PTZ-AD 2003

Številka PTZReferenčna PTZDatum efektiveRok izvršitveProizvajalecVsebina PTZReferenčni SB
001-03 PTZFAA 2002-26-0128.2.2003 Textron Lycoming, AVCO Corporation Fuel Injected Reciprotating EnginesSupersedes AD 93-02-05 Am. 39-8487 and AD 93-02-05 Am. 39-8525 
002-03 PTZFAA 2002-26-0328.2.2003 Bracket Aircraft Company, Bracket single Screen Air FilterCheck the Brackett single screen air filter assembly for correct installation.
Install an additional screen, replace the Brackett single screen air filter assembly with a double screen filter or replace with another approved design filter at a specified time.
 
003-03 PTZAUSTRO CONTROL AD 107 R215.2.2003 Rotax 912 A, F, S, Rotax 914 FInspection for possible craks in crankcase.SB-912-029R1
SB-914-018R1
004-03 PTZFAA 2003-01-0310.2.200350-100 hours or 12 months Hartzell Propeller Inc. model ( )HC-( )2Y( )-( ) propellers with hub part numbers D-6522-1, D-6522-2, D-6529-1 and D-6559-3 with the serial numbers listed in the Table 1Remove affected hubs and replace with serviceable hubs. 
005-03 PTZFAA 2003-01-0218.2.2003 CL-600-2B19 (Regional Jet Series 100 & 440) ser.no. 7003-7480 inclusiveTo prevent false smoke warnings from the smoke detectors in the cargo compartment.CF 2001-21
006-03 PTZFAA 2002-26-2018.2.2003 Model DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and MD-88 AirplanesInspection of the disconnect panel area above the aft left lavatory for chafed or damaged wires or unacceptable clearance between the wires and adjacent structure. 
007-03 PTZDGAC 1975-052-013(A) R1  EUROCOPTER SA 341/342Cancelation of AD No. DGAC 75-52-13 (B). See AD No. DGAC 2001-587-041 (A) R2.  
076-01 R1 PTZDGAC 2001-587-041(A) R28.1.2003 EUROCOPTER SA 341/342Failure of a torsion tie bar of the main rotor head.  
008-03 PTZDGAC 2003-002(A)8.1.2003 1 monthEUROCOPTER AS 350Risk of binding in the cyclic stick "nose-up" control stop position configuration. 
009-03 PTZ  Immediately after receipt of BulletinZLINMaintenance manuale revisionMSB Z 242L/43a
010-03 PTZFAA 2003-03-157.3.2003 Various Boeing and McDonnell Douglas Transport Category AirplanesRevision  to the Airplane Flight Manual 
011-03 PTZFAA 2003-03-2011.3.2003 Hartzell Propeller Inc., Model
HC-C2YR- 4CF 
propellers, installed on Pitts S-2S and S-2B airplanes with Textron Lycoming model AEIO-540-D4A5 engines.
To prevent fatique failure of Hartzell propeller hubs and blades. 
012-03 PTZ 3.3.2003 TakojVsi zrakoplovi.Prepoved uporabe radijskih postaj s 50 kHz kanalno razdelitvijo. 
013-03 PTZ 3.3.2003 01.05.2003Vsi zrakoplovi, ki letijo v kontroliranem zračnem prostoru Republike Slovenije.Obvezna uporaba barometerskega višinomerja s prikazom v čevljih. 
014-03 PTZ 3.3.2003 TakojVsi zrakoplovi, ki letijo v kontroliranem zračnem prostoru Republike Slovenije.Opremljenost s pravilno delujočim radarskim odzivnikom-transponderjem, ki deluje v »Mode A« in »Mode C«. 
015-03 PTZ 3.3.2003 21.05.2005Vsi zrakoplovi, ki letijo v kontroliranem zračnem prostoru Belgije, Francije, Nemčije, Luksemburga, Nizozemske, Švice in Italije.Opremljenost s pravilno delujočim radarskim odzivnikom-transponderjem, ki deluje tudi v »Mode S«. 
012-03 R1 PTZ 20.3.2003 TakojVsi zrakoplovi razen jadralnih s postajami z manj kot 2W močiPrepoved uporabe radijskih postaj s 50 kHz kanalno razdelitvijo. 
013-03 R1 PTZ 20.3.2003 01.05.2003Vsi zrakoplovi razen jadralnih letal, ki letijo v kontroliranem zračnem prostoru tipa C in D Republike Slovenije. Obvezna uporaba barometerskega višinomerja s prikazom v čevljih. 
014-03 R1 PTZ PREKLICANA 20.3.2003Takoj PTZ preklicana z izdajo OTZ od 28.04.2016Vsi zrakoplovi razen jadralnih letal, ki letijo v kontroliranem zračnem prostoru tipa C in D Republike Slovenije.Opremljenost s pravilno delujočim radarskim odzivnikom-transponderjem, ki deluje v »Mode A« in »Mode C«. 
016-03 PTZCF-2003-0314.3.2003In 5000 FC or not later then 1 April 2004BOMBARDIER CL-600-2B19Landing Gear Control Handle Assembly  
017-03 PTZ (superseded)CF-2003-05R1.pdf
CF-2003-05
18.3.2003In 5000 FC or not later then 1 April 2004BOMBARDIER CL-600-2B19Air Supply Ducts 
003-03 R1 PTZAUSTRO CONTROL AD 107 R31.2.2003 Rotax 912 A, F, S, Rotax 914 FInspection for possible craks in crankcase.SB-912-029R1
SB-914-018R1
69-01 R1 PTZLBA 2001-317/49.1.2003a) Nov 2001
b) Dec 2003
ASTIR CS models:
G 102 St. Astir III
G 102 Club Astir III
G 102 Club Astir IIIb
a) Reduction of Vne
b) Increase of mass balance.
MSB 306-36/3
018-03 PTZLBA 2003-12921.3.2003Before first flightASH 25 MInspection and replacement of a fuel line<BRTechnical Note No. 22
019-03 PTZFAA 2003-04-224.4.2003Next "2A" check but not later than 600 hours time-in-service from effective date.Hartzell Propeller Inc., Model
HD-E6C-3B / E13890K
propellers.
To prevent below-limit flight idle propeller blade angles. 
020-03 PTZFAA 2003-04-0426.3.2003Within 20 hours time-in-service (TIS) and thereafter at intervals not to exceed 300 hours TIS or 12 months, whichever occours first.Robinson Helicopter Company Model R22Inspecting the tail rotor pitch control assembly 
021-03 PTZFAA 2003-04-0526.3.2003Within 20 hours time-in-service (TIS) and thereafter at intervals not to exceed 300 hours TIS or 12 months, whichever occours first.Robinson Helicopter Company Model R44Inspecting the tail rotor pitch control assembly 
022-03 PTZDGAC 2003-119(B)29.3.200329.3.2003AIRBUS A319, A320, 321Fuel leak procedure (ATA 28)  
023-03 PTZDGAC 2003-099(A)  EUROCOPTER AS 350Manufacturing fault on a set of main servocontrol rods 
024-03 PTZDGAC 2003-088(AB) Before next use.PARACHUTES DE FRANCE SA PLEXPACK emergency parachuteBad fitting of the ripcord and the triggering handle. 
073-01 R1 PTZDGAC 2001-590-087(A) R1  EUROCOPTER AS 350Cancellation of 073-01 PTZ. Refer to 023-03 PTZ 
111-02 R1 PTZDGAC 2002-104(AB) R12.3.2002 ANJOU AERONAUTIQUE safety belts and restraint system Type 343-1Repetitive visual inspection and life limits. 
112-02 R1 PTZDGAC 2002-105(AB) R12.3.2002 ANJOU AERONAUTIQUE safety belts and restraint system Type 343Repetitive visual inspection and life limits. 
025-03 PTZDGAC 2003-084(B) R112.2.2003 FALCON 2000 and MYSTERE FALCON 900 aircraftFire Protection (ATA 26) 
026-03 PTZCAA-AD-T-031/200324.3.2003Until 31.12.2003WALTER a.s.Inner liners replacementMSB No. A M601D/33a
A M601D-1/7a
A M601D-11NZ/7a
A M601E/29a
A M601E-21/7a
141-02 R1 PTZDGAC 2002-586(B) R112.4.2003700 flight hours following the effective date of this AD at original issue.AIRBUS A319, A320, 321Navigation - Pitot probes (ATA 34)  
027-03 PTZFOCA HB 2003-1994.4.2003Before further flightPILATUS B4-PC 11Control column support on frame 2 - Inspection / Replacement SB No 1005
027-03 R1 PTZFOCA HB 2003-199 R14.4.2003Before further flightPILATUS B4-PC 11Control column support on frame 2 - Inspection / Replacement SB No 1005
028-03 PTZFAA 2003-06-0229.4.2003"Next ""2A"" check but not later than 600 hours time-in-service from effective date."Hartzell Propeller Inc., Model
HC-C2Y(K,R)-1BF / F8477-4
propellers.
To prevent propeller blade separation, damage to the airplane and possible loss of the airplane. 
029-03 PTZ 19.4.2003 30.06.2003Vsi zrakoplovi v registru Republike SlovenijeUporaba knjižic zrakoplova in urejanje dokumentacije zrakoplova 
030-03 PTZ 19.4.20035 hours flight time or 01.05.2003UTVA 75Pregled nosilca motorja in vpetja krilSlike
031-03 PTZFAA 2003-09-0924.6.2003Within the compliance times specified in this AD unless the actions have olready been done.Cessna models
441 and F406
Repetetive inspection and possible replacement of the wire harness, lead wires and fuel bust pump. This amandment upersedes 
FAA AD 2002-09-13.
 
032-03 PTZENAC 2003-03210.6.2003 AGUSTA A 109EModify the electrical installation of some windshield wipers kits. 
033-03 PTZENAC 2003-1094.4.2003 AGUSTA A 109EModification of passenger compartment sliding doors installation. 
039-01 R1 PTZDGAC 2001-241(B) R126.4.2003 AIRBUS A319, A320Cancelation of DGAC 2001-241 (B)  which is replaced by DGAC 2003-147 (B)
DGAC 2001-241 (B) 
DGAC 2003-147 (B)
 
034-03 PTZDGAC 2003-146(B)26.4.2003 AIRBUS A319, A320Cracks observing  POPRAVEK:
DGAC 2003-146(B)
 
035-03 PTZDGAC 2003-147(B)26.4.2003 AIRBUS A319, A320Inspection program to verify/measure affected rivet hole interior countersinks 
072-02 R2 PTZDGAC 2002-322(A) R216.4.2003 ROBIN FIRE-RESISTANT OIL HOSE LINESReplace the oil linesAPEX AIRCRAFT
SB 020310
143-02 R1 PTZDGAC 2002-637(B) R126.4.2003 AIRBUS A319, A320, A321Passenger door - investigation of the affected girt bar 
128-02 R1 PTZDGAC 2002-556(B) R130.4.2003 AIRBUS A319, A320, A321Certified limitations - Structural parts (ATA 05) 
100-02 R1 PTZDGAC 2002-452(A) R110.5.2005 EUROCOPTER Various helicopter typesMain rotor and tail rotor dynamic components - Correction of operating hours (ATA 62, 63, 64, 65) 
111-02 R2 PTZDGAC 2002-104(AB) R22.3.2002 Safeti belts and restraint system type 343-1Inspection and replacement - Life limit  
112-02 R2 PTZDGAC 2002-105(AB) R22.3.2002 Safeti belts and restraint system type 343Inspection and replacement - Life limit  
036-03 PTZCF-2003-086.6.2003Within 14 days after effective dateBOMBARDIER CL-600-2B19Cracks on the vertical beams on pressure bulkheads at fuselage station 409+128 and 559 
037-03 PTZCF-2003-096.6.2003In 2500 FC or within 250 FC after effective dateBOMBARDIER CL-600-2B19Superseded by
CF-2003-09R1.pdf
 
038-03 PTZCAA-AD-T-100/2000 R1 Before further flightZLIN
Z 142C, 
Z 242L
Service life timeMSB No. Z 242L/27a R1 or R2
Z 242L/44a
039-03 PTZCAA-AD-T-101/2000 R1 Before further flightZLIN
Z 242L
Service life timeMSB No. Z 242L/44a
040-03 PTZFAA 2003-09-1323.6.20032500 hours TIS or within next 100 hours after effective date , whichever occurs laterPiper aircrafts
PA 23, PA 23-160, PA 23-235, PA 23-250 and PA E23-250
Inspect the flap control torque tube.
Repetetive interval not to exceed 500 hours.
Piper MSB 1051B
035-03 R1 PTZDGAC 2003-147(B) R114.5.2003 AIRBUS A319, A320Overwing emergency exit door frame corners - detailed visual inspection 
041-03 PTZNPV 00-12-0330.5.2003Po vsebini PTZUTVA 75Izvršitev obveznih servisnih biltenovObvezne modifikacije za letalo UTVA 75
SB 001,
SB 004, 
SB 005, 
SB 006, 
SB 012, 
SB 019
SB 020, 
SB 022, 
SB 024, 
SB 025, 
SB 026, 
SB 027
SB 028,
SB 029, 
SB 032, 
SB 033, 
SB 034, 
SB 035
SB 036, 
SB 037, 
SB 039, 
SB 045, 
SB 047, 
SB 049, 
SB 050
SB 052, 
SB 053, 
SB 055
SPISEK MODIFIKACIJ
042-03 PTZNPV 00-12-0330.5.2003Na prvem 100 urnem periodičnem pregleduUTVA 75Pregled komande zmesi 
043-03 PTZFAA 2003-11-1420.6.200310 hours TIS after June 20, 2003, unless already accomplishedPiper aircraft
PA 34-200T,
PA 34-220T,
PA 44-180,
PA 44-180t
Visually inspect any aircraft heater fuel pump for leaking. Correct any abnormality found.Piper dated Feb. 26, 2003
MSB 1127
044-03 PTZ  Immediately after receipt of this bulletinZLIN
Z 142C
Z 242L
Safe life timeMSB No.
Z 142C/18a R1
Z 242L/34a R1
045-03 PTZ  At operators optionZLIN
Z 142C
Safe life timeMSB No.
Z 142C/19a R1
024-01 R1 PTZCAA-AD-T-004/2001 R1 Upon receiptZLIN
Z 142C
Total safe life timeMSB No. Z 142C/27a
134-02 R1 PTZ  Prior to next aerobatic flight or within next 15 flying hoursSlingsby AviationThis Issue 2 adds repetitive and re-assembly instructionsSB 179 Issue 2
046-03 PTZCAA AD 005-03-2003
 100 hours or 3 months from receiptSlingsby aviation T67B, T67C, T67M, T67M-Mk II, T67M200, T67M260, T67M260-T3A aircraftInitial nspection for the trim panel retentio and secondly provides a positive means of fastening the forward edge of the frame 2 to 3 trim panel to the fuselage intercostals at Frame 2 position.Modification Bulletin No.
M992
047-03 PTZCAA AD 008-04-2003
 Next 50 hours inspectionSlingsby aviation T67A, T67B, T67C, T67M, T67M-Mk II, T67M200, T67M260, T67M260-T3A aircraftInspection of both the alternator wiring loom starboard side and starter loom port side of engine of correct "p" clip assemblySB 180
048-03 PTZENAC 2003-17727.6.2003 Vulcanair S.p.A. P68 all ser.No.Alternate method of compliance. This AD supersedes ENAC 1998-226 dated 10. April 2003
SB 120
102-02 R1 PTZDGAC 2002-456(B) R17.6.2003 AIRBUS A319, A320, A321APIC APU - Exhaust tailpipe (ATA 49)  
101-02 R1 PTZDGAC 2002-453(B) R121.6.2003 Auxiliary power unit - APIC APS 3200 for AIRBUS A319, A320, A321Exhaust tailpipe (ATA 49)  
049-03 PTZCF-2003-1220.6.2003When indicated unless already accomplishedBOMBARDIER CL-600-2B19Craks on the frame reinforcement angles at FS640 have been discovered.  
050-03 PTZCF-2003-1420.6.2003When indicated unless already accomplishedBOMBARDIER CL-600-2B19Wing root area wire damage.  
051-03 PTZFAA 2003-12-0517.7.2003 McCauley  Propeller Systems 1A103/TCM series propellers.Inspection for cracks 
052-03 PTZENAC 2003-21410.6.2003Within next 5 flight hoursAGUSTA A 109A, A 109AII, A 109C A 109K2, A 109EInspection of the tail rotor hub and blade assembly. 
053-03 PTZ 3.5.2003During next Major Inspection or at least before 31.12.2003Socata TB 9, TB 10, TB 200, S/N 2054,2074 to 2155, 2184Check and replace parts with inverted grain flow.EADS SOCATA
DGAC 2003-285(A)
SB 10-138
054-03 PTZ apr.03No later than 200 flight hours or 1 year, whichever occurs firstBeech Models King Air, Raytheon AircraftFuselage-wing-to-fuselage fuel quantity wiring conduit sealing modificationRaytheon Aircraft 

SB 53-3400
055-03 PTZENAC 2003-23125.7.2003As of the effective date of this AD unless already accomplished. AGUSTA A109EMain rotor head damper rod-end inspection 
056-03 PTZENAC 2003-24925.7.2003As of the effective date of this AD unless already accomplished. AGUSTA A109EMain rotor head damper rod-end inspection 
057-03 PTZENAC 2003-2564.8.2003Before first flight TECHNAM P92JInspect affected aircraft in accordance with inspection instructions of the point 1.1 of the referenced TECHNAM SB  
058-03 PTZDGAC 2003-219(A)16.6.2003 TURBOMECA
ARRIUS 2F turboshaft engine No. 34084
It has been declared unairworthy 
059-03 PTZDGAC 2003-260(A)9.7.2003Before the next flight EUROCOPTER 
AS 350
Check that the lug/angled plate assembly location meets the requirements and that the protecting sheath is not damaged 
060-03 PTZDGAC 2003-263(A)4.7.2003 PARACHUTES DE FRANCE SA
Reserve canopies TECHNO 240
Reduce TECHNO 240 parachute operational limitations 
061-03 PTZDGAC 2003-270(B)23.7.2003From the effective date of this ADAIRBUS A319, A320, A321Limitations for all flights 
062-03 PTZDGAC U2003-300(A)6.8.2003Before next use CAPEWELL parachutes metallic ripcord pinsRipcord Pin Field Test
Ripcord Pin Test for Repack
 
063-03 PTZDGAC 2003-301(A)20.8.20031. Upon receipt of this AD 
2. 01.12.2003
PARACHUTES DE FRANCE SA
Reserve canopies TECHNO 240
1. Reduce TECHNO 240 parachute operational limitations 
2. Remove and replace the slider and steering lines. Modify the canopy PN marking on the marking label. This AD replaces AD DGAC 2003-263(A) which is cancelled. 
 
064-03 PTZ 20.5.2003At operator`s option.ZLIN
Z 42, Z 42M, Z 42MU, Z 142
Replacement of non-strengthened wings by strengthened wingsMSB Z 42/46a Rev 1, Z 142/43a Rev 1
065-03 PTZ 23.5.2003At operator`s option.ZLIN
Z 42, Z 42M, Z 42MU, Z 142
1. Installation of AMU1 Acceleration Unit. 2. Accomplishment of MSB Z 42/46a Rev.1 and Z 142/43a 3. Incorporation of appropriate information into the Technical Manual. 4. Cancel MSB Z 42/47a and Z 142/44a.
Z 42/46a Rev.1 and Z 142/43a
MSB Z 42/52a, Z 142/50a
066-03 PTZCF-2000-35 R115.8.20031. Within 250 hours air time or 30 days after effective date whichever occurs first.
2. Within 5000 hours air time or at next "C" check whichever occurs later.
3. Within 20000 hours air time or before 31.12.2010 whichever occurs first
BOMBARDIER
Regional Jet Fire and Overheat Control Unit
1. Install tape on the fire and overheat control unit.
2. Inspect condition of the protective tape.
3. Replace fire and overheat control unit
 
067-03 PTZCF-2003-1831.7.2003 BOMBARDIER
CL-600-1A11 (600) Challenger
Life limited landing gear parts
Determine the number of landings 
068-03 PTZCF-2003-2029.8.2003 BOMBARDIER
CL-600-2B16 (604) Challenger
Life limited landing gear parts
Determine the number of landings 
069-03 PTZCF-2003-2124.7.2003 BOMBARDIER
CL-600-2A12 (601), CL-600-2B16 (601) (Challenger)
Life limited landing gear parts
Determine the number of landings 
070-03 PTZFAA 2003-08-0422.5.20031. 50 hours TIS
2. 500 hours TIS
EUROCOPTER
EC 120B
1. Inspect single-locking devices
2.  modifying single-locking devices to make them double locking
AD DGAC 2001-373-008(A), dated 22.08.2001 ASB 67A003, dated 02.08.2001
DGAC 2001-373-008(A)
071-03 PTZLBA 2003-23421.8.2003 Becker Flugfunkwerk GmbH, 
AR4201, AR4201-() Series VHF communication equipment
Hardware modificationBecker SB 
AR 4201-01/03
072-03 PTZLBA 2003-23821.8.2003Not later than 31.12.2003GROB,
ASTIR CS and SPEED ASTIR
Modification of the Canopy Jettison System 
073-03 PTZLBA 2003-24631.7.2003With immediate effectSchempp-Hirth,
Duo Discus
Notification of corrective measures 
073-03 R1 PTZLBA 2003-246/21.8.2003Before next flightSchempp-Hirth,
Duo Discus
Perform an inspection of the upper spar cap and the spar web 
074-03 PTZFAA 2003-14-0314.8.2003 Textron Lycoming Fuel Injected Reciprotating EnginesTorque check inspections of relief valve attaching screws  
075-03 PTZFAA 97-18-02 R131.7.2003 Hartzell propeller Inc. ( ) HC - ( ) (2,3) (X,V) ( ) - ( ) Series and HA-A2V20-1B Series Propellers with Aluminium bladesInspection 
076-03 PTZFAA 2003-13-1625.8.20036 calendar months after effective date of this ADRaytheon Aircraft Company 90, 100 and 200 Series AirplanesInspect the forward side of aft pressure bulkhead for scoring damage. Repaire if scoring damage is found. 
077-03 PTZFAA 2003-13-1718.7.2003Before further flightHartzell propeller Inc. , McCauley Propeller Systems, Sensenich Propeller Manufacturing Company Inc., and Raytheon Aircraft Company PropellersMaintenance actions that amount to an overhaul of the affected propellers. 
078-03 PTZFAA 2003-15-0117.7.2003Within the compliance times specified in this AD unless the actions have olready been done. McCauley PropellerSystems, Inc.
Prop. Hub models:
B5JFR36C1101
C5JFR36C1102
B5JFR36C1103
C5JFR36C1104
Detect cracks in the propeller blade shank that could cause a failure of the propeller blade and loss of control of the airplane. 
079-03 PTZFAA 2003-15-073.9.2003As indicated, unless olready done. Honeywell International Inc., Model RE220 (RJ) Auxiliary Power UnitThe actions specified by the AD are intended to prevent APU compartment fires and fuel vapor explosion. 
054-03 R1 PTZ July 2003As soon as possible after receipt of this SB but no later than the next 200 flight hours or one year, whichever occours first. Raytheon AircraftA fluid lead check.Raytheon Aircraft

SB 53-3400 Rev 1
080-03 PTZCF-2003-2217.9.2003As indicated unless already accomplishedBOMBARDIER CL-600-2C10 (CRJ 700)
CL-600-2D24 (CRJ 900)
Visual inspection. URGENT! 
081-03 PTZCF-2003-2317.9.2003As indicated unless already accomplishedBOMBARDIER CL-600-2C10 (CRJ 700)
CL-600-2D24 (CRJ 900)
Visual inspection.
Main landing gear door. URGENT!
 
081-03 R1 PTZCF-2003-23 R117.9.2003As indicated unless already accomplishedBOMBARDIER CL-600-2C10 (CRJ 700)
CL-600-2D24 (CRJ 900)
Visual inspection.
Main landing gear door. URGENT!
 
082-03 PTZFAA 2003-17-1021.8.2003As indicated unless already accomplishedMcCauley  Propeller SystemsInspection for cracks. This AD supersedes AD
2003-15-01
 
084-03 PTZAUSTRO CONTROL AD 11615.9.2003 Rotax 912 A, F, S, Rotax 914 FIntroduction of a new oil dipstickSB-912-040R1
SB-914-026R1
085-03 PTZAUSTRO CONTROL AD 1171.9.2003 Rotax 914 FInspection of the Exhaust Muffler.ASB-914-028R1
086-03 PTZDGAC 2000-176-004(A) R313.9.2003 Eurocopter
EC 120
CANCELLATION NOTICEDGAC 2003-325(A)
087-03 PTZDGAC 2003-325(A)13.9.2003 Eurocopter
EC 120
Crack detection inspection, remove and replace any coupling tube which has one or more cracks. 
088-03 PTZDGAC U2003-373(B)  AIRBUS
A318, A319, A320, A321, A330 and A340
MMEL REPERCUSSIONS 
054-01  R1 PTZDGAC 2001-331(B) R113.9.2003 AIRBUS
A319, A320
Identify part numbers 
089-03 PTZDGAC 2003-322(A)13.9.2003100 flight hoursEUROCOPTER
Different type of helicopters
To prevent the flight control stop screws from loosening. 
090-03 PTZCAA-AD-T-068/20033.9.2003 ZLIN
Z 42, Z 42 M,
Z 42 MU, Z 142
Total safe life timeMSB No.
Z 42/46a R1
Z 142/43a R1

Z 42/52a
Z 142/50a
091-03 PTZDGAC_2003-348(A).pdf14.2.2004Within the compliance times specified in this AD unless the actions have olready been done.APEX AIRCRAFT, DR400 aircraftMain wing spar strenghteningTechnical Instruction No. 1001047 issue H dated Maj 19. 2003
092-03 PTZDGAC_2001-570(A)_R1.pdf14.2.2004 APEX AIRCRAFT, DR 400 aircraftCANCELLATION NOTICE 
093-03 PTZDGAC_2003-325(A).pdf
DGAC_2003-325(A)popravek.pdf
14.2.2004Before next flightEUROCOPTER, EC 120 helicopterThis AD replace AD 2000-176-004(A) 
094-03 PTZDGAC_2003-394(A).pdf4.2.2004Within the compliance times specified in this ADEUROCOPTER, SA 341/342 helicoptersBy Alert TelexAlert Telex 65.63
095-03 PTZDGAC_2003-208(A).pdf7.2.2004Within 10 flight hoursEUROCOPTER, AS 350 B3Check the condition of the fuel transfer line, the condition of the air exhaust duct and the clearences in the interference area.ASB 71.00.16
096-03 PTZDGAC_2003-406(A).pdf8.11.2004Within the compliance times specified in this ADEUROCOPTER, AS 350Check wear on the lock by measuring the dimension "C" on the collective lever.ASB 67.00.27
097-03 PTZFAA_AD_98-16-17_R1.pdf23.10.2003 CESSNA Model 750 Citation X Series AirplanesDetect and correct contamination and damage in the system actuator. 
098-03-2003CF-2003-23.pdf5.2.2004Within the compliance times specified in this ADBombardier - Regional Jet 700 & 900Main landing gear door 
099-03 PTZFAA_AD_2003-21-07.pdf5.2.20045 days or 10 hours time in service since 05.02.2004, whichever occours first.Cessna A.C. Model 525 AirplanesDisengage the pitch trim circuit breaker and AP servo circuit breaker and then tie strap each of them to prevent them from being engaged. 
100-03 PTZCF-2003-23R1.pdf6.2.2004Within the compliance times specified in this ADBombardier - Regional Jet 700 & 900Main landing gear door. 
101-03 PTZDGAC_2003-368(A).pdf11.10.2003Within 300 flight hours or 12 months, whichever occours first. Repeat at 100 FH or 12 months, whichever occours first.EADS SOCATA, TB9, TB10, TB200, TB20 AND TB21 aeroplanesGimbal joint aileron and elevator control inspectionEADS_SB_10-130-27.pdf
053-02 R1 PTZDGAC_2002-225(A)_R1.pdf11.10.2003 EADS SOCATA, TB9, TB10, TB200, TB20 AND TB21 aeroplanesGimbal joint aileron inspection. Cancellation notice. 
102-03 PTZDGAC_2003-320(B).pdf22.8.20035 daysINTERNATIONAL AERO ENGINES AG, V2500-A5 turbofan enginesInspection of dual GOODRICH fuel metering unit 
103-03 PTZDGAC_2003-355(B)R1.pdf15.9.2003500 FH, no later than 31.12.2005INTERNATIONAL AERO ENGINES AG, V2500-A1 and V2500-A5 turbofan enginesFuel filter cover 
104-03 PTZDGAC_2003-373(B).pdf24.9.2003From the effective date of this ADAIRBUS, A318, A319, A320, A321, A330 and A340 aircraftTemprorary loss of all display units 
105-03 PTZDGAC_2003-390(A).pdf25.10.20035 flight hoursTB 20 and TB 21 aeroplanesMain landing gear hinged strutSB 10-139
052-02 R1 PTZDGAC_2002-220(B)R1.pdf25.10.2003Before 31.12.2004 or within 4000 FH following the effective date of this AD at its original issue, whichever occours first.AIRBUS, A319, A320 aircraftModification of fuel probes 
101-03 R1 PTZDGAC_2003-368(A)_R1.pdf25.10.2004Within the compliance times specified in this AD. Repeat at intervals not exceeding 110 FH or 14 months, whichever occours first.EADS SOCATA, TB9, TB10, TB200, TB20 AND TB21 aeroplanesGimbal joint aileron and elevator control inspectionEADS_SB_10-130-27.pdf
106-03 PTZDGAC_2003-405(A).pdf8.11.2003Within 10 FHAPEX AVIATION, DR400 aeroplanesCarburator air box assemblySB 030705 dated October 03, 2003
107-03 PTZFAA_AD_2003-24-51.pdf12.2.2004Before further flightRobinson Helicopter Company (RHC), R44 and R44 IIInspection 
031-03 R1 PTZFAA_AD_2003-09-09_R1.pdf22.1.2004Within the compliance times specified in this AD unless the actions have olready been done.Cessna, Models 441 and F406Repetetive inspection and possible replacement of the wire harness, lead wires and fuel bust pump. This amandment upersedes 
052-01 R1 PTZCF-2001-15R1.pdf17.4.2001Within the compliance times specified in this AD unless the actions have olready been done.Bombardier CL-600-2B19Inspection - Lower wing plank 
108-03 PTZFAA_AD_2003-26-14.pdf20.2.2004Within next 12 months after 20.02.2004Kidde Aerospace Part Number 898052 Hand-Held Halon Fire ExtinguishersRemove the affected fire extinguishers from service 
109-03 PTZFAA_AD_2003-24-13.doc20.1.2004Within the compliance times specified in this AD unless the actions have olready been done.Cessna A.C., Models 172R, 172S, 182S, 182T, T182T, 206H and T206H airplanesInstall and update the software 
110-03 PTZCF-2003-26.pdf
SUPERSEEDED and CANCELED by007-06 PTZ
8.12.2003Within the compliance times specified in this AD unless the actions have olready been done.Bombardier, CL-600-2B19Pitch Feel Simulator 
112-03 PTZ2000-257-149(B)R1.pdf20.12.2003 AIRBUS, A319, A320 and A321CANCELLATION NOTICE 
144-02 R1 PTZDGAC_2002-640(B)R1.pdf24.12.2004 AIRBUS, A319, A320 and A321CANCELLATION NOTICE 
104-02 R1 PTZDGAC_2003-476(B)_R1.pdf31.1.2004Before December 2007AIRBUS, A319 and A329Fuel system - Additional electrical bonding in fuel tanks 
113-03 PTZDGAC_2003-465(A).pdf22.10.2003Within the compliance times specified in this AD unless the actions have olready been done.EUROCOPTER, EC 120 helicoptersTail rotor shaft damper check 
114-03 PTZLBA_2003-409.pdf9.12.2003As specified in ADDG Flugzeugbau, DG-500MExcange of spindle drive and modification of the electrical system in accordance with the instructions given in the Service Bulletin.Technical Note 843/17 issue 2 dated 25.06.2003
115-03 PTZENAC_2003-384.pdf5.12.2003As established in BT, as of the effective date of this AD unless already accomplished.AGUSTA, A 109E helicoptersReplacement of the BATT BUS circuit braker of the emergency bus electrical instalation.Bolletino Tecnico 109 EP - 39 dated 25.11.2003
116-03 PTZENAC_2003-385.pdf5.12.2003As established in BT, as of the effective date of this AD unless already accomplished.AGUSTA, A 109E helicoptersModification of radio master switch electrical system.Bolletino Tecnico 109 EP - 40 dated 25.11.2003
034-04 PTZDGAC_F-2004-059(A).pdf28.4.2004Within 550 flying hours or 6 months (whichever occours first)EUROCOPTER, EC 120 helicoptersRotor flight controlsASB 67A011