Landing Gear. Im out of the loop for conduit installations. The following is for reference only, not intended to imply I still do the installations. Midwest Aeronautical Helicopter Services offers factoryauthorized service for Robinson R22 and R44 helicopters in St. Louis, MO. RHCService. The de Havilland DH. Mosquito was a British twinengine shoulderwinged multirole combat aircraft. The crew of two, pilot and navigator, sat side by side. Airworthiness Directives. Airworthiness Directives. NOTE This AD note listing is intended as a guide only and. AD applicability on. Entire Airworthiness Directives may be accessed. Showing Results 1 5. Next  AD No. MAKECondensed description of ad note. Eurocopter. Superceded by 1. Twin Commander. Cracks in upper picture window frame channels, left and rght hand main wing spar frame support channels and aft pressure bulkhead web 6. A, B1. 3 9 3. Dassault Falcon. Landing Gear Bungee Installation' title='Landing Gear Bungee Installation' />Fuel tank modification 2. EX, 5. 0, 9. 00, 9. EX1. 3 9 1. 1Cessna. Air Conditioning motor brushes excessive wear 5. S5. 50, 5. 60, 5. XL, 6. 50. 13 8 6. Mdm_9PlGXy8/0.jpg' alt='Landing Gear Bungee Installation Tool' title='Landing Gear Bungee Installation Tool' />Bell. Published Vne airspeeds 4. Cessna. AC motor brushes wearing beyond limits 5. Turbomeca. Engine tachometer cycle counting feature Arriel Series. Diamond. Charge Air tubing and the engine firewall DA4. NG1. 3 8 1. 9Eurocopter. Anyone have input on why gear will not fully retract on a 1980 172 RG. Nose gear stows, right side stows, BUT the left side hangs down about 812. View and Download Hangar 9 14 PA18150 Super Cub instruction manual online. PA18150 Super Cub Toy pdf manual download. Plan1 Capability List 25246246D 25246341 25246348 2524638B 25246401 25246408 2524645B 2524648B 2524650B 252465421 2524665 25246651 25246738 25246811. MAIN.jpg' alt='Landing Gear Bungee Installation' title='Landing Gear Bungee Installation' />Sliding door AS3. Eurocopter. Crack in 9 degree frame SA and AS 3. Eurocopter. Center windscreen panel EC1. B4. 13 7 1. 3Dassault. Defective flight crew mask oxygen assembly Falcon 7. X1. 3 7 1. Diamond. Overextension of the MLG shock absorber DA4. Eurocopter. Undetected flight display error of a slow drift in the roll axis AS 3. Goodrich. Failure of the overload clutch good rich hoist, various helicopters. Diamond. Engine air inlet subject to icing DA4. M NG, NG1. 3 5 6. Bombardier. Left Hand engine thrust control mechanism jamming Cl 6. A, 6. 01 3. R, 6. Agusta. Tail rotor pitch control link A1. Eurocopter. Cracke cabin vibration blade EC1. B4. 13 5 1. 6Mc. Donnell Douglas. Tailboom 3. D, E, F, FF1. Robinson. Pop out floats R4. R4. 4II1. 3 5 1. Bell. Swashplate outer ring assembly 4. EP1. 3 4 9. Tecnam. Outboard aileron hinge support P2. T1. 3 4 3. Cessna. PitotStatic Anti Ice System Citation X1. Bombardier. Cracks in upper and lower web of the engine support beam CL6. A, 3. R, 6. 04. Hawker Beech. Volt DC system circuit protection 4. XP1. 3 3 2. 3Gulfstream. Performance corrections to AFM G1. Pratt Whitney. PT Disk PW2. B, B2, C PW2. 07. C, D, D1, D2, E1. Eurocopter. Supersedes 1. Crack in TRH EC1. B, B1, SA3. 65. N1, AS3. N2, N, N3. 13 3 1. Bell Helicopter. Supersedes 1. Main rotor inboard strap 2. Cessna. Inspect the fuel return assembly 1. R, S1. 3 3 1. 2Dassault. Airworthiness limitations Falcon 5. Bell. Tailboom crack 2. Turbomeca. Arriel Series. Eurocopter. Exit Window AS3. Diamond. Aft main spar DA4. Eurocopter. Sliding door AS 3. Eurocopter. MGB supporting structure AS3. Eurocopter. AS3. 50 AS 3. Bell. Float inflation hoses 2. Embraer. Brake assembly Phenom 3. Eurocopter. IGB fairing 3. Sikorsky. Spindle cuff assembly S7. Bell. Freewheel unit bearings 2. Eurocopter. Boom EC1. Eurocopter. Tail rotor EC1. Lycoming and Continental. Supersedes 1. 2 2. Turbocharger applicable TIO 5. AK1. A, TSIO 3. 60 MB, TSIO 3. RB1. 3 2. 1 1. Eurocopter. Yoke pitch horn 3. Agustasupersedes 0. Thomas coupling nuts, TR A1. Bell. Third stage turbine vibration 4. Bell. Third stage turbine vibration 4. Bell. Third stage turbine vibration 2. Bell. Main rotor yoke assembly 4. Bell. Third stage turbine vibration 2. B, 2. 06. A, 2. 06. L1. 3 2. 0 1. Agusta. Third stage turbine vibration A1. Piper. Control cable assembly failures affecting Horizontal stabilator Multiple Piper Aircraft. Bell. Hydraulic servo actuator assembly 2. L, L 1, L 3, L 4. Eurocopter. Seat rear bottom 3. Robinson. Fuel shut off valve R2. MDSupersedes 0. 3 8 5. Tail rotor 3. 69 series. Bellstaked bearings 2. Eurocopterfire extinguishing system EC1. Piaggio. Main landing gear left hinge fitting P1. Bell. Inoperative control box assembly 2. A, B, L1. 3 1. 8 1. Eurocopter. Inadvertant locking and unlocking of the collective pitch lever EC1. SA3. 65 series. 13 1. Diamond DA2. 0 Katana. Engine Inspection for excessive oil consumption DA2. A1. 13 1. 7 1. Eurocopter. Loose nut or misaligned tail rotor control stop screw AS3. Series. 13 1. 6 4. Eclipse. Hardware failure autopilot control panel and center switch EA5. Eurocopter. Crack in the control lever attachment yoke of the TGB casing assembly AS3. Eurocopter. Longitudinal main rotor actuator piston 1. C 2. 13 1. 6 1. Eurocopter. Chafing of the floats EC1. B and EC1. 30. B4. Bell. Failure of crosstube landing gear 4. Eurocopter. Improperly manufactured bypass inlet in the oil filter area EC1. Eurocopter. Failure of weight or lever tail rotor BK1. Beechcraft. Loose or failing elevator balance weights 5. P, 5. 8TC, 9. 5 C5. E5. 5, 5. 6TC1. 3 1. Eurocopter. Hydraulic pump drive pulley bearing seizure AS2. B, BA, B1, B2, B3, C, D, D1. Bell. Supersedes 0. Fatigue cracking of a TR blade 2. Bombardier. Fire barrier seal on the external baggage door Lear 4. Bombardier. Braking system Lear 6. Piper. Incorrect fuel ventilation PA 4. P, 3. 50. P, 3. T, 5. TP1. 3 1. Bell. Tailboom cracking 4. Eurocopter. AC drive pulley mount bolt BK 1. Eurocopter. Bevel gear failure BK 1. C 2. 13 1. 2 4. Eurocopter. Closed fuel tank drain EC1. ASSA3. 65. 13 1. Turbomeca. Supersedes 0. Replace injector manifolds and perform borescope inspection of flame tube and high pressure turbine area EC 1. Dassault. Tail strobe power supply and hydraulic line chaffing Falcon 9. EX1. 3 1. 1 5. Bell. Manual Teste Quati Pdf on this page. Bearing with incorrect seal material 2. B, B 1. 13 1. 1 1. Hawker Beech. Maximum altitude placard and AFM modification 8. A, B, XP1. 3 1. 1 1. Eurocopter. Inadvertant locking of the cyclic stick EC1. BO1. 05, BK1. 17, EC1. SA3. 66, SA 3. 65 series. Bombardier. Screw cap or end cap of hydraulic system accumulator Challenger 3. Cessna. Supersedes 0. Replace oil pressure switch 1. R,1. 82. S,2. 06. H,T2. 06. H1. 3 1. Cessna. Correct unsafe brake lock up condition LC4. LC4. 1, LC4. 21. 3 1. Eurocopter. Excessive axial play, bearings on main and tail rotor servo controls AS 3. Piper. Supersedes 8. Exhaust system failures PA 3. Eurocopter. Excessive power consumption of the starter generator AS3. B3, EC1. 30. B4. 13 1 4. Bell. Failure and corroison of crosstubes 4. EP1. 2 9 1. 1Eurocopter. Unsafe condition, failures of engines to reach the specified one engine inoperative rating at altitudes abouve 1. BK 1. 17 C 1 and C 2. Pratt Whitney. To prevent failure of the sun gear and planet gears on some models PT6. A 3. 8, 4. 1, 4. A, 6. B, 1. 10, 1. 12, 1. A, 1. 21, 1. 35, 1. A1. 2 9 1. Cessna. Wheel inserts becoming loose and damaging brake assemblies 5. XL, XLS1. 2 8 8. Bombardier. Revisions to certain operator maintenance documents to include new actions inspections 4. Turbomeca. Detection of geometric non conformities on PT blade fir tree roots Arriel 2. B, 2. B1. 12 8 1. Bombardier. Swapped engine fire extinguishers Lear 6. Bombardier. Short circuit events during pre delivery inspections Challenger 6. Bombardier. AD regarding air driven generator failing to power essential buses during functional tests Challenger 6. Turbomeca. Supersedes 0. Arrius 2. F turboshaft with P3 air pipe, part number 0. P3 pipe Arrius 2. F1. 2 7 4. Cessna. False cross feed command to the right hand fuel control 6. Bombardier. Horizontal stabilizer trim actuator no back and number 1 motor brake assembly can both fail dromant Challenger 3. Dassault. AD to prevent internal fuel leakage with significant fuel vapors Falcon 9.