N689EC
Registered owner: AMERICAN AIRLINES INC, TX (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
E1 HSV FAIL ON EICAS FACT 23MAY26 17:19 GSO. R & R NR 1 HSV IAW AMM 36-11-02. OPS AND LEAK CHECK GOOD.
BIRD STRIKE DURING TAKEOFF. PERFORMED BIRDSTRIKE INSPECTION IAW 05-50-08. CLEANED BIRD REMAINS OFF WINDSHIELD. NO DAMAGE/DEFECTS NOTED. AIRCRAFT OK FOR SERVICE AT THIS TIME
ADC 1 FAILED IN FLIGHT FACT 01FEB26 17:47 ALB R&R'D ADC1 AT POS 100 IAW EMB145 AMM 34-15-01. PERFORMED LEAK CHECK IAW AMM 34-13-00. OPS CHECK DONE IAW AMM 34-15-00, SYSTEM TESTED SERVICEABLE, OK FOR SERVICE.
SMOKE IN CABIN DURING CRUISE AT FL250. INSPECTED PACK SYSTEM, FOUND #200 ACM SIEZED W/ MELTED DUCTS ON #200 DUAL TEMP CONTROL VALVE. R/R'D DUCTS ON #200 DUAL TEMP CONTROL VALVE IRW AMM 21-60-01. R/R'D #200 ACM IRT AMM 21-61-03. OPS AND LEAK CHECK GOOD WITH NO VISIBLE SMOKE IN CABIN.
FA REPORTS RUBBER HOSE SMELL WITH HISSING NOISE IN A ISLE GASPER AREA BETWEEN ROWS 2 AND 8 WITH GASPER FAN RUNNING. FOUND SEAT 8B GASPER TO BE CLOGGED. R/R'D PSU GASPER AIR ASSY IAW MM 25-22-05, OPS CK GOOD.
BIRD STRIKE ON #2 ENGINE. #2 ENG CHANGE. SEE W/C 71-00-00 ON WORK PACKAGE.
REJECTED T/O WITH HSV 2 FAIL DISPLAYED MSG WENT AWAY AFTER THRUST LEVERS PULLED BACK (DEACTIVATED BLEED VLV 2). R&R'D #200 HSV IAW 36-11-02-04 OPS CHECK GOOD NO RELATED EICAS MSGS OR OTHER DEFECTS NOTED AT THIS TIME
E058889 CARGO DOOR LOWER CUTOUT FLOOR SILL CORRODED. RAR CARGO DOOR LOWER CUTOUT FLOOR SILL IAW EMB 145 SRM 51-40-02
E058596 PAX DOOR LWR AFT FLOOR SUPPORT HAS CORROSION AROUND NUT-PLATES HOLES. RAR PAX DOOR LWR AFT FLOOR SUPPORT IAW EMB 145 SRM 51-40-02.
E058611 GALLEY FLOOR CROSSBEAM AT FR-20 BETWEEN STGRS 21L/18L HAS CORROSION. BLENDED OUT CORROSION ON GALLEY FLOOR CROSSBEAM AT FR-20 BETWEEN STGRS 21L/18L IAW EMB145 SRM 51-10-03 AND FOUND REMAINIG THICKNESS TO BE WITHIN ALLOWABLE LIMITS IAW EMB145 SRM 53-21-10AD. RESTORED PROTECTIVE COATING AS REQUIRED.
E058583 PAX DOOR LWR FWD FLOOR SUPPORT HAS CORROSION AROUND NUT-PLATES HOLES. RAR PAX DOOR LWR FWD FLOOR SUPPORT IAW EMB 145 SRM 51-40-02
E058598 SERVICE DOOR LWR CENTER SILL HAS CORROSION AROUND NUT-PLATES HOLES. PREPPED, FABRICATED, AND INSTALLED DOUBLERS ON SERVICE DOOR CENTER SILL IAW EMB 145 SRM 53-21-02RE FIGURE 201 AND EO1-53-24-0604
E058125 RH AILERON DAMPENER ATTACHMENT FITTING IS GOUGED IN MULTIPLE AREAS (ON AILERON). REMOVED AND REPLACED RH AILERON DAMPENER FITTING IAW EMB 145 SRM 51-40-02
E058328 RH HORIZONTAL STAB SPHERICAL BEARING HOUSING PITTED. RPAIRED IAW SRM 55-30-02
E058190 PAX DOOR LWR AFT PROFILES HAS CORROSION AROUND NUTPLATES HOLES. REPAIRED IAW EMB 145 SRM 52-10-04 STEP 3 FIGURE 201 SHEET 3 AND PIEDMONT EO1-52-24-0623.
E056822 RH WING TORQUE BOX 1 LOWER FWD CENTER FASTENER HOLE IS OVERSIZED AND DAMAGED. PREPPED, FABRICATED, AND INSTALLED BUSHINGS AND HILOCK IN RH WING TORQUE BOX 1 LOWER FWD HOLE IAW ETS2024-145-025752 "REV A" AND EO1-57-24-0603
INCORRECT FLIGHT ATTENDANT FLASHLIGHT INSTALLED-C/A-RAR FA FLASHLIGHT WITH CORRECT LED FLASHLIGHT ASSY IAW EMB-145 AMM 33-50-16 AND ETN-EM-33-059. OPC GOOD.
E2 SHUTOFF AT FL240/ SPD 290KTS/ OIL QUANTITY WENT TO RED AT 3 QTS. FLT DECLRD EMERG. LANDED SAFELY-C/A-REMOVED AND REPLACED #2 ENGINE IAW ENGINE REMOVAL AND INSTALLATION EMB 145 WORK CARD 71-000-00 OPERATION AND LEAK CHECK ARE GOOD.
FWD FA EMERGENCY FLASHLIGHT HOLDER ASSEMBLY BROKEN-C/A-FLIGHT CREW PLACARDED FWD FA EMERGENCY FLASHLIGHT HOLDER ASSEMBLY M PROCEDURES C/W REF: MEL 25-32 AUTH: 120159M-C MOC: 056020
CA DECLARED EMERGENCY DUE TO UNRELIABLE AIRSPEED. AMBER IAS ON AIRSPEED INDICATOR FOLLOWED BY SPS ADVANCED EICAS MSG. QRH PROCEDURE C/W. AIRSPEED RETURNED TO NORMAL AND MSG CLEARED IN DESCENT.CAPT DECLARED EMERGENCY DUE TO UNRELIABLE AIRSPEED. -C/A-INTERROGATED CMC AND FOUND NO PERTINENT MESSAGES, FOUND NO WATER IN PITOT DRAINS, PITOT HEAT FUNCTIONS NORMALLY IAW AMM 30-31-00-700-801-A PERFORMED PITOT-STATIC LEAK TEST IAW AMM 34-13-00 OPS CHECK GOOD AIRCRAFT OK FOR SERVICE
FLOOR EMERGENCY LIGHTS, 2 AND 3 INOP. R & R 2 AND 3 FLOOR PROXIMITY EMERGENCY LIGHT STRIPS IAW EMB145 AMM 33-50-12. OPS CHECK GOOD
ROW 12 OVERHEAD EMERGENCY LIGHT INOP-C/A-RAR #6 EMERGENCY DC/AC INVERTER IAW EMB AMM 33-50-11-000-801-A AND 33-50-11-400-801-A. OPC GOOD
SEVENTH EMERGENCY LIGHT STRIP ON LH SIDE FLOOR WIRES DAMAGED, LIGHT INOP-C/A-RAR FLOOR STRIP EMERGENCY LIGHT IAW EMB145 AMM 33-50-12. OPS CHECK GOOD.
SPS 2 INOP WARNING AND SPS ADVANCED CAUTION ON EICAS DURING APPROACH TO LANDING. C/A PERFORMED FIM TASKS 27-36-00. SPS ADVANCED MESSAGE REMAINS, SEE AML 4558647 ITEM 2 FOR CONTINUED DISCREPANCY.
BLEED 1 LEAK IN FLIGHT (DIVERTED BACK TO DFW) NO EMERGENCY DECLARED. -C/A-OPENED PACK 1 TO VERIFY BLEED LEAK TIGHTENED HOSE CLAMPS WAITED FOR EICAS MESSAGE. OPC GOOD IAW AMM 36-00-00/ETN-EM-21-956/21-51-02.
ON DESCENT SPS 2 INOPERABLE WARNING WENT AWAY, BUT CAME RIGHT BACK AS WE RAN THE QRH SPS 1 INOPERABLE AS WELL WE ALSO RECEIVED STICK PUSHER FAIL AND SPS ADVANCED MECH, SPS FAIL. EMERGENCY DECLARED C/A-REF FIM TASK 27-36-00-810-A. PERFORMED RESET OF STALL PROTECTION SYSTEM AND OPERATIONS CHECK IAW E145 AMM 27-36-00. OPERATIONS CHECK GOOD NO MESSAGES NOTED.
SSI 53-30-48; CARGO DOOR SILL IS CORRODED. -C/A-EVALUATED CORROSION ON CARGO DOOR CENTER SILL AND FOUND TO BE OUT OF LIMITS IAW EMB 145 SRM 53-31-15AD. REMOVED AND REPLACED CARGO DOOR CENTER SILL IAW EMB 145 SRM 51-40-02 MATERIALS USED PN: 145-25480-603SD CARGO DOOR CENTER SILL.
SSI 53-30-03; FRAME 68 CARGO DOOR LATERAL L-SHAPE IS CORRODED. -C/A-ACCOMPLISHED PERMANENT REPAIR ON FRAME 68 CARGO DOOR LATERAL L-SHAPE SHEAR CLIP IAW EMB 145 SRM 53-31-04RE ITEM 4D
LH WING RIB 21 IS CRACKED INSIDE PANEL 551CB (AS MARKED).-C/A-REMOVED, FABRICATED AND INSTALLED REPAIR FILLER, DOUBLER, AND SHIM AT LH WING RIB 21 IAW EMB 145 SRM 57-20-07. MATERIAL LIST: FILLER: AL CLAD 2024 T3 OR AL CLAD 2024 T42 OR AL 7475 T7451 OR AL 7475 T761 OR AL 7075 T6 - 1.0 MM (0.040 IN) DOUBLER: AL 7475 T761 OR AL 7075 T6 - 1.3 MM (0.050 IN) SHIM: AL CLAD 2024 T3 OR AL CLAD 2024 T42
CARGO DOOR INTERNAL WEB STRUCTURE GOUGED. REPAIRED CARGO DOOR INNER WEB IAW SRM 52-30-01.
LH UPPER AFT FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 AND ABOVE STRINGER 2L, CRACK IS APPROX. 3/8? LONG ENDS ARE MARKED.-C/A-FABRICATED AND INSTALLED A REPAIR DOUBLER, FILLER, REPAIR ANGLE AND SHIM IAW EMB 145 SRM 53-31-01. MATERIALS USED: REPAIR DOUBLER ? ALCLAD 2024 ? T3 (0.080), REPAIR FILLER ? ALCLAD 2024 T3 (0.063), REPAIR ANGLE ? ALCLAD 2024 T3 (0.050), SOLID SHIM ? ALCLAD 2024 T3 (0.032).
2 PREVIOUSLY INSTALLED DOUBLERS ON CARGO DOOR LOWER WEB SECTION GOUGED. -C/A-REMOVED, FABRICATED AND INSTALLED DOUBLERS FOR CARGO DOOR INNER LOWER WEB IAW EMB 145 SRM 52-30-01 ITEM 12. MATERIAL FOR DOUBLERS: AL 7475-T761 (.040).
CARGO DOOR LOWER FRAME CORRODED AT SCREW HOLE. REMOVED AND REPLACED THE CARGO DOOR LOWER FRAME IAW SRM 51-40-02.
CENTER OMEGA BEAM AT FR 24-25 IS CORRODED. -C/A-BLENDED OUT CORROSION ON CENTER OMEGA BEAM AT FR 24-25 IAW SRM 51-10-03 AND CPM 51-14-02. REMAINING THICKNESS FOUND TO BE BEYOND LIMITS IAW SRM 53-22-10. FABRICATED AND INSTALLED A DOUBLER FOR REPAIR OF CENTER OMEGA BEAM AT FR 24-25 IAW SRM 53-22-10 ITEM 4 FIG 203 SHEET 2.
FRAME 65 IS CORRODED ABOVE CARGO DOOR SILL.-C/A-REMOVED AND REPLACED FR 65 SECTION AT CARGO DOOR CUTOUT IAW EMB 145 SRM 51-40-02. REPLACEMENT PN: 145-64106-001 FR 65 SECTION, PN: 145-03301-003 STR 16L SUPPORT (SHEAR CL
FRAME 65 CARGO DOOR SHEAR TIE WAS CORRODED. REMOVED AND REPLACED FR 65 CARGO DOOR SHEAR TIE IAW SRM 51-40-02.
DURING HMBV INSPECTION, FR 73 CRACKED BETWEEN STR 15R-16R-C/A-RAR FR 73 LOWER SECTION TO REPAIR CRACK BETWEEN STR 15R-16R IAW EMB 145 SRM 51-40-02
RH AILERON PCA FITTING HAS ELONGATED BUSHING HOLES-C/A-RAR RH AILERON PCA FITTING IAW EO-EM-27MR-112
LAV BUCKET CORRODED AROUND SERVICING NIPPLE AND DRAIN HANDLE-C/A-RAR LAV BUCKET IAW EMB 145 SRM 51-40-02 AND 51-20-03
DURING HMBV INSPECTION, QA FOUND THE LH OMEGA BEAM AT FR 24-25 CORRODED-C/A-ACCOMPLISHED PERMANENT REPAIR ON LH OMEGA BEAM AT FR 24-25 IAW ERS-EM-53MR-4163. REPAIR MATERIAL; DOUBLER- 2024T3-.063?
LT FLOOR SILL HAS CORROSION AT FR32, AS MARKED. C/A COMPLETE: BLENDED AND FOUND AREAS AT LT FLOOR SILL AT FR 32 TO BE OUT OF LIMITS, IAW EMB 145 SRM 51-10-03 AND 53-22-10. R&R LT OUTBOARD SILL NR 3, IAW EMB 145 SRM 51-40-02.
STD REQ A110 OPS A. REPLACE EPSU CRJ WC 33-002 OR EMB WC 33-700-19 PN: 11-0049 SN: 18369 POS: 2. C/A COMPLETE: PCW BY RECORDS REVIEW AND DVI OF EQUIPMENT INSTALLED ON AIRCRAFT, REF CITRIX (MTX OPS) NRWC 689-DFW-04797 DATED: 07/19/20. FOR R&R OF POS NR 2 EMERGENCY LIGHTING BATTERY ASSY PN: 2013-1A SN: 68423 AND BATTERY CHARGER PN: 11-0049 SN: 18369.
EMERGENCY FLASHLIGHT CRADLE ON LAV WALL IS BROKEN. C/A COMPLETE: R & R EMERGENCY FLASHLIGHT CRADLE ON LAV WALL, IAW EMB 145 AMM 33-50-16. OPS CHECK GOOD.
RT FLOOR SILL HAS CORROSION AT FR 31, AS MARKED. C/A COMPLETE: FOUND CORROSION ON RT FLOOR SILL AT FR 31 TO BE OUT OF LIMITS, IAW EMB 145SRM 53-22-10. R & R CABIN RT NR 2 FLOOR SILL, IAW EMB 145 SRM 51-40-02.
EMERGENCY LIGHT ON CEILING PANEL AT 7A INOP. C/A COMPLETE: REMOVED AND REPLACED BULB ON CEILING PANEL 7A, IAW EMB 145 AMM 33-50-08. CHECKS GOOD.
EMERGENCY LIGHT STRIP NR 6 HAS BROKEN CONNECTOR. C/A COMPLETE: REMOVED AND REPLACED EMERGENCY LIGHT STRIP NR 6 BROKEN CONNECTOR, IAW EMB 145 SWPM 20-21-00.
DURING PS-1 INSP FOUND EMERGENCY LIGHTS AT SERVICE DOOR AND RH WING TO FUSELAGE FAIRING INOP.-C/A-RAR #2 EMERGENCY BATTERY AND CHARGER ASSY IAW E145 AMM 33-50-04. OPERATIONAL CHECK GOOD
SUPPLEMENTAL MAIN DOOR (ENTRANCE CEILING) EMERG LIGHT INOP. CONTINUITY TO GROUND WHEN CONNECTOR P8500 (BATTERY CRADLE) DISCONNECTED AND POSITIVE WIRE AT BULB (W766-8052-20) BOTH WIRES AT BULB DISCONNECTED. NEW CRADLE NEEDED. (WHEN A NEW CRADLE INSTALLED BULB LIT FOR A MOMENT THEN NOT AGAIN)-C/A-AIRCRAFT RESTORED TO ORIGINAL CONDITION-AT TIME OF DISCOVERY OF INOP. EMERG LIGHT. MTX ACCOMPLISHED IAW EMB-145 AMM 33-50-04; AND 33-50-06. TIGHTENED PAX DOOR EMERGENCY LIGHT BACKSHELL AS REQUIRED AND REMOVED AND REPLACED #1 EMERGENCY BATTERY AND CHARGER IAW AMM 33-50-04. OPC GOOD.
#4 EMERGENCY LIGHT BATTERY HAS A BROKEN CAM LOCK.-C/A-REPLACED #4 EMERGENCY LIGHT BATTERY IAW AMM 33-50-04. OPS GOOD
UPPON ARRIVING TO THE AIRCRAFT I NOTICED THE SPEED BRAKE CB (IB) WAS POPPED OUT-C/A-FOUND SPEED BRAKE PROXIMITY SENSOR BURNT AND REMOVED AND REPLACED SENSOR IAW AMM 27-63-04 AND RAR ELECTRICAL CONNECTOR TO PROXIMITY SENSOR IAW SWPM 20-50-00. OPS CHK GOOD.
SERVICE DOOR LIGHT INOP-C/A-REPAIRED SERVICE DOOR EMERGENCY LIGHT WIRE SP3676 IAW EMB145 SWPM 20-21-00 OPC GOOD
MAIN DOOR EXTERIOR EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED MAIN DOOR EXTERIOR LIGHT IAW AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPC GOOD. NO FURTHER DEFECTS NOTED. END.
MEL 7802 - AUTH# 11-32M-C REPAIR REPAIR POSITION E2 ENG 1/2 REVERSE DISAGREE MESSAGES.E2 REV DISAGREE ON TAKEOFF ROLL ABORTED TAKEOFF PLACARDED BY: MTXID: 227446 LOGPAGE: 4541131 ITEM: 1 RESTORATION OF MEL ITEMS REVIEW THE MEL AND ENSURE APPROPRIATE MAINTENANCE ACTIONS ARE TAKEN TO RESTORE THE ITEM/SYSTEM CONDITIONS AND LIMITATIONS THAT WERE REQUIRED BY THE MEL DURING DEFERRAL.COMPLY WITH PROCEDURES IN MEL MANUAL 1-06 INCLUDING NOTIFICATION TO MOC. ENTER FACT INFORMATION INTO SABRE FMR RECORD PER GPM 04-00 AND 16-00 PERFORMED CMC DOWNLOAD IAW W/C 45-900-00 SENT TO TRENDS MEL REMAINS OPEN KVA UPDATED M PROCEDURES STILL COMPLIED WITH
SUPPLEMENTAL ENG 2 REV DISAGREE. CAUTION JUST ABOVE 80 KNOTS. ON TAKEOFF ROLL AND NO TAKEOFF CONFIG. MASTER WARNING RIGHT AFTER.-C/A-DEFERRED ENG-2 TRUST REVERSER PER MEL 78-2, AUTH# 110032-M-C. M PROCEDURES C/W. PER AMM 05-50-16, NO INSPECTION REQUIRED. NO BRAKE OVERHEAT NOTED, NO EVIDENCE OF WHEEL FUSE PLUG RELEASE. NO FURTHER DEFECTS NOTED. PERFORMED CMC DOWNLOAD IAW W/C 45-900-00 SENT TO TRENDS MEL REMAINS OPEN KVA UPDATED M PROCEDURES STILL COMPLIED WITH. T/S E2 TR REV DISAGREE IAW FIM TASK 78-34-00-810-802-1-A. FOUND E2 TR LOW STOW SWITCH WORN. REMOVED AND REPLACED STOW SWITCH REF EMB 145 AMM 78-34-01. OPS CHECK GOOD. MEL AND MPROCEDURES RESTORED.
RH EXIT ROW AFT EMERGENCY MARKER DID NOT ILLUMINATE.-C/A-REMOVED AND REPLACED #5 EMERGENCY LIGHT AC/DC INVERTER IAW EMB AMM 33-50-11 WITH WM 33-50-50. OPC OF EMERGENCY LIGHTING SYSTEM GOOD IAW EMB AMM 33-50-00-700-801-A. NO OTHER DEFECTS NOTED.
GOUGE AT FRAME 19A AND BETWEEN STRINGERS 20R AND 21R. DEPTH AT .012". 3" LONG AND 2" WIDE."MAJOR REPAIR". C/A-REPAIRED IAW ERS-EM53MR-3838.
UPPER EMERGENCY EXIT SIGN BY RT OVER WING EXIT INOP. C/A-REMOVED AND REPLACED RH UPPER EMERGENCY EXIT SIGN IAW AMM 33-50-14. OPS CHECK GOOD
FA FLASHLIGHT HOLDER NOT HOLDING FLASHLIGHT PROPERLY.-C/A-REMOVED AND REPLACED FWD CABIN FLASHLIGHT HOLDER ASSY IAW EMB145 AMM 33-50-16. OPS CHECK GOOD.
SUPPLEMENTAL PACKS SMELL DIRTY, ENGINE BLEEDS SUPPLYING AIR ON TAXI + APU SUPPLYING AIR AT GATE STILL SMELLED UNDER THOSE CONDITIONS. "TRANSFERRED TO NRWC 689-ORD-03890"-C/A-C/W ETN# ETN-EM-72-034, DEFERRED PACK 1. T/S PACK 1 DIRTY SMELL PER FIM 21-20-00-810-801-A TO STEP 36, INSPECTED #1 RECIRCULATION SYSTEM FOUND NO DEFECTS NOTED IAW EMB AMM 21-24-02 REQUIRES FURTHER T/S MEL REMAINS OPEN. REMOVED AND REPLACED PACK VALVE #1 FILTER, OPC LEAK CHECK GOOD, IAW EMB AMM 21-51-01 RAN PACK FOR 2+ HOURS WITH NO SMELL NOTED. MEL RESTORED
OVER SERVICE DOOR EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED #2 EMERGENCY LIGHT INVERTER OVER SERVICE DOOR EMERGENCY LIGHT OPC GOOD. BATTERY CHARGER ASSY P/N 11-0049 S/N 19322
TRANS FROM NRWC 689-SGF-03814 AFT GALLEY LIGHT , EXT SERVICE DOOR DC LIGHT AND #2 , #3 FLOOR EMERGENCY LIGHTS INOP-C/A-FOUND WIRE GOING TO EXT SERVICE DOOR EMERGENCY LIGHT BROKEN AND SHORTED OUT. REPAIRED HARNESS WIRE IAW EMB SWPM 20-21-00 OPS CHECK BAD REF NRWC 689-SGF-03819 #2
ENG & STAB ANTI-ICE CAME ON AFTER TAKEOFF FOLLOWED QRH PROCEDURE PER NO ICE - AICE ON EICAS MSG RETURNED TO AVP. SWITCH WAS IN AUTO POSITION. ENG REF A/ICE. C/A-REMOVED & REPLACED ANTI-ICE PANEL MODULE IAW EMB 145 20-13-10 OPS CK'D BAD SEE ITEM NR 2 FOR CONTINUATION.
SERVICE DOOR EMERGENCY LIGHT INOP. C/A-REMOVED AND REPLACED SERVICE DOOR EXTERNAL EMERGENCY LAMP IAW AMM 33-50-10-000-801-A/33-50-10-400-801-A OPC GOOD.
SERVICE DOOR EMERGENCY LIGHT INOP-C/A-RAR SERVICE DOOR EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-09-000-801-A & 33-50-09-400-801-A OPS CHECK GOOD AT THIS TIME NO FURTHER DEFECTS NOTED END
"TRANSFERRED FROM AML PAGE 4348971 ITEM 2" REF THIS LOG PAGE ITEM1 RIGHT AFT FUSELAGE BELOW ENG 2 DAMAGED AND INTERNAL STRINGER DAMAGED "MAJOR REPAIR"-C/A-PERFORMED PERMANENT REPAIR IAW ERS-EM-53MR-3485
CARGO DOOR INDICATED OPEN DURING CLIMBOUT. REMOVED DEBRIS FROM AFT CARGO DOOR SWITCH, OPS CHECKED GOOD IAW AMM 52-76-01.
ANTI-ICE DISAGREE CAUTION MESSAGE PRESENTED ON EICAS ONCE ADVANCING THRUST LEVER FOR TAKE OFF. PERFORMED A LOW SPEED ABORT OF TAKE OFF. CHECKED CONNECTOR PLUGS AT NR 1 AND 2 ENGINE ANTI ICE VALVES FOR SECURITY. RESET THE FADEC CIRCUIT BREAKERS, GROUND RAN, OPS CHECKED GOOD IAW AMM 30-00-00, NO CURRENT RELATED FAULTS ON CMC.
LEFT EXTERNAL FWD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW AMM 33-50-10-000-801-A, AND 33-50-10-400-801-A.. OPS CHECKED GOOD.
LEFT OVERWING EMERGENCY EXIT SIGN INOPERATIVE. FOUND THE ELECTRICAL CONNECTOR DISCONNECTED. CONNECTED AND SECURED THE CONNECTOR IAW AMM 33-50-14. OPS CHECKED OK.
CEILING AISLE EMERGENCY LIGHT NR 4 INOPERATIVE. REMOVED AND REPLACED THE BULB IAW AMM 33-50-08. OPS CHECKED OK.
CORROSION IN GALLEY AREA ON THE RT BEAM. REPAIRED THE BEAM IAW SRM 53-21-10, ITEM 6, FIG 205, SHEET 1.
CORROSION ON SERVICE DOOR CENTER SILL. REPAIRED SERVICE DOOR CENTER SILL AREA WITH REMAINING THICKNESS OF .045" BY INSTALLING AN INTERNAL DOUBLER IAW SRM 53-21-02.
LEFT PYLON FWD YOKE LOWER FWD FITTING CRACKED. REMOVED AND REPLACED THE YOKE FITTING IAW EO EM-54MR-386.
ON A PS-2 CHECK, FOUND MULTIPLE EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHTS BATTERY PACK NR 1 IAW AMM 33-50-04. OPS CHECKED GOOD.
FLAP FAIL, TROUBLE SHOT SYSTEM FOUND FLAP ECU TO BE BAD. REMOVED AND REPLACED FLAP ECU PERFORMED OPS CHECK IAW AMM 27-53-00 OPS CHECKS GOOD AIRCRAFT OK FOR SERVICE.
FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED THE FLASHLIGHT IAW AMM 33-50-16. OPS CHECKED GOOD. NO FURTHER DEFECTS NOTED.
SMOKE & FUMES IN THE COCKPIT AND CABIN, IN FLIGHT. IAW FIM TASK 21-20-00-810-801-A, FOUND THE RECIRCULATION FAN INOPERATIVE. REMOVED AND REPLACED THE RECIRCULATION FAN IAW AMM 21-24-01. OPS CHECKED GOOD. NO DEFECTS NOTED. PERFORMED ETN-EM-72-034, OPS CHECKED GOOD, NO DEFECTS NOTED. ON FURTHER INVESTIGATION, FOUND THAT WHEN OPERATING THE NR 2 PACK OFF, APU BLEED SMOKE AND BURNING ODOR ENTERED THE CABIN. REMOVED AND REPLACED THE RT ACM IAW AMM 21-51-03.
LAVATORY SMOKE MASTER ALARM AT GATE. SOUNDED IN ERROR, NO SMOKE. COMPLIED WITH SMOKE DETECTOR OPS CHECK IAW 26-14-00. OPS CHECKED GOOD
ABORTED TAKE OFF DUE TO SPS ADVANCED CAUTION EICAS MESSAGE AT 70 KTS. ON POST FLIGHT FOUND BUG JAMMED IN PITOT TUBE 1. PERFORMED GVI OF PITOT 1 PROBE & REMOVED REMAINS OF WASP.
F/A TRIED TO USE THE FWD FLASHLIGHT ON ARRIVAL AND WOULD NOT COME ON. REMOVED AND REPLACED FLASHLIGHT, OPS CHECK IAW STANDARD MAINT PRACTICES, OPS CHECKED GOOD
AFTER POWER UP, THE NR 2 RMU FAILED, ACCOMPANIED WITH ELECTRICAL BURNING ODOR. R & R THE NR 2 RMU. CONFIRMED THE BURNING ELECTRICAL ODOR COMING FROM RMU IAW AMM 23-81-01-000-801/23-81-01-400-801. OPS CHECKED GOOD.
WHILE PERFORMING PS-1 CHECK, FOUND MID-SECTION FWD CEILING EMERGENCY EXIT LIGHT INOPERATIVE. R & R EMERGENCY EXIT SIGN IAW AMM 33-59-15. OPS CHECK GOOD.
MAIN CABIN DOOR HARD TO OPERATE. LUBED MAIN CABIN DOOR ROLLERS IAW AMM 53-21-02. OPERATIONS CHECKED GOOD.
EMERGENCY EXIT SIGN ON LT CEILING LOOSE. SECURED EMER EXIT SIGN ON LT CEILING AS REQUIRED.
RIGHT REAR FUSELAGE I SKIN HAS 2 CRACKS AT FRAME 75, BETWEEN STRINGERS 1R & 2R. PERFORMED PERMANENT REPAIR OF RT REAR FUSELAGE I SKIN IAW ERS-EM-53MR-1831.
NUMBER 2 EMER LIGHT WIRE BROKEN UNDER FLOOR. REPAIRED NR 2 FLOOR PROXIMITY LIGHT WIRES IAW SWPM 20-21-00. FOUND DURING OPEN UP.
RIGHT UPPER AFT FUSELAGE SKIN HAS 2 CRACKS. CRACK 1 IS JUST AFT OF FRAME 75 & ABOVE STRINGER 2R, APPROX 1/4" LONG. CRACK 2 IS ON FRAME 75 AT THE FIRST FASTENER ABOVE STRINGER 2R, APPROX 3/8" LONG. EASI 8071 USED, 100-500 KHZ PROBE, FREQ=400 KHZ, V-GAIN=77.0, H-GAIN=64.0, LPF=100. PERFORMED REPAIR OF RT UPPER AFT FUSELAGE SKIN IAW ERS-EM-53MR-1831. SEE TURNOVER FOR FURTHER DETAILS.
NUMBER 4 EMER LIGHT STRIP, PLANESIDE, TERMINAL END MISSING. REPAIRED SP9110 ON NR 4 EMER LIGHT STRIP, PLANESIDE, TERMINAL END IAW SWPM20-21-00-00.
NUMBER 1 & 7 EMER FLOOR PROXIMITY LIGHT STRIPS HAVE BROKEN WIRES. UPON FURTHER INVESTIGATION FOUND NR 1 ONLY EMER FLOOR PROXIMITY LIGHT STRIP HAS BROKEN WIRES. REPLACED NR 1 LIGHT STRIP SEE BOW 207107 FOR INSTALL & OPERATIONS.
RIGHT LAVATORY FLOORBEAM CRACKED AT FWD NUTPLATE HOLE. PERFORMED CUT OUT AS REQUIRED TO REMOVE DAMAGE FROM RT LAVATORY FLOORBEAM AT FWD NUTPLATE HOLE IAW SRM 51-30-01. FABRICATED & INSTALLED DOUBLER TO REPAIR RT LAVATORY FLOORBEAM AT FWD NUTPLATE HOLE IAW ERS-EM-53MR-1836.
EMERGENCY FLOOR PROXIMITY LIGHT STRIP NR 2 IS INOPERATIVE. R & R EMER FLOOR PROXIMITY LIGHT STRIP NR 2 IAW AMM 33-50-12. OPERATIONAL TESTED GOOD.
EMERGENCY FLOOR PROXIMITY LIGHT STRIP NR 4 IS INOPERATIVE. R & R EMER FLOOR PROXIMITY LIGHT STRIP NR 4 IAW AMM 33-50-12. OPERATIONAL TESTED GOOD.
NUMBER 2 EMER LIGHT WIRE BROKE UNDER FLOOR. REPAIRED BROKEN WIRE ON NR 2 EMER LIGHT FLOOR WIRE W1928681-22 IAW SWPM 20-21-00 & SWPM 20-50-01. CRIMPER SN 6571, TURRET SN 7859, SEE NRTC BOW 207107 FOR INSTALLATION & OPERATIONS CHECK.
NUMBER 1 - 4 FLOOR STRIPS BROKEN ON RT SIDE OF CTR AISLE. R & R THE CTR AISLE NR 1 - 4 RT SIDEWALL STRIPS IAW AMM 33-50-12.
LEFT NR 1 FLOOR SUPPORT CORRODED ON PREVIOUS BLEND AT FRAME 22. R & R LT NR 1 FLOOR SUPPORT AT FRAME 22. REINSTALLED CROSSBEAM AT FWD PART IAW SRM 51-40-02.
CROSSBEAM AT FRAME 20 CORRODED ON PREVIOUS BLENDS. REMOVED & INSTALLED NEW CROSSBEAM AT FRAME 20 IAW SRM 51-40-02.
ON CLIMB SPS 2 INOPERATIVE WARNING MSG & SPS ADVANCED CAUTION MSG ON EICAS. R & R RT AOA SENSOR IAW AMM 27-36-01. OPERATIONS CHECKED GOOD.
PTRIM MAIN INOPERATIVE, AUTO TRIM FAIL, AUTO PILOT ELEVATOR PTRIM FAIL & AUTO PILOT FAILED. TRANSFERRED TO NRWC 689-DFW-02223. R & R HSA IAW AMM 27-40-02. OPERATIONS CHECKED GOOD AT THIS TIME.
PITCH TRIM MAIN INOPERATIVE MSG IN CLIMB OUT. CLEANED HSCU & PITCH TRIM PANEL. PERFORMED OPERATIONS CHECK IAW AMM 27-40-00. OPERATIONS CHECK GOOD. NO FURTHER DEFECTS NOTED. RESET PITCH TRIM 1 & 2 CB ON THE OVERHEAD PANEL.
NUMBER 6 EMER FLOOR LIGHTING STRIP IN THE CABIN INOPERATIVE. R & R FLOOR PROX EMER LIGHT STRIP NR 6 IAW AMM 33-50-12. OPERATIONS CHECKED GOOD.
DURING BOARDING, A VERY STRONG ELECTRICAL BURNING ODOR WAS NOTICED, COMING FROM COCKPIT INSTRUMENT PANEL AREA. R & R BATTERY ON FLIGHT ATTENDANT`S FLASHLIGHT IAW 33-50-05.
HAIL DAMAGE EVENT. REPLACE CTR FUSELAGE IV TOP SKIN. R & R CTR FUSELAGE IV TOP SKIN IAW SRM 53-24-01, 51-40-02, 51-20-03, 51-20-01, ETN EM-53-265 & ETN-EM-51-118.
HAIL DAMAGE EVENT. REPLACE REAR FUSELAGE I SKIN. R & R REAR FUSELAGE I SKIN IAW SRM 51-40-02, 51-40-06, 51-20-01, 51-20-03, 51-40-03, ETN-EM-51-118, ETN-EM-53-266 & 53-31-01-SI.
HAIL DAMAGE EVENT. REPLACE LT ELEVATOR OTBD UPPER SKIN TIP. R & R LT ELEVATOR OTBD UPPER SKIN TIP IAW SRM 51-40-02, 51-20-01, 51-20-03, 51-40-06, 55-20-01 & ETN EM-55-073R2 & ETN EM-55-076.
HAIL DAMAGE EVENT. REPLACE LT ELEVATOR UPPER CTR SKIN. R & R LT ELEVATOR UPPER CTR SKIN IAW EMB SRM 51-20-01, 51-20-03,51-40-02, 51-40-06, 55-20-01 & ETN-EM-55-073R2 & ETN-EM-55-076.
HAIL DAMAGE EVENT. REPLACE LT ELEVATOR INBD LE. R & R LT ELEVATOR INBD LE EMB SRM 51-40-02, 51-20-01, 55-20-01, 51-40-06 & ETN-EM-55-073R2 & ETN-EM-55-076.
HAIL DAMAGE EVENT. REPLACE RT ELEVATOR OUTER LE. R & R RT ELEVATOR OUTER LE IAW SRM 51-20-01, 51-20-03, 51-40-02, 51-40-06, 55-20-01, ERS-EM-5500-284, ETN-EM-55-073 & ETN-EM-55-076.
HAIL DAMAGE EVENT. REPLACE RT ELEVATOR MID SKIN TIP. R & R RT ELEVATOR MID SKIN TIP IAW SRM 51-40-02, 51-20-03, 51-20-01, 51-40-06, 55-20-01 & ETN EM-55-073R2 & ETN-EM-55-076.
HAIL DAMAGE EVENT. REPLACE RT ELEVATOR INBD LE. R & R RT ELEVATOR INBD LE IAW SRM 51-40-02, 51-20-03, 55-20-01, 51-40-06, ETN EM-55-073R2 & ETN-EM-55-076.
HAIL DAMAGE EVENT. REPLACE FWD FUSELAGE II SKIN WIPER. R & R FWD FUSELAGE II SKIN, WIPER PANEL, IAW SRM 51-40-02, 51-20-01, SRM 53-21-01, 51-20-03, 51-40--06 & ETN-EM-51-118 & ETN-EM-53-206.
HAIL DAMAGE EVENT. REPLACE RT ELEVATOR UPPER CTR SKIN. R & R RT ELEVATOR UPPER CTR SKIN IAW SRM 51-20-01, 51-20-03, 51-40-02, 51-40-06, 55-20-01 & ETN-EM-55-073R2 & ETN-EM-55-076.
HAIL DAMAGE EVENT. REPLACE FWD FUSELAGE I RT SKIN PANEL. R & R FWD FUSELAGE I RT SKIN IAW SRM 51-40-02, 51-20-01, 53-21-01, 51-20-03, 51-40-06, ETN-EM-53-235, ETN-EM-51-118 & ERS-EM-5300-1331.
HAIL DAMAGE EVENT. REPLACE FWD FUSELAGE I LT SKIN PANEL. R & R FWD FUSELAGE I LT SKIN IAW SRM 51-40-02, 51-20-01, 53-21-01, 51-20-03, 51-40-06 & ETN-EM-53-235 & ETN-EM-51-118.
HAIL DAMAGE EVENT, REPLACE LT ELEVATOR MID SKIN TIP. R & R LT ELEVATOR MID SKIN TIP IAW SRM 51-40-02, 51-20-01, 51-20-03, 51-40-06, 55-20-01 & ETN EM-55-073R2 & ETN-EM-55-076.
HAIL DAMAGE EVENT. RT ELEV DAMAGED ON INBD TE. RT ELEV DAMAGE ON INBD TE REPAIRED IAW ERS-EM-55MR-299.
HAIL DAMAGE EVENT. REPLACE RT CTR FUSELAGE I. R & R RT CFI IAW SRM 51-40-02, 51-40-03, 51-20-01, 51-20-03, 51-40-06, 53-21-01, ETN-EM-51-118 & ETN-EM-53-262R1.
HAIL DAMAGE EVENT. REPLACE RT HORIZONTAL STAB UPPER SKIN. R & R RT STAB UPPER SKIN IAW SRM 55-10-01SI, 51-40-02, 51-40-06, 51-20-03, 51-20-01 & ETN-EM-55-073R2.
HAIL DAMAGE EVENT. REPLACE LT STAB UPPER SKIN. R & R LT STAB UPPER SKIN IAW SRM 55-10-01SI, 51-40-02, 51-40-06, 51-20-03, 51-20-01 & ETN-EM-55-073R2 & ETN-EM-55-074.
HAIL DAMAGE EVENT. REPLACE LT CTR FUSELAGE I. R & R LT IAW SRM 51-40-02, 51-40-03, 51-20-01, 51-20-03, 51-40-06, 53-21-01, ETN-EM-51-118 & ETN-EM-53-262R1.
SPOILER FAILURE CAUTION MSG DESCENDING THROUGH FL 210 WITH SPOILER OPEN INDICATION. COMPLIED WITH SPOILER SYS OPERATIONAL CHECK IAW AMM 27-63-01-700-803-A. SPOILER OPERATIONAL CHECK GOOD, NO DEFECTS NOTED. PANELS OPEN & CLOSE AS REQUIRED. ACFT OK FOR SERVICE.
AT FLIGHT LEVEL 220, RECEIVED A STRONG ODOR OF BURNING METAL, THIS CONTINUED FOR ABOUT 10 MINUTES. DECLARED AN EMERGENCY & LANDED. PERFORMED ETN-EM-72-034, NO DEFECTS NOTED AT THIS TIME. R & R NR 2 PACK ACM IAW AMM 21-51-03. OPS CHECKED GOOD.
STRONG BURNING SMELL WITH PACK 2 ON. COMPLIED WITH ETN EM 72-034 ENG ODOR EVENT NO EFFECTS NOTED. FOUND NR 2 PACK RAM AIR VLV DUCT CUT. R & R IAW AMM 21-25-01. OPERATIONS CHECKED GOOD.
LEFT INBD FLAP VANE LE HAS CRACK & LT INBD FLAP SKIN BELOW LE CRACKED FROM NR 2 TIRE TREAD SEPARATION. R & R LT INBD FLAP IAW AMM 27-50-00. OPS CHECKED GOOD.
FLIGHT ATTENDANT FWD FLASHLIGHT BRACKET IS BROKEN. R & R FWD FLIGHT ATTENDANT FLASHLIGHT BRACKET IAW MM 25-60-00.
CAPTAIN'S FLASHLIGHT INOPERATIVE. R & R CAPTAIN`S FLASHLIGHT ASSEMBLY IAW AMM 33-50-16.
ON CLIMB OUT THROUGH 17,000 FT, NR 1 ENG OIL TEMP CLIMBED TO 124 DEGREE C. REDUCED THRUST TO REDUCE TEMP, STILL SHOWED A LARGE TEMP SPLIT WITH NR 2 ENG OIL. NO CMC EXCEEDANCE MSG. R & R NR 1 FCOC & OIL TEMP & PRESS SENSOR. OPERATIONS CHECKED GOOD FIM 79-37-00, RRMM 79-25-15 & 79-31-10. OIL FCOC COOLER ASSEMBLY PN 230735352 & SN 1821.
FORWARD BULKHEAD AT 3BC EMER EXIT SIGN INOPERATIVE. PERFORMED TROUBLESHOOTING IAW WMM 33-50-50. SECURED CONNECTOR P8530 IN FWD GALLEY CEILING PANEL. OPERATIONS CHECKED GOOD IAW 145 AMM 33-50-00.
ADVISORY FLAP LOW SPEED INDICATION PRESENTED WHEN FLAP SELECTED DURING APPROACH. REMOVED AND REPLACED LT WING FLAP VELOCITY SENSOR IAW AMM 27-51-12.OPS CHECKED OK.
RIGHT AFTER TAKEOFF TANK NR 1 SHOWED 0. 20 MIN LATER AT FL 360 BOTH TANKS SHOWED DASHES. THE GAUGES CAME BACK & WORKED AS WELL AS WE COULD TELL. DID NOT START GOING TO DASHES AGAIN UNTIL ENG SHUT DOWN. VERIFIED NO FAULT CODES ON FCU MEMORY. R & R SYS POWER SWITCH S7199 IAW AMM CH 20-13-04, OPERATIONS CHECKED OK IAW AMM CH 28-23-08 AND 28-41-00.
DURING OPERATIONS CHECK OF EMERGENCY LIGHT SYS FOUND THAT THE LT FWD BELLY LIGHT WAS INOPERATIVE & FWD GALLEY CEILING PANEL EMERGENCY LIGHT WAS INOPERATIVE. TROUBLESHOOT THE LT FWD BELLY EMERGENCY LIGHT INOPERATIVE IAW EMB 145 FIM 33-50-00-810-804-A. FOUND CONNECTOR TO NR 1 EMERGENCY POWER SUPPLY NOT CONNECTED CORRECTLY. RESEATED THE CONNECTION TO THE NR 1 EMERGENCY POWER SUPPLY IAW EMB 145 FIM 33-50-00-810-804-A, SYS CHECKED GOOD IAW EMB 145 AMM 33-50-00-700-801-A.
DURING INSTALLATION FOUND THAT NR 2 EMERGENCY LIGHT STRIP HAS A BROKEN WIRE, ACFT SIDE. REPAIRED NR 2 EMERGENCY LIGHT STRIP WIRE IAW EMB 145 SWPM 20-21-00 STEP 2.
DURING INSTALLATION FOUND THAT NR 5 EMERGENCY LIGHT STRIP CONNECTION PULLED OFF. REPAIRED NR 5 EMERGENCY LIGHT STRIP CONNECTOR IAW EMB 145 SWPM 20-21-00 STEP 6.
DURING REMOVAL FOR INSPECTION NR 8 EMERGENCY LIGHT STRIP WIRES WERE FOUND TO BE BROKEN. R & R NR 8 EMERGENCY LIGHT STRIP IAW EMB 145 AMM 33-50-12.
DURING REMOVAL FOR INSPECTION NR 5 EMERGENCY LIGHT STRIP WIRES WERE FOUND TO BE BROKEN. R 7 R NR 5 EMERGENCY LIGHT STRIP IAW EMB 145 AMM 33-50-12.
DURING REMOVAL FOR INSPECTION NR 3 EMERGENCY LIGHT STRIP WIRES WERE FOUND TO BE BROKEN. R & R NR 3 EMERGENCY LIGHT STRIP IAW EMB 145 AMM 33-50-12.
DURING REMOVAL FOR INSPECTION NR 6 EMERGENCY LIGHT STRIP WIRES WERE FOUND TO BE BROKEN. R & R NR 6 EMERGENCY LIGHT STRIP IAW EMB 145 AMM 33-50-12.
LEFT FWD BELLY EMERGENCY LIGHT INOPERATIVE. TROUBLESHOOT THE LT FWD BELLY EMERGENCY LIGHT INOPERATIVE IAW EMB145 FIM 33-50-00-810-804-A. FOUND CONNECTOR TO NR 1 EMERGENCY POWER SUPPLY NOT CONNECTED CORRECTLY. RESEATED THE CONNECTOR TO THE NR 1 EMERGENCY POWER SUPPLY IAW EMB145 FIM 33-50-00-810-804-A. SYS CHECKED GOOD IAW EMB145 AMM 33-50-00-700-801-A.
FORWARD GALLEY CEILING PANEL EMERGENCY LIGHT INOPERATIVE. FOUND CONNECTOR TO NR 1 EMERGENCY POWER SUPPLY NOT CONNECTED CORRECTLY. RESEATED THE CONNECT TO THE NR 1 EMERGENCY POWER SUPPLY IAW EMB145 FIM 33-50-00-810-804-A, SYS CHECKED GOOD IAW EMB145 AMM 33-50-00-700-801-A.
LT WING AFT EMERGENCY LIGHT INOPERATIVE. R & R LAMP IAW AMM 33-50-10. OPS CHECKED GOOD.
FLIGHT 3951, CREW REPORTED F/O FLASHLIGHT INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R FLASHLIGHT IAW AMM 33-50-16-000-801-A AND 33-50-16-400-801-A. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.
DURING B INSPECTION FOUND THE FORWARD PASSENGER FLASHLIGHT HOLDER BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD DAMAGED FLASHLIGHT HOLDER IAW EMB AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE INSPECTION, FOUND CAPTAIN`S FLASHLIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACE CAPTAINâS FLASHLIGHT. OPS CHECKED GOOD IAW AMM 33-50-16. AIRCRAFT RETURN TO SERVICE.
FLIGHT 3308, CREW REPORTED THE CAPTAINS FLASHLIGHT WOULD NOT CHARGE. OPEN
DURING MAINTENANCE INSPECTION, FOUND THE BULKHEAD FLASHLIGHT ON FLIGHT DECK INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAINâS FLASHLIGHT AND HOLDER IAW AMM 33-50-16. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
DURING B-INSPECTION FOUND THE FLIGHT ATTENDANT CONTROL PANEL EMERGENCY LIGHT CONTROL BUTTON INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLIGHT ATTENDANT CONTROL PANEL IAW EMB 145 AMM 25-27-09-000-801-A AND 25-27-09-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE INSPECTION FOUND THE LEFT AFT ABOVE WING EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LEFT AFT ABOVE WING EMERGENCY LIGHT IAW AMM TASKS 33-50-07-000-801-A AND 33-50-07-400-801-A. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
ON FLIGHT 9805 THE CREW REPORTED THE OVERWING INTERNAL EMERGENCY EXIT LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RESEATED CONNECTORS TO BOTH OVERWING INTERNAL EMERGENCY EXIT LIGHTS IAW EMB SWPM 20-50-00 IAW EMB 145 AMM 33-50-00. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE INSPECTION FOUND THE MAIN DOOR WOULD NOT OPEN FROM THE INSIDE. THE AIRCRAFT WAS REMOVED FROM SERVICE. ADJUSTED INTERNAL RED HANDLE IAW EMB 145 AMM 52-18-05. THE MAIN PASSENGER DOOR NOW OPENS FROM THE INSIDE. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING B-INSPECTION, FOUND THE LEFT EMERGENCY ESCAPE HATCH LOWER SEAL TORN. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LEFT EMERGENCY ESCAPE HATCH LOWER SEAL IAW AMM 52-21-01. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
DURING B-INSPECTION FOUND THE LAV CENTER BEAM GUSSETT CORRODED & THE LAV LEFT BEAM GUSSETT CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NEW LAV CENTER BEAM GUSSETT IAW SRM 51-40-02, AND NEW LAV LEFT BEAM GUSSETT IAW SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING B-INSPECTION, FOUND THE EMERGENCY LIGHT STRIPS NR 3, 4 & 6 NOT PROPERLY SEATED TO EXTRUSION STRIPS. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED STRIP LIGHT ASSEMBLY IN FLOOR SIDEWALL ASSEMBLY FOR FLOOR PROXIMITY STRIP LIGHT NR 3 AND RESECURED STRIP LIGHT ASSEMBLY IN FLOOR SIDEWALL ASSEMBLY FOR FLOOR PROXIMITY STRIP LIGHTS NR 4 AND 6 IAW AMM 33-50-12. OS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
DURING MAINTENANCE INSPECTION FOUND THE LEFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT OVERWING EMERGENCY LIGHT BULB IAW EMB 145 AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD IAW EMB 145 AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 3325 THE TOWER REPORTED SMOKE COMING OFF GEAR DURING LANDING ROLLOUT. REPORTED SMOKE STOPPED BEFORE EXITING RUNWAY. COULD NOT DETERMINE WHICH SIDE. THE AIRCRAFT WAS DE-ICED EARLIER. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED MAIN LANDING GEAR INSPECTION WITH NO DEFECTS NOTED IAW AMM CH 05-30-24. AIRCRAFT OK FOR RETURN TO SERVICE. NO PARTS REMOVED OR REPLACED THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 9810 THE CREW REPORTED THAT SMOKE WAS COMING FROM NR 1 ENGINE AFTER SHUTDOWN (FRONT AND BACK). THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED SHAFT PLUG IAW ROLLS ROYCE MM 72-59-15. NO SMOKE NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 4287 THE CREW REPORTED, SELECTED THE NR 1 PACK AND SMOKE CAME THRU THE VENTS. THE CREW ELECTED TO RETURN TO ORD. THE AIRCRAFT WAS REMOVED FROM SERIVCE. PERFORMED ENGINE RUNS AND DID OPERATIONAL CHECK OF NR 1 PACK AND NR 2 PACK SYSTEM IAW EMB 145 AMM 21-51-00. THE OPERATIONAL CHECK WAS GOOD NO DEFECTS OR SMOKE NOTED. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.
FOR FLIGHT 3549 DURING THE PREFLIGHT INSPECTION THE CREW OBSERVED THE EMERGENCY LIGHT SWITCH IN ARMED POSITION AND ALL EMERGENCY LIGHTS WERE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED OPERATIONAL TEST OF EMERGENCY LIGHTS IAW EMB-145 MM 33-50-00. THE EMERGENCY LIGHTS TESTED SATISFACTORY. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 3693 THE CREW REPORTED A LOUD WHIRRING NOISE THAT BEGAN AT 3000 FEET ON FINAL TO MIA FOLLOWED BY A HOT ELECTRIC WIRING ACRID ODOR DURING THE REMAINDER OF FLIGHT. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND INSTALLED ATTITUDE HEADING REFERENCE SYSTEM NR 2 FAN IAW EMB 145 AMM 34-21-03. THE OPERATIONAL CHECK WAS GOOD NO FAULTS NOTED.
DURING MAINTENANCE BASE VISIT FOUND THE LEFT OVERWING EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT OVERWING EMERGENCY LIGHT LAMP IAW EMB 145 AMM 33-50-07-000-801-A AND 33-50-07-400-801-A. THE OPERATIONAL CHECK WAS NORMAL AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 4167 THE CREW REPORTED FLASHLIGHT CIRCUIT BREAKER POPPED AND WOULD NOT RESET. THE AIRCRAFT WAS BOARDED BUT HAD NOT LEFT THE GATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND WIRE W102-3601-24 CRUSHED UNDER RIGHT FORWARD CONSOLE AND HAD CHAFED TO GROUND. REPAIRED WIRE IAW EMB AWM 20-21-00. CIRCUIT BREAKER NO LONGER POPPED AND ALL FLASHLIGHTS LED CHARGE INDICATORS WERE ILLUMINATED, REF EMB MM 33-50-16. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE BASE VISIT INSPECTION FOUND THE CENTER SERVICE DOOR SILL TO HAVE CORROSION AROUND NUT PLATE BETWEEN FRAMES 21-22 ON PREVIOUS REPAIR. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED CENTER SILL IAW EMBRAER STRUCTURAL REPAIR MANUAL 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE.
DURING MBV INSPECTION FOUND OUTBOARD AILERON FITTING HAS WORN AND OVERSIZED HOLES CAUSING HAT BUSHING TO STAY IN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE OUTBOARD ATTACH FITTING ON THE RIGHT AILERON IAW EO EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 4224 THE CREW REPORTED THE E1 HYDRAULIC PUMP FAILED. INDICATIONS WERE ALSO A LOSS OF HYDRAULIC SYSTEM 1 FLUID AND A LOSS OF HYDRAULIC SYSTEM 1 PRESSURE. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO GRR. THE AIRCRAFT LANDED SAFELY WITH NO INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1 HYDRAULIC ELECTRIC MOTOR DRIVEN PUMP IAW EMB 145 AMM 29-10-04. REMOVED AND REPLACED NR 1 ENG DRIVEN PUMP IAW EMB 145 AMM 29-10-03. REMOVED AND REPLACED NR 1 HYDRAULIC SYSTEM FILTERS IAW EMB 145 AMM 29-10-08. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
ON FLIGHT 4122, CREW REPORTED BOTH WINDSHIELDS SHATTERED ON TAKEOFF AT 125KTS. ACFT REMOVED FROM SERVICE. REMOVED AND REPLACED BOTH COCKPIT WINDSHIELDS. OPS CHECK GOOD. NO LEAKS NOTED. ACFT RETURNED TO SERVICE. LT WINDSHIELD P/N OFF NP15131112 S/N OFF 08071H7424
ON FLIGHT 4272 CREW NOTED ON THE GROUND THAT THE EMERGENCY FLOOR LIGHTS FROM 1A TO 7A WERE INOPERATIVE, AND 2 EXIT SIGNS, ONE BY SERVICE DOOR AND ONE ON FWD BULKHEAD WERE INOPERATIVE. ACFT REMOVED FROM SERVICE. REPLACED BATTERY AND CHARGER ASSEMBLY FOR BATTERY POWER SUPPLIES 1 AND 2. ACFT RETURNED TO SERVICE. (S)
DURING MBV INSPECTION FOUND CARGO DOOR SILL BETWEEN FRAMES 65-68 TO BE CORRODED. REMOVED AND REPLACED CARGO DOOR SILL IAW EMB SRM 51-40-02. ACFT WAS RETURNED TO SERVICE. (S)
DURING MBV INSPECTION FOUND CARGO DOOR SILL BETWEEN FRAMES 65-68 TO BE CORRODED. REMOVED AND REPLACED CARGO DOOR SILL IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (A)
CREW REPORTED DURING CLIMB A AIR LEAK COMING FROM THE FO'S DV WINDOW. CREW ELECTED TO RETURN TO DFW. AIRCRAFT LANDED AND RETURNED TO THE GATE SAFELY. REMOVED AND REINSTALLED REPAIRED SEAL IN RT DV WINDOW, IAW EMB145 AMM 56-10-02. PERFORMED PRESSURIZATION CHECK IAW EMB 145-AMM 21-51-00 PRESSURE CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
LIGHTNING STRIKE DAMAGE ON SKIN AT FRAME 32 BETWEEN STRINGER 10L AND 11L. MAINTENANCE REPAIRED DAMAGE IAW SRM 53-22-01 FIG 207, SKIN PATCH AT FRAME REPAIR. AIRCRAFT WAS RETURNED TO SERVICE. (M)
SAW - FOUND LIGHTNING STRIKE DAMAGE ON SKIN AT FRAME 22 STRINGER 14L AND 15L. MAINTENANCE INSTALLED SKIN REPAIR DOUBLER IAW SRM 53-21-01. AIRCRAFT WAS RETURNED TO SERVICE. (M)
SAW - LIGHTNING STRIKE DAMAGE ON SEVERAL RIVETS ON LEFT WING FUEL CELL. MAINTENANCE REPLACED RIVETS IAW SRM 51-40-02 AND 51-20-04. AIRCRAFT WAS RETURNED TO SERVICE. (M)