N10156

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 46,964 hrs · 31,195 cycles

MULTIPLE EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BPS NR 3. OPS CHECK SAT.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 46,507 hrs · 30,774 cycles

NR 1 EMERGENCY LIGHT BATTERY NOT HOLDING CHARGE. REMOVED AND REPLACED NR 1 EMERGENCY BATTERY. OPS CHECK GOOD.

Part: HANDLE — LACK OF LUBE (ZONE 800) · airframe 46,127 hrs · 30,440 cycles

MAIN CABIN DOOR HARD TO CLOSE AND LOCK. FOUND MCD HARD TO LOCK FROM INSIDE. LUBRICATED INTERNAL ACTUATING HANDLE WITH LPS. ACTUATED MCD SEVERAL TIMES. OC SAT.

Part: SCREEN — FAULTED (ZONE 100) · airframe 46,096 hrs · 30,415 cycles

BURNING SMELL, LIKE FIREWORKS, DURING CRUISE AND INTO DESCENT. PERFORMED FIM. FOUND PACK 2 EXHAUST GRATE AND DUCT TO BE AT FAULT. REMOVED AND REPLACED PACK 2 EXHAUST GRATE AND DUCT. OPS CHECK GOOD AT THIS TIME. NO FURTHER DEFECTS NOTED. NO BURNING SMELL NOTED.

Part: MUFFLER — SPLIT (RECIRC FAN) · airframe 45,792 hrs · 30,137 cycles

SMELLED SMOKE IN COCKPIT ON TAKE OFF. NO EICAS MESSAGES. ON TAKEOFF NOTICED THE SMELL OF SMOKE. APU BLEED WAS ON. BOTH PACKS WERE ON. #1 AND #2 ENGINES BLEEDS OFF. INITIAL SMELL WAS LIKE A SANDWICH OR FOOD THEM SMELL TURNED TO ELECTRICAL. NO VISIBLE SMOKE. FLASHLIGHT IS OFF AND IN THE CRADLE. SCREENS WERE NORMAL AND LIGHTING WAS NORMAL. TROUBLESHOT. FOUND RH RECIC FAN MUFFLER TO BE SPLIT IN HALF. REMOVED AND REPLACED MUFFLER AND RAN PACKS. OPS CHECK LEAK CHECK SAT. NO SMELL OF SMOKE PRESENT. NO OTHER DEFECTS NOTED.

Part: DOOR SEAL — UNSECURE (ZONE 800) · airframe 45,535 hrs · 29,869 cycles

MCD UNABLE TO LOCK/SECURE WHEN CLOSING. FOUND MCD SEAL POPPED FROM DOOR LOWER FWD, RESECURED DOOR SEAL. OPS CHECK SAT. NO FURTHER DEFECTS NOTED.

Part: SIGNAL COND UNIT — INOPERATIVE (FUEL TRANSFER) · airframe 44,109 hrs · 28,545 cycles

FUEL TRANSFER INOPERATIVE. REMOVED AND REPLACED FUEL SIGNAL CONDITIONING UNIT. OPS CHECK GOOD, PUSHED IN CIRCUIT BREAKERS.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,067 hrs · 28,509 cycles

MCD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED MCD EMERGENCY LIGHT ASSEMBLY. OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (UNKNOWN) · airframe 43,845 hrs · 28,309 cycles

MCD EMERGENCY LIGHT OUT. REMOVED AND REPLACED MCD EMERGENCY LIGHT BULB. OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (UNKNOWN) · airframe 43,421 hrs · 27,897 cycles

MCD EMERGENCY LIGHT OUT. REMOVED AND REPLACED BULB. OPS CHECK SAT.

Part: LAMP — INOPERATIVE · airframe 43,009 hrs · 27,505 cycles

MCD EMERGENCY LIGHT OUT. REMOVED AND REPLACED MCD EMERGENCY LAMP. OPS CHECK SAT.

Part: LAMP — INOPERATIVE · airframe 42,974 hrs · 27,475 cycles

MCD EMERGENCY & SEAT 18CD LIGHT INOPERATIVE. REMOVED AND REPLACED BAD BULBS AT MCD EMERGENCY LIGHT AND SEAT 18CD OH EMERGENCY LIGHT. OPS CHECK GOOD.

Part: BATTERY — INOPERATIVE · airframe 42,941 hrs · 27,448 cycles

EMERGENCY LIGHT EXIT SIGN ABOVE SERVOOR IS INOPERATIVE. REMOVED AND REPLACED #2 EMERGENCY LIGHT BATTERY. OPS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE · airframe 42,875 hrs · 27,389 cycles

THREE EMERGENCY LIGHTS OUT AT EMERGENCY ROW. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AND CHASSIS ASSEMBLY. BATTERY PACK TESTS GOOD, EMERGECY LIGHTS OPS CHECK GOOD.

Part: LAMP — INOPERATIVE · airframe 42,875 hrs · 27,389 cycles

MCD EXTERNAL EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED MCD EXTERNAL EMERGENCY LIGHT LAMP. OPS CHECK SAT

Part: BATTERY — INOPERATIVE · airframe 42,838 hrs · 27,353 cycles

THREE EMERGENCY LIGHT OUT AT EMERGENCY ROW. REMOVED AND REPLACED EMERGENCY EXIT IDENTIFIER & MARKING SIGNS ROW 18A. DURING OPS CHECK, REPLACED LIGHTS FADED DURING TEST. REMOVED AND REPLACED EMERGENCY BATTERY PACK NO 3. LIGHTS OPS CHECK GOOD.

Part: PRESSURE SENSOR — INOPERATIVE · airframe 42,767 hrs · 27,285 cycles

RUDDER OVERBOOST ON EICAS AFTER TAKEOFF. REMOVED AND REPLACED RUDDER PRESSURE SW. LEAK AND OPS CHECK SAT. PERFORMED PITOT TEST. NO FURTHER DEFECTS NOTED.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 42,553 hrs · 27,104 cycles

FO W/S SPIDER WEB CRACKED DURING FLIGHT. REMOVED AND REPLACED FO'S WINDSHIELD. OPS CHECK SAT AT THIS TIME.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,542 hrs · 27,089 cycles

MULTIPLE INTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BPS #3. OPS CHECK OF ALL CORRESPONDING LIGHTS GOOD

Part: SLEEVE — MISINSTALLED (STAB ANTI ICE) · airframe 42,528 hrs · 27,078 cycles

STAB ANTI-ICE EICAS MESSAGE POSTED IN FLIGHT. DURING APPROACH AND ICE CONDITION ANTI-ICE INOPERATIVE MESSAGE APPEARED. CMC MSG "STAB A/I LEAK" AND "STAB A/I VLV FAIL" PRESENT. STARTED PERFORMING INSTALLATION OF LEAK TEST KIT FOR HORIZONTAL STAB VERTICAL DUCTS. RE-INSTALLED HORIZONTAL STAB ANTI-ICE AND GAMA JOINT. RE-INSTALLED PANELS 322 AL AND 321DR. FOUND INTERNAL SLEEVE (5) NOT INSTALLED CORRECTLY ON LH HORIZONTAL STAB. REINSTALLED SLEEVE. PERFORMED ANTI ICING SYSTEM LEAK CHECK AND FOUND LEAK ON LH HORIZONTAL STAB PICCOLO TUBE NEAR BOLT (3). REMOVED AND REPLACED LH HORIZONTAL STAB L/E PICCOLO TUBE. INSTALLED LH HORIZONTAL STAB LEADING EDGE. FUNCTIONAL TEST SAT.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,425 hrs · 26,980 cycles

LH AND RH EMERGENCY EXIT DOOR OVERHEAD LIGHTS AND EXIT MARKERS DO NOT ILLUMINATE. REMOVED AND REPLACED BPS #3. ALL LIGHTS ILLUMINATE. OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 42,425 hrs · 26,980 cycles

MCD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED MCD EMERGENCY LIGHT. OPS CHECK SAT

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,363 hrs · 26,928 cycles

RH AND LH CABIN ESCAPE HATCH EXIT MARKING SIGNS INOPERATIVE. REMOVED AND REPLACED BATTERY POWER SUPPLY. OPS CHECK SAT.

Part: NONE — MISSING · airframe 42,201 hrs · 26,788 cycles

SERVICE DOOR RED "EXIT" IS PARTIALLY MISSING. REMOVED AND REPLACED SERVICE DOOR EXIT PLACARD. NO DEFECTS NOTED.

Part: BATTERY PACK — INOPERATIVE · airframe 42,196 hrs · 26,785 cycles

LEFT WINDOW EMERGENCY EXIT LIGHTS OUT AND RT REAR EMERGENCY LIGHTS OUT. REMOVED AND REPLACED #3 EMERGENCY LIGHT BATTERY. OPS CHECK GOOD

Part: WEB — CRACKED · airframe 42,152 hrs · 26,746 cycles

FAIRLEAD ATTACHMENT HOLE FOUND WITH OBLONG CONDITION AT F.S. 56 19115.6 ON LH SIDE FRAME WEB. ACCOMPLISHED PERMANENT REPAIR ON FRM 56.

Part: NONE — NONE · corrosion level 2 · airframe 42,152 hrs · 26,746 cycles

LH FLOOR GUSSET FR 24-38 LBL 18 HAS CORROSION SEVERAL AREAS BETWEEN AND AROUND TRACKS. REPLACED FLOOR GUSSET FR 24-29, FR 36-39

Part: NONE — NONE · corrosion level 2 · airframe 42,152 hrs · 26,746 cycles

CO-PILOT SEAT TRACKS HAS SIGNS OF CORROSION ON GUSSET. REMOVED DAMAGED DOUBLER SHEET FLOOR AND INSTALLED NEW DOUBLER SHEET FLOOR AT CO-PILOT FLOOR O/B GUSSET

Part: NONE — NONE · corrosion level 2 · airframe 42,152 hrs · 26,746 cycles

SIGNS OF CORROSION AT FR58 STR 20R STRINGER HAS SIGNS OF CORROSION. REMOVED AND REPLACED STRINGER AT FR58-60, STR 20R. NO DEFECTS NOTED AT THIS TIME.

Part: NONE — NONE · corrosion level 2 · airframe 42,152 hrs · 26,746 cycles

CENTER FLOOR TRACKS HAVE CORROSION FR 25-43 BL0. REMOVED CORROSION AT CABIN SEAT TRACK BL0 FROM FR 25-43. EVALUATED SEAT TRACK FROM FR 26, 28, 33, 34, 36 AND 38-40 FOUND TO BE WITHIN LIMITS. EVALUATED SEAT TRACK FROM FR 25, 27, 29, 30-32, 35 AND 37 FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED AS REQUIRED.

Part: NONE — NONE · corrosion level 2 · airframe 42,152 hrs · 26,746 cycles

SIGNS OF CORROSION ON FLOOR GUSSET AT FR59 TO FR60 APPROX LBL15. REMOVED AND REPLACED FLOOR GUSSET AT FR59 TO FR60 APPROX LBL 15

Part: NONE — NONE · airframe 42,152 hrs · 26,746 cycles

LH CENTER FUSELAGE I HAS DENT FWD OF FRM 20 BELOW STGR 14. EVALUATED DENT DIM ARE L=1.20 W=.780 D=.030 NF-700 FOUND TO BE OUT OF LIMITS. RECONTOURED DENT LH FUSELAGE FR20 BELOW STR 14. REEVALUATED DENT L=.550 W=.40 D=.015 NF-800 AND DENT HAS SHARP EDGE FOUND TO BE OUT OF LIMITS. PERFORMED REPAIR RIVET AT REQUIRED AREA.RESTORED FINISH AS REQUIRED.

Part: NONE — NONE · airframe 42,152 hrs · 26,746 cycles

ANGLE SHAPE FOUND CRACKED ON INBD SIDE OF MAIN FLOOR BEAM Y - 479.0 BTW STA 4154.5 & 5633.0. REMOVED AND REPLACED ANGLE AS REQUIRED

Part: NONE — NONE · corrosion level 2 · airframe 42,152 hrs · 26,746 cycles

LH WINDSHIELD HAS SIGNS OF CORROSION AT LOWER OUTBD FLANGE ON BACKSIDE. EVAL AREA AT LH WINDSHIELDS LOWER OUTBD FLANGE ON BACK SIDE, FWD ORIG THICKNESS .160" MAT LOSS .011" REMAINING MAT .149" ON AFT SIDE ORIG THICKNESS .160" MAT LOSS .018" REMAINING MAT .142 FOUND TO BE IN LIMITS.

Part: NONE — NONE · corrosion level 2 · airframe 42,152 hrs · 26,746 cycles

AGING AIRCRAFT FINDING: FLOOR PANEL 231JF AFT SUPPORT AT MAIN DOOR HAS SIGNS OF CORROSION. REMOVED AND REPLACED 1EA SHAPE U SUPPORT AFT AT MAIN DOOR

Part: NONE — NONE · airframe 42,152 hrs · 26,746 cycles

BRACKET ON RH SIDE OF VENTRAL TANK IS BROKEN. REMOVED AND REPLACED BROKEN BRACKET ON RH SIDE OF VENTRAL TANK

Part: NONE — NONE · corrosion level 2 · airframe 42,152 hrs · 26,746 cycles

UPON REMOVAL OF SHROUD FOUND CORROSION AT FR61 RH PARTITION PANEL. REMOVED AND REPLACED RH DOUBLER FWD PORTITION AT FR61. NO DEFECTS NOTED AT THIS TIME

Part: NONE — NONE · corrosion level 2 · airframe 42,152 hrs · 26,746 cycles

STIFFENER ON FR65 AT STR 14R-STR15R HAS SIGNS OF CORROSION. REPLACED STIFFENER ON FR65

Part: NONE — NONE · corrosion level 2 · airframe 42,152 hrs · 26,746 cycles

LH OB LATERAL FLOOR SUPPORT CORROSION FR 24-34 LBL30. REMOVED AND REPLACED LH OB LATERAL FLOOR SUPPORT (SILL) BTW FR24 AND FR30 LBL 30

Part: NONE — NONE · corrosion level 2 · airframe 42,152 hrs · 26,746 cycles

CORROSION FWD CENTER DOOR GUSSET FR15 LBL28. REMOVED AND REPLACED FWD ENTRY DOOR GUSSET FR15 LBL28

Part: NONE — NONE · corrosion level 2 · airframe 42,152 hrs · 26,746 cycles

CENTER FLOOR GUSSET CORROSION FR19-24 BL0. CLEANED AND EVALUATED CENTER FLOOR GUSSET CORROSION AT FR19-FR24 BL0. UPON EVALUATION FOUND TO BE 100% OUT OF LIMITS. REMOVED AND REPLACED CENTER FLOOR GUSSET.

Part: NONE — NONE · corrosion level 2 · airframe 42,152 hrs · 26,746 cycles

SERVICE DOOR SILL LOWER HAS MISSING RIVETS, SIGNS OF CORROSION, FASTENERS ARE MISS BUCKED. REMOVED AND REPLACED SERVICE DOOR SILL LWR.

Part: NONE — NONE · airframe 42,152 hrs · 26,746 cycles

CENTER FLOOR GUSSET HAS MULTIPLE AREAS OF CORROSION FR 23-25 BL0. REMOVED AND REPLACED CENTER FLOOR GUSSET AT FR 24-29 BL0. NO DEFECTS NOTED AT THIS TIME

Part: NONE — NONE · corrosion level 2 · airframe 42,152 hrs · 26,746 cycles

LH SEAT TRACK ON FLOOR CORRODED FR 53-57 LBL 18. REMOVED CORROSION FROM LBL 18 SEAT TRACKS FROM FR53-55. SEAT TRACK FROM FR56-57 FOUND TO BE OUT OF LIMITS. PERFORMED ET ON SEAT TRACKS FROM FR53-55 NO CRACKS FOUND. THICKNESS CHECK, ALL MEASUREMENTS ABOVE MIN REQUIREMENT. SEAT TRACKS FOUND TO BE WITHIN LIMITS. ALODIOED SEAT TRACK

Part: NONE — NONE · corrosion level 2 · airframe 42,152 hrs · 26,746 cycles

RH FLOOR SILL HAS SIGNS OF CORROSION FROM FR68-71. EVALUATED ON RH FLOOR SILL AT FR68-71, FOUND TO BE 100% OUT OF LIMITS. REMOVED RH FLOOR SILL. LOCATED AND DRILLED NEW RH FLOOR SILL. INSTALLED NEW RH FLOOR SILL. ALODINED AND PRIMED HOLES.

Part: NONE — NONE · airframe 42,152 hrs · 26,746 cycles

DURING ACCESS REMOVAL RH AFT CARGO FLOOR SILL FOUND BLEED AIR DUCT BRACKET CRACKED FR73 RH SIDE OF SUPPORT. REMOVED, FABRICATED AND INSTALLED REPLACEMENT BLEED AIR DUCT BRACKET AT RH AFT CARGO FLOOR SILL FR73, RH SIDE.

Part: NONE — NONE · corrosion level 2 · airframe 42,152 hrs · 26,746 cycles

LATERAL FLOOR SILL SUPPORT CORROSION FR24 RBL 32. REMOVED AND REPLACED LATERAL FLOOR SILL SUPPORT FR24, RBL32. NO DEFECTS NOTED AT THIS TIME.

Part: NONE — NONE · corrosion level 2 · airframe 42,152 hrs · 26,746 cycles

CORROSION ON FLOOR GUSSET FR20 BL0 - RBL 17, REMOVED AND REPLACED BEAM

Part: UNKNOWN — UNKNOWN · corrosion level 2 · airframe 42,152 hrs · 26,746 cycles

RH FLOOR SILL HAS SIGNS OF CORROSION AROUND NUTPLATE HOLES AT FR65 TO FR68. REMOVED AND REPLACED RH FLOOR SILL AT STGR 15 BETWEEN FR65 TO FR68

Part: NONE — NONE · corrosion level 2 · airframe 42,152 hrs · 26,746 cycles

RH FLOOR SILL JUST AFT LAV BULKHEAD HAS SIGNS OF CORROSION FR61 TO FR65. REMOVED AND REPLACED RH FLOOR SILL.

Part: NOT REPORTED — NOT REPORTED · airframe 41,912 hrs · 26,536 cycles

EXIT LIGHT STRIP AT 3-4C NOT SECURED. RESECURED EXIT LIGHT STRIP

Part: LIGHT — ODOR (GALLEY LIGHTS) · airframe 41,867 hrs · 26,493 cycles

BURNING PLASTIC ODOR COMING FROM COFFEE POTS DURING OPERATION. PERFORMED OPS CHECK OF BOTH COFFEE BREWERS. OPS CHECK SAT. UNABLE TO DETECT ODOR COMING FROM COFFEE BREWERS AND COFFEE BREWER SYSTEM. FOUND NO DEFECTS OR SIGNS OF ARCHING. NOTICED BURNING ODOR COMING FROM GALLEY CEILING LIGHTS. INSPECTED CEILING LIGHT HARDNESS FOR SIGNS OF ARCHING. NO DEFECTS NOTICED. REMOVED AND REPLACED GALLEY CEILING LIGHTS. OPS CHECK SAT. AFTER A SHORT PERIOD NOTICED ODOR HAS DISSIPATED AND NO LONGER PRESENT.

Part: CONTAINER — TORN (LIFE VEST) · airframe 41,806 hrs · 26,439 cycles

FO'S CREW LIFE VEST HAS A RIP IN BAG. REMOVED AND REPLACED LIFE VEST

Part: LAMP — INOPERATIVE · airframe 41,775 hrs · 26,409 cycles

MCD HINGE FAIRING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED FAIRING EMERGENCY LIGHT LAMP. OPS CHECK SAT

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,361 hrs · 26,027 cycles

EMERGENCY LIGHT EXIT SIGN AT ROW 18 INOPERATIVE. R&R #3 BATTERY PACK. OPS CHECK SAT. NO DEFECTS NOTED

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,347 hrs · 26,012 cycles

MCD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED MAIN CABIN DOOR EMERGENCY LIGHT ASSY AND BULB. OPERATIONAL CHECK OF THE EMERGENCY LIGHT FOUND SATISFACTORY

Part: MOUNT — DAMAGED (LT AILERON) · airframe 39,839 hrs · 24,777 cycles

LH AILERON DAMPER MOUNT IS DAMAGED. R&R LH AILERON DAMPER MOUNT.

Part: DUCT — CRACKED (BLEED AIR SYS) · airframe 39,226 hrs · 24,290 cycles

NR 2 BLEED LEAK IN FLIGHT-- FOUND CRACKED DUCT UNDER CARGO BAY FLOOR GOING TO AIR STARTER, R&R DUCT ASSY LEAK AND OPS CHECK GOOD.

Part: TEST PANEL — FAULTY (SMOKE WARNING) · airframe 39,025 hrs · 24,132 cycles

LAV SMOKE WARNING AT 30000. R2 LAV SMOKE TEST PANEL AND CLEANED SMOKE DETECTOR SENSOR, OPS CHECK GOOD.

Part: FITTING — CRACKED (FUSELAGE) · airframe 38,078 hrs · 23,400 cycles

MAIN CABIN STR 3L END FITTING IS CRACKED @ FRAME 20. REMOVED AND REPLACED LT END FITTING

Part: FLOOR SUPPORT — CORRODED (FRAME 61) · airframe 38,078 hrs · 23,400 cycles

L/H FLOOR SILL HAVE CORROSION AROUND FASTENER HOLE AT FRAME 61 L/H.............REMOVED AND REPLACED L/H FLOOR SILL

Part: ANGLE — CORRODED (FUSELAGE) · airframe 38,078 hrs · 23,400 cycles

AFT CARGO DOOR CUTOUT AFT LOWER L SHAPE ANGLE AT FRAME 58 HAVE CORROSION. REMOVED AND REPLACED CARGO DOOR CUTOUT AFT LOWER L SHAPE ANGLE.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 38,078 hrs · 23,400 cycles

RT OMEGA BEAM O/B LOWER SUPPORT IS CRACKED AT FRAME 47. REMOVED AND REPLACED RT OMEGA BEAM O/B LOWER SUPPORT.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 38,078 hrs · 23,400 cycles

CENTER OMEGA BEAM LT LOWER MATING FLANGE HAVE CORROSION AROUND FASTENER HOLES AT FRAME 24. REMOVED AND REPLACED CENTER OMEGA BEAM LT LOWER MATING FLANGE.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 38,078 hrs · 23,400 cycles

LT FLOOR SILL HAVE CORROSION ON UPPER SURFACE BETWEEN FRAMES 29-30. REMOVE AND REPLACED FLOOR SILL.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 38,078 hrs · 23,400 cycles

LT FLOOR SILL HAS CORROSION ON UPPER SURFACE BETWEEN FRAME 22-23. REMOVED AND REPLACED FLOOR SILL BETWEEN FRAME 22-23

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 38,078 hrs · 23,400 cycles

LT FLOOR SILL HAS CORROSION ON UPPER SURFACE AT FRAME 27. REMOVED AND REPLACED FLOOR SILL AT FRAME 27

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 38,078 hrs · 23,400 cycles

RT FLOOR SILL FWD OF SERVICE DOOR HAVE CORROSION AROUND FASTENER HOLES AT FRAME 18-20. REMOVED AND REPLACED RT FLOOR SILL.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 38,078 hrs · 23,400 cycles

RT FLOOR SILL HAVE CORROSION ON UPPER SURFACE BETWEEN FR 34 AND 35. REMOVED FLOOR SILL BETWEEN FR 29-35 RT SIDE TRANSFERRED HOLES TO NEW SILL. INSTALLED NEW FLOOR SILL AT FR 29-35 RT SIDE.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 38,078 hrs · 23,400 cycles

LT FLOOR SILL HAVE CORROSION ON UPPER SURFACE BETWEEN FRAME32 AND 33. REMOVED AND REPLACED LT FLOOR SILL.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 38,078 hrs · 23,400 cycles

LT OMEGA BEAM UPPER DIGITAL SUPPORT AT FRAME 15 BELOW FLIGHT ATTENDANT SEAT HAS CORROSION. REMOVED AND REPLACED OMEGA BEAM UPPER DIGITAL SUPPORT.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 38,078 hrs · 23,400 cycles

RT OMEGA BEAM I/B LOWER SUPPORT IS CRACKED. REMOVED AND REPLACED RT OMEGA I/B LOWER SUPPORT.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 38,078 hrs · 23,400 cycles

LT FLOOR SILL HAS CORROSION ON UPPER SURFACE AT FRAME 24. REMOVED AND REPLACED FLOOR SILL AT FRAME 24

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 38,078 hrs · 23,400 cycles

LT FLOOR SILL HAVE CORROSION ON UPPER SURFACE BETWEEN FRAME 34-35. REMOVED AND REPLACED LT FLOOR SILL.

Part: THRESHOLD — CORRODED (FRAMES 20-22) · airframe 38,078 hrs · 23,400 cycles

SRVICE DOOR THRESHOLD LOWER SILL FROM FRAME 20-22 HAS CORROSION AROUND FASTENERS HOLES.........REMOVED AND REPLACEDTHRESHOLD LOWER SILL

Part: FITTING — CRACKED (FUSELAGE) · airframe 38,078 hrs · 23,400 cycles

LT FRAME 58 SHEAR CLIP CRACKED AT STR 15L. REMOVED AND REPLACED SHEAR CLIP.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 38,078 hrs · 23,400 cycles

LT FLOOR SILL HAVE CORROSION ON UPPER SURFACE AT FRAME 54-57 LT. REMOVED AND REPLACED LT FLOOR SILL AT FRAME 54-57.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 38,078 hrs · 23,400 cycles

RT FLOOR SILL HAVE CORROSION ON UPPER SURFACE AT FRAME 46. REMOVED AND REPLACED RT FLOOR SILL.

Part: SUPPORT — DAMAGED (FUSELAGE) · airframe 38,078 hrs · 23,400 cycles

LT SIDEWALL CARBON FIBER SUPPORT AT FRAME 61 HAVE CORROSION BETWEEN CARBON FIBER SUPPORT AND SIDEWALL WEB AT LT FLOOR SILL. REMOVED AND REPLACED LT CARBON FIBER SUPPORT.

Part: FLOOR SUPPORT — CORRODED (FRAME 61) · airframe 41,064 hrs · 25,286 cycles

R/H OMEGA BEAM UPPER SUPPORT HAVE CORROSION ON UPPER SURFACE AT FRAME 61 RH....REMOVED AND REPLACED R/H OMEGS BEAM UPPER SUPPORT

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 38,078 hrs · 23,400 cycles

RT FLOOR SILL HAVE CORROSION ON UPPER SURFACE AT FR 46. REMOVED AND REPLACED RT FLOOR SILL AT FRAME 46.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 38,078 hrs · 23,400 cycles

LT FLOOR SILL HAVE CORROSION ON UPPER SURFACE BETWEEN FRAME 37-38. REMOVED AND REPLACED FLOOR SILL FRAME 37-38.

Part: SUPPORT ANGLE — CORRODED (FRAME 14) · airframe 41,064 hrs · 25,286 cycles

AFT CARGO DOOR CUTOUT FWD LOWER EDGE L SHAPE SUPPORT ANGLE HAVE CORROSION AT FRAME 14 L/H .........REMOVED AQND REPLACED L ANGLE SUPPORT

Part: FLOOR SUPPORT — CRACKED (FRAMES 46-47) · airframe 41,064 hrs · 25,286 cycles

MAIN CABIN L/H OMEGA BEAM O/B SUPPORT IS CRACKED BETWEEN FRAME 46-47........REMOVED AND REPLACED L/N OMEGA BEAM O/B LOWER SUPPORT

Part: FLOOR SUPPORT — CRACKED (FRAME 15) · airframe 38,078 hrs · 23,400 cycles

PASSENGER DOOR CUT OUT FWD LOWER CORNER AT FR 15 UPPER DIGITAL FLOOR SUPPORT END ANGLE IS CRACKED AT STR 15 LH.... REMOVED AND REPLACED SUPPORT ANGLE

Part: SUPPORT ANGLE — CORRODED (THRESHOLD) · airframe 38,078 hrs · 23,400 cycles

PASSENGER DOOR LOWER THRESHOLD 2EA LOWER NUT PLATES SUPPORT Z ANGLE IS CORRODED AROUND FASTENER HOLES....REMOVED AND REPLACED ANGLES

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 38,078 hrs · 23,400 cycles

AFT CARGO BAY DOOR LOWER THRESHOLD Z ANGLE SUPPORT IS CORRODED FROM FRAME 65-68. REMOVED AND REPLACED THRESHOLD Z ANGLE SUPPORT AT65-68

Part: FITTING — CRACKED (NR 1 YOKE) · airframe 38,078 hrs · 23,400 cycles

NR 1 ENG PYLON YOKE LOWER FWD LINKAGE FITTING HAVE SIGNIFICANT CRACK INDICATION IN BEND RADIUS. DETAILS FOR THIS REPAIR HAVE BEEN EMAILED TO [email protected], WITH SUBJECT 10156 SDR RAIA201809110006.

Part: WEB — CRACKED (LT MLG WW) · airframe 38,078 hrs · 23,400 cycles

LH WHEEL WELL REAR WEB IS CRACKED....REMOVED AND INSTALLED LH WHEEL WELL REAR WEB

Part: FITTING — CRACKED (NR 2 YOKE) · airframe 38,078 hrs · 23,400 cycles

NR 2 ENG PYLON YOKE LOWER FWD LINKAGE FITTING HAVE SIGNIFICANT CRACK INDICATION IN BEND RADIUS. DETAILS FOR THIS REPAIR HAVE BEEN EMAILED TO [email protected], WITH SUBJECT 10156 SDR RAIA201809110007.

Part: SUPPORT BRACKET — CRACKED (AFT CARGO DOOR) · airframe 38,078 hrs · 23,400 cycles

AFT CARGO DOOR LOWER T PROFILE LOWER ANGLE SUPPORT BRACKET IS CRACKED...REMOVED AND REPLACED AFT CARGO DOOR LOWER T PROFILE ANGLE SUPPORT BRACKET

Part: SUPPORT BRACKET — CRACKED (CARGO DOOR) · airframe 38,078 hrs · 23,400 cycles

AFT CARGO DOOR TORSION BAR LIFTING MECHANISM AFT LOWER SUPPORT BRACKET IS CRACKED. REMOVED AND REPLACED AFT TORSION BAR SUPPORT BRACKET.

Part: SUPPORT BRACKET — CRACKED (PAX DOOR) · airframe 38,078 hrs · 23,400 cycles

PASSENGER DOOR INTERIOR DOOR HANDLE SUPPORT BRACKET IS CRACKED. R&R THE PAX DOOR DOOR HANDLE SUPPORT BRACKET.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 38,078 hrs · 23,400 cycles

ANTI-ICE SHUT OFF VALVE ON LT SIDE OF THE FUSELAGE FWD OF LT WING LE HAS CRACKED SUPPORT BRACKET. REMOVED AND REPLACED ANTI ICE SHUTOFF VALVE SUPPORT BRACKET

Part: SKIN — CRACKED (FRAME 79) · airframe 41,064 hrs · 25,286 cycles

AFT FUSELAGE EXTERIOR SKIN ON R/H SIDE ABOVE ACCESS DOOR 312AR AT FRAME 79 IS CRACKED .........CUTOUT DAMAGED AREA PERFORMED BUSHING REPAIR

Part: FITTING — CRACKED (FUSELAGE) · airframe 38,078 hrs · 23,400 cycles

AFT CARGO FRAME 72 SHEAR CLIP IS CRACKED AT STR 14L. REMOVED AND REPLACED SHEAR CLIP AT FR 72.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 38,078 hrs · 23,400 cycles

AFT CARGO COMPT FRAME 73 LT SIDE FRAME SHEAR CLIP IS CRACKED BETWEEN STR 8 AND 10. REMOVED AND REPLACED AFT LT FRAME 73 SHEAR CLIP.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 38,078 hrs · 23,400 cycles

AFT CARGO COMPT FRAME 73 RT SIDE FRAME SHEAR CLIP IS CRACKED BETWEEN STR 8 & 10. REMOVED AND REPLACED AFT RT FR 73 SHEAR CLIP.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 38,139 hrs · 23,448 cycles

LT OVERWING BELLY FAIRING ATTACH ANGLE ON LT SIDE OF FUSELAGE AT FRAME 49 IS CRACKED AT 2 LOC. REMOVED AND REPLACED LT OVERWING FAIRING ATTCAH ANGLE AT FRAME 49.

Part: ANGLE — CRACKED (LT WING) · airframe 38,078 hrs · 23,400 cycles

LT OVERWING L ANGLE ON TOP OF WING I/B END IS CRACKED AT FRAME 48. C/W ETD2018-145-101410

Part: SKIN — CRACKED (FRAME 79) · airframe 41,064 hrs · 25,286 cycles

AFT FUSELAGE EXTERIOR SKIN ON R.H SIDE ABOVE ACCESS DOOR 312AR AT FRAME 79 IS CRACKED .....CUTOUT DAMAGED AREA PERFORMED BUSHING REPAIR

Part: HOLDER — CRACKED (FUSELAGE) · airframe 38,078 hrs · 23,400 cycles

AFT CARGO DOOR SUPPORT ROD CUP HOLDER AT FRAME 68 IS CRACKED ON BACKSIDE. REMOVED AND REPLACED AFT CARGO DOOR SUPPORT ROD CUP HOLDER AT FRAME 68.

Part: SUPPORT BRACKET — CRACKED (CARGO DOOR) · airframe 38,078 hrs · 23,400 cycles

AFT CARGO DOOR TORSION BAR LIFTING MECHANISM AFT UPPER SUPPORT BRACKET IS CRACKED. REMOVED AND REPLACED AFT UPPER SUPPORT BRACKET.

Part: LIGHT — LOOSE (CABIN) · airframe 36,782 hrs · 22,277 cycles

FLOOR EMERGENCY LIGHT LOOSE AT ROW 3CD. SECURED LIGHT STRIP.

Part: SUPPORT — LOOSE (PROXIMITY SWITCH) · airframe 34,961 hrs · 20,714 cycles

LANDING GEAR AIR GROUND FAIL EICAS. LANDING GEAR LEVER WOULD NOT COME UP. TIGHTENED FRONT AIR GROUND PROXIMITY SWITCH SUPPORT. R & R REAR WOW PROXIMITY SUPPORT BRACKET. PERFORMED GEAR, OPS CHECKED GOOD.

Part: ELECTRONIC UNIT — INOPERATIVE (MLG) · airframe 37,669 hrs · 22,525 cycles

LG AIR /GRD FAIL AFTER TAKEOFF LANDING GEAR WOULD'NT COME UP. R & R LANDING GEAR ELECTRONIC UNIT . OPS CHECKED GOOD.

Part: LIGHT — MISINSTALLED (RT OVERWING) · airframe 34,388 hrs · 20,223 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT ASSEMBLY IS UPSIDE DOWN. REMOVED, REPOSTIONED AND INSTALLED THE RIGHT OVERWING EMERGENCY EXIT LIGHT. OPS CHECKED GOOD.

Part: OXYGEN MASK — UNWANTED DEPLOY (CABIN) · airframe 33,628 hrs · 19,582 cycles

PASSENGER OXYGEN MASKS DEPLOYED IN FLIGHT. PERFORMED INSPECTION OF PASSENGER OXYGEN CANISTERS. FOUND MULTIPLE USED. R & R USED CANISTERS. OPS CHECKED GOOD.

Part: DUCT — LOOSE (NR 1 BLEED) · airframe 33,163 hrs · 19,233 cycles

BLEED 1 LEAK IN FLT. FOUND BLEED LEAK IN LT PYLON. RESECURRED DUCT. OPS AND LEAK CHECK GOOD.

Part: SKIN — DENTED (FUSELAGE) · airframe 33,159 hrs · 19,230 cycles

THIS ITEM HAS BEEN RECLASSIFIED AS A MAJOR REPAIR. ORIGINAL DISCREPANCY: TWO DENTS PROTRUDING FROM CENTER FUSELAGE SKIN BETWEEN FRAMES 22 AND 23, STRINGER 17L AND 18L. FWD DENT EVALUATED AND FOUND TO BE WITHIN LIMITS. AFT DENT REPAIRED IAW SRM. WHEN AVAILABLE, DETAILS OF THIS REPAIR WILL BE EMAILED TO [email protected], UNDER THE SUBJECT:RAIA201601200002.

Part: CABIN PRESSURE — MALFUNCTIONED · airframe 32,184 hrs · 18,461 cycles

CABIN OVER PRESSURE ON EICAS. PERFORMED QRH. TRIED PRESSURE IN MANUAL MODE, DIDN`T WORK. WENT BACK TO AUTO STARTED WORKING CORRECTLY.

Part: LINE — LOOSE (BLEED AIR) · airframe 31,990 hrs · 18,312 cycles

BLEED 2 OVERTEMP, STABILIZER AND WING A/I FAIL IN ICING CONDITION DURING CLIMB, RETURNED TO BLOCK. MAINTENANCE INSPECTED AND FOUND BLEED LINE LOOSE FROM THERMOSTAT TO FAN AIR VALVE. RESECURED LINE FITTING AND OPS AND LEAK CHECK GOOD.

Part: SWITCH — INOPERATIVE (PACK OVERTEMP) · airframe 31,897 hrs · 18,232 cycles

PACK 2 OVERLOAD DURING CLIMB, RETURNED TO BLOCK. MAINTENANCE DEFERRED PAC 2 SYSTEM. MAINTENANCE CLEARED PAC 2 DEFERRAL BY REPLACING THE NR 2 OVERTEMP SWITCH, OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,266 hrs · 17,722 cycles

AISLE FLOOD EMERGENCY LIGHT IS INOPERATIVE. MAINTENANCE REPLACED BULB, OPS CHECK GOOD.

Part: SHEAR TIE — CRACKED (FRAME 10) · airframe 29,408 hrs · 16,527 cycles

DURING C-CHECK, SHEAR TIE CRACKED FRAME 10 BETWEEN STRINGERS 11 AND 12. MX R & R SHEAR TIE IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CRACKED (FRAME 23-24) · airframe 29,408 hrs · 16,527 cycles

DURING C-CHECK, LT SIDE FLOOR SUPPORT HAS CRACKED SHEAR CLIP UNDERNEATH SIDE WHERE 2 SILL JOIN TOGETHER AS MARKED FRAME 23-24. MAINTENANCE R & R DAMAGED SILL SHEAR CLIP AT FRAMES 23-24 IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CORRODED (FRAMES 23-24) · corrosion level 2 · airframe 29,408 hrs · 16,527 cycles

DURING C-CHECK, CORROSION WAS FOUND ALONG LATERAL WALL SUPPORT FROM CENTER OMEGA BEAM TO RT SIDEWALL BETWEEN FRAMES 23-24. MAINTENANCE R & R LATERAL WALL SUPPORT IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CRACKED (FRAME 10) · airframe 29,408 hrs · 16,527 cycles

DURING C-CHECK, FRAME 10 BROKEN, TOP AFT OF FRAME, ON CO-PILOT SIDE. MAINTENANCE R & R FRAME IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: TEE FITTING — CORRODED (FRAME 20) · corrosion level 2 · airframe 29,408 hrs · 16,527 cycles

DURING C-CHECK TEE FITTING IS CORRODED AT FRAME 20 JUST AFT OF RAMP ANGLES. MAINTENANCE BLENDED CORROSION, AND FOUND TO BE WITHIN LIMITS IAW SRM 53-21-10 ALODINED, PRIMED AND TOPCOATED IAW CPM 51-21-04. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT BRACKET — CORRODED (FRAME 23) · corrosion level 2 · airframe 29,408 hrs · 16,527 cycles

DURING C-CHECK, BLENDED CORROSION, AND FOUND TO BE OUT OF LIMITS IAW SRM 53-22-10. MAINTENANCE R & R FRAME SUPPORT BRACKET IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ATTACH BRACKET — CRACKED (LT WING) · airframe 29,408 hrs · 16,527 cycles

LT L/E 511 INBD ATTACH BRACKET CRACKED IN UPPER RADIUS. MAINTENANCE REMOVED BRACKET, LOCATED AND DRILLED NEW BRACKET IAW SRM 51-40-02, INSTALLED NEW RT INBD L/E ATTACH BRACKET IAW AMM 20-10-01 AND 57-41-00. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: THRESHOLD — CORRODED (ZONE 100) · corrosion level 2 · airframe 29,408 hrs · 16,527 cycles

SERVICE DOOR THRESHOLD HAS CORROSION, LEVEL 2 WIDESPREAD, AROUND ATTACHED NUTPLATES AS MARKED. MAINTENANCE REMOVED CORROSION WITHIN REPAIRABLE LIMITS, INSTALLED REPAIR DOUBLERS AND RESIN ON SERVICE DOOR THRESHOLD IAW SRM 53-21-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHANNEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 29,408 hrs · 16,527 cycles

DURING C-CHECK, MAIN CABIN DOOR THRESHOLD HAS BRACKET RETAINING NUTPLATES THAT IS CORRODED. MAINTENANCE R & R 2 BRACKETS AT MAIN DOOR THRESHOLD IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 29,408 hrs · 16,527 cycles

MOUNTING FLANGE FOR PANEL 194 IS CRACKED AS MARKED BETWEEN FRAMES 48 AND 49. MAINTENANCE REPAIRED MOUNTING FLANGE FOR PANEL 194 IAW EC5320-01928. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 29,408 hrs · 16,527 cycles

DURING C-CHECK, LOWER FUSELAGE AT FWD BELLY FAIRING 191, FWD END NUTPLATE SUPPORT ANGLE HAS CORROSION, LOCAL LEVEL 2, AROUND FASTENER HOLES AT FRAME 32 FROM STRINGER 17LT-17RT. MAINTENANCE BLENDED CORROSION, 100 PERCENT MATERIAL LOSS. REMOVED SUPPORT ANGLE. LOCATED, DRILLED, ALODINED, SEALED AND INSTALLED NEW SUPPORT ANGLE REF: SRM 51-40-02, CPM 51-21-04. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 29,408 hrs · 16,527 cycles

DURING C-CHECK, MULTIPLE AREAS OF CORROSION ALONG CENTER OMEGA BEAM SILL BETWEEN FRAMES 29-36. MAINTENANCE BLENDED CORROSION, OUT OF LIMITS IAW SRM 53-22-10. R & R OMEGA BEAM SILL IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ATTACH BRACKET — CRACKED (ZONE 600) · airframe 29,408 hrs · 16,527 cycles

RT L/E 611 INBD ATTACH BRACKET CRACKED IN UPPER RADIUS. MAINTENANCE REMOVED BRACKET, LOCATED AND DRILLED NEW BRACKET IAW SRM 51-40-02, INSTALLED NEW RT INBD LE ATTACH BRACKET IAW AMM 20-10-01 AND 57-41-00. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SHUTTLE VALVE — LEAKING (BRAKE SYSTEM) · airframe 24,195 hrs · 13,121 cycles

THE CREW REPORTED THE NR 1 HYD FLUID LEVEL DROPPED TO THE AMBER RANGE DURING FLIGHT. THE ACFT DIVERTED AND LANDED WITHOUT INCIDENT. MX INSPECTED AND REPLACED THE NR 1 AND NR 4 BRAKE SHUTTLE VALVES. OPS CHECKS WERE GOOD.

Part: CHECK VALVE — TORN (FUEL SYSTEM) · airframe 23,756 hrs · 12,832 cycles

FUEL LEAKING OUT OF WING DURING FLIGHT IN TURNS. MX R & R THE RT WING TANK CHECK VALVE AT RIB 19 IAW AMM 28-11-04 WITH LEAK CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ALTIMETER — INOPERATIVE (NR 1) · airframe 21,941 hrs · 11,792 cycles

IAH - FLIGHT 2126, THE CREW REPORTED MULTIPLE EICAS MESSAGES INCLUDING "TOO LOW TERRAIN" AND PULL UP CONTINUOUSLY AT FL360, "LANDING GEAR" AURAL WARNING AT FL290 AND WOULD NOT STOP WITH THRUST LEVERS BELOW 70 PERCENT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE RADAR ALTIMETER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FAN — MALFUNCTIONED (NR 2) · airframe 21,191 hrs · 11,373 cycles

IAH - THE CREW REPORTED THAT AFTER TAKEOFF FROM IAH HAD A STRONG SMELL LIKE RUBBER IN THE COCKPIT WITH NO VISUAL SIGN OF SMOKE, AND THE SMELL DISSIPATED AFTER FIVE MINUTES. THE AIRCRAFT CONTINUED TO CRW WHERE IT LANDED WITHOUT INCIDENT. AFTER TAKEOFF FROM CRW, THE SMELL REPEATED WITH NO VISIBLE SMOKE, AND AGAIN DISSIPATED AFTER 5 MINUTES. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE PERFORMED FIM 21-200-810-801-A, REMOVED AND REPLACED THE NR 2 RECIRC FAN, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — DIRTY (FIRE DETECTION) · airframe 20,963 hrs · 11,252 cycles

FLIGHT 3082 - EWR - FLIGHT CREW REPORTED E1 FIRE DET FAIL MESSAGE RECEIVED TWICE ON CLIMBOUT IN ECLB SETTING. ALL ENGINES PARAMETERS REMAINED NORMAL. MESSAGE CLEARED AFTER 10 MIN AND NEVER CAME BACK. EWR MX CLEANED CONNECTOR P0914 AND PERFORMED FIRE DETECTION TEST SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SEAL — OUT OF POSITION (COCKPIT) · airframe 19,628 hrs · 10,528 cycles

IAH - FLIGHT 2568, DURING CLIMB, THE CREW REPORTED THAT THE F/O'S DV WINDOW SEAL POPPED OUT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE DV WINDOW PROFILE SEAL, LEAK CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STARTER GEN — INOPERATIVE (APU) · airframe 19,353 hrs · 10,384 cycles

RDU - FLIGHT 2178, DURING TAXI THE CREW REPORTED THAT THE APU GENERATOR DROPPED OFF LINE WITH AN ELECTRICAL ODOR IN THE COCKPIT. THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE INSPECTED THE AIRCRAFT, CHECKED THE ELECTRICAL WIRING, WITH NO DEFECTS NOTED. MAINTENANCE PLACED THE APU ON MEL 49-00-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. MAINTENANCE REMOVED AND REPLACED THE STARTER GENERATOR, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — INOPERATIVE (LAVATORY) · airframe 18,634 hrs · 9,975 cycles

TYS - THE LAV SMOKE DETECTOR WAS INOP. RELEASED ON MEL. PLACARD NUMBER 199785, CAME BACK IN LATER AND MAINTENANCE REMOVED AND REPLACED THE SMOKE DETECTOR IAW AMM26-14-01. OPS CHECK GOOD AND RELEASED, MEL CLEARED.

Part: THERMOSTAT — FAULTY (ANTI-ICE SYSTEM) · airframe 16,779 hrs · 8,963 cycles

EWR FLT 2558 - THE CREW REPORTED DURING CLIMBOUT IN ICING CONDITIONS, RECEIVED A WING ANTI-ICE FAIL MESSAGE FOLLOWED BY ANTI-ICE INOPERATIVE. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE LEFT WING ANTI-ICING LEAK THERMOSTAT. OPERATIONAL CHECKS WERE GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 16,274 hrs · 8,683 cycles

EWR MX - DURING SCHEDULED MAINTENANCE, EWR MX FOUND EMERGENCY LIGHT NEXT TO SERVICE DOOR INOPERATIVE. MX REMOVED AND REPLACED INVERTER NR 2 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: WARNING SYSTEM — ACTIVATED (ANTI-ICE SYSTEM) · airframe 15,204 hrs · 8,104 cycles

EWR FLIGHT 2609 - THE CREW REPORTED A ENGINE 1 ANTI-ICE FAIL MESSAGE IN FLIGHT. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND RELEASED THE AIRCRAFT IAW MEL 30-21-01. SUPPLEMENT TO FOLLOW.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 15,108 hrs · 8,056 cycles

MCI - DURING MAINTENANCE INSPECTION THE CABIN EMERGENCY LIGHT FORWARD OF THE LEFT EMERGENCY EXIT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS FOUND, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,944 hrs · 14,906 cycles

AIRCRAFT IN FOR A ROUTINE CHECK WHEN THE LEFT EMERGENCY EXIT LOWER EMERGENCY LIGHT WOULD NOT LIGHT UP. MAINTENANCE REMOVED AND REPLACED THE EXIT LIGHT IAW EMB 145XRMM 33-50-13. OPS CHECK GOOD.

Part: ISIS UNIT — INOPERATIVE (COCKPIT)

FLT 2276 DIVERTED INTO TYS FROM IAH FOR ISIS "OUT OF ORDER". R&R ISIS UNIT IAW EMB 145XR AMM 34-01-01. OPS CK GOOD. ACFT RELEASED AND RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS)

FLIGHT 2058 - EWR - FLIGHT CREW REPORTED SERVICE DOOR EMERGENCY SIGN INOPERATIVE. EWR MX REMOVED AND REPLACED SERVICE DOOR EMERGENCY EXIT SIGN IAW EMB145 AMM 33-50-09 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (S)

Part: POTENTIOMETER — DEFECTIVE (MLG) · airframe 112,506 hrs · 6,639 cycles

FLIGHT 2678 - FLIGHT CREW REPORTED AIRCRAFT PULLS TO THE RT AT TAKEOFF AT 80 KNOTS. MX REMOVED AND REPLACED FEEDBACK POTENTIOMETER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 11,702 hrs · 6,248 cycles

IAH - DURING A-CK INSPECTION THE LOWER EXIT SIGN ON THE LEFT HAND OVERWING EMERGENCY EXIT SURROUND WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EXIT SIGN, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: COMPUTER — MALFUNCTIONED (COCKPIT) · airframe 8,925 hrs · 4,789 cycles

FL 2128 - XNA TO IAH- SMOKE IN COCKPIT (ELEC) LOST CAPT MFD, PFD, ICAS, CREW DIVERTED TO DAL. MX INSPECTED AND FOUND IC-600 NR 1 TO HAVE A BURNING SMELL. REMOVED AND REPLACED IC 600 NR 1 IAW EMB 145 AMM 31-42-01 OPS CHECK GOOD. NO OTHER SMOKE, BURNING, FIRE DAMAGE DEFECT FOUND IN COCKPIT AT THIS TIME. INSPECTED CAPTS MFD, PFD AND THE EICAS FOR NORMAL OPERATION AND FUNCTIONALITY AS REQUIRED. NO DEFECT NOTED AT THIS TIME. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE

Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,896 hrs · 4,772 cycles

BTV 3A CHECK FLT NR 2414 FOUND LEFT HAND OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED LAMP FOR LEFT HAND OVERWING EMERGENCY LIGHT IAW EMB145 AMM 33-50-07. OPS CHECK GOOD. CLOSED

Part: COMPUTER — SHORTED (COCKPIT) · airframe 8,868 hrs · 4,756 cycles

YUL FLIGHT NR 2034 THE CREW REPORTED SMOKE IN THE COCKPIT AND CABIN. THEY ALSO REPORTED LOSE OF CAPTAINS MFD, PVD, AND EICAS. THE AIRCRAFT RETURNED TO YUL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 IC-600. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 8,746 hrs · 4,697 cycles

IAH - A BURNING SMELL WAS NOTED IN THE CABIN. MAINTENANCE INSPECTED THE AIRCRAFT, AND COULD NOT DUPLICATE THE ODOR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.