N824AE

Part: UPLOCK — FAILED (LT MLG) · airframe 37,010 hrs · 34,265 cycles

AFTER TAKE OFF AND RETRACTING NOSE GEAR MULTIPLE BANG NOISES FROM NOSE COMPARTMENT, CONTINUED ONCE OR TWICE AFTER CLIMBING AGAIN TO 18000 FT. R & R THE LT MLG UPLOCK BOX IAW AMM 32-30-00. OPS, FUNCTIONAL, AND LEAK CHECKED GOOD. NO ABNORMAL NOISES NOTED.

Part: SKIN — DENTED (FRAME 11) · airframe 36,230 hrs · 33,506 cycles

TDMI 824T5332 - ONETIME REPAIR - POSITION FWD FUS - PERFORM A PERMANENT REPAIR OF DENT BELOW STR13L AND FWD OF FR11 IAW EMB SRM 53-12-01 AT OR PRIOR TO 400 FC "MAJOR REPAIR" "TRANSFERRED TO NRWC 824-ABI-03546"-C/A-COMPLIED WITH PERMANT REPAIR IAW EM-53AD-2261 AND AMOC AIR-676-18-154. TDMI RESTORED SEE NRWC 824-ABI-03546 FOR TURNOVER DETAILS

Part: BATTERY — DISCHARGED (CABIN) · airframe 36,168 hrs · 33,454 cycles

RT AND LT OVERWING EMERGENCY LIGHTS DO NOT ILLUMINATE. C/A-REMOVED AND REPLACED NR 4 EMERGENCY BATTERY AND POWER SUPPLY IAW AMM 33-50-04. OPS TEST GOOD. NO OTHER DEFECTS NOTED AT THIS TIME. BATTERY CHARGER ASSY P/N 11-0049 S/N 10546.

Part: BATTERY — DISCHARGED (CABIN) · airframe 36,031 hrs · 33,324 cycles

LT AFT AND RT AFT OVERWING EXT EMERGENCY LIGHTS INOP. C/A-REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY PACK AND CHARGER IAW AMM 33-50-04. OPC GOOD. BATTERY CHARGER ASSY P/N 11-0049 S/N 16065.

Part: THERMOSTAT — MALFUNCTIONED (BLEED AIR SYS) · airframe 36,003 hrs · 33,299 cycles

BLEED 2 OVERTEMP IN ICING CONDITIONS AND WING ANTI ICE FAIL EICAS MESAGE IN ICING CONDITIONS. C/A-PERFORMED TROUBLESHOOTING PER FIM 36-11-00. RAR BLEED 2 THERMOSTAT PER AMM 36-11-06. OPC GOOD. PERFORMED TROUBLESHOOTING PER FIM 30-11-00. COULD NOT DUPLICATE DISCREPANCY. PERFORMED OPERATIONAL CHECK PER AMM 30-00-00 OPC GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,982 hrs · 33,280 cycles

BOTH AFT EXTERNAL OVERWING EMERGENCY LIGHTS INOP-C/A-REMOVED AND REPLACED BOTH EMERGENCY LIGHT BATTERY AND CHARGER #4, OPC GOOD IAW EMB AMM 33-50-04. CHARGER ASSY BATTERY P/N BA5-0933-901 S/N C00511

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 35,756 hrs · 33,061 cycles

LT EXTERIOR OVERWING EMERGENCY LIGHT INOP. C/A-REMOVED AND REPLACED LT EXTERIOR OVERWING EMERGENCY LIGHT IAW AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECK GOOD.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 35,688 hrs · 32,994 cycles

OVER WING EXTERIOR EMERGENCY LIGHTS INOP. C/A-REMOVED AND REPLACED NR 4 BATTERY CHARGER AND BATTERY HOLDER ASSY IAW AMM 33-50-04. OPS CK GOOD. BATTERY CHARGER ASY P/N 11-0049 S/N 104878.

Part: THERMOSTAT — FAILED (NR 2 BLEED) · airframe 35,486 hrs · 32,811 cycles

BLEED # 2 OVERTEMP MESSAGE ON EICAS-ON CLIMB OUT 8000 FT.-C/A-FOUND BLD 2 OVTEMP MESSAGE ON EICAS AND PRECOOLER 2 TEMPCTL SYS FAIL ON CMC. T/S PER FIM TASK 36-11-00-810-804-A AND FOUND RH FAN AIR CONTROL THERMOSTAT OPC BAD. REMOVED AND REPLACED RH FAN AIR CONTROL THERMOSTAT IAW AMM 36-11-06. OPC AND LEAK CHECK GOOD IAW AMM 36-00-00.

Part: ANTI-ICE VALVE — FAILED (NR 2 ENGINE) · airframe 35,460 hrs · 32,789 cycles

PERFORMING IN AIR ICE TEST, RCVD E2 A/I FAIL. PER QRH CANNOT ENTER ICING CONDITION RTB-LGA-C/A-REMOVED AND REPLACED ENGINE A/I VALVE IAW EMB 140 AMM 30-21-01. OPC DONE IAW EMB 140 AMM 30-00-00 ICE AND RAIN PROTECTION ADJ/TEST. NO DEFECTS NOTED.

Part: NONE — PILOT ERROR (NONE) · airframe 35,316 hrs · 32,669 cycles

AIRCRAFT NOT PRESSURIZING. CLIMBING THROUGH 10,000 FEET WE NOTICED CABIN ALTITUDE IN THE AMBER AND INDICATION AROUND 9400 FT. DESCEND BACK TO 10,000 AND RETURNED TO DFW. DID NOT TRY MANUAL PRESSURIZATION.-C/A-SUSPECT AIRCRAFT IN INCORRECT CONFIGURATION FOR CABIN PRESSURIZATION. FOUND AIRCRAFT MANUAL CONTROLER IN THE UP POSITION FULL RIGHT IN THE "DUMP" DETENT. PUSHBUTTONS IN AUTO MODE WITH THE GARDED DUMP SWITCH IN THE NORMAL UNSELECTED MODE. REF. ITEM 2. PERFORMED FUNCTIONAL TEST OF PRESSURIZATION CONTROL IN AUTO AND MANUAL MODE. OPC GOOD PER AMM 21-31-00.

Part: FLOOR SUPPORT — CRACKED (FRAMES 47-48) · airframe 33,999 hrs · 31,369 cycles

LEFT OMEGA BEAM OTBD SUPPORT IS CRACKED BETWEEN FRAMES 47 - 48. REMOVED AND REPLACED THE OMEGA BEAM IAW SRM 53-23-02, 51-20-03, AND 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FRAME 38) · airframe 33,999 hrs · 31,369 cycles

LEFT OMEGA BEAM IS CORRODED UNDER CROSSBEAM AT FRAME 38. REPAIRED IAW SRM 51-40-02, AND 53-00-10

Part: FRAME — GOUGED (FRM 60) · airframe 33,999 hrs · 31,369 cycles

FRAME 60 PREVIOUS REPAIR AT STRINGER 4L - 5L IS GOUGED. REMOVED AND REPLACED THE FRAME REPAIR REINFORCEMENT IAW SRM 53-00-04, FIG. 206, AND SRM 51-40-02.

Part: DOOR SILL — CORRODED (SERVICE DOOR) · airframe 33,999 hrs · 31,369 cycles

SERVICE DOOR CENTER SILL IS CORRODED. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-40-02, 51-40-06, AND 51-40-09

Part: FRAME — CRACKED (FR 66) · airframe 33,999 hrs · 31,369 cycles

FRAME 66 CRACKED AROUND RIVETS, STRINGERS 17L-18L. ACCOMPLISHED A DOUBLER REPAIR TO THE FRAME IAW ERS-EM-53MR-3185.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 33,999 hrs · 31,369 cycles

EXTERNAL FUSELAGE SKIN NICKED AND DENTED WITH NICKS FROM NLG BAY CUTOUT. ACCOMPLISHED A DOUBLER REPAIR IAW ERS-EM-53MR-3187.

Part: FRAME — CRACKED (FR 67) · airframe 33,999 hrs · 31,369 cycles

FRAME 67 CRACKED AROUND RIVETS, STRINGERS 17L - 18L. ACCOMPLISHED A DOUBLER REPAIR TO THE FRAME IAW ERS-EM-53MR-3185.

Part: SKIN — DENTED (FRAMES 10-11) · airframe 33,999 hrs · 31,369 cycles

SKIN DENTED BETWEEN FRAMES 10 - 11, STRINGERS 15L - 17L. ACCOMPISHED A PERMANENT REPAIR TO THE SKIN IAW ERS-EM-53MR-3181 R1.

Part: DOOR FRAME — GOUGED (CARGO BAY) · airframe 33,999 hrs · 31,369 cycles

CARGO DOOR LOWER FRAME IS GOUGED AND BENT AT FWD END. REMOVED AND INSTALLED A SERVICEABLE DOOR FRAME IAW SRM 51-40-02.

Part: FRAME — CORRODED (FRM 65) · airframe 33,999 hrs · 31,369 cycles

FRAME 65 CORRODED, AT THE CARGO DOOR LOWER STRIKER PLATE. ACCOMPLISHED A PERMANENT REPAIR IAW ERS-EM-53MR-3179.

Part: WEB — CORRODED (CARGO DOOR) · airframe 33,999 hrs · 31,369 cycles

CARGO DOOR INTERNAL WEB IS CORRODED AROUND 1 SCREW HOLE. INSTALLED A REPAIR DOUBLER IAW SRM 52-30-01.

Part: FRAME — CRACKED (FRM 72) · airframe 33,999 hrs · 31,369 cycles

FRAME 72 CRACKED, STRINGERS 16R - 17R. REMOVED AND REPLACED THE FRAME LOWER SECTION IAW SRM 51-40-02, AND 51-20-03.

Part: SHEAR TIE — CRACKED (FRAME 62) · airframe 33,999 hrs · 31,369 cycles

FRAME 62 SHEAR TIE CRACKED, STRINGER 6R - 8R. ACCOMPLISHED A REPAIR OF THE SHEAR TIE IAW SRM 53-31-04.

Part: FLOOR SUPPORT — CORRODED (FRAME 20) · airframe 33,999 hrs · 31,369 cycles

CENTER OMEGA BEAM CORRODED AT FRAME 20. REMOVED AND REPLACED THE CENTER OMEGA BEAM IN GALLEY IAW SRM 51-40-02.

Part: SHEAR TIE — CRACKED (FRAME 68) · airframe 33,999 hrs · 31,369 cycles

FRAME 68 SHEAR TIE CRACKED, STRINGERS 6L - 7L. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 53-31-04.

Part: SHEAR TIE — CORRODED (FRAME 68) · airframe 33,999 hrs · 31,369 cycles

FRAME 68 LATERAL L SHAPE CORRODED, STRINGERS 16L - 18L. REMOVED AND REPLACED IAW SRM 53-31-04, ITEM 4, FIG 212, AND SRM 51-40-02.

Part: DOOR SILL — CORRODED (CARGO) · airframe 33,999 hrs · 31,369 cycles

CARGO DOOR CUTOUT LOWER SILL CORRODED. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-40-02, AND 51-20-03.

Part: SHEAR TIE — CORRODED (FRAME 65) · airframe 33,999 hrs · 31,369 cycles

FRAME 65, LATERAL L SHAPE CORRODED AT STRINGERS 16L - 18L. ACCOMPLISHED A REPAIR TO L SHAPE IAW SRM 53-31-04, ITEM 4, FIG 212, AND SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FRAMES 43-44) · airframe 33,999 hrs · 31,369 cycles

CENTER OMEGA BEAM CORRODED BEYOND ALLOWABLE LIMITS BETWEEN FRAMES 43-44. PERFORMED A REPAIR ON THE CENTER OMEGA BEAM IAW ERS-EM-53MR-3197.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 33,875 hrs · 31,260 cycles

FOUND LEFT FWD EXTIRIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK IAW 33-50-04.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,991 hrs · 30,481 cycles

SERVICE DOOR EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED THE NR 2 DC/AC INVERTER IAW AMM 33-50-11 OPS CHECKED GOOD

Part: BRAKE — FAILED (NR 4) · airframe 32,934 hrs · 30,416 cycles

WHILE PERFORMING FCD-EM-32-025, NR 4 MLG BRAKE FAILED INSP.-C/A-REMOVED AND REPLACED NR 4 BRAKE IAW W/C 32-600-14..END.

Part: UNKNOWN — MALFUNCTIONED (HYDRAULIC SYS) · airframe 32,892 hrs · 30,368 cycles

HYD 1 LOW QTY IN FLIGHT. PERFORMED HYD FLUID TRANSFER FROM SYS2 TO SYS1 IAW ETN EM-29-023. SERVICED HYD SYS 2 IAW AMM 12-13-01. NO LEAKS NOTED AT THIS TIME. ACFT OK FOR SERVICE.

Part: CHARGER — FAILED (CABIN) · airframe 32,682 hrs · 30,156 cycles

WHILE ACCOMPLISHING WC 33-700-17, FOUND GROUP OF EMER LIGHTS IN CABIN COMING ON & THEN SHUTTING OFF. R & R BATTERY 4 & CHARGER IAW AMM 33-50-04. OPERATIONS CHECKED GOOD. EMER LIGHTING BATTERY, PN 2013-1A & SN 66545.

Part: ELECTRONIC UNIT — FAILED (LANDING GEAR) · airframe 32,294 hrs · 29,729 cycles

DURING CLIMB OUT LG FAILED TO RETRACT, WE RUN AOM 1 PROCEDURE & RETRACTED LG. MOC ADVISED US TO RETURN. LG WORKED OK FOR THE REST OF THE FLIGHT. LG & LEVER DISAGREE MSG WAS PRESENTED DURING FAILED RETRACTION. MSG DISAPPEARED AFTER WE CYCLED GEAR. REPLACED LGEU IAW MM 32-32-01. OPERATIONS CHECKED GOOD.

Part: SWITCH — FAILED (BLEED AIR SYS) · airframe 32,009 hrs · 29,390 cycles

ON CLIMBING, ENTERING ICE CONDITION, GOT 4 OPEN BUT GOT BLD 1 VLV FAIL & BLD CLOSED WHEN ICING TURNED OFF. FAIL MSG ADV CLEARED ON DESCENT, IN ICING GOT BLD1 FAIL BUT NO BLD CLOSED ADVS ON THE GND, WE DESELECTED BLD 1 CLOSED BUT GOT NO CLOSED MSG OR FAIL. R & R ENG 1 BLEED SWITCH IAW AMM 20-13-04. COMPLIED WITH OPERATIONS CHECK IAW AMM 36-11-05. NO DEFECTS NOTED.

Part: DOUBLER — CHAFED (FUSELAGE) · airframe 31,903 hrs · 29,276 cycles

PREVIOUS REPAIR AT FRAME 60 & STRINGER 5 LT IS CHAFED. R & R FRAME REPAIR DOUBLER IAW SRM 53-00-04 REPAIR ITEM 14.

Part: STIFFENER — CRACKED (VERTICAL STAB) · airframe 31,903 hrs · 29,276 cycles

RIGHT VERTICAL STABILIZER STIFFENER IS CRACKED AT LOWER HINGE ATTACH POINT. REPAIRED IAW ETN-EM-55-047R1.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,903 hrs · 29,276 cycles

LEFT UPPER FRAME NR 10 IS CRACKED BELOW DV WINDOW, LOWER SURROUND STRUCTURE. INSTALLED NEW LT UPPER FRAME 10 SECTION IAW SRM 51-40-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 31,903 hrs · 29,276 cycles

AFT FUSELAGE RT SIDE OF VERTICAL STAB, HAS A RIVET WITH SKIN CRACKS ON BOTH SIDES, AT FRAME 75 & STRINGER 2R. COMPLETED REPAIR OF AFT FUSELAGE RT SIDE OF THE VERTICAL STAB AT FRAME 75 & STRINGER 2R IAW ERS-EM-53MR-1813.

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 31,903 hrs · 29,276 cycles

RIGHT MLG WW AFT BULKHEAD WALL IS CRACKED. REPAIRED RT MLG WW BULKHEAD IAW SRM 53-23-12.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 31,903 hrs · 29,276 cycles

RIGHT LOWER ATTACHMENT ANGLE NR 1 FOR THE WING TO FUSELAGE FAIRING IS CRACKED, BETWEEN FRAMES 43 - 44, FWD OF THE PREVIOUS CUT OUT SPLICE REPAIR. REPAIRED RT OVERWING FAIRING LOWER ATTACHMENT ANGLE NR 1, BETWEEN FRAMES 43 - 44 IAW ETN-EM-53-142.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 31,903 hrs · 29,276 cycles

LEFT LOWER ATTACHMENT ANGLE NR 2. FOR THE WING TO FUSELAGE FAIRING IS CRACKED 1/2" LONG, BETWEEN FRAMES 47 - 48 ON THE TE. R & R WING TO FUSELAGE FAIRING LOWER NR 2 ATTACHMENT ANGLE IAW SRM 51-40-02.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 31,903 hrs · 29,276 cycles

LEFT UPPER ANGLE FOR THE WING TO FUSELAGE FAIRING HAS ATTACHMENT BRACKET THAT IS CRACKED. UNDERNEATH THE PULLED RIVETS, BETWEEN FRAMES 48 - 49. R & R LT UPPER ATTACHMENT BRACKET FOR UPPER WING TO FUSELAGE FAIRING ANGLE IAW SRM 51-40-02 & ETN-EM-51-110.

Part: FITTING — CHAFED (RT AILERON) · airframe 31,903 hrs · 29,276 cycles

RIGHT AILERON DAMPER FITTING IS CHAFED FROM DAMPER ROD END. R & R DAMPER FITTING IAW EO-E27MR-112.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 31,903 hrs · 29,276 cycles

CARGO DOOR HOLD OPEN SUPPORT ROD CUP HOLDER ATTACHED AT FRAME 68, HAS AFT BRACKET CRACKED AT BOTH FASTENER ATTACHMENTS. TWO EACH CRACKS ARE APPROX .5 " LONG. R & R CARGO DOOR HOLD OPEN ROD SUPPORT BRACKET IAW SRM 51-42-06.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 31,903 hrs · 29,276 cycles

CARGO DOOR TORSION RODS, FWD SUPPORT BRACKET CRACKED. R & R CARGO DOOR TORSION RODS, FWD SUPPORT BRACKET IAW SRM 51-40-02. REFERENCE NRTC E482340 FOR ADJUSTMENT & OPERATIONAL CHECK.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 31,903 hrs · 29,276 cycles

FLOOR TO WALL SUPPORT ANGLE IS CRACKED AT RT FRAME 23 AT STRINGER 15R. R & R SUPPORT ANGLE IAW SRM 51-40-02.

Part: BRACKET — CRACKED (RT MLG WW) · airframe 31,903 hrs · 29,276 cycles

WING TO FUSELAGE BRACKET CRACKED IN THE RT MLG WW. R & R WING TO FUSELAGE BRACKET IN RT WW IAW SRM 51-40-02.

Part: FITTING — WORN (RUDDER) · airframe 31,903 hrs · 29,276 cycles

RUDDER NR 2 UPPER CTR ROD FITTING BORES ARE WORN. REPLACED FITTING IAW SRM 55-40-02 & ETN EM-55-070.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 31,903 hrs · 29,276 cycles

LEFT LOWER ATTACHMENT ANGLE NR 4, FOR THE WING TO FUSELAGE FAIRING IS CRACKED 1/2" LONG, BETWEEN FRAMES 48 - 49 ON THE FWD EDGE. REPAIRED LT LOWER ATTACHMENT ANGLE NR 4 FOR THE WING TO FUSELAGE FAIRING, BETWEEN FRAMES 48 - 49 IAW SRM 51-40-02 & ETN-EM-53-142.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 31,903 hrs · 29,276 cycles

LEFT LOWER ATTACHMENT ANGLE NR 1, FOR THE WING TO FUSELAGE FAIRING IS CRACKED 1 1/4" LONG, BETWEEN FRAMES 43 - 44 ON THE PREVIOUS CUT OUT SPLICE REPAIR. REPAIRED IAW ETN-EM-53-142.

Part: HINGE FITTING — WORN (RUDDER) · airframe 31,903 hrs · 29,276 cycles

RUDDER NR 2 UPPER HINGE FITTING BORES ARE WORN. REPLACED FITTING IAW SRM 55-40-02 & ETN EM-55-070.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 31,903 hrs · 29,276 cycles

RIGHT LOWER ATTACHMENT ANGLE NR 3, FOR THE WING TO FUSELAGE FAIRING IS CRACKED 1 1/2" LONG ON THE FWD END, BETWEEN FRAMES 47 - 48. REPAIRED RT LOWER ATTACHMENT ANGLE NR 3 FOR THE WING TO FUSELAGE FAIRING, BETWEEN FRAMES 47 - 48 IAW ETN-EM-53-142.

Part: SIGN — INOPERATIVE (CABIN) · airframe 31,902 hrs · 29,275 cycles

EXIT SIGN ABOVE SERVICE DOOR WON’T ILLUMINATE. REMOVED & INSTALLED EMER EXIT SIGN ASSEMBLY ABOVE SERVICE DOOR IAW AMM 33-50-14. SUSPECT BAD LIGHT.

Part: PROXIMITY SWITCH — DISCONNECTED (NLG) · airframe 31,821 hrs · 29,191 cycles

LANDING AIR GND FAIL, ON TAKEOFF & LANDING. TROUBLE SHOT IAW FIM TASK 32-63-00-810-802-A. RECONNECTED NLG WOW PROX SWITCH IAW AMM 32-63-02. APPLIED CORROSION PROTECTION TAPE IAW ETN-32-176 R1 & PERFORMED FUNCTIONAL CHECK OF ALL LANDING GEAR PROXIMITY SWITCHES IAW AMM 32-63-05. OPERATIONS CHECKED GOOD. PERFORMED LG EXTENSION & RETRACTION, OPERATIONS CHECKED GOOD IAW AMM 32-30-00. OPERATIONS CHECKED GOOD, NO DEFECTS NOTED.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 31,259 hrs · 28,603 cycles

AFT CABIN EMER FLASHLIGHT INOPERATIVE. REPLACED AFT CABIN FLASHLIGHT IAW AMM 33-50-06. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,699 hrs · 28,102 cycles

FLOOR EMER LIGHT INOPERATIVE AT ROW 16. R & R FLOOR EMER LIGHT STRIP AT ROW 16 IAW AMM 33-50-12. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: BATTERY — DISCHARGED (CABIN) · airframe 29,932 hrs · 27,455 cycles

LEFT AFT OVERWING EXIT LIGHT INOPERATIVE. R & R NR 4 BATTERY & CHARGER IAW AMM 33-50-04. OPERATIONS CHECKED GOOD.

Part: VALVE — FAILED (BRAKE SYSTEM) · airframe 29,269 hrs · 26,880 cycles

PARKING BRAKE IS VERY HARD SET & VERY SLUGGISH TO RELEASE. R & R EMER BRAKE VLV SYS. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,010 hrs · 26,691 cycles

FLOOR STRIP EMER LIGHTS AT ROW 9 & 10 INOPERATIVE. DEFERRED IAW MEL 33-20. REPLACED FLOOR STRIP EMER LIGHTS AT ROW 9 & 10 IAW AMM 33-50-12 OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 28,943 hrs · 26,610 cycles

CAPTAIN`S FLASHLIGHT INOPERATIVE. DEFERRED CAPTAIN'S FLASHLIGHT IAW MEL 25-53 AUTH 051350-C M PROCEDURES COMPLIED WITH. R & R CAPTAIN`S FLASHLIGHT ASSEMBLY IAW AMM 33-50-16-000-801-A & 33-50-16-400-801-A. OPERATIONS CHECKED GOOD. MEL RESTORED.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 28,789 hrs · 26,457 cycles

FLASHLIGHT FIRST OFFICER`S SIDE INOPERATIVE. OPERATIONS CHECK FLIGHT OFFICER`S FLASHLIGHT GOOD IAW AMM 33-50-16.

Part: FIRE LOOP — CHAFED (APU) · airframe 28,473 hrs · 26,194 cycles

EICAS MSG, APU FIRE DET FAIL, ON EICAS CLIMBING THROUGH 25,000'. FOUND CHAFED APU FIRE DET LOOP. R & R APU FIRE DET LOOP IAW AMM 26-12-01 & OPERATIONS CHECKED GOOD IAW EMB-140 AMM 26-10-01.

Part: FLASHLIGHT — DEFECTIVE (COCKPIT) · airframe 28,326 hrs · 26,087 cycles

CAPTAIN'S FLASHLIGHT HOLDER NOT HOLDING THE FLASHLIGHT TIGHT ENOUGH TO CHARGE. R & R CAPTAIN'S FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: ROLLER — OUT OF ADJUST (PAX DOOR) · airframe 28,297 hrs · 26,062 cycles

PASSENGER DOOR DIFFICULT TO OPEN. ADJUSTED AFT UPPER ROLLER IAW AMM52-18-00, OPERATIONS CHECKED GOOD.

Part: CONNECTOR — CONTAMINATED (LT SPOILER) · airframe 28,015 hrs · 25,794 cycles

SPOILER FAIL IN FLIGHT DURING DESCENT WITH REDUCED POWER, THEY DID NOT DEPLOY. CLEANED CONTAMINATION FROM SPOILER PROX SENSOR CONNECTOR. R & R LT INBD SPOILER PROX SWITCH IAW 140 AMM 27-63-04, OPERATIONS CHECKED GOOD AT THIS TIME.

Part: CONNECTOR — LOOSE (LT SPOILER) · airframe 28,013 hrs · 25,792 cycles

ON DESCENT, SPOILER FAIL MESSAGE ON EICAS. SPOILERS WERE NOT SELECTED BUT WERE INDICATING OPEN. FOUND LT INBD SPOILER PROX SWITCH CONNECTOR LOOSE. SECURED CONNECTOR IAW 140 AMM 27-63-04. PERFORMED OPERATIONAL CHECK IAW 140 AMM 27-63-01, OPERATIONS CHECKED GOOD.

Part: PROXIMITY SWITCH — FAULTY (LT SPOILER) · airframe 28,012 hrs · 25,791 cycles

SPOILER FAIL ON LANDING ROLLOUT. R & R LT INBD SPOILER PROX SWITCH IAW AMM 27-63-04. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: UNKNOWN — ODOR · airframe 28,003 hrs · 25,782 cycles

DURING MAINTENANCE INSPECTION ON FLIGHT 9805 REPORTED AT FL 180 HAD BURNING PLASTIC SMELL WITH ICE DETECTION OVERRIDE. THE ACFT WAS REMOVED FROM SERVICE. COMPLIED WITH CW ETN-EM-72-034 FOR BURNING PLASTIC SMELL. DIDN'T SMELL ANYTHING THROUGHOUT CHECKS. INSPECTION OF AIR DISTRIBUTION DUCTS PCW ON NRWC 824-ORD-01559 NR 2 ACFT RELEASED FOR FCF PURPOSES ONLY. IAW NRWC 824-ORD-01560, THE AIRCRAFT RETURN TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 28,003 hrs · 25,781 cycles

FL 180, TURNED ICE PROTECTION KNOB TO ALL, SMELLED A BURNING SMELL, POSSIBLY ELEC. SMELL WENT FROM COCKPIT TO ROW 5, NO SMOKE OBSERVED. COMPLIED WITH ETN-EM-72-034 & FOUND NO BURNING SMELLS. COMPLIED WITH INSPECTIONS IAW ETN IAW NRWC 824-ORD-01559.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 27,004 hrs · 24,930 cycles

CAPTAIN'S FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW MM 25-60-00, OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 26,966 hrs · 24,892 cycles

MAIN DOOR DIFFICULT TO OPEN. LUBRICATED MAIN CABIN DOOR ROLLERS, OPS CHECKED GOOD IAW MM 52-10-00.

Part: LAMP — UNSERVICEABLE (EMERGENCY LIGHT) · airframe 26,918 hrs · 24,856 cycles

SIDE-HINGED MAIN DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. R & R SIDE-HINGED MAIN DOOR EXTERNAL EMERGENCY LIGHT BULB IAW AMM 33-50-10. OPS CHECK GOOD.

Part: REPAIR — CRACKED (FUSELAGE) · airframe 26,711 hrs · 24,674 cycles

DURING HEAVY CHECK FOUND PREVIOUS REPAIR MATERIAL AT FRAME 23 BETWEEN STRINGER 15R AND STRINGER 16R CRACKED. THE ACFT WAS REMOVED FROM SERVICE. REPAIRED CRACK IAW AEA EO EM-53MR-1808. THE ACFT WAS RETURNED TO SERVICE.

Part: GUSSET — CORRODED (SUPPORT BEAM) · airframe 26,731 hrs · 24,688 cycles

DURING B INSPECTION, FOUND THE LAVATORY AREA RT BEAM TOP GUSSET HAS CORROSION. REMOVED CORRODED RT BEAM TOP GUSSET, DRILLED AND INSTALLED A NEW TOP GUSSET IAW SRM 51-40-02 51-20-03. THE ACFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,731 hrs · 24,688 cycles

DURING B INSPECTION, FOUND THE AFT NR 3 EMERGENCY LIGHT IN THE CABIN INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R NR 4 BATTERY PACK POWER SUPPLY IAW AMM 33-50-04. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: LIGHT — DAMAGED (CABIN) · airframe 26,731 hrs · 24,688 cycles

DURING B INSPECTION, FOUND THE LT EMERGENCY LIGHTS 4, 7 & 8 DAMAGED. ACFT REMOVED FROM SERVICE. R & R THE EMERGENCY LIGHTS IAW AMM 33-50-12. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,714 hrs · 24,677 cycles

DURING B-INSPECTION, FOUND EMERGENCY BATTERY AND EMERGENCY BATTERY CHARGER WOULD NOT CHARGE. ACFT REMOVED FROM SERVICE. R & R THE EMERGENCY BATTERY AND EMERGENCY BATTERY CHARGER. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: FIRE DETECTOR — FAILED (CARGO BAY) · airframe 26,616 hrs · 24,608 cycles

CREW REPORTED BAGGAGE SMOKE INDICATION, BUTTON PUSHED. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 2 FIRE DETECTOR IAW 26-15-01, OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: MECHANISM — LACK OF LUBE (CABIN DOOR) · airframe 26,583 hrs · 24,582 cycles

ON FLIGHT 3202 THE FLIGHT ATTENDANT REPORTED THE MAIN CABIN DOOR WAS HARD TO OPEN AND CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBRICATED MAIN DOOR LOCK HANDLE & MECHANISM IAW EMB AMM 52-11-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,529 hrs · 24,542 cycles

DURING B INSPECTION FOUND THE CEILING EMERGENCY LIGHT ABOVE SEAT 11C INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SEAT 11C CEILING EMERGENCY LIGHT LAMP IAW AMM 33-50-08. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — MISSING (COCKPIT) · airframe 25,753 hrs · 23,820 cycles

ON FLIGHT 4280 THE CREW REPORTED THE CAPTAIN FLASHLIGHT WAS MISSING. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED NEW FLASHLIGHT IAW EMB AMM 25-60-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 25,336 hrs · 23,427 cycles

DURING B INSPECTION FOUND THE AFT EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 BATTERY AND CHARGER POWER SUPPLY IAW EMB 135 AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SCREW — MISSING (EMERGENCY LIGHT) · airframe 25,266 hrs · 23,371 cycles

ON FLIGHT 3439 THE CREW REPORTED A SCREW WAS MISSING AT THE RIGHT SIDE EMERGENCY LIGHT OVER WING AREA. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT AFT EXT EMERGENCY LIGHT ASSEMBLY. THE OPERATIONAL CHECK WAS GOOD AMM 33-50-10. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HANDLE — OUT OF ALIGNMENT (MAIN DOOR) · airframe 25,176 hrs · 23,299 cycles

FOR FLIGHT 3427 THE CREW REPORTED THE MAIN DOOR WOULD NOT OPEN FROM INSIDE, PASSENGERS STUCK ON BOARD. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSPECTED MAIN CABIN DOOR AND RE-ALIGNED ACTUATING HANDLE IAW AMM 52-18-05. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — BROKEN (COCKPIT) · airframe 24,014 hrs · 22,181 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: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 23,718 hrs · 21,910 cycles

ON FLIGHT 4549 THE CREW REPORTED THE CAPTAINS FLASHLIGHT ACTED WEAK AND INTERMITTENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLASHLIGHT BATTERY IAW EMB 140 AMM 33-50-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ACCESS PANEL — STUCK (LAVATORY) · airframe 23,167 hrs · 21,491 cycles

ON FLIGHT 2730 THE CREW REPORTED THE FLIGHT ATTENDANT WAS UNABLE TO OPEN LAV FIRE EXTINGUISHER ACCESS PANEL. THE AIRCRAFT WAS REMOVED FROM SERVICE. OPENED FIRE EXTINGUISHER DOOR, NO FURTHER ACTION REQUIRED. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 21,892 hrs · 20,438 cycles

DURING MBV INSPECTION, FOUND CARGO DOOR SILL CORRODED. REMOVED AND REPLACED CARGO SOOR SILL IAW EMBRAER STRUCTURAL REPAIR MANUAL 51-40-02.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 21,892 hrs · 20,438 cycles

DURING MAINTENANCE BASE INSPECTION FOUND FRAME 59 TO HAVE A HOLE CHAFED IN IT BETWEEN STRINGERS 4 LEFT AND 5 LEFT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FRAME 59 IAW EO-53MR-1831. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,892 hrs · 20,438 cycles

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

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 21,892 hrs · 20,438 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND FRAME 23 HAS A .5 INCH CRACK JUST ABOVE SERVICE THE DOOR SILL. REPAIRED FRAME 23 IAW EO EM-53MR-1808. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 20,523 hrs · 1,920 cycles

DURING MAINTENANCE BASE VISIT THE RAMP REPORTED THE EMERGENCY LIGHTS WERE LEFT ON. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY 1, 2, 3, 4 IAW EMB 145 AMM 33-50-04. SERIAL NUMBERS: 104946, 78789, 104936 AND 79756. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 19,447 hrs · 18,277 cycles

DURING INSPECTION FOR FLIGHT 4512 THE EMERGENCY FLASHLIGHT HOLDER WAS FOUND TO HAVE A BROKEN RETAINER CLIP. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLASHLIGHT HOLDER. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE HARNESS — ARCED (LANDING GEAR) · airframe 19,159 hrs · 18,031 cycles

ON FLIGHT 4442 DURING THE CLIMB THE CREW REPORTED A LOUD CONTINUOUS BANGING SOUND WHEN GEAR SELECTED UP. THE HYDRAULIC SYSTEM 1 PRESSURE WAS VARYING BETWEEN 2700 & 3000 PSI. THE BANGING STOPPED WHEN GEAR SELECTED DOWN AND LOCKED. THE CREW DECLARED AN EMERGENCY AND RETURNED TO JFK. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSPECTED NOSE LANDING GEAR DOWN/UP LOCK SYSTEM AND FOUND PROXIMITY SWITCH AND CONNECTOR P0040 WITH SIGNS OF ARCING. REMOVED AND REPLACED PROXIMITY SWITCH AND HARNESS P0773 PER EMB-140 AMM 32-61-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 18,837 hrs · 17,724 cycles

ON FLIGHT 3816 DURING THE CLIMBOUT THE CREW RECEIVED A MESSAGE INDICATION THAT THE CARGO DOOR WAS OPEN. THE CREW ELECTED TO RETURN TO FIELD, AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED BAGGAGE DOOR WARNING TEST IAW AMM 52-76-00 AND COULD NOT DUPLICATE THE PROBLEM. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: POWER SUPPLY — DISCHARGED (EMERGENCY LIGHTS) · airframe 17,796 hrs · 16,774 cycles

DURING INSPECTION, FOUND THAT THE EMERGENCY FLOOR LIGHT FROM THE EXIT AFT DID NOT ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NUMBER 4 BATTERY POWER SUPPLY. OPERATIONAL CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 16,540 hrs · 15,611 cycles

ON FLIGHT 4350, CREW REPORTED EMERGENCY FLOOR LIGHT STRIPS 1 - 4 STRIPS CAME ON DURING TEST BUT THEN WENT OFF AFTER ABOUT ONE SECOND. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED BATTERY PACK POWER SUPPLY PER AMM 33-50-04. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: ENGINE — ODOR (NR 2)

SJC - FLT 3174 - SMELL AND HAZE IN CABIN DECLARED EMERGENCY AND FOLLOWED EMERGENCY PROCEDURES. REPLACED NR 2 ENGINE. OPS CHECKS AND LEAK CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: ENGINE — MALFUNCTIONED (RIGHT)

SJC - FLT 3174 - SMELL AND HAZE IN CABIN. REPLACED RIGHT ENGINE WITH OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: WIRE — BROKEN (EXIT DOOR)

RT FWD EMERGENCY EXIT EXTERNAL LIGHT INOPERATIVE. REPAIRED BROKEN WIRE SEGMENT BETWEEN SPLICES SP7377 AND P2198 IN WIRE HARNESS AT EXIT DOOR. OPERATIONAL CHECK GOOD AND AIRCRAFT RETURNED TO SERVICE. (K)

Part: A/C PACK — CONTAMINATED (BOTH)

ON CLIMB OUT FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN. RECEIVED LAV SMOKE INDICATION ON EICAS. RAN BOTH ENGINES WITH BOTH PACKS ON TO BURN OUT RESIDUAL OIL FROM BLEED DUCTS. RESIDUAL OIL IN DUCTS WAS FROM THE ENGINE THAT WAS PREVIOUSLY MOUNTED ON THE LT SIDE. AC RETURNED TO SERVICE. (K)

Part: CARBON SEAL — LEAKING (NR 1 ENGINE)

AFTER TAKEOFF CREW GOT VISIBLE SMOKE IN CABIN AND A LAV SMOKE EICAS MESSAGE. REPLACED NR 1 ENGINE DUE TO CARBON SEAL LEAKING. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (SW21200600331) (K)

Part: FAN — BURNED (CABIN)

AFTER TAKEOFF CREW GOT VISIBLE SMOKE IN CABIN AND LAV SMOKE EICAS MESSAGE. REPLACED RECIRCULATION FAN. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (SW21200600536) (K)

Part: STRINGER — CHAFED (FUSELAGE)

STRINGER 19R WAS FOUND TO BE CHAFED AT THE AFT BELLY PANEL. BLENDED THE CHAFED AREA AND FABRICATED AND ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 30 CHAPTER 53-24-02. (M)

Part: FLOOR SUPPORT — CORRODED (FS 25)

ABI - THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 25. REMOVED THE CORROSION BY MAKING A CUTOUT. FABRICATED A FILLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 30, CHAPTER 53-00-10. (M)

Part: FLOOR SUPPORT — CORRODED (FS 20)

A PREVIOUS REPAIR, REF FAA FOR 337 DATED DEC 9, 2004, OF THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. REMOVED THE EXISTING REPAIR AND CLEANED THE AREA. FABRICATED A REPAIR PLATE AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, EMB145/1142 REV 30, CHAPTERS 53-00-10 FIG 201. (M)

Part: CONTROL UNIT — INOPERATIVE (HORIZONTAL STAB)

DUAL PITCH TRIM FAILURE. PERFORMED RESET PROCEDURES IN AOM AND PROCEEDED ON WITH NO INCIDENT. REPLACED THE HSCU. OPS CHECK GOOD. AC RETURNED TO SERVICE. (K)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN MBV INSPECTION, THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED BELOW SRM LIMITS AT FRAME 20. BLENDED THE CORRODED AREA AND PERFORMED NDT INSPECTION. FABRICATED AN EXTERNAL ANGLE, FILLER, PLATE AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM EMB-145/1142 REV 22, CHAPTER 53-21-10 FIGURE 201. (M)

Part: ENGINE — FAILED (LEFT)

AFTER TAKEOFF WHEN PACK WAS SELECTED ON THE COCKPIT FILLED WITH SMOKE AND CONTINUED UNTIL NR 1 PACK WAS SHUT OFF BY CREW. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE IAW EMB MM. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M)