# STC SH1018EA - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Rilpa Enterprises, Ltd, Canada - Description: Installation of Casey shroud type heater. - Applied: September 15, 1975 - Status date: September 20, 2016 - Product: Aircraft, Rotorcraft - Certification basis: Part 21 - Data sheets: [TCDS H2SW](https://openairdocs.org/tcds/H2SW) - Certificate PDF: https://openairdocs.org/files/sha256/35/76/3576cdbe0ff98c4b9c3e28e4b576d40c23b4140ac8eea1e39c62c276544f8bf5 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/5BA0539A9D333EAC8625804A004FDB8F.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SH1018EA ## ADs that name it (0) None. ## Approved models (9) - Bell Helicopter Textron (Canada) 206 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) - Bell Helicopter Textron (Canada) 206A ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) - Bell Helicopter Textron (Canada) 206A-1 (OH-58A) ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) - Bell Helicopter Textron (Canada) 206B ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) - Bell Helicopter Textron (Canada) 206B-1 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) - Bell Helicopter Textron (Canada) 206L ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) - Bell Helicopter Textron (Canada) 206L-1 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) - Bell Helicopter Textron (Canada) 206L-3 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) - Bell Helicopter Textron (Canada) 206L-4 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) ## What the certificate says Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record. FAA Form 8110-2 (5/14) Page 1 of Part of the Signature Title SH1018EA RILPA Enterprises Ltd. 480 Aviation Way N.E. Calgary, Alberta T2E 7G3 Canada Civil Air Regulations. 6 Installation of Casey shroud type heater in one of the following configurations: Configuration A: Installed in accordance with Casey Copter’s Installation Instructions CCA 25-206, Revision C, dated June 8, 1976 and drawing No. 250-206 (5 sheets) Issue D, June 10, 1976. (See Description of Type Design Change continued on Page 3 of 5) 1. Limited to above models equipped with Detroit Diesel Allison 250 series engines. 2. Maintenance schedule should be preformed in accordance with Section 12 of the Installation Instructions applicable to the specified configuration. 3. Configuration B only eligible on Bell 206B Helicopter Serial Numbers 2821 and 2828. 4. Configurations A, C, D, E, H, I and J eligible only on helicopter models 206, 206A, 206A-1, 206B and 206B-1. 5. Configurations F and K eligible only on helicopter model 206L. (See Limitations and Conditions continued on Page 5 of 5) Raymond H. Reinhardt Acting Manager New York Aircraft Certification Office Bell 206, 206A, 206A-1, 206B, 206B-1, 206L, 206L-1, 206L-3 and 206L-4 October 27, 1995, May 7, 1997, September 14, 2000 November 1, 2000, September 20, 2016 February 4, 1976, September 27, 1976, November 14, 1979, December 8, 1980, June 5, 1981, (See Date Amended continued on Page 5 of 5) September 15, 1975 October 16, 1975 IMPORT H2SW 5 FAA Form 8110-2 (5/14) Page 2 of To (Name and address of transferee) From (Name and address of grantor) 5 SH1018EA FAA Form 8110-2 (5/14) Page 3 of 5 Date Reissued: September 20, 2016 Description of Type Design Change (continued): Configuration B: Kit 250-206E-2 in accordance with Casey Copter’s Installation Instructions 25-206E-2, Revision 1 and Drawing No. 250-206E Issue F. Configuration C: Kit 250-206-2, in accordance with Casey Copter’s Installation Instructions 25-206-2, Revision 2, April 10, 1979 and Drawing 250-206 (5 sheets), Revision F, August 5, 1978. Configuration D: Kit 250-206-2-A, in accordance with Casey Copter’s Installation Instructions 25-206-2-A, Issue A, December 15, 1979 and Drawing 250-206-2-A (5 sheets), Revision A, December 15, 1979. Configuration E: Kit 250-206E-2, in accordance with Casey Copter’s Installation Instructions 25-206E-2, Revision 2, March 18, 1980 and Drawing No. 250-206-E (5 sheets), Revision G, March 18, 1980. Configuration F: Kit 250-206L-2, in accordance with Casey Copter’s Installation Instructions 25-206L-2, Basic Issue, October 6, 1978 and Drawing No. 250-206-L (6 sheets), Revision G, April 6, 1980. Configuration G: Kit 250-206L1-2, in accordance with Casey Copter’s Installation Instructions Issue A, April 10, 1980 and Drawing No. 250-206L1 (6 sheets), Revision B, April 7, 1980. Configuration H: Kit 250-206-3, in accordance with one of the following: 1. Casey Copter’s Installation Instructions 25-206-2, Revision 2, April 10, 1979, Drawing 250-206 (5 sheets), Revision F, August 5, 1978 and Engineering Change Order CCA 80-15, April 22, 1980. 2. Casey Copter’s Installation Instructions 25-206-3, Issue, May 11, 1981 and a. Drawing 250-206-3, Issue N.C., May 12, 1981, or b. Casey Copter’s Drawing 250-206-3 (5 sheets), Revision A, June 21, 1982. 3. Casey Copter’s Installation Instructions 25-206-3, Issue A, February 1, 1988 and a. Top Drawing List TD250-206-3, Issue B, dated February 1, 1988 or b. Top Drawing List TD250-206-3, Issue C, dated October 18, 1989. Configuration I: Kit 250-206-3-A in accordance with one of the following: 1. Casey Copter’s Installation Instructions 25-206-3-A, Issue A, December 15, 1979, Drawing 250-206-2-A, (5 sheets), Revision A, December 15, 1979 and Engineering Change Order CCA 80-16, May 3, 1980. 2. Casey Copter’s Installation Instructions 25-206-3-A, Basic Issue, June 2, 1981 Drawing 250-206-3-A, Issue N.C., July 7, 1981. 3. Casey Copter’s Installation Instructions 25-206-3-A, Revision A, July 15, 1982 Drawing 250-206-3-A (5 sheets), Revision A, July 15, 1982 4. Casey Copter’s Installation Instructions 25-206-3-A, Issue B, February 1, 1988 and Top Drawing List TD250-206-3A,Issue B, February 1, 1988. (See Description of Type Design Change continued on Page 4 of 5) SH1018EA FAA Form 8110-2 (5/14) Page 4 of 5 SH1018EA Date Reissued: September 20, 2016 Description of Type Design Change (continued): Configuration J: Kit 250-206E-3, in accordance with one of the following: 1. Casey Copter’s Installation Instructions 25-206E-2, Revision 2, March 18, 1980, Drawing No. 250-206-E (5 sheets), Revision G, March 18, 1980 and Engineering Change Order CCA 80-14, April 2, 1980 2. Casey Copter’s Installation Instructions 25-206E-3, Basic Issue, June 30, 1981 and Drawing 250-206E-3, Issue N.C., July 7, 1981 3. Casey Copter’s Installation Instructions 25-206E-3, Revision A, August 26, 1983 and Drawing 250-206E-3 (5 sheets), Revision A, July 6, 1982 -or- Casey Copter’s Drawing 250-206E-3 (10 sheets), Revision B, May 25, 1983 Configuration K: Kit 250-206L-3, in accordance with one of the following: 1. Casey Copter’s Installation Instructions 25-206L-2, Basic Issue, October 6, 1978, Drawing No. 250-206L (6 sheets), Revision G, April 6, 1980 and Engineering Change Order CCA 80-17, April 28, 1980. 2. Casey Copter’s Installation Instructions 25-206L-3, Basic Issue, June 22, 1981, Drawing 250-206L3, Issue N.C., July 7, 1981. 3. Casey Copter’s Installation Instructions 25-206L-3, Revision A, July 22, 1982 and Drawing 250-206L-3 (6 sheets), Revision A, July 14, 1982. 4. Casey Copter’s Installation Instructions 25-206L-3, Issue B, February 1, 1988 and Top Drawing List TD250-206L3, Issue C, February 1, 1988. Configuration L: Kit 250-206L1-3, in accordance with one of the following: 1. Casey Copter’s Installation Instructions 25-206L1-2, Issue A, April 10, 1980, Drawing No. 250-206L1 (6 sheets) Revision B, April 7, 1980 and Engineering Change Order CCA 80-18, April 28, 1980. 2. Casey Copter’s Installation Instructions 25-206L1-3, Basic Issue, June 22, 1981, and a. Drawing 250-206L1-3, Issue N.C., July 7, 1981, or b. Casey Copter’s Drawing 250-206L1-3. Issue N.C., July 7, 1981, or c. Casey Copter’s Drawing 250-206L1-3 (6 sheets), Revision A, August 14, 1982. 3. Casey Copter’s Installation Instructions 25-206L1-3, Basic Issue, June 22, 1981, and a. Drawing 250-206L1-3, Issue N.C., July 7, 1981, or b. Casey Copter’s Drawing 250-206L1-3. Issue N.C., July 7, 1981, or c. Casey Copter’s Drawing 250-206L1-3 (6 sheets), Revision A, August 14, 1982. 4. Casey Copter’s Installation Instructions 25-206L1-3, Issue A, February 1, 1988, and a. Top Drawing List TD250-206L1-3, Issue C, February 1, 1988, or b. Top Drawing List TD250-206L1-3, Issue D, dated October 18, 1989. Configuration M: Kit 206-C20-TX2 in accordance with: Casey Copter’s Installation Instructions 206-S-102, Issue N.C., September 22, 1983 and Drawing 250-206E-3 (10 sheets), Revision B, May 25, 1983. (See Description of Type Design Change continued on Page 5 of 5) FAA Form 8110-2 (5/14) Page 5 of 5 Date Reissued: September 20, 2016 Description of Type Design Change (continued): Configuration N: Kit 206L-C28-HS2 in accordance with one of the following: 1. Casey Copter’s Installation Instructions 206-S-001, Issue N.C., November 4, 1982 and Drawing 206L-C28-HS2 (6 sheets), Issue N.C., November 4, 1982. 2. Casey Copter’s Installation Instructions 206-S-101, Issue A, February 1, 1988 and Top Drawing List TD206-D-005, Issue A, February 1, 1988. Configuration O: Kit 206L-C30-TX1 in accordance with one of the following: 1. Casey Copter’s Installation Instructions 206-S-002, Issue N. C., January 5, 1983 and Drawing 206L-C30-TX1 (9 sheets), Issue N.C., January 5, 1983. 2. Casey Copter’s Installation Instructions 206-S-002, Revision A, September 26, 1983 and Drawing 206L-C30-TX1 (9 sheets), Revision A, June 30, 1983. 3. Casey Copter’s Installation Instructions 206-S-002, Revision B, February 1, 1988 and Top Drawing TD 206L-C30-TX1, February 1, 1988. 4. Casey Copter’s Installation Instructions 206-S-002, Issue C, October 14, 1992 and Top Drawing List TD206L-C30-TX1, Issue D, October 14, 1992. 6. Configurations G, L and N eligible only on helicopter model 206L-1. 7. Configuration M eligible only on helicopter model 206B serial numbers 3567 and up. 8. Configuration O eligible only on helicopter models 206L-3 and 206L-4. 9. The installer must determine whether this design change is compatible with previously approved modifications. 10. If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission. Date Amended (continued): January 19, 1982, March 9, 1984, March 23, 1984, September 9, 1988, October 18, 1989, May 13, 1993 ----------END---------- SH1018EA ## Every issue (1) - September 20, 2016: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/35/76/3576cdbe0ff98c4b9c3e28e4b576d40c23b4140ac8eea1e39c62c276544f8bf5) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.