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					                               WOODSTONE CORP
   N3276T                  TECHNICAL BULLETIN COMPLIANCE

Technical Bulletin                                 Title
                                 Quick Reaction Trimble Trimpack GP Sys
 TB 1-1520-210-20-17
                                          C/W not installed this acft
                             One Time And Recurring Insp, Tail Rotor Blades
 TB 1-1520-210-20-32
                                   UH-1-96-ASAM-03 C/W insp blades OK
                                  Assignment Of Life To Main Rotor Yoke
 TB 1-1520-210-20-33
                            SOF UH-1-96-04 / Time calculated as per AD81-19-02
                        Night Vision Goggle, Op And Nav/Position Light Inspection
 TB 1-1520-210-20-34
                                          C/W not installed this acft
                           Insp of Oil Debris Detect Sys, Self Sealing, Oil Fitting
 TB 1-1520-210-20-35
                                          C/W not installed this acft
                                  Night Vision Goggle Flight Restrictions
 TB 1-1520-210-20-36
                                          C/W not installed this acft
                               Revision of Tail Rotor Slider Retirement Life
 TB 1-1520-210-20-38
                             UH-1-98-01 & 03 / S/N 14475 installed TBO adjusted
                                 Mandatory Inspection of Rod End Clevis
 TB 1-1520-210-20-41
                          SOF UH-1-98-07 / Red S/N CC10263 & White S/N AF8920
                         Mandatory Inspect And Removal of Elevator Assemblies
 TB 1-1520-210-20-42
                        UH-1-99-ASAM-01 & 02 / R/H S/N AC 0673 & L/H S/N AC 0431
                               Mandatory Inspect Of Tail Rotor Control Tube
 TB 1-1520-210-20-43
                                   UH-1-99-ASAM-02 C/W insp cage # OK
                           Time Report/Temp Retire Life, UH-1 Tail Rotor Blades
 TB 1-1520-210-20-46
                               UH-1-00-ASAM-01 C/W not applicable this acft
                       Mandatory Inspection of Tail Boom Verticle Fin Spar Assembly
 TB 1-1520-210-20-47
                                                UH-1-00-07
                                  One Time Inspection of Mast Assembly
 TB 1-1520-210-20-50
                                     SOF UH-1-00-09 & 10 / C/w by PHI
                          UH-1F Mandatory Inspection and Removal of Elevator Assys
 TB 1-1520-210-20-51
                               UH-1-01-ASAM-01 / C/W not applicable this acft
                                     Inspection of Turnbuckle Body
 TB 1-1520-210-20-54
                                            SOF UH-1-01-05
                                One-Time Inspection of Rotor Control Parts Kit
 TB 1-1520-210-20-57
                                     SOF UH-1-01-06 C/W bolts replaced
                                    Inspection of Rotor Control Parts Kit
 TB 1-1520-210-20-58
                                     SOF UH-1-02-01 C/W bolts replaced
                                   Aircraft Inspection of Turnbuckle Body
 TB 1-1520-210-20-59
                                               SOF UH-1-02-02
                                      Improved Inertia Reel Installation
 TB 1-1520-210-20-60
                                    UH-1-02-ASAM-02 / UH-1-01-ASAM-04
                        1,000-Hour Retirement Life for the Collective Lever Assembly
 TB 1-1520-210-20-61
                               SOF UH-1-02-03 / C/W insp not applicable by P/N
                       Mandatory Changeout Main Rotor Pitch Horn Attachment Bolts
 TB 1-1520-210-20-62
                                   C/W insp implemented 50 hr torque check
                         Inspection of UH-1 Main Rotor Pitch Horn Attachment Bolts
 TB 1-1520-210-20-63
TB 1-1520-210-20-63
                       UH-1-MIM-2003-001 C/W insp implemented 50 hr torque check
                            AVUM And AVIM Manual Nondestructive Inspect
TB 1-1520-210-23-1
                                   Reviewed manual and installed in library
                                     Tail Boom Vertical Spar Assembly
TB 1-1520-210-30-01
                                 SOF UH-1-00-05 / UH-1-99-03 / UH-1-00-06
                                  Inspection of 42-Degree Gearbox Asbly
TB 1-1520-210-30-02
                                SOF UH-1-00-08 C/W not applicable this gbx
                       One Time Inspect Of Swashplate Anti-Drive Link Assemblies
TB 1-1520-236-20-14
                                        C/W not applicable to this acft
                                          Oil Debris Detection Sys
TB 1-1520-243-20-25
                               UH-1-98-ASAM-01 C/W not applicable this acft
                                          Oil Debris Detection Sys
TB 1-1520-243-20-26
                               UH-1-98-ASAM-04 C/W not applicable this acft
                               Inspection of Tail Rotor Driveshaft Coupling
TB 1-1520-243-20-27
                         UH-1-00-ASAM-04 C/W insp no affected couplings installed
                                  One Time Inspection of Magnetic Brake
TB 1-1520-243-20-28
                        UH-1-01-ASAM-03 C/W insp no affected mag brakes installed
                                      Inspection of Power Shaft Bolts
TB 1-1520-243-20-29
                                              UH-1-01-ASAM-05
                          One Time Inspection of Pilot and Co-pilot Safety Belt
TB 1-1520-243-20-30
                                   UH-1-02-ASAM-01 C/W insp latches OK
                                Oil Debris Detection System Chip Detector
TB 1-1520-243-20-31
                                          C/W not applicable this acft
                      Operational Restriction All UH-1 Series Aircraft T53-L-13B Eng
TB 1-2840-229-20-10
                                  UH-1-97-01 N/A by engine model number
                                         High Pressure Fuel Fitting
TB 1-2840-229-20-12
                                   UH-1-97-ASAM-03 / UH-1-97-ASAM-04
                        Screening Proc for UH-1 Series Acft with T53-L-13 Engine
TB 1-2840-229-20-15
                      SOF UH-1-98-04 / SOF UH-1-98-05 N/A by engine model number
                           Install of Coated N2 Spur Gears T53-L-13B Engines
TB 1-2840-229-20-16
                        SOF UH-1-98-06 C/W not applicable by engine model number
                            Rev to Procedures for T53-L-13B Engine Installed
TB 1-2840-229-20-18
                        SOF UH-1-98-08 C/W not applicable by engine model number
                                        Sandy Environ/Combat Ops
TB 1-2840-229-20-2
                                              Reviewed manual
                        Suspense Date for Mandatory N2 Spur Gear Replacement
TB 1-2840-229-20-21
                                               SOF UH-199-01
                                  Revision to Safety of Flight UH-1-99-01
TB 1-2840-229-20-24
                                               SOF UH-1-99-04
                            Interim Retirement Life P/N 1-100-078-07 Impeller
TB 1-2840-229-20-26
                                               SOF UH-1-00-02
                                UH-1 & AH-1 Helicopters with T-53 Engine
TB 1-2840-229-20-27
                                     SOF UH-1-00-04 / SOF UH-1-00-03
                                      T-53 Turbine Wheel Components
TB 1-2840-229-20-28
                                                 UH-1-00-06
                                 Final Life Limits for Turbine Components
TB 1-2840-229-20-29
                                                 UH-1-01-01
                            Fail Vibration Screening IAW TB 1-2840-229-20-15
TB 1-2840-229-20-30
                                                 UH-1-01-02
                                    Suspect Engine Reduction Gear Box
TB 1-2840-229-20-31
TB 1-2840-229-20-31
                                UH-1-02-ASAM-03
                      Operational Restriction: Eng, T53-L-13B
TB 1-2840-229-20-9
                                    UH-1-96-03
                              Tail Hub Assy, Sealant
TB 55-1500-206-30-2
                              C/W insp sealant present
    N3276T
             Signature
 3-May-04
              M. Peck
  10,118.5
28-Jun-04
              M. Peck
   10133.2
22-Feb-03
               UNK
   10059.3
28-Jun-04
              M. Peck
   10133.2
 3-May-04
              M. Peck
  10,118.5
 3-May-04
              M. Peck
  10,118.5
 3-May-04
              M Peck
  10,118.5
 3-May-04
              M Peck
  10,118.5
28-Jun-04
              M. Peck
   10133.2
28-Jun-04
              M. Peck
   10133.2
28-Jun-04
              M. Peck
   10133.2
 24-Jul-02
             E. Aguaya
    9935.5
     1-Jan
               UNK
3-May-04
              M. Peck
 10,118.5


28-Jun-94
              M. Peck
  10133.2
28-Jun-04
              M. Peck
  10133.2




28-Jun-04
              M. Peck
  10133.2
28-Jun-04
              M. Peck
  10133.2
28-Jun-04
              M. Peck
              M. Peck
   10133.2
28-Jun-04
              M. Peck
   10133.2
 24-Jul-02
              E Aguaya
    9,935.5
28-Jun-04
              M. Peck
  10,133.2
28-Jun-04
              M. Peck
   10133.2
28-Jun-04
              M. Peck
  10,133.2
28-Jun-04
              M. Peck
  10,133.2
29-Jun-04
              M. Peck
   10133.2
29-Jun-04
              M. Peck
   10133.2
10-Feb-03
              M. Avila
29-Jun-04
              M. Peck
   10133.2
28-Jun-04
              M. Peck
  10,133.2
28-Jun-04
              M. Peck
  10,133.2
28-Jun-04
              M. Peck
   10133.2
 3-May-04
              M. Peck
  10,118.5
 3-May-04
              M. Peck
  10,118.5
 3-May-04
              M. Peck
  10,118.5
28-Jun-04
              M. Peck
  10,133.2




28-Jun-04
              M. Peck
            M. Peck
  10133.2


28-Jun-04
            M. Peck
  10133.2

				
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posted:1/19/2012
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