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applicable to it. Refer to Type Certification Standard Equipment Schedule Lists:
- 00E000A0007/C1S for A321-111 Model
- 00E000A0006/C1S for A321-112 Model
- 00E000A0004/COS for A321-131 Model
- 00E000A0211/COS for A321-211 Model
- 00E000A0231/COS for A321-231 Model
Refer to Note 4 for list of A321 airplane model FAA Type Definitions.
Serial Numbers Eligible:
A321 Aircraft, all series, all models, are produced in Hamburg (Germany) under approval LBA.G.0009 or I-A9 issued by LBA to
Airbus.
A German Export Certificate of Airworthiness endorsed as noted under “Import Requirement”, must be submitted for each
individual aircraft for which application for U.S. certification is made.
A28NM Page 18 of 22
Import Requirements:
A FAA Standard Airworthiness Certificate may be issued on the basis of a German Export Certificate of Airworthiness, signed
by a representative of the Luftfahrt-Bundesamt (LBA) of Germany, containing the following statement: “The airplane covered by
this certificate has been examined, tested, and found to conform to the type design approved under Type Certificate No. A28NM
and to be in condition for safe operation.”
The U.S. airworthiness certification basis for aircraft type certificated under FAR Section 21.29 and exported by the country of
manufacture is FAR Sections 21.183(c) or 21.185(c). The U.S. airworthiness certification basis for aircraft type certificated
under FAR Section 21.29 exported from countries other than the country manufacture (e.g., third party country) is FAR Sections
21.183(d) or 21.185(b). Notwithstanding that FAR section 21.183(d) and 25.185(b) do not specifically address or require
certification by the foreign civil airworthiness authority of the country of manufacture, such certification is the only practical
way for an applicant to show, and the Federal Aviation Administration (FAA) to find conformity to the FAA-approved type
design and condition for safe operation. Additional guidance is contained in FAA advisory Circular 21-23, Airworthiness
Certification of Civil Aircraft, Engines, Propellers, and Related Products Imported into the United States.
Certification Basis (A321-100 and A321-200)
a. Part 25 of the FAR effective February 1, 1965, including amendments 25-1 through 25-56 thereto.
b.1. Plus the following sections of Part 25 as amended by amendments 25-1 through:
- 25-58 (Section 25.812(e))
- 25-63 (Section 25.25(a)(3))
- 25-67 (Section 25.807(c)(7))
- 25-70 (Section 25.1411(a)(2))
(Applied per FAA derivative aircraft policy – reference FAA order 8110.4A)
b.2. Airbus elected to comply with portions of FAR 25.562, Amendment 64, for the passenger seats only. FAR
paragraphs 25.562(c)(5) and 25.562(c)(6) do not apply.
c. Part 34 of the FAR effective September 10, 1960, including amendments 34-1.
d. Part 36 of the FAR effective December 1, 1965, including amendments 36-1 through 36-20 thereto.
e. FAA Special Conditions issued for the A320 in accordance with Section 21.16 of the FAR and published in the
Federal Register as follows:
1) January 27, 1989:
- Electronic Flight Controls
- Active Controls
- Engine Controls and Monitoring
- Protection from Lightning and Unwanted Effects of Radio Frequency (RF) Energy
- Flight Characteristics
- Flight Envelope Protection
- Side Stick Controllers
- Flight Recorder.
(2) June 9, 1989
- Computerized Airplane Flight Manual
f. For precision approach and landing, the applicable technical requirements are complemented by AC 120-29 and AC
120-28c.
For the automatic flight control system, the applicable technical requirements are complemented by AC 20-57A for
automatic landing and by AC 25.1329-1A for cruise.
Use of JAR AWO where applicable to the requirements above, is acceptable.
g. The following sections of the FAR have been complied with through equivalent safety demonstrations in addition to
the equivalent safety findings applicable from the original A320 certification basis:
- 25.101, 25.105, 25.109, 25.113, 25.115, 25.735, for rejected take-off and landing performance
- 25.305, 25.331, 25.333, 25.335, 25.341, 25.345, 25.349, 25.351, 25.371, 25.373, 25.391, 25.427, for design gust
criteria
-25.783(e) bulk cargo door
- 25.783(f) for passenger doors
- 25.807(c) for maximum passenger capacity
- 25.933(a) for thrust reversing system.
h. Optional requirements elected:
- 25.801 for ditching.
- 25.1419 for icing.
A28NM Page 19 of 22
Note 1 - Weight and Balance
a. Current weight and balance report including list of equipment, entitled "Aircraft Inspection Report" included in certificated
empty weight, and loading instructions, must be in each aircraft at the time of original certification and at all times thereafter,
　
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