Številka PTZ | Referenčna PTZ | Datum efektive | Rok izvršitve | Proizvajalec | Vsebina PTZ | Referenčni SB |
001-03 PTZ | FAA 2002-26-01 | 28.2.2003 | | Textron Lycoming, AVCO Corporation Fuel Injected Reciprotating Engines | Supersedes AD 93-02-05 Am. 39-8487 and AD 93-02-05 Am. 39-8525 | |
002-03 PTZ | FAA 2002-26-03 | 28.2.2003 | | Bracket Aircraft Company, Bracket single Screen Air Filter | Check 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 PTZ | AUSTRO CONTROL AD 107 R2 | 15.2.2003 | | Rotax 912 A, F, S, Rotax 914 F | Inspection for possible craks in crankcase. | SB-912-029R1
SB-914-018R1 |
004-03 PTZ | FAA 2003-01-03 | 10.2.2003 | 50-100 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 1 | Remove affected hubs and replace with serviceable hubs. | |
005-03 PTZ | FAA 2003-01-02 | 18.2.2003 | | CL-600-2B19 (Regional Jet Series 100 & 440) ser.no. 7003-7480 inclusive | To prevent false smoke warnings from the smoke detectors in the cargo compartment. | CF 2001-21 |
006-03 PTZ | FAA 2002-26-20 | 18.2.2003 | | Model DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and MD-88 Airplanes | Inspection 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 PTZ | DGAC 1975-052-013(A) R1 | | | EUROCOPTER SA 341/342 | Cancelation of AD No. DGAC 75-52-13 (B). See AD No. DGAC 2001-587-041 (A) R2. | |
076-01 R1 PTZ | DGAC 2001-587-041(A) R2 | 8.1.2003 | | EUROCOPTER SA 341/342 | Failure of a torsion tie bar of the main rotor head. | |
008-03 PTZ | DGAC 2003-002(A) | 8.1.2003 | 1 month | EUROCOPTER AS 350 | Risk of binding in the cyclic stick "nose-up" control stop position configuration. | |
009-03 PTZ | | | Immediately after receipt of Bulletin | ZLIN | Maintenance manuale revision | MSB Z 242L/43a |
010-03 PTZ | FAA 2003-03-15 | 7.3.2003 | | Various Boeing and McDonnell Douglas Transport Category Airplanes | Revision to the Airplane Flight Manual | |
011-03 PTZ | FAA 2003-03-20 | 11.3.2003 | | 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 | Takoj | Vsi zrakoplovi. | Prepoved uporabe radijskih postaj s 50 kHz kanalno razdelitvijo. | |
013-03 PTZ | | 3.3.2003 | 01.05.2003 | Vsi zrakoplovi, ki letijo v kontroliranem zračnem prostoru Republike Slovenije. | Obvezna uporaba barometerskega višinomerja s prikazom v čevljih. | |
014-03 PTZ | | 3.3.2003 | Takoj | Vsi 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 | 21.05.2005 | Vsi zrakoplovi, ki letijo v kontroliranem zračnem prostoru Belgije, Francije, Nemčije, Luksemburga, Nizozemske, vice in Italije. | Opremljenost s pravilno delujočim radarskim odzivnikom-transponderjem, ki deluje tudi v »Mode S«. | |
012-03 R1 PTZ | | 20.3.2003 | Takoj | Vsi zrakoplovi razen jadralnih s postajami z manj kot 2W moči | Prepoved uporabe radijskih postaj s 50 kHz kanalno razdelitvijo. | |
013-03 R1 PTZ | | 20.3.2003 | 01.05.2003 | Vsi 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 | | 20.3.2003 | Takoj | Vsi 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 PTZ | CF-2003-03 | 14.3.2003 | In 5000 FC or not later then 1 April 2004 | BOMBARDIER CL-600-2B19 | Landing Gear Control Handle Assembly | |
017-03 PTZ (superseded) | CF-2003-05R1.pdf
CF-2003-05 | 18.3.2003 | In 5000 FC or not later then 1 April 2004 | BOMBARDIER CL-600-2B19 | Air Supply Ducts | |
003-03 R1 PTZ | AUSTRO CONTROL AD 107 R3 | 1.2.2003 | | Rotax 912 A, F, S, Rotax 914 F | Inspection for possible craks in crankcase. | SB-912-029R1
SB-914-018R1 |
69-01 R1 PTZ | LBA 2001-317/4 | 9.1.2003 | a) 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 PTZ | LBA 2003-129 | 21.3.2003 | Before first flight | ASH 25 M | Inspection and replacement of a fuel line<BR | Technical Note No. 22 |
019-03 PTZ | FAA 2003-04-22 | 4.4.2003 | Next "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 PTZ | FAA 2003-04-04 | 26.3.2003 | Within 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 R22 | Inspecting the tail rotor pitch control assembly | |
021-03 PTZ | FAA 2003-04-05 | 26.3.2003 | Within 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 R44 | Inspecting the tail rotor pitch control assembly | |
022-03 PTZ | DGAC 2003-119(B) | 29.3.2003 | 29.3.2003 | AIRBUS A319, A320, 321 | Fuel leak procedure (ATA 28) | |
023-03 PTZ | DGAC 2003-099(A) | | | EUROCOPTER AS 350 | Manufacturing fault on a set of main servocontrol rods | |
024-03 PTZ | DGAC 2003-088(AB) | | Before next use. | PARACHUTES DE FRANCE SA PLEXPACK emergency parachute | Bad fitting of the ripcord and the triggering handle. | |
073-01 R1 PTZ | DGAC 2001-590-087(A) R1 | | | EUROCOPTER AS 350 | Cancellation of 073-01 PTZ. Refer to 023-03 PTZ | |
111-02 R1 PTZ | DGAC 2002-104(AB) R1 | 2.3.2002 | | ANJOU AERONAUTIQUE safety belts and restraint system Type 343-1 | Repetitive visual inspection and life limits. | |
112-02 R1 PTZ | DGAC 2002-105(AB) R1 | 2.3.2002 | | ANJOU AERONAUTIQUE safety belts and restraint system Type 343 | Repetitive visual inspection and life limits. | |
025-03 PTZ | DGAC 2003-084(B) R1 | 12.2.2003 | | FALCON 2000 and MYSTERE FALCON 900 aircraft | Fire Protection (ATA 26) | |
026-03 PTZ | CAA-AD-T-031/2003 | 24.3.2003 | Until 31.12.2003 | WALTER a.s. | Inner liners replacement | MSB No. A M601D/33a
A M601D-1/7a
A M601D-11NZ/7a
A M601E/29a
A M601E-21/7a |
141-02 R1 PTZ | DGAC 2002-586(B) R1 | 12.4.2003 | 700 flight hours following the effective date of this AD at original issue. | AIRBUS A319, A320, 321 | Navigation - Pitot probes (ATA 34) | |
027-03 PTZ | FOCA HB 2003-199 | 4.4.2003 | Before further flight | PILATUS B4-PC 11 | Control column support on frame 2 - Inspection / Replacement | SB No 1005 |
027-03 R1 PTZ | FOCA HB 2003-199 R1 | 4.4.2003 | Before further flight | PILATUS B4-PC 11 | Control column support on frame 2 - Inspection / Replacement | SB No 1005 |
028-03 PTZ | FAA 2003-06-02 | 29.4.2003 | "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 | 30.06.2003 | Vsi zrakoplovi v registru Republike Slovenije | Uporaba knjižic zrakoplova in urejanje dokumentacije zrakoplova | |
030-03 PTZ | | 19.4.2003 | 5 hours flight time or 01.05.2003 | UTVA 75 | Pregled nosilca motorja in vpetja kril | Slike |
031-03 PTZ | FAA 2003-09-09 | 24.6.2003 | Within 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 PTZ | ENAC 2003-032 | 10.6.2003 | | AGUSTA A 109E | Modify the electrical installation of some windshield wipers kits. | |
033-03 PTZ | ENAC 2003-109 | 4.4.2003 | | AGUSTA A 109E | Modification of passenger compartment sliding doors installation. | |
039-01 R1 PTZ | DGAC 2001-241(B) R1 | 26.4.2003 | | AIRBUS A319, A320 | Cancelation of DGAC 2001-241 (B) which is replaced by DGAC 2003-147 (B)
DGAC 2001-241 (B)
DGAC 2003-147 (B) | |
034-03 PTZ | DGAC 2003-146(B) | 26.4.2003 | | AIRBUS A319, A320 | Cracks observing POPRAVEK:
DGAC 2003-146(B) | |
035-03 PTZ | DGAC 2003-147(B) | 26.4.2003 | | AIRBUS A319, A320 | Inspection program to verify/measure affected rivet hole interior countersinks | |
072-02 R2 PTZ | DGAC 2002-322(A) R2 | 16.4.2003 | | ROBIN FIRE-RESISTANT OIL HOSE LINES | Replace the oil lines | APEX AIRCRAFT
SB 020310 |
143-02 R1 PTZ | DGAC 2002-637(B) R1 | 26.4.2003 | | AIRBUS A319, A320, A321 | Passenger door - investigation of the affected girt bar | |
128-02 R1 PTZ | DGAC 2002-556(B) R1 | 30.4.2003 | | AIRBUS A319, A320, A321 | Certified limitations - Structural parts (ATA 05) | |
100-02 R1 PTZ | DGAC 2002-452(A) R1 | 10.5.2005 | | EUROCOPTER Various helicopter types | Main rotor and tail rotor dynamic components - Correction of operating hours (ATA 62, 63, 64, 65) | |
111-02 R2 PTZ | DGAC 2002-104(AB) R2 | 2.3.2002 | | Safeti belts and restraint system type 343-1 | Inspection and replacement - Life limit | |
112-02 R2 PTZ | DGAC 2002-105(AB) R2 | 2.3.2002 | | Safeti belts and restraint system type 343 | Inspection and replacement - Life limit | |
036-03 PTZ | CF-2003-08 | 6.6.2003 | Within 14 days after effective date | BOMBARDIER CL-600-2B19 | Cracks on the vertical beams on pressure bulkheads at fuselage station 409+128 and 559 | |
037-03 PTZ | CF-2003-09 | 6.6.2003 | In 2500 FC or within 250 FC after effective date | BOMBARDIER CL-600-2B19 | Superseded by
CF-2003-09R1.pdf | |
038-03 PTZ | CAA-AD-T-100/2000 R1 | | Before further flight | ZLIN
Z 142C,
Z 242L | Service life time | MSB No. Z 242L/27a R1 or R2
Z 242L/44a |
039-03 PTZ | CAA-AD-T-101/2000 R1 | | Before further flight | ZLIN
Z 242L | Service life time | MSB No. Z 242L/44a |
040-03 PTZ | FAA 2003-09-13 | 23.6.2003 | 2500 hours TIS or within next 100 hours after effective date , whichever occurs later | Piper 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 PTZ | DGAC 2003-147(B) R1 | 14.5.2003 | | AIRBUS A319, A320 | Overwing emergency exit door frame corners - detailed visual inspection | |
041-03 PTZ | NPV 00-12-03 | 30.5.2003 | Po vsebini PTZ | UTVA 75 | Izvršitev obveznih servisnih biltenov | Obvezne 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 PTZ | NPV 00-12-03 | 30.5.2003 | Na prvem 100 urnem periodičnem pregledu | UTVA 75 | Pregled komande zmesi | |
043-03 PTZ | FAA 2003-11-14 | 20.6.2003 | 10 hours TIS after June 20, 2003, unless already accomplished | Piper 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 bulletin | ZLIN
Z 142C
Z 242L | Safe life time | MSB No.
Z 142C/18a R1
Z 242L/34a R1 |
045-03 PTZ | | | At operators option | ZLIN
Z 142C | Safe life time | MSB No.
Z 142C/19a R1 |
024-01 R1 PTZ | CAA-AD-T-004/2001 R1 | | Upon receipt | ZLIN
Z 142C | Total safe life time | MSB No. Z 142C/27a |
134-02 R1 PTZ | | | Prior to next aerobatic flight or within next 15 flying hours | Slingsby Aviation | This Issue 2 adds repetitive and re-assembly instructions | SB 179 Issue 2 |
046-03 PTZ | CAA AD 005-03-2003
| | 100 hours or 3 months from receipt | Slingsby aviation T67B, T67C, T67M, T67M-Mk II, T67M200, T67M260, T67M260-T3A aircraft | Initial 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 PTZ | CAA AD 008-04-2003
| | Next 50 hours inspection | Slingsby aviation T67A, T67B, T67C, T67M, T67M-Mk II, T67M200, T67M260, T67M260-T3A aircraft | Inspection of both the alternator wiring loom starboard side and starter loom port side of engine of correct "p" clip assembly | SB 180 |
048-03 PTZ | ENAC 2003-177 | 27.6.2003 | | 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 PTZ | DGAC 2002-456(B) R1 | 7.6.2003 | | AIRBUS A319, A320, A321 | APIC APU - Exhaust tailpipe (ATA 49) | |
101-02 R1 PTZ | DGAC 2002-453(B) R1 | 21.6.2003 | | Auxiliary power unit - APIC APS 3200 for AIRBUS A319, A320, A321 | Exhaust tailpipe (ATA 49) | |
049-03 PTZ | CF-2003-12 | 20.6.2003 | When indicated unless already accomplished | BOMBARDIER CL-600-2B19 | Craks on the frame reinforcement angles at FS640 have been discovered. | |
050-03 PTZ | CF-2003-14 | 20.6.2003 | When indicated unless already accomplished | BOMBARDIER CL-600-2B19 | Wing root area wire damage. | |
051-03 PTZ | FAA 2003-12-05 | 17.7.2003 | | McCauley Propeller Systems 1A103/TCM series propellers. | Inspection for cracks | |
052-03 PTZ | ENAC 2003-214 | 10.6.2003 | Within next 5 flight hours | AGUSTA A 109A, A 109AII, A 109C A 109K2, A 109E | Inspection of the tail rotor hub and blade assembly. | |
053-03 PTZ | | 3.5.2003 | During next Major Inspection or at least before 31.12.2003 | Socata TB 9, TB 10, TB 200, S/N 2054,2074 to 2155, 2184 | Check and replace parts with inverted grain flow. | EADS SOCATA
DGAC 2003-285(A)
SB 10-138 |
054-03 PTZ | | apr.03 | No later than 200 flight hours or 1 year, whichever occurs first | Beech Models King Air, Raytheon Aircraft | Fuselage-wing-to-fuselage fuel quantity wiring conduit sealing modification | Raytheon Aircraft
SB 53-3400 |
055-03 PTZ | ENAC 2003-231 | 25.7.2003 | As of the effective date of this AD unless already accomplished. | AGUSTA A109E | Main rotor head damper rod-end inspection | |
056-03 PTZ | ENAC 2003-249 | 25.7.2003 | As of the effective date of this AD unless already accomplished. | AGUSTA A109E | Main rotor head damper rod-end inspection | |
057-03 PTZ | ENAC 2003-256 | 4.8.2003 | Before first flight | TECHNAM P92J | Inspect affected aircraft in accordance with inspection instructions of the point 1.1 of the referenced TECHNAM SB | |
058-03 PTZ | DGAC 2003-219(A) | 16.6.2003 | | TURBOMECA
ARRIUS 2F turboshaft engine No. 34084 | It has been declared unairworthy | |
059-03 PTZ | DGAC 2003-260(A) | 9.7.2003 | Before 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 PTZ | DGAC 2003-263(A) | 4.7.2003 | | PARACHUTES DE FRANCE SA
Reserve canopies TECHNO 240 | Reduce TECHNO 240 parachute operational limitations | |
061-03 PTZ | DGAC 2003-270(B) | 23.7.2003 | From the effective date of this AD | AIRBUS A319, A320, A321 | Limitations for all flights | |
062-03 PTZ | DGAC U2003-300(A) | 6.8.2003 | Before next use | CAPEWELL parachutes metallic ripcord pins | Ripcord Pin Field Test
Ripcord Pin Test for Repack | |
063-03 PTZ | DGAC 2003-301(A) | 20.8.2003 | 1. 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 | | 20.5.2003 | At operator`s option. | ZLIN
Z 42, Z 42M, Z 42MU, Z 142 | Replacement of non-strengthened wings by strengthened wings | MSB Z 42/46a Rev 1, Z 142/43a Rev 1 |
065-03 PTZ | | 23.5.2003 | At 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 PTZ | CF-2000-35 R1 | 15.8.2003 | 1. 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 PTZ | CF-2003-18 | 31.7.2003 | | BOMBARDIER
CL-600-1A11 (600) Challenger
Life limited landing gear parts | Determine the number of landings | |
068-03 PTZ | CF-2003-20 | 29.8.2003 | | BOMBARDIER
CL-600-2B16 (604) Challenger
Life limited landing gear parts | Determine the number of landings | |
069-03 PTZ | CF-2003-21 | 24.7.2003 | | BOMBARDIER
CL-600-2A12 (601), CL-600-2B16 (601) (Challenger)
Life limited landing gear parts | Determine the number of landings | |
070-03 PTZ | FAA 2003-08-04 | 22.5.2003 | 1. 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 PTZ | LBA 2003-234 | 21.8.2003 | | Becker Flugfunkwerk GmbH,
AR4201, AR4201-() Series VHF communication equipment | Hardware modification | Becker SB
AR 4201-01/03 |
072-03 PTZ | LBA 2003-238 | 21.8.2003 | Not later than 31.12.2003 | GROB,
ASTIR CS and SPEED ASTIR | Modification of the Canopy Jettison System | |
073-03 PTZ | LBA 2003-246 | 31.7.2003 | With immediate effect | Schempp-Hirth,
Duo Discus | Notification of corrective measures | |
073-03 R1 PTZ | LBA 2003-246/2 | 1.8.2003 | Before next flight | Schempp-Hirth,
Duo Discus | Perform an inspection of the upper spar cap and the spar web | |
074-03 PTZ | FAA 2003-14-03 | 14.8.2003 | | Textron Lycoming Fuel Injected Reciprotating Engines | Torque check inspections of relief valve attaching screws | |
075-03 PTZ | FAA 97-18-02 R1 | 31.7.2003 | | Hartzell propeller Inc. ( ) HC - ( ) (2,3) (X,V) ( ) - ( ) Series and HA-A2V20-1B Series Propellers with Aluminium blades | Inspection | |
076-03 PTZ | FAA 2003-13-16 | 25.8.2003 | 6 calendar months after effective date of this AD | Raytheon Aircraft Company 90, 100 and 200 Series Airplanes | Inspect the forward side of aft pressure bulkhead for scoring damage. Repaire if scoring damage is found. | |
077-03 PTZ | FAA 2003-13-17 | 18.7.2003 | Before further flight | Hartzell propeller Inc. , McCauley Propeller Systems, Sensenich Propeller Manufacturing Company Inc., and Raytheon Aircraft Company Propellers | Maintenance actions that amount to an overhaul of the affected propellers. | |
078-03 PTZ | FAA 2003-15-01 | 17.7.2003 | Within 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 PTZ | FAA 2003-15-07 | 3.9.2003 | As indicated, unless olready done. | Honeywell International Inc., Model RE220 (RJ) Auxiliary Power Unit | The actions specified by the AD are intended to prevent APU compartment fires and fuel vapor explosion. | |
054-03 R1 PTZ | | July 2003 | As soon as possible after receipt of this SB but no later than the next 200 flight hours or one year, whichever occours first. | Raytheon Aircraft | A fluid lead check. | Raytheon Aircraft
SB 53-3400 Rev 1 |
080-03 PTZ | CF-2003-22 | 17.9.2003 | As indicated unless already accomplished | BOMBARDIER CL-600-2C10 (CRJ 700)
CL-600-2D24 (CRJ 900) | Visual inspection. URGENT! | |
081-03 PTZ | CF-2003-23 | 17.9.2003 | As indicated unless already accomplished | BOMBARDIER CL-600-2C10 (CRJ 700)
CL-600-2D24 (CRJ 900) | Visual inspection.
Main landing gear door. URGENT! | |
081-03 R1 PTZ | CF-2003-23 R1 | 17.9.2003 | As indicated unless already accomplished | BOMBARDIER CL-600-2C10 (CRJ 700)
CL-600-2D24 (CRJ 900) | Visual inspection.
Main landing gear door. URGENT! | |
082-03 PTZ | FAA 2003-17-10 | 21.8.2003 | As indicated unless already accomplished | McCauley Propeller Systems | Inspection for cracks. This AD supersedes AD
2003-15-01 | |
084-03 PTZ | AUSTRO CONTROL AD 116 | 15.9.2003 | | Rotax 912 A, F, S, Rotax 914 F | Introduction of a new oil dipstick | SB-912-040R1
SB-914-026R1 |
085-03 PTZ | AUSTRO CONTROL AD 117 | 1.9.2003 | | Rotax 914 F | Inspection of the Exhaust Muffler. | ASB-914-028R1 |
086-03 PTZ | DGAC 2000-176-004(A) R3 | 13.9.2003 | | Eurocopter
EC 120 | CANCELLATION NOTICE | DGAC 2003-325(A) |
087-03 PTZ | DGAC 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 PTZ | DGAC U2003-373(B) | | | AIRBUS
A318, A319, A320, A321, A330 and A340 | MMEL REPERCUSSIONS | |
054-01 R1 PTZ | DGAC 2001-331(B) R1 | 13.9.2003 | | AIRBUS
A319, A320 | Identify part numbers | |
089-03 PTZ | DGAC 2003-322(A) | 13.9.2003 | 100 flight hours | EUROCOPTER
Different type of helicopters | To prevent the flight control stop screws from loosening. | |
090-03 PTZ | CAA-AD-T-068/2003 | 3.9.2003 | | ZLIN
Z 42, Z 42 M,
Z 42 MU, Z 142 | Total safe life time | MSB No.
Z 42/46a R1
Z 142/43a R1
Z 42/52a
Z 142/50a |
091-03 PTZ | DGAC_2003-348(A).pdf | 14.2.2004 | Within the compliance times specified in this AD unless the actions have olready been done. | APEX AIRCRAFT, DR400 aircraft | Main wing spar strenghtening | Technical Instruction No. 1001047 issue H dated Maj 19. 2003 |
092-03 PTZ | DGAC_2001-570(A)_R1.pdf | 14.2.2004 | | APEX AIRCRAFT, DR 400 aircraft | CANCELLATION NOTICE | |
093-03 PTZ | DGAC_2003-325(A).pdf
DGAC_2003-325(A)popravek.pdf | 14.2.2004 | Before next flight | EUROCOPTER, EC 120 helicopter | This AD replace AD 2000-176-004(A) | |
094-03 PTZ | DGAC_2003-394(A).pdf | 4.2.2004 | Within the compliance times specified in this AD | EUROCOPTER, SA 341/342 helicopters | By Alert Telex | Alert Telex 65.63 |
095-03 PTZ | DGAC_2003-208(A).pdf | 7.2.2004 | Within 10 flight hours | EUROCOPTER, AS 350 B3 | Check 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 PTZ | DGAC_2003-406(A).pdf | 8.11.2004 | Within the compliance times specified in this AD | EUROCOPTER, AS 350 | Check wear on the lock by measuring the dimension "C" on the collective lever. | ASB 67.00.27 |
097-03 PTZ | FAA_AD_98-16-17_R1.pdf | 23.10.2003 | | CESSNA Model 750 Citation X Series Airplanes | Detect and correct contamination and damage in the system actuator. | |
098-03-2003 | CF-2003-23.pdf | 5.2.2004 | Within the compliance times specified in this AD | Bombardier - Regional Jet 700 & 900 | Main landing gear door | |
099-03 PTZ | FAA_AD_2003-21-07.pdf | 5.2.2004 | 5 days or 10 hours time in service since 05.02.2004, whichever occours first. | Cessna A.C. Model 525 Airplanes | Disengage 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 PTZ | CF-2003-23R1.pdf | 6.2.2004 | Within the compliance times specified in this AD | Bombardier - Regional Jet 700 & 900 | Main landing gear door. | |
101-03 PTZ | DGAC_2003-368(A).pdf | 11.10.2003 | Within 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 aeroplanes | Gimbal joint aileron and elevator control inspection | EADS_SB_10-130-27.pdf |
053-02 R1 PTZ | DGAC_2002-225(A)_R1.pdf | 11.10.2003 | | EADS SOCATA, TB9, TB10, TB200, TB20 AND TB21 aeroplanes | Gimbal joint aileron inspection. Cancellation notice. | |
102-03 PTZ | DGAC_2003-320(B).pdf | 22.8.2003 | 5 days | INTERNATIONAL AERO ENGINES AG, V2500-A5 turbofan engines | Inspection of dual GOODRICH fuel metering unit | |
103-03 PTZ | DGAC_2003-355(B)R1.pdf | 15.9.2003 | 500 FH, no later than 31.12.2005 | INTERNATIONAL AERO ENGINES AG, V2500-A1 and V2500-A5 turbofan engines | Fuel filter cover | |
104-03 PTZ | DGAC_2003-373(B).pdf | 24.9.2003 | From the effective date of this AD | AIRBUS, A318, A319, A320, A321, A330 and A340 aircraft | Temprorary loss of all display units | |
105-03 PTZ | DGAC_2003-390(A).pdf | 25.10.2003 | 5 flight hours | TB 20 and TB 21 aeroplanes | Main landing gear hinged strut | SB 10-139 |
052-02 R1 PTZ | DGAC_2002-220(B)R1.pdf | 25.10.2003 | Before 31.12.2004 or within 4000 FH following the effective date of this AD at its original issue, whichever occours first. | AIRBUS, A319, A320 aircraft | Modification of fuel probes | |
101-03 R1 PTZ | DGAC_2003-368(A)_R1.pdf | 25.10.2004 | Within 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 aeroplanes | Gimbal joint aileron and elevator control inspection | EADS_SB_10-130-27.pdf |
106-03 PTZ | DGAC_2003-405(A).pdf | 8.11.2003 | Within 10 FH | APEX AVIATION, DR400 aeroplanes | Carburator air box assembly | SB 030705 dated October 03, 2003 |
107-03 PTZ | FAA_AD_2003-24-51.pdf | 12.2.2004 | Before further flight | Robinson Helicopter Company (RHC), R44 and R44 II | Inspection | |
031-03 R1 PTZ | FAA_AD_2003-09-09_R1.pdf | 22.1.2004 | Within 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 | |
052-01 R1 PTZ | CF-2001-15R1.pdf | 17.4.2001 | Within the compliance times specified in this AD unless the actions have olready been done. | Bombardier CL-600-2B19 | Inspection - Lower wing plank | |
108-03 PTZ | FAA_AD_2003-26-14.pdf | 20.2.2004 | Within next 12 months after 20.02.2004 | Kidde Aerospace Part Number 898052 Hand-Held Halon Fire Extinguishers | Remove the affected fire extinguishers from service | |
109-03 PTZ | FAA_AD_2003-24-13.doc | 20.1.2004 | Within 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 airplanes | Install and update the software | |
110-03 PTZ | CF-2003-26.pdf
SUPERSEEDED and CANCELED by007-06 PTZ | 8.12.2003 | Within the compliance times specified in this AD unless the actions have olready been done. | Bombardier, CL-600-2B19 | Pitch Feel Simulator | |
112-03 PTZ | 2000-257-149(B)R1.pdf | 20.12.2003 | | AIRBUS, A319, A320 and A321 | CANCELLATION NOTICE | |
144-02 R1 PTZ | DGAC_2002-640(B)R1.pdf | 24.12.2004 | | AIRBUS, A319, A320 and A321 | CANCELLATION NOTICE | |
104-02 R1 PTZ | DGAC_2003-476(B)_R1.pdf | 31.1.2004 | Before December 2007 | AIRBUS, A319 and A329 | Fuel system - Additional electrical bonding in fuel tanks | |
113-03 PTZ | DGAC_2003-465(A).pdf | 22.10.2003 | Within the compliance times specified in this AD unless the actions have olready been done. | EUROCOPTER, EC 120 helicopters | Tail rotor shaft damper check | |
114-03 PTZ | LBA_2003-409.pdf | 9.12.2003 | As specified in AD | DG Flugzeugbau, DG-500M | Excange 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 PTZ | ENAC_2003-384.pdf | 5.12.2003 | As established in BT, as of the effective date of this AD unless already accomplished. | AGUSTA, A 109E helicopters | Replacement of the BATT BUS circuit braker of the emergency bus electrical instalation. | Bolletino Tecnico 109 EP - 39 dated 25.11.2003 |
116-03 PTZ | ENAC_2003-385.pdf | 5.12.2003 | As established in BT, as of the effective date of this AD unless already accomplished. | AGUSTA, A 109E helicopters | Modification of radio master switch electrical system. | Bolletino Tecnico 109 EP - 40 dated 25.11.2003 |
034-04 PTZ | DGAC_F-2004-059(A).pdf | 28.4.2004 | Within 550 flying hours or 6 months (whichever occours first) | EUROCOPTER, EC 120 helicopters | Rotor flight controls | ASB 67A011 |
