Helicopteros

AIRCREW TRAINING MANUAL

BELL UH-1H PERFORMANCE PLANNING MANUAL
ENSPIRE AVIATION

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BELL UH-1H
PERFORMANCE PLANNING MANUAL
ENSPIRE AVIATION

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AIRCREW TRAINING MANUAL

BELL UH-1H PERFORMANCE PLANNING MANUAL
ENSPIRE AVIATION

CONTENTS

PAGE 3–4 5–9 CHARTS 10 11 12 13 14 27. MAX TORQUE AVAILABLE HOVER CEILING HOVER POWER REQUIRED CONTROL MARGIN 1 CONTROL MARGIN 2 AIRSPEEDOPERATING LIMITS PERFORMANCE PLANNING CHART PROCEDURES FOR USE

15 – 26 CRUISE CHARTS

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AIRCREW TRAINING MANUAL

BELL UH-1H PERFORMANCE PLANNING MANUAL
ENSPIRE AVIATION

UH-1 PERFORMANCE PLANNING CARD

CURRENT CONDITIONS PA TAKE-OFF WEIGHT CAL FACTOR
1 3 5

FAT LOAD FUEL

2 4 6

CHART VALUE MAX TORQUE AVAIL MAX ALLOWABLE GW (IGE) MAX ALLOWABLE GW (OGE) PREDICTED HOVER TORQUEGO/NO GO TORQUE (IGE) GO/NO GO TORQUE (OGE) DCM
7 8 9 10 11 12 13 14

IND TRQ

MAXIMUM CONDITIONS PA LOAD
15 17

FAT FUEL

16 18

CHART VALUE MAX TORQUE AVAIL MAX ALLOWABLE GW (IGE) MAX ALLOWABLE GW (OGE) GO/NO GO TORQUE (IGE) GO/NO GO TORQUE (OGE) DCM
19 20 21 22 23 24

IND TRQ

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AIRCREW TRAINING MANUAL

BELL UH-1H PERFORMANCE PLANNING MANUAL
CRUISE DATA

UH-1 PERFORMANCEAVIATION CARD PLANNING ENSPIRE
FAT 26 GW 27

PA 25

IAS CRUISE MAX ENDCRUISE DATA OR R/C MAX RANGE VNE
28 31 34 37

IND TRQ
29 32

FUEL FLW
30 33 36 25 PA

FAT 26 35 GW 27

FUEL MANAGEMENT START STOP PPH CRUISE
38

IAS

IND TRQ FUEL FLW

39 MAX END OR R/C

MAX RANGE

40 41 42

RESERVE VNE BURNOUT

FUEL MANAGEMENT WEIGHT COMPUTATION START BASIC WEIGHT STOP CREW ANDFLT EQUIP PPH MISSION RESERVE EQUIP BURNOUT OPERATING WEIGHT FUEL WEIGHT PAX, BAGGAGE COMPUTATION BASIC WEIGHT TAKE-OFF WEIGHT CREW AND FLT EQUIP MISSION EQUIP OPERATING WEIGHT FUEL PAX, BAGGAGE TAKE-OFF WEIGHT
43 44 45 46 47 48 49

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AIRCREW TRAINING MANUAL

BELL UH-1H PERFORMANCE PLANNING MANUAL
ENSPIRE AVIATION

TASK: Prepare the UH-1 Performance Planning Card. CONDITIONS: Given datafrom weight and balance, the Aircraft operators manual, environmental conditions, and a blank performance planning card STANDARDS: Correctly compute performance planning data according to procedures given in the aircraft operator's manual and the description below. DESCRIPTION: 1. Crew Actions. The PC will ensure that aircraft performance data to complete the mission are available and thataircraft limitations will not be exceeded. The most accurate performance data can be obtained by using existing conditions. Predicted hover torque should be determined using the conditions forecast for the time of departure. The PC may direct the other RCM to assist in completing these data as necessary.

2. Procedures. a. The PPC is used as an aid to organize performance data; this form must be usedfor evaluations. Instructions for completing the PPC are provided below; the numbered paragraphs coincide with the numbers on the PPC. b. The same PPC data will suffice for consecutive takeoffs and landings when aircraft gross weight or environmental conditions have not increased significantly; that is, 200 pounds gross weight, 5 degrees Celsius, or 500 feet PA. NOTE: The Current Conditionssection of the PPc, items (I) through (14), is based on conditions existing at initial takeoff (departure). Crew members use this information to validate the PPC comparing the aircraft's actual performance to the planned performance. If the current conditions are the same as the maximum conditions for the mission period, this section need not be completed.

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AIRCREW TRAINING MANUAL

BELL UH-1HPERFORMANCE PLANNING MANUAL
ENSPIRE AVIATION

1. P.A.* Record the current PA forecast for the time of departure. 2. F.A.T.Record the current FAT forecast for the time of departure 3. Takeoff GWT.* Record the current takeoff gross weight for the time of departure 4. Load.* Record the maximum weight of the load(s) expected during the mission 5. Cal Factor* Record the calibration factor (data...