AND DEPLOY LIGHTS 2. Affected Throttle CHECK IDLE 3. Emergency Stow Switch .. ACTUATE ON AFFECTED ENGINE 4, Airspeed... IEDUCE TO 125 KIAS OR BELOW AFTER THRUST REVERSER STOWS, 3 DO NOT EXCEED 200 KIAS 5. Reverser Indicator Lights UNLOCK AND DEPLOY LIGHT EXTINGUISHED. ARM AND HYD. PRESS ON LIGHT ILLUMINATED 6. Thrust Reversers.. CHECK IN 6. Land as soon as possible. IF THRUST REVERSER WILL NOT STOW: 7. Thrust Reverser Circuit Breaker é Throttle (Affected Engine) CUTOFF 9. Airspood . MAINTAIN 10 KIAS OR BELOW 10. Refer to SINGLE ENGINE APPROACH AND LANDING: Procedure; Tab 12, Procedure B. CHECK IN OR TRAINING PURPOULG CMLyFlightSafety THRUST REVERSER UNLOCK ee Ue) SCC | oc | ~ Emergency Stow Switch....... AGTUATE (ON AFFECTED ENGINE) 2. Thrust Reverser Levers... CHECK STOWED (FULL FWD) POSITION ~ IF LIGHTS WILL NOT EXTINGUISH: 3. Thrust Reverser Circuit Breaker CHECK IN. 4. Maintain 200 KIAS or below. 5. Land as soon as practical 1. Thwust fleverser Levers... HECK STOWED (FULL FWD) POSITION mS 2. Emergency Stow Switch ... VERIFY NORM IF LIGHT IS STILL ILLUMINATED: Airspeed is -MAINTAIN 200 KIAS OR BELOW 4. Hydraulic Press On Light - CHECK IF HYD PRESS ON LIGHT IS ILLUMINATED: 5. Atfected Thrust Reverser Circuit Breaker 6. Land as soon as possible. -~~_ IF HYD PRESS ON LIGHT IS NOT ILLUMINATED: 5. Land as soon as practical = Landing Gear Handle «0... CHECK DOWN (150 KTS OPTIMUM) 2 Gear Control Circuit Breaker CHECK IN 3. Ausilaty Geer Handle ..PULL T-HANDLE AND ROTATE TO LOCK \ 4. Rudder. YAW AIRPLANE (IF NECESSARY ‘TO ACHIEVE DOWNLOGK LIGHT) -PULL KNOB TO BLOW DOWN (FOR POSITIVE LOCK) 5. Auxiliary Gear Control ~\ Advisory ~ Indicates inoperative Pump. 1. Land as soon as practical. (The speedorakes, thrust reversers and gear may not operate using normal procedures.) E19 FOR TRAINNES PURPOSES ONLCITATION II PILOT CHECKLIST—MODI 50/551 4. Speedbrake Control Circuit Breaker 2. Gear Control Circuit Breaker. 3. Thrust Reverser Circuit Breakers... «PULL (ONE AT A TIME) IF SYSTEM DEPRESSURIZED: 4. Circuit Breakers... RESET (ONE ATA TIME) Leave circuit breaker pulled which caused systam to deprescurize, 5. Land as soon as practical. Reset landing gear or speedbrake control (not Thrust Reverser) Circuit Breaker(s) if piled, prior to landing. IF SYSTEM REMAINS PRESSURIZED (Indicates system bypass valve has failed): 4. Circuit Breaker RESET (ONE AT A TIME) 3, Land ax eoorvae poseibes fe syelem broace-value has tiie te hydraulic system may overheat. 1. Antiskid Switch 2. Skid Control Circuit Breaker. IF LIGHT REMAINS ON: 3. Antiskid Switen.. 4. Multiply Landing Distance by... {6 (UNs 0001-0626) (UNs 0627 AND ON) 5. Be prepared to use the emergency brake system. 1 1. Skid Gono! Circuit Breaker... ESET IF LIGHTS REMAIN ON: . 2. Wheel Brake Failure anos lan ruse amecgeny bits eston ir litling Brake Pedals... REMOVE FEET FROM BRAKE PEDALS Emergency Brake Hanch PULL (AS REQUIRED) .8 (UNs 0001-0626) 1.5 (UNs 0827 AND ON) 10 REVIEW TAB 120, eee Multiply Landing Distance by. mn 8 D8 TRAININS BURPOSES CMLyFlightSafety 1. Throttle ssnens INCREASE POWER 2. Engine Anti lee Controls... CHECK SW|S) AND CIRCUIT BREAKER(S) 3. Leave icing environment. MOMENTARY ILLUMINATION (Cycles on and off) Advisory ~ Indicates failure of normal temperature controller or a wing heating element, LOSS OF HOT AIR SUPPLY (Valve will not open or possible 1. Windshield Bleed Air Switch and Valves 2. Windshield Alcohol Anti-Ice.. 3. Leave icing environment. IF WINDSHIELD BLEED SW LOW OR HI: INTERMITTENT ILLUMINATION (Airflow stops) 1, Windshield Bleed ir Switch is HI. : 2. Windshield Bleed Air Valves 7 SELECT LOW REDUCE CONTINUOUS ILLUMINATION (Airfiow stops, probable controller failure) OFF AS REQUIRED 1. Windstield Bleed Air Switch and Valves 2. Windshield Alcohol Anti-Ice..... 3. Leave icing environment. IF WINDSHIELD BLEED AIR SW OFF: WIS AIR O'HEAT LIGHT ON MOMENTARY OR CONTINUOUS: Advisory ~ Indicates probable solenoid valve failure or leak. Windshield air temperature is not regulated. Windshield heat damage is possible. Maintenance is required. 1. Windshield Bleed Air Manual Valves .CLOSED E21 POR THAINING PURPOSES Cnt 10CITATION I PILOT CHECKLIST—MODEL 550/551 1. Pitot-Static Switch and Circuit Breaker(s) 2, Determine inoperatve system. 1. Surface Deice Circuit Breaker CHECK IN 2, Surface Deice Switch. RESET 3. Surface Deice Switch. son SURFACE DEICE IF SURFACE DEICE BOOTS FAIL TO INFLATE: 4, Leave icing environment. IF SURFACE DEICE BOOTS CONTINUE TO CYCLE WITH SURFACE DEICE SWITCH IN OFF POSITION: 4, Surface Deice Circuit Breaker PULL, 5. Leave icing environmont. 1. Warning Light Circuit Breaker ... CHECK 2. Instruments (Hydraulic, Electrical and Engine) ...u...-MONITOR £22 OH TRAINING BURPOEES CNLYAdvisory ~ Indicates unlocked/unlatched nose or tallcone coors, taulure or improper position af one or more door switch(es}, andlor possible disengagement of the lower forward cabin door pin. ON THE GROUND: 1. Correct condition prior to fight. IN FLIGHT: 1. Cabin Altitude SELECT TO 9500 FEET Airspeed. REDUCE Passangor Advisory Light. PASS SAFETY Cabin Door - KEEP CLEAR Doscend to lower altitude. 7A eR Land as soon as practical. ‘Advisory ~ Incicates that 2 high temperature condition exists in the nese avionics compartment. ON THE GROUND: 1. Determine the cause of annunciator illumination before next fight. IN FLIGHT: 1. Land as soon as practical 2. Determine the cause of annunciator illumination beiore next fight. £23 FOR TRAINING PLAPOSES OnLy12 CITATION Il PILOT CHECKLIST—MODEL 550/551 1. Brake Pedals REMOVE FEET FROM BRAKE PEDALS PULL AS REQUIRED sveect 6 (UNs 0001-0626) 1.5 (UNs 0627 AND ON) 2. Emergency Brake Handle 2. Multpiy Landing Distance by... 1, Seais(Belts/Harnesses. Avionics and Flight Instruments. Radar Altimeter... Passenger Advisory Lights.. ns Passenger Seats. GHEGK FULL UPRIGHT/QUTEOARD AND POSITIONED AFT OR FWD TO CLEAR EXIT DOORS: 2 3 4, Vacr and Fan Speed Settings 5 6 7. Flaps. T.0. AND APPR 8 Engine Synchronizer... OFF 9. Fuel Crossfeed... : CHECK 10. Ignition (Operating Engine)... ON DOWN/LOCKED 11. Landing Gear... 12. Antiskid.. CHECK ON 48. Landing LiDhts 0 cnc _ON 14, Airspeed. . ~ Maer +10 KIAS MINIMUM 1. Autopilot and Yaw Damper..... aaaey OFF 16. Pressurization CHECK ZERO DIFFERENTIAL 17. Speedbrakes RETRACTED PRIOR TO 50 FEET 48. Flaps. LAND (WHEN LANDING ASSURED) 19. Airpseed.. Vaee E24 For ING PURPOSES Chiy Configuration AA >~ ©) geen Throttle (Operating Engine)... 7.0. POWER . Airplane Pitch Altitude . 7.5 DEGREES Flaps... 7.0. & APPR |. Climb Spee Vag + 10 KIAS MINIMUM. . Landing Gear . UP Flaps (When Clear of Obstacle)... Climb Speed. RETRACT AT Vege +10 Ven Thrust maximum continuous power. - Throttles.. IDLE Brakes “APPLY ‘Speedbrakes EXTEND ‘Thrust Reverser ..DEPLOY (AFTER NOSE WHEEL ON GROUND) Reverser Indicator Lights ........CHEGK ILLUMINATION OF ARM, UNLOCK AND DEPLOY LIGHTS. Reverser Power 5 ~AS REQUIRED Thrust Reverser .. REVERSER LEVERS TO IDLE REVERSE AT 60 KIAS E25 FUR TRAINING PLAPOSES UML13 CITATION If PILOT CHECKLIST—MODEL 550/551 1. SeatsiBelts/Harnesses....... SECURE 2. Vagr and Fan Speed Settings ..... CONFIRM 3. Airspeed: Flaps 15° Vapp Flaps 0° or Unknown, Vagr + 15 KIAS Flap Control Circuit Breakers. Multiply landing distance by 1.8. CHECK IN Avionics and Flight Instruments CHECKISET Passenger Advisory Lights... 4 5. 6. 7. Radar Altimeter 8. 9. SET ..PASS SAFETY Passenger Seats........ CHECK FULL UPRIGHT/OUTBOARD AND POSITIONED AFT OR FWD TO CLEAR EXIT DOORS 10. Engine Synchronizer, 11. Fuel Crossfeed . 42. Ignition senneenesceeON 19. Landing Gear DOWN/LOCKED 14, Antiskid CHECK ON. 15. Landing Lights ON 16. Autopilot and Yew Damper OFF 17. Annunciator Panel... CLEAR 18. Pressurization 19. Speedbrakes MAXIMUM GLIDE EMERGEN! NDING CHECK ZERO DIFFERENTIAL RETRACTED (PRIOR TO 50 FEET) 1. Airspeed... REFER TO MAXIMUM GLIDE SPEED CHART BELOW 2, Flaps. UP 8, Spesdbrakes.. RETRACT 4, Landing Gear z aur uP 5. Transponder EMERGENCY 6. ATC. . seoseneADVISE 7. Passenger Advisory Switon PASS SAFETY 8 Shoulder Heiness SECURE 9. Landing Gear, Speedbrakes and Flaps .. AS REQUIRED MAXIMUM GLIDE SPEED ~ AOA .35 [WEKSHT] 9,500] 10,000] 10,500 | 11,000 [11,500 [12,000 | 12,500 | 13,000 so | 123 | ve | 129 | 132 | 155 | 198 SPEED Kins 4 6.28 FOR TRANIIG PURPOSTS onyFlightSafety ©) EMERGENCY EVAt Nalo)y| 4. Throttle... BOTH OFF 2, LH/RH Engine Fire Switches BOTH PRESS = 3. LH/RH Fire Bottle Armed Switches. " BOTH PRESS, (IF FIRE SUSPECTED) 4, Battery Switch OFF | 5. Airplane Outside. CHECK FOR BEST ESCAPE ROUTE: IF THRU CABIN DOOR, 6. Cabin Door. OPEN! 7. Move away from airplane. ~~ |IF THRU ESCAPE HATCH 6. Escape Hatch REMOVE AND THROW HATCH OUT OF AIRPLANE 7. Move away from airplane. E27 roa T ING PURICITATION II PILOT CHECKLIST—MODEL 550/551 THIS PAGE INTENTIONALLY LEFT BLANK £28