N13949

Part: PANEL — BLOCKED (BLEED AIR SYS) · airframe 31,496 hrs · 23,642 cycles

TYS - A/C RETURNED TO BASE AFTER LEAVING EWR TO BNA WHEN CREW HAD A ECIAS MESSAGE OG THE BLEED 2 OVER TEMP IN ICING CONDITIONS. MAINTENANCE FOUND THE ACESS PANEL 414CB LT PANEL TO THE FAN AIR VALVE/PRE COOLER INSTALL ON THE RT SIDE AND THE 424CB RT PANEL TO THE FAN AIR VALVE /PRE-COOLER INSTALL ON THE LEFT SIDE, CAUSING BOTH PRE COOLERS TO BE BLOCKED. RE-INSTALL PANELS IN THE CORRECT POSITION. PERFORMED OPS TEST OF THE AIR BLEED SYSTEM IAW EMB 145 MM 36-00-00. OPS CHECK GOOD AND WAS RELEASED.

Part: UNKNOWN — ODOR (CABIN) · airframe 30,180 hrs · 22,677 cycles

EN ROUTE TO GSO THE CREW REPORTED A BURNING SMELL IN FRONT OF THE CABIN. THE AIRCRAFT DIVERTED TO MOB WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED AN INSPECTION OF THE AIRCRAFT, HIGH-POWER ENGINE RUNS AND OPERATES THE AIR CONDITIONING PACKS HOWEVER THE CONDITION COULD NOT BE DUPLICATED.

Part: POTENTIOMETER — FAULTY (COCKPIT) · airframe 29,890 hrs · 22,454 cycles

FLIGHT 2488 - EWR - FLIGHT CREW REPORTED PFD DIM/BRT CONTROL INTERMITTENT BRIGHT/DIM, PRODUCING ELECTRICAL ODOR. EWR MX REMOVED AND REPLACED BRIGHT/DIM POTENTIOMETER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 29,587 hrs · 22,232 cycles

TYS - DENT AT EXTERNAL FUSELAGE FRM 20 STR 1-3L. FABRICATED AND INSTALLED DOUBLER AND FILLER AT STR 1L AND 1R, AND STR 4L AND 5L. PRIMED AND PAINTED REPAIR.

Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 29,587 hrs · 22,232 cycles

TYS - WINDSHIELD FRAME CORRODED UNDER NUT PLATE RT SIDE LOWER FRAME. CUT OUT DAMAGED SECTION OF WINDSHIELD FRAME ON RT SIDE. FABRICATED FILLER AND INSTALLED FILLER AND NUT PLATE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 29,587 hrs · 22,232 cycles

TYS - RT EXTERNAL SKIN FWD OF FRM 75 BETWEEN STR 1R AND 2R HAS DEEP BLEND FROM PREVIOUS REPAIR. INSTALLED INTERNAL DOUBLER AND EXTERNAL PATCH. PERFORMED EDDY CURRENT AND NO CRACKS NOTED.

Part: HOSE — WORN (APU) · airframe 29,211 hrs · 21,944 cycles

MCI - FLIGHT 3026, THE CREW REPORTED A STRONG FUEL SMELL ON TAKE OFF ROLL. THE CREW ABORTED TAKE OFF AND RETURNED TO THE GATE WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE APU ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 9-22-10 IAH MAINTENANCE REMOVED AND REPLACED APU DRAIN LINE, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DRAIN LINE — CRACKED (APU) · airframe 29,218 hrs · 21,950 cycles

CHS - IAH - FLIGHT DIVERTED TO TYS BECAUSE OF FUEL SMELL IN COCKPIT AFTER TAKEOFF. TYS MX VERIFIED THE FUEL SMELL COMING FROM APU. APU PLACED ON MEL LP--2625735. REMOVED AND REPLACED APU FUEL DRAIN HOSE, LEAK CHECK GOOD.

Part: APU — ODOR (APU BAY) · airframe 29,192 hrs · 21,932 cycles

CHS - IAH - FLIGHT DIVERTED TO TYS BECAUSE OF FUEL SMELL IN COCKPIT AFTER TAKEOFF. TYS MX VERIFIED THE FUEL SMELL COMING FROM APU. APU PLACED ON MEL LP--2625735. SDR FILED OPEN PENDING CORRECTIVE ACTION.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 29,152 hrs · 21,900 cycles

CLE FLT 2297 CREW REPORTED FUEL SMELL AFTER TAKEOFF. CREW REPORTED SMELL DISSIPATED AFTER APU SHUT-DOWN. IN CLE MAINTENANCE INSPECTED AND FOUND NO FUEL SMELL. OPERATIONAL CHECKS GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 29,129 hrs · 21,883 cycles

IAH - FLIGHT 3079, DURING POST FLIGHT INSPECTION THE CREW REPORTED THE EMERGENCY EXIT SIGN ON THE RIGHT SIDE TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FIVE EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HYDRAULIC LINE — LEAKING (LT MLG) · airframe 28,597 hrs · 21,482 cycles

CLE FLT 2243 THE CREW REPORTED A HYDRAULIC SYSTEM 1 FAIL DURING CLIMB. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE HYDRAULIC HOSE ON THE LEFT MAIN GEAR ACTUATOR. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,977 hrs · 19,502 cycles

AIRCRAFT IN FOR A ROUTINE INSPECTION WHEN THE EMERGENCY LIGHT IN THE CEILING PANEL AT ROW 12 WAS FOUND INOP. MAINTENANCE REMOVED AND REPLACED THE LIGHT BULB IAW EMB 145 AMM 33-50-08. OPS CHECK GOOD AND WAS RELEASED.

Part: CONTACTOR — MALFUNCTIONED (ELECTRICAL) · airframe 24,235 hrs · 18,250 cycles

IAH - FLIGHT 2350, THE CREW REPORTED THAT AT FL360, THE AIRCRAFT LOST ALL ELECTRICAL POWER FOR 10 SECONDS, POWER RETURNED FOR 2 SECONDS, WAS INTERMITTENT FOR 2 MINUTES WITH T/O CONFIG, AUTOPILOT, FLAPS, STALL WARNINGS. THE POWER WAS FINALLY RESTORED AFTER THREE MINUTES. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ESSENTIAL BUSS CONTACTOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (A)

Part: COMPUTER — INTERMITTENT (COCKPIT) · airframe 24,222 hrs · 18,241 cycles

FLIGHT 2882 - EWR - FLIGHT CREW REPORTED ELECTRICAL POWER LOSS IN FLIGHT AT 35,000 FT WITH A LOUD THUMP, MFD, PFD, EICAS ALL RED "X", AP FAIL. STALL TEST LIGHT ILLUMINATED BUT EVERYTHING CAME BACK A FEW SECONDS LATER. CREW LANDED ACFT AS PLANNED WITHOUT INCIDENT. EWR MX REMOVED AND REPLACED NR 1 INTEGRATED COMPUTER IC600 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (S)

Part: ACTUATOR — LEAKING (NLG DOOR)

FLIGHT 3082 - DIVERTED FROM IAH - HYD IN SYSTEM 1 LEAKED, HYD SYSTEM I FAILURE. MX REMOVED AND REPLACED NOSE LANDING GEAR DOOR ACTUATOR AND HOSES IAW EMB 145 32-33-03. OPS CHECK GOOD AND LEAK CHECK GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (A)

Part: FRAME — CRACKED (FUSELAGE) · airframe 22,898 hrs · 17,357 cycles

TYS MOD - DURING ROUTINE MX FOUND FRAME 81 CRACKED AT THE 6 O'CLOCK POSITION. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND A/C WAS RELEASED FOR SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,307 hrs · 16,950 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,086 hrs · 16,037 cycles

CLE FLIGHT 2414 - THE CREW REPORTED THE RIGHT AISLE PATH EMERGENCY LIGHT STRIP WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 20,802 hrs · 15,824 cycles

IAH - FLIGHT 2824, THE CREW REPORTED A 115VAC OFF BUSS INDICATION WITH A BURNING SMELL IN THE COCKPIT. MAINTENANCE INSPECTED THE AIRCRAFT AND COULD NOT DUPLICATE ANY DISCREPANCY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 20,903 hrs · 15,897 cycles

BNA - DURING MAINTENANCE INSPECTION THE NUMBER TWO EMERGENCY LIGHT BATTERY WAS FOUND TO BE NOT HOLDING A CHARGE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BATTERY PACK, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SENSOR — INTERMITTENT (LANDING GEAR) · airframe 20,350 hrs · 15,475 cycles

GRK - FLIGHT 2963, THE CREW REPORTED A LANDING GEAR AIR GROUND FAILURE. THE CREW RESET THE SYSTEM SUCCESSFULLY AND THE AIRCRAFT LANDED AT GRK WITHOUT INCIDENT. ON FLIGHT 2114 THE DISCREPANCY RETURNED, AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE RIGHT HAND WEIGHT ON WHEELS PROXIMITY SWITCH, OPERATIONALLY CHECKED WITH NO EFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 20,332 hrs · 15,458 cycles

DURING A CURRENT 1C/5C INSPECTION CORROSION WAS FOUND ON BOTH ENDS OF A COMPOSITE CROSSMEMBER FLOOR SUPPORT AT FR PANEL 231FF. MAINTENANCE REPAIRED THE OMEGA BEAM AT THE DESIGNATED AREA IAW SRM 53-00-10.REMOVED AND REPLACED THE RAMP ANGLE IAW SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: WIRE HARNESS — BURNED (CABIN LIGHTS) · airframe 20,318 hrs · 15,448 cycles

FLT NR 1271 ABOVE SEAT 15A PASSENGER REPORTED SEEING SMOKE AND BURNING SMELL. REMOVED AND REPLACED SIDEWALL LIGHT HARNESS IAW EMB145 IPC 33-21-06. OPS CHECK GOOD IAW EMB145 AMM 33-21-00.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 20,255 hrs · 15,401 cycles

DURING SERVICE/ROUTINE CHECK, FOUND EMERGENCY LIGHT FWD AISLE STRIP INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY NR 2 IAW EMB-145 AMM 33-50-04. OPS CHECK GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,231 hrs · 15,382 cycles

BTV DURING ROUTINE/SERVICE CHECK FOUND EMERGENCY EXIT LIGHT ON CEILING AT 1A INOP. ALSO EMERGENCY EXIT LIGHT ON COCKPIT STEP INOP. REMOVED AND REPLACED NR 3 EMERGENCY LIGHT INVERTER IAW AMM 33-50-11. OPS CHECK GOOD.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 19,580 hrs · 14,879 cycles

DURING AC ROUTINE MAINTENANCE, MX FOUND REAR AND FRONT FLOOR EMERGENCY LIGHTS INOP. MX FOUND CONNECTOR PLUG AT INVERTER NR 6 DISCONNECTED. MX RECONNECTED CONNECTOR PLUG AND PERFORMED OPERATIONAL TESTS SUCCESSFULLY. AC WAS APPROVED TO RETURN TO SERVICE.

Part: ELEVATOR — OUT OF RIG · airframe 16,933 hrs · 12,768 cycles

IAH - FLIGHT 2703, THE CREW REPORTED THAT THEY HAD INSUFFICENT TRAVEL ON THE ELEVATOR FOR ROTATION. THE CREW ABORTED THE TAKEOFF WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, AND ELEVATOR RIGGING WITH NO DEFECTS BEING NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACM — SEIZED (NR 1) · airframe 16,243 hrs · 12,212 cycles

CREW REPORTED STRONG ODOR OF MELTING RUBBER PREVALENT WITHIN A/C CABIN DURING PACK USAGE. MX INSP AND RELEASED A/C IAW MEL 21-51-00/1. SUPPLEMENT TO FOLLOW. MX REPLACED NR 1 ACM. OPS CHECKS GOOD.

Part: COMPUTER — INACCURATE (NAVIGATION) · airframe 16,195 hrs · 12,169 cycles

FLT 2609 - RIC - AFTER TAKEOFF, THE CREW REPORTED THAT HEADING WAS NOT MATCHING COMPASS IN DG AND SLVD MODE. CREW RETURNED TO RIC AND LANDED WITHOUT INCIDENT. RIC MAINTENANCE UPDATED NAV DATA BASE. OPERATIONAL CHECK WAS PERFORMED SUCCESFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: HOLDER — CRACKED (FLASHLIGHT) · airframe 16,119 hrs · 12,112 cycles

DURING ROUTINE MAINTENANCE, THE F/A`S FLASHLIGHT HOLDER/CHARGER WAS FOUND CRACKED AND THE FLASHLIGHT WOULD NOT STAY LOCKED ONTO THE HOLDER. MAINTENANCE REPLACED THE FLASHLIGHT HOLDER. OPERATIONAL CHECKS WERE GOOD.

Part: DUCT — RUPTURED (LT ENGINE) · airframe 15,600 hrs · 11,703 cycles

IAH - FLIGHT 2654, ON TAKEOFF THE CREW REPORTED A NUMBER ONE ENGINE OVERTEMP AND FIRE WARNING. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE 13TH STAGE ENGINE BLEED TUBE TO BE RUPTURED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BLEED TUBE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THIS PART IS NOT SERIALIZED, AND TIMES ARE NOT AVAILABLE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 14,827 hrs · 11,131 cycles

CREW REPORTED THE LAST THREE ROWS OF AISLE EMERGENCY LIGHTING INOPERATIVE. FOUND LOOSE CONNECTION ON THE LIGHTS AND RECONNECTED. ITEM REPEATED ON THE NEXT FLIGHT AND MAINTENANCE REPLACED THE NUMBER 6 EMERGENCY INVERTED. OPS CHECK GOOD.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 14,689 hrs · 11,015 cycles

DURING SERVICE AND ROUTINE INSPECTION ON RON BTV, MAINTENANCE FOUND SEVERAL FORWARD CABIN EMERGENCY LIGHTS AND LT HAND FORWARD EXTERNAL EMERGENCY LIGHTS INOPERATIVE IN ALL MODES. RESECURED CONNECTOR TO NR 1 EMERGENCY LIGHT BATTERY AS REQUIRED, OPS CHECKED GOOD IAW EMB145 AMM 33-50-00. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — LOOSE (EMERGENCY LIGHTS) · airframe 146,889 hrs · 11,015 cycles

EWR FLIGHT 2167- CREW REPORTED THE EMERGENCY LIGHT IN FRONT OF SEAT 3BC WAS INOPERATIVE. MAINTENANCE INSPECTED THE LIGHT ASSEMBLY AND RESECURED THE ELECTRICAL CONNECTORS AND THE EMERGENCY LIGHT OPERATIONAL CHECK WAS GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 14,658 hrs · 10,992 cycles

EMERGENCY LIGHTS BELOW COCKPIT DOOR AND ABOVE MAIN CABIN DOOR INOP. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT INVERTER AS PER THE EMB AMM 33-50-11. EMERGENCY LIGHTS OPERATIONALLY CHECKED NORMAL AND AIRCRAFT WAS RELEASED.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 14,436 hrs · 10,817 cycles

CREW REPORTED THAT THE EMERGENCY LIGHTS WILL NOT TURN ON. MAINTENANCE INSPECTED AND REMOVED AND REPLACED THE POSITION 6 EMERGENCY LIGHT INVERTER. ALL OPERATIONAL CHECKS WERE GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 14,428 hrs · 10,811 cycles

DURING PRE-FLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT BATTERY CHARGER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 14,374 hrs · 10,765 cycles

MCI LOG SQUAWK FWD OVER THE WING AISLE EXIT LOCATOR SIGN INOP. REMOVED AND REPLACED NR 4 BATTERY POWER SUPPLY IAW EMB 145 AMM 33-50-04. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 14,369 hrs · 10,760 cycles

FLIGHT NR 3233, THE CREW REPORTED THAT THE RT SIDE EMERGENCY EXIT LIGHT WILL NOT ILLUMINATE. MAINTENANCE INSPECTED AND RESET THE EMERGENCY LIGHT SYSTEM. ALL OPERATIONAL CHECKS WERE GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

DURING ROUTINE MAINTENANCE THE EMERGENCY LIGHT IN AISLE AT ROW 12 WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT BULB AT ROW 12 EMERGENCY LIGHT. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (ROW 15-17)

DURING ROUTINE MAINTENANCE THE EMERGENCY FLOOR LIGHT STRIP WAS INTERMITTENT AT ROW 15-17. MAINTENANCE REPLACED THE FLOOR LIGHT STRIP AT ROW 15-17. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — MALFUNCTIONED (ROW 12)

IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY LIGHTS FROM ROW 12 AFT WERE INOPERATIVE. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY LIGHTS WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

CREW REPORTED, SERVICE DOOR EMERGENCY LIGHT BULB BURNED OUT. MAINTENANCE REMOVED AND REPLACED LIGHT BULB IAW EMB145 AMM 33-50-06. OPS CHECKED GOOD.

Part: ENGINE — FAILED (RIGHT)

EWR FLT 2247, THE CREW REPORTED A LOUD BANG FROM NR 2 ENGINE, ITT WENT TO 900 CELSIUS. POWER WAS REDUCED, TEMP STAYED AT 900 CELSIUS FOR 5 SECONDS, THEN ENGINE NR 2 FLAMED OUT. AIRCRAFT DIVERTED TO CLE AND LANDED WITHOUT FURTHER DIFFICULTY. NR 2 ENGINE WAS REPLACED.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHT)

CREW REPORTED, "EMERGENCY EXIT SIGN BACKLIGHT INOPERATIVE ABOVE SEAT 1A. MAINTENANCE REMOVED AND REPLACED NR 1 EMERGENCY EXIT LIGHT BATTERY PACK. IAW EMB145 AMM #33-50-04. OPS.CHECKED GOOD.

Part: SHEAR TIE — CORRODED · corrosion level 2 · airframe 11,328 hrs · 8,340 cycles

DURING C-CHECK SHEAR CLIPS WHERE FOUND TO HAVE CORROSION BETWEEN FRAMES 56 TO 60 AND STRINGERS 21 LEFT AND 20 RIGHT. MAINTENANCE REMOVED AND REPLACED AFFECTED SHEAR CLIPS IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,328 hrs · 8,340 cycles

DURING C-CHECK SHEAR CLIPS WHERE FOUND TO HAVE CORROSION BETWEEN FRAMES 67 TO 69 AT STRINGERS 21 LT TO 20 RT. MAINTENANCE REMOVED AND REPLACED AFFECTED SHEAR CLIPS IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BUTT STRAP — CORRODED (LAVATORY) · corrosion level 2 · airframe 11,328 hrs · 8,340 cycles

DURING C-CHECK CENTER BUTTSTRAP AT LAV WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED AFFECTED BUTTSTRAP IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BRACKET — CORRODED (CARGO) · corrosion level 2 · airframe 11,328 hrs · 8,340 cycles

SHV DURING C CHECK CORROSION WAS FOUND ON PULLEY BRACKETS BETWEEN FRAMES 67 TO 68, BETWEEN STRINGERS 21 LEFT AND 20 RIGHT. MAINTENANCE REMOVED AND REPLACED AFFECTED BRACKET IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: STRINGER — CORRODED (CABIN) · corrosion level 2 · airframe 11,328 hrs · 8,340 cycles

SHV DURING C CHECK STRINGER 21 RIGHT WAS FOUND TO HAVE CORROSION BETWEEN SPLICES AT FRAMES 52 TO 53 AND FRAMES 60 TO 61. MAINTENANCE REMOVED AND REPLACED AFFECTED STRINGER IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,328 hrs · 8,340 cycles

SHV DURING C-CHECK SHEAR CLIPS WHERE FOUND TO HAVE CORRSION BETWEEN FRAMES 61 TO 66 AT STRINGERS 21 LEFT TO 20 RIGHT. MAINTENANCE REMOVED AND REPLACED AFFECTED SHEAR CLIPS IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: STRINGER — GOUGED · airframe 11,328 hrs · 8,340 cycles

SHV DURING C CHECK REPAIR DOUBLER ON T REINFORCEMENT ON STRINGER 19 RIGHT BETWEEN FRAMES 52 TO 53 WAS FOUND GOUGED. MAINTENANCE REMOVED DAMAGED AND PERFORMED A DOUBLER REPAIR IAW EMB SRM 53-24-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: STRINGER — GOUGED · airframe 11,328 hrs · 8,340 cycles

SHV DURING C CHECK REPAIR DOUBLER ON T REINFORCEMENT ON STRINGER 19 LEFT WAS FOUND TO HAVE A GOUGE BETWEEN FRAMES 52 TO 53. MAINTENANCE REMOVED DAMAGE AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BUTT STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,328 hrs · 8,340 cycles

SHV DURING C-CHECK CENTER BUTTSTRAP WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 59 TO 61. MAINTENANCE REMOVED AND REPLACED AFFECTED BUTTSTRAP IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 11,328 hrs · 8,340 cycles

DURING C-CHECK THE CENTER FLOORBEAM SUPPORT COLUMN WAS FOUND TO HAVE CORROSION AT FRAME 60. MAINTENANCE REMOVED AND REPLACED AFFECTED COLUMN IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 11,328 hrs · 8,340 cycles

SHV- DURING C CHECK THE AFT EXTERNAL FRAME ON CARGO DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FRAME IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SKIN — CORRODED (CARGO) · corrosion level 2 · airframe 11,328 hrs · 8,340 cycles

SHV- DURING C CHECK CORROSION WAS FOUND ON CARGO FLOOR SKIN BETWEEN FRAMES 68 AND 73 AT STRINGERS 21L AND 20R. MAINTENANCE REMOVED AND REPLACED AFFECTED SKIN IAW CONTINENTAL EXPRESS EA 5330-01061. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SILL — CORRODED (CABIN) · corrosion level 2 · airframe 11,328 hrs · 8,340 cycles

SHV- DURING C CHECK THE SERVICE DOOR AFT SILL WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 22 AND 23. MAINTENANCE REMOVED DAMAGE AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5320-01089. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE

Part: SKIN — CORRODED (CABIN) · corrosion level 2 · airframe 11,328 hrs · 8,340 cycles

SHV DURING C CHECK CORROSION WAS FOUND ON THE CABIN UNDERFLOOR SKIN BETWEEN FRAMES 50 AND 61. MAINTENANCE REMOVED AND REPLACED AFFECTED SKIN IAW CONTINENTAL EXPRESS EA 5330-01061. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SKIN — CORRODED (CARGO) · corrosion level 2 · airframe 11,328 hrs · 8,340 cycles

SHV DURING C CHECK CORROSION WAS FOUND ALONG CARGO FLOOR SKIN BETWEEN FRAMES 65 TO 68 AT STRINGERS 21L AND 2OR. MAINTENANCE REMOVED AFFECTED SKIN IAW CONTINENTAL EXPRESS EC 5330-01234. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: CLIP — CORRODED · corrosion level 2 · airframe 11,328 hrs · 8,340 cycles

SHV DURING C CHECK CORROSION WAS FOUND ON SHEAR CLIP AT FRAME 65 BETWEEN STRINGERS 20R AND 19R. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CLIP IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BUTT STRAP — CORRODED · corrosion level 2 · airframe 11,328 hrs · 8,340 cycles

DURING C-CHECK CORROSION WAS FOUND ON CENTER BUTT STRAP BETWEEN FRAMES 59 AND 61. MAINTENANCE REMOVED AND REPLACED AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SKIN — CORRODED (CARGO) · corrosion level 2 · airframe 11,328 hrs · 8,340 cycles

SHV DURING C CHECK CORROSION WAS FOUND ON CARGO FLOOR SKIN BETWEEN FRAMES 61 AND 65 AT STRINGERS 21L TO 20R. MAINTENANCE REMOVED AND REPLACED AFFECTED SKIN IAW CONTINENTAL EXPRESS EC 5330-01234 AND EA 5330-01061. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: STRAP — CRACKED (CABIN) · airframe 11,328 hrs · 8,340 cycles

SHV-DURING C CHECK A SPLICE ANGLE ON THE CENTER BEAM TO BUTTSTRAP BETWEEN FRAMES 14 AND 16 WAS FOUND CRACKED. MAINTENANCE PERFORMED AN ANGLE SPLICE REPAIR TO AFFECTED BEAM IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: STRAP — CORRODED (CABIN) · corrosion level 2 · airframe 11,328 hrs · 8,340 cycles

DURING C-CHECK THE FOWARD DIGITAL ON LEFT HAND OMEGA BEAM WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A SPLICE REPAIR IAW CONTINENTAL EXPRESS EC 5320-01074. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: NUT PLATE — CORRODED (CABIN) · corrosion level 2 · airframe 11,328 hrs · 8,340 cycles

SHV- DURING C-CHECK THE PASSENGER DOOR THRESHOLD MOUNTING BRACKETS NUT PLATES WERE FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKETS IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: GUSSET — CORRODED (CABIN) · corrosion level 2 · airframe 11,328 hrs · 8,340 cycles

SHV-DURING C CHECK THE AFT FLOOR GUSSET WAS FOUND TO HAVE NUMEROUS AREAS OF CORROSION AND GOUGING. MAINTENANCE REMOVED AND REPLACED THE AFFECTED GUSSET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: GUSSET — CORRODED (CABIN) · corrosion level 2 · airframe 11,328 hrs · 8,340 cycles

SHV-DURING C CHECK FOWARD FLOOR GUSSET WAS FOUND TO HAVE NUMEROUS AREAS OF CORROSION AND GOUGING. MAINTENANCE REMOVED DAMAGE AREAS AND PERFORMED A SPLICE REPAIR IAW EMB 145 SRM 51-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BEAM — CORRODED (CABIN) · corrosion level 2 · airframe 11,328 hrs · 8,340 cycles

DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 16 AND 24. MAINTENANCE REMOVED AND REPLACED AFFECTED OMEGA BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BUTT STRAP — CORRODED (FLOORBEAM) · corrosion level 2 · airframe 11,328 hrs · 8,340 cycles

DURING C-CHECK, BUTTSTRAP ON THE CENTER FLOORBEAM BETWEEN FRAMES 18 TO 23 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 11,328 hrs · 8,340 cycles

SHV-DURING C CHECK THE CENTER FLOOR BEAM RAMP ANGLE SUPPORT WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: UPLOCK — FAILED (RT MLG)

CLE FLIGHT 3092 THE CREW REPORTED WHEN THE GEAR WAS RETRACTED RECEIVED A LANDING GEAR LEVER DISAGREE WARNING MESSAGE ALONG WITH A RIGHT MAIN GEAR UNLOCK LIGHT. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT MAIN GEAR UPLOCK BOX. OPERATIONAL CHECKS WERE GOOD.

Part: INVERTER — INOPERATIVE (CABIN)

CLE FLIGHT#3237 THE CREW REPORTED THE EMERGENCY EXIT ROW LIGHT AT 12C WAS INOPERATIVE.MAINTENANCE REPLACED THE #5 INVERTER.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CONTROL UNIT — INOPERATIVE (COCKPIT)

IAH- THE CREW NOTED AFTER TAKEOFF THAT THE NOSE GEAR DOOR HANGS AFTER RETRACTION, CLOSES AT 235 KTS. MAINTENANCE REMOVED AND REPLACED THE LGEU, PERFORMED A OPERATIONAL CHECK OF LANDING GEAR SYSTEM. NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,318 hrs · 6,753 cycles

TYS DURING A ROUTINE MAINTENANCE FOUND THE LEFT EMERGENCY EXIT LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE BULB AND THE OPS CHECK WAS GOOD. AIRCRAFT RELEASED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

WHILE PERFORMING A SERVICE CHECK THE MECHANIC NOTED THAT THE EMERGENCY LIGHT IN THE BACK ROW AND OVERWING DID NOT ILLUMINATE. IAH- MAINTENANCE REMOVED AND REPLACED THE #4 EMERGENCY BATTERY, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE,

Part: SWITCH — STICKS

RIC - FLT #3516 - Crew reported a Baggage door open warning indication on takeoff roll. The crew aborted the take-off and returned to the gate. Maintenance cleaned the cargo door micro-switch. The system operationally tested satisfactory and the aircraft was approved for return to service.

Part: LIGHT — INOPERATIVE (EXTERIOR) · corrosion level 2 · airframe 7,352 hrs · 5,368 cycles

IAH - DURING C-CHECK INSPECTION, THE FORWARD LEFT HAND EXTERNAL EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 7,352 hrs · 5,368 cycles

IAH - DURING C-CHECK INSPECTION, THE BOTH OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK IN ACCORDANCE WITH EMB-145 M/M 33-50-00-710-001-A00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 7,352 hrs · 5,368 cycles

IAH - DURING C-CHECK INSPECTION, THE CENTER BUTT STRAP WAS FOUND TO BE CORRODED BETWEEN FRAMES 59 AND 60. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF BUTT STRAP IN ACCORDANCE WITH E,B-145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — CORRODED (EXTERIOR) · corrosion level 2 · airframe 7,352 hrs · 5,368 cycles

IAH - DURING C-CHECK INSPECTION, THE FORWARD RIGHT HAND EXTERNAL EMERGENCY EXIT LIGHT WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,352 hrs · 5,368 cycles

IAH - DURING C-CHECK INSPECTION, BOTH OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BOTH LIGHT ASSEMBLIES, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: APU — LEAKING (TAIL)

IAH- APU BLEED PUTTING SMOKE IN CABIN AND LAV. MAINTENANCE REMOVED AND REPLACED THE APU ASSEMBLY IAW EMB145 MAINTENANCE MANUAL 49-10-01, LEAK AND OPERATIONAL CHECK GOOD AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — DEFECTIVE (LAVATORY) · airframe 7,238 hrs · 5,283 cycles

APU BLEED CAUSES LAV SMOKE DETECTOR TO GO OFF. MEL 49-52-02, PLACARD 007786. MAINTENANCE REMOVED AND REPLACED LAV SMOKE DETECTOR IAW EMB145 MM 26-14-00. OPS CHECKED GOOD.

Part: APU — LEAKING (TAIL)

IAH - FLIGHT 4197, THE CREW REPORTED THAT AT INITIAL POWER UP WITH THE APU RUNNING, SMOKE WAS NOTICED IN THE CABIN WITH A LAV SMOKE WARNING. MX PLACED THE APU ON MEL 49-32-02 CONTROL NUMBER 007738, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 03/16/01 THE AIRCRAFT RETURNED TO IAH WHERE MX PERFORMED AN OPERATIONAL CHECK OF THE LAV SMOKE DETECTOR WITH NO DEFECTS NOTED. MX REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE DISCREPANCY REPEATED ON FLIGHT 4267 03/16/01, AND MX REMOVED AND REPLACED THE LAV SMOKE DETECTOR, AND RELEASED THE AIRCRAFT FOR RETURN TO SERVICE. THE DISCREPANCY REPEATED AGAIN ON FLIGHT 4203, WHERE MAINTENANCE PLACED THE APU ON MEL.

Part: STRUT — DAMAGED (NLG)

IAH - FLT 4126 - ON CLIMB, THE CREW REPORTED THAT THE NOSE GEAR WOULD NOT RETRACT. A FLY-BY OF THE TOWER WAS PERFORMED AND IT WAS DISCOVERED THAT THE NOSE WHEELS WERE TURNED AT A NINTY DEGREE ANGLE TO THE STRUT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED THE NOSE LANDING GEAR, PERFORMED A STRUCTURAL INSPECTION, AND INSTALLED A SERVICEABLE NOSE LANDING GEAR ASSEMBLY. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M0

Part: ENGINE — FAILED (LEFT)

CLE - FLT 4076 - THE CREW REPORTED THE NR 1 ENGINE HAD A POWER SURGE ON TAKEOFF FROM CLEVELAND. THE TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE IAW CONTINENTAL EXPRESS GMM VOLUME 13 SECTION 2 TASK CARD 6271001. THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE (M)

Part: DRAG ANGLE — CRACKED (VERTICAL STAB)

IAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICLE STABILIZER TO FUSELAGE DRAG ANGLE WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-01101, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ACFT TT: 3,986.1 HOURS. CYCLES: 3,063. (X)

Part: DRAG ANGLE — CRACKED (VERTICAL STAB)

IAH - DURING C-CHECK INSPECTION, THE LEFT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE, IAW CONTINENTLAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-01101, AND THE AIRCRAFT WAS APROVED FOR RETURN TO SERVICE. ACFT TT: 3,986.1. CYCLES: 3,063. (X)

Part: CONTROL UNIT — FAILED (SPOILER SYSTEM)

EWR - FLT 4088 - CREW REPORTED ASYMETRIC SPOILER DEPLOYMENT AT FL350-360 AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED SPOILER CONTROL UNIT AND OPS CHECKED SPOILERS AND SPEED BRAKE GOOD. (M)

Part: LIGHT — INOPERATIVE (EMER EXIT)

BTV - CO4218 - DURNG 4A INSPECTION MAINTENANCE FOUND RIGHT AFT EMERGENCY LIGHT INOPERATIVE. CLEANED CONTACTS ON LIGHT SOCKET, OPS CHECKED GOOD. (M)

Part: APU — SMOKING (AFT FUSELAGE)

EWR - FLT 4315 - CREW REPORTED APU CAUSED SMOKE ON GROUND WITH PACKS RUNNING, MAINTENANCE FOUND APU INOPERATIVE. PLACED APU ON MEL 49-00-00. AFTER MAINTENANCE TROUBLESHOOTING FOUND APU TO BE CAUSING THE SMOKE PROBLEM. REMOVED AND REPLACED APU WITH SERVICEABLE UNIT. OPS CHECKED APU AND PACKS GOOD. (M)

Part: WIRE — INOPERATIVE (LT MLG)

EWR - DURING OVERNIGHT MAINTENANCE, FOUND LEFT DOWN LOCKED INDICATION ON SYSTEM ONE INOPERATIVE. MAINTENANCE FOUND AND REPAIRED A BROKEN WIRE AT SP1422. OPS CHECKED SYSTEM GOOD. (M)

Part: POWER SUPPLY — INOPERATIVE (EXTERIOR)

IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EXTERIOR EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY LIGHT POWER SUPPLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: WHEEL — OUT OF POSITION (NLG)

IAH - FLT 4126 - ON CLIMB, THE CREW REPORTED THAT THE NOSE GEAR WOULD NOT RETRACT. A FLY-BY OF THE TOWER WAS PERFORMED AND IT WAS DISCOVERED THAT THE NOSE WHEELS WERE TURNED AT A NINTY DEGREE ANGLE TO THE STRUT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT, WHERE THE DISCREPANCY IS CURRENTLY UNDER INVESTIGATION. (M)

Part: VALVE — STUCK (NR 1 PACK)

IAH - FLT 968 - THE CREW REPORTED A BURNING SMELL FROM THE NR 1 AIR CONDITIONING PACK AT TAKEOFF THRUST. MAINTENANCE UNSTUCK THE NR 1 PACK VALVE, SATISFACTORILY RAN THE ENGINES ON THE GROUND AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X)

Part: VALVE — FAILED (NLG)

IAH - FLT 4175 - THE CREW REPORTED THE NOSE LANDING GEAR WOULD NOT EXTEND WHEN THE GEAR CONTROL LEVER WAS PLACED IN THE DOWN POSITION. THE CREW MANUALLY EXTENDED THE GEAR AND LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR DOOR SOLENOID VALVE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X)