Summary of Airworthiness Directives published by Luftfahrt-Bundesamt / Germany

Transcription

1 Summary of Airworthiness Directives published by LuftfahrtBundesamt / Germany LuftfahrtBundesamt Airworthiness Directive Section Braunschweig G E R M A N Y Tel. +49 (0) Fax +49 (0) ad@lba.de URL Aircraft: Airbus Helicopters Deutschland GmbH / MBBBK 117 German Type Certificate No.: 3049 / EASA.R.010 No. LTANr. Date of issue Effected Series Description of Problem Service Bulletins (SB) Note / all Cargo hook inadvertently release BK 117 SB No. 804 Rev.1 dated Siren SB No. 10A dated AD A1 Static longitudinal control travel stability BK 117 SB No. 404 dated A1 Control rods Incorrect labelling of control rods BK 117 AB No. BK all Main transmission gear / Correct installation of freewheel BK 117 AB No. BK 1172 dated / all Flight Control System Installation of "Stick Position Augumentation System" AD / A3 Tail rotor blades Bonding due to improper possible separation of erosion protective shell BK 117 AB No. BK 1173 Rev. 1 dated AD all Tail rotor gearbox Attachment bolts P/N LN BK 117 AB No. BK 1174 dated A1 Accessory Record List of Time Change Items (TCI), Introduction of retirement time limits BK 117 ASB No. BK dated all Check Tee Valve Possibility of a manufacturing defect BK 117 ASB No. BK dated / all Main rotor head Hex. bolts for blade connections BK 117 ASB No. BK Rev. 1 dated and Rev. 2 dated AD A1, A3 and A4 Flight Manual Procedure modification in case of chip indication in engine oil system A1, A3 and A4 General Lettering of V NE Schedule placard (Correction) BK 117 A1 and A3 Flight Manual Rev. 5 and A4 Rev. 1 dated BK 117 ASB No. BK dated Page 1 of 11

2 / all Electrical bonding / Electrostatics / Fuel System Reduction of fire hazard BK 117 ASB No. BK , 90105, and SB No. BK AD R BK117A1, A3, A4, B1, B2 and C1 Main Rotor Main Rotor (MR) Blades Inspection / ASBMBBBK , Rev. 4, dated AD R A1, A3, A4, B1, B2 and C1 Life limited parts changing life limitations and introducing new life limited parts BK 117 ASB No. BK Rev. 1 dated , No. BK and 110 both dated R A1, A3, A4, B1, B2 and C1 Failure of the vertical fin of the tail boom ASBMBBBK , Rev. 5, dated AD / R MBBBK117 A1, A3, A4, B1, B2 und C1 (ATA 63) Rotor Drive Main Rotor Mast Inspection ECD ASBMBBBK , dated or AH ASB MBBBK Rev. 1, dated AD all Main gear / main transmission Life limited parts BK 117 ASB No. BK dated September 30, R MBBBK117 A1, MBBBK 117 A3, MBBBK 117 A4, MBBBK 117 B1, MBBBK 117 B2, MBBBK 117C1 (ATA 04) Time Limits and Maintenance Checks Airworthiness Limitation Items Amendment MBBBK117 A1 bis B2 Aircraft Maintenance Manual Appendix A15 with Rev. 42a MBBBK117 C1 Aircraft Maintenance Manual Appendix A15 with Rev. 25a AD R all Fuselage Retrofit of a hook system for the doors of the transmission and engine cowlings A1 up to C1 Tail Rotor Drive of bearings in tail rotor transmission and intermediate gearbox, reduction of the inspection interval for magnetic plug A1 up to B2 and C1 Tail unit Inspection of the Wall Thickness of the Skin Panelling of the Vertical Fin A1 up to C1 Main Rotor System Introduction of a life limit for main rotor blades with bolted lead inner weights BK 117 SB No. BK , Rev. 2 dated MBBBK 117 ASB No. ASBMBBBK , dated MBBBK117 ASB No. ASBMBBBK Rev. 1, dated MBBBK117 ASB No. ASBMBBBK , dated R MBB BK 117 C1 and C2 Placards & Markings Pressure Altitude (PA) Limitation Rotorcraft Flight Manual Amendment Power Plant Engine MAX N1 Check ASBMBBBK Rev. 4, dated ASB MBB BK117 C2 71A003 Rev. 3, dated AD R MBBBK 117 C2 Fire Protection System Fire Extinguishing System Injection Tube Clamps Page 2 of 11 ASB MBB BK 117 C2 26A001, dated

3 R MBBBK 117 C2 Tail Rotor System Control Lever Inspection/ ASB MBB BK 117 C 264A002 Rev. 1, dated ASB MBB BK 117 C 264A002 Revision 2, dated AD R EC135 series, EC635 series and MBBBK 117 C2 Rotors Flight Control CyclicStick Locking Device Modification ASB EC13567A 015, dated ASB MBB BK117C 267A008, dated BO 105 A, BO 105 C, BO 105 LS A1, BO 105 D, BO 105 DS, BO 105 DB, BO 105 DBS, BO 105 DB4, BO 105 DBS4, BO 105 DBS5, BO 105 S, MBBBK 117 A1, MBBBK 117 A3, MBBBK 117 A4, MBBBK 117 B1, MBBBK 117 B2, MBBBK 117 C1 Tail Rotor Balance Weights & Control Lever Inspection / GmbH BK 117 ASB MBBBK , dated GmbH BO105 ASB BO , dated R MBBBK 117 C2 (ATA 04) Time Limits / Maintenance Checks Airworthiness Limitations Revision AHD MBB BK 117 C2 MSM Rev. 17, dated , or Rev. 18, dated ,or Rev.19, dated , or Rev. 20, dated AHD ASB MBBBK 117 C204A008, dated AD R R EC 135 P1(CDS), EC 135 P1(CPDS), EC 135 P2(CPDS), EC 135 P2+, EC 135 T1(CDS), EC 135 T1(CPDS), EC 135 T2(CPDS), EC 135 T2+, EC 635 T1(CPDS), EC 635 P2+, EC 635 T2+, MBBBK 117 C2 Optional Equipment External Mounted Hoist System Visual Check / ASB MBB BK117 C285A024 Rev. 1, dated ASB EC13585A036 Rev. 2, dated Goodrich Corporation SB Rev. 2, dated AD Page 3 of 11

4 R BO 105 A, BO 105 C, BO 105 D, BO 105 LS A1, BO 105 LS A3, BO 105 S, MBBBK 117 A1, MBBBK 117 A3, MBBBK 117 A4, MBBBK 117 B1, MBBBK 117 B2, MBBBK 117 C1 Rotors Flight Control CyclicStick Locking Device Modification Eurocopter Canada Limited ASBBO 105 LS 4010, dated ASB BO , dated ASB MBBBK , dated AD R MBBBK 117 C2 Airworthiness Limitations Tail Rotor Intermediate Gear Box (IGB) Bevel Gear Reduced Life Limit ECD ASB MBB BK117 C204A005, Rev. 02, dated AD R MBBBK 117 C2 Tail Rotor Drive Tail Rotor (T/R) Drive Shaft Inspection ASB MBB BK 177 C265A003, dated R Alle Equipment / Furnishings DLok Hook of the Rescue Hoist Inspection / Removal from Service / R MBBBK 117 C2 (ATA 67) Rotor Flight Controls Upper Control Bellcrank Assembly Modification / Inspection / FAA Airworthiness Directive Lifesaving Systems Corp. GmbH ASB MBB BK117 C267A011 Rev. 1, dated AD R2 AD R EC 135 P1(CDS), EC 135 P1(CPDS), EC 135 P2(CPDS), EC 135 P2+, EC 135 T1(CDS), EC 135 T1(CPDS), EC 135 T2(CPDS), EC 135 T2+, EC 635 T1(CPDS), EC 635 P2+, 635 T2+, MBBBK 117 C2 Rotor Flight Controls Tail Rotor, Cyclic and Collective Control Levers Inspection / Repair GmbH ASB EC13567A019 Rev. 3, dated or Rev. 4, dated ASB MBB BK117 C267A010 Rev. 3, dated AD R R AB139, AW139, S92A, MBBBK117 C2, EC 135 (ATA 25) CANCELLED: Equipment / Furnishings Spectrolab Nightsun XP Searchlight Inspection / Removal / Eurocopter UK Ltd. SB Issue A, dated SB Issue A, dated SB Issue A, dated Agusta B.T , dated Keystone Helicopter SB 1011 Rev. C, dated AD R2 Page 4 of 11

5 R EC 135 P1 (CDS), EC 135 P1 (CPDS), EC 135 P2 (CPDS), EC 135 P2+, EC 135 T1 (CDS), EC 135 T1 (CPDS), EC 135 T2 (CPDS), EC 135 T2+, EC 635 T1 (CPDS), EC 635 P2+, EC 635 T2+, MBBBK 117 C2 (ATA 31) Indicating and Recording Systems Instrument Control Panel Flight Limitation / Modification ASB EC13531A053 Rev. 2, dated ASB MBB BK 117 C231A041, Rev. 2 dated AD R EC 135 P1(CPDS), EC 135 P2(CPDS), EC 135 P2+, EC 135 T1(CPDS), EC 135 T2(CPDS), EC 135 T2+, EC 635 T1(CPDS), EC 635 P2+, EC 635 T2+, MBBBK117 C2 (ATA 33) Lights Instrument Lighting Display Brightness for Flight in Night Vision Goggle (NVG) Mode Modification ASB EC13533A009 Rev. 2, dated ASB MBB BK117 C233A013 Rev. 2, dated AD R MBBBK117 C2 Electrical Power Generator Relay After Junction Box Modification ASB MBB BK117 C224A008, Rev. 1, dated MBB BK117 C2 Rotorcraft Flight Manual TR 11, dated AD MBBBK 117 C2 Auto Flight ThreeAxisAutopilot Automatic Leveloff Function Revised Flight Manual Procedure MBBBK 117 C2 Rotor Flight Controls Main Rotor Controls Power Boosted Section Inspection / Rigging ASB MBB BK117 C222A012, dated (ECD) ASB MBB BK117 C267A012, dated MBB BK117 C2 AMM, TR 12b, dated R MBBBK 117 A3, MBBBK 117 A4, MBBBK 117 B1, MBBBK 117 B2, MBBBK 117 C1 (ATA 85) Optional Equipment External Rescue Hoist System Deactivation / Modification EASB MBB BK , Rev. 1, dated AD R1 Page 5 of 11

6 R MBBBK 117 C2 (ATA 24) Electrical Power Generator Control Unit Identification / MBBBK 117 C2 (ATA 24) Electrical Power Generator Control Unit Identification / (ECD) ASB MBB BK117 C224A008, Rev. 1, dated ASB MBB BK117 C224A010, Rev. 1, dated ASB MBB BK117 C224A010, Rev. 2, dated ASB MBB BK117 C224A006, Rev. 3, dated AD MBBBK117 A1, MBBBK117 A3, MBBBK117 A4, MBBBK117 B1, MBBBK117 B2, MBBBK117 C1 (ATA 24) Electrical Power Generator Control Unit Identification / ASB MBBBK , dated MBBBK 117 C2 (ATA 52) Doors Sliding Door Emergency Jettison System Inspection (ECD) ASB MBB BK117 C252A015, dated MBBBK117 A1, MBBBK117 A3, MBBBK117 A4, MBBBK117 B1, MBBBK117 B2, MBBBK117 C1, MBBBK117 C2, BO 105 LS A3, BO 105 LS A3 Superlifter (LBA EMZ 0654/3058 und EASA STC ) (ATA 64) Tail Rotor Pitch Links (Improperly Repaired by Able Engineering & Component Services) Inspection Able Engineering & Component Services ASB No , Rev. IR, dated MBBBK117 C2 (ATA 22) Auto Flight Autopilot Dispatch Restriction GmbH ASB MBBBK117 C222A013, dated Master Minimum Equipment List BK117 C2 (EC145) Series dated Page 6 of 11

7 R MBBBK 117 C2 (ATA 33) Lighting Flight Control Display System Wire Harness Modification EASB MBBBK117 C288A008, dated EASB MBBBK117 C288A008, Rev. 01, dated AD R AW109SP, AB139, AW139 and AB412 (all Models). BHTI Bell 212, 214 and 412 (all Models). BHTC Bell 429 and 430. AH AS 365 N3, AS 332 L2 and EC225 LP. AHD MBBBK117 C2, EC135 and EC635 (all Models). MDHI MD900. Sikorsky S61 (all Models), S76A, S76B, S76C and S92A. (ATA 25) Equipment / Furnishing Hoist Test / AHD ASB MBBBK117 C285A038, Rev. 5, dated or Rev. 6, dated ASB MBBBK117 C285A045, dated ASB EC13585A058, Rev. 6, dated or Rev. 7, dated or Rev. 8, dated ASB EC13585A064, dated AH ASB AS , Rev. 6, dated or Rev. 7, dated ASB AS , dated or Rev. 1, dated ASB AS , Rev. 6, dated or Rev. 7, dated ASB AS , dated or Rev. 1 dated ASB EC22525A133, Rev. 6, dated or Rev. 7, dated ASB EC22525A187, dated or Rev. 1, dated Finmeccanica,Helicopter Division: BT139443, dated or Rev. A, dated BT 109SP100, dated or Rev. A, dated BHTC ASB , Rev. B, dated (Ref. Goodrich ASB Rev. 5) AD R MBBBK 117 A1, A3, A4, B1, B2, C1 and C2 (ATA76) Engine Controls N2 Control Arm Inspection / Modification ASB MBBBK117 C276A005, dated ASB MBBBK11760A126, dated R MBBBK 117 A3, A4, B1 and C2 (ATA 65) Air Conditioning Drive Pulley Inspection Metro ASB MA14521B003 Rev. B, dated AD R1 Page 7 of 11

8 EC 135 P1 (CDS), EC 135 P1 (CPDS), EC 135 P2+, EC 135 P2 (CPDS), EC 135 T1 (CDS), EC 135 T1 (CPDS), EC 135 T2+, EC 135 T2 (CPDS), EC 635 P2+, EC 635 T1 (CPDS), EC 635 T2, MBBBK 117 C2 (ATA 22) Auto Flight System Longitudinal, Lateral and Yaw Actuator / Control Rod Attachment Hardware Inspection / ASB EC13522A015, dated ASB EC 13522A015, Rev. 01, dated ASB MBB BK117 C222A009, dated ASB MBB BK117 C222A009, Rev. 01, dated EC 135 AMM Rev. 10 or later MBB BK 117 C2 AMM Rev. 12 or later MBBBK 117 C2 (ATA 67) Rotor Flight Controls Lateral and Longitudinal Trim Actuator Inspection ASB MBBBK117 C 267A20, dated R MBBBK117 C2, MBBBK117 D2 (ATA 85) Optional Equipment External Rescue Hoist System Inspection / Modification AHD ASB MBBBK117 C285A041 Rev. 3, dated or Rev. 4, dated ASB MBBBK117 D285A002, dated or Rev. 1, dated AD R MBBBK117 C2 (ATA 22) Auto Flight Automatic Flight Control System Wiring Modification Rotorcraft Flight Manual Amendment AHD SIN 2659S22 Rev. 0, dated AHD SB MBBBK117 C Rev. 0, dated AHD BK117 C2 AFCS FMS 9.21 Temp. Rev R MBBBK117 A1, MBBBK117 A3, MBBBK117 A4, MBBBK117 B1, MBBBK117 B2, MBBBK117 C1, MBBBK117 C2, MBBBK117 C2e, BO105 A, BO105 C, BO105 D, BO105 S, BO105 LS A3 (ATA 62) Main Rotor Swashplate Assembly Inspection / AHD ASB MBBBK11740A115, dated or Rev. 1, dated or Rev. 2, dated or Rev. 3, dated or Rev. 4, dated ASB MBBBK117C262A007, dated or Rev. 1, dated or Rev. 2, dated or Rev. 3, dated or Rev. 4, dated ASB BO10540A107, dated or Rev. 1, dated or Rev. 2, dated or Rev. 3, dated or Rev. 4, dated BO105LS40A12, dated or Rev. 1, dated or Rev. 2, dated or Rev. 3, dated or Rev. 4, dated ASB BO105 LS A3STC0654/305840A2, dated or Rev. 1, dated AD R3 Page 8 of 11

9 R SA 365 N, SA 365 N1, AS 365 N2, AS 365 N3, EC 155 B, EC 155 B1, AS 332 C, AS 332 C1, AS 332 L, AS 332 L1, AS 332 L2, EC 225 LP, MBBBK 117 A1, MBBBK 117 A3, MBBBK 117 A4, MBBBK 117 B1, MBBBK 117 B2, MBBBK 117 C1, MBBBK 117 C2, AB 212, AB 412, AB 412EP (ATA 25) Equipment & Furnishings Emergency Flotation System Rotorcraft Flight Manual (Supplement) AD R MBBBK117 C2 (ATA 88) Wiring / Harness Hoist Control Pendant Wiring Harness Inspection / Modification AHD ASB MBBBK117 C288A009, dated MBBBK117 C2 (ATA 24) Electrical Power Terminal Lugs Inspection / AHD ASB MBBBK117 C224A013 Rev. 0, dated or Rev. 1, dated R MBBBK117 C2, MBBBK117 C2e, MBBBK117 D2, MBBBK117 D2m (ATA 62) Main Rotor Main Rotor Blade Vibration Absorber Modification AHD ASB MBBBK117 C262A009, dated or Revision 1, dated AHD ASB MBBBK117 D262A001, dated or Revision 1, dated AD R MBBBK117 A1, MBBBK117 A3, MBBBK117 A4, MBBBK117 B1, MBBBK117 B2, MBBBK117 C1 (ATA 90) Electrical Power Ground Reference Connection Retrofit / Rotorcraft Flight Manual Amendment BK117 A3 RFM, TR 9, dated BK117 A4 RFM, TR 5, dated BK117 B1 RFM, TR 6, dated BK117 B2 RFM, TR 1, dated BK117 C1C RFM, TR 1, dated BK117 C1 RFM, TR 2. Dated ECD ASBMBBBK Revision 02, dated MBBBK117 C2 (ATA 88) Wiring / Harness Collective Lever Wiring Harness Inspection AHD ASB MBBBK117 C288A010 Revision 1, dated R MBBBK117 A3 MBBBK117 A4 MBBBK117 B1 MBBBK117 B2 MBBBK117 C1 (ATA 52) Doors Jettison System Adhesive Seal Removal AHD ASB MBBBK11720A114 Revision 1, dated , or Revision 2 dated AD Page 9 of 11

10 MBBBK117 D2 (ATA 71) Power Plant Engine Mount Bushings Inspection AHD ASB MBBBK117 D271A002 dated R MBBBK117 C2, MBBBK117 C2e, MBBBK117 D2, MBBBK117 D2m (ATA 29) Hydraulic Power Plate Assembly Attachment Points Inspection / Check AHD ASB MBBBK117 C229A003, dated , or Revision 1, dated , or Revision 2, dated AHD ASB MBBBK117 D229A001, dated , or Revision 1, dated , or Revision 2, dated AD R MBBBK117 C2, MBBBK117 C2e, MBBBK117 D2, MBBBK117 D2m (ATA 21) Air Conditioning Air Inlet Cover Ring Inspection / Modification AHD ASB MBBBK117 C221A011, dated AHD ASB MBBBK117 D221A004, dated MBBBK 117 A1, MBBBK 117 A3, MBBBK 117 A4, MBBBK 117 B1, MBBBK 117 B2, MBBBK 117 C1, MBBBK 117 C2, MBBBK 117 C2e (ATA 65) Tail Rotor Drive Tail Rotor Gearbox Housing Inspection AHD ASB MBBBK11730A119, dated AHD ASB MBBBK117 C265A007, dated MBBBK117 D2 MBBBK117 D2m (ATA 63) Main Rotor Drive Rotor Mast Nut and Helical Gear Support Reidentification AH ASB MBBBK117 D263A001, dated MBBBK117 D2 MBBBK117 D2m (ATA 67) Rotors Flight Control Cable Cut Flip Guard AH ASB MBBBK117 D267A002, dated MBBBK117 C2 MBBBK117 C2e MBBBK117 D2 MBBBK117 D2m (ATA 24) Electrical Power Overhead Panel Shock Mounts AH ASB MBBBK117 C224A015, dated AH ASB MBBBK117 D224A004, dated MBBBK117 D2 (ATA 67) Rotors Flight Control Trim Actuators AH ASB MBBBK117 D267A005, dated Page 10 of 11

11 MBBBK117 D2 Rotorcraft Flight Manual Limitations Section Amendment AH BK117 D2, TR 1, dated AH BK117 D2m, TR 2, dated AH BK117 D2 (Helionix Step 2), TR 1, dated AH BK117 D2m (Helionix Step 2), TR 1, dated MBBBK117 C2 MBBBK117 D2 (ATA 25) Equipment & Furnishing Outboard Load System Inspection / AH ASB MBBBK117 C285A042, dated AH ASB MBBBK117 D285A003, dated MBBBK117 D2 (ATA) Rotorcraft Flight Manual Emergency Procedures Section Amendment END AH Flight Manual BK117 D2, TR 2, dated AH Flight Manual BK117 D2 (Helionix Step 2), TR2, dated AH Flight Manual BK117 D2m (Helionix Step 2), TR 2, dated Datum der letzten Änderung: Hinweis: Die Erstellung und Pflege der Übersichtslisten ist eine ServiceLeistung des LuftfahrtBundesamtes. Obwohl wir die Übersichtslisten mit größtmöglicher Sorgfalt bearbeiten, können wir keine Fehler ausschließen. Bitte beachten Sie, dass deshalb keine Gewährleistung hinsichtlich Richtigkeit und Vollständigkeit für diese Listen übernommen werden kann. Weiterhin ist zu beachten, dass noch weitere Lufttüchtigkeitsanweisungen, z. B. für Motor, Propeller oder andere Ausrüstung für Ihr Luftfahrzeug gelten könnten. Page 11 of 11