Mandatory Action Jan. 2017

Similar documents
Mandatory Action - SAFETY ALERT

SAFETY ALERT / SAFETY DIRECTIVE

Glasair Sportsman T3 Tailwheel Suspension System P/N: ABI-51526

Service Bulletin. SB-GA Issue 1. Subject: Horizontal Stabiliser Attachment Area Inspection and Reinforcement. Applicability: Amendments:

BMAA Defect Alert #0057: Light Sport Aircraft Ltd SB19 Cracking of the Rear Fuselage Bulkhead

ULTRALIGHT AIRCRAFT AIRWORTHINESS NOTICE

AVIATION INVESTIGATION REPORT A01Q0009 LOSS OF CONTROL ON TAKE-OFF

FLAP, AILERON, FLAP/FUSELAGE AND STABILATOR GAP SEAL INSTALLATION AND MAINTENANCE MANUAL

Section C75-CA-2. Elevator Controls

Airworthiness Directive Schedule

AVIATION INVESTIGATION REPORT A06O0141 LOSS OF CONTROL AND COLLISION WITH TERRAIN

June 16, 1947 OPTIONAL CHANGE SERVICE BULLETIN NO. 17 INSTALLATION STEERABLE TAIL WHEEL. (Includes Supplement 1 and Supplement 2)

Service Bulletin No.: DAC Rev 3 Date Issued: October 27, 1999 Title: 2-Speed Electric Prime Fuel Pump Page: 1 of 8

P.O. Box 3149 Albany, GA Phone (229) Fax (229) March 7, 2006 FLAP CONTROL TORQUE SHAFT REPLACEMENT

Ayres service bulletin Corporation

SERVICE BULLETIN. No. SB-AG-49 August 1, 2008 SEAT SUPPORT BRACKET INSPECTION AND REPAIR

The Subject Matter Of This Service Bulletin Is Incorporated In Whole Or In Part In An FAA Issued Airworthiness Directive

2. MODEL: F-28A, F-28C, F-28F, 280, 280C, 280F, and 280FX

A Product Line of Sonex Aircraft LLC 511 Aviation Road Oshkosh, WI Tel. (920) Fax. (920)

P.68 AND AP68TP VARIANTS SERVICE LETTER. No. 24. AIRCRAFT AFFECTED: All P.68 and AP68TP Aircraft Variants

Service Bulletin No: Ref No: 331 Modification No: EC , EC ATA Chapter: 27

LETTER. Piper Aircraft Corporation Lock Haven, Pennsylvania, U.S.A. FAA/DOA SO-1 Approved December 8, 1978 S

PLANE POWER, Ltd. CONVERSION KIT TAL24-70C

Aero Vent Cabin Ventilation System

Instructions for Continued Airworthiness

Section 75-CA-2. Elevator Controls

Hangar 6, Halfpenny Green Airport, Bobbington, Stourbridge, West Mids. DY7 5DY Tel: +44 (0) or SERVICE BULLETIN

REASON FOR REVISION: To clarify effectivity by including RAM P/N cross reference. INTRODUCTION:


Instructions for Continued Airworthiness for the Installation of the HD Extended Maule Main Gear Assembly ABI-4022X

EA Installation Manual Ignition/Starter Switch Panel For Two Magnetos

SERVICE BULLETIN. No. SB-AG-54 Revision IR; 6/6/2011 S2R-T660 ELEVATOR PUSH-PULL TUBE END FITTING INSPECTION

SERVICE BULLETIN #0001 Page 1 of 1

SERVICE LETTER. Multi-engine TITLE NACELLES/PYLONS - NACELLE FITTING INSPECTION EFFECTIVITY

Mtn View Aviation An AP Enterprises, LLC Company PO Box 31 Hubbard, OR MVA-206C10M&O. Installation Instructions

TO ALL EXEC 90 AND EXEC 162F OWNERS MANDATORY COMPLIANCE BULLETIN M-21 THIS BULLETIN IS MANDATORY AND MUST BE COMPLIED WITH

SUBJECT: Kelly Aerospace Energy Systems Service Bulletin 038 A ES TCM P/N Inspection of Slip Ring End Housings for Cracks

performance S T O L Installation Instructions Manual No. PSTOL-013 Double Slotted Flaps for Piper PA-18 Series Aircraft

Airworthiness Directive Schedule

P68 SERIES. SERVICE BULLETIN No. 115

1. SUBJECT: Replacement of the Low Point Drain Valve. 3. EFFECTIVITY: TH-28; Serial Number 3004 and 3006

2019 MICHIGAN STATE SKILLS USA CHAMPIONSHIPS TASK & MATERIALS LIST SKILL OR LEADERSHIP AREA: AVIATION MAINTENANCE TECHNOLOGY

SAMPLE BLUE STAR CONVERSION INSTALLATION OF CONTINENTAL IO-470-N BEECH MODEL J35, K35, M35 LWS C-470-N. REVISION 2. September 16, 1992 STC SA5635SW

Airworthiness Directive Schedule

GlaStar / Sportsman Service Bulletin 64- MANDATORY

Service Bulletin No: Ref No: 170 Modification No: EC ATA Chapter: 53

SERVICE BULLETIN

Cessna Main Gear Fairings

SERVICE LETTER NUMBER 173

Ican remember the day I first took

RECREATIONAL AIRCRAFT CONDITION REPORT ALL AIRCRAFT

Power Flow System Extractor Exhaust System Instructions for Continued Airworthiness PFS-13201

1 ASW 22 - Maintenance Manual - 1

SB-GA Issue 6

TO ALL EXEC, EXEC 90 AND EXEC 162F OWNERS ADVISORY BULLETIN A-43 THIS BULLETIN IS BEING ISSUED TO AMEND BULLETINS M-21 AND A-39

INSTRUCTIONS FOR CONTINUED AIRWORTHINESS AND EQUIPMENT MAINTENANCE MANUAL FOR Bell 212/ 412 CARGO NET/TROOP SEAT

SERVICE BULLETIN THIS BULLETIN IS FAA APPROVED FOR ENGINEERING DESIGN

PC-6 PILATUS AIRCRAFT LTD. CH-6371 STANS, SWITZERLAND SERVICE BULLETIN SERVICE BULLETIN NO: REF NO: 188 MODIFICATION NO: ATA CHAPTER: 53

Airglas, Inc. Instructions for Continued Airworthiness Including Installation, Maintenance and Service Instructions MANUAL NO.

Airworthiness Directive Schedule

MAIN ROTOR BLADE ABRASION STRIP DAILY INSPECTION REQUIREMENTS

AVIAT AIRCRAFT INC. P.O. Box South Washington Afton, WY USA Fax:

Section 75-ZA-3 Fin & Rudder Cable Fairing Installation

Comanche Tail Problems and Cures

Seabee Annual Inspection Procedures

AIRWORTHINESS DIRECTIVE

PILATUS AIRCRAFT LTD. CH-6371 STANS, SWITZERLAND SERVICE BULLETIN SERVICE BULLETIN NO: REF NO: 106 MODIFICATION NO: ATA CHAPTER: 28

SERVICE BULLETIN American Legend Aircraft Company considers compliance mandatory

LAA TYPE ACCEPTANCE DATA SHEET TADS 162 ZENAIR CH 601HD/HDS

TEMPORARY REVISION NUMBER

Installation Instructions

SERVICE BULLETIN. No Compliance mandatory. Inspection/Repair of Main Landing Gear Mounting Attachment

The New Piper Aircraft, Inc Piper Drive Vero Beach, Florida, U.S.A

2016 AeroLEDs LLC Rev: A Page 1

Nomad FLIGHT CONTROLS AILERONS INSPECTION AND INCORPORATION OF MOD N634. All spare ailerons with the above part numbers.

SUBJECT: Single Engine Service Bulletin SB Revision 1: Cosmetic Window Repair

COMPLIANCE: As required by Kelly Aerospace Service Bulletin 033 (Attached)

SAMPLE BLUE STAR CONVERSION INSTALLATION OF CONTINENTAL IO-470-C OR IO-470-N BEECH MODELS THROUGH F-33 LWS STC # SA5527SW REVISION 5

2016 AeroLEDs LLC Rev: A Page 1

A Product Line of Sonex Aircraft LLC 511 Aviation Road Oshkosh, WI Tel. (920) Fax. (920)

Aileron Pulley Shield ICA Supplement

BRACKETT AERO FILTERS, INC.

AIRWORTHINESS DIRECTIVE

SUBJECT: MAIN ROTOR DRIVE, ENGINE-TO- TRANSMISSION DRIVE SHAFT RETAINING NUTS INSPECTION/REPLACEMENT

MAINTENANCE RECORD (THIS FORM IS TO BE RETAINED IN THE AIRCRAFT LOG)

Airworthiness Directive Schedule

Zenair Europe Service Letter

AVIAT AIRCRAFT INC. P.O. Box South Washington Afton, WY USA Fax:

BRACKETT AERO FILTERS, INC.

500W Series Instructions for Continued Airworthiness

SíMIPLEX*,, SERVICE LETTER SL2OlO-OOl. SÍMPLEX rrrt. Mar L7,2070. on of Revision lnitial Release. AvlaClon [ülsslon Equlpment.

ABI-180/185 TAIL GEAR ASSEMBLY

American Champion Aircraft Corp. Rochester, WI 53167

BRACKETT AERO FILTERS, INC.

AVIATION INVESTIGATION REPORT A00P0208 MAIN-ROTOR BLADE FAILURE

Airworthiness Directive Schedule

TABLE of CONTENTS. PFS REV C Page 2 of 20 05/22/07

Airworthiness Directive Schedule

CHAPTER 3 LIFE-LIMITED COMPONENTS

Service Bulletin No.: DAC Rev 2 Date Issued: Oct 04, 2016 Title: Installation of LED Anti-Collision and Position light Assembly

Transcription:

Quality aircraft since 1974 Mandatory Action Jan. 2017 Issue Date January 2017, Rev. 1 Subject Inspection of the Horizontal Stabilizer tail attachment brackets Affected Models All CH (Chris Heintz designs) series of aircraft. This includes the Zodiac and STOL models. All Canadian Advanced Ultralight CH (Chris Heintz designs) series of aircraft. Compliance Time Before next flight Required Parts As required Inspection Frequency Annual (on-going) Subject/Purpose Transportation Safety Board of Canada - AVIATION SAFETY ADVISORY A16O0137-D1-A1 Zenair Zodiac CH-601A Risk of structural failure of the horizontal stabilizer Page 1 of 7

Inspection: Remove the Horizontal Stabilizer (H.S.) rear and front attachment bolts. Clean the area and inspect the parts. Look for cracks, deformation, improperly installed rivets, rivet and bolt edgedistances, material thicknesses, check that the riveted joints are fastened tightly together and everything else at the attachment brackets on the fuselage and H.S. Inside the H.S., the upper parts of the forward attachment brackets and associated rivets and holes could be viewed by shining a flashlight through the triangular cut-out which the bracket comes out of. Use the Airframe Drawings, the Design Standards manual and the assembly instructions when inspecting. If you do not have all the information, purchase it from Zenair Ltd. http://zenair.weebly.com/zenair-service-area.html If you did not assemble the airframe, hire a certified aircraft mechanic to complete the inspection. If you are not able to properly inspect inside the H.S. forward attachment brackets and associated rivets, cut out the area as shown in the following sketch. Add a cover plate after inspection as shown. Fasten into place with 18 rivets A4 around the perimeter of the cover plate. If the brackets are to be replaced, the cut out holes can be made larger. See FAA AC-43-13-1B section 4-32, Figure 4-16 when adding a covering. Page 2 of 7

Inspection continued. Above assembly drawing is for a typical CH 601 aircraft. Each CH design is different. Use your airframe model blueprints (drawings) and not the above example for inspection and installation. Page 3 of 7

Inspection continued. View of H.S. rear attachment bracket. A crack is developing in the part. Part must be replaced. View of H.S. front attachment bracket. Bolt hole was not properly drilled. Part must be replaced. Page 4 of 7

Inspection continued. Above parts must be replaced. Above part must be replaced. Page 5 of 7

Inspection continued. Above part must be replaced. The two above photos are from the same aircraft. It is possible that due to an elongated hole, the stabilator bracket cracked as the bolt was moving in the hole. Above part must be replaced. Page 6 of 7

Above photos are from a few CH 601 aircraft. Each CH design is different. Use your airframe model blueprints (drawings) and not the above examples for inspection and installation. Action: Replace parts that do not match the aircraft airframe blueprints (drawings). Replace parts that have been drilled or assembled incorrectly. The H.S. must fit snug to the fuselage fittings. Bolts when tight must not bend the H.S. fittings. Correct type rivets must be installed properly as per the design standards manual. If you did not assemble your airframe, hire a certified aircraft mechanic to complete this task. Log book entry must be made. When reinstalling, use new AN bolts and self locking bolts. Torque them as per AC 43-13 1B and 2B. Do not over tighten the bolts. Once installed, check control cable tensions, all connections, interferences, etc. See http://www.newplane.com/service_letters_bulletines/control%20cable%20tensions%20zodiac.pdf including all other continued airworthiness documentation and make sure your aircraft is up-todate before flying. When the aircraft is parked outside, lock the control cables. Strong winds can cause significant damage to the control system. For additional information contact Zenair Ltd. ZENAIR LTD, HURONIA AIRPORT, MIDLAND, ONTARIO, CANADA L4R 4K8 TEL:(705) 526-2871 - FAX:(705)526-8022 zenair.com@gmail.com Page 7 of 7