N11194

Part: LIGHT — INOPERATIVE · airframe 37,519 hrs · 24,664 cycles

LH WING INSPECTION LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT. OPS CHECK SAT

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 36,987 hrs · 24,183 cycles

EMERGENCY LIGHT INOP AT SEAT 18A. R&R INVERTER ASSY #2 WITH #3. OPS CHECK SAT, RETURNED TO ORIGINAL POSITIONS. FOUND INVERTER ASSY NOT TO BE AT FAULT. FOUND EMERGENCY BATTERY PACK #3 TO BE AT FAULT. R&R EMERGENCY BATTERY #3. OPS CHECK SAT. NO FURTHER DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,882 hrs · 24,086 cycles

SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. R&R SERVICE DOOR EMERGENCY LIGHT. OPS CHECK SAT.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 36,681 hrs · 23,909 cycles

OVERWING EXIT EMERGENCY LIGHT IN CABIN INOPERATIVE. R&R #2 EMERGENCY LIGHT BATTERY POWER SUPPLY. OPS CHECK SAT.

Part: SEAT FRAME — CRACKED (SEAT 19A) · airframe 36,314 hrs · 23,598 cycles

SEAT S 2A, 3A, 5A, 7A, 10A, 19A, 20A, 21A, AND 23A HAVE A CRACK IN THE RADIUS BELOW THE AISLE SIDE ARMREST. R&R PASSENGER SEAT 2A, 23A, 21A, 20A, 19A, 5A, 7A & 10A.

Part: MOUNT — CORRODED (RADAR ALTIMITER) · corrosion level 2 · airframe 36,001 hrs · 23,320 cycles

CORROSION ON RAD ALT 2 ANTENNA MOUNTING PLATES AND SKIN. BOTH FWD AND AFT RAD ALT 2 ANTENNA MOUNTING PLATES REMOVED. REMOVED FWD AND AFT RAD ALT 2 MOUNTING PLATES. REMOVED SERVICE CORROSION. CUT OUT DAMAGED AREA. MEASURED SKIN THICKNESS THAT WAS BLENDED USING MICROMETER. FOUND MINIMUM THICKNESS TO BE 0.062". PERFORMED EDDY CURRENT INSPECTION. CUT THICKNESS TEST PERFORMED ON BLENDED AREAS AT FWD AND AFT ANTENNA BY AVTECH TESTING. FOUND NO LOSS OF THICKNESS GREATER THAN 10%. FAB FILLER FROM 2024T3 .063" AND DOUBLER FROM 2024T3 .080" DRILLED, COUNTERSUNK, ALODINED AND SURFACE PRIMED. INSTALLED PERMANENT REPAIR ON NR 2 RA AFT ANTENNA BASE. REPLACED NR 2 RA FWD ANTENNA BASE. ALODINED PRIME AND APPLIED EXT COATING. INSTALLED NEW FWD NR 2 RA ANTENNA. INSTALLED AFT NR 2 RA ANTENNA. OPERATIONS AND LEAK CHECK SATISFACTORY. CORROSION LEVEL II.

Part: PLATE — CORRODED (RADI RAD ANTENNA) · corrosion level 2 · airframe 36,001 hrs · 23,320 cycles

CORROSION ON RAD ALT 2 ANTENNA MOUNTING PLATED AND SKIN. BOTH FWD AND AFT RAD ALT 2 ANTENNA MOUNTING PLATED REMOVED. REMOVED FWD AND AFT RAD ALT 2 MOUNTING PLATES. REMOVED SERVICE CORROSION. CUT OUT DAMAGED AREA. MEASURED SKIN THICKNESS THAT WAS BLENDED USING MICROMETER. FOUND MINIMUM THICKNESS TO BE 0.062". PERFORMED EDDY CURRENT INSPECTION. NO DEFECTS NOTED. UT THICKNESS TEST PERFORMED ON BLENDED AREAS AT FWD AND AFT RAD ALT ANTENNAE. FOUND NO LOSS OF THICKNESS GREATER THAN 10%. FAB FILLER FROM 2024T3 .063" AND DOUBLER FROM 2024T3 .080" DRILLED, COUNTERSUNK, ALODINED AND SURFACE PRIMED. INSTALLED PERMANENT REPAIR ON NR 2 R/A AFT ANTENNA BASE. OPERATIONS AND LEAK CHECK SATISFACTORY.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,950 hrs · 23,268 cycles

ALL EMERGENCY LIGHTS ARE INOPERATIVE. COCKPIT SWITCH WAS IN THE ARMED POSITION. R&R ALL BATTERY POWER SUPPLY. OPERATIONS CHECK SATISFACTORY.

Part: SKIN — CRACKED (LT WING LE) · airframe 35,948 hrs · 23,265 cycles

FOUND CRACK ON LT WING LEADING EDGE #3 SKIN AT OUTBOARD VORTILLON MOUNTING POINT. FOUND CRACK TO BE APPROXIMATELY HALF AN INCH IN LEGNTH ON THE FWD SIDE OF THE VENT HOLE AND FOUND AN ADDITIONAL CRACK ON THE AFT SIDE OF THE VENT HOLE AND FOUND AN ADDITIONAL CRACK ON THE AFT SIDE OF THE VENT HOLE TO BE APPROXIMATELY .20". REMOVED THE REST OF THE VORTILLONS ON LT LEADING EDGE #3. FOUND CRACKS ON #2 AND #3 VORTILLON MOUNTING POINTS. #2 VORILLON MOUNTING POINT HAS A CRACK FWD OF THE VENT HOLE THAT APPROXIMATELY .5" IN LENGTH AND AFT OF THE VENT HOLE APPROXIMATELY .10". VORTILLON #3 MOUNTING POINT HAS A CRACK FWD OF THE VENT HOLE THAT IS APPROXIMATELY .5" AND 2 CRACKS AFT OF THE VENT HOLE, ONE BEING .10" AND THE OTHER .05". R&R LT WING LEADING EDGE. OPERATIONS CHECK SATISFACTORY. NO DEFECTS NOTED.

Part: SKIN — CRACKED (VORTILON) · airframe 35,948 hrs · 23,265 cycles

SUSPECTED CRACKS ON RT LEADING EDGE #3 VORTILLON MOUNTING POINTS. REMOVED ALL RT LEADING EDGE #3 VORTILLONS. PERFORMED INSPECTION OF VORTILLON MOUNTING POINTS. FOUND CRACKS AND DAMAGE AT VORTILLON MOUNTING POINTS 6, 7, AND 8. #6 VORTILLON MOUNTING POINT HAS A CRACK AFT OF THE VENT HOLE APPROX .40 INCHES IN LENGTH, A CUT IN THE METAL APROX .10" AFT OF THE VENT HOLE, A CRACK COMING OFF OF THE CUT APPROXIMATELY .15" AND A GOUGE THAT TAKES THE SHAPE OF THE VENT HOLE CIRCUMFERENCE. #7 VORTILLON MOUNTING POINT HAS A CRACK FWD OF THE VENT HOLE APPROXIMATELY .60" AND A CUT AFT OF THE VENT HOLE. #8 VORTILLON MOUNTING POINT HAS A CRACK APPROXIMATELY .50" FWD OF THE VENT HOLE AND A GOUGE AFT OF THE VENT HOLE THAT TAKES THE SHAPE OF THE CIRCUMFERENCE OF THE VENT HOLE.

Part: RELAY — FAILED (MLG) · airframe 35,433 hrs · 22,820 cycles

LANDING GEAR AIR/GROUND SYSTEM FAILURE IN FLIGHT. PERFORMED LANDING GEAR WOW PROXIMITY SWITCHES OPS CHECK. R&R RELAY K0278. NO DEFECTS NOTED AT THIS TIME. PERFORMED GEAR SWINGS. OPS CHECK SAT.

Part: SKIN — CANNING (FRAMES 19-20) · airframe 34,690 hrs · 22,156 cycles

OIL CANNING PREVIOUS REPAIR ON SKIN AT FR 19 - FR 20, STR 10L-12L, JUST AFT OF PAX DOOR. REPAIRED OIL CANNING PREVIOUS REPAIR ON SKIN AT FR19-FR20, STR 10L-12L

Part: SKIN — DAMAGED (RUDDER) · airframe 34,690 hrs · 22,156 cycles

RUDDER 1 LEFT HAND SKIN AFT NUT PLATE ATTACHED HOLES ELONGATED. INSTALLED REPAIR DOUBLER, FILLER AND NUT PLATE FOR RUDDER 1 LEFT HAND SKIN AFT NUT PLATE.

Part: ACM — NOISY (AC BAY) · airframe 34,290 hrs · 21,780 cycles

HIGH PITCH NOISE FROM EMERGENCY EXIT ROW. FOUND PACK NR 1 AFTER RUNNING IT FOR 10 MINUTES. R&R NR 1 ACM. OPS CHECK AND LEAKED CHECK SAT AT THIS TIME.

Part: CRADLE — INOPERATIVE (BATTERY PACK) · airframe 33,779 hrs · 21,349 cycles

RH EXTERNAL FWD EMERGENCY LIGHT OUT. REMOVED AND REPLACED #2 EMERGENCY LIGHT BATTERY CRADLE. OPS CHECK SAT.

Part: PROXIMITY SWITCH — MALFUNCTIONED (NLG) · airframe 32,367 hrs · 19,995 cycles

MULTIPLE EICAS FAIL MESSAGES DURING FLIGHT. R & R THE NOSE LANDING GEAR PROXIMITY SWITCH, OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,788 hrs · 19,411 cycles

GALLEY EMERGENCY LIGHT INOPERATIVE. R & R THE BULBS IAW AMM 33-29-03. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,788 hrs · 19,411 cycles

EMERGENCY LIGHT AT ROW 18 CD INOPERATIVE. REMOVED AND REPLACED THE BULBS AND PERFORMED AN OPS CHECK IAW AMM 33-50-00. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,729 hrs · 19,358 cycles

EMERGENCY LIGHT OVER AT 18A INOP. RR LIGHT BULB, OPS CHECK SAT.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,663 hrs · 19,280 cycles

EMERGENCY LIGHT AT THE CABIN DOOR INOPERATIVE. REPLACED THE LAMPS. OPS CHECKED CHECKED GOOD.

Part: BUTTON — STUCK (INTERPHONE) · airframe 31,445 hrs · 19,064 cycles

CABIN INTERPHONE AND CABIN EMERGENCY ON PANEL ILLUMINATED. FOUND FA FORWARD BACK UP BUTTON STICKING. RELEASED THE BUTTON, OPS CHECK OF INTERPHONE SYS.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 30,888 hrs · 18,561 cycles

ALL EMERGENCY LIGHT BATTERIES DRAINED. R & R THE BATTERY PACKS. CHECK SATISFACTORY, NO DEFECTS NOTED.

Part: SKIN — CRACKED (FRAME 78) · airframe 30,103 hrs · 18,009 cycles

DURING A C-CHECK, THE FUSELAGE SKIN WAS CRACKED AT FRAME 78 STRINGERS 4 - 5R. REPAIRED THE SKIN IAW SRM 53-32-01. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FRAME 78) · airframe 30,103 hrs · 18,009 cycles

DURING A C-CHECK, THE FUSELAGE SKIN WAS FOUND CRACKED AT FRAME 78 STRINGERS 4 - 5L. REPAIRED THE SKIN IAW SRM 53-32-01. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CRACKED (FRAMES 59) · airframe 30,103 hrs · 18,009 cycles

DURING A C CHECK. RT OMEGA BEAM CRACKED AT FRAME 59. REPAIRED THE OMEGA BEAM IAW SRM 53-24-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DENTED (FRAMES 19-20) · airframe 29,417 hrs · 17,505 cycles

DURING GROUND INSPECTION, A DENT WAS IDENTIFIED AFT OF THE PASSENGER DOOR BETWEEN FRAMES 19-20 AND STR 14-15 LT. MAINTENANCE REMOVED THE DAMAGE AND PERFORMED A FILLER/DOUBLER REPAIR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE ON 05/03/16.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 28,326 hrs · 16,712 cycles

DURING ROUTINE MAINTENANCE THE AFT GALLEY WALL EXIT IDENTIFIER WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 2 EMERGENCY LIGHT INVERTER. OPS CHECKS WERE GOOD.

Part: STRUCTURE — DAMAGED (TE FLAP) · airframe 24,187 hrs · 13,905 cycles

FLAP FAILED AT 8 DEGREES DURING TAKEOFF. MAINTENANCE COMPLIED WITH GVI OF FLAPS AND SURROUNDING AREA OF DAMAGE. MAINTENANCE R & R RT INBD FLAP IAW AMM 27-50-00, ZERO RIG AND OPS CHECKED GOOD. APPROVED FOR RETURN TO SERVICE.

Part: CONTROL MODULE — FAILED (CABIN LIGHTS) · airframe 23,994 hrs · 13,784 cycles

THE CREW REPORTED F/A AND PASSENGER SMELLED SMOKE IN THE FRONT OF CABIN. MAINTENANCE INSPECTED AND REPLACED THE CABIN LIGHT CONTROL MODULE. OPS CHECKS WERE GOOD.

Part: LIGHT — FAILED (CABIN) · airframe 23,981 hrs · 13,774 cycles

SMOKE WAS REPORTED COMING OUT OF CABIN SIDEWALL LIGHTS AT ROW 5BC. MX R & R THE SIDEWALL LIGHT ASSEMBLY AND OPS CHECKED GOOD. ACFT APPROVED FOR RETURN TO SERVICE.

Part: WIRE HARNESS — DAMAGED (CABIN LIGHTS) · airframe 22,674 hrs · 12,943 cycles

DURING MX ROW 4/5 CABIN LIGHT HARNESS WAS FOUND BURNED. THE LIGHT HARNESS AT ROW 4/5 WAS REPLACED AND OPS CHECKS WERE GOOD.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 18,622 hrs · 10,282 cycles

OMEGA BEAM SUPPORT AT FRAME 46 TO 48 CRACKED. R & R SUPPORT.

Part: SILL — CORRODED (CABIN) · corrosion level 2 · airframe 18,622 hrs · 10,282 cycles

CABIN FLOOR L ANGLE AT FRAME 23 RT CORROSION AT NUT PLATE MARKET IN RED. FABRICATED AND INSTALLED NEW ANGLE.

Part: THRESHOLD — CORRODED (PAX DOORWAY) · airframe 18,622 hrs · 10,282 cycles

THRESHOLD AT PAX DOOR HAS CORROSION AROUND NUT PLATES. BLENDED CORROSION, WITHIN LIMITS.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,622 hrs · 10,282 cycles

LEFT SILL FROM FRAME 23 TO 29 CORROSION AS MARKED. R & R SILL.

Part: SILL — CORRODED (FUSELAGE) · airframe 18,622 hrs · 10,282 cycles

CORROSION ON RT FLOOR SILL AT FR 61. BLENDED CORROSION, FOUND TO BE WITHIN LIMITS TREATED, PRIMED AND PAINTED.

Part: PRESSURE SWITCH — INOPERATIVE (A/C PACK) · airframe 17,920 hrs · 9,819 cycles

A/C PACK 1 OVERLOADED. R & R NR 1 PACK OVERPRESSURE SWITCH. OPS CHECKED GOOD. ACFT RELEASED AND RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 14,682 hrs · 7,860 cycles

THE CREW REPORTED WITH THE ANTI-ICE SYSTEM ON HAD A ELECTRICAL SMELL. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS OF THE ANTI-ICE SYSTEM. NO DEFECTS WERE FOUND AND NO SMELLS WERE NOTICED.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE) · airframe 14,679 hrs · 7,859 cycles

FLIGHT 3008 - IAD - FLIGHT CREW REPORTED AUTO PRESS FAIL IN FLIGHT. MX REMOVED AND REPLACED DIGITAL PRESS CONTROLLER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: UNKNOWN — SMOKE (GALLEY) · airframe 8,898 hrs · 4,672 cycles

FLIGHT 2756 - EWR - FLIGHT ATTENDANT AND PASSENGER IN SEAT 2A REPORTED WHAT THEY THOUGHT WAS SMOKE COMING FROM AFT TRASH BIN IN GALLEY. FLIGHT ATTENDANT DISCHARGED HALOGEN FIRE EXTINGUISHER INTO BIN AND PASSENGERS WERE EVACUATED. EWR MX INSPECTED THE AREA NO SIGNS OF BURNING OR SMOKE FOUND. MX REMOVED AND REPLACED FIRE EXTINGUISHER. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SKIN — CORRODED (CARGO DOOR)

DURING C-CHECK, CARGO DOOR INNER SKIN HAS CORROSION AROUND NUT PLATE HOLES. MX REPAIRED CORRODED AREAS ON CARGO DOOR INNER SKIN NUT PLATE HOLES IAW EC523001193. THE ACFT WAS APPROVED TO RETURN FOR SERVICE. (K)

Part: PRESSURE SWITCH — INOPERATIVE (RUDDER)

FLT 0002 -OKC- FLIGHT CREW REPORTED RUDDER 2 SYSTEM INOP ON APPROACH AND DECLARED EMERGENCY AND IT LANDED SAFELY WITHOUT INCIDENT. MAINTENANCE RESET RUDDER SYSTEM 2 AND RELEASED THE ACFT ON A FERRY FLIGHT TO AUS. REMOVED AND REPLACED BOTH PRESSURE SWITCHES. OPERATIONALLY CHECKED SATISFACTORY AND ACFT WAS RELEASED TO RETURN FOR SERVICE. (S)

Part: RELAY — FAILED (SMOKE DETECTOR) · airframe 6,020 hrs · 3,201 cycles

FLT 524 - MCI TO RDU - WHILE FLIGHT CREW WAS PERFORMING PRE-FLIGHT WALK AROUND AND SYS CHECKS, ENCOUNTER THAT THE BAGGAGE SMOKE DETECTOR TEST FAIL. MX PERSONNEL REMOVED AND REPLACED RELAY K0630 AND OPERATIONALLY CHECKED SATISFACTORY AND AIRCRAFT WAS RELEASE TO RETURN FOR SERVICE IN AIRWORTHY CONDITIONS.

Part: COFFEEMAKER — SMOKE (GALLEY) · airframe 5,751 hrs · 3,062 cycles

FLT 216 - SAT TO SMF - CREW REPORTED RIGHT COFFEE POT WAS SMOKING A/C WAS RELEASED ON MEL 25-60-02/03 CAT D CONTROL 132221. A/C ARRIVED TO ONT FOR SVC/RTN CHECKS AND OVERNIGHT INSPECTION. MX BREWED COFFEE SEVERAL TIMES AND NO SMOKE WAS NOTED AT ANY TIME, OPERATIONALLY CHECKED SATISFACTORY AND A/C WAS RELEASED TO RETURN FOR SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 983 hrs · 506 cycles

TYS - THE RT REAR FUSELAGE WAS FOUND DENTED AT FRAME 67 AND MAINTENANCE REPAIRED THE DAMAGE AREA WITH A FILLER AND A EXTERNAL DOUBLER IAW EMB IC2006/2190. ALL WORK WAS ACCOMPLISHED AND A/C WAS RELEASED BACK TO SERVICE.