Att_L-9_Prime_Contractor_Tech_Directives_FFP_Amendment_4.xlsx
XLSX spreadsheet 418 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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L-9 Prime Contractor Tech Directive FFP, Amendment 03 N00019-15-R-2004
&F Page &P of &N Print Date: &D
The Summary tab is a rollup of the other tabs and will automatically populate.
Within each tab, fill in the Subcontractor Price for each Techincal Directive (TD) and the Prime Price for each. If there is more than one Principal Subcontractor/JV team member, insert additional columns as neccessary for all additional Principal Subcontractors/JV team members. Replace "Sub Contractor #1" with the name of the Subcontractor/JV team member.
For Concurrent with AEPD TDs, Induction and Delivery costs should already be included in the price for AEPD events (CLINs x002, x003, x007, x008, and x030).
For Drop-In TDs, the associated Induction and Delivery costs will be included in CLINs x020, x021, and x033.
For In-Field TDs, there should be no Induction or Delivery costs.
Totals per each Option Period (sum of all TDs with the applied quantities) at the bottom of the Summary tab shall be used on Attachment L-7 [Prime Contractor Cost Summary FFP].
Fill out applicable part(s) in accordance with proposal(s) being submitted (Part A – Airframe (CLINs X001-X046), Part B – Engine (CLINs X060-X112), and/or Combined).
Executive Summary
| CLIN | CLIN Description | Location | BASE PERIOD | Option Period 1 | Option Period 2 | Option Period 3 | Option Period 4 | Option Period 5 | Option Period 6 | Row Labels | Sum of BASE PERIOD2 | Sum of Option Period 12 | Sum of Option Period 22 | Sum of Option Period 32 | Sum of Option Period 42 | Sum of Option Period 52 | Sum of Option Period 62 |
| X013 | Technical Directives, Modifications and Retrofit | Concurrent with AEPD | 263 | 237 | 84 | 48 | 7 | 0 | 0 | Concurrent with AEPD | 263 | 237 | 84 | 48 | 7 | 61 | 61 |
| X013 | Technical Directives, Modifications and Retrofit | Drop-In | 61 | 61 | 61 | 61 | 61 | 61 | 61 | CLIN X013 - Concurrent with AEPD | 263 | 237 | 84 | 48 | 7 | 0 | 0 |
| X013 | Technical Directives, Modifications and Retrofit | In-Field | 61 | 61 | 61 | 61 | 61 | 61 | 61 | CLIN X035 - Concurrent with AEPD | 0 | 0 | 0 | 0 | 0 | 61 | 61 |
| X035 | RAAF Technical Directives, Modifications and Retrofits | Concurrent with AEPD | 0 | 0 | 0 | 0 | 0 | 61 | 61 | Drop-In | 61 | 61 | 61 | 61 | 61 | 122 | 122 |
| X035 | RAAF Technical Directives, Modifications and Retrofits | Drop-In | 0 | 0 | 0 | 0 | 0 | 61 | 61 | CLIN X013 - Drop-in | 61 | 61 | 61 | 61 | 61 | 61 | 61 |
| X035 | RAAF Technical Directives, Modifications and Retrofits | In-Field | 0 | 0 | 0 | 0 | 0 | 61 | 61 | CLIN X035 - Drop-In | 0 | 0 | 0 | 0 | 0 | 61 | 61 |
| X082 | Technical Directive Incorporation Engine | Concurrent with Engine Induction for Repair | 203 | 232 | 319 | 406 | 464 | 522 | 638 | In-Field | 61 | 61 | 61 | 61 | 61 | 122 | 122 |
| X099 | Technical Directive Incorporation Engine | Concurrent with Engine Induction for Repair | 29 | 29 | 29 | 58 | 58 | 58 | 58 | CLIN X013 - In-Field | 61 | 61 | 61 | 61 | 61 | 61 | 61 |
| CLIN X035 - In-Field | 0 | 0 | 0 | 0 | 0 | 61 | 61 | ||||||||||
| X013 | Technical Directives, Modifications and Retrofit | All locations | 385 | 359 | 206 | 170 | 129 | 122 | 122 | Concurrent with Engine Induction for Repair | 232 | 261 | 348 | 464 | 522 | 580 | 696 |
| X035 | RAAF Technical Directives, Modifications and Retrofits | All locations | 0 | 0 | 0 | 0 | 0 | 183 | 183 | CLIN X082 - Concurrent with Engine Induction for Repair | 203 | 232 | 319 | 406 | 464 | 522 | 638 |
| X082 | Technical Directive Incorporation Engine | All locations | 203 | 232 | 319 | 406 | 464 | 522 | 638 | CLIN X099 - Concurrent with Engine Induction for Repair | 29 | 29 | 29 | 58 | 58 | 58 | 58 |
| X099 | Technical Directive Incorporation Engine | All locations | 29 | 29 | 29 | 58 | 58 | 58 | 58 | Grand Total | 617 | 620 | 554 | 634 | 651 | 885 | 1001 |
| Color Code Legend | |||||||||||||||||
| Aircraft - US Navy only | |||||||||||||||||
| Aircraft - RAAF only | |||||||||||||||||
| Engine - Combined US Navy, RAAF, FMS |
L-9 Prime Contractor Tech Directive FFP, Amendment 03 N00019-15-R-2004
&F Page &P of &N Print Date: &D
Summary
| TOTAL FFP COST Per SLIN | ||||||||||||||||||||||||||||
| SLIN | SERVICE LETTER / SERVICE BULLETIN / SB-ATA-Number | TD Type | DESCRIPTION | WORK LOCATION | UNIT | BASE PERIOD | Option Period 1 | Option Period 2 | Option Period 3 | Option Period 4 | Option Period 5 | Option Period 6 | BASE PERIOD | Option Period 1 | Option Period 2 | Option Period 3 | Option Period 4 | Option Period 5 | Option Period 6 | BASE PERIOD | Option Period 1 | Option Period 2 | Option Period 3 | Option Period 4 | Option Period 5 | Option Period 6 | ||
| X013AA | P8 -SL-53-0053 | AFB | MISSING FASTENERS ON SILL NEAR THE LOWER OF FORWARD CARGO DOOR CORNERS | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 6 | 3 | 0 | 0 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013AB | P8-SL-53-0057 | AFB | Four missing fasteners at STA 479 | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 7 | 8 | 0 | 0 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013AC | P8-SL-51-0002 | AFB | P-8A – Non-Conforming BSAA and Primer Adhesion Parts From TC Systems | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 0 | 0 | 0 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013AD | P8-SL-53-008 R1 | AFB | Inspect and Rework Temporary Fasteners Installed in Frame 500F (Forward Cargo Compartment) Possible tie to CP 3984 | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 2 | 0 | 0 | 0 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013AE | P8-SL-20-0041 | AFB | ELECTRICAL CONNECTOR BACKSHELLS POTENTIALLY MISSING PROTECTIVE BARRIER TAPE IN THE OUTER FRONT SPAR AND WING TIPS | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 7 | 8 | 4 | 0 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013AF | 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 | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 2 | 0 | 0 | 0 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013AG | P8-SL-53-0051 | AFB | POSSIBLE MISSING FASTENERS | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 7 | 3 | 0 | 0 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013AH | P8-SL-28-0012 | AFB | AUXILIARY FUEL TANKS INTERSPACE DEBRIS CONTAINMENT | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 7 | 0 | 0 | 0 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013AI | P8-SL-53-0052 | AFB | RIDING CONDITION BETWEEN BRACKET AND HEAD OF HI LOKS | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 7 | 6 | 0 | 0 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013AJ | P8-SL-99-0002 | AFB | EARLY WARNING & SELF PROTECTION (EWSP) - WIRE BUNDLE -W9317 CONNECTOR MS3459W32-6S CONTACT RETENTION DEFICIENCY | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 0 | 0 | 0 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013AK | P8-SL-47-0004 | AFB | ON BOARD INERT GAS GENERATING SYSTEM (OBIGGS) ELECTRICAL CONNECTORS POTENTIALLY CLOCKED INCORRECTLY | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 7 | 8 | 0 | 0 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013AL | 737-SL-53-103-A | AFB | BS 578 TO 639 STUB BEAM FASTENERS MISSING COUNTER BORE WASHER | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 2 | 6 | 0 | 0 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013AM | 737-SL-57-0106-A | AFB | LH AND RH WING NACELLE SUPPORT OUTBOARD SIDELOAD BACKUP FITTING – MISSING FILLET SEAL | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 7 | 7 | 0 | 0 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013AN | P8-SL-28-0014 | AFB | UARRSI PARTS NOT PRIMED IAW MIL-STD-889 | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 7 | 6 | 0 | 0 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013AO | P8-SL-53-0009-A | AFB | FUSELAGE – FLOOR BEAM – RIDING CONDITION BETWEEN FASTENERS AND TUBE ASSEMBLY | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 5 | 7 | 2 | 0 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013AP | RESERVED | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 0 | 0 | 0 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |||
| X013AQ | P8-SL-53-0024 | AFB | P-8A – Inspection and Rework Incorrect Channel Frame and Bulkhead Surfaces | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 2 | 0 | 0 | 0 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013AR | 737-SL-27-227 | AFB | RUDDER FEEL AND CENTERING INSTALLATION – FASTENERS UNDERTORQUED | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 0 | 0 | 0 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013AS | 737-SL-28-080-A | AFB | POTENTIAL UNDER-TORQUED FUEL SUMP DRAIN AND AN UNDER-TORQUED BULKHEAD FITTING NUT | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 2 | 0 | 0 | 0 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013AT | P8-SL-20-0038 | AFB | WIRE BUNDLE IMPROPERLY SECURED ALONG MISSION EQUIPMENT COOLING DUCT | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 0 | 0 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013AU | 737-SL-55-019-E | AFB | VERTICAL STABILIZER REAR SPAR SHIM MIGRATION | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 7 | 8 | 2 | 0 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013AV | P8-SL-53-0061 | AFB | SECTION 41 ELONGATED FASTENER HOLES COMMON TO STRINGERS | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 4 | 1 | 0 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013AW | P8-SL-57-0015 | AFB | DISCREPANT SHORT FLAP FAIRING RIVETS | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 7 | 6 | 0 | 0 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013AX | P8-SL-53-0082 | AFB | STA 178 BULKHEAD CLIP ASSEMBLIES MAY HAVE ELONGATED RIVET HOLES | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 7 | 8 | 5 | 0 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013AY | 737-SL-32-198-A | AFB | WIRES POTENTIALLY CONTACTING MAIN LANDING GEAR (MLG) | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 7 | 8 | 6 | 0 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013AZ | P8-SL-53-0067 | AFB | POTENTIALLY UNINSTALLED RIVETS AT STA 727E AND 727F | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 2 | 0 | 0 | 0 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013BA | P8-SL-28-0030 | AFB | AERIAL REFUELING DRAIN FITTING MISALIGNED YP004, YP006-YP031 will require the removal of the G2 Galley | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 7 | 8 | 6 | 6 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013BB | P8-SL-99-0005 | AFB | RADAR WARNING RECEIVER (RWR) OMNI BLADE ANTENNA FASTENER OVER-TORQUE | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 4 | 0 | 0 | 0 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013BC | P8-SL-96-0015 | AFB | STORES MANAGEMENT SYSTEM (SMS) CONNECTOR DISCREPANCY | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 0 | 1 | 0 | 0 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013BD | P8-SL-53-0058 | AFB | GAP CONDITION BETWEEN FRAME AND INTERCOSTAL | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 7 | 8 | 0 | 0 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013BE | P8-SL-53-0070-A | AFB | 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 | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 7 | 8 | 6 | 2 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | ||||
| X013BF | P8-SL-21-0021-A | AFB | ELECTRONIC SUPPORT MEASURES (ESM) FORWARD ARRAY COOLING LINE MAY BE RIDING AGAINST PROTECTIVE SHROUD Below decking. (222AF) Requies oxygen cabinet removal. | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 6 | 8 | 6 | 4 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013BG | P8-SL-53-0093 | AFB | SECTION 44 POTENTIALLY DISCREPANT FASTENER TAIL HEIGHTS | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 7 | 8 | 2 | 0 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013BH | P8-SL-53-0062 | AFB | POTENTIALLY DISBONDED NUTPLATES IN THE NOSE LANDING GEAR WHEEL WELL | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 5 | 6 | 0 | 0 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013BI | P8-SL-51-0004 | AFB | MASKING APPLIED IN INCORRECT LOCATION ON 111A6202-402 LOWER CHORD | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 6 | 6 | 0 | 0 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013BJ | P8-SL-53-0007 | AFB | P-8A – Inspection and Rework Scuff Plate Installation on Forward Cargo Door | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 0 | 0 | 0 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013BK | P8-SL-53-0038-A | AFB | SECTION 43 AFT PRESSURE BOX MISSING FASTENERS | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 7 | 2 | 0 | 0 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013BL | P8-SL-53-0039 | AFB | LEFT AFT WING-TO-BODY PANEL FASTENER NUTPLATE IS DAMAGED | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 0 | 1 | 0 | 0 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013BM | P8-SL-53-0050 | AFB | POSSIBLE MISSING SEALANT ON FASTENERS | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 7 | 7 | 0 | 0 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013BN | P8-SL-53-0059 | AFB | BODY FITTING BRACKET MAY BE INSTALLED INCORRECTLY | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 7 | 8 | 2 | 0 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013BO | P8-SL-53-0063 | AFB | DISCREPANT FASTENERS COMMON TO SKIN, FRAME AND INTERCOSTAL | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 7 | 8 | 3 | 0 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013BP | P8-SL-53-0015-A | AFB | OPEN HOLE IN STRUCTURE – MISSING FASTENER | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 2 | 0 | 0 | 0 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013BQ | P8-SL-53-0047 | AFB | POTENTIAL OF THREE UNINSTALLED FUSELAGE RIVETS IN SECTION 48 | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 7 | 3 | 0 | 0 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013BR | P8-SL-21-0001 | AFB | Incorrect fasteners issued and installed | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 0 | 0 | 0 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013BS | P8-SL-57-0002 | AFB | Inspection of Suspect Fastener Installations | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 0 | 0 | 0 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013BT | 737-SL-57-108 | AFB | FRONT SPAR LEADING EDGE STRAP CORROSION PREVENTION | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 4 | 0 | 0 | 0 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013BU | P8-SL-53-0088 | AFB | POTENTIAL RIDING FASTENER CONDITION AND TOOL MARK DAMAGE Requires MID Tank Group (MTG) 7 and 8 removal | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 0 | 0 | 0 | 1 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013BV | P8-SL-53-0089 | AFB | ADVANCED AIRBORNE SYSTEM (AAS) ALTERNATE RETRACT SYSTEM (ARS) – AIRFRAME TO ARS INTERFACE ISSUE Remove Auxiliary Fuel Tank No. 4 is optional. Seems workable with tank in place. | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 0 | 0 | 6 | 3 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013BW | P8-SL-51-0007 | AFB | POST-ASSEMBLY BRUSH SEALING APPLICATION FOR WTBF FASTENERS | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 7 | 1 | 0 | 0 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013BX | P8-SL-53-0076 | AFB | RIDING FILLER | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 7 | 8 | 6 | 2 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013BY | P8-SL-53-0084-A | AFB | POTENTIAL SURFACE DAMAGE AT FLOOR BEAM STIFFENER | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 7 | 8 | 5 | 2 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013BZ | P8-SL-57-0016 | AFB | POTENTIAL UNINSTALLED COUNTERBORE WASHERS COMMON TO RADIUS LEAD-IN BOLT AT THE FRONT SPAR CHORD WEB JOINT | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 7 | 8 | 6 | 6 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013CA | P8-SL-28-0029 | AFB | AFT INTEGRAL FUEL TANK VENT/TRANSFER TUBE PRESSURE RELIEF VALVE - PROTECTIVE CAP | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 7 | 8 | 6 | 6 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013CB | P8-SL-53-0085-A | AFB | DISCREPANT MACHINED FAILSAFE STRAPS RESULTING IN POTENTIAL GAPS BETWEEN FRAME AND SKIN | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 7 | 8 | 2 | 0 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013CC | P8-SL-23-0019 | AFB | FOKKER-ELMO NOTICE OF ESCAPEMENT (NOE) - SUSPECT BACKSHELL ON WIRE HARNESS W0865 RECEPTACLE D5228J | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 0 | 0 | 0 | 3 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013CD | P8-SB-28-0002 | AFB | Pressure Fueling System - Fill Valve Adapter Shaft Assembly - Inspection and Replacement (Should be a SL to inspect for cracked adapter plates) | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 0 | 1 | 0 | 0 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013CE | P8-SL-52-0024 | AFB | POTENTIAL SEALANT VOIDS COMMON TO AFT BAILOUT DOOR REVEAL INSTALLATION | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 7 | 8 | 6 | 13 | 7 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013CF | P8-SL-51-0008 | AFB | POTENTIAL UNAPPLIED CORROSION INHIBITING COMPOUND (CIC) ON SEAT TRACK STRUCTURE | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 5 | 8 | 2 | 0 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013CG | P-8-AFC-22 | AFC | P-8A MODIFICATION OF ONBOARD INERT GAS GENERATING SYSTEM (OBIGGS) EQUIPMENT (OOMA WUC 1000000) (TCD 31 December 2018) | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 0 | 0 | 0 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013CH | P-8-AFC-49 | AFC | P-8A WIRING RACEWAY TIE-ROD INSTALLATION; MODIFICATION OF (OOMA WUC 1000000). (TCD 30 June 2022) | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 0 | 0 | 0 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013CI | P-8-AFC-68 | AFC | P-8A FWD, AFT AND AUX FUEL TANK 10 FILL ORIFICES, REPLACEMENT OF (OOMA WUC 1000000) (TCD 31 December 2018) | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 0 | 0 | 0 | 0 | 0 | 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013CJ | P8 -SL-53-0053 | AFB | MISSING FASTENERS ON SILL NEAR THE LOWER OF FORWARD CARGO DOOR CORNERS | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013CK | P8-SL-53-0057 | AFB | Four missing fasteners at STA 479 | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013CL | P8-SL-51-0002 | AFB | P-8A – Non-Conforming BSAA and Primer Adhesion Parts From TC Systems | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013CM | P8-SL-53-008 R1 | AFB | Inspect and Rework Temporary Fasteners Installed in Frame 500F (Forward Cargo Compartment) Possible tie to CP 3984 | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013CN | P8-SL-20-0041 | AFB | ELECTRICAL CONNECTOR BACKSHELLS POTENTIALLY MISSING PROTECTIVE BARRIER TAPE IN THE OUTER FRONT SPAR AND WING TIPS | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013CO | 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 | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013CP | P8-SL-53-0051 | AFB | POSSIBLE MISSING FASTENERS | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013CQ | P8-SL-28-0012 | AFB | AUXILIARY FUEL TANKS INTERSPACE DEBRIS CONTAINMENT | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013CR | P8-SL-53-0052 | AFB | RIDING CONDITION BETWEEN BRACKET AND HEAD OF HI LOKS | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013CS | P8-SL-99-0002 | AFB | EARLY WARNING & SELF PROTECTION (EWSP) - WIRE BUNDLE -W9317 CONNECTOR MS3459W32-6S CONTACT RETENTION DEFICIENCY | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013CT | P8-SL-47-0004 | AFB | ON BOARD INERT GAS GENERATING SYSTEM (OBIGGS) ELECTRICAL CONNECTORS POTENTIALLY CLOCKED INCORRECTLY | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013CU | 737-SL-53-103-A | AFB | BS 578 TO 639 STUB BEAM FASTENERS MISSING COUNTER BORE WASHER | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013CV | 737-SL-57-0106-A | AFB | LH AND RH WING NACELLE SUPPORT OUTBOARD SIDELOAD BACKUP FITTING – MISSING FILLET SEAL | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013CW | P8-SL-28-0014 | AFB | UARRSI PARTS NOT PRIMED IAW MIL-STD-889 | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013CX | P8-SL-53-0009-A | AFB | FUSELAGE – FLOOR BEAM – RIDING CONDITION BETWEEN FASTENERS AND TUBE ASSEMBLY | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013CY | RESERVED | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |||
| X013CZ | P8-SL-53-0024 | AFB | P-8A – Inspection and Rework Incorrect Channel Frame and Bulkhead Surfaces | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013DA | 737-SL-27-227 | AFB | RUDDER FEEL AND CENTERING INSTALLATION – FASTENERS UNDERTORQUED | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013DB | 737-SL-28-080-A | AFB | POTENTIAL UNDER-TORQUED FUEL SUMP DRAIN AND AN UNDER-TORQUED BULKHEAD FITTING NUT | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013DC | P8-SL-20-0038 | AFB | WIRE BUNDLE IMPROPERLY SECURED ALONG MISSION EQUIPMENT COOLING DUCT | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013DD | 737-SL-55-019-E | AFB | VERTICAL STABILIZER REAR SPAR SHIM MIGRATION | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013DE | P8-SL-53-0061 | AFB | SECTION 41 ELONGATED FASTENER HOLES COMMON TO STRINGERS | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013DF | P8-SL-57-0015 | AFB | DISCREPANT SHORT FLAP FAIRING RIVETS | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013DG | P8-SL-53-0082 | AFB | STA 178 BULKHEAD CLIP ASSEMBLIES MAY HAVE ELONGATED RIVET HOLES | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013DH | 737-SL-32-198-A | AFB | WIRES POTENTIALLY CONTACTING MAIN LANDING GEAR (MLG) | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013DI | P8-SL-53-0067 | AFB | POTENTIALLY UNINSTALLED RIVETS AT STA 727E AND 727F | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013DJ | P8-SL-28-0030 | AFB | AERIAL REFUELING DRAIN FITTING MISALIGNED YP004, YP006-YP031 will require the removal of the G2 Galley | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013DK | P8-SL-99-0005 | AFB | RADAR WARNING RECEIVER (RWR) OMNI BLADE ANTENNA FASTENER OVER-TORQUE | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013DL | P8-SL-96-0015 | AFB | STORES MANAGEMENT SYSTEM (SMS) CONNECTOR DISCREPANCY | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013DM | P8-SL-53-0058 | AFB | GAP CONDITION BETWEEN FRAME AND INTERCOSTAL | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013DN | P8-SL-53-0070-A | AFB | 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 | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | ||||
| X013DO | P8-SL-21-0021-A | AFB | ELECTRONIC SUPPORT MEASURES (ESM) FORWARD ARRAY COOLING LINE MAY BE RIDING AGAINST PROTECTIVE SHROUD Below decking. (222AF) Requies oxygen cabinet removal. | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013DP | P8-SL-53-0093 | AFB | SECTION 44 POTENTIALLY DISCREPANT FASTENER TAIL HEIGHTS | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013DQ | P8-SL-53-0062 | AFB | POTENTIALLY DISBONDED NUTPLATES IN THE NOSE LANDING GEAR WHEEL WELL | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013DR | P8-SL-51-0004 | AFB | MASKING APPLIED IN INCORRECT LOCATION ON 111A6202-402 LOWER CHORD | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013DS | P8-SL-53-0007 | AFB | P-8A – Inspection and Rework Scuff Plate Installation on Forward Cargo Door | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013DT | P8-SL-53-0038-A | AFB | SECTION 43 AFT PRESSURE BOX MISSING FASTENERS | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013DU | P8-SL-53-0039 | AFB | LEFT AFT WING-TO-BODY PANEL FASTENER NUTPLATE IS DAMAGED | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013DV | P8-SL-53-0050 | AFB | POSSIBLE MISSING SEALANT ON FASTENERS | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013DW | P8-SL-53-0059 | AFB | BODY FITTING BRACKET MAY BE INSTALLED INCORRECTLY | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013DX | P8-SL-53-0063 | AFB | DISCREPANT FASTENERS COMMON TO SKIN, FRAME AND INTERCOSTAL | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013DY | P8-SL-53-0015-A | AFB | OPEN HOLE IN STRUCTURE – MISSING FASTENER | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013DZ | P8-SL-53-0047 | AFB | POTENTIAL OF THREE UNINSTALLED FUSELAGE RIVETS IN SECTION 48 | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013EA | P8-SL-21-0001 | AFB | Incorrect fasteners issued and installed | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013EB | P8-SL-57-0002 | AFB | Inspection of Suspect Fastener Installations | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013EC | 737-SL-57-108 | AFB | FRONT SPAR LEADING EDGE STRAP CORROSION PREVENTION | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013ED | P8-SL-53-0088 | AFB | POTENTIAL RIDING FASTENER CONDITION AND TOOL MARK DAMAGE Requires MID Tank Group (MTG) 7 and 8 removal | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013EE | P8-SL-53-0089 | AFB | ADVANCED AIRBORNE SYSTEM (AAS) ALTERNATE RETRACT SYSTEM (ARS) – AIRFRAME TO ARS INTERFACE ISSUE Remove Auxiliary Fuel Tank No. 4 is optional. Seems workable with tank in place. | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013EF | P8-SL-51-0007 | AFB | POST-ASSEMBLY BRUSH SEALING APPLICATION FOR WTBF FASTENERS | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013EG | P8-SL-53-0076 | AFB | RIDING FILLER | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013EH | P8-SL-53-0084-A | AFB | POTENTIAL SURFACE DAMAGE AT FLOOR BEAM STIFFENER | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013EI | P8-SL-57-0016 | AFB | POTENTIAL UNINSTALLED COUNTERBORE WASHERS COMMON TO RADIUS LEAD-IN BOLT AT THE FRONT SPAR CHORD WEB JOINT | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013EJ | P8-SL-28-0029 | AFB | AFT INTEGRAL FUEL TANK VENT/TRANSFER TUBE PRESSURE RELIEF VALVE - PROTECTIVE CAP | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013EK | P8-SL-53-0085-A | AFB | DISCREPANT MACHINED FAILSAFE STRAPS RESULTING IN POTENTIAL GAPS BETWEEN FRAME AND SKIN | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013EL | P8-SL-23-0019 | AFB | FOKKER-ELMO NOTICE OF ESCAPEMENT (NOE) - SUSPECT BACKSHELL ON WIRE HARNESS W0865 RECEPTACLE D5228J | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013EM | P8-SB-28-0002 | AFB | Pressure Fueling System - Fill Valve Adapter Shaft Assembly - Inspection and Replacement (Should be a SL to inspect for cracked adapter plates) | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013EN | P8-SL-52-0024 | AFB | POTENTIAL SEALANT VOIDS COMMON TO AFT BAILOUT DOOR REVEAL INSTALLATION | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013EO | P8-SL-51-0008 | AFB | POTENTIAL UNAPPLIED CORROSION INHIBITING COMPOUND (CIC) ON SEAT TRACK STRUCTURE | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013EP | P-8-AFC-22 | AFC | P-8A MODIFICATION OF ONBOARD INERT GAS GENERATING SYSTEM (OBIGGS) EQUIPMENT (OOMA WUC 1000000) (TCD 31 December 2018) | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013EQ | P-8-AFC-49 | AFC | P-8A WIRING RACEWAY TIE-ROD INSTALLATION; MODIFICATION OF (OOMA WUC 1000000). (TCD 30 June 2022) | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013ER | P-8-AFC-68 | AFC | P-8A FWD, AFT AND AUX FUEL TANK 10 FILL ORIFICES, REPLACEMENT OF (OOMA WUC 1000000) (TCD 31 December 2018) | Drop-In | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013ES | P8 -SL-53-0053 | AFB | MISSING FASTENERS ON SILL NEAR THE LOWER OF FORWARD CARGO DOOR CORNERS | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013ET | P8-SL-53-0057 | AFB | Four missing fasteners at STA 479 | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013EU | P8-SL-51-0002 | AFB | P-8A – Non-Conforming BSAA and Primer Adhesion Parts From TC Systems | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013EV | P8-SL-53-008 R1 | AFB | Inspect and Rework Temporary Fasteners Installed in Frame 500F (Forward Cargo Compartment) Possible tie to CP 3984 | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013EW | P8-SL-20-0041 | AFB | ELECTRICAL CONNECTOR BACKSHELLS POTENTIALLY MISSING PROTECTIVE BARRIER TAPE IN THE OUTER FRONT SPAR AND WING TIPS | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013EX | 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 | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013EY | P8-SL-53-0051 | AFB | POSSIBLE MISSING FASTENERS | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013EZ | P8-SL-28-0012 | AFB | AUXILIARY FUEL TANKS INTERSPACE DEBRIS CONTAINMENT | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013FA | P8-SL-53-0052 | AFB | RIDING CONDITION BETWEEN BRACKET AND HEAD OF HI LOKS | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013FB | P8-SL-99-0002 | AFB | EARLY WARNING & SELF PROTECTION (EWSP) - WIRE BUNDLE -W9317 CONNECTOR MS3459W32-6S CONTACT RETENTION DEFICIENCY | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013FC | P8-SL-47-0004 | AFB | ON BOARD INERT GAS GENERATING SYSTEM (OBIGGS) ELECTRICAL CONNECTORS POTENTIALLY CLOCKED INCORRECTLY | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013FD | 737-SL-53-103-A | AFB | BS 578 TO 639 STUB BEAM FASTENERS MISSING COUNTER BORE WASHER | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013FE | 737-SL-57-0106-A | AFB | LH AND RH WING NACELLE SUPPORT OUTBOARD SIDELOAD BACKUP FITTING – MISSING FILLET SEAL | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013FF | P8-SL-28-0014 | AFB | UARRSI PARTS NOT PRIMED IAW MIL-STD-889 | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013FG | P8-SL-53-0009-A | AFB | FUSELAGE – FLOOR BEAM – RIDING CONDITION BETWEEN FASTENERS AND TUBE ASSEMBLY | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013FH | RESERVED | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |||
| X013FI | P8-SL-53-0024 | AFB | P-8A – Inspection and Rework Incorrect Channel Frame and Bulkhead Surfaces | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013FJ | 737-SL-27-227 | AFB | RUDDER FEEL AND CENTERING INSTALLATION – FASTENERS UNDERTORQUED | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013FK | 737-SL-28-080-A | AFB | POTENTIAL UNDER-TORQUED FUEL SUMP DRAIN AND AN UNDER-TORQUED BULKHEAD FITTING NUT | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013FL | P8-SL-20-0038 | AFB | WIRE BUNDLE IMPROPERLY SECURED ALONG MISSION EQUIPMENT COOLING DUCT | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013FM | 737-SL-55-019-E | AFB | VERTICAL STABILIZER REAR SPAR SHIM MIGRATION | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013FN | P8-SL-53-0061 | AFB | SECTION 41 ELONGATED FASTENER HOLES COMMON TO STRINGERS | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013FO | P8-SL-57-0015 | AFB | DISCREPANT SHORT FLAP FAIRING RIVETS | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013FP | P8-SL-53-0082 | AFB | STA 178 BULKHEAD CLIP ASSEMBLIES MAY HAVE ELONGATED RIVET HOLES | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013FQ | 737-SL-32-198-A | AFB | WIRES POTENTIALLY CONTACTING MAIN LANDING GEAR (MLG) | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013FR | P8-SL-53-0067 | AFB | POTENTIALLY UNINSTALLED RIVETS AT STA 727E AND 727F | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013FS | P8-SL-28-0030 | AFB | AERIAL REFUELING DRAIN FITTING MISALIGNED YP004, YP006-YP031 will require the removal of the G2 Galley | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013FT | P8-SL-99-0005 | AFB | RADAR WARNING RECEIVER (RWR) OMNI BLADE ANTENNA FASTENER OVER-TORQUE | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013FU | P8-SL-96-0015 | AFB | STORES MANAGEMENT SYSTEM (SMS) CONNECTOR DISCREPANCY | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013FV | P8-SL-53-0058 | AFB | GAP CONDITION BETWEEN FRAME AND INTERCOSTAL | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013FW | P8-SL-53-0070-A | AFB | 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 | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | ||||
| X013FX | P8-SL-21-0021-A | AFB | ELECTRONIC SUPPORT MEASURES (ESM) FORWARD ARRAY COOLING LINE MAY BE RIDING AGAINST PROTECTIVE SHROUD Below decking. (222AF) Requies oxygen cabinet removal. | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013FY | P8-SL-53-0093 | AFB | SECTION 44 POTENTIALLY DISCREPANT FASTENER TAIL HEIGHTS | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013FZ | P8-SL-53-0062 | AFB | POTENTIALLY DISBONDED NUTPLATES IN THE NOSE LANDING GEAR WHEEL WELL | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013GA | P8-SL-51-0004 | AFB | MASKING APPLIED IN INCORRECT LOCATION ON 111A6202-402 LOWER CHORD | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013GB | P8-SL-53-0007 | AFB | P-8A – Inspection and Rework Scuff Plate Installation on Forward Cargo Door | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013GC | P8-SL-53-0038-A | AFB | SECTION 43 AFT PRESSURE BOX MISSING FASTENERS | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013GD | P8-SL-53-0039 | AFB | LEFT AFT WING-TO-BODY PANEL FASTENER NUTPLATE IS DAMAGED | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013GE | P8-SL-53-0050 | AFB | POSSIBLE MISSING SEALANT ON FASTENERS | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013GF | P8-SL-53-0059 | AFB | BODY FITTING BRACKET MAY BE INSTALLED INCORRECTLY | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013GG | P8-SL-53-0063 | AFB | DISCREPANT FASTENERS COMMON TO SKIN, FRAME AND INTERCOSTAL | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013GH | P8-SL-53-0015-A | AFB | OPEN HOLE IN STRUCTURE – MISSING FASTENER | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013GI | P8-SL-53-0047 | AFB | POTENTIAL OF THREE UNINSTALLED FUSELAGE RIVETS IN SECTION 48 | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013GJ | P8-SL-21-0001 | AFB | Incorrect fasteners issued and installed | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013GK | P8-SL-57-0002 | AFB | Inspection of Suspect Fastener Installations | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013GL | 737-SL-57-108 | AFB | FRONT SPAR LEADING EDGE STRAP CORROSION PREVENTION | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013GM | P8-SL-53-0088 | AFB | POTENTIAL RIDING FASTENER CONDITION AND TOOL MARK DAMAGE Requires MID Tank Group (MTG) 7 and 8 removal | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013GN | P8-SL-53-0089 | AFB | ADVANCED AIRBORNE SYSTEM (AAS) ALTERNATE RETRACT SYSTEM (ARS) – AIRFRAME TO ARS INTERFACE ISSUE Remove Auxiliary Fuel Tank No. 4 is optional. Seems workable with tank in place. | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013GO | P8-SL-51-0007 | AFB | POST-ASSEMBLY BRUSH SEALING APPLICATION FOR WTBF FASTENERS | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013GP | P8-SL-53-0076 | AFB | RIDING FILLER | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013GQ | P8-SL-53-0084-A | AFB | POTENTIAL SURFACE DAMAGE AT FLOOR BEAM STIFFENER | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013GR | P8-SL-57-0016 | AFB | POTENTIAL UNINSTALLED COUNTERBORE WASHERS COMMON TO RADIUS LEAD-IN BOLT AT THE FRONT SPAR CHORD WEB JOINT | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013GS | P8-SL-28-0029 | AFB | AFT INTEGRAL FUEL TANK VENT/TRANSFER TUBE PRESSURE RELIEF VALVE - PROTECTIVE CAP | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013GT | P8-SL-53-0085-A | AFB | DISCREPANT MACHINED FAILSAFE STRAPS RESULTING IN POTENTIAL GAPS BETWEEN FRAME AND SKIN | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013GU | P8-SL-23-0019 | AFB | FOKKER-ELMO NOTICE OF ESCAPEMENT (NOE) - SUSPECT BACKSHELL ON WIRE HARNESS W0865 RECEPTACLE D5228J | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013GV | P8-SB-28-0002 | AFB | Pressure Fueling System - Fill Valve Adapter Shaft Assembly - Inspection and Replacement (Should be a SL to inspect for cracked adapter plates) | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013GW | P8-SL-52-0024 | AFB | POTENTIAL SEALANT VOIDS COMMON TO AFT BAILOUT DOOR REVEAL INSTALLATION | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013GX | P8-SL-51-0008 | AFB | POTENTIAL UNAPPLIED CORROSION INHIBITING COMPOUND (CIC) ON SEAT TRACK STRUCTURE | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013GY | P-8-AFC-22 | AFC | P-8A MODIFICATION OF ONBOARD INERT GAS GENERATING SYSTEM (OBIGGS) EQUIPMENT (OOMA WUC 1000000) (TCD 31 December 2018) | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013GZ | P-8-AFC-49 | AFC | P-8A WIRING RACEWAY TIE-ROD INSTALLATION; MODIFICATION OF (OOMA WUC 1000000). (TCD 30 June 2022) | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X013HA | P-8-AFC-68 | AFC | P-8A FWD, AFT AND AUX FUEL TANK 10 FILL ORIFICES, REPLACEMENT OF (OOMA WUC 1000000) (TCD 31 December 2018) | In-Field | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X035AA | P8 -SL-53-0053 | AFB | MISSING FASTENERS ON SILL NEAR THE LOWER OF FORWARD CARGO DOOR CORNERS | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 0 | 0 | 0 | 0 | 0 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X035AB | P8-SL-53-0057 | AFB | Four missing fasteners at STA 479 | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 0 | 0 | 0 | 0 | 0 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X035AC | P8-SL-51-0002 | AFB | P-8A – Non-Conforming BSAA and Primer Adhesion Parts From TC Systems | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 0 | 0 | 0 | 0 | 0 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X035AD | P8-SL-53-008 R1 | AFB | Inspect and Rework Temporary Fasteners Installed in Frame 500F (Forward Cargo Compartment) Possible tie to CP 3984 | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 0 | 0 | 0 | 0 | 0 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X035AE | P8-SL-20-0041 | AFB | ELECTRICAL CONNECTOR BACKSHELLS POTENTIALLY MISSING PROTECTIVE BARRIER TAPE IN THE OUTER FRONT SPAR AND WING TIPS | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 0 | 0 | 0 | 0 | 0 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X035AF | 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 | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 0 | 0 | 0 | 0 | 0 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X035AG | P8-SL-53-0051 | AFB | POSSIBLE MISSING FASTENERS | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 0 | 0 | 0 | 0 | 0 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X035AH | P8-SL-28-0012 | AFB | AUXILIARY FUEL TANKS INTERSPACE DEBRIS CONTAINMENT | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 0 | 0 | 0 | 0 | 0 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X035AI | P8-SL-53-0052 | AFB | RIDING CONDITION BETWEEN BRACKET AND HEAD OF HI LOKS | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 0 | 0 | 0 | 0 | 0 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X035AJ | P8-SL-99-0002 | AFB | EARLY WARNING & SELF PROTECTION (EWSP) - WIRE BUNDLE -W9317 CONNECTOR MS3459W32-6S CONTACT RETENTION DEFICIENCY | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 0 | 0 | 0 | 0 | 0 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X035AK | P8-SL-47-0004 | AFB | ON BOARD INERT GAS GENERATING SYSTEM (OBIGGS) ELECTRICAL CONNECTORS POTENTIALLY CLOCKED INCORRECTLY | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 0 | 0 | 0 | 0 | 0 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X035AL | 737-SL-53-103-A | AFB | BS 578 TO 639 STUB BEAM FASTENERS MISSING COUNTER BORE WASHER | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 0 | 0 | 0 | 0 | 0 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X035AM | 737-SL-57-0106-A | AFB | LH AND RH WING NACELLE SUPPORT OUTBOARD SIDELOAD BACKUP FITTING – MISSING FILLET SEAL | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 0 | 0 | 0 | 0 | 0 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X035AN | P8-SL-28-0014 | AFB | UARRSI PARTS NOT PRIMED IAW MIL-STD-889 | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 0 | 0 | 0 | 0 | 0 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X035AO | P8-SL-53-0009-A | AFB | FUSELAGE – FLOOR BEAM – RIDING CONDITION BETWEEN FASTENERS AND TUBE ASSEMBLY | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 0 | 0 | 0 | 0 | 0 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X035AP | RESERVED | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 0 | 0 | 0 | 0 | 0 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |||
| X035AQ | P8-SL-53-0024 | AFB | P-8A – Inspection and Rework Incorrect Channel Frame and Bulkhead Surfaces | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 0 | 0 | 0 | 0 | 0 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X035AR | 737-SL-27-227 | AFB | RUDDER FEEL AND CENTERING INSTALLATION – FASTENERS UNDERTORQUED | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 0 | 0 | 0 | 0 | 0 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X035AS | 737-SL-28-080-A | AFB | POTENTIAL UNDER-TORQUED FUEL SUMP DRAIN AND AN UNDER-TORQUED BULKHEAD FITTING NUT | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 0 | 0 | 0 | 0 | 0 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X035AT | P8-SL-20-0038 | AFB | WIRE BUNDLE IMPROPERLY SECURED ALONG MISSION EQUIPMENT COOLING DUCT | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 0 | 0 | 0 | 0 | 0 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X035AU | 737-SL-55-019-E | AFB | VERTICAL STABILIZER REAR SPAR SHIM MIGRATION | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 0 | 0 | 0 | 0 | 0 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X035AV | P8-SL-53-0061 | AFB | SECTION 41 ELONGATED FASTENER HOLES COMMON TO STRINGERS | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 0 | 0 | 0 | 0 | 0 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X035AW | P8-SL-57-0015 | AFB | DISCREPANT SHORT FLAP FAIRING RIVETS | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 0 | 0 | 0 | 0 | 0 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | |
| X035AX | P8-SL-53-0082 | AFB | STA 178 BULKHEAD CLIP ASSEMBLIES MAY HAVE ELONGATED RIVET HOLES | Concurrent with AEPD | FFP | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | 0 | 0 | 0 | 0 | 0 | 1 | 1 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 | $ - 0 |
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