Text
From the PDF’s text layer: layout, tables and figures are lost. The PDF is the document.
Query with SQL
duckdb -csv -c "SELECT p.page, p.text_source, p.text, f.rights_holder, f.license FROM 'https://openairdocs.org/data/latest/service_document_file_page.parquet' p JOIN 'https://openairdocs.org/data/latest/service_document_file.parquet' f USING (file_sha256) WHERE p.file_sha256 = 'b93b0d1ca0f08177795b4740eac7a74f76d2b2e2ebf193458172221e79faf508' ORDER BY p.page"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT p.page, p.text_source, p.text, f.rights_holder, f.license FROM 'https://openairdocs.org/data/latest/service_document_file_page.parquet' p JOIN 'https://openairdocs.org/data/latest/service_document_file.parquet' f USING (file_sha256) WHERE p.file_sha256 = 'b93b0d1ca0f08177795b4740eac7a74f76d2b2e2ebf193458172221e79faf508' ORDER BY p.page
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
KODIAK® 100 SB14‐07 Page 1 of 1 ®
SUBJECT: Elevator Control System – Cushion Edging Inspection REVISION: 01 DATE: 11/23/2015 EFFECTIVITY: KODIAK 100 Series Aircraft Serial Numbers 100-0001 through 100-0149
SUMMARY The accompanying Field Service Instruction (FSI) provides instruction for inspecting cushion edging installed on the elevator control anti-rotation guide. One operator reported one piece of edging became lodged in the guide slot and prevented the elevator from moving through its full range of travel during a preflight check.
COMPLIANCE The initial inspection in Section 5.1 of the FSI accompanying this Mandatory Service Bulletin must be complied with prior to further flight. Note: The FSI includes both an initial inspection as well as a recurring inspection.
The recurring inspection shall be continued until compliance with SB15-01, Yoke Anti-rotation Guide Wear Pad Upgrade, is completed.
Document Number Document Title FSI-105 Elevator Control System – Cushion Edging Inspection
FAA APPROVAL STATUS The instructions attached to this Service Bulletin have demonstrated compliance with all applicable Federal Aviation Regulations and are approved by the Federal Aviation Administration.
CREDIT AND WARRANTY INFORMATION Quest will reimburse up to .5 of an hour of labor costs associated with the inspection portion of this bulletin.
Parts and labor related to the recurring inspections referenced in the FSI will not be covered. Refer to Quest’s warranty information regarding submitting invoices for reimbursement.
If damage is found, refer to the SPECIAL INSTRUCTIONS section of this bulletin.
Quest Customer Service Phone: (208) 263-1111 Toll Free: 1 (866) 263-1112 Email: customerservice@questaircraft.com
SPECIAL INSTRUCTIONS If damage requiring replacement of stripping is found, Quest will supply qty. (40 inches) P/N M22529/2-3R-25 CUSHION EDGING per aircraft, at no cost to owner, and reimburse up to 1 hour of labor costs associated with the replacement portion of this bulletin. Contact Quest Customer Service to place order, and refer to Quest’s web site for information on submitting invoices for reimbursement.
MANDATORY SERVICE BULLETIN Quest Aircraft Company LLC, 1200 Turbine Drive, Sandpoint, ID 83864 __________________________________________________ CONFIDENTIALITY NOTICE: The information contained in this docum ent and any attachments are the property of Quest Aircraft Desi gn LLC, and/or Quest Aircraft Company LLC, and may be used only by the intended recipient. In the event that this document has been transmitted or forwarded to you in error, please notify the sender immediately by calling 208 -263-1111. No person other than the intended recipient is authorized to read, print, retain, copy, and/or disseminate this document or any part of it. After notifying the sender of receipt, please destroy the document and any attachments. This document may contain information that is proprietary, privileged, confidential, and/or otherwise legally exempt from disclosure. Any erroneous transmission and/or receipt of this document shall not constitute waiver of any applicable protectio ns against unauthorized use or disclosure of the information. QUEST ® , KODIAK ® , and logos are trademarks or registered trademarks of Quest Aircraft Design LLC, and licensed to Quest Aircraft Company LLC. English is the authoritative text of Quest Aircraft Design LLC, and Quest Aircraft Design LLC technical publications. If a technical publication is translated, then the English version will control.
Uncontrolled if printed