Steve Pierce said:
Sorry I posted the wrong link.
Still the wrong link... HBAW 97-01 was amended by 97-01B to allow field approvals again...
ORDER: 8300.10
APPENDIX: 3
BULLETIN NUMBER: HBAW 97-01B (Amended)
BULLETIN TITLE: Revised Approval Criteria For Tundra Tire
Installations
EFFECTIVE DATE: 04-22-97
REINSTATED DATE: 12-03-02
TRACKING NUMBER: NTSB Recommendation A-95-13
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1. PURPOSE. To inform all Flight Standards Field Office managers, supervisors, and aviation safety inspectors (ASI) (airworthiness) that HBAW 97-01 has been revised to incorporate the provisions of the FAA Reauthorization Act of 1996. ASIs will be authorized to issue field approvals for certain types of tundra tire installations.
2. ACTION. ASIs are authorized to perform field approvals, using applicable information in advisory circular (AC) 23-17, Systems and Equipment Guide for Certification of Part 23 Airplanes, as revised, FAA Order 8300.10, volume 2, chapter 1, Perform Field Approval of Major Repairs and Major Alterations, and the following guidance.
A. Each ASI must be trained and authorized before performing tundra tire field approvals. Each authorized ASI must have satisfactorily completed the Aircraft Alterations and Repair course #21811. A signed statement of authorization from the ASI's district office manager will be placed in the ASI's file. The authorization will state that the ASI is authorized to perform field approvals for tundra tire installations. The statement will also include the ASI's background, and training (formal and OJT) with tundra tire field approvals.
B. All tires used for field approved tundra tire installations must be either Technical Standard Order (TSO) or Parts Manufacturer Approval (PMA) approved and limited to size 35x15 tires and smaller.
C. A copy of AC 23-17, as revised, will be given to the owner/operator of the aircraft prior to issuing a field approval for tundra tires.
D. The aircraft will be weighed and a worst case forward and aft C/G for both the aircraft's new empty weight and gross weight must be determined before a field approval is issued.
E. The owner/operator will ensure that the aircraft wing/tail/and control surfaces have not been improperly altered and the aircraft is properly rigged.
F. A series of maintenance operational check flights must be completed with the aircraft and conducted in accordance with the aircraft's flight manual or limitations (ref: Title 14 of the Code of Federal Regulations part 91, section 91.407). One flight(s) will be conducted at minimum weight at the most forward and at the most aft C/G. The second flight(s) must be at gross weight at the most forward and at the most aft C/G. No passengers will be permitted on the maintenance operational check flights.
G. After the flights are completed, the pilot will sign the aircraft's airframe maintenance (log) book, certifying that the aircraft is safe to operate within the operational limits of the aircraft's design.
3. INQUIRIES. This bulletin was developed by AFS-340. Any questions concerning this bulletin should be directed to AFS-340 at (202) 267-3796.
4. LOCATION. The material in this bulletin will be incorporated in FAA Order 8300.10, volume 2, chapter 1, Perform Field Approval of Major Repairs and Major Alterations. Until the new material is incorporated, inspectors should make written reference in the margin of the affected chapter.
/s/ David E. Cann
Manager, Aircraft Maintenance Division