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Crew . . . . . . . . . . . . . . . . . . 2
Passengers . . . . . . . Up to 180 (dense)
Typical Two-class . . . . . . 150
2 CFMI CFM56-5 or
2 IAE V2500 with up to 26,500lb thrust each
Two crew member design
Two primary flight displays (PFD)
Two navigation displays (ND)
Electronic Centralised Aircraft Monitor (ECAM)
Two Multipurpose Control and Display Units (MCDU)
Span 111ft 10in
Length 123ft 23in
Height 38ft 7in
Fuselage width 12ft 11in
wing sweepback 24.96 deg. @ quarter chord
wing area 1,317.5sq ft
Range 2,700 - 2,900nm
MTOW 162,000lb
MLW 142,200lb
MZFW 134,500lb
operating weight empty 92,100lb
max fuel capac. 6,300USg
Engine thrust 2x 25,000lb - 26,500lb
Range (with 150 passengers):
2,900nm
Max operating speed 350kts 0.82mach
Max cruise speed 487kts @
28,000ft 454kts @37,000ft
TO field length 5,630ft
Landing field length 4,750ft
NWA A320-200 / CFM56-5A1 -- Check List | |
| SAFETY CHECK | |
| Landing Gear Lever........................................Down | |
| Engine Master Switches....................................Off | |
| START CHECKLIST | |
| Logbook...................................................Checked | |
| Circuit Breakers..........................................Normal | |
| ADIRS (inertial navigation system)........................NAV | |
| Oxygen....................................................On | |
| Emergency Lights..........................................Armed | |
| Pressurization............................................Auto | |
| Engine/Wing Anti-Ice......................................Off | |
| Air Conditioning..........................................Set | |
| Electrical................................................Set | |
| Hydraulics................................................Set | |
| Fire Pushbuttons..........................................In | |
| Instruments...............................................Flags Normal | |
| Altimeters................................................Set | |
| ECAM (systems monitor)....................................Doors, Status Checked | |
| Fuel......................................................Check Release Minimum | |
| Check Fuel on Board | |
| Anti-Skid/Nose Wheel Steering.............................On | |
| Gear......................................................Down & Green | |
| Switching.................................................Normal | |
| Takeoff Warning...........................................Checked | |
| Engine Master Switches....................................Off | |
| MCDU......................................................Set | |
| FINAL ITEMS BEFORE GATE DEPARTURE | |
| ADIRS.....................................................Align Lights Out | |
| Beacon....................................................On | |
| Fuel Pumps................................................Auto & On | |
| Sliding Windows...........................................Both Locked | |
| Doors.....................................................All Green, Slides Armed | |
|
| |
| BEFORE TAXI CHECK | |
| Engine/Wing Anti-Ice.......................................Off (On) | |
| ECAM Status................................................Checked | |
| Wave Off...................................................Received | |
| TAKEOFF CHECK | |
| Allowable Takeoff Weight (166,400 lbs).....................Checked | |
| Flaps......................................................Set 1+F, Green | |
| Or 3+F, Green | |
| Trim.......................................................Set | |
| APU........................................................Off | |
| Controls...................................................Free & Normal | |
| Thrust Mode................................................Take Off (Flex Set) | |
| V Bug + __ kts.............................................Checked & Set | |
| FINAL TAKEOFF ITEMS (at runway) | |
| Packs...(Air Conditioning).................................On (Off) | |
| Takeoff Memo...............................................All Green | |
| Engine Mode Selector.......................................Ignition | |
| Flaps......................................................Set 1+F Or 3+F | |
| Transponder................................................Code Set, Auto | |
| CLIMB CHECK | |
| Landing Lights.............................................Retract | |
| Packs......................................................On | |
| Gear.......................................................Up | |
| Engine Mode Selector.......................................Normal (Ignition) | |
| Flaps......................................................Up | |
| Speed Brakes...............................................Disarmed | |
| AT 18,000 ft MSL | |
| Altimeters.................................................Standard (29.92) | |
| DESCENT CHECK | |
| Pressurization.............................................Checked | |
| Allowable Landing Weight (141,900 lbs).....................Checked | |
| APPROACH CHECK (10,000') | |
| Altimeters.................................................Set | |
| V Bug + __ kts.............................................Set | |
| ECAM Status................................................Checked | |
| Approach Briefing (IFR/VFR)................................Complete | |
| LANDING CHECK | |
| Approach Freq & Courses(ILS,ADF,MARKERS)...................Set | |
| RADIO ALTIMETER............................................Set | |
| Altimeter..................................................Set | |
| Auto Brakes................................................Armed | |
| Engine Mode Selector.......................................Ignition | |
| Missed Approach Procedure..................................Checked | |
| FINAL LANDING ITEMS | |
| Gear.......................................................Down | |
| Flaps......................................................Set 3+F/4+F Green | |
| Speed Brakes...............................................Armed | |
| AFTER LANDING CHECK | |
| Landing Lights.............................................Retract | |
| Engine/Wing Anti-Ice.......................................Off | |
| Engine Mode Selector.......................................Normal | |
| Flaps......................................................Up | |
| Speed Brakes...............................................Disarmed | |
| Radar......................................................Off | |
| APPROACHING THE GATE | |
| APU........................................................Start | |
| AFTER PARKING AT GATE | |
| Beacon.....................................................Off | |
| Fuel Pumps.................................................Off | |
| Engine Master Switches.....................................Off | |
| Brakes.....................................................Off | |
| SECURING CHECK | |
| ADIRS......................................................Off | |
| Oxygen.....................................................Off | |
| Exterior Lights............................................Nav On | |
| APU Bleed..................................................Off | |
| Integral Lights............................................Off | |
| Transponder................................................Standby | |
| Emergency Exit Lights......................................Off | |
| APU Master Switch..........................................Off | |
| Battery 1 & 2..............................................Off | |
| CLB |
| V1,Vr,V2 Take-Off speeds @ 150,000#, 145,000#, and 140,000# |
| (ISA Conditions) / Configure 1: Flaps+1 (Flaps 2 is never used for T/O @ NWA) |
| T/O weight V1 / Vr / V2 Flaps |
| 150,000# 148 /148 /148 1+F |
| 145,000# 146 /146 /146 " |
| 140,000# 143 /143 /143 " |
| ROC(FPM) and speed (Kts) (Below 10,000') |
| aprox. 3800 FPM at 250 Kts |
| ROC(FPM) and climb speed (Kts/Mach) (Above 10,000' to Cruise FL) |
| aprox. 2200 FPM at 310 Kts (from 10,000' - 20,000') |
| aprox. 1800 FPM at 310 Kts (from 20,000' - 26,000') |
| aprox. 1200 FPM at .78M (from 26,000' - 35,000') |
| --------------------------------------------------------------- |
| CRZ |
| Typical Cruise Speed @ 135,000# (IAS/Mach cruise) FL350 |
| Standard Cruise Speed at NWA is .78M at all weights from FL310 thru FL390 |
| LRC (Long Range Cruise) @ 135,000# |
| FL390 - FL370 = .79M |
| FL350 = .78M |
| FL330 = .77M |
| FL310 = .74M |
| FL290 = .71M |
| MCC (Minimum Cost Cruise) Varies with winds, fuel costs, crew costs, |
| altitude, and weight. Not calculated at this time. |
| ------------------------------------------------------------ |
| DSC |
| ROD(FPM) and speed (Mach/Kts) (From Cruise FL to 10,000') |
| Hold .78M 'til 290 Kts. Idle power - aprox. 2500 FPM |
| ROD(FPM) and speed (Kts) (Below 10,000' to FAF) |
| ROD (rate of descent) varies with ATC requirements, but is between 1000 |
| and 3000 FPM. In a "Perfect World" - 250 Kt idle descent, then slow and |
| configure on speed so as to not add power until on glide slope. |
| Vref Approach Bug speeds @ 130,000#, 135,000#, and 140,000# |
| Flaps FULL |
| LNDG weight Vref Flaps |
| 130,000# 129 FULL |
| 135,000# 132 " |
| 140,000# 134 " |
AIRPORT OPERATIONS: |
| Runway slope (mean) +/- 2% |
| Runway altitude 8000 ft |
| Wind: |
|
| X wind: max demonstrated for takeoff 29 Kt |
| X wind: max demonstrated for landing 33 Kt |
| X wind: max demonstrated gust 38 Kt |
| max tail wind 10 Kt |
| *Max crosswind values have been demonstrated with flight controls in normal law as well as in direct law with and without yaw damper. |
|
SPEED LIMITATIONS: |
| VMCA 105 Kt |
| VMCG conf 1 + F 107 Kt |
| conf 2 105 Kt |
| conf 3 105 Kt |
MAX FLAPS, SLATS speeds: |
| POS SLATS FLAPS SPD REMARKS |
1 18 0 230 Int.Appr 1 18 10 215 T.O. 2 22 15 200 T.O./Appr 3 22 20 185 T.O./Appr/Ldg 4/FULL 27 35 177 LDG |
GEAR DOWN SPEEDS: |
| Max speed with landing gear extended (VLE) 280 Kt/ M.67 |
| Max speed at which the landing gear may be extended (VLO extension) 250 Kt |
| retracted (VLO retraction) 220 Kt |
| MAX TYRE SPEED: |
| Ground speed 195 kt |
POWER PLANT: |
Thrust Setting/EGT Limits: |
| OPERATING CONDITION TIME EGT |
| LIMIT LIMIT |
| TO and GA 5 min 890 C |
| MCT unlim 855 C |
| CL unlim 855 C |
| Starting 725 C |
OIL: |
| Max continuous temperature 140 C |
| Max transient temperature (15 min) 155 C |
| Minimum starting temperature -40 C |
RPM: |
| N1 max 102% |
| N2 max 105% |
REVERSE THRUST: |
Selection of REV thrust in flight is prohibited |
| Backing of aircraft with reverse thrust is not permitted. Maximum reverse should not be used below 70 Kts (idle reverse is allowed down to a/c stop). |
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