Copy_of_Weight_and_Balance_Forms.xls
XLS spreadsheet 79 KB Posted
- Attached to
- National CWN Helicopter Services Federal contract opportunity
- Solicitation number
- 12024B19R9000
- Issued by
- Department of Agriculture Forest Service
About this file
Weight and Balance Forms to be utillized.
View the file
Other files for this federal contract opportunity
| File | Type | Posted |
|---|---|---|
| Amendment_4_SF_30.pdf | ||
| Amendment_3_SF_30.pdf | ||
| Amendment_2_SF_30.pdf | ||
| Transcript_of_Pre-proposal_conference_on_August_15th..pdf | ||
| FINAL._Solicitation_12024B19R9000_Amendment_1.pdf | ||
| Amendment_1_SF_30_.pdf | ||
| Solicitation_No._12024B19R9000_(8.1.2019).pdf |
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Text version
Form A
| Form A : List of approved equipment | Date Weighed | Date Weighed | ||||||||
| Page | A/C Make, Model, Series | Registration Number | Serial Number | In A/C | ON 'C' Chart | In A/C | ON 'C' Chart | |||
| Location and Description of Item | Weight | Arm | Moment | Lat. Arm | Lat. Moment | |||||
| X: Item was on the aircraft at the time aircraft was weighed or is included in the basic weight | ||||||||||
| O: Item was off the aircraft at the time aircraft was weighed or is not included in the basic weight. | ||||||||||
| C: Item is on Form C when installed. |
Form B
| Form B : Aircraft Weighing Record | ||||||||||
| Make, Model, Series | Registration Number | Serial Number | Date | |||||||
| Datum is | Leveling Means | Weighing Procedures References | Scale Location | |||||||
| Scale Readings | ||||||||||
| Scale | Reading | Tare | Net Weight | Long. Arm | Moment | Lat. Arm | Moment | |||
| Left Front or Nose | ||||||||||
| Right Front | ||||||||||
| Left Aft or Tail | ||||||||||
| Right Aft | ||||||||||
| Basic Weight | Total | |||||||||
| Fuel & Oil at Time of Weighing | Notes | |||||||||
| Full | Defueled | Drained | ||||||||
| Fuel | ||||||||||
| Oil Engine | ||||||||||
| Oil Transmission | ||||||||||
| Oil Tail Gearboxes | ||||||||||
| Hydraulic Fluid | ||||||||||
| Items Weighed not part of Basic Weight | Items not Weighed but part of Basic Weight | |||||||||
| Item | Weight | Arm | Moment | Item | Weight | Arm | Moment | |||
| Total (–) | Total (+) | |||||||||
| Adjusted Basic Weight of Aircraft as Weighed | ||||||||||
| CG | Moment | |||||||||
| Total Empty Weight of Aircraft as Adjusted | Longitudinal EW. CG | |||||||||
| Lateral EW CG | ||||||||||
| Aircraft Weighed By | Scales | |||||||||
| Print Name : | Type : | |||||||||
| Signature : | Serial Number : | |||||||||
| Certificate Type and Number : | Calibration Date : |
Form C
| Form C : Continuous History of Equipped Weight After Weighing | |||||||||||
| Make, Model, Series | Registration Number | Serial Number | Page Number | ||||||||
| Date mm/dd/yyyy | Description of Item | Weight Change | Current Total Equipped Weight | ||||||||
| Added (+) | Removed (--) | ||||||||||
| Weight | Arm | Moment | Weight | Arm | Moment | Weight | CG | Moment |
Form A EX
| Form A : List of approved equipment | Date Weighed | Date Weighed | ||||||||
| 9/15/09 | ||||||||||
| Page | A/C Make, Model, Series | Registration Number | Serial Number | In A/C | ON 'C' Chart | In A/C | ON 'C' Chart | |||
| 1 of 1 | Bell 205A -1 | N12345 | 66666 | |||||||
| Location and Description of Item | Weight | Arm | Moment | Lat. Arm | Lat. Moment | |||||
| Fuselage: | ||||||||||
| Ballast | 25.3 | + 8.5 | 215.1 | + 3.4 | 86 | X | ||||
| Battery | 52.5 | + 8.5 | 446.3 | X | ||||||
| Wire Strike kit upper and lower | O | |||||||||
| Pulse light kit | X | |||||||||
| Strobe | X | |||||||||
| Cargo Hook | X | |||||||||
| Cabin: | ||||||||||
| Instruments | ||||||||||
| Radios | ||||||||||
| Automated Flight Following | ||||||||||
| Seats | ||||||||||
| Engine Deck: | ||||||||||
| Rotor brake | X | |||||||||
| T-53 engine | X | |||||||||
| 212 Rotor assy | X | |||||||||
| Tail: | ||||||||||
| Fast Fin | X | |||||||||
| Strake Kit | X | |||||||||
| 212 Tail Rotor Assy | X | |||||||||
| Strobe Light | X | |||||||||
| Removable Equipment: | ||||||||||
| Fill Pump | C | |||||||||
| Rappel Kit | C | |||||||||
| Survival Kit | C | |||||||||
| First Aid Kit | X | |||||||||
| Fire Tank | 395.2 | + 125 | 49400 | C | ||||||
| X: Item was on the aircraft at the time aircraft was weighed or is included in the basic weight | ||||||||||
| O: Item was off the aircraft at the time aircraft was weighed or is not included in the basic weight. | ||||||||||
| C: Item is on Form C when installed. |
Form B EX
| Form B : Aircraft Weighing Record | ||||||||||
| Make, Model, Series | Registration Number | Serial Number | Date | |||||||
| Bell, 205A -1 | N12345 | 66666 | 9/15/09 | |||||||
| Datum is | Leveling Means | Weighing Procedures References | Scale Location | |||||||
| 7.60" aft of cabin nose | Plumb line from top of left main door frame | CFR, part 29 / OEM Maint. Manual chapter 8 / Type Certificate DS | Jack points | |||||||
| Scale Readings | ||||||||||
| Scale | Reading | Tare | Net Weight | Long. Arm | Moment | Lat. Arm | Moment | |||
| Left Front or Nose | 1478 | 0 | 1478 | + 61.69 | 91177.8 | - 30 | 44340 | |||
| Right Front | 1116 | 0 | 1116 | + 61.69 | 68846.1 | + 30 | 33480 | |||
| Left Aft or Tail | 1215 | 0 | 1215 | + 211.58 | 257069.7 | - 30 | 36450 | |||
| Right Aft | 1974 | 0 | 1974 | + 211.58 | 417658.9 | + 30 | 59220 | |||
| Basic Weight | Total | 5783 | 144.46 | 834752.5 | 2.06 | 11910 | ||||
| Fluids (Fuel & Oil and Etc) at Time of Weighing | Notes | |||||||||
| Full | Defueled | Drained | Oil and unusable fule in basic weight | |||||||
| Fuel | X | |||||||||
| Oil Engine | X | |||||||||
| Oil Transmission | X | |||||||||
| Oil Tail Gearboxes | X | |||||||||
| Hydraulic Fluid | X | |||||||||
| Items Weighed not part of Basic Weight | Items not Weighed but part of Basic Weight | |||||||||
| Item | Weight | Arm | Moment | Item | Weight | Arm | Moment | |||
| Useable fuel (if full) | 1457.5 | + 150.4 | 219208 | Unusable fuel (if drained) | 16.5 | + 144 | 3276 | |||
| Total (–) | 1457.5 | Total (+) | 16.5 | |||||||
| Adjusted Basic Weight of Aircraft as Weighed | ||||||||||
| CG | Moment | |||||||||
| Total Empty Weight of Aircraft as Adjusted | 5783 | Longitudinal EW. CG | + 144.46 | 834752.5 | ||||||
| Lateral EW CG | + 2.06 | 11910 | ||||||||
| Aircraft Weighed By | Scales | |||||||||
| Print Name : | Type : | |||||||||
| Signature : | Serial Number : | |||||||||
| Certificate Type and Number : | Calibration Date : |
Form C EX
| Form C : Weight & Balance Running Total | |||||||||||
| Make, Model, Series | Registration Number | Serial Number | Page Number | ||||||||
| Bell, 205A -1 | N12345 | 66666 | 1 of ? | ||||||||
| Date mm/dd/yyyy | Description of Item | Weight Change | Current Total Equipped Weight | ||||||||
| Added (+) | Removed (--) | ||||||||||
| Weight | Arm | Moment | Weight | Arm | Moment | Weight | CG | Moment | |||
| 12/31/09 | Aircraft as weighed | 5783 | + 144.46 | 834752.5 | |||||||
| 7/15/10 | Survival Kit | 50.5 | + 200 | 10100 | 5833.5 | ||||||
| 7/15/10 | Rappel Mount kit | 38.2 | + 100 | 3820 | 5871.7 | ||||||
| 7/15/10 | Sorenson Tank and Snorkel | 389.6 | + 125.5 | 48894.8 | 6261.3 | + 143.35 | 897567.3 |
File details come from the government source that posted it.