1801/PCN/FORM F Flashcards
1801
Types of Flight
S - Scheduled Air Transport N - Nonscheduled Air Transport G - General Aviation M - Military X - Other than any of the defined categories above
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Flight Rules I
If it is intended the entire flight will be operated under IFR
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Flight Rules Y
If the flight initially will be operated under IFR followed by one or more subsequent changes of flight rules
1801
Flight Rules V
If it is intended that entire flight will be operated under VFR
1801
Flight Rules Z
If the flight initially will be operated under VFR followed by one or more subsequent changes of flight rules
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Wake Turbulence Category M
Medium 15,501 - 299,999 lbs.
Maximum certified aircraft take-off weight
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Equipment Code: S
Standard Equipment is considered to be VHF RTF, VOR and ILS
1801
Equipment Code: D
DME
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Equipment Code: G
GNSS
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Equipment Code: H
HF RTF
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Equipment Code: I
INERTIAL NAVIGATION
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Equipment Code: M1
ATC RTF SATCOM (INMARSAT)
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Equipment Code: R
Performance Based Navigation: PBN codes described in Box 18
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Equipment Code: T
TACAN
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Equipment Code: U
UHF RTF
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Equipment Code: W
RVSM APPROVED
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Equipment Code: X
MNPS APPROVED
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Equipment Code: Y
VHF with 8.33 kHZ channel spacing
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Equipment Code: LB1
Transponder - Mode S including aircraft identification, pressure altitude, extended quitter (ADS-B) and enhanced surveillance capability
ADS-B with dedicated 1090 MHz ADS-B “out” capability
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FLIGHT RULES
V - VFR
I - IFR
Y - IFR TO VFR
Z - VFR TO IFR
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Cruising Speed Types
Knots “N”
Mach “M”
Kilometers per Hour “K”
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Level Types
Flight Level “F”
Altitude in Hundreds of Feet “A”
Altitude in tens of meters “M”
VFR
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STS/
STATUS/SPECIAL HANDLING
STATE
SAR - Search and Rescue
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PBN/
Indication of RNAV and/or RNP capabilities
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PBN/A1
RNAV 10 (RNP 10)
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PBN/B1
RNAV 5 ALL PERMITTED SENSORS
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PBN/C1
RNAV 2 ALL PERMITTED SENSORS
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PBN/D1
RNAV 1 ALL PERMITTED SENSORS
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PBN/L1
RNP 4
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PBN/O1
BASIC RNP 1 ALL PERMITTED SENSORS
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PBN/S2
RNP APCH WITH BARO-VNAV
1801
NAV/GPS
Significant date related to navigation equipment, other than the PBN codes
PER/D
Aircraft Performance Data
Approach Speed Category D - 141 to 166 knots
PCN
Pavement Classification Number
R-Rigid
F-Flexible
A - High Strength
B - Medium Strength
C - Low Strength
D - Ultra-Low Strength
W - High; no tire pressure limit
X - Medium; tire pressure limited to 254 psi
Y - Low; tire pressure limited to 181 psi
Z - Very Low; tire pressure limited to 73 psi
T - Technical study
U - Based on “using aircraft” experience
Form F
MAC
MEAN AERODYNAMIC CORD (MAC). The theoretical average or mean chord of a lifting surface such as the wing of a fixed-wing aircraft. Typically, a wing chord is longer at the root near the body and it tapers to a shorter chord at the tip. The MAC is a statistical, overall average chord, representative of an entire wing, used in aerodynamic computations and analysis.
%MAC = [(CG - LEMAC)/Wing Length] X 100
Because Wing Length = TEMAC - LEMAC, then:
- if our CG is at the TEMAC, then we have 100%MAC.
- if CG is at LEMAC, then we have 0% MAC
