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T-38

  1. GROUND STEADY STATE
    Start RPM
    None
  2. GROUND STEADY STATE
    RPM IDLE and (Fluctuation)
    46.5-49.5 (46.5-49.5)
  3. GROUND STEADY STATE
    RPM MIL and (Fluc)
    99-100.5 (99-100.5)
  4. GROUND STEADY STATE
    RPM MAX and (Fluc)
    99-100.5 (99-100.5)
  5. GROUND STEADY STATE
    EGT at Start
    • 925(MAX)
    • *845 Abort the start
  6. GROUND STEADY STATE
    EGT at Idle (Fluc)
    None
  7. GROUND STEADY STATE
    EGT at MIL (Fluc)
    630-645
  8. GROUND STEADY STATE
    EGT at MAX (fluc)
    630-645
  9. GROUND STEADY STATE
    Nozzle at Start (flux)
    None
  10. GROUND STEADY STATE
    Nozzle at Idle (fluc)
    77-92 (None Allowed)
  11. GROUND STEADY STATE
    Nozzle MIL (Fluc)
    0-20 (+-3)
  12. GROUND STEADY STATE
    Nozzle MAX (fluc)
    50-85 (+-3)
  13. GROUND STEADY STATE
    Fuel Flow at Start (Fluc)
    360 (MAX)
  14. GROUND STEADY STATE
    Fuel Flow at Idle (Fluc)
    400-600 Std Day (+-25)
  15. GROUND STEADY STATE
    Fuel Flow at MIL (Fluc)
    2100-2500 Sea Lvl (+-50)
  16. GROUND STEADY STATE
    Fuel Flow at MAX (Fluc)
    No Max Fuel Flow (+-50)
  17. GROUND STEADY STATE
    Oil Pressure at Start (Fluc)
    None
  18. GROUND STEADY STATE
    Oil Pressure at Idle (Fluc)
    5-20 (+-2)
  19. GROUND STEADY STATE
    Oil Pressure at MIL (Fluc)
    20-55 (+-2)
  20. GROUND STEADY STATE
    Oil Pressure at MAX (Fluc)
    20-55 (+-2)
  21. GROUND STEADY STATE
    Maximum time allowed in MIL
    30min
  22. GROUND STEADY STATE
    Maximum time allowed in MAX
    5min
  23. FLIGHT STEADY STATE
    RPM at START (fluc)
    None
  24. FLIGHT STEADY STATE
    RPM at IDLE (fluc)
    None
  25. FLIGHT STEADY STATE
    RPM at MIL (fluc)
    99-104 (+-1)
  26. FLIGHT STEADY STATE
    RPM at MAX (fluc)
    99-104 (+-1)
  27. FLIGHT STEADY STATE
    EGT at START (fluc)
    • 925 (Max)
    • *845 Abort start
  28. FLIGHT STEADY STATE
    EGT at IDLE (fluc)
    None
  29. FLIGHT STEADY STATE
    EGT at MIL (fluc)
    630-645
  30. FLIGHT STEADY STATE
    EGT at MAX (fluc)
    630-645
  31. FLIGHT STEADY STATE
    Nozzle at START (fluc)
    None
  32. FLIGHT STEADY STATE
    Nozzle at IDLE (fluc)
    None
  33. FLIGHT STEADY STATE
    Nozzle at MIL (fluc)
    0-20 (+-3)
  34. FLIGHT STEADY STATE
    Nozzle at MAX (fluc)
    50-85 (+-3)
  35. FLIGHT STEADY STATE
    Fuel Flow at START (fluc)
    360 (MAX)
  36. FLIGHT STEADY STATE
    Fuel Flow at IDLE (fluc)
    200 Minimum Std Day
  37. FLIGHT STEADY STATE
    Fuel Flow at MIL (fluc)
    (+-50)
  38. FLIGHT STEADY STATE
    Fuel Flow at MAX (fluc)
    (+-50)
  39. FLIGHT STEADY STATE
    Oil Pressure at START (fluc)
    Indication Only
  40. FLIGHT STEADY STATE
    Oil Pressure at IDLE (fluc)
    5 (Min)
  41. FLIGHT STEADY STATE
    Oil Pressure at MIL (fluc)
    20-55 (+-2)
  42. FLIGHT STEADY STATE
    Oil Pressure at MAX(fluc)
    20-55 (+-2)
  43. FLIGHT STEADY
    Maximum time allowed for MIL operation
    30min
  44. FLIGHT STEADY
    Maximum time allowed for MAX operation
    15min
  45. Abort start if EGT reaches
    845
  46. Abort aircraft if EGT exceeds
    925
  47. In both GROUND and FLIGHT STEADY STATE, the EGT is allowed a fluctuation in how much temperature?
    15 degrees (or +-7.5 degrees)
  48. Maximum allowable transient RPM
    107 percent
  49. Normal thrust is ________ or ________, whichever occurs first.
    98.5% or 630 degrees
  50. If a sudden change of ____ PSI, or greater, in oil pressure occurs at any stabilized RPM reference check list.
    10
  51. During cold weather starts, oil pressure may exceed limitations. This is a normal indication as long as the oil pressure continues to _______ as engine oil warms.
    Decrease
  52. Do not exceed ____ mins in mil power with the oil pressure above ___ psi.
    5, 55
  53. WRT oil supply, zero-G flight is limited to _____ seconds and negative-G is limited to _____ seconds.
    10, 30
  54. Following rapid throttle movements, nozzle position should stabilize within permissible fluctuation range within _____ seconds.
    10
  55. HYDRAULIC PRESSURE

    Minimum_______ Maximum_______
    Normal Range________ to ________
    • 1500psi, 3200psi
    • 2850psi, 3200psi
  56. OXYGEN PRESSURE

    Normal Range________ to ________
    50psi, 120psi
  57. AIRSPEED LIMITATIONS
    FLAPS 1%-45%
    300 KIAS
  58. AIRSPEED LIMITATIONS
    FLAPS 46%-60%
    240 KIAS
  59. AIRSPEED LIMITATIONS
    FLAPS OVER 60%
    220 KIAS
  60. AIRSPEED LIMITATIONS Nose Wheel Tire
    240 Kts Ground Speed
  61. AIRSPEED LIMITATIONS
    Main Wheel Tire
    12-ply
    195 kts GS
  62. AIRSPEED LIMITATIONS
    Main Wheel Tire 14-ply
    204 kts GS
  63. Extension / Retraction of the landing gear at bank angles greater than _____ or at load factors greater than _____ can result in overstress failure of the main landing gear side brace trunion.
    45 degrees, +1.5G
  64. DASH-1 PROHIBITED MANEUVERS
    List them
    • -- Vertical stalls
    • -- Intentional spins
    • -- Continuous aileron rolls at any load factor other than +1.0 G or exceeding ¾ stick deflection
  65. WSSP LIMITATIONS
    Asymetrical G?
    0 to +3
  66. WSSP LIMITATIONSSymetrical G?
    0 to +4.0
  67. WSSP LIMITATIONS
    Normal Capacity?
    140 Lbs
  68. WSSP LIMITATIONS
    Max Speed
    400 KIAS
  69. WSSP LIMITATIONS
    SB Open/Turbulence
    350 KIAS
  70. WSSP LIMITATIONS
    Abrupt Control
    240 KIAS
  71. AIRSPEED LIMITATIONS
    Canopy?
    50 KIAS
  72. 50 KIAS
  73. AIRSPEED LIMITATIONS
    Gear
    240 KIAS
  74. AIRSPEED LIMITATIONS
    Gear Doors
    240 KIAS
  75. AIRSPEED LIMITATIONS
    Nose Wheel Steering
    65 KIAS
  76. What is the the acronym that helps you remember the Fluctuation Limits?
    R.O.N.

    • +-1 RPM
    • +-2 Oil
    • +-3 Nozzle
Author
Thriller
ID
112032
Card Set
T-38
Description
T-38 Ops Limits
Updated

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