N12126

Part: SHEAR TIE — CORRODED (FRAME 65) · airframe 41,602 hrs · 25,290 cycles

FWD CARGO DOOR SHEAR CLIP AT FR 65 HAS SIGNS OF CORROSION....REMOVED & REPLACED SHEAR CLIP AT FR 65.

Part: SUPPORT ANGLE — CRACKED (FRAME 23) · airframe 41,602 hrs · 25,290 cycles

CENTER OMEGA BEAM L/H LOWER SPLICE ANGLE SUPPORT BRACKED IS CRACKED AT FRAME 23....REMOVED & REPLACED CENTER OMEGA BEAM LOWER SPLICE ANGLE SUPPORT BRACKET.

Part: SHEAR TIE — CRACKED (FRAME 24) · airframe 41,602 hrs · 25,290 cycles

MAIN CABIN FRAME 24 SHEER CLIP IS CRACKED AT STR 14 R/H....REMOVED AND REPLACED CRACKED SHEER CLIP.

Part: SHEAR TIE — CRACKED (FRAME 24) · airframe 41,602 hrs · 25,290 cycles

MAIN CABIN FRAME 24 SHEER CLIP IS CRACKED AT STR 15 R/H....REMOVED & REPLACED SHEER CLIP AT STR 15 R/H.

Part: FLOOR SUPPORT — CORRODED (FRAMES 29-30) · airframe 41,602 hrs · 25,290 cycles

R/H FLOOR SILL HAVE CORROSION ON UPPER SURFACE BETWEEN FRAME 29 & 30.... REMOVED & REPLACED FLOOR SILL AT FRAME 29 & 30.

Part: FLOOR SUPPORT — CORRODED (FRAMES 28-30) · airframe 41,602 hrs · 25,290 cycles

L/H FLOOR SILL HAVE CORROSION FROM FRAME 28 THRU 30....REMOVED AND REPLACED FLOOR SILL ON L/H SIDE AT FR 28 THRU 30.

Part: FLOOR SUPPORT — CORRODED (FRAMES 37-38) · airframe 41,602 hrs · 25,290 cycles

L/H FLOOR SILL HAVE PITTING CORROSION BETWEEN FRAME 37 AND 38....REMOVED AND REPLACED L/H FLOOR SILL AT FRAME 37 AND 38.

Part: ANGLE — CORRODED (THRESHOLD) · airframe 41,602 hrs · 25,290 cycles

PASSENGER DOOR THRESHOLD AFT NUTPLATE "Z" ANGLE HAVE CORROSION AROUND FASTNER HOLE....REMOVED & REPLACED PASSENGER DOOR THRESHOLD "Z" ANGLE.

Part: FLOOR SUPPORT — CORRODED (FRAMES 24-26) · airframe 41,602 hrs · 25,290 cycles

L/H FLOOR SILL HAVE LIGHT CORROSION BETWEEN FR 24 THRU 26....REMOVED AND REPLACED L/H FLOOR SILL AT FR 24 THRU 26.

Part: THRESHOLD — CORRODED (FRAMES 20-22) · airframe 41,602 hrs · 25,290 cycles

SERVICE DOOR LOWER THRESHOLD HAVE CORROSION BETWEEN FRAME 20 THRU 22....REMOVED AND REPLACED SERVICE DOOR LOWER THRESHOLD

Part: FLOOR SUPPORT — CORRODED (FRAMES 34-35) · airframe 41,602 hrs · 25,290 cycles

R/H FLOOR SILL HAVE CORROSION ON UPPER SURFACE BETWEEN FRAME 34 & 35....REMOVED AND REPLACED R/H FLOOR SEAL AT FRAME 34 & 35.

Part: STRUCTURE — CORRODED (FRAME 22) · airframe 41,602 hrs · 25,290 cycles

R/H OMEGA BEAM STOP SIGN HAVE CORROSION AT FRAME 22....REMOVED AND REPLACED OMEGA BEAM STOP SIGN AT FR 22.

Part: FLOOR SUPPORT — CORRODED (FRAMES 20-23) · airframe 41,602 hrs · 25,290 cycles

L/H FLOOR SILL HAVE CORROSION ON UPPER SURFACE AT FR 20,22 & 23.... REMOVED & REPLACED L/H FLOOR SILL AT FR 20,22 & 23.

Part: SHEAR TIE — CRACKED (FRAME 80) · airframe 41,602 hrs · 25,290 cycles

AFT FUSELAGE INSIDE ACCESS 312AR FRAME 80 SHEER CLIP IS CRACKED BETWEEN STR 5 & 6 LH....REMOVED AND REPLACED SHEER CLIP AT FRAME 80 L/H.

Part: SHEAR TIE — CRACKED (FRAME 80) · airframe 41,602 hrs · 25,290 cycles

AFT FUSELAGE INSIDE ACCESS 312AR FRAME 80 SHEER CLIP IS CRACKED BETWEEN STR 5 & 6 R/H....REMOVED AND REPLACED CRACKED SHEER CLIP AT FRAME 80 R/H

Part: SKIN — GOUGED (FRAME 67) · airframe 41,602 hrs · 25,290 cycles

AFT FUSELAGE EXTERIOR SKIN IS GOUGED INSIDE PYLON ACCESS PANEL 424DB R/H SIDE @ FR 67....REMOVED DAMAGE AND INSTALLED DOUBLER AND FILLER.

Part: SUPPORT FRAME — CORRODED (CARGO BAY) · airframe 41,602 hrs · 25,290 cycles

CARGO DOOR LIFTING AND LOWERING SYS SUPPORT FRAME HAS POSSIBLE CRACK....REMOVED AND REPLACED CARGO DOOR LIFTING AND LOWERING SYSTEM SUPPORT FRAME.

Part: SHEAR TIE — CRACKED (FRAME 72) · airframe 41,602 hrs · 25,290 cycles

SHEER CLIPS ARE CRACKED AT FR 72 ST 14L & ST 15L....REMOVED & REPLACED SHEER CLIPS AT FR 72 ST 14L & ST 15L.

Part: FLOOR SUPPORT — CORRODED (FRAME 46) · airframe 41,602 hrs · 25,290 cycles

SIGNS OF CORROSION ON R/H FLOOR SILL AT FR 46....REMOVED & REPLACED R/H FLOOR SILL AT FR 46.

Part: STRUCTURE — CRACKED (THRUST REVERSER) · airframe 41,602 hrs · 25,290 cycles

#2 ENGINE T/R HAS CRACK ON UPPER I/B SIDE BELOW UPPER T/R DOOR....COMPLIED WITH ETD2018-145-115961

Part: BRACKET — CRACKED (TEMP CONTROL) · airframe 41,602 hrs · 25,290 cycles

ANTI-ROTATION BRACKET ON DUAL TEMP CONTROL VALVE IS CRACKED. REMOVED AND REPLACED ANTI-ROTATION BRACKET ON DUAL TEMP CONTROL VALVE.

Part: MOUNT BRACKET — CRACKED (FRAME 58) · airframe 41,602 hrs · 25,290 cycles

L/H BLEED DUCT MOUNTING BRACKET AT FR 58 IS CRACKED....REMOVED AND REPLACED L/H AFT BLEED DUCT MOUNTING BRACKET AT FR 58.

Part: MECHANISM — CRACKED (FLOOR HATCH) · airframe 41,602 hrs · 25,290 cycles

UNDER FLOOR HATCH MECHANISM IS CRACKED. PREFORMED REPAIR ON UNDER FLOOR HATCH MECHANISM.

Part: SUPPORT FITTING — GOUGED (LT AILERON) · airframe 41,602 hrs · 25,290 cycles

L/H AILERON PCA I/B ROD END SUPPORT FITTING ON L/E OF AILERON O/B HAT BUSHING HOLE IS GOUGED... COMPLIED WITH ETD2018-145-116119.

Part: AIR DUCT — LEAKING (BLEED AIR SYS) · airframe 40,413 hrs · 24,283 cycles

BLEED 1 LEAK IN ICING CONDITION. R&R RT ENGINE BLEED DUCT IN PYLON. OPS AND LEAK CHECK GOOD.

Part: SHUTOFF VALVE — LEAKING (NR 1 BLEED) · airframe 38,052 hrs · 22,323 cycles

NR 1 BLEED LEAK IN FLIGHT. R & R THE PRSOV. OPS CHECKED GOOD

Part: PROXIMITY SWITCH — FAILED (MLG WOW) · airframe 36,905 hrs · 21,361 cycles

LANDING GEAR AIR GROUND FAIL EICAS MESSAGE AT GEAR UP. REMOVED AND REPLACED FWD WOW PROXIMITY SENSOR AND BACKSHELL. OPS CHECKED GOOD.

Part: SCHRADER VALVE — LEAKING (LANDING GEAR) · airframe 36,819 hrs · 21,290 cycles

LANDING GEAR AIR/GROUND FAIL EICAS MSG AFTER DEPARTURE. INSPECTED AND FOUND NITROGEN SCHRADER VALVE TO BE LEAKING NITROGEN. R2 VALVE LEAK CHECK GOOD. PERFORMED GEAR SWING. OPS CHECK GOOD, BEFORE R & R VERIFIED VALVE WAS SEALED AND CLOSED, LEAKING INTERNALLY.

Part: BULB — INOPERATIVE (EXTERIOR LIGHT) · airframe 36,258 hrs · 20,846 cycles

RIGHT FWD WING, FUSELAGE FAIRING EXTERIOR FLOOD LIGHT, NR 4 INOPERATIVE. RELAMPED RT FWD WING, FUSELAGE EXTERIOR EMERGENCY LIGHT. OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,875 hrs · 20,564 cycles

PAX DOOR EMERGENCY FLOOD LIGHT NR 13 INOPERATIVE. R & R PAX DOOR EMERGENCY FLOOD LIGHT NR 13 BULB. OPS CHECK GOOD.

Part: ACM — SEIZED (NR 1) · airframe 34,946 hrs · 19,830 cycles

PAC 2 VALVE CLOSED EICAS MESSAGE FOLLOWED BY SMOKE IN CABIN & COCKPIT. MAINTENANCE INSPECTED AND FOUND NR 1 ACM TO BE SEIZED, REPLACED NR 1 ACM, OPS CHECK GOOD.

Part: SMOKE DETECTOR — INTERMITTENT (LAVATORY) · airframe 34,035 hrs · 19,220 cycles

PILOT REPORTED LAVATORY SMOKE INDICATED INTERMITTENTLY. MX R & R THE LAV SMOKE DETECTOR WITH OPS CHECKED GOOD.

Part: ACM — FROZEN (NR 1) · airframe 33,657 hrs · 18,968 cycles

THE CREW REPORTED AN ELECTRIC BURNING ODOR AND SMOKE IN THE COCKPIT DURING FLIGHT. THE ACFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE ACFT AND FOUND THE NR 1 ACM TO BE FROZEN. MAINTENANCE PLACED THE NR 1 PACK ON MEL, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. MAINTENANCE R & R THE NR 1 ACM, OPERATIONALLY TESTED WITH NO DEFECTS, REMOVED THE MEL, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACM — SEIZED (NR 1) · airframe 33,655 hrs · 18,967 cycles

THE CREW REPORTED AN ELECTRICAL BURNING ODOR AND SMOKE IN THE COCKPIT DURING FLIGHT. MAINTENANCE INSPECTED AND FOUND NR 1 ACM SEIZED.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 33,396 hrs · 18,792 cycles

THE CREW REPORTED A BURNING ELECTRICAL ODOR IN FLIGHT, AFTER A WINDSHIELD HEAT NR 1 FAILED MESSAGE. OPEN

Part: TURBINE — DAMAGED (NR 1 ENGINE) · airframe 33,311 hrs · 18,740 cycles

PILOT REPORTED ENGINE NR 1 OUT AT 25,000' CLIMBING OUT. CREW PERFORMED DIVERSION TO RIC WHERE ACFT LANDED SAFELY. MAINTENANCE R & R NR 1 ENGINE ASSY WITH OPS AND LEAK CHECKS GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIRE LOOP — FAULTY (NR 1 NACELLE) · airframe 32,181 hrs · 18,011 cycles

THE CREW REPORTED ENGINE NR 1 FIRE DETECT FAIL MESSAGE ON EICAS. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE FIRE DETECTION LOOP. OPS CHECKS WERE GOOD.

Part: SEAL — OUT OF POSITION (PAX DOOR) · airframe 29,713 hrs · 16,465 cycles

CREW REPORTED THE MAIN CABIN DOOR DIFFICULT TO OPEN AND/OR CLOSE. MX REPOSITIONED THE DOOR SEAL AND CLEANED AND LUBED WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 29,606 hrs · 16,401 cycles

CREW REPORTED A LOSS OF PRESSURIZATION AT FL 280. PERFORMED AN EMERGENCY DESCENT, DECLARED EMERGENCY, AND LANDED SAFELY. R & R THE DIGITAL PRESSURE CONTROLLER WITH OPS CHECKS SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRUCTURE — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 29,331 hrs · 16,227 cycles

DURING C-CHECK CORROSION AROUND NUTPLATES ON FWD LOWER CORNER OF BAGGAGE DOOR. MX REPAIRED CARGO DOOR LOWER FORWARD NUTPLATES IAW EC5330-01293. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CRACKED (ZONE 200) · airframe 29,331 hrs · 16,227 cycles

DURING C-CHECK, FRAME 10 CRACKED UNDER RT DV WINDOW. MX R & R FRAME 10 AT RT UNDER DV WINDOW IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE HARNESS — FAULTY (CABIN) · airframe 27,365 hrs · 14,967 cycles

BURNING ODOR REPORTED FROM CEILING LIGHT 16A. REMOVED AND REPLACED SEAT 16A ELECTRICAL WIRE HARNESS ASSY WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RELAY — FAILED (CABIN PRESSURE) · airframe 26,184 hrs · 14,197 cycles

AT FL370. CABIN INDICATED 8800 & TURNED AMBER QUICKLY FOLLOWED BY AN INCREASE IN CABIN ALT TO 10,500 FT. FLIGHT DIVERTED. MX R & R 2 RELAY'S K0412 AND K0264, OPS CHECKED GOOD AND ACFT RELEASED AND RETURNED TO SERVICE.

Part: PITOT LINE — CONTAMINATED (PITOT/STATIC SYS) · airframe 23,294 hrs · 12,333 cycles

FLIGHT 2293 IAH TO RSW THE CAPTAIN LOST NR 1 AIRSPEED, HE SLAVED TO THE NR 2 AIRSPEED WHICH ALSO WENT AWAY FOR TWO MINUTES WHEN THE AIRSPEED INDICATION RETURNED. THE AIRCRAFT DIVERTED TO BHM WHERE MAINTENANCE INSPECTED THE AIRCRAFT, DRAINED WATER FROM THE PITOT STATIC LINES, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SENSOR — FAULTY (NR 1 ENGINE) · airframe 22,434 hrs · 11,863 cycles

CLE FLT 2463 THE CREW REPORTED A HIGH VIBRATION INDICATION ON THE NR 1 HP ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT TAXIED BACK TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE COMPRESSOR VIBRATION SENSOR. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,213 hrs · 11,194 cycles

FLIGHT 2993 - EWR - FLIGHT CREW REPORTED EXIT EMERGENCY LIGHT INOP. EWR MX REMOVED AND REPLACED EMERGENCY LIGHT AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: CONTROL UNIT — FAULTY (HORIZ STAB) · airframe 20,401 hrs · 10,747 cycles

IAH FLT 3147 THE CREW REPORTED A MAIN PITCH TRIM INOP MESSAGE ON CLIMB. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE HORIZONTAL STAB CONTROL UNIT (HSCU). OPERATIONAL CHECKS WERE GOOD.

Part: UNKNOWN — VIBRATION (AC PACK) · airframe 20,062 hrs · 10,564 cycles

IAH - FLIGHT 2444, THE CREW REPORTED A VIBRATION COMING FROM PACK 2. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, PERFORMED GVI OF THE NUMBER TWO PACK, OPERATIONAL AND LEAK CHECKED ALL WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED TO SERVICE.

Part: A/C PACK — MALFUNCTIONED (NR 1) · airframe 20,060 hrs · 10,563 cycles

IAH/PIT- PACK 1 OVERLOAD DURING FLIGHT. A/C DIVERTED TO TYS. TYS PLACED PACK 1 ON MEL.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 19,700 hrs · 10,374 cycles

RIC - DURING ROUTINE INSPECTION, MX FOUND FRONT WING FUSELAGE EMERGENCY LIGHT INOPERATIVE. MX REMOVED AND REPLACED NR 1 LIGHT BATTERY CHARGER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 19,082 hrs · 10,041 cycles

SHV - DURING C-CHECK VISUAL INDICATION OF CRACKS AROUND RIVET HEADS ON EXTERNAL FUSELAGE SKIN RT SIDE BETWEEN FRAMES 72-80. MAINTENANCE REPAIRED EXTERNAL FUSELAGE SKIN RT SIDE BETWEEN FRAMES 72-80 IAW EC5330-01980. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 19,082 hrs · 10,041 cycles

SHV - DURING C-CHECK FRAME 68 IS CRACKED AT CARGO DOOR ROD HOLD OPEN SUPPORT. MAINTENANCE REPAIRED FRAME 68 AT CARGO DOOR ROD HOLD OPEN SUPPORT IAW EC5330-01719 REV B. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 19,082 hrs · 10,041 cycles

SHV - DURING C-CHECK RT UPPER SEAT TRACKS SUPPORT HAS CORROSION (LEVEL 2) BETWEEN FRAMES 47-52. MAINTENANCE REPAIRED RT UPPER SEAT TRACKS SUPPORT BETWEEN FRAMES 47-52 IAW EC5320-01481. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 19,082 hrs · 10,041 cycles

SHV - DURING C-CHECK VISUAL INDICATION OF CRACKS AROUND RIVET HEADS ON EXTERNAL FUSELAGE SKIN LT SIDE BETWEEN FRAME 72-80. MAINTENANCE REPAIRED EXTERNAL FUSELAGE SKIN ON LT SIDE BETWEEN FRAME 72-80 IAW EC5330-01980. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,082 hrs · 10,041 cycles

SHV - DURING C-CHECK LT UPPER SEAT TRACKS SUPPORT HAS CORROSION (LEVEL 2) BETWEEN FRAMES 47-52. MAINTENANCE REPAIRED LT UPPER SEAT TRACKS SUPPORT BETWEEN FRAMES 47-52 IAW EMB-145 SRM 51-21-06 AND EC5320-01485. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — WORN (AILERON) · airframe 19,082 hrs · 10,041 cycles

SHV - DURING C-CHECK LT AILERON PCA ATTACHMENT BRACKET HAS MIGRATING HAT BUSHING. MAINTENANCE REMOVED AND REPLACED LT AILERON PCA ATTACHMENT BRACKET HAT BUSHINGS IAW EC5740-01152 REV B AND REMOVED AND REINSTALLED LT AILERON IAW AMM 27-10-00. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: VALVE — INOPERATIVE (NR 2) · airframe 18,225 hrs · 9,591 cycles

FLIGHT 2036 - ALB - FLIGHT CREW REPORTED BLEED 1 AND 2 OVER TEMP IN ICING CONDITIONS. CREW DIVERTED FLIGHT TO ALB AND LANDED ACFT UNEVENTFULLY. MX REMOVED AND REPLACED NR 2 FAN AIR VALVE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: VALVE — INOPERATIVE (NR 1) · airframe 18,225 hrs · 9,591 cycles

FLIGHT 2036 - ALB - FLIGHT CREW REPORTED BLEED 1 AND 2 OVER TEMP IN ICING CONDITIONS. CREW DIVERTED FLIGHT TO ALB AND LANDED ACFT UNEVENTFULLY. MX REMOVED AND REPLACED NR 1 FAN AIR VALVE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: FITTING — GOUGED (HORIZ STAB) · airframe 9,410 hrs · 4,920 cycles

TYS, DURING A SCHEDULED INSPECTION THE HORIZONTAL STAB WAS FOUND WITH A GOUGED BUSHING RACE AT THE RIGHT OUTBOARD FLANGE. MAINTENANCE REAMED BOTH INBOARD AND OUTBOARD HOLES OF THE RIGHT HORIZ STAB FITTING, TREATED AND INSTALLED OVERSIZE BUSHINGS IAW IC2006-145/4251 AND SRM 55-10-02.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 8,544 hrs · 4,461 cycles

IAH - DURING MAINTENANCE INSPECTION, THE EXIT SIGN ABOVE THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 8,533 hrs · 4,456 cycles

GALLEY CEILING EMERGENCY LIGHT INOP. REMOVED AND REPLACED GALLEY CEILING EMERGENCY LIGHT IAW EMB 145XR AMM 33-50-04. OPS CHECK GOOD.

Part: HOSE — RUPTURED (HYD SYSTEM) · airframe 5,660 hrs · 2,961 cycles

NR 1 ENG, ENGINE DRIVEN HYD PUMP PRESSURE LINE RUPTURED. THE LOCATION OF THE RUPTURE WAS ABOUT THE MIDDLE OF THE LINE. MAINTENANCE REMOVED AND REPLACED PRESSURE LINE AND ENGINE DRIVEN HYDRAULIC PUMP. HYD SYSTEM WAS SERVICED, OPS & LEAK CHECKED GOOD. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE.

Part: ODOR — DETECTED (CABIN)

IAH FLIGHT NR 2039, THE CREW REPORTED A STRONG BURNING ODOR WHEN THE ANTI-ICE SYSTEM WAS ON. MAINTENANCE INSPECTED AND PERFORMED ANTI-ICE TEST. NO DEFECTS OR EVIDENCE OF A BURNING ODOR. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ODOR — DETECTED (COCKPIT) · airframe 3,412 hrs · 1,800 cycles

GSO-CO3472, CREW REPORTED, "SMOKE SMELL IN COCKPIT DURING DESCENT." MAINTENANCE IN GSO INSPECTED THE AIRCRAFT. NO EVIDENCE OF SMOKE SMELL. ALL SYSTEMS NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: CHARGER — INOPERATIVE (CABIN)

CLE FLIGHT 2048 THE CREW REPORTED THE EMERGENCY LIGHT WAS INOPERATIVE ON THE LEFT SIDEWALL. MAINTENANCE INSPECTED AND REPLACED THE NR 3 EMERGENCY LIGHT BATTERY AND CHARGER. OPERATIONAL CHECKS WERE GOOD.

Part: FUSE — BLOWN (EMERGENCY LIGHT)

DURING PREFLIGHT INSPECTION THE CREW FOUND THE LEFT EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK FUSE AND OPERATIONALLY TESTED THE LIGHTING SYSTEM.