N650AA

Part: WIRE — BURNED (ZONE 200) · airframe 63,126 hrs · 21,747 cycles

OBSERVED SPARKS BEHIND P-70 PANEL WHEN WATER HEATER CIRCUIT BREAKERS WERE PUSHED IN. REPAIRED DAMAGE WIRE AND SECURED PER STANDARD PRACTICES. OPS CHECK NORMAL.

Part: SOLENOID — DEFECTIVE (RUDDER) · airframe 62,250 hrs · 21,434 cycles

MIA - CREW REPORTED RUDDER RATION AND EICAS MESSAGE. EMERGENCY DECLARED FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RUDDER RATIO SOLENOID. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SHROUD — MISSING (CABIN) · airframe 61,701 hrs · 21,231 cycles

THE EMERGENCY ESCAPE PATH LIGHT SHROUD IS MISSING AT 15D. REPLACED SHROUD FOR EMERGENCY ESCAPE PATH LIGHT AT 15D. OPS CHECKED NORMAL.

Part: SHROUD — BROKEN (CABIN) · airframe 61,701 hrs · 21,231 cycles

THE ESCAPE PATH LIGHT SHROUD AT 12D IS BROKEN. REPLACED SHROUD FOR ESCAPE PATH LIGHT AT 12D. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,701 hrs · 21,231 cycles

THE TOP LAMP FOR EMERGENCY ESCAPE PATH LIGHT AT 9D INOPERATIVE. REPLACED LAMP FOR SEAT 9D ESCAPE PATH LIGHT, OPS CHECK NORMAL.

Part: SHROUD — MISSING (CABIN) · airframe 61,701 hrs · 21,231 cycles

THE AFT EMERGENCY ESCAPE PATH LIGHT SHROUD AT 17D IS MISSING. REPLACED SHROUD FOR THE AFT EMERGENCY ESCAPE PATH LIGHT AT 17D. OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,701 hrs · 21,231 cycles

THE TOP LAMP FOR EMERGENCY ESCAPE PATH LIGHT AT 29D INOPERATIVE. REPLACED LAMP FOR THE TOP POSITION EMERGENCY ESCAPE PATH LIGHT AT 29D. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,701 hrs · 21,231 cycles

LEFT AISLE BULLNOSE EMERGENCY FLOODLIGHT AT ROW 23 INOPERATIVE. REPLACED LAMP FOR LEFT AISLE BULLNOSE EMERGENCY FLOODLIGHT AT ROW 23. OPS CHECK NORMAL.

Part: SHROUD — BROKEN (CABIN) · airframe 61,701 hrs · 21,231 cycles

THE EMERGENCY ESCAPE PATH LIGHT SHROUD IS BROKEN ON THE FORWARD POSITION OF 16D. REPLACED SHROUD FOR THE FORWARD POSITION EMERGENCY ESCAPE PATH LIGHT AT 16D. OPS CHECK NORMAL.

Part: RIB — CORRODED (TE FLAP) · corrosion level 3 · airframe 61,463 hrs · 21,144 cycles

CORROSION AT FASTENER HOLES AND NUT PLATES ON 2 INBOARD RIBS AFT OF REAR SPAR. INSTALLED NEW RIB PER ESO 90399.

Part: SPAR — CORRODED (TE FLAP) · corrosion level 3 · airframe 61,463 hrs · 21,144 cycles

CORROSION ON INNER SIDE OF UPPER FORWARD SPAR CHORD, 7 AND 24 TO 36 INCHES FROM INBOARD END. REPLACED UPPER FORWARD SPAR CHORD PER SRM 51-10-02 IAW ESO90399.

Part: SKIN PANEL — CORRODED (TE FLAP) · corrosion level 3 · airframe 61,463 hrs · 21,144 cycles

CORROSION FOUND ON CENTER LOWER SKIN PANEL INSIDE SKIN. INSTALLED BONDED DOUBLER REPAIR PER SRM 51-70-10-2R.

Part: SKIN PANEL — DAMAGED (TE FLAP) · airframe 61,463 hrs · 21,144 cycles

DENT IN LOWER SKIN PANEL 10 INCHES FROM OUTBOARD END 14 INCHES FROM TRAILING EDGE. INSTALLED FLUSH BONDED DOUBLER REPAIR PER SRM 51-70-10-2R E58-4844695.

Part: SKIN PANEL — DAMAGED (TE FLAP) · airframe 61,461 hrs · 21,143 cycles

DENT IN LOWER SKIN PANEL 10 INCHES FROM OUTBOARD END 14 INCHES FROM TRAILING EDGE. INSTALLED FLUSH BONDED DOUBLER REPAIR PER SRM 51-71-10-2R.

Part: SKIN — CORRODED (TE FLAP) · corrosion level 3 · airframe 61,463 hrs · 21,144 cycles

AFT LOWER SKIN PLATE HAS CORROSION ON INBOARD RIBS. INSTALLED FABRICATED SKIN PER ESO 90399.

Part: SKIN PANEL — DAMAGED (TE FLAP) · airframe 61,463 hrs · 21,144 cycles

INBOARD UPPER INTER SPAR SKIN PANEL HAS PUNCTURE ON INNER SKIN AT CENTER BAY ON OUTBOARD END. INSTALLED EXTERNAL BONDED DOUBLER PER SRM 51-70-10-2R-2.

Part: LENS — MISSING (CABIN) · airframe 60,818 hrs · 20,920 cycles

RIGHT NUMBER 2 DOOR AFT EMERGENCY EXIT LIGHT MISSING LENS. REPLACED LIGHT ASSEMBLY FOR RIGHT NUMBER 2 DOOR AFT EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: PROCESSING UNIT — INOPERATIVE (FUEL SYSTEM) · airframe 60,796 hrs · 20,912 cycles

PTY - INFLIGHT BOG-MIA. THE RIGHT SIDE FUEL TANK TOTALIZER AND TOTAL FUEL TOTALIZER WENT BLANK. FLIGHT DIVERTED PTY LANDED WITHOUT INCIDENT. REMOVED AND REPLACED FUEL QUANTITY PROCESSOR UNIT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 60,578 hrs · 20,833 cycles

RIGHT OVERWING AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT OVERWING AFT EXTERIOR EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: STRAP — CRACKED (FUSELAGE) · airframe 59,798 hrs · 20,562 cycles

AFT CARGO FLOORBEAM STABILIZER STRAP CRACKED AT APPROXIMATELY STATION 1360 RIGHT BUTTLINE 60 AFT CARGO CEILING AREA. CUT AND DRILLED REPAIR PLATE. SEALED AND RIVETED REPAIR PER SRM 51-20-02-0G, 51-40-01-0G.

Part: STRAP — CORRODED (APU BAY) · corrosion level 2 · airframe 59,798 hrs · 20,562 cycles

CORROSION ON LOWER SURFACE OF AFT ATTACH FLANGE FOR AUXILIARY POWER UNIT INLET DOOR HOUSING. INSTALLED NEW STRAP, DOUBLERS, AND FILLERS PER EA B757-53-012084.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,798 hrs · 20,562 cycles

CORROSION ON CREASE ANGLE STATION 756 WATERLINE 208 LEFT BUTTLINE 63 TO 64 STRINGER 17 LEFT. INSTALLED SPLICE REPAIR STATIONS 756 TO 768 PER AARD 53-30-13-1.

Part: SUPPORT ANGLE — CRACKED (CARGO DOOR) · airframe 59,798 hrs · 20,562 cycles

AFT CARGO DOOR UPPER SUPPORT ANGLE CRACKED. REPLACED ANGLE PER SRM 51-10-02.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 59,798 hrs · 20,562 cycles

STATION 700 BEAM UPPER T-CAP CRACKED. STATION 700 FLOORBEAM CRACK REPAIR PER SRM 53-00-51-2R REPAIR 3.

Part: ANGLE — DAMAGED (CARGO DOOR) · airframe 59,798 hrs · 20,562 cycles

AFT CARGO DOOR BOTTOM EDGE SEAL LANDING HAS A HOLE IN IT 28 INCHES FROM THE AFT END. REPLACED AFT CARGO DOOR LOWER SEAL LANDING FORMED ANGLE AND SPLICES PER SRM 51-10-02-0G.

Part: SKIN — DENTED (FUSELAGE) · airframe 59,798 hrs · 20,562 cycles

LARGE AREA DENT IN OIL CANNING AT FRAME STATIONS 430 TO 440, AND STRINGER 15 RIGHT TO 16 RIGHT. REPAIR COMPLETED PER SRM 53-00-01-2R 3 WITH THE DEVIATION APPROVED BY EA B757-53-012011, ISSUE DATE 07-23-2010.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,798 hrs · 20,562 cycles

CORROSION ON FLOORBEAM STATIONS 1640 TO 1658. REPAIRED PER IAW SRM 53-00-51-2R 3.

Part: WEB — CORRODED (CARGO BAY) · corrosion level 2 · airframe 59,798 hrs · 20,562 cycles

AFT CARGO - CORROSION ON WEB AT STRINGER 29 LEFT BETWEEN STATIONS 1400 TO 1420. INSTALLED WEB STATIONS 1400 TO 1420 AT STRINGER 29 LEFT SRM 51-10-02-0G 9.

Part: FITTING — CORRODED (CARGO BAY) · corrosion level 2 · airframe 59,798 hrs · 20,562 cycles

FORWARD CARGO COMPARTMENT THRESHOLD POD LOCK FITTING IS CORRODED AT STATION 620. INSTALLED SERVICEABLE FORWARD CARGO COMPARTMENT THRESHOLD POD LOCK FITTING AT STATION 620 PER AARD 51-00-05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,798 hrs · 20,562 cycles

CORROSION ON FLOORBOARD SUPPORT. REPLACED FLOOR BOARD SUPPORT.

Part: FITTING — CORRODED (CARGO BAY) · corrosion level 2 · airframe 59,798 hrs · 20,562 cycles

FORWARD CARGO TIE DOWN FITTING RIGHT SIDE STATION 625 CORRODED. INSTALLED FITTING AT STATION 625 RIGHT SIDE OF FORWARD CARGO PER AARD 51-00-05.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,798 hrs · 20,562 cycles

STATION 1620 AT END OF STRINGER 30 THERE IS A 5 INCH CRACK MIGRATING FORWARD ON THE BOTTOM RIGHT FLANGE OF THE STRINGER. INSTALLED STRINGER SPLICE IAW SRM 53-00-03-2 R1.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,798 hrs · 20,562 cycles

RIGHT NUMBER 4 DOOR FORWARD FLOOR DRAIN SUPPORT CORRODED. REMOVED AND REPLACED RIGHT NUMBER 4 DOOR FORWARD DRAIN SUPPORT.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,798 hrs · 20,562 cycles

CORROSION ON TOP OF FLOOR SUPPORT STATIONS 1661 TO 1681 AT LEFT BUTTLINE 1 TO RIGHT BUTTLINE 1 WATERLINE 208. INSTALLED NEW FLOOR SUPPORT PER IAW AARD 51-00-05.

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,798 hrs · 20,562 cycles

AFT CARGO - CORROSION ON FITTING THAT HOLDS THE END OF STRINGER 30 AT STATION 1620. INSTALLED NEW STRINGER BRACKET PER SRM 53-00-03-2R.

Part: STRINGER — DENTED (FUSELAGE) · airframe 59,798 hrs · 20,562 cycles

LARGE DENT ON STRINGER 16 STATION 620. INSTALLED EXTERNAL DOUBLER REPAIR PER SRM 53-00-03 2R 1.

Part: FITTING — CORRODED (CARGO BAY) · corrosion level 2 · airframe 59,798 hrs · 20,562 cycles

FORWARD CARGO COMPARTMENT THRESHOLD POD LOCK FITTING IS CORRODED AT STATION 610. INSTALLED SERVICEABLE FITTING ASSEMBLY. AREA AT STATION 610 SEALED AND TREATED AFTER FINAL INSTALLATION PER SRM 51-20-01-0G.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,798 hrs · 20,562 cycles

CORROSION ON INTERCOSTAL FLOOR SUPPORT, STATIONS 1640 TO 1660, LEFT BUTTLINE 1 TO RIGHT BUTTLINE 1, WATERLINE 208. REMOVED AND REPLACED INTERCOSTAL FLOOR SUPPORT IAW AARD 51-00-05.

Part: FITTING — CORRODED (CARGO BAY) · corrosion level 2 · airframe 59,798 hrs · 20,562 cycles

FORWARD CARGO COMPARTMENT THRESHOLD POD LOCK FITTING IS CORRODED AT STATION 600. INSTALLED SERVICEABLE FORWARD CARGO COMPARTMENT THRESHOLD POD LOCK FITTING AT STATION 600.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,798 hrs · 20,562 cycles

AFT CARGO, CORROSION ON WEB AT STRINGER 28 LEFT BETWEEN STATIONS 1400 TO 1420. REMOVED AND INSTALLED NEW WEB AT STATIONS 1400 TO 1420 STRINGER 28 LEFT PER SRM 51-10-02-0G LINE 8.

Part: PAN — GOUGED (L4 DOOR) · airframe 59,798 hrs · 20,562 cycles

LEFT NUMBER 4 PASSENGER DOOR HANDLE PAN GOUGED. REPLACED HANDLE PAN AS PER ESO 90108.

Part: PRESSURE PANEL — MISREPAIRED (FUSELAGE) · airframe 59,798 hrs · 20,562 cycles

PREVIOUS REPAIRS ON PRESSURE DECK DON"T EXTEND UNDER AFT ANGLE AT STA 1720. INSTALLED DOUBLER ON AFT PRESSURE DECK AT STATIONS 1712 TO 1720 LEFT BUTTLINE 46 TO RIGHT BUTTLINE 40 IAW SRM 53-60-51-2R 2.

Part: SKIN — DAMAGED (TE FLAP) · airframe 61,463 hrs · 21,144 cycles

TOP OF SKIN LEFT INBOARD MAIN FLAP INBOARD END DENT IS DELAMINATED. REMOVED 2 BY 4 INCHES SKIN AND CORE, HOT BONDED NEW CORE, FABRICATED AND INSTALLED HOT BONDED DOUBLER PER SRM 51-71-10-2R FIGURE 209.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,960 hrs · 19,909 cycles

FORWARD SECTION COACH EMERGENCY LIGHTS ON SEATS DIM. REPLACED BATTERY PACK AT SEAT 9D.

Part: PLACARD — INCORRECT (CABIN) · airframe 57,960 hrs · 19,909 cycles

CENTER LAVATORY WALL EMERGENCY ARROW INCORRECT. REPLACED CENTER LAVATORY WALL EMERGENCY ARROW.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,960 hrs · 19,909 cycles

EMERGENCY LIGHTS ON SEATS IN CENTER COACH SECTION INOPERATIVE. REPLACED LIGHT ASSEMBLY AFT AT SEAT 18D.

Part: MODULE — FAILED (CABIN) · airframe 57,960 hrs · 19,909 cycles

CENTER SECTION COACH EMERGENCY LIGHTS ON SEATS IN MID CABIN INOPERATIVE. REPLACED MODULE AT SEAT 20D.

Part: PLACARD — INCORRECT (CABIN) · airframe 57,960 hrs · 19,909 cycles

FORWARD GALLEY WALL EMERGENCY EXIT ARROW IS INCORRECT. REPLACED FORWARD GALLEY WALL EMERGENCY ARROW.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,884 hrs

SJU - EMERGENCY AISLE LIGHT FROM SEATS 16D TO 25D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY AISLE LIGHT FROM SEATS 16D TO 25D.

Part: CONNECTOR — LOOSE (CABIN) · airframe 56,522 hrs

SFO - SEAT 20D EMERGENCY LIGHT INOPERATIVE. SECURED LOOSE SIDE WALL EMERGENCY LIGHT CONNECTION.

Part: LIGHT — BROKEN (CABIN) · airframe 56,522 hrs

SFO - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 18D BROKEN. REPLACED LIGHT ASSEMBLY FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 18D.

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,207 hrs · 19,631 cycles

PRESSURE DECK CORRODED. REPAIRED IAW EA B757-53-006093.

Part: LENS — MISSING (CABIN) · airframe 56,447 hrs

DFW - FORWARD GALLEY FLOOD LIGHT MISSING LENS. REPLACED LENS FOR FORWARD GALLEY FLOOD LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,447 hrs

DFW - SEAT PROXIMITY LIGHT ON 1E INOPERATIVE. REPLACED LAMP FOR EMERGENCY PATH LIGHT AT SEAT 1E.

Part: LENS — MISSING (CABIN) · airframe 56,477 hrs

DFW - EXIT LIGHT AT LEFT NUMBER FOUR DOOR SIDEWALL MISSING LENS. REPLACED LIGHT ASSEMBLY FOR EXIT LIGHT AT LEFT NUMBER FOUR DOOR SIDEWALL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,447 hrs

DFW - THE 18D SEAT PROXIMITY LIGHT INOPERATIVE. REPLACED LAMP FOR EMERGENCY PATH LIGHT ON SEAT 18D.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,447 hrs

DFW - THE 3E SEAT PROXIMITY LIGHT INOPERATIVE. REPLACED LAMP FOR EMERGENCY PATH LIGHT ON SEAT 3E.

Part: VALVE — FAULTED (PARK BRAKE) · airframe 55,394 hrs

MIA PARK BRAKE LIGHT AND EICAS ON AFTER ONE HOUR AND 20 MINUTES. LANDED MIA WITHOUT INCIDENT. REPLACED PARK BRAKE VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — INOPERATIVE (EMERGENCY LIGHTS) · 54,837 cycles

LGA EMERGENCY LIGHT AT SEAT 18D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT SEAT 18D. SYSTEM GROUND CHECKED NORMAL OPS.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · 54,837 cycles

LGA EMERGENCY LIGHT AT SEAT 18D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT SEAT 18D. SYSTEM GROUND CHECKED NORMAL OPS.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT RT NUMBER FOUR SLIDE INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT RT NR FOUR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT RIGHT NUMBER THREE DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT NUMBER THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — DAMAGED (EMERGENCY LIGHTS) · airframe 52,663 hrs

MIA - EMERGENCY LIGHT AT SEAT 24D HAS DAMAGED LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 24D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — MISINSTALLED (CABIN)

MIA INFLIGHT T2160/08NOV - FLIGHT ATTENDANTS REPORTED FIRE IN OVERHEAD ROW 11. FLIGHT ATTENDANTS USED HALON EXTINGUISHER WHICH CREATED SMOKE IN CABIN. AIRCRAFT RETURNED TO MIA AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND FLUORESCENT LIGHT AT RIGHT SEAT ROW 11. INSTALLED INCORRECTLY WITH PRONGS BENT. ACCOMPLISHED DETAILED INSPECTIONS AND REPLACED LIGHT ASSEMBLY BALLAST AT SEAT ROW 11 AND 12. MAINTENANCE REPORTED NO EVIDENCE OF FIRE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHTS AT SEAT ROWS 16DEF TO 25DEF INOPERATIVE. REPLACED BATTERY PACK AT CEILING AT BIN 20DEF FOR EMERGENCY LIGHTS AT SEAT ROWS 16DEF TO 25DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - EMERGENCY EXIT SIGN LIGHT IN CABIN INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY EXIT SIGN LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

MIA - EMERGENCY EXIT LIGHT AT SEAT 4C INOPERATIVE. RELAMPED EMERGENCY EXIT LIGHT AT SEAT 4C. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CYLINDER — INOPERATIVE (NOSE GEAR)

DFW INFLIGHT T1276/21FEB - ARRIVED DFW WITH RIGHT NOSE TIRE/WHEEL ASSEMBLY MISSING. PASSENGERS DEPLANED VIA PORTABLE STAIRS AND BUSSED TO TERMINAL. REPLACED NOSE GEAR PISTON AXLE ASSEMBLY, TIRES AND WHEELS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

SFO - EMERGENCY LIGHTS FROM SEAT ROWS 9D TO 15D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS FROM SEAT ROWS 9D TO 15D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHT AT SEAT 18D HAS LENS MISSING. INSTALLED NEW LENS AT SEAT 18D FOR EMERGENCY LIGHT MISSING LENS AT SEAT 18D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — DISLODGED (EMERGENCY LIGHTS)

DFW - EMERGENCY ESCAPE PATH LIGHT AT SEAT 32D INOPERATIVE. FOUND CONNECTOR PINS UNDER SEAT 32D DISLODGED. REINSTALLED CONNECTORS AT SEAT 32D FOR EMERGENCY ESCAPE PATH LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PUMP — LEAKING (HYD SYSTEM)

EN ROUTE DIVERTED TO ORD DUE TO CENTER SYSETM HYD QUANTITY LOSS. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED NR 2 CENTER SYSTEM ELECTRIC PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SPRING — OUT OF ADJUST (GIRT BAR)

DURING ACCOMPLISHMENT OF ENGINEERING REQUEST TO CHECK GIRT BAR SPRINGS AT EACH PASSENGER DOOR POSITION, FOUR GIRT BAR SPRINGS OUT OF ADJUSTMENT. ADJUSTED FOUR GIRT BAR SPRINGS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT ROW 16 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT ROW 16. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: DOOR — STUCK (MAIN PAX)

LAX - FLT 159 - ON ARRIVAL, L1 DOOR DIFFICULT TO OPEN. ASSIST BOTTLE FIRED AND SLIDE PARTIALLY DEPLOYED. SLIDE DID NOT FULLY DEPLOY BECAUSE OF JETBRIDGE. REPLACED DOOR SLIDE AND DOOR ASSIST BOTTLE. (M)

Part: HYDRAULIC LINE — BROKEN (HYD SYSTEM)

(LINE) EN ROUTE, MIA-BOG LOSS OF LEFT SYSTEM HYDRAULIC FLUID INDICATION. DECLARED EMERGENCY AND LANDED AT MBJ WITHOUT INCIDENT. CHECKED AND FOUND BROKEN HYDRAULIC LINE ON NOSE GEAR DOOR ACTUATOR. REPLACED HYDRAULIC LINE. REPLENISHED SYSTEM. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: COFFEEMAKER — DIRTY (GALLEY)

SJU - FLT 623 - EN ROUTE SJU-FLL - FLIGHT ATTENDANT REPORTED SMOKE ODOR AROUND 2R AREA. AIR INTERRUPTED AND LANDED SJU WITHOUT INCIDENT. INSPECTED AREA AND FOUND BURNED TEA BAG RAPPER AND TIED RAP UNDER COFFEE MAKER IN THE MID GALLEY. REMOVED BOTH COFFEE MAKERS AND CLEANED AREA. REPLACED BOTH COFFEE MAKERS AS PRECAUTIONARY ACTION. INSPECTED FORWARD CARGO AND E/E COMPARTMENT. NO EVIDENCE OF SMOKE. (M)

Part: O-RING — LEAKING (HYDRAULIC SYS)

DEN - FLT 278 - EN ROUTE DFW-ANC, DETECTED HYDRAULIC QUANTITY INDICATION ILLUMINATE. DIVERTED DEN AND LANDED WITHOUT FURTHER INCIDENT. REPLACED RIGHT PRESSURE SWITCH O-RING. SERVICED HYDRAULIC SYSTEM. LEAK CHECKS GOOD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: HARNESS — BROKEN (CABIN)

JFK - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHT AT SEAT 23D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT HARNESS AT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

TUL - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHT AT SEAT 19D INOPERATIVE. RE-SEATED EMERGENCY EXIT LIGHT PIN AT SIDE WALL CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: AIR DISTR — ODOR (CABIN)

SFO - FLT 1376 - AFTER T/O SFO DURING INITIAL CLIMB-OUT, ELECTRICAL ODOR NOTED IN CABIN AND COCKPIT. A/C RETURNED TO SFO AND LANDED W/O INCIDENT. CHECKED OPERATION OF ALL PACKS AND CABIN/COCKPIT LIGHTING WITH NO DEFECTS FOUND. ACCOMP FUNCTIONAL CHECK FLT AND PROBLEM REPEATED. REPEATED CHECK OF COCKPIT/CABIN LIGHTING INCLUDING FULL BRIGHT OPERATION WITH NO DEFECTS FOUND. CLEANED HYDRAULIC RESERVOIR PRESSURE MODULE CHECK VALVES AND REPLACED FILTER. CHECKED EQUIP COOLING SYSTEM WITH NO DEFECTS FOUND. ACCOMP PACK BURN OUT PROCEDURE ON BOTH PACKS. ACCOMP SECOND FUNCTIONAL CHECK FLT WITH NO DEFECTS FOUND. SYSTEMS OPERATIONAL CHECKED NORMAL WITH NO ODOR NOTED NOTED. A/C RETURNED TO SERV. (M)

Part: FLOORBEAM — CORRODED (BS 324)

FLOORBEAM AT STATION 324 RBL 58 AND RBL 59 HAD CORROSION BLENDED BEYOND SRM LIMITS. PER MRB 75-763. (M)

Part: FLOOR STRUCTURE — CORRODED (BS 300)

FLOOR STRUCTURE AT STATION 300 RBL 40 HAD CORROSION BLENDED BEYOND SRM LIMITS. PER MRB 757-769. (M)

Part: DOOR PANEL — GOUGED (L4 DOOR)

L-4 EXTERNAL HANDLE PAN HAS A GOUGE BEYOND SRM LIMITS, AREA WAS BLENDED OUT. PER MRB 757-771. (M)

Part: SKIN — GOUGED (BS 36)

FUSELAGE SKIN HAS GOUGES BLEND OUT BEYOND SRM LIMITS. PER MRB 757-774. (M)

Part: DOOR PAN — GOUGED (R4 DOOR)

R-4 DOOR HANDLE PAN HAS A SMALL GOUGE. AFTER BLENDING IS BEYOND SRM LIMITS. PER MRB 757-762. (M)

Part: STRUCTURE — DAMAGED (BS 1384)

AFT CARGO DOOR SURROUND STRUCTURE LOWER STILL CHORD AT STATION 1384, UPPER SURFACE, HAD CORROSION BLENDED BEYOND SRM LIMITS. PER MRB 757-772. (M)

Part: DECK PLATE — CORRODED (BS 1720)

DECK PLATE HAS CORROSION REMOVAL ON UPPER SURFACE AT VARIOUS LOCATIONS. MATERIAL REMAINING IS BEYOND SRM LIMITS. PER MRB 757-767. (M)

Part: FLOORBEAM — CORRODED (BS 365)

FLOORBEAM AT STATION 365, RBL 10 AND RBL 58 HAD CORROSION REMOVED BEYOND SRM LIMITS. PER MRB 757-765. (M)