Multi-Engine SOP

ME-001 What is the maximum fuel imbalance for the DA42 Diamond? ME-002 What is the Vmca (Minimum Control Speed Air) for the DA42 Diamond? ME-003 What is the maximum oil consumption per hour for the DA42 Diamond? ME-004 What is the maximum engine starting altitude for the DA42 Diamond (TAE 125-02-99)? ME-005 What are the RPM limits for the DA42 Diamond? ME-006 What is the propeller brand of the DA42 Diamond? ME-007 Which engine oil is used in the DA42 Diamond? ME-008 What are the minimum and maximum oil levels (in liters) for the DA42 Diamond? ME-009 How is the elevator actuated in the DA42 Diamond? ME-010 What are the VA, VMCA, and VNE speeds respectively for the DA42 Diamond (1785 kg / MTOW)? ME-011 When does the landing gear unsafe warning horn activate in the DA42 Diamond when the gear is not down? ME-012 What is the best glide speed for the DA42 Diamond? ME-013 What is the final approach speed with flaps in the LDG position for the DA42 Diamond? ME-014 How does the landing gear system operate in the DA42 Diamond? ME-015 What is the Maximum Take-Off Mass (MTOM) for the DA42 Diamond? ME-016 What is the operating speed range in icing conditions for the DA42 Diamond? ME-017 Which types of fuel are approved for use in the DA42 Diamond? ME-018 What is the airframe structure type of the DA42 Diamond? ME-019 What is the maximum demonstrated crosswind limit for the DA42 Diamond? ME-020 What is the landing gear extension and retraction time for the DA42 Diamond? ME-021 Which engine is installed on ERAH Aviation DA42 Diamond aircraft? ME-022 The speeds for VA (1785 kg), VMCA, VNE, and VLE are respectively: (Ref: POH Page 2 – 4) ME-023 Which engine does the DA42 have? (Ref: POH Page 1 - 24) ME-024 You have an engine failure requiring an emergency landing. Your actions: (Ref: POH Page 3 – 67) ME-025 The DA42 Diamond main battery is _____ and is stored in _____. (Ref: POH Page 7 – 61) ME-026 Following an engine power loss in the DA42 Diamond, engine power was restored by selecting ECU B during the engine troub... ME-027 Ambient fresh air for the cabin in the DA42 Diamond is provided via: (Ref: POH Page 7 – 13) ME-028 The engine speed (RPM) limitations for the DA42 Diamond are: (Ref: POH Page 2 – 7) ME-029 To prevent the propeller pitch locks from engaging during an in-flight engine shutdown in the DA42 Diamond, pilots must ... ME-030 How much total fuel, including unusable fuel, can be carried in the main tanks of the DA42 Diamond? (Ref: POH Page 2 – 2... ME-031 How many fuel injection nozzles are there per engine in the DA42 Diamond? (Ref: POH Page 7 – 39) ME-032 What is the best single-engine rate of climb speed VYSE for the DA42 Diamond? (Ref: POH Page 3 – 5) ME-033 The DA42 Diamond landing gear is described as: (Ref: POH Page 7 – 14) ME-034 Cabin heating and ventilation in the DA42 Diamond are provided as follows: (Ref: POH Page 7 – 25) ME-035 Which IAS is required for a Vy or Vx climb in the DA42 Diamond (at MTOW)? (Ref: POH Page 4A – 3 / SOP p. 15) ME-036 Which engine oil is approved for use in the DA42? (Ref: POH Page 2 – 9) ME-037 What is the maximum permissible propeller overspeed RPM in the DA42 Diamond? (Ref: POH Page 2 – 7) ME-038 The electrical power system of the DA42 is a: (Ref: POH Page 7 – 54) ME-039 What is the maximum load that can be placed in the standard cabin baggage compartment behind the rear seats in the DA42 ... ME-040 What are the maximum landing gear operating speeds for the DA42 Diamond? (Ref: POH Page 2 – 4) ME-041 Minimum RPM required to achieve feathering transition in the DA42 Diamond: (Ref: POH Page 7 – 30) ME-042 What is the DA42 Diamond VFE (Approach - APP)? (Ref: POH Page 2 – 4) ME-043 The DA42 SOP specifies the minimum altitude for OEI operations as ...... (Ref: SOP Page 32) ME-044 What type of propeller is used on the DA42 Diamond? (Ref: POH Page 7 – 29) ME-045 In the DA42 Diamond, the ailerons, elevator, and wing flaps are actuated by: (Ref: POH Page 7 – 4) ME-046 In the event of a complete electrical failure in the DA42 Diamond, how long can you expect emergency battery power to la... ME-047 An attempt to unfeather/restart the engine (TAE 125-02) in the DA42 Diamond may result in an altitude loss of up to ....... ME-048 If a landing gear indicator light fails to show locked after manual extension in the DA42 Diamond, below what maximum ai... ME-049 During Lazy Eights, Chandelles, steep turns, and similar maneuvers in the DA42 Diamond, a bank angle of no more than ...... ME-050 What is the DA42 Diamond VFE (LDG - landing) speed? (Ref: POH Page 2 – 4) ME-051 When does the landing gear warning horn sound in the DA42 Diamond? ME-052 What is the final approach speed with flaps in the APP position for the DA42 Diamond? ME-053 What is the final approach speed with flaps in the UP position for the DA42 Diamond? ME-054 What is the minimum oil quantity for the DA42 Diamond? ME-055 What is the maximum oil quantity for the DA42 Diamond? ME-056 Which of the following correctly lists the DIAMOND DA42 'Landing with Gear Up' checklist items in order? ME-057 Which of the following is the correct sequence for the DIAMOND DA42 'Emergency Descent' checklist? ME-058 Which Emergency checklist in the Twin-Engine (DA42) contains the following items: Cabin heat & defrost OFF / Canopy UNLA... ME-059 In the DA42 'LANDING WITH ONE ENGINE INOPERATIVE' checklist, what are the actions for Adjustable backrests, Safety harne... ME-060 In the DA42 'ENGINE FAILURE DURING FLIGHT AND ENGINE SHUTDOWN' checklist, what are the respective settings for Power, Ai... ME-061 In the DA42 'ENGINE FAILURE DURING TAKE-OFF' checklist (with sufficient runway remaining), what are the items correspond... ME-062 According to the ERAH DA-42 SOP, what is the maximum permissible ground wind limit during ground operations (including T... ME-063 According to the ERAH DA-42 SOP, what is the maximum permissible tailwind component for take-off and landing? ME-064 What are the wing span, total length, and height dimensions of the DA-42 aircraft respectively? (Ref: SOP Page 11) ME-065 According to the DA-42 SOP, which indication must be used to synchronize both engines during normal operations? ME-066 According to the DA-42 SOP, to what % LOAD is climb power set during the 'After Take-Off Checklist' at a safe altitude? ME-067 During ground operations in the DA-42, for how many minutes at most may the engines be operated above idle to prevent ex... ME-068 What is the SOP rule regarding fuel crossfeed on the ground in the DA-42? (Ref: SOP Page 12) ME-069 What is the correct practice during ground operations in the DA-42 to prevent damage to the nose wheel and tires? (Ref: ... ME-070 According to the DA-42 SOP (at MTOW 1785 kg), what are the stall speeds in Flaps UP (Vs) and Flaps LDG (Vso) configurati... ME-071 According to the DA-42 SOP, what is the maneuvering speed (VA) at a mass of 1542 kg? (Ref: SOP Page 15) ME-072 According to the DA-42 SOP, what is the maximum structural cruising speed (VNO / start of the yellow arc)? (Ref: SOP Pag... ME-073 According to the DA-42 SOP, what are the Vr (Rotation) and 50 ft (V50) speeds for a normal take-off (at 1785 kg MTOW) re... ME-074 According to the DA-42 SOP, what is the Cruise Climb airspeed? (Ref: SOP Page 15) ME-075 According to the DA-42 SOP, what is the one-engine-inoperative best angle of climb speed (VXSE)? (Ref: SOP Page 15) ME-076 During the DA-42 exterior preflight inspection (Walk Around), what is checked at the water drain under the right center ... ME-077 During the DA-42 exterior inspection, what action is performed via the gascolator located at the underside of each engin... ME-078 What is the standard engine starting sequence in the DA-42 and the reason for it? (Ref: SOP Page 18) ME-079 After the 'GLOW' annunciation extinguishes before engine start in the DA-42, what is the maximum starter engagement time... ME-080 During engine start in the DA-42, if oil pressure does not move into the green range within how many seconds must the en... ME-081 During the ECU TEST procedure in the DA-42 'Before Take-Off Checklist', what action is performed and what is observed? (... ME-082 How is the VOTER switch (ECU A / AUTO / ECU B) test performed during the DA-42 'Before Take-Off Checklist'? (Ref: SOP Pa... ME-083 During ground warm-up in the DA-42, what minimum oil temperature (°C) must be reached before advancing the power levers ... ME-084 According to the DA-42 SOP, what are the minimum oil temperature, coolant temperature, and gearbox temperature (°C) requ... ME-085 During the DA-42 normal take-off procedure, when is the landing gear selected UP? (Ref: SOP Page 21) ME-086 According to the DA-42 SOP, what are the power setting and target airspeed on the downwind leg of the traffic pattern? (... ME-087 According to the DA-42 SOP, what actions and target airspeed are used abeam the touchdown point on downwind in the traff... ME-088 According to the DA-42 SOP, what is the target airspeed on the base leg and during the turn to final approach? (Ref: SOP... ME-089 According to the DA-42 SOP, what is the correct sequence and target airspeed for the Go-Around (Balked Landing) procedur... ME-090 According to the DA-42 SOP, how long is it recommended to run the engines at IDLE before shutdown to allow turbocharger ... ME-091 According to the DA-42 SOP, above what minimum altitude above ground level (AGL) must all training maneuvers (Steep Turn... ME-092 According to the DA-42 SOP, what are the entry airspeed, bank angle, and initial power setting for the Steep Turn maneuv... ME-093 According to the DA-42 SOP, in what configuration and at what airspeed is the Slow Flight maneuver flown? (Ref: SOP Page... ME-094 According to the DA-42 SOP, what is the maximum bank angle permitted if turns are performed during Slow Flight? (Ref: SO... ME-095 According to the DA-42 SOP, how must power be reduced during the deceleration phase of a Power-Off Stall and why? (Ref: ... ME-096 According to the DA-42 SOP, during a Power-On Stall (Clean configuration), what power setting and pitch attitude are app... ME-097 According to the DA-42 SOP, what is the primary safety rule regarding One Engine Inoperative (OEI) training maneuvers? (... ME-098 When practicing a simulated engine failure (Zero Thrust) in the DA-42, to what setting is the power lever of the simulat... ME-099 Which engine is the 'Critical Engine' on the DA-42 and what is the aerodynamic reason for it? (Ref: SOP Page 32) ME-100 During One Engine Inoperative (OEI) flight in the DA-42, what bank angle toward the operating engine and slip/skid indic... ME-101 What airspeed range and actions are required when unfeathering and restarting a feathered engine in flight in the DA-42?... ME-102 According to the DA-42 SOP, what are the entry airspeed and engine power settings for the Vmca Demonstration maneuver? (... ME-103 According to the DA-42 SOP, upon the FIRST occurrence of which indication must recovery from a Vmca Demonstration be ini... ME-104 According to the DA-42 SOP, what is the correct control input during recovery from a Vmca Demonstration? (Ref: SOP Page ... ME-105 In the DA-42 G1000 system, which alert level is accompanied by a continuous repeating aural tone and flashing red text? ... ME-106 On the DA-42 G1000 PFD, above what coolant temperature (°C) does the red 'L/R ENG TEMP' Warning annunciation illuminate?... ME-107 On the DA-42 G1000 PFD, above what engine oil temperature (°C) does the red 'L/R OIL TEMP' Warning annunciation illumina... ME-108 On the DA-42 G1000 PFD, below what oil pressure (bar) does the red 'L/R OIL PRES' Warning annunciation illuminate? (Ref:... ME-109 On the DA-42 G1000 PFD, above what gearbox temperature (°C) does the red 'L/R GBOX TEMP' Warning annunciation illuminate... ME-110 On the DA-42 G1000 PFD, above what fuel temperature (°C) does the red 'L/R FUEL TEMP' Warning annunciation illuminate? (... ME-111 On the DA-42 G1000 PFD, above what alternator output current (Amps) does the red 'L/R ALTN AMPS' Warning annunciation il... ME-112 On the DA-42 G1000 PFD, below what usable fuel quantity (US Gallons) in the respective main tank does the amber 'L/R LOW... ME-113 On the DA-42 G1000 PFD, below what voltage does the amber 'L/R VOLTS LOW' Caution annunciation illuminate? (Ref: SOP Pag... ME-114 What do the amber 'PITOT FAIL' and 'STALL HT FAIL' Caution annunciations on the DA-42 G1000 PFD indicate respectively? (... ME-115 In the DA-42 G1000 system, if both 'L/R ECU A FAIL' and 'L/R ECU B FAIL' illuminate on the same engine in flight, what d... ME-116 According to the DA-42 SOP, if an engine failure occurs during the take-off roll before reaching Vmca (or with sufficien... ME-117 According to the DA-42 SOP, what steps are followed during a Go-Around / Balked Landing with One Engine Inoperative (OEI... ME-118 What is the correct emergency procedure for an 'Engine Fire on Ground' in the DA-42? (Ref: SOP Page 59) ME-119 In the event of an 'Electrical Fire in Flight' in the DA-42, which switches are turned OFF after setting the Emergency S... ME-120 During the 'Manual Extension of Landing Gear' procedure in the DA-42, below what airspeed must the aircraft be kept and ... ME-121 If the 'DOOR OPEN' annunciation illuminates in flight in the DA-42, below what airspeed should the aircraft be reduced a... ME-122 If both alternators fail in flight (Dual Alternator Failure) in the DA-42, what actions are taken to conserve battery po... ME-123 If a high coolant temperature ('L/R ENG TEMP') warning occurs in flight in the DA-42, what should be checked and perform... ME-124 When a high fuel temperature ('L/R FUEL TEMP') warning occurs in flight in the DA-42, what action is taken to reduce the... ME-125 On the DA-42 G1000 airspeed tape, what are the speed ranges for the White Arc, Green Arc, and Yellow Arc respectively? (...