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defined in FAR Part 25.959. This "unusable" fuel is included in System Fuel as indicated in paragraph d. above, and need not be
accounted for separately.
f. System oil is the weight of all remaining in the engine, constant speed drive, lines, and tanks after subtracting the oil in the
tanks which is above the standpipe (zero gauge) levels. The engine oil capacities shown elsewhere in this data sheet include only
the usable oil for which the tanks must be placarded.
Note 2:
The aircraft must be operated in accordance with the DGAC-approved FAA Airplane Flight Manual. ("DGAC-approved" is
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.
A28NM Page 7 of 22
Note 4:
The A319 basic definition for U.S. import certification is contained in the following documents:
-AI/EA-S 413.0969/96 for A319-111 model
-AI/EA-S 413.1012/96 for A319-112 model
-AI/EA-S 413.3100/96 (Mod 25699 supplement) for A319-112 model
-AI/EA-S 413.2504/96 for A319-113 model
-AI/EA-S 413.2505/96 for A319-114 model
-AI/EA-S 413.0393/97 for A319-131 model
-AI/EA-S 413.0396/97 for A319-132 model
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”. This document is not applicable to the A319 for Corporate Jet
use, but rather Airbus document AI/SE-M2/95A-1038/99 “Airworthiness Limitation Items”.
Note 6:
If modification 25469 or 26968 is embodied on models with CFM engines, the airplane is qualified for CAT III B precision
approach. This does not constitute operational approval.
Note 7:
Modification 25303 (for CFM engine) or 25302 (for IAE engine) are part of the FAA Type Design and shall be implemented on
any A319 aircraft entered on the U.S. register, 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.
Note 9:
If Modification 26716 or 26717 is embodied on models with IAE engines, the airplane is qualified for CAT III B precision
approach. This does not constitute operational approval.
Note 10:
The type design definitions and certification standard equipment lists as referenced in Note 4 are complemented by document
00D000A0546/C0S “A319-100/A321-200 FMGC Type Standard Evolution” and document 00J000A0067/C0S “A319-111/112
ATC Transponder Type Standard Evolution”.
Note 11:
A319 for Corporate Jet use are defined through the following set of modifications:
- Modification 28238 (0 to 6 ACTs)
- Modification 28162 (extension of flight envelope up to 41,000 ft)
- Modification 28342 (modification of CG limits)
Note 12:
On A319 for Corporate Jet use, the certification of installing up to six Additional Center Tanks (ACT) in bulk version is defined
by modification 28238. The approval together with structural and system provisions was subject of compliance demonstrated to
Advisory Circular AC 25-8.
Note 13:
On A319 for Corporate Jet use, exemptions to the following paragraphs of the FAR have been granted when the airplane is not
operated for hire or for public transport
(Granted APR 9, 2001, Exemption No. 7489):
25.785(h)(2) Flight Attendant seat locations which do not provide for direct view of the cabin
25.807(d)(7) Distance between exits
25.813(e) Installation of Interior Doors in between passenger compartments
A28NM Page 8 of 22
Note 14:
If modification 26610 is embodied on A319-112 airplanes, the engine performance and gaseous emission levels are improved.
The engine denomination changes to /2P (DAC IIC Dual Annual Combustor).
CFM56-5B6/P engine can be intermixed with CFM56-5B6/2P (DAC IIC Dual Annual Combustor) engine on the same aircraft
(AFM Supplement).
II. Type A320-100/200 Series Transport Category Airplanes
Model A320-111, Approved December 15, 1988
Model A320-211, Approved December 15, 1988;
Model A320-231, Approved July 6, 1989;
Model A320-212, Approved November 26, 1990;
Model A320-232, Approved November 12, 1993;
Model A320-233, Approved November 17, 1995;
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