CommutAir. DHC 8-Q311 - MSN N837CA - Maintenance History AIRWORTHINESS DIRECTIVES - APPLIANCES STATUS REPORT Nov-17 8-Nov-17 Directives
|
|
- Dina Cole
- 5 years ago
- Views:
Transcription
1 To prevent loss of attitude/heading reference information 14/07/1986 Amendment Applies to Sperry Corporation AHZ-600 Attitude Heading Reference System (AHRS), known to be installed in, but not limited to, DeHavilland Model DHC-8, British Aerospace Model BAe , Cessna Model 650, and Aerospatiale Model ATR-42 series airplanes, certificated in any category. Modify the Sperry Corporation AH-600 Strapdown Attitude and Heading Reference Unit (AHRU) by incorporating modifications in accordance with the following Sperry Service Bulletins or later revisions approved by the Manager, Western Aircraft Certification Office, FAA, Northwest Mountain Region: , dated April 7, 1986 (Modification T); , dated April 7, 1986 (Modifications S & V); , dated April 7, 1986 (Modification U); , dated April 22, 1986 (Modification Z); , dated April 22, 1986 (Modification AA); and , dated April 22, 1986 (Modification AB). N/A by Mod To reduce the possibility of AHRS attitude and heading computations being contaminated, which can result in frozen attitude and heading displays on both instrument panels, accomplish the following 13/03/1987 Applicable to the following models of Sperry Electronics Flight Instrument Systems (EFIS) Symbol Generators, which have not been modified to Mod Level S or subsequent: MODEL SPERRY PART NUMBER SG SG SG A. Prior to fiirther flight, install a placard adjacent to the first pilot's electronic attitude direction indicator (EADI), in full view of the pilot, stating "FLIGHT INTO KNOWN IMC PROHIBITED." B. Modification of the Sperry EFIS Symbol Generator models listed above to Mod Level S or subsequent, or installation of the following Sperry EFIS Symbol Generator models, constitutes terminating action of the operational and placard requirements of paragraph A., above: MODEL SPERRY PART NUMBERS MOD LEVEL (OR SUBSEQUENT) SG V SG AD SG U SG S B. Modification of the Sperry EFIS Symbol Generator models listed above to Mod Level S or subsequent, or installation of the following Sperry EFIS Symbol Generator models, constitutes terminating action of the operational and placard requirements of paragraph A., above: MODEL SPERRY PART NUMBERS MOD LEVEL (OR SUBSEQUENT) SG V SG AD SG U SG S N/A by Part Number 1 of 11 11/8/2017
2 Honeywell Attitude & heading system 05/02/1990 Honeywell AH-600 Attitude and Heading Reference System (AHRS) Strapdown Attitude and Heading Reference Unit (AHRU), part numbers , - 932, -933, -934, -935, and -936, with serial numbers 0100 through Within 10 days after January 9, 1989 (the effective date of Amendment ), inspect airplanes with Honeywell AH-600 AHRS installed to determine the part number, serial number, and Mod Level of the strapdown AHRU installed in the pilot s (Number 1) AHRS. Prior to further flight after inspection, remove all AHRU part numbers , -932, -933, -934, -935, and -936 with serial numbers 0100 through 0277, without Mod Level F", from service in the pilot's (Number 1) AHRS. Install the same part number with Mod Level "F" incorporated, or modify the AHRU in accordance with Honeywell Inc., Service Bulletin , dated August 2, Within 60 calendar days after the effective date of this amendment, inspect airplanes with Honeywell AH-600 AHRS installed to determine the part number, serial number, and Mod Level of the strapdown AHRU installed in copilot's (Number 2) AHRS and the auxiliary (Number 3) AHRS. Within 45 days after the inspection, remove all AHRU part numbers , -932, - 933, -934, -935, and -936, with serial numbers 0100 through 0277, without Mod Level "F", from service in the copilot's (Number 2) AHRS and the auxiliaiy (Number 3) AHRS. Install the same part number with Mod Level "F" incorporated, or modify the AHRU in accordance with Honeywell, Inc., Service Bulletin , dated August 2, N/A by Part Number Honeywell vertical gyro 30/03/1990 Within 60 days after the effective date of this AD, inspect the Model VG-14A vertical gyros to determine the serial number. 1. If the vertical gyros have serial numbers listed in Table 1 of Honeywell Alert Service Bulletin , Revision 1, dated November 20, 1989, and have the letter "D" marked out on the modification status plate, no further action is Honeywell Model VG-14A vertical gyro, required, and the airplane may be returned to part number , with serial service. numbers listed in Honeywell Alert 2. If the vertical gyros have serial numbers listed Service Bulletin , Revision 1, in Table 1 of Honeywell Alert Service Bulletin 21- dated November 20, , Revision 1, dated November 20, 1989, and do not have the letter "D" marked out on the modification status plate, prior to further flight, remove the gyro, replace the liquid levels, test, and verify operation, in accordance with the procedures specified in paragraph 2., Accomplishment Instructions, of the service bulletin. N/A, NO Vertical Gyro installed in aircraft. AHRS and STBY Gyro only 2 of 11 11/8/2017
3 Rockwell transponders 26/03/1993 TDR-94D Mode S transponders, P/N CPN Within the next 10 calendar days after the , installed on, but not effective date of this AD, fabricate a placard with limited to the following, certificated in the following words in letters at least 0.10-inch any category: Aerospatiale ATR-42 and in height and install this placard within the pilot's ATR-72 series airplanes Saab 340A and clear view on the instrument panel: "OPERATION 340B airplanes Short Model SD3-60 OF TCAS II IN ANY MODE OTHER THAN THE "TA airplanes de Havilland DHC-7 and DHC-8 ONLY" MODE IS PROHIBITED." series airplanes British Aerospace ATP (b) Within the next 6 calendar months after the airplanes Gulfstream G-ll, G-lll, and G-IV effective date of this AD, modify the software of series airplanes Dassault Mystere-Falcon the Mode S transponders in accordance with the 50, Mystere-Falcon 200, and Mystere- Accomplishment Instructions section of Collins Falcon 900 airplanes Canadair Challenger Service Bulletin TDR-94/94D-34-6, Revision 2, CL-601 airplanes British Aerospace HS dated September 21, The placard required A airplanes by paragraph (a) of this AD is no longer required Beechcraft 300 series airplanes after this modification is incorporated. N/A due to Part Number. Parts Number installed on aircraft Rockwell TCAS 04/02/1994 Traffic Alert and Collision Avoidance System II processors that are installed on, but not limited to the following airplanes (all serial numbers), certificated in any category: General Aviation Airplanes: Astra Model 1125 airplanes; BAC Model 1-11 airplanes; British Aerospace Model airplanes; Beech Models C90A, B200, 300, 350, and 400A airplanes; Canadair Models CL-600, CL-600-2B16, CL-601, CL A, and CL-601-3A airplanes; Learjet Models 31, 55, and 60 airplanes; Falcon Models 20, 50,200, and 900 airplanes Gulfstream Models G2 and G3 airplanes; British Aerospace Models HS airplanes; and Sabreliner Model 60 airplanes. Air Transport Airplanes: Aerospatiale Models ATR-42 and ATR-72 airplanes; Airbus Industries Models A300B2, A-300B, and A-320 airplanes; British Aerospace Models ATP and 146 airplanes; Boeing Models 707, 727, 737, 747, 757, and 767 airplanes; British Aerospace/Aerospatiale Model Concorde SST airplanes; de Havilland DHC-7 and DHC-8 series airplanes; McDonnell Douglas Models DC-8, DC-9, and DC-10, MD-80, and MD-11 airplanes; Ilyushin Model IL-86 airplanes; Lockheed Model L-1011 airplanes; SAAB Models SF340A and SF340B airplanes; and Shorts Models SD airplanes. Prior to December 31, 1994, unless already accomplished. To prevent collisions or near misses caused by incompatibility between the traffic alert and collision avoidance system (TCAS) II processors and the current air traffic control system, accomplish the following: (a) Incorporate "Change 6.04A Enhanced" by accomplishing either (1) or (2) below, as applicable: (1) Remove any TCAS II processor with a part number (P/N) suffix listed in the "Existing P/N Suffix" column of the table below, and install a corresponding TCAS II processor with a P/N listed in the "New P/N Suffix" column of the table below: Existing P/N Suffix New P/N Suffix -001,-002,-011, , or ,- 111, or NOTE 1: Collins SB No. 16, TTR , dated December 9, 1993, specifies procedures for incorporating the referenced New P/N suffixes. (2) Change the part number of the TCAS II unit on board the aircraft by reprogramming the software with a data loader in order to obtain the New P/N Suffix as specified in the following table: Existing P/N Suffix New P/N Suffix NOTE 2: Units with P/N suffix of -001, -002, -011, - 102, -111, and -612 cannot be reprogrammed on board the aircraft. N/A by STC ST00844WI-D installing TCAS II change 7. 3 of 11 11/8/2017
4 Lap Belt Assemblies and Restraint Systems Prevent compressor wheel rupture 11/25/ /01/1997 Lap belt assemblies and restraint systems, as listed in Pacific Scientific SB , and Pacific Scientific SB ; as installed on aircraft and rotorcraft Sundstrand Aerospace SB No. SB-T-62T , Revision 2, dated November 5, 1996 Sundstrand Aerospace SB No. SB-T- 62T , Revision 1, dated September 9, 1996 Sundstrand Aerospace SB No. SB-T-62T , dated July 22, 1996 Within 90 days after the effective date of this AD, remove the applicable lap belt assemblies and restraint systems, and replace them with new design assemblies in accordance with Pacific Scientific SB , or Pacific Scientific SB , as applicable. Remove from service compressor wheels in accordance with the procedures described in the Accomplishment Instructions of Sundstrand Aerospace Service Bulletin (SB) No. SB-T-62T , Revision 2, dated November 5, 1996, Revision 1, dated September 9, 1996, or Original, dated July 22, 1996, and the drawdown schedule described in Table 2 of Revision 2 only, dated November 5, 1996, and replace with serviceable parts. (b) This AD establishes a new life limit of 6,000 cycles for existing uninstalled compressor wheels, identified as Sundstrand P/Ns , , and Pacific Scientific SB or Pacific Scientific SB Accomplishment Instructions of Sundstrand Aerospace Service Bulletin (SB) No. SB-T-62T , Revision 2, dated November 5, 1996, Revision 1, dated September 9, 1996, or Original, dated July 22, 1996 N/A due Pacific Scientific not installed on aircraft. N/A due to Part Number of Compressor Wheel Fire extinguisher bottle cartridge 07/03/1997 Within 30 days after the effective date of this Fire extinguisher bottle cartridges AD, accomplish the following: (squibs) having part numbers (P/N) (1) Pull the applicable circuit breakers and and -25; as installed in, but not disconnect the electrical connector from any limited to, the following airplane models, Pacific Scientific Company, HTL/Kin-Tech certificated in any category: Division, fire extinguisher bottle cartridge (squib) de Havilland Model DHC-7 series having P/N or CAUTION: airplanes; Prior to removing the electrical connector from de Havilland Model DHC and -300 the fire extinguisher bottle cartridge, ensure that series airplanes; the technician is grounded properly. Cartridges General Dynamics Convair Model 340, are electrostatic discharge (ESD) sensitive. 440, and C-131 (military) series airplanes (2) Perform a one-time visual inspection of the modified in accordance with electrical receptacle of the cartridge and its Supplemental Certificate SA41100; mating connector to detect the presence of Lockheed Model 382 series airplanes; aluminum foil in the area of the pins of the and cartridge and the connector. The aluminum foil Sabreliner Model NA , -65, and - may have the appearance of solder. Remove any 75A series airplanes. aluminum foil that is present. Complied with Ex Factory by Tyrolean records. 4 of 11 11/8/2017
5 Prevent such erroneous altitude interpretations 20/08/2001 This AD applies to CTL-92 transponder control panel part numbers , , , 622- (1) Modify the altitude encoder inputs of the CTL , and (serial 92 transponder control panels. Within the next numbers as specified in Rockwell Collins 10 hours time-in- service (TIS) after August 20, Service Bulletin 33 (CTL ), dated 2001 (the effective date of this AD). Modify in April 2001), that are installed in aircraft. accordance with the Accomplishment These CTL-92 transponder control panels Instructions section of Rockwell Collins Service are installed in, but not limited to, the Bulletin 33 (CTL ), dated April5, following aircraft that are certificated in (2) Do not install, on any aircraft, an affected CTLany category: 92 transponder control panel that has not been (1) Aerospatiale ATR42 and ATR72 series modified as required by paragraph (d)(1) of this airplanes; AD. As of August 20, 2001 (the effective date of (2) Saab Aircraft Models 340B and this AD). Modify in accordance with the SF340A airplanes; Accomplishment Instructions section of Rockwell (3) Embraer EMB-120 series airplanes; Collins Service Bulletin 33 (CTL ), dated (4) dehavilland DHC-8 series airplanes; April5, and (5) Raytheon Models C90A, B200, 350, and 1900D airplanes. Part Number installed is N/A by S/B CTL Prevent erroneous altitude resolutions 03/05/2002 This AD applies to TDR-94 Mode S transponders (Collins part number (CPN) ) and TDR-94D Mode S transponders (CPN ) that derive altitude information from a Gillham (gray code) encoded pressure altitude source and are installed on, but not limited to, the following airplanes that are certificated in any category: (1) Aerospatiale ATR42 series airplanes; (2) dehavilland DHC-7 and DHC-8 series airplanes; and (3) Short Brothers Models SD3-60 and SD3-60 SHERPA airplanes. Determine whether the altitude information from any TDR-94 Mode S transponder (CPN ) or TDR-94D Mode S transponder (CPN ) is derived from a digital air data source or a Gillham (gray code) encoded source. Accomplish the modification in accordance with Rockwell Collins Service Bulletin No. 17 (TDR- 94/94D ), dated February 8,1999, Service Bulletin 17, Revision No. 1, dated May 15, 2000, or Service Bulletin 20 (TDR- 94/94D-34-20), Revision No. 1, dated May 2, Collins Product Information Letter No. 71, dated January 1999, references Service Bulletin 17, dated February 8,1999. N/A by Part Number. Part Number To prevent overfueling of the APU during the start sequence 11/20/09 Hamilton Sundstrand Power Systems T- 62T-46C12 auxiliary power units (APUs) At the next FADEC removal, but no later than 18 months after the effective date of this AD, upgrade the software in the APU FADEC from software version to version , and change the FADEC part number (P/N) from E to F. (g) Use paragraphs 3. A through 3.F.(2) of the Accomplishment Instructions of Hamilton Sundstrand Power Systems Service Bulletin No , Revision 2, dated March 9,2009, to do the software upgrade and the FADEC P/N change N/A by Model Number. APU APS500/T-62-T-40C7B/ A installed on aircraft 5 of 11 11/8/2017
6 Protective Breathing Equipment (PBE) 9/2/11 B/E Aerospace protective breathing equipment (PBE) units having part number (P/N) These PBE units may be installed on (or carried or stowed on board), various transport category airplanes, certificated in any category. Within 120 days after the effective date of this AD, inspect to determine the serial number of the PBE units installed in the aircraft, in accordance with the Accomplishment Instructions of B/E Aerospace Service Bulletin (1) For any PBE that has a serial number from M to M inclusive: Before further flight, replace the PBE with a serviceable PBE, except as provided by paragraph (g)(2) of this AD. (2) For any PBE that has a label showing that it has been restored in accordance with B/E Aerospace Service Bulletin : The replacement has been done, and no further action is required by paragraph (g) of this AD. (3) For any PBE not having a serial number from M to M inclusive: No further action is required by paragraph (g) of this AD. B/E Aerospace Service Bulletin B/E Aerospace PBE not installed in Aircraft. ESSEX PB&R CORPORATION PBE Installed. Part Number MR10049N. 6 of 11 11/8/2017
7 Sicma Aero Seat 88xx, 89xx, 90xx, 91xx, 92xx, 93xx, 95xx, and 96xx series passenger seat assemblies 11/23/11 (f) Unless already done, do the following actions. (1) At the later of the compliance times specified in paragraphs (f)(1)(i) and (f)(1)(ii) of this AD, do a general visual inspection of the backrest links having P/Ns and , in accordance with Part One of Sicma Aero Seat Service Bulletin , Issue 4, dated March 19, 2004, including Annex 1, Issue 2, dated March 19, 2004: This AD applies to Sicma Aero Seat 88xx, (i) Before 6,000 flight hours on the backrest link 89xx, 90xx, 91xx, 92xx, 93xx, 95xx, and since new. 96xx series passenger seat assemblies (ii) Within 900 flight hours or 5 months after the identified in Annex 1, Issue 2, dated effective date of this AD, whichever occurs March 19, 2004, of Sicma Aero later. Seat Service Bulletin , Issue 4, (2) If, during the inspection required by dated March 19, 2004, that have paragraph (f)(1) of this AD, cracking is found backrest links having part numbers between the side of the backrest link and the (P/Ns) and lock-out pin hole but the cracking does not pass 104-2; and that are installed on, but not this lock-out pin hole (refer to Figure 2 of Sicma limited to, Aero Seat Service Bulletin , Issue 4, the airplanes identified in table 1 of this dated March 19,2004, including Annex 1, Issue 2, AD, certificated in any category. This AD dated March 19, 2004): Within 600 flight hours does not apply to Sicma Aero Seat series or 3 months after doing the inspection, 9140, 9166, 9173, 9174, 9184, 9188, whichever occurs first, replace both backrest 9196, 91B7, 91B8, 91C0, 91C2, 91C4, links of the affected seat with new, improved 91C5, 9301, and 9501 passenger seat backrest links having P/Ns and assemblies , in accordance with Part Two of Sicma Aero Seat Service Bulletin , Issue 4, dated March 19, 2004, including Annex 1, Issue 2, dated March 19, (3) If, during the inspection required by paragraph (f)(1) of this AD, cracking is found that passes beyond the lock-out pin hole (refer to Figure 2 of Sicma Aero Seat Service Bulletin , Issue 4, dated March 19, 2004, including Sicma Aero Seat Service Bulletin , Issue 4, dated March 19, 2004 N/A TO EQUIPMENT NOT INSTALLED 7 of 11 11/8/2017
8 Air Transport Association (ATA) of America Code 25: Equipment/Furnishing s. 11/21/11 (c) This AD applies to Sicma Aero Seat Model 9401, 9402, 9404, 9505, 9406, 9407, 9408, and 9409 series passenger seat assemblies, all part numbers, except front row and aft facing seats, and those modified to ''Amendment B'' standard. These passenger seat assemblies are installed on, but not limited to, ATR-GIE Avions de Transport Régional Model ATR42-200, -300, -320, and -500 airplanes and Model ATR72-101, -201, -102, -202, -211, -212, and - 212A airplanes. Note 1: This AD applies to Sicma Aero Seat passenger seat assemblies as installed on any airplane, (g) Within 6 months after the effective date of this AD, perform a detailed inspection for cracking of the central and lateral spreaders of the affected seats, in accordance with paragraph 2/A1., ''Checking procedures of lateral and central spreaders,'' of the Accomplishment Instructions of Sicma Aero Seat Service Bulletin , Issue 4, dated February 12, (1) If no cracking is found on any central spreader, repeat the detailed inspection thereafter at intervals not to exceed 550 flight hours until the replacement specified in paragraph (h) of this AD is done. (2) If no cracking or only cracks that are shorter than 8 millimeters (mm) (0.315 inch) are found on any lateral spreader, repeat the detailed inspection thereafter at intervals not to exceed 550 flight hours until the replacement specified in paragraph (h) of this AD is done. (3) If all cracks found on any central spreader are shorter than 8 mm (0.315 inch), before further flight, repair the affected spreader, in accordance with paragraphs 2/A through C2. of the Accomplishment Instructions of Sicma Aero Seat Service Bulletin , Revision 3, dated June 30, Within 550 flight hours after doing the repair, do the detailed inspection specified in paragraph (g) of this AD, and repeat the inspection thereafter at intervals not to exceed 550 flight hours until the replacement specified in paragraph (h) of this AD is done. (4) If one or more cracks are found that are 8 mm (0.315 inch) or longer on any lateral or central spreader, before further flight, replace the affected spreader, in accordance with Sicma Aero Seat Service Bulletin , Revision 1, dated June 26, S/S N/A N/A N/A N/A N/A N/A N/A N/A N/A N/A by P/N installed. This AD is superseded by AD ######## -- Joint Aircraft System Component (JASC)/Air Transport Association (ATA) of America Code 3/13/12 This AD applies to Aviation Communication & Surveillance Systems (ACSS) traffic alert and collision avoidance system (TCAS) units with part numbers identified in ACSS Technical Newsletter , Revision B, dated August 3, 2011, as installed on but not limited to various transport and small airplanes, certificated in any category. Note 1 to paragraph (c) of this AD: Table 1 of this AD also provides a crossreferenced list of part numbers with associated service bulletins to help operators identify affected parts. Within 36 months after the effective date of this AD, upgrade software for the ACSS TCAS, in accordance with the Accomplishment Instructions of the applicable ACSS publication identified in table 1 of this AD. Note 2 to paragraph (g) of this AD: ACSS Service Bulletin (ATA Service Bulletin ), Revision 03, dated June 30, 2011, contains three part numbers (P/Ns , , and ) that were never produced. Within 36 months after the effective date of this AD, upgrade software for the ACSS TCAS, in accordance with the Accomplishment Instructions of the applicable ACSS publication identified in table 1 of this AD. N/A by P/N installed 8 of 11 11/8/2017
9 ######## -- Air Transport Association (ATA) of America Code 25: Equipment/Furnishing s. 5/9/12 (1) This AD applies to Sicma Aero Seat Model 9401, 9402, 9404, 9405, 9406, 9407, 9408, and 9409 series passenger seat assemblies, all part numbers, except front row and aft facing seats, and those modified to ''Amendment B'' standard. These passenger seat assemblies are installed on, but not limited to, ATR GIE Avions de Transport Régional Model ATR42-200, -300, -320, and -500 airplanes and Model ATR72-101, -201, -102, -202, -211, -212, and - 212A airplanes. (2) This AD applies to Sicma Aero Seat passenger seat assemblies as installed on any airplane, This paragraphs restates the actions required by paragraph (g) of AD , Amendment (76 FR 68304, November 4, 2011). For Sicma Aero Seat Model 9401, 9402, 9404, 9406, 9407, 9408, and 9409 series passenger seat assemblies: Within 6 months after November 21, 2011 (the effective date of AD ), perform a detailed inspection for cracking of the central and lateral spreaders of the affected seats, in accordance with paragraph 2/A1., ''Checking procedures of lateral and central spreaders,'' of the Accomplishment Instructions of Sicma Aero Seat Service Bulletin , Issue 4, dated February 12, (1) If no cracking is found on any central spreader, repeat the detailed inspection thereafter at intervals not to exceed 550 flight hours until the replacement specified in paragraph (i) of this AD is done. (2) If no cracking or only cracks that are shorter than 8 millimeters (mm) (0.315 inch) are found on any lateral spreader, repeat the detailed inspection thereafter at intervals not to exceed 550 flight hours until the replacement specified in paragraph (i) of this AD is done. (3) If all cracks found on any central spreader are shorter than 8 mm (0.315 inch), before further flight, repair the affected spreader, in accordance with paragraphs 2/A through C2. of the Accomplishment Instructions of Sicma Aero Seat Service Bulletin , Revision 3, dated June 30, Within 550 flight hours after doing the repair, do the detailed inspection specified in paragraph (g) of this AD, and repeat the inspection thereafter at intervals not to exceed Sicma Aero Seat Service Bulletin , Revision 1, dated June 26, N/A by P/N installed. This AD supersedes AD of 11 11/8/2017
10 ######## -- 34, Navigation. 6/16/15 This AD applies to Zodiac Aerotechnics (formerly Intertechnique Aircraft Systems) flightcrew oxygen mask regulators, all part number (P/N) MA10, MC10, MC20, MF10, MF20, MLC20, MLD20, MRA005, MRA022, and MRA023 series; certificated in any category; installed on, but not limited to, airplanes manufactured by Airbus, ATR, BAE Systems ( Certificate previously held by British Aerospace), Boeing, Bombardier ( Certificate previously held by Canadair, De Havilland Canada), Cessna, Dassault, EADS CASA, EMBRAER, Gulfstream, Hawker Beechcraft ( Certificate previously held by Raytheon, Beech), Israel Aircraft Industries (IAI), McDonnell Douglas, Piaggio, Pilatus, Piper, and SOCATA. Except as provided by paragraph (i) of this AD: Within 24 months after the effective date of this AD, inspect the inflatable harness fitted to each flightcrew oxygen mask regulator to determine if the inflatable harness is installed with a part number and a batch number identified in Appendix I of Zodiac Aerospace Service Bulletin MXH , Revision 7, dated September 1, 2011 (for all 11 airplanes other than Bombardier airplanes); or Appendix I of Zodiac Aerospace Service Bulletin MXH , Revision 3, dated June 23, 2011 (for Bombardier airplanes). Note 1 to paragraph (g) of this AD: Referring only to Appendix II of Zodiac Aerospace Service Bulletin MXH , Revision 7, dated September 1, 2011; or Appendix II of Zodiac Aerospace Service Bulletin MXH , Revision 3, dated June 23, 2011; to identify a specific oxygen mask regulator is insufficient to demonstrate that the inflatable harness fitted to that oxygen mask regulator is not listed in Appendix I of Zodiac Aerospace Service Bulletin MXH , Revision 7, dated September 1, 2011; or Appendix I of Zodiac Aerospace Service Bulletin MXH , Revision 3, dated June 23, Within 24 months after the effective date of this AD, replace the inflatable harness with a new or re-identified harness, in accordance with the Accomplishment Instructions of Zodiac Aerospace Service Bulletin MXH , Revision 7, dated September 1, 2011 (for all airplanes other than Bombardier airplanes); or Zodiac Aerospace Service Bulletin MXH , Revision 3, dated June 23, 2011 (for Bombardier airplanes). N/A by P/N installed 10 of 11 11/8/2017
11 ######## -- Joint Aircraft System Component (JASC)/Air Transport Association (ATA) of America Code 35; Oxygen. 7/15/16 This AD applies to B/E Aerospace Protective Breathing Equipment (PBE), part number (P/N) , that is installed on airplanes. (g) Inspection Within 3 months after July 15, 2016 (the effective date of this AD), while still in the stowage box, physically inspect the PBE pouch to determine if it has an intact vacuum seal. Do this inspection following paragraph III.A.1. of the Accomplishment Instructions in B/E Aerospace Service Bulletin No , Rev. 000, dated February 4, (h) Replacement (1) If a PBE pouch is found that does not have an intact vacuum seal during the inspection required in paragraph (g) of this AD: Before further flight or following existing minimum equipment list (MEL) procedures, replace the PBE with a PBE, P/N , following paragraphs III.C., III.D.(4), III.D.(6), and III.D.(7) of the Accomplishment Instructions in B/E Aerospace Service Bulletin No , Rev. 001, dated April 12, 2016, or replace it with another FAAapproved serviceable PBE. (2) If a PBE pouch is found during the inspection required in paragraph (g) of this AD where the vacuum seal is intact: Within 18 months after July 15, 2016 (the effective date of this AD), remove PBE, P/N , and replace the PBE with PBE, P/N , following paragraphs III.C., III.D.(4), III.D.(6), and III.D.(7) of the Accomplishment Instructions in B/E Aerospace Service Bulletin No , Rev. 001, dated April 12, 2016, or replace it with another FAAapproved serviceable PBE. (h) Replacement (1) If a PBE pouch is found that does not have an intact vacuum seal during the inspection required in paragraph (g) of this AD: Before further flight or following existing minimum equipment list (MEL) procedures, replace the PBE with a PBE, P/N , following paragraphs III.C., III.D.(4), III.D.(6), and III.D.(7) of the Accomplishment Instructions in B/E Aerospace Service Bulletin No , Rev. 001, dated April 12, 2016, or replace it with another FAAapproved serviceable PBE. (2) If a PBE pouch is found during the inspection required in paragraph (g) of this AD where the vacuum seal is intact:within 18 months after July 15, 2016 (the effective date of this AD), remove PBE, P/N , and replace the PBE with PBE, P/N , following paragraphs III.C., III.D.(4), III.D.(6), and III.D.(7) of the Accomplishment Instructions in B/E Aerospace Service Bulletin No , Rev. 001, dated April 12, 2016, or replace it with another FAAapproved serviceable PBE. N/A by P/N installed 11 of 11 11/8/2017
(a) This airworthiness directive (AD) becomes effective November 23, 2011.
2011-21-08 SICMA AERO SEAT: Amendment 39-16831 Docket No FAA-2010-0040; Directorate Identifier 2008-NM-203-AD Effective Date (a) This airworthiness directive (AD) becomes effective November 23, 2011 Affected
More informationAIRWORTHINESS DIRECTIVE
FAA Aviation Safety AIRWORTHINESS DIRECTIVE www.faa.gov/aircraft/safety/alerts/ www.gpoaccess.gov/fr/advanced.html 2011-21-08 SICMA AERO SEAT: Amendment 39-16831. Docket No. FAA-2010-0040; Directorate
More informationAirworthiness Directive
Airworthiness Directive AD No.: 2018-0262 Issued: 06 December 2018 EASA AD No.: 2018-0262 Note: This Airworthiness Directive (AD) is issued by EASA, acting in accordance with Regulation (EU) 2018/1139
More informationRevisions to this AML must be coordinated between the STC holder and the responsible Aircraft Certification Office (ACO), and require FAA approval.
For ADS-B Out & In Airworthiness 2. Introduction This document is the Federal Aviation Administration (FAA) Approved Model List (AML) for Supplemental Type Certificate (STC) Number ST00835DE, for installing
More informationHoneywell International Inc.: Amendment ; Docket No. FAA ; Directorate Identifier 2012-NM-191-AD.
2012-26-15 Honeywell International Inc.: Amendment 39-17310; Docket No. FAA-2012-1315; Directorate Identifier 2012-NM-191-AD. (a) Effective. Date This AD is effective January 24, 2013. (b) Affected ADs
More informationFAA REPAIR STATION U0KR250X CAPABILITIES LIST
FAA REPAIR STATION U0KR250X CAPABILITIES LIST In accordance with FAR 145.215 (a); CRS U0KR250X is approved to perform maintenance, preventive maintenance and alterations on the Airframes / Articles listed
More informationFAA REPAIR STATION U0KR250X CAPABILITIES LIST
FAA REPAIR STATION U0KR250X CAPABILITIES LIST In accordance with FAR 145.215 (a); CRS U0KR250X is approved to perform maintenance, preventive maintenance and alterations on the Airframes / Articles listed
More informationADAPTER CABLE P/N. Airbus 300/B2/B4 AC-2K C 7/24/02 ANY 290F F /1/74
The Fuel Quantity Adapter Cable Supplements are sorted alphabetically by Aircraft type, then by applicable test set. The Adapter Cable part number and the document number are provided as well as the document
More informationAIRCRAFT SERVICE CHANGE
AIRCRAFT SERVICE CHANGE NUMBER 077 SUBJECT NAVIGATION (ATA 34) TCAS 7.1 INSTALLATION JUNE 12, 2012 PILOTS INFORMATION SHEET TCAS 7.1 INSTALLATION This service change upgrades TCAS 2000 or 3000SP systems
More informationAmendment Docket No. FAA ; Directorate Identifier 2010-CE-041-AD
Page 1 2011-02-02 SOCATA Amendment 9-16575 Docket No. FAA-2010-0948; Directorate Identifier 2010-CE-041-AD PREAMBLE Effective Date (a) This airworthiness directive (AD) becomes effective March 1, 2011.
More informationAirworthiness Directive
Airworthiness Directive AD No.: 2016-0206 [Correction: 14 October 2016] Issued: 13 October 2016 Note: This Airworthiness Directive (AD) is issued by EASA, acting in accordance with Regulation (EC) 216/2008
More informationAvidyne Corporation: Amendment ; Docket No. FAA ; Directorate Identifier 2008-CE-047-AD.
2009-05-05 Avidyne Corporation: Amendment 39-15829; Docket No. FAA- 2008-1210; Directorate Identifier 2008-CE-047-AD. Effective. Date (a) This AD becomes effective on April 3, 2009. Affected ADs (b) This
More information[Docket No. FAA ; Directorate Identifier 2005-NM-071-AD; Amendment ; AD ]
[Federal Register: May 9, 2007 (Volume 72, Number 89)] [Rules and Regulations] [Page 26285-26287] From the Federal Register Online via GPO Access [wais.access.gpo.gov] [DOCID:fr09my07-2] DEPARTMENT OF
More informationHONEYWELL, INC.
Page 1 2009-08-01 HONEYWELL, INC. Amendment 39-15874 Docket No. FAA-2008-0899; Directorate Identifier 2008-NM-022-AD PREAMBLE Effective Date (a) This AD becomes effective May 14, 2009. Affected ADs (b)
More information[Docket No. FAA ; Directorate Identifier 2008-NM-022-AD; Amendment ; AD ]
[Federal Register: April 9, 2009 (Volume 74, Number 67)] [Rules and Regulations] [Page 16121-16124] From the Federal Register Online via GPO Access [wais.access.gpo.gov] [DOCID:fr09ap09-8] DEPARTMENT OF
More informationBiweekly , report of Safety Information Publications between 07/03/ /03/2011
2011-0048 2011-03-18 ) LTD AVRO146RJ, 146 Time Limits / Maintenance Checks - Airworthiness Limitations - Amendment / Implementation CF-2011-04 2011-03-17 BOMBARDIER DHC-8 Cracking of the Outer Wing Fuel
More information[Docket No. FAA ; Directorate Identifier 2015-CE-012-AD; Amendment ; AD ]
[Federal Register Volume 81, Number 112 (Friday, June 10, 2016)] [Rules and Regulations] [Pages 37492-37494] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR Doc
More informationAirworthiness Directive
Airworthiness Directive AD No.: 2018-0259R1 Issued: 07 February 2019 Note: This Airworthiness Directive (AD) is issued by EASA, acting in accordance with Regulation (EU) 2018/1139 on behalf of the European
More information[Docket No. FAA ; Directorate Identifier 2015-CE-017-AD] SUMMARY: The FAA is correcting a notice of proposed rulemaking (NPRM) that
This document is scheduled to be published in the Federal Register on 09/04/2015 and available online at http://federalregister.gov/a/2015-21934, and on FDsys.gov [4910-13-P] DEPARTMENT OF TRANSPORTATION
More informationEMERGENCY AIRWORTHINESS DIRECTIVE
EMERGENCY AIRWORTHINESS DIRECTIVE Aircraft Certification Service Washington, DC We post Emergency ADs on the internet at "www.faa.gov" U.S. Department of Transportation Federal Aviation Administration
More informationBOMBARDIER, INC
Page 1 2010-18-08 BOMBARDIER, INC Amendment 39-16421 Docket No. FAA-2009-1110; Directorate Identifier 2009-NM-116-AD PREAMBLE Effective Date (a) This airworthiness directive (AD) becomes effective October
More information[Docket No. FAA ; Directorate Identifier 2015-CE-012-AD] Airworthiness Directives; B/E Aerospace Protective Breathing Equipment Part Number
This document is scheduled to be published in the Federal Register on 01/15/2016 and available online at http://federalregister.gov/a/2016-00374, and on FDsys.gov [4910-13-P] DEPARTMENT OF TRANSPORTATION
More information[Docket No. FAA ; Directorate Identifier 2017-CE-014-AD] Airworthiness Directives; Rockwell Collins, Inc. Traffic Surveillance System
This document is scheduled to be published in the Federal Register on 07/03/2017 and available online at https://federalregister.gov/d/2017-13948, and on FDsys.gov [4910-13-P] DEPARTMENT OF TRANSPORTATION
More informationAirworthiness Directive
Airworthiness Directive AD No.: 2011-0201R1 Issued: 29 July 2016 EASA AD No.: 2011-0201R1 Note: This Airworthiness Directive (AD) is issued by EASA, acting in accordance with Regulation (EC) 216/2008 on
More informationAirworthiness Directive
Airworthiness Directive AD No.: 2018-0200 Issued: 06 September 2018 EASA AD No.: 2018-0200 Note: This Airworthiness Directive (AD) is issued by EASA, acting in accordance with Regulation (EC) 216/2008
More information[Docket No. FAA ; Directorate Identifier 2010-NM-018-AD; Amendment ; AD R3]
[Federal Register Volume 77, Number 35 (Wednesday, February 22, 2012)] [Rules and Regulations] [Pages 10352-10355] From the Federal Register Online via the Government Printing Office [www.gpo.gov] [FR
More information[Docket No. FAA ; Directorate Identifier 2005-CE-34-AD; Amendment ; AD ]
[Federal Register: December 12, 2005 (Volume 70, Number 237)] [Rules and Regulations] [Page 73355-73358] From the Federal Register Online via GPO Access [wais.access.gpo.gov] [DOCID:fr12de05-4] DEPARTMENT
More information[Docket No. FAA ; Directorate Identifier 2014-NM-035-AD; Amendment ; AD R1]
[Federal Register Volume 79, Number 209 (Wednesday, October 29, 2014)] [Rules and Regulations] [Pages 64305-64306] From the Federal Register Online via the Government Printing Office [www.gpo.gov] [FR
More informationAVIATION COMMUNICATION AND SURVEILLANCE SYSTEMS, LLC
Page 1 2012-02-08 AVIATION COMMUNICATION AND SURVEILLANCE SYSTEMS, LLC Amendment 39-16931 Docket No. FAA-2010-1204; Directorate Identifier 2010-NM-147-AD PREAMBLE (a) Effective Date This AD is effective
More informationBOMBARDIER INC. (FORMERLY CANADAIR)
Page 1 2009-10-10 BOMBARDIER INC. (FORMERLY CANADAIR) Amendment 39-15906 Docket No. FAA-2009-0448; Directorate Identifier 2009-NM-052-AD. PREAMBLE Effective Date (a) This airworthiness directive (AD) becomes
More information[Docket No. FAA ; Directorate Identifier 2010-NM-147-AD; Amendment ; AD ]
[Federal Register Volume 77, Number 25 (Tuesday, February 7, 2012)] [Rules and Regulations] [Pages 6000-6003] From the Federal Register Online via the Government Printing Office [www.gpo.gov] [FR Doc No:
More informationAIRWORTHINESS DIRECTIVE
EASA AIRWORTHINESS DIRECTIVE AD No.: 2013-0234R2 Date: 07 October 2013 Note: This Airworthiness Directive (AD) is issued by EASA, acting in accordance with Regulation (EC) No 216/2008 on behalf of the
More informationThis AD supersedes AD No , Amendment (78 FR 24041, April 24, 2013).
2014-05-10 Airbus Helicopters (Type Certificate Previously Held By Eurocopter France): Amendment 39-17783; Docket No. FAA-2013-0822; Directorate Identifier 2013-SW-004-AD. (a) Applicability. This AD applies
More information[Docket No. FAA ; Product Identifier 2017-NM-111-AD; Amendment ; AD ]
[Federal Register Volume 83, Number 178 (Thursday, September 13, 2018)] [Rules and Regulations] [Pages 46377-46380] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR
More information[Docket No. FAA ; Product Identifier 2017-NM-141-AD; Amendment ; AD ]
[Federal Register Volume 83, Number 178 (Thursday, September 13, 2018)] [Rules and Regulations] [Pages 46369-46372] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR
More information[Docket No. FAA ; Product Identifier 2017-NM-072-AD; Amendment 39-
This document is scheduled to be published in the Federal Register on 03/26/2018 and available online at https://federalregister.gov/d/2018-05013, and on FDsys.gov [4910-13-P] DEPARTMENT OF TRANSPORTATION
More informationTHE BOEING COMPANY
Page 1 2012-21-08 THE BOEING COMPANY Amendment 39-17224 Docket No. FAA-2010-0856; Directorate Identifier 2010-NM-117-AD PREAMBLE (a) Effective Date This AD is effective November 27, 2012. (b) Affected
More informationAIRWORTHINESS DIRECTIVE
EASA AIRWORTHINESS DIRECTIVE AD No.: 2014-0014 Date: 14 January 2014 Note: This Airworthiness Directive (AD) is issued by EASA, acting in accordance with Regulation (EC) No 216/2008 on behalf of the European
More information[Docket No. FAA ; Directorate Identifier 2003-NE-65-AD; Amendment ; AD ]
[Federal Register: March 14, 2005 (Volume 70, Number 48)] [Rules and Regulations] [Page 12404-12406] From the Federal Register Online via GPO Access [wais.access.gpo.gov] [DOCID:fr14mr05-3] DEPARTMENT
More information[Docket No. FAA ; Product Identifier 2017-NM-069-AD; Amendment. AGENCY: Federal Aviation Administration (FAA), Department of Transportation
This document is scheduled to be published in the Federal Register on 05/21/2018 and available online at https://federalregister.gov/d/2018-09732, and on FDsys.gov [4910-13-P] DEPARTMENT OF TRANSPORTATION
More information[Docket No. FAA ; Product Identifier 2018-NM-096-AD; Amendment ; AD ]
[Federal Register Volume 83, Number 236 (Monday, December 10, 2018)] [Rules and Regulations] [Pages 63394-63396] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR
More informationMODEL ELIGIBILITY LIST for Model 107STC
Revision Original A B C D E F G H I J K L M Date 13-Dec-07 7-May-08 26-Jun-08 2-Dec-08 27-Mar-09 30-Jun-09 10-Jul-09 27-Aug-09 19-Mar-10 17-May-10 12-Jul-10 22-Jul-10 24-Sep-10 9-Dec-10 Description Original
More informationLog of Revisions. VS QC-Form 33 Rev AH, 30 May 2017 Page 1 of 6. Printed 5/30/2017. EVAS MODEL ELIGIBILITY LIST for Model 107STC
Revision Original A B C D E F G H I J K L 24-Sep-10 Log of Revisions Date Description 13-Dec-07 Original release, eligibility: STC by EVAS Model Number (page 1); STC by Aircraft Model Name (page 2); portable*
More informationBOMBARDIER, INC.
Page 1 2010-14-02 BOMBARDIER, INC. Amendment 39-16347 Docket No. FAA-2009-1227; Directorate Identifier 2009-NM-119-AD PREAMBLE Effective Date (a) This airworthiness directive (AD) becomes effective August
More informationAirworthiness Directive Schedule
Airworthiness Directive Schedule Propellers & Propeller Governors 29 September 2016 Notes 1. This AD schedule is applicable to the Hamilton Standard series propellers. 2. The Federal Aviation Administration
More information[Docket No. 93-CE-37-AD; Amendment ; AD R1]
[Federal Register: October 22, 2002 (Volume 67, Number 204)] [Rules and Regulations] [Page 64794-64798] From the Federal Register Online via GPO Access [wais.access.gpo.gov] [DOCID:fr22oc02-4] DEPARTMENT
More informationBAE SYSTEMS (OPERATIONS) LIMITED
Page 1 2009-15-08 BAE SYSTEMS (OPERATIONS) LIMITED (FORMERLY BRITISH AEROSPACE REGIONAL AIRCRAFT) Amendment 39-15971 Docket No. FAA-2009-0398; Directorate Identifier 2008-NM-193-AD PREAMBLE Effective Date
More information[Docket No. FAA ; Product Identifier 2016-NE-23-AD; Amendment 39-
This document is scheduled to be published in the Federal Register on 09/17/2018 and available online at https://federalregister.gov/d/2018-20142, and on govinfo.gov [4910-13-P] DEPARTMENT OF TRANSPORTATION
More informationTable 1 to Paragraph (c) of This AD--Affected Airplane Models
2013-18-09 Honeywell ASCa Inc.: Amendment 39-17582. Docket No. FAA-2013-0707; Directorate Identifier 2013-NM-158-AD. (a) Effective. Date This AD becomes effective October 3, 2013. (b) Affected ADs None.
More informationAirworthiness Directive
Airworthiness Directive AD No.: 2018-0064 Issued: 23 March 2018 Note: This Airworthiness Directive (AD) is issued by EASA, acting in accordance with Regulation (EC) 216/2008 on behalf of the European Union,
More informationEMERGENCY AIRWORTHINESS DIRECTIVE
EMERGENCY AIRWORTHINESS DIRECTIVE Aircraft Certification Service Washington, DC We post Emergency ADs on the internet at "www.faa.gov" U.S. Department of Transportation Federal Aviation Administration
More informationTHE BOEING COMPANY
Page 1 2013-04-05 THE BOEING COMPANY Amendment 39-17362 Docket No. FAA-2010-0036; Directorate Identifier 2009-NM-077-AD PREAMBLE (a) Effective Date This AD is effective March 28, 2013. (b) Affected ADs
More informationRevo, Incorporated: Amendment ; Docket No. FAA ; Directorate Identifier 2012-CE-013-AD.
2013-08-14 Revo, Incorporated: Amendment 39-17431; Docket No. FAA-2012-0845; Directorate Identifier 2012-CE-013-AD. (a) Effective. Date This airworthiness directive (AD) is effective June 13, 2013. (b)
More informationBOMBARDIER INC.
Page 1 2012-03-08 BOMBARDIER INC. Amendment 39-16949 Docket No. FAA-2011-0994; Directorate Identifier 2010-NM-143-AD PREAMBLE (a) Effective Date This airworthiness directive (AD) is effective April 4,
More information[Docket No. FAA ; Product Identifier 2017-CE-014-AD; Amendment 39-
This document is scheduled to be published in the Federal Register on 11/15/2017 and available online at https://federalregister.gov/d/2017-24066, and on FDsys.gov [4910-13-P] DEPARTMENT OF TRANSPORTATION
More information[Docket No. FAA ; Directorate Identifier 2012-NM-191-AD; Amendment ; AD ]
[Federal Register Volume 78, Number 6 (Wednesday, January 9, 2013)] [Rules and Regulations] [Pages 1735-1739] From the Federal Register Online via the Government Printing Office [www.gpo.gov] [FR Doc No:
More informationFederal Aviation Administration, DOT 26.3
Federal Aviation Administration, DOT 26.3 as critical as the specific ice accretion defined for that flight phase. Configuration differences and their effects on ice accretions must be taken into account.
More informationNotification of a Proposal to issue an Airworthiness Directive
Notification of a Proposal to issue an Airworthiness Directive PAD No.: 18-132 Issued: 28 September 2018 Note: This Proposed Airworthiness Directive (PAD) is issued by EASA, acting in accordance with Regulation
More information[Docket No. FAA ; Directorate Identifier 2015-CE-018-AD] Airworthiness Directives; PIAGGIO AERO INDUSTRIES S.p.
This document is scheduled to be published in the Federal Register on 07/06/2015 and available online at http://federalregister.gov/a/2015-16293, and on FDsys.gov [4910-13-P] DEPARTMENT OF TRANSPORTATION
More information[Docket No. FAA ; Product Identifier 2017-CE-014-AD; Amendment ; AD ]
[Federal Register Volume 82, Number 219 (Wednesday, November 15, 2017)] [Rules and Regulations] [Pages 52827-52830] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR
More information[Docket No. FAA ; Directorate Identifier 2015-NM-101-AD] Airworthiness Directives; The Boeing Company Airplanes
This document is scheduled to be published in the Federal Register on 12/31/2015 and available online at http://federalregister.gov/a/2015-32850, and on FDsys.gov [4910-13-P] DEPARTMENT OF TRANSPORTATION
More information[Docket No. FAA ; Directorate Identifier 2012-NM-006-AD; Amendment ; AD ]
[Federal Register Volume 78, Number 159 (Friday, August 16, 2013)] [Rules and Regulations] [Pages 49903-49906] From the Federal Register Online via the Government Printing Office [www.gpo.gov] [FR Doc
More informationHawker 850XP. Supplement Pack
Hawker 85XP Supplement Pack The supplements contained in this supplement pack may not have been approved yet by foreign regulatory agencies. To determine approval status, view our web page at http://pubs.beechcraft.com
More information[Docket No. FAA ; Directorate Identifier 2008-CE-047-AD; Amendment ; AD ]
[Federal Register: February 27, 2009 (Volume 74, Number 38)] [Rules and Regulations] [Page 8856-8860] From the Federal Register Online via GPO Access [wais.access.gpo.gov] [DOCID:fr27fe09-4] DEPARTMENT
More informationAirworthiness Directive
Airworthiness Directive AD No.: 2017-0060 Issued: 07 April 2017 EASA AD No.: 2017-0060 Note: This Airworthiness Directive (AD) is issued by EASA, acting in accordance with Regulation (EC) 216/2008 on behalf
More information[Docket No. FAA ; Directorate Identifier 2006-NE-18-AD; Amendment ; AD ]
[Federal Register: May 19, 2006 (Volume 71, Number 97)] [Rules and Regulations] [Page 29072] From the Federal Register Online via GPO Access [wais.access.gpo.gov] [DOCID:fr19my06-2] DEPARTMENT OF TRANSPORTATION
More informationAirworthiness Directive
Airworthiness Directive AD No.: 2016-0146R1 Issued: 26 July 2018 EASA AD No.: 2016-0146R1 Note: This Airworthiness Directive (AD) is issued by EASA, acting in accordance with Regulation (EC) 216/2008 on
More information[Docket No SW-25-AD; Amendment ; AD R1]
[Federal Register: July 6, 2004 (Volume 69, Number 128)] [Rules and Regulations] [Page 40539-40541] From the Federal Register Online via GPO Access [wais.access.gpo.gov] [DOCID:fr06jy04-4] DEPARTMENT OF
More information[Docket No. FAA ; Product Identifier 2013-NE-24-AD; Amendment ; AD ]
[Federal Register Volume 84, Number 48 (Tuesday, March 12, 2019)] [Rules and Regulations] [Pages 8802-8805] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR Doc No:
More informationAirworthiness Directive
Airworthiness Directive AD No.: 2017-0069 Issued: 25 April 2017 Note: This Airworthiness Directive (AD) is issued by EASA, acting in accordance with Regulation (EC) 216/2008 on behalf of the European Union,
More informationGULFSTREAM AEROSPACE CORPORATION
Page 1 2011-24-02 GULFSTREAM AEROSPACE CORPORATION Amendment 39-16866 Docket No. FAA-20110572; Directorate Identifier 2011-NM-009-AD. PREAMBLE (a) Effective Date This AD is effective January 3, 2012. (b)
More informationLANDING GEAR - REPLACEMENT OF NOSE LANDING GEAR RETRACT PLUNGER ASSEMBLY
Beechcraft TITLE: SERVICE BULLETIN LANDING GEAR - REPLACEMENT OF NOSE LANDING GEAR RETRACT PLUNGER ASSEMBLY 1. Planning Information A. Effectivity (1) Airplanes (a) Civil (i) (ii) (b) Military (i) The
More informationEASA Safety Information Bulletin
EASA SIB No: 2008-73 EASA Safety Information Bulletin SIB No.: 2008-73 Issued: 11 August 2008 Subject: Honeywell Flight Management System (FMS) Early Descent Behaviour. Ref. Publication: Federal Aviation
More informationAirworthiness Directive
Airworthiness Directive AD No.: 2017-0098 Issued: 07 June 2017 EASA AD No.: 2017-0098 Note: This Airworthiness Directive (AD) is issued by EASA, acting in accordance with Regulation (EC) 216/2008 on behalf
More information[Docket No. FAA ; Directorate Identifier 2009-NM-193-AD; Amendment ; AD ]
[Federal Register: January 12, 2010 (Volume 75, Number 7)] [Rules and Regulations] [Page 1527-1529] From the Federal Register Online via GPO Access [wais.access.gpo.gov] [DOCID:fr12ja10-3] DEPARTMENT OF
More informationAirworthiness Directive Schedule
Airworthiness Directive Schedule Aeroplanes 28 July 2016 Notes 1. This AD schedule is applicable to Cessna 175 series aircraft manufactured under FAA Type Certificate No. 3A17. 2. The Federal Aviation
More information[Docket No. FAA ; Directorate Identifier 2000-NE-08-AD; Amendment ; AD ]
[Federal Register: December 26, 2007 (Volume 72, Number 246)] [Rules and Regulations] [Page 72915-72917] From the Federal Register Online via GPO Access [wais.access.gpo.gov] [DOCID:fr26de07-3] DEPARTMENT
More information[Docket No. FAA ; Directorate Identifier 2016-NM-006-AD; Amendment ; AD ]
[Federal Register Volume 82, Number 27 (Friday, February 10, 2017)] [Rules and Regulations] [Pages 10258-10262] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR Doc
More information[Docket No. FAA ; Product Identifier 2017-NM-122-AD; Amendment ; AD ]
[Federal Register Volume 83, Number 154 (Thursday, August 9, 2018)] [Rules and Regulations] [Pages 39326-39331] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR Doc
More information[Docket No. FAA ; Directorate Identifier 2013-NM-085-AD; Amendment
This document is scheduled to be published in the Federal Register on 04/03/2014 and available online at http://federalregister.gov/a/2014-07318, and on FDsys.gov [4910-13-P] DEPARTMENT OF TRANSPORTATION
More information[Docket No. FAA ; Product Identifier 2018-NM-046-AD; Amendment ; AD ]
[Federal Register Volume 83, Number 189 (Friday, September 28, 2018)] [Rules and Regulations] [Pages 48927-48930] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR
More informationTHE CESSNA AIRCRAFT COMPANY
Page 1 2010-20-10 THE CESSNA AIRCRAFT COMPANY Amendment 39-16444 Docket No. FAA-2010-0380; Directorate Identifier 2009-NM-009-AD PREAMBLE Effective Date (a) This AD becomes effective November 1, 2010.
More informationAirworthiness Directive
Airworthiness Directive AD No.: 2012-0053R1 Issued: 27 November 2018 Note: This Airworthiness Directive (AD) is issued by EASA, acting in accordance with Regulation (EU) 2018/1139 on behalf of the European
More information[Docket No. FAA ; Directorate Identifier 2007-NM-027-AD; Amendment ; AD ]
[Federal Register: April 3, 2007 (Volume 72, Number 63)] [Rules and Regulations] [Page 15818-15820] From the Federal Register Online via GPO Access [wais.access.gpo.gov] [DOCID:fr03ap07-6] DEPARTMENT OF
More information[Docket No. FAA ; Directorate Identifier 2012-NM-230-AD; Amendment. Airworthiness Directives; The Boeing Company Airplanes
This document is scheduled to be published in the Federal Register on 10/02/2013 and available online at http://federalregister.gov/a/2013-24029, and on FDsys.gov [4910-13-P] DEPARTMENT OF TRANSPORTATION
More information[Docket No. FAA ; Directorate Identifier 2015-NM-101-AD; Amendment. AGENCY: Federal Aviation Administration (FAA), DOT.
This document is scheduled to be published in the Federal Register on 08/31/2016 and available online at http://federalregister.gov/a/2016-20686, and on FDsys.gov [4910-13-P] DEPARTMENT OF TRANSPORTATION
More informationREIMS AVIATION S.A.
Page 1 2011-07-03 REIMS AVIATION S.A. Amendment 39-16640 Docket No. FAA-2011-0058; Directorate Identifier 2010-CE-071-AD PREAMBLE Effective Date (a) This airworthiness directive (AD) becomes effective
More informationAVOX SYSTEMS AND B/E AEROSPACE
Page 1 2009-21-10 AVOX SYSTEMS AND B/E AEROSPACE Amendment 39-16049 Docket No. FAA-2009-0915; Directorate Identifier 2009-NM-224-AD PREAMBLE Effective Date (a) This airworthiness directive (AD) is effective
More information[Docket No. FAA ; Directorate Identifier 2013-NM-081-AD] Airworthiness Directives; The Boeing Company Airplanes
This document is scheduled to be published in the Federal Register on 08/05/2013 and available online at http://federalregister.gov/a/2013-18800, and on FDsys.gov [4910-13-P] DEPARTMENT OF TRANSPORTATION
More informationAirworthiness Directive Schedule
Airworthiness Directive Schedule Aeroplanes 22 October 2015 Notes 1. This AD schedule is applicable to Britten-Norman Islander BN-2A Mk III-1, BN-2A Mk III-2 and BN-2A Mk III-3 series aircraft manufactured
More informationAirworthiness Directive
Airworthiness Directive AD No.: 2017-0237 Issued: 04 December 2017 EASA AD No.: 2017-0237 Note: This Airworthiness Directive (AD) is issued by EASA, acting in accordance with Regulation (EC) 216/2008 on
More informationTHE BOEING COMPANY
Page 1 2010-23-03 THE BOEING COMPANY Amendment 39-16492 Docket No. FAA-2010-1040; Directorate Identifier 2010-NM-207-AD. PREAMBLE Effective Date (a) This AD is effective November 22, 2010. Affected ADs
More informationDassault Aviation (Formerly Avions Marcel Dassault-Breguet Aviation (AMD/BA))
Page 1 2008-04-14 Dassault Aviation (Formerly Avions Marcel Dassault-Breguet Aviation (AMD/BA)) Amendment 39-15386 Docket No. FAA-2007-28941; Directorate Identifier 2006-NM-276-AD PREAMBLE Effective Date
More information[Docket No. FAA ; Directorate Identifier 2015-NM-101-AD; Amendment ; AD ]
[Federal Register Volume 81, Number 169 (Wednesday, August 31, 2016)] [Rules and Regulations] [Pages 59830-59834] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR
More informationSUPPORT SERVICES GMBH
Page 1 2011-18-13 328 SUPPORT SERVICES GMBH (TYPE CERTIFICATE PREVIOUSLY HELD BY AVCRAFT AEROSPACE GMBH; FAIRCHILD DORNIER GMBH; DORNIER LUFTFAHRT GMBH) Amendment 39-16795 Docket No. FAA-2010-1163; Directorate
More informationAmendment Docket No. FAA ; Directorate Identifier 2010-NM-099-AD
Page 1 2011-06-09 AIRBUS Amendment 39-16634. Docket No. FAA-2010-1162; Directorate Identifier 2010-NM-099-AD PREAMBLE Effective Date (a) This airworthiness directive (AD) becomes effective April 26, 2011.
More informationBF Goodrich Avionics Systems, Inc. SKYWATCH SKY497
Página 1 de 6 RGL Home Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [63 FR 66746 No. 232 12/03/98]
More informationAirworthiness Directive
Airworthiness Directive AD No.: 2017-0257R1 Issued: 09 January 2018 EASA AD No.: 2017-0257R1 Note: This Airworthiness Directive (AD) is issued by EASA, acting in accordance with Regulation (EC) 216/2008
More informationDEPARTMENT OF TRANSPORTATION. Federal Aviation Administration. 14 CFR Part 39. [Docket No NE-08-AD; Amendment ; AD ]
[Federal Register: May 9, 2002 (Volume 67, Number 90)] [Rules and Regulations] [Page 31113-31115] From the Federal Register Online via GPO Access [wais.access.gpo.gov] [DOCID:fr09my02-2] DEPARTMENT OF
More information[Docket No. FAA ; Directorate Identifier 2010-NM-177-AD; Amendment ; AD ]
[Federal Register Volume 77, Number 168 (Wednesday, August 29, 2012)] [Rules and Regulations] [Pages 52212-52217] From the Federal Register Online via the Government Printing Office [www.gpo.gov] [FR Doc
More information