N379AA

Part: UNKNOWN — VIBRATION (WING) · airframe 103,386 hrs · 16,854 cycles

AIRCRAFT NOT GROUNDED: PILOT REPORTS ON APPROACH, GEAR DOWN, FLAPS 25, SPEED (IAS) APPROX. 140-145 KT, WHEN CONTROL WHEEL TURNED LEFT, BUFFET FELT ON RIGHT SIDE OF AIRCRAFT. MAINTENANCE PERFORMED SATISFACTORY INSPECTION AND OPERATIONAL CHECK OF FLAPS/AILERONS/SPOILERS. NO DISCREPANCIES. OPS NORMAL IAW AMM 27-11-00-001 (4A2 NOTE) NO HISTORY PER MOC.

Part: BATTERY — NO TEST (FLASHLIGHT) · airframe 103,127 hrs · 16,804 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY FLASHLIGHT UNDER FORWARD FACING FLIGHT ATTENDANT SEAT ON LIGHT SIDE OF AIRCRAFT AT MID GALLEY INOPERATIVE. MAINTENANCE REPLACED BATTERY AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: BULB — BURNED OUT (NLG INDICATOR) · airframe 103,087 hrs · 16,797 cycles

AIRCRAFT NOT GROUNDED: PILOT REPORTS NOSE LANDING GEAR GREEN LIGHT FAILED TO ILLUMINATE AFTER LANDING GEAR DEPLOYED. CREW DID MISSED APPROACH. EMERGENCY DECLARED. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND BOTH BULBS FOR THE NOSE GEAR ANNUNCIATOR BURNED OUT. REPLACED BULBS. OPS CHECK GOOD.

Part: ACTUATOR — INACCURATE (AUTOPILOT) · airframe 102,970 hrs · 16,763 cycles

UNCOMMANDED RIGHT AUTOPILOT DISCONNECT. CONNECTED, AND DISCONNECTED AGAIN. REMOVED AND REPLACED THE LOWER LCCA IN THE LT WHEEL WELL IAW MM 27-11-14. OPS & LEAKED CHECKED IAW MM 27-11-14, AND MM 22-00-02.

Part: ACM — DEFECTIVE (RIGHT) · airframe 102,694 hrs · 16,692 cycles

FLIGHT EXPERIENCED A RIGHT PACK OVERHEAT, RESULTING IN A LOSS OF CABIN PRESSURE. CABIN PRESSURE UNABLE TO HOLD AT CRUISE ALTITUDE ON ONE PACK SLOW LOSS OF PRESSURE TO CABIN ALTITUDE 12,000. MASKS DID NOT DEPLOY, EMERGENCY DECLARED, AND FLIGHT LANDED WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED RT PACK LOW LIMIT VALVE IAW AMM 21-51-11. FIELD REPORTS THE RT ACM IS AT FAULT. REPLACED RT ACM IAW AMM 21-51-03.

Part: A/C PACK — FAULTED (RIGHT) · airframe 102,356 hrs · 16,621 cycles

DURING CRUISE, FLIGHT FL 390, LOWER EICAS MESSAGE FOR THE RIGHT PACK TEMPERATURE, AND RIGHT PACK INOPERATIVE, DISPLAYED THE FOLLOWING QRH GUIDANCE BEFORE RESET COULD BE ATTEMPTED. CABIN ALTITUDE MASTER WARNING RECEIVED WITH LEFT PACK STILL OPERATING. MAINTENANCE ACCOMPLISHED ATBT & TII, LEFT HEAT EXCHANGER IAW AMM 21-51-02, AND REPLACED THE RIGHT PACK OVERHEAT SENSOR 5-49 IAW AMM 21-51-18, AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: FLASHLIGHT — INOPERATIVE (MID GALLEY) · airframe 102,162 hrs · 16,583 cycles

MID GALLEY FLIGHT ATTENDANT SEAT EMERGENCY FLASHLIGHT WAS INOPERATIVE. REPLACED THE FLASHLIGHT IAW AMM 25-60-00. OPS CHECKED NORMAL.

Part: FLASHLIGHT — INOPERATIVE (FWD GALLEY) · airframe 102,162 hrs · 16,583 cycles

FORWARD GALLEY FLIGHT ATTENDANT SEAT FLASHLIGHT WAS INOPERATIVE. REPLACED THE FLASHLIGHT IAW AMM 25-60-00. OPS CHECKED NORMAL.

Part: ACTUATOR — INOPERATIVE (OXYGEN MASKS) · airframe 102,076 hrs · 16,555 cycles

THE CABIN DEPRESSURIZED IN FLIGHT AND THE MASKS AT ROW 43CEG DID NOT DEPLOY. REPLACED O2 DOOR ACTUATOR AT SEAT 43CEG IAW AMM 35-21-15.

Part: DUCT — DISCONNECTED (GROUND AIR) · airframe 102,078 hrs · 16,556 cycles

AIRCRAFT WOULD NOT MAINTAIN PRESSURE. INTIALLY PACK PRESSURE OFF WITH A PACK INOPERATIVE LIGHT. FOLLOWED QRH PROCEDURES, DECENDED TO 31,000 FEET, CABIN ALTITUDE WAS SLOWLY CLIMBING. CONTINUED DECENT TO 24,000 FEET, COULD NOT CONTROL THE CABIN ALTITUDE, TRIED TO CONTROL CABIN IN MANUAL MODE AND WAS UNSUCCESSFUL AND CONTINUED DECENT TO 10,000 FEET. CABIN ALTITUDE LIGHT, QRC PROCEDURES FOLLOWED, NO EMERGENCY DECLARED AND DIVERTED. THE AIRCRAFT WAS GROUNDED. FOUND DUCT GOING FROM THE MUFFLER TO THE GROUND AIR CONNECTION DISCONNECTED. SECURED THE DUCT AND PERFORMED SATISFACTORY OPERATIONAL CHECK, NO LEAKS NOTED IAW AMM 21-21-02.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 102,047 hrs · 16,545 cycles

MID GALLEY LT AFT FLT ATTENDANT SEAT FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE FLASHLIGHT BATTERY IAW AMM 25-64-00, OPS CHECKED OK.

Part: COMPUTER — FAULTY (COCKPIT) · airframe 101,479 hrs · 16,419 cycles

AIRCRAFT WAS GROUNDED: AT TAKEOFF, LOSS OF AUTO THROTTLE AND FLIGHT DIRECTOR AIR SPEED MONITOR AND ALTERNATIVE POINTER ON THE CAPTAIN SIDE. SWITCHED TO INSTRUMENTAL SOURCE TO RIGHT SIDE, AUTOPILOT INOPERABLE. EMERGENCY DECLARED, FLIGHT LANDED OVERWEIGHT WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED MODE CONTROL PANEL, FLIGHT CONTROL LEFT (SEE AALA201808319034) AND RIGHT COMPUTERS PER MM 22-11-02 AND MM 22-11-01 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 101,479 hrs · 16,419 cycles

AIRCRAFT WAS GROUNDED: AT TAKEOFF, LOSS OF AUTO THROTTLE AND FLIGHT DIRECTOR AIR SPEED MONITOR AND ALTERNATIVE POINTER ON THE CAPTAIN SIDE. SWITCHED TO INSTRUMENTAL SOURCE TO RIGHT SIDE, AUTOPILOT INOPERABLE. EMERGENCY DECLARED, FLIGHT LANDED OVERWEIGHT WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED MODE CONTROL PANEL, FLIGHT CONTROL LEFT (SEE AALA201808319034) AND RIGHT (SEE AALA201808319035) COMPUTERS PER MM 22-11-02 AND MM 22-11-01 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 101,433 hrs · 16,408 cycles

RIGHT MID FLIGHT ATTENDANT JUMP SEAT FLASHLIGHT WAS INOPERATIVE. REPLACED THE FLASHLIGHT BATTERY IAW AMM 25-64-00. OPS CHECKED NORMAL.

Part: BATTERY — NO TEST (FLASHLIGHT) · airframe 101,042 hrs · 16,324 cycles

FLASHLIGHT LOCATED UNDER FLIGHT ATTENDANT SEAT, NEXT TO SEAT 17B, WAS NOT ACCEPTING A CHARGE. MAINTENANCE REPLACED THE BATTERY AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: CIRCUIT CARD — FAULTY (FLOW CONTROL) · airframe 100,973 hrs · 16,310 cycles

BETWEEN 16000 AND 24000 FEET HAD A HARD TIME REGULATING CABIN TEMPERATURE. ONE PACK HAD ALREADY BEEN PUT ON MEL, EMERGENCY WAS DELCARED AND AIRCRAFT RETURNED TO BLOCK. AIRCRAFT LANDED WITHOUT INCIDENT. NO OVERWEIGHT LANDING. CHANGED EQUIPMENT AND REDEPARTED. REPLACED FLOW CONTROL CARD PER AMM 21-51-09PB401. AIRCRAFT WAS GROUNDED.

Part: SWITCH — FAULTY (OVERHEAT) · airframe 100,973 hrs · 16,310 cycles

BETWEEN 16,000 AND 24,000 FEET, HAD A HARD TIME REGULATING CABIN TEMPERATURE. ONE PACK HAD ALREADY BEEN PUT ON MEL, EMERGENCY WAS DELCARED AND AIRCRAFT RETURNED TO DEPARTURE. AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS GROUNDED. REPLACED COMPRESSOR DISCHARGE OVERHEAT SWITCH IAW 21-51-19-01.

Part: LIGHT — INOPERATIVE (SEAT 38B) · airframe 99,694 hrs · 16,077 cycles

SEAT 38B MOUNTED EMERGENCY LIGHT INOPERATIVE. REPLACED THE EMERGENCY LIGHT ASSY IAW AMM 33-51-10, OPS OK.

Part: LIGHT — INOPERATIVE (SEAT 38B) · airframe 99,694 hrs · 16,077 cycles

SEAT38B MOUNTED EMERGENCY LIGHT INOPERATIVE. MAINTNENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY IAW AMM 33-51-10 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: SHADE — BROKEN (CABIN) · airframe 99,489 hrs · 16,036 cycles

AIRCRAFT WAS NOT GROUNDED. WINDOW SHADE 20J EMERGENCY EXIT ROW BROKEN. REPLACED WINDOW SHADE PER AMM 25-21-10.

Part: GIRT BAR — OBSTRUCTED (L4 DOOR SLIDE) · airframe 99,157 hrs · 15,980 cycles

AIRCRAFT WAS NOT GROUNDED. VERIFY DEBRIS AT 4L GIRT BAR. VERIFIED NO DEBRIS AT 4L GIRT BAR.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 98,283 hrs · 15,818 cycles

EMERGENCY LIGHTS BATTERY FAILED TO TEST. REMOVED AND REPLACED BATTERY ASSEMBLY. OPERATIONAL CHECKED GOOD.

Part: LENS — MISSING (CABIN) · airframe 97,643 hrs · 15,694 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHT OVERHEAD AISLE ADJACENT TO SEAT 37BC HAS A MISSING LENS COVER. INSTALLED LENS COVER IAW AMM 33-51-04. OPERATIONAL CHECK GOOD.

Part: LENS — MISSING (CABIN) · airframe 97,643 hrs · 15,694 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHT OVERHEAD AISLE ADJACENT TO SEAT 23BC HAS A MISSING LENS COVER. INSTALLED LENS COVER IAW AMM 33-51-04. OPERATIONAL CHECK GOOD.

Part: CONNECTOR — LOOSE (CABIN) · airframe 97,643 hrs · 15,694 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHT ON THE CLOSET ADJACENT TO ROW 20H IS INOPERATIVE. RESET LOOSE CONNECTOR AT ROW 20H IAW AMM 33-51-10. OPERATIONAL CHECK GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 97,207 hrs · 15,627 cycles

AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT EMERGENCY FLASHLIGHT ACROSS FROM M2 LAVATORY IS INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT BATTERY IAW AMM 25-64-01. OPERATIONAL CHECK GOOD.

Part: BATTERY — NO TEST (FLASHLIGHT) · airframe 97,103 hrs · 15,611 cycles

FLIGHT ATTENDANT FLASHLIGHT MIDDLE SEAT LEFT WILL NOT TEST. REMOVED AND REPLACED THE FLASHLIGHT BATTERY. OPS CHECKED GOOD.

Part: BATTERY — NO TEST (FLASHLIGHT) · airframe 97,103 hrs · 15,611 cycles

FLIGHT ATTENDANT FLASHLIGHT MIDDLE SEAT RIGHT WILL NOT TEST. REMOVED AND REPLACED THE FLASHLIGHT BATTERY. OPS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 96,347 hrs · 15,478 cycles

AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT EMERGENCY FLASHLIGHT MIDDLE RIGHT SEAT IS INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT IAW AMM 25-05-03. OPERATIONAL CHECK GOOD.

Part: FLASHLIGHT — BROKEN (CABIN) · airframe 96,347 hrs · 15,478 cycles

AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT EMERGENCY FLASHLIGHT FORWARD CENTER SEAT IS BROKEN. REMOVED AND REPLACED FLASHLIGHT IAW AMM 25-05-03. OPERATIONAL CHECK GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 96,204 hrs · 15,451 cycles

AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT EMERGENCY FLASHLIGHT MID CABIN LEFT AFT SIDE IS INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT BATTERY IAW AMM 25-64-01. OPERATIONAL CHECK GOOD.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 95,821 hrs · 15,382 cycles

L1 DOOR EMERGENCY EXIT SIGN LENS COVER IS DETACHED. REINSTALLED EXIT SIGN LENS COVER IAW AMM 33-51-09. OPERATIONAL CHECK GOOD.

Part: ACM — SEIZED (RIGHT) · airframe 94,247 hrs · 15,124 cycles

CABIN TEMPERATURE NEVER REDUCED AFTER TAKE-OFF. RIGHT PACK PUTTING OUT HOT AIR, LEFT TEMPERATURE CONTROLLER INOPERATIVE. CABIN REACHED MAX OF 99 DEGREES. THE AIRCRAFT WAS GROUNDED. REPLACED RIGHT ACM.

Part: CONTROLLER — FAULTY (RT A/C PACK) · airframe 95,892 hrs · 15,393 cycles

CABIN TEMPERATURE NEVER REDUCED AFTER TAKE-OFF. RIGHT PACK PUTTING OUT HOT AIR / LEFT TEMPERATURE CONTROLLER INOPERATIVE. CABIN REACHED MAX OF 99 DEGREES. THE AIRCRAFT WAS GROUNDED. REPLACED THE CABIN TEMPERATURE CONTROLLER AND CLEANED ZONE TEMPERATURE SENSOR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 93,927 hrs · 15,057 cycles

AIRCRAFT WAS IN BASE MX. CABIN FLOORBEAM AT FS 325 IS CORRODED, BETWEEN RBL 16 & 38. ACCOMPLISHED UPPER CHORD REPAIR IAW SRM 53-00-51-2R.

Part: HOSE — CONTAMINATED (ZONE 100) · airframe 93,785 hrs · 15,028 cycles

AIRCRAFT WAS GNDED. FOUND THE RT OFF WING ESCAPE SYS INFLATION HOSE DEFORMED & CONTAMINATED WITH FLUID. INSPECTED HOSE & FOUND SUITABLE FOR FUTURE FLIGHT IAW EA 259370. TII CREATED FOR REINSPECT NO LATER THAN EVERY 7 DAYS & REPLACEMENT NO LATER THAN 30 DAY. R & R HOSE IAW AMM 25-65-22.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 90,464 hrs · 14,462 cycles

LEFT FUSELAGE EMERGENCY LIGHT AFT WING BODY FAIRING IS INOPERATIVE. RELAMPED LT FUSELAGE EMERGENCY LIGHT AFT WING BODY FAIRING IAW MM 33-51-06. OPERATIONALLY CHECKED NORMAL.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 90,115 hrs · 14,411 cycles

DURING APPROACH THE F1 LAVATORY SMOKE DETECTOR WENT OFF. R & R SMOKE DETECTOR. PERFORMED OPERATIONAL CHECK IAW AMM 26-13-01-024-010, 26-13-01-424-004 & 26-13-00-715-090. SYS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 90,115 hrs · 14,411 cycles

TWO EACH WING SLIDE LIGHTS JUST AFT OF LT WING INOPERATIVE. REPLACED LAMPS AT L396 & L645 IAW MM 33-51-06-902-082. SYS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 89,371 hrs · 14,257 cycles

EMERGENCY LIGHT LOCATED ON THE AFT SIDE OF THE RT AFT SERVICE DOOR L392 IS INOPERATIVE. R & R EMER LIGHT LAMP IAW AMM33-51-06. SYS CHECKED NORMAL.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 88,778 hrs · 14,158 cycles

CORROSION AT FWD CARGO OUTER CHORD MAIN SILL STATION 569. REMOVED CORROSION & ACCOMPLISHED REPAIR IAW EA B767-53-037037.

Part: TEE FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 88,778 hrs · 14,158 cycles

FORWARD CARGO DOOR SILL UPPER T CAP CORRODED ON INBD SIDE OF LOWER ANGLE AT STATION 566 & RBL 48. REPAIRED IAW EA B767-57-037021.

Part: STRAP — CORRODED (FUSELAGE) · airframe 88,778 hrs · 14,158 cycles

FAIL SAFE STRAP FROM STATIONS 456 TO 610 CORRODED. REPLACED FAIL SAFE STRAP.

Part: STRAP — CRACKED (FUSELAGE) · airframe 88,778 hrs · 14,158 cycles

ACCESSORY COMPARTMENT HAS A CRACK IN OUTER CHORD STRAP AFT OF BULKHEAD 1725.50 ABOVE STRINGER 7 RT NEAR FWD LOWER CORNER OF AUXILIARY POWER UNIT INTAKE DOOR ASSEMBLY. ACCOMPLISHED REPAIR IAW SRM 53-80-01-2R REPAIR 5.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 88,778 hrs · 14,158 cycles

FORWARD RT DOOR UPPER CORNER EMER LIGHT INOPERATIVE. REPLACED BATTERY CHARGER. OPERATIONS CHECKED NORMAL.

Part: WIRE HARNESS — INOPERATIVE (BLEED AIR SYS) · airframe 88,696 hrs · 14,141 cycles

RIGHT ENG PRESS RELIEF VLV EICAS MSG. EMER DECLARED FLIGHT DIVERTED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED LOWER PART OF HARNESS. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 88,599 hrs · 14,126 cycles

LEFT NR 1 DOOR EXTERNAL EMER LIGHT INOPERATIVE. REPLACED LAMP FOR LT NR 1 DOOR EXTERNAL EMER LIGHT. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 88,151 hrs · 14,060 cycles

EMERGENCY EXIT SIGN AT 21AB INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT SIGN. OPERATIONS CHECKED NORMAL.

Part: LIGHT — DEFECTIVE (CABIN) · airframe 88,151 hrs · 14,060 cycles

EMERGENCY LIGHT AT SEAT 20HJ DIM. REPLACED LAMP FOR EMER LIGHT. OPERATIONS CHECKED NORMAL.

Part: SEAL — UNSECURE (COCKPIT) · airframe 86,921 hrs · 13,862 cycles

MCO CREW REPORTED CAPTAIN`S LT SIDE WINDOW DEVELOPED VERY LOUD SQUEAL, NOISE & AIR LEAK. DESCENDED TO 10,000 FEET TO REDUCE DIFFERENTIAL PRESS. EMERGENCY DECLARED FLIGHT LANDED MCO WITHOUT INCIDENT. SECURED LT NR 2 WINDOW FRAME SEAL AT TOP OF WINDOW FRAME FWD OF UPPER LT CORNER OF FRAME. SECURED LT NR 2 WINDOW FRAME SEAL AT TOP OF WINDOW FRAME FWD OF UPPER LT CORNER OF FRAME. SYS GND CHECKED NORMAL, OPERATION CLOSED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 86,401 hrs · 13,768 cycles

SEAT 23B SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 23B, OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 85,460 hrs · 13,603 cycles

LT SIDE FUSELAGE MOUNTED NR 4 SLIDE ILLUMINATION EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LAMP FOR LT SIDE FUSELAGE MOUNTED NR 4 SLIDE ILLUMINATION EMERGENCY EXIT LIGHT. OPERATIONS CHECKED NORMAL.

Part: SMOKE DETECTOR — DEFECTIVE (LAVATORY) · airframe 85,123 hrs · 13,550 cycles

ZRH ON APPROACH M1 LAVATORY SMOKE DETECTOR ACTIVATED. CREW INSPECTED & NOTHING ABNORMAL NOTED. FLIGHT LANDED ZRH WITHOUT INCIDENT. REPLACED SMOKE DETECTOR AT M1 LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 83,743 hrs · 13,321 cycles

CORROSION FOUND ON STRINGER 38 RT AT BS 1575. REMOVED STRINGER DAMAGE & INSTALLED STRINGER REPAIR IAW SRM 53-00-03-2R-2.

Part: SKIN — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 83,743 hrs · 13,321 cycles

CORROSION ON HORIZONTAL STABILIZER CENTER SECTION UPPER SKIN AT AFT EDGE RT BUTTLINE 14 AT THE AFT SPAR. REMOVED CORROSION AND INSTALLED DOUBLER REPAIR IAW EA B767-55-030229.

Part: SKIN — CORRODED (FUSELAGE) · airframe 83,743 hrs · 13,321 cycles

SKIN BULGING AT STA 1263 AND STRINGER 37 LEFT. REMOVED DAMAGED SKIN AND INSTALLED DOUBLER IAW SRM 53-00-01-2R-1.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 82,357 hrs · 13,114 cycles

AFT LEFT SIDE CEILING EMERGENCY LIGHT AT AFT GALLEY INOPERATIVE. REPLACED LAMP FOR AFT LEFT SIDE CEILING EMERGENCY LIGHT. OPS CHECKS NORMAL.

Part: LENS — MISSING (CABIN) · airframe 82,357 hrs · 13,114 cycles

EMERGENCY LIGHT LENS MISSING AT 26 ABC. INSTALLED EMERGENCY LIGHT LENS COVER AT 26 ABC. OPS CHECK NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 82,355 hrs · 13,113 cycles

EMERGENCY (EMP) SEAT MOUNTED LIGHTS AT SEATS 22 TO 24 RIGHT SIDE INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY. OPS CHECKED NORMAL.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 82,355 hrs · 13,113 cycles

THE EMERGENCY (EMP) SEAT MOUNTED LIGHT AT 22L INOPERATIVE. REMOVED AND REPLACED MOLEX CONNECTOR AND PIN AT SEAT 22L. OPS CHECKED NORMAL.

Part: FILTER — DEFECTIVE (RT ENGINE) · airframe 81,886 hrs · 13,044 cycles

DFW - CREW REPORTED RIGHT ENGINE FUEL FILTER EICAS MESSAGE. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED FUEL FILTER AND FUEL DIFFERENTIAL PRESSURE SWITCH. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 81,081 hrs · 12,920 cycles

EMERGENCY LIGHT AT SEAT MOUNT ROW 31B INOPERATIVE. REPLACED LIGHT ASSEMBLY AT SEAT 31B. OPS CHECK NORMAL.

Part: LENS — MISSING (CABIN) · airframe 81,081 hrs · 12,920 cycles

EMERGENCY LIGHT LENS AT LAVATORY A-6 WALL. REPLACED LENS FOR EMERGENCY LIGHT AT LAVATORY A-6 WALL. OPS CHECK NORMAL.

Part: SIGN — MISSING (CABIN) · airframe 78,830 hrs · 12,553 cycles

LEFT NUMBER 1 DOOR EXIT SIGN MISSING. REPLACED EXIT SIGN AT LEFT NUMBER 1 DOOR. OPS CHECK NORMAL.

Part: SPAR — CRACKED (LT PYLON) · airframe 78,183 hrs · 12,450 cycles

FOUND CRACK IN LEFT PYLON STRUT FORWARD UPPER SPAR WEB AROUND FEEDER CABLE CUTOUT. REMOVED DAMAGE AND ACCOMPLISHED DOUBLER REPAIR PER EA B767-54-020072.

Part: TAIL CONE — DENTED (FUSELAGE) · airframe 78,183 hrs · 12,450 cycles

DENT AT TAIL CONE LEFT SIDE AT BASE OF RUDDER. INSTALLED EXTERNAL DOUBLER PER SRM 53-00-01-2R-14.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 78,183 hrs · 12,450 cycles

RIVETS INSTALLED IN STATIONS 1567 TO 1577 STRINGERS 19 TO 22 RIGHT DAMAGED. ACCOMPLISHED DOUBLER REPAIR PER EA B767-53-020249.

Part: INDICATOR — FAILED (ALTIMETER) · airframe 77,610 hrs · 12,369 cycles

MIA - CREW REPORTED CAPTAINS ALTIMETER FAILED DURING TAKEOFF ROLL. EMERGENCY DECLARED FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. REPLACED CAPTAINS ALTIMETER INDICATOR AND LEFT AIR DATA COMPUTER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FITTING — LEAKING (BLEED AIR SYS) · airframe 75,832 hrs · 12,093 cycles

LAX - INFLIGHT DFW-HNL. CREW REPORTED ON TAKEOFF LEFT ENGINE BLEED LIGHT AND PRESSURE RELIEF VALVE MESSAGE ILLUMINATED. EMERGENCY DECLARED FLIGHT DIVERTED LAX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND ELBOW FITTING ON THE PRESSURE RELIEF VALVE WITH THREADS STRIPPED. REPLACED ELBOW ASSEMBLY. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 75,584 hrs · 12,060 cycles

LEFT OVERWING SLIDE EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT OVERWING SLIDE EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 74,940 hrs · 11,948 cycles

LHR - AFT RIGHT LAVATORY SMOKE DETECTOR WENT OFF FOR SHORT TIME. FLIGHT LANDED LHR WITHOUT INCIDENT. REPLACED SMOKE DETECTOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: OVEN — DIRTY (GALLEY) · airframe 73,615 hrs · 11,720 cycles

LHR - INFLIGHT CDG-MIA. CREW REPORTED STRONG ELECTRICAL SMELL IN COCKPIT AND FORWARD CABIN. FLIGHT DIVERTED LHR LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. INSPECTED ALL ELECTRICAL SYSTEMS COULD NOT DUPLICATE ODOR. FOUND FOOD RESIDUE IN FORWARD GALLEY OVEN CAUSING SMOKE. CLEANED GALLEY OVEN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,694 hrs · 11,550 cycles

DURING HEAVY CHECK, LOCAL CORROSION WAS FOUND ON THE STA 347 FLOORBEAM UPPER CAP BETWEEN RBL 54.5 AND RBL 68.25. THE CORROSION WAS CENTRALIZED AROUND NUT PLATE SCREW HOLES ON THE FLANGE OF THE INNER CHORD. ALL CORROSION WAS REMOVED BY BLENDING. THE BLENDS WERE REINFORCED USING A REPAIR STRAP OF 0.050€? CRES 301 ½ HARD / STAINLESS STEEL UNDER ENGINEERING AUTHORIZATION B767-53-011246.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 69,806 hrs · 11,035 cycles

WHEN SHUT AIRCRAFT POWER OFF COCKPIT EMERGENCY LIGHT CAME ON WITH EMERGENCY SWITCH IN OFF POSITION. REPLACED EMERGENCY LIGHT ASSEMBLY.

Part: STRAP — DAMAGED (FLOORBEAM) · airframe 66,711 hrs · 10,554 cycles

STABILIZATION STRAP FOR MAIN DECK FLOORBEAM WAS SEVERED. REMOVED PREVIOUS INTERIM REPAIR. AREA OF DISCREPANCY IS 3.25 INCH FORWARD AND 2.4 INCH AFT INBOARD OUTBOARD. INSTALLED REPAIR STRAP PER SRM 53-10-51 2R FIG 201 AND MRB 767 3351.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,818 hrs

DFW - EMERGENCY LIGHT AT LEFT SIDE AFT OF WING INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT SIDE AFT OF WING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS)

MIA - EXTERNAL EMERGENCY LIGHT AT LEFT AFT OF WING INOPERATIVE. REPLACED LAMP FOR EXTERNAL EMERGENCY LIGHT AT LEFT AFT OF WING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

SFO - EMERGENCY LIGHTS ON LEFT SIDE SEAT ROWS 5 TO 7 INOPERATIVE. REPLACED BATTERY PACK M379 FOR EMERGENCY LIGHTS ON LEFT SIDE SEAT ROWS 5 TO 7. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT LEFT AFT OVERWING INOP. RELAMPED EMERGENCY LIGHT AT LEFT AFT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

DFW - FOUND EMERGENCY LIGHT AT SEAT 5H INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 5H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (CABIN)

MIA - EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR SLIDE HAS LENS COVER MISSING. REPLACED LENS FOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SFO - EMERGENCY LIGHT AT LEFT SEATS 20B TO 24B INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 22A FOR INOPERATIVE EMERGENCY LIGHTS AT LEFT HAND SEATS 20B TO 24B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — INOPERATIVE (EMERGENCY LIGHTS)

SFO - EMERGENCY LIGHT AT SEAT 29B HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 29B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

SFO - EMERGENCY LIGHT ON LEFT HAND SIDE FORWARD CABIN INOPERATIVE. RELAMPED EMERGENCY LIGHT ON LEFT HAND SIDE FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

CDG ALL EMERGENCY LIGHTS AT RT AFT CABIN INOPERATIVE. FOUND FUSE ON POWER SUPPLY BLOWN AND CONNECTORS ON RIGHT HAND SEATS 35HJ AND 39HJ DAMAGED. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS WITH FUSE ON POWER SUPPLY BLOWN. SYSTEM GROUND CHECKED NORMAL OPERATION. PLACARDED EMERGENCY LIGHTS ON SEAT 35HJ AND 39HJ INOP PER MEL 33 16A. CONNECTORS NOT IN STOCK IN CDG. REPAIRED SHORTED CONNECTOR AT 39H EMERGENCY PATH LIGHT AND CLEARED MEL AT LAX. SYSTEM GROUND CHECKED NORMAL OPERATION. (SUPP CLOSED)

Part: WIRE — LOOSE (EMERGENCY LIGHT)

SFO - EMERGENCY LIGHT ON SEAT 13H IS INOPERATIVE. REINSTALLED LOOSE ELECTRICAL CONNECTION AT SEAT 13H FOR EMERGENCY LIGHT ON SEAT 13H. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: LIGHT — LOOSE (CABIN)

DFW - EMERGENCY LIGHT AT SEAT 36B INOPERATIVE. SECURED LOOSE CONNECTION FOR EMERGENCY LIGHT AT SEAT 36B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

MIA - EMERGENCY EXIT LIGHT ON G2 FORWARD GALLEY INOPERATIVE. FOUND CONNECTOR LOOSE. SECURED CONNECTOR FOR EMERGENCY EXIT LIGHT ON G2 FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SFO - EMERGENCY LIGHTS AT 2B THROUGH 6B INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT 2B THROUGH 6B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT SEAT 13HJ INOPERATIVE. INSTALLED SEAT HARNESS FOR EMERGENCY LIGHT AT SEAT HJ. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SOCKET — LOOSE (EXTERIOR)

SFO - DURING OVERNIGHT MAINTENANCE, L2 DOOR OUTSIDE EMERGENCY LIGHT INOPERATIVE. RESEATED L2 DOOR EMERGENCY LIGHT SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: VOR SYSTEM — MALFUNCTIONED (COCKPIT)

COPILOTS VOR HAS OFF FLAG NEEDLE DOES NOT POINT TO STATION NO COURSE ON CDI. DME WORKS ONLY WITHIN 25 MILES OR LESS FROM STATIONS. RIGHT VOR RECEIVER BITE TEST CARRIED OUT, NO FAULTS SHOWN TEST PASS OK. (M)

Part: IDG — FAILED (RT ENGINE)

FRA - FL 84 - ONE HOUR AFTER TAKEOFF RIGHT GEN DRIVE LIGHT CAME ON GEN DISCONNECTED. REPLACED RIGHT IDG. OPS AND LEAK CHECK NORMAL PER AMM 24-11-01-04. (M)

Part: WIRE — BROKEN (CABIN)

ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING SEATS 3A AND 3B INOPERATIVE. REPLACED CONNECTOR FOR EMERGENCY ESCAPE PATH LIGHTING SEATS 3A AND 3B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: PIN — DEFECTIVE (CONNECTOR)

LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHT AT SEAT 34H INOPERATIVE. REPLACED CONNECTOR PIN ON SEAT 34H EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — LOOSE (CABIN)

MIA - FLT 26 - AFTER LANDING BEFORE NEXT FLIGHT EMERGENCY EXIT ESCAPE SEAT PATH LIGHT AT SEAT 26H INOPERATIVE. SECURED LOOSE WIRE BEHIND SEAT 26H LIGHT ASSEMBLY. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: SKIN — CORRODED (FUSELAGE)

AFW - FUSELAGE SKIN HAS CORROSION REMOVAL ON UPPER SURFACE AS SHOWN ON SKETCH, REQUEST ENGG APPROVAL TO CONTINUE IN SERVICE. BLENDOUT CORROSION AND REFINISH BLENDED AREA PER SRM. IT IS ACCEPTABLE FOR CONTINUED SERVICE WITH NOTED CONDITION. PERFORM HFEC TO ENSURE NO CRACKS. (M)

Part: SKIN — CORRODED (FUSELAGE)

AFW - FORWARD CARGO DOOR CUT OUT LOWER CHORD HAD CORROSION BLENDED BEYOND SRM LIMITS AT STATION 568. REQUEST ENGINEERING APPROVAL TO CONTINUE AS IS. BYE CHECK FOR CRACKS. BLEND OUT CORROSINO AND DYE CHECK TO ENSURE CRACK FREE. REFINISH THE BLENDED AREA PER SRM. IT IS ACCEPTABLE FOR RETURNED SERVICE WITH NOTED CONDITION. (M)

Part: WIRE — BROKEN (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SIGN AT G5 WALL NEEDS REPAIR. REPAIRED EMERGENCY EXIT SIGN WALL WIRING. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: FAN — FAILED (ACM BAY)

YUL - FLT 80 - 3 HOURS INTO FLT STRONG ELECTRICAL BURNING ODOR IN CABIN ALONG WITH LEFT RECIRC FAN INOP MESSAGE ILLUMINATED ON EICAS. DIVERTED AND LANDED YUL WITHOUT INCIDENT. REPLACED LEFT RECIRCULATION FAN. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: OVEN — DIRTY (GALLEY)

LHR - FLT 136 - DURING FLIGHT FIRST CLASS OVEN SMOKES. CLEANED DEBRIS FROM FIRST CLASS OVEN. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: CONNECTOR — FAILED (SEAT 28H)

DFW - DURING OVERNIGHT MAINTENANCE, SEAT 28H EMERGENCY EXIT FLOOR PATH LIGHT WAS INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — BROKEN (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE EMERGENCY, EXIT LIGHT ASSEMBLY BY FS3 LAVATORY BROKEN. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY BY FS3 LAVATORY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: OVEN — DEFECTIVE (CABIN)

LHR - FLT 46 - EN ROUTE NR 2 FIRST CLASS OVEN SMOKING. TURNED OVEN OFF AND SMOKE DISSIPATED. LANDED LHR WITHOUT INCIDENT. PULLED CIRCUIT BREAKERS AND BANDED AND DEFERRED PER PD. ORD REPLACED FIRST CLASS OVEN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — FAILED (ROW 32H)

EZE - DURING MAINTENANCE CHECK, EMERGENCY EXIT PATH LIGHTS FROM PASSENGER SEAT ROW 32H AFT INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH CONNECTOR AT SEAT ROW 36H. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: CONNECTOR — LOOSE (ROW 19 A/B)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR LIGHTS AT PASSENGER SEAT ROW 19 A/B INOPERATIVE. RECONNECTED LOOSE EMERGENCY EXIT LIGHT CONNECTOR AT PASSENGER SEAT ROW 19 A/B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FLOORBEAM — CORRODED (BS 1480)

AFW - FLOORBEAM AT STATION 1480 HAS CORROSION REMOVAL ON UPPER SURFACE AS SHOWN ON SKETCHES. FABRICATED STRAP FROM 301.5 HARD STAINLESS STEEL .050 INCH THICK APPLIED TWO COATS OF BMS-10-11 PRIMER TO THE STRAP AND FLOORBEAM. FILLED BLENDED AREA WITH BMS5-92. INSTALLED STRAP WET WITH BMS5-95 SEALANT PROSEAL OF 70 USING BAC B30NW6 HI-LOCKS. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

AFW - FLOORBEAM AT RBL 33 HAS CORROSION REMOVAL ON UPPER SURFACE AS SHOWN ON SKETCH. BLEND OUT ALL CORROSION. DYE PENETRANT INSPECT AND ROTO-PEEN REPAIRS AREA. ALODINE ALL BARE SURFACES. FINISH WITH 2 COATS OF BMS-10-11 PRIMER. FILL BLEND WITH BMS5-95. (M)

Part: SWITCH — SHORTED (L4 DOOR)

LAX - DURING OVERNIGHT CHECK, CABIN EMERGENCY LIGHTS WOULD NOT ILLUMINATE. REPLACED SHORTED EMERGENCY LIGHT SWITCH AT L4 DOOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: BUS — MALFUNCTIONED (RIGHT)

RIGHT BUS TRIPPED OFF DURING FLIGHT, FOLLOWED PROCEDURES STILL HAVE RIGHT BUS ISOLATION LIGHT WITH ASSOCIATED EICAS AND STATUS MESSAGES. ACCOMPLISHED BPCU BITE AND BITE DISPLAYED DELTA P TRIP AND OVERLAP ZONE FOR RIGHT GEN SYSTEM ON LAST FLT STATUS. RESET SUCCESSFUL. RUN UP BOTH ENGINES AND BITE DISPLAYED NO FURTHER FAULTS. (M)

Part: LIGHTS — MALFUNCTIONED (CABIN)

MIA - FLT 0063 - EN ROUTE ORY/MIA DURING CRUISE, EMERGENCY EXIT LIGHTS INTERMITTENTLY ILLUMINATED. NO OTHER ABNORMAL INDICATIONS AND AIRCRAFT PROCEEDED TO MIA LANDING WITHOUT INCIDENT. ACCOMPLISHED GROUND CHECK OF EMERGENCY EXIT LIGHTS WITH NO DEFECTS FOUND. UNABLE TO DUPLICATE PROBLEM. SYSTEM GROUND CHECKED, NORMAL OPERATION AND AIRCRAFT RETURNED TO SERVICE. (X)

Part: CONNECTOR — NEED SECURING (CABIN)

SFO - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT 20B INOPERATIVE. RECONNECTED LOOSE CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL — DEFECTIVE (GALLEY)

SFO - EMERGENCY EXIT LIGHT BY FIRST CLASS GALLEY UNDER CENTER FLIGHT ATTENDANT SEAT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BY FIRST CLASS GALLEY UNDER CENTER FLIGHT ATTENDANT SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. (W)

Part: EEL CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 7H AND 21H INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR BY PAX SEAT ROW 7H. SYSTEM GROUND CHECKED NORMAL OPERATION. (W)