AD COMPLIANCE LIST SAAB340A 1/5

Transcription

1 SERIAL :057 AUDIT DATE :29 SEPT 2004 AD COMPLIANCE LIST SAAB340A 1/5 CTRY AD NUMBER AD SUBJECT SB REFERENCE EFFECTIVITY METHOD OF REPEAT COMPLIANCE INTERVAL DC generating-system-gcu- Undervoltage protection R2,AD1-196R wtihtout Mod 2533 already done CW by 5 nov 2007 by replacing GCU with -007B 1-196R1 Starter generator brush SAAB MRB AND Terminating Inspection and measurement USED LP /07/ Inspection of the retract actuator VCW iaw SB QAE bracket attachment bolt LP2596, SF340A, 340B Elevator/Aileron All CW 01 NOV 2003 trim tab fitting QAE W/O SF340A, 340B Insp. of windshield ALL CW 01 NOV 2003 wiper arm assy QAE W/O US Fire extinguishing system OAS SB ALL CW SB 19 MAY 2003 Bottle cartridges TELFORD US CTL-92 Transponder MOD ROCKWELL CTL-92 N/A BY PN KING N/A Altitude encoder inputs COLLINS #33 MST67A INSTALLED US R1 Various models Allied signals TPA-81A CAS81 N/A TCAS 67 SYSTEM N/A TCAS INSTALLED COMP.LETTER28/05/04 US This ad made applicable within FEEL ALL NA BY PN N/A Swedish ad 1-094R5 1294R1 UK Seats R1 ALL CW TELFORD 21APR2003 N/A NA FEEL US R1 Ad made applicable within Swedish SELA TDS ALL N/A BY S/N TELFORD N/A ad 1-094R5 90/ FEV ( ) SAAB SF340A Prevention of power CW V TELFORD APR2003 turbine overspeed SF340A + 340B Models Inspection of engine mounts CW TELFORD MAY SF340A + 340B MLG NRWC Replacement of assistor spring AERO GEN 23 FEV SF340A, 340B Main L/G CW WO QAE503026

2 Separation bolt harness 01 APR SF B Modification of refuelling door All CW BY 05 MAY 2005 SF340A + 340B Inspection of MLG harness SF340A/340B Nacelle/Pylon fire protection CW TELFORD MAY / CW SB26-029,30 TELFORD MAY 2003 TERMINAING 1-179R1 SF340A Model Replace hydraulic pump power wires REV N/A BY S/N NA CTRY AD NUMBER AD SUBJECT SB REFERENCE EFFECTIVITY METHOD OF COMPLIANCE SF340A + 340B Inspection of CWSB internal structure TELFORD MAY New retract actuator bracket CW SB attachment bolt TELFORD MAY Replacement of hydraulic hoses CW SB TELFORD MAY Removal of DC test switches R CW SB TELFORD Replacement of main pitot static tubes 1-161R2 ( R R1 (2000-NM Inspection of structure for removed bonding primer Installation of improved air circulation fan Insp. electrical connector at refuel panel 20 MAY CW SB TELFORD MAY CW SB TELFORD MAY R CW SB21-018,033R TELFORD MAY CW SB TELFORD REPEAT INTERVAL TERMINAING MRB N/A

3 16 APR Inst. of new circuit breaker for landing gear CW SB ,27 OCT Inspection of wing flap fittings AD1-153 NDT ON WO AT38819 INSP. CW LAST VISUAL WO QAE TERMINAL VISUAL Flap inspection, replacement of bolt and bushing Replacement of cargo compartment smoke detectors Inspection of wiring in cabin compartment ceiling Wings MLG support assembly, bearing housing NDT Introduction of new hydraulic swivel brackets Flight idle stop solenoid bracket screw Modify insulation to prevent aileron interference 1-139R1 Inspection of brake Installation combinations 1-135R CW SB TELFORD NA BY PN 21 MAY CW SB WO APR CW SB WO APR CW SB TELFORD MAY REV CWNRWC AMER EAGLE21NOV CW SB ON CWV TELFORD MAY CW SB OCT 1999 LETTER CW SB ON DEC 1998 Insp. / Replace engine mounts R CW SB ON FEV 1999 NDT DUE AT FL TERMINATED BY P/N MOD REF C N/A CTRY AD NUMBER AD SUBJECT SB REFERENCE EFFECTIVITY METHOD OF COMPLIANCE Examine nose wheels for correct R CW SB heat treatment TELFORD APR 2003 REPEAT INTERVAL

4 1-133 Cold expansion of holes in horizontal stab spar CW SB ON MARS Securing of power control quadrant CW SB ON power cam screw 28 MARS Inspection of brake CW SB Installation combinations TELFORD MAY R1 Engine air intake modification R , CW SB30-73R1 ON JULY R1 Flaps Replacement of support R , 386- CW SB ON633025, strap 404, , ,29DEC1999, R R R R , , , , , , , , , , , , R AUG1999 Flight idle stop override knob CW SB ON OCT 1997 LETTER Inspection of windshield wiper arm assembly CW SB APR JULY 2001 Horizontal stabilizer insp SUPERSEDED BY1-133 CW 02 JAN 2001 Forward lav. waste bin fire extinguisher Foreign ad s mandated applicable by LFV Sweden Anti-skid system Improved hubcap drive coupling Inspect / Modify wiring to the nacelle fire ex , N/A BY S/N N/A All CW TELFORD , APR CW SB MARS CW SB FEV 1998 TERMINAING ONE TME MRB STATUS BOARD 4000HRS N/A

5 1-075R R R R C REV.A Brake stack inspection All CW SB ,SB TELFORD APR 2003 Stabilizer Rudder nose rib CW SB FEV 2001 Flap fittings CW SB Engine controls-flight idle stop ,031, JUNE CW SB ,032, OCT 1997 Engine controls beta stop CW SB MAY1996 Prop brake valve limit switch , -033 All N/A ACORDING TO SB6-032 SB WHEN PROP BRAKE DISCONNECTED MLG retract actuator bracket bolt CWVSB TELFORD APR2003 Elevator and aileron coves CW AD JUN1995 AC generator control relays CW SB APRIL 1993 Fuselage Protective shield All CW SB APR 2002 N/A NEW BRAKE CTRY AD NUMBER AD SUBJECT SB REFERENCE EFFECTIVITY METHOD OF COMPLIANCE Bleed air sensor loops CW SB REPEAT INTERVAL

6 DEC Fuel access door CW SB JAN Refuel/Defuel panel lights All CW AD MARS REV.A Nacelle lower drag strut assembly R CW SB DEC Passenger door handle FCD SEP Emergency lighting CW SB MARS R1 Lavatory circuit breaker , CW SB OCT Low hydraulic pressure warning R CWSB29-004R JULY Forward cowling doors CW SB MARS Auto pilot electrical wire size NA BY NA Installation of new ECU COMP LETTER 23 NOV REV.A Stabilizer Top closure rib / CW SB EXPRESS AIRLINE REV.A , REV.A Inspect/Rework of wing and horizontal stab OCT CW APR 1993 Nacelle Drag strut bolts CW SB FCD TELFORD JULY 1990 AC generators All CW SB REV1 MODD MDW /TELFORD TERMNATING

7 APR 2004 Inspection of composite structure NA BY PN NA REV.B R REV.E REV.B Modification of emer lighting activation circuit Inspection for leaks and security of air couplings CW SB TELFORD APR CW SB C DEC CW SB FCD Installation of water traps for pitot tubes 08 APR 1989 Fuel system optical sensor bonding CWV SB TELFORD FEV1989 Inspection of power control cable A-024 REV 2 All CWVSB76A024R2 TELFORD APR2003 Landing gear emer Extension explosive bolt Prop hub assemblies Inspect cabin fluorescent lighting system All CWVSB TELFORD APRIL2003 DOWTYROTOL All CWVSB NA BY PN TELFORD APRIL CWVSB TELFORD APR2003

8 CTRY AD NUMBER AD SUBJECT SB REFERENCE EFFECTIVITY METHOD OF REPEAT COMPLIANCE INTERVAL REV B Flap restriction MOD 1462, R1 CW IMPORT AND DEL. TELFORD APR Installation of continuous ignition R1 All INCORPORATED CWV R2 system AT DELIVERY TELFORD APR REV.A Inspect cabin fluorescent lighting R INCOPORATED AT system DELIVERY 11JUN REV.A Installation of tail deicer valve R1 All INCORPORATED AT heater blanket DELIVERY11 JUN Engine control cable sealing INCORPORATED AT DELIVERY 11JUN REV.A Modification of pitch trim NA BY N/A syncronizer REV.E Propeller beta tube failure DOWTY 004 up with INCORPORATED AT A1021R14 certain PN DELIVERY 11JUN REV.A Rudder limiter higher speed stop N/A BY S/N N/A REV.C Cold weather MODS VARIOUS N/A BY S/N N/A GE engine MOD All INCORPORATED BY MFG DELIVERY DOCUMENT 11 JUN GE engine MOD All INCORPORATED BY MFG DELIVERY DOCUMENT Inspection and replacement of welded parts VARIOUS, , , , , all by Rev 1 All 11 JUN 1986 INCOPORATED BY MFG DELIVERY DOCUMENT 11 JUN 1986 Last updated : Important notices

9 Note: Shaded areas represent equivalent related USAD`s this is mostly used for import purposes and are for reference only all AD`s recognized by Transport Canada must be signed off according to the primary AD and it`s related SB.