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thereafter 1400 RPM
END OF CHECKLIST
Page 4B - 30 Rev. 5 15-Nov-2007 Doc. No. 7.01.05-E
4B.9 LANDING WITH HIGH LANDING MASS
CAUTION
Damage of the landing gear can result from a hard landing with a flight mass above the maximum landing mass.
NOTE
If M.M 42-088 is carried out, a landing with a mass between 1700 kg (3748 lb) and 1785 kg (3935 lb) is admissible. It constitutes an abnormal operating procedure. A "Hard Landing Check" is only required after a hard landing, regardless of the actual landing mass. Refer to Section 4A.6.11 - APPROACH & LANDING for landings with a mass up to 1700 kg (3748 lb).
Perform landing approach according to Section 4A.6.11 - APPROACH & LANDING, but maintain an increased airspeed during final landing approach.
Approach speed .......................... min. 82 KIAS with FLAPS APP min. 86 KIAS with FLAPS UP
Final approach speed...................... min. 78 KIAS with FLAPS LDG
Minimum speed on go-around ............... 82 KIAS
END OF CHECKLIST
Doc. No. 7.01.05-E Rev. 5 15-Nov-2007 Page 4B - 31
' 4B.10 L/R FUEL TRANSFER FAIL (IF AUX. TANKS ARE INSTALLED)
' If the fuel quantity in a main tank does not increase during fuel transfer:
' 1. Switch OFF both fuel transfer pumps. '
' CAUTION ' An imbalance in the auxiliary tanks is approved when the ' imbalance in the main tanks is less than 1 US gal (3.8 liters).
'
' 2. Check fuel imbalance in the main tanks; use crossfeed function to keep the LH
' and RH main tank imbalance within the permissible limit of 1 US gal (3.8 liters).
' 3. Switch the remaining fuel pump ON.
' 4. Use crossfeed function to keep the LH and RH main tank imbalance within the
' permissible limit of 1 US gal (3.8 liters).
'
'
' END OF CHECKLIST
Page 4B - 32 Rev. 5 15-Nov-2007 Doc. No. 7.01.05-E
CHAPTER 5
PERFORMANCE
Page
5.1 INTRODUCTION .......................................5-2
5.2 USE OF THE PERFORMANCE TABLES AND DIAGRAMS ......5-2
5.3 PERFORMANCE TABLES AND DIAGRAMS..................5-3
5.3.1 AIRSPEED CALIBRATION...........................5-3
5.3.2 FUEL FLOW DIAGRAM .............................5-6
5.3.3 INTERNATIONAL STANDARD ATMOSPHERE...........5-7
5.3.4 STALLING SPEEDS................................5-8
5.3.5 WIND COMPONENTS ..............................5-9
5.3.6 TAKE-OFF DISTANCE.............................5-10
5.3.7 CLIMB PERFORMANCE - TAKE-OFF CLIMB ...........5-17
5.3.8 CLIMB PERFORMANCE - CRUISE CLIMB .............5-20
5.3.9 ONE ENGINE INOPERATIVE CLIMB PERFORMANCE ...5-23
5.3.10 CRUISING (TRUE AIRSPEED TAS) .................5-26
5.3.11 LANDING DISTANCE.............................5-28
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