27.01B
ABNORMAL AND EMERGENCY PROCEDURES
A340
15 FEB 13
QUICK REFERENCE HAND BOOK
LANDING WITH SLATS OR FLAPS JAMMED (Cont'd) If FLAPS jammed > 0:
MAINTAIN SLATS/FLAPS CONFIGURATION Recommended speed for diversion: MAX SPEED -10 kt Increased fuel consumption. Note:
‐ In case the SPD LIM flag is displayed on the PFD, use the MAX SPEED displayed on the ECAM status page ‐ In case of a go-around with CONF FULL selected, the L/G GEAR NOT DOWN warning is triggered at landing gear retraction ‐ In some cases, MAX SPEED -10 KT may be a few knots higher than the VFE. In this situation, pilots may follow the VFE. MAX SPEED
Flaps
F=0
Slats
S=0
NO LIMITATION
0
255 kt
1
215 kt
0
215 kt
1
2
F>3
196 kt
186 kt
180 kt
205 kt
CAUTION For flight with SLATS or FLAPS extended, fuel consumption is increased. Refer to the fuel flow indication. As a guideline, determine the fuel consumption in clean configuration at the same altitude without airspeed limitation (e.g. From ALTERNATE FLIGHT PLANNING tables) and multiply this result by the applicable Fuel Penalty Factor provided in the QRH Refer to FPE-FPF Fuel Penalty Factors Tables , to obtain the fuel penalty required to reach the destination in the current configuration.
DGA MSN 0075 F-RAJA
ABNORMAL AND EMERGENCY PROCEDURES
A340
QUICK REFERENCE HAND BOOK
27.02A 15 FEB 13
LOW ENERGY WARNING The ″SPEED SPEED SPEED″ synthetic voice is triggered every 5 s, each time the aircraft’s energy becomes lower than a threshold under which thrust shall be increased.
"SPEED SPEED SPEED" Increase the thrust until the warning stops and, depending on the circumstances, adjust the pitch accordingly.
DGA MSN 0075 F-RAJA
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ABNORMAL AND EMERGENCY PROCEDURES
A340
QUICK REFERENCE HAND BOOK
27.04A 15 FEB 13
SIDESTICK / RUDDER PEDALS STIFF Even if the autopilot is disengaged, the sidesticks and/or the rudder pedals may be stiff. This may affect either: ‐ Both sidesticks (CAPT and F/O) at the same time, but not the rudder pedals or ‐ One sidestick and the rudder pedals at the same time. The piloting technique remains the same: The aircraft remains responsive. However, the flight crew should keep in mind that they may need to use extra force on the sidesticks and/or the rudder pedals.
AP DISENGAGEMENT................................................................................CONFIRM CONSIDER TRANSFERRING CONTROL TO PNF For decrab, rollout, or engine failure: BE PREPARED TO APPLY EXTRA FORCE ON RUDDER PEDAL
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PRELIMINARY PAGES RECORD OF AMENMENTS
1/2 15 FEB 13
A340 QUICK REFERENCE HAND BOOK
SEQ
REVISION DATE
INSERTED INSERTED DATE
BY
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18 NOV 11
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25 NOV 11
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19 MAR 12
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30 MAR 12
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03 APR 12
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09 MAY 12
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24 JUL 12
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03 AUG 12
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17 DEC 12
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01 JAN 13
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15 FEB 13
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DGA A340 FOR A/C: F-RAJA
PRELIMINARY PAGES RECORD OF AMENMENTS
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PRELIMINARY PAGES LIST OF EFFECTIVE OPERATIONS ENGINEERING BULLETIN
Identification
1/2 15 FEB 13
Title
OEB20 Issue 2
Erroneous Vertical Profile During RNAV, LOC and LOC B/C Approaches ECAM Entry None
OEB26 Issue 1
Erroneous Radio Altimeter (RA) Height Indication
OEB44 Issue 1
ECAM Entry None Variations of the engine N1 parameters associated with oscillations of the flow control valves of the packs on the ground None ECAM ENTRY
DGA MSN 0075 F-RAJA
A340
QUICK REFERENCE HAND BOOK
PRELIMINARY PAGES LIST OF EFFECTIVE OPERATIONS ENGINEERING BULLETIN
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DGA MSN 0075 F-RAJA
2/2 15 FEB 13
A340
QUICK REFERENCE HAND BOOK (1)
M
R R R R R R R R R R R R R R R R R R
R
R
PRELIMINARY PAGES LIST OF EFFECTIVE SECTIONS/SUBSECTIONS
Localization PLP-LEOEB PLP-LESS PLP-LETDU GEN ABN-22 ABN-24 ABN-25 ABN-26 ABN-27 ABN-28 ABN-29 ABN-30 ABN-31 ABN-32 ABN-34 ABN-70 ABN-80 NP-NP NP-NCL FPE-SPD FPE-FPF FPE-IFL-MAT FPE-IFL-VAP FPE-IFL-LD FPE-IFL-VAF FPE-IFL-24 FPE-IFL-27 FPE-IFL-27A FPE-IFL-28 FPE-IFL-29 FPE-IFL-30 FPE-IFL-32 FPE-IFL-34 FPE-IFL-36 FPE-IFL-70 FPE-OEI FPE-TEI FPE-AEO FPE-CAB FPE-OPD OPS
Subsection Title LIST OF EFFECTIVE OPERATIONS ENGINEERING BULLETIN LIST OF EFFECTIVE SECTIONS/SUBSECTIONS LIST OF EFFECTIVE TEMPORARY DOCUMENTARY UNITS General Auto-Flight Electrical Equipment Fire Protection Flight Controls Fuel Hydraulic Ice and Rain Protection Indicating / Recording Systems Landing Gear Navigation Engines Miscellaneous Normal Procedures Normal Checklist Speeds Fuel Penalty Factors Runway Condition Assessment Matrix for Landing VAPP Determination without Failure Landing Distance without Failure VAPP Determination with Failure Landing Distance with Electrical System Failure Landing Distance with Flight Controls System Failure Landing Distance with Slats and Flaps System Failure Landing Distance with Fuel System Failure Landing Distance with Hydraulic System Failure Landing Distance with Anti Ice System Failure Landing Distance with Brake System Failure Landing Distance with Navigation System Failure Landing Distance with Bleed System Failure Landing Distance with Engine System Failure One Engine Inoperative Two or Three Engines Inoperative All Engines Operative Flight Without Cabin Pressurization Operating Data Operational Data
(1) Evolution code : N=New, R=Revised, E=Effectivity, M=Moved
DGA MSN 0075 F-RAJA
1/2 15 FEB 13
Rev. Date 15 FEB 13 15 FEB 13 15 FEB 13 15 FEB 13 15 FEB 13 15 FEB 13 15 FEB 13 15 FEB 13 15 FEB 13 15 FEB 13 15 FEB 13 15 FEB 13 15 FEB 13 15 FEB 13 15 FEB 13 15 FEB 13 15 FEB 13 15 FEB 13 01 JAN 13 15 FEB 13 01 JAN 13 01 JAN 13 30 MAY 12 03 AUG 12 10 JUL 12 30 MAY 12 30 MAY 12 30 MAY 12 30 MAY 12 30 MAY 12 30 MAY 12 30 MAY 12 30 MAY 12 30 MAY 12 30 MAY 12 07 APR 11 07 APR 11 15 FEB 13 07 APR 11 01 JAN 13 15 FEB 13
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QUICK REFERENCE HAND BOOK
PRELIMINARY PAGES LIST OF EFFECTIVE SECTIONS/SUBSECTIONS
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DGA MSN 0075 F-RAJA
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QUICK REFERENCE HAND BOOK (1)
M
R
PRELIMINARY PAGES LIST OF EFFECTIVE TEMPORARY DOCUMENTARY UNITS
Localization ABN-25 Cockpit Door Fault Criteria: (D44099 or 25-4181 or 25-3161)
DU Title
1/2 15 FEB 13
DU identification
DU date
00013675.0001001
15 FEB 13
Impacted DU: 00010505 Cockpit Door Fault Reason for issue:
Subsequent to a few reported cases of reinforced Cockpit door latch jams, this Temporary DU is issued to further explain the switch operation, and provide the following applicable procedures, in the event of a Cockpit door latch jam: ‐ For door opening: Ensure that the switch is maintained in the UNLOCK position, until the door is fully open. ‐ For door closing: Ensure that the switch is released to the NORM position before closing the door. ‐ To open and close the door, in case of Cockpit door FAULT, to prevent possible electrical latch overheating that could damage the latches. ‐ To open and close the door, in case of Cockpit door FAULT, to prevent possible electrical latch overheating that could damage the latches. This Temporary DU will be cancelled when a final solution is found to prevent the latches from overheating. (1) Evolution code : N=New, R=Revised, E=Effectivity
DGA MSN 0075 F-RAJA
