N14325

Part: SERVICE PANEL — CORRODED (BS 986.5) · airframe 62,296 hrs · 32,960 cycles

INSPECTION FOUND CORROSION AND 3 POPPED RIVETS AT FORWARD EDGE OF LAV SERVICE PANEL, STA 986.5, RBL 25. A REPAIR WAS INSTALLED IAW ECRA 5331-01355.

Part: SKIN — CORRODED (BS 500C) · airframe 62,296 hrs · 32,960 cycles

FWD CARGO FUSELAGE SKIN HAS CORROSION AT STA 500C+18 LBL-17. SKIN REPAIR PER SRM 53-00-01 REPAIR 31 FIG 201.

Part: STRINGER — CORRODED (BS 867 S26R) · airframe 62,296 hrs · 32,960 cycles

AFT BAG BIN STA 867 STRINGER 26 RT HAS CORROSION. INSTALLED REPAIR PER SRM 53-00-03 FIG 201.

Part: STRINGER — CORRODED (BS 500C S26L) · airframe 62,296 hrs · 32,960 cycles

FWD CARGO STA 500C S26L CORROSION. INSTALLED REPAIR AT S26L STA 500C IN FWD CARGO IAW SRM 53-00-03 REPAIR 1.

Part: ANGLE — CRACKED (BS 348-350 S16L) · airframe 62,296 hrs · 32,960 cycles

ANGLE CRACKED STA 348-350 STR 16L. REMOVED & REPLACED ANGLE PER ECRA 5311-01364.

Part: SKIN — CRACKED (LT NACELLE) · airframe 62,296 hrs · 32,960 cycles

NR 1 ENG PYLON CRACKED AT ACCESS PANEL 5727. INSTALLED DOUBLER PER ECRA 5430-01230.

Part: BRACKET — CRACKED (BS 351 S16L) · airframe 62,296 hrs · 32,960 cycles

ANGLE BRACKET CRACKED STA 351 STR 16L. REMOVED AND REPLACED BRACKET PER ECRA 5311-01364.

Part: BRACKET — CRACKED (BS 348-351 S16L) · airframe 62,296 hrs · 32,960 cycles

ANGLE BRACKET CRACKED STA 348-351 STR 16L. REMOVED & REPLACED BRACKET PER ECRA 5311-01364.

Part: FRAME — CORRODED (BS 227) · airframe 62,296 hrs · 32,960 cycles

STA 227 LBL 5 TO RBL 5 FRAME CORRODED. REPAIR ACCOMP PER ECRA 5311-01366.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 62,296 hrs · 32,960 cycles

C-1 DOOR CUTOUT FED FRAME CRACKED AT LWR STOP PAD MOUNT. REMOVED AND REPLACED PER SRM 51-40-02.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 62,296 hrs · 32,960 cycles

FWD CARGO STRINGER 27L HAS CORROSION ON IT AT STA 500C+18 LBL. REPAIRED STRINGER PER SRM 53-00-03.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,296 hrs · 32,960 cycles

FWD CARGO LWR FRAME HAS CORROSION ON FED SIDE AT STA 500D LBL 16 TO LBL 21. REPLACED FWD CARGO LWR FRAME PER SRM 53-00-07.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 62,296 hrs · 32,960 cycles

C-2 DOOR CUTOUT FWD FRAME HAS CRACK. REPLACED FWD FRAME PER SRM 51-40-02 BOEING DRAWING 65-47959.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,296 hrs · 32,960 cycles

UPPER FRAME SECTION STA 440 STR 17R-14R HAS CRACK AT FASTENER HOLE. REPLACED UPPER FRAME AT STA 440 IAW SRM 51-40-02.

Part: SHEAR TIE — CRACKED (BS 500D) · airframe 62,296 hrs · 32,960 cycles

INSPECTION FOUND A .5 INCH CRACK IN LEFT FRAME SHEAR TIE AT STA 500D BETWEEN STRINGERS 10L AND 11L. THE SHEAR TIE WAS REMOVED AND A NEW SHEAR TIE WAS INSTALLED IAW BOEING DRAWING 69-73057 AND SRM 51-40-02.

Part: CHARGER — INOPERATIVE (AFT GALLEY) · airframe 62,092 hrs · 32,865 cycles

INSPECTION FOUND THE LAST 4 SEAT MOUNTED EMERGENCY LIGHTS OUT. THREE BATTERY CHARGERS IN THE AFT GALLEY WERE REMOVED AND REPLACED IAW AMM 33-51-51. THE EMERGENCY LIGHTS NOW OPERATE NORMALLY.

Part: SKIN — CRACKED (BS 727D-727E) · airframe 61,281 hrs · 32,492 cycles

INSPECTION FOUND A 1.5 INCH CRACK IN RT FUSELAGE SKIN AT STA 727D-727E, S22R-24R, AT AFT EMERGENCY LIGHT. THE SKIN WAS REPAIRED IAW ECRA 5330-03682.

Part: SIGN — INOPERATIVE (EMERGENCY EXIT) · airframe 61,281 hrs · 32,492 cycles

THE RIGHT OVERWING ESCAPE DOOR EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. THE EXIT SIGN WAS REMOVED AND REPLACED IAW REFERENCE TO SWP 20-13-12 AND BRUCE WDM 33-50-00.

Part: SKIN — CRACKED (STA 727D-727E) · airframe 58,946 hrs · 31,403 cycles

INSPECTION FOUND A 3" CRACK IN FUSELAGE SKIN BELOW EMERGENCY LIGHT AT STA 727D-727E, S22L TO S24L. AN INTERIM REPAIR WAS INSTALLED IAW ECRA 5330-03560 AND A DIP WAS ISSUED TO PERFORM A PERMANENT REPAIR WITHIN 24 MONTHS OR 6,000 FLIGHT CYCLES WHICHEVER COMES FIRST.

Part: SKIN — CRACKED (BS 867) · airframe 57,895 hrs · 30,898 cycles

INSPECTION FOUND A 3.375 INCH CRACK IN FUSELAGE SKIN AFT OF AFT CARGO DOOR AT STA 867, S23R. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-00-01, DETAIL X, FIGURE 201, REPAIR 31, PAGE 231.

Part: ACTUATOR — INOPERATIVE (NLG) · airframe 56,801 hrs · 30,365 cycles

WHEN THE GEAR HANDLE WAS PLACED DOWN ON FINAL APPROACH, THE NLG DID NOT EXTEND. THE CHECKLIST WAS RUN AND THE GEAR WAS EXTENDED MANUALLY WITH THREE GREEN LIGHTS RECEIVED. THE AIRCRAFT LANDED NORMALLY. MAINTENANCE REMOVED AND REPLACED THE NLG LOCK ACTUATOR IAW MM 32-33-21. IN ADDITION, THE NLG HYDRAULIC MODULE WAS REPLACED AS A PRECAUTIONARY MEASURE IAW MM 32-33-31. LEAK AND OPERATIONAL CHECKS WERE GOOD.

Part: SKIN — CRACKED (BS 727E) · airframe 56,676 hrs · 30,309 cycles

CRACK IN FUSELAGE SKIN AT STA 727E, STRINGER 18, 2.5 IN. REPAIRED CRACK PER SRM 53-00-01, FIG 201.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 55,726 hrs · 29,868 cycles

INSPECTION FOUND SKIN BULGED AND RIVET HEADS STRESSED AT STA 360 AND S28L. THE E&E DOOR CUTOUT BEAM LOWER T-CHORD WAS FOUND CORRODED. THE T-CHORD WAS REPAIRED IAW ECRA 5311-01229.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 55,726 hrs · 29,868 cycles

INSPECTION FOUND A 1.75 INCH CRACK IN C-1 DOOR INNER SKIN AT CENTER LIGHTENING HOLES. A DOUBLER WAS INSTALLED IAW ECRA 5232-01063.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 55,726 hrs · 29,868 cycles

INSPECTION FOUND A .5 INCH CRACK IN C-2 DOOR OUTER SKIN. THE CRACK WAS LOCATED AT THE AFT UPPER CORNER OF C-2 DOOR HANDLE CUTOUT. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-30-01.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 55,726 hrs · 29,868 cycles

INSPECTION FOUND THE AFT CARGO COMPARTMENT DOOR CUTOUT FORWARD FRAME CORRODED ON I/B SIDE AT STA 794, L26R TO L27R. THE CORRODED AREA WAS CUT OUT AND DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-70-11.

Part: DOOR FRAME — CORRODED (STA) · airframe 55,726 hrs · 29,868 cycles

INSPECTION FOUND THE R-2 AFT DOOR FRAME CORRODED AT STA 996, RBL 48. A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-70-11.

Part: GATE — CORRODED (R-2 DOOR) · airframe 55,726 hrs · 29,868 cycles

INSPECTION FOUND THE R-2 DOOR LOWER GATE CORRODED ON INTERIOR AND EXTERIOR SURFACE. THE LOWER GATE WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 55,726 hrs · 29,868 cycles

INSPECTION FOUND FLOORBEAM CORRODED AT STA 344, LBL 48 TO RBL 48. THE FLOORBEAM SECTION WAS REMOVED AND REPLACED IAW SRM 53-10-51.

Part: SKIN — GOUGED (LT WING LE) · airframe 52,527 hrs · 28,236 cycles

INSPECTION FOUND LT WING LEADING EDGE SKIN GOUGED AT CENTER AUX TRACK ICE DOOR CUTOUT (UNDER NR 1 SLAT). REPAIRED IAW SRM 51-70-16.

Part: SKIN — CRACKED (NR 5 SLAT) · airframe 52,527 hrs · 28,236 cycles

INSPECTION FOUND FIVE 1 INCH CRACKS IN NR 5 SLAT SKIN LOWER SURFACE I/B OF AUX TRACK. A DOUBLER WAS INSTALLED IAW SRM 57-43-01.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 52,527 hrs · 28,236 cycles

INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT AT STA 540, RBL 2 AND AT LBL 2. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-10-2.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 51,806 hrs · 27,787 cycles

INSPECTION FOUND AFT PRESSURE BULKHEAD WEB CORRODED AT STA 1016 JUST LEFT OF BL 0. REPAIRED WEB IAW SRM 53-80-08 AND BOEING DRAWING 65C28106.

Part: SKIN — DENTED (C-2 DOOR) · airframe 46,766 hrs · 24,896 cycles

INSPECTION FOUND THREE DENTS IN C-2 DOOR SKIN AT TEN INCHES FROM AFT SIDE AND FROM FIVE INCHES ABOVE PAINT LINE TO THIRTEEN INCHES ABOVE PAINT LINE. THE DENTED AREA WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW SRM 52-00-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 46,766 hrs · 24,896 cycles

INSPECTION FOUND AFT BAGGAGE BIN CENTER FLOOR SUPPORT CORRODED AT STA 727D, RBL 18. A NEW SUPPORT AND REPAIR ANGLES WERE INSTALLED IAW SRM 51-20-01.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 46,766 hrs · 24,896 cycles

INSPECTION FOUND STRINGER 4L SPLICE CRACKED AT STA 907. THE SPLICE WAS REMOVED AND REPLACED IAW SRM 53-00-03, FIGURE 203.

Part: WEB — CRACKED (STA 312) · airframe 46,766 hrs · 24,896 cycles

INSPECTION FOUND A 1/4" CRACK IN STRESS WEB AT FLOORBEAM ATTACH POINT, STA 312, BL 0. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-10-02.

Part: FITTING — CORRODED (CABIN) · airframe 46,766 hrs · 24,896 cycles

INSPECTION FOUND L-1 DOOR AFT GIRT BAR LATCH MOUNT CORRODED. THE GIRT BAR LATCH MOUNT WAS REMOVED AND REPLACED IAW SRM 51-40-00.

Part: ANGLE — CORRODED (STA 944-991.5) · airframe 46,766 hrs · 24,896 cycles

INSPECTION FOUND L-2 DOOR Z-ANGLE CORRODED AT STA 944-991.5. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 46,766 hrs · 24,896 cycles

INSPECTION FOUND FLOOR SUPPORT CORRODED AT FASTENER HOLES, STA 294-312, LBL 12. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-2.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 46,766 hrs · 24,896 cycles

INSPECTION FOUND A 1INCH CRACK IN WEB ANGLE AT STA 927-947.5, BL 0. THE WEB ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02.

Part: SKIN — GOUGED (@ DORSAL FIN) · airframe 46,766 hrs · 24,896 cycles

INSPECTION FOUND FUSELAGE SKIN GOUGED AT FORWARD END ON DORSAL FIN MOUNT AREA. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-00-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 46,766 hrs · 24,896 cycles

INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 947.5-967, RBL 18. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-40-00.

Part: FITTING — CORRODED (FUSELAGE) · airframe 46,766 hrs · 24,896 cycles

INSPECTION FOUND GALLEY MOUNTS CORRODED AT STA 946.5, LBL 14 AND RBL 8. THE GALLEY MOUNTS WERE REMOVED AND REPLACED IAW SRM 53-10-03.

Part: FLOORBEAM — CORRODED (STA 1016) · airframe 46,766 hrs · 24,896 cycles

INSPECTION FOUND FLOORBEAM CORRODED AT STA 1016, LBL 21 TO LBL 35. A CAP WAS INSTALLED ON BEAM IAW ECRA 5310-03851, REV A.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 46,766 hrs · 24,896 cycles

INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT AT STA 540, BL 0. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 46,766 hrs · 24,896 cycles

INSPECTION FOUND LT AFT LAV WALL SUPPORT CORRODED AT STA 1013, LBL 5 AND H STRAP CORRODED AT STA 1012, LBL 5, UNDER LAV WALL SUPPORT. THE SUPPORT AND STRAP WERE REMOVED AND REPLACED IAW SRM 53-10-3.

Part: FLOORBEAM — CORRODED (STA 967 & 986.5) · airframe 46,766 hrs · 24,896 cycles

INSPECTION FOUND FLOORBEAM SECTIONS CORRODED AT STA 967, RBL 17.5 AND AT STA 986.5, RBL 16 TO LBL 46. THE FLOORBEAM SECTIONS WERE REMOVED AND REPLACED IAW ECRA 5310-03851.

Part: WEB — CORRODED (STA 1016&1020) · airframe 46,766 hrs · 24,896 cycles

INSPECTION FOUND WEB CORRODED AT STA 1020, LBL 23 AND AT STA 1016, RBL 7 - LBL 16. A NEW WEB WAS INSTALLED ON LEFT OF CENTER BBL 0 TO LBL 38 AND A NEW WEB WAS INSTALLED ON RIGHT OF CENTER BBL 0 TO RBL 38 IAW SRM 53-10-3.

Part: FLOOR SUPPORT — CORRODED (STA 1006-1016) · airframe 46,766 hrs · 24,896 cycles

INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 1006-1016, LBL 5. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 53-10-3.

Part: STRINGER — CRACKED (STA 907) · airframe 46,766 hrs · 24,896 cycles

INSPECTION FOUND AN 1/8" CRACK IN STRINGER 4R SPLICE AND STRINGER 6R SPLICE AT STA 907. THE STRINGER SPLICES WERE REMOVED AND NEW STRINGER SPLICES WERE INSTALLED IAW SRM 51-10-02.

Part: SKIN — DENTED (CARGO DOOR) · airframe 45,703 hrs · 24,392 cycles

INSPECTION FOUND C-1 DOOR OUTER SKIN DENTED JUST AFT OF DOOR HANDLE. THE DENTED SECTION OF SKIN WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 52-00-01, FIGURE 203.

Part: MEGAPHONE — INOPERATIVE (AFT CABIN) · airframe 45,421 hrs · 24,255 cycles

THE AFT CABIN MEGAPHONE WAS FOUND INOPERATIVE. THE MEGAPHONE WAS REMOVED AND REPLACED.

Part: WIRE — DAMAGED (CABIN) · airframe 45,148 hrs · 24,119 cycles

INSPECTION FOUND ROW 14-21 SEAT EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE FOUND A DAMAGED WIRE UNDER SEAT 19B. THE WIRE WAS REPAIRED IAW MM 20-10-13 AND OPERATION CHECKED GOOD.

Part: FLOORBEAM — CORRODED (BS 986.5)

INSPECTION FOUND LOWER SURFACE OF FLOORBEAM AT NUT PLATE FOR R-2 DOOR GIRT BAR LATCH, STA 986.5 CORRODED. A STRAP REPAIR WAS INSTALLED IAW ECRA 5360-01030 AND SRM 53-00-51, FIGURE 203.

Part: SKIN — CRACKED (CARGO DOOR)

INSPECTION FOUND A 1 INCH CRACK AT LIGHTENING HOLE OF C-1 DOOR INTERNAL SKIN. REPAIRED IAW ECRA 5230-01500.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION FOUND MID-AISLE EMERGENCY EXIT LIGHT AT STA 628 INOPERATIVE. THE EMERGENCY LIGHT BATTERY PACK WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD.

Part: TIRE — FAILED (LT MLG)

FLT NR 0216 - ORD - THE LEFT MLG NR 1 TIRE THREW ITS TREAD ON TAKEOFF FROM PHX DESTINED FOR EWR. THE CREW WAS NOTIFIED OF THE TIRE DAMAGE AND ELECTED TO DIVERT TO ORD DUE TO THE WEATHER CONDITIONS IN EWR. THE AIRCRAFT LANDED AT ORD WITHOUT INCIDENT. MAINTENANCE FOUND THAT THE NR 1 TIRE CAP WAS GONE, BUT THE TIRE WAS STILL INFLATED. THERE WERE DENTS IN THE LEFT INBOARD AFT FLAP AND THERE WAS DAMAGE TO BOTH THE LEFT GEAR INNER AND CENTER DOORS. THE NR 1 AND NR 2 TIRE/WHEEL ASSEMBLIES WERE REMOVED AND REPLACED. THE LEFT INBOARD AFT FLAP WAS REMOVED AND REPLACED. THE LEFT GEAR INNER AND CENTER DOORS WERE REMOVED AND PLACED ON CDL. (M)

Part: RETRACT MECH — BINDING (NR 2 SLAT)

CLE - FLT 1567 - THE AIRCRAFT EXPERIENCED AN UNCOMMANDED ROLL 30 DEGREES TO THE LT AND THEN 30 DEGREES TO THE RT WHILE ON DESCENT INTO CLE. AUTOPILOT WAS ON AND THE YAW DAMPENER AT TIME OF OCCURRENCE SHOWED FULL LEFT. AIRCRAFT LANDED AT CLE WITHOUT INCIDENT. THE SDR WILL REMAIN OPEN FOR PART INFO PENDING CORRECTIVE ACTION. SUPPLEMENT - A READING OF THE FLIGHT DATA RECORDER REVEALED ACFT ONLY ROLLED 3 DEGREES TO THE LT AND THE CAPTAIN OVER-CORRECTED 9 DEGREES TO THE RT. ENGINEERING CONCLUDED NR 2 SLAT WAS BINDING AND AUTOPILOT WORKED PROPERLY COMPENSATING FOR THE ROLL. NR 2 SLAT WAS ADJUSTED. BOEING HAS ASSUMED INVESTIGATION. A 60-DAY HISTORY SINCE THIS OCCURRENCE REVEALED NO REPEATS. (X)

Part: SKIN — CRACKED (NR 5 LE SLAT)

HOU - INSPECTION FOUND A .25 INCH CRACK IN LOWER SKIN OF NR 5 SLAT AT SLAT ACTUATOR. THE SKIN WAS REPAIRED IAW ECRA 5750-01159 AND BOEING DRAWING 65C30133. (M)

Part: CHANNEL — CRACKED (LT PYLON)

HOU - INSPECTION FOUND A 10 INCH CRACK IN LEFT PYLON SPAR WEB CHANNEL ON INBOARD EDGE AT STATION 305-315. THE AREA WAS REPAIRED IAW SRM 51-10-02 AND IN REF TO BOEING DRAWING NR 313A1355. (M)

Part: SKIN — CRACKED (NR 6 LE SLAT)

HOU - INSPECTION FOUND A .25 INCH CRACK IN LOWER SKIN OF NR 6 SLAT AT SLAT ACTUATOR. THE SKIN WAS REPAIRED IAW ECRA 5750-01159 AND BOEING DRAWING 65C30133. (M)

Part: RETRACT MECH — LACK OF LUBE (LANDING GEAR)

CLE - FLT 1483 - THE NOSE GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER TAKEOFF FROM CLE. THE GEAR WAS EXTENDED WITH ALL INDICATIONS NORMAL AND THE AIRCRAFT WAS RETURNED TO CLE. MAINTENANCE INSPECTED THE NLG AND FOUND NO DEFECTS. ALL NLG FITTINGS WERE LUBRICATED AND SENSORS WERE CLEANED. THE NOSE GEAR WAS SWUNG THREE TIMES WITH OPERATION AND INDICATIONS CHECKING NORMAL. THE AIRCRAFT HAS COMPLETED OVER 15 FLIGHTS WITHOUT A REPEAT OF THE PROBLEM. (X)