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denomination changes to /P.
CFM56-5B/”non-P” engine can be intermixed with CFM56-5B/P engine on the same aircraft.
Note 15:
On the series A321-200, one Additional Center Tank (ACT) in bulk version is defined by modification 25453 (high pressure
system). Its approval together with structural and system provisions was subject of compliance demonstrated to Advisory
Circular (AC) 25-8.
Note 16:
The type design definitions and certification standard equipment lists as referenced in Note 4 above are complemented by
document 00D000A0546/C0S “A319-100/A321-200 FMGC Type Standard Evolution”.
Note 17:
On the series A321-200, one or two Additional Center Tanks (ACT) in bulk version are defined by modification 30422 (low
pressure system). Their approval together with structural and system provisions was subject of compliance demonstrated to AC
25-8.
Note 18:
On the series A321-200, Weight Variant 001, VFE speed in Configuration 1 is increased from 230 to 235 kts, and in
Configuration 1+F increased from 215 to 225 kts (as identified by speed limitation placard installed by modification 28960).
Note 19:
If modification 26610 is embodied on A321-111airplanes, the engine performance and gaseous emission levels are improved.
The engine denomination changes to /2P (DAC IIC Dual Annual Combustor).
CFM56-5B1/P engine can be intermixed with CFM56-5B1/2P (DAC IIC Dual Annual Combustor) engine on the same aircraft
(AFM Supplement).
Note 20:
If modification 27640 is embodied on A321-211airplanes, the engine performance and gaseous emission levels are improved.
The engine denomination changes to /2P (DAC IIC Dual Annual Combustor).
CFM56-5B3/P engine can be intermixed with CFM56-5B3/2P (DAC IIC Dual Annual Combustor) engine on the same aircraft
(AFM Supplement).
A28NM Page 21 of 22
DATA PERTINENT TO ALL MODELS
Auxiliary Power Unit (APU)
GARRETT AIRESEARCH GTCP 36-300(A) (Standard)
(Specification 31-5306B)
APIC APS 3200 (Option - Mod 22562)
(Specification ESR 0802, Rev A)
AlliedSignal 131-9[A] (Option – Mod 25888)
(Specification 4900 M1E 03 19 01)
APU Limits:
GTCP 36-300 (A)
- Maximum Allowable Speed 69,204 rpm (107 %)
- Maximum Gas Temperature
at turbine outlet (ISA + 35°C)
rated output 638°C
overtemp. shutdown 711°C
Maximum on starting 1038°C
APS 3200
- Maximum Rotor Speed 49,300 rpm (105 %)
- Maximum EGT 742°C
- Maximum for Start 900°C at altitudes below 25000 ft
982°C at altitudes below 25000 ft
131-9[A]
- Maximum Allowable Speed Nominal 51,728 rpm (106 %)
Overshoot 53,875 rpm (110 %)
- Maximum Gas Temperature
at turbine outlet 675°C
rated output (ISA + 23°C) 585°C
overtemp. shutdown (ISA) 706°C
maximum on starting (ISA) 1080°C below 35000 ft,
1108°C above 35000 ft
(ISA + 40°C) 1090°C below 35000 ft,
1120°C above 35000 ft
APU Approved oils:
See GARRETT Report GT-7800 or in conformity with MIL-L-IAS, MIL-L23699 or DERD 2487 for the GTCP 36-300, Usable
Capacity: 5.8 liters
See APIC Maintenance Manual for approved oils for the APS 3200
See Model Specification 31-12048A-3B for Allied Signal 131-9[A]
Center of Gravity Range (% Mean Aerodynamic Chord):
See DGAC-Approved Airplane Flight Manual, U.S. Version.
Hydraulic Fluids:
- Type IV - Specification NSA 30.7110.
- Capacity (Reservoirs and Systems):
System Liters Gallons
Green 100 26
Yellow 75 20
Blue 60 16
Pressure: 3000 ± 200 PSI (207 ± 4 bar)
A28NM Page 22 of 22
Tires:
- See Airbus Service Bulletin (SB) A320-32-1007
Datum:
Station 0 (100 inches forward of fuselage nose).
Reference Mean Aerodynamic Chord (MAC):
165.10 inches / 4.1935 m (leading edge of MAC: Sta. 700.85 inches).
Leveling Means:
Clinometer on the cabin seat track rails.
Service Information:
- Service bulletins, structural repair manuals, vendor manuals, aircraft flight manuals, and overhaul and maintenance manuals,
which contain a statement that the document DGAC-approved, are accepted by the FAA and are considered FAA approved.
These approvals pertain to the type design only. The reference to service bulletins includes any type of service instructions
(letters, repair approvals, etc.). The reference to DGAC-approved includes findings made by DGAC designees and/or design
organizations which are equally as acceptable as those made directly by the DGAC.
- Other available service documents for the Airbus include:
a. Illustrated Parts Catalog
b. Wiring Diagram Manual
c. Maintenance Manual
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