N907FD

Part: SPAR — CORRODED (RT WING) · airframe 52,273 hrs · 21,563 cycles

RT WING REAR SPAR WEB CORRODED AT RT FUEL SHUTOFF VALVE AT VALVE MATING SURFACE AREA. REPAIR IAW EA F-5710-131557. ACCOMPLISHED EA NR F-5710-131557 WING-RT REAR SPAR WEB CORROSION AT FUEL SHUTOFF VALVE, THIS IS A MAJOR REPAIR WITH NO FOLOW=UP INSPECTION REQUIRED.

Part: BUSHING — CORRODED (BRACE FITTING) · corrosion level 2 · airframe 52,273 hrs · 21,563 cycles

LT WING PYLON DIAGONAL BRACE FITTING " WING SIDE" HAS MIGRATING BUSHINGS. REMOVED 2 EA BUSHINGS IAW SOPM 20-50-03 FOUND CORROSIONS IN LUG BORE, REAMED LUG TO A FINAL DIAMETER OF 1.640 IN. AND HFEC FOUND NO DAMAGE OR DEFECTS IAW NTM 51-00-00 PT6 FIG 11 COMPLIED WITH EA F-5740-131546. THIS A MAJOR 'A' REPAIR

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 52,273 hrs · 21,563 cycles

DURING SURVEILLENCE FOUND SEAT TRACK FLANGE CRACKED AT APROX STA 490, RBL 415.5. REPAIRED SEAT TRACK IAW SRM 53-00-52 FIG 1, REPAIR 1, THIS IS A CATEGORY A REPAIR NO FOLLOW-UP INSPECTIONS REQUIRED.

Part: SKIN — DENTED (BS 1704 S20L) · airframe 52,273 hrs · 21,563 cycles

DENT ON FUSELAGE SKIN, BS 1704, S20L, IN THE LAP SEAM. EVALUATED DENT AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG. 101, DETAIL 3, DUE TO PROXIMITY TO SKIN SPLICE. ACCOMPLISHED SKIN DOUBLER REPAIR IAW EA F-5330-131129, REV DATE 10/21/09; "FUSELAGE - PLATES AND SKIN - (AD 2006-11-11) - SKIN REPAIR NEAR BS 1701, S20L LAP SPLICE". THIS REPAIR IS CLASSIFIED AS A CAT. "B" MAJOR REPAIR, WITH THE FOLLOWING FOLLOW UP TRACKING: SUPPLEMENTAL INSPECTIONS (SSID) IAW AD 2006-11-11, ON OR BEFORE 37,500 FC.

Part: DOOR FRAME — CORRODED (L2 DOORWAY) · corrosion level 2 · airframe 52,273 hrs · 21,563 cycles

L2 DOOR CUTOUT FWD FRAME, LWR, BS 690 INBD SIDE, HAS AN APPROX 4 INCH SECTION OF CORROSION, DIRECTLY ABOVE FLOOR LEVEL. ACCOMPLISHED L2 DOOR SURROUND WEB CORROSION REPAIR IAW EA F-5310-131540, DATED 10/07/09, REV-. THIS REPAIR IS CLASSIFIED AS A CAT. "A" MAJOR REPAIR.

Part: FRAME — DAMAGED (BS 820) · airframe 52,273 hrs · 21,563 cycles

MAIN DECK BS 820, S2L, AFTER REMOVAL OF TV MONITOR, DOUBLERS FOUND DOUBLE DRILLED HOLES. CUTOUT DAMAGED FRAME AT BS 820, S5L-S5R IAW SRM 53-00-07, FIG. 201, REPAIR NR 1. REMOVED 2 EA ACFT BRACKETS, LAV BRACKET, ELEV BRACKET FOR FOM IAW SRM 51-40-02. FABRICATED FRAME ON MAE TRAVELER NR T9/809365 / FABRICATED CHANNEL NR 1 ON MAE TRAVELER NR T9/809366/ AND CHANNEL NR 2 ON MAE TRAVELER NR T9/809367. LOCATED AN DRILLED FRAME AND REPAIR PARTS IAW SRM 51-40-05. TREATED AND PRIMED ALL PARTS IAW SRM 51-20-01. INSTALLED FRAME, ALL REPAIR PARTS, AND PARTS REMOVED FOR FOM IAW SRM 51-40-02 / 53-00-07, FIG 201, REPAIR NR 1, AT BS 820, S5L-S5R. THIS REPAIR IS CLASSIFIED AS A CAT "A" MAJOR REPAIR.

Part: FRAME — DAMAGED (FS800) · airframe 52,273 hrs · 21,563 cycles

MAIN DECK STA 800 L/BL8 (APPROX) AFTER REMOVAL OF TV MONITOR DOUBLERS FOUND WITH DOUBLE DRILLED HOLES. CUT OUT DAMAGED FRAME AT STA 800 STR 5L TO 5R IAW SRM 53-00-07 FIG 2014 R1,REMOVED 2 EA. ACFT BRACKET 1 EA LAV BRACKET 1 EA ELEV BRACKET FOR FOM IAW SRM 51-40-02, FABRICATED FRAME ON MAE TRAVELER NR T9/809365, FABRICATED CHANNEL NR1 ON TRAVELER NR T9/809366 AND CHANNEL NR 2 ON NR T9/809367, LOCATED AND DRILLED HOLES ON FRAME AND ALL REPAIR PARTS IAW SRM 51-40-05, TREATED AND PRIMED IAW SRM 51-20-01, AND INSTALLED ALL REPAIR PARTS REMOVED IAW SRM 51-40-02 AND 53-00-07 FIG 210 REPAIR 1. THIS IS AN "A" REPAIR. MAJOR REPAIR.

Part: BRACKET — MISALIGNED (ZONE 100) · airframe 52,273 hrs · 21,563 cycles

ACFT HAS INCOMING MISSING STRUCTURE THAT IS NEEDED TO ASSEMBLE THE E-7 RACK. DUE TO THE DISCREPANCY AFFECTING THE PTF MOD , NEW BRACKETS WERE FAB, AND INSTALLED ON MAE EA NR 3002772/ 757-5362-16-F2323, AND MAE W/C 118550428ACSR01, THIS NR IS FOR TRACKING PURPOSES ONLY. MAJOR ALTERATION. .

Part: WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,273 hrs · 21,563 cycles

MAIN CABIN DECK AFT FLOOR WEB CORRODED STA 1700 TO 1720 BL O, TO LBL 53, REMOVED CORR, REMOVED ANGLE IAW SRM 51-40-02. RECEIVED NEW ANGLE ON MAE TRAV NR T9/808947, P/N 7075-0.071B, FABRICATED NEW DOUBLER REPAIR MAT PN 2024-T3.063C, INSTALLED NEW ANGLE AND REPAIR DOUBLER STA 1700-1720, LBL4 TO LBL53, IAW SRM 53-60-51. CATEGORY "A". MAJOR REPAIR.

Part: MOUNT — CORRODED (NR 1 PYLON) · corrosion level 2 · airframe 52,273 hrs · 21,563 cycles

NR1 ENG PYLON FWD ENG MOUNT PAD CORRODED. REMOVED CORROSION AT NR 1 ENG PYLON FWD LWR WEB (MOUNT) IAW SRM 54-50-01. ORIG MAT THICKNESS AT FWD BLENDOUT AREA .263, AFTER REWORKED .261, AND AT MIDDLE BLENDOUT AREA ORIG MAT THICKNESS .264, AFTER REWORKED .261, AND AT AFT BLEND OUT AREA ORIG MAT .263, AFTER REWORKED .260. FOUND TO BE WITHIN LIMITS ON ALL 3 REWORKED AREAS IAW SRM 54-50-01, FIG 101, DETAIL II. FLAP PEENED REWORKED AREAS IAW SOPM 20-10-03 AND PRIMED IAW SRM 51-20-01. MINOR.

Part: SEAT TRACK — CORRODED (BS 700-740) · corrosion level 2 · airframe 52,273 hrs · 21,563 cycles

MAIN DECK, BS 700-740, LBL 45.5, SEAT TRACK ASSY HAS CORROSION IN SEVERAL AREAS. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52. ORIGINAL MAT THICKNESS .071" / REMOVED .016". FABRICATED NEW SEAT TRACK MAT. 60-6549/24, BATCH NR 1544829 IAW SRM 51-10-02 AND SRM 53-30-02. INSTALLED NEW SEAT TRACK IAW SRM 51-40-02, AT BS 700-740, LBL 45.5.

Part: SKIN — DAMAGED (ZONE 100) · airframe 52,273 hrs · 21,563 cycles

FUSELAGE SKIN, BS 715, BETWEEN S24L/ 25L, SKIN HAS AN OUTWARD PUNCTURE, APPROX 12" AFT OF ANOTHER DOUBLER REPAIR. TRIMMED OUT DAMAGED AREA IAW SRM 53-00-01, FIG 201. FABRICATED REPAIR PARTS (DOUBLER AND FILLER) IAW SRM 53-00-01, FIG 201 AND SRM 53-30-01, FIG 1, ITEM 18. INSTALLED ALL REPAIR PARTS AT BS 715, S24L-S25L, IAW SRM 51-40-02. THIS REPAIR IS CLASSIFIED AS A CAT. "A" MAJOR REPAIR.

Part: CREASE BEAM — CORRODED (BS 664-753) · corrosion level 2 · airframe 52,273 hrs · 21,563 cycles

MAIN DECK FLOOR, BS 664-753, LBL 64, IS CORRODED IN SEVERAL AREAS. REMOVED CORROSION IAW SRM 51-10-02. BLENDED ORIGINAL THICKNESS, .080", AFTER REWORK, LOST .028" THICKNESS. FOUND TO BE OUT OF LIMITS IAW SRM 53-30-13. -REMOVED CREASE BEAM IAW SRM 51-40-02, FROM BS 664-753, LBL 64. RECEIVED NEW CREASE BEAM, LOCATED AND DRILLED IAW SRM 51-40-05, AT BS 664-753, LBL 64. INSTALLED NEW CREASE BEAM, AND 3 EACH WEBS FROM BS 664-753, LBL 64, IAW SRM 51-40-02. WEBS WERE ORIGINALLY REMOVED ON STAND ALONE NON-ROUTINES. THIS REPAIR IS CLASSIFIED AS A CAT "A" MAJOR REPAIR.

Part: SHEAR TIE — CORRODED (BS 1320) · corrosion level 2 · airframe 52,273 hrs · 21,563 cycles

AFT CARGO COMPT - SHEAR TIE CORRODED AT FRAME 1320, BTW S-28L TO S-29L, WL138.5. REMOVED SHEAR TIE FROM STA 1320 S28L TO 29L. FABRICATED NEW SHEAR TIE IAW MAE TR NR T9/806073. LOCATED AND DRILLED NEW SHEAR TIE IAW SRM 51-70-16. TREATED AND PRIMED IAW SRM 51-20-01. INSTALLED NEW SHEAR TIE AT STA 1320, S28L TO S29L IAW SRM 51-40-02. MINOR REPAIR.

Part: FLOORBEAM — DAMAGED (BS 1640) · airframe 52,273 hrs · 21,563 cycles

FLOOR BEAM AT BS 1640 REQUIRES REPLACEMENT DUE TO EXISTING REPAIRS. REMOVED FLOORBEAM AT BS 1640, LBL 63 TO RBL 63, IAW SRM 51-40-02. ANODIZED NEW FLOORBEAM IAW BAC 5019, REV. U, P.O. NR MSC0012758. FABBED NEW FLOOR BEAM FROM BAC1518-338, BATCH NR 0001692300 IAW DWG 146N5089. LOCATED AND DRILLED NEW FLOOR BEAM IAW SRM 51-40-05. TREATED AND PRIMED NEW FLOOR BEAM IAW SRM 51-20-01. PAINTED NEW FLOORBEAM IAW SRM 51-21-10. INSTALLED NEW FLOORBEAM IAW SRM 51-40-02, AT BS 1640, LBL 63 TO RBL 63. THIS REPAIR IS CLASSIFIED AS A CAT. "A" MAJOR REPAIR.

Part: FLOORBEAM — DAMAGED (ZONE 100) · airframe 52,273 hrs · 21,563 cycles

FLOORBEAM AT STA 1661, REQUIRES REPLACEMENT DUE TO EXISTING REPAIRS. REMOVED FLOORBEAM IAW SRM 51-40-02, FABED NEW FLOORBEAM BAC1518-338, IAW SRM 51-40-05. INSTALLED NEW FLOORBEAM STA 1661, RBL TO LBL 63, IAW SRM 51-40-02. CATEGORY "A" , MAJOR REPAIR.

Part: SKIN — DENTED (BS 690 S24-25L) · airframe 52,273 hrs · 21,563 cycles

FUSELAGE, LHS, BS 690, BETWEEN S24L/25L, SKIN HAS DENTS. FOUND TO BE OUT OF LIMITS PER SRM 53-00-01, FIG. 101, DETAIL 3. CUT OUT DAMAGED AREA PER SRM 53-00-01, FIG. 201, REPAIR NR 3. FABRICATED REPAIR DOUBLER PER DWG 143N3691. LOCATED, DRILLED, TREATED REPAIR PARTS PER SRM 51-40-05 / 51-20-01. INSTALLED COUNTERSINK WASHERS AND REPAIR DOUBLER IAW SRM 53-00-01, FIG. 201, REPAIR 3. THIS REPAIR IS CLASSIFIED AS A CAT. "B" MAJOR REPAIR.

Part: SKIN — MISREPAIRED (NR 7 SLAT) · airframe 52,273 hrs · 21,563 cycles

PREVIUSLY INSTALLED FLASH REPAIR AT NR 7 L/E SLAT, EXTERNAL SKIN, NOT INSTALLED PER SRM. CUT AND REMOVED EXISTING REPAIR ON NR 7 L/E SLAT EXTERNAL SKIN IAW SRM 57-43-01 FIG 201 REPAIR 1 , FABRICATED REPAIR PLATE ON TRAV. T9/ 806985AND DOUBLER IN TRAV T9/ 806984, AND FABRICATED STRAPS IAW SRM 57-43-01 FIG. 201 REPAIR 1, LOCATED AND DRILLED ALL REPAIR PARTS IAW SRM 51-40-05. TREATED AND PRIMED IAW SRM 51-20-01 AND INSTALLED PART IAW SRM 57-43-01 FIG. 201 REPAIR 1, THIS IS A MAJOR "A" REPAIR NO FOLOW-UP INSPECTION REQUIRED.

Part: WEB — WORN (NR 1 PYLON) · airframe 52,273 hrs · 21,563 cycles

NUMBER 2 PYLON 311N5040-6 UPPER AFT WEB IS WORN AT APPROX. PPS 162 - 172. BLENDED WORN AREA AT APPROX PPS 170.90. ORIGINAL MATERIAL THICKNESS .063", AFTER REWORK .054"; D=.009", L=1.0", W=.700". FOUND TO BE OUT OF LIMITS PER SRM 54-50-01, NOTE "B", DETAIL 3. FLOURESCENT PENETRANT INSPECTED AREA PER SOPM AND EA F-5450-131124. NO DAMAGE REMAINS AND AREA IS CRACK-FREE. CLEANED AND APPLIED BMS 10-11 TYPE 1 PRIMER PER EA F-5450-131124. THESE REWORK INSTRUCTIONS FOR NR 1 PYLON, ARE CLASSIFIED AS A CAT. "A" MAJOR REPAIR, PER EA F-5450-131124, REV DATE 10/02/09.

Part: SKIN — DAMAGED (BS 1918-1941) · airframe 52,273 hrs · 21,563 cycles

APU COMPARTMENT INTERNAL SKIN HAS UNIDENTIFIED HOLE ABOUT 3/8", BETWEEN FS 1918.9 & 1941, AT 1 (ONE) O'CLOCK POSITION. REMOVED APU COMP. SKIN FROM STA. 1918.9 TO 1941 TO FOM IAW SRM 51-40-02, REPAIR SKIN IAW SRM 51-70-10 AND REINSTALLED IAW SRM 51-40-02 AND 51-40-00, THIS A MAJOR REPAIR NO FOLOW-UP INSPECTION REQUIRED.

Part: FLOOR SUPPORT — CORRODED (BS 680-740) · corrosion level 2 · airframe 52,273 hrs · 21,563 cycles

MAIN DECK FLOOR SUPPORT STA 680-740 AND RBL 65 HAS SEVERAL AREAS OF CORROSION REMOVED CORRISION INBD CHORD STA 680-740, RBL 65 IAW SRM 53-30-13. MAT THICKNESS .190", MAT REMOVED .100", MAT REMAINING .090". FOUND OUT OF LIMITS IAW SRM 53-30-13, PG 102, FIG 101. REMOVED AND REPLACE INBD CHORD ( PN 143N8328-54 BATCH NUMBER 1693914 "ON") FROM STA 680-740 AND RBL 65, WL 208 IAW SRM 51-40-02.

Part: CREASE BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,273 hrs · 21,563 cycles

STA 1277- 1287 LT CREASE BEAM CORRODED. REMOVED CREASE BEAM IAW SRM 51-40-02, FABRICATED NEW BEAM FROM MAT BAC1515-5537075T6511, IAW SRM 51-30-01, INSTALLED CREASE BEAM STA 1180-1290, LBL 60, IAW SRM 51-40-02, MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,273 hrs · 21,563 cycles

BS 700 FLOORBEAM UPPER CAP CORRODED B/T LBL 45- LBL TO AT FS 700 B/T B/L 36.5 TO B/L 70 LT A FLOORBEAM REPAIR WAS ACCOMPLISHED, DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION, ON MAE WC 118350502BZ2R02, AND EA 757-5335-16-F2279, REV B, DATED 10/06/2009. THIS NON ROUTINE IS FOR TRACKING PURPOSES ONLY. MAJOR ALTERATION.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,273 hrs · 21,563 cycles

MAIN CABIN, STA 345-365, APROX BL0 FLOOR SUPPORT HAS CORROSION. BLENDED AREA IAW SRM 51-10-02 DAMAGE L=1" X W=1" X D .010 FOUND TO BE OUT OF LIMITS IAE SRM 52-00-51 DETAIL 2, REMOVED FLOOR SUPPORT BETWEEN STA 345-365 AND FABRICATED 2 EA SUPPORT BRACKETS ON TRAV NR T9/ 806127 AND RECEIVE NEW SUPPORT PN BAC 1506-3384 AND INSTALLED PARTS IAW SRM 51-40-02, THIS IS A MAJOR "A" REPAIR NO FOLLOW-UP INSP REQUIRED.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,273 hrs · 21,563 cycles

BULK CARGO COM, STA 1500 BETWEEN STR 28L-29L, WL 138 FRAME CORRODED AND HAVE MISSING SHEAR TIE. FRAME FOUND OUT OF LIMITS IAW SRM 53-60-07 FIG 101 DET 1, REMOVED 2 EA, INTERCOSTAL AND REINSTALLED IAW SRM 51-40-02. REMOVED AND REPLACED FRAME ASSY STA 1500 BETWEEN STR 24L-24RIAW SRM 51-40-02 FAB. SHEAR TIE ON TRAVELER NR T9/805678 AND INSTALLED IAW SRM 51-40-02. THIS IS A MAJOR 'A' REPAIR NO FOLLOW-UP INSPECTION REQUIRED.

Part: CREASE BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,273 hrs · 21,563 cycles

LBL 62 FLOORBOARD SUPPORT FS, 395-377 CORRODED REMOVED CORROSION IAW SRM 51-10-02. ORIGINAL MAT .050 MAT LOSS IS .050 FOUND TO BE OUT OF LIMITS IAW SRM 53-0051 FIG 101 DETAIL 2 RMOVED CREASE BEAM IAW SRM 51-40-02. FABED NEW ON TRAVELER NR T9/ 804601 IAW SRM 53-10-15-2 LOCATED, DRILLED AND INSTALLED IAW SRM 51-40-05 AND 51-40-02 ( INSTALLED NEW CREASE BEAM FROM FST 295-395 LBL 60 ) W/L 208 THIS IS A MAJOR " A" REPAIR NO FOLOW-UP INSP REQUIRED.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,273 hrs · 21,563 cycles

STA 740 RBL 60 UPPER CAP CORRODED (FLOORBEAM ). AT BS 740 B/T RBL 30 TO RBL 63 , FLOORBEAM REPAIR WAS ACCOMPLISHED DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION ON MAE. W/C 118350441BZR03, AND MAE EA NR 757-5335-16-F2280 REV B DATED 09/11/2009, NON-ROUTINE IS FOR TRACKING PURPOSES ONLY, THIS A MAJOR ALTERATION.

Part: SKIN — DENTED (NR 2 PYLON) · airframe 52,273 hrs · 21,563 cycles

NR 2 PYLON PNL 443 BR LAND SKIN DENTED COMPLIED WITH EA F-5450-131126 DATED 10/07/09, PYLON NR 2 ENG STRUT SIDE SKIN DAMAGE REPAIR , THIS A MAJOR "A " REPAIR NO FOLLOW-UP INSP REQUIRED.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,273 hrs · 21,563 cycles

BULK CARGO COMP STA 1520 BETWEEN STR 27R AND 28R, WL 138, FRAME SHEAR TIE HAS BARE METAL AND SURFACE CORROSION. REMOVED SHEAR TIE, FABRICATED NEW SHEAR TIE AND INSTALLED IAW SRM 51-40-02, THIS IS A MAJOR "A" REPAIR NO FOLLOW-UP INSPECTIONS REQUIRED.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 52,273 hrs · 21,563 cycles

LT WING, OTBD FLAP, L/E, BEHIND NR 4 SPOILER, IS CREASED. CHECKED LIMITS OF DENT/CREASE AND FOUND OUT OF LIMITS IAW SRM 57-53-01; A=1.0", W=.044", A/Y=22.7. ACCOMPLISHED DOUBLER REPAIR ON LT WING, OTBD FLAP, L/E, BEHIND NR 4 SPOILER, IAW SRM 57-53-01, REPAIR NR 2. REPAIR PARTS FABRICATED ON MAE TRAVELERS T9/805253, T9/805251. THIS REPAIR IS CLASSIFIED AS A CAT. "A" MAJOR REPAIR.

Part: PANEL — CRACKED (NR 1 L/E SLAT) · airframe 52,273 hrs · 21,563 cycles

LT WING NR 1 SLAT, INBD NOSE COVE PANEL HAS A 1" CRACK DIRECTLY FWD OF THE INBD DRIVE TRACK. REMOVED NR 1 SLAT SEAL RETAINER FOR REPAIR ACCESS. REMOVED CRACKED COVE PANEL IAW SRM 51-40-02. FABRICATED NEW COVE PANEL IAW MAT ID SHT7075-T6, .050" THICK, BATCH NR 0001610155, IAW SRM 57-43-01, FIG. 1, DETAIL 1. INSTALLED NEW COVE PANEL SKIN ON LT WING NR1 L/E SLAT, JUST FWD OF THE INBD DRIVE TRACK IAW 51-40-02. RE-INSTALLED NR 1 SLAT SEAL RETAINERS, PREVIOUSLY REMOVED FOR ACCESS. THIS REPAIR IS CLASSIFIED AS A CAT "A" MAJOR REPAIR WITH NO FOLLOW UP TRACKING.

Part: STRAP — CORRODED (ZONE 200) · airframe 52,273 hrs · 21,563 cycles

THE APU AIR INLET DOOR ASSY FWD MOUNTING LAND ON EMPANAGE IS CORRODED. REMOVED DAMAGED SUPPORT IAW SRM 51-40-02, REMOVED CORROSION IAW SRM 51-10-02, CHECKED LIMITS ORIG MAT .100, BLENDED 2 EA AREAS 1.0" X 2.0" X .060" OUT OF LIMITS IAW SRM 53-80-05 FIG 101 DET 3, FABED NEW SUPPORT ON TRAVELER T9/805156 IAW DWG 148N3138, LOCATED AND DRILLED SUPPORT IAW SRM 51-40-05 AND INSTALLED IAW SRM 51- 40-02 THIS IS A MAJOR "A" REPAIR WITH NO FOLLOW-UP INSPECTIONS REQUIRED.

Part: SKIN — CORRODED (BS 1380) · corrosion level 2 · airframe 52,273 hrs · 21,563 cycles

THE AFT CARGO DOOR CUT OUT FWD JAMB LOWER SECTION, HAS 2EA AREAS OF CORROSION ADJACENT TO THE LOWER STOP FITTING. REMOVED DAMAGED PART, FABRICATED REPAIR PLATE 2024T3.090C, SHIM 2024T3.100C, INSTALLED REPAIR PARTS IAW SRM 51-00-02. STA 1380, STRG- 22-27R. MAJOR REPAIR.

Part: SEAT TRACK — MISLOCATED (ZONE 200) · airframe 52,273 hrs · 21,563 cycles

MCD STA 1540-1640 LBL 45 FOUND INCOMING SEAT TRACK NOT "JIGGING" ON TOOLING (MISLOCATED) REMOVED SEAT TRACK IAW SRM 51-40-02 , FAB NEW SEAT TRACK FROM BAC 1520-792 BATCH 0001541897, LOCATED AND DRILLED IAW SRM 51-40-02 TRATED AND PRIMED IAW SRM 51-21- 01 INSTALLED NEW SEAT TRACK IAW SRM 51-40-02 STA 1540-1640 LBL 45, THIS IS A MAJOR "A" REPAIR NO FOLLOW-UP INSPECTION REQUIRED.

Part: SEAT TRACK — MISALIGNED (ZONE 200) · airframe 52,273 hrs · 21,563 cycles

MCD STA 1540-1640 LBL 24 FOUND INCOMING SEAT TRACK NOT "JIGGING" ON TOOLING. REMOVED SEAT TRACK STA 1540-1640 LBL 24 FAB NEW SEAT TRACK FROM BAC 1520-792 BATCH NR 0001514831 TREATED AND PRIMED NEW SEAT TRACK IAW SRM 51-20-01 INSTALLED NEW SEAT TRACK IAW SRM 51-40-02 THIS IS A MAJOR "A" REPAIR, NO FOLOW-UP INSPECTION REQUIRED.

Part: WEB — CRACKED (ZONE 100) · corrosion level 2 · airframe 52,273 hrs · 21,563 cycles

FWD CARGO COMPT, BILGE AREA, STA. 680 - 700, RBL 3, WL 148.5, WEB INTERCOSTAL LWR LEG HAVE CORROSION. DOT NR 102-026. NOTE: AFTER REMOVAL FOUND TO BE CRACKED AT 3 FASTENER HOLES. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53. REMOVED ANGLES SUPPORTS FOR ACCESS AND INTERCOSTAL IAW SRM 51-40-02. ROUTED TO FABSHOP INTERCOSTAL. RECEIVED FROM FAB SHOP INTERCOSTAL TRAVELER #: T9/805255. LOCATED AND DRILLED INTERCOSTAL IAW SRM 51-40-05. TREATED AND PRIMED INTERCOSTAL IAW SRM 51-20-01. INSTALLED ANGLES SUPPORTS REMOVED FOR ACCESS AND INTERCOSTAL IAW SRM 51-40-02.

Part: INTERCOSTAL — DAMAGED (BS 820-839) · airframe 52,273 hrs · 21,563 cycles

FWD CARGO COMPT, INTERCOSTAL WEB BTW FS 820 AND 839, S-26R UPPER EDGE DAMAGED AT FASTENER HOLE, DAMAGE CLEANUP IS OUT OF LIMITS IAW SRM 53-00-04, DETAIL I, FIG 101. NOTE: DAMAGE CLEANUP WAS EXISTING. REMOVED TRANSITION PANEL IAW SRM 51-40-02 FOR ACCESS FROM STA 765 TO 846 RT SIDE, REMOVED DAMAGED INTERCOSTAL WEB IAW SRM 51-40-02. RECEIVED NEW INTERCOSTAL FROM FAB SHOP TRAVELER NR T9/805621, LOCATED AND DRILLED IAW SRM 51-40-05. TREATED AND PRIMED IAW SRM 51-20-01 AND INSTALLED NEW INTERCOSTAL WEB FROM STA 820 TO 839, S-26R IAW SRM 51-40-02. REINSTALLED TRANSITION PANEL IAW SRM 51-40-02. MINOR REPAIR.

Part: FRAME — DENTED (BS 720) · airframe 52,273 hrs · 21,563 cycles

FWD CARGO COMPT, BILGE AREA, STA 720, BL-0, WL 154, TOP OF FRAME HAS SMALL DENT AND SMALL CHAFE MARK ON TOP SURFACE. DOT NR102-013. TRIMMED OUT DAMAGED AREA IAW SRM 53-00-07, FIG 201; PERFORMED HFEC IAW NTM 51-00- 19, PT 6 ON INITIAL FASTENER HOLES COMMON TO REPAIR, NO CRACK INDICATION NOTED; RECEIVED NEW PART REPAIR "J" SECTION FROM FAB SHOP TRAVELER #T9/804941; LOCATED & DRILLED REPAIR "J" SECTION ON STA 720 BL-0, WL-154 IAW SRM 53-00-07, FIG 201, REPAIR 5; TREATED AND PRIMED IAW SRM 51-20-01; INSTALLED REPAIR "J" SECTION ON STA 720, BL-0, WL-154 IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,273 hrs · 21,563 cycles

SEAT TRACK F,S 1540- 1640, RBL 48. REMOVED SEAT TRACK AT FS. 1540-1640 RBL 48, FABRICATED AND INSTALLED IAW SRM 51-40-02, THIS IS A MAJOR "A" REPAIR NO FOLLOW-UP INSP REQUIRED.

Part: SUPPORT — CORRODED (BS 365-418) · corrosion level 2 · airframe 52,273 hrs · 21,563 cycles

STA 365 - 418 RBL 24 SEAT TRACK SUPPORT CORRODED. REMOVED CORROSION. REMOVED .030 INCHES MATERIAL FROM .080 INCHES ORIGINAL OUT OF LIMITS IAW SRM 53-00-52. REMOVED SUPPORT AT RBL 24 STA 365-418. RECEIVED NEW SUPPORT IAW TRAVELER NR T9/803243 IAW SRM 53-10-51. INSTALLED NEW SUPPORT AT RBL 24 STA 365-418 IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,273 hrs · 21,563 cycles

SEAT TRACK, 24 L, FST. 1540-1640 L CORRODED. REMOVED SEAT TRACK, FABRICATED NEW PART AND INSTALLED IAW SRM 51-40-02, THIS IS A MAJOR "A" REPAIR WITH NO FOLOW-UP INSPECTION REQUIRED.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,273 hrs · 21,563 cycles

SEAT TRACK 24R, FST. 1540- 1640 R, IS CORRODED. REMOVED SEAT TRACK, FABRICATED NEW PART AND INSTALLED IAW SRM 51-40-02, THIS IS A MAJOR "A" REPAIR NO FOLLOW-UP INSP REQUIRED.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,273 hrs · 21,563 cycles

MAIN DECK FLOORBEAM AT BS 377, LBL 3-20, UPPER CHORD HAS AREAS OF CORROSION. REMOVED CORROSION AT BS 377, LBL 3-20, IAW SRM 53-00-51. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL 3; ORIGINAL MATL- .125 INCH, AFTER REWORK- .090 INCH. REPAIR ACCOMPLISHED ON W/O 45411, N/R N00002. THIS IS A CAT. "A" MAJOR REPAIR.

Part: FLOORBEAM — NONE (ZONE 200) · airframe 52,273 hrs · 21,563 cycles

BS 377, LBL 58, FLOORBEAM HAS EXISTING REPAIR THAT INTERFERES WITH INSTALLATION OF RCB, ON MOD W/C 118350472RCBR08 AND W/C 118350431AZ2R03. REMOVED PREVIOUS REPAIR AND CUT OUT DAMAGED AREA AT BS 377, LBL70-RBL 34, IAW SRM 53-00-51, FIG 201, REPAIR NR 3. FABRICATED UPPER T-CHORD MATL BAC 1505-100617/20, 7075-T73, IAW SRM 53-00-51, FIG 201, REPAIR NR 3. RECEIVED -2 AND -3 ANGLES ON MAE TRAVELER NR T9/803815. RECEIVED -4 AND -5 STRAPS ON MAE TRAVELER NR T9/803814. INSTALLED UPPER T-CHORD AND ALL REPAIR PARTS AT BS 377, LBL 70-RBL 34, IAW SRM 53-00- 51, FIG 201, REPAIR NR 3. THIS IS A CAT "A" MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 52,273 hrs · 21,563 cycles

STA 365 FLOORBEAM RBL 10 CORRODED UPPER SURFACE. REMOVED CORROSION IAW SRM 53-00-51. ORIGINAL MATERIAL .125 MATERIAL REMOVED .025. AFTER REPAIR .100 INCH. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL III. REMOVED DAMAGED AREA AND PREVIOUS REPAIR IAW SRM 53-00-51, FIG 201, REPAIR STA 365 LBL 15 TO RBL 70. RECEIVED -2 AND -3 REPAIR ANGLES ON MAE TRAVELER NR T9/803017. RECEIVED -4 AND -5 REPAIR STRAPS ON MAE TRAVELER NR T9/803018. FABRICATED UPPER T-CHORD MATERIAL BAC1505-100617/20 7075-T73 IAW SRM 53-00-51 FIG 201, REPAIR III. INSTALLED UPPER T-CHORD AND REPAIR PARTS STA 365, RBL 70 TO LBL 15 IAW SRM 53-00-51, FIG 201 REPAIR III THIS IS A CATEGORY "A" . (MAJOR REPAIR)