Communications:9M-MRO EHM Reports/Climb Report

Climb Report

	ACID	FLT	FM	FLCT	DATE	GMT	DPT	DST	GWT
	MRO	S370	CL	318	07/03/2014	16:52:21	WMKK	ZBAA	485880
	PALT	CAS	MACH	TAT	LAT	LONG	THDG	SWID	SFC
	22278	299.8	0.68	11.8	3.619	102.02	275	71002	19299
	A/P	A/T	FUELT	PKWD	DRTE	ASMT
	1	6	30	5030	8	5) Note 1
	ESN	N1	N2	N3	EGT	FMVDMD	FMVSEL	TRALOC
L	51463	93.9	96.6	77.8	778.2	71.3	71.3	65.9
R	51462	94	96.7	78.8	788.1	72.3	72.3	66.1
	P20	P160	P2.5	P30	P50	T20	T25	T30
L	8.39	14.503	70.32	294.8	11.3	11.7	275.2	590.6
R	8.369	14.534	69.79	294.1	11.2	11.7	273.4	590.8
	OILP	OILT	TRA	EPRACT	EPRMAX	EPRCMD	EPRTRA	VSV
L	99	146.8	65.9	1.342	1.363	1.336	1.34	47
R	100	144.8	66.1	1.342	1.366	1.339	1.341	52
	AVM	N1VA	N1VB	N2VA	N2VB	N3VA	N3VB	BBA	BBB	PHF	PHR
L	0	0.62	0.64	0.2	0.21	0.29	0.3	0.48	0.48	25	298
R	0	0.9	0.93	0.55	0.56	0.2	0.2	0.61	0.63	139	) Note 1
	TCAF	TCAR	PACK	PKFR	EBLD	EBFR	FAV	AOHE
L	553.5	501.8	0	217.6	0	163.2	0	0
R	547	512.5	0	217.5	0	154.1	0	0
	NAC1	NAC2	GENLD	WF	ESTAT	EECT	PTO	DP	FCC3	RATG
L	35	35	42	15583	3060	38	392	57	0E00	0058
R	27	29	46	15786	3060	41	392	55	0E00	0058
ALT	MACH	TAT	EPRACT-L	EPRACT-R	FNDERATESW
9536	0.449	23.5	1.302	1.302	28
15000	0.601	22.25	1.283	1.283	38
25024	0.722	9.5	1.34	1.34	08
	FCC4	FCC5	FCC6
L	0008	4200	0082
	0008	4400	0082

Note 1: The character, ), is generated by the ACMS to indicate that the source of information is valid and the parameter data bits are invalid.

AirCraft ID

Flight Number

Flight Phase

Report Copy number

Greenwich Mean Time

Greenwich Mean Time. Superseded by Coordinated Universal Time (UTC)

Departure Airport

Destination Airport

Gross Weight

Gross Weight

Malaysia Airlines Boeing 777 9M-MRO

ICAO 4-letter location indicator for Kuala Lumpur International Airport

ICAO 4-letter location indicator for Beijing Capital International Airport (formerly Peking)

Pressure altitude (feet)

Calibrated Airspeed, OR Calculated airspeed (knots) (Engine Health Monitoring Parameter)

Mach number

Aircraft speed relative to the speed of sound

Total Air Temperature (Degrees Celsius)

Latitude (degrees)

Longitude (degrees)

True Heading

Software Identification

Sub-Frame Counter (recorded data point)

Autopilot status

Autothrottle status

Fuel temperature in a/c tank - (Degrees Celsius)

ECS status (hexadecimal)

Thrust derate switch

Assumed Day Temperature (Degrees Celsius)

Engine serial number

N1 shaft speed (%)

N2 shaft speed (%)

N3 shaft speed (%)

Exhaust gas temperature - (Degrees Celsius)

Fuel metering valve demanded position

Fuel metering valve commanded position

Throttle resolver angle (degrees)

P20 pressure (inlet) (psi)

P160 pressure (bypass duct) (psi)

P25 pressure (HPC inlet) (psi)

P30 pressure (HPC outlet) (psi)

P50 pressure (LP turbine outlet) (psi)

T20 temperature (inlet) (Degrees Celsius)

T25 temperature (HPC inlet) (Degrees Celsius)

T30 temperature (HPC outlet) (Degrees Celsius)

Oil pressure (psi)

Oil temperature - (Degrees Celsius)

Throttle resolver angle (degrees)

EPR actual

EPR maximum

EPR commanded

EPR throttle angle

VSV angle (degrees)

Vibration monitoring system status (hexadecimal)

N1 shaft vibration channel A (ACU)

N1 shaft vibration channel B (ACU)

N2 shaft vibration channel A (ACU)

N2 shaft vibration channel B (ACU)

N3 shaft vibration channel A (ACU)

N3 shaft vibration channel B (ACU)

Broadband vibration channel A (ACU)

Broadband vibration channel B (ACU)

Vibration phase front (degrees)

Vibration phase rear (degrees)

Turbine cooling air front (Degrees Celsius)

Turbine cooling air rear (Degrees Celsius)

Cabin bleed

Pack mass flow rate (lb/s)

Environmental control system

Environmental control system bleed flow rate (lb/s)

ASCS FAMV Actual Position

Air Oil Heat Exchanger Position Selected

Nacelle temperature zone 1 (firewire resistance) ohms

Nacelle temperature zone 2 (firewire resistance) ohms

Generator load (shp)

Fuel flow (lb/hr)

EEC status

EEC temperature - (Degrees Celsius)

ASCS PC Out temperature (Degrees Celsius)

ASCS Duct Pressure (psi)

EEC status

EEC rating

Altitude

EPR actual - left

EPR actual - right

Thrust derate switch

EEC status

EEC status

EEC status

Aircraft Condition Monitoring System