N12318

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,524 hrs · 32,835 cycles

FUSELAGE SKIN CRACKED ABOVE STR 22R 3 INCHES FWD OF STA 727E AND ABOVE PREVIOUS REPAIR. INSTALLED REPAIR PER EC/RA 5331-01378.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 63,524 hrs · 32,835 cycles

STRINGER 27L HAS CORROSION STA 380 TO 400. REPAIRED PER SRM 53-00-03 FIG 201 SHEET 7 OF 7 PAGE 207.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 63,524 hrs · 32,835 cycles

C-2 DOOR INNER SKIN CENTER AFT LIGHTENING HOLE CRACKED. REPAIRED PER ECRA 5232-01097.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,524 hrs · 32,835 cycles

CABIN FWD ENTRY, STRINGER 11L FWD SIDE OF L-1 DOOR CUTOUT WEB FWD UPPER SUPPORT CLIP CRACKED. REMOVED AND REPLACED INTERCOSTAL WEB AND SHEAR TIE REF ECRA 5311-01382.

Part: SPLICE PLATE — CRACKED (NR 2 PYLON) · airframe 63,524 hrs · 32,835 cycles

NR 2 PYLON LT SPLICE PLATE IS CRACKED AT NAC STA 345.28 AND NAC WL 118.95. REMOVED AND REPAIRED CRACKED SECTION ON NR 2 PYLON I/B SPLICE PLATE REF ECRA 5421-01016.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,524 hrs · 32,835 cycles

FWD CABIN NR 14L INTERCOSTAL AFT OF L-1 DOOR CUTOUT STRINGER CRACKED AT STA 360. REMOVED AND REPLACED PER ECRA 5311-01382.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 63,524 hrs · 32,835 cycles

CABIN FWD ENTRY, NR 15 INTERCOSTAL AFT OF L-1 DOOR CUTOUT STRINGER CRACKED STA 360. REMOVED AND REPLACED STRINGER SPLICE 15L STA 360 PER ECRA 5311-01382.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,524 hrs · 32,835 cycles

CABIN FWD ENTRY, L-1 DOOR UPPER HINGE AT STRINGER 10L, O/B CLIP FOR WEB IS CRACKED AT AFT END STA 303. L-1 DOOR SURROUND S-10L UPPER HINGE INTERIM REPAIRED PER ECRA 5311-01381.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 63,524 hrs · 32,835 cycles

C1 DOOR OUTER SKIN CRACKED JUST ABOVE DOOR HANDLE TOP CORNER. REPAIRED PER SRM 52-00-01 FIG 201 PAGE 203.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,524 hrs · 32,835 cycles

TWO INCH CRACKED IN FUSELAGE SKIN, AT THE AFT LOWER CORNER OF R-1 DOOR CUTOUT. REPAIRED PER ECRA 5331-01367.

Part: BUSHING — CORRODED (VERTICAL STAB) · airframe 63,524 hrs · 32,835 cycles

VERTICAL FIN FED RIGHT FITTING HAVE CORROSION IN BUSHING. REPLACED PER ECRA 5530-01493.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,524 hrs · 32,835 cycles

FRAME CRACKED AT STA 727C B/W STR 8RT 9RT. INSTALLED REPAIRED PER ECRA 5310-04683.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 63,524 hrs · 32,835 cycles

VERTICAL STAB, LEFT AFT O/B FITTING FOUND CORROSION ON BOTH FACES. AFTER REMOVED BUSHINGS REPAIRED AS PER ECRA 5530-01494.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 63,524 hrs · 32,835 cycles

FUSELAGE FRAME STA 727C MIS-DRILLED. REPAIR PER ECRA 5310-04683.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 63,524 hrs · 32,835 cycles

ABB HEAVY IGC CORROSION STR 26 R STA 790. REPAIRED PER SRM 53-00-03.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 63,524 hrs · 32,835 cycles

AFT CARGO AFT DOOR FRAME CRACKED AT LOWER STOP PAD REMOVED AND REPLACED AFT CARGO DOOR AFT FRAME PER SRM 51-40-02 REF DWG 65-47960

Part: STRAP — CORRODED (FUSELAGE) · airframe 63,524 hrs · 32,835 cycles

STA 847 STR 25 R LOWER STRAP CORRODED. REMOVED, FABRICATED NEW STRAP AND INSTALLED PER SRM 51-40-02.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 63,524 hrs · 32,835 cycles

FWD BAG BIN FWD DOOR FRAME CRACKED AT LWR STOP PAD INSTALLED DOOR FRAME REF SRM 51-40-02 AND EA 5310-04443.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 63,524 hrs · 32,835 cycles

AFT CARGO DOOR FWD FRAME CRACKED AT LOWER STOP PAD REMOVED AND REPLACED AFT CARGO FWD FRAME PER DWG 65-47959 AND SRM 51-40-02.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 63,524 hrs · 32,835 cycles

C2 DOOR OUTER SKIN CRACKED AT DOOR HANDLE CUT-OUT. CUTOUT DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER PER SRM 52-00-01 FIG 201 REPAIR NR 3

Part: WEB — CORRODED (BS 787 S27R) · airframe 63,524 hrs · 32,835 cycles

ABB WEB CORRODED AT STA 787 STR 27R. REMOVED AND REPLACED WEB REF SRM 51-40-02.

Part: PAN — CRACKED (CARGO DOOR) · airframe 63,524 hrs · 32,835 cycles

C2 DOOR FWD SIDE PAN, UPPER AND LOWER HALVES CRACKED AT SPLICE. INSTALLED NEW PANS ON DOOR ASSY.

Part: SHEAR TIE — CORRODED (BS 500D S28L) · airframe 63,524 hrs · 32,835 cycles

FBB BELT FRAME HAS CORROSION STA 500D AT S28L. REWORKED AND REPLACES SHEAR TIE REF SRM 53-00-01 & 51-40-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,524 hrs · 32,835 cycles

FUSELAGE FRAME CRACKED STA 767 B/W STR 8/9 RT. REPAIRED PER EA5310-04498.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,524 hrs · 32,835 cycles

FUSELAGE FRAME CRACKED STA380 B/W STR 8/9 RT. REPAIRED PER EA 5310-04498.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,524 hrs · 32,835 cycles

FUSELAGE FRAME CRACKED STA480 B/W STR 8/9 RT. REPAIRED PER EA5310-04498.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,524 hrs · 32,835 cycles

FUSELAGE FRAME CRACKED STA 400 B/W STR 8/9. REPAIRED PER EA 5310-85405.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,524 hrs · 32,835 cycles

FUSELAGE FRAME CRACKED STA 787 B/W STR 8/9. REPAIRED PER EA5310-04498.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,524 hrs · 32,835 cycles

R-2 DOOR CUTOUT CRACKED AT UPPER HINGE UPPER AREA. REPAIR COMPLETED IAW SRM 53-60-01 FIG 201.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,524 hrs · 32,835 cycles

FUSELAGE FRAME CRACKED AROUND RIVET ABOVE S-9L. REPAIRED PER EA 5310-04498.

Part: FRAME — CRACKED (BS 767 S9L) · airframe 63,524 hrs · 32,835 cycles

STATION 767 FUSELAGE FRAME CRACKED AROUND RIVET ABOVE S-9L. REPAIRED PER EA 5310-04498.

Part: FRAME — CRACKED (BS 907 S8-9L) · airframe 63,524 hrs · 32,835 cycles

FRAME CRACKED STA 907 BETWEEN S8L AND S9L. REPAIRED PER ECRA 5310-04498.

Part: FRAME — CRACKED (BS 847 S8-9) · airframe 63,524 hrs · 32,835 cycles

FRAME CRACKED AT STA 847 BETWEEN STR 8 & 9. REPAIRED PER EA 5310-04498.

Part: FRAME — CRACKED (BS 827 S9L) · airframe 63,524 hrs · 32,835 cycles

FUSELAGE FRAME CRACKED AT STA 827 AROUND RIVET ABOVE S-9L. REPAIRED PER EA 5310-04498.

Part: FRAME — CRACKED (BS 867 S9L) · airframe 63,524 hrs · 32,835 cycles

STA 867 FUSELAGE FRAME CRACKED AROUND RIVET ABOVE S-9L. REPAIRED FUSELAGE FRAME STA 867 ABOVE S-9L PER EA 5310-04498.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,524 hrs · 32,835 cycles

FUSELAGE FRAME CRACKED STA440 B/W STR 8/9 LT. REPAIRED PER EA 5310-04498.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,524 hrs · 32,835 cycles

FRAME CRACKED AT STA 907 B/W STR 8/9. REPAIRED PER EA 5310-04498.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,524 hrs · 32,835 cycles

FUSELAGE FRAME CRACKED STA 807 B/W STA 8/9. REPAIR PER EA5310-04498.

Part: FRAME — CRACKED (BS 727E S9L) · airframe 63,524 hrs · 32,835 cycles

STA 727E FUSELAGE FRAME CRACKED AROUND RIVET ABV S-9L. REPAIRED PER EA5310-04498.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,524 hrs · 32,835 cycles

FRAME CRACKED B/W STA400 STR 8 AND 9 PER EA 5310-04498.

Part: FRAME — CRACKED (BS 887 S8-9R) · airframe 63,524 hrs · 32,835 cycles

FUSELAGE FRAME CRACKED STA 887 BETWEEN STA 8 & 9 RT. REPAIRED PER EA 5310-04498.

Part: FRAME — CRACKED (BS 867 S8-9R) · airframe 63,524 hrs · 32,835 cycles

FUSELAGE FRAME CRACKED AT STA 867 BETWEEN STR 8 & 9 RIGHT. REPAIRED PER EA5310-04498.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,524 hrs · 32,835 cycles

FUSELAGE CRACKED AT STA480 B/W STR 8 AND 9. REPAIRED PER EA 5310-04498

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 63,524 hrs · 32,835 cycles

CABIN FWD ENTRY FLOOR SUPPORT STA 294.5 AND RBL 31.5 PREVIOUS REPAIR STRAP HAS CORROSION UNDER, AROUND NUT PLATE HOLE. INSTALLED SECT "T" CHORD AND REINSTALLED STRAP PER SRM 53-10-51.

Part: FITTING — CRACKED (FUSELAGE) · airframe 63,524 hrs · 32,835 cycles

CABIN FWD ENTRY INTERCOSTAL 15L AFT OF L1 DOOR CUTOUT WEB FWD SUPPORT CLIP CRACKED. INSTALLED CLIP PER SRM 53-40-02.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 63,524 hrs · 32,835 cycles

STR 27 RT CORRODED AT APPROX STA 320. REMOVED AND REPLACED STRINGER 27 RIGHT STA 320 PER SRM 51-40-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,524 hrs · 32,835 cycles

L2 DOOR CUTOUT CRACKED AT LOWER HINGE LWR AREA. REPAIRED AND INSTALLED PER ECRA 5331-01364.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,524 hrs · 32,835 cycles

STA 320 BETWEEN S-20L AND 2-21L CRACK IN FRAME. CUTOUT DAMAGED AREA, INSTALLED REPAIR DOUBLER AND FILLER REF SRM 51-70-11.

Part: ANGLE — CORRODED (R2 DOOR) · airframe 63,524 hrs · 32,835 cycles

SURFACE CORROSION ON R2 DOOR Z-ANGLE FROM STA 967 TO 993. REMOVED AND REPLACED PER SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,524 hrs · 32,835 cycles

CABIN FWD ENTRY FLOORBEAM STA 344 TOP AND AROUND CORRODED FROM RBL 10 LBL 10. INSTALLED SECTION "T" CHORD & SPLICE PER SRM 53-10-51.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,524 hrs · 32,835 cycles

CORROSION UNDER FLOORBEAM FLANGE AT STA 1016 FROM LBL 9 - LBL 17. PRIMED AND INSTALLED NEW FLOORBEAM CAP IN REF TO ECRA 5310-03851.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 63,524 hrs · 32,835 cycles

RIGHT I/B SEAT TRACK CORRODED FROM STA 913 TO 936. REMOVED DAMAGED SEAT TRACK AND INSTALLED NEW SEAT TRACK AND REPAIRED STA 887, 947 RIGHT I/B TRACK PER SRM 53-00-52 FIG 201.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 63,524 hrs · 32,835 cycles

LEFT I/B CABIN SEAT TRACK CORRODED STA 827 TO STA 913. REMOVED AND REPLACED FROM STA 827 TO STA 907 PER SERM 53-00-52.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 63,524 hrs · 32,835 cycles

R2 FWD FUSELAGE DOOR FRAME CRACKED BETWEEN S-10R AND S-11R. REMOVED DAMAGED FRAME AND INSTALLED NEW FRAME PER SRM 51-40-02 PARAGRAPH 4 AND 7.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 63,524 hrs · 32,835 cycles

SURFACE CORROSION ON LEFT I/B SEAT TRACK AT STA 927. REMOVED AND REPLACED FROM STA 927 TO 947.5 LEFT, TREATED AND PRIMED PER SRM 53-00-52.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,524 hrs · 32,835 cycles

CABIN FWD ENTRY WEB FWD OF R-1 DOOR CUTOUT BETWEEN STRINGERS 11R AND 12R O/B SUPPORT CRACKED. REMOVED AND REPLACED WEB PER SRM 53-00-04, 53-00-01, AND 51-40-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,524 hrs · 32,835 cycles

CABIN FWD ENTRY INTERCOSTAL WEB LOWER SIDE OF R-1 DOOR LOWER HINGE CRACKED AT FWD I/B CORNER. REMOVED AND REPLACED INTERCOSTAL WEB PER SRM 53-00-04, 53-00-01, AND 51-40-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,524 hrs · 32,835 cycles

RIGHT MAIN FRAME CRACKED STA 616 JUST BELOW MAIN DECK FLOOR INSTALLED STIFFENING ANGLE AND FILLER PER ECRA 5311-01158.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,524 hrs · 32,835 cycles

MAIN FRAME CRACKED STA 616 LT JUST BELOW MAIN DECK FLOOR INSTALLED STIFFENING ANGLE AND FILLER PER ECRA 5311-01158.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,524 hrs · 32,835 cycles

CABIN FWD ENTRY INTERCOSTAL BETWEEN STRINGER 10R AND 11R O/B SUPPORT ANGLE CRACKED. REMOVED AND REPLACED INTERCOSTAL REF SRM 53-00-04 AND 53-00-01, 51-40-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,524 hrs · 32,835 cycles

CABIN FWD ENTRY INTERCOSTAL WEB FWD OF R-1 DOOR CUTOUT BETWEEN STRINGERS 12R AND 13R O/B SUPPORT CRACKED. REMOVED AND REPLACED INTERCOSTAL WEB PER SRM 53-00-04, 53-00-01, 51-40-02.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 63,524 hrs · 32,835 cycles

CORROSION ON FWD SIDE OF APB LWR VERTICAL CHANNEL STIFFENER AND SKIN AT BL 0 STA 1016. FABRICATED AND INSTALLED ALL REPAIR PARTS, REPAIRED STIFFENER PER EA 5310-04045 REV B.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,524 hrs · 32,835 cycles

CABIN FWD ENTRY INTERCOSTAL WEB BETWEEN STA 294.5 AND 312 BL 0 TOP ANGLE AFT END CRACKED. REMOVED AND REPLACED PER SRM 51-40-02.

Part: ANGLE — CORRODED (L2 DOOR) · airframe 63,524 hrs · 32,835 cycles

SURFACE CORROSION ON L-2 DOOR Z-ANGLE FROM STA 942 TO 993. REMOVED AND REPLACED Z-ANGLE FROM STA 913-1010 REF SRM 51-40-02.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 63,524 hrs · 32,835 cycles

CABIN FWD ENTRY FLOORBEAM STA 328 AT LBL 10 2 AT HOLES ELONGATED. REMOVED AND REPLACED PER SRM 53-10-51 REPAIR 5.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,955 hrs · 32,564 cycles

INSPECTION FOUND FRAME TO SKIN ATTACH POINT CORRODED AT BS 967 JUST I/B OF S27L. A REPAIR WAS INSTALLED IAW ECRA 5310-04654B.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,955 hrs · 32,564 cycles

INSPECTION FOUND CORROSION AT FRAME ATTACH POINT, STA 927 JUST I/B OF S27L, LBL 27 TO RBL 27. A REPAIR WAS INSTALLED IAW ECRA 5310-04655.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 62,955 hrs · 32,564 cycles

INSPECTION FOUND STRINGER 25L CORRODED FROM STA 967-986.5, LBL 17. A REPAIR WAS INSTALLED IAW SRM 53-00-03, PAGE 206, FIGURE 201.

Part: SKIN — CRACKED (BS 761 S18-19R) · airframe 58,751 hrs · 30,639 cycles

INSPECTION FOUND A 2.5 INCH CRACK IN FUSELAGE SKIN AT STA 761, S18R TO 19R. REPAIRED IAW SRM 53-00-01, REPAIR 31.

Part: SKIN — CRACKED (BS 727E) · airframe 58,253 hrs · 30,414 cycles

INSPECTION FOUND A 1.5 INCH CRACK IN RIGHT FUSELAGE SKIN ABOVE S24R AND TWO INCHES FORWARD OF STA 727E. A REPAIR WAS INSTALLED IAW ECRA 5331-01222.

Part: SHEAR TIE — CORRODED (BS 500D) · airframe 58,253 hrs · 30,414 cycles

INSPECTION FOUND SHEAR TIE AND SUPPORT ANGLE CORRODED ON LOWER BULKHEAD AT STA 500D BETWEEN STRINGERS 27L AND 26L. THE SHEAR TIE, SUPPORT ANGLE, AND WEB WERE REMOVED AND THE AREA WAS CLEANED. A NEW SHEAR TIE AND SUPPORT ANGLE AND THE ORIGINAL WEB WERE INSTALLED IAW SRM 53-00-07, REPAIR NR 3.

Part: BULKHEAD — CANNING (FUSELAGE) · airframe 53,080 hrs · 27,752 cycles

INSPECTION FOUND AFT PRESSURE BULKHEAD WEB REPAIR LIFTING OFF AT EDGES AT STA 1016. INSTALLED INTERIM REPAIR PER PART 1 OF ECRA 5311-01174. A DIP WAS ISSUED TO REINSPECT THE REPAIR AT INTERVALS NOT TO EXCEED 12,000 CYCLES.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 53,080 hrs · 27,752 cycles

INSPECTION FOUND A 2 INCH CRACK IN RIGHT KEELBEAM AT STA 727. A NEW KEELBEAM SECTION WAS SPLICED IN IAW ECRA 5311-01176.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 53,080 hrs · 27,752 cycles

INSPECTION FOUND A 2 INCH CRACK IN LT KEELBEAM AT STA 727. A NEW KEELBEAM SECTION WAS SPLICED IN IAW ECRA 5311-01176.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 53,080 hrs · 27,752 cycles

AN IMPROPER REPAIR WAS DISCOVERED ON THE AFT PRESSURE BULKHEAD DOME WEB JUST AFT OF THE Y-CHORD BETWEEN S9R AND S11R DURING A 4C CHECK AT HOBBY. THE AREA WAS REPAIRED IAW ECRA 5311-01174.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 53,080 hrs · 27,752 cycles

INSPECTION FOUND RIGHT O/B FLOOR RAIL CORRODED AT BS 827. A FLOOR RAIL REPAIR ANGLE WAS INSTALLED IAW SRM 53-00-53.

Part: GALLEY TRACK — CORRODED (FUSELAGE) · airframe 53,080 hrs · 27,752 cycles

INSPECTION FOUND FLOOR SUPPORT UNDER GALLEY MOUNT CORRODED AT STA 277-290, RBL 14. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-02.

Part: CARGO TRACK — CRACKED (FUSELAGE) · airframe 53,080 hrs · 27,752 cycles

INSPECTION FOUND A 1 INCH CRACK IN FLANGE ON LT TIE DOWN RAIL AT BS 727D. THE CRACKED SECTION OF TIE DOWN RAIL WAS REMOVED AND REPLACED IAW SRM 53-00-53.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 53,080 hrs · 27,752 cycles

INSPECTION FOUND STRINGER 28L CORRODED AT STA 500D. THE CORROSION WAS REMOVED AND THE AREA WAS REPAIRED IAW SRM 53-30-12.

Part: BELTFRAME — CORRODED (FUSELAGE) · airframe 53,080 hrs · 27,752 cycles

E&E COMPARTMENT HAS 5 INCHES OF CORROSION ON BELTFRAME BETWEEN STRINGER S27L AND S27R AT STA 360. REPAIRED BELTFRAME PER SRM 53-00-07.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,080 hrs · 27,752 cycles

CABIN FLOORBEAM (BS 312) TOP CHORD CORRODED AT FASTENER HOLES. INSTALLED NEW FLOORBEAM UPPER CHORD IAW SRM 53-10-51.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,008 hrs · 27,153 cycles

RIGHT PRESSURE DECK IN WHEEL WELL CRACKED (1.5 INCH). REPAIRED PRESSURE DECK PER SRM 53-60-51.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,008 hrs · 27,153 cycles

LEFT PRESSURE DECK IN WHEEL WELL CRACKED (1 INCH). REPAIRED PRESSURE DECK PER SRM 53-60-51.

Part: KEELBEAM — WORN (FUSELAGE) · airframe 49,183 hrs · 25,664 cycles

INSPECTION FOUND NUTS MILLED INTO KEEL BEAM JUST FORWARD OF BULKHEAD AT STA 727 LT SIDE. REPAIRED KEEL BEAM IAW ECRA 5310-03740.

Part: SKIN — DENTED (E&E DOOR) · airframe 49,183 hrs · 25,664 cycles

INSPECTION FOUND THE E&E DOOR DENTED AT R/H SIDE OF HANDLE. A DOUBLER WAS INSTALLED IAW SRM 52-00-01, FIGURE 203.

Part: SEAT TRACK — CORRODED (STA 380-540) · airframe 49,183 hrs · 25,664 cycles

INSPECTION FOUND L/H O/B SEAT TRACK CORRODED AT STA 380-540. THE CORROSION WAS REMOVED IAW SRM 53-00-52. THE AREA AT STA 410 WAS BEYOND ALLOWABLE LIMITS. THE SEAT TRACK WAS REMOVED AND REPLACED FROM STA 380-480 IAW SRM 53-00-52. THE SEAT TRACK WAS TREATED AND PRIMED FROM STA 380-540 IAW SRM 53-00-52.

Part: SEAT TRACK — CRACKED (STA 727B) · airframe 49,183 hrs · 25,664 cycles

INSPECTION FOUND A 1/2" CRACK IN R/H O/B SEAT TRACK AT STA 727B, RBL 45.57. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5321-01123.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 49,183 hrs · 25,664 cycles

INSPECTION FOUND RT SUPPORT ANGLE CORRODED AROUND SCREW HOLE IN FORWARD CARGO COMPARTMENT AT STA 500A-500B. THE SUPPORT ANGLE WAS REPLACED IAW SRM 51-40-02 AND 51-40-10.

Part: SKIN — DENTED (STA 400) · airframe 49,183 hrs · 25,664 cycles

INSPECTION FOUND FUSELAGE SKIN DENTED FORWARD OF STA 400 BELOW S22R. A DOUBLER WAS INSTALLED IAW SRM 51-40-03.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 48,248 hrs · 25,189 cycles

INSPECTION FOUND EMERGENCY EXIT LIGHT INOPERATIVE AT LT WING TRAILING EDGE. THE CHARGER AND BATTERY ASSEMBLY WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD.

Part: PANEL — GOUGED (NR 1 PYLON)

INSPECTION FOUND NR 1 ENGINE PYLON ACCESS PANEL NR 5727L CUTOUT GOUGED IN TWO PLACES. REPAIRED IAW ECRA 5430-01581.

Part: FITTING — CRACKED (TE FLAP TRACK)

INSPECTION FOUND A .5 INCH CRACK IN LT WING NR 3 FLAP TRACK FAIRING FORWARD FITTING AT FORWARD END OF FLAP TRACK I/B LOWER CORNER. A NEW FITTING WAS INSTALLED IAW SRM 51-30-1 AND 51-30-5.

Part: GATE — CORRODED (R-1 DOOR)

INSPECTION FOUND R-1 DOOR LOWER GATE CORRODED AROUND STOPS. THE R-1 DOOR LOWER GATE ASSEMBLY WAS REMOVED AND REPLACED.

Part: SEAT TRACK — CORRODED (BS 344-380)

INSPECTION FOUND LEFT O/B SEAT TRACK CORRODED AT STA 344-380. A NEW SECTION OF SEAT TRACK WAS INSTALLED IAW SRM 53-00-52.

Part: FLOORBEAM — CORRODED (BS 328)

INSPECTION FOUND FLOORBEAM CORRODED AT ATTACH HOLES, STA 328, RBL 13 TO RBL 49. REPAIRED FLOORBEAM IAW SRM 51-10-51, FIGURE 205.

Part: FLOORBEAM — CORRODED (BS 986)

INSPECTION FOUND FLOORBEAM CORRODED AT STA 986, RBL 45 TO LBL 45. REPAIRED IAW ECRA 5310-03938.

Part: FLOORBEAM — CORRODED (BS 967)

INSPECTION FOUND FLOORBEAM CORRODED AT STA 967, RBL 45 TO LBL 45. THE FLOORBEAM UPPER CHORD WAS REPLACED IAW ECRA 5310-03851.

Part: TIE STRAP — CRACKED (STA 767-867)

INSPECTION FOUND A .75 INCH CRACK IN AFT BAGGAGE BIN DOOR JAMB FORWARD CORNER TIE STRAP AT STA 767-867, RBL 26. THE STRAP WAS REPLACED IAW SRM 51-30-02.

Part: FLOORBEAM — CORRODED (BS 1016)

INSPECTION FOUND FLOORBEAM CORRODED AT STA 1016. A NEW UPPER T-CHORD WAS INSTALLED ON FLOORBEAM IAW ECRA 5310-03851.

Part: SEAT TRACK — CORRODED (BS 344-348)

INSPECTION FOUND LT I/B SEAT TRACK CORRODED AT STA 344-348. A NEW SECTION OF SEAT TRACK WAS SPLICED IAW SRM 53-00-52.

Part: STRINGER — CRACKED (BS 500)

INSPECTION FOUND A .5 INCH CRACK IN STRINGER 16R AT STA 500C. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 53-00-03, FIGURE 201.

Part: SEAT TRACK — CORRODED (BS 290.5)

RIGHT OUTBOARD SEAT TRACK CORRODED AT STA 290.5. FABRICATED AND INSTALLED NEW SECTION OF TRACK PER SRM 53-00-52.

Part: FRAME — CRACKED (CARGO DOOR)

INSPECTION FOUND A 1 INCH CRACK IN FORWARD CARGO BIN DOOR FORWARD LOWER CORNER FRAME. THE FORWARD CARGO DOOR FORWARD LOWER CORNER FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: WEB — CRACKED (CARGO DOOR)

INSPECTION FOUND A 1 INCH CRACK IN AFT CARGO DOOR WEB OVER THE CENTER SPRINGS. A DOUBLER WAS INSTALLED IAW ECRA 5230-01450.

Part: TORQUE LINK — BROKEN (RT MLG)

A RT MLG TIRE BLEW OUT AFTER TOUCHDOWN. THERE WAS VIBRATION AND THE AIRCRAFT STOPPED ON THE RUNWAY. THERE WERE NO INDICATIONS OF A PROBLEM PRIOR TO LANDING. MAINTENANCE FOUND THE RT TORQUE LINK BROKEN AND THE GEAR ROTATED 90 DEGREES. THE RT MLG WAS REMOVED AND REPLACED DUE TO DAMAGE CAUSED ON LANDING. THE GEAR WAS CYCLED SEVERAL TIMES IAW MM 32-32-00 WITH OPERATION AND INDICATIONS CHECKING GOOD. A MANUAL GEAR EXTENSION WAS ALSO PERFORMED IAW MM 32-34-00 AND OPERATION CHECKED GOOD. A HARD LANDING AND HIGH DRAG/SIDE LOAD LANDING INSPECTION WAS PERFORMED ON THE NLG, LT MLG, AND RT MLG IAW MM 05-51-51, PAGES 201-206 AND ALL CHECKS WERE GOOD.

Part: RAM AIR ACTUATOR — DAMAGE (RIGHT)

AFTER TAKEOFF, UNABLE TO PRESSURIZE IN AUTO OR MANUAL. MAINTENANCE FOUND RAM DOOR IN FULL OPEN. ROTABLE PARTS CHG (0650273 SN 03027).

Part: HYD LINE — CHAFED (B HYD SYST)

THE B-SYSTEM HYDRAULIC QUANTITY WENT TO ZERO WHILE EN ROUTE TO MCO. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE HYDRAULIC FLEX LINE FROM ACOUSTIC FILTER TO B-HYDRAULIC PRESSURE MODULE CHAFED. THE LINE WAS REMOVED AND REPLACED. THE HYDRAULIC SYSTEM WAS SERVICED AND LEAK CHECKS WERE GOOD.

Part: CLEARANCE DOOR — OUT OF POSITION (LT TE MIDFLAP)

THE FLAPS WOULD NOT EXTEND BEYOND 8 DEGREES DURING FLAP EXTENSION FOR LANDING. THE FLAPS WOULD NOT MOVE USING ALTERNATE FLAP SYSTEM. THE LEADING EDGE DEVICES WENT TO FULL EXTENSION. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LT INBOARD FLAP JAMMED ON MIDFLAP TORQUE SHAFT CLEARANCE DOOR. THE CLEARANCE DOOR WAS REMOVED AND PLACED ON CONFIGURATION DEVIATION LIST(CDL) 57-19.

Part: SENSOR — INOPERATIVE (LT MLG)

THE LT MLG RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER TAKEOFF. THE GEAR WAS CYCLED, BUT THE LIGHT REMAINED ILLUMINATED. WHEN GEAR WAS EXTENDED ALL THREE GREEN LIGHTS ILLUMINATED WITH NO RED LIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE FOUND THE LEFT MLG UPLOCK SENSOR AT FAULT. THE LT UPLOCK SENSOR WAS REPLACED. IN ADDITION, THE M988 CARD WAS REPLACED AS A PRECAUTIONARY MEASURE, OPERATIONAL CHECKS WERE GOOD IAW MM 32-09-01.