TH-73 Limits (2026),,, Exams of Advanced Education

TH-73 Limits (2026),,,,,,,,,,,,

Typology: Exams

2025/2026

Available from 02/23/2026

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TH-73 Limits
N1 minimum - Answer 51%
N1 cautionary - Answer 51-60%
N1 continuous operation - Answer 60-100.1%
N1 takoff/max - Answer 100.1-103.2%; 103.2% max (5 min)
N1 transient - Answer 103.8% (30 sec)
N1 note #2: IDLE N1 may decrease below ______ when the generator and
other aircraft systems are turned on - Answer 60%
N2 minimum - Answer 95%
N2 cautionary - Answer 95-101%
N2 continuous operation - Answer 101-103%
N2 takeoff/max - Answer 103% max
N2 transient - Answer 108% (10 sec)
N2 caution #1: An N2 indication of ______ corresponds with an actual N2
value of ______ to ______. The N2 transient region begins at ______. Protracted
operation at N2 values of ______ should be avoided to minimize the possibility
of N2 overspeed - Answer 103%; 102.5%; 103.49%; 103.01%; 103%
ITT continuous operation - Answer 755 °C max
ITT takeoff/max - Answer 755-810 °C; 810 °C max
ITT transient - Answer 860 °C (5 sec)
ITT start max - Answer 870 °C
ITT start transient - Answer 980-1090 °C (2 sec); 1090 °C max
ITT note #1: a linear variation applies above ______, ten seconds, and ______,
two seconds - Answer 870 °C; 980 °C
TRQ continuous operation - Answer 100% max
TRQ takeoff/max - Answer 100-108.5%; 108.5% max (5 min)
TRQ transient - Answer 115% (6 sec)
NR pwr-on minimum - Answer 95%
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TH-73 Limits N1 minimum - Answer 51% N1 cautionary - Answer 51-60% N1 continuous operation - Answer 60-100.1% N1 takoff/max - Answer 100.1-103.2%; 103.2% max (5 min) N1 transient - Answer 103.8% (30 sec) N1 note #2: IDLE N1 may decrease below ______ when the generator and other aircraft systems are turned on - Answer 60% N2 minimum - Answer 95% N2 cautionary - Answer 95-101% N2 continuous operation - Answer 101-103% N2 takeoff/max - Answer 103% max N2 transient - Answer 108% (10 sec) N2 caution #1: An N2 indication of ______ corresponds with an actual N value of ______ to ______. The N2 transient region begins at ______. Protracted operation at N2 values of ______ should be avoided to minimize the possibility of N2 overspeed - Answer 103%; 102.5%; 103.49%; 103.01%; 103% ITT continuous operation - Answer 755 °C max ITT takeoff/max - Answer 755-810 °C; 810 °C max ITT transient - Answer 860 °C (5 sec) ITT start max - Answer 870 °C ITT start transient - Answer 980-1090 °C (2 sec); 1090 °C max ITT note #1: a linear variation applies above ______, ten seconds, and ______, two seconds - Answer 870 °C; 980 °C TRQ continuous operation - Answer 100% max TRQ takeoff/max - Answer 100-108.5%; 108.5% max (5 min) TRQ transient - Answer 115% (6 sec) NR pwr-on minimum - Answer 95%

NR pwr-on cautionary - Answer 95-101% NR pwr-on continuous operation - Answer 101-103% NR pwr-on takeoff/max - Answer 103% max NR pwr-on transient - Answer 108% (10 sec) NR pwr-off minimum - Answer 90% NR pwr-off continuous operation - Answer 90-110% NR pwr-off takeoff/max - Answer 110% max NR pwr-off transient - Answer 80% (10 sec) Fuel pressure cautionary - Answer 0-7 psi Fuel pressure continuous operation - Answer 7-25 psi Fuel pressure takeoff/max - Answer 25 psi max Minimum fuel: minimum fuel on landing shall be no less than ______ in the No. 1 cell - Answer 50 lbs Minimum fuel warning: sideward flight and crosswind hovering when indicated fuel quantity is less than ______ may result in engine flameout - Answer 22 lbs Minimum fuel note: the No. 1 and No. 2 fuel cells each contain ______ of unusable fuel - Answer 9 lbs Engine oil pressure minimum - Answer 40 psi Engine oil pressure cautionary - Answer 40-80 psi (with N1 < 72%) Engine oil pressure continuous operation - Answer 80-110 psi Engine oil pressure takeoff/max - Answer 110 psi max Engine oil pressure note: during cold starting conditions the oil pressure can temporarily exceed ______; it reduces as oil temperature increases - Answer 110 psi Engine oil temp minimum - Answer -25 °C Engine oil temp continuous operation - Answer 10-115 °C Engine oil temp takeoff/max - Answer 115 °C max Engine oil temp transient - Answer 127 °C (5 min with N1 at 61+-1%)

Maximum forward speed at touchdown after engine failure - Answer 50 kts Maximum operating altitude - Answer 15,000 ft Minimum ambient air temperature - Answer -13 °F (-25 °C) Maximum sea level ambient air temperature - Answer 122 °F (50 °C) The maximum ambient air temperature for operation decreases with pressure altitude at the standard lapse rate of ______ °C (______ °F) every ______ ft (______ m) up to ______ ft (______ m) - Answer 2; 3.6; 1000; 305; 15,000; 4572 max gross weight for ground operations (towing and takeoff prohibited) - Answer 6393 lb (2900 kg) max gross weight - Answer 6283 lbs (2850 kg) min gross weight for flight - Answer 3803 lbs (1725 kg) max gross weight with external load attached to cargo hook - Answer 6944 lbs (3150 kg) Automatic flight control system minimum use height: MUH with both helipilot operative: Fly attentive below ______; fly manually below ______ - Answer 500 ft AGL; 250 ft AGL Automatic flight control system minimum use height: MUH with one helipilot inoperative (SAS 1 or SAS 2): fly attentive below ______; fly manually below ______ - Answer 500 ft AGL; 500 ft AGL Flight director modes minimum use hight: All FD modes when in cruise, climb, and descent - Answer 500 ft AGL Flight director modes minimum use height: All FD modes during approach - Answer 50 ft AGL Flight director engaged, or coupled, with any helipilot inop: maximum airspeed - Answer 100 KIAS Flight director engaged, or coupled, with any helipilot inop: fly attentive above ______; fly manually below ______ - Answer 500 ft AGL; 500 ft AGL Cargo hook loading limit: from -1000 to 9000 ft - Answer 3086 lbs (1400 kg) Cargo hook loading limit: above 9000 ft: decrease ______ every ______ from ______ - Answer 110 lbs (50 kg); 1000 ft; 3086 lbs (1400 kg)

Prohibited Operations - Answer 1. The TH-73A is prohibited from operating in icing conditions

  1. IFR operations are prohibited with any doors open/removed or with an external load Prohibited Maneuvers - Answer 1. Aerobatic maneuvers
  2. Protracted operations in the AVOID areas of the height velocity diagram
  3. Intentional entry into retreating blade stall Vne (max IFR airspeed) - Answer Lesser of 145 KIAS or Vne (power on) Vmini (min IFR airspeed) - Answer 60 KIAS Vmin app (min IFR approach airspeed) - Answer 60 KIAS Vmax app (max IFR approach airspeed) - Answer 130 KIAS Minimum airspeed in autorotation (without close external references) - Answer 60 KIAS Maximum airspeed with torque between 100 and 108.5% (takeoff power range) - Answer 75 KIAS Vne with one or both doors open or removed - Answer 85 KIAS Vne during door opening and closing operation - Answer 70 KIAS Maximum speed for searchlight extension, orientation, and retraction - Answer 120 KIAS Vne with external loads attached to cargo hook: from sea level to 5000 ft - Answer 100 KIAS Vne with external loads attached to cargo hook: above 5000 ft: decrease ______ every ______ from ______ - Answer 3 kts; 1000 ft; 100 KIAS Nose-up operations - Answer 12 deg Side-up operations - Answer 10 deg Nose-down operations - Answer 2 deg Nose-down operations (unobstructed tail) - Answer 5 deg Flight with one helipilot inop: max air speed - Answer 130 KIAS Flight with one helipilot inop: max rate of climb - Answer 750 fpm