Attachment_8_Technical_Directives.xlsx
XLSX spreadsheet 41 KB Posted
- Attached to
- P-8A Airframe and Engine Depot Maintenance Competition Federal contract opportunity
- Solicitation number
- N00019-15-R-2004
About this file
Section J Attachments
View the file
Other files for this federal contract opportunity
Show all 50
P-8A Airframe and Engine Depot Maintenance Competition has more files on GovTribe.
On GovTribe
Work with this file on GovTribe
- Download the original file
- Contacts named in this file
- Similar government files
- Ask GovTribe AI about this file
Text version
Depot Planning
| TD Type | SL/SB | Description |
| AFB | P8 -SL-53-0053 | MISSING FASTENERS ON SILL NEAR THE LOWER OF FORWARD CARGO DOOR CORNERS |
| AFB | P8-SL-53-0057 | Four missing fasteners at STA 479 |
| AFB | P8-SL-51-0002 | P-8A – Non-Conforming BSAA and Primer Adhesion Parts From TC Systems |
| AFB | P8-SL-53-008 R1 | Inspect and Rework Temporary Fasteners Installed in Frame 500F (Forward Cargo Compartment) Possible tie to CP 3984 |
| AFB | P8-SL-20-0041 | ELECTRICAL CONNECTOR BACKSHELLS POTENTIALLY MISSING PROTECTIVE BARRIER TAPE IN THE OUTER FRONT SPAR AND WING TIPS |
| AFB | P8-SL-28-0018 | AFT AUXILIARY FUEL TANK NO. 9 EXTERNAL FITTING (INTERCONNECT PAN) IS MISSING ORIENTATION MARKINGS, PART NUMBER (P/N) MW2-05-4093/3 |
| AFB | P8-SL-53-0051 | POSSIBLE MISSING FASTENERS |
| AFB | P8-SL-28-0012 | AUXILIARY FUEL TANKS INTERSPACE DEBRIS CONTAINMENT |
| AFB | P8-SL-53-0052 | RIDING CONDITION BETWEEN BRACKET AND HEAD OF HI LOKS |
| AFB | P8-SL-99-0002 | EARLY WARNING & SELF PROTECTION (EWSP) - WIRE BUNDLE -W9317 CONNECTOR MS3459W32-6S CONTACT RETENTION DEFICIENCY |
| AFB | P8-SL-47-0004 | ON BOARD INERT GAS GENERATING SYSTEM (OBIGGS) ELECTRICAL CONNECTORS POTENTIALLY CLOCKED INCORRECTLY |
| AFB | 737-SL-53-103-A | BS 578 TO 639 STUB BEAM FASTENERS MISSING COUNTER BORE WASHER |
| AFB | 737-SL-57-0106-A | LH AND RH WING NACELLE SUPPORT OUTBOARD SIDELOAD BACKUP FITTING – MISSING FILLET SEAL |
| AFB | P8-SL-28-0014 | UARRSI PARTS NOT PRIMED IAW MIL-STD-889 |
| AFB | P8-SL-53-0009-A | FUSELAGE – FLOOR BEAM – RIDING CONDITION BETWEEN FASTENERS AND TUBE ASSEMBLY |
| AFB | 737-SL-32-168 | POTENTIALLY INCORRECT MAIN LANDING GEAR AXLE INSTALLATION |
| AFB | P8-SL-53-0024 | P-8A – Inspection and Rework Incorrect Channel Frame and Bulkhead Surfaces |
| AFB | 737-SL-27-227 | RUDDER FEEL AND CENTERING INSTALLATION – FASTENERS UNDERTORQUED |
| AFB | 737-SL-28-080-A | POTENTIAL UNDER-TORQUED FUEL SUMP DRAIN AND AN UNDER-TORQUED BULKHEAD FITTING NUT |
| AFB | P8-SL-20-0038 | WIRE BUNDLE IMPROPERLY SECURED ALONG MISSION EQUIPMENT COOLING DUCT |
| AFB | 737-SL-55-019-E | VERTICAL STABILIZER REAR SPAR SHIM MIGRATION |
| AFB | P8-SL-53-0061 | SECTION 41 ELONGATED FASTENER HOLES COMMON TO STRINGERS |
| AFB | P8-SL-57-0015 | DISCREPANT SHORT FLAP FAIRING RIVETS |
| AFB | P8-SL-53-0082 | STA 178 BULKHEAD CLIP ASSEMBLIES MAY HAVE ELONGATED RIVET HOLES |
| AFB | 737-SL-32-198-A | WIRES POTENTIALLY CONTACTING MAIN LANDING GEAR (MLG) |
| AFB | P8-SL-53-0067 | POTENTIALLY UNINSTALLED RIVETS AT STA 727E AND 727F |
| AFB | P8-SL-28-0030 | AERIAL REFUELING DRAIN FITTING MISALIGNED YP004, YP006-YP031 will require the removal of the G2 Galley |
| AFB | P8-SL-99-0005 | RADAR WARNING RECEIVER (RWR) OMNI BLADE ANTENNA FASTENER OVER-TORQUE |
| AFB | P8-SL-53-0058 | GAP CONDITION BETWEEN FRAME AND INTERCOSTAL |
| AFB | P8-SL-53-0070-A | POSSIBLE RIDING CONDITION BETWEEN TIE ROD ASSEMBLY PIN AND STRINGER recommended this service letter be accomplished concurrently |
with the Air Frame Change (AFC 54) related to Ref /B/ for aircraft YP003, YP006-YP010./B/ CP809-03665, Correct Wiring – Raceway – Tie-Rod Installation, Upper Lobe
| AFB | P8-SL-21-0021-A | ELECTRONIC SUPPORT MEASURES (ESM) FORWARD ARRAY COOLING LINE MAY BE RIDING AGAINST PROTECTIVE SHROUD Below decking. (222AF) Requies oxygen cabinet removal. |
| AFB | P8-SL-53-0093 | SECTION 44 POTENTIALLY DISCREPANT FASTENER TAIL HEIGHTS |
| AFB | P8-SL-53-0062 | POTENTIALLY DISBONDED NUTPLATES IN THE NOSE LANDING GEAR WHEEL WELL |
| AFB | P8-SL-51-0004 | MASKING APPLIED IN INCORRECT LOCATION ON 111A6202-402 LOWER CHORD |
| AFB | P8-SL-53-0007 | P-8A – Inspection and Rework Scuff Plate Installation on Forward Cargo Door |
| AFB | P8-SL-53-0038-A | SECTION 43 AFT PRESSURE BOX MISSING FASTENERS |
| AFB | P8-SL-53-0050 | POSSIBLE MISSING SEALANT ON FASTENERS |
| AFB | P8-SL-53-0059 | BODY FITTING BRACKET MAY BE INSTALLED INCORRECTLY |
| AFB | P8-SL-53-0063 | DISCREPANT FASTENERS COMMON TO SKIN, FRAME AND INTERCOSTAL |
| AFB | P8-SL-53-0015-A | OPEN HOLE IN STRUCTURE – MISSING FASTENER |
| AFB | P8-SL-53-0047 | POTENTIAL OF THREE UNINSTALLED FUSELAGE RIVETS IN SECTION 48 |
| AFB | P8-SL-21-0001 | Incorrect fasteners issued and installed |
| AFB | P8-SL-57-0002 | Inspection of Suspect Fastener Installations |
| AFB | 737-SL-53-107 | SECTION 41 FLOOR INTERCOSTAL IMPROVEMENT new part number intercostals are one-way interchangeable by attrition. |
| AFB | P8-SL-51-0007 | POST-ASSEMBLY BRUSH SEALING APPLICATION FOR WTBF FASTENERS |
| AFB | P8-SL-53-0076 | RIDING FILLER |
| AFB | P8-SL-53-0084-A | POTENTIAL SURFACE DAMAGE AT FLOOR BEAM STIFFENER |
| AFB | P8-SL-57-0016 | POTENTIAL UNINSTALLED COUNTERBORE WASHERS COMMON TO RADIUS LEAD-IN BOLT AT THE FRONT SPAR CHORD WEB JOINT |
| AFB | 737-SL-57-111 | MESH GASKETS FOR FUEL TANK ACCESS DOORS |
| AFB | 737-SL-57-108 | FRONT SPAR LEADING EDGE STRAP CORROSION PREVENTION |
| AFB | P8-SL-28-0029 | AFT INTEGRAL FUEL TANK VENT/TRANSFER TUBE PRESSURE RELIEF VALVE - PROTECTIVE CAP |
| AFB | P8-SL-53-0085-A | DISCREPANT MACHINED FAILSAFE STRAPS RESULTING IN POTENTIAL GAPS BETWEEN FRAME AND SKIN |
| AFB | P8-SL-27-0010 | SPOILER PULLEY BRACKET BOLT CHAFING HYDRAULIC TUBE |
| AFB | P8-SL-53-0067 | POTENTIALLY UNINSTALLED RIVETS AT STA 727E AND 727F |
| AYB | P8-PN-15-0083 | Replacement of Special Screw in the End Bell Assembly, PN 6430603-3, of the Starter/Generator, PN 28B545-9 |
| AFB | P8-SL-99-0005 | RADAR WARNING RECEIVER (RWR) OMNI BLADE ANTENNA FASTENER OVER-TORQUE |
| AFB | P8-SL-96-0015 | STORES MANAGEMENT SYSTEM (SMS) CONNECTOR DISCREPANCY |
| AFB | P8-SL-53-0065 | POTENTIAL INSUFFICIENT FILLET SEAL BETWEEN SUPPORT BRACKET AND STIFFENERS |
| AFB | P8-SL-53-0058 | GAP CONDITION BETWEEN FRAME AND INTERCOSTAL |
| AFB | P8-SL-53-0070-A | POSSIBLE RIDING CONDITION BETWEEN TIE ROD ASSEMBLY PIN AND STRINGER |
| AFB | P8-SL-53-0077 | POSSIBLE INCORRECT SPACER INSTALLATION FOR SECTION 41 WIRE BUNDLE SUPPORT BRACKET |
| AFB | P8-SL-51-0004 | MASKING APPLIED IN INCORRECT LOCATION ON 111A6202-402 LOWER CHORD |
| AFB | P8-SL-53-0007 | P-8A – Inspection and Rework Scuff Plate Installation on Forward Cargo Door |
| AFB | P8-SL-53-0081 | INADEQUATE TEFLON COVERAGE BENEATH VENTRAL FINS |
| AFB | P8-SL-53-0079 | MISSING FINSHES ON CUT EDGES OF SKIN, DOUBLER AND DRAIN HOLE |
| AFB | P8-SL-52-0018 | INSPECTION FOR FLIGHT DECK DOOR BLOWOUT PANEL TAPE |
| AFB | P8-SL-53-0078 | TEFLON FINISH INCORRECTLY LOCATED ON FUSELAGE SKIN BENEATH ESM RADOME |
| AFB | P8-SL-53-0038-A | SECTION 43 AFT PRESSURE BOX MISSING FASTENERS |
| AFB | P8-SL-53-0039 | LEFT AFT WING-TO-BODY PANEL FASTENER NUTPLATE IS DAMAGED |
| AFB | P8-SL-53-0050 | POSSIBLE MISSING SEALANT ON FASTENERS |
| AFB | P8-SL-53-0059 | BODY FITTING BRACKET MAY BE INSTALLED INCORRECTLY |
| AFB | P8-SL-53-0063 | DISCREPANT FASTENERS COMMON TO SKIN, FRAME AND INTERCOSTAL |
| AFB | P8-SL-53-0015-A | OPEN HOLE IN STRUCTURE – MISSING FASTENER |
| AFB | P8-SL-52-0007 | BAILOUT DOOR INNER SKIN PANEL NOTICE OF ESCAPEMENT (NOE) |
| AFB | P8-SL-52-0007 | BAILOUT DOOR INNER SKIN PANEL NOTICE OF ESCAPEMENT (NOE) |
| AFB | P8-SL-53-0054-B | MISSING SEALANT COMMON TO FASTENER HEADS, NUTS AND WASHERS |
| AFB | P8-SL-53-0012 | SEAT TRACK INSTALLATION – OPEN PILOT HOLES |
| AFB | P8-SL-53-0047 | POTENTIAL OF THREE UNINSTALLED FUSELAGE RIVETS IN SECTION 48 |
| AFB | P8-SL-21-0001 | Incorrect fasteners issued and installed |
| AFB | 737-SL-20-0052-A | WIRE BUNDLE SUPPORT BRACKETS IN NOSE GEAR E/E BAY INCORRECTLY INSTALLED |
| AFB | 737-SL-78-069-A | THRUST REVERSER LATCH BEAM FAIRING MISSING SEALANT |
| AFB | 737-SL-53-097 | POTENTIALLY INSUFFICIENT GRIP LENGTH FOR FLIGHT DECK FORWARD PANEL SUPPORT FASTENERS AT STA 204, WL 208, RBL & LBL 29 |
| AFB | 737-SL-24-195-B | CIRCUIT BREAKER TERMINAL SCREWS INSPECTION AND REPLACEMENT |
| AFB | P8-SL-25-0008 | E111 and E112 Rack Tie Rod Support Assembly |
| AFB | P8-SL-57-0002 | Inspection of Suspect Fastener Installations |
| AFB | P8-SL-53-0087-A | SHORT GRIP LENGTH FASTENERS COMMON TO TAILCONE ASSEMBLY |
| AFB | P8-SL-35-0013 | POTENTIAL SCRIBE MARKS ON CREW OXYGEN CYLINDER SUPPORT RAIL |
| AFB | P8-SL-33-0007 | WING ILLUMINATION LIGHT WIRE TERMINAL STACK-UP MAY HAVE OMITTED A LOCK WASHER |
| AFB | P8-SL-34-0023 | INSUFFICIENT CLEARANCE BETWEEN W0422 HARNESS AND E4-2 ELECTRICAL EQUIPMENT RACK |
| AFB | 737-SL-27-216 | STABILIZER POSITION SENSOR INPUT ROD WASHER INSTALLATION DISCREPANCY |
| AFB | P8-SL-21-0017 | DRAW-THRU FAN MOUNTING AND ISOLATOR BOLTS SAFETY CABLE COULD BE INCORRECTLY INSTALLED |
| AFB | 737-SL-28-099 | POSSIBLE MISSING FINISH ON APU DRAIN MAST TUBE |
| AFB | P8-SL-51-0007 | POST-ASSEMBLY BRUSH SEALING APPLICATION FOR WTBF FASTENERS |
| AFB | P8-SL-53-0075 | SEAL VOIDS BETWEEN PARTS IN THE NOSE WHEEL WELL |
| AYB | P8-SL-31-0001 | REMOTE INTERFACE UNIT (RIU) LOADED WITH INCORRECT SOFTWARE NUMBER NOTICE OF ESCAPEMENT (NOE) |
| AFB | P8-SL-23-0005-A | AERO SEAL POSSIBLY MISSING ON VERY HIGH FREQUENCY (VHF) ANTENNA |
| AFB | P8-SL-53-0071 | POSSIBLE DISCREPANT FOD CONDITION 178 BULKHEAD |
| AFB | P8-SL-53-0074 | POSSIBLE DISCREPANT CORROSION INHIBITING COMPOUND FROM FOOT PRINT OF SKATE ANGLE |
| AFB | P8-SL-53-0076 | RIDING FILLER |
| AFB | P8-SL-53-0084-A | POTENTIAL SURFACE DAMAGE AT FLOOR BEAM STIFFENER |
| AFB | 737-SL-57-111 | MESH GASKETS FOR FUEL TANK ACCESS DOORS |
| AFB | P8-SL-20-0043 | INCORRECT CONNECTOR IDENTIFICATION SLEEVES - WIRE HARNESS W7693 |
| AFB | P8-SL-20-0044 | INCORRECT CONNECTOR IDENTIFICATION SLEEVES - WIRE HARNESS W8702 |
| AFB | P8-SL-20-0045 | INCORRECT CONNECTOR IDENTIFICATION SLEEVES -WIRE HARNESS W8765 |
| AFB | 737-SL-28-086-D | P/N 343A2212-3/-4 WATER SCAVENGE TUBE CLEARANCE |
| AFB | P8-SL-57-0016 | POTENTIAL UNINSTALLED COUNTERBORE WASHERS COMMON TO RADIUS LEAD-IN BOLT AT THE FRONT SPAR CHORD WEB JOINT |
| P-8-AFC-22 | IDP–03466-045 | P-8A MODIFICATION OF ONBOARD INERT GAS GENERATING SYSTEM (OBIGGS) EQUIPMENT (OOMA WUC 1000000) |
| P-8-AFC-23 REV A | IDP-03489-001 Rev A, | P-8A HEATING SYSTEM, WEAPONS BAY TEMPERATURE CONTROL (OOMA WUC 1000000) |
| P-8-AFC-41 | IDP-03614-001 | P-8A RIGHT WING LEADING EDGE, WIRE BUNDLE INSTALLATIONS W1142 AND W1146, MODIFICATION OF (OOMA WUC 1000000 |
| P-8-AFC-43 | IDP-03628-001 | P-8A SPECIAL MISSION POD (SMP) POWER FEEDER CONNECTORS, REPLACEMENT OF (OOMA WUC 1000000) |
| P-8-AFC-46 | IDP-03574-001 Rev A, | P-8A WEAPONS BAY HEAT SYSTEM, MODIFICATIONS OF (OOMA WUC 1000000). |
| P-8-AFC-47 | IDP-03964-001 Rev A, | P-8A WEAPONS BAY DOOR SEALS, MODIFICATIONS OF (OOMA WUC 1000000) |
| P-8-AFC-48 REV A | IDP-03574-001 Rev A | P-8A WEAPONS BAY HEAT, DUCTING SYSTEM, MODIFICATION OF (OOMA WUC 1000000) |
| P-8-AFC-49 | IDP-03665-001 | P-8A WIRING RACEWAY TIE-ROD INSTALLATION; MODIFICATION OF (OOMA WUC 1000000). |
| P-8-AFC-51 | IDP-03873-001 Rev B | P-8A P5 PANEL, WIRE BUNDLE, MODIFICATION OF (OOMA WUC 1000000). |
| P-8-AFC-52 | IDP-03793-001 | P-8A AUXILIARY POWER UNIT (APU) WIRE BUNDLE; MODIFICATION OF (OOMA WUC 1000000). |
| P-8-AFC-53 | IDP-03874-001 | P-8A RIGHT WING LEADING EDGE WIRE BUNDLE, MODIFICATION OF (OOMA WUC 1000000). |
| P-8-AFC-54 | IDP-03875-001 | P-8A LOWER LOBE, SECTION 41, RACEWAY WIRING AND BRACKETS; MODIFICATION OF (OOMA WUC 1000000). |
| P-8-AFC-55 | IDP-03878-001 | P-8A WEAPONS BAY, WIRE BUNDLE W8719 AND PNEUMATIC TUBE P/N 212A4651-1, LOOP CLAMP; MODIFICATION OF (OOMA WUC 1000000). |
| P-8-AFC-57 | IDP-03759-001 | P-8A FLIGHT MANAGEMENT COMPUTER (FMC) DUAL IN-LINE PACKAGE (DIP) SWITCH, RETROFIT OF (OOMA WUC 1000000). |
| P-8-AFC-59 | IDP-03958-001 | P-8A FLIGHT DECK WIRE BUNDLE ROUTING, MODIFICATION OF (OOMA WUC 1000000). |
| P-8-AFC-65 REV A | IDP-04418-001 Rev A | P-8A DATA STORAGE ARCHITECTURE UPDATE (DSAU), INSTALLATION OF (OOMA WUC 1000000). Several Amendments in this change affect BUNO's differently. |
| P-8-AFC-68 | IDP-03622-001 | P-8A FWD, AFT AND AUX FUEL TANK 10 FILL ORIFICES, REPLACEMENT OF (OOMA WUC 1000000) |
| P-8-AFC-72 | IDP-04537-001 | P-8A MULTI-MISSION MARITIME AIRCRAFT (MMA) INCREMENT 2 CAPABILITY, INSTALLATION OF (OOMA WUC 1000000) Many amendments to this AFC |
| P-8-AFC-75 | IDP-04736-001 Rev A | P-8A EARLY WARNING AND SELF PROTECTION (EWSP) 6TH SENSOR, INSTALLATION OF (OOMA WUC 1000000) |
| P-8-AFC-50 | IDP-03785-001 | P-SA DRY BAY FIRE PROTECTION SYSTEM (DBFPS) WIRE BUNDLE CLAMP, MODIFICATION OF Many amendments to this AFC |
| AFC-56 | IDP-03988-001 Rev B | P-8A WING TANK, FUEL QUANTITY INDICATING SYSTEM (FQIS) WIRING AND TUBE ASSEMBLY; MODIFICATION OF Includes both A1 and A2 |
| P-8-AFC-84 | IDP-04000-001 | P-8A FUEL QUANTITY INDICATING SYSTEM, MODIFICATION OF (25 BUNO Block I and 13 BUNO Block2) concurrently with AVC-5938, and subsequent to or concurrently with AVC-5923 and AVC-5924. |
| AFC-40 | IDP-03664-001 | P-8A FWD, AFT AND AUX FUEL TANK 10 FILL ORIFICES, REPLACEMENT |
N00019-15-R-2004 &"-,Bold"&24Technical Directives List Part A Attachment 8
&P
File details come from the government source that posted it. Updated .