N975FD

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,698 hrs · 23,523 cycles

LEFT EXTERIOR EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED THE BULB IAW MM 33-50-2610. OPS CHECKED NORMAL.

Part: B-NUT — NOT SEATED (HYDRAULIC SYS) · airframe 62,380 hrs · 23,288 cycles

REACHING CRUISE FL390, RECEIVED RT HYDRAULIC QTY EICAS STATUS MESSAGES SHOWED 0.49 AND DECREASING SLOWLY. COMPLIED WITH QRH. RESERVOIR LIGHT ON OVERHEAD PANEL ALSO CAME ON. ON DESCENT AT 10000' RECEIVED RT HYDRAULIC ENGINE PUMP ECIAS. COMPLIED WITH QRH AND TURNED OFF ENGINE PUMP. AT 2000', RECEIVED RT HYDRAULIC SYS PRESSURE EICAS. COMPLIED WITH QRH. QTY DROPPED TO 0.14. PRESSURE DROPPED TO 100 PSI. HEAVY LEAKAGE IN RT WHEELWELL AREA. LEAK COMING FROM FITTING B-NUT ON BOTTOM OF BRAKE ACCUMULATOR. REF IPC 32-44-05-01, ITEM 900. RESEATED AND SECURED SAME. SERVICED HYD SYS TO FULL REF AMM 12-12-01. PRESSURIZED HYD SYS. NO LEAKS NOTED FROM WHEELWELL AREA. INSPECTED ALL FILTER DPI'S FOR RT HYD SYSTEM. NONE EXTENDED, REF AMM 29-11-00-2. RAN ENGINGE IAW JRH CHAP6. ALL PARAMETERS AND INDICATIONS NORMAL PERFORMED HYDRAULIC LEAK CK ON ELEVATOR, HORIZONTAL STABILIZER AND RUDDER IAW AMM 27-23-00-0 AND 27-41-11-864-022. NO DEFECTS NOTED. OPERATED ALL 3 HYDRAULIC SYS FOR 30 MINUTES. NO FLUID LOSS WAS NOTED, OK FOR FLIGHT.

Part: WIRE — OPEN (L1 DOOR) · airframe 62,224 hrs · 23,181 cycles

L1 ENTRY DOOR SLIDE LIGHT WILL NOT ILLUMINATE WHEN DOOR IS ARMED. FOUND WIRE W3582-0015-20 OPEN AT GROUNDING TERMINAL. REPAIRED GND GD2916-AC AS REQUIRED. REF WDM 25-66-11 & SWP CH 20. L1 PAX DOOR GIRT BAR & LT OPERATIONS CHECKED NORMAL IAW MM 25-66-11-2-0.

Part: DOOR — JAMMED (CABIN) · airframe 62,144 hrs · 23,115 cycles

INBOUND CREW SOMEHOW OPENED RT NR 1 DOOR WHILE STILL ARMED & SLIDE GIRT BAR STILL ATTACHED TO THRESHOLD & DOOR WAS JAMMED IN THE MIDWAY POSITION. RT NR 1 PAX CABIN DOOR EMER POWER RESERVOIR PRESS DEPLETED, SLIDE INTACT. REMOVED CREW FROM LT NR 1 DOOR. R & R RT POWER RESERVOIR IAW MM 52-11-30-4.

Part: TRANSMISSION — LEAKING (TE FLAP) · airframe 62,126 hrs · 23,103 cycles

ON APPROACH RECEIVED TE FLAP DISAGREE. RAN QRH LANDED FLAPS 20. R & R, OPERATIONS CHECKED LT INBD TE FLAP TRANSMISSION IAW AMM 27-51-06-4.

Part: FITTING — OBSTRUCTED (GIRT BAR) · airframe 612 hrs · 22,473 cycles

ON ARRIVAL AFTER BLOCK IN NOTICE THE SLIDE LIGHT ON LT SIDE WAS OUT. INSPECTED L1 DOOR SLIDE GIRT BAR ATTACH FITTINGS. REMOVED DEBRIS FROM GIRT BAR FLOOR FITTINGS. CYCLED MODE SELECTOR LEVER ON DOOR SEVERAL TIMES. DOOR ARMS & SLIDE LIGHT OPERATIONS CHECKED GOOD IAW MM 52-11-00-0.

Part: GIRT BAR — MISINSTALLED (L1 DOOR) · airframe 60,943 hrs · 22,271 cycles

AT DEPARTURE L1 CABIN DOOR SLIDE LIGHT INOPERATIVE WHEN TRYING TO ARM DOOR PER CREW. SMP FOUND GIRT BAR NOT INSTALLED PROPERLY INTO RETAINERS. ATTACHED GIRT BAR IAW 52-11-25-5. GIRT BAR CHECKS GOOD. DOOR ARMING OPERATIONS CHECKS GOOD. CLEARED MEL.

Part: LIGHT — INOPERATIVE (L1 DOOR) · airframe 60,937 hrs · 22,267 cycles

DURING POST FLIGHT CHECK FOUND THAT THE L1 DOOR SLIDE ARM LIGHT DOES NOT ILLUMINATE WITH DOOR SLIDE ARMED. RELAMPED L1 DOOR SLIDE ARM LIGHT. SYS TESTS NORMAL, ACFT OK FOR SERVICE IAW AMM 52-11-00.

Part: SKIN PANEL — DENTED (TE FLAP) · airframe 60,768 hrs · 22,114 cycles

RIGHT INBD TE FLAP LOWER SURFACE HAS A DENT, 15 INCHES FROM OTBD EDGE, MFSTA 285. REPAIRED RT INBD TE MAIN FLAP LOWER SURFACE AS NEEDED IAW SRM 57-53-01. MEASURED NOTED DENT FOUND TO BE OUT OF LIMITS IAW SRM 57-53-01. RT INBD TE MAIN FLAP LOWER SURFACE REPAIRED IAW SRM 57-53-01 & REPAIR PROCESS SRM 51-70-10, REPAIR 2. EA F-5750-T0306721 COMPLIED WITH FOR TRACKING. MAJOR REPAIR.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 60,768 hrs · 22,114 cycles

LT WING UPPER SKIN AT EDGE OF BODY SPLICE CORRODED. REPAIRED IAW EA F-5730-T0307309, STEPS 1 - 9, PT 1.

Part: STRUCTURE — CHAFED (CARGO DOOR) · airframe 60,768 hrs · 22,114 cycles

FORWARD CARGO DOOR LOWER EDGE BEAM CHAFED ALONG ENTIRE LENGTH. BLENDED AREA & REMOVED DAMAGE IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 52-30-02, FIG 101, DETAIL IV. R & R LOWER EDGE BEAM IAW SRM 51-40-02.

Part: SKIN — DENTED (FUSELAGE) · airframe 60,768 hrs · 22,114 cycles

PRODUCTION REQUEST FUSELAGE CROWN BETWEEN STATION 1480 - 1500 & BTW STRINGER 1 & STRINGER 2L THERE IS A DENT. ACCOMPLISHED EA F-5330-T0307820, A, PT 1. FUSELAGE, PLATES & SKINS, CROWN SKIN & STRINGER REPAIR, STATION 1480 TO STATION 1500, STRINGER 1 & STRINGER 2L. EVALUATED DENT, OIL CANNING, OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DETAIL III.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 60,768 hrs · 22,114 cycles

FOUND SCRIBE LINE AT STRINGER 20L LAP SEAM FROM BS 1657 - BS 1720 RUNNING UNDER A LAP SPLICE DOUBLER AT BS 1701. ACCOMPLISHED EA F-5330-T0 306957 FUSELAGE PLATES & SKINS, INCOMING SKIN REPAIR. REPLACEMENT & SCRIBE DAMAGE REPAIR BETWEEN STA 1657 & 1720, STRINGER 18L & 21L. THIS IS A CAT B REPAIR IAW FAA FORM 8110-3, DATED 03/24/2014. MAJOR REPAIR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 60,768 hrs · 22,114 cycles

REPAIR ASSESSMENT FUSELAGE SKIN REPAIR BS 1690 - 1710 STRINGER 19L - STRINGER 21L, 1ST & 2ND STAGE APPROVALS. ACCOMPLISHED EA F-5330-T0 306957 FUSELAGE, PLATES & SKINS, INCOMING SKIN REPAIR. REPLACEMENT & SCRIBE DAMAGE REPAIR BETWEEN STA 1657 & 1720, STRINGER 18L & 21L. THIS IS A CAT B REPAIR IAW FAA FORM 8110-3, DATED 03/24/2014. MAJOR REPAIR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 60,768 hrs · 22,114 cycles

BLEND REPAIR TO FUSELAGE SKIN AT BS 1709, STRINGER 21L - STRINGER 22L. ACCOMPLISHED EA F-5330-T0306957, PT 1. TITLE, FUSELAGE & PLATES & SKINS, INCOMING SKIN REPAIR REPLACEMENT & SCRIBE DAMAGE REPAIR, BETWEEN STATION 1657 & 1720, STRINGER 18L & 21L. THIS IS A CAT B REPAIR IAW FAA FORM 8110-3, DATED 03/24/2014. MAJOR REPAIR.

Part: FITTING — CRACKED (NR 1 PYLON) · airframe 60,768 hrs · 22,114 cycles

NUMBER 1 PYLON UPPER INBD HOLE OF VERTICAL FLANGE OF STRUT TO DIAGONAL BRACE FITTING HAS A CRACK INDICATION. ACCOMPLISHED EA F-5450-T0306349, NACELLES & PYLON, PYLONS STRUCTURES DEVIATION TO EO F-5450-7-5006, DUE TO CRACK IN BULKHEAD AT BRACE FITTING MOUNT HOLE. MAJOR REPAIR CAT A.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 60,768 hrs · 22,114 cycles

FOUND SCRIBE LINE AT STRINGER 14R LAP SEAM FROM BS 638.750 - BS 661. ACCOMPLISHED EA F-5330-T0306962. FUSELAGE PLATES & SKINS SCRIBE LINE REPAIR, STRINGER 14R, STATION 440 TO STATION 499 & STATION 638 TO STATION 661. IAW FAA FORM 8110-3, DATED 03/14/2014 FOR APPROVAL. MAJOR REPAIR CAT A.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 60,768 hrs · 22,114 cycles

FOUND SCRIBE LINE AT STRINGER 14R LAP SEAM FROM BS 440 - BS 498.842. REQUIRES ADDITIONAL STRIPPING FROM BS 540 - BS 660, DUE TO PROXIMITY OF SCRIBE LINE TO LAP SEAM. ACCOMPLISHED EA F-5330-T0306962, FUSELAGE PLATES & SKINS SCRIBE LINE REPAIR, STRINGER 14R, STATION 440 TO STATION 449 & STATION 638 TO STATION 661. IAW FAA FORM 8110-3, DATED 03/14/2014 FOR APPROVAL. MAJOR REPAIR CAT A.

Part: FRAME — CRACKED (BS 395) · airframe 60,768 hrs · 22,114 cycles

BS 395 FRAME CRACKED BETWEEN STRINGER 2 & 3L. PERFORMED SPLICE REPAIR OF FRAME IAW EA 757-5312-16-F4517 REV.

Part: TEE FITTING — CORRODED (BS 1037-1060) · corrosion level 2 · airframe 60,768 hrs · 22,114 cycles

TEE FITTING BELOW LT KEEL BEAM AT BS 1037 - 1060 HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 53-00-71, FIG 101, DETAIL IX. INSTALLED NEW TED FITTING IAW SRM51-40-02 & DWG 144N8180. MINOR REPAIR.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 60,768 hrs · 22,114 cycles

FRAME AT STATION 1640, BETWEEN STRINGER 17R - STRINGER 18R HAS NUMEROUS INCOMING FASTENER HOLES WHICH ARE ELONGATED & HAS SHORT PITCH. ACCOMPLISHED REPAIR ON WC 60001648350001 & EA 757-5362-16-F4479, REV DATED APRIL 4, 2014. FUSELAGE FRAME SPLICE REPAIR AT STATION 1640, BETWEEN STRINGER 14R & STRINGER 20R. REFERENCE FAA FORM 8110-3. THIS NON-ROUTINE IS FOR TRACKING PURPOSES ONLY. CATEGORY B REPAIR, MAJOR REPAIR.

Part: FRAME SPLICE — GOUGED (FUSELAGE) · airframe 60,768 hrs · 22,114 cycles

MDC FRAME SPLICE GOUGED, BS 377, STRINGER 6R. REPAIR ACCOMPLISHED ON WC 60001648360001 & EA 757-5312-16-F4477 REV DATED APRIL 7, 2014. INCOMING FRAME REPAIR AT STATION 377, STRINGER 5R TO STRINGER 7R. CATEGORY B REPAIR MAJOR REPAIR.

Part: SKIN — CORRODED (BS 1400) · corrosion level 2 · airframe 60,768 hrs · 22,114 cycles

AFT CARGO BAY BS 1400 SKIN STRAP CORRODED BETWEEN STRINGER 27-28L. NO REWORKS AREA PERMITTED ON CIRCUMFERENTIAL SKIN STRAP IAW SRM 53-00-01, FIG 101, PG 106. DAMAGED STRAP WAS REPLACED FOR A NEW ONE IAW SRM 51-40-02 & DWG 146N3300 SHEET 4.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,768 hrs · 22,114 cycles

AFT CARGO COMPARTMENT STATION 1380 RT, REVEAL STRAP HAS EXISTING REPAIR DOUBLER CORRODED. SDR WAS GENERATED IN ERROR MINOR REPAIR.

Part: SKIN — CORRODED (NR 1 NACELLE) · corrosion level 2 · airframe 60,768 hrs · 22,114 cycles

NR 1 PYLON RT AFT SKIN INTERNAL SURFACE BETWEEN STATIONS 144 & 153, LOWER AREA HAS CORROSION & MISSING PRIMER. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 54-50-01, FIG. 102, DETAIL III. ACCOMPLISHED EA F-5450-T0305710, PT 1. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 1640) · corrosion level 2 · airframe 60,768 hrs · 22,114 cycles

FLOORBEAM BS 1640, LBL 58 UPPER SURFACE CORRODED. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL III. R & R FLOORBEAM IAW SRM 51-40-02 & DWG 146N5109 & 146N5089.

Part: GATE — CORRODED (L2 DOOR) · corrosion level 2 · airframe 60,768 hrs · 22,114 cycles

L2 DOOR LOWER GATE LIP HAS CORROSION. R & R L2 DOOR LOWER GATE ASSEMBLY IAW AMM 52-11-38-4. ADJUSTED & CHECKED GATE ASSEMBLY IAW AMM 52-11-00-5, CHECKED GOOD.

Part: SKIN — DAMAGED (BS 1678-1720) · airframe 60,768 hrs · 22,114 cycles

FOUND SCRIBE LINE AT STRINGER 10R LAP SEAM FROM BS 1678.875 - 1720. ACCOMPLISHED EA F-5330-T0 306384. REPAIR CLASSIFIED AS CATEGORY B MAJOR.

Part: SKIN — DAMAGED (ZONE 200) · airframe 60,768 hrs · 22,114 cycles

FOUND SCRIBE LINE AT STRINGER 14L LAP SEAM FROM BS 1396.437 - 1397.25. ACCOMPLISHED EA F-5330-T0306496 A.

Part: STRINGER — CHAFED (BS 1640-1661) · airframe 60,768 hrs · 22,114 cycles

AFT CARGO BAY STRINGER 28L BETWEEN FS 1640 - 1661 CHAFED. FOUND OUT OF LIMITS IAW SRM 53-00-03 FIG 101 DET II. REPAIRED STRINGER IAW SRM 53-00-03 FIG 201 REPAIR 2. REPAIR CLASSIFIED AS CATEGORY A MAJOR.

Part: FRAME — DAMAGED (BS 1520) · airframe 60,768 hrs · 22,114 cycles

AFT CARGO BAY FRAME INNER FLANGE AT BS 1520 BETWEEN STRINGER 26 - 27L DENTED & GOUGED. BLENDED GOUGE IAW SRM 51-10-02, FOUND TO BE WITHIN LIMITS IAW SRM 53-00-07, FIG. 101, DETAIL II. NO DENTS ALLOWED ON FRAME AND OUT OF LIMITS IAW SRM 53-00-07, FIG. 101. REMOVED FRAME. LOCATED AND DRILLED NEW FRAME IAW SRM 51-4-05. INSTALLED NEW FRAME IAW SRM 51-40-02.

Part: STRINGER SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 60,768 hrs · 22,114 cycles

AFT CARGO BAY STRINGER SPLICE 26L BS 1450 - 1470, CORRODED. REMOVED CORROSION IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 53-00-03 & DWG 146N3820. REMOVED STRINGER SPLICE IAW SRM 51-40-02, LOCATED, DRILLED & INSTALLED SPLICE IAW SRM 51-40-02 & DWG 146N3820.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,768 hrs · 22,114 cycles

AFT PIT FRAME 1640 HAS CORROSION AT LOWER WEB AREA BETWEEN STRINGERS 27L - 28L. REMOVED CORROSION ON AFT PIT FRAME 1640, LOWER WEB, BETWEEN STRINGER 27L - 28L IAW SRM 51-10-02. ORIGINAL MATERIAL .063, MATERIAL LOSS .014, MATERIAL REMAINING .049, OUT OF LIMITS IAW SRM 53-00-07, FIG 101, DETAIL II. R & R FRAME, STATION 1640, STRINGER 24L - 24R IAW SRM 51-40-02 & DWG 146N1023, SH 1, REV F.

Part: SKIN — DAMAGED (BS 270) · airframe 60,768 hrs · 22,114 cycles

SKIN AT BS 270 HAS A LIGHTNING STRIKE. BLENDED OUT DAMAGE, AND FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DET II. CUT OUT DAMAGE, HFEC ORIG HOLES & REPAIRED SKIN IAW SRM 53-00-01 FIG 201 REPAIR 15.

Part: SHEAR TIE — CORRODED (BS 1640) · corrosion level 2 · airframe 60,768 hrs · 22,114 cycles

SHEAR TIE AT BS 1640 BETWEEN STRINGERS 25-26R CORRODED. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE DELAMINATED THROUGH 50% OF ORIGINAL MATERIAL IAW SRM 51-10-02. ORIG. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-40-02 AND DRAWING 146N1023, SHEET 1. MAJOR REPAIR.

Part: STRINGER SPLICE — CORRODED (BS 1615-1325) · corrosion level 2 · airframe 60,768 hrs · 22,114 cycles

AFT CARGO STRINGER SPLICE 25L AT BS 1615 - 1625, HAS CORROSION AROUND FASTENERS WITH BUBBLED PAINT. REMOVED STRINGER SPLICE AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-03, FIG. 101, DETAIL II. LOCATED AND DRILLED NEW STRINGER SPLICE IAW SRM 51-40-05 AND DWG 146N3703, REV. A. INSTALLED STRINGER SPLICE IAW SRM 51-40-02 AND DWG 146N3703. MAJOR REPAIR (CAT. "A")

Part: CREASE BEAM — CORRODED (BS 295-420) · corrosion level 2 · airframe 60,768 hrs · 22,114 cycles

CREASE BEAM, STRINGER 17L, BS 297 - 420, FOUND CORRODED OUT OF LIMITS. LOCATED & DRILLED NEW CREASE BEAM IAW SRM 53-30-13 & DWG 141N8322. INSTALLED CREASE BEAM IAW SRM 51-40-02 & DWG 141N8322.

Part: FLOORBEAM — DAMAGED (BS 1681) · airframe 60,768 hrs · 22,114 cycles

MAIN CABIN DECK FLOORBEAM UPPER TEE LOWER SURFACE NICKED & SCRATCHED, BS 1681, LBL 64 - RBL 64.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,768 hrs · 22,114 cycles

STRINGER 9L, STATION 395 TO STATION 440 IS CORRODED. REMOVED CORROSION IAW SRM 51-10-02, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-03, FIG 101, DETAIL II. R & R STRINGER 9L, STATION 395 - 440 IAW SRM 51-40-02 & DWG 141N3370.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,768 hrs · 22,114 cycles

STATION 1360 FRAME IS CORRODED BETWEEN STRINGERS 26R TO 27R. REMOVED CORROSION IAW SRM 51-10-02. ORIG THICKNESS .071 REMAINING THICKNESS .060, OUT OF LIMITS IAW SRM 53-00-07 FIG 101 DETAIL II. REMOVED FRAME ASSY AT STA 1360 S24R TO S24L IAW SRM 51-40-02. FABRICATED NEW FRAME. INSTALLED NEW FRAME AT STA 1360 FROM S24R TO S24L IAW SRM 51-40-02 AND DRAWING 146N1009, SHT 3, REV D. MAJOR REPAIR CAT A.

Part: SKIN — CORRODED (NR 2 PYLON) · corrosion level 2 · airframe 60,768 hrs · 22,114 cycles

NUMBER 2 PYLON INBD FWD SKIN IS CORRODED AT DOOR AT PPS 106.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 60,768 hrs · 22,114 cycles

MAIN CABIN DECK FLOORBEAM UPPER CHORD AT BS 377 HAS AREAS WITH NICKS & SCRATCHES. REMOVED FLOORBEAM IAW SRM 51-40-02. INSTALLED FLOORBEAM IAW SRM 51-40-02 & DWG 141N5113.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 60,768 hrs · 22,114 cycles

MAIN CABIN SEAT TRACK BET BS 1180 - BS 1280, LBL 45 HAS NICKS & SCRATCHES. FS 1180 - 1280, LBL 45 SEAT TRACK, BLENDED DAMAGE IAW SRM 51-10-02, MATERIAL LOSS .039. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52 FIG101 DETAIL V. R & R SEAT TRACK IAW DWG 146N5217.

Part: SKIN — CORRODED (NR 2 PYLON) · airframe 60,768 hrs · 22,114 cycles

NUMBER 2 PYLON INBD SKIN IS CORRODED AT LOWER SPAR FWD OF MID BULKHEAD FITTING. MINOR REPAIR.

Part: CREASE BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 60,768 hrs · 22,114 cycles

BS 1280 - 1290, STRINGER 17L CREASE BEAM CORRODED, BLENDED AREA IAW SRM 51-10-02 FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13 FIG 101 DET 2. R & R CREASE BEAM IAW DWG 146N5590.

Part: SEAT TRACK — MISALIGNED (ZONE 200) · airframe 60,768 hrs · 22,114 cycles

INCOMING CONDITION SEAT TRACK AT STATION 377 TO 440 LBL 45.5 HAS A FASTENER INSTALLED ON FWD INNER CROWN WITH SHORT ED SEAT TRACK WAS OUT OF LIMITS IAW SRM 51-40-06 FIG 3 TABLE IV. REMOVED SEAT TRACK LBL 45 STATION 377 TO 440 IAW SRM 51-40-02. PURCHASED NEW SEAT TRACK PN 1520-792 BATCH NR 1180394 PROFILED NEW SEAT TRACK IAW DRAWING 141N5131. LOCATED & DRILLED SEAT TRACK IAW SRM 51-40-05, INSTALLED NEW SEAT TRACK STATION 377 TO 440 IAW SRM 51-40-02 DRAWING 141N5131.

Part: FLOORBEAM — CORRODED (BS 740) · corrosion level 2 · airframe 60,768 hrs · 22,114 cycles

MAIN CABIN, FLOORBEAM BS 740, BETWEEN LBL 45 - 60, HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL III. REMOVED AND REPLACEDFLOORBEAM IAW SRM 51-40-02 AND DWG 143N5065. REPAIR IS CLASSIFIED AS CATEGORY "A" MAJOR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,768 hrs · 22,114 cycles

MAIN DECK CABIN FLOORBEAM UPPER TEE AT BS 345 HAS AREAS WITH NICKS, SCRATCHES & CORROSION. AFTER REWORK, FOUND TO BE OUT OF LIMITS. REMOVED FLOORBEAM TEE IAW SRM 51-40-02. LOCATED, DRILLED IAW SRM 51-40-02 & DRAWING 141N5111. INSTALLED FLOORBEAM TEE IAW SRM 51-40-02 & DRAWING 141N5111. REPAIR IS CLASSIFIED AS CATERGORY A MAJOR.

Part: FLOORBEAM — DAMAGED (BS 365) · airframe 60,768 hrs · 22,114 cycles

MAIN DECK CARGO FLOORBEAM UPPER TEE HAS NICKS & SCRATCHES AT BS 365. FOUND TO BE OUT OF LIMITS. INSTALLED NEW FLOORBEAM TEE IAW SRM 51-40-02 AND DWG 141N5112. MAJOR REPAIR.

Part: SEAT TRACK — CRACKED (BS 700-780) · airframe 60,768 hrs · 22,114 cycles

MAIN CABIN SEAT TRACK BETWEEN BS 700 - 780 LBL 25, DAMAGED. SEAT TRACK FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52 FIG 101 FOOTNOTE H. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-02 AND DRAWING 143N5085. REPAIR CLASSIFIED AS CATEGORY A MAJOR.