STC SR00275DE

Number   This certificate issued to:

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Original Product 7\SH&HUWLILFDWH1XPEHU Make:

VHHFRQWLQXDWLRQVKHHW IRUDGGLWLRQDOGDWHV By Direction of the Administrator Signature:

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1. The installer must determine whether this design change is compatible with previously approved modifications.

(Limitations and Conditions continued on Page 4 of 5) 06/18/1996 10/22/2024 06/21/2006 04/16/1997 06/08/2026 06/27/2022 08/17/2018 ✔ Joe B. Carrier, ODA administrator Air Methods, LLC, ODA-635841-NM 5 Installation of Emergency Medical Interior System in accordance with Configuration Data identified on Sheet 3; Rotorcraft Flight Manual Supplement (RFMS) number identified on Sheet 3; and Instructions for Continued Airworthiness (ICA) identified on Sheet 3.

(Description of Type Design Change continued on Page 3 of 5)

Number   (IIHFWLYH'DWH I Transferr Endorsementt Transfer the ownership of Supplemental Type Certificate Number:

Too (Name and address of transferee):

Date oI transfer:

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United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate  (Continuation Sheet) Number  (IIHFWLYH'DWH  $Q\DOWHUDWLRQRIWKLVFHUWLILFDWHLVSXQLVKDEOH E\D ILQH RIQRW H[FHHGLQJRULPSULVRQPHQWQRWH[FHHGLQJ \HDUVRUERWK7KLVFHUWLILFDWH PD\ EHWUDQVIHUUHGRUPDGH DYDLODEOHWR WKLUGSHUVRQVE\OLFHQVLQJDJ UHHPHQWVLQDFFRUGDQFHZLWK&)53RVVHVVLRQ RIWKLV6XSSOHPHQWDO7\SH &HUWLILFDWH 67& GRFXPHQWE\SHUVRQVRWKHUWKDQ WKH 67&KROGHUGR HVQRWFRQVWLWXWHULJKWVWRWKHGHVLJQGDWD QRUWRDOWHUDQ DLUFU DIW DLUFUDIWHQJLQH KROGHU$Q 67&KROGHUZKRDOORZVDSHUVRQWRXVHWKH67&WRDOWHUDQDLUFUDIWDLUFUDIWHQJLQHRUSURSHOOHUPXVWSURYLGH WKDWSHUVRQZLWKZULWWHQ SHUPLVVLRQ DFFHSWDEOHWR WKH)$$ 5HI &)5  )$$  3DJH BBBRI BBB SR00275DE 06/08/2026 Date Amended (Continued from Page 1): 08/09/2017; 06/06/2012; 02/07/2012; 06/27/2008 Description of Type Design Change (Continued from Page 1):

---Configuration/Data/RFMS/ICA---

1. Standard (Original)---Configuration Control Drawing (CCD) 189-9000 Rev -, dated 1/07/1996, or later approved revision/ RFMS 080-0219, Rev -, dated 4/16/1997, or later FAA approved revision/ ICA 050-0219, Rev A dated 4/09/1997, or later FAA accepted revision.

2. Basic---Master Drawing List (MDL) 181-9001 Rev A, dated 4/17/1997, or later approved revision/ RFMS 080-0219, Rev -, dated 4/16/1997, or later FAA approved revision/ ICA 050-0219, Rev A dated 4/09/1997, or later FAA accepted revision.

3. Alternate---MDL 181-9092, Rev - dated 6/27/2008, or later approved revision/ RFMS 080-0403 Rev IR, dated 6/27/2008 and 080-0663 Rev IR dated 4/1/2016, or later FAA approved revisions/ ICA 050-0477 Rev IR dated 4/30/2008 and 050-0663 Rev IR dated 4/01/2016, or later FAA accepted revision.

4. -001 Configuration---MDL 181-9092-001 Rev IR dated 1/28/2012, or later approved revision/ RFMS 080-0403 Rev D dated 5/10/2011, or later FAA approved revision/ ICA 050-0477 Rev C dated 12/05/2011 or later FAA accepted revision.

5. -002 Configuration---MDL 181-9092-002 Rev IR dated 2/02/2012, or later approved revision/ RFMS 080-0403 Rev D dated 5/10/2011, or later FAA approved revision/ ICA 050-0477 Rev C dated 12/05/2011 or later FAA accepted revision.

6. -003 Configuration---MDL 181-9092-003 Rev E dated 7/12/2012, or later approved revision/ RFMS 080-0403 Rev F dated 5/17/2012, or later FAA approved revision/ ICA 050-0477 Rev E dated 5/16/2012 or later FAA accepted revision.

7. -004 Configuration---MDL 181-9092-004 Rev G dated 9/05/2013, or later approved revision/ RFMS 080-0403 Rev F dated 5/17/2012 and 080-0663 Rev IR dated 4/01/2016, or later FAA approved revisions/ ICA 050-0477 Rev F dated 5/16/2013 and 050-0663 Rev IR dated 4/01/2016 or later FAA accepted revisions.

(Description of Type Design Change continued on Page 4 of 5) 35

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate  (Continuation Sheet) Number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escription of Type Design Change (Continued from Page 3):

---Configuration/Data/RFMS/ICA---

8. -005 Configuration---CCD 189-9154 Rev D dated 6/16/2022, or later approved revision/ RFMS 080-0403 Rev J dated 5/20/2022, or later FAA approved revision/ ICA 050-0477 Rev J dated 4/18/2022 or later FAA accepted revision. IF ALLS is installed as part of the -005 Configuration, RFMS 080-0663 Rev A dated 8/06/2018 or later FAA approved revision and ICA 050-0663 Rev A dated 8/06/2018, or later FAA accepted revisions are required.

Limitations and Conditions (Continued from Page 1):

2. A copy of this certificate must be maintained as part of the permanent records for the modified rotorcraft.

3. 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.

4. A copy of the FAA approved Rotorcraft Flight Manual Supplement (RFMS) is required for this installation.

5. A copy of the FAA accepted Instructions for Continued Airworthiness (ICA) is required for this installation.

6. This STC is applicable to all serial numbers for the Bell Textron Canada Limited Model 407.

7. Carry-on equipment (such as isolettes and medical portable electronic devices) may require FAA approval. Airworthiness considerations such as structural, electrical, electrical loads, electromagnetic compatibility, flammability, passenger compartment interior compliance, and operator considerations have not been approved for carry-on equipment.

Certification Basis:

Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the Bell Textron Canada Limited Model 407 installation of Emergency Medical Interior System is as follows:

(Certification Basis continued on Page 5 of 5) 45

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate  (Continuation Sheet) Number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ertification Basis (Continued from Page 4):

a. The type certification basis for Bell Textron Canada Limited Model 407 is shown on TCDS H2SW for parts not changed or not affected by the change.

b. The certification basis for parts changed or affected by the change since the reference date of application, June 18, 1996, is based upon part 27 as amended by Amendment 27-30. Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant/not significant changes in FAA Order 8110.48, the certification basis for this modification was determined to be:

Regulations at the latest amendment level -27.1365(c) at Amdt 27-35 Regulations at an intermediate amendment level -NONE Regulations at the amendment level in TCDS H2SW -ALL

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