2. Limitations (DA-42) Flashcards
What information can we extract from limitations section of DA42 AFM ?
- Operating limitations
- Instrument marking
- Placards
What is the manoeuvring speed if MAM 42-088 or OAM 42-054 or both incorporated up to 1542 kg ?
120 KIAS
Do not make full or abrupt control surface movement above this speed.
Va
What is the manoeuvring speed if MAM 42-088 or OAM 42-054 or both incorporated above 1542 kg ?
126 KIAS
Do not make full or abrupt control surface movement above this speed.
Va
What is the manoeuvring speed if neither MAM 42-088 nor OAM 42-054 incorporated above 1468 kg up to 1700kg ?
124 KIAS
Do not make full or abrupt control surface movement above this speed.
Va
What is the manoeuvring speed if neither MAM 42-088 nor OAM 42-054 incorporated between1250 kg 1468 kg ?
121 KIAS
Do not make full or abrupt control surface movement above this speed.
Va
Max flaps extended speed in landing configuration ?
111 KIAS
Do not exceed these speeds with the given flap setting.
Vfe (ldg)
Max flaps extended speed in approach configuration ?
137 KIAS
Do not exceed these speeds with the given flap setting.
Vfe (app)
Max landing gear operating speed for extension ?
194 KIAS
Do not operate the landing above this speed
VLOE
Max landing gear operating speed for retraction ?
156 KIAS
Do not operate the landing above this speed
VLOR
Max. landing gear extended speed ?
194 KIAS
Do not exceed this speed with the landing gear extended.
VLE
Minimum control speed airborne ?
68 KIAS
With one engine inoperative keep airspeed above this limit.
VMCA
Max structural cruising speed
155 KIAS
VNO
Do not exceed this speed except in smooth air,and then only with caution
Never exceed speed in smooth air ?
194 KIAS
VNE
Do not exceed this speed in any operation.
Marking speed : White arc ?
56 - 111 KIAS
Operating range with flaps fully extended
Marking speed : green arc ?
62 - 155 KIAS
Normal operating range
Marking speed : yellow arc ?
155 - 194 KIAS
‘Caution range’ - “Only in smooth air”.
Marking speed : Blue radial ?
82 KIAS
VYSE
Best rate of climb speed, single engine
Marking speed : Red radial (low) ?
68 KIAS
VMCA
Minimum control speed, single engine.
Marking speed : Red radial (high) ?
194 KIAS
VNE
Maximum speed for all operations
Max RPM limitations ?
2300 RPM
shown as propeller RPM
Max RPM overspeed, and for how long ?
2500 RPM ( max 20 s)
Max take-off power ?
99 kW at 2300 RPM (100% load)
Max continuous power ?
99 kW at 2300 RPM (100% load)
Fuel temperature :
* Min ?
* Max ?
- Min : -30°C
- Max : +75°C
Oil pressure :
* Min ?
* Max ?
- Min : 1.0 bar
- Max : 6.5 bar
indicated values are corrected for pressure altitude
Oil temperature :
* Min ?
* Max ?
- Min : -30°C
- Max : +140°C
TAE 125-02-99 (MÄM 42-198 carried out)
Coolant temperature :
* Min ?
* Max ?
- Min : -30°C
- Max : +105°C
TAE 125-02-99 (MÄM 42-198 carried out)
Voltage :
* Min ?
* Max ?
- Min : 24.1 V
- Max : 32.0 V
TAE 125-02-99 (MÄM 42-198 carried out)
Amperage :
- Max ?
- Max : 60 A
TAE 125-02-99 (MÄM 42-198 carried out)
Oil quantity per engine :
* Min ?
* Max ?
* Max oil consumption ?
- Min : 4.5 L
- Max : 6 L
- Max oil consumption : 0.1 L/h
per engine
Gearbox temperature Maximum ?
120°C
Propeller diameter :
187 cm
Propeller pitch angle (@ 0.75 R) ?
- 12° : low pitch
- 15° : start lock position
- 81° : feathered position
What is the freezing point of the coolant ?
-36°C (water/ cooler protection)
Max restart altitude ?
- 6000 ft (TAE 125-01 engine installed)
- 8000 ft (TAE 125-02-99 engine installed)
Restart airspeed margin ?
80 to 120 KIAS
Minimum flight mass ?
1250 kg
Max TOM ?
- 1700 kg: MÄM 42-088 not carried out
- 1785 kg: MÄM 42-088 carried out
Maximum Zero Fuel Mass ?
1650 kg
Maximum Landing Mass
1700 kg
Max. load in cabin baggage compartment ?
45 kg
behind rear seats
Max. load in nose baggage compartment ?
30 kg
in fuselage nose
Max. load in baggage extension ?
18 kg
behind cabin baggage compartment
Max. load, cabin baggage compartment and baggage
extension together ?
45 kg
Datum Plane (DP)
2.196 m (forward of the most forward point of the root rib
on the stub wing)
Where can you found center of gravity limitations ?
AFM - 2 . LIMITATIONS - 2.8
What is the effect of exceeding the center of gravity limitations ?
Reduce controllability and stability
What’s approved maneuvres ?
1) All normal flight maneuvers;
2) Stalling (with the exception of dynamic stalling;
3) Lazy Eights, Chandelles, as well as steep turns and similar maneuvers, in which an angle of bank of not more than 60° is attained.
dynamic stalling, lazy eights
Aerobatics, spinning and flight maneuvers with more than 60°
of bank are not permitted in the Normal Category. Stalling
with asymmetric power or one engine inoperative is not
permitted.
Manoeuvering load factors at VA ?
- Positive : 3.8
- Negative : -1.52
Manoeuvering load factors at VNE ?
- Positive : 3.8
- Negative : 0
Manoeuvering load factors with flaps APP or LDG ?
Positive : 2.0
Not specified for negative
What’s happen if we exceed max powerplant load factor and time limits ?
Write the table ( LOAD FACTOR - TIME LIMIT )
will lead to a L/R OIL PRES warning
(LOAD FACTOR / TIME LIMIT)
* -0.2 : 5s
* -0.3 : 4s
* -0.4 : 3s
* -0.5 : 2s
Max operating altitude ?
18000 ft (pressure altitude)
Is it possible to fly into known thunderstorms ?
No, PROHIBITED
What is the minimum operationnal equipment ( flight and navigation instruments Serviceable) that must be aboard in a daytime VFR flight ?
- Airspeed indicator (on G1000 PFD or backup)
- Altimeter (on G1000 PFD or backup)
- Magnetic compass
- 1 Headset, used by pilot in command
What is the minimum operationnal equipment ( Engine instruments Serviceable) that must be aboard in a daytime VFR flight ?
- Fuel qty. (2x)
- Oil press. (2x)
- Oil temp. (2x)
- Coolant temp. (2x)
- Coolant level indicator (2x)
- Gearbox temp. (2x)
- Load (2x)
- Prop. RPM (2x)
- Fuel temp. left & right tank
What is the minimum operationnal equipment ( Other operationnal minimum equipment Serviceable) that must be aboard in a daytime VFR flight ?
- Stall warning system
- Variable elevator stop
- Alternate means for fuel quantity indication (see Section 7.9)
- Safety belts for each occupied seat
- Airplane Flight Manual
What jet fuel can be used for DA42 ?
- JET A-1 (ASTM D 1655),
- JET A (ASTM D 1655),
- JET Fuel No. 3 (GB6537-94),
- JET Fuel No. 3 (China, GB 6537-2006),
- ** JP-8** (MIL-DTL-83133)
Additionally, if MÄM 42-198 is incorporated: - TS-1 (GOST 10227-86),
- TS-1 (Ukraine GSTU 320.00 1U9943011-99),
- and blends of the above listed Jet Fuel grades.
Diesel Fuel (fih bzzaf d ta39idat):
Only if MÄM 42-037 is incorporated: Diesel (EN 590)
Total fuel quantity (main tanks) ?
2 x 26.0 USG
Total fuel quantity (both tanks) ?
2 x 39.7 USG
Total fuel quantity (auxiliary tanks) ?
2 x 13.7 USG
Usable fuel quantity (both tanks) ?
2 x 38.2 USG
Usable fuel quantity (main tanks) ?
2 x 25.0 USG
Usable fuel quantity (Auxiliary tanks) ?
2 x 13.2 USG
Max permissible difference (dissymmetry) ?
5 USG
Is it possible to take-off for a night VFR or IFR with an empty battery ?
NO
check for DAYTIME VFR
Solution : charge the battery without external power supply
Is it possible to fly with the seal on the emergency switch broken in IFR flights ?
NO
The canopy and the passenger door must be blocked by the key lock during operation of the airplane ?
NO
Is it possible to use Portable Electronic Devices (PED) during low visibility approaches ?
NO, PROHIBITED
Can we use the sun visors during T/O and landing ?
No, just during cruise
Can we use GWX 68 weather radar on ground ? and what’s the minimum safe distance ?
NO, 2.8m
Never use it in the hangar