N625AE

Part: RUDDER — FAILED (ZONE 300) · airframe 53,020 hrs · 50,986 cycles

RUDDER SYSTEM 1/2 INOP, YAW DAMPER FAIL AND AUTOPILOT FAIL EICAS MESSAGE DISPLYED. RAN QRH RUDDER 1-2 INOP MESSAGE PERSISTED.

Part: YAW DAMPER — FAILED (RUDDER SYS) · airframe 53,020 hrs · 50,986 cycles

RUDDER SYSTEM 1-2 INOP, YAW DAMPER FAILED, AND AUTOPILOT FAIL EICAS MESSAGE DISPLAYED. RAN QRH RUDDER 1-2 INOP MESSAGE PERSISTED. PERFORMED T/S IRT FIM 27-22-00-804-A STEPS 1-2, 9 THRU 19, FOUND TO BE TRANSITORY. AIRCRAFT OK FOR SERVICE.

Part: WARNING MESSAGE — ACTIVATED (RUDDER) · airframe 53,020 hrs · 50,986 cycles

DURING CLIMB, RUD SYSTEM 1/2 INOP EICAS MESSAGE, FOLLOW QRH AND SELECTED #2 OFF AND #1 SYSTEM RETURNED.

Part: UNKNOWN — ODOR (CABIN) · airframe 52,339 hrs · 50,245 cycles

POSSIBLE LIGHTNING STRIKE WITH BURNING ODOR IN CABIN AND FLIGHT DECK AT ABOUT 20K AND ODOR DISAPATED. ALL INSTRUMENTS NORMAL. PERFORMED LIGHTNING STRIKE INSP IAW EMB AMM 05-50-01 DAMAGE FOUND AND DOCUMENTED ON LP 305315 SEQ 2 AND 3, NO OTHER DEFECTS NOTED. NO BURNING SMELL NOTED. ALL SYSTEMS OPS NORMAL.

Part: SLEEVE — MELTED (TEMP CNTL VALVE) · airframe 52,339 hrs · 50,245 cycles

BURNING SULFUR SMELL IN FLIGHT DECK AND CABIN. IN CRUISE FL340 ODOR DISSIPATED. FACT 04MAY24 17:35 CLT INSPECTED PACK 1 AND 2 FOUND MELTED SLEEVES ON TEMP CONTROL VLV ON PACK 1 IRW AMM 21-51-00. RAN ENGINES AND PACK 2 WITH CREW. NO DEFECTS NOTED WITH PACK 1 OFF. SEE NEXT PAGE SEQ 1 FOR MEL OF PACK 1.

Part: UNKNOWN — ODOR (E/E BAY) · airframe 51,959 hrs · 49,793 cycles

ELECTRICAL BURNING SMELL COMING FROM FORWARD ELECTRONICS COMPARTMENT. R+R PAA IAW AMM 23 31 01 OPS CHECK GOOD AT THIS TIME A/C OK FOR SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 50,944 hrs · 48,623 cycles

PITOT 2 INOP EICAS MESSAGE DISPLAYED. T/S W/U FOR PITOT 2 MSG ON EICAS. R/R RELAY K0054 IAW AMM 30-31-01 NO FIX. SLAVED IN PITOT 2 SENSOR. HEAT CAME ON. TEMPORARILY REINSTALLED OLD PITOT SENSOR. REQUIRES FURTHER T/S.

Part: NONE — NONE · airframe 50,115 hrs · 47,705 cycles

UPON TAKEOFF, CAB ALT AND RATE INDICATIONS SHOWED 0 FROM 2000 TO 8000 FT IN AUTO MODE. FACT 24FEB23 21:52 CLT CYCLED CPAM C/B, PERFORMED PRESSURIZATION CONTROL SYSTEM FUNCTIONAL TEST IN AUTO MODE IAW AMM 21-31-00-700-802-A. SYSTEM OPS NORMAL, OK FOR SERVICE

Part: PUMP — FAULTED (NR 2 ENGINE FUEL) · airframe 49,808 hrs · 47,357 cycles

DURING TAKE OFF E2 LOW FUEL PRESS DISPLAYED ON EICAS WHEN OPERATING ON PUMP 2B. VERIFIED 2A AND 2C OPERATING NORMALLY... P/C C/B A4 ON LH DC DIST. BOX. T/S IAW FIM 28-45-00-810-802-A. R & R ELECTRIC FUEL PUMP 2B IAW AMM 28-21-01. UPON REMOVAL FOUND DEBRIS ON PUMP INTAKE SCREEN, PROBABLE CAUSE OF ISSUE. OPS CHECK IAW AMM 28-45-00 GOOD.

Part: NONE — NONE · airframe 48,935 hrs · 46,371 cycles

PDIS 625 27-41 2719362 12JUN22 CLT CLOSE PITCH TRIM INOP DURING FLIGHT ON CAPT AND FO YOKE SWITCHES. FACT 12JUN22 18:26 CLT T/S WITH REF TO FIM 27-43-00-810-801-A REMOVED AND REPLACED HSCU IAW AMM 27-40-01. OPS CHECK GOOD. NO OTHER DEFECTS NOTED AT THIS TIME. OK FOR SERVICE

Part: NONE — NONE · airframe 48,865 hrs · 46,304 cycles

E913652 - RH WING RIB 21 IS CRACKED .... REPAIRED RH WING RIB 21 IAW PIEDMONT EO1-57-22-0119.

Part: NONE — NONE · airframe 48,865 hrs · 46,304 cycles

E913662 - LH WING RIB 21 IS CRACKED .... REPAIRED LH WING RIB 21 IAW PIEDMONT EO1-57-22-0116

Part: NONE — NONE · airframe 48,865 hrs · 46,304 cycles

E911901 - THERE IS A POSSIBLE SKIN CRACK AROUND A RIVET ON FR 78, STGR 6L - 7L .... FABRICATED AND INSTALLED SERVICEABLE SKIN BUSHING ON FR 78 BTW STR 6L-7L IAW EMB 145 SRM 53-32-01, ITEM 9, FIG. 213 AND EO1-53-22-0098

Part: NONE — NONE · airframe 48,865 hrs · 46,304 cycles

E911899 - THERE IS A POSSIBLE SKIN CRACK AROUND A RIVET ON FR 79, STGR 4L - 5L .... FABRICATED AND INSTALLED SERVICEABLE SKIN BUSHING ON FR 79 BTW STR 4L-5L IAW EMB 145 SRM 53-32-01, ITEM 9, FIG. 213 AND EO1-53-22-0098

Part: NONE — NONE · airframe 48,865 hrs · 46,304 cycles

E911897 - THERE IS A POSSIBLE SKIN CRACK AROUND A RIVET ON FR 78, STGR 8R - 9R .... FABRICATED AND INSTALLED SERVICEABLE SKIN BUSHING ON FR 78 BTW STR 8R-9R IAW EMB 145 SRM 53-32-01, ITEM 9, FIG. 213 AND EO1-53-22-0099

Part: NONE — NONE · airframe 48,865 hrs · 46,304 cycles

E913854 - FR 72 IS CRACKED BTW STR 17L-16L ....REPAIRED FR 72 CRACK BETWEEN STR 17L-16L IAW PIEDMONT EO1-53-22-0093.

Part: RIB — CRACKED (LT WING) · airframe 48,865 hrs · 46,304 cycles

E913228 - LH WING RIB #21 IS CRACKED .... ACCOMPLISHED REPAIR OF LH WING RIB 21 UPPER FLANGE IAW EMB 145 SRM 57-20-07 ITEM 4 AND EO1-57-22-0095

Part: NONE — NONE · corrosion level 2 · airframe 48,865 hrs · 46,304 cycles

SUPPLEMENTAL INFORMATION TO ADD CORRECTIVE ACTION .... E913095 - LH OUTBD SEAT TRACK SUPPORT IS CORRODED AT FR 46 .... COMPLETED REPAIR OF LH UPPER SEAT TRACK SUPPORT AT FR46 IAW EMB 145 SRM 53-00-11RE ITEM 5 AND EO1-53-22-0106

Part: FRAME — CRACKED (ZONE 200) · airframe 48,865 hrs · 46,304 cycles

E913086 - FR 24 IS CRACKED BTW STR 16R-15R. .... COMPLETED INSTALLATION OF SERVICEABLE FR 24 FRAME SECTION AND FRAME SPLICE IAW EMB 145 SRM 53-00-04, ITEM 4, FIG. 201 AND PIEDMONT EO1-53-22-0094

Part: STRUCTURE — DAMAGED (EMERGENCY EXIT) · airframe 48,865 hrs · 46,304 cycles

E912663 - LH PASSENGER ESCAPE HATCH INTERNAL STRUCTURE IS CHAFED 3 EACH .... INSTALLED AND EDGE SEALED SERVICEABLE REPAIR DOUBLER ON LH PASSENGER ESCAPE HATCH INTERNAL STRUCTURE IAW ETD2022 145-013959 AND PIEDMONT EO1-52-22-0086

Part: SKIN — CRACKED (CARGO DOOR) · airframe 48,865 hrs · 46,304 cycles

E912739 - CARGO DOOR EXTERNAL SKIN IS CRACKED AT AFT UPPER CORNER OF HANDLE CUTOUT .... FABRICATED DOUBLER, FILLED AND INSTALLED DOUBLER AND FILLER ON CARGO DOOR EXTERNAL SKIN AROUND HANDLE CUTOUT IAW ETD2022-145-014172 AND EO1-52-22-0085

Part: ATTACH BRACKET — GOUGED (COCKPIT) · airframe 48,865 hrs · 46,304 cycles

E912960 - CO-PILOT BULKHEAD OTBD UPPER ATTACHMENT BRACKET IS GOUGED .... REMOVED AND INSTALLED NEW SERVICEABLE CO-PILOT BULKHEAD OTBD UPPER ATTACHMENT SHEET BRACKET IAW EMB145 SRM 51-40-02

Part: FRAME — CRACKED (ZONE 200) · airframe 48,865 hrs · 46,304 cycles

E912957 - FRAME 14 IS GOUGED BETWEEN STRINGERS 5R-6R .... PERFORMED PERMANENT REPAIR ON FRAME14 BETWEEN STRINGERS 5R-6R IAW EO1-53-22-0096.

Part: FRAME — CRACKED (ZONE 100) · airframe 48,865 hrs · 46,304 cycles

E912942 - FR 66 IS CRACKED BTW STR 18L-17L .... REMOVED AND REPLACED FR 66 LOWER SECTION IAW EMB 145 SRM 51-40-02.

Part: NONE — NONE · airframe 48,865 hrs · 46,304 cycles

E912615 - BAGGAGE DOOR WEBBING IS GOUGED 4 EACH 3 AT PREVIOUS REPAIR .... REACCOMPLISHED REPAIRES AT HB4/VB3, HB3/VB4 IAW EMB 145 SRM 52-30-01 RE ITEM 12, FABRICATED DOUBLER, FILLER AND INSTALLED SERVICEABLE DOUBLER AND FILLER AT HB4-VB1 IAW ETD2022-145-013791, SRM 52-30-01RE ITEM 12 AND EO1-52-22-0084

Part: NONE — NONE · corrosion level 2 · airframe 41,060 hrs · 37,485 cycles

E913853 - RH OUTBD CARGO FLOOR SILL IS CORRODED JUST FWD OF FR 71 .... REMOVED AND REPLACED RH OUTBD CARGO FLOOR SILL JUST FWD OF FR 71 IAW EMB145 SRM 51-40-02

Part: NONE — NONE · airframe 48,865 hrs · 46,304 cycles

E913751 - BAGGAGE DOOR LOWER L BRACKET FWD EDGE IS BROKEN OFF .... RAR BAGGAGE DOOR LOWER L BRACKET IAW EMB 145 SRM 51-40-02

Part: NONE — NONE · airframe 48,865 hrs · 46,304 cycles

E913771 - 52-21-06 CORROSION ON RH PASSENGER CABIN ESCAPE HATCH LOWER INTERNAL AND EXTERNAL FRAME .... CORROSION ON RH PASSENGER CABIN ESCAPE HATCH LOWER INTERNAL FOUND TO BE NON-SIGNIFICANT DAMAGE IAW EMB145 SRM 51-10-05, AND REMOVED AND REPLACED THE EXTERNAL FRAME IAW EMB145 SRM 51-40-02.

Part: NONE — NONE · airframe 41,060 hrs · 37,485 cycles

E913852 - RH OUTBD AFT CARGO CARGO FLOOR SILL IS CORRODED AT FWD END AT FR 71 .... REMOVED AND REPLACED RH OUTBD AFT CARGO FLOOR SILL AT FR 71 IAW EMB145 SRM 51-40-02.

Part: NONE — NONE · airframe 48,865 hrs · 46,304 cycles

E912345 - VERTICAL STAB TO FUSELAGE LH DRAG ANGLE IS CRACKED AT FWD END .... RAR LH VERTICAL STAB TO FUSELAGE DRAG ANGLE FWD SECTION IAW EMB 145 SRM 51-40-02

Part: NONE — NONE · airframe 48,819 hrs · 46,264 cycles

PDIS 625 32-60 2719062 26MAR22 PHL CLOSE LG AIR/GND FAIL DISPLAYED ON EICAS AFTER TAKE OFF. FACT 26MAR22 04:33 PHL REF LP 271907-1 FOR LOW NLG STRUT PRESSURE WORK DONE PERFORMED EXT AND RETRACTION IAW AMM 32-30-00 OPS CHECK GOOD NO FAULTS FOUND

Part: WARNING BUZZER — FALSE ACTIVATION (COCKPIT) · airframe 47,481 hrs · 44,842 cycles

CREW CALLED AND STATED ON TAKEOFF ROLL TRIM AURAL SOUNDED AND MASTER CAUTION LIGHT TRIGGERED. THEY ABORTED THE TAKEOFF. NO EICAS MESSAGES DISPLAYED HAD CREW CHECK CMC NO MESSAGES ON CMC. ADVISED CREW TO RECHECK ALL T/O SETTINGS. HISTORY: NO HISTORY IN 30 DAYS. SECOND ATTEMPT AT TAKEOFF WAS UNEVENTFUL.

Part: SLEEVE — UNSECURE (BLEED SYSTEM) · airframe 47,206 hrs · 44,542 cycles

BLEED 2 LEAK ON CLIMB OUT. C/W QRH AND MESSAGE EXTINGUISHED. MAINTENANCE: T/S IN REF TO FIM 36-20-00-810-802-A. FOUND LOOSE SLEEVE ON NR 2 BLEED LINE IN AFT AVIONICS BAY RESECURED SLEEVE, AS REQUIRED. PERFORMED AIR BLEED SYSTEM OPERATIONS CHECK, IAW AMM 36-00-00-700-803-A/500. OPERATIONS CHECK GOOD, OK FOR SERVICE AT THIS TIME.

Part: COMPRESSOR — CONTAMINATED (NR 1 ENGINE) · airframe 47,049 hrs · 44,350 cycles

DURING TAKE OFF AT TAKE OFF THRUST FINE WHITE SMOKE APPEARED IN COCKPIT AND CABIN WITH BOTH PACKS AND RECIRCS ON. MAINTENANCE: BORESCOPED #1 ENGINE, FOUND OIL IN THE COMPRESSOR FLOW PATH EXTENSION FROM THE FRONT SUMP. ENGINE #1 REQUIRES R&R WITHIN 100 FLIGHT HOURS, SEE HA300 SEQ. 5, 6 & 7 FOR MAINTENANCE PERFORMED & DMT.

Part: PRESSURE SWITCH — FAULTY (ANTI-ICE SYSTEM) · airframe 46,758 hrs · 44,019 cycles

PDIS 625 30-10 2260201 09APR20 ROC CLOSE WING A/ICE FAIL WARNING MESSAGE IN FLIGHT 2 TIMES, C LEARED WHEN NO LONGER IN ICING CONDITIONS. CMC SHOWS WING 2 A/ICE BURST MSG FACT 09APR20 20:00 ROC R+R DIFFERENTIAL PRESSURE SWITCH IAW AMM 30-11-06. O PS CHECKED IAW AMM 30-00-00. OPS CHECK GOOD. OK FOR SERVICE

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,637 hrs · 42,750 cycles

DISCREPANCY: FRAME 68 L-PROFILE IS CORRODED AT THE BOTTOM AT THE CARGO DOOR CUTOUT. CORRECTIVE ACTION: REPAIRED AREA IAW SRM 53-31-04-RE ITEM 4 AND EO1-53-19-0379.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,637 hrs · 42,750 cycles

DISCREPANCY: POSSIBLE CRACK AROUND RIVET AT FR 78 BTW STR 4R-5R. CORRECTIVE ACTION: PERFORMED DYE PENETRANT INSP CRACK INDICATED. REPAIRED AREA IAW SRM53-32-01 AND EO1-53-19-03914.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,637 hrs · 42,750 cycles

DISCREPANCY: FRAME 65 L-PROFILE IS CORRODED AT THE BOTTOM AT THE CARGO DOOR CUTOUT. CORRECTIVE ACTION: PERFORMED REPAIR IAW SRM 53-31-04 AND EO1-53-19-0378.

Part: VALVE — FAILED (NR 1 PACK) · airframe 45,614 hrs · 42,725 cycles

ABORTED TAKEOFF AT 80 KNOTS DUE TO PACK 1 OVERLOAD EICAS MESSAGE. PACK 1 SELECTED OFF. R & R NR 1 PACK VALVE IAW AMM 21-51-01 OPS CHECK GOOD OK FOR SERVICE. NO EMERGENCY DECLARED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,717 hrs · 41,726 cycles

NDIS 625 33-51 0017010 19FEB19 SBY CLOSE RIGHT HAND EMERGENCY EXIT LIGHT INOP FACT 19FEB19 09:45 SBY RR RIGHT HAND EMERGENCY EXIT LIGHT IAW AMM 33-50-14 P/N ON EMERGENCY EXIT LIGHT 7444-36 P/N OFF EMERGENCY EXIT LIGHT 7444-36

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,374 hrs · 41,336 cycles

MAIN DOOR EMERGENCY LIGHT INOP. REMOVED THE MAIN DOOR EMERGENCY LIGHT COVER IAW AMM TASK #25-23-04-000-801-A. REMOVED THE EMERGENCY LIGHT ASSEMBLY FROM THE MAIN DOOR EMERGENCY LIGHT COVER AND REPLACED WITH NEW ASSEMBLY AND RETAINED HARDWARE INSTALLED MAIN DOOR EMERGENCY LIGHT COVER IAW AMM TASK 25-23-04-400-801-A. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,369 hrs · 41,330 cycles

FLOOR EMERGENCY LIGHT STRIP BETWEEN ROWS 15 AND 16 INOP. R&R LIGHT STRIP. OPS CK GOOD IAW AMM TASK 33.50.12.00/400.801.A.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,030 hrs · 40,934 cycles

MAIN ENTRY DOOR HINGE COVER EMERGENCY LIGHT DOES NOT ILLUMINATE. R&R BULB IAW AMM 33-50-10-000/400-801-A. OPS CHECK GOOD.

Part: DUCT — LEAKING (WING) · airframe 43,672 hrs · 40,498 cycles

ON CLIMBOUT GOT WING AI FAIL CAUTION MESSAGE WITH WING 2 AI LEAK IN CMC. R&R 2 CLAMPS NR 2 DUAL TEMP CTRL VLV NO FIX. INSP FOUND LEAK AT Y DUCT NEAR DUAL TEMP CTRL VLV. C/W FIM TASK 30-11-00-810-807-A SUB TASK 817-001-A. R&R DEFECTIVE AS REQ OPS CHECK NO LEAKS NOTED OK FOR SERVICE.

Part: UPLOCK — MALFUNCTIONED (LT MLG) · airframe 43,648 hrs · 40,470 cycles

AFTER TAKEOFF AND GEAR RETRACTION LEFT MAIN LANDING GEAR UPLOCK CYCLED BETWEEN GREEN AND DASHES. R&R LT MLG UPLOCK BOX IAW AMM 32-33-10. ADJUSTED INSTALLATION OF UPLOCK PROX SWITCHES. LEAK CHECK AND LANDING GEAR RETRACTION CHECK GOOD. NO EICAS MESSAGES OR OTHER DEFECTS NOTED. OPERATIONAL CHECK GOOD. OK FOR SERVICE.

Part: HEATER — FAILED (NR 3 PITOT) · airframe 42,909 hrs · 39,620 cycles

NR 3 PITOT INOPERATIVE CAUTION MESSAGE ON EICAS, FOUND HEATING ELEMENT WIRES BURNED. THE NR 3 PITOT HEAD WILL NOT HEAT. R & R PITOT STATIC SENSOR IAW AMM 34-13-02. OPS AND LEAK CHECKED GOOD IAW AMM 30-31-00. REPAIRED WIRING IAW SWPM 20-21-00.

Part: A/C PACK — WARNING MESSAGE (NR 2)

PDIS 625 21-50 1244181 14DEC17 ERI ASSGN PACK 2 OVLD AND PACK 2 OVHT EICAS MESSAGES APPEARED. 9853 HISTORY: . MEL 14DEC17 10:35 ERI C34804 21-13-1 1 AIR CON PACK .

Part: UNKNOWN — SMOKE (NR 1 ENGINE) · airframe 42,313 hrs · 38,996 cycles

SMOKE COMING OUT OF NR 1 ENGINE TAILPIPE. INSP LPT3 BLADES AND RTBS FOR OIL POOLING OR EVIDENCE OF OIL, NO HISTORY OF SMOKE REPORTED ON SHUT DOWN, NO SMOKE OBSERVED ON SHUT DOWN AT MDT. OK FOR SVC, REF FIM 72-00-00-810-812.

Part: FAN — FAILED (RECIRCULATION) · airframe 42,110 hrs · 38,779 cycles

BURNING ODOR IN THE COCKPIT COMING FROM THE NR 1 PACK. R & R THE NR 1 RECIRCULATION FAN IAW MM 21-24-01. OPS CHECKED GOOD, OK FOR SERVICE

Part: RMU — MALFUNCTIONED (NR 2) · airframe 42,032 hrs · 38,696 cycles

NR 2 VHF TRANSMITS CARRIER ONLY WITH ENGINES RUNNING. R & R THE NR 2 RMU IAW AMM 23-81-01-400-801-A. OPS CHECKED IAW AMM 23-81-00-700-801-A. OPS CHECKED GOOD, OK FOR SERVICE.

Part: SWITCH — FAILED (NLG WOW) · airframe 41,896 hrs · 38,554 cycles

AFTER GEAR RETRACTION, THE NR 1&2 ENGINE REVERSERS DISAGREE EICAS CAUTION MESSAGE APPEARED. DURING GEAR EXTENSION THE MESSAGE EXTINGUISHED. FOLLOWED FIM FOR ENG REVERSER DISAGREE FIM ASSOCIATED NOSE PROXIMITY SENSOR FAILED CMC MESSAGE TO CAUSES ISSUE. R & R THE NOSE GEAR WOW SWITCH

Part: SWITCH — FAILED (MLG WOW) · airframe 41,895 hrs · 38,552 cycles

AFTER TAKEOFF, LANDING GEAR AIR - GND FAILED EICAS MESSAGE. CMC FOUND A MESSAGE FOR NOSE WOW FAIL IAW FIM 32-63-810-802A. CHANGED THE NOSE GEAR WOW SWITCH IAW 32-63-02. SWUNG GEAR AND CLEARED CMC WHEN MTC COMPLETED.

Part: SWITCH — FAILED (NLG WOW) · airframe 41,895 hrs · 38,552 cycles

AFTER TAKEOFF, ENG 1-2 REVERSER DISAGREE EICAS MESSAGE. R & R THE NOSE GEAR WOW SWITCH.

Part: WARNING MESSAGE — FALSE ACTIVATION (THRUST REVERSERS) · airframe 41,892 hrs · 38,547 cycles

AFTER TAKEOFF ENG 1-2 THRUST REVERSER DISAGREE EICAS MESSAGE. PERFORMED NR 1 AND 2 THRUST REVERSER OPERATIONAL CHECK IAW 78-31-01-700-810-A. OPS CHECKED GOOD. OK FOR SERVICE AT THIS TIME.

Part: WARNING MESSAGE — ILLUMINATED · airframe 41,892 hrs · 38,547 cycles

AFTER TAKE OFF LANDING GEAR AIR-GROUND FAIL EICAS MESSAGE. OPEN

Part: FLOOR SUPPORT — CORRODED (FRAMES 24-25) · airframe 41,448 hrs · 38,106 cycles

CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 24-25 REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, ETN-EM-53-139, AND ETN-53-150

Part: BRACKET — CORRODED (EMERGENCY EXIT) · airframe 41,448 hrs · 38,106 cycles

CORROSION ON LT EMERGENCY EXIT LOWER BRACKET. REMOVED AND REPLACED THE BRACKET IAW SRM 51-40-02 AND SRM 51-20-01.

Part: SPAR — CRACKED (LT WING) · airframe 41,448 hrs · 38,106 cycles

LEFT WING SPAR LOWER FLANGE CRACKED OTBD OF RIB 9. REPAIRED THE SPAR IAW ERS-EM-57MR-784.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,448 hrs · 38,106 cycles

HALF OF EMERGENCY LIGHT STRIP NR 4 IS INOPERATIVE. REMOVED AND REPLACED THE LIGHT IAW AMM 33-50-12.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 41,382 hrs · 38,041 cycles

ARCFT WILL NOT PRESSURIZE CORRECTLY, CABIN RATE FROM + 700 TO 359 THEN DASHES. LOST CABIN ALTITUDE INDICATIONS AS WELL. . REMOVED AND REPLACED AUTO PRESSURIZATION DIGITAL CONTROLLER IAW AMM 21-31-01 OPS CHECKED GOOD.

Part: UPLOCK — MALFUNCTIONED (MLG) · airframe 41,309 hrs · 37,977 cycles

UPON GEAR EXTENSION, THE MAIN LANDING GEAR DID NOT EXTEND. CREW ATTEMPTED A SECOND TIME AND GEAR FULLY EXTENDED. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE RT MLG UP LOCK BOX ASSY IAW EMB MM CH 32-33-10. OPERATIONAL AND FUNCTIONAL CHECKS GOOD .

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,468 hrs · 37,167 cycles

SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE BULB IAW AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECKED GOOD.

Part: DOOR SEAL — DIRTY (CABIN DOOR) · airframe 39,852 hrs · 36,621 cycles

FLIGHT ATTENDANT ADVISES MAIN CABIN DOOR IS DIFFICULT TO OPEN. CLEANED MAIN DOOR SEAL IAW 52-10-04. NO DEFECTS NOTED.

Part: SEAL — MISSING (COCKPIT WINDOW) · airframe 39,717 hrs · 36,495 cycles

LOUD UNKNOWN NOISE NEAR THE FLIGHT DECK. SOUNDED LIKE RAIN ON THE METAL ROOF. REFERENCE ITEMS 2 & 3 OF THIS LOG PAGE FOR CORRECTIVE ACTIONS. HUMP SEAL ON CAPTAINS WINDOW AT 1 O'CLOCK POSITION MISSING. DEFERRED IAW AMM 56-10-01. AERODYNAMIC SEALANT LOOSE BETWEEN WINDSHIELD FRAME & FUSELAGE AT 5 O'CLOCK POSITION ON CAPTAINS FWD WINDOW. DEFERRED IAW FMR IAW ETN EM 51-061.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,434 hrs · 36,248 cycles

SERVICE DOOR LINER EMER LIGHT INOPERATIVE. R & R SERVICE DOOR LINER EMER LIGHT BULB IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,397 hrs · 36,219 cycles

SERVICED DOOR EMER LIGHT INOPERATIVE. R & R LAMP IN SERVICE DOOR EMER LIGHT FIXTURE IAW AMM 33-50-09-000-801-A & 33-50-09-400-801-A. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 39,066 hrs · 35,883 cycles

CAPTAIN`S FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED THE FLASHLIGHT ASSY, OPS CHECKED GOOD IAW AMM 33-50-16.

Part: RIB — CRACKED (RT WING) · airframe 38,771 hrs · 35,619 cycles

RIGHT WING RIB 5 CRACKED ON AFT LARGE LIGHTNING HOLE AT 7 O'CLOCK POSITION. ACCOMPLISHED REPAIR OF RT WING RIB 5 IAW ERS-EM-57MR-551.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 38,771 hrs · 35,619 cycles

SERVICE DOOR CUT OUT AFT FRAME HAS AREA OF CORR0SION ABOVE THE FLOOR LINE. REPAIRED THE SERVICE DOOR CUT OUT AFT FRAME, ABOVE THE FLOOR LINE IAW SRM 53-00-04, 51-40-02.

Part: DOUBLER — GOUGED (FUSELAGE) · airframe 38,771 hrs · 35,619 cycles

FRAME 65 REPAIR DOUBLER, BETWEEN STRINGER 12R & 13R IS GOUGED. FOUND DURING OPEN UP. ACCOMPLISHED REPAIR TO FRAME 65 REPAIR DOUBLER IAW ERS-EM-53MR-1789.

Part: FRAME — CORRODED (FUSELAGE) · airframe 38,771 hrs · 35,619 cycles

L SHAPE AT FRAME 65, BETWEEN STRINGER 16L - 17L CORRODED. INSTALLED SERVICEABLE REPAIR SECTION IAW SRM 51-40-02 & 53-31-04.

Part: STRUCTURE — CORRODED (LAVATORY) · airframe 38,771 hrs · 35,619 cycles

THE LAVATORY BUCKET IS CORRODED. INSTALLED REPAIR DOUBLER & NUTPLATES IAW SRM 51-40-02 & SRM 51-40-09. SEE WIPS & TASKS FOR DETAILS.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,771 hrs · 35,619 cycles

LEFT UPPER FUSELAGE SKIN CRACKED AT FRAME 75, JUST ABOVE STRINGER 2L. REPAIRED CRACK AT FRAME 75, JUST ABOVE STRINGER 2L IN LT FUSELAGE SKIN IAW ERS-EM-53MR-1800.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,771 hrs · 35,619 cycles

RIGHT UPPER FUSELAGE SKIN CRACKED AFT OF FRAME 75, JUST ABOVE STRINGER 2R CRACK ENDS MARKED. REPAIRED FRAME 75 RT IAW ERS-EM-53MR-1799.

Part: LIGHT — CRACKED (CABIN) · airframe 38,771 hrs · 35,619 cycles

LEFT NR 2 EMER LIGHT STRIP EXTRUSION CRACKED. R & R LT NR 2 EMER LIGHT STRIP EXTRUSION IAW AMM 33-50-12. SEE BOW 205187 FOR OPERATIONS CHECK.

Part: WARNING SYSTEM — ACTIVATED (ANTI-ICE SYSTEM) · airframe 38,747 hrs · 35,598 cycles

UPON ENTERING ICING CONDITIONS, RECEIVED ICE CONDITION ANTI-ICE INOPERATIVE MASTER WARNING MSG. PERFORMED OPERATIONS CHECK OF ANTI-ICE SYS AFTER CORRECTIVE ACTION ON ITEM 1 ON THIS LG PG IAW AMM 30-00-00 & FOUND WORKING SATISFACTORY.

Part: WIRE — BROKEN (CABIN) · airframe 38,660 hrs · 35,526 cycles

AFT EMER LIGHTING PROXIMITY STRIP INOPERATIVE, BROKEN WIRE. R & R AFT FLOOR EMER LIGHTING PROXIMITY STRIP IAW AMM 33-50-12-000-801 & 33-50-12-400-801. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — DIM (CABIN) · airframe 38,297 hrs · 35,191 cycles

FLIGHT ATTENDANT FWD FLASHLIGHT DIM. R & R FLIGHT ATTENDANT FWD FLASHLIGHT IAW AMM 33-50-16-000-801-A & 33-50-16-400-801-A. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 37,397 hrs · 34,403 cycles

FUSELAGE FRAME 1A DAMAGED AT STRINGER 15R. REPAIRED FUSELAGE IAW ERS-EM-53MR-1171.

Part: BATTERY — DISCHARGED (CABIN) · airframe 37,364 hrs · 34,379 cycles

FUSELAGE EMER LIGHT FWD OF RT WING DIM. R & R NR 2 EMER BATTERY ASSEMBLY & CHARGER IAW AMM 33-50-04. BATTERY CHARGER ASSEMBLY PN 11-0049, SN 13314.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 37,280 hrs · 34,299 cycles

EMERGENCY LIGHTS AT ROW 3 INOPERATIVE. R & R NR 2 DC & AC INVERTER. OPERATIONS CHECKED GOOD IAW AMM 33-50-11.

Part: SIGN — DEFECTIVE (CABIN) · airframe 36,982 hrs · 34,050 cycles

EMERGENCY LIGHTING MARKER SIGN AT GALLEY AISLE CEILING ONLY ILLUMINATES AROUND THE EDGES. INSTALLED EMER LIGHTING MARKER SIGN AT GALLEY AISLE IAW AMM 33-50-08. OPERATIONS CHECKED GOOD.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 36,733 hrs · 33,844 cycles

FLIGHT ATTENDANT REPORTED FWD CABIN FLASHLIGHT HOLDER BROKEN. REMOVED & INSTALLED FLASHLIGHT BASE IAW 33-50-16.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 36,672 hrs · 33,785 cycles

LEFT OVERWING EMER LIGHT INOPERATIVE. R & R THE LT UPPER OVERWING EXTERIOR EMER LIGHT LAMP IAW AMM TASKS 33-50-10-000-801-A & 33-50-10-400-801-A. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,672 hrs · 33,785 cycles

FORWARD CTR AISLE CEILING EMER LIGHT INOPERATIVE. R & R FWD CTR AISLE CEILING EMER LIGHT LAMP IAW AMM 33-50-08-000-801-A & 33-50-08-400-801-A. OPERATIONS CHECKED GOOD.

Part: BRACKET — BROKEN (FLASHLIGHT) · airframe 36,210 hrs · 33,412 cycles

RE-ENTER MEL 25-53 LOG PAGE 3628428 ITEM 1. FLIGHT ATTENDANT FLASHLIGHT BRACKET BROKEN. R & R FLIGHT ATTENDANT FLASHLIGHT BRACKET IAW AMM 33-50-16. OPERATIONS CHECKED GOOD. MEL RESTORED.

Part: BRACKET — BROKEN (FLASHLIGHT) · airframe 36,203 hrs · 33,404 cycles

FLIGHT ATTENDANT FLASHLIGHT BRACKET BROKEN. DEFERRED MEL 25-53. MAINT PROCEDURES COMPLIED WITH.

Part: CONNECTOR — DIRTY (CABIN) · airframe 36,170 hrs · 33,379 cycles

EMERGENCY EXIT LIGHT ON BULKHEAD WALL IN FRONT OF 3B DOES NOT ILLUMINATE. CLEANED CONNECTOR & OPERATIONS CHECKED IAW AMM 33-50-00 OK FOR SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 35,408 hrs · 32,676 cycles

COCKPIT STEP EMER LIGHT INOPERATIVE. R & R NR 1 INVERTER IAW AMM 33-50-11. OPERATIONS CHECKED GOOD.

Part: TRANSDUCER — FAILED (MLG) · airframe 34,696 hrs · 32,095 cycles

AFTER TOUCHDOWN GOT BRAKE DEGRADED, ACFT FELT LIKE IT WAS SLIPPING ON TAXI LT BRAKE WEAKER THAN RT BRAKES. I COULDN’T LOCK LT SIDE AT LOW SPEED BUT RT WOULD LOCK. TROUBLE SHOT IAW EMB-145 FIM TASK 32-41-00-810-816-A FOR CMC MESSAGE, BRAKE WHEEL SPEED TRANSDUCER 3 FAIL. R & R SPEED TRANSDUCER IAW EMB-145 AMM 32-41-03, OPERATIONS CHECKED GOOD.

Part: SKIN — GOUGED (FUSELAGE) · airframe 34,458 hrs · 31,912 cycles

DURING MAINTENANCE INSPECTION ON FLIGHT 2897 FOUND LT FUSELAGE SKIN INSIDE LT PYLON PANEL 414DB GOUGED 2 PLACES JUST ABOVE LOWER PYLON SKIN. THE ACFT WAS REMOVED FROM SERVICE. REPAIRED LT FUSELAGE SKIN INSIDE LT PYLON PANEL 414DB GOUGES JUST ABOVE LOWER PYLON SKIN IAW AEA ERS-EM-53MR-164. THE ACFT RETURNED TO SERVICE.

Part: CONNECTOR — BROKEN (CABIN) · airframe 34,458 hrs · 31,912 cycles

NUMBER 1 EMERGENCY EXIT LIGHT STRIP FLOOR CONNECTOR BROKEN. REPAIRED NR 1 EMERGENCY EXIT LIGHT STRIP FLOOR CONNECTOR IAW SWPM 20-21-00 STEP 6.

Part: SKIN — CORRODED (FUSELAGE) · airframe 34,458 hrs · 31,912 cycles

INTERNAL SKIN CORRODED BETWEEN FRAMES 13 & 14, STRINGERS 19R & 20R. REPAIRED CTR FUSELAGE 1 SKIN IAW AEA EO ERS-EM-53MR-145.

Part: YOKE — CRACKED (RT PYLON) · airframe 34,458 hrs · 31,912 cycles

RIGHT PYLON LOWER YOKE CRACKED. REMOVED & INSTALLED SERVICEABLE YOKE IAW EO EM-5400MR-386.

Part: HOLDER — DAMAGED (CABIN) · airframe 34,458 hrs · 31,912 cycles

NUMBER 1 EMERGENCY LIGHT STRIP HOLDER DAMAGED REQUIRES REPLACEMENT. R & R NR 1 EMERGENCY LIGHT STRIP HOLDER IAW AMM 33-50-12.

Part: STRAP — CORRODED (FUSELAGE) · airframe 34,458 hrs · 31,912 cycles

CIRCUMFERENTIAL STRAP CORRODED BETWEEN FRAMES 13 & 14, BETWEEN STRINGERS 21L - 16R. BLENDED TO REMOVE CORROSION ON CIRCUMFERENTIAL STRAP BETWEEN FRAMES 13 & 14, BETWEEN STRINGERS 21L - 16R IAW CPM 51-15-02 & REMAINING THICKNESS AT BLENDED AREAS ON CIRCUMFERENTIAL STRAP BETWEEN FRAMES 13 & 14, BETWEEN STRINGERS 21L - 16R FOUND TO BE WITHIN LIMITS IAW AEA ERS-EM-53MR-145.

Part: ANTENNA — CORRODED (DME) · airframe 34,458 hrs · 31,912 cycles

REMOVE ANTENNA PN DMNI50-4-2, SN 17163 BASE ERODED & CORRODED.

Part: STRAP — CORRODED (FUSELAGE) · airframe 34,458 hrs · 31,912 cycles

LONGITUDINAL STRAP CORRODED BETWEEN FRAMES 13 & 14, BETWEEN STRINGERS 18R & 17R. BLENDED TO REMOVE CORROSION ON LONGITUDINAL STRAP BETWEEN FRAMES 13 & 14, BETWEEN STRINGERS 18R & 17R IAW CPM 51-14-02 & REMAINING THICKNESS AT BLENDED AREAS ON LONGITUDINAL STRAP BETWEEN FRAMES 13 & 14, BETWEEN STRINGERS 18R & 17R FOUND TO BE WITHIN ALLOWABLE LIMITS IAW AEA ERS-EM-53MR-145.

Part: CONNECTOR — BROKEN (CABIN) · airframe 34,458 hrs · 31,912 cycles

NUMBER 1 EMERGENCY EXIT LIGHT STRIP FLOOR CONNECTOR BROKEN. REPAIRED NR 1 EMERGENCY EXIT LIGHT STRIP FLOOR CONNECTOR IAW SWPM 20-21-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,306 hrs · 31,795 cycles

PASSENGER CABIN FLOOR EMERGENCY LIGHT STRIP ROWS 3 - 6 DO NOT ILLUMINATE. RE CHECKED PASSENGER CABIN FLOOR EMERGENCY STRIP LIGHTS IAW EMB 145 AMM 33-50-00, NO FAULT FOUND.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,342 hrs · 30,995 cycles

EMERGENCY LIGHT AT CEILING AISLE AFT POSITION INOPERATIVE. R & R LAMP IN AFT AISLE CEILING EMERGENCY LIGHT IAW AMM 33-50-08-000-801-A AND 33-50-08-400-801-A. OPS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 33,332 hrs · 30,986 cycles

EMERGENCY LIGHTS WILL NOT TURN OFF, BATTERIES DEAD. R & R EMERGENCY BATTERY NR 1 GALLEY AREA IAW AMM 33-50-04.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 33,332 hrs · 30,986 cycles

NR 3 EMERGENCY BATTERY DEAD. R & R BATTERY IAW AMM 33-50-04.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 33,332 hrs · 30,986 cycles

NR 3 EMERGENCY BATTERY IS DEAD. R & R EMERGENCY BATTERY IAW AMM 33-50-04.

Part: ELECTRONIC UNIT — INOPERATIVE (MLG) · airframe 33,156 hrs · 30,842 cycles

AFTER TAKEOFF RECEIVED AN EICAS LANDING GEAR DISAGREE MESSAGE. CREW COMPLIED WITH AOM VOL 1 PROCEDURES AND DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. R & R LT LANDING GEAR ELETRONINC UNIT IAW AMM 32-32-01. PERFORMED MLG SWING. THE OPS CHECKED GOOD IAW AMM 32-30-00. ACFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 32,653 hrs · 30,431 cycles

DURING B INSPECTION FOUND THE RIGHT OVER WING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVER WING EMERGENCY LIGHT LAMP IAW EMB AMM TASK 33-50-10-000-801-A AND 33-50-10-400-801A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT ASSY — FAILED (AFT CABIN) · airframe 32,179 hrs · 30,057 cycles

FLIGHT 3282, FLIGHT ATTENDANT AND PASSENGERS REPORTED ODOR OF SMOKE AROUND SEATS 15 -17. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. INSPECTED AND FOUND ELECTRICAL ODOR COMING FROM AFT FLASHLIGHT. REMOVED AND REPLACED FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: PUMP — MALFUNCTIONED (HYDRAULIC SYS) · airframe 31,377 hrs · 29,395 cycles

ON FLIGHT 3461 THE CREW REPORTED THAT EN ROUTE FROM MEM, EICAS DISPLAYED "ENGINE 2 HYDRAULIC PUMP FAIL" FOLLOWED BY "HYDRAULIC SYS 2 FAIL' AND 'RUDDER SYS 2 FAIL'. PERFORMED ALL APPROPIATE CHECKLIST AND DECLARED AN EMERGENCY. THE CREW CALLED FOR CFR TO BE ON STANDBY. THE AIRCRAFT LANDED NORMALLY WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 ENGINE HYDRAULIC PUMP IAW AMM 29-10-03. THE OPERATIONAL AND LEAK CHECK IAW RRMM 72-00-00 CHECK WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 31,172 hrs · 29,239 cycles

ON FLIGHT 2749 THE CREW REPORTED THE FIRST OFFICER’S FLASHLIGHT HOLDER WAS BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLASHLIGHT HOLDER. THE OPERATIONAL CHECK WAS GOOD WORK DONE IAW EMB 145 AMM 33-50-16. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT ASSY — INOPERATIVE (AFT CABIN) · airframe 30,641 hrs · 28,788 cycles

FLIGHT 3301, CREW REPORTED THE REAR FLASHLIGHT IN THE CABIN DOES NOT WORK. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT CABIN FLASHLIGHT IAW AMM 33-50-16. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 30,377 hrs · 28,576 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY FLOOR LIGHT STRIPS NR 4 AND NR 5 INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 5 POWER INVERTER IAW EMB 145 AMM 33-50-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 30,239 hrs · 28,457 cycles

DURING B INSPECTION, FOUND THE NR 4 AND 5 EMERGENCY LIGHT STRIPS INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. INSPECTED CONNECTION TO LIGHT AND TO BATTERY POWER SUPPLY. NO DEFECTS NOTED. PERFORMED OPS CHECK OF EMERGENCY LIGHTS IAW AMM 33-50-00. OPS CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 30,086 hrs · 28,329 cycles

DURING MAINTENANCE INSPECTION FOUND THE 1ST EMERGENCY FLOOR STRIP AND SERVICE DOOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. TROUBLESHOT IAW EMB 145 WM 33-50-5. REMOVED AND REPLACED THE NR 2 INVERTER IAW EMB 145 AMM 33-50-11. THE OPERATIONAL CHECK WAS GOOD IAW EMB 145 AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: RIB — CHAFED (LT WING) · airframe 29,883 hrs · 28,146 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT WING PANEL 551CB OUTBOARD RIB CHAFED BY PCA HOSE. AIRCRAFT REMOVED FROM SERVICE. REPAIRED CHAFED RIB IAW AEA EO-EM-57MR-608. AIRCRAFT RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 29,885 hrs · 28,149 cycles

DURING MAINTENANCE INSPECTION FOUND THE NR 8 EMERGENCY LIGHT STRIP HAS BROKEN WIRES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE NR 8 EMERGENCY LIGHT STRIP WIRES IAW EMB 145 SWPM 20-21-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 29,885 hrs · 28,149 cycles

DURING B-INSPECTION FOUND THE EMERGECNY LIGHT STRIP WIRE BROKEN AT FLOORBOARD 251FF. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED EMERGENCY LIGHT STRIP WIRE AT FLOOR PANEL 251FF IAW EMB 145 WM 20-21-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,075 hrs · 27,523 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE MAIN DOOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN DOOR EMERGENCY LIGHT IAW AMM TASKS 33-50-06-000-801-A AND 33-50-06-400-801-A. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CRADLE — DAMAGED (COCKPIT) · airframe 29,050 hrs · 27,605 cycles

ON FLIGHT 3597 THE CREW REPORTED THE CAPTAIN’S FLASHLIGHT CRADLE--THE LOWER CLIP IS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED CAPTAIN’S FLASHLIGHT CRADLE IAW EMB MM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: MODULE — MALFUNCTIONED (CABIN PRESSURE) · airframe 28,479 hrs · 27,078 cycles

ON FLIGHT 2935 THE CREW REPORTED THAT DURING THE CLIMB THE CABIN RATE OF CHANGE IDICATION WAS INOPERABLE. THE CREW ELECTED TO RETURN TO MSN. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CABIN PRESSURE ACQUISTION MODULE PER AMM 21-32-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: RIB — CRACKED (LT WING) · airframe 28,188 hrs · 26,860 cycles

LT WING RIB CRACKED. COMPLIED WITH AEA EO EM-57MR-573.

Part: RIB — CRACKED (LT WING) · airframe 28,185 hrs · 26,859 cycles

DURING PHASE 4 INSPECTION FOUND THE LEFT WING RIB 5 CRACKED, BETWEEN SPAR II AND SPAR III. THE AIRCRAFT WAS REMOVED FROM SERVICE. THE CORRECTIVE ACTION INFORMATION IS PENDING.

Part: BATTERY — DISCHARGED (CABIN) · airframe 28,064 hrs · 26,756 cycles

FOR FLIGHT 9812 MAINTENANCE REPORTED THE EMERGENCY LIGHTS INOPERABLE AFT OF THE EXIT ROW AND BOTH OVER WING LIGHTS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 BATTERY AND CHARGER IAW WC 33-700-19. THE OPERATIONAL CHECK WAS GOOD IAW WC 33-700-17. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,857 hrs · 26,588 cycles

FOR FLIGHT 4364 DURING THE PREFLIGHT INSPECTION FOUND THE LEFT OVERWING AFT EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT AFT EMERGENCY LAMP BULB. THE OPERATIONAL CHECK WAS GOOD IAW EMB 145 MM 33-50-10. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 25,493 hrs · 24,718 cycles

FOR FLIGHT 2969 MAINTENANCE FOUND NUMEROUS EMERGENCY LIGHTS INOPERABLE IN THE AFT CABIN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NR 4 EMERGENCY BATTERY AND CHARGER POWER SUPPLY. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 25,451 hrs · 24,684 cycles

FOR FLIGHT 2789 DURING THE INSPECTION FOUND THE OVERWING EMERGENCY LIGHTS TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 BATTERY AND BATTERY CHARGER IAW W/C 33-700-19. THE OPERATIONAL CHECK WAS GOOD IAW W/C 33-700-17. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SEALANT — WORN (FUEL TANK) · airframe 25,184 hrs · 24,481 cycles

ON FLIGHT 3210 UPON DESCENT THE CREW REPORTED THE ODOR OF JET FUEL PERMEATING THE COCKPIT ESPECIALLY THE FIRST OFFICER'S SIDE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED SEALANT ON LARGE BOLT 7 INCHES FROM UPPER SPAR CAP APPROXIMATELY STATION 480. THE LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,947 hrs · 24,287 cycles

DURING THE MAINTENANCE BASE VISIT FOUND THE CENTER BEAM AT FRAME 25 TO BE CORRODED UNDER THE CARBON CROSS BEAM. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE CENTER BEAM AT FRAME 25 CORROSION UNDER THE CARBON CROSS BEAM EMB 145 IAW EMB 145 SRM 53-00-10 FIG 203 SHEET 1. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CARBON SEAL — LEAKING (NR 2 ENGINE) · airframe 24,568 hrs · 23,920 cycles

ON FLIGHT 4225 ON ROTATION, CREW REPORTED SMOKE IN COCKPIT AND CABIN. CREW DECLARED AN EMERGENCY AND RETURNED TO GRB WITHOUT INCIDENT. AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 0 CARBON SEAL ASSEMBLY IAW R & R MM 72-25-25-000-801 AND 72-25-25-400-801. THE AIRCRAFT WAS RETURNED TO SERVICE. REMOVED AND REPLACED THE NUMBER 0 CARBON SEAL ASSEMBLY IAW RR MM 72-25-25-000-801 AND 72-25-25-400-801. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SEALANT — DAMAGED (WING) · airframe 23,867 hrs · 23,323 cycles

ON FLIGHT 3695 THE CREW REPORTED THAT ON APPROACH, HAD A FUEL SMELL IN THE COCKPIT. THE AIRCRAFT WAS REMOVED FROM SERVICE. RESEALED BOLT AT FRONT SPAR JUST INBOARD OF RIB 1 LEFT CENTER TANK. REFERENCE EMB 145 SRM 51-20-01. LEAK CHECK GOOD IAW AMM 28-11-00. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,320 hrs · 22,407 cycles

DURING PS-1 INSPECTION FOUND LEFT EMERGENCY EXIT WALL MARKER INOPERABLE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED EXIT WALL MARKER LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD IAW EMB AMM 33-50-14. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL MODULE — ODOR (GALLEY LIGHTS) · airframe 22,163 hrs · 21,857 cycles

ON FLIGHT 4152, CREW REPORTED BURNING ODOR COMING FROM THE GALLEY IN FLIGHT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED CONTROL MODULE ASSY IAW AMM 33-21-01. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (BRAKE) · airframe 21,790 hrs · 21,490 cycles

ON FLIGHT 4345, CREW REPORTED AFTER LANDING UPON GEAR EXTENSION THEY GOT 2 EICAS MESSAGES 1 FOR INBOARD BRAKES INOP AND 1 FOR OUTBOARD BRAKES INOPERATIVE. THEY RECYCLED GEAR WITH NO HELP. DECLARED EMERGENCY AND LANDED USING THRUST REVERSERS BRAKES APPEARED TO WORK NORMALLY. AIRCRAFT TAXIED TO GATE SAFELY WITH NO FURTHER INCIDENT. CREW INSPECTION SHOWED NO APPARENT PHYSICAL DEFECTS. REMOVED AND REPLACED BRAKE CONTROL UNIT. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (BRAKE SYSTEM) · airframe 21,790 hrs · 21,490 cycles

ON FLIGHT 4345, CREW REPORTED UPON GEAR EXTENSION THEY RECEIVED 2 EICAS MESSAGES 1 FOR INBD BRAKES INOPERATIVE AND 1 FOR OTBD BRAKES INOPERATIVE. THEY RECYCLED GEAR WITH NO HELP. CREW DECLARED EMERGENCY AND LANDED USING THRUST REVERSERS. BRAKES APPEARED TO WORK NORMALLY. ACFT TAXIED TO GATE SAFELY WITH NO FURTHER INCIDENTS. CREW INSP SHOWED NO APPARENT PHYSICAL DEFECTS. REMOVED AND REPLACED BRAKE CONTROL UNIT. OPS CHECK GOOD. ACFT RETURNED TO SERVICE.

Part: FADEC — UNKNOWN (ENGINE) · airframe 20,435 hrs · 20,218 cycles

ON FLIGHT 3936 DURING DESCENT CREW REPORTED AT FL190 AIR SPEED 290KTS IT EXPERIENCED A LIGHTNING STRIKE. SHORTLY AFTER ENGINE 1 ITT BEGAN TO RISE UP INTO THE RED. ALL OTHER ENGINE INDICATION READINGS NORMAL. PERFORMED PRECAUTIONARY SHUTDOWN OF ENGINE 1. DECLARED EMERGENCY. LANDED IN ORD WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. COMPLETED LIGHTNING STRIKE INSPECTION AND REMOVED AND REPLACED BOTH FADECS PER ROLLS ROYCE SUGGESTION. NO ENGINE PROBLEMS FOUND. AIRCRAFT RETURNED TO SERVICE.

Part: INU — MALFUNCTIONED (NR 1)

RMU 1 NAV 1 FREQUENCY WINDOW DASHES ONLY FREQUENCY NOT SELECTABLE. REMOVED AND REPLACED NR 1 INERTIAL NAVIGATION UNIT IAW EMB MM 34-32-01. OPS CHECK GOOD, AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 19,171 hrs · 18,962 cycles

DURING MAINTENANCE, FOUND RIGHT FRAME 4 BENT AND SKIN CRACKED. REPAIRED BY REPLACING FRAME AND SKIN IAW EMB SRM 51-40-02. A/C WAS RETURNED TO SERVICE.

Part: SEAL — FAILED (COCKPIT WINDOW) · airframe 19,075 hrs · 18,874 cycles

AFTER TAKEOFF CAPTS COCKPIT WINDOW SEAL BLEW OUT IN FLIGHT.

Part: SEAL — FAILED (COCKPIT WINDOW) · airframe 19,075 hrs · 18,874 cycles

AFTER TAKEOFF CAPTS COCKPIT WINDOW SEAL BLEW OUT IN FLIGHT.

Part: LIGHT — INOPERATIVE (CABIN)

FOUND OVERHEAD EXIT IDENTIFIER FOR SERVICE AND MAIN ENTRY DOOR DOES NOT ILLUMINATE. REPLACED OVERHEAD EXIT IDENTIFIER AT ROW 1A. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BALLAST — FAULTY (CABIN)

ELECTRICAL TYPE ODOR IN ROWS 6 AND 7. REPLACED CEILING LIGHT BALLAST OVER SEAT 6A IAW EMB 145 AMM 33-21-05. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: A/C PACK — FOD (NR 1)

ORD - FLT 4095 - CREW NOTED A STRONG BURNING RUBBER SMELL. SMOKE DETECTOR LIGHT ILLUMINATED WITH NO VISIBLE SMOKE. FOUND FOD INSIDE THE PACK ONE NACA INLET (RUBBER). REMOVED RUBBER AND PERFORMED OPERATIONAL CHECK OF THE ACM WITH NO DISCREPANCIES NOTED. PERFORMED FUNCTIONAL CHECK FLIGHT WITH NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. (M)

Part: WIRE HARNESS — CHAFED (NR 2 ENGINE)

ORD - FLT 4136 - CREW REPORTED A FLAME OUT IN SMOOTH AIR LEVEL AT FL280 JUST AFTER LEVEL OFF. THRUST LEVERS HAD NOT BEEN MOVED FROM THRUST SET POSITION IN CLIMB MODE. LOSS N1, N2, AND ITT. IGNITION A/B CAME ON ABOUT 30 SECONDS BETWEEN EVENTS. NO PRECIPATATION REPORTED. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE EXTERNAL CONTROL B HARNESS IAW EMB MM. AN FCF WAS PERFORMED WITH NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: PRESSURE SWITCH — FAILED (RUDDER)

DFW - FLT 3764 - AUTOPILOT FAIL RUDDER SYSTEM 1-2 INOPERATIVE. ALSO, RAI NR 2 RUDDER PRESSURE SWITCH PERFORMED OPERATIONAL CHECK ON RUDDER SYSTEM AND AUTO PILOT SYSTEM IAW EMB 145 AMM 27-22-00 AND 22-11-00. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

MAINTENANCE REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHTING STRIP BETWEEN SEAT 12A AND 13A INOPERATIVE. MAINTENANCE REPLACED THE LIGHT STRIP AT ROW 12 AND 13. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: CONTROL UNIT — MALFUNCTIONED (E/E BAY)

HOU - FLT 3926 - AFTER TAKEOFF CREW RECEIVED LANDING GEAR AIR/GROUND FAIL MESSAGE. AIRCRAFT RETURNED TO FIELD AND AN EMERGENCY WAS DECLARED. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

FOUND FRAME 65 SHEAR TIE CORRODED. REMOVED CORROSION BY CUT OUT. FABRICATED A REPLACEMENT SPLICE. REPAIR DONE IAW SRM.

Part: FRAME — DAMAGED (FUSELAGE)

FOUND NUMEROUS UNDOCUMENTED BLENDED AREAS ON FORWARD DIGITAL. REMOVED BLENDED AREAS BY CUT OUT. FABRICATED A REPLACEMENT STRAP ALSO FABRICATED TWO DOUBLERS AND SHIMS. REPAIR DONE IAW SRM.

Part: BEAM — CORRODED (DOOR FRAME)

FOUND CARGO DOOR CUTOUT LOWER SILL BEAM CORRODED. REMOVED CORRODED SILL (BEAM). INSTALLED NEW BEAM IAW SRM. (B8349)

Part: CHANNEL — CORRODED (FUSELAGE)

FOUND CORROSION ON RT HAT CHANNEL AT FRAME 20. REMOVED CORROSION BY CUT OUT. FABRICATED A CHANNEL REPAIR DOUBLER AND FILLER. REPAIR DONE IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE)

FOUND CORROSION ON GALLEY CENTER FLOORBEAM AT FRAME 20. REMOVED CORROSION BY CUTOUT. FABRICATED A REPAIR DOUBLER AND FILLER. REPAIR DONE IAW SRM.

Part: FRAME — DENTED (FUSELAGE)

FOUND FRAME 72 DENTED AT STRINGERS 14 RT AND 16 RT IN CARGO COMPARTMENT. RECONTOURED DENT. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW SRM. (B8349)

Part: FRAME — DENTED (FUSELAGE)

FOUND FRAME 71 DENTED AT STRINGER 16R IN CARGO COMPARTMENT. RECONTOURED DENT. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW SRM. (B8349)

Part: FRAME — DENTED (FUSELAGE)

FOUND FRAME 72 DENTED AT STRINGERS 14 LT AND 15 LT IN CARGO COMPARTMENT. RECONTOURED DENT. FABRICATED A REPAIR DOUBLER USING CHANNEL FRAME. REPAIR DONE IAW SRM. (B8349)

Part: STRINGER — CHAFED (FUSELAGE)

FOUND STRINGER 19L CHAFED. BLENDED CHAFE, FABRICATED AND INSTALLED TWO DOUBLER ANGLES IAW EMB GST-2182/02, AEA ETN-51--020. (M)

Part: STRINGER — CHAFED (FUSELAGE)

ABI - FOUND STRINGER 19R CHAFED. BLENDED CHAFED, FABRICATED AND INSTALLED A DOUBLER ANGLE, IAW EMB 145 SRM 145/1142, CHAPTER 53, REV 18 53-24-02, AEA ETN-51-020. (M)

Part: BEAM — DAMAGED (FUSELAGE)

FOUND UNDOCUMENTED BLENDED AREAS ON LEFT OMEGA BEAM (PREVIOUS REPAIR) AT FRAME 20. REMOVED PREVIOUS REPAIR AND FABRICATED A DOUBLER, FILLER, PLATE AND TWO SHIMS. REPAIR DONE IAW SRM. (B8349)

Part: SILL — DAMAGED (DOOR FRAME)

FOUND NUMEROUS UNDOCUMENTED BLENDED AREAS ON SERVICE DOOR CENTER SILL. FILLED BLENDED AREAS WITH EPOXY RESIN, SANDED AREA SMOOTH. FABRICATED REPAIR DOUBLER. REPAIR DONE IAW SRM.

Part: WINDSHIELD — CORRODED (PILOT WINDSHIELD)

FOUND PILOT WINDSHIELD CUTOUT LOWER STRIP HAS 6 CORRODED HOLES. REMOVED CORROSION BY REAMING HOLES 2 AND 4 TO ALLOWABLE LIMITS. REAMED HOLES 1 AND 4 TO .313 TO REMOVE CORROSION. FABRICATED TO FREEZE PLUGS. REPAIR DONE IAW SRM. (B8349)

Part: SKIN — DENTED (FUSELAGE)

ABI - DURING MBV INSPECTION, FOUND A DENT 5.5 INCH AFT OF FRAME 19 BELOW STRINGERS 15L. PERFORMED EDDY CURRENT INSPECTION AND THICKNESS TEST AND FOUND NO DEFECTS. (M)

Part: SKIN — DENTED (FUSELAGE)

ABI - DURING MBV MAINTENANCE, FOUND DENT 3 INCHES FORWARD OF FRAME 20, BELOW STRINGERS 15L. PERFORMED EDDY CURRENT AND THICKNESS CHECK AND FOUND NO DEFECT. DENT TREATED FOR CORROSION AND ACCEPTED AS IS IAW EMB GST-2182/02. (M)

Part: SKIN — DENTED (FUSELAGE)

ABI - DURING MBV MAINTENANCE, FOUND A DENT 3 INCH AFT OF FRAME 20, BELOW STRINGER 11L. PERFORMED EDDY CURRENT INSPECTION AND FOUND NO DEFECTS. DENT ACCEPTED AS IS IAW EMB GST-2182/02, SURFACE PROTECTION APPLIED. (M)

Part: SKIN — DENTED (FUSELAGE)

ABI - DURING MBV INSPECTION MAINTENANCE FOUND A DENT 4 INCHES FORWARD OF FRAME 20 BELOW STRINGER 15L. PERFORMED EDDY CURRENT INSPECTION AND THICKNESS TEST AND FOUND NO DEFECTS. (M)

Part: SKIN — DENTED (FUSELAGE)

ABI - DURING MBV INSPECTION, MAINTENANCE FOUND A DENT BETWEEN FRAMES 17 AND 18 AND STRINGER 21-20L. PERFORMED EDDY CURRENT INSPECTION AND FOUND NO DEFECTS. DENT FOUND TO BE WITHIN EMB145 SRM 53-21-10, TABLE 102 LIMITS. (M)

Part: SKIN — DENTED (FUSELAGE)

ABI - DURING MBV INSPECTION MAINTENANCE FOUND A DENT 8 INCH AFT OF FRAME 20, BELOW STRINGER 11L. PERFORMED EDDY CURRENT INSPECTION AND FOUND NO DEFECTS. DENT ACCEPTED AS IS IAW EMB GST-2182/02, SURFACE PROTECTION RESTORED. (M)

Part: UNKNOWN — ODOR (COCKPIT)

IND - FLT 4079 - WHEN CREW SELECTED APU BLEED AS BLEED SOURCE, THERE WAS A DEFINITE ODOR AND SMOKE IN CABIN. LAV SMOKE DETECTOR ACTIVATED. APU WAS MEL. 050-125D 49-2. FOUND APU OIL OVERSERVICED. DRAINED TO PROPER LEVEL. OPS CHECK GOOD. (X)

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY)

CLE - FLT 4337 - BAGGAGE SMOKE LIGHT CAME ON IN FLIGHT. DISCHARGED BOTH FIRE BOTTLES AND DECLARED AN EMERGENCY. AIRCRAFT HAD NORMAL LANDING. INSPECTED CARGO AREA. NO EVIDENCE OF SMOKE OR FIRE DAMAGE. FOUND FORWARD SMOKE DETECTOR FAULTED. REMOVED AND REPLACED FORWARD SMOKE DETECTOR AND BOTH DISCHARGED BOTTLES. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: CONTROLLER — MALFUNCTIONED (COCKPIT)

FLT 4239 - ORD - FLIGHT CREW NOTED ELECTRICAL SMELL ON APPROACH TO ORD. REMOVED AND REPLACED FLIGHT GUIDANCE CONTROLLER. OPS CHECK GOOD. (M)