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considered equivalent to "FAA-approved".)
Note 3:
Life limitations are provided in the A319/A320/A321 Maintenance Planning Document, Section 9 “Airworthiness
Limitation Section”, Sub-Sections 9-1-2 and 9-1-3 - Approved by DGAC.
Note 4:
The A320 basic definition for U.S. import certification is contained in the following documents:
- AI/A 414.282/88 for the A320 Models -111 and -211
- AI/EA-A 413.628/89 for the A320 Model -231
- AI/EA-A 412.1631/90 for the A320 Model -212
- AI/EA-A 414.0665/93 for the A320 Model -232
- AI/EA-S 413.2143/95 for the A320 Model -233
- AI/EA-S 413.0150/95 for the A320 Model -214
- AI/EA-S 413.3004/96 (supplement) for the A320 Model -214.
Note 5:
Maintenance criteria to comply with certification requirements for systems are given in Airbus Document AI/ST4/955.061/89
“Certification Maintenance Requirements (FAA version)” (CMR).
Maintenance criteria to comply with certification requirements for structure are given in Airbus Document AI/SEM4/
95A.0252/96 “Airworthiness Limitation Items”.
Note 6:
If modification 20758 is embodied, the airplane is certified for CAT III B precision approach (fail operational) and landing. This
does not constitute an operational approval.
Note 7:
All Models of A320 airplanes manufactured after January 1, 1997 must have either modification 25302 (for IAE engines) or
25303 (for CFM engines) installed, before the individual U.S. standard Certificate of Airworthiness can be issued.
Note 8:
If modification 25800 is embodied on models with CFM56-5B engines, the engine performance is improved. The engine
denomination changes to /P.
CFM56-5B/”non-P” engine can be intermixed with CFM56-5B/P engine on the same aircraft.
A28NM Page 14 of 22
Note 9:
If modification 26610 is embodied on A320-214 airplanes, the engine performance and gaseous emission levels are improved.
The engine denomination changes to /2P (DAC IIC Dual Annual Combustor).
CFM56-5B4/P engine can be intermixed with CFM56-5B4/2P (DAC IIC Dual Annual Combustor) engine on the same aircraft
(AFM Supplement).
Note 10:
For A320-200 series airplanes with OCTOPUS Airplane Flight Manual, Airbus elected to comply with Part 25 Amendment 25-
92.
III. Type A321-100/200 Series Transport Category Airplanes
Model A321-111, Approved December 20, 1995;
Model A321-112, Approved December 20, 1995;
Model A321-131, Approved December 20, 1995;
Model A321-211, Approved September 18, 1997;
Model A321-231, Approved September 18, 1997:
Engines:
Model A321-111, Two CFMI Model CFM56-5B1 or CFM56-5B1/P or CFM56-5B1/2P jet engines;
Model A321-112, Two CFMI Model CFM56-5B2 or CFM56-5B2/P jet engines;
Model A321-131, Two IAE Model V2530-A5 jet engines
Model A321-211, Two CFMI Model CFM56-5B3/P or CFM56-5B3/2P jet engines
Model A321-231, Two IAE Model V2533-A5 jet engines
See Note 14 for description of “P” engine designations
Fuel:
See Installation Manual - Documents CFM 2026 or IAE-0043
SPECIFICATION
NOMENCLATURE FRANCE U.S.A U.K.
Kerosene MIL-T83133A (JP8)
Air 3405C ASTM D 1655 (JET A1) (JET A) DERD 2494
Wide Cut Air 3407 ASTM D 1655 (JET B) DERD 2454
Air 3407 (TR4) MIL-T 5624 (JP4) DERD 2454
High Flash Point Air 3404 MIL-T 5624 (JP5) DERD 2452
Additives: See CFMI "Specific Operating Instructions," CFM TPOI-13 or IAE V2500 “Installation and Operating Manual”
IAE-0043, 4.5. The above mentioned fuels and additives are also suitable for the APU.
Engine Limits
CFMI CFM56-5B1 or -5B1/P
or –5B1/2P
CFMI CFM56-5B2 or -5B2/P CFMI CFM56-5B3/P
or –5B3/2P
Engine Limitation Data Sheets Data Sheets Data Sheets
E37NE E38NE (FAA) E37NE E38NE (FAA) E37NE E38NE (FAA)
Static Thrust at Sea Level
- Take-off (5 min)** 13 344 daN (30,000 lb) 13 789 daN (31 000 lb) 14 234 daN (32,000 lb)
(Flat rated 30°C)
Maximum Continuous 12 940 daN (29,090 1b) 12 940 daN (29,090 1b) 12940 daN (29,090 lb)
(Flat rated 25°C)
Maximum Engine Speed
- N1 rpm (%) 5,200 (104) 5,200 (104) 5,200 (104)
- N2 rpm (%) 15,183 (105) 15,183 (105) 15,183 (105)
Max Gas Temperature
(°C)
- Take-off (5 min)** 950 950 950
- Max Continuous 915 915 915
- Starting * 725 725 725
A28NM Page 15 of 22
Max Oil Temperature
(Supply Pump Inlet; °C)
- Take-off, Stabilized 140 140 140
- Transient (15 min max) 155 155 155
Min. Press. (PSI) 13 13 13
Approved Oils See SB CFMI 79-001-OX See SB CFMI 79-001-OX See SB CFMI 79-001-OX
IAE V2530-A5 IAE V2533-A5
Engine Limitation Data Sheets E40NE (FAA) Data Sheets E40NE (FAA)
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