N601DW
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| American Eagle Airlines Inc | Operator | 2010-06-28 – 2010-06-28 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
WX RADAR FAILED IN FLIGHT.AMBER WX INSCRIPTIONS AND GIVING ERRONEOUS READINGS.WX RADAR TEST FAILED....FIX:PERFORMED OPERATIONAL CHECK OF WX RTA REF. AMM 34-42-00-700-801-A OPS CHECK GOOD. OK FOR SERVICE
CENTER "T" PROFILE CRACKED ON THE FWD PRESSURE BULKHEAD,FWD FACE, UPPER AREA... FIX: INSTALLED NEW FWD PRESSURE BULKHEAD "T"PROFILE IAW EMB-145 SRM 51-40-02.
FWD PRESSURE BULKHEAD CRACKED.... FIX:INSTALLED DOUBLER, FILLER AND SHIMS FOR REPAIR OF FWD PRESSURE BULKHEAD AT UPPER CENTER AREA IAW ETD2019-145-069777 REV A.
UPPER "L" PROFILE FRAME ON FWD PRESSURE BULKHEAD IS GOUGED NEAR CENTER POST... FIX: REMOVED PROFILE,REPAIRED PER ETD2019-145-072931, REINSTALLED PROFILE FRAME ON FWD PRESSURE BULKHEAD IAW ENB SRM 51-40-02
WINDSHIELD CENTER POST LOWER FITTING BROKEN. R & R WINDSHIELD CENTER POST LOWER FITTING IAW EO1-53-19-0192 AND SB 145-53-007.
BLEED 1 VALVE CLOSED ADVISORY DISPLAYED AFTER T/O WITH VERY LOW BLEED TEPERATURE. RAN ENGINE 1 ON GROUND AT DIFFERENT THRUST SETTINGS AND PERFORMED ENG BLEED VALVE OPERATIONAL CHECK IAW AMM 36-11-05. NO ISSUES NOTED. OKAY FOR SERVICE.
FLOOR EMERGENCY LIGHTS INOPERATIVE AT THE EMERGENCY EXIT. R & R THE INVERTER IAW AMM 33-50-11.
BOTH BLEEDS OVERTEMP WARNINGS AT 16K, AFTER ICE PROTECTION HAD BEEN ON FOR 5 MINUTES. APU WAS NOT ON. REMOVED AND REPLACED THE NR 1 & 2 THERMOSTAT FAN A/C AND THERMOSTAT MOUNT TUB ASSY IAW SB 145-36-0028.
BLEED 1 LEAK EICAS MESSAGE DISPLAYED DURING CLIMBOUT. REMOVED AND REPLACED THE TUBES IAW AMM 36-13-00. PERFORMED A BLEED AIR LEAK CHECK IAW AMM 36-00-00. PERFOMED AN EBV FUNCTIONAL CHECK IAW AMM 36-11-05. LEAK AND OPS CHECKED GOOD. OK FOR SERVICE.
DURING CRUISE ALTITUDE, THE STBY ALTIMETER WAS INDICATING 1800 FEET LOWER THAN ADC AND THE STBY AIRSPEED INDICATOR WAS 25 KNOTS SLOWER THAN ADC. R & R THE STANDBY ALTIMETER IAW AMM 34-11-01. OPS CHECKED GOOD.
AT WHEELS UP, TWO LOUD THUMPING NOISES WERE HEARD COMING FROM NOSE AREA, ALONG WITH A HISSING SOUND. NO ABNORMAL INDICATIONS NOTED. EVALUATION FLIGHT SATISFACTORY.
OVERHEAD EMERGENCY LIGHT AT THE PAX DOOR WAS FOUND INOPERATIVE. R & R THE BULB.
LEFT BRAKES APPEAR TO BE SMOKING ON LANDING. NR 2 HYD QTY APPEARED TO BE DROPPING. FOUND THE LEFT MAIN BRAKE INBD LEAKING WHEN HYD PRESSURE IS APPLIED. R & R THE MAIN BRAKE ASSY IAW AMM 32-49-03. OPS CHECKED GOOD, OK FOR SERVICE.
DURING NR 2 ENGINE START, NR 2 PITOT INOPERATIVE CAUTION MESSAGE CAME INTO VIEW. OPS CHECKED GOOD.
LOW PRESSURE COMPRESSION INDICATION AT HIGHEST POINT IN THE YELLOW RANGE. CLEANED THE FADEC 1A & 1B CONNECTORS IAW MM 70-00-00, RAN ACFT, NO DEFECTS NOTED.
FIRST OFFICER`S ALTITUDE INDICATION MISSING ON PFD. TURNED OFF AVIONCIS AND PDU FOR 15 MIN. OPS CHECKED GOOD.
LT WING RIB 5 CRACKED. REPLACED LT RIB 5 IAW ERS EO EM-57MR-764.
FRAME 60 -61 PROTRUSION AT STRINGER 17L. ACCOMPLISHED REPAIR TO FRAME 60 - 61 AT STRINGER 17L IAW ERS-EM-53MR-2555.
VERTICAL STAB LT DRAG ANGLE CRACKED AFT OF FR 75 PREVIOUS REPAIR. PERFORMED PERMANENT REPAIR OF VERTICAL STAB LT DRAG ANGLE AFT OF FR 75 IAW SRM 51-40-02.
LT FLOORBEAM WEB CORRODED AT CENTER AISLE CROSSMEMBER AT FR 29. PERFORMED PERMANENT REPAIR OF CENTER AISLE CROSSMEMBER AT FR 29 IAW ERS-EM-53MR-2552
FRAME 65 PREVIOUS REPAIR GOUGED BTW STR 12R - 13R. PERFORMED PERMANENT REPAIR ON FR 65 BTW STR 12R-13R IAW ERS-EM-53MR-2545.
FUSELAGE SKIN HAS PROTRUSION AND OIL CANNING BETWEEN FRAMES 7 AND 8 STR 13L - 15L. PERFORMED PERMANENT REPAIR OF FR 7-8 STR 13L-15L IAW ERS-EM-53MR-2522.
LT FLOORBEAM WEB CORRODED AT CENTER AISLE CROSSMEMBER AT FR 38. PERFORMED PERMANENT REPAIR OF CENTER AISLE CROSSMEMBER AT FR 38 IAW SRM 53-00-10 ITEM 3 FIG 202 SHEET 1.
EMERGENCY LIGHT ABOVE SERVICE DOOR INOPERATIVE. REMOVED AND REPLACED THE INVERTER IAW AMM 33-50-11. OPS CHECKED GOOD IAW AMM 33-50-00.
CABIN FLASHLIGHT HAS NO RED CHARGE LIGHT. REMOVED AND REPLACED CABIN FLASH LIGHT IAW STANDARD MTX PRACTICES.
ON PUTTING GEAR DOWN FOR FINAL APPROACH, EICAS MESSAGE BRAKE DEGRADE. WENT AROUND DID AOM1 CHECKLIST. DECLARED EMERGENCY AND LANDED WITHOUT INCINDENT. PERFORMED MAIN BRAKE FUNCTIONAL CHECK IAW AMM 32-41-00. FNC FAILED AT STEP J.2.H. CONTINUED FROM AMM 32-41-00. STEP J2H, PASS FNC OF MAIN BRAKE SYSTEM. UTILIZE BRAKE FIELD ANALYZER IAW 32-41-00. NO FAULT NOTED. PERFORM HIGH SPD TAXI WITH FLT CREW. NO MESSAGE NOTED.
EMERGENCY LIGHT IN THE SERVICE DOOR INOPERATIVE. REPAIRED WIRE FOR SERVICE DOOR AT SPLICE SP7376 IAW SWPM 20-21-00, EMERGENCY LIGHTS OPS CHECK GOOD IAW AMM 33-50-00.
FIRST OFFICERS FLASHLIGHT NOT SECURE TO FLASHLIGHT BASE. R & R FIRST OFFICERS FLASHLIGHT BASE IAW AMM 33-50-16.
EMERGENCY HYD BRAKE LINE, UNDER COCKPIT FLOOR CRACKED & LEAKING. REPAIRED EMER HYD BRAKE LINE IAW AMM 20-10-03. LEAK & OPERATIONS CHECKED GOOD.
FORWARD FLIGHT ATTENDANT FLASHLIGHT HOLDER IS BROKEN & DOES NOT HOLD FLASHLIGHT PROPERLY. R & R FLASHLIGHT ASSEMBLY IAW AMM 33-50-16, NO DEFECT NOTED.
AFT FLASHLIGHT INOPERATIVE. CHANGE FLASHLIGHT HOLDER.
SERVICE DOOR EMER LIGHT INOPERATIVE. R & R REMOVABLE SPLICE AT SERVICE DOOR EMER EXTERNAL LIGHT IAW SWPM 20-21-00. OPERATIONS CHECKED GOOD.
YAW DAMP FAIL. R & R RUDDER SYS 2 PRESS SWITCH IAW AMM 27-23-04. PERFORMED LEAK CHECK, LEAK CHECKED GOOD. PERFORMED OPERATIONS CHECK RUDDER SYS 2 IAW AMM 27-263-00. OPERATIONS CHECKED GOOD.
CAPTAINS FLASHLIGHT NOT CHARGING. R & R CAPTAINS FLASHLIGHT IAW AMM 33-50-16. 0PERATIONS CHECKED GOOD.
MULTIPLE CABIN EMER LIGHTS INOPERATIVE. SUSPECT PROBLEM WITH EPSU NR 3. R & R NR 3 EMER LIGHT BATTERY & CHARGER IAW WC 33-700-19. OPERATIONS CHECKED GOOD, NO DEFECTS NOTED AT THIS TIME.
COCKPIT STEP EMER LIGHT INOPERATIVE. R & R EMER LIGHT DC & AC INVERTER IAW AMM 33-50-11. OPERATIONS CHECKED GOOD.
EMERGENCY LIGHT STRIP ON FLOOR BY 6A INOPERATIVE. R & R EMER LIGHT STRIP BY 6A IAW AMM 33-50-12. OPERATIONS CHECKED GOOD, NO DEFECTS NOTED.
FIRST OFFICERS FLASHLIGHT INOPERATIVE. TROUBLE SHOT FIRST OFFICERS FLASHLIGHT, FOUND LAMP BURNED OUT. R & R LAMP IAW CMM 25-60-11.
1/2 OF EMER LIGHTING NOT WORKING. R & R NR 4 EMER BATTERY ASSEMBLY IAW AMM 33-50-04. OPERATIONS CHECKED GOOD IAW AMM 33-50-00.
ESCAPE PATH EMER LIGHTING ON LT SIDE ROWS 7 - 15 OTS. R & R NR 4 AC TO DC INVERTER IAW AMM 33-50-11. OPERATIONS CHECKED GOOD.
CABIN NR 5 FLOOR PROXIMITY STRIP LIGHT INOPERATIVE. R & R CABIN NR 5 FLOOR PROXIMITY STRIP LIGHT IAW AMM 33-50-12. OPERATIONS CHECKED GOOD.
WHILE RUNNING PROCEDURES FOR ITEM NR 1, RECEIVED PACK 2 OVLD, FOLLOWED BY BURNING SMELL. FOUND BLOWN SLEEVE FWD OF D C V CAUSING BURNING SMELL. R & R SLEEVE AMM 21-60-01. LEAK CHECK & OPERATIONS CHECKED GOOD AT THIS TIME.
DURING CLIMB CREW RECEIVED PACK 1 OVLD MSG FOLLOWED BY PACK 1 OVLD MSG. CREW COMPLIED WITH AOM VOL 1 PROCEDURES, DECLARED AN EMER & RETURNED WITHOUT INCIDENT. FOUND BROKEN CLAMP AT PACK 1 VALVE. R & R CLAMP IAW AMM 21-51-01. LEAK & OPS CHECKED GOOD.
FRAME 75 SKIN AT FASTENER AREA CRACKED ABOVE STRINGER 2R. ACCOMPLISHED FRAME 75 ABOVE STRINGER 2R SKIN REPAIR IAW ERS-EM-53MR-984.
FRAME 75 FASTENER SKIN AREA CRACKED BELOW STRINGER 2L. ACCOMPLISHED FRAME 75 BELOW STRINGER 2L SKIN REPAIR IAW ERS-EM-53MR-984.
CRACK ON LT WING SPAR III AT HOLE FOR MLG HARNESS AT APPROX THE 7 O'CLOCK POSITION BETWEEN RIBS 3 & 4. ACCOMPLISHED REPAIR ON LT WING SPAR III AT HOLE FOR MLG HARNESS IAW ERS-EM-57MR-349. FOUND DURING EO-EM-5700-662.
CRACK ON RT WING SPAR III AT HOLE FOR MLG HARNESS AT APPROX THE 4 O'CLOCK POSITION BETWEEN RIBS 3 & 4. ACCOMPLISHED REPAIR ON RT WING SPAR III AT HOLE FOR MLG HARNESS IAW ERS-EM-57MR-350. FOUND DURING EO-EM-5700-662.
WIRE FOR FLOOR PROXIMITY LIGHT STRIP NR 4 IS MISSING CONNECTOR WHERE IT PASSES THRU THE FLOORBOARD. INSTALLED CONNECTOR TO NR 4 PROXIMITY LIGHT STRIP IAW SWPM 20-21-0. FOUND DURING OPEN UP.
WIRE FOR FLOOR PROXIMITY LIGHT STRIP NR 8 IS MISSING CONNECTOR WHERE IT PASSES THRU THE FLOORBOARD. INSTALLED CONNECTOR TO NR 8 PROXIMITY LIGHT STRIP IAW SWPM 20-21-00. FOUND DURING OPEN UP.
SERVICE DOOR FRAME CORRODED BELOW AFT LOWER ROLLER. PERFORMED SERVICE DOOR FRAME CORROSION REPAIR IAW ERS EM -53MR-971.
LEFT PYLON FWD LOWER YOKE FWD ENG MOUNT SUPPORT IS CRACKED. ACCOMPLISHED REPAIR TO LT PYLON FWD LOWER YOKE FWD ENG MOUNT SUPPORT IAW EO-EM-54MR-386 PART A.
LAVATORY CTR OMEGA BEAM HAS MULTIPLE CORRODED AREAS. REPAIRED LAVATORY CTR BEAM AT AFFECTED RIVET HOLE, 2.4 INCHES FWD OF FRAME 60 IAW ERS-EM-53MR-963.
LEFT PYLON FWD LOWER YOKE FWD ENG MOUNT SUPPORT IS CRACKED. ACCOMPLISHED REPAIR TO LT PYLON FWD LOWER YOKE FWD ENG MOUNT SUPPORT IAW EO-EM-54MR-386 PART A.
FRAME 75 SKIN AT FASTENER AREA CRACKED ABOVE STRINGER 2R. ACCOMPLISHED FRAME 75 ABOVE STRINGER 2R SKIN REPAIR IAW ERS-EM-53MR-984.
LEFT MLG AFT UPPER TRUNNION OTBD LOWER MOUNT FLANGE HAS CRACK INDICATION. R & R LT MLG AFT UPPER TRUNNION IAW ERS-EM-5700-344. SEE TURN OVER FOR DETAILS.
FRAME 75 FASTENER SKIN AREA CRACKED BELOW STRINGER 2L. ACCOMPLISHED FRAME 75 BELOW STRINGER 2L SKIN REPAIR IAW ERS-EM-53MR-984.
CRACK ON RT WING SPAR III AT HOLE FOR MLG HARNESS AT APPROX THE 4 O'CLOCK POSITION BETWEEN RIBS 3 & 4. ACCOMPLISHED REPAIR ON RT WING SPAR III AT HOLE FOR MLG HARNESS IAW ERS-EM-57MR-350.
CRACK ON LT WING SPAR III AT HOLE FOR MLG HARNESS AT APPROX THE 7 O'CLOCK POSITION BETWEEN RIBS 3 & 4. ACCOMPLISHED REPAIR ON LT WING SPAR III AT HOLE FOR MLG HARNESS IAW ERS-EM-57MR-349.
CAPTAINS FLASHLIGHT SWITCH BROKEN. REPLACED IAW AMM-33-51-01.
FLIGHT ATTENDANT INFORMED CAPTAIN & MX THAT THE MAIN CABIN DOOR IS DIFFICULT TO OPERATE. PERFORM ADJUSTMENT OF PAX MAIN DOOR, IAW AMM 52-18-00.
EMERGENCY FLOOR LIGHTING STRIP 3RD FROM FRONT FOUND INOPERATIVE. R & R EMER FLOOR LIGHTING STRIP 3RD FROM FRONT IAW AMM 33-50-12. OPERATIONS CHECKED GOOD.
CAPTAIN`S FLASHLIGHT HOLDER WILL NOT CHARGE FLASHLIGHT. R & R FLASHLIGHT ASSEMBLY IAW AMM 33-50-16.
AT 190 IN CRUISE VIB HP NR 2 JUMPED INTO YELLOW RANGE. REDUCED THRUST TO IDLE & ARROW RETURNED TO GREEN. HOWEVER EVEN WITH THRUST LEVER IN IDLE ARROW INTERMITTENTLY WENT OUT OF LIMITS. UPON INITIAL DESCENT ARROW PEGGED FULL OUT OF LIMITS AT THAT TIME PERFORMED A PRECAUTIONARY SHUTDOWN. R & R ENG NR 2 HP COMPRESSOR VIBRATION SENSOR IAW RR MM 77-41-10. OPERATIONAL CHECK OK.
RIGHT BLEED DUCT FLANGE CRACKED. R & R BLEED DUCT, OPS CHECKED GOOD IAW AMM 36-11-09.
EICAS MESSAGE "W/S 2 HEAT FAIL" RESET IAW AMM AOM, VOL 1 BUT IT FAILED AGAIN. ODOR SIMILAR TO SOMETHING GETTING WARM/HOT WAS DETECTED. THAT WENT AWAY WITH W/S 2 OFF. R & R NR 2 WINDSHIELD TEMP CONTROLLER IAW AMM 30-42-01. OP'S CHECK GOOD. NO DEFECTS NOTED AT THIS TIME.
LANDED, AT A HIGH SPEED TURNOFF ACFT SWERVED AND NOSE STEERING WENT INOPERATIVE . UNABLE TO RE-ENGAGE NOSE STEERING . TAXIED CLEAR OF RUNWAYS WITH DIFFERENCIAL THRUST. INSPECTED NLG ASSY AND PERFORMED ACFT TAXING AMM 9-20-00. NO EICAS MSG AT THIS TIME. ACFT OK FOR SERVICE.
ON FLIGHT 2850 THE CREW REPORTED THE MAIN PASSENGER DOOR WOULD NOT OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED DEBRIS AND CYCLED DOOR SEVERAL TIMES. NO DEFECTS NOTED AMM1 52-10-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE INSPECTION FOUND MAIN DOOR EMERGENCY LIGHT INOPERABLE. C/W REMOVED AND REPLACED MAIN DOOR EMERGENCY LIGHT ASSEMBLY IAW EMB AMM 33-50-06-000-802-A AND 33-50-06-400-802-A, OPERATION CHECK GOOD. THE AIRCRAFT RETURNED TO SERVICE.
DURING MAINTENANCE INSPECTION WHILE DOING INSTALLATION OF THE RIGHT WING RIB 5QC FOUND THE RIGHT MAIN LANDING GEAR AFT TRUNNION CRACKED AT HI-LOK HOLE. THE AIRCRAFT WAS REMOVED FROM SERVICE FOR HMBV INSPECTION. REMOVED AND REPLACED THE RIGHT AFT TRUNNION IAW EO EM-57MR-671. THE AIRCRAFT WAS RETURNED TO SERVICE UPON COMPLETION OF THE HMBV CHECK.
DURING MAINTENANCE INSPECTION FOUND FRAME 70 GOUGED AT STRINGER 13 RIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW AEA EO EM-53MR-2075. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE INSPECTION FOUND FRAME 65 GOUGED AT STRINGER 13 RIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW AEA EO EM-53MR-2077. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE INSPECTION FOUND THE RIGHT WING RIB 5 CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT WING RIB 5 IAW EO EM-57MR-595. THE AIRCRAFT WAS RETURNED TO SERVICE UPON COMPLETION OF THE HMBV CHECK.
DURING HEAVY CHECK, FOUND FUSELAGE INNER SKIN CORRODED BETWEEN FR 13-14, STR 20R-19R. PERFORMED PERMANENT REPAIR IAW EO-EM-53MR-2079.
CARGO DOOR CUT-OUT LOWER FWD SECTION CORRODED. REPAIRED CARGO DOOR CUT-OUT FWD SECTION IAW EO EM-53MR-1129.
DURING MAINTENANCE INSEPCTION FOUND THE CARGO DOOR SILL CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLETED INSTALLATION OF CARGO DOOR SILL AND RE-INSTALLED CARGO RAMP SUPPORT AT FR66 AND FR67 IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING B INSPECTION FOUND THE 2EA PROX LIGHTS HAVE BROKEN WIRES AT PROX LIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE 2EA PROX LIGHTS IAW EMB 145 AMM 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.
FLIGHT 2910, CREW REPORTED AT 30,000 FT, HEARD A LOUD BANG. ALL INSTURMENT INDICATIONS NORMAL & A SMOOTH CRUISE CONDITION NOTED. UNABLE TO POSITIVELY IDENTIFY NOISE & SUSPECTED THAT A TIRE MAY HAVE BURST IN THE WHEEL WELL. DECLARED AN EMERGENCY & PERFORMED TIRE DAMAGE CHECKLIST. LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. PERFORMED BOROSCOPE INSPECTION OF RT ENGINE COMPRESSOR FORWARD AND AFT SECTIONS AND OF RT ENGINE TURBINE SECTION IAW MM 72-50-00-200-801 NO ABNORMAL CONDITIONS NOTED. ACCOMPLISHED RT ENGINE PERFORMANCE RUNS IAW MM 72-00-00. PERFORMED RETRACTION & EXTENSION OF MLG IAW AMM 32-30-00. NO DEFECTS NOTED. ACCOMPLISHED RT ENGINE VIBRATION CHECK IAW MM 72-50-00, OPS CHECKED NORMAL. FDR DATA DOWNLOAD IAW 31-700-05. RT ENGINE FAN CASE ASSY HAS SCRATCHES & GOUGES FROM ELEVEN TO ABOUT ONE O'CLOCK POSITIONS I AREA C PERFORMED BLEND OF RT ENGINE FAN CASE IAW MM 72-25-30. AIRCRAFT RETURNED TO SERVICE.
ON FLIGHT 4368 THE CREW REPORTED THE AFT FLIGHT ATTENDANT FLASHLIGHT WOULD NOT HOLD CHARGE. REMOVED & REPLACED THE FLASHLIGHT ASSEMBLY IAW EMB 145 AMM 33-50-16. THE OPERATIONAL TEST WAS GOOD. NO FURTHER DEFECTS. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 4197 THE CREW REPORTED THAT DURING CLIMB THROUGH 9000 FEET, RECEIVED A NR 1 ENGINE 1 BLEED LEAK MESSAGE ON EICAS. THE CREW PERFORMED THE EPC/AOM VOL 1 CHECK LIST AND DECLARED AN EMERGENCY. AFTER ACCOMPLISHING EMERGENCY CHECKLIST, THE LIGHT WENT OUT. THE AIRCRAFT RETURNED TO BNA AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BLEED TUBE ASSEMBLY AT FR 69 IAW EMB-145 AMM 36-11-09. THE LEAK CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE INSPECTION, FOUND THE FORWARD CABIN EMERGENCY FLASHLIGHT ASSEMBLY HOLDER CRACKED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FORWARD CABIN EMERGENCY FLASHLIGHT ASSEMBLY IAW AMM TASK 33-50-16-000-801/33-50-16-400-801. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
FLIGHT 2826, THE CREW REPORTED THE F/OâS FLASHLIGHT WAS INOPERATIVE, AIRCRAFT REMOVED FROM SERVICE. REPLACED FLASHLIGHT BATTERY IAW AMM 33-50-16. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
ON FLIGHT 4343 THE CREW REPORTED THAT ON THE START OF DESCENT THE CAPTAIN TRIED TO BRING HIS SEAT FORWARD INTO LANDING POSITION AND WAS UNABLE. THE CAPTAIN NOTICED THE RIGHT SIDE SEAT TRACK PIN WAS BROKEN. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS TOWED TO THE GATE DUE TO THE CAPTAIN WAS NOT ABLE TO REACH THE RUDDER PEDALS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REINSTALLED ROLL PIN ON SEAT LOCK PIN IAW CMM 25-11-71. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE BASE VISIT FOUND THE RIGHT ENGINE FORWARD LOWER YOKE CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED THE RIGHT ENGINE LOWER YOKE IAW EO EM-54MR-386. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE BASE VISIT FOUND THE LEFT FORWARD OVERWING EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT FORWARD OVERWING EMERGENCY LIGHT IAW EMB 145 AMM 33-50-07-000-801-A AND 33-50-07-400-801-A. THE OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLT 3224 DURING CRUISE THE CREW REPORTED AT FLIGHT LEVEL 360 ENCOUNTERED A 10 SECOND DURATION OF SEVERE TURBULENCE. THE CREW ALSO NOTICED A BURNING ELECTRICAL ODOR AFTER THE TURBULENCE. THE CAPTAIN DECLARED AN EMERGENCY AND ELECTED TO DIVERT TO GGG. THE FLIGHT ATTENDANT AND 5 PASSENGERS WERE INJURED. THE FLIGHT ATTENDANT WAS UNABLE TO COMPLETE DUTIES. THE SEAT BELT SIGN WAS ON AND A PUBLIC ANNOUNCEMENT WAS MADE PRIOR TO ENTERING TURBULENCE. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED SEVERE TURBULENCE OR BUFFETING CONDITION INSPECTION IAW W/C 05-200-03. PERFORMED DIGITAL FLIGHT DATA RECORDER DOWNLOAD W/C 31-700-05. R & R THE DIGITAL FLIGHT DATA RECORDER ASSEMBLY. OPS TESTED GOOD IAW AMM 31-31-00. R & R COCKPIT VOICE RECORDER IAW AMM 23-71-01. ALSO FOUND AVIONICS MASTER 2 PUSH BUTTON LAMPS TO ALL BE BURNED OUT. R & R LAMPS IAW AMM 20-13-04. THE OPERATIONAL CHECK WAS GOOD. THE SMOKE ODOR DID NOT RETURN DURING INSPECTION. THE AIRCRAFT WAS RETURNED TO SERVICE.
FOR FLIGHT 2757 THE CAPTAIN REPORTED THAT AFTER LANDING DURING BRAKING THERE WAS AN AGGRESSIVE TO VIOLENT BRAKE GRABBING. REGARDLESS OF HOW SOFT THE BRAKES WERE APPLIED, THE BRAKES GRABBED HARD AND ERRATIC. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BRAKE CONTROL UNIT PER EMB MM 32-41-02. THE OPERATIONAL TAXI CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
AFTER LANDING THE CREW OF FLIGHT 3762 REPORTED A STRONG ELECTRICAL SMELL IN THE COCKPIT. AFTER ENGINE RUNS A STRONG OIL SMELL WAS PRESENT IN THE COCKPIT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED ENGINE RUN PER THE GROUND HANDLING CHECKLIST AND FOUND IT TO BE AN OIL BURNING SMELL. ACCOMPLISHED INTERNAL AND EXTERNAL OIL LEAKS PER RRMM 79-37-00. NO LEAKS NOTED. FOUND ENGINE TO BE CHANGED ON 12-18-09 AT CMH. SMELL WAS DETERMINED TO BE CAUSED BY ENGINE BREAK IN. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS OKâED FOR SERVICE. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 4113 THE CREW REPORTED ENCOUNTERED ICE ON CLIMBOUT AT 8000 FEET AND RECEIVED BLEED 1-2 LEAK WARNING ON EICAS. THE CREW ALSO REPORTED A FOUL SMELL IN THE COCKPIT AND CABIN. THE CREW ELECTED TO RETURN TO CHM AT A NORMAL DESCENT RATE. LANDING WEIGHT WAS OKAY. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED GAMMA CLAMP LOCATED BETWEEN FRAMES 60 AND 70 IAW AMM 36-11-09. PERFORMED OPERATIONAL CHECK 36-00-00. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 3252 THE CREW REPORTED A STALL PROTECTION SYSTEM ADVANCED FLAP LOW SPEED EICAS MESSAGE PRESENT IN FLIGHT. EICAS INDICATED FLAPS AS AMBER BOX AND AMBER DASH. AMBER DASH FLAP INDICATIONS WERE ON BOTH DISPLAYS. AN EMERGENCY WAS DECLARED UPON ARRIVAL INTO DFW. AIRCRAFT LANDED WITH NO INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED BLOWN FUSE F0098. REMOVED AND REPLACED LEFT FLAP DRIVE MOTOR UNIT. REMOVED AND REPLACED FLAT ELECTRONIC CONTROL UNIT. ALL WORK PERFORMED IAW EMB 145 AMM 20-13-08, 27-53-01 AND 27-53-02. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
DURING IMBV, THE GALLEY FLOOR CENTER BEAM WAS FOUND CORRODED. REMOVED DAMAGED BEAM. PREPPED, CLEANED, ALODINED, PRIMED AND INSTALLED NEW BEAM IAW EMB SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.
ON FLIGHT 4481, MAINTENANCE REPORTED THE LEFT OVER WING EXIT MARKER AFT INOPERATIVE DURING A PS CHECK. REMOVED AND REPLACE INVERTER. OPERATION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
DURING IMBV THE GALLEY CENTER FLOORBEAM WAS FOUND CORRODED. REMOVED CORRODED FLOORBEAM, ALODINED AND PAINTED FASTENER HOLES AND INSTALLED NEW FLOORBEAM IAW EMB SRM 51-40-02 AND 51-40-03. ACFT RETURNED TO SERVICE.