Service Information: Moravan
There will be over 135,000 documents in our Service Information Indexes. If the SB that you need is not yet a link (or is not listed), Contact Us. Please mention the AD No. in your message.
Most SBs are displayed in PDF format. (Use your Browser's 'Edit | Find' function to locate an SB by number.)
| Name | Revision | Lang | Subject | Date |
|---|---|---|---|---|
| SB Z42/36 | en | Mandatory All Manufactured Airplanes Z42M, Z42MU, Z142, Z142C and Z242L | 04/06/1994 | |
| SB Z42/46a | 1 | en | Mandatory Increasing of Safe Life Time of the ZLIN Z42, Z42M, Z42MU and Z142 Aircraft | 05/20/2003 |
| SB Z42/52a | en | Mandatory Determination of Aircraft Individual Safe Life Limit Based on Analysis of Data from AMU1 Acceleration Registration Unit | 05/23/2003 | |
| SB Z50/37a | en | Mandatory Sporadically Occured Failure of the Rudder Control Cable | 06/06/1996 | |
| SB Z50M-08a | en | Mandatory Sporadically Occured Failure of the Rudder Control Cable | 06/06/1996 | |
| SB Z142/30 | en | Mandatory All Manufactured Airplanes Z42M, Z42MU, Z142, Z142C and Z242L | 04/06/1994 | |
| SB Z142/43a | 1 | en | Mandatory Increasing of Safe Life Time of the ZLIN Z42, Z42M, Z42MU and Z142 Aircraft | 05/20/2003 |
| SB Z142/48a | en | Mandatory Production End of PND, PN, CSN 63 5388 and CSN 63 5387 Rubber Hoses for Manufacturing of Low-Pressure and High-Pressure Hose Assemblies Used on Z142 Aircraft | 02/25/2002 | |
| SB Z142/50a | en | Mandatory Determination of Aircraft Individual Safe Life Limit Based on Analysis of Data from AMU1 Acceleration Registration Unit | 05/23/2003 | |
| SB Z142C/1 | en | Mandatory All Manufactured Airplanes Z42M, Z42MU, Z142, Z142C and Z242L | 04/06/1994 | |
| SB Z142C/3 | en | Mandatory Airplanes Z142C, Prouction Nos. 0542-0550 Airplanes Z242L, Productions No. 0540, 0541, 0651-0657 | 06/29/1993 | |
| SB Z142C/4a | en | Mandatory The Z142C Aircraft Serial No. 525, Serial No. 0542 through Serial No. 0550 | 12/06/1993 | |
| SB Z142C/6a | en | Mandatory Provision of the Airplane with the Alternate Static Source L 242.8259, which Conforms with the Applicable Requirements of FAR 23.1325 | 04/28/1994 | |
| SB Z142C/7a | en | Mandatory At the Extreme Deflection of the Nose-Wheel Steering the Screw of the Spring-Mechanism L242.4217 May Interfere with the Nose-Wheel Strut Body | 05/17/1994 | |
| SB Z142C/11a | en | Mandatory During the Operation Some Cases of Loosening the Fire Extinguisher from the Holder Occured | 02/08/1996 | |
| SB Z142C/17a | 1 | en | Mandatory New Limits for Acrobatic Operation for Z142C and Z242L Aircraft | 10/31/2000 |
| SB Z142C/18a | 1 | en | Mandatory Precise Definition of Safe Life Time of the ZLIN Z 142C and Z 242L Aircraft | 04/15/2003 |
| SB Z142C/19a | 1 | en | Mandatory Increasing of Safe Life Time of the ZLIN Z142C Aircraft | 04/15/2003 |
| SB Z142C/24a | en | Mandatory Unification of Flight Manuals of the Z142C Aircraft's Validity for Aircrafts to 16 Series and from 17 Series Including into the One Manual | 01/31/2002 | |
| SB Z142C/25a | en | Mandatory Time Limitations Canceling (1500 Flight Hours) of the Main Clamping Bolts, Connecting the Fuselage Rear Parts and Fuselage Shell Unification of Maintenance Manual, Vol 1 of the Z142C Aircraft's Validity for Aircrafts to 16 Series and from 17 Series Including into the One Manual | 09/25/2002 | |
| SB Z142C/27a | en | Mandatory Determination of Individual Safe Life Limit of Z142C Aircraft Based on Analysis of Data from AMU1 Acceleration Registration Unit | 04/23/2003 | |
| SB Z143L/4a | en | Mandatory During the Operation Some Cases of Loosening the Fire Extinguisher from the Holder Occured | 02/08/1996 | |
| SB Z143L/26a | en | Mandatory 3.1. Change of the Fuel Low Level Measuring from S/N 0053 Inclusive 3.2. Check List Supplementing with S-TEC System 55 Autopilot Inspection | 07/09/2002 | |
| SB Z242/5 | en | Mandatory The Correct Function of the L242-1510-03.00 Bushing May be Inadversely affected by the Dimensional Tolerances of Parts | 07/26/1993 | |
| SB Z242L/03 | en | Mandatory Alternation of Engine Speed Indicator Colour Identification According to Service Bulletin 369/I of the Company Lycoming and Putting Interpretation of FAR 23.1549 by Civil Aviation Inspection More Precise | 04/16/1993 | |
| SB Z242L/2 | en | Mandatory All Manufactured Airplanes Z42M, Z42MU, Z142, Z142C and Z242L | 04/06/1994 | |
| SB Z242L/4 | en | Mandatory All Z242L Aircraft Up to Serial No. 659 | 04/30/1993 | |
| SB Z242L/6 | en | Mandatory Airplanes Z142C, Prouction Nos. 0542-0550 Airplanes Z242L, Productions No. 0540, 0541, 0651-0657 | 06/29/1993 | |
| SB Z242L/8a | en | Mandatory Cracks Occurence and Breaking - Off the Elastic Strip which Attaches the Flexible Control Rod of the Porpeller Governor | 04/26/1994 | |
| SB Z242L/11a | en | Mandatory At the Extreme Deflection of the Nose-Wheel Steering the Screw of the Spring-Mechanism L242.4217 May Interfere with the Nose-Wheel Strut Body | 05/17/1994 | |
| SB Z242L/13a | 1 | en | Mandatory Results of the Review of the Rigging Measurements and the In-Flight Checks of the Z242L and Z142C Fleet | 04/30/1995 |
| SB Z242L/15a | en | Mandatory Cranks on the Exhaust Muffler First Chamber Faces (Part/No. L242.6671-01.00) | 04/20/1995 | |
| SB Z242L/17a | en | Mandatory When Handling the Auxiliary Tank Cap, the Wire Lockring on the Auxiliary Ttank Filler Flap can Loosen | 08/08/1995 | |
| SB Z242L/22a | en | Mandatory Under the Influence of the Cotter Pin Wear and Corrosion the Porpeller RPM Control System as well as Control System of the Throttle and the Mixture of the Cooling Flap if Installed | 05/24/1996 | |
| SB Z242L/27a | 2 | en | Mandatory Increasing of Safe Life Time of the ZLIN Z 242L Aircraft | 04/15/2003 |
| SB Z242L/37a | 1 | en | Mandatory New Limits for Acrobatic Operation for Z142C and Z242L Aircraft | 10/31/2000 |
| SB Z242L/38a | 1 | en | Mandatory Precise Definition of Safe Life Time of the ZLIN Z 142C and Z 242L Aircraft | 04/15/2003 |
| SB Z242L/41a | en | Mandatory In the Supplements No. 3 of the Z242L Aircraft Flight Manual was Implementation within the Engine Check the Missing of Adjustment of Propeller | 02/26/2002 | |
| SB Z242L/42a | en | Mandatory Possibility of Tube Loosing in "Tee" Assembly, P/N L242.7100-06.00 or L242.7600-06.00 and in "Elbow" Assembly, P/N L242.7100-05.00 in Aircraft Oil System | 10/07/2002 | |
| SB Z242L/44a | en | Mandatory Determination of Individual Safe Life Limit of Z242L Aircraft Based on Analysis of Data from AMU1 Acceleration Registration Unit | 04/23/2003 | |
| SB Z242L/49a | en | Mandatory Acceleration Monitoring Unit | 02/15/2007 | |
| SB Z326/81 | en | Mandatory When Exceeding Repeatedly Prescribed Airspeeds and Load Factors During Maneuvers, the Awelding Point Failure can Occurred in the Front Leveling Point Area | 07/30/1987 | |
| SB Z526/62 | en | Mandatory When Exceeding Repeatedly Prescribed Airspeeds and Load Factors During Maneuvers, the Awelding Point Failure can Occurred in the Front Leveling Point Area | 07/30/1987 | |
| SB Z726/15 | en | Mandatory When Exceeding Repeatedly Prescribed Airspeeds and Load Factors During Maneuvers, the Awelding Point Failure can Occurred in the Front Leveling Point Area | 07/30/1987 |