BEFORE START AFTER START

Transcription

1 BEFORE START ENGINE START AFTER START - Version 03

2 1.a. BEFORE START LOADSHEET...CHECK TAKEOFF DATA..... ENTER/REVISE TAKEOFF DATA... XCHECK COCKPIT DOOR...CLOSED SEAT BELTS ADJUST MCDU...PERF TO SEAT BELTS.ADJUST MCDU.F-PLN EXT PWR..OFF ORDER. BEFORE START C/L down to the line BEFORE START down to the line.. PERFORM ANNOUNCE.. BEFORE START C/L down to the line COMPLETED Confirm any takeoff weight limitation. Ask for external power disconnection

3 1.b. BEFORE START NW STRG DISC MEMO.....CHECK WINDOWS and DOORS. CHECK CLOSED THR LEVERS.. IDLE PUSHBACK/START CLEARANCE.OBTAIN WINDOWS.CHECK BEACON ON PARKING BRAKE ACCU PRESS. CHECK PARKING BRAKE. ON ORDER. BEFORE START C/L below the line BEFORE START C/L below the line PERFORM ANNOUNCE.. BEFORE START C/L COMPLETE GROUND CREW COMMUNICATION ESTABLISH CAUTION! DO NOT PERFORM the pushback if NW STRG DISC not displayed on the ECAM MEMO to avoid damages to the nose landing gear. The BRAKE ACCU PRESS must be in the green band When PARKING BRAKE is ON: brake pressure is shown PARK BRK MEMO is displayed

4 ENG START SEL....IGN/START BLEED PRESSURE CHECK ANNOUNCE... STARTING ENGINE 1 MASTER SW 1.ON START VALVE OPENS N2 INCREASES (N3 for RR) IGNITER FUEL FLOW EGT N1..CHECK OIL PRESS START VALVE CLOSE 50% N2 (GE) Between 43% and 48% N2 (PW) 50% N3 (RR) ENG IDLE PARAMETERS..CHECK NORMAL ANNOUNCE... STARTING ENGINE 2 REPEAT START SEQUENCE FOR ENG AUTOMATIC ENGINE START SEQUENCE GE RR PW Start ENG 2 ONCE AVAIL is displayed for ENG 1 XX.X Check BLEED PRESSURE on ECAM page. ECAM ENGINE page

5 ENG START SEL. NORM 3.a. AFTER START End of START sequence : Signal for actions APU BLEED.OFF 1. GND SPLRS ARM 2. RUD TRIM RESET 3. FLAPS SET 4. PITCH TRIM..SET ECAM STATUS. CHECK ECAM DOOR PAGE....CHECK 5. ENG ANTI ICE AS RQRD WING ANTI ICE..AS RQRD ANNOUNCE. CLEAR TO DISCONNECT 6. APU MASTER SW OFF ENG START SEL back to NORM 5 6 Overhead Panel ENGINE WHEEL ECAM Pedestal 2

6 3.b. AFTER START AFTER START C/L NWS TOWING FAULT LT extinguished CHECK Observe the ECAM MEMO: engines started 0 2 t (min.) To stabilize engine hot section temperature: 3 min (GE) / 5 min (PW & RR) / 3 min (RR if engines have been stopped for 1.5 hr or less) minimum at or near IDLE Engine started High power t If icing conditions : GE : RR : PW :

7 ENG START SEL....IGN/START BLEED PRESSURE CHECK ANNOUNCE... STARTING ENGINE 1 2. AUTOMATIC ENGINE START SEQUENCE MASTER SW 1.ON START VALVE OPENS N2 INCREASES Select IGN(N3 for RR) Set ENG master Wait 3 sec. IGNITERSTART switch to ON FUEL FLOW EGT N1..CHECK ENG 1 is started first because it powers the blue hydraulic system, which pressurizes the parking OIL PRESS START brake. VALVE CLOSE 50% N2 (GE) Between 43% and 48% N2 (PW) DO NOT 50% SET N3 the (RR) MASTER switch ON before all amber crosses and messages have disappeared on ENG engine IDLE parameters PARAMETERS..CHECK (upper ECAM display). NORMAL Start ENG 2 ONCE AVAIL is displayed for ENG 1 ANNOUNCE... STARTING ENGINE 2 REPEAT START SEQUENCE FOR ENG 2.. GE RR PW Check BLEED PRESSURE on ECAM page. ECAM ENGINE page

8 ENG START SEL....IGN/START BLEED PRESSURE CHECK ANNOUNCE... STARTING ENGINE 1 2. AUTOMATIC ENGINE START SEQUENCE MASTER SW 1.ON DO START NOT SET VALVE the OPENS MASTER switch ON before EGT amber crosses and messages have disappeared on N2 engine INCREASES parameters (N3 for (upper RR) ECAM display). IGNITER FUEL FLOW EGT ENG 1 is started first because it powers the blue hydraulic system, which pressurizes the parking N1..CHECK brake. OIL PRESS START VALVE Starting CLOSE a hot engine 50% N2 (GE) EEC performs a dry crank to Between (1 st start: 43% EGT>100 C and 48% N2 (PW) reduce engine temperature 50% 2 N3 nd start: (RR) EGT>150 C) ENG IDLE PARAMETERS..CHECK NORMAL Start ENG 2 ONCE AVAIL is displayed for ENG 1 ANNOUNCE... STARTING ENGINE 2 REPEAT START SEQUENCE FOR ENG 2.. GE RR PW Check BLEED PRESSURE on ECAM page. ECAM ENGINE page

9 ENG START SEL....IGN/START BLEED PRESSURE CHECK ANNOUNCE... STARTING ENGINE 1 2. AUTOMATIC ENGINE START SEQUENCE MASTER SW 1.ON START VALVE OPENS N2 INCREASES (N3 for RR) ENG 1 is started first because it powers the blue hydraulic system, which pressurizes the parking IGNITER brake. FUEL FLOW EGT N1 DO NOT SET the MASTER switch ON before..check all amber crosses and messages have disappeared on OIL engine PRESS parameters (upper ECAM display). START VALVE CLOSE 50% N2 (GE) Between 43% and 48% N2 (PW) 50% N3 (RR) ENG IDLE PARAMETERS..CHECK NORMAL Start ENG 2 ONCE AVAIL is displayed ANNOUNCE... STARTING ENGINE 2 REPEAT START SEQUENCE FOR ENG 2.. GE RR for ENG 1 PW Check BLEED PRESSURE on ECAM page. ECAM ENGINE page

10 NORMAL ENGINE IDLE PARAMETERS AT ISA SEA LEVEL GE: N1 about 23% EGT.about 360 C N2 about 63% FF about 550 kg/h (1210 lb/h) PW: FF about 580 kg/h (1280 lb/h) N2 about 59% EPR about 1.010% EGT about 320 C N1 about 23% RR: FF about 820 kg/h (1800 lb/h) N3 about 63% EPR about 1.015% EGT about 380 C N1 about 22.6% N2 about 47% Upper ECAM Lower ECAM

11 ENG START SEL. NORM 3.a. AFTER START End of START sequence : Signal for actions APU BLEED.OFF 1. GND SPLRS ARM Turn APU BLEED OFF just after engine start to avoid ingesting engine exhaust gases. 2. RUD TRIM RESET 3. FLAPS SET 4. PITCH TRIM..SET ECAM STATUS. CHECK ECAM DOOR PAGE....CHECK 5. ENG ANTI ICE AS RQRD WING ANTI ICE..AS RQRD ANNOUNCE. CLEAR TO DISCONNECT 6. APU MASTER SW OFF ENG START SEL back to NORM 5 6 Overhead Panel ENGINE WHEEL ECAM Pedestal 2

12 PITCH TRIM SET Set Takeoff CG on the pitch trim wheel For this purpose, use the actual CG indicated on the ECAM : 4 The Takeoff CG value must be within the green band limits.

13 WHEN ARE ENG & WING ANTI ICE REQUIRED? Engine anti-ice OAT or TAT 10 C with visible moisture in the air, standing water, slush, ice or snow on the taxiways or runways ICING CONDITIONS expected ENG ANTI ICE must be ON Wing anti-ice Prevent ice formation OR Ice accumulation on the wing leading edges OR Ice accumulation on the visual ice indicator or on the windshield wipers WING ANTI ICE recommended CAUTION! In icing conditions, minimise flight duration with the slats extended.

14 FAULT 3.b. AFTER START If nosewheel steering has exceeded 93 AFTER START C/L NWS TOWING FAULT LT extinguished CHECK Observe the ECAM MEMO: FAULT NO GO Maintenance action required engines started 0 2 Illumination of the red oversteer warning light t (min.) To stabilize engine hot section temperature: 3 min (GE) / 5 min (PW & RR) / 3 min (RR if engines have been stopped for 1.5 hr or less) minimum at or near IDLE Engine started High power t If icing conditions : GE : RR : PW :

15 3.b. AFTER START AFTER START C/L NWS TOWING FAULT LT extinguished CHECK Observe the ECAM MEMO: NW STRG still disconnected + at least 1 engine running engines started 0 2 t (min.) To stabilize engine hot section temperature: 3 min (GE) / 5 min (PW & RR) / 3 min (RR if engines have been stopped for 1.5 hr or less) minimum at or near IDLE Engine started High power t If icing conditions : GE : RR : PW :

16 3.b. AFTER START AFTER START C/L NWS TOWING FAULT LT extinguished CHECK Observe the ECAM MEMO: If icing conditions > 30min OR Significant engine vibration engines started 0 2 On ground, perform an ENGINE RUN-UP (60% N1 minimum) for approximately 30 sec prior to higher thrust in order to centrifuge any ice from the engine s rotating parts t (min.) ENG ANTI ICE ON To stabilize engine hot section temperature: Continuous ignition automatically selected 3 min (GE) / 5 min (PW & RR) / 3 min (RR if engines have been stopped for 1.5 hr or less) minimum at or near IDLE Engine started High power t If icing conditions : GE : RR : PW :

17 3.b. AFTER START AFTER START C/L NWS TOWING FAULT LT extinguished CHECK Observe the ECAM MEMO: engines started On ground, perform an ENGINE RUN-UP (50% N1 If icing conditions recommended) for 10 sec prior to take off t (min.) order to 0 & centrifuge any ice from 2the engine s rotating parts OAT 1 C If holding on the ground, perform it once every hour To stabilize engine hot section temperature: 3 min (GE) / 5 min (PW & RR) / 3 min (RR if engines have been stopped for 1.5 hr or less) minimum at or near IDLE Engine started High power t If icing conditions : GE : RR : PW :

18 3.b. AFTER START AFTER START C/L NWS TOWING FAULT LT extinguished CHECK Observe the ECAM MEMO: If icing conditions & engines OAT started 3 C On ground, perform PERIODIC ENGINE RUN-UP (50% N1 recommended) to centrifuge any ice from the engine s rotating parts at intervals not greater than 15 min. t (min.) Take off should be preceded by a STATIC RUN-UP (50% N1 0 recommended) with2 observation of all primary parameters ENG ANTI ICE ON To stabilize engine hot section temperature: Continuous ignition automatically selected 3 min (GE) / 5 min (PW & RR) / 3 min (RR if engines have been stopped for 1.5 hr or less) minimum at or near IDLE Engine started High power t If icing conditions : GE : RR : PW :