AROW
Documentation required in aircraft (91.9, 91.203)
A | Airworthiness certificate |
R | US Registration |
O | Operating limitation |
W | Weight and balance |
HEAT-SAM
Required inspections (91.409, 91.413)
H | Hired for passengers or flight instruction | 100 hrs |
E | ELT | 12 mos |
A | Annual | 12 mos |
T | Transponder | 24 mos |
For IFR (91.411) | ||
S | Static pressure system | 24 mos |
A | Altimeter | 24 mos |
M | Mode C automatic pressure reporting system | 24 mos |
20/30 Rule
Fuel requirements (91.151, 91.167)
20 | 20 minutes, VFR day or night |
30 | 30 minutes, IFR day or night |
2/1 Flight Time
Rule of thumb for fuel consumption and flight time
R22 Beta II (10 gal/hr or 1 lb/min) or R44 Astro (15 gal/hr or 1.5 lbs/min) |
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2 | Main fuel gage is a 2-hour gage | |
1 | Aux fuel gage is a 1-hour gage |
CAMAFOOTS
Required VFR Equipment (91.205b)
C | Compass |
A | Airspeed indicator |
M | Manifold pressure |
A | Altimeter |
F | Fuel gage |
O | Oil temperature |
O | Oil pressure |
T | Tachometers (engine and rotor) |
S | Seatbelts |
TOMATOE A FLAMES
Required VFR Equipment (91.205b)
T | Tachometer |
O | Oil pressure |
M | Magnetic compass |
A | Airspeed indicator |
T | Temperature gage for liquid cooled engines |
O | Oil temp |
E | Emergency equipment (if beyond power-off glide distance over water, pyrotechnic signaling device and PFD) |
A | Anti-collision lights (AIRPLANES ONLY) |
F | Fuel gage |
L | Landing gear position indicator |
A | Altimeter |
M | Manifold pressure gage |
E | Emergency Locator Transmitter (AIRPLANES ONLY) |
S | Safety belts and shoulder harnesses |
GOAL-T
R22/R44 required equipment (POH)
G | Governor |
O | Outside air temperature gage |
A | Alternator |
L | Low rotor RPM warning system (light and horn) |
T | Electric or hydraulic trim (R44 only) |
NAIL-GI/CI
R22/R44 VFR night lighting (POH)
N | Navigation |
A | Anticollision |
I | Instrument |
L | Landing |
GI | Ground illumination |
CI | Celestial illumination |
FLAPS
Required equipment, Night VFR (91.205)
F | Fuses |
L | Landing light, if operated for hire |
A | Anti-collision lights |
P | Position lights (red on right is wrong) |
S | Source of electricity (battery, alternator, or generator) |
GRABCARD-N
Required IFR equipment (91.205d)
G | Generator/alternator |
R | Rate of turn/turn coordinator |
A | Sensitive altimeter |
B | Slip-skid indicator ball |
C | Clock with hours, minutes, and seconds |
A | Attitude indicator |
R | Radios (appropriate to navigation facilites used) |
D | Directional gyro |
N | Navigation equipment (other than GPS, appropriate to route) |
Taken alive, In a fix, Goin’ to heaven
Emergency squawk codes
7500 | Taken alive–hostage situation |
7600 | In a fix–lost radio communications |
7700 | Goin’ to heaven–emergency |
AVE-F, MEA, Clearance Limit
Lost communications procedures (91.185)
Squawk 7600 |
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If VFR | Remain VFR and land as soon as practicable, otherwise… | |
Route (AVE F) | ||
A | Assigned | Fly last assigned in ATC clearance, otherwise… |
V | Vectored | If being vectored, direct to fix, route, or airway specified in vector clearance, otherwise… |
E | Expected | Route as advised in Expected Further Clearance (EFC), otherwise… |
F | Filed | Route as filed in flight plan |
Altitude (MEA) | ||
M | Minimum | Minimum IFR altitude, otherwise… |
E | Expected | Expected altitude in EFC, otherwise… |
A | Assigned | Assigned altitude in last clearance |
Leave Clearance Limit | ||
If CL is IAF | Leave clearance limit at EFC time, if received; otherwise, as per flight plan ETA | |
If CL is not IAF | Leave clearance limit at EFC time; otherwise, proceed to IAF and descend for approach at ETA |
IP-TA-FERR
Position reporting (IFR)
I | Identification |
P | Position |
T | Time |
A | Altitude |
F | Flight conditions (VFR or IFR, for FSS only) |
E | ETA over next reporting point |
R | Name of next reporting point |
R | Remarks |
NEDD
Malfunction reporting (91.187)
N | N-number |
E | Affected equipment |
D | Degree affected |
D | Desired assistance |
AVRRRRTTTTTT Normal Vis
Required visual references for IFR landing (91.175)
A | Approach lights |
V | Visual glide slope indicator |
R | Runway |
R | …markings |
R | …lights |
R | …end identifier lights |
T | Threshold |
T | …markings |
T | …lights |
T | …zone |
T | …zone markings |
T | …zone lights |
Normal rate of descent and maneuver | |
Visibility prescribed for the approach |
VAAAACUM Loss Compromises Final ETA
IFR required reports (91.183, 91.187)
V | Vacating assgned altitude |
A | Altitude change, VFR-on-top |
A | Arrival at clearance limit (time and arrival) |
A | Arrive/leave holding fix (time and altitude) |
A | Any other safety of flight issue, incl hazardous weather |
C | Change of filed TAS, greater of +/- 5% or 10 knots |
U | Unable to climb/descend 500 ft/min |
M | Missed approach |
Loss | of any navigation, approach, or communication capability |
(If not in radar contact) | |
C | Compulsory reporting points or any fix used to define route |
F | FAF or OM inbound |
E | ETA change >3 minutes |
RAFT-V
Clearance items
C | Cleared to… |
R | Route |
A | Altitude |
F | Frequency for departure |
T | Transponder code |
V | Void time |
6 T’s
When crossing any fix or FAF
T | Turn to new heading |
T | Time |
T | Twist (set OBS/radios) |
T | Throttle, adjust power as necessary |
T | Talk, communications as required |
T | Track, bracket or track new course |
TIMES ABC
Pre-approach checks
T | Tune GPS, NAV/COM frequencies, and OBS |
I | Identify correct NAV station |
M | Marker beacon test/audio on |
E | External annunciators (GPS/NAV) |
S | Set altimeter |
A | Align DG and compass |
B | Brief approach procedures |
C | Compute speeds and runway required |
Very Good Airmen Do Procedures Right
VOR checks (91.171)
Within preceding 30 days | |
V | VOR test facility +/-4 degrees |
G | Ground checkpoint +/-4 degrees |
A | Airborne checkpoint +/-6 degrees |
D | Dual VOR receivers, within 4 degrees of eachother |
P | Prominent ground point along centerline of a VOR airway, >20 NM from VOR, +/-6 degrees |
R | Record (PEDS) date, place, bearing error, and signature |
ANDS
Compass acceleration error
AN | Accelerate north |
DS | Decelerate south |
UNOS
Compass turning error
UN | Undershoot north |
OS | Overshoot south |
IFR Certified GPS in lieu of ADF and DME
AIM 1.1.19
FOR | USE |
DME | DME at and above FL240 |
DME | Flying a DME arc |
Determining position over | a DME fix |
Determining position over | an NDB/compass locator |
Determining position over | a fix defined by an NDB/CL bearning crossing a VOR/LOC course |
Navigating TO/FROM | an NDB/CL |
Holding | Holding over an NDB/CL |
Weather within lateral limits of B, C, D, E to the SFC
Flight rules (91.155c-d, 91.157)
FOR | VISIBILITY AND CEILING |
VFR | 3 SM visibility and 1000′ ceiling |
SVFR | Helicopters, clear of clouds, day or night |
IFR/SVFR | Less than 3 SM visibility or 1000′ ceiling |
Substitutes for OM and MM
91.175
FOR | USE |
OM | CL, PAR, ASR, and (if authorized in IAP) DME, VOR, or NDB fix |
MM | Compass locator or PAR |
Where under 91.205b does it list in the acronymn CAMAFOOTS, manifold pressure? It does if you are a fixed wing pilot. But we are heli pilots and it doesn’t apply. It applies under the POH of Robinson’s list of MEL’s. For Rotorcraft under 91.205b it lists, seat belt and safety harness. So we can take everything else from CAMAFOOTS minus the M and add S, S and we have SOFATACOS.
91.205(b)(8): Manifold pressure gauge for each altitude engine.
Can you explain why this would only apply to fixed wing aircraft? Shoulder harnesses should also be included, since this is required under ~(17), depending on the date of manufacture.
Thanks for your comment!
Altitude engine….only altitude engine that would come close would be a P51 Mustang with a two stage supercharger. It still doesn’t apply to helicopters. I have been taught CAMAFOOTS forever as well and I believe if I reading and researching correctly, it’s incorrect.
Look it up…this is absolutely correct! Thanks Chris.
91.205-b-17
Helicopter manufactured after 1992 a shoulder harness for each seat
Yea technically speaking don’t need Manifold Pressure gauge for helicopter but good luck flying without it. Also if you read the FARS 91.9. You have to operate the helicopter within it’s operating limits per the POH. So how do you do that without a MAP Gauge