N14628

Part: RELAY — FAULTY (COCKPIT) · airframe 45,044 hrs · 23,776 cycles

STANDBY POWER OFF LIGHT CAME ON INTERMITTENTLY ON TAXI OUT. T/S PER AMM 24-54-00, SSM 24-34-11, AND WDM 91-03-24, R&R'D R330 STANDBY POWER INDICATOR LIGHT RELAY, PERFORMED OPS CHECKS PER AMM 24-54-00, ALL OPS NORMAL.

Part: FRAME — CORRODED (FUSELAGE) · airframe 43,050 hrs · 22,644 cycles

ABB STA 767 FWD SIDE OF FRAME HAS CORROSION BL 0 TO S27R AND TOP OF FRAME. REPAIRED FRAME STA 767 IN ABB, BL 0 TO S27R REF SRM 53-00-07 REPAIR 3.

Part: FRAME — CORRODED (FUSELAGE) · airframe 43,050 hrs · 22,644 cycles

CORROSION ON FRAME STA 807 FWD SIDE BETWEEN STR 27 LT AND 27 RT. CUT OUT DAMAGED SECTION OF SHEAR TIE, FABRICATED REPAIR PARTS AND INSTALLED REF SRM 53-00-07.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,050 hrs · 22,644 cycles

CABIN CREASE BEAM WEB AT FLOOR STA 847 TO 867 STR 17 RT HAVE CORROSION. INSTALLED NEW SHEAR WEB PER SRM 51-40-02 PARGRAPH 4 AND 51-10-02 PARGRAPH 8.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 43,007 hrs · 22,625 cycles

DURING S CHECK FOUND SEVERAL EMER LIGHTS INOP, LT OVERWING EXIT SIGN LIGHT, CABIN CENTER SEAT LIGHTS. R&R EMERGENCY LIGHT BATTERY PACK AT M1669. OPS CHECK GOOD IAW 737M/M 33-51-51.

Part: DETECTOR — FAILED (OVERHEAT SYS) · airframe 40,563 hrs · 21,331 cycles

ON DESCENT INTO EWR THE LEFT WING BODY OVERHEAT LIGHT STARTED FLICKERING AND THEN STAYED ON STEADY. THE CHECKLIST WAS RUN, RESULTING IN THE APU BEING SHUTDOWN. THE LIGHT REMAIN ON FOR THE REST OF THE FLIGHT. AN EMERGENCY WAS DECLARED AND LANDING ACCOMPLISHED AT EWR. REF L/P 4995839 FOR T/S. R&R DETECTOR M487 PER AMM 26-18-11-401. OPS CHECK GOOD PER AMM 26-18-00-705. OK TO CONT.

Part: FRAME — CORRODED (BS 747 S26L/R) · airframe 37,096 hrs · 19,556 cycles

CORROSION ON FRAME AT STATION 747 STRINGER 26R TO 26L. BURNISHED CORROSION FROM S-26R TO S-26L, FROM 27R TO 26R FOUND TO BE OUT OF LIMITS AND REPAIRED PER SRM 53-00-07 REPAIR 3. ALL OTHER AREAS FOUND TO BE WITHIN ALLOWABLE LIMITS, TREATED AND PRIMED REF SRM 53-60-07.

Part: FLOOR SUPPORT — CORRODED (BS 807 S26R) · airframe 37,096 hrs · 19,556 cycles

CORROSION ON FLOOR TRACK AT STATION 807 STRINGER 26R. INSTALLED REPAIR SPLICES AND NEW SECTION OF TIE DOWN RAIL REF SRM 53-00-03 / 53-60-53.

Part: FRAME — CRACKED (BS 400 S8-9R) · airframe 37,096 hrs · 19,556 cycles

RIGHT FRAME IS CRACKED AT FASTENER FOR AIR GRILL SUPPORT RAIL MOUNT LOCATED AT STATION 400 BETWEEN STRINGERS 8 AND 9. REMOVED DAMAGED AREA, AND INSTALLED REPAIR DOUBLERS A AND B PER EA 5310-04498 OPS-2.

Part: FRAME — CRACKED (BS 440 S8-9R) · airframe 37,096 hrs · 19,556 cycles

RIGHT FRAME IS CRACKED AT FASTENER FOR AIR GRILL SUPPORT RAIL MOUNT LOCATED AT STATION 440 BETWEEN STRINGERS 8 AND 9. REPAIRED FRAME AT STATION 440 RIGHT BETWEEN STRINGERS 8 AND 9 RIGHT PER EA 5310-04498.

Part: FRAME — CRACKED (BS 827 S8-9R) · airframe 37,096 hrs · 19,556 cycles

RIGHT FRAME IS CRACKED AT FASTENER FOR AIR GRILL SUPPORT RAIL MOUNT LOCATED AT STATION 827 BETWEEN STRINGERS 8 AND 9. REPAIRED RIGHT FRAME AT FASTENERS FOR AIR GRILL SUPPORT RAIL MOUNT AT STATION 827 BETWEEN S-9R AND S-9R PER EC/RA 5310-04827.

Part: FRAME — CRACKED (BS 907 S8-9L) · airframe 37,096 hrs · 19,556 cycles

LEFT FRAME IS CRACKED AT FASTENER FOR AIR GRILL SUPPORT RAIL MOUNT LOCATED AT STA 907 BETWEEN STRINGERS 8 AND 9. TRIMMED OUT CRACKED AREA AND INSTALLED REPAIR DOUBLERS PER EA 5310-04498 OP 2.

Part: FRAME — CRACKED (BS 380 S8-9R) · airframe 37,096 hrs · 19,556 cycles

RIGHT FRAME IS CRACKED AT FASTENER FOR AIR GRILL SUPPORT RAIL MOUNT LOCATED AT STATION 380 BETWEEN STRINGERS 8 AND 9. REPAIRED FRAME AT STATION 380 RIGHT BETWEEN STRINGERS 8 AND 9 RIGHT PER EA 5310-04498.

Part: FRAME — CRACKED (BS 867 S8-9L) · airframe 37,096 hrs · 19,556 cycles

LEFT FRAME IS CRACKED AT FASTENER FOR AIR GRILL SUPPORT RAIL MOUNT LOCATED AT STATION 867 BETWEEN STRINGERS 8 AND 9. ACCOMPLISHED LEFT FRAME REPAIR AT STATION 867 BETWEEN STRINGER 8 AND 9 PER EA5310-04498 OP 2.

Part: FRAME — CRACKED (BS 827 S8-9L) · airframe 37,096 hrs · 19,556 cycles

LEFT FRAME IS CRACKED AT FASTENER FOR AIR GRILL SUPPORT RAIL MOUNT LOCATED AT STATION 827 BETWEEN STRINGERS 8 AND 9. ACCOMPLISHED AIR CONDITIONING (A/C) FUSELAGE CRACK INTERIM REPAIR AT STATION 827 PASSENGER SERVICE UNIT ATTACH BRACKETS BETWEEN S-8 TO S-9 PER ECRA 5310-04827.

Part: FRAME — CRACKED (BS 787 S8-9L) · airframe 37,096 hrs · 19,556 cycles

LEFT FUSELAGE FRAME STATION 787 IS CRACKED BETWEEN STRINGERS 8L AND 9L. REPAIRED FRAME PER EA 5310-04498 OP 2.

Part: FRAME — CRACKED (BS 440 S8-9L) · airframe 37,096 hrs · 19,556 cycles

LEFT FRAME CRACKED AT FASTENER FOR AIR GRILL SUPPORT RAIL MOUNT LOCATED AT STATION 440 BETWEEN STRINGERS 8 AND 9. REPAIRED FRAME PER EA 5310-04498, OP 02.

Part: BRACKET — CRACKED (HORIZONTAL STAB) · airframe 37,096 hrs · 19,556 cycles

HORIZONTAL STABILIZER CENTER SECTION TRUSS STRUCTURE HAS A CRACKED BRACKET AT APPROXIMATELY STATION 1121 LEFT SIDE CENTER. REMOVED AND REPLACED CRACKED FITTING ON HORIZONTAL STABILIZER CENTER SECTION TRUSS AT APPROXIMATELY STATION 1121 LEFT SIDE CENTER IAW B737 SRM 51-40-02.

Part: ATTACH FITTING — CRACKED (BS 706) · airframe 37,096 hrs · 19,556 cycles

SUPPORT ANGLE CLIP IS CRACKED AT LEFT SIDE STATION 706 AND WINDOW UPPER U-CHANNEL INTERCOSTAL. REMOVED SUPPORT ANGLE CLIP AT STATION 706, FABRICATED, TREATED, PRIMED AND INSTALLED SUPPORT ANGLE CLIP AT STATION 706L REF SRM 51-40-02.

Part: FRAME — CRACKED (BS 400 S8-9L) · airframe 37,096 hrs · 19,556 cycles

LEFT FRAME CRACKED AT FASTENER FOR AIR GRILL SUPPORT RAIL MOUNT LOCATED AT STATION 400 BETWEEN STRINGERS 8 AND 9. REPAIRED FRAME PER EA 5310-04498.

Part: FRAME — CRACKED (BS 787 S8-9R) · airframe 37,096 hrs · 19,556 cycles

RIGHT FRAME CRACKED AT FASTENER FOR AIR SUPPORT RAIL MOUNT LOCATED AT STATION 787 BETWEEN STR 8 AND STR 9. REPAIRED FRAME AT STATION 787 BETWEEN STRINGERS 8 AND 9 PER EA5310-04498 OP2.

Part: FRAME — CRACKED (BS 867 S8-9R) · airframe 37,096 hrs · 19,556 cycles

RIGHT FRAME IS CRACKED AT FASTENER FOR AIR GRILL SUPPORT RAIL MOUNT LOCATED AT STATION 867 BETWEEN STR 8 AND STR 9. REPAIRED RIGHT FRAME AT STATION 867 BETWEEN STR 8 AND STR 9 PER EA 5310-04498 OP2.

Part: ANGLE — CORRODED (BS 927-1006) · airframe 30,886 hrs · 16,308 cycles

INSPECTION FOUND R-2 DOOR ANGLE CORRODED ON UPPER SURFACE AT STA 927-1006, RBL 46. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 30,886 hrs · 16,308 cycles

INSPECTION FOUND UPPER SURFACE OF FLOORBEAM CORRODED AT NUT PLATE HOLE, STA 986.5, RBL 43. INSTALLED REPAIR IAW SRM 53-60-51.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,697 hrs · 14,144 cycles

THE FIRST CLASS CABIN SEAT EMERGENCY LIGHTS WOULD NOT TEST. THE M1674 POWER SUPPLY WAS REMOVED AND REPLACED IAW MM 33-51-51.

Part: SKIN — GOUGED (HORIZONTAL STAB) · airframe 24,779 hrs · 13,110 cycles

INSPECTION FOUND RT HORIZONTAL STABILIZER LOWER SKIN GOUGED AT STAB STA 111. THE GOUGED AREA OF SKIN WAS REMOVED AND A DOUBLER AND FILLER WERE INSTALLED IAW SRM 55-10-01, FIGURE 207.

Part: SKIN — CHAFED (FUSELAGE) · airframe 24,779 hrs · 13,110 cycles

UPPER FUSELAGE SKIN WORN AT STA 867 RBL 5 AND LBL 5 UNDER DORSAL FIN, APPROX 3 X 10 INCH. CUT OUT DAMAGE AND REPAIRED PER SRM 53-00-01 FIG 202.

Part: GROUND WIRE — LOOSE (O/H EMER LT) · airframe 19,540 hrs · 10,209 cycles

THE OVERHEAD EMERGENCY LIGHT AT L-1 DOOR FAILED TO ILLUMINATE DURING EMERGENCY LIGHT CHECK. MAINTENANCE FOUND NUT BACKED OFF OF GROUND 622 GROUNDING STUD AND GROUND WIRE LOOSE. THE NUT WAS REPLACED AND THE GROUND WIRE WAS SECURED. OPERATIONAL CHECKS WERE GOOD.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 18,707 hrs · 9,760 cycles

INSPECTION FOUND FLOORBEAM CORRODED AROUND NUT PLATE HOLES AT STA 986, RBL 4. THE CORROSION WAS CLEANED AND A STRAP REPAIR WAS INSTALLED IAW SRM 53-00-51, FIGURE 203.

Part: SKIN — GOUGED (FLAP) · airframe 18,707 hrs · 9,760 cycles

INSPECTION FOUND NR 1 MID FLAP SKIN GOUGED BY NR 2 FAIRING PRELOAD PAD. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5753-01152.

Part: CHARGER — INOPERATIVE (ROW 5 - 9) · airframe 16,813 hrs · 8,699 cycles

INSPECTION FOUND IN SEAT EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE FROM ROW 5 TO 9. MAINTENANCE FOUND THE M1668 EMERGENCY LIGHT BATTERY CHARGER INOPERATIVE. THE BATTERY CHARGER WAS REMOVED AND REPLACED, OPERATION OF THE LIGHTS CHECKED GOOD.

Part: INVERTER — BURNT (E/E BAY)

THE CABIN CREW REPORTED FUMES HAVING A HOT PLASTIC SMELL IN THE CABIN AND COCKPIT WHILE EN ROUTE FROM CLE TO PHL. THE AIRCRAFT WAS DIVERTED TO MDT WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE STATIC INVERTER AT FAULT. THE STATIC INVERTER WAS REMOVED AND REPLACED, OPERATIONAL CHECKS WERE GOOD.