Phenom 100 Limitations

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shaunmcquain
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80182
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Phenom 100 Limitations
Updated:
2011-06-24 13:19:41
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Phenom Limitations
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Phenom 100 Limitations
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  1. Max Ramp Weight
    10,516
  2. Max TKO WT
    10,472
  3. Max LDG WT
    9,766
  4. Max Zero Fuel WT
    8,444
  5. Yaw Damper must be engaged:
    1.
    2.
    • > 25,000'
    • > 250 KIAS
  6. Vlo
    180 Kts
  7. Vlo EMER
    250 Kts
  8. Vle
    275 kts
  9. Vmc (highest T/O)
    97 KIAS
  10. Vmc (LDG)
    86 KIAS
  11. Vmc (LDG in Ice)
    97 KIAS
  12. Mmo
    .70 Mach
  13. Vmo
    275 Kts
  14. Vo
    Maneuvering 186 KIAS
  15. Max Flaps Extended:
    Y/D Ops
    Y/D Inop
    • Y/D Ops 15,000'
    • Y/D INOP 12,000'
  16. Max Tire Ground Speed
    139 Kts
  17. Max Load:
    F/U
    F/D (1, 2, Full)
    • F/U +3.27g
    • F/D +2.00g
  18. Maximum Load:

    Wardrobe:
    Lav Cab:
    AFT Bag:
    FWD Bag:
    • Wardrobe - 66 lbs.
    • Lav Cab - 33 lbs.
    • Aft Bag - 353 lbs.
    • Fwd Bag - 66 lbs.
  19. Max Runway Slope
    -2% to +2%
  20. Max TKO/LDG Tailwind
    10Kts
  21. Max Demonstrated X-Wind
    17kts
  22. Battery Start Voltage/After start
    • Start 24V
    • Ater Start 23.8V
  23. Battery Charging Voltage
    27V
  24. Generator Load Ground/ In Flight
    • Ground 250A each
    • In Flight 300A each below FL340
  25. GPU Limits:
    Voltage -
    Current -
    Min. For Battery Charging
    • Voltage - 25V-29V
    • Current - 800A-1000A
    • Charge - 27V
  26. What Looks at GPU for proper Polarity and volts?
    GCU 1
  27. Max Fuel Gal. (lbs.)
    • 425 gal.
    • 2850 lbs.
    • Includes unusable
  28. Usable Fuel Per Tank - gal. (lbs.)
    • 209 gal.
    • 1,403 lbs.
  29. Max Fuel Imbalance
    220 lbs.
  30. Minimum Fuel Tank Temp.
    -37c
  31. Max Fuel Tank Temp:
    Ground
    In Flight
    • Ground 52c
    • In Flight 80c
  32. Allowed Fuel Types
    • Jet A
    • Jet A1
    • JP 8
  33. Can you fuel from One Side
    Yes, up to 60% full f/ one side provided gravity txfr button is open
  34. FUEL 1(2) LO LEVEL comes on when
    </= 198 lbs.
  35. Starter Limits:
    1
    2
    3
    4
    Then
    • 1 - 60 sec.
    • 2 - 60 sec.
    • 3 - 15 min.
    • 4 - 30 min.
    • Then - Repeat
  36. Max Differential Pressure
    Max Differential Over Pressure
    Max Neg. Pressure
    Max Differential Pressure for T/O and LDG
    • 8.3 PSID
    • 8.6 PSID
    • -0.4
    • -0.2
  37. Min. Temp and A/S to operate Wing/Stab anti-ice
    • -40c
    • 150 KIAS
  38. A/Ice:
    1. If SAT/TAT is between _ & _ then _ & _ _
    5c & 10c then Eng. 1 & 2 Switches on
  39. During Cold Starts run engines _ min. after reaching _c
    • 3 min.
    • 14c
  40. SAT/TAT < 5c or ice formation
    • WSHLD 1 & 2 - ON
    • ENG 1 & 2 - On
    • Wing/Stab Switch - ON
  41. When is the A/P prohibited
    • 1. SVR Ice
    • 2. Unusual control force when checked
    • 3. Indication of Frequent re-trim in St/Level Flight
  42. Auto Pilot:
    - Minimum engagement Alt.
    - S.E.
    - Min. Use
    - Allowable Alt. Loss
    • 500' AGL
    • 1000' AGL
    • Twice Allowable Altitude Loss 108', 50' below MDA, or 195' whichever is higher
    • 54' AGL
  43. Max Thrust:
    Time
    Max ITT
    N2
    N1
    Oil Pressure
    Oil Temp.
    • 10 min. (intended for single engine)
    • 845c
    • 100.4%
    • 100%
    • n/a
    • n/a
  44. TKO Thrust:
    Time
    Max ITT
    N2
    N1
    Oil Pressure
    Oil Temp.
    • 5 min.
    • 830c
    • 100.4%
    • 100%
    • 170psi
    • 14c-130c
  45. Max Cont. Climb:
    Time
    Max ITT
    N2
    N1
    Oil Pressure
    Oil Temp.
    • n/a
    • 830c
    • 100.4%
    • 100%
    • 170psi
    • 14c-130c
  46. Ground Idle:
    N2
    Oil Pressure
    Oil Temp.
    • 54%
    • 170psi
    • -40c to 130c
  47. Flight Idle S.L.:
    N2
    Oil Pressure
    Oil Temp.
    • 59%
    • n/a
    • +14c to 130c
  48. Max Start Limitation:
    ITT
    Oil pressure
    Oil Temp
    • 830c can go to 950c for 5 sec
    • 0-275psi
    • -40c
  49. Max Transient:
    ITT
    N2
    N1
    Oil Temp.
    • 830c
    • 102% (20 sec.)
    • 101% (20 sec.)
    • 130c-141c (90 sec.)

    • 862c ITT (for 20 sec. in Norm. & ATR TKO Modes)
    • 845c ITT (for ATR TKO Mode only)
  50. Max TKO Altitude
    10,000'
  51. EICAS "CAB ALTITUDE HI"
    10,000'
  52. When do the PAX O2 masks drop
    14,500' +250'/-500'
  53. O2 psi:
    Green
    White
    Yellow
    • Green - > 1590psi, but </= 1850psi
    • White - > 730psi, but </= 1589psi
    • Yellow - < 730 psi
  54. What does EMER, 100%, and Norm O2 modes mean
    • Emer - 100% O2 plus pos. press. to keep smoke out
    • 100% - 100% O2 all the time
    • Norm - O2 provided as needed
  55. Flaps:

    Pre-mod. Post-mod.
    Deg./ KIAS
    F1
    F2
    F3
    Full
    • Pre-mod
    • F1 10/200
    • F2 26/160
    • F3 36/145
    • Full 36/145

    • Post-mod
    • F1 10/200
    • F2 26/160
    • F3 26/145
    • Full 36/145
  56. Engine Oil:
    Max/Min. Capacity
    4.11qts/3.15qts considering 2 degree slope max
  57. Oil level must be checked within:
    10 min. of engine shutdown
  58. What is the Max allowable oil consumption:
    • .018 gal/hr
    • .18 gal/10 hr period
    • .72 qts/10hr period
  59. What type of oil is allowed:
    • Must comply with MIL-PRF-23699F
    • e.g. BP2380; Mobil 254; Mobil Jet II
  60. What systems are hydraulic
    Gear and Brakes
  61. When must the hydraulic level be checked
    Check every 15 days or next flight w/e is last
  62. When is the hydraulic pump turned on/off
    What is the psig min/max
    When is Hyd. pressure relief
    • On/off - 2400 +/- 50
    • Max psig 3000 +/- 50
    • Relief at 3250psi
  63. The hydraulic pump is _ VDC on _ bus
    28VDC on DC Bus 2
  64. What type of Hydrualic fluid should be used
    Synthetic hydrocabon base MIL-PRF-87257B
  65. The Hydraulic Temp Switch Monitors What to shutoff
    Fluid temp and motor temp to shut off
  66. Tire Pressure:

    Main
    Nose
    • Main - 166-176
    • Nose - 112-122
  67. Required Crew/ requirements
    • 1 pilot
    • Pilot must be in left seat
    • A/P & F/D must be ops for single pilot
    • Must use a headset w/ mounted mic
  68. Fuel:
    Unusable normal
    Unusable Failure of Jet pump & DC Pump
    Fuel Cannot tx when qty reaches what
    • 22 lbs.
    • 91.3 lbs. failed side tank
    • 308 lbs. SE
    • 363 lbs. Dual eng.
  69. Powerplant:
    1. Type
    2. Thrust
    3. Controlled
    4. Max ATR use
    5. Max Ops Temp
    • 1. PW617F-E; F= FADEC E=Embraer
    • 2. Thrust 1696 lbs. per side
    • 3. Controlled via a dual Channel FADEC= full, authority, digetal, engine, control
    • 4. 10 min. after tko
    • 5. ISA +35c
  70. F1 TKO= _ degree pitch ATT
    F2 TKO= _ degree pitch ATT
    • F1 11 degree/9.5 degrees
    • F2 9 degree
  71. 1. A/cond. ops on gnd
    2. Max A/cond. alt.
    3. Pwrd off what bus
    • 1. one gen on or GPU - book says both gens
    • 2. FL410
    • 3. Shed bus
  72. What is the certified climb gradient?
    2% to 1500' ???
  73. What does the "big red button" kill
    • A/P
    • Y/D
    • Trim
    • Pusher
  74. What type batteries do we have?
    Benefits
    Remove
    • Lead Acid
    • no thermil rwy
    • remove @ 0c

    Can remove charge replace attach GPU and charge the other battery
  75. Do we need both batteries to start
    Start Batt pwrs _ bus via _
    Starter cuts
    • Yes, Batt. pwr everything but shed bus
    • Start Batt pwrs DC 1 (2) via QSC (quiet start contactor)
    • 48%-49% N2
  76. How many invertors, pwrs ?, on _ bus
    • 1 invertor
    • powers plugs
    • on shed bus
  77. PED Belts/ON- the ON means
    Turns invertors to power pax plugs on/off
  78. Emerg. bus has?
    • Aviate - ELT, PAX mask, Nac heat
    • Navigate - AHRS1, Mag Light, NAV1
    • Communicate - Audio Panel 1, TXDR1
    • et.al.
  79. W.O.W.
    • Brake cont. sys
    • L/G Cont. lever
    • FADEC (Full Auth. Dig. Eng. Cont.)
    • Elect Sys- On Ground All Buses but Shed; In Flt - Hot, Emer, Central
    • Lights (bags)
    • A/C & Press.
    • Fuel Indication
    • Flaps
    • DCU/GEA
  80. Explain brake system
    Steel brake by wire system like a reastat
  81. How do you check brake wear pins?
    Set P-Brake
  82. If we lose brakes:
    RWY
    E-Brake
    • 50% more rwy
    • 6 full brake apps no A/Skid
  83. On gear retraction what stop wheel spin
    • Nose has pad in well
    • Main auto apply brakes
  84. Describe the Pressurization system
    • 1 outflow valve
    • 1 pressure relief valve

    PRSOV reg. to 28psi +/- 3psi

    Ram air goes through heat exchanger to cool bleed air
  85. How many static wicks
    • 3 times each aileron
    • 2 times top rudder
    • 2 times each elevator
  86. Hydraulic pump is pwrd by _ bus
    central bus
  87. What is the only thing on the central bus
    Hydraulics
  88. Hydraulic pump is controlled by _ bus
    DC Bus 2
  89. De-ice cycle
    Total is 1 min.

    • 6 sec. tail
    • 6 sec. outboard
    • 6 sec. inboard
    • 42 sec. break
  90. What does the electric fuel pump do and at what psi does it kick on
    Backs up the ejector pumps and comes on for start and when fuel lo press < 6psi
  91. DCU- data concentrator unit
    takes info from TKO Pwr, Doors, FMS, ADC, MFD

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