N826AE

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,014 hrs · 31,586 cycles

UPON COURTESY CHECK FOUND RH OVER WING EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED EMERGENCY LIGHT BULB OVER WING ON RH SIDE IAW EMB 140 AMM 33-50-10 OPC GOOD NO FURTHER DEFECTS NOTED AT THIS TIME

Part: ACM — ODOR (NR 1) · airframe 35,859 hrs · 31,418 cycles

MEL 21-30 AUTH 110241D-C ON TAXI OUT, BOTH PACKS RUNNING, CABIN AND COCKPIT FILLED WITH STRONG SMELL OF SMOKE. TURNED OFF PACK #1 AND SMELL WENT AWAY.REF LOG PAGE 4599679 ITEM 2. PACK 1 ACM REQ REPLACEMENT AND PERFORM ETN-EM-21-062.-C/A-RAR LH ACM IAW EO-EM-2100-048R2. NO FURTHER DEFECTS NOTED AND OPC GOOD.MEL ITEM RESTORED

Part: A/C PACK — SMOKE · airframe 35,856 hrs · 31,413 cycles

ON TAXI OUT BOTH PACKS RUNING CABIN AND COCKPIT FILLED WITH STRONG SMELL OF SMOKE TURNED OFF PACK 1 AND SMELL WENT AWAY-C/A-C/W EMB-140 FIM TASK 21-20-00-810-801-A AIR CONDITION ABNORMAL SMELL NO SMELLS NOTED. C/W ETN-EM-72-034 NO SMELLS NOTED . PERFORMED GVI OF ACM IAW EMB-140 AMM 21-51-03 NO DEFECTS NOTED

Part: SKIN — DENTED (FUSELAGE) · airframe 35,475 hrs · 31,016 cycles

FUSELAGE DENTED AFT OF FR65 BETWEEN STR 19L-20L. C/A-C/W ERS-EM-53MR-3878.

Part: SKIN — GOUGED (FUSELAGE) · airframe 35,474 hrs · 31,015 cycles

DISCREPANCY: 53-10 FUSELAGEFUSELAGE MAIN, STRUCTURE - FUSELAGE SKIN GOUGED BELOW CARGO DOOR AFT OF FRAME 65 BETWEEN STRINGERS 19-20L. MAJOR REPAIR. C/A-REPAIRED FUSELAGE AFT OF FR65 BETWEEN STR 19-20L IAW ERS-EM-53MR-3878.

Part: ROLLER — DIRTY (CABIN DOOR) · airframe 34,513 hrs · 30,195 cycles

MAIN CABIN DOOR HANDLE VERY HARD TO OPEN AND CLOSE. C/A-CLEAN AND LUBE DOOR ROLLERS IN REF TO AMM 52-10-01, OPC GOOD AND AMM 53-21-02.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 34,401 hrs · 30,087 cycles

SUPPLEMENTAL AFT FLASH LIGHT IS INOP. C/A-DEFERED AFT F/A FLASH LIGHT C/W MEL PROCEDURES. REMOVED AND REPLACED AFT FA FLASHLIGHT AND CRADLE OPC GOOD IAW AMM 33-50-16 MEL ITEM RESTORED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,366 hrs · 30,054 cycles

NR 4 FLOOR EMERGENCY LIGHT STRIP IS INOP. C/A-REMOVED AND REPLACED NR 4 FLOOR EMERGENCY LIGHT STRIP IAW AMM 30-50-12 OPS CHECK GOOD.

Part: SWITCH — FAULTY (AC BAY) · airframe 33,586 hrs · 29,361 cycles

PK 1 OVL CAUTION MESSAGE LOST CABIN PRESS AT FL240 DECLARE EMR PK 2 CLSD ADVISORY. -C/A-FOUND CMC MESSAGES PACK NR 1 OVERPRESSURE AND HAD CB NR 2 PACK TRIPPING IAW AMM 45-45-00. REMOVED AND REPLACED PACK NR 1 OVERPRESSURE SWITCH IAW AMM 21-51-06. REMOVED AND REPLACED NR 2 PACK VALVE IAW AMM 21-51-01. PERFORMED OPERATIONAL TEST IAW AMM 21-51-00 OPC GOOD. NO DEFECTS NOR MESSAGES FOUND AT THIS TIME. PERFORMED OPC OF PACK NR 1 IAW AMM TASK 21-51-00-700-802-A. OPC GOOD.

Part: DISPLAY — FAILED (COCKPIT) · airframe 33,341 hrs · 29,148 cycles

ON FINAL FO PFD FAILED AND NOTICED BURNING SMELL IN CKPT. PULLED PFD 2 CB AS SAFETY PRECAUTION. UPON FURTHER INSP FOUND PFD TO BE THE BURNING SMELL C/W M FUNCTION SWAPED PFD AN MFD APPLIED CB COLLAR TO MFD. REMOVED AND REPLACED FO MFD IAW AMM 34-22-01. SWAPPED BACK FO'S PFD UNIT TO FO'S MFD UNIT POSITION. OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,251 hrs · 29,069 cycles

NR 2 CEILING EMERGENCY LIGHT INOPERATIVE. R & R THE NR 2 CEILING EMERGENCY LIGHT BULB IAW AMM 33-50-08. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,890 hrs · 28,761 cycles

MAIN PAX DOOR EMERGENCY LIGHT DOES NOT COME ON. REMOVED AND REPLACED THE EMERGENCY LIGHT ASSY. OP TESTED OK. IAW AMM 33-30-02 AND AMM 33-50-10.

Part: LIGHT — INOPERATIVE (ROWS 7 AND 8) · airframe 32,762 hrs · 28,652 cycles

EMERGENCY LIGHT STRIPS AT ROWS 7 & 8 WERE INOPERATIVE. R & R THE EMERGENCY LIGHT STRIP IAW AMM 33-50-12. OPS CHECKED GOOD. NO DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,751 hrs · 28,642 cycles

EMERGENCY LIGHT AT ROWS 7 & 8 WERE INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-12. OPS CHECKED GOOD. NO DEFECTS NOTED.

Part: WARNING MESSAGE — FALSE ACTIVATION (NR 2 BLEED SYS) · airframe 32,692 hrs · 28,592 cycles

NR 2 BLEED LEAK OCCURED AT APPROX 500FT. PERFORMED AN OPS CHECK OF THE BLEED SYSTEM IAW AMM 36-11-10, AND AMM 36-00-00. OPS CHECKED GOOD.

Part: BEAM — CORRODED (CARGO THRESHOLD) · corrosion level 2 · airframe 32,393 hrs · 28,302 cycles

CORROSION ON THE CARGO DOOR THRESHOLD BEAM AT FRAME 65. BLENDED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-31-15, REMOVED THE THRESHOLD BEAM IAW AMM 53-31-09, AND SRM 51-40-02. LOCATED , DRILLED, ALODINED, AND INSTALLED IAW SRM 51-20-03, 51-40-02, AND CPM 51-21-04.

Part: SHEAR TIE — CRACKED (FRAME 80) · airframe 32,393 hrs · 28,302 cycles

CRACKED SHEAR TIE, FRAME 80, BETWEEN STRINGERS 6R AND 7R. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, SRM 51-20-03, CPM 51-21-05, AND 51-21-06.

Part: SKIN — GOUGED (FRAME 25) · airframe 32,393 hrs · 28,302 cycles

GOUGE IN THE SKIN AT FRAME 25 BETWEEN STRINGERS 21L AND 21R. CUT OUT THE DAMAGED AREA IAW SRM 53-22-01, REPAIR TYPE A, PERFORMED HFEC INSPECTION, NO DEFECTS NOTED IAW NIM 51-00-00-916-801-A00. FABRICATED A FILLER AND DOUBLER , APPLIED ALODINE AND PRIMER IAW SRM 53-22-01 51-21-01, CPM 51-21-03, AND 51-21-04. INSTALLED IAW SRM 51-21-01, AND 51-40-02, SEALED AND APPLIED TOP COAT IAW SRM 51-21-01 AND CPM 51-21-06.

Part: FITTING — CRACKED (FUSELAGE) · airframe 32,393 hrs · 28,302 cycles

CRACK IN SHEAR CLIP AT FRAME 67 BETWEEN STRINGERS 6L AND 7L. REMOVED CRACKED SHEAR CLIP, LOCATED DRILLED AND APPLIED ALODINE TO NEW SHEAR CLIP AND INSTALLED IAW SRM 51-40-02, 53-31-04, 51-20-03 AND CPM 51-21-04.

Part: FITTING — CRACKED (FUSELAGE) · airframe 32,393 hrs · 28,302 cycles

CRACK IN SHEAR CLIP AT FRAME 24 BETWEEN STRINGERS 16 R AND 17 R. REMOVED CRACKED SHEAR CLIP, LOCATED DRILLED AND APPLIED ALODINE TO NEW SHEAR CLIP AND INSTALLED IAW SRM 51-40-02, 53-31-04, 51-20-03 AND CPM 51-21-04.

Part: FITTING — CRACKED (FUSELAGE) · airframe 32,393 hrs · 28,302 cycles

CRACK IN SHEAR CLIP AT FRAME 25 BETWEEN STRINGERS 15R AND 16 R. REMOVED CRACKED SHEAR CLIP, LOCATED, DRILLED ALODINED AND INSTALLED NEW SHEAR CLIP IAW SRM 51-40-02, 51-20-03 AND CPM 51-21-04.

Part: FRAME — CRACKED (FRAME 23) · airframe 32,393 hrs · 28,302 cycles

CRACK IN FRAME 23 BETWEEN STRINGERS 14 R AND 15 R-C/A-INSTALLED EWIS PROTECTION IAW SWMP 20-21-00, REMOVED OMEGA BEAM STANTION TO FOM IAW EMB 145 SRM 51-40-02, REMOVED AIRCONDITION DUCT IAW AMM 21-20-04. REMOVED CRACKED FRAME 23 FROM STRINGER 13R TO A9 R, LOCATED DRILLED, ALODINED, SEALED AND INSTALLED FRAME BETWEEN STRINERGS 13R AND 19 R IAW EMB 145 SRM 51-40-02, 51-21-04, 53-00-04 AND CPM 51-21-04 AND 51-21-03. REINSTALLED PREVIOUSLY REMOVED AIR CONDITION DUCT IAW AMM 21-20-04, REINSTALLED FRAME STANTION IAW SRM 51-40-02 AND REMOVED EWIS PROTECTION IAW SWPM 20-21-00

Part: FITTING — CRACKED (FUSELAGE) · airframe 32,393 hrs · 28,302 cycles

CRACK IN SHEAR CLIP AT FRAME 68 BETWEEN STRINGERS 6L AND 7L. REMOVED CRACKED SHEAR CLIP, LOCATED DRILLED AND APPLIED ALODINE TO NEW SHEAR CLIP AND INSTALLED IAW SRM 51-40-02, 53-31-04, 51-20-03 AND CPM 51-21-04.

Part: SUPPORT — CRACKED (FRAMES 47-48) · airframe 32,393 hrs · 28,302 cycles

CRACK IN RT OMEGA BEAM INBORED SUPPORT BETWEEN FRAMES 47 AND 48. REMOVED, LOCATED, DRILLED, AND ALODINED NEW SUPPORTS IAW SRM 51-40-02, 51-20-03, AND CPM 51-21-04. INSTALLED THE SUPPORTS IAW SRM 51-40-01, AND 53-23-02.

Part: SHEAR TIE — CRACKED (FRAME 61) · airframe 32,393 hrs · 28,302 cycles

CRACK IN SHEAR TIE, FRAME 61 BETWEEN STRINGER 6 - 7L. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02 , 51-20-03, AND CPM 51-21-04.

Part: SHEAR TIE — CRACKED (FRAME 73) · airframe 32,393 hrs · 28,302 cycles

CRACK IN SHEAR TIE AT FRAME 73, BETWEEN STRINGERS 8R AND 10R. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, 51-20-03, CPM 51-21-04, AND 51-21-05

Part: SHEAR TIE — CRACKED (FRAME 65) · airframe 32,393 hrs · 28,302 cycles

CRACKED SHEAR TIE, FRAME 65 BETWEEN STRINGERS 18L AND 19L. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-20-02, 51-20-03, AND CPM 51-21-04.

Part: FLOOR SUPPORT — CORRODED (FRAME 27) · corrosion level 2 · airframe 32,393 hrs · 28,302 cycles

CORROSION ON THE CENTER OMEGA BEAM, FRAME 27. REMOVED CORROSION IAW SRM 51-40-02, 51-10-03. FOUND TO BE OUT OF LIMITS IAW SRM 53-22-10, CUT OUT THE DAMAGED AREA, FABRICATED, LOCATED, AND DRILLED A REPAIR ANGLE, FILLER AND SHIMS IAW SRM 53-00-10, AND 51-20-03. PERFORMED NDT IAW NIM INTRODUCTION SECTION D, NO DEFECTS NOTED. ASSEMBLED THE REPAIR IAW SRM 53-00-10, 51-40-02, CPM 51-21-04, 51-21-05, AND 51-21-06

Part: CONNECTOR — BROKEN (CABIN) · airframe 31,934 hrs · 27,812 cycles

NUMBER 1 CABIN FLOOR PROXIMITY LIGHT WIRE CONNECTOR BROKEN. R & R NR 1 CABIN FLOOR PROXIMITY LIGHT STRIP IAW AMM 33-50-12. SEE NRWC 826-ABI-02103 FOR OPERATIONAL CHECK.

Part: WIRE — BROKEN (CABIN) · airframe 31,934 hrs · 27,812 cycles

LEFT NR 5 PROXIMITY LIGHT HAS BROKEN WIRE AT BASE OF LIGHT. R & R LT NR 5 PROXIMITY LIGHT STRIP IAW AMM 33-50-12. OPERATIONAL CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 31,548 hrs · 27,406 cycles

EXTERIOR RT WING TO FUSELAGE EMER LIGHT INOPERATIVE. R & R RT EXTERIOR EMER LIGHT BULB ON WING TO FUSELAGE FAIRING IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: INDICATOR — FAILED (ISIS) · airframe 31,440 hrs · 27,285 cycles

STANDBY EHSI SCREEN INOPERATIVE, 1/2 OF SCREEN HAS LINE GOING THROUGH IT. R & R ISIS INDICATOR IAW AMM 34-01-01. LEAK & FNC GOOD IAW AMM 34-13-00 & 34-01-01.

Part: DUCT — BROKEN (AC BAY) · airframe 31,257 hrs · 27,082 cycles

AIR CONDITIONING PACKS COULD NOT SUPPLY ENOUGH AIR FOR AIR CONDITIONING OR PRESSURIZATION. COULD NOT MAINTAIN REQUIRED CABIN ALTITUDE. TRANSFERRED TO NRWC 826-DFW-01971. FOUND LT RAM AIR DUCT BROKEN & LT RAM AIR CHECK VLV BACKWARD INSTALLED. R & R LT RAM AIR DUCT ASSEMBLY. INSTALLED LT RAM AIR VLV CORRECTLY IAW AMM 21-25-02. PERFORMED ACFT SYS, OPERATIONS CHECKED IAW AMM 21-51-00 & PRESS SYS. OPERATIONS CHECKED IAW AMM 21-31-00. ALL CHECKED GOOD.

Part: CARBON SEAL — DEFECTIVE (NR 1 ENGINE) · airframe 30,221 hrs · 26,241 cycles

SMOKE COMING FROM E1 AFTER BEING SHUTDOWN 15 PLUS MINUTES. COMPLIED WITH ETN-79--15 UP TO STEP 12 TDMI 826T7221 SCHEDULE A 50 FLIGHT HOURS. R & R LPT SHAFT PLUG & MAGNETIC CARBON SEAL.

Part: VALVE — FAILED (BLEED AIR SYS) · airframe 29,492 hrs · 25,601 cycles

DURING TAXI OUT, HS VLV 2 FAIL ON EICAS WITH BOTH ENGS RUNNING. R & R HS VLV 2 IAW AMM 36-11-02. OPERATIONS CHECKED GOOD.

Part: ISIS — MALFUNCTIONED (COCKPIT) · airframe 29,377 hrs · 25,471 cycles

ISIS ONLY SHOWS RT HALF OF DISPLAY LT HALF IS BLANK. R & R ISIS IAW AMM 34-01-01. OPERATIONS & LEAK CHECKED GOOD.

Part: SMOKE DETECTOR — INOPERATIVE (CARGO BAY) · airframe 28,914 hrs · 25,045 cycles

WHILE PERFORMING WORK CARD NR 26-200-06 AFT CARGO SMOKE DETECTOR MX LED FAILED TO ILLUMINATE. REMOVED & INSTALLED SERVICEABLE AFT CARGO SMOKE DETECTOR IAW AMM 26-15-01, OPERATIONS CHECKED GOOD.

Part: SMOKE DETECTOR — FAILED (CARGO BAY) · airframe 28,397 hrs · 24,616 cycles

FIRE DETECTION TEST FAILED BAGGAGE WARNING LIGHT DOES NOT ILLUMINATE DURING TEST, STAYS ILLUMINATED AFTER TEST. R & R NR 2 BAGGAGE COMPARTMENT SMOKE DETECTOR IAW AMM 26-15-01, OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT ASSY — INOPERATIVE (CABIN) · airframe 27,996 hrs · 24,248 cycles

EMERGENCY FLASHLIGHT NR 3 INOPERATIVE. R & R FLASHLIGHT AND HOLDER ASSY IAW AMM 33-50-16. OPS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,859 hrs · 24,146 cycles

DURING EMERGENCY LIGHT TEST FOUND FLOOR LIGHT STRIPS 6, 7, 8 INOPERATIVE. R & R INVERTER ASSY NR 6 IAW AMM 33-50-11. PERFORMED OPS CHECKED IAW AMM 33-50-00. OPS CHECKED GOOD.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 27,779 hrs · 24,091 cycles

COCKPIT SMELLS STRONGLY OF A FISH. CLEANED COCKPIT IAW AMM 25-00-00.

Part: CRADLE — WORN (FLASHLIGHT) · airframe 27,480 hrs · 23,831 cycles

FLASHLIGHT IS NOT CHARGING PROPERLY, VIBRATION CAUSE CHARGE LIGHT TO GO OUT. R & R FLASHLIGHT CRADLE ASSY IAW AMM 33-50-16, OPS CHECKED GOOD AT THIS TIME.

Part: LIGHT — DAMAGED (CABIN) · airframe 27,377 hrs · 23,747 cycles

THE LT NR 2 EMERGENCY LIGHT DAMAGED. R & R EMERGENCY LIGHT IAW AMM 33-50-12.

Part: LIGHT — DAMAGED (CABIN) · airframe 27,377 hrs · 23,747 cycles

THE LT NR 8 EMERGENCY LIGHT DAMAGED. R & R EMERGENCY LIGHT IAW AMM 33-50-12.

Part: LIGHT — DAMAGED (CABIN) · airframe 27,377 hrs · 23,747 cycles

THE LEFT NR 1 EMERGENCY LIGHT DAMAGED. R & R THE EMERGENCY LIGHT IAW AMM 33-50-12.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 27,377 hrs · 23,747 cycles

COCKPIT CEILING EMERGENCY LIGHT AT DOOR INOPERATIVE. R & R EMERGENCY LIGHT IAW AMM 32-50-05. OPS CHECKED GOOD

Part: LIGHT — DAMAGED (CABIN) · airframe 27,377 hrs · 23,747 cycles

THE LT NR 6 EMERGENCY LIGHT DAMAGED. R & R EMERGENCY LIGHT IAW AMM 33-50-12.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,166 hrs · 23,545 cycles

THE CREW REPORTED THAT UPON ENTERING THE ACFT THEY FOUND THE EMERGENCY LIGHTS ON THE FLOOR DEAD EXCEPT IN BACK OF ACFT. THE ACFT WAS REMOVED FROM SERVICE. EMERGENCY LIGHTS OPS CKD INITIALLY; AS PRECAUTIONARY MEASURE RECHARGED AND THE OPS CHECK WAS GOOD IAW MM 33-50-00. THE ACFT WAS RETURNED TO SERVICE.

Part: PITOT SYSTEM — CONTAMINATED (PITOT/STATIC SYS) · airframe 27,168 hrs · 23,547 cycles

THE CREW REPORTED THAT UPON DESCENT THE NR 2 ALTIMITER DISPLAYED A RED X. THE CREW RAN THE APPROPRIATE CHECKLIST AND DECLARED AN EMERGENCY. THE ACFT LANDED WITHOUT INCIDENT. THE ACFT WAS REMOVED FROM SERVICE. DRAINED WATER FROM PITOT SYS IAW AMM 34-13-00 AND OPS CHHECKED ADC SYS IAW AMM 34-15-00. THE ACFT WAS RETURNED TO SERVICE.

Part: CONTROL UNIT — UNSERVICEABLE (HORIZONTAL STAB) · airframe 26,991 hrs · 23,400 cycles

CREW REPORTED THAT AFTER TAKEOFF, RECEIVED A PTRIM MAIN INOP WARNING. DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. BACKUP TRIM WAS STILL OPERATIONAL. ACFT REMOVED FROM SERVICE. R & R THE HORIZONTAL STABILIZER CONTROL UNIT. OPS CHECKED GOOD IAW AMM 27-40-01 AND IAW AMM 27-40-00-700-802-A. ACFT RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 26,911 hrs · 23,320 cycles

DURING B INSPECTION FOUND THE EMERGENCY EXIT SIGN NEXT TO SERVICE DOOR INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY EXIT SIGN NEXT TO SERVICE DOOR IAW EMB 140 AMM 33-50-13. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR SEAL — UNSECURE (CABIN DOOR) · airframe 26,586 hrs · 23,051 cycles

ON FLIGHT 2890 THE CREW REPORTED THE MAIN CABIN DOOR SEAL WAS COMING OFF IN UPPER CORNER. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN DOOR FRAME RUBBER SEAL IAW EMB AMM 53-21-01. LEAK CHECK GOOD. PERFORMED TEST OF THE MAIN DOOR INTERNAL ACTUATING HANDLE IAW EMB AMM 52-18-00-820-801A. THE OPERATIONAL CHECK WAS WITHIN LIMITS WITH AN AVERAGE FORCE OF 40 LBS NEEDED TO OPEN DOOR. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STOP FITTING — OUT OF ADJUST (MAIN DOOR) · airframe 26,567 hrs · 23,035 cycles

ON FLIGHT 3268 THE FLIGHT ATTENDANT REPORTED THE MAIN DOOR WAS HARD TO OPEN AND IT WAS HARD TO LOCK THE HANDLE THAT KEEPS THE DOOR LOCKED IN THE OPEN POSITION. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED THREE SHIM WASHERS FROM MAIN DOOR OPEN STOP AS NEEDED. THE OPERATIONAL CHECK WAS GOOD IAW EMB 140 AMM 52-18-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 26,504 hrs · 22,982 cycles

FLIGHT 3567. MAIN CABIN DOOR HARD TO OPEN AND CLOSE. LUBRICATED MAIN DOOR SEAL IAW AMM 52-18-00-600-801. CHECKED GOOD WITH LOAD OF 37 LBS IAW AMM 52-18-00-820-801. AIRCRAFT RETURNED TO SERVICE.

Part: SEAL — LACK OF LUBE (PAX DOOR) · airframe 26,500 hrs · 22,973 cycles

FLIGHT 3466, FLIGHT ATTENDANT REPORTEDLY HAD DIFFICULTY OPENING MAIN PASSENGER DOOR, FUNCTIONS BUT WAS TOUGHER THAN NORMAL. LUBRICATED MAIN DOOR SEAL IAW AMM 52-18-00-600-801, 2J3. FUNCTIONS GOOD WITH LOAD OF 37 LBS IAW AMM 52-18-00-820-801. AIRCRAFT RETURNED TO SERVICE.

Part: DOOR — BINDING (MAIN PAX) · airframe 26,463 hrs · 22,935 cycles

FLIGHT 9802, CREW REPORTED MAIN PASSENGER DOOR VERY DIFFICULT TO OPEN AND CLOSE. LUBRICATED MAIN DOOR SEAL IAW AMM 52-18-00-600-801, 2J3. FUNCTIONED GOOD WITH LOAD OF 37 LBS IAW AMM 52-18-00-820-801. AIRCRAFT RETURNED TO SERVICE.

Part: SEAL — LACK OF LUBE (PAX DOOR) · airframe 26,446 hrs · 22,917 cycles

FLIGHT 3457, FLIGHT ATTENDANT REPORTED MAIN CABIN DOOR HARD TO OPEN. LUBRICATED MAIN DOOR SEAL IAW AMM 52-18-00-600-801, 2J3. CHECKED GOOD WITH LOAD OF 37LBS IAW AMM 52-18-00-820-801. AIRCRAFT RETURNED TO SERVICE.

Part: ROLLER — OUT OF ADJUST (MAIN DOOR) · airframe 26,427 hrs · 22,904 cycles

FOR FLIGHT 3567 THE FLIGHT ATTENDANT REPORTED THE MAIN DOOR WAS DIFFICULT TO OPEN AND CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. MAIN DOOR ROLLERS ADJUSTED IAW AMM 52-10-01 AND MAIN DOOR INTERNAL HANDLE TESTED IAW AMM 52-18-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 26,421 hrs · 22,900 cycles

ON FLIGHT 3482 THE FLIGHT ATTENDANT REPORTED THE MAIN CABIN DOOR WAS HARD TO OPEN AND CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBRICATED MAIN PASSENGER DOOR FRAME ROLLERS IAW EMB-145 53-21-02. THE OPERATIONAL CHECK OPENING & CLOSING OF MAIN DOOR WAS GOOD IAW EMB-145 AMM 52-10-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROLLER — DIRTY (CABIN DOOR) · airframe 26,383 hrs · 22,866 cycles

ON FLIGHT 4498 THE FLIGHT ATTENDANT REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND DIRT & DEBRIS IN ROLLERS CLEANED LUBED, REMOVED SECURITY STICKERS ON SEAL PERFORMED OPERATIONAL TEST OF MAIN PASSENGER DOOR. OPEN/ CLOSE GOOD AMM 52-10-00, 52-10-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR SEAL — DIRTY (MAIN DOOR) · airframe 26,373 hrs · 22,856 cycles

DURING MAINTENANCE INSPECTION FOUND THE MAIN DOOR DIFFICULT TO OPEN AND CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND DOOR SEAL STICKY. CLEANED DOOR SEAL AND PERFORMED OPERATIONAL CHECK IAW EMB AMM 52-10-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROLLER — MALFUNCTIONED (PAX DOOR) · airframe 26,090 hrs · 22,598 cycles

ON FLIGHT 4340 THE CREW REPORTED THE MAIN PASSENGER DOOR WAS HARD TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. SERVICED MAIN PASSENGER DOOR ROLLERS AS PER EMB-140 AMM 53-21-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 25,928 hrs · 22,463 cycles

ON FLIGHT 3333 THE FLIGHT ATTENDANT REPORTED THE MAIN CABIN DOOR WAS HARD TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBED MAIN DOOR IAW EMB 20-10-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GRIP — LOOSE (PAX DOOR) · airframe 25,902 hrs · 22,447 cycles

ON FLIGHT 2891 THE CREW REPORTED THE MAIN CABIN DOOR HANDLE GRIP WAS LOOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE PASSENGER DOOR HANDLE GRIP AS REQUIRED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FITTING — OUT OF ADJUST (CABIN DOOR) · airframe 25,886 hrs · 22,437 cycles

ON FLIGHT 2810 THE FLIGHT ATTENDANT REPORTED THE MAIN DOOR WAS DIFFICULT TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED WASHER ON NR 1 ARM FITTING LOWER PART AS PER ETN # EM-52-013R1 AND EMB AMM 52-18-06. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 52-18-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROLLER — DIRTY (ENTRY DOOR) · airframe 25,828 hrs · 22,391 cycles

ON FLIGHT 2985 THE CREW REPORTED THE MAIN ENTRY DOOR WAS DIFFICULT TO OPEN AND CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. CHECKED DOOR RIG IAW AMM 52-18-00. ALL RIG PINS GO IN, ALL GAPS ARE CORRECT. FOUND MAIN DOOR FRAME ROLLERS ALL GUMMED UP. CLEANED AND LUBED ROLLERS IAW AMM 53-21-02. THE OPERATIONAL CHECK WAS GOOD IAW 52-18-00, 35 LBS CLOSE, 45 LBS OPEN. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — MALFUNCTIONED (MAIN) · airframe 25,741 hrs · 22,322 cycles

FOR FLIGHT 2756 THE CREW REPORTED THAT AFTER ENGINE SHUT DOWN THE NR 1 AND NR 2 BATTERY VOLTS DROPPED TO 23.5 IN APPROX 10 SECONDS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 MAIN BATTERY IAW W/C 24-600-00 AND THE NR 2 BATTERY IAW W/C 24-600-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: VELOCITY SENSOR — INOPERATIVE (TE FLAP) · airframe 25,610 hrs · 22,226 cycles

ON FLIGHT 3233 THE CREW REPORTED THAT ON APPROACH INTO CRP WHEN SELECTING FLAPS FROM 9 TO 22 RECEIVED FLAP FAIL CAUTION MESSAGE ON EICAS. FLAPS WERE STUCK AT 20. FOLLOWED AOM 1 PROCEDURE AND DECLARED AN EMERGENCY AS A PRECAUTION. THE LANDING WAS UNEVENTUFL. PERFOMRED OPERATIONAL CHECK OF FLAPS IAW EMB AMM 27-51-00 MULTIPLE TIMES COULD NOT DUPLICATE. AIRCRAFT OK FOR CONTINUED SERVICE. ON FLIGHT 3230 REPEAT ISSUE THE CREW REPORTED THAT WHEN SELECTING FLAPS FROM 9 TO 22 THEY RECEIVED FLAP LOW SPEED ADVISORY ON EICAS. FLAPS WENT TO 22 ON SHORT FINAL, WE RECEIVED FLAP FAIL CAUTION. UNEVENTFUL LANDING WAS MADE. REMOVED AND REPLACED LEFT FLAP VELOCITY SENSOR IAW EMB AMM 27-51-12. REMOVED AND REPLACED THE CONNECTOR AT RIGHT HAND TRANSMISSION BRAKE. THE FUCNTIONAL FLIGHT CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — MALFUNCTIONED (TE FLAP) · airframe 25,598 hrs · 22,218 cycles

ON FLIGHT 2997 THE CREW REPORTED THAT DURING APPROACH FLAPS 22 AND CONFIGURING TO FLAPS 45 FLAP FAIL EICAS MESSAGE FLAP POSITION VERIFIED ON RMU AT 30 DEGREES AOM1 PROCEDURE COMPLIED WITH. THE CREW DECLARED AN EMERGENCY AND THE LANDING WAS UNEVENTFUL. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOLLOWED FIM TASK 27-51-00-810-816-A FOUND TO BE IN A TRANSITORY CONDITION. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 27-51-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HANDLE — OUT OF POSITION (CABIN DOOR) · airframe 24,952 hrs · 21,630 cycles

FLIGHT 4404, FLIGHT ATTENDANT REPORTED THE MAIN CABIN DOOR WAS HARD TO OPEN. INSPECTED AND FOUND MAIN DOOR HANDLE OFF THE ROLLER AND LOWER ROLLER LOOSE, INSTALLED HANDLE IAW EMB 140 AMM 52-18-05 AND RE-SECURED ROLLER IAW EMB 140 AMM 52-18-00, PERFORMED TEST OF HANDLE AND FOUND AT 41.88 LBS IAW EMB AMM 52-18-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HANDLE — UNSECURE (MAIN CABIN DOOR) · airframe 24,870 hrs · 21,550 cycles

FLIGHT 4167, FIRST OFFICER AND THE FLIGHT ATTENDANT REPORTED THEY WERE UNABLE TO OPEN MAIN CABIN DOOR FROM INSIDE. GATE AGENT OPENED DOOR FROM OUTSIDE. AIRCRAFT REMOVED FROM SERVICE. FOUND MAIN DOOR INTERNAL HANDLE NOT PROPERLY SECURED. SECURED HANDLE IAW AMM 52-18-05. OPS CHECKED GOOD IAW AMM 52-18-00. AIRCRAFT RETURNED TO SERVICE.

Part: FRAME — BENT (FUSELAGE) · airframe 24,808 hrs · 21,490 cycles

DURING MAINTENANCE INSPECTION FOUND FRAME 24 BENT BETWEEN STRINGER 14R & 15R. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FRAME 24 BETWEEN STRINGER 14R & 15R IAW EMB SRM 53-00-04, ITEM 4. FABRICATED SPLICE PLATE IAW SRM 51-30-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,600 hrs · 21,278 cycles

DURING B INSPECTION, FOUND THE RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED BULB IAW AMM 33-50-10-000-801-A/33-50-10-400-801-A. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SWITCH — UNSERVICEABLE (FLASHLIGHT) · airframe 24,600 hrs · 21,278 cycles

DURING B INSPECTION, FOUND THE AFT FLASH LIGHT HAS BROKEN SWITCH. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED AFT FLASHLIGHT. IAW 33-50-16-000-801-A AND 33-50-16-400-801-A. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,600 hrs · 21,278 cycles

DURING B INSPECTION, FOUND THE RIGHT FORWARD EXIT EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED BULB IN RIGHT FORWARD EXIT EMERGENCY LIGHT IAW AMM 33-50-10-000-801-A/33-50-10-400-801-A. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CRADLE — BROKEN (COCKPIT) · airframe 24,497 hrs · 21,176 cycles

DURING B INSPECTION FOUND THE CAPTAIN’S EMERGENCY FLASHLIGHT CRADLE BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S EMERGENCY FLASHLIGHT CRADLE IAW EMB AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (RT WING) · airframe 24,474 hrs · 21,155 cycles

DURING B INSPECTION FOUND THE AFT RIGHT WING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT WING AFT EMERGENCY LIGHT BULB IAW EMB AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 24,460 hrs · 21,140 cycles

DURING B INSPECTION FOUND THE RIGHT LOWER WING EMERGENCY LIGHT IS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BULB AS REQUIRED IAW EMB 140 AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 24,376 hrs · 21,061 cycles

DURING PS-1 INSPECTION FOUND THE RIGHT FORWARD LOWER FAIRING EXTERNAL EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LIGHT BULB IAW EMB-140 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. NO OTHER DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HANDLE — MISINSTALLED (PAX DOOR) · airframe 22,847 hrs · 19,715 cycles

ON FLIGHT 3965 THE CREW REPORTED, UNABLE TO OPEN THE MAIN PASSENGER DOOR FROM THE INSIDE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REINSTALLED PASSENGER DOOR INTERNAL HANDLE CORRECTLY IAW EMB 140 AMM 52-15-05. PERFORMED OPERATIONAL CHECK IAW EMB 140 AMM 52-18-00-820-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 22,749 hrs · 19,626 cycles

DURING MAINTENANCE BASE VISIT FOUND FRAME19 HAS ELONGATED HOLE JUST BELOW STRINGER 14. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FRAME 19 IAW EO EM-53MR-1847. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 22,749 hrs · 19,626 cycles

DURING MAINTENANCE BASE VISIT FOUND FRAME 17 HAS ELONGATED HOLE JUST BELOW STRINGER 14. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FRAME 17 IAW EO EM-53MR-1846. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 22,749 hrs · 19,626 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND FRAME 17 HAS AN ELONGATED HOLE JUST BELOW STRINGER 14. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FRAME 17 IAW EO EM-53MR-1846. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 22,749 hrs · 19,626 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND FRAME 19 HAS AN ELONGATED HOLE JUST BELOW STRINGER 14. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FRAME 19 IAW EO EM-53MR-1847. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 22,749 hrs · 19,626 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND THE RIGHT FRAME 23 CRACKED AT FLOOR LEVEL. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FRAME 23 IAW EO EM-53MR-1808. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,749 hrs · 19,626 cycles

DURING MAINTENANCE INSPECTION, FOUND CENTER OMEGA BEAM BETWEEN FRAME 24 AND 25 TO BE CORRODED. REPAIRED IAW SRM 53-00-10. ACFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,749 hrs · 19,626 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND THE LEFT OMEGA BEAM HAS CORROSION AT FRAME 20. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED LEFT HAND OMEGA BEAM AT FRAME 20 IAW EMB SRM 53-00-10. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: TRIM SWITCH — FAULTY (COCKPIT) · airframe 22,745 hrs · 19,621 cycles

MAIN PITCH TRIM FAIL IN CLIMB RETURNED TO DFW NO OTHER PROBLEMS NOTED. REMOVED AND REPLACED CAPTS CONTROL YOKE PITCH TRIM SWITCH IAW AMB 140 AMM 27-40-03. OPS CHECK GOOD AT THIS TIME.

Part: PROBE — INOPERATIVE (FUEL QTY) · airframe 22,367 hrs · 19,317 cycles

AFTER TAKEOFF THE CREW NOTICED THE FUEL GAUGES WERE FLUCTUATING. THE FUEL INDICATIONS CONTINUED TO RISE AND FALL. THE CREW DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT WAS REMOVED FROM SERVICE. ACCOMPLISHED REMOVAL AND INSTALLATION OF THE RIGHT 1A PROBE IAW AMM 28-41-02. OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: ELECTRONIC UNIT — INOPERATIVE (LANDING GEAR) · airframe 22,187 hrs · 19,181 cycles

ON FLIGHT 2707 THE CREW REPORTED THAT ON TAKEOFF DURING THE CLIMB RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE. THE CAPTAIN DECLARED AN EMERGENCY AND ELECTED TO RETURN TO DFW. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BRACKET — BROKEN (RT MLG) · airframe 22,102 hrs · 19,116 cycles

ON FLIGHT 4344THE CREW REPORTED THAT AFTER TAKEOFF ON CLIMBOUT AT 12000 FEET RECEIVED LANDING AIR/GROUND FAIL MESSAGE. THE MESSAGE STAYED ON CONTINUOUSLY AND REMAINED ON. THE CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO ORD. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT MAIN LANDING GEAR REAR AIR GROUND (WEIGHT ON WHEELS) PROXIMITY SWITCH BRACKET BUSHING AND HARDWARE IAW CMM 32-10-01. ADJUSTED AND OPERATIONAL CHECKS WERE GOOD IAW EMB AMM 32-63-05, REF NRWC 826-ORD-00250. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 22,029 hrs · 19,042 cycles

DURING MAINTENANCE BASE VISIT FOUND ALL THE EMERGENCY LIGHTS POWERED BY THE NR 1 BATTERY INOPERATIVE. THE AIRCRAFT WAS REMOVED FROM SERVICE. THE NR 1 BATTERY VOLTAGE WAS NORMAL BUT IT WAS DETERMINED THROUGH NEW BATTERY INSTALLATION THAT THE SUSPECT BATTERY COULD NOT SUPPORT A LOAD. REMOVED AND REPLACED THE NR 1 BATTERY AND CHARGER ASSEMBLY IAW EMB140 AMM 33-50-04. THE OPERATIONAL CHECK OF WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,275 hrs · 15,762 cycles

DURING MAINTENANCE BASE INSPECTION THE CARGO DOOR SILL WAS FOUND TO BE CORRODED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED CARGO DOOR SILL PLATE IAW EMBRAER SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 18,275 hrs · 15,762 cycles

DURING MAINTENANCE BASE INSPECTION AND DURING THE CARGO DOOR SILL REMOVAL FRAME 67 WAS FOUND TO BE CRACKED. AIRCRAFT REMOVED FROM SERVICE. REPAIRED FRAME 67 IAW SRM 53-00-04 FIGURE 201. AIRCRAFT RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,275 hrs · 15,762 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE SERVICE DOOR CENTER SILL CORRODED. AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CENTER SERVICE DOOR SILL IAW EMBRAER STRUCTURAL REPAIR MANUAL 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 18,275 hrs · 15,762 cycles

DURING MAINTENANCE BASE INSPECTION AND DURING THE CARGO DOOR SILL REMOVAL FOUND FRAME 66 TO BE CRACKED. AIRCRAFT REMOVED FROM SERVICE. REPAIRED FRAME 66 IAW EMBRAER STRUCTURAL REPAIRS MANUAL 53-00-04 FIGURE 201, ITEM 4. AIRCRAFT RETURNED TO SERVICE.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,275 hrs · 15,762 cycles

DURING MAINTENANCE BASE INSPECTION FRAME 65 SHEAR CLIP WAS FOUND TO BE CORRODED. AIRCRAFT REMOVED FROM SERVICE. REPAIRED FRAME 65 SHEAR CLIP IAW EO EM-53MR-1129. AIRCRAFT WAS RETURNED TO SERVICE.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,275 hrs · 15,762 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE CENTER HAT BEAM CORRODED AT FRAME 20. AIRCRAFT REMOVED FROM SERVICE. REPAIRED HAT BEAM IAW SRM 53-21-10. AIRCRAFT WAS RETURNED TO SERVICE.

Part: FITTING — CORRODED (FUSELAGE) · airframe 18,275 hrs · 15,762 cycles

DURING MAINTENANCE BASE INSPECTION FOUND FRAME 68 SHEAR CLIP TO BE CORRODED. AIRCRAFT REMOVED FROM SERVICE. REPAIRED SHEAR CLIP IAW EO-EM-53MR-1129. AIRCRAFT WAS RETURNED TO SERVICE.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,275 hrs · 15,672 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND THE CENTER HAT BEAM CORRODED AT FRAME 20. AIRCRAFT REMOVED FROM SERVICE. REPAIRED THE HAT BEAM IAW EMBRAER STRUCTURAL REPAIR MANUAL 53-21-10. AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRINGER — CHAFED (FUSELAGE) · airframe 18,275 hrs · 15,762 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THAT STRINGER 19 LEFT IS CHAFED AT FRAME 53. AIRCRAFT REMOVED FROM SERVICE. REPAIRED STRINGER 19 LT BETWEEN FRAMES 52-53 IAW SRM 53-24-03 FIGURE 201. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,362 hrs · 112,223 cycles

DURING MBV INSPECTION, FOUND SERVICE DOOR FORWARD SILL CORRODED. REMOVED AND REPLACED FORWARD SILL IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE.

Part: PROFILE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,362 hrs · 11,223 cycles

DURING MBV INSPECTION, FOUND VERTICAL PROFILE AT FRAME 23 AND STRINGER 15R CORRODED. REMOVED AND REPLACED PROFILE IAW EMB 140 SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 145,592 hrs · 11,223 cycles

DURING MBV INSPECTION, FOUND SERVICE DOOR AFT SILL CORRODED. REMOVED AND REPLACE AFT SILL IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,362 hrs · 11,223 cycles

DURING MBV INSPECTION, FOUND LT OMEGA BEAM CORRODED. REPAIRED OMEGA BEAM IAW SRM 53-00-10. AIRCRAFT WAS RETURNED TO SERVICE.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 145,592 hrs · 13,362 cycles

DURING MBV INSPECTION, FOUND SERVICE DOOR AFT SILL SUPPORT CLIP CORRODED. REMOVED AND REPLACED CLIP IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE.

Part: PROFILE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,362 hrs · 11,223 cycles

DURING MBV INSPECTION, FOUND CENTER HAT BEAM UPPER PROFILE TO RAMP PROFILE CORRODED AT FRAME 20 CROSSMEMBER. REMOVED AND REPLACED PROFILE IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE.

Part: FAN — OBSTRUCTED · airframe 13,294 hrs · 11,167 cycles

ACID BURNING ODOR ON FLIGHT DECK AND CABIN ON TAXI IN, NO VISIBLE SMOKE. FOUND INSULATION SUCKED INTO BOTH COOLING FANS. REPAIRED INSULATION IAW EMB AMM 25-81-01. PERFORMED GROUND ENGINE RUNS WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHT) · airframe 12,334 hrs · 10,397 cycles

FOUND CABIN EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED NUMBER 1 AND NUMBER 3 POWER SUPPLIES IAW AMERICAN EAGLE WORK CARD 33-700-19. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: SILL — CORRODED (FUSELAGE)

DURING INSPECTION FOUND SERVICE DOOR CENTER SILL CORRODED. REPAIRED SERVICE DOOR SILL BY INSTALLING A DOUBLER IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING INSP, FOUND LT OMEGA BEAM AT FRAME 20 LT, CORRODED. REPAIRED OMEGA BEAM BY INSTALLING A DOUBLER IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K)

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

FA REPORTED A BURNING SMELL AT 16000 FT. DECLARED EMERGENCY AND RETURNED TO FIELD. THE FLIGHT ATTENDANT NOTICED AFTER LANDING THAT THE FORWARD OVERHEAD ENTRY LIGHT ABOVE HIS SEAT WAS BURNED OUT. CONTACTED MAINTENANCE, VERIFIED THAT THE BULBS WERE BURNED AND REPLACED THEM. OPS CHECK WAS GOOD AND NO SMELL WAS REPORTED. (K)