N17196

Part: BATTERY PACK — DISCHARGED (ZONE 200) · airframe 413,577 hrs · 27,597 cycles

NR 2 EMERGENCT LIGHT BATTERY PACKS NOT HOLDING CHARGE. R & R THE NR 2 BATTERY PACKS. OP CHECKED GOOD.

Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 41,340 hrs · 27,565 cycles

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

Part: FLAP SYSTEM — FAULTED · airframe 41,262 hrs · 27,488 cycles

FLAP FAIL AT 9 DEGREES. ON DESCENT, FLAPS MOVED TO 9 DEGREES, GREEN FLAP LIGHT INDICATED, THEN FLAP FAIL MESSAGE. R & R FLAP RESET SWITCH. OPS CHKD SAT. NO FAIL MESSAGE. INSPECTED MECHANICAL LINES SHROUD, ROLLERS & CONNECTORS. SECURED CONNECTORS P3683 & P3682. OPS FLAPS. COULD NOT DUPLICATE FAULT. PERFORMED OPS CHKS OF FLAPS. NO FLAP FAIL MESSAGES ON EICAS OR CMC. OPS FLAPS WHILE SHAKING ALL 4 HARNESSES TO FECU. LISTENED TO INBD & OTBD ACTUATORS FOR ABNORMAL NOISES OR GRAZING. NONE DETECTED. GENERAL VISUAL INSPS OF ACTS FOR CORRORION OR DEFECTS. NO DEFECTS NOTED. GVI ON CONNECTORS & BACKSHELLS. NO CODES RECEIVED FROM FLAP BREAKOUT BOX. CANNOT DUPLICATE FAULT. R & R RT INBD FLAP, OTBD ACT 2. R & R RT OTBD FLAP OTBD ACT. R & R LT INBD FLAP OTBD ACT. R & R OTBD FLAP OTBD ACT. COMPLIED WITH RT & LT FLAP 0 DEGREE RIGGING. OPS CHK OF FLAPS SYS. OPS CHKD SAT. R & R LT INBD FLAP INBD ACT. FLAPS OPS SAT. PERFORMED OPS CHK OF FLAPS. NO FLAP MESSAGES ON CMC. OPS FLAPS WHILE SHAKING ALL 4 HARNESSES TO FECU. LISTENED TO INBD & OTBD ACTS FOR NOISES OR GRAZING. NO DEFECTS. GVI OF ACTS FOR CORROSION OR DEFECTS. NO DEFECTS. GVI ON CONNECTORS & BACKSHELLS. NO CODES RECEOVED FROM FLAP BREAKOUT BOX.

Part: SENSOR — DAMAGED (ZONE 500 FLAP) · airframe 40,949 hrs · 27,196 cycles

FLAP FAIL ON APPROACH. CMC SHOWED LT FLAP VELO SENSOR FAIL. FOUND LT VELO SENSOR ELECTRICAL CONNECTOR DAMAGED. REMOVED AND REPLACED RECEPTACLE J1111. REMOVED AND REPLACED LT FLAP VELOCITY SENSOR. FLAPS OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 40,771 hrs · 27,020 cycles

RH EXTERNAL EMERGENCY LIGHT ABOVE RH PACK PANEL INOPERATIVE. REMOVED AND REPLACED BULB. OPS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 40,658 hrs · 26,898 cycles

SERVICE DOOR UPPER AND LOWER EMERGENCY EXIT LIGHTS INOPERATIVE. SUSPECT BAD EMERGENCY LIGHT BATTERY. REMOVED AND REPLACED #2 EMERGENCY LIGHT BATTERY. OPS CHECK SAT.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 40,658 hrs · 26,898 cycles

RIGHT EXTERIOR FWD EMERGENCY EXIT LIGHT INOPERATIVE AND HOUSING DAMAGED. REMOVED AND REPLACED LIGHT ASSEMBLY. OPS CHECK GOOD.

Part: CHARGER — INOPERATIVE (ZONE 200) · airframe 40,400 hrs · 26,670 cycles

MULTIPLE EMERGENCY LIGHTS INTERIOR AND EXTERIOR INOPERATIVE. REMOVED AND REPLACED BATTERY CHARGER ASSEMBLY. OPS CHECK SAT.

Part: VALVE — INTERMITTENT (NR 1 A/C PACK) · airframe 39,932 hrs · 26,226 cycles

ON CLIMB OUT, BLEED 1 OVERTEMP FOLLOWED BY BLEED 2 OVERTEMP, BLEED 1 & 2 VALVE FAIL MESSAGE ASSOCIATED WITH WING 1 & 2 ANTI ICE FAIL MESSAGE. FOUND PACK 1 VALVE TO BE INTERMITTENTLY OPEN & CLOSE UNCOMMANDED. R & R NR 1 PACK VALVE. OPS CHK SAT. PERFORMED AIR BLEED SYS OPS TEST. JUMPING RELAY K0528 BETWEEN A2-A1, C2-C3, D2-D1. NO DEFECTS NOTED. OPS CHK BY JUMPING HSPS P1203 BETWEEN PINS B & C. NO DEFECTS NOTED, PERFORMED BLEED AIR OPS CHK USING HI STAGE VALVE TEST BOX,, NO DEFECTS NOTED. PERFORMED DVI OF ALL PACK DUCTS. NO DEFECTS NOTED & INSPECTED BLEED AIR DUCTS, NO DEFECTS NOTED. PERFORMED WING A/I TEST. OPS CHK SAT. REMOVED 1 & 2 FAV FILTERS, PERFORMED GVI, NO DEFECTS NOTED. INSTALLED 1 & 2 FAV FILTERS.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,743 hrs · 26,044 cycles

CENTER OMEGA BEAM HAS CORROSION PRESENT BETWEEN FR59 AND FR61. REPAIR CENTER OMEGA BEAM BETWEEN FR59 AND FR61.

Part: PROFILE — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,743 hrs · 26,044 cycles

CORROSION FOUND NEAR FR65 AND STGR 16L ON PROFILE. REMOVED AND REPLACED LOWER SECTION OF SHEAR CLIP AT FRAME 65.

Part: FRAME — CORRODED (ZONE 100) · airframe 39,743 hrs · 26,044 cycles

UPON REMOVAL OF BAGGAGE DOOR PROTECTOR STRIP, FOUND CORROSION ON FRAME 66 DIRECTLY UNDER REMOVED PROTECTOR STRIP AREA. REMOVED AND REPLACED BAGGAGE DOOR SILL. APPLIED TOP COAT TO BAGGAGE DOOR SILL.

Part: DOOR SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,743 hrs · 26,044 cycles

UPON REMOVAL OF BAGGAGE DOOR PROTECTOR STRIP, FOUND CORROSION ON FRAME 66 DIRECTLY UNDER REMOVED PROTECTOR STRIP AREA. REMOVED AND REPLACED BAGGAGE DOOR SILL. APPLIED TOP COAT TO BAGGAGE DOOR SILL.

Part: PLATE — CORRODED (ZONE 100) · airframe 39,743 hrs · 26,044 cycles

FOUND CORROSION ON INSIDE TOP MID PORTION OF BUMPER PLATE, APPROX 5 IN THE LENGTH FROM TOP DOWN. AFTER CLEANING BUMPER PLATE NO CORROSION FOUND.

Part: LIGHT — CRACKED (ZONE 200) · airframe 39,743 hrs · 26,044 cycles

FOUND RH FLOOR PROXIMITY LIGHT COVER PN SG9632 TO BE CRACKED. REPLACED RH FLOOR PROXIMITY LIGHT COVER.

Part: SKIN — DAMAGED (ZONE 200) · airframe 39,743 hrs · 26,044 cycles

FOUND HOLE THROUGH AIRCRAFT 0.15748 IN. IN DIAMETER 2.5 IN AFT OF FRAME 23, AND 1 IN BELOW STRINGER 3L. REPAIRED OPEN HOLE THROUGH FUSELAGE SKIN 2.5" OFF OF FRAME 23 AND 1" BELOW STR 3L

Part: BATTERY PACK — UNKNOWN (UNKNOWN) · airframe 38,739 hrs · 25,155 cycles

FOUND LH AND RH OVERWING EMERGENCY LIGHTS TO DIM & SHUT OFF AFTER BEING SWITCHED ON. REMOVED AND REPLACED NUMBER 4 EMERGENCY LIGHT BATTERY. LIGHT OPS CHECK GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 38,382 hrs · 24,815 cycles

MAIN CABIN DOOR EMERGENCY EXIT LIGHT DOES NOT WORK. RESECURED FWD CABIN EMERGENCY DOOR LIGHT CONNECTORS. OPS CHECK GOOD

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 38,025 hrs · 24,509 cycles

MCD DIFFICULT TO UNLOCK AND OPEN. ADJUSTED MCD INTERNAL HANDLE CABLE. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 38,023 hrs · 24,508 cycles

MAIN CABIN DOOR HARD TO OPEN FROM THE INSIDE. FOUND INNER DOOR HANDLE NOT SITTING PROPERLY WHILE DOOR IS FULLY CLOSED AND LATCHED. MEASURED FORCE NEEDED TO OPEN DOOR FROM FOLDING FLAP POSITION TO UNLOCKED DOOR POSITION. FORCE NEEDED TO UNLOCK DOOR RECORDED AS 244LBS. TIGHTENED MAIN DOOR INNER HANDLE BOX. OPS CHECK FAIL. ADJUSTED MAIN DOOR ROLLERS. OPS CHECK FAIL. ADJUSTED MCD ROLLERS BACK TO ORIGINAL POSITION. ADJUSTED FWD AND AFT UPPER DOOR ROLLERS AND REMOVED AND REPLACED UPPER AFT LATERAL GUIDE SEAT. PERFORMED MCD INTERNAL, ACTUATING HANDLE TEST. FORCE REQUIRED TO ACTUATE HANDLE WAS 49LBS. RIG CHECK SAT. NO FURTHER DEFECTS NOTED.

Part: UNKNOWN — UNKNOWN · airframe 37,989 hrs · 24,476 cycles

EMERGENCY LIGHT BATTERIES DEPLETED. RE-CHARGED EMERGENCY BATTERIES AND PERFORMED EMERGENCY LIGHT TEST. OPS CHECK SAT

Part: LIGHT — LOOSE (CABIN) · airframe 37,906 hrs · 24,406 cycles

CABIN FWD FLOOR BOARD PHOTO ILLUMINESCENT STRIPS LOOSE SECURED FOWARD PHOTO ILLUMINANT STRIPS

Part: INVERTER — INOPERATIVE (NR 3) · airframe 37,505 hrs · 24,054 cycles

GALLEY AND ROW 3CD EMERGENCY LIGHTS NOT ILLUMINATING. REMOVED AND REPLACED #3 INVERTER. OPS CHECK SAT.

Part: NONE — INOPERATIVE · airframe 37,392 hrs · 23,950 cycles

BULKHEAD EMERGENCY LIGHT INOP. EMERGENCY OP MSG DISPLAYED ON EICAS. R&R #2 BATTERY PACK. EMG LIGHTS STILL REMAINS INOP. R&R BATTERY HOLDER. EMG LIGHT ABOVE SERVICE DOOR STILL REMAINS INOP. R&R EMER LIGHT DC/AC INVERTER #1. OPS CHECK SAT, NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: BATTERY PACK — INOPERATIVE · airframe 37,324 hrs · 23,890 cycles

AFT GALLEY EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED #2 EMERGENCY LIGHT BATTERY. REMOVED AND REPLACED #3 EMERGENCY LIGHT INVERTER. OPS CHECK SAT

Part: LIGHT — INOPERATIVE · airframe 37,167 hrs · 23,746 cycles

EXIT MARKING SIGN INOP IN ROW 3CD. R&R EMERGENCY EXIT SIGN IN ROW 3.  OPS CHECK SAT

Part: LAMP — FLUTTER · airframe 36,856 hrs · 23,543 cycles

SERVICE DOOR EXTERNAL EMERGENCY EXIT LIGHT FLICKERS. REMOVED AND REPLACED SERVICE DOOR EXTERNAL EMERGENCY LIGHT. OPS CHECK SAT

Part: NONE — NONE · airframe 36,672 hrs · 23,295 cycles

BOTH ENGINE FIRE BOTTLE SQUIBS AND APU FIRE BOTTLE SQUIB SAFTIED WRONG. REMOVED AND REPLACED SAFETIES SECURING ENGINE FIRE BOTTLE SQUIBS AND APU FIRE BOTTLE SQUIB

Part: NONE — NONE · airframe 36,357 hrs · 23,032 cycles

MCD VERY DIFFICULT TO OPEN FROM INTERIOR AND EXTERIOR. PERFORMED OPS CHECK OF MAIN CABIN DOOR. DOOR OPERATES NORMALLY. NO FURTHER DEFECTS NOTED AT THIS TIME

Part: CABLE — LOOSE (AILERON SYS) · airframe 35,912 hrs · 22,622 cycles

AILERON CONTROLS LOOSE IN FLIGHT. REMOVED AND REPLACED LT UPPER AILERON CABLE (WING SECTION).

Part: DOUBLER — UNKNOWN · airframe 35,887 hrs · 22,599 cycles

INSPECT THE FWD PRESSURE BULKHEAD TO LOCATE 9 CIRCULAR DOUBLER AND REMOVE DOUBLER. ACCOMPLISH A PERMANENT REPAIR. REMOVED CIRCULAR DOUBLER. DRILLED FASTENER HOLE TO OVERSIZED. TREATED AND PRIMED. RESTOWED TO ORIGINAL FINISH. REINSTALLED REMOVED DOUBLER AS PERMANENT REPAIR.

Part: WINDOW FRAME — CORRODED · airframe 35,887 hrs · 22,599 cycles

LH FWD COCKPIT WINDOW FRAME POSSIBLE CORROSION AFT SIDE. REMOVED CORROSION ON LH FWD COCKPIT WINDOW AT AFT SIDE FRAME, NO DAMAGE FOUND, BLENDED AREAS. FOUND TO BE WITHIN LIMITS.

Part: FLOOR SUPPORT — CORRODED (FRMS 61-64) · airframe 35,887 hrs · 22,599 cycles

RH AFT CABIN FRAMES 61-64, SUSPECTED CORROSION AROUND FLOOR SILL. REMOVED AND REPLACED SILL AT RH FLOOR SUPPORT BETWEEN FR 61-64, STR 15R.

Part: CHANNEL — CORRODED (FRMS 58-61) · airframe 35,887 hrs · 22,599 cycles

CENTER FUSELAGE 4, Y=-479, FRAME 61 TO 58 SIGNS OF CORROSION ON HAT BEAM. REMOVED AND REPLACED GUSSET AT CENTER FUSELAGE 4, 4=-479, FRAME 61-58

Part: FLOOR SUPPORT — CORRODED (FRMS 58-61) · airframe 35,887 hrs · 22,599 cycles

CENTER FUSELAGE 4, Y=0.0, FRAME 61 TO 58, SIGNS OF CORROSION HAT BEAM. REMOVED AND REPLACED GUSSET AT FLOOR SUPPORT BETWEEN FR 59 @ FR 61.

Part: CHANNEL — CORRODED (FRMS 58-60) · airframe 35,887 hrs · 22,599 cycles

CENTER FUSELAGE 4, Y=479, FRAME 60-58 SIGNS OF CORROSION ON HAI BEAM. AFTER EVAL FURTHER HAI BEAM SECTION FOUND TO BE CORRODED IN A 100% ON FASTENERS DRAIN HOLES. REMOVED GUSSET BEAM FROM RH Y=479 AT FR 60-58. INSTALLED GUSSET.

Part: SUPPORT BRACKET — CRACKED · airframe 22,599 hrs

FRM SUPPORT BRACKET CRACKED IN AFT CARGO COMP AT AFT BLK HEAD UPPER SURFACE BETWEEN O1L AND O1R, X=24389.5. REMOVED SHEAR CLIP IN AFT CARGO COMP AFT BLK HEAD, FAB SUPPORT BRACKET, SHEAR CLIP. INSTALLED SHEAR CLIP ON AFT CARGO AT BLK HEAD UPPER SURFACE BETWEEN 01L AND 01R.

Part: STRINGER — CORRODED (FRMS 20-22 S16R) · airframe 35,887 hrs · 22,599 cycles

SERVICE DOOR LOWER STRINGER 16R BETWEEN FRAMES 20 AND 22 RH SHOWS CORROSION EVIDENCE. REMOVED DAMAGE CHANNEL. LOCATED, DRILLED AND INSTALLED NEW CHANNEL AT SERVICES DOOR LOWER CUT OUT BETWEEN FR 20 - FR 22. APPLIED ALODINE, PRIMER AND TOP COAT HOLES AND RIVET HEAD.

Part: SUPPORT BRACKET — CRACKED (AFT CARGO) · airframe 35,887 hrs · 22,599 cycles

FRM SUPPORT BRACKET CRACKED IN AFT CARGO COMP. AT BULK HEAD UPPER SURFACE BETWEEN OIL ANNOIR, X=24389.5. REMOVED SHEAR CLIP IN AFT CARGO COMP. AFT BULK HEAD. FABRICATED SUPPORT BRACKET, SHEAR CLIP MAT USED 7075 T6 .032". INSTALLED SHEAR CLIP ON AFT CARGO AT BULK HEAD UPPER SURFACE BETWEEN OIL AND BIN.

Part: FLOOR SUPPORT — CORRODED (FRMS 61-64) · airframe 35,887 hrs · 22,599 cycles

SIGNS OF CORROSION LH SILL (UPPER FLOOR) BETWEEN FRM 61 AND FRM 64 ABOVE STGR 16. REMOVED DAMAGE SILL, LOCATED AND DRILLED NEW SILL AT LH FLOOR SUPPORT BETWEEN FR 61-64 STR 161. APPLIED ALODINE AND PRIMED HOLES. INSTALLED NEW SILL AND APPLIED TOP COAT.

Part: FLOOR SUPPORT — CORRODED (FRMS 61-64) · airframe 35,887 hrs · 22,599 cycles

SIGNS OF CORROSION LH SILL (UNDER FLOOR) BETWEEN FRM 61 AND FRM 64 ABOVE STGR 16. REMOVED DAMAGE SILL, LOCATED AND DRILLED NEW SILL AT LH FLOOR SUPPORT BETWEEN FR 61-64 STR 16L. APPLIED ALODINE AND PRIME HOLES. INSTALLED NEW SILL AND APPLIED TOP COAT.

Part: SKIN — DENTED (FRAMES 56-57) · airframe 36,340 hrs · 21,641 cycles

FLIGHT 4126 A SMALL DENT WAS DISCOVERED IN THE LEFT HAND AFT FUSELAGE APPROXIMATELY 8" BELOW THE LAST PAX WINDOW. MAINTENANCE REMOVED THE DAMAGE AND PERFORMED A TYPE A1 REPAIR IAW EMB-145 SRM 53-24-01 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: YOKE — CRACKED (NR 1 ENGINE.) · airframe 33,079 hrs · 20,515 cycles

ACFT WAS IN FOR AN A-CHECK WHEN INSPECTION FOUND THE NR 1 ENGINE FORWARD YOKE LOWER MOUNT ATTACH POINT FWD. FITTING CRACKED. MAINTENANCE REMOVED AND REPLACED THE ENGINE YOKE IAW EA 26-2014-063.ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,068 hrs · 19,073 cycles

DURING MX INSPECTION, THE EMERGENCY LIGHTS WERE DISCOVERED INOPERATIVE. MX REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHT BATTERY PACK. OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DISPLAY — FAILED (COCKPIT) · airframe 29,311 hrs · 17,852 cycles

THE CREW REPORTED A BURNING PLASTIC ODOR IN THE COCKPIT FOLLOWED BY THE CAPTAIN`S PFD FAILURE AND PFD CIRUIT BREAKER TRIPPED. MAINTENANCE REPLACED THE CAPTAIN`S PFD. OPS CHECKED GOOD.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,656 hrs · 17,366 cycles

THE CREW REPORTED THAT THE GALLEY DOOR LOWER LT EMERGENCY SIGN WAS INOPERATIVE. MAINTENANCE R & R THE AFFECTED SIGN, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,012 hrs · 16,902 cycles

DURING ROUTINE MAINTENANCE THE EXIT ROW EMERGENCY LIGHTING WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 3 EMERGENCY LIGHT BATTERY. OPS CHECKS WERE GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,264 hrs · 15,651 cycles

DURING ROUTINE MAINTENANCE THE OVERHEAD EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT INVERTER. OPS CHECKS WERE GOOD.

Part: UNKNOWN — MALFUNCTIONED (SPOILER) · airframe 15,092 hrs · 8,171 cycles

ORD-BUF FLT 6102 THE CREW REPORTED A SPOILER FAIL MESSAGE IN FLT. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. THE MESSAGE WENT AWAY AFTER GEAR RETRACTION INTO CLE. MAINTENANCE INSPECTED AND COULD NOT DUPLICATE. RELAYS KO030 AND KO031 WERE REPLACED FOR PRECAUTIONARY PURPOSES. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ACTUATOR — MALFUNCTIONED (HORIZ STAB) · airframe 11,345 hrs · 6,102 cycles

IAH - FLIGHT 2784, AT TAKEOFF THE CREW REPORTED A MAIN PITCH TRIM INOP. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER ACTUATOR, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FADEC — FAULTY (NR 1 ENGINE) · airframe 10,854 hrs · 5,835 cycles

CLE FLIGHT 2031 - THE CREW REPORTED ON CLIMBOUT ENGINE NR 1 FUEL FLOW FLUCTUATED APPROXIMATELY 250 LBS FROM STABLE FLOW RESULTING IN FLUCTUATIONS IN N1 AND ITT. FLUCTUATIONS WENT AWAY AFTER LEVEL OFF IN CRUISE. ON TAXI IN ALSO RECEIVED A RUDDER HARDOVER AND A E1 SHORT DISPATCH MESSAGE. MAINTENANCE INSPECTED AND REPLACED THE NR 1B FADEC. OPERATIONAL CHECKS WERE GOOD.

Part: SWITCH — INOPERATIVE (BLEED AIR SYS) · airframe 10,691 hrs · 5,739 cycles

FLIGHT 2717 - EWR - FLIGHT CREW REPORTED BLEED 1 LOW TEMP IN ICED CONDITION, ANTI-ICE INOP, WING ANTI-ICE FAIL, STAB ANTI-ICE FAIL. FLIGHT CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED BLEED 1 PUSH-BUTTON AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 9,338 hrs · 4,992 cycles

FLIGHT 2353 - EWR - FLIGHT CREW REPORTED BURNING SMELL IN CABIN DURING ENTIRE FLIGHT, BUT IT WAS UNNOTICED IN THE FLIGHT DECK. EWR MX RAN PACKS WITH APU BLEED AND ENGINE BLEEDS AT VARIOUS POWER SET AND INSPECTED NR 2 PACK AREA AND CABIN LIGHTING, BUT COULD NOT DUPLICATE THE SMELL. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)

SAT - DURING MAINTENANCE INSPECTION THE FORWARD EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (A)

Part: FADEC — INOPERATIVE (NR 1 ENGINE)

FLT 0417 - SAT - FLIGHT CREW REPORTED E1 FLUCTUATIONS IN FUEL FLOW-N1-ITT FL270. MX PERSONNEL REMOVED AND REPLACED E1 FADEC 1B AND FPMU. OPERATIONALLY CHECKED SATISFACTORY AND AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE. FADEC 1B: P/N 23078837, S/N BX 161593, TSN:8335, CSN:4504. FPMU: P/N 23077658, S/N SCP05086, TSN:7523, CSN:3995 (A)

Part: UNKNOWN — LEAKING (LT WING) · airframe 7,168 hrs · 3,759 cycles

FLT 0074, FLIGHT CREW REPORTED LEFT WING FUEL LEAK IN FLIGHT. SEALED CLEAR ICE DETECTOR WIRE CONDUIT. OPERATIONALLY AND LEAK CHECK SATISFACTORY. ACFT WAS RELEASED TO RETURN FOR SERVICE. (S)

Part: LINKAGE — OUT OF ADJUST (PAX DOOR) · airframe 7,024 hrs · 3,687 cycles

FLT 0226 - SMF - FLIGHT CREW REPORTED MAIN CABIN DOOR HARD TO OPEN FROM INSIDE. PERSONNEL ADJUSTED HANDLE LINKAGE AND LUBED DOOR, OPERATIONALLY CHECKED SATISFACTORY. AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE.

Part: CONDUIT — CRACKED (ICE DETECTOR) · airframe 6,655 hrs · 3,486 cycles

FLT 0216 - ONT - ON 03/12/2008 FLIGHT CREW REPORTED WHAT APPEARED TO BE FUEL LEAKING FROM LT WING, MX PERSONNEL INSPECTED THE AIRCRAFT AND NO FUEL LEAKS WERE FOUND. ON 03/14/2008 FLT 0010 - ONT - FLIGHT CREW REPORTED AGAIN LT WHEEL WELL FUEL LEAK. MX PERSONNEL CLEANED AND INSPECTED LT SIDE BELLY ACCESS PANEL AND NO DRIPS WERE NOTED AT THAT TIME. ON 0316/2008 FLT 0107 - ONT - FLIGHT CREW REPORTED A FUEL LEAK COMING FROM THE LT WHEEL WELL. MX PERSONNEL RE-INSPECTED AND FOUND ICE DETECTOR CONDUIT CRACKED, MX PERSONNEL REMOVED AND REPLACED ICE DETECTOR CONDUIT OPERATIONALLY AND LEAK CHECKED SATISFACTORY. AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 3,215 hrs · 1,702 cycles

BTV DURING SERVICE CHECK FOUND MAIN DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED BULB IAW EMB145XR AMM 33-50-06. OPS CHECK GOOD.