N1 N1C N2 EGT FF PS13
N1 868 869 875 5850 1320 06892
N2 868 869 875 5850 1320 06892
P25 T25 P3 T3 P49 SVA
S1 11155 0557 1243 4313 06150 069
S2 11137 0556 1231 4324 06142 068
BAF ACC LP GLE PD TN P2 T2
T1 094 082 00 035 40 180 04219 N255
T2 096 082 00 023 36 180 04215 N271
ECW1 ECW2 EVM OIP OIT OIQH
V1 03D01 00008 08000 245 121 0000
V2 03D01 00008 08004 234 120 0000
VB1 VB2 PHA
V3 024 005 043
V4 007 001 078
WFQ ELEV AOA SLP CFPG CIVV
X1 02652 N003 0025 0000 N0001 0001
X2 02772 N001 0025 0000 N0000 0003
RUDD RUDT AILR AILL STAB ROLL YAW
X3 0000 0008 N001 N006 N008 N000 N000
RSP2 RSP3 RSP4 RSP5 FLAP SLAT
X4 N000 0000 0000 0000 0000 0000
X5 0000 0000 0000 0000 0000 0000
THDG LONP LATP WS WD FT FD
X6 1905 E0019 N450 050 011 0110 XXXX
X7 XXXX E0019 N450 050 011 0108 0785
Flight Operations & Line Assistance Getting to Grips with Aircraft Performance Monitoring
HOW TO RECORD IN-FLIGHT PARAMETERS
4.4.2.1.3. Parameters taken from report <02>
Report output APM input Remarks Codification example
A/C TAILNO Tail Number XXXXXX
DATE DATE Date AAA99
FLT FLNO Flight Number 9999
UTC FCASE Hour/min. taken far case ident 999999
CODE - Trigger logic code (see below for details) 5000 or 4000 on all fly-by-wire aircraft depending on the engine type fitted on the aircraft.
DMU/SW For aircraft/engine type check and report XXXXXX
CODE format variations. The last three digits allo stable frame identification X=Engine type (C=cfm, I=IAE) X=Engine version 1…8 X=Hardware number 0..9 XXX=Software version(001..009)
Two values read. Enter the mean value. Standard altitude (eg –500 or 35000 ft)
ALT ALT Mach Number (eg 0.78) X9999 (eg N0500 or 35000)
MN MACH Total Air Temperature (eg –10°C) 999 (eg 780)
TAT TAT X999 (eg N100)
Values from two systems read. Enter the mean value.
GW MASS Gross Weight 9999
CG CFPG CG FPAC Center of gravity Calculated Flight Path Acceleration 999
CIVV VV (-0.9999 to 4.0000 g) Calculated Inertial Vertical Speed N9999 to 40000
(-999 to 999 ft/min) N999 to 0999
THDG THDG True Heading (0° to 359.9°) 0000 to 3599
LATP LAT Latitude (N89.9° to S89.9°) N899 to S899
WS CWI Wind speed (0 to 100 kt) 000 to 100
WD DWI Wind direction (0° to 359°) 000 to 359
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：getting to grips with aircraft performance monitoring(39)
