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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 = '8a64985f69d24319e1020557e41eb010dac47ec58cd5c7494ddaef23b1cfefe7' 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 = '8a64985f69d24319e1020557e41eb010dac47ec58cd5c7494ddaef23b1cfefe7' 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.
FIGURE 6: NACELLE NUMBER 1 - FRONT SPAR FITTING AFT LUGS - SURFACE HIGH FREQUENCY
EDDY CURRENT INSPECTION (SHEET 1 OF 3) Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: July 29, 2004 A3514Revision 1 November 09, 2016 37 of 48 BOEING SERVICE BULLETIN A3514
ALERTALERT
The step numbers shown below agree with the numbers shown in the circle symbols in the figure.
More DataQtyIdentificationNameTaskStep
(a)1-Front Spar FittingInspect1
(b) (c)2-Front Spar Fitting Aft Lug Inspect2
(a) Do a magnetic inspection of the front spar fitting to find if the material is aluminum or steel. Use a magnet to find if there is a magnetic force that pulls the magnet to the front spar fitting. If there is a magnetic force, the front spar fitting is made from steel. If there is no magnetic force, the front spar fitting is made from aluminum.
(b) For aluminum front spar fitting, do a surface HFEC inspection around the lug hole on the two sides of each aft lug of the front spar fitting for any crack in accordance with 707, 720 NDT Manual Part 6, 51-00- 00, Figure 4 or Figure 23.
FIGURE 6: NACELLE NUMBER 1 - FRONT SPAR FITTING AFT LUGS - SURFACE HIGH FREQUENCY
EDDY CURRENT INSPECTION (SHEET 2 OF 3) Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: July 29, 2004 A3514Revision 1 November 09, 2016 38 of 48 BOEING SERVICE BULLETIN A3514
ALERTALERT
More DataQtyIdentificationNameTaskStep
(c) For steel front spar fitting, do a surface HFEC inspection around the lug hole on the two sides of each aft lug of the front spar fitting for any crack in accordance with 707, 720 NDT Manual Part 6, 51-00-00, Figure 13 or Figure 24.
FIGURE 6: NACELLE NUMBER 1 - FRONT SPAR FITTING AFT LUGS - SURFACE HIGH FREQUENCY
EDDY CURRENT INSPECTION (SHEET 3 OF 3) Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: July 29, 2004 A3514Revision 1 November 09, 2016 39 of 48 BOEING SERVICE BULLETIN A3514
ALERTALERT
FIGURE 7: NACELLE NUMBER 2 - FRONT SPAR FITTING AFT LUG - SURFACE HIGH FREQUENCY EDDY
CURRENT INSPECTION (SHEET 1 OF 3) Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: July 29, 2004 A3514Revision 1 November 09, 2016 40 of 48 BOEING SERVICE BULLETIN A3514
ALERTALERT
The step numbers shown below agree with the numbers shown in the circle symbols in the figure.
More DataQtyIdentificationNameTaskStep
(a)1-Front Spar FittingInspect1
(b) (c)1-Front Spar Fitting Aft Lug Inspect2
(a) Do a magnetic inspection of the front spar fitting to find if the material is aluminum or steel. Use a magnet to find if there is a magnetic force that pulls the magnet to the front spar fitting. If there is a magnetic force, the front spar fitting is made from steel. If there is no magnetic force, the front spar fitting is made from aluminum.
(b) For aluminum front spar fitting, do a surface HFEC inspection around the lug hole on the two sides of the aft lug of the front spar fitting for any crack in accordance with 707, 720 NDT Manual Part 6, 51-00-00, Figure 4 or Figure 23.
FIGURE 7: NACELLE NUMBER 2 - FRONT SPAR FITTING AFT LUG - SURFACE HIGH FREQUENCY EDDY
CURRENT INSPECTION (SHEET 2 OF 3) Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: July 29, 2004 A3514Revision 1 November 09, 2016 41 of 48 BOEING SERVICE BULLETIN A3514
ALERTALERT
More DataQtyIdentificationNameTaskStep
(c) For steel front spar fitting, do a surface HFEC inspection around the lug hole on the two sides of the aft lug of the front spar fitting for any crack in accordance with 707, 720 NDT Manual Part 6, 51-00-00, Figure 13 or Figure 24.
FIGURE 7: NACELLE NUMBER 2 - FRONT SPAR FITTING AFT LUG - SURFACE HIGH FREQUENCY EDDY
CURRENT INSPECTION (SHEET 3 OF 3) Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: July 29, 2004 A3514Revision 1 November 09, 2016 42 of 48 BOEING SERVICE BULLETIN A3514
ALERTALERT
FIGURE 8: NACELLE NUMBER 3 - FRONT SPAR FITTING AFT LUG - SURFACE HIGH FREQUENCY EDDY
CURRENT INSPECTION (SHEET 1 OF 3) Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: July 29, 2004 A3514Revision 1 November 09, 2016 43 of 48 BOEING SERVICE BULLETIN A3514
ALERTALERT
The step numbers shown below agree with the numbers shown in the circle symbols in the figure.
More DataQtyIdentificationNameTaskStep
(a)1-Front Spar FittingInspect1
(b) (c)1-Front Spar Fitting Aft Lug Inspect2
(a) Do a magnetic inspection of the front spar fitting to find if the material is aluminum or steel. Use a magnet to find if there is a magnetic force that pulls the magnet to the front spar fitting. If there is a magnetic force, the front spar fitting is made from steel. If there is no magnetic force, the front spar fitting is made from aluminum.
(b) For aluminum front spar fitting, do a surface HFEC inspection around the lug hole on the two sides of the aft lug of the front spar fitting for any crack in accordance with 707, 720 NDT Manual Part 6, 51-00-00, Figure 4 or Figure 23.
FIGURE 8: NACELLE NUMBER 3 - FRONT SPAR FITTING AFT LUG - SURFACE HIGH FREQUENCY EDDY
CURRENT INSPECTION (SHEET 2 OF 3) Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: July 29, 2004 A3514Revision 1 November 09, 2016 44 of 48 BOEING SERVICE BULLETIN A3514
ALERTALERT
More DataQtyIdentificationNameTaskStep
(c) For steel front spar fitting, do a surface HFEC inspection around the lug hole on the two sides of the aft lug of the front spar fitting for any crack in accordance with 707, 720 NDT Manual Part 6, 51-00-00, Figure 13 or Figure 24.
FIGURE 8: NACELLE NUMBER 3 - FRONT SPAR FITTING AFT LUG - SURFACE HIGH FREQUENCY EDDY
CURRENT INSPECTION (SHEET 3 OF 3) Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: July 29, 2004 A3514Revision 1 November 09, 2016 45 of 48 BOEING SERVICE BULLETIN A3514
ALERTALERT
FIGURE 9: NACELLE NUMBER 4 - FRONT SPAR FITTING AFT LUGS - SURFACE HIGH FREQUENCY
EDDY CURRENT INSPECTION (SHEET 1 OF 3) Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: July 29, 2004 A3514Revision 1 November 09, 2016 46 of 48 BOEING SERVICE BULLETIN A3514
ALERTALERT
The step numbers shown below agree with the numbers shown in the circle symbols in the figure.
More DataQtyIdentificationNameTaskStep
(a)1-Front Spar FittingInspect1
(b) (c)2-Front Spar Fitting Aft Lug Inspect2
(a) Do a magnetic inspection of the front spar fitting to find if the material is aluminum or steel. Use a magnet to find if there is a magnetic force that pulls the magnet to the front spar fitting. If there is a magnetic force, the front spar fitting is made from steel. If there is no magnetic force, the front spar fitting is made from aluminum.
(b) For aluminum front spar fitting, do a surface HFEC inspection around the lug hole on the two sides of each aft lug of the front spar fitting for any crack in accordance with 707, 720 NDT Manual Part 6, 51-00- 00, Figure 4 or Figure 23.
FIGURE 9: NACELLE NUMBER 4 - FRONT SPAR FITTING AFT LUGS - SURFACE HIGH FREQUENCY
EDDY CURRENT INSPECTION (SHEET 2 OF 3) Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: July 29, 2004 A3514Revision 1 November 09, 2016 47 of 48 BOEING SERVICE BULLETIN A3514
ALERTALERT
More DataQtyIdentificationNameTaskStep
(c) For steel front spar fitting, do a surface HFEC inspection around the lug hole on the two sides of each aft lug of the front spar fitting for any crack in accordance with 707, 720 NDT Manual Part 6, 51-00-00, Figure 13 or Figure 24.
FIGURE 9: NACELLE NUMBER 4 - FRONT SPAR FITTING AFT LUGS - SURFACE HIGH FREQUENCY
EDDY CURRENT INSPECTION (SHEET 3 OF 3) Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: July 29, 2004 A3514Revision 1 November 09, 2016 48 of 48 BOEING SERVICE BULLETIN A3514