AD COMPLIANCE LIST SAAB340A 1/5

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 1-197 DC generating-system-gcu- Undervoltage protection 24-026R2,AD1-196R1 004-367 wtihtout Mod 2533 already done CW by 5 nov 2007 by replacing GCU with -007B 1-196R1 Starter generator brush SAAB 340-24-026 004-367 MRB243103 AND243101 Terminating Inspection and measurement USED LP2974 29/07/04 1-195 Inspection of the retract actuator 340-32-131 004-459 VCW iaw SB32-131 QAE bracket attachment bolt LP2596, 29-11-04 1-194 SF340A, 340B Elevator/Aileron 340-51-025 All CW 01 NOV 2003 trim tab fitting QAE W/O510045 1-193 SF340A, 340B Insp. of windshield 340-30-088 ALL CW 01 NOV 2003 wiper arm assy QAE W/O510037 US 2001-22-14 Fire extinguishing system OAS SB 22-09-97 ALL CW SB 19 MAY 2003 Bottle cartridges TELFORD 0419.033 US 2001-15-17 CTL-92 Transponder MOD ROCKWELL CTL-92 N/A BY PN KING N/A Altitude encoder inputs COLLINS #33 MST67A INSTALLED US 95-26-15R1 Various models Allied signals TPA-81A-34-84 CAS81 N/A TCAS 67 SYSTEM N/A TCAS INSTALLED COMP.LETTER28/05/04 US 94-24-10 This ad made applicable within FEEL 25-20- ALL NA BY PN N/A Swedish ad 1-094R5 1294R1 UK 017-03-93 Seats 25-20-1294R1 ALL CW TELFORD 21APR2003 N/A NA FEEL US 90-07-08R1 Ad made applicable within Swedish SELA TDS ALL N/A BY S/N TELFORD N/A ad 1-094R5 90/11980 387.004 18FEV 2003 1-021 (88-07-08) SAAB SF340A Prevention of power 340-76-018 004-078 CW V TELFORD 0419.036 28 APR2003 turbine overspeed 1-192 SF340A + 340B Models Inspection of engine mounts 340-71-059 004-459 CW TELFORD 0419.008 20 MAY 2003 1-191 SF340A + 340B MLG 340-32-130 004-459 NRWC 14791 Replacement of assistor spring AERO GEN 23 FEV 2004 1-189 SF340A, 340B Main L/G 340-32-128 004-459 CW WO QAE503026

Separation bolt harness 01 APR 2004 1-187 SF340 + 340B Modification of refuelling door 340-57-042 All CW BY 05 MAY 2005 SF340A + 340B Inspection of 1-186 MLG harness 1-184 SF340A/340B Nacelle/Pylon fire protection 340-32-127 004-459 CW TELFORD 0419.007 16 MAY 2003 340-26-029/-26-030 004-459 CW SB26-029,30 TELFORD 0419.009 15 MAY 2003 TERMINAING 1-179R1 SF340A Model Replace hydraulic pump power wires 340-29-021 REV 2 004-028 N/A BY S/N NA CTRY AD NUMBER AD SUBJECT SB REFERENCE EFFECTIVITY METHOD OF COMPLIANCE 1-176 SF340A + 340B Inspection of 340-54-043 004-459 CWSB54-043 internal structure TELFORD 0419.010 14 MAY 2003 1-173 New retract actuator bracket 340-32-124 004-459 CW SB32-124 attachment bolt TELFORD 0419.011 15 MAY 2003 1-170 Replacement of hydraulic hoses 340-29-022 004-459 CW SB29-022 TELFORD 0419.032 17 MAY 2003 1-169 Removal of DC test switches 340-24-023R2 004-379 CW SB24-023 TELFORD 0419.031 1-167 Replacement of main pitot static tubes 1-161R2 (2001-23-12R1 1-160R1 (2000-NM-420 1-156 200-23-15 Inspection of structure for removed bonding primer Installation of improved air circulation fan Insp. electrical connector at refuel panel 20 MAY 2003 340-34-145 004-459 CW SB34-145 TELFORD 0419.027 20 MAY 2003 340-51-020 004-459 CW SB 51-020 TELFORD0419.028 15 MAY 2003 340-21-039R1 004-108 CW SB21-018,033R TELFORD 0419.012 05MAY 2003 340-28-022 004-459 CW SB28-022 TELFORD0419.026 REPEAT INTERVAL TERMINAING MRB N/A

16 APR 2003 1-155 2001-06-14 Inst. of new circuit breaker for landing gear 340-32-120 004-459 CW SB32-120 018978,27 OCT 2001 1-153 Inspection of wing flap fittings 340-57-037 004-459 AD1-153 NDT ON WO 502006 AT38819 INSP. CW LAST VISUAL WO 511050QAE TERMINAL VISUAL 1-152 2000-23-19 1-151 2000-14-03 1-149 2000-12-14 1-146 2000-12-07 1-145 99-22-17 1-143 99-27-08 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 1-141 99-19-41 Modify insulation to prevent aileron interference 1-139R1 Inspection of brake Installation combinations 1-135R1 99-04-07 340-57-035 004-459 CW SB57-034 TELFORD 0419.066 NA BY PN 21 MAY 2003 340-26-023 004-459 CW SB26-023 WO127363 11 APR2002 340-92-027 004-459 CW SB92-027 WO 127361 11APR 2002 340-57-036 004-444 CW SB 57-036 TELFORD 0419.025 13 MAY 2003 340-29-009 REV 2 004-339 CWNRWC138509 AMER EAGLE21NOV2001 340-76-043 004-459 CW SB 76-043 ON 84780 CWV TELFORD 0419.067 05 MAY 2003 340-53-061 004-459 CW SB53-061 646723 18OCT 1999 LETTER 340-32-114 004-459 CW SB32-114 ON 602449 10DEC 1998 Insp. / Replace engine mounts 340-71-057R1 004-453 CW SB71-057 ON603122 04 FEV 1999 NDT DUE AT 44819 6000FL TERMINATED BY P/N53162-4 MOD REF C N/A CTRY AD NUMBER AD SUBJECT SB REFERENCE EFFECTIVITY METHOD OF COMPLIANCE 1-134 Examine nose wheels for correct 340-32-116R1 004-451 CW SB 32-116 heat treatment TELFORD 0419.030 16 APR 2003 REPEAT INTERVAL

1-133 Cold expansion of holes in horizontal stab spar 340-55-34 004-439 CW SB55-034 ON13284 01 MARS 2001 1-128 Securing of power control quadrant 340-76-042 004-439 CW SB76-042 ON654010 99-21-31 power cam screw 28 MARS 2000 1-127 Inspection of brake 340-32-114 004-439 CW SB32-114 98-22-03 Installation combinations TELFORD 0419.024 16 MAY 2003 1-119R1 Engine air intake modification 340-30-073R1 004-219, 402-459 CW SB30-73R1 ON668721 98-15-10 06 JULY 2000 1-117R1 Flaps Replacement of support 340-57-033R2 004-384, 386- CW SB57-033 ON633025, 99-04-17 strap 404, 406-408, 619284,29DEC1999, 1-116 98-08-16 1-115R1 98-20-11 1-110R2 99-19-21 1-106R1 98-09-06 1-094R5 96-25-20, 93-06-06, 94-06- 05, 95-05-03, 95-22-12, 96-08-02, 96-25- 20, 91-10-01, 91-15-15, 93-04-02, 93-14- 12, 93-24-16, 94-01-06 1-085R1 97-03-18 1-079 97-16-04 410-413 24AUG1999 Flight idle stop override knob 340-76-041 004-399 CW SB 76-041 ON526804 02 OCT 1997 LETTER 09-06-1998 Inspection of windshield wiper arm assembly 340-30-081 004-399 CW SB 30-081 127361 17 APR 2002 668722 12 JULY 2001 Horizontal stabilizer insp. 340-55-033 + 034 004-439 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 340-25-235 121, 125-360 N/A BY S/N N/A All CW TELFORD 0419.033,0419.029 18 APR 2003 340-32-107 004-378 CW SB 32-107 482922 08 MARS1997 340-26-015 004-345 CW SB26-015 532917 28 FEV 1998 TERMINAING ONE TME MRB STATUS BOARD 4000HRS N/A

1-075R1 95-22-05 1-074 96-08-06 1-072 96-25-06R1 1-070R1 96-18-03 1-067 96-17-05 1-064R1 96-03-08 1-061 94-18-05C 1-060 REV.A 94-12-02 1-057 93-25-14 1-055 93-12-02 Brake stack inspection 340-32-105 + 110 All CW SB 32-105,SB32-106 TELFORD0419.023 16 APR 2003 Stabilizer Rudder nose rib 340-55-032 004-369 CW SB 55-032 13644 19 FEV 2001 Flap fittings 340-57-027 004-379 CW SB57-027 Engine controls-flight idle stop 340-76- 032,031,034 570099 09 JUNE1998 004-379 CW SB 76-031,032,038 526804 02 OCT 1997 Engine controls beta stop 340-76-034 004-379 CW SB76-034 441681 09 MAY1996 Prop brake valve limit switch 340-61-032, -033 All N/A ACORDING TO SB6-032 SB61-033 WHEN PROP BRAKE DISCONNECTED MLG retract actuator bracket bolt 340-32-094 004-346 CWVSB32-094 TELFORD 0419.022 23 APR2003 Elevator and aileron coves 340-51-012 004-260 CW AD 51-012 346129 11 JUN1995 AC generator control relays 340-24-22 004-325 CW SB24-022 151665 24 APRIL 1993 Fuselage Protective shield 340-53-028 All CW SB 53-028 200476 07 APR 2002 N/A NEW BRAKE CTRY AD NUMBER AD SUBJECT SB REFERENCE EFFECTIVITY METHOD OF COMPLIANCE 1-054 Bleed air sensor loops 340-36-006 004-339 CW SB 36-006 93-02-09 REPEAT INTERVAL

107711 19 DEC 1992 1-052 Fuel access door 340-57-020 004-299 CW SB 57-020 92-22-13 146549 31 JAN 1993 1-050 Refuel/Defuel panel lights All CW AD 92-03-09 92-03-09 503327 20MARS 1992 1-049 REV.A Nacelle lower drag strut assembly 340-54-027R1 004-166 CW SB 54-027 92-14-01 338394 02 DEC1995 1-048 Passenger door handle 340-52-014 004-259 FCD 92-010 92-06-02 11 SEP 1992 1-047 92-03-05 Emergency lighting 340-33-030 004-179 CW SB 33-030 5033620MARS1992 1-045 92-03-11R1 Lavatory circuit breaker 340-25-181 004-169, 171-219 CW SB 25-181 248507 11 OCT 1994 1-043 Low hydraulic pressure warning 340-29-004R1 004-138 CWSB29-004R1 92-07-01 232958 21JULY 1994 1-042 Forward cowling doors 340-71-035 004-200 CW SB 71-35 91-24-06 50336 20MARS 1992 1-041 Auto pilot electrical wire size 340-34-068 079-199 NA BY NA 91-14-17 1-037 Installation of new ECU 340-77-006 004-159 COMP LETTER 23 NOV 2002 1-036 REV.A 91-14-02 Stabilizer Top closure rib 340-55-022/023 031-194 CW SB 55-023 EXPRESS AIRLINE 1-035 REV.A 90-13-04, 90-26-06 1-034 90-05-10 1-033 REV.A 90-03-03 Inspect/Rework of wing and horizontal stab 29716 26 OCT 2002 340-55-027 + 57-017 004-138 CW 151686 30APR 1993 Nacelle Drag strut bolts 340-54-026 004-166 CW SB54-026 FCD TELFORD 0419.021 19 JULY 1990 AC generators 340-24-016 All CW SB 24-016 REV1 MODD MDW /TELFORD 0419.020 TERMNATING

1-031 90-21-16 04 APR 2004 Inspection of composite structure 340-51-006 103-139 NA BY PN NA 1-030 89-23-18 1-029 89-09-04 1-027 89-03-13 1-025 89-07-04 1-024 REV.B 87-24-51R1 1-023 88-19-09 1-022 REV.E 93-19-01 1-016 REV.B 88-11-02 Modification of emer lighting activation circuit Inspection for leaks and security of air couplings 340-33-028 004-159 CW SB 33-28 TELFORD 0419.013 24 APR 2003 340-21-022 003-138 CW SB 34-056 C21550 05 DEC1988 340-34-056 004-138 CW SB34-056 FCD Installation of water traps for pitot tubes 08 APR 1989 Fuel system optical sensor bonding 340-28-006 004-106 CWV SB 28-006 TELFORD 0419.014 05FEV1989 Inspection of power control cable 340-76A-024 REV 2 All CWVSB76A024R2 TELFORD 0419.015 15 APR2003 Landing gear emer Extension explosive bolt Prop hub assemblies Inspect cabin fluorescent lighting system 340-32-041 All CWVSB32-041 TELFORD 0419.016 23 APRIL2003 DOWTYROTOL 340-61-54 All CWVSB NA BY PN TELFORD 0419.019 23 APRIL 2003 340-33-021 004-078 CWVSB33-021 TELFORD 0419.017 21 APR2003

CTRY AD NUMBER AD SUBJECT SB REFERENCE EFFECTIVITY METHOD OF REPEAT COMPLIANCE INTERVAL 1-015 REV B Flap restriction 340-27-036 004-138 MOD 1462,1784 86-06-03R1 CW IMPORT AND DEL. TELFORD 0419.018 23 APR 2003 1-014 Installation of continuous ignition 340-74-002R1 All INCORPORATED CWV 85-26-01R2 system AT DELIVERY TELFORD 0419.077 15 APR 2003 1-013 REV.A Inspect cabin fluorescent lighting 340-33-013R2 004-044 INCOPORATED AT system DELIVERY 11JUN 1986 1-010 REV.A Installation of tail deicer valve 340-30-015R1 All INCORPORATED AT 87-03-02 heater blanket DELIVERY11 JUN 1986 1-009 Engine control cable sealing 340-76-007 004-048 INCORPORATED AT 86-18-07 DELIVERY 11JUN1986 1-008 REV.A Modification of pitch trim 340-27-028 004-029 NA BY N/A 86-16-07 syncronizer 1-007 REV.E Propeller beta tube failure DOWTY 004 up with INCORPORATED AT 86-13-02 61-A1021R14 certain PN DELIVERY 11JUN1986 1-006 REV.A Rudder limiter higher speed stop 340-27-018 004-048 N/A BY S/N N/A 1-004 REV.C Cold weather MODS VARIOUS 004-048 N/A BY S/N N/A 90-17-14 1-003 GE engine MOD 340-72-003 All INCORPORATED BY MFG DELIVERY DOCUMENT 11 JUN1986 1-002 GE engine MOD 340-72-002 All INCORPORATED BY MFG DELIVERY DOCUMENT 1-001 Inspection and replacement of welded parts VARIOUS, 340-26- 001, 36-001, 71-003, 71-004, 71-005 all by Rev 1 All 11 JUN 1986 INCOPORATED BY MFG DELIVERY DOCUMENT 11 JUN 1986 Last updated : 2004-07-05 Important notices

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.