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Revision T ransmittal May 29 , 2019 T O:
Cessna Distributors and Single Engine Authorized Service Facilities and CPC's
SUBJECT :
Single Engine Service Bulletin SEB93 - 5 Revision 2 , Lower Forward Doorpost and Strut Fitting Inspection and Modification.
REASON FOR
REVISION T o add additional serial numbers for the Model
206.
REQUIRED ACTION
• Please replace any copy of SEB93 - 5 with the attached copy of SEB93 - 5 Revision 2 in its entirety .
• Model 210 - 5
(205) , 206 , P206 / TP206 , U206 / TU206 airplanes that have been modified by the installation of SK206 - 42 , SK206 - 42A , SK206 - 42B or SK206 - 42C , compliance with SEB93 - 5 Revision 2 is not required.
• Model 207 / T207 airplanes that have been modified by the installation of SK207 - 19 (or latest revision) , compliance with SEB93 - 5 Revision 2 is not required.
• Model 207 / T207 airplanes that have been modified by the installation of SK206 - 42 , SK206 - 42A , SK206 - 42B or SK206 - 42C must comply with SEB93 - 5 Revision 2 and the applicable steps outlined in the Accomplishment Instructions of SK207 - 19A or later revision.
LOG OF
EFFECTIVE P AGES Page No.
Date Page No.
Date 1 May 29 , 2019 4 May 29 , 2019 2 May 29 , 2019 5 May 29 , 2019 3 May 29 , 2019 6 May 29 , 2019 * * * * * * * Page 1 of 1 T o obtain satisfactory results , procedures specified in this publication must be accomplished in accordance with accepted methods and prevailing government regulations.
Cessna Aircraft Company cannot be responsible for the quality of work performed in accomplishing the requirements of this publication.
Cessna Aircraft Company , Customer Service , P .O.
Box 7706 , Wichita , Kansas 67277 , U.S.A.
(316) 517 - 5800 , Facsimile
(316) 517 - 7271 www .cessnasupport.com
COPYRIGHT © 2019
No text on this page: it may be a figure. Open the PDF to see it.
S i n g l e E n g i n e Service Bulletin May 29 , 2019 SEB93 - 5 Revision 2 TITLE LOWER FOR W ARD
DOORPOST AND STRUT
FITTING
INSPECTION AND
MODIFICA TION
EFFECTIVITY Model Serial Numbers 210–5
(205) 205 - 0551 , 205 - 0556 thru 205 - 0577 206 206 - 0001 thru 206 - 0275 P206 / TP206 P206 - 0001 thru P206 - 0603 , P20600604 thru P2060647 U206 / TU206 676 , U206 - 0276 thru U206 - 1444 , U20601445 thru U20607020 207 / T207 20700001 thru 20700788
PURPOSE Service Experience indicates the possibility of cracks developing in the lower area of the forward cabin doorpost.
An inspection for cracks in this area must be conducted.
If a crack is found , the doorpost shall be modified by installing a service kit.
Non - compliance with this Service Bulletin may result in failure of a lower cabin doorpost and may compromise the structural integrity of the airplane.
COMPLIANCE MANDA T OR Y .
This service document must be accomplished as follows:
A.
Initial Inspection:
1.
Airplanes with 4 , 000 hours or more total time in service shall be inspected within the next 200 hours of operation or 12 months , whichever occurs first.
2.
Airplanes with less than 4 , 000 hours total time in service shall be inspected upon reaching 4 , 000 hours total time in service or within the next 200 hours of operation , whichever occurs later .
Original Issue:
March 26 , 1993 Revision 1:
September 8 , 1995 Revision 2:
May 29 , 2019 Page 1 of 6 T o obtain satisfactory results , procedures specified in this publication must be accomplished in accordance with accepted methods and prevailing government regulations.
Cessna Aircraft Company cannot be responsible for the quality of work performed in accomplishing the requirements of this publication.
Cessna Aircraft Company , Customer Service , P .O.
Box 7706 , Wichita , Kansas 67277 , U.S.A.
(316) 517 - 5800 , Facsimile
(316) 517 - 7271 www .cessnasupport.com
COPYRIGHT © 1993
NOTE:
For model 210 - 5
(205) , 206 , P206 / TP206 , U206 / TU206 airplanes that have been modified by the installation of SK206 - 42 , SK206 - 42A , SK206 - 42B or SK206 - 42C , compliance with SEB93 - 5 Revision 2 is not required.
NOTE:
For model 207 / T207 airplanes that have been modified by the installation of SK207 - 19 or later revision , compliance with SEB93 - 5 Revision 2 is not required.
NOTE:
Model 207 / T207 airplanes that have been modified by the installation of SK206 - 42 , SK206 - 42A , SK206 - 42B or SK206 - 42C must comply with SEB93 - 5 Revision 2 and the applicable steps outlined in the Accomplishment Instructions of SK207 - 19A or later revision.
B.
Repetitive Inspections:
1.
For model 210 - 5
(205) , 206 , P206 / TP206 , U206 / TU206 airplanes , accomplish every 1 , 000 hours of operation after the initial inspection until installation of SK206 - 42 (or latest revision).
2.
For 207 / T207 model airplanes (including aircraft that have been modified by the installation of SK206 - 42 , SK206 - 42A , SK206 - 42B , or SK206 - 42C) , accomplish every 1 , 000 hours of operation after the initial inspection until installation of SK207 - 19 or applicable steps outlined in the Accomplishment Instructions of SK207 - 19A or later revision.
APPROV AL F AA approval has been obtained on technical data in this publication that af fects airplane type design.
LABOR - HOURS Approximately
1.5 labor - hours to inspect doorposts.
Approximately
36.0 labor - hours per airplane to install SK206 - 42 or SK207 -
19.
MA TERIAL Please contact a T extron A viation Authorized Service Facility for current cost and availability of parts listed in this service document.
Part Number Description Qty / Airplane SK206 - 42D Lower Forward Doorpost Bulkhead And Wing Strut Fitting Reinforcement Kit 1 SK207 - 19A Lower Forward Doorpost Bulkhead And Wing Strut Fitting Reinforcement Kit 1 U000701 (See Note
1) T ype I , Class B Adhesive (EA9309.3NA 25 Grams) 1 Note 1:
Required for the installation of SK206 - 42D and SK207 - 19A , or later revision.
SEB93 - 5 Revision 2 Page 2 May 29 , 2019
ACCOMPLISHMENT
INSTRUCTIONS Lower Forward Doorpost Bulkhead And Wing Strut Fitting Inspection Accomplishment Instructions , and Service Kits SK206 - 42D and SK207 - 19A;
Lower Forward Doorpost Bulkhead And Wing Strut Fitting Reinforcement instructions are attached.
DESCRIPTION The following procedures provide instructions to inspect the lower area of the forward cabin doorpost for cracks.
APPROV AL F AA approval has been obtained on technical data in this publication that af fects airplane type design.
REFERENCE SK206 - 42D - Lower Forward Doorpost Bulkhead And Wing Strut Fitting Reinforcement (Revision D or later revision) SK207 - 19A - Lower Forward Doorpost Bulkhead And Wing Strut Fitting Reinforcement (Revision A or later revision) Change In W eight And Balance Model .
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210 - 5
(205) , 206 , P206 / TP206 , U206 / TU206 , 207 / T207 W eight Change .
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No Change
ACCOMPLISHMENT
INSTRUCTIONS
1.
Doorpost Bulkhead Inspection:
A.
Pull back the upholstery covering the left and right floorboards at the intersection of the forward doorpost and floor .
Remove and retain the upholstery and heater ducts on both sides at the bottom of the forward left and right doorpost.
The critical inspection area must be fully exposed.
B.
(Refer to Figure 1 , Sheet 2 , Details B and C.)
V isually inspect areas shown for cracks.
If there are cracks present , they should be visible at the intersection of the doorpost and the forward doorpost bulkhead.
Look for cracks that follow the contour of the wing strut support fitting.
C.
If cracks are present:
(1) For 210 - 5
(205) , 206 , P206 / TP206 , U206 / TU206 model airplanes , install SK206 - 42D (or later revision) prior to further flight.
(2) For 207 / T207 model airplanes , install SK207 - 19A (or later revision) prior to further flight.
D.
If cracks are not present , repetitive inspections of the critical area shall be accomplished per the compliance section of SEB93 - 5 , or later revision.
2.
Make an entry in the airplane logbook that states compliance and method of compliance with this Service Bulletin and if applicable , when the next inspection is due.
SEB93 - 5 Revision 2 May 29 , 2019 Page 3
B21699 U206/TU206 SHOWN (207/T207 TYPICAL)
FORWARD DOORPOST
AND BULKHEAD ASSEMBLY (REFERENCE)
WING STRUT CUFF (REFERENCE)
WING STRUT (REFERENCE) B
DETAIL A SEB93-5R1 Figure 1. Lower Doorpost Bulkhead and Wing Strut Fitting Inspection (Sheet 1) SEB93-5 Revision 2 Page 4 May 29, 2019
B21728
VISUALLY INSPECT FOR
POSSIBLE CRACKS AT
THESE LOCATIONS
CRITICAL INSPECTION AREA
LOOK FOR CRACKS FOLLOWING
THE CONTOUR OF THE WING
DETAIL B C STRUT SUPPORT FITTING
WING STRUT
SUPPORT FITTING (REFERENCE)
DETAIL C (LEFT SHOWN,
RIGHT TYPICAL) SEB93-5R1 Figure 1. Lower Doorpost Bulkhead and Wing Strut Fitting Inspection (Sheet 2) SEB93-5 Revision 2 May 29, 2019 Page 5
No text on this page: it may be a figure. Open the PDF to see it.
CREDIT Not applicable OWNER
NOTIFICA TION Dear Cessna Owner:
Service Experience indicates the possibility of cracks developing in the lower area of the forward cabin doorpost.
An inspection for cracks in this area must be conducted.
If a crack is found , the doorpost shall be modified by installing a service kit.
Non - compliance with this Service Bulletin may result in failure of a lower cabin doorpost and may compromise the structural integrity of the airplane.
Please contact a T extron A viation Authorized Service Facility for detailed information regarding the accomplishment of this service bulletin on your airplane.
Compliance is MANDA T OR Y .
This service document must be accomplished as follows:
A.
Initial Inspection:
1.
Airplanes with 4 , 000 hours or more total time in service shall be inspected within the next 200 hours of operation or 12 months , whichever occurs first.
2.
Airplanes with less than 4 , 000 hours total time in service shall be inspected upon reaching 4 , 000 hours total time in service or within the next 200 hours of operation , whichever occurs later .
NOTE:
For model 210 - 5
(205) , 206 , P206 / TP206 , U206 / TU206 airplanes that have been modified by the installation of SK206 - 42 , SK206 - 42A , SK206 - 42B or SK206 - 42C , compliance with SEB93 - 5 Revision 2 is not required.
NOTE:
For model 207 / T207 airplanes that have been modified by the installation of SK207 - 19 or later revision , compliance with SEB93 - 5 Revision 2 is not required.
NOTE:
Model 207 / T207 airplanes that have been modified by the installation of SK206 - 42 , SK206 - 42A , SK206 - 42B or SK206 - 42C must comply with SEB93 - 5 Revision 2 and the applicable steps outlined in the Accomplishment Instructions of SK207 - 19A or later revision.
B.
Repetitive Inspections:
1.
For model 210 - 5
(205) , 206 , P206 / TP206 , U206 / TU206 airplanes , accomplish every 1 , 000 hours of operation after the initial inspection until installation of SK206 - 42 (or latest revision).
2.
For 207 / T207 model airplanes (including aircraft that have been modified by the installation of SK206 - 42 , SK206 - 42A , SK206 - 42B , or SK206 - 42C) , accomplish every 1 , 000 hours of operation after the initial inspection until installation of SK207 - 19 or applicable steps outlined in the Accomplishment Instructions of SK207 - 19A or later revision.
* * * * * * * SEB93 - 5 Revision 2 Page 6 May 29 , 2019
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