P6-4 P18-3 Low Air flow detected (*) Or Sensor Power Loss (*) Possible causes for the air mass flow to drop are failure of the cooling fan, a clogged air filter and a even cabin decompression. For the

P6-4AB ENG. Bleed Air Temperature > 254 degree C / 490 degree F Or ENG. Bleed Air Pressure > 220 PSI On GND. Refer to MEL 36-05 [Engine Bleed Air Shutoff Valve], MEL 36-09 [High Stage Valve], MEL

Accomplish this NNC only when directed by the NNC [Smoke, Fire or Fumes] i.e. in the following cases : - anytime the smoke or fumes become a serious threat to the crew or passengers - after the smoke,

Note : Do not use this NNC for annunciated smoke, fire or fumes events, such as engine and APU fire, cargo fire, wheel well fire, window arcing or lavatory smoke. for the latter however, consider accomplishing

Do not use RAAS callouts or alerts for navigation. Do not use RAAS callouts or alerts as a substitude for NOTAM or ATIS information. Narrow Runway (30m) Operation Max crosswind component at 10m (32.8 ft)

Condition : During a ground start, an abort engine start condition occurs. On GND The conditions to abort and an engine start are published in FCOM [Engine Start Procedure] and further by [Cold Weather

P6-3B Gear Lever Lock Solenoid “LATCH & PRESS WARN” “AIR/GND RELAY” P6-3D Air/Gnd Relay “AIR/GND RELAY” This NNC applies to the Landing Gear Lever! If the Landing Gear Lever moves UP, but the Landing

If brakes produce smoke after landing and/or Brake Temp amber light (as installed) is illuminated or the Brake Temperature Monitoring System (as installed) indicates a brake temperature of 5 units or more

P92-CF (EMDP) Transfer Bus 2 - 115v ac (EMDP) P6-2B (EDP) DC Bus 1 Sect 22 - 28v dc (EDP) System A Hydraulic Pressure near 0 PSI or System A Hydraulic Quantity near 0 USG or Both Hydraulic Pump LOW PRESSURE

Fuel Quantity Indicator error annunciation? Yes > NNC FUEL QTY IND INOP No > Crossfeed (was) open? Yes > With all Main Tank Fuel Boost Pumps ON different fuel pump output pressure may still cause

Condition: UNABLE REQD NAV PERF-RNP is shown. The actual navigation performance is not sufficient. Choose one: On a procedure or airway with an RNP alerting requirement: Select an alternate procedure or

Condition: One or more of these occurs: An IRS fault occurs On the ground, if the ALIGN light is also illuminated, the present position entry is possibly incorrect. Choose one: On the ground: Go to step

P6-1D Transfer Bus 1 Sect 1-115v ac P18-2A Stanby Bus Sect 1-115 ac (as wired) Transfer Bus 2 Sect 2-115v ac (optional FMC 2) Condition : “FMC” message or MENU page on both (M) CDU Other indications are

Condition: The trailing edge flaps are less than 1. Objective: To configure for a landing with trailing edge flaps less than 1. Choose one: Trailing edge flap asymmetry exists: Go to step 2 Trailingedge

Condition: The trailing edge flaps are not in the commanded position. Objective: To configure the airplane for landing. Choose one: Trailing edge flap asymmetry exists: Go to the Trailing Edge Flap Asymmetry

Condition: Uncommanded stabilizer trim movement occurs continuously. Control column Hold firmly Autopilot (if engaged) Disengage Do not re-engage the autopilot. Control airplane pitch attitude manually

Condition : A flight control is jammed or restricted in roll, pitch, or yaw. Autopilot (if engaged) Disengage Autothrottle (if engaged) Disengage Verify that the thrust is symmetrical. Overpower the jammed

Condition : The leading edge devices fail to extend and trailing edge flaps are less than 1. Objective : To configure for a landing with leading edge devices retracted and trailing edge flaps less than

Correct Entry Code has been entered and the FDAS is programmed to automatically unlock after a time delay ➝ If the person that entered the correct access code is not identified or is not authorized to

Preflight Procedure - First Officer For EDTO flight, accomplish the following Fuel Crossfeed Valve Check on the ground prior to engine start: CROSSFEED selector - Open Verify that the VALVE OPEN light