N14604

Part: TRANSDUCER — FAILED (MLG) · airframe 45,045 hrs · 23,767 cycles

ANTI SKID INOP LIGHT ON FORWARD PANEL ILLUMINATED IN-FLIGHT. WENT OUT PRIOR TO LANDING. PREVIOUS HISTORY. RAN QRH. REMOVED AND REPLACED NR 3 MAIN WHEEL TRANSDUCER IAW MM 32-42-11. OPS CHECKED GOOD. NO OTHER DEFECT NOTED AT THIS TIME. ROTABLE PARTS CHANGE WAS INDICATED - TT 1390944 SN OFF 01114 TRANSDUCER, MLG OFF 03-3246-9-0001 1114 ON 03-3246-9-0001 5056.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,843 hrs · 22,604 cycles

MAIN FRAME CRACKED STA 616 RT SIDE JUST ABOVE FUEL TANK. REPAIRED MAIN FRAME AT STA 616 RT JUST ABOVE FUEL TANK REF ECRA 5311-01487. HOWEVER, WITHIN 9000 FLIGHT CYCLES AND AT INTERVALS NOT TO EXCEED 9000 FLIGHT CYCLES THEREAFTER, PERFORM AN INSPECTION PER PART 2 OF ECRA 5311-01487. INTERIM REPAIR ACCOMPLISHED PER ECRA 5311-01487, PART 1. WITHIN 9000 FLIGHT CYCLES AND AT INTERVALS NOT TO EXCEED 9000 FLIGHT CYCLES THEREAFTER, PERFORM AN INSPECTION PER PART 2 OF ECRA 5311-01487.

Part: SKIN — CRACKED (BS 303) · airframe 42,843 hrs · 22,604 cycles

SUPPORT TASK FWD ENTRY DOOR LWR HINGE CUTOUT HAS CRACK INDICATION AT 2EA FASTENERS HOLE (MARKED) JUST BELOW WL 236.68 AND FWD OF STA 303.90 REF TASK INSTRUCTION ITEM 20.0 OF EA 5330-037 36 REV B -OPERATION 03. INSTALLED REPAIR REF EC/RA 5330-04014.

Part: SKIN — CRACKED (L1 DOOR) · airframe 42,843 hrs · 22,604 cycles

L-1 DOOR AFT SIDE INNER SKIN & REINFORCEMENT STRIP CRACKED AT 4TH STOP PIN MOUNT FROM BOTTOM REPAIR ACCOMPLISHED PER ECRA 5210-02149.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 42,843 hrs · 22,604 cycles

RT HORIZONTAL STAB, LOWER T/E SKIN NEAR AFT SPAR, STAB STA 125 .00 APPROX APPEARS TO BE CRACKED. TRIMMED OUT CRACKED SECTION OF SKIN AND INSTALLED FILLER AND REPAIR DOUBLER FROM STAB STA 111 TO STA 166, SEALED REPAIR AND RESTORED FINISH PER ECRA 5510-01616 REV A. ADDED WEIGHT OF REPAIR DOUBLER WAS 2.55 LBS.

Part: SKIN — CORRODED (FUSELAGE) · airframe 42,843 hrs · 22,604 cycles

STA 907 LT AFT SIDE OF BEAM, SKIN HAVE CORROSION BETWEEN STR 19 LT AND 24 LT CTN 53-310-218. REMOVED AND REPLACED SPLICE STRAP AT STA 907 STR 19-24 LT REF SRM 51-40-02.

Part: FRAME — CORRODED (FUSELAGE) · airframe 42,843 hrs · 22,604 cycles

CORROSION ON FRAME STA 907 BETWEEN STR 21R - STR 22R AT SKIN ATTACH POINT. INSTALLED FRAME REPAIR AT SKIN ATTACHMENT REF SRM 53-00-07, ATTACH HEAT TREAT FORM 43.0150 AND 44.0008.

Part: BEAM — CORRODED (FUSELAGE) · airframe 42,843 hrs · 22,604 cycles

AFT CARGO STA 907 RT AFT SIDE OF BEAM SKIN HAVE CORROSION. REPLACED SKIN SPLICE, SRM 51-40-02.

Part: SKIN — CORRODED (FUSELAGE) · airframe 42,843 hrs · 22,604 cycles

FWD CARGO COMPARTMENT DOOR CUTOUT AFT LWR CORNER HAS DEEP CORROSION. INSTALLED REPAIR DOUBLER AT DAMAGED AREA PER SRM 53-00-01 REPAIR 32.

Part: HINGE FITTING — WORN (SPOILER) · airframe 42,843 hrs · 22,604 cycles

NR 4 GROUND SPOILER O/B HINGE FITTING WORN (ON WING). REMOVED AND REPLACED FITTING IN REF TO SRM 51-40-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,843 hrs · 22,604 cycles

SUPPORT TASK, FUSELAGE FRAME CRACKED AT STA 827 BETWEEN STR 8 & 9 LT. REPAIRED FRAME AT STA 827 LT BETWEEN STR 8& STR 9 PER ECRA 5311-01484. DIP GENERATED ON L/P 9715509.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,843 hrs · 22,604 cycles

SUPPORT TASK FUSELAGE FRAME CRACKED AT STA 867 BETWEEN STR 8&9 RT. REPAIRED CRACKED FRAME PER EA 5310-04498.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,843 hrs · 22,604 cycles

SUPPORT TASK FUSELAGE FRAME CRACKED AT STA 747 BETWEEN STR 8 & 9 RT. REPAIRED FRAME AT STA 747 BETWEEN STR 8 & 9 RT. REF EA 5310-04498, DIP GENERATED ON NON-ROUTINE LG PG 9715509 SEQ N00700.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,843 hrs · 22,604 cycles

SUPPORT TASK FUSELAGE FRAME CRACKED AT STA 727A BETWEEN STR 8&9 RT. INSTALLED REPAIR ANGLES A&B PER EA 5310-04498 OP 02.

Part: ANGLE — CORRODED (L1 DOOR) · airframe 42,843 hrs · 22,604 cycles

L1 DOOR L-ANGLE HAS CORROSION STA 312 TO 344. INSTALLED NEW L-ANGLE ON L-1 REF SRM 51-40-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,843 hrs · 22,604 cycles

SUPPORT TASK FUSELAGE FRAME CRACKED AT STA 400 BETWEEN STR 8&9 RT (SEE ATTACHED FORMS 44.0008 AND 43.0150). TRIMMED OUT DAMAGE AND INSTALLED REPAIR ANGLES PER EA 5310-04498.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,843 hrs · 22,604 cycles

SUPPORT TASK FUSELAGE FRAME CRACKED AT STA 727B BETWEEN STR 8 & 9 RT. TRIMMED OUT DAMAGE AND INSTALLED REPAIR DOUBLER ANGLES REF EA 5310-04498 (SEE ATTACHED .0008 FORMS).

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,843 hrs · 22,604 cycles

SUPPORT TASK FUSELAGE FRAME CRACKED AT STA 787 BETWEEN STR 8&9LT (SEE ATTACHED FORMS 44.0008). REPAIRED FUSELAGE FRAME AT STA 787 BETWEEN STR 8&9LT PER EA 5310-04498.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 42,843 hrs · 22,604 cycles

FLOORBEAM STA 986.5 LBL 11 TO LBL 31 HAS CORROSION. INSTALLED STRAP REPAIR, TREATED AND PRIMED REF SRM 53-00-51.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,843 hrs · 22,604 cycles

SUPPORT TASK FUSELAGE FRAME CRACKED AT STA 380 BETWEEN STR 8& 9 RT (SEE ATTACHED FORMS 44.0008 AND 43.0150). TRIMMED OUT DAMAGE, INSTALLED REPAIR ANGLES REF EA 5310-04498.

Part: ANGLE — CRACKED (STAB STA 83.5) · airframe 36,569 hrs · 19,303 cycles

INSPECTION FOUND A .5 INCH CRACK IN LT HORIZONTAL STABILIZER LEADING EDGE WEB L-ANGLE AT STAB STA 83.5. A REPAIR WAS INSTALLED IAW ECRA 5510-01883.

Part: FRAME — CRACKED (BS 482) · airframe 36,569 hrs · 19,303 cycles

INSPECTION FOUND A .75 INCH CRACK IN FORWARD CARGO DOOR CUTOUT AFT FRAME WEB AT LOWER DOORSTOP FITTING, STA 482, WL 160, S24L. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 36,569 hrs · 19,303 cycles

INSPECTION FOUND A .5 INCH CRACK IN FORWARD CARGO DOOR CUTOUT FORWARD FRAME WEB AT LOWER DOORSTOP FITTING, WL 160, S24R. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: ATTACH FITTING — CRACKED (BS 360) · airframe 36,569 hrs · 19,303 cycles

INSPECTION FOUND A 1 INCH CRACK IN ATTACHMENT CLIP AFT OF L-1 DOOR AT STA 360, STRINGER 11L. THE ATTACHMENT CLIP WAS REPLACED IAW ECRA 5311-01306. A DIP WAS CREATED TO REINSPECT THE CLIP AT INTERVALS NOT TO EXCEED 6,000 FLIGHT CYCLES.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 36,569 hrs · 19,303 cycles

INSPECTION FOUND R-2 DOORWAY Z-ANGLE CORRODED JUST AFT OF DOORWAY AT STA 986.5, RBL 46. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHT) · airframe 34,297 hrs · 18,126 cycles

THE EMERGENCY LIGHT AT SEAT 24 ABC WAS FOUND INOPERATIVE. THE LIGHT HARNESS WAS REPLACED IAW MM 33-51-81.

Part: COOLING FAN — FAILED (E/E BAY) · airframe 28,110 hrs · 14,846 cycles

AN OBJECTIONABLE ODOR WAS DETECTED BY FLIGHT ATTENDANT AND PASSENGERS JUST PRIOR TO DESCENT INTO COS. NO SIGN OF SMOKE WAS DETECTED IN CABIN OR COCKPIT. ALL ELECTRICAL SYSTEMS AND FLUID LEVELS CHECKED NORMAL. THE AIRCRAFT LANDED AT COS WITHOUT INCIDENT. MAINTENANCE FOUND THE EQUIPMENT COOLING FAN FAILED AND THE CIRCUIT BREAKER WAS POPPED. THE FAN WAS TEMPORARILY PLACARD INOPERATIVE FOR FUTURE REPLACEMENT.

Part: ENGINE — LEAKING (NR 2) · airframe 21,613 hrs · 11,268 cycles

SHORTLY AFTER TAKEOFF FROM EWR SMOKE ENTERED THE CABIN AND THE LAV SMOKE DETECTORS ACTIVATED. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED SAFELY. THE SMOKE DISSIPATED RAPIDLY ONCE ON THE GROUND. THE AIRCRAFT TAXIED TO THE GATE UNDER ITS OWN POWER. MAINTENANCE FOUND OIL IN THE NR 2 ENGINE BLEED DUCTS. THE NR 2 ENGINE WAS REMOVED AND REPLACED. BOTH COALESCER BAGS WERE REPLACED. THE ENGINE WAS RUN AND OPERATIONAL CHECKS WERE GOOD.

Part: SKIN — LIGHTNING STRIKE (BS 727 - 1016)

INSPECTION FOUND LIGHTNING STRIKE DAMAGE TO LT LOWER FUSELAGE SKIN AT STA 727-908 AT OR BELOW PAINT LINE AND AT STA 908-1016 BELOW L17L. THE DAMAGED AREA WAS REPAIRED BY BURNISHING AND INSTALLING PLUG RIVETS IAW SRM 53-00-01, FIGURE 219.

Part: BATTERY CHARGER — INOPERATIVE (CABIN)

INSPECTION FOUND EMERGENCY PATH LIGHTS INOPERATIVE FROM ROW 5 TO 9. MAINTENANCE FOUND THE M1135 BATTERY CHARGER INOPERATIVE. THE BATTERY CHARGER WAS REMOVED AND REPLACED, OPERATION OF THE PATH LIGHTS WAS RESTORED.

Part: EEL FUSE — FAILED (CABIN)

IAH - FLT 1510 - INSPECTION FOUND MIDDLE ZONE OF AISLE PATH LIGHTING INOPERATIVE. A BLOWN FUSE WAS FOUND IN THE AFT EMERGENCY PATH LIGHTING BATTERY PACK. THE FUSE WAS REPLACED AND OPERATION OF THE AISLE PATH LIGHTING WAS RESTORED. (X)