1. BASIC LIMITS - Sheet1 (1) Flashcards
Min Crew required to operate the helo under normal conditions are?
pilot, copilot, aircrewman
419 T5
769° CONTINUOUS
810° 30 MIN MILITARY
829° 10 MIN MAX
416/416A T5
713° CONTINUOUS
753° 30 MIN MILITARY
773°/792° 10 MIN MAX
T5 INDICATION OF A HOT START
650°
T5 Peak Momentary
900
T5 INDICATIONS OF A POST ENGINE SHUTDOWN FIRE
320°
2 Engnine Overheat Warning
302°C/ 575°F
Ng GROUND IDLE
60.5-70% (VARIES W/ OAT)
Ng STARTER DROPOUT
51-58%
Ng NORMAL OPERATION
60.5-101.1%
Ng MAX
101.10%
Ng TRANSIENT
102.9% for 30 seconds
Normal Starter Engagment to Gnd Idle
60 sec
ALL Ng Limits
60.5 – 70 Ground Idle – Varies w/ OAT (2.1.9)
51 – 58 Starter Dropout (2.1.11.1)
60.5 – 101.1 Normal Operation (Fig 4-1 Sheet 1 of 3)
101.1 Maximum Military Operation (Fig 4-1 Sheet 1 of 3)
102.9 30 Sec Max (Fig 4-1 Sheet 1 of 3)
20 Minimum for Engine Start – Introduce Fuel (7.4)
26-32 Max Ng Start
Nf NORMAL OPERATION
100-105%
Nf MAX
110%
Nf TRANSIENT
111- 125% (5SEC)
Nf OVERSPEED (Momentary)
129%
What does Nf over speed do?
Reduces Wf to 75 +/- 2% Ng
All Nf Limits
111 – 125 5 sec (4.2.1.3.2)
110 +/- 2 Overspeed Protection Activates – Reducing WF to 75 +/- 2%Ng (2.1.6)
110 Maximum (Fig 4-1 Sheet 1 of 3)
100 – 105 Normal Operation (Fig 4-1 Sheet 1 of 3)
Q NORMAL
100%
Q PRECAUTIONARY
100-137%
Climb Q for <60K? >60K?
110%; 121%
Q 30MIN MILITARY
121%
Q MAX
137% (<10MIN)
Q TRANSIENT OVERTORQUE
160% <1MIN
Contingency Power for <2 min 419 single or dual engine operations?
157% Q and may reach as high as 105% Ng and 925C
All Q Limits
160 Max for 1min (Fig 4-1)
137 Maximum Operation for 10min/ Engine Overtorque (Fig 4-2)
121 Military Operation for 30min/Climbing Q for GW > 60K (Fig 4-2; 4.4.5)
110 Climbing Torque for Gross Weight < 60,000 lbs (4.4.5)
100 – 137 Precautionary Range (Fig 4-1 sheet 1 of 3)
100 Max Continuous (Fig 4-2)
Nr NORMAL
100-105% <50k lbs
103-105% >50k lbs
Nr PRECAUTIONARY
95-100% LOW END
105-118% HIGH END
Nr MAX
118%
Nr OVERSPEED
118%-129% (Visual Inspection)
>129% (Removal)
Rotor brake limits assiociated with Nr: apply High pressure rotor brake? Low Pressure? Light on?
50 +/- 4 to 25 +/- 4 Rotor Brake – RTR BK Light On (2.4)
50 or Below High Pressure Rotor Brake can be engaged (2.4.3.2)
25 or Less Low Pressure Rotor Brake Engagement (2.4.3.1)
All Nr limits
> 129: Removal of inspection parts
118-129: Visual Inspection of M/R hub, T/R hub, and T/R Drive shaft
118 Maximum Operations (Fig 4-1 Sheet 1 of 3)
104– 107 Flat Pitch (7.5)
105 – 118 Precautionary Range – High (Fig 4-1)
103 – 105 For Gross Wt 50,000 to 73,500 (Fig 4-1)
100 – 105 For Gross Wt < 50,000 lbs (Fig 4-1)
95 – 100 Precautionary Range – Low (Fig 4-1 Sheet 1 of 3)
50 +/- 4 to 25 +/- 4 Rotor Brake – RTR BK Light On (2.4)
50 or Below High Pressure Rotor Brake can be engaged (2.4.3.2)
25 or Less Low Pressure Rotor Brake Engagement (2.4.3.1)
ENGINE OIL TEMPS
NORMAL: 40°-135°C
10MIN MILITARY: 136°-145°C
MAX: 145°C
Max Allowable time for ENG OIL High press CL during Engine Starts?
3 min
NGB OIL TEMPS
NORMAL: 40°-130°C
60MIN 131°-145°C
MAX: 145°C
EXCURSIONS ABOVE 130 REQUIRE A SERVICEABILITY CHECK.
MGB OIL TEMPS
NORMAL: 40°-120°C
60MIN MILITARY: 121°-145°C
MAX: 145°C
EXCURSIONS ABOVE 120 REQUIRE A SERVICEABILITY CHECK.
MGB OIL PRESSURES
MIN: 25psi
NORMAL: 50-65psi
MAX: 150psi
If MGB Oil pressure decreases to less that 45 or by more than 10 in flight Land as soon as practacle.
HYDRAULIC PRESSURE
MIN: 2600PSI
NORMAL: 2600-3300PSI
MAX: 3300PSI
AIRSPEED
30 Rearward
35 Sideward
Below 40 Airspeed indicators are unreliable
85 Autorotation Min Sink Rate
110 Autorotation Max Glide Rate
130 maneuvering Airspeed
140 Landing Gear Actuation
150 Forward
150 Landing Gear Extended 150 External Load
150 EAPS Door Closed 130 Maneuvering Flight
Hover Turns of 360 Deg. < 15sec are prohibited
ANGLE OF BANK
GW< 56000lbs & DA>3000 & A/S>130KIAS: 60°
GW<56000lbs & DA>3000 OR GW<56000lbs & A/S>130KIAS: 45°
GW>56000lbs: 30°
ACCELERATION LIMITS
- 5-2.0Gs: GW=56000lbs & DA=3000’
0. 5-1.5Gs: GW>56000lbs OR DA>3000’
LANDING LIMITS
<46.5k main gear/tail skid: 672fpm
46.5k-69.75k main gear: 360fpm
HOOK LIMITS
SINGLE POINT: 36000lbs
DUAL POINT: 21600lbs individually 36000lbs total
Min Hook weight: 1pt? 2pt?
4k
1k per hook
LATERAL CG LIMITS
8.5” right-13.5” left
ICING LIMITS
ICE DETECT ON: Forecast or known trace-unlimited; light-30 minutes
ICE DETECT OFF: Forecast or known trace-unlimited day/night; light-30 minutes day only
Visible moisture <4°C: EAPS closed, engine, windshield, pitot heat, FLIR anti-ice on
DUAL ENGINE TORQUE OPERATION
MAX CONTINUOUS: 100% MILITARY: 121% 30MINS MAX: 148% 10MINS CONTINGENCY (419): 157% 2MINS TRANSIENT: 160% 1MIN
SINGLE ENGINE TORQUE OPERATION
MAX CONTINUOUS: 100% MILITARY: 121% 30MINS MAX: 148% 10MINS CONTINGENCY (419): 157% 2MINS TRANSIENT: 160% 1MIN
Nf Overspeed Protection
110+/-2%
Contingency Power
157%Q; 5000 shp for 2 minutes followed by 1 hour at maximum continuous.
Can expect 105 Ng and 925°C T5
WIND LIMITS
> 100: A/C to Hangar deck(Boat)
> 60: A/C into wind, blades removed, gust lock on, pylon spread (Boat SOP)
> 45<60: tanks full, blades folded, struts deflated, pylon spread
Basic:
60 kts: Max for a/c to be tied down.
> 45Kts - No Rotor engagement/disengagement, Blade or Pylon fold
> 20 Kts - Pylon fold into wind
Cabin Floor Static Limit
300 lbs/ft²
APP LIMITS
EXH TEMP - 621°C
RPM - 110% (102±1% GENS OFF/Nr ≤95%)
- 100% Normal Operation
10,000 Max Altitude – PA
6 +/- 1 Low Oil Pressure w/ Auto Shutdown
2800-3100 Accum Press Gauge >= 50deg
2000-2800 <50deg
Water Operating Limits
Stay afloat 2 hrs in 1-3’ waves, winds 7-16kts, 10° Roll, water tazi 8 kts at 46,500lbs.
How long can Compas Fail CL remain illuminated after the start?
5-8 sec
How long can BIM CL remain illuminated after the start?
2min
How long can IMDS CL remain illuminated after the start?
??????
Nf OVERSPEED PROTECTION
110 +/- 2 %
Shut down requirement?
1 min of:
Taxi
Ops at or above min gov with min collective pitch or
Gnd idle