ICA014502-B, CHKLST

Pilot checklist for ICON A5 Light Sport Aircraft (S-LSA)

Effective Date

5/26/21

All

ICA016024 ICON A5 POH

The latest edition of the ICON A5 Pilot Operating Handbook. For aircraft with 4-Blade E-Props propellers and MTOW 1570 lb.

Effective Date

03/22/2024

ALL

ICA015920 ICON A5 POH

The latest edition of the ICON A5 Pilot Operating Handbook. For aircraft with 4-Blade E-Props propellers and MTOW 1510 lb.

Effective Date

01/04/2024

ALL

ICA013115 ICON A5 POH

The latest edition of the ICON A5 Pilot Operating Handbook. For aircraft with 3-Blade Sensenich propellers and MTOW 1510 lb.

Effective Date

06/21/2023

ALL

ICON A5 650 Edition

The pilot's operating handbook for the 650kg edition of the ICON A5, certifying it for operations in the Republic of Korea and other relevant markets.

Effective Date

06/17/2022

SD-071323-A

Internally and externally inspect the left and right wings for wing skin damage caused by the left-hand and right-hand flap brackets.

Effective Date

08/16/2023

00184, 00186, 00187

SD-101722-A

Pilot and Copilot rudder pedal assemblies need to be inspected for proper bushing installation.

Effective Date

11/28/22

00126-00133, 00135, 00139, 00142-00146, 00148-00150, 00152-00156, 00158-00159, 00161

SD-092122-A

Immediate inspection and potential re-crimp of all 4 AWG wire to terminal connections

Effective Date

09/22/22

00135-00136, 00139-00146, 00148-00150, 00152-00159

SD-111521-C

Slipping Autopilot Bridle Cable Clamps

Effective Date

8/15/22

00139-00142, 00145, and 00149

SD-100421-A

Inspect fuel pressure relief block. Replace if non-conforming.

Effective Date

10/04/21

00056-00074, 00076-00135, 00137-00139, and 00142

SD-101419-A

Inspect fuel pump in compliance with Rotax ASB-912 i-011iS and replace fuel pump if affected.

Effective Date

11/27/19

00008, 00033, 00034, 00042, 00080-00085, 00088-00116

SD-090419-B

Perform new engine start procedure during each start sequence.

Effective Date

10/16/19

00001-00114

SD-071719-A

Remove and replace with new bolt at Elevator Pushrod to Aft Pitch Sector.

Effective Date

7/17/19

00001, 00004-00092, 00094-00099, 00101, 00102, 00104

SD-043019-A

Inspect IPS bridle C-ends, reinstall if not looped through quick link properly

Effective Date

01/19/18

00001-00021

SD-040717-A

Replace flap control tube aluminum rod ends with CRES rod ends

Effective Date

01/19/18

00001-00019

SD-031717-A

Install ball bearing using Loctite 603

Effective Date

01/19/18

00001-00019

SB-050224-A

Inspect for chafing between the rudder pedal cables and the floorboards and/or floorboard retainer bracket; trim parts to alleviate chafing as applicable. This is mandatory.

Effective Date

07/08/2024

00001-00062, 00064-00083, 00085-00100, 00102-00163, 00165-00184, 00186-00190, 00192, 00194-00198, 00199, 00201, 00204, 00205

SB-012724-A

Retrofit reed switch style NLG actuators with mechanical limit switches with long arms.

Effective Date

05/16/2024

If SB-080323 was NOT completed: 00001-00015, 00018-00027, 00029-00033, 00035, 00036, 00038- 00049, 00051-00072, 00074, 00076-00083, 00085, 00086, 00088-00182, 00184-00188

SB-012624-A

Inspect the clearance at the NLG limit switch and install longer switch arms. This is mandatory.

Effective Date

05/16/2024

00016, 00017, 00034, 00037, 00087, 00183, 00189-00192, 00194-00203, 00205, 00206, 00208, 00209, 00213, 00215 ///// IF SB-080323 was completed: 00001-00015, 00018-00027, 00029-00033, 00035, 00036, 00038- 00049, 00051-00072, 00074, 00076-00083, 00085, 00086, 00088-00182, 00184-00188

SB-032420-C

Mandatory Recurring Inspection of Nose Landing Gear (NLG) Actuator Rigging and NLG Actuator Stop Switches

Effective Date

05/16/2023

00001-00015, 00018-00027, 00029-00033, 00035, 00036, 00038-00049, 00051-00072, 00074, 00076-00083, 00085, 00086, 00088-00182, 00184-00188

SB-022724-A

Inspect security of IPS Rocket Motor and report results to ICON. This is mandatory.

Effective Date

04/22/2024

00001-00074, 00076-00129, 00131-00216

SB-112723-A

Inspect fuel tank and replace if nonconforming.

Effective Date

03/20/2024

00159-00196, 00198, 00199, 00202, 00203

SB-072823-A

Perform push/pull test of water rudder pivot flange; if bond fails, replace parts.

Effective Date

11/20/2023

00001-00148, 00150-00161, 00163-00168, 00170-00192

SB-022723-A

Inspect for stator wire harness chafing. If present, add F4 tape and/or reposition wires. This is mandatory to maintain airworthiness.

Effective Date

11/10/2023

00001 – 00136, 00139 – 00146, 00148 – 00150, 00152 – 00159, 00161, 00163, 00166, 00174

SB-050223-A

Install a Wing Fold Tube Cover to the inside of the parachute egress chamber. This is mandatory to maintain airworthiness.

Effective Date

11/06/2023

00001, 00003-00150, 00152-00202

SB-042123-B

Make a logbook entry reflecting the updated IPS Service Interval date, as described below. This is mandatory to maintain airworthiness.

Effective Date

10/10/2023

00004, 00006-00007, 00010-00011, 00013, 00021-00022, 00025-00026, 00029, 00031-00032, 00034-00157, 00159-00177, 00180

SB-080323-B

Nose Landing Gear Limit Switch Retrofit. Retrofit reed switch style NLG actuators with non-magnetic limit switches.

Effective Date

11/20/2023

00001-00015, 00018-00033, 00035-00036, 00038- 00072, 00074-00086, 00088-00182, 00184-00188

SB-041323-B

Perform a one-time inspection of the ELT antenna to identify any corrosion and remove and replace the ELT assembly as necessary.

Effective Date

09/07/2023

00001 – 00185

SB-030223-A

Inspect the CPS wires for any chafing and secure the CPS wires to the knock sensor bracket.

Effective Date

03/31/2023

00001 – 00136, 00139 – 00146, 00148 – 00150, 00152 – 00159, 00161, 00163, 00166

SB-022323-B

Adjust the position of the throttle cable to provide clearance between the throttle cable and lower intake plenum mount.

Effective Date

05-15-2023

00001 – 00136, 00139 – 00146, 00148 – 00150, 00152 – 00159, 00161, 00163, 00166

SB-112222-A

Inspect the flap gas strut for proper installation of the ball socket and rod end.

Effective Date

02/10/23

00001, 00003–00136, 00138–00146, 00148–00150, 00152–00159, 00161, 00163, 00166, 00170, 00172–00174, 00176, 00177

SB-011323-A

Inspect the Kevlar insulated or spiral wrapped wire harness for proper installation on the engine. If not properly installed, remove the cable ties, and resecure the wire harnesses.

Effective Date

01/19/23

00002–00136, 00139–00146, 00148–00150, 00152–00159, 00161, 00163, 00166, 00170

SB-101722-D

Inspect the canopy latch mechanism for proper torque and installation. Adjust the canopy latch mechanism if torque specifications are not met.

Effective Date

08/19/24

00130–00153; 00155; 00156; 00158–00166

SB-121622-A

Increase Torque of Fuel Filler Neck Clamps

Effective Date

1/12/23

00021–00176

SB-122722-A

Verify the current torque level of the jam nut on the rod end of the nose landing gear (NLG) actuator. If proper torque not present, apply proper torque.

Effective Date

12/27/22

00004–00015, 00017–00024, 00026–00074, 00076–00137, 00139, 00141–00142, 00144–00145, 00148–00150, 00152–00159, 00161, 00163, 00166

SB-120722-B

Disable the autopilot until Garmin software 9.13 and ICON configuration file are installed. The autopilot can be re-enabled and operated once the software is installed.

Effective Date

12/29/22

00139, 00141, 00142, 00144, 00145, 00148, 00149, 00150, 00152, 00153, 00155, 00156, 00158, 00159, 00161, 00166

SB-091222-A

1. Inspect installed Garmin GSA 28 servos for affected serial number (ref. Garmin Service Bulletin No. 22016). 2. Remove affected GSA-28 servo(s) and replace with a Garmin GSA 28 Mod 1 servo(s) (part number 011-02927-11).

Effective Date

10/17/22

00154 - 00161

SB-062322-B

Inspect the air rudder upper hinge pin for proper torque. The torque shall be between 48.7 in-lbs and 58.7 in-lbs

Effective Date

06/23/22

00001 – 00137, 00139, 00141 – 00146, 00148 – 00149, 00151, 00153

SB-051522-A

Inspect fuel pumps for ROTAX serial numbers S/N 180500 up to S/N 203724. If the ROTAX fuel pump is within this range (including S/N 180500 and S/N 203724), comply with ROTAX Service Bulletin SB-912i-013 dated 11 April 2022.

Effective Date

05/15/22

00001 - 00144

SB-111721-B

Check the Torque Value of the Quick Drain Valve and Correct as Necessary

Effective Date

04/02/22

00126-00132, 00134, 00135, 00139, 00141, 00142

SB-112221-A

Fuel pump assembly and connector contact replacement. Additional preflight and runup checks are required until replacement.

Effective Date

12/20/21

00089-00092, 00094, 00096-00113, 00115-00121, 00123-00125, 00127-00131, 00133, 00135, 00139, 00142

SB-110521-A

Fuel pump connector/contact replacement.

Effective Date

12/20/21

00093, 00095, 00114, 00122, 00126, 00134, 00141, 00144

SB-080321-A

Inspect and photograph Parachute System retention bracket attachment point area for dimensions of previous repair and submit results to ICON for further analysis.

Effective Date

08/12/21

00124, 00125, 00126, 00128, 00131, 00133, 00136

SB-092718-B

Inspect fuel level sensor for non‐conformance. Replace non‐ conforming units. 

Effective Date

5/31/21

00001-00028, 00030-00037, 00040, 00046, 00049, 00051-00053, 00126-00131

SB-121020-A

Application of Loctite 242 to the BRS parachute rocket actuation Bowden cable

Effective Date

01/19/21

00001-00125

SB-032420-A

Recurring Inspection of the NLG actuator rigging, and NLG actuator stop switches

Effective Date

6/8/20

ALL

SB-112619-A

Upgrade MSC software version to 3.1 (PN: ICA010570 rev E)

Effective Date

11/26/19

00001-00116

SB-041018-B

Inspect all brake master cylinder rod ends for corrosion and replace if necessary, replace brake master cylinder lower attachment bolts and carriage bolts with drilled head bolt for safety wiring

Effective Date

6/14/18

00001-00020, 00022-00036

SB-051818-C

Remove and Replace the Rudder Centering Spring

Effective Date

6/27/18

00022-00028, 00030-00036, 00039

SB-082718-A

Replace existing fuel sump system with latest version of system

Effective Date

08/27/18

00022-00036

SB-033018-B

Inspect engine oil return hose fitting for proper clearance from firewall and retorque both oil tank and engine oil return fittings

Effective Date

3/30/18

00001-00036

SB-032118-B

Replace the wing inboard roll bellcrank on both wings with new design bellcrank.

Effective Date

3/21/18

00001-00020, 00022-00025, 00028, 00030-00032

SB-110917-D

Install a retaining strap to improve Roll Pulley Bracket security

Effective Date

11/9/17

00001, 00003-00028

SB-050718-A

Verify correct torque on the forward horizontal tail attachment bracket and aft pitch pulley pivot bolt.

Effective Date

5/7/18

00022-00027

SB-051818-C

Remove and Replace the Rudder Centering Spring

Effective Date

5/18/18

00022-00028, 00030-00036, 00039

SB-073018 REV B

MSC Software Upgrade Version 3.0

Effective Date

7/30/18

00001-00044

SB-082718-A

Replace existing fuel sump system with latest version of system

Effective Date

8/27/18

00022-00036

SB-010218 REV A

DAC Software Upgrade Version 3.23

Effective Date

1/2/18

00001-00020, 00023, 00025, 00026

SB-050718-A

Verify correct torque on the forward horizontal tail attachment bracket and aft pitch pulley pivot bolt

Effective Date

5/18/18

00022-00027

SB-031318-A

Replace all six engine mount bolts with the new design

Effective Date

3/21/18

00001-00033 (excluding serial numbers that have completed MRA00363-A)

SB-072816-A

Inspect flexible engine compartment fuel and oil lines and replace if damaged

Effective Date

5/26/16

00001, 00003-00010

SB-060716-A

Comply with Rotax Service Bulletin SB-912 i-006

Effective Date

5/26/16

00001, 00003-00012

SL-081524-A

Update the Garmin G3X software from currently installed software to Garmin G3X software version 9.51

Effective Date

11/01/2024

00073, 00139 – 00146, 00148 – 00224

SL-090624-A

Revise Chapters 2 and 9 of the Pilot’s Operating Handbook and insert the new FAA Weight Exemption Letter No. 10829D. This is required for continued airworthiness. NOTE: The Weight Exemption Letter 10829D is only valid for U.S.-registered, Light Sport Aircraft. For all other aircraft, refer to the applicable registration and/or certification requirements.

Effective Date

10/18/2024

00001-00224

SL-072224-A

Apply sealant over the canopy latch screws to resolve and/or prevent water intrusion into the cockpit.

Effective Date

08/19/24

00001-00224

SL-051324-A

Update the Garmin G3X software from currently installed software to Garmin G3X software version 9.41

Effective Date

SUPERSEDED BY SL-081524-A

00073, 00139 – 00146, 00148 – 00222

SL-010424-A

Update Pilot’s Operating Handbook (POH) pages to ICA015920 ICON A5 POH, Issue A.

Effective Date

04/08/2024

00005, 00016, 00036, 00056, 00073, 00075, 00099, 00111, 00112, 00158, 00161, 00165, 00171, 00176, 00185, 00188, 00192, 00198-00200, 00202-00205, 00207, 00208, 00210, 00211

SL-021224-B

Update the Garmin G3X software from currently installed software to Garmin G3X software version 9.33

Effective Date

04/30/2024

00073, 00139 – 00146, 00148 – 00215

SL-090723-A

Release of Garmin G3X Software 9.31

Effective Date

10/25/2023

00073, 00139 – 00146, 00148 – 00195, 00197 – 00206

SL-050923-A

Update the Garmin G3X software from currently installed software to Garmin G3X software version 9.22.

Effective Date

06/02/23

00073, 00139–00146, 00148–00189

SL-120122-A

Verify the correct parachute and rocket service dates of the IPS are entered into the aircraft logbook.

Effective Date

12/01/22

ALL

SL-031422-A

At the next condition inspection, ensure that fuel filters are replaced with ROTAX fuel filters, Labeled “ROTAX” with Part No. 874060.

Effective Date

03/21/22

ALL

SL-051622-A

Redressal of ROTAX SL-912i-005R2 use of non-ROTAX replacement parts

Effective Date

05/16/22

ALL

SL-081221-A

Reminder: Mitigation of air contamination in engine lubrication system.

Effective Date

08/26/21

ALL

SL-070120-A

ICON is offering an upgrade to the Digital to Analogue Converter (DAC) software. This upgrade will allow for the illumination of both the “LAND AIRCRAFT” Caution Light and the “ENGINE” Warning Light on the Annunciator Panel if the engine oil pressure drops below minimum pressure. The illumination of the LAND AIRCAFT and ENGINE annunciator lights supplement the oil pressure gauge and its accompanying red LED light that illuminates when the oil pressure drops below minimum.

Effective Date

9/15/20

00001-00124

SL-042920-B

ICON has updated the bonding adhesive for the seawing tip mounting pins to a higher strength and begun to non-permanently seal/bond the seawing tip to the Seawings™.

Effective Date

07/10/2024

00001-00074

SL-042820-B

This engineering improvement is included on Aircraft Serial Number (ASN) 00075 and greater; however, we have become aware that the work instructions may not have been performed correctly on ASN 00075-00094 (inclusive). This Service Letter includes instructions on how to perform the disassembly, inspection, and proper re-installation of the sealed Seawing Tips.

Effective Date

07/16/2024

00075-00094

SL-121619-A

Optional Improvement - Removal and Replacement of Wing Hang Pins

Effective Date

1/16/20

00001, 00002, 00005, 00006, 00009, 00012, 00015, 00017, 00018, 00020, 00023-00034, 00036, 00038, 00040-00043, 00045-00047, 00049, 00050, 00052-00072, 00074, 00076-00097, 00099-00101, 00103-00108

N-042619

Handling Instructions for Aircraft Controls in High Wind Conditions

Effective Date

4/26/19

ALL

N-032119

Maintenance Manual Update

Effective Date

3/21/19

ALL

N-051316 REV A

Fuel Tank Wear

Effective Date

5/13/16

ALL