N951LF

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

A (C) CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT AT FRAME 34 AND STRINGERS 34R TO 34L IN FORWARD CARGO COMPARTMENT. REMOVED AND REPLACED FLOORBOARD SUPPORT AT FRAME 34 FROM STRINGER 34R TO 34L IN FORWARD PIT.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

AT (C) CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT FROM FRAME 31 TO 34 AT STRINGER 34L IN FORWARD CARGO COMPARTMENT. REMOVED AND REPLACED FLOORBOARD SUPPORT FROM FRAME 31 TO 34, STRINGER 34L IN FORWARD PIT.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

AT (C) CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT AT FRAME 34 ABOVE STRINGER 34 IN FORWARD CARGO COMPARTMENT. REMOVED AND REPLACED FLOORBOARD SUPPORT AT FRAME 34 JUST ABOVE 34L IN FORWARD CARGO COMPARTMENT.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

A (C) CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT FROM FRAME 28 TO 31 AT STRINGER 34R.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

AT (C) CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT FROM FRAME 31 TO 33 AT STRINGER 34R IN FORWARD CARGO COMPARTMENT. FABRICATED NEW FLOORBOARD SUPPORT. TREATED, PRIMED, TOP COATED AND INSTALLED FLOORBOARD SUPPORT FROM FRAME 31 TO 33 AT STRINGER 34R.

Part: INTERCOSTAL — CORRODED

AT C-CHECK, FOUNDINTERCOSTAL AT FORWARD CARGO COMPARTMENT BETWEEN FRAME 51 AND 52 RBL 27 HAS SURFACE CORROSION. REMOVED AND REPLACED INTERCOSTAL AT AFT CARGO COMPARTMENT BETWEEN FRAME 51 AND FRAME 52, RBL 27. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

AT C-CHECK, OFUND AFT CARGO COMPARTMENT FLOOR INTERCOSTAL CORRODED AT FRAME 54 AND RBL 17. REMOVED CORROSION FROM INTERCOSTAL AT FRAME 54, RBL 17. NO MEASUREABLE MATERIAL LOSS. TREATED, PRIMED AND APPLIED TOPCOAT. (M)

Part: FLOORBOARD — PUNCTURED (CABIN)

AT C-CHECK, FOUND AFT CABIN FLOORBOARD NR 261DF HAS MULTIPLE PUNCTURES. REPAIRED AFT CABIN FLOORBOARD PANEL NR 261DF. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

AT C-CHECK, OFUND AFT CARGO FLOOR INTERCOSTAL IS CORRODED AT FRAME 56 AND RBL 22-24. REMOVED CORROSION FROM INTERCOSAL AT FRAME 56, RBL 22-24. NO MEASUREABLE MATERIAL LOSS. TREATED, PRIMED AND APPLIED TOPCOAT. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

AT C-CHECK, FOUND AFT CABIN FLOOR SUPPORT HAS CORROSION AT STATION 3850 AND RBL 32. REMOVED LIGHT CORROSION AT NUT PLATE AT STATION 3850 AND RBL 32. FOUND TO BE WITHIN LIMITS. TREATED, PRIMED AND TOPCOAT APPLIED. (M)

Part: STRINGER — CORRODED (FUSELAGE)

AT C-CHECK, FOUND AFT CABIN FUSELAGE STRINGER FLOOR LEVER UPPER SURFACE CORRODED BETWEEN FRAMES 68-69 AT STATION 3280. REMOVED AND REPLACED STRINGER 21L BETWEEN FRAMES 68 AND 69 STATION 3280. (M)

Part: CROSSBEAM — DAMAGED (NR 1 ENGINE)

AT C-CHECK, FOUND NR 1 ENGINE FORWARD MOUNT CROSSBEAM HAS NICKS, SCRATCHES, AND GOUGING. INSPECTED AND CLEANED DAMAGED AREA. REPAIRED NR 1 ENGINE FORWARD MOUNT CROSSBEAM BY REMOVING AND REPLACING BUSHING. (M)

Part: SKIN — DAMAGED (CROWN)

AT C-CHECK, FOUND UPPER FUSELAGE CROWN AREA BETWEEN FRAMES 52 AND 53 STRINGER 1 LT AND 1 RT VHF ANTENNA MOUNT SURFACE HAS TOOL MARKS AROUND PERIPHERY. UPON FURTHER EVALUATION OF UPPER FUSELAGE CROWN AREA BETWEEN FRAME 52 AND FRAME 53, STRINGER 1L AND 1R, VHF ANTENNA MOUNT SURFACE, FOUND TOOLING MARKS TO BE CHIPPED PAINT AND NO DAMAGE TO STRUCTURE NOTED. TREATED AND PRIMED BARE METAL. (M)

Part: PLATE — CORRODED (FUSELAGE)

AT C-CHECK, FOUND INTERCOSTAL AT AFT CARGO COMPARTMENT FRAME 48 TO 49, LBL 27 WITH SURFACE CORROSION. REMOVED AND REPLACED INTERCOSTAL PLATE AT AFT CARGO COMPARTMENT, FRAME 48 TO FRAME 49, LBL 27. (M)

Part: FITTING — CORRODED (FLOOR SUPPORT)

AT C-CHECK, FOUND FLOOR SUPPORT FITTING AT AFT CARGO COMPARTMENT FRAME 56, LBL 12 IS CORRODED AROUND 2 EACH FASTENER HOLES. REMOVED AND REPLACED FLOOR SUPPORT FITTING AT FRAME 56, LBL 12, IN AFT CARGO PIT. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

AT C-CHECK, FOUND INTERCOSTAL LOCATED BETWEEN FRAME 50 AND 51 RBL 27 AT AFT CARGO COMPARTMENT IS CORRODED AT FORWARD END. (M)

Part: MOUNT — DAMAGED (NR 1 ENGINE)

AT C-CHECK, FOUND NR 1 ENGINE FORWARD MOUNT STOP SERIAL NR 0313-PTE HAS GOUGING IN BOLT HOLES. CLEANED NR 1 ENGINE FORWARD MOUNT STOP, S/N 0313. NO GOUGING NOTED. DIMENSIONS CHECKED AND FOUND TO BE WITHIN LIMITS. (M)

Part: FITTING — CORRODED (FLOOR SUPPORT)

AT C-CHECK, FOUND FLOOR SUPPORT FITTING AT AFT CARGO COMPARTMENT FRAME 56 BL 0 IS CORRODED AROUND 2 EACH FASTENER HOLES. REMOVED AND REPLACED FLOOR SUPPORT FITTING AT FRAME 56, BL 0 IN AFT CARGO PIT. (M)

Part: SILL — CORRODED (PAX DOOR)

AT C-CHECK, FOUND CORROSION AT L2 DOOR INBOARD OF AFT GIRT BAR ATTACH PLATE AT FRAME 68 AND LBL 50. REMOVED AND REPLACED L2 DOOR SILL, LOWER FORWARD CORNER FITTING, DRAINS AND ANGLE AT FRAME 67, LEFT LOWER, UNDER SILL. (M)

Part: PAN — CORRODED (AFT LAVATORY)

AT C-CHECK, FOUND CORROSION ON LEFT AFT LAVATORY FLOOR PAN ASSEMBLY ATTACH POINTS FOR BLOW-OUT DOOR FRAME, 8 PLACES. AFTER EVALUATION, FOUND NO CORROSION ON LEFT AFT LAVATORY FLOOR PAN ASSEMBLY, ATTACHMENT POINTS FOR BLOW OUT DOOR FRAME. (M)

Part: SILL — CORRODED (L2 DOOR)

AT (C) CHECK, FOUND L2 DOOR SILL HAS RIVET HEADS THAT HAVE EXFOLIATED CORROSION BETWEEN FR 66 AND FR 68. REMOVED AND REPLACED L2 DOOR SILL, LOWER FORWARD CORNER FITTING, DRAINS AND ANGLE AT FRAME 67, LT LOWER UNDER SILL. (SDR NR 23431924)

Part: FLOORBOARD — CORRODED (MAIN CABIN)

AT C-CHECK, FOUND CORROSION ON MAIN CABIN FLOORBOARD PANEL NR 222FF. REPAIRED MAIN CABIN FLOORBOARD NR 222FF. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

AT C-CHECK, FOUND CORROSION AT R2 DOOR FLOORBEAM 8 INCHES INBOARD OF DOOR CUT OUT FROM FRAMES 66 TO 68 RBL 50. REPAIRED CORRODED AREA AT R2 DOOR FLOORBEAM, 8 INCHES INBOARD OF DOOR CUTOUT FROM FRAMES 66 TO 68, RBL 50. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

AT C-CHECK, FOUND CORROSION ON MAIN CABIN FLOORBOARD PANEL NR 221FF. REMOVED SURFACE CORROSION FROM FLOORBOARD 221FF. MATERIAL LOSS FOUND TO BE WITHIN LIMITS. TREATED AND PRIMED. (M)

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE)

AT C-CHECK, FOUND 5 DAMAGED AREAS ON FLOORBOARD SUPPORT AT FRAME 59 BETWEEN STRINGER 42R AND 43L IN AFT CARGO COMPARTMENT. REMOVED AND REPLACED FLOORBOARD SUPPORT AT FRAME 59 ON RIGHT SIDE. (M)

Part: FITTING — CORRODED (FUSELAGE)

AT C-CHECK, FOUND CORROSION ON FITTING AT FRAME 59 AND STRINGER 41R IN AFT CARGO BAY. FITTING AT FRAME 59, RIGHT STRINGER 41 OF FLOOR STRUCTURE REMOVED AND REPLACED. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

AT C-CHECK, FOUND CORROSION ON FLOORBEAM AT FRAME 20 AT RBL 12. REMOVED AND REPLACED FLOORBEAM AND SPLICE AT FRAME 20, RBL 12. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

AT C-CHECK, FOUND SEAT TRACK CORRODED BETWEEN FRAMES 20 AND 21 AT RBL 32. REMOVED AND REPLACED SEAT TRACK FROM RBL 32, FRAME 12 TO 24. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

AT C-CHECK, FOUND FLOORBOARD SUPPORT CORRODED AT RIGHT STRINGER 38 BETWEEN FRAME 58 AND 59 ON AFT LOWER CARGO BAY FLOOR. REMOVED AND REPLACED FLOOR SUPPORT FRAME BETWEEN FRAME 58 AND 59. (M)

Part: FITTING — GOUGED (EMERGENCY EXIT)

AT C-CHECK, FOUND GOUGES ON THE LATCHES OF THE LOWER FITTING OF THE RT FORWARD EMERGENCY EXIT DOOR. REMOVED AND REPLACED LOWER LATCH FITTINGS ON RT FORWARD EMERGENCY EXIT DOOR. (M)

Part: PLATE — WORN (R2 DOOR)

AT C-CHECK, FOUND R2 DOOR CAM PLATE FOR DOOR HANDLE BACK MECHANISM ROLLER HAD WEAR MARKS. REMOVED AND REPLACED FITTING ON R2 DOOR, DOOR HANDLE BACK MECHANISM. (M)

Part: STRUCTURE — CORRODED (CABIN FLOOR)

AT C-CHECK, OFUND CORROSION ON AFT CABIN FLOOR STRUCTURE AT FRAME 67 PLUS 13 INCHES TO FRAME 67 AT LBL 45. REMOVED AND REPLACED AFT CABIN FLOOR STRUCTURE AT FRAME 67 PLUS 13 INCHES TO FRAME 67 AT LBL 45. (M)

Part: ATTACH FITTING — CORRODED (GIRT BAR)

AT (C) CHECK FOUND AFT CABIN NR 2 RT DOORWAY, FORWARD GIRT BAR ATTACH FITTING PLATE, WITH CORROSION. REMOVED AND REPLACED FORWARD GIRT BAR ATTACH FITTING PLATE ON AFT CABIN NR 2 RT DOORWAY.

Part: ATTACH FITTING — CORRODED (RT NR 2 DOOR)

AT (C) CHECK FOUND AFT CABIN NR 2 RT DOORWAY AFT GIRT BAR ATTACH FITTING PLATE WITH CORROSION. REMOVED AND REPLACED AFT GIRT BAR ATTACH FITTING PLATE ON AFT CABIN NR 2 RT DOORWAY.

Part: STRUCTURE — CORRODED (CABIN FLOOR)

AT C-CHECK, FOUND CORROSION ON FLOOR STRUCTURE AT FRAME 69 PLUS 3 INCHES TO 69 PLUS 10 INCHES AND LBL 50 IN CABIN. REMOVED AND REPLACED AFT CABIN FLOOR STRUCTURE AT FRAME 69 PLUS 3 INCHES TO FRAME 69 PLUS 10 INCHES, LBL 50. (M)

Part: LATCH — DAMAGED (EMERGENCY DOOR)

AT (C) CHECK, FOUND GOUGE ON FORWARD LT EMERGENCY EXIT DOOR LOWER AFT FITTING LATCH. REMOVED AND REPLACED FORWARD LT EMERGENCY EXIT DOOR, LOWER AFT LATCH FITTING.

Part: FLOOR SUPPORT — BENT (FUSELAGE)

AT C-CHECK, FOUND FLOOR PANEL SUPPORT FOR FLOOR PANEL 232WF IS BENT. FORMED FLOOR PANEL SUPPORT AT FLOOR PANEL NR 232WF BACK TO ORIGINAL CONTOUR. (M)

Part: FLOOR PANEL — CORRODED (AFT CARGO BAY)

AT C-CHECK, FOUND DAMAGE ON UPPER SKIN AND CORROSION ON FLOOR PANEL NR 151BF IN AFT CARGO BAY. FABRICATED AND INSTALLED NEW AFT CARGO COMPARTMENT, FLOOR PANEL NR 151BF. (M)

Part: PAN — CORRODED (AFT LAVATORY)

AT C-CHECK, FOUND CORROSION ON LEFT AFT LAVATORY FLOOR PAN ASSEMBLY ATTACH POINTS FOR BLOW-OUT DOOR FRAME, 8 PLACES. AFTER EVALUATION, FOUND NO CORROSION ON LEFT AFT LAVATORY FLOOR PAN ASSEMBLY, ATTACHMENT POINTS FOR BLOW OUT DOOR FRAME. (M)

Part: FLOOR PANEL — CORRODED (AFT LAV)

AT (C) CHECK FOUND AFT LAV FLOOR PANEL WITH CORROSION AT NUMEROUS LOCATIONS AT ATTACHMENT POINTS FOR BLOW OUT DOOR FRAME. REPAIRED AFT LAV FLOOR PANEL, CORROSION AT ATTACHMENT POINTS FOR BLOW OUT DOOR FRAME. REMOVED AND REPLACED INSERTS.

Part: FLOOR PANEL — CORRODED (AFT CARGO COMPT)

AT C-CHECK FOUND EXFOLIATED CORROSION AT AFT CARGO COMPARTMENT FLOOR PANEL 151DF. FABRICATED AND INSTALLED FLOOR PANEL NR 151DF, AFT CARGO COMPARTMENT. (M)

Part: FLOOR PANEL — CORRODED (AFT CARGO BAY)

AT C-CHECK, FOUND CORROSON ON FLOOR PANEL NR 152BF IN AFT CARGO COMPARTMENT. FABRICATED, PRIMED AND INSTALLED AFT CARGO FLOOR PANEL NR 152BF. (M)

Part: FLOOR PANEL — CORRODED (AFT CARGO BAY)

AT C-CHECK, FOUND CORROSION ON FLOOR PANEL NR 152EF IN AFT CARGO BAY. FABRICATED, TREATED, PRIMED AND INSTALLED AFT CARGO COMPARTMENT FLOOR PANEL NR 152EF. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

AT C-CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT BETWEEN FRAME 48 AND FRAME 50 ABOVE STRINGER 38L IN AFT LOWER CARGO BAY. REMOVED AND REPLACED FLOORBOARD SUPPORT AT FRAME 48L TO 52L, STRINGER 38L IN AFT LOWER CARGO BAY. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

AT C-CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT AT FRAME 63 ABOVE STRINGER 39R IN AFT LOWER CARGO BAY. REMOVED AND REPLACED FLOORBOARD SUPPORT AT FRAME 63 ABOVE STRINGER 39R. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

AT C-CHECK, FOUND CRACK ON FLOORBOARD SUPPORT AT FRAME 56 AND STRINGER 42R IN AFT LOWER CARGO COMPARTMENT. REMOVED AND REPLACED FLOORBOARD SUPPORT AT FRAME 56 AND STRINGER 42R. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

AT C-CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT BETWEEN FRAME 62 AND 63 ABOVE STRINGER 37L IN AFT CARGO BAY. REMOVED AND REPLACED FLOORBOARD SUPPORT BETWEEN FRAME 62 AND 63 ABOVE STRINGER 37L. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

AT C-CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT AT FRAME 63 ABOVE STRINGER 38L IN AFT CARGO BAY. REMOVED AND REPLACED FLOORBOARD SUPPORT AT FRAME 63 ABOVE STRINGER 38L. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

AT C-CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT AT FASTENER HOLE BETWEEN FRAME 60 AND 61 ABOVE STRINGER 43L IN AFT LOWER CARGO BAY. REMOVED AND REPLACED FLOORBOARD SUPPORT BETWEEN FRAME 60 AND 61 ABOVE STRINGER 43L. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

AT C-CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT BETWEEN FRAME 58 AND 59 ABOVE STRINGER 38R IN AFT LOWER CARGO COMPARTMENT. REMOVED AND REPLACED FLOORBOARD SUPPORT BETWEEN FRAME 58 AND 59 ABOVE STRINGER 38R. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

AT C-CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT BETWEEN FRAME 49 AND FRAME 50 ABOVE STRINGER 43L IN AFT CARGO BAY. INSTALLED NEW FLOORBAORD SUPPORT BETWEEN FRAME 49 AND 50 ABOVE STRINGER 43L IN AFT CARGO BAY. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

AT C-CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT AT FRAME 59 ABOVE STRINGER 40L IN AFT LOWER CARGO COMPARTMENT. REMOVED AND REPLACED FLOORBOARD SUPPORT CHANNEL AT FRAME 59 ABOVE STRINGER 40L. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

AT C-CHECK, FOUND FLOORBOARD SUPPORT CORRODED AT FRAME 58 BETWEEN STRINGER 38R AND 40R IN AFT LOWER CARGO COMPARTMENT. REMOVED FLOORBOARD SUPPORT, FABRICATED AND INSTALLED NEW FLOORBOARD SUPPORT AT FRAME 58 BETWEEN STRINGER 38R AND 40R. (M)

Part: FLOOR PANEL — CORRODED (FUSELAGE)

AT C-CHECK, FOUND CORROSION AND BARE METAL ON SEVERAL NUT PLATES AND CLIP NUTS AND THEIR UPPER AND LOWER MOUNTING SURFACE IN FORWARD CARGO COMPARTMENT BETWEEN RIGHT FRAME 28 TO FRAME 34, RIGHT STRINGER R-S 34 TO CENTER B/L. FABRICATE, ALODINED, PRIMED, APPLIED TOPCOAT AND INSTALLED INTERCOSTAL BETWEEN FRAME 28 TO FRAME 34, STRINGER 34R. (M)

Part: FRAME — CORRODED (FUSELAGE)

AT C-CHECK, FOUND CORROSION ON LEFT SIDE OF FRAME BETWEEN FRAME 24 AND 35 AT STRINGER 34L TO CENTER BUTT LINE. FABRICATED AND INSTALLED FLOOR SUPPORTS FRAME BETWEEN FRAME 24 TO FRAME 34 AT STRINGER 34L. (M)

Part: THRESHOLD — CORRODED (R2 DOOR)

AT (C) CHECK FOUND R2 DOOR THRESHOLD HAS 5 CORRODED RIVETS. REMOVED AND REPLACED CORRODED RIVETS AT R2 DOOR THRESHOLD.

Part: SKIN — CRACKED (LT MLG DOOR)

AT C-CHECK, FOUND LEFT MLG WHEEL WELL DOOR INTERIOR SKIN CRACKED AT STATION 17255. REPAIRED DOOR IAW SRM 52-81-14, PAGE 258-264, FIGURE 205. (M)

Part: PRECOOLER — DELAMINATED (NR 1 ENGINE)

AT C-CHECK, FOUND NR 1 ENGINE INTAKE PRECOOLER, ON BOTH SIDES OF THRUST REVERSER C-DUCT DELAMINATED. REPAIRED PRECOOLER IAW SRM 54-02-00. (M)

Part: ACCESS PANEL — DELAMINATED (FUSELAGE)

AT C-CHECK, FOUND RIGHT BELLY FAIRING ACCESS PANEL, 198GB, DELAMINATED STATION 2456. REPAIRED PANEL IAW SRM 51-77-12, PAR 3B, FIGURE 3. (M)

Part: FAIRING — DELAMINATED (FUSELAGE)

AT C-CHECK, FOUND RIGHT BELLY FAIRING 197GB, DELAMINATED. REPAIRED BELLY FAIRING 197GB IAW SRM S3-4S-12, PAGE 220 FIG 205. (M)

Part: FAIRING — DELAMINATED (FUSELAGE)

AT C-CHECK, FOUND BELLY FAIRING 192AB DELAMINATED. REPAIRED FAIRING IAW SRM 51-77-12 PAR 3B, FIGURE 3. (M)

Part: FAIRING — DELAMINATED (FUSELAGE)

AT C-CHECK, FOUND BELLY FAIRING 197CB DELAMINATED. REPAIRED FAIRING IAW SRM S3-45-12 PAGE 220, FIGURE 205. (M)

Part: SKIN — ERODED (VERTICAL STAB)

AT C-CHECK, FOUND VERTICAL STABILIZER LEADING EDGE WITH EROSION STATION 4869. REPAIRED VERTICAL STABILIZER IAW SRM 55-30-00, PATE 123. (M)

Part: SKIN — DELAMINATED (THRUST REVERSER)

AT C-CHECK, FOUND NR 1 ENGINE THRUST REVERSER SKIN DELAMINATED. REPAIRED NR 1 THRUST REVERSER IAW SRM V2500, 54-30-00, REPAIR NR 22. (M)

Part: COUPLING — DELAMINATED (THRUST REVERSER)

AT C-CHECK, FOUND NR 1 ENGINE LEFT THRUST REVERSER COUPLING OUTER SKIN C-DUCT DELAMINATED AND MISSING MATERIAL. REPAIRED 'C' DUCT IAW SRM V2500, REPAIR NR 4, REV 31. (M)

Part: FAIRING — DELAMINATED (FUSELAGE)

AT C-CHECK, FOUND BELLY FAIRING 197EB DELAMINATED. REPAIRED FAIRING IAW SRM S3-4S-12, PAGE 220 FIGURE 205. (M)

Part: ACOUSTIC PANEL — DENTED (NR 1 ENGINE)

AT C-CHECK FOUND NR 1 ENGINE AIR INTAKE ACOUSTIC PANEL DENTED. REPAIRED ACOUSTIC PANEL IAW SRM 54-10-00, PAGE 110, SEC 11. (M)

Part: ACCESS PANEL — DELAMINATED (LT WING)

AT C-CHECK,F OUND LEADING EDGE ROOT WING 192DT ACCESS PANEL DELAMINATED. REPAIR PANEL IAW SRM 51-73-00, PAGES 1 AND 2. (M)

Part: SKIN — CRACKED (HORIZ STAB)

AT C-CHECK, FOUND LEFT HORIZONTAL STABILIZER LEADING EDGE CRACKED AND SEVERAL DENTS. REPAIRED CRACK IAW SRM 55-14-11, FIGURE 205. DENTS WERE REPAIRED PER PER SRM 51-77-11, REV 61. (M)

Part: LINER — ERODED (NR 2 ENGINE)

AT C-CHECK FOUND NR 2 ENGINE AIR INTAKE ATTRITION LINING WITH EROSION. REPAIRED ATTRITION LINING IAW EM 72-32-85 PAGE 6, FIGURE 72-32-85-990-016. (M)

Part: DUCT — CORRODED (THRUST REVERSER)

AT C-CHECK, FOUND NR 1 ENGINE THRUST REVERSER C-DUCT, RIGHT, WITH CORROSION ON UPSIDE. REPAIRED RIGHT THRUST REVERSER IAW ENGINEER REPORT 2078002, REF, CV03-0799. (M)

Part: COVER — BROKEN (T/E FLAP FAIRING)

AT C-CHECK, FOUND OUTBOARD FLAP, RIGHT FAIRING TRACK, 633AR, BROKEN COVER. REPLACED COVER IAW SRM 51-76-00. (M)

Part: COVER — BROKEN (T/E FLAP)

AT C-CHECK, FOUND OUTBOARD FLAP, RIGHT FAIRING TRACK, 632R, BROKEN COVER. REPLACED COVER IAW SRM 51-76-00, REV 60. (M)

Part: SKIN — DENTED (REAR CONE)

AT C-CHECK, FOUND DENT ON REAR CONE SKIN FS 82, STATION 38035. REPAIRED DENT IAW SRM 53-51-11 FIGURE 203 PAGE 217-218. (M)

Part: DUCT — DELAMINATED (THRUST REVERSER)

AT C-CHECK, FOUND NR 2 ENGINE RIGHT THRUST REVERSER COWLING OUTER SIDING C-DUCT DELAMINATED. REPAIRED DAMAGE IAW SRM V2500, PAGE 201-206, FIGURE 201. (M)

Part: DUCT — DELAMINATED (THRUST REVERSER)

AT C-CHECK, FOUND NR 2 ENGINE LEFT THRUST REVERSER COWLING, OUTER SKIN C-DUCT DELAMINATED. C-DUCT REPAIRED IAW SRM V2500 54-30-00, REPAIR NR 4. (M)

Part: TRACK — DAMAGED (T/E FLAP FAIRING)

AT C-CHECK, FOUND OUTBOARD FLAP RIGHT FAIRING TRACK 632CB, DAMAGED ON RIGHT SIDE STATION 3059. REPAIRED TRACK IAW SRM 51-77-12, PAGE 10, FIGURE 3. (M)

Part: COWLING — PUNCTURED (NR 2 ENGINE)

AT C-CHECK FOUND NR 2 ENGINE INTAKE UP WITH TWO PUNCTURES AT THE 7 AND 2 O'CLOCK POSITIONS. REPAIRED AIR INTAKE COWL IAW EM 71-11-11-300-015. (M)

Part: ACOUSTIC PANEL — DETERIORATED (NR 2 ENGINE)

AT C-CHECK, FOUND NR 2 ENGINE AIR INTAKE ACOUSTIC PANEL WITH DETERIOATION. REPAIRED ACOUSTIC PANEL IAW SRM V2500, 54-10-00, PAGE 100, SEC11. (M)

Part: BEARING — WORN (T/E FLAP FAIRING)

AT C-CHECK, FOUND OUTBOARD FLAP, RIGHT FAIRING TRACK 632CB, WITH FREEPLAY AT STATION 3059. REPLACED BEARINGS OF STAY ASSEMBLY IAW PMS 01-05-27. (M)

Part: DUCT — CORRODED (THRUST REVERSER)

AT C-CHECK, FOUND NR 1 ENGINE THRUST REVERSER C-DUCT, LEFT, WITH CORROSION ON UPSIDE. REPAIRED LEFT THRUST REVERSER IAW RE 2078006, REF CV03-0917-01. (M)

Part: ANGLE — BROKEN (LT WING)

AT C-CHECK, FOUND BROKEN ANGLE BEHIND SLAT NR 3 STOP, LEADING EDGE LEFT WING. REPAIRED ANGLE IAW SRM 51-20-00. (M)

Part: TRACK — DENTED (T/E FLAP FAIRING)

AT C-CHECK, FOUND LEFT WING FAIRING TRACK, 533CB INTERIOR, DENTED. REPAIRED FAIRING TRACK IAW SRM 51-77-12 PAGE 10, FIGURE 3. (M)