Attachment_8_Technical_Directives.xlsx
XLSX spreadsheet 17 KB Posted
- Attached to
- P-8A Airframe and Engine Depot Maintenance Competition Federal contract opportunity
- Solicitation number
- N00019-15-R-2004
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Section J Attachment 8
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| Part A Airframe TDs | ||
| SERVICE LETTER / SERVICE BULLETIN | TD Type | DESCRIPTION |
| P8 -SL-53-0053 | AFB | MISSING FASTENERS ON SILL NEAR THE LOWER OF FORWARD CARGO DOOR CORNERS |
| P8-SL-53-0057 | AFB | FOUR MISSING FASTENERSAT STA 479 |
| P8-SL-51-0002 | AFB | P-8A – NON-CONFORMING BSAA AND PRIMER ADHESION PARTS |
| P8-SL-53-008 R1 | AFB | INSPECT AND REWORK TEMPORARY FASTENERS IN STALLED IN FRAME 500F |
| P8-SL-20-0041 | AFB | ELECTRICAL CONNECTOR BACKSHELLS POTENTIALLY MISSING PROTECTIVE BARRIER TAPE IN THE OUTER FRONT SPAR AND WING TIPS |
| P8-SL-28-0018 | AFB | AFT AUXILIARY FUEL TANK NO. 9 EXTERNAL FITTING (INTERCONNECT PAN) IS MISSING ORIENTATION MARKINGS, PART NUMBER (P/N) MW2-05-4093/3 |
| P8-SL-53-0051 | AFB | POSSIBLE MISSING FASTENERS |
| P8-SL-28-0012 | AFB | AUXILIARY FUEL TANKS INTERSPACE DEBRIS CONTAINMENT |
| P8-SL-53-0052 | AFB | RIDING CONDITION BETWEEN BRACKET AND HEAD OF HI LOKS |
| P8-SL-99-0002 | AFB | EARLY WARNING & SELF PROTECTION (EWSP) - WIRE BUNDLE -W9317 CONNECTOR MS3459W32-6S CONTACT RETENTION DEFICIENCY |
| P8-SL-47-0004 | AFB | ON BOARD INERT GAS GENERATING SYSTEM (OBIGGS) ELECTRICAL CONNECTORS POTENTIALLY CLOCKED INCORRECTLY |
| 737-SL-53-103-A | AFB | BS 578 TO 639 STUB BEAM FASTENERS MISSING COUNTER BORE WASHER |
| 737-SL-57-0106-A | AFB | LH AND RH WING NACELLE SUPPORT OUTBOARD SIDELOAD BACKUP FITTING – MISSING FILLET SEAL |
| P8-SL-28-0014 | AFB | UARRSI PARTS NOT PRIMED IAW MIL-STD-889 |
| P8-SL-53-0009-A | AFB | FUSELAGE – FLOOR BEAM – RIDING CONDITION BETWEEN FASTENERS AND TUBE ASSEMBLY |
| 737-SL-32-168 | AFB | POTENTIALLY INCORRECT MAIN LANDING GEAR AXLE INSTALLATION |
| P8-SL-53-0024 | AFB | P-8A – Inspection and Rework Incorrect Channel Frame and Bulkhead Surfaces |
| 737-SL-27-227 | AFB | RUDDER FEEL AND CENTERING INSTALLATION – FASTENERS UNDERTORQUED |
| 737-SL-28-080-A | AFB | POTENTIAL UNDER-TORQUED FUEL SUMP DRAIN AND AN UNDER-TORQUED BULKHEAD FITTING NUT |
| P8-SL-20-0038 | AFB | WIRE BUNDLE IMPROPERLY SECURED ALONG MISSION EQUIPMENT COOLING DUCT |
| 737-SL-55-019-E | AFB | VERTICAL STABILIZER REAR SPAR SHIM MIGRATION |
| P8-SL-53-0061 | AFB | SECTION 41 ELONGATED FASTENER HOLES COMMON TO STRINGERS |
| P8-SL-57-0015 | AFB | DISCREPANT SHORT FLAP FAIRING RIVETS |
| P8-SL-53-0082 | AFB | STA 178 BULKHEAD CLIP ASSEMBLIES MAY HAVE ELONGATED RIVET HOLES |
| 737-SL-32-198-A | AFB | WIRES POTENTIALLY CONTACTING MAIN LANDING GEAR (MLG) |
| P8-SL-53-0067 | AFB | POTENTIALLY UNINSTALLED RIVETS AT STA 727E AND 727F |
| P8-SL-28-0030 | AFB | AERIAL REFUELING DRAIN FITTING MISALIGNED |
| P8-SL-99-0005 | AFB | RADAR WARNING RECEIVER (RWR) OMNI BLADE ANTENNA FASTENER OVER-TORQUE |
| P8-SL-96-0015 | AFB | STORES MANAGEMENT SYSTEM (SMS) CONNECTOR DISCREPANCY |
| P8-SL-53-0058 | AFB | GAP CONDITION BETWEEN FRAME AND INTERCOSTAL |
| P8-SL-53-0070-A | AFB | POSSIBLE RIDING CONDITION BETWEEN TIE ROD ASSEMBLY PIN AND STRINGER |
| P8-SL-21-0021-A | AFB | ELECTRONIC SUPPORT MEASURES (ESM) FORWARD ARRAY COOLING LINE MAY BE RIDING AGAINST PROTECTIVE SHROUD |
| P8-SL-53-0093 | AFB | SECTION 44 POTENTIALLY DISCREPANT FASTENER TAIL HEIGHTS |
| P8-SL-53-0062 | AFB | POTENTIALLY DISBONDED NUTPLATES IN THE NOSE LANDING GEAR WHEEL WELL |
| P8-SL-51-0004 | AFB | MASKING APPLIED IN INCORRECT LOCATION ON 111A6202-402 LOWER CHORD |
| P8-SL-53-0007 | AFB | P-8A – INSPECTION AND REWORK SCUFF PLATE INSTALLATION ON FORWARD CARGO DOOR |
| P8-SL-53-0038-A | AFB | SECTION 43 AFT PRESSURE BOX MISSING FASTENERS |
| P8-SL-53-0039 | AFB | LEFT AFT WING-TO-BODY PANEL FASTENER NUTPLATE IS DAMAGED |
| P8-SL-53-0050 | AFB | POSSIBLE MISSING SEALANT ON FASTENERS |
| P8-SL-53-0059 | AFB | BODY FITTING BRACKET MAY BE INSTALLED INCORRECTLY |
| P8-SL-53-0063 | AFB | DISCREPANT FASTENERS COMMON TO SKIN, FRAME AND INTERCOSTAL |
| P8-SL-53-0015-A | AFB | OPEN HOLE IN STRUCTURE – MISSING FASTENER |
| P8-SL-53-0047 | AFB | POTENTIAL OF THREE UNINSTALLED FUSELAGE RIVETS IN SECTION 48 |
| P8-SL-21-0001 | AFB | INCORRECT FASTENERS ISSUED AND INSTALLED |
| P8-SL-57-0002 | AFB | INSPECTION OF SUSPECT FASTENER INSTALLATIONS |
| 737-SL-57-108 | AFB | FRONT SPAR LEADING EDGE STRAP CORROSION PREVENTION |
| P8-SL-53-0088 | AFB | POTENTIAL RIDING FASTENER CONDITION AND TOOL MARK DAMAGE |
| P8-SL-53-0089 | AFB | ADVANCED AIRBORNE SYSTEM (AAS) ALTERNATE RETRACT SYSTEM (ARS) – AIRFRAME TO ARS INTERFACE ISSUE |
| P8-SL-51-0007 | AFB | POST-ASSEMBLY BRUSH SEALING APPLICATION FOR WTBF FASTENERS |
| P8-SL-53-0076 | AFB | RIDING FILLER |
| P8-SL-53-0084-A | AFB | POTENTIAL SURFACE DAMAGE AT FLOOR BEAM STIFFENER |
| P8-SL-57-0016 | AFB | POTENTIAL UNINSTALLED COUNTERBORE WASHERS COMMON TO RADIUS LEAD-IN BOLT AT THE FRONT SPAR CHORD WEB JOINT |
| P8-SL-28-0029 | AFB | AFT INTEGRAL FUEL TANK VENT/TRANSFER TUBE PRESSURE RELIEF VALVE - PROTECTIVE CAP |
| P8-SL-53-0085-A | AFB | DISCREPANT MACHINED FAILSAFE STRAPS RESULTING IN POTENTIAL GAPS BETWEEN FRAME AND SKIN |
| P8-SL-23-0019 | AFB | FOKKER-ELMO NOTICE OF ESCAPEMENT (NOE) - SUSPECT BACKSHELL ON WIRE HARNESS W0865 RECEPTACLE D5228J |
| P8-SB-28-0002 | AFB | PRESSURE FUELING SYSTEM - FILL VALVE ADAPTER SHAFT ASSYEMBLY - INSPECTION AND REPLACEMENT |
| P8-SL-52-0024 | AFB | POTENTIAL SEALANT VOIDS COMMON TO AFT BAILOUT DOOR REVEAL INSTALLATION |
| P8-SL-51-0008 | AFB | POTENTIAL UNAPPLIED CORROSION INHIBITING COMPOUND (CIC) ON SEAT TRACK STRUCTURE |
| P-8-AFC-22 | AFC | P-8A MODIFICATION OF ONBOARD INERT GAS GENERATING SYSTEM (OBIGGS) EQUIPMENT |
| P-8-AFC-49 | AFC | P-8A WIRING RACEWAY TIE-ROD INSTALLATION; MODIFICATION OF |
| P-8-AFC-68 | AFC | P-8A FWD, AFT AND AUX FUEL TANK 10 FILL ORIFICES, REPLACEMENT OF |
| Part B Engine TDs | ||
| SERVICE LETTER / SERVICE BULLETIN | TD Type | DESCRIPTION |
| 0853 | SB | Compressor Front Stator Assembly (72-32-00) - Actuation Compressor Stator Inlet Guide Vane Ring Assembly Durability Improvement |
| 0863 | SB | ENGINE-Compressor Front Stator Assembly (73-32-00)-On Wing Inspection of Pre CFM56-7b S/B 72-0811 Actuation Compressor |
| 0864 | SB | Low Pressure Turbine Rotor/Stator Assembly (72-54-00) - Spare Parts Release for CFM56-7B IPC |
| 0006 | SB | Rework in Field of Fan Containment Case B1 Flange at Holes No. 84 and 85 |
| 0172 | SB | ENGINE - LPT Rotor/Stator Assembly (72-54-00) - Replacement of Broken Stud of T49.5 EGT Sensor Retaining Plate |
| 0188 | SB | LPT ROTOR/STATOR ASSEMBLY (72-54-00) - REWORK OF THE LPT CASE RAIL "0" SUPPORT RING AND REIDENTIFICATION OF THE LPT CASE. |
| 0888 | SB | ENGINE - Fan and Booster Assembly (72-21-00) - Fan Blade Moment-Weight Mismarking |
| 0929 | SB | ENGINE FIRE DETECTOR WIRE ROUTING CHANGE |
| 0935 | SB | ENGINE FLANGES |
| 0921-R2 | SB | ENGINE - Fan Frame Assembly (72-23-00) - Introduction of an Anti-Erosion Paint On the Fan Frame Assembly |
| 0781-R01 | SB | ENGINE - General (72-00-00) - Fan Disk Pressure Faces Inspection |
| 0811 | SB | ENGINE - HPT/LPT Nozzle Shroud Assembly (72-53-00) - New Shroud HPT Stator Hanger with Modified Air Filter |
| 0825-03 | SB | High Pressure Turbine Rotor Assembly (72-52-00) - HPT Rotor Blade Management |
| 0616-R01 | SB | Low Pressure Turbine Rotor/Stator Assembly (72-54-00) - Spare Parts Release for CFM56-7B IPC |
| 0780-R02 | SB | Rework for Fan Containment Case B1 Flange at Fire Detector |
Location
| 0423 Rev1 | SB | CFM56 7B Right Side Cooling Air-HPTACC Tube Bolts Change for Error-Proof Assembly |
| 0718 | SB | Application of PTFE Lubricant Varnish on V-Groove Outer |
Ring
0797 SB APU - 3.0 INCH DIAMETER SURGE CONTROL VALVE -
Inspection of the Chrome Plating on the Butterfly Shaft, PN 3180688-1, Used on the 3.0 Inch Diameter Surge Control Valve, PN 3291238-2
| 055-C | SL | This Service Bulletin releases a redesigned HPT rotor disk P/N 2410M49P02 (76 blade configuration) to improve the producibility of the disk. The air slot of the old HPT rotor disk (P/N 2410M49P01) is cut into the disk using a milling operation that leaves the air slot geometry nonsymmetrical. The new HPT rotor disk features a more symmetrically shaped air slot generated by a form. |
| 0003 | SB | ENGINE FLANGES |
| 0553 Rev1 | SB | ENGINE - Fan Frame Assembly (72-23-00) - Introduction of an Anti-Erosion Paint On the Fan Frame Assembly |
| 0525 | SB | ENGINE - General (72-00-00) - Fan Disk Pressure Faces Inspection |
| 0816 | SB | ENGINE - HPT/LPT Nozzle Shroud Assembly (72-53-00) - New Shroud HPT Stator Hanger with Modified Air Filter |
| 0821 | SB | High Pressure Turbine Rotor Assembly (72-52-00) - HPT Rotor Blade Management |
| 0580-R04 | SB | Rework for Fan Containment Case B1 Flange at Fire Detector |
Location
| 0056 | SB | CFM56 7B Right Side Cooling Air-HPTACC Tube Bolts Change for Error-Proof Assembly |
| 0996 | SB | Application of PTFE Lubricant Varnish on V-Groove Outer |
Ring
7032 SB APU - 3.0 INCH DIAMETER SURGE CONTROL VALVE -
Inspection of the Chrome Plating on the Butterfly Shaft, PN 3180688-1, Used on the 3.0 Inch Diameter Surge Control Valve, PN 3291238-2 0929-R02 SB This Service Bulletin releases a redesigned HPT rotor disk P/N 2410M49P02 (76 blade configuration) to improve the producibility of the disk. The air slot of the old HPT rotor disk (P/N 2410M49P01) is cut into the disk using a milling operation that leaves the air slot geometry nonsymmetrical. The new HPT rotor disk features a more symmetrically shaped air slot generated by a form.
N00019-15-R-2004 &"Arial,Bold"&20 Technical Directives Attachment 8
&P
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