N822AE

Part: FLASHLIGHT — MISSING (AFT CABIN) · airframe 39,383 hrs · 36,055 cycles

AFT F/A FLASHLIGHT MISSING. C/A: FLIGHT CREW PLACARDED AFT F/A FLASHLIGHT, REF MEL 25-53AUTH 110065-C MOC 680820.

Part: SIGN — INOPERATIVE (CABIN) · airframe 38,967 hrs · 35,567 cycles

FWD EMERG EXIT SIGN AT 11 ABC INOP. REPLACED EMERG EXIT SIGN FWD AT SEAT 11 ABC OPERATION CHECK GOOD PER AMM 33-50-10.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,866 hrs · 35,480 cycles

MAIN DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED MAIN DOOR EXTERNAL EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-06-000-801-A AND 33-50-06-400-801-A. OPS CHECK GOOD.

Part: SLEEVE — LEAKING (AC EXHAUST) · airframe 38,121 hrs · 34,730 cycles

DURING CLIMB PACK 1/2 VLV CLOSED. LEVEL AT 13,000 CAB ALT CONTINUED TO CLIMB AFTER RESETING PACK 1. RETURN TO DFW-C/A-FOUND LEAK AT THE AIR CONDITIONING EXHAUST SLEEVE. RESECURED CLAMPS REF. AMM 20-10-10. PERFORMED AIR CONDITIONING OPC IAW AMM EMB 140 AMM 21-00-00. OPC OK. NO LEAK NOTED.

Part: O-RING — LEAKING (NR 2 BLEED) · airframe 38,081 hrs · 34,683 cycles

BLEED 2 LEAK ENROUTE. COMPLIED WITH QRH PROCEDURES. DID NOT LAND OVERWEIGHT-C/A-FOUND LEAK ON JOINT 20 AND 22 REMOVED AND REPLACED O-RING IAW EMB 140 AMM 36-11-10. PERFORMED AIR BLEED SYSTEM ON BLEED 2 SYS ONLY IAW EMB 140 AMM 36-00-00 TASK 36-00-00-700-803-A. OPC OK.

Part: DRIVE ASSY — INOPERATIVE (TE FLAPS) · airframe 38,065 hrs · 34,668 cycles

FLAP FAIL AFTER LANDING STUCK AT 1-C/A-REMOVED AND REPLACED FLAP SHROUD DRIVER IN LH, INBOARD FLAP 1 IAW EMB 140 AMM 27-50-00 AND S.B. NO:145-57-0012. OPERATIONAL CHECK GOOD IAW EMB 140 AMM 27-51-00-700-801-A.

Part: WARNING MESSAGE — FALSE ACTIVATION (NR 1 A/C PACK) · airframe 37,884 hrs · 34,503 cycles

PACK 1 FAIL MSG IN FLIGHT. EMERGENCY DECLARED FLT -C/A-PERFORMED OPERATIONAL CHECK OF PACK 1 IAW ERJ 140 AMM 21-20-00-700-801-A. OPS CHECK NORMAL. NO DEFECTS NOTED

Part: MECHANISM — LACK OF LUBE (CABIN DOOR) · airframe 37,552 hrs · 34,158 cycles

FA REPORTS MAIN CABIN DOOR IS DIFFICULT TO CLOSE DUE TO LOOSE HANDLE-C/A-AT THIS TIME LUBRICATED MAIN DOOR LOCKING MECHANISM IAW AMM 52-10-00.OPS. CK FOUND OK.DOOR HANDLE FOUND OK.

Part: NOT REPORTED — DENTED (FUSELAGE) · airframe 37,054 hrs · 33,644 cycles

DENT FOUND BELOW CARGO DOOR BETWEEN FRAMES 66 AND FRAMES 67 AND STRG21R AND STRG 20L. MAJOR REPAIR. C/A-REPAIRED DENT BELOW CARGO DOOR IAW ERS-EM-53MR-3826. SEE NRWC 822-ABI-03335 FOR DETAILS.

Part: SMOKE DETECTOR — NO TEST (CARGO BAY) · airframe 36,990 hrs · 33,571 cycles

CAPT REPORTS CARGO SMOKE DETECTOR PUSH BUTTON LIGHT STAYS ON WHEN TESTED. REMOVED AND REPLACED #2 CARGO SMOKE DETECTOR IAW E140 AMM 26-15-01 AND SMOKE DETECTOR RELAY K0629 IAW E140 AMM 20-13-02 OPS CK GOOD

Part: TRIM SWITCH — DIRTY (COCKPIT) · airframe 36,760 hrs · 33,328 cycles

"PIRIM MAIN INOP" MSG DURING FLIGHT. C/A-ACCOMPLISHED INSPECTION, CLEANING AND LUBRICATION OF PILOT AND CO-PILOT PITCH TRIM SWITCHES IAW AMM 27-40-03. ALSO PERFORMED OPS CHECK OF HOR/STAB ELECTRICAL/ELECTRONIC SYSTEM, ALL CHECKS GOOD IAW AMM 27-40-00.

Part: ROLLER — OBSTRUCTED (CABIN DOOR) · airframe 36,388 hrs · 33,001 cycles

MAIN CABIN DOOR HARD TO OPEN + CLOSE. C/A-REMOVED FOD FROM MAIN DOOR ROLLER. OPENED AND CLOSED DOOR SEVERAL TIMES. HANDLE LOAD IS 40 LBS. OPC GOOD REF IAW AMM 52-18-00.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 36,090 hrs · 32,702 cycles

FOUND EMERGENCY EXIT LIGHT IN FWD CABIN BY GALLEY INOP. C/A-REMOVED AND REPLACED EMERGENCY LIGHT DC/AC INVERTER 1 IAW AMM 33-50-11. OPC GOOD.

Part: WHEEL — DEFECTIVE (NLG) · airframe 36,006 hrs · 32,619 cycles

HIGH SPEED VIBRATION APPEARS TO COME FROM NOSE WHEEL 40-70 KNOTS. C/A-FOUND NLG TIRES TO BE OUT OF ROUND. REMOVED AND REPLACED LT NLG WHEEL AND TIRE ASSY IAW W/C 32-700-17. REMOVED AND REPLACED RT NLG WHEEL AND TIRE ASSY IAW W/C 32-700-17. GREASED NLG TORQUE LINKS IAW AMM 32-34-00. A/C OK FOR SERVICE. NLG WHEEL P/N 3-1551 S/N 10263014P.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,498 hrs · 32,100 cycles

AFT FLOOR PROXIMITY STRIP AT ROW 16 INOP-C/A-REMOVED AND REPLACED AFT FLOOR PROXIMITY STRIP AT ROW 16A C/W IAW AMM 33-50-01. OPS IS GOOD.

Part: PROXIMITY SWITCH — CORRODED (SPOILER) · airframe 35,423 hrs · 32,025 cycles

"SPOILER FAIL" EICAS CAUTION PRESENTED IN FLIGHT MULTIPLE TIMES WITH SPEED BRAKE LEVER CLOSED. FOUND CORROSION ON SPOILER PROX SWITCHES. R&R ALL FOUR SPOILER PROX SWITCHES IAW AMM 27-63-04, OPS CHECK GOOD.

Part: HANDLE — FAILED (COCKPIT) · airframe 35,400 hrs · 32,003 cycles

FIRE EXTINGUISHER T HANDLE DOES NOT ILLUMINATE DURINGFIRE DET TEST. REMOVED AND REPLACED RT ENG FIRE EXTINGUISHING HANDLE IAW AMM 26-21-01. OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 35,344 hrs · 31,933 cycles

EMERGENCY LIGHTS AT EXIT SIGNS AT EMERGENCY EXIT WING DOORS ARE INOP. REMOVED AND REPLACED NR 3 BATTERY POWER SUPPLY IAW AMM 33-50-04. OPERATIONAL CHECK GOOD. BATTERY CHARGER ASSY P/N 11-0049 S/N 12334.

Part: ROLLER — DIRTY (MAIN DOOR) · airframe 35,312 hrs · 31,891 cycles

FLIGHT ATTENDANT REPORTED MAIN DOOR DIFFICULT TO CLOSE AND LATCH. C/A-CLEANED & LUBRICATED MAIN DOOR FRAME ROLLERS IAW AMM 53-21-02. OPC GOOD AT THIS TIME.

Part: DUCT — LEAKING (NR 2 BLEED SYS) · airframe 35,298 hrs · 31,872 cycles

NR 2 BLEED LEAK, IN FLIGHT, MESSAGE STAYED PRESENT FOR AT LEAST 5 - 6 MINUTES BEFORE GOING AWAY. DIVERTED BACK TO DEPARTURE. FOUND THE DUCT IN THE NR 2 PYLON LEAKING, REMOVED AND REPLACED THE DUCT IAW AMM 36-11-09, OPS AND LEAK CHECKED GOOD.

Part: CLAMP — LEAKING (NR 2 BLEED SYS) · airframe 35,298 hrs · 31,870 cycles

NR 2 ENGINE BLEED LEAK, NR 2 BLEED LEAK.. ADJUSTED THE CROSSBLEED CLAMPS IAW AMM 36-10-01, PERFORMED AN OPS CHECK OF THE NR 2 BLEED SYSTEM, NO MESSAGE NOTED WITH THE NR 2 ENGINE RUNNING AND PACKS RUNNING IAW AMM 36-00-00.

Part: DRAG ANGLE — CRACKED (FRAMES 75 - 76) · airframe 35,296 hrs · 31,868 cycles

RIGHT FWD VERTICAL STAB TO FUSELAGE DRAG ANGLE WAS CRACKED AT THE AFT END FASTENER. REMOVED AND REPLACED THE DRAG ANGLE IAW SRM 51-40-02.

Part: FITTING — CRACKED (FRAME 20) · airframe 35,296 hrs · 31,868 cycles

PAX DOOR CUTOUT REINFORCEMENT FITTING WAS CRACKED AT FRAME 20, STRINGER 3L. REMOVED AND REPLACED THE REINFORCEMENT FITTING IAW SRM 51-40-02.

Part: FRAME — CRACKED (FRAME 23) · airframe 35,296 hrs · 31,868 cycles

FRAME 23 WAS CRACKED BETWEEN STRINGERS 15R - 16R. REPAIRED THE FRAME IAW SRM 53-00-04.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 35,296 hrs · 31,868 cycles

EMERGENCY LIGHT STRIP AT 241BF HAD BROKEN WIRES ON THE ACFT SIDE. REPAIRED THE WIRES IAW SWPM 20-21-00.

Part: SUPPORT — CRACKED (RT OVERWING EXIT) · airframe 35,296 hrs · 31,868 cycles

RIGHT OVERWING EMERGENCY EXIT HATCH LOWER SUPPORT WAS CRACKED AT THE FWD END, INSIDE LOWER BAY. REMOVED AND REPLACED THE SUPPORT IAW SRM 51-40-02.

Part: YOKE — CRACKED (LT WING) · airframe 35,296 hrs · 31,868 cycles

LEFT ENGINE FWD LOWER PYLON YOKE WAS CRACKED. REMOVED AND REPLACED THE LT FORWARD LOWER PYLON YOKE FITTING IAW EO EM-54MR-386.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 35,296 hrs · 31,868 cycles

EMERGENCY EXIT LIGHT LENS CRACKED ON CEILING PANEL 253CLC-C/A-COMPLETE:REMOVED AND REPLACED EMERGENCY EXIT LIGHT LENS ON CEILING PANEL 253 CLC IAW CD CMM 25-28-24

Part: BATTERY — DISCHARGED (CABIN) · airframe 35,290 hrs · 31,862 cycles

EMERGENCY LIGHT INOP AT ROW 7A FLOOR PROXI STRIP, AND OVERWING HATCH. REMOVED AND REPLACED NUMBER 3 BATTERY AND BATTERY POWER SUPPLY IAW AMM 33-50-04. OPS CK GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 35,204 hrs · 31,788 cycles

FOUND BATTERY POWER SUPPLY NR 3 TO BE INOP DURING PS-1 CHECK. REMOVED AND REPLACED NR 3 BATTERY POWER SUPPLY IAW AMM 33-50-04 OPC GOOD A/C OK FOR SERVICE.

Part: O-RING — DAMAGED (BLEED AIR SYS) · airframe 35,122 hrs · 31,689 cycles

BLEED 1 LEAK IN FLIGHT. INSPECTED FOR BLEED 1 LEAK FOUND JOINT 11 AND 13 LEAKING. REMOVED AND REPLACE ORINGS AT JOINT 11 AND 13 AND OPS CHECKS AND LEAK CHECK GOOD IAW AMM 36-11-10.

Part: ACM — FAILED (LEFT) · airframe 34,616 hrs · 31,154 cycles

BOTH PACKS INOPERATIVE DURING CLIMB OUT. REMOVED AND REPLACED THE LT ACM IAW AMM 21-51-03. OPS CHECKED GOOD. NO LEAKS NOTED. R & R THE CONDENSER MIXER IAW AMM 21-51-04. OPS CHECK FAILED. COMPLIED WITH A NR 2 PACK OPS CHECK IAW AMM 21-51-00. FOUND COUPLING NR 6 DAMAGED AND LEAKING. REMOVED AND REPLACED THE COUPLING IAW ETN-EM-21-056. OPS CHECKED GOOD IAW AMM 21-51-00. NO LEAKS FOUND.

Part: SIGNAL COND UNIT — FAILED (FUEL) · airframe 34,463 hrs · 30,977 cycles

AFTER TAKEOFF, FUEL QUANTITY INDICATIONS WENT TO AMBER DASHES AND EICAS MESSAGE E1/2 LOW FUEL MESSAGE PRESENTED. RMOVED AND REPLACED THE WING FUEL CONDITIONING UNIT IAW AMM 28-40-01, OPS CHECKED GOOD IAW AMM 28-40-00.

Part: SMOKE DETECTOR — CONTAMINATED (LAVATORY) · airframe 34,462 hrs · 30,975 cycles

LAVATORY SMOKE DETECTION TEST FAILED IAW PS-2 MTX W. C. CLEANED LINT FROM THE LAVATORY SMOKE DETECTOR, PERFORMED AN OPS CHECK IAW AMM 26-14-00. OPS CHECKED GOOD.

Part: FLASHLIGHT — FAILED (CABIN) · airframe 34,394 hrs · 30,918 cycles

VISIBLE SMOKE IN THE COCKPIT, CLIMBING THROUGH FL180. SMELLED LIKE ELECTRICAL SMOKE, FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN. FOUND THE FWD FA AND AFT FA FLASHLIGHT TO HAVE ELECTRICAL ODORS.

Part: DOOR — OUT OF ADJUST (MAIN PAX) · airframe 34,182 hrs · 30,715 cycles

F/A REPORTED THE MAIN CABIN DOOR DIFFICULT TO OPEN. DOOR ADJUSTED AND TESTED IAW AMM 52-10-01. OPS CHECKED GOOD.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 33,594 hrs · 29,988 cycles

FWD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT CRADLE IS BROKEN. REMOVED AND REPLACED THE CRADLE IAW AMM 33-50-16. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,422 hrs · 29,819 cycles

EMERGENCY FLOOR PROXIMITY LIGHTING STRIP AT ROWS 15 AND 16 INOP. REMOVED AND REPLACED EMERGENCY FLOOR PROXIMITY LIGHTING STRIP AT ROWS 15-16 IAW AMM33-50-12. OPS CHECK GOOD.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 32,921 hrs · 29,309 cycles

MAIN CABIN DOOR VERY DIFFICULT TO OPEN. CLEANED AND LUBRICATED LOWER FORWARD AND AFT ROLLERS ON MAIN CABIN DOOR IAW EMB-140 AMM 52-18-00. OOR OPENS AND CLOSES PROPERLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,441 hrs · 28,842 cycles

AFT AISLE EMERGENCY CEILING LIGHT INOPERATIVE. R & R AFT AISLE EMERGENCY CEILING LIGHT BULB IAW AMM 33-50-08, OPS CK GOOD.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 32,012 hrs · 28,381 cycles

CARGO DOOR CUT OUT LOWER CTR SILL CORRODED. REPAIRED CARGO DOOR CTR SILL IAW SRM 51-40-02 & 51-20-01.

Part: CASE — CHAFED (EMERGENCY LIGHT) · airframe 32,012 hrs · 28,381 cycles

RIGHT OVERWING PANEL EMER LIGHT ASSEMBLY INTERIOR CASE IS CHAFED. R & R RT OVERWING PANEL EMER LIGHT ASSEMBLY IAW AMM 33-50-10.

Part: FRAME — CORRODED (FUSELAGE) · airframe 32,012 hrs · 28,381 cycles

FRAME 65 IS CORRODED UNDER FWD LOWER CARGO DOOR GUIDE PLATE. REPAIRED FRAME 65 UNDER FWD LOWER CARGO DOOR GUIDE PLATE IAW SRM 53-31-04 ITEM 4E FIG 212.

Part: HINGE FITTING — CORRODED (ELEVATOR TAB) · airframe 32,012 hrs · 28,381 cycles

LEFT ELEVATOR SERVO TAB INBD HINGE FITTING CORRODED AT BONDING WIRE ATTACHMENT. R & R LT ELEVATOR SERVO TAB INBD HINGE FITTING IAW AMM 55-22-01, SRM 51-20-03 & CPM 51-21-04. SN 2149. SEE BOW 216840 FOR INSTALLATION OF BOLT WITH BONDING JUMPER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 31,989 hrs · 28,358 cycles

LEFT UPPER FUSELAGE SKIN CRACKED IN 2 PLACES. CRACK 1 IS JUST AFT OF FRAME 75 & ABOVE STRINGER 2L. CRACK IS APPROX 3/8" LONG. CRACK 2 IS AT THE FIRST FASTENER AFT OF FRAME 75 ON STRINGER 2L, CRACK IS APPROX 1/4". FABRICATED & INSTALLED REPAIR PARTS FOR LT FRAME 75 IAW ERS-EM-53MR-2066. SEE TURN OVER FOR DETAILS.

Part: SKIN — CRACKED (FUSELAGE) · airframe 31,989 hrs · 28,358 cycles

RIGHT UPPER FUSELAGE SKIN CRACKED AT FIRST FASTENER, BELOW STRINGER 2R. CRACK IS APPROX 3/8" LONG. PERFORMED REPAIR OF RT UPPER FUSELAGE SKIN CRACKS IAW ERS-EM-53MR-2072.

Part: WIRE — BROKEN (CABIN) · airframe 31,492 hrs · 27,820 cycles

AFT ROW EMER LIGHT FLOOR STRIP HAS BROKEN WIRE. R & R AFT ROW EMER LIGHT FLOOR STRIP IAW MM 33-50-12. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,342 hrs · 27,686 cycles

MAIN DOOR OVERHEAD EMER LIGHT INOPERATIVE. R & R MAIN DOOR OVERHEAD EMER LIGHT IAW AMM 33-50-06. OPERATIONS CHECKED GOOD.

Part: BRAKE — FIRE (LT MLG) · airframe 30,912 hrs · 27,258 cycles

AFTER LANDING, ACFT BEHIND US REPORTED LT INBD TIRE ON FIRE, THEN WENT OUT SHORTLY. R & R NR 2 BRAKE ASSEMBLY IAW WC 32-600-14. R & R NR 2 BRAKE TEMP SENSOR IAW AMM 32-47-01. OPERATIONS CHECKED GOOD.

Part: CONNECTOR — DAMAGED (ELT) · airframe 30,452 hrs · 26,853 cycles

ELT FAILED TEST, WC 25-700-07, TRIPLE FLASHES. DEFERRED IAW MEL 25-59. MX PROCEDURES COMPLIED WITH. R & R FWD ELT& COAXIAL CONNECTOR IAW SWPM 20-20-01. OPERATIONS CHECK GOOD & MEL 25-59 RESTORED.

Part: ELECTRONIC UNIT — FAULTY (LANDING GEAR) · airframe 30,220 hrs · 26,669 cycles

ON CLIMB OUT RELAY CLICKING BEHIND CAPTAIN SEAT. CYCLED ALL 3 PUMPS, FUEL, CLICKING REMAINED, RETURNED TO LAND. REPLACED LG ELECTRONICS UNIT IAW AMM 32-32-01. OVERWEIGHT LANDING, LANDING PERFORMED SINK RATE LAST 500 FEET AT 100 FEET PER MINUTE. OVERWEIGHT LANDING INSPECTION NOT REQUIRED DUE TO SINK RATE IAW MNTC WC 05-200-01 & AMM 05-50-25.

Part: PITOT SYSTEM — CONTAMINATED · airframe 30,128 hrs · 26,607 cycles

IN CRUISE AT ALT OF 32000 THE CAP'S AIRSPEED FAILED & STARTED TO DECREASE FROM 234 KTS TO A LOW OF 150 KTS. AT 150 KTS THE AIRSPEED CLIMBS RAPIDLY BACK TO NORMAL. WE HAD STARTED A DECENT TO 24'000 WHEN THE AIRSPEED RETURNED TO NORMAL. THE ACFT HAD RECENTLY CLIMBED THOUGH MODERATE RAIN & CLOUDS AFTER AIRSPEED RETURNED TO NORMAL. CONTINUED TO WORK NORMALLY FOR THE REMAINDER OF THE FLIGHT. DRAINED WATER FROM PITOT SYS & PERFORMED OPERATIONS CHECK & LEAK CHECK IAW AMM 34-13-00. OPERATIONS CHECKED GOOD. ACFT IS COMPLIANT FOR CONTINUED CAT II OPERATION.

Part: CONNECTOR — DIRTY (WHEEL SPEED SENS) · airframe 29,140 hrs · 25,683 cycles

DURING TAXI BELOW 25 KNOTS WHILE APPLYING BRAKES, ANTI-SKID CYCLES ON & OFF. CLEANED WHEEL SPEED SENSOR CONNECTOR W514 IAW SWPM 20-50-00. MAIN BRAKE SYS OPS CHECKED GOOD IAW AMM 32-41-00. TAXIED ACFT IAW GHC. NO DEFECTS NOTED.

Part: CONTROL UNIT — MALFUNCTIONED (BRAKE SYSTEM) · airframe 29,140 hrs · 25,683 cycles

DURING TAXI AT APPROX 15 KTS WHILE APPLYING LIGHT BRAKING THE ANTI-SKID WAS ACTIVATING. AT ONE POINT FULL TOE BRAKES WERE APPLIED WITH NO BRAKING ACTION. REMOVED & INSTALLED BCU IAW AMM 32-41-02 & NR 1 BRAKE IAW WC 32-600-14.

Part: FLASHLIGHT — ODOR (CABIN) · airframe 28,980 hrs · 25,579 cycles

FLIGHT ATTENDANT FWD FLASHLIGHT BURNING SMELL IN CLIMB. R & R FWD FLIGHT ATTENDANT FLASHLIGHT ASSEMBLY IAW AMM 33-50-16, OPERATIONS CHECKED GOOD.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 28,638 hrs · 25,300 cycles

AFTER E1 SHUTDOWN RELAYS MADE CLICKING NOISE FOR 30 SEC THEN NOTICED SMELL OF ELEC. INSPECTED LT & RT SIDE RELAY COMPARTMENT & AFT FASTENER & CLOSET FOR ELECT CONTACTS WITH ENG. BLEED PACK ON & OFF AS WELL AS INTERIOR LIGHTINGS. FOUND NO UNUSUAL RELAY CLICKING OR ANY SMELL. ACFT RETURNED TO SERVICE IAW AMM 20-13-03 21-20-10 23-81-00.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 28,408 hrs · 25,068 cycles

CAPTAIN`S FLASHLIGHT INOPERATIVE. RE LAMP CAPTAIN`S FLASHLIGHT, OPERATIONS CHECKED GOOD.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 27,393 hrs · 24,109 cycles

LEFT OMEGA BEAM HAS CORROSION AT CARBON CROSSBEAM BETWEEN FRAMES 57 AND 59. REPAIRED OMEGA BEAMIAW E.O. EM-53MR-2192. AIRCRAFT RETURNED TO SERVICE.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 27,393 hrs · 24,109 cycles

RT HAT CHANNEL OTBD SUPPORT ANGLE IS CRACKED BETWEEN FRAMES 47 AND 48. REPAIRED IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 27,393 hrs · 24,109 cycles

FLOOR SUPPORT ANGLE BETWEEN FRAMES 23 AND 24 IS CRACKED BETWEEN STRINGERS 14 AND 15R. INSTALLED NEW FLOOR SUPPORT ANGLE IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 27,393 hrs · 24,109 cycles

LEFT MLG WHEEL WELL AFT BULKHEAD WALL IS CRACKED. REPAIRED LT MLG WHEEL WELL AFT BULKHEAD WALL IAW SRM 53-23-12 FIGURE 205. AIRCRAFT RETURNED TO SERVICE.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 27,393 hrs · 24,109 cycles

RT HAT CHANNEL INBD SUPPORT ANGLE IS CRACKED BETWEEN FRAMES 47 AND 48. REPAIRED IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 27,393 hrs · 24,109 cycles

CARGO DOOR HOLD OPEN ROD SUPPORT ON AFT SIDE OF FRAME 68 IS CRACKED. REMOVED AND REPLACED ROD SUPPORT IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 27,393 hrs · 24,109 cycles

FRAME 23 IS CRACKED BETWEEN STRINGERS 14 AND 15 RIGHT. REPAIRED FRAME IAW SRM 53-00-04. AIRCRAFT RETURNED TO SERVICE.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 27,393 hrs · 24,109 cycles

FRAME SUPPORT ANGLE AT FRAME 24 IS CRACKED BETWEEN STRINGER 14 AND 15 RIGHT. INSTALLED NEW ANGLE IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: STRINGER — CORRODED (21 LEFT) · airframe 27,393 hrs · 24,109 cycles

STRINGER 21L BETWEEN FRAME 12 AND FRAME 13 HAS AREAS OF CORROSION. REPAIRED STRINGER IAW SRM 53-00-03. AIRCRAFT RETURNED TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 27,393 hrs · 24,109 cycles

FRAME 72 IS BENT AND CRACKED JUST ABOVE THE RT OTBD FLOOR SUPPORT. COMPLIED WITH REPAIR OF FRAME IAW SRM 53-00-04. AIRCRAFT RETURNED TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 27,393 hrs · 24,109 cycles

FRAME 10 IS CRACKED AT THE TOP BELOW THE F/O DV WINDOW SILL. REMOVED AND REPLACED THE UPPER HALF OF RT SIDE FR 10 IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: SILL — CORRODED (SERVICE DOOR) · airframe 27,393 hrs · 24,109 cycles

CENTER SERVICE DOOR SILL HAS CORROSION. REMOVED AND REPLACED SILL IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 27,393 hrs · 24,109 cycles

FRAME 23 SUPPORT ANGLE IS CRACKED BETWEEN STRINGERS 14 AND 15 RIGHT. REMOVED AND REPLACED SUPPORT ANGLE IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 27,393 hrs · 24,109 cycles

NR 6 EMERGENCY LIGHT STRIP INOPERATIVE, FOUND BROKEN WIRE. R & R NR 6 EMERGENCY LIGHT STRIP IAW AMM 33-50-12. OPS CHECKED GOOD.

Part: WIRE — PULLED (EMERGENCY LIGHT) · airframe 27,393 hrs · 24,109 cycles

RIGHT AFT STOWAGE EMERGENCY LIGHT WIRES PULLED OUT OF CONNECTOR. REPLACED RT AFT STOWAGE EMERGENCY LIGHT WIRE CONNECTORS AND ACCOMPLISHED FLASHLIGHT OPS CHECK IAW AMM 33-50-16-400-801-A STEP 3J(2).

Part: FITTING — DAMAGED (LT AILERON) · airframe 27,393 hrs · 24,109 cycles

LEFT AILERON HAS TOOL DAMAGED ON INBD HINGE FITTING AREA. R & R LT AILERON INBD HINGE FITTING IAW EO EM-27MR-112.

Part: WIRE — TORN (EMERGENCY LIGHT) · airframe 27,393 hrs · 24,109 cycles

EMERGENCY LIGHT STRIP, NR 4 WIRES ARE TORN OFF. R & R EMERGENCY LIGHT STRIP NR 4 IAW AMM 33-50-12. REF BOW137724 FOR OPS CHECK.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,393 hrs · 24,109 cycles

NR 4 EMERGENCY LIGHTING BATTERY, NO POWER FROM CHARGER TO LIGHTS. R & R NR 4 EMERGENCY LIGHTING BATTERY.

Part: LIGHT — DAMAGED (CABIN) · airframe 27,393 hrs · 24,109 cycles

EMERGENCY LIGHT STRIP NR 1 IS TORN & CRACKED. REPLACED THE NR 1 EMERGENCY LIGHT STRIP IAW AMM 33-50-12. REF BOW 137724 FOR OPT CHECK.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 27,393 hrs · 24,109 cycles

EMERGENCY LIGHT STRIP CONNECTORS AT FLOOR PANELS 251BF AND 251DF BROKEN. REPLACED CONNECTORS AT SPLICES SP9036 AND SP9116 IAW SWPM 20-21-00. SEE BOW 137724 FOR OPS CHECK.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,393 hrs · 24,109 cycles

EMERGENCY LIGHTS NOT WORKING AFT OF EMERGENCY EXITS. REPLACED NR 4 EMERGENCY LIGHT BATTERY AND CHARGER IAW WC 33-700-19.

Part: CRADLE — DAMAGED (FLASHLIGHT ASSY) · airframe 27,277 hrs · 24,011 cycles

F/A FLASHLIGHT CRADLE DAMAGED. R & R FWD CABIN FLASHLIGHT AND CRADLE IAW AMM 33-50-16. OPS CHECKED GOOD.

Part: LAMP — UNSERVICEABLE (EMERGENCY LIGHT) · airframe 27,239 hrs · 23,974 cycles

EMERGENCY LIGHT OVER SEAT 11A INOPERATIVE. R & R LAMP IAW AMM 33-50-08. OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE INDICATION (NR 2 OIL TEMP) · airframe 27,186 hrs · 23,922 cycles

DURING CLIMBOUT, NR 2 ENGINE OIL TEMP INCREASED TO 115 DEGREES AT FL 350. DURING DESCENT IT STAYED IN 100 DEGREE RANGE. PERFORMED GROUND RUNS AT MAX TAKEOFF, CRUISE, AND IDLE. NR 2 ENGINE OIL TEMP REMAINED WITHIN LIMITS IAW MM 71-00-00-200-801. PEFORMED CMC DOWNLOAD BEFORE AND AFTER ENGINE RUNS WITH NO EXCEEDANCE LIMITS PRESENT. ACFT OK FOR RETURN TO SERVICE.

Part: HOLDER — BROKEN (COCKPIT) · airframe 26,648 hrs · 23,402 cycles

DURING B INSPECTION FOUND THE FIRST OFFICER’S FLASHLIGHT HOLDER BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT ASSEMBLY IAW EMB 140 AMM 33-50-16-000-801-A AND 33-50-16-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 25,979 hrs · 22,786 cycles

ON FLIGHT 3318 THE CREW REPORTED THE FIRST OFFICER’S FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT IAW GENERAL MAINTENACE PRACTICES NO DEFECTS NOTED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CRADLE — BROKEN (COCKPIT) · airframe 25,649 hrs · 22,517 cycles

ON FLIGHT 2723 THE CREW REPORTED THE COCKPIT FLASHLIGHT CRADLE BEHIND THE CAPTAINS SEAT WAS BROKEN. IT WOULD NOT HOLD THE FLASHLIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE COCKPIT FLASHLIGHT CRADLE BEHIND THE PILOT SEAT IAW EMB 140 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLAPPER VALVE — FAULTY (RT WING) · airframe 25,480 hrs · 22,401 cycles

ON FLIGHT 3211 THE CREW WAS ADVISED BY DEPARTURE CONTROL THAT AN AA PILOT SAID IT LOOKED LIKE A LOT OF FUEL WAS COMING OUT OF THE RIGHT WING. A PASSENGER ALSO NOTIFED THE FLIGHT ATTENDANT ABOUT A LOT OF WHITE VAPOR (FUEL) COMING FROM THE RIGHT WING. THE FLIGHT ATTENDANT CONFIRMED THIS. THE CREW COMPLIED WITH THE FUEL LEAK CHECK LIST AND RETURNED TO DFW. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT WING FLAP VALVE IAW EMB 140 AMM 28-11-04. THE OPERATIONAL CHECK WAS GOOD NO LEAKS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 25,002 hrs · 21,955 cycles

DURING MAINTENANCE INSPECTION FOUND THE NR 7 CABIN EMERGECNY LIGHT STRIP HAS BROKEN WIRES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CABIN EMERGENCY FLOOR PROXIMITY STRIP LIGHT IAW AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ENGINE — LEAKING (NR 2) · airframe 24,901 hrs · 21,853 cycles

ON FLIGHT 4410 THE CREW REPORTED THAT WHILE IN CRUISE RECEVIED A LAV SMOKE WARNING. THE CREW PULLED THE LAV BREAKERS PER CHECKLIST AND THE LAV SMOKING WARNING WENT OUT. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. ENGINE LEAKING, REMOVE AND REPLACE NR 2 ENGINE.

Part: SMOKE DETECTOR — DIRTY (LAVATORY) · airframe 24,900 hrs · 21,851 cycles

FLIGHT 4463, THE CREW REPORTED THAT SHORTLY AFTER TAKEOFF THEY RECEIVED A LAV SMOKE WARNING. FLIGHT ATTENDANT COULD SMELL AN ODOR OF ELECTRICAL BURNING. DECLARED AN EMERGENCY AND LAVATORY SMOKE AND CABIN FIRE/SMOKE/FUMES CHECKLIST WERE COMPLIED WITH. PRIOR TO LANDING FLIGHT ATTENDANT INDICATED THE ODOR HAD DISSIPATED AND CONDITIONS WERE STABLE. LANDED WITHOUT INCIDENT BACK AT DEPARTURE. AIRCRAFT REMOVED FROM SERVICE. INSPECTED ALL CABIN PSU PRINTED CIRCUIT BOARDS AND LAVATORY BALLAST AND SMOKE DETECTOR. ALL PSU UNITS FOUND NORMAL EXCEPT LAVATORY SMOKE DETECTOR HAD EXCESSIVE DUST ACCUMULATION. REMOVED AND REPLACED SMOKE DETECTOR AND PERFORMED AN OPS CHECK, IT WAS GOOD PER MM 26-14-00. AIRCRAFT RETURNED TO SERVICE.

Part: DRAIN — CLOGGED (WATER COLLECTOR) · airframe 24,843 hrs · 21,804 cycles

AFTER TAKEOFF, REACHING ACCELERATION ALTITUDE RECEIVED A LAVATORY SMOKE INDICATION ON THE EICAS. RAN LAVATORY SMOKE CHECKLIST, FLIGHT ATTENDANT INVESTIGATED LAVATORY. NO SMOKE WAS FOUND. FLIGHT ATTENDANT REPORTED THAT A WHITE COLOR MIST WAS COMING FROM THE FLOOR VENTS AT ROW 8 AND IT SMELLED LIKE A WET MOLDY SOCK. CREW DECLARED AN EMERGENCY AND RETURNED FOR LANDING. AIRCRAFT LANDED WITHOUT INCIDENT. PERFORM EM-72-034R4. NO ODOR NOTED. PERFORM OPS CHECK OF LAVATORY SMOKE DETECTOR SYS IAW 26-14-00. OPS CHECKED GOOD. FOUND WATER COLLECTOR CLOGGED, UNCLOGGED DRAIN IAW 21-51-05. FOUND RECIRCULATION MUFFLER LOOSE, SECURED IAW 21-24-02. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — SMOKE (CABIN) · airframe 24,836 hrs · 21,797 cycles

ON FLIGHT 4471, THE CREW REPORTED THAT DURING THE TAKEOFF ROLL THEY NOTICED SMOKE IN THE CABIN AND COCKPIT 400 AGL LAVATORY SMOKE ON EICAS. THE CREW DECLARED AN EMERGENCY AND RETURNED. THE AIRCRAFT WAS REMOVED FROM SERVICE. THE OPERATIONAL CHECK OF THE LAVATORY SMOKE DETECTOR SYS OPS CHECKED GOOD. PERFORMED GROUND RUNS AND OPS CHECK OF PACKS PER ETN EM-72-034 R4. NO SMOKE NOTED IN CABIN OR COCKPIT. ALL SYSTEMS NORMAL, SUSPECTED CONDENSATION. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: OIL SYSTEM — OVERSERVICED (ENGINES) · airframe 24,259 hrs · 21,218 cycles

FLIGHT 3969, CREW REPORTED A FAINT ODOR OF UNBURNED OIL IN COCKPIT AND CABIN, DURING CLIMB AND DESCENT FOR SHORT PERIODS OF TIME. AIRCAFT REMOVED FROM SERVICE. FUNCTIONAL CHECK FLIGHT FOUND TO BE SATISFACTORY. PERFORMED OPERATIONAL CHECK OF LEFT AND RIGHT ENGINE FOR FAINT ODOR OF UNBURNED OIL IN COCKPIT AND CABIN IAW AE ETN EM-72-034 R4. FOUND NR 1 AND NR 2 ENGINE TO BE OVER SERVICED. NO FURTHER DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CHARGER — BROKEN (COCKPIT) · airframe 24,025 hrs · 20,999 cycles

DURING B-INSPECTION FOUND THE FIRST OFFICER'S EMERGENCY FLASHLIGHT CHARGER BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FIRST OFFICER’S BASE FLASHLIGHT IAW EMB140 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (ROW 16) · airframe 23,986 hrs · 20,959 cycles

DURING MAINTENANCE INPSECTION FOUND THE ROW 16 EMERGENCY LIGHT STRIP INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED WIRE CONNECTOR IAW WM 20-50-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,954 hrs · 20,931 cycles

B-INSPECTION, FOUND THE EMERGENCY LIGHTING FLOOR PROXIMITY STRIP AT SEATS 7 AND 8 DOES NOT ILLUMINATE. THE AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLOOR PROXIMITY LIGHT STRIP IAW AMM 33-50-12. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — FAILED (EMERGENCY LIGHT) · airframe 23,954 hrs · 20,931 cycles

DURING B-INSPECTION, FOUND THE LAST EMERGENCY LIGHT FLOOR PROXIMITY STRIP HAD BAD CONNECTOR. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLOOR PROXIMITY LIGHT STRIP IAW AMM 33-50-12. THE OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 23,791 hrs · 20,771 cycles

ON FLIGHT 4458 THE CREW REPORTED THAT DURING DESCENT THE PACKS EMITTED A MUSTY ODOR AND THE COCKPIT WINDOWS CONDENSED ON THE INSIDE. RATE OF DESCENT WAS NOT EXCESSIVE. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED TROUBLESHOOTING IAW ETN NO. EM-72-034R4 - FOUND NO MIST IN CABIN OR COCKPIT - NO UNUSUAL ODORS EITHER - INSPECTED ENGINE INLETS & EXHAUST - NO EVIDENCE OF OIL LEAKAGE. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 23,774 hrs · 20,756 cycles

ON FLIGHT 4500 THE CREW REPORTED A STRONG OIL ODOR IN THE COCKPIT NOTICED FIRST DURING DESCENT THRUST LEVER AT FLT IDLE. DURING SINGLE ENGINE TAXI NR 1 ENG OFF OIL ODOR GOT STRONGER THEN DISSIPATED. SUSPECT NR 1 ENG OIL SMELL. THE FLIGHT ATTENDANT REPORTED A LIGHT ODOR IN THE CABIN. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED TROUBLESHOOTING IAW ETN EM 72034R4. NO OIL ODOR DETECTED. INSPECTED THE EXHAUST. NO OIL FOUND. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SAFETY WIRE — BROKEN (COCKPIT EXTINGUI) · airframe 23,610 hrs · 20,613 cycles

FLIGHT 4549, CREW REPORTED A BROKEN SAFETY WIRE ON THE COCKPIT FIRE EXTINGUISHER. AIRCRAFT REMOVED FROM SERVICE. INSTALLED FRESH STRAND OF SAFETY WIRE. AIRCRAFT RETURNED TO SERVICE.

Part: STRINGER — CHAFED (FUSELAGE) · airframe 22,989 hrs · 20,066 cycles

DURING MAINTENANCE BASE VISIT FOUND STRINGER 19 RIGHT PREVIOUS REPAIR AT FRAME 52/53 CHAFED ON INNER SURFACE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED PREVIOUS REPAIR, FABRICATED PREPPED INSTALLED REPAIR IAW EO EM-53MR-1434. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,697 hrs · 19,832 cycles

ON FLIGHT 2969 THE CREW REPORTED THE RIGHT AFT OVERWING EMERGENCY LIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT OVERWING EMERGENCY LIGHT IAW EMB 145 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: VALVE — BROKEN (CABIN PRESSURE) · airframe 21,795 hrs · 19,079 cycles

ON FLIGHT 4475 THE CREW REPORTED THAT DURING THE CLIMB THE PRESSURIZATION WAS INOPERABLE IN AUTO AND MANUAL MODES. THE CAPTAIN ELECTED TO RETURN TO DCA. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED NEW GROUND CONNECTION VALVE IAW AMM 21-22-04. NO DEFECTS NOTED.PERFORMED LEAK CHECK IAW AMM 21-31-00. NO LEAKS NOTED. FOUND AND REMOVED BROKEN VALVE FROM DUCTING. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTACT — DIRTY (EXIT SIGN) · airframe 21,423 hrs · 18,736 cycles

FOR FLIGHT 2969 DURING PRE FLIGHT INSPECTION FOUND THE RIGHT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED CONTACT POINTS IAW AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 18,776 hrs · 16,637 cycles

PRIOR TO FLIGHT 2850 MAINTENANCE FOUND THE AFT FLOOR EMERGENCY LIGHTING STRIP TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED CONNECTOR FOR AFT EMERGENCY LIGHTING STRIP IAW EMB-140 AWM 20-21-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 16,988 hrs · 15,038 cycles

ON FLIGHT 4823, CREW REPORTED LAST LAMP ON FLOOR EXIT LIGHTS INOPERATIVE. ISSUED MEL 33-30.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 145,581 hrs · 15,038 cycles

CREW REPORTED LAST LAMP ON FLOOR EXIT LIGHTS INOPERATIVE. NO FURTER CORECTIVE ACTION REQUIRED LAST LIGHTS ON EMB-135 ARE NOT OPERATIONAL AS PART OF DESIGN.

Part: PROXIMITY SWITCH — MALFUNCTIONED (NLG) · airframe 15,984 hrs · 14,186 cycles

ON FLIGHT 4706, CREW REPORTED AFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED AND LANDED IN JFK SAFELY. REMOVED AND REPLACED LGEU, NOSE LANDING GEAR DOWN LOCK PROX SWITCH, AND LEFT MAIN LANDING GEAR DOWN LOCK PROX SWITCH. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: DUCT — DISCONNECTED (A/C PACK) · airframe 13,438 hrs · 11,375 cycles

IN CLIMB FLIGHT ATTENDANT REPORTED THAT THE CABIN WOULD NOT COOL, CREW TRIED TO RESET PACKS AND NR 1 PACK DROPPED OFF LINE. PRESS IN CABIN WOULD NOT HOLD SO CREW DROPPED TO 10,000 FT AND TRIED TO RESET PACKS AND BLEED NR 1 PACK STILL DROPPED OFF AND CABIN STILL NOT COOLING RETURNED TO CLT. RECONNECTED PACK NR 2 BLEED DUCT LINE IAW EMB AMM 36-11-09-400-801-A. AIRCRAFT RETURN TO SERVICE.

Part: SEAT TRACK — CORRODED (FUSELAGE)

FOUND LEFT OUTBOARD SECOND AFT SEAT TRACK FROM FRONT CORRODED. REPLACED SEAT TRACK IAW EMB 140 AMM 53-01-06. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: PLATE — CORRODED (FUSELAGE)

FOUND SERVICE DOOR CENTER SILL PLATE CORRODED. REPLACED CENTER SILL PLATE IAW EMB SRM 51-40-2. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: DOUBLER — CORRODED (FRAME)

FOUND DOUBLER AT FRAME 22 ON RIGHT HAT BEAM CORRODED. INSTALLED NEW DOUBLER IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

SAW - FOUND LEFT FORWARD OUTBOARD SEAT TRACK CORRODED. REPLACED SEAT TRACK IAW EMB 140 AMM 53-01-06. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BEARING — CORRODED (VERTICAL STAB)

FOUND VERTICAL STABILIZER SPHERICAL BEARINGS CORRODED. REPLACED BOTH VERTICAL STABILIZER SPHERICAL BEARINGS IAW EMB AMM 55-37-00. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

FOUND LEFT SECOND FROM FORWARD INBOARD SEAT TRACK CORRODED. REPLACED SEAT TRACK IAW EMB 140 AMM 53-01-00. AIRCRAFT WAS RETURNED O SERVICE. (M)

Part: SKIN — DENTED (PAX DOOR)

FOUND PASSENGER DOOR SKIN HAS A DENT. REPAIRED DENT IAW EMB SRM 52-10-01 PATE 402 BY INSTALLING AN EXTERNAL DOUBLER. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FOUND LEFT FORWARD INBOARD SEAT TRACK CORRODED. REPLACED SEAT TRACK IAW EMB 140 AMM 53-01-06. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BUSHING — MIGRATED (HORIZONTAL STAB)

FOUND HORIZONTAL STABILIZER NR 3 BUSHING HAS EVIDENCE OF MIGRATING. REMOVED AND REPLACED HORIZONTAL STABILIZER NR 3 BUSHING IAW EMB SRM 55-10-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: REPAIR — CORRODED (FLOOR SUPPORT)

FOUND REPAIR DOUBLER AT FRAME 20 ON LEFT OMEGA BEAM CORRODED. REPLACED DOUBLER ON LEFT OMEGA BEAM IAW EMB SRM 53-00-10 FIG 201. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: INDICATOR — MALFUNCTIONED (FUEL QTY)

CREW NOTED AFTER TAKEOFF THAT THE RT FUEL TANK WAS LOOSING ABOUT 300LB PER MINUTE, SO THEY RETURNED FOR MAINTENANCE. INSPECTED RT FUEL SYSTEM AND FOUND NO LEAKS. ALSO CALCULATED FUEL BURN OF LT AND RT ENGINES FOUND TO BE NORMAL. NO DEFECTS NOTED. AC RETURNED TO SERVICE. (SW21200404944)

Part: SEAT — INOPERATIVE (COCKPIT)

LAX - FLT 3161 - CAPTAIN REPORTED THE PILOTS SEAT WOULD NOT LOCK IN PLACE. MAINTENANCE REMOVED AND REPLACED THE PILOTS SEAT IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (GALLEY)

DURING AN MBV INSPECTION, THE LEFT FLOORBEAM AT FRAME 20 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. BLENDED THE CORRODED AREA AND PERFORMED AN NDT INSPECTION. FABRICATED AN EXTERNAL ANGLE, FILLER, SHIMS AND PLATE. REPAIR DONE IAW EMB 145 SRM, SRM 145/1142 REV 23, CHAPTER 53-21-10 FIGURE 201. (M)

Part: STRINGER — CHAFED (FUSELAGE)

DURING AN MBV INSPECTION, FOUND STRINGER 19R WAS FOUND CHAFED BEYOND SRM LIMITS. BLENDED THE CHAFED AREA AND PERFORMED AN NDT INSPECTION. FABRICATED A REPAIR ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB REPAIR STATEMENT IC2003-145/3093A, EMB SRM SRM EMB-145/1142 REV 23, 53-24-02 PAGES 201-204 AND STANDARD SRM PRACTICES. (M)

Part: WARNING LIGHT — ILLUMINATED (MLG)

DURING DESCENT CREW REPORTED GEAR UNSAFE. EMERGENCY WAS DECLARED AND AIRCRAFT LANDED WITH NO FURTHER INCIDENTS. UPON LANDING CREW RECEIVED THREE GREEN INDICATION FOR THE LANDING GEAR.