TextOCR
This text is OCR from a scan. OCR can misread letters and numbers.
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 = '6eefc76918fb89d45b327b69daaa22c7b7215470c175e905dc2ef5cd9ef4b38c' 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 = '6eefc76918fb89d45b327b69daaa22c7b7215470c175e905dc2ef5cd9ef4b38c' 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.
RA" REIMS AVIATION INDUSTRIES REIMB AVATION INOUSTRIES 51360 PRUNAY - FRANCE SERVICE BULLETIN N° F406-58 REV 1 REFERENCE MANUFACTURER: N° F406-58 REV 1 N° ATA: 27 Date: October 27, 2006 TITLE: RUDDER PULLEY BRACKET INSPECTION
EFFECTIVITY Model Serial Numbers F406 F406- 0002/0003/0004/0006/0008/0009/0010/0012/0013/0017/0024/0025/ 0039/0042/0044/0045/0066/0070/0073/0074/0075/0077/0080/0081/ 0082/0083/0084/0085/0086/0087/ 0088/0089/0090/0092
PURPOSE This Service Bulletin is intented to inform F406 owners of the discovery of cracks about the pulley bracket 6015511-1. This pulley bracket is installed with the camera hole option. Non compliance with this Service bulletin may allow undetected cracks to go in the pulley bracket which could result in rudder control failure.
Scope of revision 1: Integration of an extent of tolerance for the realization of the assembly of the pulley.
COMPLIANCE Mandatory A. Prior to the next flight, the initial inspection specified in paragraph 1 section ACCOMPLISHMENT INSTRUCTIONS must be accomplished.
B. If cracks are not found, repeat the inspection every 50 hours of operation or 1 month, whichever occurs first and until accumulating 100 hours of operation or 2 months since the initial Inspection, installation of the pulley bracket 4061-2701-1 specified in paragraph 2 section ACCOMPLISHMENT INSTRUCTIONS must be accomplished.
C. If cracks are found, prior to the next flight, the installation of the pulley bracket 4061-2701-1 specified in paragraph 2 section ACCOMPLISHMENT INSTRUCTIONS must be accomplished.
APPROVAL This REIMS AVIATION INDUSTRIES Service Bulletin is attached to a CNU EASA approval number:
CN F-2005-080.
Service Bulletin N° F406-58 REV 1 Page 1 October 27, 2006
RA REIMS AVIATION INDUSTRIES REIVIS AVATION INDUSTRES 51360 PRUNAY - FRANCE
MAN-HOURS Approximately 1.0 man-hour per airplane for inspection.
Add approximately 10 man-hours per airplane for modification.
MATERIAL The following are available from:
REIMS AVIATION INDUSTRIES Aérodrome de Reims Prunay 51360 Prunay Tel: 03.26.48.46.65 Fax: 03.26.49.18.5/
PART NUMBER DESCRIPTION QTY / AIRCRAFT NAS1738B5-2 RIVET 1 NAS1738B4-2 RIVET 3 4061-2701-1 PULLEY BRACKET 1 CREDIT Not applicable
ACCOMPLISHMENT INSTRUCTIONS
1. Perform Initial Inspection:
A. Remove panels 5212006-2, 5212006-18 and 5811002-32 in the fuselage. (Refer to section 53-20-04 page 201 of the Maintenance Manual) B. (Refer to Figure 1.) Inspect visually for cracks in the pulley bracket 6015511-1.
(1) If cracks are not found, repeat the inspection every 50 hours of operation or 1 month until accumulating 100 hours of operation or 2 Months or until the installation of the pulley bracket 4061-2701-1 as specified in paragraph 2.
(a) Complete the information on the attached pulley bracket information Form and send the form to Reims Aviation Industries. This form shall be completed and sent to Reims Aviation industries after each inspection until installation of the modification pulley bracket.
Service Bulletin N° F406-58 REV 1 Page 2 October 27, 2006
RA REIMS AVIATION INDUSTRIES REIMS AVATION INDUSTRIES 51360 PRUNAY - FRANCE
(2) If a crack is found, install the pulley bracket 4061-2701-1 as specified in paragraph 2.
(a) Complete the information on the attached pulley bracket information Form and send the form to Reims Aviation Industries.
2. Installation of 4061-2701-1 pulley bracket:
A. Remove rudder control cable 6017104-50 (Refer to section 27-20-01 page 201 of the Maintenance Manual) B. (Refer to Figure 1). Remove all fasteners installed in the 6015511-1 Pulley Bracket.
C. Remove from the pulley bracket 6015511-1: pulley S-378-4, screw MS27039-4-16, washer AN960-416L, nut MS21042L4 and pin NAS5427K10.
D. (Refer to Figure 2). Position pulley S-378-4, screw MS27039-4-16, washer AN960-416L, nut MS21042L4 and pin NAS5427K10.
E. Position pulley support 4061-2701-1 in place of 6015511-1 F. Using existing holes, backdrill the pulley support, deburr the holes and remove any debris from the area.
NOTA: The angular angle certified by RAI for the positioning of the pulley support is 39/43° (with theoretical angle 39°23").
If the existing holes do not allow to have the correct positioning of the cable in the throat of the pulley with the angular extent, please contact the customer service.
G. Re-Install rudder control cable 6017104-50 (Refer to section 27-20-01 page 202 of the Maintenance Manual).
NOTA: To validate the correct positioning of the pulley support the control cable must be in the throat of the pulley.
3. Make an entry in the airplane logbook.
OWNER NOTIFICATION The Service Bulletin F406-58 rev1 dated 27 October 2006 will be addressed to the owners of the F406 airplanes. It is recommended to the customers to contact REINS AVIATION INDUSTRIES for any further information relating to the application of the Service Bulletin F406-58 REV 1 on your airplane.
REIMS AVIATION INDUSTRIES Aérodrome de Reims Prunay 51360 Prunay A l'attention du Support Client Tel: 03.26.48.46.53 Fax: 03.26.49.18 57 Service Bulletin N° F406-58 REV 1 Page 3 October 27, 2006
RA" REIMS AVIATION INDUSTRIES REIMS AVATION INDURTRES 51360 PRUNAY - FRANCE 6017104-50 MS27039-4-16 S-378-4 AN960-416L NAS427K10 _MS21042L4 4061-2701-1 FIGURE1 - PULLEY BRACKET (Refer to section 27-20-03 of the IPC)
ANO AF RIVET 3 REOD/-1
8.L 59 AAD SF RIVET 12 1 REOD/- I -4061-2701-1 (TYP) 39° 23' FIGURE1 - PULLEY BRACKET ATTACH C BRKT (REF) Service Bulletin N° F406-58 REV 1 Page 4 October 27, 2006
REIMS AVIATION INDUSTRIES RA
SPECIAL INSPECTION FORM TITLE
PULLEY BRACKET INSPECTION FROM :
• Company Name of Technical Manager:
Address Telephone Fax AFFECTED AIRCRAFT F406 S/N Maintenance Inspection Phase _Date Total flight hours Total landings Pulley Bracket Condition 4061-2701-1 Installation (yes / no) Comments Send to: REIMS AVIATION INDUSTRIES Aérodrome de Reims-Prunay 51360 Prunay France Tel : (33)3.26.48.46.65 Fax: (33)3.26.49.18.57 Service Bulletin N° F406-58 REV 1 Page 5 October 27, 2006
RA" REIMS AVIATION INDUSTRIES REIMS AVIATION INDUSTRIES 51360 PRUNAY - FRANCE SERVICE BULLETIN N° F406-58 REV 1 REFERENCE MANUFACTURER: N° F406-58 REV 1 N° ATA: 27 Date: October 27, 2006 TITLE: RUDDER PULLEY BRACKET INSPECTION
EFFECTIVITY Model Serial Numbers F406 F406- 0002/0003/0004/0006/0008/0009/0010/0012/0013/0017/0024/0025/ 0039/0042/0044/0045/0066/0070/0073/0074/0075/0077/0080/0081/ 0082/0083/0084/0085/0086/0087/ 0088/0089/0090/0092
PURPOSE This Service Bulletin is intented to inform F406 owners of the discovery of cracks about the pulley bracket 6015511-1. This pulley bracket is installed with the camera hole option. Non compliance with this Service bulletin may allow undetected cracks to go in the pulley bracket which could result in rudder control failure.
Scope of revision 1: Integration of an extent of tolerance for the realization of the assembly of the pulley.
COMPLIANCE Mandatory A. Prior to the next flight, the initial inspection specified in paragraph 1 section ACCOMPLISHMENT INSTRUCTIONS must be accomplished.
B. If cracks are not found, repeat the inspection every 50 hours of operation or 1 month, whichever occurs first and until accumulating 100 hours of operation or 2 months since the initial Inspection, installation of the pulley bracket 4061-2701-1 specified in paragraph 2 section ACCOMPLISHMENT INSTRUCTIONS must be accomplished.
C. If cracks are found, prior to the next flight, the installation of the pulley bracket 4061-2701-1 specified in paragraph 2 section ACCOMPLISHMENT INSTRUCTIONS must be accomplished.
APPROVAL This REIMS AVIATION INDUSTRIES Service Bulletin is attached to a CNU EASA approval number:
CN F-2005-080.
Service Bulletin N° F406-58 REV 1 Page 1 October 27, 2006
RA" REIMS AVIATION INDUSTRIES REIMS AVIATION INDUSTRIES 51360 PRUNAY - FRANCE
MAN-HOURS Approximately 1.0 man-hour per airplane for inspection.
Add approximately 10 man-hours per airplane for modification.
MATERIAL The following are available from:
REIMS AVIATION INDUSTRIES Aérodrome de Reims Prunay 51360 Prunay Tel: 03.26.48.46.65 Fax: 03.26.49.18.57
PART NUMBER DESCRIPTION QTY / AIRCRAFT NAS1738B5-2 RIVET 1 NAS1738B4-2 RIVET 3 4061-2701-1 PULLEY BRACKET 1 CREDIT Not applicable
ACCOMPLISHMENT INSTRUCTIONS
1. Perform Initial Inspection:
A. Remove panels 5212006-2, 5212006-18 and 5811002-32 in the fuselage. (Refer to section 53-20-04 page 201 of the Maintenance Manual) B. (Refer to Figure 1.) Inspect visually for cracks in the pulley bracket 6015511-1.
(1) If cracks are not found, repeat the inspection every 50 hours of operation or 1 month until accumulating 100 hours of operation or 2 Months or until the installation of the pulley bracket 4061-2701-1 as specified in paragraph 2.
(a) Complete the information on the attached pulley bracket information Form and send the form to Reims Aviation Industries. This form shall be completed and sent to Reims Aviation industries after each inspection until installation of the modification pulley bracket.
Service Bulletin N° F406-58 REV 1 Page 2 October 27, 2006
RA REIMS AVIATION INDUSTRIES REIMS AVIATION INDUSTRES 51360 PRUNAY - FRANCE
(2) If a crack is found, install the pulley bracket 4061-2701-1 as specified in paragraph 2.
(a) Complete the information on the attached pulley bracket information Form and send the form to Reims Aviation Industries.
2. Installation of 4061-2701-1 pulley bracket:
A. Remove rudder control cable 6017104-50 (Refer to section 27-20-01 page 201 of the Maintenance Manual) B. (Refer to Figure 1). Remove all fasteners installed in the 6015511-1 Pulley Bracket.
C. Remove from the pulley bracket 6015511-1: pulley S-378-4, screw MS27039-4-16, washer AN960-416L, nut MS21042L4 and pin NAS5427K10.
D. (Refer to Figure 2). Position pulley S-378-4, screw MS27039-4-16, washer AN960-416L, nut MS21042L4 and pin NAS5427K10.
E. Position pulley support 4061-2701-1 in place of 6015511-1 F. Using existing holes, backdrill the pulley support, deburr the holes and remove any debris from the area.
NOTA: The angular angle certified by RAI for the positioning of the pulley support is 39/43° (with theoretical angle 39°23).
If the existing holes do not allow to have the correct positioning of the cable in the throat of the pulley with the angular extent, please contact the customer service.
G. Re-Install rudder control cable 6017104-50 (Refer to section 27-20-01 page 202 of the Maintenance Manual).
NOTA: To validate the correct positioning of the pulley support, the control cable must be in the throat of the pulley.
3. Make an entry in the airplane logbook.
OWNER NOTIFICATION The Service Bulletin F406-58 rev1 dated 27 October 2006 will be addressed to the owners of the F406 airplanes. It is recommended to the customers to contact REIMS AVIATION INDUSTRIES for any further information relating to the application of the Service Bulletin F406-58 REV 1 on your airplane.
REIMS AVIATION INDUSTRIES Aérodrome de Reims Prunay 51360 Prunay A l'attention du Support Client Tel: 03.26.48.46.53 Fax: 03.26.49.18 57 Service Bulletin N° F406-58 REV 1 Page 3 October 27, 2006
RA" REIMS AVIATION INDUSTRIES REIVE AVATION INDUSTRIES 51360 PRUNAY - FRANCE -6017104-50 MS27039-4-16 ,S-378-4 AN960-416L NAS427K10 _MS21042L4 4061-2701-1 FIGURE1 - PULLEY BRACKET (Refer to section 27-20-03 of the IPC) 5811130 BHD MAO 4F RIVET 12 3 REQD/-1 AMO 5F RIVET 12 1 REQD/- I +4061-2701-1 1·YP) 39° 23' 39 FIGURE1 - PULLEY BRACKET ATTACH Q_BRKT (REF) Service Bulletin N° F406-58 REV 1 Page 4 October 27, 2006
REIMS AVIATION INDUSTRIES RA
SPECIAL INSPECTION FORM TITLE
PULLEY BRACKET INSPECTION FROM :
Company Name of Technical Manager:
Address Telephone Fax AFFECTED AIRCRAFT F406 S/N Maintenance Inspection Phase Date Total flight hours Total landings Pulley Bracket Condition 4061-2701-1 Installation (yes / no) Comments Send to: REIMS AVIATION INDUSTRIES Aerodrome de Reims-Prunay 51360 Prunay France Tel: (33)3.26.48.46.65 Fax: (33)3.26.49.18.57 Service Bulletin N° F406-58 REV 1 Page 5 October 27, 2006