What it approves
Installation of a Flight Data System KIT 130ND-3130100
What the certificate says
From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.
Number SR00338BO
FAA Form 8110-2 (8/13) Page 1 of 3 This certificate issued to:
North Flight Data Systems, LLC 1214 Hawn Avenue Shreveport, LA 71107 Part 27 of the Federal Aviation Regulations.
Original Product - Type Certificate Number: H9EU Make: Airbus Helicopter Model: EC130B4 and AS350B3
Installation of a Flight Data System KIT 130ND-3130100 in accordance with Master Drawing List MDL130N3130001, Revision B, dated January 9, 2014, or later FAA-approved revision.
1. The appropriate Rotorcraft Flight Manual Supplement must be carried on the helicopter during all flights as follows:
a. For EC130B4, North Flight Data Systems Document 130NF3130001, Revision A, dated February 10, 2014, or later FAA-approved revision, or;
b. For AS350B3, North Flight Data Systems Document 130NF3130003, Revision IR, dated February 10, 2014, or later FAA-approved revision.
(continued on Page 3 of 3)
Date of Application: March 7, 2013 Date reissued:
Date of Issuance: February 10, 2014 Date amended:
Signature Robert G. Mann
Manager, Boston Aircraft Certification Office Title
SUPPLEMENTAL TYPE CERTIFICATE, FAA FORM 8110-2 (CONTINUED)
FAA Form 8110-2 (8/13) Page 2 of 3
TRANSFER
ENDORSEMENT
To (Name of transferee)
(Address of transferee)
(Number and street)
(City, State, and ZIP Code)
From (Name of grantor)
(Address of grantor)
(Number and street)
(City, State, and ZIP Code)
Number SR00338BO February 10, 2014
FAA Form 8110-2 (8/13) Page 3 of 3
Limitations and Conditions: (continued from Page 1 of 3)
2. Maintenance must be in accordance with the instructions for continued airworthiness contained in North Flight Data Systems Document 130ND31301, Revision B, dated October 23, 2013, or later FAA-approved revision must be made available to the operator at the time of installation.
3. The ICA must be made available to the operator at the time of installation.
4. Compatibility of this design with previously approved modifications must be determined by the installer.
Certification Basis:
Based on 14 CFR § 21.115 and § 21.101, and the FAA policy for design changes that are identified as not significant in FAA Order 8110.48, the certification basis for the Airbus Helicopters aircraft with the installation of the Flight Data System KIT 130ND-3130100 is as defined in TCDS H9EU.
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