Airworthiness directives, 2006

439 ADs took effect in 2006. Every AD since 1946 has a page with its text, status and the registered aircraft it may apply to.

Query with SQL
duckdb -csv -c "SELECT d.ad_number, d.status, d.subject, d.makes, d.models, d.effective_date
  FROM 'https://openairdocs.org/data/latest/faa_directive.parquet' d
  WHERE year(coalesce(d.effective_date, d.publication_date, d.issue_date)) = 2006
  ORDER BY coalesce(d.effective_date, d.publication_date, d.issue_date) DESC, d.ad_number DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

Earlier years
AD 2006-21-12HistoricalSupersedes AD 2003-22-13, to inspect ailerons. · AeroSpace Technologies Of Australia Pty N22B, N22S and N24AEffective Nov 8, 2006 · Replaced by AD 2009-26-08AD 2006-20-12Replaces clamp bases on fuel tank vent systems. · Boeing 717-200Effective Nov 8, 2006AD 2006-20-11HistoricalRivet inspection · Boeing 757-200 Series, 757-200CB Series and 757-200PF SeriesEffective Nov 8, 2006 · Replaced by AD 2016-22-09AD 2006-20-08HistoricalRod ends of aileron power control actuator, superseding AD 99-05-04 · Embraer EMB-145, EMB-145EP, EMB-145ER and 4 moreEffective Nov 8, 2006 · Replaced by AD 2025-08-07AD 2006-21-11HistoricalFlexible lubrication pipes · Turbomeca Turmo IVA and Turmo IVCEffective Nov 3, 2006 · Replaced by AD 2009-02-08AD 2006-21-09Identification plate of torque box · Boeing 777-200 SeriesEffective Nov 3, 2006AD 2006-21-08HistoricalHeatshields in belly fairing · Airbus A330-201, A330-202, A330-203 and 8 moreEffective Nov 3, 2006 · Replaced by AD 2014-16-19AD 2006-20-10Attach angles on the firewall mounted hopper rinse tank shelf · Air Tractor AT-802 and AT-802AEffective Nov 3, 2006AD 2006-20-09HistoricalCertain crankshafts replacing · Lycoming Engines AEIO-360-A1B6, AEIO-360-A1E6, AEIO-540-D4A5 and 82 moreEffective Nov 3, 2006 · Replaced by AD 2012-19-01AD 2006-20-07Adds an additional life limit for third- and fourth-stage turbine wheels · Rolls-Royce 250-C30, 250-C30G, 250-C30G/2 and 11 moreEffective Nov 2, 2006AD 2006-20-05Inspect chafing in skin of wing-to-fuselage fairing · BAE Systems BAe 146-100A, BAe 146-200A and BAe 146-300AEffective Nov 2, 2006AD 2006-20-04Inspection of chain assemblies of elevator trim system · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 moreEffective Nov 2, 2006AD 2006-20-03Girt bar position of forward passenger doors · Airbus A319-111, A319-112, A319-113 and 20 moreEffective Nov 2, 2006AD 2006-20-02Longitudinal rows of fasteners in the bonded skin panels · Boeing 747-100 Series, 747-100B Series, 747-100B SUD Series and 9 moreEffective Nov 2, 2006 · Supersedes AD 96-23-02AD 2006-20-01Incorporate restrictions for high altitude operations. · Airbus A310-203, A310-204, A310-221 and 5 moreEffective Nov 2, 2006AD 2006-17-07 R1High pressure compressor (HPC) front hubs and HPC disk · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 18 moreEffective Nov 2, 2006 · Supersedes AD 2006-17-07AD 2006-19-12HistoricalEngine struts investigation · Boeing 777-200 Series and 777-300 SeriesEffective Oct 30, 2006 · Replaced by AD 2016-23-02AD 2006-21-02Operating Limitations, Abnormal Procedures, and Normal Procedures · Textron 400, 400A, 400T and 1 moreEffective Oct 25, 2006AD 2006-19-11Seat stop relocation · GA 8 Airvan GA8Effective Oct 25, 2006AD 2006-19-10Adjust crew seat break-over bolts · Cirrus Design SR20 and SR22Effective Oct 24, 2006 · Supersedes AD 2005-17-19AD 2006-19-09Passenger seat mod kit · Textron B300Effective Oct 24, 2006AD 2006-19-07Attachment landing assemblies of blow- down panels of wing leading edges · Airbus A330-201, A330-202, A330-203 and 15 moreEffective Oct 24, 2006AD 2006-19-04Honeywell COM unit and Mode S transponder · Bombardier BD-700-1A10, BD-700-1A11, 550 and 26 moreEffective Oct 17, 2006AD 2006-19-03Fabrication and installation of a wire harness guard in the right wheel well of the main landing gear (MLG) · Boeing DC-10-10, DC-10-10F, DC-10-15 and 8 moreEffective Oct 17, 2006AD 2006-19-02Cracking of the fuselage outer skin at frames 28A and 30A above stringer 30 · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 6 moreEffective Oct 17, 2006 · Supersedes AD 97-14-02AD 2006-20-51HistoricalAirplane Flight Manual to prohibit takeoffs at less than full-rated thrust · Boeing 777-200 Series and 777-200LREffective Oct 16, 2006 · Replaced by AD 2006-20-51 R1AD 2006-20-06HistoricalMain fuel pump (MFP) inlet strainer · General Electric CF34-10E2A1, CF34-10E5, CF34-10E5A1 and 3 moreEffective Oct 16, 2006 · Replaced by AD 2007-12-15AD 2006-19-05Tail rotor (T/R) slider · California Department of Forestry UH-1H, UH-1F, TH-1L and 36 moreEffective Oct 16, 2006AD 2006-18-17HistoricalYaw damper actuator portion of the upper and lower rudder power control modules (PCMs) · Boeing 747-400 Series, 747-400D Series and 747-400F SeriesEffective Oct 13, 2006 · Replaced by AD 2008-13-03AD 2006-18-16Wing spigot bearing retainer kit · Textron 390Effective Oct 13, 2006AD 2006-18-14HistoricalCyclic life of stage 1 HPT discs, and stage 1 LPT discs · Rolls-Royce Deutschland TAY 650-15 and TAY 651-54Effective Oct 13, 2006 · Replaced by AD 2016-17-01AD 2006-18-13Hardover prevention system (HOPS) in the roll axis due to a short circuit in the wiring harness · Gulfstream Aerospace GV and GV-SPEffective Oct 13, 2006AD 2006-18-12Hot detection system of the tail pipe harness of the engine nacelles · Saab AB, Saab Aerosystems SAAB 340B and 340A (SAAB SF340A)Effective Oct 13, 2006AD 2006-18-08Nosewheel tires · Bombardier BD-700-1A10, BD-700-1A11, Aviation Tires and 7 moreEffective Oct 11, 2006AD 2006-18-07Replacing the very high frequency (VHF) antenna located in position 1 of the fuselage with a new, improved VHF antenna · Embraer ERJ 170-100 LR, ERJ 170-100 SE, ERJ 170-100 STD and 1 moreEffective Oct 11, 2006AD 2006-18-06Stainless steel ribs left- and right-hand engine pylons · Airbus A318-111, A318-112, A319-111 and 19 moreEffective Oct 11, 2006AD 2006-18-05Disconnect panel · Boeing DC-9-14, DC-9-15, DC-9-15F and 12 moreEffective Oct 11, 2006 · Supersedes AD 2003-03-08AD 2006-19-08Exhaust bends in curvature bend area · Stemme Stemme S10-VTEffective Oct 10, 2006AD 2006-18-03Flap system interface wiring · Embraer EMB-145XREffective Oct 4, 2006AD 2006-18-02Replacing the clamp bases for the fuel vent pipe · Boeing DC-9-11, DC-9-12, DC-9-13 and 15 moreEffective Oct 4, 2006AD 2006-17-07HistoricalFretting and fluorescent magnetic particle inspections (FMPI) for cracking in the area of the tierod holes on the HPC front hubs · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 18 moreEffective Oct 4, 2006 · Replaced by AD 2006-17-07 R1AD 2006-18-01Notar fan system tension-torsion (TT) straps. · MD Helicopters MD900Effective Oct 3, 2006 · Supersedes AD 2004-23-15AD 97-06-13 R1Rescinds AD 97-06-13. · Rolls-Royce RB211-Trent-892B-17, RB211-Trent 875-17, RB211-Trent 877-17 and 2 moreEffective Oct 2, 2006 · Supersedes AD 97-06-13AD 2006-19-06Propeller shaft · Pratt & Whitney Canada PW118, PW118A, PW118B and 14 moreEffective Sep 29, 2006AD 2006-17-17Rivets on left and right control column torque tube assemblies · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 8 moreEffective Sep 29, 2006AD 2006-17-16Wing rear spar lower girder · F.28 Mark 0070 and F.28 Mark 0100Effective Sep 29, 2006AD 2006-17-15Replacing the clamp bases for the fuel vent pipe with improved clamp bases · Boeing DC-10-10, DC-10-10F and MD-10-10FEffective Sep 29, 2006AD 2006-19-01Tapered housing of each main servo-control (MSC) · Airbus Helicopters AS355E, AS350B, AS350B1 and 4 moreEffective Sep 27, 2006AD 2006-18-11Auxiliary fuel system · ONE ONLY STC (Leading Edge Group LLC, The STC SA1078NE or 5 others)Effective Sep 27, 2006AD 2006-17-13Replacing the existing attachment bolts for the seat belts with longer attachment bolts · RECARO Aircraft Seats SeatsEffective Sep 27, 2006