Event:

Instructor:

DryWetWeight:

Aircraft:Spot:

Crnt Wx:

Fcst Wx:

Date:

Student:

Weight:

Max Tmp:

Max PA:

Max DA:

	Heavy B	FWD CG	Moment
Basic Wt:	2033.00	1975.90	2295.73
Crew Fwd:	0	0	0
Oil:	12	12	22
Op Wt:	2045.0	1987.9	2317.73
Takeoff
Op Wt:	2045.0	1987.9	2317.73
Fuel: 70g65g	469	469	545.92
Crew Aft:			0
Baggage:			0
Gross Wt(1):	2514.0	2456.9	2863.65 (116.6)
External OPS
Op Wt:		1987.9	2317.73
Fuel:		335	381.23
Crew Aft:			0
Ext Load			160.65
Gross Wt(2):		2472.9	2859.61 (115.64)
Landing
Op Wt:		1987.9	2317.73
Fuel (10g):		67	74.17
Crew Aft:			0
Baggage:			0
Gross Wt(3):		2054.9	2391.90 (116.4)


T/O GW: (1)	⚠️2514.0
CG Range:	106.00 - 113.7
T/O CG:	⚠️116.56
Lnd GW: (3)	⚠️2054.9
CG Range:	106.00 - 114.2
Lnd CG:	⚠️116.40

HIGE/HOGE: ⓘTorque values are derived from quadratic regression of NATOPS chart. Error when compared to user chart interpretation is average 0.25% Q. (stdDev 0.75% Q)	⚠️61 / 69
Fuel@2900:	128g

"Get Lucky"
Operational Risk Management Worksheet

Hazard Types	Mitigated Risk Level
Personal Risk Assessment/Human Factors (Work distractions / Illness / Etc...)
PIC
SNA/SNA/IP/Aircrew
Sleep
PIC
SNA/SNA/IP/Aircrew
Weather
Ceilings (VMC: L) \| (<1000 or <3SM: M) \| (<INST MINS: H)
Wind (>5kts below RWOP: L) \| (<5kts below RWOP: M) \| (>RWOP: H)
SIGMET Reasonable probability of entry? Yes: M \| No: L
Night
IMC Reasonable probability of night IMC? Yes: M \| No: L
Illumination Low Light: M \| High Light: L
Crew Proficiency for Assigned Event (IP Only)
PIC
IP/Aircrew
Pressure to Complete Mission
PIC
SNA/SNA/IP/Aircrew

Highest Risks and Associated Controls

Side	Series	Weight	Moment	Arm
050	C	2150.1	2509.59	116.72
051	C	2152.7	2501.44	116.20
056	C	2106.73	2461.61	116.85
057	C	2147.18	2494.31	116.17
058	C	2147.6	2508.21	116.79
060	C	2155.63	2520.1	116.91
061	C	2136.7	2481.8	116.15
062	C	2150.1	2494.85	116.03
063	C	2159.7	2525.26	116.93
065	C	2146.2	2502.22	116.59
066	C	2164.63	2519.61	116.40
067	C	2171.45	2523.43	116.21
069	C	2138.2	2490.94	116.50
070	C	2126.2	2471.41	116.24
071	C	2146.7	2500	116.46
072	C	2140.2	2503.33	116.97
074	C	2119.73	2478.04	116.90
075	C	2140.7	2475.48	115.64
076	C	2122.7	2462.33	116.00
077	C	2146.8	2498.94	116.40
078	C	2148.3	2490.26	115.92
079	C	2138.7	2509.93	117.36
080	C	2149.97	2497.2	116.15
082	C	2155.63	2507.14	116.31
083	C	2145.37	2493.77	116.24
084	C	2131.33	2475.36	116.14
085	C	2157.2	2502.05	115.99
086	C	2153.2	2498.59	116.04
087	C	2163.7	2508.75	115.95
088	C	2158.2	2509.46	116.28
089	C	2157.7	2511.68	116.41
090	C	2166.2	2499.53	115.39
092	C	2125.67	2476.46	116.50
093	C	2150.2	2503.18	116.42
094	C	2155.3	2510.05	116.46
095	C	2167.57	2515.27	116.04

Side	Series	Weight	Moment	Arm
096	C	2162.98	2514.94	116.27
097	C	2148.2	2491.47	115.98
098	C	2152.7	2495.2	115.91
099	C	2154.7	2508.78	116.43
100	C	2151.7	2504	116.37
101	C	2104.7	2451.88	116.50
102	C	2153.2	2503.58	116.27
103	C	2152.2	2508.65	116.56
104	C	2154.3	2502.21	116.15
106	C	2156.2	2518.96	116.82
107	C	2145.7	2508.8	116.92
108	C	2144.33	2491.94	116.21
109	C	2141.7	2497.99	116.64
110	C	2150.3	2496.01	116.08
112	C	2147.3	2494.86	116.19
113	C	2119.2	2469.86	116.55
114	C	2158.7	2521.59	116.81
115	C	2150.3	2501.42	116.33
116	C	2134.27	2480.2	116.21
117	C	2155.14	2503.49	116.16
118	C	2146.13	2498.18	116.40
120	C	2135.83	2496.22	116.87
121	C	2153.28	2504.05	116.29
122	C	2138.3	2481.16	116.03
125	C	2141.24	2488.49	116.22
126	C	2142.23	2488.81	116.18
127	C	2151.13	2508.42	116.61
128	C	2157.2	2513.28	116.51
129	C	2166.13	2512.96	116.01
130	C	2151.2	2499.99	116.21
131	C	2127.9	2508.82	117.90
133	C	2157.23	2507.56	116.24
134	C	2143.2	2484.97	115.95
135	C	2159.53	2508.53	116.16
136	C	2155.7	2511.57	116.51
137	C	2140.33	2484.8	116.09

Side	Series	Weight	Moment	Arm
unk	B	0	0	NaN
140	B	1984.2	2347.98	118.33
141	B	1979.5	2342.89	118.36
142	B	1972.1	2324.78	117.88
143	B	1986.53	2344.07	118.00
144	B	1964	2330.6	118.67
145	B	1975.9	2295.73	116.19
146	B	2012.5	2356.73	117.10
147	B	1995.6	2350.04	117.76
148	B	1986.8	2359.7	118.77
149	B	1977.7	2350.01	118.83
150	B	1986.13	2359.11	118.78
153	B	1987.5	2355.26	118.50
154	B	2030	2386.59	117.57
155	B	1983.13	2361.82	119.10
156	B	1998	2364.95	118.37
157	B	2022.5	2402.79	118.80
158	B	2008	2375.46	118.30
159	B	2000.7	2371.43	118.53
160	B	2014.5	2389.02	118.59
161	B	1990.2	2364.39	118.80
162	B	2020.5	2386.09	118.09
164	B	2018.2	2385.51	118.20
165	B	1994.3	2376.69	119.17
166	B	1996.7	2361.74	118.28
167	B	1986.63	2348.35	118.21
168	B	2033	2396.09	117.86
169	B	2010.5	2391.31	118.94
171	B	1985	2337.91	117.78
173	B	1994.2	2348.51	117.77
174	B	2002.2	2363.53	118.05
176	B	1971.33	2335.13	118.45
181	B	1993.63	2365.31	118.64
182	B	2009.6	2373.36	118.10
183	B	1998.53	2352.28	117.70
184	B	1978.5	2336.7	118.10
185	B	1997.2	2373.87	118.86
186	B	1987.5	2361.03	118.79
187	B	1999.53	2349.09	117.48
188	B	1983.83	2359.28	118.93
189	B	1988.5	2340.97	117.73
190	B	1981.1	2344.45	118.34

Updated: October 2021

Name	Weight	Dry	Wet	Squadron
Santa	190	210	220	TW-5
CO KAMAN	155	165	173	HT- 8
KAMAN	155	165	173	HT- 8
XO ONEILL	238	248	256	HT- 8
ONEILL	238	248	256	HT- 8
BEATTIE	210	220	228	HT- 8
BLACK	210	220	228	HT- 8
BENGE	227	237	245	HT- 8
BUEHLER	220	230	238	HT- 8
BROWN,R	197	207	215	HT- 8
CAHILL	150	160	168	HT- 8
CANHAM	200	210	218	HT- 8
CARPIO	128	138	146	HT- 8
CERNY	175	185	193	HT- 8
CHINO	180	190	198	HT- 8
COLETTA	160	170	178	HT- 8
COLLINS	207	217	225	HT- 8
COLUNGA	182	192	200	HT- 8
CRAFT	167	177	185	HT- 8
CUNNINGHAM,E	172	182	190	HT- 8
CUNNINGHAM,G	165	175	183	HT- 8
DIDIER	175	185	193	HT- 8
EDWARDS	145	155	163	HT- 8
ENZINGER	185	195	203	HT- 8
FLOWERS	190	200	208	HT- 8
FROSLEE	147	157	165	HT- 8
GARCIA	171	181	189	HT- 8
GAY	190	200	208	HT- 8
GEHRKE	235	245	253	HT- 8
GORNTO	195	205	213	HT- 8
GREINER	142	152	160	HT- 8
GRIFFIN	270	280	288	HT- 8
HAND	190	200	208	HT- 8
HARDERS	174	184	192	HT- 8
HARNED	190	200	208	HT- 8
HENNING	216	226	234	HT- 8
HERRERA	149	159	167	HT- 8
HOFFMAN	230	240	248	HT- 8
HOLLINGER	230	240	248	HT- 8
HORN	235	245	253	HT- 8
HORNER	176	186	194	HT- 8
KADZ	185	195	203	HT- 8
KAMENSKY	182	192	200	HT- 8
KIFFER	200	210	218	HT- 8
KILGORE	195	205	213	HT- 8
LEE	215	225	233	HT- 8
LINSKY	142	152	160	HT- 8
LOTT	190	200	208	HT- 8
LOWD	200	210	218	HT- 8
LUTZ	210	220	228	HT- 8
MAHNE	160	170	178	HT- 8
MARIE	180	190	198	HT- 8
MAYNARD	155	165	173	HT- 8
MAZEL	220	230	238	HT- 8
MCCABE	220	230	238	HT- 8
MCCRAY	180	190	198	HT- 8
MCGUCKIN	175	185	193	HT- 8
MEIER	230	240	248	HT- 8
MELICK	175	185	193	HT- 8
MURPHY	220	230	238	HT- 8
OCONNELL	155	165	173	HT- 8
PALMER	222	232	240	HT- 8
PERMENTER	181	191	199	HT- 8
POWANDA	170	180	188	HT- 8
RANUM	155	165	173	HT- 8
REGIS	160	170	178	HT- 8
RILEY	190	200	208	HT- 8
RIVERA	225	235	243	HT- 8
ROYER	175	185	193	HT- 8
SCHNEIDER	187	197	205	HT- 8
SCHULTZ	200	210	218	HT- 8
SCOTT	210	220	228	HT- 8
SEIDERS	200	210	218	HT- 8
SMOAK	180	190	198	HT- 8
SOMMA	165	175	183	HT- 8
SPENCER	165	175	183	HT- 8
STEFFEN	183	193	201	HT- 8
STURGIS	195	205	213	HT- 8
SYKORA	167	177	185	HT- 8
TASNEY	235	245	253	HT- 8
TEAL	205	215	223	HT- 8
TELLES-GOINS	160	170	178	HT- 8
THOMAS	165	175	183	HT- 8
USNER	210	220	228	HT- 8
VANDAL	175	185	193	HT- 8
VANDENBROEKE	200	210	218	HT- 8
WEBB	180	190	198	HT- 8
WELLS	190	200	208	HT- 8
WERRELL	220	230	238	HT- 8
WILLIAMS,P	255	265	273	HT- 8
WRIGHT	215	225	233	HT- 8
CO	170	190	200	HT-18
XO	190	210	220	HT-18
ALLEN	155	175	185	HT-18
ANGEL	180	200	210	HT-18
AUSTIN	200	220	230	HT-18
BARTH	170	190	200	HT-18
BAUM	210	230	240	HT-18
BELANGER	145	165	175	HT-18
BILDZUKEWICZ	130	150	160	HT-18
BORNEMAN	160	180	190	HT-18
BROWN	145	165	175	HT-18
BURGESS	170	190	200	HT-18
BUTLER	180	200	210	HT-18
COFSKY	190	210	220	HT-18
CRAFT	155	175	185	HT-18
CROWNOVER	210	230	240	HT-18
CRYSLER	185	205	215	HT-18
CULLEN	200	220	230	HT-18
CULP	200	220	230	HT-18
DAVIS	190	210	220	HT-18
DONATI	170	190	200	HT-18
ELLIS	135	155	165	HT-18
EVANSKI	220	240	250	HT-18
FALCE	200	220	230	HT-18
GAWNE	180	200	210	HT-18
GUARD	160	180	190	HT-18
HAGLUND	165	185	195	HT-18
HALLER	130	150	160	HT-18
HANS	200	220	230	HT-18
HARRINGTON	210	230	240	HT-18
HAST	200	220	230	HT-18
HECK	210	230	240	HT-18
HELLER	225	245	255	HT-18
HORNER	150	170	180	HT-18
HOUSEMAN	170	190	200	HT-18
HUMPHREYS	170	190	200	HT-18
JANOSKY	175	195	205	HT-18
KANGAS	120	140	150	HT-18
KEEF	170	190	200	HT-18
KELLY	155	175	185	HT-18
LANASA	195	215	225	HT-18
LEIBOVICH	170	190	200	HT-18
LOEB	190	210	220	HT-18
LORENZ	170	190	200	HT-18
MACUS	190	210	220	HT-18
MANNARINO	140	160	170	HT-18
MCKIE	180	200	210	HT-18
MILLER	160	180	190	HT-18
MILLIS	140	160	170	HT-18
MULHOLLAND	195	215	225	HT-18
NELSON,R	195	215	225	HT-18
O'CONNELL	195	215	225	HT-18
PARSONS,N	210	230	240	HT-18
PARSONS,R	170	190	200	HT-18
PETROSINO	160	180	190	HT-18
PICHA	180	200	210	HT-18
REGIS	215	235	245	HT-18
ROBIE	125	145	155	HT-18
ROSEANO	180	200	210	HT-18
ROSEANU	160	180	190	HT-18
SCARFO	190	210	220	HT-18
SCHEIMREIF	220	240	250	HT-18
SCHUBRING	195	215	225	HT-18
SCOTT	190	210	220	HT-18
SING	115	135	145	HT-18
SIVERS	200	220	230	HT-18
SKALSKI	145	165	175	HT-18
SNELL	185	205	215	HT-18
SPARKOWSKI	190	210	220	HT-18
SPLATT	200	220	230	HT-18
SPURLIN	190	210	220	HT-18
STERRETT	160	180	190	HT-18
TYLER	200	220	230	HT-18
TYRON	200	220	230	HT-18
WALDRON	195	215	225	HT-18
WEPPLO	135	155	165	HT-18
WILL	155	175	185	HT-18
ASPHOLM	170	190	200	HT-28
BASTEMEYER	200	220	230	HT-28
BAXTER	190	210	220	HT-28
BLUME	210	230	240	HT-28
BREAK	135	155	165	HT-28
BUGBEE	210	230	240	HT-28
CHAMBERS	210	230	240	HT-28
CARD	170	190	200	HT-28
CHANG	165	185	195	HT-28
CLARK	180	200	210	HT-28
COCO	170	190	200	HT-28
COLLINS	140	160	170	HT-28
COOPER	190	210	220	HT-28
COUILLARD	180	200	210	HT-28
CURRY	190	210	220	HT-28
CURTIS	190	210	220	HT-28
DAU	190	210	220	HT-28
DAVIS,J	215	235	245	HT-28
DAVIS,N	140	160	170	HT-28
DEBBINK	185	205	215	HT-28
EGAN	210	230	240	HT-28
ELLWOOD	200	220	230	HT-28
FREEMAN	175	195	205	HT-28
GIBBONS	218	238	248	HT-28
GORMLEY	170	190	200	HT-28
GOULD	190	210	220	HT-28
GRANCAGNOLO	230	250	260	HT-28
GYZBOWSKI	210	230	240	HT-28
HAFENSTEINER	120	140	150	HT-28
HELGERSON	215	235	245	HT-28
HILL	175	195	205	HT-28
HOPPER	160	180	190	HT-28
HUDSON	220	240	250	HT-28
ISBELL	190	210	220	HT-28
JACOBS	225	245	255	HT-28
JUDD	160	180	190	HT-28
KARR	180	200	210	HT-28
KELLNER	200	220	230	HT-28
KENSHALO	180	200	210	HT-28
KERZIE	140	160	170	HT-28
KLUMP	255	275	285	HT-28
KLYNMAN	130	150	160	HT-28
KOLCZYNSKI	210	230	240	HT-28
KORVER	185	205	215	HT-28
KROLL	135	155	165	HT-28
LENICK	185	205	215	HT-28
LONG	200	220	230	HT-28
MARCUM	150	170	180	HT-28
MARTIN	230	250	260	HT-28
MAUSTELLER	225	245	255	HT-28
MCKERREN	225	245	255	HT-28
MINETTE	180	200	210	HT-28
MOORE	200	220	230	HT-28
MOURITSEN	180	200	210	HT-28
NEASE	175	195	205	HT-28
O'BRIEN	150	170	180	HT-28
OUELLETTE	185	205	215	HT-28
PAGLIARULO	170	190	200	HT-28
PARKINGTON	145	165	175	HT-28
PAVELKO	180	200	210	HT-28
PELZER	235	255	265	HT-28
PETERSEN	230	250	260	HT-28
PUSINS	195	215	225	HT-28
REYNOLDS	205	225	235	HT-28
SHIPP	200	220	230	HT-28
SKELLEY	165	185	195	HT-28
SLEEPER	190	210	220	HT-28
SNIPES	150	170	180	HT-28
SONCINI	215	235	245	HT-28
STEWART	175	195	205	HT-28
STILES	160	180	190	HT-28
STREFF	180	200	210	HT-28
SWEENEY	185	205	215	HT-28
TEMPLIN	175	195	205	HT-28
TOPP	160	180	190	HT-28
TRAMELL	210	230	240	HT-28
TREMAINE	215	235	245	HT-28
TROUBLEFIELD	190	210	220	HT-28
UMEMURA	200	220	230	HT-28
VIRDEN	185	205	215	HT-28
WARD	210	230	240	HT-28
WEBB	220	240	250	HT-28
WEITHMAN	180	200	210	HT-28
WESTERMANN	190	210	220	HT-28
WHEATON	170	190	200	HT-28
WILLSEY	230	250	260	HT-28
WOOTEN	180	200	210	HT-28
WRIGHT	145	165	175	HT-28
YODER	200	220	230	HT-28
LAMI	216	226	234	HITU
SCOTT	210	220	228	HITU
CHAMBERS	210	220	228	HITU
WRIGHT	152	162	170	HITU
FROSLEE	147	157	165	HITU
ROSENAU	170	180	188	HITU
ROSA	175	185	193	TW-5
LABERGE	210	220	228	TW-5
FARMER	250	260	268	TW-5
SULPIZIO	180	190	198	TW-5
ROBBINS	180	190	198	TW-5

How To Use

This applet mimics the weight and balance form used by TW-5 aircrews flying the TH-57B/C

After completion of the form, you may copy the url to share the results with another crew member, instructor, or duty officer.

Remember: "Garbage in, garbage out." Your form will only be as accurate as the information you enter into the appropriate fields. Some entries have no effect on the final result and are for information purposes only. Other entries are used in the calculation of total weight and center of gravity.

Event

The event field is for information purposes only.

Instructor

Start typing your instructor's last name to bring up a dropdown of options matching the typed characters. Pick the appropriate instructor (be careful with common last names). The instructor's weight with wet vest will autopopulate into the form. You may select the dry vest weight or manually change the weight as necessary. The instructor weight value will be used to calculate Crew Forward weight.

The instructor list can be viewed from the "Inst List" tab to quickly verify all weights are current.

Aircraft

Aircraft are listed numerically in the dropdown box. Select "unkB" or "unkC" if you do not have an aircraft assigned. The form will automatically calculate heaviest and most forward CG for your series of aircraft. If an aircraft is selected, the weight and moment will be autopopulated into the form. The aircraft spot is for information purposes only.

The aircraft list can be viewed from the "A/C List" tab to quickly verify all weights and moments are current.

Weather

The current and forecast weather are for information purposes only.

Date

The date will autopopulate to today's date. It is for information purposes only.

Student

Student name is for information purposes only, but will help identify who completed the form when it is sent to another person.

Student Weight

Enter the student weight including all gear. This does not include any bags or passengers which will be entered later. Student weight is used to calculate Crew Forward.

Max Temperature, Pressure Altitude, and Density Altitude

These values are obtained from the DD-175-1. Only the Density Altitude is used to calculate HIGE/HOGE power requirements. Temperature and PA are for information purposes only, but may be used to manually calculate DA.

Fuel

Select presets of 70 or 65 gallons, or a manually enter fuel in gallons. The "Set Max" button will set the maximum amount of fuel, up to 91 gallons, to keep the aircraft below 3200 lbs given the current Takeoff Gross Weight.

Crew Aft

Enter the weight of any passengers or rear crew members.

Baggage

Enter the weight of any gear loaded into the cargo area.

External Load Operations

Check the "External OPS" checkbox to bring up the external ops section and include it in the overall calculations. Set the expected fuel load at the time of the first pick, the weight of the crewman, and the weight of the load. The "Set Max" button will calculate the maximum fuel load you may take to remain below 3350 lbs with the load and 3200 lbs without the load.

Results Table

The results table is color coded to quickly see all parameters in limits or any problem areas. When out of limits, the field will become red and a yellow caution emoji will be displayed. The HIGE/HOGE field will turn yellow when HIGE is above 85% Q and red when HIGE is above 100% Q.

Copy Permalink

The permalink will automatically copy the current url to your clipboard to be shared. The url encodes information to display the same form on another device.

Reset Form

The reset button will clear out all form values. This can be undone by hitting the back button in your browser and refreshing the page with a fully encoded url.