# STC SA4745NM

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: LifePort Inc, United States
- Description: Installation of Lifeport Patient Loading and Support System.
- Applied: October 12, 1988
- Status date: November 23, 1993
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A25CE](https://openairdocs.org/tcds/A25CE), [TCDS A27CE](https://openairdocs.org/tcds/A27CE), [TCDS A28CE](https://openairdocs.org/tcds/A28CE), [TCDS A37CE](https://openairdocs.org/tcds/A37CE), [TCDS A7CE](https://openairdocs.org/tcds/A7CE), [TCDS A10SW](https://openairdocs.org/tcds/A10SW), [TCDS A2PC](https://openairdocs.org/tcds/A2PC), [TCDS A20SO](https://openairdocs.org/tcds/A20SO), [TCDS A3SO](https://openairdocs.org/tcds/A3SO), [TCDS A7SO](https://openairdocs.org/tcds/A7SO), [TCDS A8EA](https://openairdocs.org/tcds/A8EA), [TCDS 3A15](https://openairdocs.org/tcds/3A15), [TCDS 3A16](https://openairdocs.org/tcds/3A16), [TCDS 3A20](https://openairdocs.org/tcds/3A20), [TCDS A14CE](https://openairdocs.org/tcds/A14CE), [TCDS A23CE](https://openairdocs.org/tcds/A23CE), [TCDS A24CE](https://openairdocs.org/tcds/A24CE), [TCDS A31CE](https://openairdocs.org/tcds/A31CE), [TCDS 2A4](https://openairdocs.org/tcds/2A4)
- Certificate PDF: https://openairdocs.org/files/sha256/18/8c/188cddefa5f07f1e0661da65df416b5ae361feb69ef826ba7a06c54bb724329a
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/FB5C5F31A16C282785256CC2000E3E58.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA4745NM

## ADs that name it (0)

None.

## Approved models (101, first 50)

- Mitsubishi Heavy Industries Ltd. MU-2B-10 ([TCDS A2PC](https://openairdocs.org/tcds/A2PC))
- Mitsubishi Heavy Industries Ltd. MU-2B-15 ([TCDS A2PC](https://openairdocs.org/tcds/A2PC))
- Mitsubishi Heavy Industries Ltd. MU-2B-20 ([TCDS A2PC](https://openairdocs.org/tcds/A2PC))
- Mitsubishi Heavy Industries Ltd. MU-2B-25 ([TCDS A2PC](https://openairdocs.org/tcds/A2PC))
- Mitsubishi Heavy Industries Ltd. MU-2B-26 ([TCDS A10SW](https://openairdocs.org/tcds/A10SW))
- Mitsubishi Heavy Industries Ltd. MU-2B-26 ([TCDS A2PC](https://openairdocs.org/tcds/A2PC))
- Mitsubishi Heavy Industries Ltd. MU-2B-26A ([TCDS A10SW](https://openairdocs.org/tcds/A10SW))
- Mitsubishi Heavy Industries Ltd. MU-2B-30 ([TCDS A2PC](https://openairdocs.org/tcds/A2PC))
- Mitsubishi Heavy Industries Ltd. MU-2B-35 ([TCDS A10SW](https://openairdocs.org/tcds/A10SW))
- Mitsubishi Heavy Industries Ltd. MU-2B-35 ([TCDS A2PC](https://openairdocs.org/tcds/A2PC))
- Mitsubishi Heavy Industries Ltd. MU-2B-36 ([TCDS A10SW](https://openairdocs.org/tcds/A10SW))
- Mitsubishi Heavy Industries Ltd. MU-2B-36 ([TCDS A2PC](https://openairdocs.org/tcds/A2PC))
- Mitsubishi Heavy Industries Ltd. MU-2B-36A ([TCDS A10SW](https://openairdocs.org/tcds/A10SW))
- Mitsubishi Heavy Industries Ltd. MU-2B-40 ([TCDS A10SW](https://openairdocs.org/tcds/A10SW))
- Mitsubishi Heavy Industries Ltd. MU-2B-60 ([TCDS A10SW](https://openairdocs.org/tcds/A10SW))
- Raytheon Aircraft Company 100 ([TCDS A14CE](https://openairdocs.org/tcds/A14CE))
- Raytheon Aircraft Company 200 (A100-1 (U-21J)) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company 200C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company 200CT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company 200T ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company 300 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company 300LW ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company 36 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Raytheon Aircraft Company 58 ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Raytheon Aircraft Company 58A ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Raytheon Aircraft Company 58TC ([TCDS A23CE](https://openairdocs.org/tcds/A23CE))
- Raytheon Aircraft Company 58TCA ([TCDS A23CE](https://openairdocs.org/tcds/A23CE))
- Raytheon Aircraft Company 65-90 ([TCDS 3A20](https://openairdocs.org/tcds/3A20))
- Raytheon Aircraft Company 65-A90 ([TCDS 3A20](https://openairdocs.org/tcds/3A20))
- Raytheon Aircraft Company A100 (U-21F) ([TCDS A14CE](https://openairdocs.org/tcds/A14CE))
- Raytheon Aircraft Company A100A ([TCDS A14CE](https://openairdocs.org/tcds/A14CE))
- Raytheon Aircraft Company A200 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company A200 (C-12A) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company A200C (UC-12B) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company A200CT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company A36 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Raytheon Aircraft Company A36TC ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Raytheon Aircraft Company B100 ([TCDS A14CE](https://openairdocs.org/tcds/A14CE))
- Raytheon Aircraft Company B200 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company B200C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company B200CT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company B200T ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company B300 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company B300C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company B36TC ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Raytheon Aircraft Company B90 ([TCDS 3A20](https://openairdocs.org/tcds/3A20))
- Raytheon Aircraft Company C90 ([TCDS 3A20](https://openairdocs.org/tcds/3A20))
- Raytheon Aircraft Company C90A ([TCDS 3A20](https://openairdocs.org/tcds/3A20))
- Raytheon Aircraft Company E90 ([TCDS 3A20](https://openairdocs.org/tcds/3A20))
- Raytheon Aircraft Company F90 ([TCDS A31CE](https://openairdocs.org/tcds/A31CE))

All 101: https://openairdocs.org/stc/SA4745NM/models.md

## What the certificate says

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA1745N1 This certificate issued to: Lifeport, Inc, a Washington Corporation Part * of the Regulations Original Product -Type bertificate Number: * See attached FAA Approved Model List (AML) Make: * No. SA4745NM for list of approved airplane Model: * models and applicable airworthiness regulations.

Description of Type Design Change: Installation of Lifeport Patient Loading and Suppor ystem in accordance with Lifeport Installation Instructions and Drawings as listed o the FAA Approved Model List (AML) of this STC, or later FAA approved revisions.

Limitations and Conditions: Approval of this change in type design applies to the above model aircraft only. This approval should not be extended to aircraft of this model on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any other previously approved modification, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this Certificate and FAA Approved Model List (AML) No. SA4745NM, dated July 20, 1989, or later FAA approved revision, must be is taffeds and he sup thing aunt is celess for opened tal martin fed until sunvendered, suspended, revoked, or a termination date is otherwise established by the Administrator sf the Federal Aviation Administration .

Date of Application: October 12, 1988 Fule missued: August 1, 1989, February 28, 1990 Date of Issuance: July 20, 1989 Jateauceded: January 12, 1990, July 25, 1990 FEDERAL VIATIO By Direction of the Administrator (Signature) TOMINISTRATO Assistant Manager, Seattle Aircraft Certification Office

12808 N.E. 95th St. Vancouver, WA 98682 AFM SUPPLEMENT NO. AND DATE 11/23/93 NO. 8 11/23/93 NO. 7 11/23/93 No. 23 11/23/93 Issue Date: July 20, 1989 NO.8 REVISION NO AND DATE NR 12/20/89 G 3/6/92 E 1/29/93 A 3/6/92 NR 12/20/89 G 3/6/92 E 1/29/93 A 3/6/92 NR 12/20/89 G 3/6/92 D 3/6/92 E 1/29/93 A 3/6/92 A 10/26/93 IR 2/26/93

FAA SEALED DRAWING/ DRAWING LIST LIFEPORT PATIENT LOADING AND SUPPORT SYSTEM NUMBER Model 100-1 Model 300-9 510-9050 510-4000 Model 100-1 Model 300-9 510-9050 510-4000 Model 100-2 Model 300-7 Model 320-1 510-9050 510-4400 510-4405 510-2080 FOR CERTIFICATION BASIS FOR ALTERATION CAR 3, Dated 5/15/56 FAR 23, Dated 2/1/64 FAR 23, Dated 2/1/65 FAR 23 ORIGINAL TYPE CERTIFICATE NUMBER A7CE A25CE A28CE A37CE AIRCRAFT MODEL 401,A,B,402,A,B,C 411,A,414,A, 421,A,B,C 425 404 90₺ It₺ AIRCRAFT MAKE CESSNA Page 1 of 8 ITEM

LifePort, Inc. 12808 N.E. 95th St. Vancouver, WA 98682 Issue Date: July 20, 1989 AFM SUPPLEMENT REVISION NO NO. AND DATE AND DATE NO. 11 11/23/93 G 3/6/92 E 1/29/93 IR. 5/5/93 NO. 11 11/23/93 D 3/6/92 D 3/6/92 E 1/29/93 IR 5/5/93

FAA SEALED DRAWING/ DRAWING LIST FAA APPROVED MODEL LIST (AML) NO. SA4745NM FOR LIFEPORT PATIENT LOADING AND SUPPORT SYSTEM CERTIFICATION BASIS FOR NUMBER ALTERATION Model 300-10 FAR 23, Dated 2/1/65 510-9050 510-5000 FAR 23, Dated 2/1/65 Model 320-2 Model 320-3 510-9050 510-5000 ORIGINAL TYPE CERTIFICATI NUMBER A27CE A27CE AIRCRAFT MODEL 501 551 AIRCRAFT MAKE CESSNA (Continued) Page 2 of 8 ITEM

WILL WIL LEIL. 12808 N.E. 95th St. Vancouver, WA 98682 Issue Date: July 20, 1989 AFM SUPPLEMENT REVISION NO NO. AND DATE AND DATE No. 14 11/23/93 A 5/14/92 No. 14 11/23/93 A 5/14/92

FAA SEALED DRAWING/ DRAWING LIST LIFEPORT PATIENT LOADING AND SUPPORT SYSTEM NUMBER 510-5800 510-5800 FOR CERTIFICATION BASIS FOR ALTERATION CAR 3, Dated 5/15/1956 CAR 3, Dated 5/15/1956 ORIGINAL TYPE CERTIFICATI NUMBER ЗА15 3A16 AIRCRAFT MODEL 36, A36, B36, A36TC, B36TC 58, 58A, 58TC, 58TCA AIRCRAFT MAKE BEECH Page 3 of 8 ITEM

LitePort, Inc. 12808 N.E. 95th St. Vancouver, WA 98682 Issue Date: July 20, 1989 AFM REVISION NO. SUPPLEMENT NO. AND DATE AND DATE No. 5 11/23/93 NR 12/20/89 G 3/6/92 E 1/29/93 A 3/6/92 No. 5 11/23/93 NR 12/20/89 G 3/6/92 E 1/29/93 A 3/6/92 No. 5 11/23/93 NR 12/20/89 G 3/6/92 E 1/29/93 A 3/6/92 NR 12/20/89 No. 5 11/23/93 G 3/6/92 E 1/29/93 A 3/6/92

FAA SEALED DRAWING/ DRAWING LIST FAA APPROVEU MUUEL LISI (AML) NO. SA4/40NM FOR CERTIFICATION BASIS FOR NUMBER ALTERATION CAR 3, Dated 5/15/56 Model 100-3 Model 300-7 510-9050 510-9000 Model 100-3 FAR 23, Dated 2/1/65 Model 300-7 510-9050 510-9000 Model 100-3 FAR 23, Dated 2/1/65 Model 300-7 510-9050 510-9000 Model 100-3 FAR 23, Dated 2/1/65 Model 300-7 510-9050 510-9000 ORIGINAL TYPE CERTIFICATI NUMBER 3A20 A14CE A24CE A31CE AIRCRAFT MODEL 65-90, 65-490 B90, C90, E90, Hº0 COA 100, A100, A100A A100C B100 200, 200A,, 200C 200T,200CT,A200, A200C, A200CT B200, B200C,B200T B200CT, 300, 3OOLW, B300, B300-C F90 AIRCRAFT MAKE BEECH Page 4 of 8 ITEM

12808 N.E. 95th St. Vancouver, WA 98682 Issue Date: July 20, 19 AFM SUPPLEMENT NO. AND DATE No. 6 11/23/93 No. 6 11/23/93 REVISION NO. AND DATE G 3/6/92 E 1/29/93 G 3/6/92 E 1/29/93

FAA SEALED DRAWING/ DRAWING LIST FAA APPROVED MODEL LIST (AML) NO. SA4745NM FOR LIFEPORT PATIENT LOADING AND SUPPORT SYSTEM CERTIFICATION BASIS FOR ALTERATION NUMBER CAR 3, Dated 5/15/56 Model 300-1 Model 300-3 Model 300-5 510-9050 CAR 10, Dated 3/28/55 Model 300-1 and Model 300-3 CAR 3, Dated 5/15/56 Model 300-5 510-9050 ORIGINAL TYPE CERTIFICATI NUMBER A10SW A2PC AIRCRAFT MODEL MU-2B-25. MU-2B-35, MU-2B-26 MU-2B-36 MU-2B-26A MU-2B-36A MU-2B-40. MU-2B-60, MU-2B, MU-2B-10, MU-2B-20, MU-2B-15, MU-2B-30, MU-2B-35, MU-2B-25, MU-2B-36, MU-2B-26 AIRCRAFT MAKE MITSUBISHI Page 5 of 8 ITEM

12808 N.E. 95th St. Vancouver, WA 98682 AFM SUPPLEMENT NO. AND DATE No. 12 11/23/93 No. 13 11/23/93 No. 19 11/23/93 No. 9 11/23/93 No. 9 11/23/93 Issue Date: July 20, 1989 REVISION NO. AND DATE B 3/6/92 B 3/6/92 A 11/13/92 D 7/22/93 D 7/22/93

FAA SEALED DRAWING/ FAA APPROVED MODEL LIST (AML) NO. SA4745NM FOR LIFEPORT PATIENT LOADING AND SUPPORT SYSTEM CERTIFICATION BASIS DRAWING LIST FOR NUMBER ALTERATION CAR 3, Dated 5/15/56 510-3100 CAR 3, Dated 5/15/56 510-3100 510-4200 CAR 3, Dated 5/15/56 510-3400 510-3400 ORIGINAL TYPE CERTIFICATE NUMBER A20SO (Includes T-1020 Version) ASEA (Includes T-1040 Version) A2350 A350 A7SO AIRCRAFT MODEL PA-31,PA31-300 PA-31-325, PA-31-350 PA-31P, PA-31T, PA-31T1, PA-31T2, PA-31T3, PA-31P-350 PA-42, PA42-720 PA-42-1000 PA32-260, 32-300 325-300, 32R-300; 32RT-300, 32R-301 32R-301T PA34-200, 34-200T, 34-220T AIRCRAFT MAKE PIPER Page 6 of 8 ITEM

LitePort, Inc. 12808 N.E. 95th St. Vancouver, WA 98682 Issue Date: July 20, 1989 AFM SUPPLEMENT NO. AND DATE 11/23/93 No. 17 REVISION NO. AND DATE IR 5/5/93

FAA SEALED DRAWING/ DRAWING LIST FAA APPROVED MODEL LIST (AML) NO. SA4745NM FOR LIFEPORT PATIENT LOADING AND SUPPORT SYSTEM CERTIFICATION BASIS FOR NUMBER ALTERATION FAR 23 510-6900 ORIGINAL TYPE CERTIFICATE NUMBER 2A4 AIRCRAFT MODEL 690, 690A, 690B 690C, 690D AIRCRAFT MAKE Twin Commander Page 7 of 8 ITEM

LHU OIL 1HO. 12808 N.E. 95th St. Vancouver, WA 98682 AFM SUPPLEMENT NO. AND DATE NA NA NA NA Manager, Aircraft Modification Branch Seattle Aircraft Certification Office Issue Date: July 20, 1989 FAA SEALED DRAWING/ DRAWING LIST REVISION NO. AND DATE M 11/11/93 C 11/11/93 S 12/9/93 D 7/24/92 FAA Approved: Ce Make: Dee 15,1993 FAA APPROVED MODEL LIST (AML) NO. SA4745NM FOR LIFEPORT PATIENT LOADING AND SUPPORT SYSTEM NUMBER The following control drawings are also approved for use with the above installations: 100-1000 100-1003 300-1000 310-1000 Description Eligible Sled Assemblies Eligible Narrow Door AeroSleds Eligible PLUS Optional Equipment Finish and Trim Specification Page 8 of 8 100-1000 100-1003 300-1000 310-1000

## Every issue (2)

- November 23, 1993: Amended, Current. [certificate](https://openairdocs.org/files/sha256/18/8c/188cddefa5f07f1e0661da65df416b5ae361feb69ef826ba7a06c54bb724329a)
- July 25, 1990: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/5f/48/5f487780a1b9c1428832201fd18961a51290a9fc9d6fd7a5454764759ae2e975)

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