N244US

Part: LIGHT — INOPERATIVE (COCKPIT)

ALB - PILOT REPORTED THAT THE COCKPIT EVACUATION LIGHT WOULD NOT ILLUMINATE WITH COCKPIT SWITCH IN THE ON POSITION. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M)

Part: HARNESS — FAILED (NR 1 GENERATOR)

BOS - FLT 2993 - ON CLIMB-OUT FROM BOS, EN ROUTE TO FLL, THE NR 1 GENERATOR BUS OFF LIGHT ILLUMINATED. CREW TRIED TO RESET GENERATOR WITH NO HELP. THE APU WAS ALREADY ON MEL SO THE FLIGHT RETURNED TO FIELD AT BOS AND LANDED WITHOUT FURTHR INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REPAIRED THE NR 1 ENGINE GENERATOR FEEDER CABLES AT LEADING EDGE OF LEFT WING, INBOARD SIDE, PER BOEING STANDARD PRACTICE 20-30-13 AND 20-61-19. INSTALLED NEW CABLES AND FIREWALL DISCONNECT. OPS CHECK GOOD. CLEARED MEL ON APU BY REMOVING AND REPLACING THE APU LOAD STAT (P/N 129552-11). (M)

Part: TIE CLIP — CRACKED (FUSELAGE)

CLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 787, STRINGER 20R. INSTALLED TIE CLIP PER EO 5393G227. (M)

Part: FLOORBEAM — CORRODED (CABIN)

CLT - FOUND FLOORBEAM CORRODED 2 INCHES BY 2 INCHES, BS 986.5, LBL 38. INSTALLED NEW FLOOR SUPPORT PER SRM 51-10-1. (M)

Part: FLOORBEAM — CRACKED (CABIN)

CLT - FOUND FLOORBEAM CRACKED, BS 520, LBL 45 UPPER CHORD AFT RADIUS. INSTALLED DOUBLER PER EA 67455. (M)

Part: ANGLE — CRACKED (FUSELAGE)

CLT - FOUND ANGLE CRACKED 1.5 INCHES, BS 350, STRINGER 16L. REPLACED SUPPORT ANGLE PER SRM 51-10-2. (M)

Part: STRINGER CLIP — CRACKED (FUSELAGE)

CLT - FOUND STRINGER TIE CLIP CRACKED .25 INCH, BS 520, STRINGER 19L. INSTALLED DOUBLER PER SRM 51-40-03. (M)

Part: SKIN — CRACKED (FUSELAGE)

CLT - FOUND OUTER SKIN CRACKED 3 INCHES, AFT ENTRY DOOR CUTOUT LOWER FORWARD CORNER STATION 947. INSTALLED EXTERNAL SKIN TRIPLER PER SRM 53-30-3. (M)

Part: SKIN — CRACKED (FUSELAGE)

CLT - FOUND SKIN CRACKED .3 INCHES, STATION 948 SKIN UPPER END SERVICE DOOR HINGE CUTOUT. INSTALLED DOUBLER PER SRM 53-30-3. (M)

Part: STRAP — CRACKED (FUSELAGE)

CLT - FOUND STRAP CRACKED .750 INCH, S-5A STRAP STATION 1138 LT SIDE. INSTALLED INTERIM REPAIR PER EA 67518 AND SRM 53-00-01 FIG 221. (M)

Part: STRINGER CLIP — CRACKED (FUSELAGE)

CLT - FOUND TIE CLIP CRACKED .250 INCH, BS 706, STRINGER 3R. REMOVED AND REPLACED PER SRM 51-10-1. (M)

Part: FLOORBEAM — CRACKED (CABIN)

CLT - FOUND 2 CRACKS IN FLOORBEAM .100 INCH, BS 663, WL 208 UPPER T-CAP. INSTALLED REPAIR PER TR 57-10-04. (M)

Part: SKIN — CRACKED (FUSELAGE)

CLT - FOUND SKIN CRACKED 1.5 INCH, BS 727A PLUS 8 INCHES STRINGER 19L. REPAIRED DOUBLER PER SRM 53-30-3. (M)

Part: SKIN — CRACKED (FUSELAGE)

CLT - FOUND SKIN CRACKED .5 INCH, BS 727A PLUS 17 INCHES STRINGER 19L. REPAIRED DOUBLER PER SRM 53-30-3. (M)

Part: TIE CLIP — CRACKED (FUSELAGE)

CLT - FOUND TIE CLIP CRACKED .5 INCH, STATION 787, STRINGER 3R. INSTALED NEW TIE CLIP PER EO 5393G227. (M)

Part: SKIN — CRACKED (FUSELAGE)

CLT - FOUND AFT SKIN CRACKED .350 INCH, BS 951 AFT GALLEY DOOR LOWER HINGE CUTOUT. INSTALLED DOUBLER PER SRM 53-30-3. (M)

Part: ANGLE — CRACKED (FUSELAGE)

CLT - FOUND ANGLE CRACKED 2 INCHES, BS 350, STRINGER 15L. REMOVED AND REPLACED ANGLE PER SRM 51-10-2 AND SRM 51-40-02. (M)

Part: SKIN — CRACKED (FUSELAGE)

CLT - FOUND INNER SKIN PLATE CRACKED 1 INCH, AFT SERVICE DOOR FUSE. CUTOUT TORQUE BOX INBOARD SIDE. INSTALLED DOUBLER AND FILLER PER TR 53-30-07A. (M)

Part: FLOORBEAM — CRACKED (CABIN)

CLT - FOUND FLOORBEAM CRACKED .500 INCH, BS 520, LBL 24 UPPER CHORD AFT RADIUS. REPAIRED PER EA 67455. (M)

Part: ANGLE — CORRODED (FUSELAGE)

CLT - FOUND Z-ANGLE CORRODED 24 INCHES BY 1 INCH, AFT SERVICE DOOR BS 947 TO BS 986 RT. INSTALLED NEW Z-ANGLE PER SRM 51-10-02. (M)

Part: STRINGER — CRACKED (FUSELAGE)

CLT - FOUND STRINGER CRACKED 3 INCHES, STATION 1006 TO 1009, STRINGER 27R. REPAIRED PER BOEING DWG 65-46558. (M)

Part: FLOORBEAM — CRACKED (CABIN)

CLT - FOUND BEAM CRACKED 3 INCHES, BS 520, RBL 24, WL 208. INSTALLED REPAIR ANGLE PER EA 67455. (M)

Part: FRAME — CRACKED (FUSELAGE)

CLT - FOUND FRAME .125 INCH CRACKED, STATION 887, STRINGER 19L. REMOVED AND INSTALLED DOUBLER PER SRM 53-10-4 FIG 9. (M)

Part: FLOORBEAM — CRACKED (CABIN)

CLT - FOUND FLOORBEAM CRACKED .250 INCH, STATION 520, RBL 45 UPPER CHORD RADIUS. INSTALLED REPAIR PER EA 67455. (M)

Part: FRAME — CRACKED (FUSELAGE)

CLT - FOUND FRAME CRACKED 1.5 INCH, BS 350, AT STRINGER 15L DOOR STOP FITTING. REPAIRED PER SRM 51-10-2. (M)

Part: SKIN — CRACKED (FUSELAGE)

CLT - FOUND SKIN CRACKED .5 INCH, BS 764.5 AT STRINGER 19L. INSTALLED FILLER AND DOUBLER PER 53-30-3 FIG 6. (M)

Part: FLOORBEAM — CORRODED (CABIN)

CLT - FOUND FLOORBEAM CORRODED 3 INCHES BY 3 INCHES AND 2 INCHES BY 2 INCHES, BS 986.5 4 INCHES, RBL AND 4 INCHES THROUGH 12 INCHES LBL. FABRICATED NEW T-CAP AND ANGLE DOUBLER PER TR 53-60-01. (M)

Part: WEB — CRACKED (FUSELAGE)

CLT - FOUND WEB CRACKED .5 INCH, STRINGER 10L SUPPORT WEB BS 350. REPLACED WEB PER SRM 51-10-02. (M)

Part: SUPPORT FITTING — CRACKED (RT WING)

CLT - FOUND SUPPORT FITTING CRACKED .200 INCH, RT WING LANDING GEAR BEAM. ACCOMPLISHED PART A PER TR 57-40-10. (M)

Part: ANGLE — CORRODED (FUSELAGE)

CLT - FOUND Z-ANGLE CORRODED 1 INCH BY 1 INCH, AFT ENTRY DOOR SILL Z-ANGLE. INSTALLED NEW Z-ANGLE PER SRM 51-10-1 AND 51-30-0. CORROSION LEVEL 1. (M)

Part: STRINGER — CORRODED (FUSELAGE)

CLT - FOUND STRINGER CORRODED 2 INCHES, STATION 947 STRINGER 27L. REMOVED AND REPLACED PER SRM 53-10-03. (M)

Part: FITTING — CRACKED (BULKHEAD)

CLT - FOUND BULKHEAD FITTING CRACKED .750 AND .375 INCH, BS 663.75 BULKHEAD FITTING RT SIDE WL 191.5 POCKET. REMOVED AND REPLACED BULKHEAD FITTING PER EA 67452, 67457 AND 67412. (M)

Part: FRAME — CORRODED (FUSELAGE)

CLT - FOUND FRAME CORRODED 2.5 INCHES, BS 967, STRINGER 26R AT SKIN ATTACH POINT. INSTALLED DOUBLER FRAME REPAIR PER SRM 53-10-4. CORROSION LEVEL 2, C53-208-01. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

CLT - FOUND FLOORBEAM CORRODED 12 INCHES BY 1 INCH, 3 AREAS AT STATION 344, LBL 8 THROUGH LBL 18. REPAIRED T-CAP PER TR 53-10-13. CORROSION LEVEL 2. (M)

Part: ANGLE — CRACKED (FUSELAGE)

CLT - FOUND ANGLE CRACKED 4 INCHES, STATION 727B LBL 40. REPLACED PER SRM 51-10-1. (M)

Part: STRINGER — CRACKED (FUSELAGE)

CLT - FOUND SEVERAL CRACKS .125 INCH OR LESS, INSIDE CHANNEL STRINGER 15L, BETWEEN STATION 520 AND 540. INSTALLED STRINGER REPAIR SECTION PER SRM 53-10-3. (M)

Part: WEB — CRACKED (FUSELAGE)

CLT - FOUND WEB/STIFFENER CRACKED 6 INCHES, STATION 727, LBL 13 BETWEEN VERT SUPPORT BEAMS. REPLACED PART PER SRM 51-10-1. (M)

Part: TIE CLIP — CRACKED (FUSELAGE)

CLT - FOUND TIE CLIP CRACKED .25 INCH, BS 706, STRINGER 5R. REMOVED AND REPLACED PER SRM 51-10-1. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

CLT - FOUND INTERCOSTAL CRACKED 1 INCH AND 2 INCHES, FLOOR SUPPORT BETWEEN STATION 380 TO 400 BL 0. REPAIRED PER SRM 51-10-01. (M)

Part: TIE CLIP — CRACKED (FUSELAGE)

CLT - FOUND TIE CLIP CRACKED .5 INCH, STATION 787 STRINGER 7R. REPLACED TIE CLIP PER SRM 51-10-1. (M)

Part: TIE CLIP — CRACKED (FUSELAGE)

CLT - FOUND TIE CLIP CRACKED .5 INCH, STATION 767, STRINGER 11R. FABRICATED NEW CLIP PER SRM 51-10-1 AND DWG 6945156. (M)

Part: TIE CLIP — CRACKED (FUSELAGE)

CLT - FOUND TIE CLIP CRACKED 1 INCH, STATION 706, STRINGER 3R. REPAIRED PER EO 5393G227. (M)

Part: TIE CLIP — CRACKED (FUSELAGE)

CLT - FOUND TIE CLIP CRACKED 1 INCH, STATION 663, STRINGER 10L. REPAIRED PER EO 5393G227. (M)

Part: TIE CLIP — CRACKED (FUSELAGE)

CLT - FOUND TIE CLIP CRACKED .25 INCH, BS 597, STRINGER 5R. REMOVED AND REPLACED TIE CLIP PER SRM 51-10-1. (M)

Part: TIE CLIP — CRACKED (FUSELAGE)

CLT - FOUND TIE CLIP CRACKED .25 INCH, BS 787, STRINGER 3R. INSTALLED NEW TIE CLIP PER SRM 51-10-1. (M)

Part: CLIP — CRACKED (FUSELAGE)

CLT - FOUND TIE CLIP CRACKED .25 INCH, BS 787, STRINGER 7R. INSTALLED NEW TIE CLIP PER SRM 51-10-1. (M)

Part: TIE CLIP — CRACKED (FUSELAGE)

CLT - FOUND TIE CLIP CRACKED .25 INCH, BS 787, STRINGER 5R. INSTALLED NEW TIE CLIP PER SRM 51-10-1. (M)

Part: TIE CLIP — CRACKED (FUSELAGE)

CLT - FOUND TIE CLIP CRACKED .25 INCH, BS 685, STRINGER 4L TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-10-1. (M)

Part: TIE CLIP — CRACKED (FUSELAGE)

CLT - FOUND TIE CLIP CRACKED .25 INCH, BS 727A, STRINGER 4L. INSTALLED NEW TIE CLIP PER SRM 51-10-1. (M)

Part: KEEL BEAM — CORRODED (BS 727)

TPA - DURING CX-5 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND MINOR CORROSION 4 INCH BY 6 INCH BOTTOM KEEL BEAM STATION 727 STRINGER 26L. CORROSION LEVEL 1. INSTALLED DOUBLER PER SRM 53-30-3 FIG 28. (M)

Part: SKIN — CRACKED (BS 328)

TPA - DURING CX-5 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A .25 INCH CRACK AT LOWER HINGE CUTOUT ON DOOR STRINGER 17L, BS 312 SKIN. INSTALLED DOUBLER PER TR 52-10-05. (M)

Part: SKIN — CRACKED (BS 767)

BOS - DURING RON, FOUND .75 INCH CRACK ON SKIN AT STATION 767 ON STRINGER 21L. VISUAL CONFIRMED BY EDDY CURRENT AND DYE PENETRANT. INSTALLED DOUBLER AT STATION 767 ON STRINGER 21L PER SRM 53-30-3 FIG 6, PAGES 11 TO 12B, SHEETS 1 TO 4. (M)

Part: CSD OIL COOLER — BIRD STRIKE (NR 2 ENGINE)

BOS - FLT 2851 - DURING TAKEOFF, TWO SEA GULLS STRUCK THE NR 2 ENGINE. AFTER INGESTION, THERE WAS A SMELL IN THE CABIN. FLIGHT RETURNED TO FIELD AT BOS AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE ACCOMPLISHED BIRD STRIKE CONDITIONAL INSPECTION PER MM 5-51-201 AND ACCOMPLISHED TAKEOFF POWER CHECK PER MM 5-51-20. REMOVED AND REPLACED THE NR 2 ENGINE CSD OIL COOLER PER MM 24-11-21 DUE TO CONDITIONAL INSPECTION CHECK. PERFORMED ENGINE RUNUP. ALL PARAMETERS WITHIN LIMITS. NO LEAKS NOTED. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

BWI - FLT 2639 - BEFORE DEPARTURE, THE CAPTAIN REPORTED THE EMERGENCY LIGHT AT THE AFT LEFT ENTRY DOR WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)

Part: ANGLE — CORRODED (BS 344-350)

CLT - DURING VISUAL CHECK INSPECTION, FOUND A 6 INCH BY 2 INCH AREA OF CORROSION AT BS 344 - BS 350, LBBL 60, WL 208.10 ANGLE BEAM CHORD. REPAIRED DOUBLER PER EA 64341 AND SRM 53-40-3. (M)

Part: SKIN — CRACKED (BS 733-736)

TPA - DURING CX-4 CHECK VISUAL INSPECTION, FOUND A 2.5 INCH CRACK IN EXTERNAL SKIN LOCATED BETWEEN STATION 733 AND 736 AND STRINGER 8L. INSTALLED DOUBLER PER SRM 53-30-3 FIG 1 A 64060 AND SB 52-1096. (M)

Part: SKIN — CRACKED (GALLEY DOORWAY)

TPA - DURING CX-4 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK IN UPPER CORNER OF LOWER FORWARD GALLEY DOOR CUTOUT EXTERNAL SKIN. INSTALLED DOUBLER PER EA 62369. (M)

Part: SKIN — CRACKED (BS 727)

CLT - DURING HM DROP IN VISUAL INSPECTION, FOUND A 1 INCH CRACK ON SKIN STATION 727A STRINGER 18R. INSTALLED DOUBLER PER SRM 53-30-3 AND EA 63480. (M)

Part: SKIN — CRACKED (BS 727)

CLT - DURING HM DROP INVISUAL INSPECTION, FOUND A 1 INCH CRACK STRINGER 18R 2 INCH AFT OF BS 727A SKIN. INSTALLED DOUBLER PER SRM 53-30-3 FIG 6 AND EA 63480. (M)

Part: SKIN — CRACKED (BS 727)

CLT - DURING HM DROP IN VISUAL INSPECTION, FOUND A 2 INCH CRACK 6 INCH AFT OF STATION 727E STRINGER 16L. INSTALLED DOUBLER PER SRM 53-30-3 FIG 6. (M)

Part: SKIN — CRACKED (BS 793)

CLT - DURING HM DROP IN VISUAL INSPECTION, FOUND A 2 INCH CRACK STRINGER 16L BS 793 SKIN. INSTALLED DOUBLER PER SRM 53-30-3 FIG 6. (M)

Part: GCU — MALFUNCTIONED (NR 2)

DTW - FL2232, EN ROUTE FROM CLT TO DTW, FLIGHT ATTENDANT ADVISED CREW OF A BURNING ELECTRICAL SMELL AFT OF FORWARD BULKHEAD AROUND SEAT ROWS 4, 5 AND 6. SHORTLY THEREAFTER, THE CIRCUIT BREAKERS FOR THE NR 2 AFT FUEL BOOST PUMP AND NR 2 TR TRIPPED. THE NR 2 TR READ 0 AMPS AND 28 VOLTS. INTERMITTENTLY, THE LEFT ANTI-SKID OFF AND FIRST OFFICER AUX PITOT STATIC AMBER LIGHTS ILLUMINATED, PMS EXTERNAL FAIL WITH CODES 96 AND 99 AND A FLAG IN THE NR 2 EPR GAUGE. ON DESCENT, ALL LIGHTS AND FLAGS WENT OUT AND PMS OPERATED NORMALLY. CREW DID NOT RESET BOOTS PUMP OR TR CIRCUIT BREAKERS TO AVOID THE POSSIBLE RETURN OF THE BURNING ODOR. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE CHECKED APPLICABLE WIRING. RE

Part: TRU — MALFUNCTIONED (NR 2)

DTW - FL2232, EN ROUTE FROM CLT TO DTW, FLIGHT ATTENDANT ADVISED CREW OF A BURNING ELECTRICAL SMELL AFT OF FORWARD BULKHEAD AROUND SEAT ROWS 4, 5 AND 6. SHORTLY THEREAFTER, THE CIRCUIT BREAKERS FOR THE NR 2 AFT FUEL BOOST PUMP AND NR 2 TR TRIPPED. THE NR 2 TR READ 0 AMPS AND 28 VOLTS. INTERMITTENTLY, THE LEFT ANTI-SKID OFF AND FIRST OFFICER AUX PITOT STATIC AMBER LIGHTS ILLUMINATED, PMS EXTERNAL FAIL WITH CODES 96 AND 99 AND A FLAG IN THE NR 2 EPR GAUGE. ON DESCENT, ALL LIGHTS AND FLAGS WENT OUT AND PMS OPERATED NORMALLY. CREW DID NOT RESET BOOTS PUMP OR TR CIRCUIT BREAKERS TO AVOID THE POSSIBLE RETURN OF THE BURNING ODOR. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE CHECKED APPLICABLE WIRING. RE

Part: BOOST PUMP — FAILED (NR 2)

DTW - FL2232, EN ROUTE FROM CLT TO DTW, FLIGHT ATTENDANT ADVISED CREW OF A BURNING ELECTRICAL SMELL AFT OF FORWARD BULKHEAD AROUND SEAT ROWS 4, 5 AND 6. SHORTLY THEREAFTER, THE CIRCUIT BREAKERS FOR THE NR 2 AFT FUEL BOOST PUMP AND NR 2 TR TRIPPED. THE NR 2 TR READ 0 AMPS AND 28 VOLTS. INTERMITTENTLY, THE LEFT ANTI-SKID OFF AND FIRST OFFICER AUX PITOT STATIC AMBER LIGHTS ILLUMINATED, PMS EXTERNAL FAIL WITH CODES 96 AND 99 AND A FLAG IN THE NR 2 EPR GAUGE. ON DESCENT, ALL LIGHTS AND FLAGS WENT OUT AND PMS OPERATED NORMALLY. CREW DID NOT RESET BOOTS PUMP OR TR CIRCUIT BREAKERS TO AVOID THE POSSIBLE RETURN OF THE BURNING ODOR. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE CHECKED APPLICABLE WIRING. RE

Part: CIRCUIT BREAKER — MALFUNCTIONED (COCKPIT)

CLT - FLT 790 - AT FL290, FLT ATTENDANT ADVISED CREW OF A BURNING ELECTRICAL SMELL IN CABIN AROUND LOW 6D. AT THE SAME TIME, THE NR 2 MAIN AFT BOOST PUMP CIRCUIT BREAKER TRIPPED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE GASPER FAN AS PRECAUTIONARY DUE TO FAN APPEARED TO BE HOT AND IS LOCATED BELOW ROW 6DEF. OPS CHECKED GOOD. REPLACED APU GENERATOR CONTROL BREAKER DUE TO MAIN CONTACTS SMELLED BURNED AND BREAKER WAS HOT WHILE IN OPERATION. OPS CHECKED GOOD. ALSO, REPLACED NR 2 TRU AS PRECAUTIONARY AS DIRECTED BY MAINTENANCE CONTROL. OPS CHECKED GOOD. CHECKED WIRING TO MAIN AFT FUEL BOOST PUMP. NO DEFECTS NOTED. REMOVED AND REPLACED MAIN AFT FUEL BOOST PUMP PER MM. O

Part: GCU — MALFUNCTIONED (NR 2)

CLT - FLT 790 - AT FL290, FLT ATTENDANT ADVISED CREW OF A BURNING ELECTRICAL SMELL IN CABIN AROUND LOW 6D. AT THE SAME TIME, THE NR 2 MAIN AFT BOOST PUMP CIRCUIT BREAKER TRIPPED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE GASPER FAN AS PRECAUTIONARY DUE TO FAN APPEARED TO BE HOT AND IS LOCATED BELOW ROW 6DEF. OPS CHECKED GOOD. REPLACED APU GENERATOR CONTROL BREAKER DUE TO MAIN CONTACTS SMELLED BURNED AND BREAKER WAS HOT WHILE IN OPERATION. OPS CHECKED GOOD. ALSO, REPLACED NR 2 TRU AS PRECAUTIONARY AS DIRECTED BY MAINTENANCE CONTROL. OPS CHECKED GOOD. CHECKED WIRING TO MAIN AFT FUEL BOOST PUMP. NO DEFECTS NOTED. REMOVED AND REPLACED MAIN AFT FUEL BOOST PUMP PER MM. O

Part: PUMP — MALFUNCTIONED (NR 2)

CLT - FLT 790 - AT FL290, FLT ATTENDANT ADVISED CREW OF A BURNING ELECTRICAL SMELL IN CABIN AROUND LOW 6D. AT THE SAME TIME, THE NR 2 MAIN AFT BOOST PUMP CIRCUIT BREAKER TRIPPED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE GASPER FAN AS PRECAUTIONARY DUE TO FAN APPEARED TO BE HOT AND IS LOCATED BELOW ROW 6DEF. OPS CHECKED GOOD. REPLACED APU GENERATOR CONTROL BREAKER DUE TO MAIN CONTACTS SMELLED BURNED AND BREAKER WAS HOT WHILE IN OPERATION. OPS CHECKED GOOD. ALSO, REPLACED NR 2 TRU AS PRECAUTIONARY AS DIRECTED BY MAINTENANCE CONTROL. OPS CHECKED GOOD. CHECKED WIRING TO MAIN AFT FUEL BOOST PUMP. NO DEFECTS NOTED. REMOVED AND REPLACED MAIN AFT FUEL BOOST PUMP PER MM. O

Part: GASPER FAN — MALFUNCTIONED (CABIN)

CLT - FLT 790 - AT FL290, FLT ATTENDANT ADVISED CREW OF A BURNING ELECTRICAL SMELL IN CABIN AROUND LOW 6D. AT THE SAME TIME, THE NR 2 MAIN AFT BOOST PUMP CIRCUIT BREAKER TRIPPED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE GASPER FAN AS PRECAUTIONARY DUE TO FAN APPEARED TO BE HOT AND IS LOCATED BELOW ROW 6DEF. OPS CHECKED GOOD. REPLACED APU GENERATOR CONTROL BREAKER DUE TO MAIN CONTACTS SMELLED BURNED AND BREAKER WAS HOT WHILE IN OPERATION. OPS CHECKED GOOD. ALSO, REPLACED NR 2 TRU AS PRECAUTIONARY AS DIRECTED BY MAINTENANCE CONTROL. OPS CHECKED GOOD. CHECKED WIRING TO MAIN AFT FUEL BOOST PUMP. NO DEFECTS NOTED. REMOVED AND REPLACED MAIN AFT FUEL BOOST PUMP PER MM. O

Part: SKIN — CRACKED (BS 807)

ROA - DURING CX-3 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND A 2 INCH CRACK FUSELAGE SKIN BS 807 STR 19L. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3, FIG 6. (X)

Part: CSD DRAIN PLUG — BROKEN (NR 1 ENG CSD)

SAV - FL403 - THE NR 1 ENG CSD LOW PRESS LIGHT BEGAN TO BLANK AND THE FREQ WAS FLUCTUATING ERRATICALLY. ABNORMAL CHECKLIST WAS FOLLOWED, THE NR 1 ENG CSD WAS DISCONNECTED. THE APU WAS ON MEL AND WITH ONLY ONE POWER SOURCE, THE FLT DIVERTED TO SAV. FLT LANDED W/O FURTHER INCIDENT. UPON ARRIVAL, MX INSPECTED THE NR 1 ENG CSD MAGNETIC CHIP DETECT AND NOTED THAT BOLTHEAD WAS BROKEN OFF. SERVICED CSD AND NOTED OIL LEAKING AT SAME LOCATION. R/R'D DRAIN PLUG ASSY ALONG WITH MAGNETIC CHIP DETECTOR. NO CONTAMINATION WAS NOTED ON REMOVED PLUG. R/R'D IN LINE FILTER. NO CONTAMINATION NOTED. SAFETY WIRED THE MENTIONED ITEMS AND RAN ENG. NO LEAKS NOTED. VOLTS AND FREQ GOOD. OPS CHECK NORMAL. (M)

Part: HEAT MANIFOLD — FAILED (NR 1 ENGINE)

BWI - FL250, ON CLIMB-OUT OF BWI, THE NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED. CAPTAIN BROUGHT POWER BACK TO IDLE AND LGIHT EXTINGUISHED. FLIGHT RETURNED TO FIELD AT BWO WITH NR 1 ENGINE AT IDLE. CAPTAIN DID DECLARE AN EMERGENCY. FLIGHT LANDED WITHOUT FURTHER INCIDENT. THE NR 1 ENGINE WAS NOT SHUT DOWN IN FLIGHT. MAINTENANCE FOUND THE NR 1 ENGINE FUEL HEAT MANIFOLD ASSY HAD BLOWN. LOWERED NR 1 ENGINE TO GAIN ACCESS TO MANIFOLD. REPLACED MANIFOLD. REINSTALLED ENGINE. OPERATIONAL CHECK AND LEAK CHECK GOOD. (M)

Part: FAN — FAILED (CABIN)

EWR - FL 634 - WHILE DESCENDING TO FINAL APPROACH, CABIN AND COCKPIT CREW NOTICED A STRONG INTENSE ELECTRICAL BURNING SMELL THROUGHOUT THE ENTIRE AIRCRAFT. CAPTAIN DECLARED AN EMERGENCY. FLIGHT LANDED WITHOUT INCIDENT AND TAXIED TO THE GATE. MAINTENANCE REMOVED AND REPLACED BURNED GASPER FAN MOTOR PER MM. OPERATIONAL CHECK GOOD. (M)

Part: BATTERY — FAILED (CABIN)

SYR - MAINTENANCE FOUND THE FORWARD RIGHT CABIN EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED BATTERIES. OPS CHECK GOOD. (M)

Part: SKIN — CRACKED (BS 767)

ROA - DURING A-CHECK, VISUAL INSPECTION FOUND .75 INCH CRACK LOCATED AT STA 767 AT S20R SKIN. INSTALLED DOUBLER PER SRM 53-30-3 FIG 6 PAGES 11 THROUGH 12B. (X)

Part: FLOORBEAM — CORROSION (BS 1016)

INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 8 INCHCORROSION FLOOR BEAM F/S 1016 BL 0 TO RBL 12. SPLICED IN FLOOR BEAM T-CAPAND DOUBLERS REPAIRED PER SRM 53-10-9 EA 41313. (M)

Part: BULKHEAD — CRACKED (BS 178)

INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 1INCH CRACK IN 178 BULKHEAD TWO PLACES LEFT SIDE AT LOWER LEFT MOUNT FORRADAR. INSTALLED DOUBLERS, REPAIRED PER TR 53-10-11.(M)

Part: KEELBEAM — CORRODED (BS 710-727)

INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH DIAMETERCORRODED AREA PLUS 4 KEEL BEAM RBL 6.4 FS 727 TO FS 710. SPOT FACED HOLESINSTALLED, INSTALLED REPAIR STRAP. REPAIRED PER EA 41303. (M)

Part: BULKHEAD — CRACKED (BS 178)

INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND APPROX 1 INCHCRACK IN 178 BULKHEAD 2 PLACES RIGHT SIDE AT LOWER RIGHT MOUNT FOR RADAR.INSTALLED DOUBLER AND FILLERS, REPAIRED PER TR 53-10-11.(M)

Part: AC GENERATOR — LOOSE WIRE (RT ENGINE)

CMH - FL 868 - AFTER DEPARTURE FROM CMH, NR 2 AND NR 3 TRANSFORMER RECEIVER UNITS FAILED. FLIGHT RETURNED TO CMH AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND A LOOSE ENGINE GENERATOR FEED HARNESS WIRE. WIRE 'S' WAS LOOSE AT THE NR 2 GENERATOR. SECURED WIRE IN TO TERMINAL. (M)

Part: STRINGER — CORRODED (BS 948-993)

ROA - DURING CX-6 CHECK VISUAL INSPECTION, FOUND 45 INCHES OF STRINGER 27L CORRODED, STRINGER 27L BETWEEN STATION 948 TO 993. REMOVED CORROSION AND INSTALLED STRINGER SPLICE. (M)

Part: STRINGER — CORROSION (BS 965)

ROA - DURING 'CX-6' CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 6 INCHES OF STRINGER CORRODED STRINGER 27R AT STATION 965. REMOVED CORROSION AND INSTALLED STRINGER SPLICE. (M)

Part: SKIN — CRACKED (BS 780)

ROA - DURING CX-6 CHECK VISUAL INSPECTION, CONFIRMED WITH HFEC FOUND FUSELAGE SKIN CRACK, 4.25 INCH LONG, STRINGER 18L, STATION 780. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3. (M)

Part: PUMP — FAILED ('A' HYD SYS)

CLT - FLT 2126 - FLIGHT EN ROUTE BWI TO ATL WHEN 'A' SYSTEM HYDRAULICS FAILED. CREW DIVERTED FLIGHT TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NR 2 ENGNE HYDRAULIC PUMP. REPLACED 'A' SYSTEM RETURN AND BOTH CASE DRAIN FILTERS. NO LEAKS NOTED. (W)

Part: HYD FITTING — LEAKING (LT MLG)

PHL - FLT 8610 - FLIGHT EN ROUTE BUT TO ACY WHEN AIRCRAFT LOST 'A' SYSTEM HYDRAULICS. FLIGHT DIVERTED TO PHL WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENACNE REPLACED BROKEN FITTING AT LEFT MAIN GEAR DOWN LINE RESTRICTOR. ALSO, REPLACED NR 1 AND NR 2 ENGINE 'A' SYSTEM HYDRAULIC PUMPS, PRECAUTIONARY. (Z)