ELEC EMER CONFIGPNF FL 260 ALL AC BUSES FAULT ELEC EMER LAND ASAP ECAM ACTIONS DECISION CONFIGURATION LANDING GEAR EXTENSION FINAL APPR

Transcription

1 ELEC EMER CONFIG FL 260 ELEC EMER LAND ASAP ECAM ACTIONS ALL AC BUSES FAULT CONFIGURATION LANDING GEAR EXTENSION FINAL APPR LANDING & DECELERATION A330 - Version 02a

2 WEATHER WEATHER LDG DIST OPERATIONAL AND OPERATIONAL AND COMMERCIAL CONSIDERATIONS CM1 FLIES THE AIRCRAFT LOSS OF AP, A/THR DETECTION NAVIGATES LAND ASAP Short term decision CONSIDER AUTOMATION USE 1. ELEC EMER CONFIG COMMUNICATES MAYDAY ECAM ACTIONS ECAM PROCEDURE SYSTEM DISPLAY RR & PW : GE : USE SUMMARY.....CRUISE part RETURN TO NORMAL TASK SHARING, or SUMMARY NOTIFY ATC PURSER / PAX PURSER / PAX OPS

3 2. APPROACH PREPARATION ECAM...REVIEW SUMMARY...USE FMGS.PREPARE APPR BRIEFING.....PERFORM FMGS PREPARATION : Done upon request STANDARD + MANUAL INSERTION OF VAPP APP BRIEFING : STANDARD + QRH QRH 1.00 ELEC EMER CONFIG summary : APP, LDG & G/A parts

4 For slats extension : LAND RECOVERY..ON FLIES THE AIRCRAFT LOSS OF AP 3. APPROACH ECAM ACTIONS Approach synthesis The Land recovery p/b Removes non necessary loads (AP1, remaining fuel pump, Radar, HF, ADR) Restores equipment required for landing (SFCC 1, LGCIU 1, BSCU 1, ILS1, speed limits) FLIGHT IS FROZEN TO PERMIT THE PROCEDURE APPLICATION ON THE M/FTD

5 ELEC EMER CONFIG Electrical Emergency configuration = loss of all AC BUSES It may be caused by : the loss of one engine and the failure of the opposite generator OR the loss of all GEN OR the loss of all engines simultaneous loss of all GEN suspect a short-circuit Probability of a successful APU GEN coupling is low Note: The EMER GEN is driven by the Green hydraulic system and powered by the Engine Driven Pump in this case

6 WEATHER WEATHER LDG DIST OPERATIONAL AND OPERATIONAL AND COMMERCIAL CONSIDERATIONS CM1 FLIES THE AIRCRAFT LOSS OF AP, A/THR DETECTION NAVIGATES LAND ASAP Short term decision CONSIDER AUTOMATION USE ENG THRUST LOCKED Single Chime (every 5 sec) Move the thrust levers to the actual thrust position COMMUNICATES MAYDAY 1. ELEC EMER CONFIG ECAM ACTIONS ECAM PROCEDURE SYSTEM DISPLAY RETURN TO NORMAL TASK SHARING RR & PW : GE : USE SUMMARY.....CRUISE part, or SUMMARY NOTIFY ATC PURSER / PAX PURSER / PAX OPS

7 ECAM PROCEDURE Monitor FUEL page fuel is fed from one side only (L FUEL PUMP 2 or STBY R PUMP 2) Thrust control : EPR mode (normal situation) Overhead panel N1 rated mode A330 RR & PW

8 WEATHER WEATHER LDG DIST OPERATIONAL AND OPERATIONAL AND COMMERCIAL CONSIDERATIONS CM1 FLIES THE AIRCRAFT LOSS OF AP, A/THR DETECTION NAVIGATES LAND ASAP Short term decision CONSIDER AUTOMATION USE 1. ELEC EMER CONFIG COMMUNICATES MAYDAY Monitor FUEL page ECAM ACTIONS ECAM PROCEDURE SYSTEM DISPLAY USE SUMMARY.....CRUISE part fuel is fed from one side only RETURN (L FUEL TOPUMP NORMAL 2 or STBY TASKRSHARING PUMP 2), or SUMMARY Standby status : NOTIFY ATC PURSER / PAX PURSER / PAX OPS RR & PW : GE : A330 GE

9 SYSTEM DISPLAY Optional Only EWD available : If needed, analyse SYSTEM page displayed on the upper ECAM screen: OTHER SYSTEM PAGES ELEC CONFIRM. CLEAR PRESS ELEC key on ECP PRESS and HOLD ELEC PAGE DISPLAYED....ANALYSE REQUEST.. CLEAR ELEC? PRESS key on ECP......RELEASE

10 To display the status : CONFIRM READ ANNOUNCE? key on ECP.PRESS and HOLD QRH 1.00 ELEC EMER CONFIG SYS REMAINING Status overflow : PAGE release the key on ECP and push it again within 2 sec to display the next page Observe the ECAM MEMO: QRH 1.00 Compute the LDG DIST with the SUMMARY, according to the estimated weight at DEST Review FCOM 3.02 procedure (If time permits)! Important note regarding fuel consumption speed indication reliability FCOM

11 USE OF SUMMARY E/WD PROC 1 LR 3 5 XX VAPP IN CRZ 2 APP PREP 7 4 APP 8 6 BRIEFING

12 USE OF SUMMARY E/WD PROC 1 LR 3 5 XX VAPP IN CRZ 2 APP PREP 7 4 APP 8 6 BRIEFING

13 APPROACH SYNTHESIS Approach flown manually with raw data : no AP ALTN LAW FD A/THR CONF 1 CONF 2 GO AROUND NO GEAR RETRACTION FINAL APPR NO AUTO CALLOUTS CONF 3 LANDING GEAR GRAVITY EXTENSION DIRECT LAW MANUAL PITCH TRIM USE LANDING & DECELERATION BE AWARE OF : NO REVERSER NO NWS NO AUTO BRK PARTIAL LOSS OF GRND SPOILERS