Checklist for Cessna 150 G5
CESSNA 150 G5 · Checklist
Overview
This document serves as a checklist for the Cessna 150 G5, providing pilots with a structured approach to preflight, flight, and post-flight procedures. It is designed to ensure that all critical steps are followed to maintain safety and compliance with operational standards. The checklist includes various sections that cover essential tasks and checks that pilots must perform before and during flight, as well as after landing. This document is intended for use by pilots operating the Cessna 150 G5, offering a clear and concise reference to enhance flight safety and efficiency.
- Perform a thorough Preflight Inspection to ensure aircraft safety.
- Follow the correct Engine Start Procedures to avoid damage.
- Complete all Before Takeoff checks to ensure readiness for flight.
- Conduct Post-Flight Procedures to secure the aircraft and log the flight.
Document
Source
Originally published by static.garmin.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Checklist
- Pages
- 10
- File size
- 814 KB
- Publisher
- static.garmin.com
Common. One of the most common aircraft types we track.
Most owners only have the POH. Here's the essential set for the CESSNA 150 G5.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
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In this document
Preflight Inspection
The Preflight Inspection section outlines the necessary checks to be performed before flight. This includes verifying fuel levels, checking oil levels, inspecting the aircraft's exterior for damage, and ensuring that all control surfaces are functioning properly.
Engine Start Procedures
This section details the steps required to safely start the engine. It includes checking the fuel selector, ensuring the mixture is rich, and following the correct sequence for starting the engine to prevent damage.
Before Takeoff
The Before Takeoff section lists the critical checks that must be completed prior to departure. This includes verifying that the flight controls are free and correct, ensuring the flaps are set for takeoff, and confirming that the instruments are functioning properly.
Post-Flight Procedures
Post-Flight Procedures provide a checklist for actions to take after landing. This includes securing the aircraft, completing the flight log, and conducting a post-flight inspection to identify any potential issues.
Safety notes
- Always verify fuel levels before flight.
- Ensure that all control surfaces are functioning correctly before takeoff.
Full document text
EASA European Aviation Safety Agency SUPPLEMENTAL TYPE CERTIFICATE 10064473 This Supplemental Type Certificate is issued by EASA, acting in accordance with Regulation (EC) No. 216/2008 on behalf of the European Community, its Member States and of the European third countries that participate in the activities of EASA under Article 66 of that Regulation and in accordance with Commission Regulation (EU) No. 748/2012 to GARMIN (EUROPE) LIMITED LIBERTY HOUSE HOUNSDOWN BUSINESS PARK SOUTHAMPTON Hampshire SO40 9LR UNITED KINGDOM and certifies that the change in the type design for the product listed below with the limitations and conditions specified meets the applicable Type Certification Basis and environmental protection requirements when operated within the conditions and limitations specified below: Original Type Certificate Number: SEE EASA APPROVED MODEL LIST Type Certificate Holder: SEE EASA APPROVED MODEL LIST Type: SEE EASA APPROVED MODEL LIST Model: SEE EASA APPROVED MODEL LIST Description of Design Change: Installation of Garmin G5 Electronic Flight Instrument. EASA Certification Basis: a. The certification basis for parts not changed or not affected by this change remains unchanged from the original approval. b. The certification basis for parts changed or affected by this change is FAR Part 23: 23.301(a), 23.303, 23.305(a)(b), 23.307(a), 23.337(a)(b), 23.561(a)(b)(3), 23.561(e), 23.601, 23.603, 23.605(a), 23.607(b), 23.613(a)(b), 23.771(a), 23.773(a)(2), 23.777(a)(b), 23.853(a), 23.1301, 23.1303(a)(b)(c)(f), 23.1307, 23.1309(a)(b)(c)(d)(e), 23.1311(a)(1)(2)(3)(6)(7)(b), 23.1321(c)(d)(e), 23.1322, 23.1323(a)(b)(c), 23.1325(a)(b), For the European Aviation Safety Agency Cologne, Germany, 30 January 2018 See Continuation Sheet(s) 10053322 Dominique ROLAND Head of General Aviation and Remotely Piloted Aircraft Systems (RPAS) SUPPLEMENTAL TYPE CERTIFICATE - 10064473 - GARMIN (EUROPE) LIMITED - 309167 An Agency of the European Union TE.CERT.00091-003 © European Aviation Safety Agency. All rights reserved. ISO9001 Certified. Page 1 of 2 EASA European Aviation Safety Agency 23.1327(a)(1)(2), 23.1329(g)(h), 23.1331(a)(b)(1)(c), 23.1351(a), 23.1353(h), 23.1357(a)(b)(c)(d), 23.1359, 23.1365(a)(b)(d)(e), 23.1381(a)(b), 23.1431(a)(b), 23.1529, 23.1541, 23.1543(b), 23.1545(a)(b)(c), 23.1555(a) (b), 23.1581(a)(b)(d)(f), 23.1585(a). The requirements for environmental protection and the associated certified noise and/or emissions levels of the original product are unchanged and remain applicable to this certificate/ approval. Associated Technical Documentation: Installation in accordance with Garmin Master Drawing List (MDL) 005-01112-01, Revision 8, dated October 18, 2017. Instructions for Continued Airworthiness (ICA) as listed in above MDL. Operate in accordance with Garmin G5 Airplane Flight Manual Supplement as listed in above MDL. For EASA STC 10064473 Approved Models refer to Garmin Authorized Model List, 005-01112-46, Revision 1 or later revisions of the above listed documents approved by EASA. (1) The installation of the G5 requires the retention of existing mechanical airspeed indicator, altimeter, and vertical speed indicator. (2) For installations in aircraft approved for IFR operations: (a) If the G5 is installed as the primary attitude indicator, the existing rate of turn indicator must be retained. (b) If the G5 is installed as the rate of turn indicator, the existing primary attitude indicator must be retained. (3) For installations in aircraft approved for VFR-only operations, the G5 can be installed as the attitude indicator and rate of turn indicator without retention of either the existing attitude indicator or rate of turn indicator. (4) Aircraft modified by this STC must be operated in accordance with the Airplane Flight Manual Supplement (AFMS) identified above. (5) Aircraft modified by this STC must be maintained in accordance with the Instructions for Continued Airworthiness (ICA) identified above. (6) If the holder agrees to permit another person to use this certificate to alter the product, the holder must give the other person written evidence of that permission. Limitations/Conditions: Prior to installation of this design change it must be determined that the interrelationship between this design change and any other previously installed design change and/ or repair will introduce no adverse effect upon the airworthiness of the product. End - 10053322 An Agency of the European Union SUPPLEMENTAL TYPE CERTIFICATE - 10064473 - GARMIN (EUROPE) LIMITED - 309167 TE.CERT.00091-003 © European Aviation Safety Agency. All rights reserved. ISO9001 Certified. Page 2 of 2 EASA Authorized Model List G5 EASA AML STC EASA STC Number 10064473 Installation of Garmin G5 Electronic Instrument System Safety Agency Issued Date: Revised Date: (See Revision History for full list of revisions) European Aviation Safety Agency Paul HATTON Project Certification Manager Raad Hatter Aviation European Certification General Aviation EASA Authorized Model List G5 EASA AML STC Page 1 of 8 005-01112-46 Rev 1 Date EASA Authorized Model List, STC Number 10064473 See cover Original EASA Authorized Model List G5 EASA AML STC Model List Revision Log Description Jonap Aviation Europea 005-01112-46 Rev 1 Page 2 of 8 Safety Certification General Aviation Agency EASA Authorized Model List, STC 10064473 Aircraft Make (TCDS Holder) [common name or previous make] AT-3 (AERO AT SP.z o.o.) Bölkow BO 207 (AIRBUS DEFENCE AND SPACE GmbH) [Bölkow] Aircraft Model (alias) AT-3R100 Bölkow 207, Bölkow 207T Type Certificate Number EASA.A.021 TC Cert. Basis* MDL 005-01112-01 Model List Limitations Rev. Date Rev.** CS-VLA Rev 8 Rev 1 EASA.A.553 CAR Part 3 Amdt 3-1 to Rev 8 Rev 1 3-5 15 May 1956 Bölkow BO 208 (AIRBUS DEFENCE AND SPACE GmbH) [Bölkow] Bölkow Junior, Bölkow BO 208 C Junior EASA.A.358 CAR Part 3 Rev 8 Rev 1 Amdt 3-1 to 3-7 15 May 1956 Bölkow BO 209 (AIRBUS DEFENCE AND SPACE GmbH) [Bölkow]
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Bölkow BO 209 MONSUN, Bölkow BO 209 S EASA.A.357 FAR-23 through 23-9 Rev 8 Rev 1 Aviation Safety Agency Certification General Aviation EASA Authorized Model List G5 EASA AML STC 005-01112-46 Rev 1 Page 3 of 8 EASA Authorized Model List, STC 10064473 Aircraft Make (TCDS Holder) [common name or previous make] Aircraft Model (alias) L 200 (Aircraft Industries a.s.) [LET] L-200 A, L-200 D Type Certificate Number EASA.A.043 TC Cert. Basis* MDL 005-01112-01 Model List Rev. Date Limitations Rev.** BCAR normal Rev 8 Rev 1 amdt 6 CAR Part 3 normal BVF usage group P normal Aviation Safety Agency EASA Authorized Model List G5 EASA AML STC 005-01112-46 Rev 1 Page 4 of 8 European Certification General Aviation EASA Authorized Model List, STC 10064473 Aircraft Make (TCDS Holder) [common name or previous make] Aircraft Model (alias) HR200 and R2000 series (Alpha Aviation Concept Ltd.) HR200-100, HR200-120. HR200-120B, HR200-160, HR200-100S, R2100, R2100A, R2160, R2160D, R2112, R2160i, R2120U Type Certificate Number EASA.IM.A.086 TC Cert. Basis* MDL 005-01112-01 Model List Rev. Date Limitations Rev.** Various see Rev 8 Rev 1 TCDS Aquila AT01 (Aquila Aviation International GmbH) AT01 EASA.A.527 CS-VLA Rev 8 Rev 1 EASA Authorized Model List G5 EASA AML STC 005-01112-46 Rev 1 Page 5 of 8 Aviation European Safety Certification Agency General Aviation TC Cert. Basis* MDL 005-01112-01 Rev.** Model List Limitations Rev. Date Rev 8 Rev 1 EASA Authorized Model List, STC 10064473 Туре Certificate Number EASA.A.374 FAR 23 through Amt. 28 France SC Aircraft Make (TCDS Holder) [common Aircraft Model (alias) name or previous make] ATL (C.E.A.P.R.) [Robin] ATL, ATL "S", ATL "L" DR 200 Series (C.E.A.P.R.) [Robin] DR 300 Series, DR 400 Series (C.E.A.P.R.) [Robin] HR 100 Series, R 1000 Series (C.E.A.P.R.) [Robin] EASA Authorized Model List G5 EASA AML STC DR 200, DR 220, DR 221 B, DR 250, DR 220 A, DR 253, DR 250-160, DR 220 B, DR 253 B, DR 250 B, DR 220 AB, DR 250 B-160, DR 221 DR 340, DR 315,DR 360, DR 380, DR 300/108, DR 300/180 R, DR 300/140, DR 300/125, DR 300/120, DR 400/125, DR 400/140, DR 400/160, DR 400/180, DR 400/180 R, DR 400/2+2, DR 400/120, DR 400/125i, DR 400/140 B, DR 400/120 A, DR 400/160 D, DR 400/120 D, DR 400/180 S, DR 400/100, DR 400 RP, DR 400 NGL, DR 400/200 R, DR 400/500, DR 400/2001 CTC23 Issue 1 EASA.A.510 Various See TCDS Rev 8 Rev 1 EASA.A.367 Various see TCDS Rev 8 Rev 1 HR 100-200, HR 100-200 B, HR 100-210, HR 100-210 D, HR 100-285 Tiara, HR 100-250 TR, HR 100-285 C, R 1180 T, R 1180 TD EASA.A.368 Various see Rev 8 Rev 1 TCDS Aviation European Safety Certification General Aviation 005-01112-46 Rev 1 Page 6 of 8 Agency EASA Authorized Model List, STC 10064473 Aircraft Make (TCDS Holder) [common name or previous make] R3000 (C.E.A.P.R.) [Robin] Aircraft Model (alias) Туре Certificate TC Cert. Basis* MDL 005-01112-01 Model List Rev. Date Limitations R 3000/100, R 3000/120, R300/120 D, Number EASA.A.372 Rev.** FAR 23 Rev 8 Rev 1 R 3000/140, R 3000/160, R 3000/160 S, through R 3000/180 Amdt 23 P2002 (Construzioni Aeronautiche Tecnam S.r.l) DV 20 (Diamond Aircraft Industries GmbH) G 115 (GROB AIRCRAFT AG) HB 21 (HB-Flugtechnik GmbH) P2002-JF, P2002-JR EASA.A.006 CS-VLA Rev 8 Rev 1 DV 20, DV 20 E EASA.A.439 CS-VLA Rev 8 Rev 1 G 115, G 115A, G 115B, G 115C, G 115C2, G 115D, EASA.A.364 FAR 23 Amdt Rev 8 Rev 1 G 115D2, G 115EG, 32 HB 21, HB 21/2400, HB 21/2400 B, HB 21 V1, HB 21 V2 EASA.A.434 LFSM 1-Nov. Rev 8 Rev 1 1975 HB 23 (HB-Flugtechnik GmbH) HB 23/2400, HB 23/2400 SP, HB 23/2400 Scanliner, HB 23/2400 V2 EASA.A.433 Various see Rev 8 Rev 1 TCDS T67 (Slingsby Advanced Composites Ltd) [Firefly] MS880, Rallye 100, Rallye 150, Rallye MS 880B, MS 880B-D, MS 881, MS 885, MS 886, 180 (Socata) MS 890, MS 892, MS 893, MS 894, Rallye 235 (Socata) [MS 890 and Rallye 235 Series] MS 883, MS 887, MS 884, Rallye 100-S, Rallye 100 S-D, Rallye 100 ST, Rallye 100 ST-D, Rallye 110 ST, Rallye 150 T, Rallye 150 T-D, Rallye 150 ST, Rallye 150 ST-D, Rallye 150 SV, Rallye 150 SVS, Rallye 180 T, Rallye 180 T-D, Rallye 180 TS MS 890 A, MS 890 B, MS 892 A.150, MS 892 B.150, MS 892 E.150, MS 892 E-D.150, MS 893 A, MS 893 B, MS 893 E, MS 893 E-D, T67A, T67B Firefly, T67C Firefly, T67M Firefly, T67M-MkII Firefly, T67M200 Firefly EASA.A.390 Various see TCDS Rev 8 Rev 1 EASA.A.377 AIR 2052 - Ed. Rev 8 Rev 1 Novembre 1959 MS 894 A, MS 894 C, MS 894 E, Rallye 235 E, Rallye 235 E-D, Rallye 235 A, Rallye 235 C, Rallye 235 F Z 26 (ZLIN AIRCRAFT A.S.) [Morovan] Z 126, Z 126 T, Z 226 B, Z 226 T, Z 226 A, Z 226 M, EASA.A.379 French Norme AIR 2052 - Ed. Rev 8 Rev 1 Novembre 1959 Z 226 MS, Z 326, Z 326 A, Z 326 M, Z 526, Z 526 A, EASA.A.353 Various see TCDS Rev 8 Rev 1 EASA Authorized Model List G5 EASA AML STC Z 526 F, Z 526 L, Z 526 AFS, Z 526 AFS-V, Z 526 M, Z 726, Z 726 K 005-01112-46 Rev 1 Page 7 of 8 Aviation European Safety Certification General Aviatio Ac EASA Authorized Model List, STC 10064473 Aircraft Make (TCDS Holder) [common name or previous make] Aircraft Model (alias) Z 50 (ZLIN AIRCRAFT A.S.) [Morovan] Z 50 L, Z 50 LA, Z 50 LS, Z 50 LX, Z 50 M Type Certificate Number EASA.A.108 TC Cert. Basis* [* TC Certification Basis - See Type Certificate Data Sheet applicable to aircraft for complete certification basis.] [** Later EASA-approved revisions of the Master Drawing List may be used.] Limitations: ********END****** 14 CFR Part 23, incl. Amdt. 23-1 through 23- 14 MDL 005-01112-01 Rev.** Model List Rev. Date Limitations Rev 8 Rev 1 Safety European Ava Certification General Aviation Aviation EASA Authorized Model List G5 EASA AML STC 005-01112-46 Rev 1 Page 8 of 8 Agency
What's in the CESSNA 150 G5 TCDS
A Type Certificate Data Sheet (TCDS) is the FAA's record of what an aircraft type was approved as. It is the source of truth for weights, seating, fuel and the rules the design was certified against. Expand any line to see what it means.
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