N14125

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 49,227 hrs · 32,030 cycles

EMERGENCY LIGHT #2 BPS INOPERATIVE. REMOVED AND REPLACED #2 BPS. OPS CHECK GOOD.

Part: SIGN — INOPERATIVE (ZONE 200) · airframe 48,480 hrs · 31,497 cycles

EXIT ROW OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT SIGN. NO DEFECTS NOTED.

Part: SKIN — DAMAGED (ZONE 200) · airframe 48,295 hrs · 31,232 cycles

DAMAGE TO RIGHT SIDE OF NOSE AT FRAME 7, BETWEEN STRINGER 6R AND 9R. FOUND DENT LOCATED AT FRAME 7 BETWEEN STRINGER 6R AND 9R. FOUND SKIN CREASES BETWEEN FRAME 6 AND 7 AND STRINGERS 6R AND 9R. NO INTERNAL DAMAGE IS NOTED. NO RIVETS FOUND POPPED. CUT OUT FILLER AREA AT REPAIR AREA FR7 BTW STR 6R-9R. FABRICATED REPAIR DOUBLER 2024T3 .050 AND FILLER SAME AS ORIGINAL THICKNESS .032 2024T3 FOR FR 7 BTW STR 6-9R INSTALLED. COMPLIED WITH INSPECTION OF INSTALLATION OF REPAIR DOUBLER. NO DEFECTS NOTED AT THIS TIME.

Part: LIGHT — MISINSTALLED (ZONE 200) · airframe 48,052 hrs · 30,900 cycles

FLOOR EMERGENCY EXIT STRIP BACKWARDS AT 1A. REINSTALLED EMERGENCY STRIP CORRECTLY.

Part: DUCT — UNSECURE · airframe 47,976 hrs · 30,825 cycles

ON DEPARTURE SMOKE COMING OUT OF VENT AT SEAT 7A. SMOKE FOUND TO BE CONDENSATION/VAPOR FROM PACKS SYSTEM. INSPECTED WATER SPRAY NOZZLES. NO DEFECTS NOTED. UPON FURTHER INSPECTION FOUND RECIRC FAN DUCT AT 7A UNSECURED. RESECURED RECIRC FAN DUCT. OPS CHECK SAT. NO LEAKS/VAPOR DETECTED.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 47,875 hrs · 30,724 cycles

RH SIDE CENTER FAIRING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED RH SIDE CENTER FAIRING EMERGENCY LIGHT. OPS CHECK SAT.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 47,580 hrs · 30,422 cycles

MULTIPLE EMERGENCY LIGHTS/EXIT SIGNS ARE INOPERATIVE. REMOVED AND REPLACED BATTERY POWER SUPPLY. OPS CHECK SAT.

Part: INVERTER — INOPERATIVE (ZONE 200) · airframe 47,375 hrs · 30,208 cycles

AFT OVERHEAD EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED AFT OVERHEAD EMERGENCY EXIT SIGN. OPS CHECK FAILED. REMOVED AND REPLACED #4 EMERGENCY LIGHT DC/AC INVERTER. OPS CHECK SAT.

Part: LAMP — INOPERATIVE · airframe 47,208 hrs · 30,063 cycles

RH EXTERNAL OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED RH OVERWING EMERGENCY BULB. OPS CHECK SAT

Part: UNKNOWN — UNKNOWN · airframe 47,045 hrs · 29,917 cycles

LIGHTNING STRIKE DURING DECENT THROUGH 8,000. PERFORMED LIGHTNING STRIKE INSPECTION. ALL 5 DISPLAY UNITS MAGNETIZED DUE TO LIGHTNING STRIKE. REMOVED AND REPLACED ALL 5 DISPLAY UNITS. NO FURTHER DEFECTS. FO WINDSHIELD SHOWS SIGNS OF STRIKE. REMOVED AND REPLACED FO'S WINDSHIELD. OPS AND LEAK CHECK SAT. STATIC WICK ON TOP OF RUDDER MISSING. REMOVED AND REPLACED TAIL BOOM ASSEMBLY.

Part: LAMP — INOPERATIVE · airframe 47,013 hrs · 29,887 cycles

COCKPIT CEILING EMERGENCY LIGHT OUT. REMOVED AND REPLACED COCKPIT CEILING EMERGENCY LIGHT. OPS CHECK SAT.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,740 hrs · 29,643 cycles

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

Part: LAMP — INOPERATIVE · airframe 45,399 hrs · 28,445 cycles

INOPERATIVE AISLE EMERGENCY LIGHT LAMP LOCATED AT WING EMERGENCY EXIT. REMOVED AND REPLACED AISLE EMERGENCY LIGHT LAMP LOCATED AT WING EMERGENCY EXIT. OPS CHECK PASS.

Part: NONE — NONE · airframe 45,202 hrs · 28,262 cycles

LARGE EXIT SIGN NEXT TO RH EMERGENCY EXIT DOOR DOES NOT ILLUMINATE. R&R EXIT MARKING SIGN ASSEMBLY. OPS CHECK SAT

Part: RIB — CRACKED (FUSELAGE) · airframe 45,007 hrs · 28,070 cycles

FF2, LH FUSE OVER WINDSHIELD, RIB OVER HEAD PANEL HORIZONTAL CRACKED AT ANCHOR NUT LOCATION. PANEL REPAIRED

Part: DOUBLER — CORRODED (FRMS 68-69) · airframe 45,007 hrs · 28,070 cycles

CORROSION ON LOWER REAR FUSE 1, ON ANTENNA DOUBLER FOR AFT RADIO ALTIMETER #2 BTW FR 68-69. SKIN REPAIRED.

Part: DOUBLER — CORRODED (FRMS 56-65) · airframe 45,007 hrs · 28,070 cycles

CORROSION ON LOWER REAR FUSE 1, ON ANTENNA DOUBLER FOR FWD RADIO ALTIMETER #2 BTW FR 65-56. SKIN REPAIRED.

Part: FLOOR SUPPORT — CORRODED (FRMS 46-53) · airframe 45,007 hrs · 28,070 cycles

ON CF3:CENTER OMEGA BEAM BTW FR46-53 LOWER FLANGE CORRODED. CF3, CENTER BEAM BLENDED OUT OF LIMITS BTW FR 47 & 48. PERFORMED CUT OUT BTW FR 47 & 48. CF3 CENTER BEAM REPAIRED WITH REPAIR DOUBLER ANGLE

Part: FRAME — CRACKED (FRM 59 S16-17L) · airframe 45,007 hrs · 28,070 cycles

FR 59 BTW STR 16-17 FOUND CRACKED. CRACKED SECTION OF FRAME 59, BTW STR 16-17. REMOVED FOR REPAIR. REPAIR PARTS FOR CRACKED FR 59, BTW STR 16-17 LOCALLY FABRICATED. FR 59, BTW STR 16-17 REPAIRED (SPLICED BTW STR 17-18).

Part: SKIN — DENTED (FRMS 11-12) · airframe 45,007 hrs · 28,070 cycles

DENT WITH RIVET PLUGS ON R/H LOWER FWD FUSE 2, BTW FR 11-12 AND BTW STR 20R-21R. PERFORMED CUT-OUT ON R/H LOWER FWD FUSE 2, BTW FR 11-12 AND BTW STR 20R-21R. PREDRILLED DOUBLER RIVETS LAYOUT IN SKIN ON R/H LOWER FWD FUSE 2, BTW FR 11-12 AND BTW STR 20R-21R. FABRICATED REPAIR DOUBLER & REPAIR FILLER. LOCATED AND DRILLED TO FINAL SIZE REPAIR DOUBLER & REPAIR FILLER. INSTALLED REPAIR DOUBLER & REPAIR FILLER ON R/H LOWER FWD FUSE 2, BTW FR 11-12 AND BTW STR 20R-21R. REPAIRED SKIN ON R/H LOWER FWD FUSE 2, BTW FR 11-12 AND BTW STR 20R-21R

Part: YOKE — CRACKED (PYLON) · airframe 45,007 hrs · 28,070 cycles

FOLLOWING NDT INSPECTION ON TASK 54-50-00-255-803-A00, 2X CRACKS FOUND ON PYLON YOKES UPPER FLANGE 2X HOLES LOCATIONS. OPEN L/H AND R/H PYLON YOKES UPPER FLANGE 1ST OVER SIZE. AFTER NDT INSPECTION (STILL CRACKED) OPEN HOLES 2ND OVER SIZE NO CRACK INDICATION FOUND ON BOTH PYLON REWORK HOLES. (4X) BUSHINGS LOCALLY FABRICATED (MADE REPAIR PARTS) (2X FLUSH PYLON + 2X PYLON BUSHINGS). INSTALLED L/H AND R/H PYLON YOKES UPPER FLANGE BUSHINGS AND NEW FASTENERS.

Part: FLOOR SUPPORT — CORRODED (FRMS 18-20) · airframe 45,007 hrs · 28,070 cycles

CF1, R/H, BEAM HAT SECTION, BTW FRAMES 18-20, FOUND CORRODED. ON CF1, R/H, BEAM HAT SECTION, BTW FR18-20 BLENDED AND FOUND OUT OF LIMIT. ON CF1, R/H, BEAM HAT SECTION, BTW FR18-20 REPAIRED

Part: SHEAR TIE — CRACKED (FRM 71 S6-10L) · airframe 45,007 hrs · 28,070 cycles

RF1, AT FR 71 BTW STR 6L-10L, SHEAR CLIP CRACKED. SHEAR CLIP FR 71 BTW STR 6L-10L WAS REMOVED. RF 1, AT FR 71 BTW STR 6L-10L, NEW SHEAR CLIP LOCALLY FABRICATED. REPLACED SHEAR CLIP AT FR 71 BTW STR 6L-10L WITH NEW LOCALLY FABRICATED SHEAR CLIP

Part: FRAME — CORRODED (FRM 65) · airframe 45,007 hrs · 28,070 cycles

RF1, AT FR 65, FRAME UPPER Z SECTION CORRODED AT ANCHOR NUT LOCATIONS RF1, FR65 ON FRAME UPPER Z AT ANCHOR NUT LOCATION, FRAME BLENDED OUT OF LIMIT. RF1, FR65 REPAIRED

Part: ARMREST — CRACKED (SEAT 23A) · airframe 44,676 hrs · 27,756 cycles

SEAT 23A, 20A, 10A, 9A, 8A, 5A, 4A, 3A ARMREST STRUCTURE IS CRACKED. R&R SEAT ASSEMBLY AT 23A, 20A, 10A, 9A, 8A, 5A, 4A, 3A

Part: SEAL — DETERIORATED (COCKPIT WINDOW) · airframe 44,653 hrs · 27,732 cycles

DECLARED EMERGENCY, DUE TO LOUD NOISE FROM DV WINDOW CAPT SIDE. UPON RETURN TO HRL DETECTED DV WINDOW SEAL ON CAPT SIDE COMING APART. R&R CAPT SIDE DV WINDOW SEAL. PERFORMED WATER PENETRATION AND PRESSURIZATION. LEAK AND PRESSURIZATION OPS CHECK SAT.

Part: LIGHT — UNSECURE (CABIN) · airframe 44,490 hrs · 27,585 cycles

PHOTO LUMINESCENT STRIP DOES NOT ILLUMINATE PROPERLY (HAS BREAKS). RE SECURED PHOTO LUMINESCENT STRIP.

Part: SKIN — CRACKED (AFT FUSELAGE) · airframe 44,409 hrs · 27,514 cycles

CRACK ON LOWER REAR FUSE 1, BETWEEN FR 75-75A AND BETWEEN STR 21L-21R. ON LOWER REAR FUSE 1, BETWEEN FR 75-75A BETWEEN STR 21L-21R, PAINT STRIPPED FOR INVESTIGATION. ON LOWER FUSE 1, BETWEEN FR 75-75A BETWEEN STR 21L-21R, CUT-OUT PERFORMED FOR ENGINE REVIEW. CRACK ON LOWER REAR FUSE 1, BETWEEN FR 75-75A AND BETWEEN STR 21L-21R REPAIRED.

Part: SKIN — DENTED (FRAMES 3-4) · airframe 44,409 hrs · 27,514 cycles

DENT ON FWD FUSE 1 BETWEEN FRAMES 3-4 STR 9-11R. DOUBLER AND FILLER FABRICATED, LOCATED AND DRILLED. DENT ON FWD FUSE BETWEEN FR 3-4 STR 9-11R, REPAIRED.

Part: SKIN — CANNING (FRAMES 20-21) · airframe 44,409 hrs · 27,514 cycles

DENT WITH OIL CANNING EFFECT ON LT CENTER FUSE 1, BETWEEN FR 20-21 AND BETWEEN STR 13P-14P. DENT WITH OIL CANNING AT LT CENTER FUSE 1, BETWEEN FR 20-21, AND BETWEEN STR 13P-14P REPAIRED.

Part: SKIN — CANNING (FRAMES 22-23) · airframe 44,409 hrs · 27,514 cycles

DENT WITH OIL CANNING EFFECT ON LT CENTER FUSE 1, BETWEEN FR 22-23 AND BETWEEN STR 14P-15P. DENT WITH OIL CANNING AT LT CENTER FUSE 1, BETWEEN FR 22-23 AND BETWEEN STR 14P-15P REPAIRED.

Part: FILTER — DIRTY (BLEED AIR SYS) · airframe 44,356 hrs · 27,474 cycles

BLEED 1 OVERHEAT. INSPECTED & RAN BLLED 1 ADJUSTMENT AND TEST. NO FAULTS FOUND. CLEANED FAN AIR VALVE FILTER. OPS CHECK GOOD.

Part: WIRE HARNESS — SPARKS (SIDEWALL LIGHT) · airframe 43,381 hrs · 26,659 cycles

PAX AT 24CD NOTICED SPARKS AND FUMES COMING FROM OVERHEAD AREA NEAR SIDEWALL. R & R THE LIGHT ASSY HARNESS. OPS CHECKED GOOD .

Part: BATTERY — WEAK (CABIN) · airframe 42,914 hrs · 26,294 cycles

SERVICE DOOR EXIT IDENTIFIER (LIGHT #10) IS INOP. R&R #2 EMERGENCY BATTERY POWER SUPPLY. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,914 hrs · 26,294 cycles

RT FWD WING EMERGENCY FLOOD LIGHT (LIGHT # 4) IS INOP. R&R RT FWD WING EMERGENCY FLOOD LIGHT BULB. OPS CHECK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 42,440 hrs · 25,933 cycles

ON CLIMBOUT BAG DOOR OPEN & CABIN FAIL TO PRESSURIZE. CLOSED BAG DOOR & PERFORMED PRESSURIZATION. BAG DOOR INDICATION NORMAL. NO LEAKS NOTED.

Part: GUSSET — CORRODED (FRAME 59) · airframe 42,400 hrs · 25,906 cycles

CENTER GUSSET AT FRAMEV59 HAS SIGNS OF CORROSION. REMOVED AND RPLACED CENTER GUSSET AT FRAME 59

Part: FLOORBOARD — CORRODED (CABIN) · airframe 42,400 hrs · 25,906 cycles

R/H DIGITAL OF SERVICE DOOR AT FLOORBOARD 232DF HAS CORROSION AROUND SCREW HOLE .........REMOVED CORRODED SECTION FABRICATED DOUBLER INSTALLED DOUBLER ON R/N DIGITAL SILL AFT OF SERVICE DOOR

Part: FLOOR SUPPORT — CORRODED (FRAME 18) · airframe 42,400 hrs · 25,906 cycles

L/H OMEGA BEAM DIGITAL AT FRAME 18 AFT U CHANEL OF PAX DOOR HAS CORROSION. REMOVED AND REPLACED U CHANEL AFT OF PAX DOOR

Part: SUPPORT — CRACKED (CARGO BAY) · airframe 42,400 hrs · 25,906 cycles

CARGO BAY FWD RAMP ANGLE AND UPPER AND LOWER SUPPORTS ARE CRACKED ......REMOVED AND REPLACED CARGO BAY FWD RAMP ANGLE AND UPPER AND LOWER SUPPORTS

Part: ANGLE — CRACKED (CARGO BAY) · airframe 42,400 hrs · 25,906 cycles

CARGO BAY AFT RAMP ANGLE AND UPPER AND LOWER SUPPORTS ARE CRACKED...........REMOVED AND REPLACED CARGO BAY AFT RAMP ANGLE AND UPPER AND LOWER SUPPORTS

Part: ANGLE — CORRODED (DOOR FRAME) · airframe 42,400 hrs · 25,906 cycles

CARGO BAY DOOR CUT OUT Z ANGLE HAS CORROSION......REMOVE AND REPLACED CARGO BAY DOOR CUTOUT Z ANGLE

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 42,043 hrs · 25,634 cycles

SMOKE IN THE COCKPIT. PERFORMED FIM TASK 21-20-00. NO DEFECTS NOTED. NO SMOKE DETECTED DURING ENGINE RUNS.

Part: THERMOSTAT — FAILED (NR 1 BLEED) · airframe 41,985 hrs · 25,585 cycles

BLEED 1 OVERTEMP EICAS MSG ON CLIMBOUT. PERFORMED QRH CHECKLIST, MESSAGE CLEARED. R/R HIGH TEMP THERMOSTAT. PERFORMED OPS CHECK. OPS CHECK GOOD.

Part: ANTI-ICE SYSTEM — FAILED (NR 1 ENGINE) · airframe 41,293 hrs · 24,997 cycles

ENGINE NR 1 ANTI-ICE FAIL WHILE IN ICING CONDITIONS. DEFERRED E-1 ANTI-ICE VALVE. MORE INFORMATION WHEN AVAILABLE.

Part: GENERATOR — MALFUNCTIONED (NR 3) · airframe 40,804 hrs · 24,590 cycles

GEN 3 OFF BUSS EICAS MESSAGE. R&R NR 3 ENG GEN OPS CHECK GOOD AT THIS TIME.

Part: BOLT — LOOSE (CABIN DOOR)

POST FLIGHT, FOUND CABIN DOOR HARD TO OPEN. FOUND 2 EACH BOLTS LOOSE ON INTERIM HANDLE BRACKET. TIGHTENED BOLTS. OPS CHECK GOOD.

Part: UNKNOWN — UNKNOWN (ELEVATOR CABLES) · airframe 40,457 hrs · 24,334 cycles

ELEVATOR CONTROL CABLES FELT STIFF, LIKE THE CABLES WERE RUBBING. PERFORMED VISUAL INSPECTION OF ELEVATOR CONTROL CABLES. NO DISCREPANCIES NOTED. ISOLATED THE ELEVATOR SYSTEM. STARTED ENGINES AND DETERMINED THE ELEVATOR CONTROL COLUMNS VIBRATED WHEN THE RT ENGINE WAS AT IDLE. VIBRATION CEASED WHEN POWER ADVANCED. THE RT ENGINE VIBRATION LEVEL WAS WITHIN LIMITS ON EICAS. NO FURTHER ACTION REQUIRED. PERFORMED RIG PIN INSTALATION AND REMOVAL, AND A FREEDOM OF MOVEMENT CHECK. NO DISCREPANCIES NOTED.

Part: CLAMP — LOOSE (BLEED SYS) · airframe 40,066 hrs · 24,003 cycles

NR 1 BLEED LEAK DURING FLIGHT. BLEED LEAK CHECKED. FOUND MULTIPLE LEAKS IN PYLON. LOOSENED AND TIGHTENED ALL CLAMPS. LEAK TESTED GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION (CARGO DOOR) · airframe 38,819 hrs · 22,922 cycles

CARGO DOOR OPEN INDIDCATION DURING FLIGHT. PERFORMED OPS CHECK OF THE CARGO DOOR WARNING SYSTEM, OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,198 hrs · 22,401 cycles

LT AND RT OVERWING EMERGENCY LIGHTS NR 5 & 6, INOPERATIVE. R & R THE NR 4 EMERGENCY LIGHT BATTERY PACK. OPS CHECKED GOOD.

Part: SWITCH — FAILED (NR 2 MASTER)

ON ROTATION, LOST MFD1, PFD2, NR 2 FMS DISPLAY, AND NR 2 COMMS. AFTER RUNNING THE CHECKLIST, FOUND THE NR 2 AVIONICS MASTER SWITCH HAD TRIPPED. R & R THE NR 2 AVIONIC MASTER SWITCH. OPS CHECKED GOOD.

Part: ANTI-ICE VALVE — INOPERATIVE (NR 2) · airframe 37,150 hrs · 21,515 cycles

ANTI-ICE INOPERATIVE IN ICING CONDITIONS, FOLLOWED BY SPS/ICE SPEEDS. INSPECTED AND FOUND NR 2 ENG ANTI-ICE VALVE TO BE INTERNALLY DAMAGED NOT ALLOWING PROPER FLOW OF AIR INTO BLEED SYS. REMOVED AND REPLACED ANIT-ICE VALVE OPS CHECK GOOD.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 36,814 hrs · 21,240 cycles

ENGINE 2 REVISED FAIL EICAS MSG, NO THRUST ON ENGINE NR 2, IDLE POWER ONLY, SINGLE ENGINE APPROACH AND LANDING. DEFERRED IAW MEL 78-30-00 CAT C.

Part: DOOR SEAL — OUT OF ADJUST (CARGO DOOR) · airframe 36,754 hrs · 21,185 cycles

BAG DOOR OPEN INDICATION IN FLIGHT. CLEANED AND ADJUSTED DOOR VENT DOOR SEAL AND CLEANED MICROSWITCHES. OPS CHECK GOOD.

Part: WARNING LIGHT — ACTIVATED (CARGO DOOR) · airframe 36,548 hrs · 21,028 cycles

BAGGAGE DOOR OPEN INDICATION IN FLIGHT.

Part: SWITCH — INOPERATIVE (THRUST REVERSER) · airframe 36,461 hrs · 20,957 cycles

ENGINE 2 REVERSER FAIL ON EICAS. R & R THRUST REVERSER TRANSIT SWITCHES. OPS CHECK GOOD.

Part: FADEC — MALFUNCTIONED (ENGINE) · airframe 36,285 hrs · 20,815 cycles

ENGINE THRUST REVERSER FAIL EICAS MSG DURING CRUISE, EMERGENCY LANDING. R & R FADEC 2A. OPS CHECK GOOD.

Part: LAMP — BURNED (CABIN LIGHT) · airframe 35,991 hrs · 19,991 cycles

ACFT WAS CRUISING, WHEN A BURNING ODOR OCCURRED ABOVE SEAT 11A. ACFT LANDED WITHOUT INCIDENT AFER ALL OVERHEAD LIGHTS WERE TURNED OFF. ACFT WAS THEN FERRIED, WHERE MAINTENANCE RELAMPED SIDEWALL LIGHT AT SEAT 11A IAW AMM 33-21-06 AND OPS CHECKED GOOD AND NO OTHER DEFFECTS NOTED. ACFT WAS RELEASED BACK TO SERVICE.

Part: YOKE — CRACKED (ENGINE MOUNT) · airframe 35,124 hrs · 19,941 cycles

DURING C-CHECK, THE RT ENGINE FORWARD LOWER YOKE FITTING WAS FOUND TO BE CRACKED. MAINTENANCE R & R THE FITTING IAW EC5450-01160. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CRACKED (FRM 10) · airframe 35,124 hrs · 19,941 cycles

DURING C-CHECK, THE LT FRAME 10 WAS FOUND TO BE CRACKED BETWEEN STRINGERS 9-10L. MAINTENANCE R & R THE FRAME IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CRACKED (FRM 10) · airframe 35,124 hrs · 19,941 cycles

DURING C-CHECK, THE RT FRAME 10 WAS FOUND TO BE CRACKED BETWEEN STR 9R-10R. MAINTENANCE R & R THE FRAME IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BALLAST — FAULTY (CABIN LIGHTS) · airframe 33,756 hrs · 19,035 cycles

THE CREW REPORTED ELECTRICAL ODOR FROM ROWS 4 AND 5. MAINTENANCE INSPECTED AND REPLACED THE LIGHT BALLASTS. OPS CHECKED GOOD.

Part: WIRE HARNESS — FAULTY (CABIN LIGHTS) · airframe 33,757 hrs · 19,036 cycles

THE CREW REPORTED, AN ODOR AROUND SEAT 4A AND 5A. MAINTENANCE INSPECTED AND REPLACED THE SIDE WALL LIGHT HARNESS ASSEMBLY. OPS CHECKS WERE GOOD.

Part: TARGET — OUT OF ADJUST (NLG WOW) · airframe 31,840 hrs · 17,824 cycles

LANDING GEAR AIR/GROUND FAILED AND TRUST REVERSER DISAGREE AFTER TAKEOFF. ADJUSTED NLG WOW SWITCH TARGET IAW AMM 32-63-05. OPS CHECKED GOOD. ACFT APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 29,968 hrs · 16,668 cycles

DURING ROUTINE MX, THE EMERGENCY EXIT ROW SIGNS WERE FOUND INOPERATIVE. MX RECONNECTED THE NR 3 EMERGENCY LIGHT BATTERY CHARGER CONNECTOR P8031. OPS CHECKED GOOD.

Part: FITTING — DAMAGED (LT AILERON) · airframe 29,723 hrs · 16,495 cycles

DURING C-CHECK. LT AILERON PCA ATTACHMENT BRACKET HAS MIGRATED HAT BUSHING. R & R LT AILERON PCA FITTING IAW EC5750-01177. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (CARGO DOORWAY) · corrosion level 2 · airframe 29,723 hrs · 16,495 cycles

DURING C-CHECK, CARGO DOOR LOWER BEAM CORRODED. R & R CARGO DOOR LOWER BEAM IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — CORRODED (ZONE 200) · corrosion level 2 · airframe 29,723 hrs · 16,495 cycles

DURING C-CHECK THE FRAME 75 FITTING AT STRINGER 1R (12:00 POSITION) WAS FOUND TO HAVE FRETTING CORROSION BETWEEN THE FITTING AND SKIN. MX REMOVED THE CORROSION AND PERFORMED THE REPAIR IAW EC5310-01317, REV B. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 29,723 hrs · 16,495 cycles

DURING C-CHECK THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED AT FRAMES 20-22 AND STRINGERS 15-16R. MX R & R THE SILL IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 29,723 hrs · 16,495 cycles

DURING C-CHECK THE RT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 23. MX R & R THE OMEGA BEAM IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CRADLE — DAMAGED (FLASHLIGHT) · airframe 29,233 hrs · 16,170 cycles

CREW REPORTED FORWARD CABIN FLASHLIGHT NOT CHARGING. R & R THE FORWARD CABIN FLASHLIGHT CRADLE ASSY WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — SMOKE (NR 2) · airframe 28,554 hrs · 15,930 cycles

AFTER TAKEOFF THE CREW REPORTED A LAVATORY SMOKE INDICATION IN FLIGHT. THE ACFT RETURNED AND LANDED WHERE MX DETERMINED THE SOURCE OF THE SMOKE TO BE THE NR 2 ENGINE. THE ACFT WAS FLOWN UNDER A SPECIAL FLIGHT PERMIT TO WHERE THE NR 2 ENGINE WAS REPLACED, ENGINE OPS CHECKS PERFORMED AND THE DISCREPANCY CLEARED.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 28,522 hrs · 15,741 cycles

DURING ROUTINE MX, THE LT EMERGENCY EXIT SHROUD LIGHT AND OVERWING EMERGENCY CEILING EXIT SIGN WAS FOUND INOPERATIVE. MX INSPECTED AND REPLACED THE NR 4 EMERGENCY LIGHT INVERTER. OPS CHECKED GOOD.

Part: UNKNOWN — ODOR (CABIN)

CREW REPORTED A BURNING ODOR IN THE COCKPIT AND CABIN AFTER TAKEOFF. THE ACFT LANDED WITHOUT INCIDENT, MX INSPECTED THE ACFT, COMPLIED WITH FIM, ALL WITH NO DEFECTS NOTED. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — LEAKING (LEFT PYLON) · airframe 26,303 hrs · 14,264 cycles

AFTER TAKEOFF THE CREW REPORTED SMOKE BEGAN TO FILL CABIN AFTER SELECTING ENGINE BLEED AIR ON TAKEOFF. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MX INSPECTED ACFT AND R & R THE NR 1 ENGINE, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 24,262 hrs · 12,940 cycles

SHV - ABORTED TAKEOFF AT 60 KTS DUE TO FO DV WINDOW YELLOW TAB SHOWING UNLOCKED. PERFORMED OPERATIONAL CHECK OF F/O DV WINDOW IAW EMB 145 AMM 56-11-00. OPS CHECK GOOD. DV WINDOW VERIFIED CLOSED AND LOCKED.

Part: VALVE — INOPERATIVE (RT WING) · airframe 23,302 hrs · 12,411 cycles

FLIGHT 3009 - EWR - FLIGHT CREW REPORTED THAT AFTER T/O FUEL INDICATOR ON NR 2 SIDE DECREASING AT HIGH RATE. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. EWR MX REMOVED AND REPLACED RT WING FLAP VALVE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: DUCT — LEAKING (BLEED AIR SYS) · airframe 22,213 hrs · 11,815 cycles

CLE FLT 2197 THE CREW REPORTED A NR 2 BLEED LEAK MESSAGE ON THE EICAS CLIMBING THRU 17000. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE BLEED DUCT FROM THE PRE-COOLER TO BLEED VALVE. OPERATIONAL CHECKS WERE GOOD.

Part: PROXIMITY SENSOR — INOPERATIVE (LANDING GEAR) · airframe 21,002 hrs · 11,152 cycles

IAH - FLIGHT 2857, THE CREW REPORTED A AN SPS ADVANCE WARNING INDICATION DURING ALL PHASES OF FLIGHT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT DOWNLOCK PROXIMITY SWITCH, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 19,446 hrs · 10,315 cycles

SHV - DURING C-CHECK (ZONE-311) EXTERNAL SKIN AT FRAME 77, HAS (2) SKIN CRACKS AT RIVETS (.081" & .043"). MAINTENANCE PERFORMED REPAIR OF ON ZONE-311 FUSELAGE EXTERNAL SKIN FRAME 77 IAW EC5330-02012. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 19,446 hrs · 10,315 cycles

SHV - DURING C-CHECK (ZONE - 311) EXTERNAL SKIN AT FRAME 79, HAS (5) SKIN CRACKS AT RIVETS (.059", .074", .061", .046" AND .017'). MAINTENANCE PERFORMED REPAIR ON ZONE 311 EXTERNAL SKIN AT FRAME 79 (5) PLACES IAW EC 5330-02012. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 19,446 hrs · 10,315 cycles

SHV - DURING C-CHECK (ZONE - 311) EXTERNAL SKIN AT FRAME 80, HAS (2) SKIN CRACKS AT RIVETS (.031" & .046"). MAINTENANCE REPAIRED (ZONE-311) EXTERNAL SKIN @ FRAME 80 (2) IAW EC5330-02012. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 1 · airframe 19,446 hrs · 10,315 cycles

SHV - DURING C-CHECK SERVICE DOOR CENTER SILL HAS CORROSION (LEVEL 1 LOCAL). MAINTENANCE REPAIRED CENTER SERVICE DOOR FLOOR SILL IAW EMB-145XR SRM 53-21-02 AND CPM 51-21-04/05/06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 19,446 hrs · 10,315 cycles

SHV - DURING C-CHECK (ZONE-311) SKIN AT FRAME 78, HAS CRACKED SKIN AT RIVET (.054"). MAINTENANCE PERFORMED REPAIR ON ZONE-311 FUSELAGE EXTERNAL SKIN AT FRAME 78 IAW EC5330-02012. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 3 · airframe 19,446 hrs · 10,315 cycles

SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION (LEVEL 3 LOCAL) AT LIGHTENING HOLES BETWEEN FRAMES 49-50. MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM BETWEEN FRAMES 49-50 IAW EMB-145XR EC5310-01466. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — OVERTEMP (MASTER) · airframe 19,236 hrs · 10,249 cycles

IAH - FLIGHT 2160, THE CREW REPORTED A BATTERY ONE OVERTEMP PEAKING AT 83 DEGREES. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE MAIN BATTERY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: GARLOCK SEAL — LEAKING (NR 1 ENGINE) · airframe 18,261 hrs · 9,660 cycles

VPS - FLIGHT 2408 - DURING CRUISE THE CREW REPORTED AN E1 LOW OIL PRESSURE MESSAGE. THE CREW SHUT DOWN THE NUMBER ONE ENGINE AS A PRECAUTION, AND DIVERTED TO VPS WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, AND REMOVED AND REPLACED THE NUMBER ONE ENGINE AIR TURBINE STARTER GARLOCK SEAL, OPERATIONALLY TESTED WITH NO LEAKS OR DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 18,257 hrs · 9,657 cycles

FLIGHT 2916 - THE CREW REPORTED A RAPID DECOMPRESSION AT FL360, AND THAT THE CABIN ALT REACHED 13000FT. THE AIRCRAFT LANDED AT TUL WITHOUT INCIDENT WHERE MX INSPECTED ACFT, R & R THE PNEUMATIC OUTFLOW VALVE, OPS TESTED WITH NO DEFECTS, AND ACFT APPROVED FOR RETURN TO SERVICE.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 18,257 hrs · 9,657 cycles

IAH - FLIGHT 2916 - THE CREW REPORTED A RAPID DECOMPRESSION AT FL360, AND THAT THE CABIN ALT REACHED 13000FT, THE AIRCRAFT LANDED AT TUL WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND THE AIRCRAFT WAS FERRIED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED AND REPLACED DIGITAL CONTROLLER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: OUTFLOW VALVE — DEFECTIVE (CABIN PRESSURE) · airframe 18,246 hrs · 9,648 cycles

TYS - AIRCRAFT EN ROUTE FROM CLT TO IAH WHEN THE AUTO PRESSURE SYSTEM FAIL INFLIGHT. AIRCRAFT DIVERTED BACK TO CLT AND WAS MEL (169978). IAH - MAINTENANCE REMOVED AND REPLACED THE ELECTRO PNEUMATIC OUTFLOW VALVE IAW EMB 145XR MM 21-31-03. OPS CHECK GOOD AND RELEASED TO SERVICE. LOG PAGE 2520610.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 18,042 hrs · 9,531 cycles

IAH - FLIGHT 3133, THE CREW REPORTED A BURNING SMELL INTERMITTENTLY EN ROUTE, AND ON APPROACH. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT CABIN AND COCKPIT FOR A BURNING SMELL WITH NO DEFECTS NOTED. THE AIRCRAFT WAS SUBSEQUENTLY APPROVED FOR RETURN TO SERVICE.

Part: BLEED VALVE — INOPERATIVE (APU) · airframe 17,432 hrs · 9,212 cycles

IAH - FLIGHT 2099, THE CREW REPORTED THAT THE APU BLEED VALVE WAS STUCK OPEN DURING CLIMB. THE ACFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MX R&R THE APU BLEED VALVE, OPS TESTED WITH NO DEFECTS. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — SMOKE (CABIN) · airframe 11,179 hrs · 5,923 cycles

IAH - DURING POST-FLIGHT INSPECTION THE CREW REPORTED A SMOKE/BURNING SMELL NEAR ROWS 16-18. MAINTENANCE INSPECTED THE AIRCRAFT WITH NO DISCREPANCIES NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — CHAFED (RT AILERONS) · airframe 9,845 hrs · 5,215 cycles

TYS DURING A 2C INSPECTION THE RIGHT AILERON PCA ATTACHMENT BRACKET HAS DAMAGE WHERE THE HAT BUSHINGS WERE GOUGED. MAINTENANCE REMOVED AND REPLACED THE PCA BRACKET IAW EC 5750-01177. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: TANK — CORRODED (FUEL STORAGE) · airframe 9,845 hrs · 5,215 cycles

TYS DURING A 2C INSPECTION CORROSION WAS FOUND BENEATH A FUEL LINE SUPPORT BRACKET ON THE VENTRAL TANK. MAINTENANCE CUT OUT THE CORRODED AREA, FAB A DOUBLER IAW EC2810-01017, SRM 57-10-03, APPLIED FUEL TANK SEALANT AND FUEL VAPOR COATING IAW EMB XR SRM 51-40-02, 01 AND AMM 28-11-00. LEAK CHECKS GOOD. ACFT WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: SILL — CORRODED (FUSELAGE) · airframe 9,845 hrs · 5,215 cycles

TYS DURING A 2C INSPECTION THE FWD L ANGLE IN THE CARGO DOORWAY WAS FOUND WITH CORROSION. MAINTENANCE REMOVED THE CARGO DOOR SILL AND THE CORROSION; FR 68 SHEAR CLIP, REPAIRED CARGO DOOR SILL, ALODINED, PRIMED, PAINTED AND SEALED EC 5330-01458. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: VALVE — LEAKING (APU) · airframe 8,236 hrs · 4,367 cycles

CLE FLIGHT 3260 - THE CREW REPORTED A STRONG FUEL SMELL IN THE COCKPIT WHEN APU STARTING. MAINTENANCE REPLACED THE APU BLEED VALVE. OPERATIONAL CHECKS WERE GOOD.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 5,914 hrs · 3,143 cycles

CRP - DURING MAINTENANCE INSPECTION THE NUMBER TWO EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO EMERGENCY LIGHT BATTERY CHARGER, OPERATIONALLY CHECKED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. NO TIMES ARE AVAILABLE ON THIS PART.