# STC SA02248LA - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Sky IMD Inc, United States - Description: Installation of Sensor Pod and wiring for a passenger operated monitoring system - Applied: July 16, 2008 - Status date: January 30, 2014 - Product: Aircraft, Single-Engine - Certification basis: Part 3, Part 21, Part 23 - Data sheets: [TCDS 3A19](https://openairdocs.org/tcds/3A19), [TCDS 3A12](https://openairdocs.org/tcds/3A12), [TCDS 3A13](https://openairdocs.org/tcds/3A13), [TCDS A4CE](https://openairdocs.org/tcds/A4CE), [TCDS A13EU](https://openairdocs.org/tcds/A13EU), [TCDS A4EU](https://openairdocs.org/tcds/A4EU), [TCDS A42EU](https://openairdocs.org/tcds/A42EU) - Certificate PDF: https://openairdocs.org/files/sha256/14/74/1474e06647ac9b3b71ea9e246119f1556e699a263d36f1955ca2378d7f7af130 - Approved model list and other attachments: [AML SA02248LA.pdf](https://openairdocs.org/files/sha256/4f/11/4f11e3f21a67b78ca7d641ba0d031c102f6a9a54cd0196417c584e10ea8b1582) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/0C22022FBC20172686257C75005995C7.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA02248LA ## ADs that name it (0) None. ## Approved models (35) - Cessna Aircraft Company 152 ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - Cessna Aircraft Company 172M ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172N ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172P ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172Q ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172R ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172S ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 182E ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 182F ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 182G ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 182H ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 182J ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 182K ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 182L ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 182M ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 182N ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 182P ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 182Q ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 182R ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 182S ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 182T ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 206H ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company F152 ([TCDS A13EU](https://openairdocs.org/tcds/A13EU)) - Cessna Aircraft Company F172M ([TCDS A4EU](https://openairdocs.org/tcds/A4EU)) - Cessna Aircraft Company F172N ([TCDS A4EU](https://openairdocs.org/tcds/A4EU)) - Cessna Aircraft Company F172P ([TCDS A4EU](https://openairdocs.org/tcds/A4EU)) - Cessna Aircraft Company F182P ([TCDS A42EU](https://openairdocs.org/tcds/A42EU)) - Cessna Aircraft Company F182Q ([TCDS A42EU](https://openairdocs.org/tcds/A42EU)) - Cessna Aircraft Company FR182 ([TCDS A42EU](https://openairdocs.org/tcds/A42EU)) - Cessna Aircraft Company R182 ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company T182T ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company T206H ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company TR182 ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company TU206G ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company U206G ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) ## 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. United States Of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate This certificate has been reissued to replace the original certificate reported as lost Number SA02248LA This Certificate issued to Part * of the * Regulations. Description of Type Design Change: Installation of Sensor Pod and wiring for a passenger operated monitoring system in accordance with Sky IMD Inc. Master Document List (MDL) Document No. PD01 revision I, dated July 21, 2011 or later FAA approved revision; Approved Model List (AML) No. SA02248LA revision B, dated December 29, 2011 or later FAA approved revision; and Instructions for Continued Airworthiness (ICA) Document No. 622 revision F, dated July 20, 2011 or later FAA approved revision. Limitations and Conditions: This STC is for installation of the sensor pod and wiring from the sensor pod into the fuselage. This STC does not include power to the sensor pod or the sensor control unit. (See page 3 for continued Limitations and Conditions) SKY IMD Inc. 530 Bragato Road San Carlos, CA 94070 Original Product Type Certificate Number : Date reissued : January 30, 2014 Date amended : February 16, 2011, December 29, 2011 (Signature) Supervisor, Technical and Administrative Support Staff Los Angeles Aircraft Certification Office (Title) Date of application : July 16, 2008 Date of issuance : August 25, 2009 * See attached FAA Approved Model List (AML) Number SA02248LA Rev. B or later FAA approved revision for list of approved airplane models and applicable airworthiness regulations. United States Of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate (SA02248LA Continuation Sheet) The installation should not be incorporated in any airplane unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the airplane. The approval of this modification applies only to the airplane model series listed in the approved model list. A copy of this STC must be included in the permanent records of the modified airplane. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission. For operational approval of any device that contains lithium batteries in equipment connected to this STC provisions should be tested per the Lithium Battery Operational Performance Standards of RTCA/DO-311. Flight Standards may require the operator to show that the portable device’s batteries met certain test criteria for their operational approval. This change has been determined to be a no acoustic change in accordance with 14 CFR 21.93(b) Weight Limit Changes to 172, 182 & 206 models: Cessna 172M/N and F172M/N Cessna 182N Maximum Takeoff Weight: 2260 lbs Maximum Takeoff Weight: 2910 lbs Maximum Landing Weight: 2260 lbs Maximum Landing Weight: 2760 lbs Cessna 172P and F172P Cessna 182P/Q and F182P/Q Maximum Takeoff Weight: 2360 lbs Maximum Takeoff Weight: 2910 lbs Maximum Landing Weight: 2360 lbs Maximum Landing Weight: 2910 lbs Cessna 172Q/S Cessna R182, TR182, and FR182 Maximum Takeoff Weight: 2510 lbs Maximum Takeoff Weight: 3060 lbs Maximum Landing Weight: 2510 lbs Maximum Landing Weight: 3060 lbs Cessna 172R Cessna 182R, 182S, 182T, and T182T Maximum Takeoff Weight: 2410 lbs Maximum Takeoff Weight: 3060 lbs Maximum Landing Weight: 2410 lbs Maximum Landing Weight: 2910 lbs Cessna 182E/F/G/H/J/K/L/M Cessna U206G, TU206G, 206H, T206H Maximum Takeoff Weight: 2760 lbs Maximum Takeoff Weight: 3560 lbs Maximum Landing Weight: 2760 lbs Maximum Landing Weight: 3560 lbs - End - ### AML SA02248LA.pdf FAA Approved Models List (AML) No. SA02248LA, Rev. B Page 1 of 2 FAA APPROVED MODEL LIST (AML) NO. SA02248LA, Rev. B For SKY IMD, INC. INSTALLATION OF SENSOR POD Issue Date: December 29, 2011 Item Aircraft Make Aircraft Model Certification Basis for Alteration Original Type Certificate Number FAA Approved Master Document List Airplane Flight Manual Supplement Left Strut Mount (Series 1 Pod) Right Strut Mount (Series 1 Pod) Belly Mount Left Strut Mount (Series 2 Pod) Right Strut Mount (Series 2 Pod) 1 Cessna 152 CAR 3 3A19 PD01, Rev. E, dated June 9, 2009 or later FAA approved revisions. PD45, Rev. IR, dated 12/22/10, or later FAA approved revisions X X Installation Not Allowed Installation Not Allowed Installation Not Allowed 2 Cessna F152 CAR 3 A13EU PD01, Rev. E, dated June 9, 2009 or later FAA approved revisions. PD45, Rev. IR, dated 12/22/10, or later FAA approved revisions X X Installation Not Allowed Installation Not Allowed Installation Not Allowed 3 Cessna 172M, 172N, 172P, 172Q CAR 3 3A12 PD01, Rev. E, dated June 9, 2009 or later FAA approved revisions. PD46, Rev. A, dated 12/22/10, or later FAA approved revisions X X X X X 4 Cessna 172R, 172S Part 23 3A12 PD01, Rev. E, dated June 9, 2009 or later FAA approved revisions. PD46, Rev. A, dated 12/22/10, or later FAA approved revisions X X X X X 5 Cessna F172M, F172N, F172P CAR 3 A4EU PD01, Rev. E, dated June 9, 2009 or later FAA approved revisions. PD46, Rev. A, dated 12/22/10, or later FAA approved revisions X X X X X 6 Cessna 182E, 182F, 182G, 182H, 182J, 182K, 182L, 182M, 182N, 182P, 182Q, 182R, R182, TR182 CAR 3 3A13 PD01, Rev. E, dated June 9, 2009 or later FAA approved revisions. PD47, Rev. A, dated 12/22/10, or later FAA approved revisions X X X X X Notes: Items 1 & 2 only one pod may be installed per aircraft Items 3 - 10 up to two pods may be installed per aircraft FAA Approved: Manager, Airframe Branch Los Angeles Aircraft Certification Office FAA Approved Models List (AML) No. SA02248LA, Rev. B Page 2 of 2 FAA APPROVED MODEL LIST (AML) NO. SA02248LA, Rev. B For SKY IMD, INC. INSTALLATION OF SENSOR POD (Continued) Issue Date: December 29, 2011 Item Aircraft Make Aircraft Model Certification Basis for Alteration Original Type Certificate Number FAA Approved Master Document List Airplane Flight Manual Supplement Left Strut Mount (Series 1 Pod) Right Strut Mount (Series 1 Pod) Belly Mount Left Strut Mount (Series 2 Pod) Right Strut Mount (Series 2 Pod) 7 Cessna 182S, 182T, T182T Part 23 3A13 PD01, Rev. E, dated June 9, 2009 or later FAA approved revisions. PD47, Rev. A, dated 12/22/10, or later FAA approved revisions X X X X X 8 Cessna F182P, F182Q, FR182 CAR 3 A42EU PD01, Rev. E, dated June 9, 2009 or later FAA approved revisions. PD47, Rev. A, dated 12/22/10, or later FAA approved revisions X X X X X 9 Cessna U206G, TU206G CAR 3 A4CE PD01, Rev. G, dated June 10, 2010 or later FAA approved revisions. PD48, Rev. A, dated 12/22/10, or later FAA approved revisions X X X X X 10 Cessna 206H, T206H Part 23 A4CE PD01, Rev. G, dated June 10, 2010 or later FAA approved revisions. PD48, Rev. A, dated 12/22/10, or later FAA approved revisions X X X X X Notes: Items 1 & 2 only one pod may be installed per aircraft Items 3 - 10 up to two pods may be installed per aircraft FAA Approved: Manager, Airframe Branch Los Angeles Aircraft Certification Office Rev NC: Initial Release, dated 08/25/09 Rev A: Added U206 Series, added configuration and AFMS columns, corrected 172R and 172S Certification Basis, dated 02/16/11 Rev B: Reformatted AML. Added Strut Mount configuration for 206 Series. Added Series 2 Pod configurations for 172, 182, and 206 series ## Every issue (4) - January 30, 2014: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/14/74/1474e06647ac9b3b71ea9e246119f1556e699a263d36f1955ca2378d7f7af130), [AML SA02248LA.pdf](https://openairdocs.org/files/sha256/4f/11/4f11e3f21a67b78ca7d641ba0d031c102f6a9a54cd0196417c584e10ea8b1582) - December 29, 2011: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/d3/7e/d37e4ca75713ddf1653ee059a4600845063beb905a0867cc4e0c6c251ec425ee), [AML SA02248LA.pdf](https://openairdocs.org/files/sha256/77/29/772992f70ff543cfe01ab281a1bc363d49ae07e7a59b3a465ce520bf44c538ce) - February 16, 2011: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/d1/4f/d14f94bbd08ec55aa7c94a4ae369fb5f8215001430e5068b622389f955f3a9b7), [sa02248la AML.pdf](https://openairdocs.org/files/sha256/26/ce/26ce12f4cc3de788d7dd2171def2b03e36af3ae3932b8d7478b5c8c559eaa92d) - August 25, 2009: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/97/93/9793a44188d3d9be7b68edae27c4d2c339b65e718e771098b9172c8315152f17), [AML SA02248LA SKY IMD Inc.pdf](https://openairdocs.org/files/sha256/05/68/0568905e8bc982aca4bfb3a370577cf136049438fbd9a2030b85d4e6f22af32e) --- 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.