N69311

Part: ATTACH FITTING — CRACKED (BS 312) · airframe 62,840 hrs · 33,718 cycles

INSPECTION FOUND A .5 INCH CRACK IN H-STRAP ON FUSELAGE STRUCTURE STA 312 L-1 DOOR LOWER HINGE ATTACH FITTING. A REPAIR WAS INSTALLED IAW ECRA 5311-01342.

Part: SKIN — CORRODED (BS 1006) · airframe 62,840 hrs · 33,718 cycles

INSPECTION FOUND SKIN STRAP CORRODED AT STA 1006, S27R, BL 0 TO RBL 8. THE CORRODED SECTION OF SKIN STRAP WAS REMOVED AND A DOUBLER AND TRIPLER WERE INSTALLED IAW ECRA 5331-01327.

Part: FITTING — CRACKED (NR 2 PYLON) · airframe 62,840 hrs · 33,718 cycles

INSPECTION FOUND A 1 INCH CRACK IN NR 2 ENGINE PYLON AFT HORSE COLLAR (FITTING). THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-10-02 AND 51-40-02.

Part: STRUCTURE — CORRODED (BS 227.8) · airframe 62,840 hrs · 33,718 cycles

INSPECTION FOUND CHORD CORRODED AT STA 227.8, RBL 9 TO LBL 9. A LOWER O/B CHORD REPAIR WAS INSTALLED IAW ECRA 5311-01340.

Part: WEB — CRACKED (FUSELAGE) · airframe 62,840 hrs · 33,718 cycles

INSPECTION FOUND A 1 INCH CRACK IN WEB JUST FORWARD OF L-2 DOOR AT STA 942, S11L. THE CLOSE OUT WEB WAS REMOVED AND REPLACED IAW ECRA 5311-01335.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,840 hrs · 33,718 cycles

INSPECTION FOUND A .75 INCH CRACK IN STUB FRAME FOR L-2 DOOR UPPER HINGE AREA, STA 947.5, S11L. THE FRAME WAS REPAIRED IAW ECRA 5311-01335.

Part: STRAP — CRACKED (FUSELAGE) · airframe 62,840 hrs · 33,718 cycles

INSPECTION FOUND A .5 INCH CRACK IN H-STRAP AT THE UPPER L-1 DOOR HINGE ATTACH FITTING, STA 312. THE H-STRAP WAS REPLACED IAW ECRA 5311-01337.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 62,840 hrs · 33,718 cycles

INSPECTION FOUND A .5 INCH CRACK AT AFT END OF ATTACHMENT CLIP, STA 294-309, S10L. THE CLIP WAS REPLACED IAW ECRA 5311-01337.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,840 hrs · 33,718 cycles

INSPECTION FOUND A 1 INCH CRACK IN INTERCOSTAL WEB AT RIVET LOCATED AT STA 294.5, S12L. THE INTERCOSTAL WEB WAS REMOVED AND REPLACED IAW ECRA 5311-01339.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 62,840 hrs · 33,718 cycles

INSPECTION FOUND A 1.5 INCH CRACK AT I/B CORNER OF ATTACHMENT CLIP, STA 360, S10L. THE CLIP WAS REMOVED AND REPLACED IAW ECRA 5311-01339.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 62,840 hrs · 33,718 cycles

INSPECTION FOUND STRINGER 26R CORRODED ON FORWARD END BETWEEN STA 1006-1016. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,840 hrs · 33,718 cycles

INSPECTION FOUND SHEAR TIE CORRODED AT STA 1006, S27R. THE SHEAR TIE WAS REMOVED AND REPLACED IAW MM 51-40-02.

Part: GUSSET — CRACKED (NLG WW) · airframe 62,840 hrs · 33,718 cycles

INSPECTION FOUND A 2 INCH CRACK IN NOSE WHEEL WELL GUSSET AT END OF NLG DRAG BRACE. THE GUSSET WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: FLAP TRACK — CORRODED (T/E FLAP) · airframe 62,840 hrs · 33,718 cycles

INSPECTION FOUND CORROSION INSIDE THE AFT TRANSMISSION MOUNT HOLE OF THE NR 8 FLAP TRACK, RT WING, WS 289-511. THE CORROSION IN THE BORE WAS REAMED, SHOT PEENED, PLATED AND A SLEEVE BUSHING WAS INSTALLED IAW CMM 57-53-15, PAGE 16, FIGURE 6 AND SOPM 20-42-10 AND 20-42-03.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 62,840 hrs · 33,718 cycles

INSPECTION FOUND A 1 INCH CRACK IN FORWARD CARGO DOOR CUTOUT AFT FRAME AT LOWER DOOR STOP FITTING, STA 440, S17R TO 24R. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: PAN — CRACKED (L1 DOOR) · airframe 62,840 hrs · 33,718 cycles

INSPECTION FOUND A .5 INCH CRACK (THREE EACH) IN L-1 DOOR AFT PAN AT NR 5, NR 6, AND NR 7 STOP FITTING ADJUSTMENT ACCESS HOLES. A DOUBLER REPAIR WAS INSTALLED AT EACH CRACK LOCATION IAW ECRA 5210-01941.

Part: FITTING — CORRODED (FUSELAGE) · airframe 62,840 hrs · 33,718 cycles

INSPECTION FOUND STRINGER 17R END FITTING CORRODED JUST BELOW FLOOR LINE AT STA 1016. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: FITTING — CORRODED (FUSELAGE) · airframe 62,840 hrs · 33,718 cycles

INSPECTION FOUND STRINGER 27L END FITTING CORRODED IN BOLT HOLES, STA 1016. THE END FITTING WAS REMOVED AND REPLACED IAW SRM 51-40-12.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 62,840 hrs · 33,718 cycles

INSPECTION FOUND AFT PRESSURE BULKHEAD FORWARD FACE LOWER CHORD ANGLE CORRODED AT STA 1016 FROM S27L T0 S27R. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: FITTING — CORRODED (FUSELAGE) · airframe 62,840 hrs · 33,718 cycles

INSPECTION FOUND STRINGER 27R END FITTING CORRODED IN BOLT HOLES AT STA 1016. THE END FITTING WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 62,840 hrs · 33,718 cycles

INSPECTION FOUND A 1.5 INCH CRACK IN FORWARD CARGO DOOR CUTOUT FORWARD FRAME AT LOWER STOP FITTING, STA 440. THE FORWARD FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 62,840 hrs · 33,718 cycles

INSPECTION FOUND A 1.5 INCH CRACK IN RT WHEEL WELL CEILING PRESSURE DECK ABOVE O/B END OF GROUND SPOILER CONTROL VALVE, STA 664, RBL 40. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-60-51 AND 51-40-02.

Part: WEB — CORRODED (FUSELAGE) · airframe 62,840 hrs · 33,718 cycles

INSPECTION FOUND WEB CORRODED FROM STA 986.5 TO 1006, S21R. THE WEB WAS REMOVED AND REPLACED IAW SRM 53-60-15 AND 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,840 hrs · 33,718 cycles

INSPECTION FOUND FLOORBEAM CORRODED ON UPPER AND LOWER SURFACE AT STA 986.5, LBL 43. THE CORRODED T-CHORD SECTION OF BEAM WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,840 hrs · 33,718 cycles

INSPECTION FOUND SURFACE CORROSION AROUND SCREW HOLES ON FLOORBEAM AT STA 1016 FROM LBL 30 TO LBL 34, S19L-S21L. THE CORROSION WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-00-51.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,840 hrs · 33,718 cycles

INSPECTION FOUND A 0.65 INCH CRACK IN CLIP AT STA 616, S8L. THE CLIP WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,840 hrs · 33,718 cycles

INSPECTION FOUND A .5 INCH CRACK IN CLIP AT STA 597, S8L. THE CLIP WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: SPAR — CORRODED (SS 196.2-200.3) · airframe 58,896 hrs · 31,895 cycles

INSPECTION FOUND THE LT HORIZONTAL STABILIZER REAR SPAR UPPER CAP CORRODED FROM STAB STA 196.2 TO 200.3. THE LT HORIZONTAL STABILIZER ASSEMBLY WAS REMOVED AND REPLACED MM 27-41-11, PAGE 401, FIGURE 401.

Part: SKIN — CRACKED (NR 1 NACELLE) · airframe 58,896 hrs · 31,895 cycles

INSPECTION FOUND A 0.35 INCH CRACK IN NR 1 ENGINE UPPER PYLON PANEL (SKIN) 5727L. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5430-01230, REV B.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,924 hrs · 30,408 cycles

INSPECTION FOUND A 1.8 INCH CRACK IN FUSELAGE SKIN 3 INCHES AFT OF STA 727D AND BELOW S23R. THE SKIN WAS REPAIRED IAW ECRA 5330-03090.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 53,389 hrs · 29,064 cycles

INSPECTION FOUND LIGHT CORROSION ON O/B FLANGE OF LEFT KEELBEAM FROM BS 663-727. INSTALLED REPAIR IAW ECRA 5311-01167.

Part: FITTING — CRACKED (I/B T/E PANEL) · airframe 53,389 hrs · 29,064 cycles

INSPECTION FOUND A .5 INCH CRACK IN LT WING UPPER AFT INBOARD T/E PANEL OUTBOARD SUPPORT FITTING. A NEW SUPPORT FITTING WAS INSTALLED IAW SRM 51-10-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,389 hrs · 29,064 cycles

INSPECTION FOUND CORROSION ALONG THE ENTIRE UPPER SECTION OF FLOORBEAM AT STA 967. THE CORRODED AREA OF FLOORBEAM WAS CUT OUT AND A REPAIR SECTION WAS INSTALLED IAW ECRA 5311-01142.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 53,389 hrs · 29,064 cycles

INSPECTION FOUND LT TIE DOWN RAIL CORRODED AT FASTENERS ON LOWER SURFACE AT STA 947 IN THE AFT CARGO COMPARTMENT. THE TIE DOWN RAIL WAS REMOVED AND REPLACED IAW SRM 53-00-53.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,389 hrs · 29,064 cycles

INSPECTION FOUND CORROSION ON FRAME AT STA 793 BETWEEN S26R AND S25R IN AFT CARGO COMPARTMENT. THE FRAME WAS REPAIRED IAW SRM 51-40-02.

Part: ANGLE — CRACKED (NR 1 PYLON) · airframe 53,389 hrs · 29,064 cycles

INSPECTION FOUND A 4 INCH CRACK IN NR 1 ENGINE PYLON ANGLE FOR AFT LOWER O/B ACCESS PANEL. A NEW ANGLE WAS INSTALLED IAW SRM 51-10-02.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 53,389 hrs · 29,064 cycles

INSPECTION FOUND FORWARD BAGGAGE BIN SKIN SHEAR TIE CORRODED AT STA 460, S28R. THE CORRODED AREA WAS CUT OUT AND A REPAIR DOUBLER AND SHEAR TIE WERE INSTALLED IAW SRM 53-00-07.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 53,389 hrs · 29,064 cycles

INSPECTION FOUND A .2500 INCH CRACK IN VHF RIGHT FORWARD SUPPORT AFT CARGO COMPARTMENT BRACKET AT STA 727D. A NEW SUPPORT BRACKET WAS INSTALLED IAW SRM 51-10-02.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 53,389 hrs · 29,064 cycles

INSPECTION FOUND A 1 INCH AND .5000 INCH CRACK IN AFT BAGGAGE BIN FLOOR PANEL 1536X AT STA 794.5-807. A DOUBLER WAS INSTALLED AT EACH CRACK LOCATION IAW SRM 53-30-53.

Part: SUPPORT — CRACKED (RT WING) · airframe 53,389 hrs · 29,064 cycles

INSPECTION FOUND A .5000 INCH CRACK IN RT WING UPPER MOST I/B T/E PANEL SUPPORT. A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-02.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 53,389 hrs · 29,064 cycles

INSPECTION FOUND A 7.5 INCH CRACK IN FORWARD BAGGAGE BIN WEB AT FORWARD LOWER DOOR JAMB, STA 440. A NEW SECTION OF WEB WAS INSTALLED IAW SRM 51-70-13.

Part: GALLEY TRACK — CORRODED (NR 3 GALLEY) · airframe 53,389 hrs · 29,064 cycles

INSPECTION FOUND NR 3 GALLEY I/B AFT MOUNT CORRODED. THE GALLEY MOUNT WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,389 hrs · 29,064 cycles

INSPECTION FOUND A 1 INCH CRACK IN LT MAIN FRAME BELOW MAIN DECK FLOOR AT STA 616. A DOUBLER ANGLE WAS INSTALLED IAW ECRA 5311-01158.

Part: STIFFENER — GOUGED (FLAP TRACK) · airframe 53,389 hrs · 29,064 cycles

INSPECTION FOUND RT WING NR 6 FLAP TRACK FAIRING I/B STIFFENER GOUGED. THE STIFFENER WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-40-02.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 53,389 hrs · 29,064 cycles

INSPECTION FOUND CORROSION ON CORNER BRACKET O/B OF DOOR CUTOUT RT AFT CORNER FWD ACC COMPT, STA 219. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 53,389 hrs · 29,064 cycles

INSPECTION FOUND UPPER AND LOWER SURFACE OF FLOOR SUPPORT CORRODED BETWEEN STA 967 AND 986.5. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-10-02.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,389 hrs · 29,064 cycles

INSPECTION FOUND CORROSION AROUND NUT CLIP HOLES ON LT AFT LAV WALL SUPPORT HAT CHANNEL. THE WALL SUPPORT HAT CHANNEL WAS REPLACED IAW SRM 51-40-02.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 53,389 hrs · 29,064 cycles

INSPECTION FOUND L-2 DOOR Z-ANGLE CORRODED AT BS 947-986, LBL 48. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,389 hrs · 29,064 cycles

INSPECTION FOUND RT AFT LAV WALL SUPPORT HAT SECTION CORRODED. THE WALL SUPPORT HAT SECTION WAS REPLACED IAW SRM 51-40-02.

Part: WEB — CORRODED (FUSELAGE) · airframe 53,389 hrs · 29,064 cycles

INSPECTION FOUND WEB AT RT LAV WATER SUPPLY LINE FITTING AFT OF STA 1006 CORRODED. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 53-60-15.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 53,389 hrs · 29,064 cycles

INSPECTION FOUND R-1 DOOR Z-ANGLE CORRODED AT STA 227-350. A NEW Z-ANGLE WAS INSTALLED IAW SRM 53-10-15.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 53,389 hrs · 29,064 cycles

INSPECTION FOUND A 1 INCH CRACK IN CEILING WEB OF LT WHEEL WELL AT BS 663, LBL 32. THE CRACKED AREA WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-60-51, FIGURE 203.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 53,389 hrs · 29,064 cycles

INSPECTION FOUND A .5 INCH CRACK IN FLOOR SUPPORT AND SHIM MISSING AT STA 540 BETWEEN LEFT I/B AND O/B SEAT TRACK. A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-10-02.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 53,389 hrs · 29,064 cycles

INSPECTION FOUND A .25 INCH CRACK IN FLOOR SUPPORT AT STA 380-400, BL 0. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 53,389 hrs · 29,064 cycles

INSPECTION FOUND A .5 INCH CRACK IN MAIN DECK FLOOR SUPPORT AT STA 540, BL 0 TO LEFT I/B SEAT TRACK. A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-10-02.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 53,389 hrs · 29,064 cycles

INSPECTION FOUND FORWARD LAV WALL SUPPORT CORRODED AT STA 307, LBL 13 TO 15. THE WALL SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,389 hrs · 29,064 cycles

INSPECTION FOUND FLOORBEAM CORRODED AT STA 312, RBL 21. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, FIGURE 203.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 53,389 hrs · 29,064 cycles

INSPECTION FOUND FLOOR SUPPORT CORRODED JUST AFT OF STA 947.5, LBL 30 TO LBL 40. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: SKIN — DENTED (BS 312-345) · airframe 49,781 hrs · 27,156 cycles

INSPECTION FOUND FUSELAGE SKIN DENTED AT BS 312-345, S22L. THE SKIN WAS REPAIRED IAW SRM 53-00-01.

Part: SKIN PANEL — WORN (HS ATT. AREA) · airframe 49,781 hrs · 27,156 cycles

INSPECTION FOUND L/H FUSELAGE SKIN CUTOUT LOWER PANEL WORN WITH RIVET PULLING THROUGH AT HORIZONTAL STABILIZER ATTACH FITTING. THE SKIN CUTOUT LOWER PANEL WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: SKIN — CRACKED (L/H HOR STAB) · airframe 49,781 hrs · 27,156 cycles

INSPECTION FOUND A 3/4" CRACK IN L/H HORIZONTAL STABILIZER SKIN AT REAR SPAR APPROXIMATELY 65" FROM I/B AREA. THE CRACKED AREA WAS TRIMMED OUT AND A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5510-01613.

Part: SKIN — CRACKED (#2 ENG PYLON) · airframe 49,781 hrs · 27,156 cycles

INSPECTION FOUND A 0.2" CRACK AT O/B AFT CORNER OF #2 PYLON I/B UPPER ACCESS SKIN PANEL #5827. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5430-01230.

Part: SKIN — CRACKED (#2 PYLON) · airframe 49,781 hrs · 27,156 cycles

INSPECTION FOUND A 1/2" CRACK AT LOWER AFT CORNER OF #2 PYLON O/B ACCESS SKIN PANEL #5824. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5430-01204, FIGURE 3.

Part: SKIN — CRACKED (STA 373) · airframe 49,781 hrs · 27,156 cycles

INSPECTION FOUND A 1/2" CRACK IN FUSELAGE EXTERIOR SKIN AT E&E BAY EXHAUST CUTOUT, STA 373. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5330-02894.

Part: SKIN — CRACKED (C-2 DOOR) · airframe 49,781 hrs · 27,156 cycles

INSPECTION FOUND A 3/8" CRACK IN C-2 DOOR EXTERIOR SKIN AT AFT UPPER CORNER OF DOOR HANDLE CUTOUT. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-00-01, FIGURE 202.

Part: SEAT TRACK — CRACKED (STA 727B) · airframe 49,781 hrs · 27,156 cycles

INSPECTION FOUND A 5/8" CRACK IN R/H O/B SEAT TRACK AT STA 727B. THE CRACKED AREA WAS TRIMMED OUT AND A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5321-01121.

Part: DOUBLER — CRACKED (#2 VHF ANT.) · airframe 49,781 hrs · 27,156 cycles

INSPECTION FOUND A 6" CRACK IN INTERIOR DOUBLER ON #2 VHF ANTENNA AT FWD CARGO COMPARTMENT. THE DOUBLER WAS REPLACED IAW SRM 51-20-01, 51-20-05, 51-40-02, AND 51-40-08.

Part: SKIN — DAMAGED (STA 178) · airframe 49,781 hrs · 27,156 cycles

INSPECTION FOUND FUSELAGE SKIN DAMAGED AT STA 178, RBL 5. REPAIRED SKIN IAW SRM 53-00-01.

Part: DOOR FRAME — CRACKED (CARGO DOOR)

INSPECTION FOUND A 5 CRACK IN FORWARD CARGO DOOR AFT LOWER CORNER AND A 2 CRACK WAS LOCATED AT THE FORWARD LOWER CORNER. BOTH THE FORWARD AND AFT LOWER CORNERS OF DOOR FRAME WERE REMOVED AND REPLACED IAW SRM 51-10-2.

Part: FRAME — CRACKED (BS 727)

INSPECTION FOUND A 1 INCH CRACK IN FRAME AT STA 727, STRINGER 14L. REPAIRED IAW ECRA 5310-03926.

Part: SKIN — CRACKED (L2 DOORWAY)

INSPECTION FOUND A .25 INCH CRACK IN SKIN AT L-2 DOOR CUTOUT LOWER HINGE AREA. REPAIRED IAW ECRA 5360-01026.

Part: BRACKET — CRACKED (BS 520)

INSPECTION FOUND A 1 INCH CRACK IN EXPANSION JOINT BRACKET AT BS 520, LBL 45.5. A NEW BRACKET WAS INSTALLED IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (BS 907-930)

INSPECTION FOUND RIGHT O/B SEAT TRACK CORRODED AT STA 907-930. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52.

Part: SEAT TRACK — CORRODED (BS 370)

INSPECTION FOUND LT SEAT TRACK CORRODED AT STA 370. A NEW SEAT TRACK WAS INSTALLED IAW SRM 53-00-52, FIGURE 202.

Part: SEAT TRACK — CORRODED (BS 328-344)

INSPECTION FOUND RT CENTER SEAT TRACK CORRODED AT STA 328-344. A SEAT TRACK REPAIR WAS INSTALLED IAW SRM 53-00-52, FIGURE 202.

Part: STRINGER — CORRODED (BS 1016)

INSPECTION FOUND STRINGER 29R CORRODED AT STA 1016. THE AREA WAS REPAIRED BY INSTALLING A FORMED CHANNEL SECTION WITH FASTENERS IAW SRM 51-70-11, FIGURE 1.

Part: FLOORBEAM — CORRODED (BS 927)

INSPECTION FOUND FLOORBEAM CORRODED AT STA 927, RT O/B SEAT TRACK. THE FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 53-60-51.

Part: FLOORBEAM — CORRODED (BS 328)

INSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT FASTENER HOLE LOCATIONS, STA 328. A NEW UPPER CHORD WAS INSTALLED IAW SRM 53-10-51, FIGURE 205.

Part: FLOORBEAM — CORRODED (BS 312)

INSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT FASTENER HOLE, STA 312. A NEW FLOORBEAM UPPER CHORD WAS INSTALLED IAW SRM 53-10-51, FIGURE 205.

Part: SWITCH — INOPERATIVE (NLG)

THE AIRCRAFT HAD A HISTORY OF THE NOSE GEAR RED UNSAFE LIGHT ILLUMINATING IN FLIGHT. MAINTENANCE REMOVED AND REPLACED THE NOSE GEAR LOCK SWITCH IAW MM 32-61-41. THE NOSE GEAR DOWN SENSOR WAS REPLACED IAW MM 32-61-51. IN ADDITION, THE LANDING GEAR LOGIC CARDFILE UNIT WAS REPLACED AND TESTED IAW MM 32-09-20, PAGES 401-424. ALL CHECKS WERE NORMAL. THE AIRCRAFT HAS FLOWN FIVE FLIGHTS WITHOUT REPEAT OF THE PROBLEM SINCE THIS CORRECTIVE ACTION WAS IMPLEMENTED.

Part: LOGIC CARDS — INOPERATIVE (NLG)

THE NOSE GEAR RED UNSAFE AND GREEN LIGHTS REMAINED ILLUMINATED AFTER GEAR RETRACTION DEPARTING CLE. THE GEAR WAS LOWERED AND NORMAL INDICATIONS WERE SHOWN. THE AIRCRAFT WAS RETURNED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE M1215 AND M983 LANDING GEAR LOGIC CARDS. IN ADDITION, THE NLG LOCK SENSOR WAS ADJUSTED IAW MM 32-61-41, PAGES 401-406. THE GEAR WAS SWUNG SEVERAL TIMES WITH OPERATION AND INDICATIONS CHECKING GOOD.

Part: BALLAST — BURNT (CABIN)

SMOKE WAS SEEN COMING FROM LIGHT AREA OF FIRST CLASS CLOSET WHILE AIRCRAFT WAS AT GATE AFTER PASSENGERS WERE DEPLANED. THE SMOKE STOPPED AFTER EXTERNAL POWER WAS REMOVED FROM BUS AND BATTERY WAS TURNED OFF. MAINTENANCE FOUND THE FORWARD GALLEY WORK LIGHT BALLAST INSIDE COAT CLOSET AT FAULT. THE BALLAST WAS REMOVED AND REPLACED, NO OTHER DISCREPANCIES WERE NOTED.

Part: LOGIC CARD — INOPERATIVE (NLG)

FLT NR 1796 - PHL - THE NOSE GEAR RED LIGHT AND GREEN LIGHT ILLUMINATED WHILE IN FLIGHT FROM IAH TO PHL. PILOT TRIED GEAR HANDLE UP WITH NO CHANGE. WHEN GEAR WAS EXTENDED FOR LANDING AT PHL ALL THREE GREEN LIGHTS ILLUMINATED WITH NO RED. MAINTENANCE FOUND THE M983 LOGIC CARD AT FAULT. THE M983 LOGIC CARD WAS REMOVED AND REPLACED. THE SYSTEM WAS TESTED WITH NO DEFECTS NOTED. THE NOSE GEAR WAS CYCLED IAW MM 32-09-20 WITH OPERATION AND INDICATIONS CHECKING GOOD. (M)

Part: FLOOR — CORRODED (BS 312)

HOU - INSPECTION FOUND A 48 INCH BY 2 INCH AREA OF THE CABIN CENTER FLOOR STRUCTURE CORRODED AT STATION 312. THE AREA WAS REPAIRED PER SRM 53-10-51, FIGURE 205. (M)

Part: SKIN — TORN (BS 1006)

HOU - THE FUSELAGE SKIN WAS TORN WHEN CONTACTED BY A STAND WHILE AIRCRAFT WAS IN D-CHECK MAINTENANCE. THE TEAR WAS LOCATED AT STATION 1006, STRINGER 4R-5R. THE SKIN WAS REPAIRED IAW ECRA 5330-02306. (M)

Part: FLOORBEAM — CRACKED (BS 520)

HOU - INSPECTION FOUND A 1 INCH CRACK IN CABIN FLOORBEAM AT BS 520, RBL 45.5. THE FLOORBEAM WAS REPAIRED IAW ECRA 5320-01208. (X)

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

HOU - THE AFT CABIN EMERGENCY AISLE LIGHTING BATTERY PACK FAILED THE 15 MINUTE DURATION TEST. THE BATTERY PACK WAS REMOVED AND REPLACED AND OPERATION OF THE EMERGENCY AISLE LIGHTING WAS RESTORED. (X)

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

HOU - THE R-2 DOOR OVERHEAD EMERGENCY EXIT SIGN BATTERY PACK FAILED THE 15 MINUTE DURATION TEST. THE BATTERY PACK WAS REMOVED AND REPLACED AND OPERATION OF THE EMERGENCY EXIT SIGN WAS RESTORED. (X)

Part: CARDFILE — INOPERATIVE (LG LOGIC UNIT)

FLT NR 0578 - IAH - THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM IAH. THE OVERRIDE TRIGGER WAS USED AND THE GEAR RETRACTED, BUT THE WARNING HORN SOUNDED INTERMITTENTLY. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A LANDING GEAR LOGIC UNIT CARDFILE AT FAULT. THE CARDFILE WAS REMOVED AND REPLACED. A TAKEOFF WARNING CHECK AND SIMULATED GEAR RETRACTION WAS PERFORMED AND ALL SYSTEMS CHECKED GOOD. (W)