N620AE
Registered owner: AMERICAN AIRLINES INC, TX (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| American Eagle Airlines Inc | Operator | 2011-11-18 – 2011-11-18 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
PDIS 620 30-31 2696001 11SEP22 CLT CLOSE PITOT 1 INOP MESSAGE IN FLIGHT, WAS NOT IN ICING. WENT AWAY WHEN LANDING FACT 11SEP22 21:25 CLT UPON ARRIVAL TO A/C NO EICAS OR CMC MESSAGES WERE DISPLAYED. PERFORMED OPS CHECK IAW AMM 30-31-00-700-801-A OPS CHECK GOOD. A/C OK FOR SERVICE.
PDIS 620 33-40 2687161 27JUN22 CLT CLOSE WHILE IN FLIGHT TAXI LIGHT DEPARTED AIRCRAFT INSPECTED FOUND NO DAMAGE TO A/C SECURED WIRING REF PIEDMONT BULLINTON 20-21 A/C OKAY FOR SERVICE FACT 27JUN22 02:06 ROA INSTALLED TAXI LIGHT ASSY IAW 33-42-02-04, OPS CK GOOD CLEAR MEL.
PDIS 620 21-51 2756261 29MAR22 CLT CLOSE PACK 1 VALVE CLOSED MESSAGE IN FLIGHT. C/W FLT CREW PROCEDURES FACT 01APR22 01:30 ROA FOUND INLET BOOT BLOWN OFF #1 HEAT EXCHANGER. R/R'D BOOT PER AMM 21-51-02, OPS CK GOOD CLEAR MEL.
PDIS 620 71-10 2746611 04DEC21 CLT CLOSE EXTREME VIBRATION ON #1 ENGINE IN FLT @ 3000 FT. 00 FACT 04DEC21 15:42 CLT FOUND #1 ENGINE OIL DOOR OPEN AND AIR START VALVE DOOR OPEN AND COWL DAMAGED. R+R #1 LOWER COWL IAW 71-12-01-000-802A AND 71-12-01-400-802A
STRONG BURNING SMELL OBSERVED IN THE COCKPIT AND CABIN IN ICING CONDITION. PERFORMED OPS CHECK OF ANTI/ICE MESSAGES AND PACKS IAW EMB 145 AMM 30-00-00-700-801-A OPS CHECK GOOD NO SMOKE SMELL NOTED.
STRONG ELECTRICAL ODER IN FLIGHT DECK FOLLOWED BY TCAS FAIL. PERFORMED GVI OF FLIGHT DECK AND FWD AVIONICS. RAN ENGINES AT FULL POWER WITH PACKS ON. NO EVIDENCE OF ELECTRICAL SMELL OR ANY OTHER DEFECTS NOTED REF LOGPAGE 240803 SEQ 2 FOR TCAS MEL A/C OK FOR SERVICE.
PDIS 620 32-49 2362062 31MAR21 ORD CLOSE. AFTER SELECTING GEAR DOWN, BRAKE DEGRADED MSG APPEARED ON EICAS, MSG PERSISTED AFTER LANDING. LH OTBD BRAKE TEMP HIGHER THAN NORMAL (STILL IN THE GREEN RANGE)(NO RELATED CMC MESSAGES). FACT 01APR21 13:30 ORD. R&R RH BRAKE CONTROL VALVE IAW AMM 32-41-06, OPS CHECK AND LEAK CHECK GOOD. NO EICAS MESSAGE PRESENT AT THIS TIME. ALL OTHER INDICATIONS NORMAL OK FOR SERVICE
PANEL 241DF EMERGENCY LIGHT INOPERABLE. R & R PANEL 241DF EMERGENCY FLOOR STRIP LIGHT ASSEMBLY, IAW AMM 33-50-112. SPLICED NEW CONNECTORS AT PANEL 241DF EMERGENCY LIGHT, IAW STANDARD MAINTENANCE PRACTICES.
PITOT 1 INOPERABLE DISPLAYED ON EICAS AFTER TAKE OFF. REMOVED AND REPLACED NR 1 PITOT SENSOR, IAW AMM 34-13-01. OPERATIONS CHECK AND LEAK CHECK GOOD. OK FOR SERVICE REQUIRES FILET SEALANT AROUND BASE SEE SEQ 2 THIS LP. CORRECT LP 231995-1.
IN FLT COMS 1/2 EXPERIENCED STATIC FOLLOWED BY BURNING SMELL AND COM 1 GOING OUT. MAINTENANCE: R & R NO1 ICU, IAW AMM 23-00-01. COMM 1 OPERATIONS GOOD (SHORT SIGNED). R & R NR 2 INTEGRATED COMM UNIT, IAW AMM 23 00 01. COMMS 2 OPERATIONS CHECK GOOD. OK FOR SERVICE.
FOUND IC-2 C/B POPPED (D-30) WITH BURNING SMELL AT NR 2 IC-600. R & R NR 2 IC-600, REF AMM 31-42-01. PERFORMED OPERATIONS CHECK, PER AMM 31-42--00-700-801-A. ALL CHECKS NO BURNING SMELL. OK FOR SERVICE.
PDIS 620 30-21 2453941 02OCT20 MDT. CLOSE E2 ANTI ICE FAIL WITH NO ICING CONDITION. FACT 03OCT20 20:29 MDT. DOWNLOADED CMC DATA, ENGINE 2 ANTI ICE VALVE FAIL OCC. BEGAN T/S W/ FIM 30-21-00-810-804. DURING BLOCK 11 VALVE SEIZED IN OPEN, FOUND DAMAGED. INSPECTED DUCT, NO FOD NOTED. R & R NR 2 ENGINE INLET VALVE, IRT AMM 30-21-01-000/400-801. LEAK CHECKS 30-00-00-700-802, 30-21-00-700-803, AND 30-21-00-700-804 GOOD. NO CMC MESSAGES. OK FOR SERVICE.
FRAME 68 FLOOR SUPPORT CLEAT AFT BAGGAGE BAY DOOR HAS CORROSION FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED FLOOR SUPPORT CLEAT FR 68 AFT CARGO IAW EMB145 SRM 51-40-02, 51-20-03, 51-21-04, 51-21-05, AND 51-21-06.
ON T/O TAT1 INOP W/ NO CONFIG MSG. C/W FIM 30-33-00-810-801A. MSG CLEARED AND D/N RETURN. TAT 1 INOP ON T/O ASSOCIATED W/ NO CONFIG WARNING. PERFORMED FIM TASK 30-33-00-810-801A. R&R RELAYS K0495,K0534,K0325,K0059. R&R TAT CURRENT SENSOR IAW 30-33-01 NO FIX. R&R TAT PROBE #1 IAW 34-15-03. OPS CHECKED TAT 1 IAW 30-33-00. OPS CHECK GOOD. OK FOR SERVICE.
AFTER TAKEOFF ATTEMPT, WHEN THRUST LEVERS WERE SET TO TAKEOFF THRUST, HEAVY SMOKE APPEARED IN THE COCKPIT. ONCE THRUST LEVERS WERE MOVED BACK TO IDLE, SMOKE CLEARED. MX TROUBLESHOT ISSUES AND DETERMINED TO BE THE NR 1 ENGINE BLEED SYSTEM, WHEN THRUST LEVERS ARE ADVANCED.
CAPTS WINDOW PILLAR CRACKED, BTWEEN W/S AND DV WINDOWS....FIX: PERFORMED EDDY CURRENT INSPECION AT CAPT,S PILLAR INNER AND OUTER SURFACE SKIN. NO CRACKS FOUND AT HIS TIME. PILLAR FOUND TO BE SEPARATING AT SEAM. NOTE: A/C FERRIED TO SBY WHERE 7 RIVETS REPLACED DUE TO BEING SHEARED
AFTER T/O, IN FLIGHT, STRONG CHEMICAL ODOR IN COCKPIT, LASTED WHOLE FLIGHT....FIX: RAN ENGINES WITH BLEEDS AND PACKS FOR 20 MINUTES.CLEANED RECIRC FAN INLET SCREENS AS REQ NO ODOR NOTED AT THIS TIME.OK FOR SERVICE.SEE SEQ IN WORK PACKAGE DATED 11/11/19 FOR T/S.
PITOT 1 INOP CAUTION MESSAGE APPEARED INTERMITTENTLY DURING TAXI....FIX: R&RD RELAY K0111 AND K0060 IAW 32-15-02. REF FIM 30-31-00. OPS CHECK GROUND TAXI CHECK GOOD.OK FOR SERVICE
PITOT 1 MOMENTARILY DISPLAYED ON EICAS AFTER ENG START.....FIX:PITOT 1 CAUTION MESSAGE TRANSITORY OPS CHECK PITOT STATIC HEAT IAW 30-31-00 ALL PROBED HEATED ACCORDINGLY RAN ENG 2 AND THEN #1 CAUTION LIGHT NEVER APPEARED. STARTED #1 ENGINE AND THEN #2 CAUTION NEVER APPEARED
PDIS 620 30-31 2202552 29OCT19 PHL CLOSE PITOT 1 INOP CAUTION MESSAGE AFTER ENG START FACT 30OCT19 05:48 PHL R/R RELAY K0056 AND PITOT CURRENT SENSOR #1 K0053 IAW SWPM 20-13-03. R/R STATIC PITOT SENSOR IAW AMM 30-31-02.SLAVED PITOT SENSOR #1 IAW AMM 34-13-01. ALL NO FIX. FURTHER TROUBLE SHOOTING IS REQ'D. SEE LOG PAGE 220256 SEQ.#1. DISCREPANCY CURRENTLY IN WORK IN PHL
PDIS 620 30-31 2202542 28OCT19 PHL CLOSE PITOT 1 INOP CAUTION LIGHT ILLUMINATED AFTER PUSH BA CK. (INTERMITTENT) 20058 00 EK FACT 28OCT19 19:57 PHL RNRD PITOT #1 SWITCH, REF AMM 20-13-03 OPS CHECK REF AMM 30-31-00, OPS GOOD. A/C OK FOR SERVICE.
FLIGHT DECK CEILING EMERGENCY LIGHT BULB INOP. REPLACED THE BULB. OPS CHECK GOOD
PDIS 620 76-10 1911661 27SEP18 ROA CLOSE REJECTED TAKE OFF DUE NO.2 ENGINE LOSS OF POWER. 26010 00 VAG FACT 27SEP18 22:52 ROA PERFORMED AC ENGINE RUN. START AND HIGH POWER IAW EM B AMM 71-00-01 NO DEFECTS NOTED OK FOR SERVICE.
A BURNING MATCH ODOR IN THE COCKPIT AND AT ROWS 4 - 6 FOR APPROXIMATELY 1 MINUTE DURING DESCENT, AROUND 20K FT. NOTHING ABNORMAL NOTED. CONDITION DID NOT RETURN REST OF FLIGHT. DROPPED PSU PANELS AT ROWS 4 - 6, INSPECTED AREA AND FOUND NO DISCREPANCIES. OK FOR SERVICE.
NR 2 BLEED VALVE FAILED EICAS MESSAGE DISPLAYED DURING TAKEOFF ROLL AFTER POWER LEVELS WERE ADVANCED. ABORTED THE TAKEOFF.
NR 1 BLEED VALVE FAILED EICAS MESSAGE DURING TAKE OFF. REJECTED THE TAKE OFF. R & R THE NR 1 BLEED VALVE IAW AMM MPP 36-11-05-04. OPS CHECKED GOOD.
DURING TAKEOFF ROLL, THE SPOILERS DEPLOYED AND THE NR 1 BLEED VALVE FAILED EICAS MESSAGES DISPLAYED. INSPECTED AND DETERMINED THE SPOILER DEPLOYMENT TO BE CONSISTENT WITH NORMAL GROUND SPOILER AUTO-DEPLOY SEQUENCE. ACFT OVER 30KTS AND TL RETARDED FOR REJECTED TAKEOFF. TROUBLESHOT THE NR 1 BLEED VALVE FAIL IAW FIM 36-11-00-810-805A. GROUND RAN THE ACFT AND PERFORMED AN OPS CHECK IAW 36-11-05-700-802-A. OPS CHECKED GOOD.
EICAS MESSAGE FOR THE NR 2 BLEED FAIL DURING TAKEOFF, ABORTED TAKEOFF. MESSGAE CLEARED PRIOR TO CREW ENGINE SHUT DOWN. GROUND RAN CND AND NO EICAS OR CMC MESSAGE. OK FOR SERVICE.
NR 1 BLEED LEAK EICAS MESSAGE DURING CLIMBOUT, FOLLOWED QRH AND MESSAGE WENT OUT AFTER 3 MINUTES 20 SECONDS. OPEN.
NR 1 BLEED LEAK EICAS MESSAGE, DURING CLIMBOUT. COMPLIED WITH QRH. MESSAGE WENT OUT. R & R DUCT TEMP SENSOR FOR THE NR 1 PACK IAW AMM 21-60-03-400-801A. OPS CHECKED GOOD. OK FOR SERVICE AT THIS TIME.
NR 1 BLEED LEAK EICAS MESSAGE DURING CLIMBOUT, COMPLIED WITH QRH, MESSAGE WENT OUT. INSPECTED IAW FIM 36-20-00-810-801-A, NO DEFECTS NOTED. PERFORMED AN OPS CHECK IAW AMM 36-00-00-700-803-A/500, OPS CHECKED GOOD, NO MESSAGES. OK FOR SERVICE.
CARGO DOOR OPEN & CLOSE CABLE PULLEY SUPPORT AT FRAME 69 BETWEEN STRINGERS 4R AND 5R IS CRACKED APPROXIMATELY ONE INCH. -REMOVED AND REPLACED CABLE PULLEY BRACKET IAW SRM 51-40-02.
RT WING GROUND SPOILER HAS A .500 INCH CRACK ON THE OTBD HINGE FITTING. REMOVED AND REPLACED THE HINGE FITTING IAW AMM 20-10-01.
RT AILERON PCU ATTACH FITTING HAS OVERSIZED HAT BUSH BORES. REMOVED AND REPLACED FITTING IAW EO EM-27MR-112
LEFT FUSELAGE TO WING FAIRING LATERAL PANEL. LOWER ATTACH ANGLE CRACKED AT THE AFT END. R & R THE ATTACH ANGLE IAW ETN-EM-53-142.
FA REPORTS MAIN CABIN DOOR DIFFICULT TO OPEN.AIRCRAFT FOUND TO BE WITHIN 5LBS OR LESS THAN THE MAX LOAD CRITERIA (45-50LBS)-C/A-DEFERRED PER FMR REF ETN-EM-52-029 TDMI AUTHORIZATION NUMBER 620T5251. PERFORMED THE ADJUSTMENT OF THE PASSENGER MAIN DOOR IN ACCORDANCE WITH AMM 52-18-00 AND REDUCED THE AVERAGE MAXIMUM LOAD OF THE INTERNAL HANDLE PULL TEST TO A VALUE OF LESS THAN 45LBS. COMPLETE:WITH ALL THE ADJUSTMENTS AND THE REPLACEMENTS OF PARTS STATED IN THE WIPS BELOW AND THE ACFT OFF JACKS. PERFORMED A FINAL PULL TEST ON THE PAX DOOR AND RECORD THE OUT OF DOCK VALUE OF 36 LBS. WHICH IS WITH IN LIMITS IAW AMM 52-18-00 THAT GIVES YOU A 50 LBS. MAX LIMIT TDMI RESTORED
MAIN CABIN DOOR HARD TO OPEN. LUBRICATED THE HINGE ROLLERS IAW AMM-53-21-62. OPS CHECKED GOOD.
MAIN CABIN DOOR HARD TO OPEN. LUBRICATED THE MAIN DOOR AND PULL TESTED INTERNAL ACTUATING HANDLE IAW AMM 52-18-00 AND ETN EM-52-029. FOUND TO BE WITHIN LIMITS.
SHEET METAL UNDER NR 2 WING LOOKS CRACKED BY WHEEL WELL. INSPECTED A/C AND FOUND 5.5" CRACK ON RT MLG AFT RIB PN 145-72166-002 ITEM TRANSFERRED TO LOG PAGE 4069199 ITEM 1. C/W PERMANENT REPAIR ON RT MLG AFT RIB IAW ERS-EM-5300-2647.
AFT GALLEY AFT SIDE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE NR 3 INVERTER IAW AMM 33-50-11. OPS CHECKED GOOD.
FA STATES MAIN DOOR GETTING INCREASINGLY HARD TO OPEN AND CLOSE. LUBED MCD ROLLERS PER AMM 53-21-02. NO FURTHER DEFECTS NOTED.
FORWARD FLT ATTENDANT FLASHLIGHT BRACKET BROKEN. REMOVED AND REPLACED FLASHLIGHT ASSY IAW MM 33-50-16. OPS CHECKED OK.
P TRIM MAIN INOP. CLEANED ALL 3 PITCH TRIM SWITCHES PER AMM 27-40-03. PERFORMED FIM TASK 27-43-00-810-801 OPS CHECK PITCH & TRIM SYSTEM GOOD FOUND TO BE TRANSITORY CONDITION.
MAIN CABIN DOOR IS VERY DIFFICULT TO OPEN. PERFORMED LUBE OF MAIN DOOR FRAME ROLLERS IAW MM 53-21-02 AND MAIN DOOR HANDLE ACTUATING TEST IAW MM 52-10-01 OP TEST OK
MAIN DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED MAIN DOOR EMERGENCY LIGHT LAMP IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A. OPS CHECKED GOOD.
MAIN PASSENGER DOOR IS HARD TO OPEN. LUBRICATED MAIN ENTRANCE DOOR RUBBER SEAL IAW-AMM-52-18-04, OPS CHECK GOOD.
MAIN DOOR EMERGENCY LIGHT INOPERATIVE. R & R MAIN PASSENGER DOOR EMERGENCY LIGHT IAW AMM 33-50-06-000-801. OPS CHECK GOOD.
MAIN DOOR EMERGENCY LT INOPERATIVE. R & R MAIN DOOR EMERGENCY LIGHT LAMP IAW AMM 33-50-06-000-801-A AND 33-50-06-400-801-A. OPS GOOD AT THIS TIME.
MAIN CABIN DOOR EMER LIGHT INOPERATIVE. R & R MAIN CABIN DOOR EMER LIGHT IAW AMM 33-50-06-000-801-A & 33-50-06-400-801-A. OPERATIONS CHECKED GOOD.
BRAKE INBD INOPERATIVE MSG PRESENTED UPON GEAR EXTENSION. PERFORMED GO AROUND & COMPLETED AOM 1 PROCEDURES, NORMAL LANDING, ALL BRAKE TEMPS INDICATOR REMAINED IN THE GREEN 324M3800. FOUND INBD SOV TRIPPED, RESET INBD BRAKES OPERATIONS CHECKED OK. R & R BCU FOR PRECAUTIONARY REASONS IAW AMM CH 32-41-02. BRAKE SYS FUNCTION CHECKED OK IAW AMM CH 32-41-00.
MAIN CABIN DOOR EMER LIGHT INOPERATIVE. R & R MAIN DOOR EMER LIGHT BULB IAW AMM 33-50-10-000-801-A & 33-50-01-400-801-A. OPERATIONS CHECKED GOOD.
MAIN DOOR EXTERIOR EMER LIGHT INOPERATIVE. R & R MAIN DOOR EMER LIGHT LAMP IAW AMM 33-50-06-000-801-A & 33-50-06-400-801-A. OPERATIONS CHECKED GOOD.
ROW 3 AISLE EMER LIGHT INOPERATIVE. REPLACED ROW 3 AISLE EMER OVERHEAD LIGHT BULB IAW AMM 33-50-08-000-801-A & 33-50-08-400-801-A.
VERY STRONG NOXIOUS ODOR COMING FROM AN AREA AROUND 10A. REPLACED CEILING LIGHT BALLAST AT SEAT 9A IAW AMM 33-21-05 & PSU PANEL AT 8 - 9A IAW AMM 25-22-04. OPERATIONS CHECKED GOOD.
LEFT UPPER FUSELAGE SKIN CRACKED AT 1ST FASTENER BELOW STRINGER 2L ON FRAME 75. CRACK IS APPROX 3/8" LONG. LT UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 & ABOVE STRINGER 2L. CRACK IS APPROX 1/4" LONG. LT UPPER FUSELAGE SKIN CRACK REPAIRED IAW ERS-EM-53MR-1754.
THE SERVICE DOOR CUT OUT AFT FRAME IS CORRODED JUST BELOW THE BOTTOM ROLLER. PERFORMED REPAIR ON SERVICE DOOR CUT OUT AFT FRAME FOR CORROSION JUST BELOW BOTTOM ROLLER IAW ERS-EM-53-MR-1721.
RIGHT UPPER FUSELAGE SKIN CRACKED ON FRAME 75 AT THE 1ST FASTENER BELOW STRINGER 2R. CRACK IS APPROX 1/2" LONG. ACCOMPLISHED REPAIR IAW ERS-EM-53MR-1748.
LIGHTNING STRIKE BETWEEN FRAME 74 - 75, BETWEEN STRINGER 21L, FOUND DURING LIGHTNING STRIKE INSPECTION. ACCOMPLISHED LIGHTNING STRIKE REPAIR IAW ERS-EM-53MR-1749.
LIGHTNING STRIKE BETWEEN FRAME 72 - 73, BETWEEN STRINGER 21R - 20. ACCOMPLISHED LIGHTNING STRIKE REPAIR IAW ERS-EM-53MR-1750.
FRAME 65 GOUGED UPPER CTR AREA. REPAIRED FRAME 65 GOUGE IAW ERS-EM-53MR-1731.
LIGHTNING STRIKE, BETWEEN FRAME 59 & 60, BETWEEN STRINGER 21L - 21R. REMOVED DAMAGE BY DRILLING NR 21 HOLE AT THE STRIKE & INSTALLED BUTTON HEAD RIVET & WASHER IN DRILLED LOCATION IAW SRM 53-00-01 & 5120-03.
LIGHTNING STRIKE ON EXTERNAL SKIN AFT OF FRAME 61, BETWEEN STRINGER 21L - 21R. REPAIRED LIGHTNING STRIKE ON EXTERNAL SKIN IAW ERS-EM-53MR-173.
LIGHTNING STRIKE BETWEEN FRAME 60 - 61 & BELOW STRINGER 21L - 21R. REPAIRED LIGHTNING STRIKE IAW ERS-EM-53MR-1738.
LIGHTNING STRIKE BETWEEN FRAME 75 - 75A, STRINGER 20R - 21R. PERFORMED LIGHTNING STRIKE REPAIR IAW SRM 53-00-01.
LIGHTNING STRIKE BETWEEN FRAME 62 - 63, BETWEEN STRINGER 21L & 21R. REMOVED DAMAGE BY DRILLING NR 21 HOLE AT THE STRIKE. INSTALLED BUTTON HEAD RIVET & WASHER IN DRILLED LOCATION IAW SRM 53-00-01 & 51-20-03.
CEILING PANEL 253 CLC HAS BROKEN WIRE, FOUND ON OPEN UP. REPAIRED EMER EXIT LIGHT WIRE ON PANEL 253CLC IAW SWPM 20-21-00.
LIGHTNING STRIKE, BETWEEN FRAME 71 - 72, STRINGER 21R, FOUND DURING LIGHTNING STRIKE INSPECTION. REMOVED DAMAGE BY DRILLING NR 10 HOLE AT THE STRIKE & INSTALLED BUTTON HEAD RIVET & WASHER IN DRILLED LOCATION IAW SRM 53-00-01 & 51-20-03.
THE EXTERNAL SKIN OF THE FUSELAGE IS CRACKED AT THE RIVET, AT FRAME 75 & 4 INCHES BELOW THE RT AFT CORNER OF THE DORSAL FIN. ACCOMPLISHED REPAIR TO RT UPPER FUSELAGE SKIN CRACKS IAW ERS-EM-53MR-1748.
THE EXTERNAL SKIN OF THE FUSELAGE IS CRACKED AT THE RIVET, AT FRAME 75 & 4 INCHES BELOW THE LT AFT CORNER OF THE DORSAL FIN. LT UPPER FUSELAGE SKIN CRACK REPAIRED IAW ERS-EM-53MR-1754.
LEFT UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 & ABOVE STRINGER 2L. CRACK IS APPROX 1/4" LONG. REPAIRED IAW ERS-EM-53MR-1754.
NUMBER 7 EMER LIGHT STRIP INOPERATIVE. R & R NR 7 EMER LIGHT STRIP IAW AMM 33-50-12. OPERATIONS CHECKED GOOD.
RIGHT UPPER FUSELAGE SKIN CRACKED ON FRAME 75, AT THE 1ST FASTENER BELOW STRINGER 2R. CRACK IS APPROX 1/2" LONG. EASI 8071 USED, 100-500KHZ PROBE, FREQ=400 KHZ, V-GAIN=78.0, H-GAIN=65.0, LPF=100. ACCOMPLISHED REPAIR TO RT UPPER FUSELAGE SKIN CRACKS IAW ERS-EM-53MR-1748.
RED LIGHT ON CAPTAINS FLASHLIGHT IS NOT ILLUMINATED. R & R CAPTAINS FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.
FLIGHT ATTENDANT`S FLASHLIGHT CRADLE IS BROKEN. R & R THE FLASHLIGHT CRADLE IAW AMM 33-50-16-000-801-A & 33-50-16-400-801-A. OPS CHECKED GOOD AT THIS TIME.
EMERGENCY LIGHTED SIGN ON THE AFT SIDE OF G2 GALLEY INOPERATIVE. INSTALLED SERVICEABLE EMER LIGHT IAW AMM 33-50-14. OPERATIONS CHECKED GOOD.
MAIN CABIN DOOR HARD TO OPERATE. LUBE MAIN CABIN DOOR IAW AMM 52-118-00. OPERATIONS CHECKED GOOD.
AFT CABIN EMER FLASHLIGHT INOPERATIVE. R & R AFT CABIN EMER FLASHLIGHT IAW TASK 33-50-16-000-801-A & TASK 33-50-16-400-801-A. OPERATIONS CHECKED GOOD.
BURNING SMELL FROM PACK 2 UNDER FLIGHT ATTENDANT CONTROL. IN AUTO MODE UNDER PILOT CONTROL THE SMELL WENT AWAY. REF LOG PAGE 3754935 ITEM 2 RT ENG DUE REPLACEMENT. REF NRWC 620-ORD-02391. END DURING TROUBLESHOOTING OF BURNING SMELL FOUND RT RAM AIR DISTRIBUTION DUCT CRACKED. R & R RT RAM AIR DISTRIBUTION DUCT IAW AMM 21-25-01. COMPLIED WITH TECHNICAL SERVICES WORK SCOPE FOR ENGINE PRODUCING SLIGHT BURNING OIL SMELL AT POWER. REFERENCE NRWC 620-ORD-02391 FOR DISCREPANCIES GENERATED BY INSPECTION.
FOUND LT ELEVATOR REPLACEABLE TIP & SURROUNDING SKIN TO BE MELTED NRWC 620-MQT- 02377. PERFORMED PERMANENT REPAIR IAW ERS-EM-55MR-232.
OVERHEAD EMER EXIT LIGHT AT EXIT ROW INOPERATIVE. R & R OVERHEAD EMER EXIT LIGHT IAW AMM 33-50-08. OPERATIONS CHECKED GOOD.
AFT EMER LIGHTS WILL NOT ILLUMINATE. R & R NR 4 EMER LIGHT BATTERY & CHARGER ASSEMBLY. OPERATIONS CHECKED GOOD IAW WORK CARD 33-700-19. BATTERY CHARGER ASSEMBLY PN 11-0049 SN 14895.
DURING CLIMB NOTICED AIRPLANE WOULDN'T BURN FUEL FROM LT TANK WITH CROSS FEED OFF. PERFORMED ENG IDLE RUN ON BOTH ENGS IAW 72-00-00 & FOUND BOTH FUEL QTY INDICATORS OPERATING NORMAL, ALSO PERFORMED CHECK OF FUEL CROSS FEED VLV IAW MM 28-21-04 & NO DEFECTS FOUND. SYS OPERATING NORMAL. COMPLIED WITH FUEL QTY MEASURING STICK IAW AMM 12-11-04 & COMPARED TO DIGITAL READING, NO FAULT NOTED. PERFORMED POWER ENG RUNS IAW AMM 71-00-01. FUEL CONSUMPTION WAS IDENTICAL FOR BOTH ENGS NO FAULTS NOTED.
AFT FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT IAW AMM 25-60-04. OPS CHECKED GOOD.
AISLE OVERHEAD EMERGENCY LIGHT AT SEAT 17 AB INOPERATIVE. R & R AISLE OVERHEAD EMERGENCY LIGHT LAMP AT SEAT 17 AB IAW AMM 33-50-10, OPERATIONS CHECKED GOOD.
CABIN DOOR IS DIFFICULT TO OPEN FROM INSIDE THE ACFT. LUBRICATED MAIN DOOR MECHANIC SYS, OPERATION OF DOOR WORKING GOOD AMM 52-10-01.
AFTER TAKEOFF SELECTED GEAR UP EICAS INSTANTLY WENT FROM DOWN TO UP WITH NO TRANSITION INDICATION. CHECKED RMU, RMU INDICATED DOWN & LOCKED, EICAS INDICATED UP. GEAR POSITION IN QUESTION RAN ABNORMAL LG EXTENSION CHECKLIST, GEAR CAME DOWN WITH GEAR ELEC OVERRIDE SWITCH IN GEARS & DOORS POSITION. DECLARED EMERGENCY, LANDED SAFELY MIA. R & R LGEU IAW AMM 32-32-01 & PERFORMED OPERATIONS CHECK IAW AMM 32-30-00.
LIGHTNING STRIKE, SVC BUS CB POPPED. BURNING SMELL NOTICED. TRANSFERRED TO NRWC 620-CVG-01921. COMPLIED WITH LIGHTNING STRIKE INSPECTION WORK CARD 05-200-00.
AFTER DEPARTURE GOT TAT 1 HEAT FAIL ON EICAS. ACFT WAS REMOVED FROM SERVICE. R & R NR 1 TAT PROBES IAW AMM 34-15-03. OPERATIONS CHECKED GOOD AT THIS TIME, MEL 30-17 RESTORED.
EMERGENCY LIGHT STRIP AT ROW 17 & 18 INOPERATIVE. AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED REMOVABLE SPLICES IAW EMB 145 WM 20-21-00. OPC GOOD. MEL RESTORED
DECLARED EMERGENCY DFW INADVERTENT SPOILER OPEN IN FLIGHT. DURING MAINTENANCE INSPECTION ON FLIGHT 2871 FOUND USED SPEDBRAKE DURING DESCENT AND FAILED TO RETRACT WHEN COMMANDED TO FOLLOWED EPC + AOM AND RETRACTED SPEED BRAKES. AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED SPEED BRAKE COMMAND LEVER IAW EMB AMM 27-63-03.OPS CHECK GOOD.
SPOILERS WOULD NOT CLOSE AFTER ACTIVATION. CLOSED SPOILERS & THEY STAYED OPEN. TRANSFERRED TO NRWC 620-CMH-0183. R & R SPOILER CONTROL UNIT IAW AMM 27-63-02, OPERATIONS CHECKED GOOD IAW NRWC 620-CMH-01831.
SPOILERS WOULD NOT CLOSE AFTER ACTIVATION CLOSED SPOILERS & THEY STAYED OPEN.
SPOILERS WOULD NOT STOW AT BOTTOM OF DESCENT WITH HANDLE IN CLOSED POSITION, THRUST LEVERS ADVANCED. PULLED CBS IAW AOM. INSPECTED SPOILER HYD ACTUATION & PERFORMED SPOILER SYS OPERATIONS CHECK IAW AMM 27-62-00 & 27-63-01. NO DEFECTS NOTED, OPERATIONS CHECKED GOOD. NO SPOILER CMC MESSAGES FROM TODAY 12-28-13.
FOUND 2 FLOOR PROXIMITY LIGHT WIRES AT FRAME 33 BETWEEN STRINGERS 15L & 16L DAMAGED. REPLACED 2 FLOOR PROXIMITY LIGHT AT FRAME 33 BETWEEN STRINGERS 15L & 16L IAW EMB 145 SWPM 20-21-00.
INTERNAL FUSELAGE SKIN CORRODED BETWEEN FR-13 AND FR-14 STR-20R TO STR-18R. REPAIRED IAW AEA EO-53MR-2230.
FRAME 65, SHEAR TIE CORRODED. REPAIRED IAW EO EM-53MR-1129.
NUMBER 5 PROXIMITY LIGHT, ACFT SIDE CONNECTOR MISSING. REPLACED THE NR 5 PROXIMITY LIGHT, ACFT SIDE CONNECTOR THAT WAS MISSING IAW EMB145 SWPM 20-00-03 PAGE 65, OPERATIONS CHECKED GOOD.
IAW AEA WC 33-700-19, REMOVED BATTERY PN 2013-1A & SN 103165.
NUMBER 4 PROXIMITY LIGHT, ACFT SIDE CONNECTOR MISSING. REPLACED THE NR 4 PROXIMITY LIGHT, ACFT SIDE CONNECTOR THAT WAS MISSING IAW EMB 145 SWPM 20-00-03 PG 65, OPERATIONS CHECKED GOOD.
NUMBER 6 PROXIMITY LIGHT, ACFT SIDE CONNECTORS MISSING 2. REPLACED THE NR 6 PROXIMITY LIGHT, ACFT SIDE CONNECTORS THAT WERE MISSING 2 IAW EMB 145 SWPM 20-00-03 PG 65, OPERATIONS CHECKED GOOD.
NUMBER 2 PROXIMITY LIGHT, ACFT SIDE CONNECTOR MISSING. REPLACED THE NR 2 PROXIMITY LIGHT, ACFT SIDE CONNECTOR THAT WAS MISSING IAW EMB145 SWPM 20-00-03, OPERATIONS CHECKED GOOD.
EMERGENCY LIGHT HOLDER FLOOR STRIP BROKEN. EMERGENCY LIGHT HOLDER FLOOR STRIP R & R IAW EMB 145 AMM 33-50-12.
EMERGENCY LIGHT STRIP NR 3 HAS DAMAGED WIRE. R & R NR 3 EMERGENCY LIGHT STRIP IAW EMB 145 AMM 33-50-10, OPERATIONS CHECKED GOOD.
FWD F/A HEADSET IN CABIN HAS AN ODOR TO IT. R & R F/A HEAD SET, IAW AMM 23-31-03. OPS CHECK GOOD.
WHILE AWAITING GPU CONNECTION WITH NR 2 ENGINE RUNNING, ENGINE SHUTDOWN ON ITS OWN BOTH FUEL PUMPS WERE OFF. PERFORMED A FUEL LOW PRESSURE WARNING TEST ALSO PERFORMED ENGINE RUN AND SHUTDOWN IAW GROUND HANDLING CHECKLIST SYS FOUND TO BE OPERATING NORMAL IAW AMM 28-45-00 AND 72-00-00.
DURING B INSPECTION FOUND THE LEFT WING EMERGENCY LANDING LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT EMERGENCY LANDING LIGHT LAMP IAW EMB AMM 33-41-02-000-801-A AND 33-41-02-400-801-A. THE OPERATIONAL CHECK WAS GOOD. NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING B INSEPECTION, FOUND THE SERVICE DOOR EMERGENCY EXTEROR LIGHT INOPERATIVE DUE TO A BROKEN WIRE. REPAIRED BROKEN WIRE IAW EMB WM 20-21-00. AIRCRAFT RETURNED TO SERVICE.
DURING MAINTENANCE INSPECTION FOUND THE CAPTIANâS EMERGENCY FLASHLIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAINâS EMERGENCY FLASHLIGHT IAW EMB AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING B INSPECTION FOUND THE SERVICE DOOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SERVICE DOOR LIGHT LAMP IAW EMB 145 AMM 33-26-05-000-801-A AND 33-26-05-400-801-A, NO FIX. INSPECTED FOUND BROKEN WIRE. REPAIRED PER WIRING MANUAL 20-50-00. THE OPERATIONAL CHECK OF THE LIGHT LAMP WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 3572 THE CREW REPORTED THAT SHORTLY AFTER TAKEOFF THE MASTER WARNING WENT OFF AND THEY RECEIVED A RED "BLD 2 LEAK" EICAS MESSAGE. AN ASSOCIATED CONDITION: RADIOS BECAME SCRATCHY AND UNREADABLE. THE CREW DECLARED AN EMERGENCY AND ELECTED TO RETURN TO SDF. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE "O" RINGS AT BLEED SYSTEM 2 JOINT 18 IAW AMM CH 36-11-10. NO LEAKS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING B INSPECTION FOUND THE RIGHT AFT OVERWING EMERGENCY MARKED IN CABIN DID NOT ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 5 AC/DC INVERTER IAW EMB AMM 33-50-11. THE OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM AND RIGHT AFT OVERWING CABIN EMERGENCY MARKER GOOD IAW EMB AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 3564 THE CREW REPORTED THAT AFTER THEY RETRACTED THE GEAR AFTER TAKEOFF, THE CREW HEARD REPETITIVE BANGING NOISE AND RIGHT MAIN GEAR CYCLED FROM UP & LOCKED TO IN TRANSITION BACK TO UP & LOCK EVERY 2 MINUTES. CREW TOOK DELAY VECTORS TO BURN OFF GAS - LANDED BELOW MAX LANDING WEIGHT. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED & REPLACED THE RIGHT MAIN LANDING GEAR UPLOCK BOX IAW EMB 145 AMM 32-33-10. PERFORMED OPERATIONAL CHECK OF THE LANDING GEAR. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 3458 THE CREW REPORTED THAT ON LANDING GEAR RETRACTION THEY HAD A CONSTANT BANGING NOISE WITH RIGHT MAIN GEAR LIGHT CYCLING FROM WHITE (UP) TO AMBER (UNSAFE). THE CREW DECLARED AN EMERGENCY AND RETURNED TO MIA. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND ELECTRICAL CONNECTOR BOTTOM ON RIGHT UPLOCK BOX PROX SWITCH LOOSE. RE-INSTALLED IAW EMB 145 AMM 32-33-10 AND C/W EXT AND RETRACTION, THE OPERATIONAL TEST CHECK WAS GOOD IAW EMB 145 AMM 33-30-00. THE AIRCRAFT WAS RETURNED TO SERVICE.
FOR FLIGHT 4078 THE CREW REPORTED THE CAPTAINâS FLASHLIGHT HOLDER WAS BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FLASHLIGHT. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 3207 THE CREW REPORTED THAT IMMMEDIATELY UPON SELECTING ON AIR CONDITIONING A SQUEAL SOUND WAS HEARD FOLLOWED BY AN ELECTRICAL SMOKE SMELL FROM THE NR 2 PACK. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED RIGHT HAND AIR CYCLE MACHINE AND CORECTED ALL DUCT LEAKS IAW EMB-145 AMM 21-51-03. ALL OPS CHECKS AND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED NR 3 EMERGENCY BATTERY AND CHARGER.
DURING MAINTENANCE INSPECTION FOUND THE FIRST OFFICERâS FLASHLIGHT SWITCH BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICERâS FLASHLIGHT IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING B INSPECTION FOUND THE EMERGENCY LIGHT AT ROW 12A INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT OVERWING EMERGENCY LIGHT LAMP AT SEAT 12A IAW EMB 145 AMM 33-50-07-000-801-A AND 33-50-07-400-801-A. THE OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT IS RETURNED TO SERVICE.
FLIGHT 3584, CREW REPORTED IN CRUISE AT FLIGHT LEVEL 370 HAD WING ICE FAIL. TROUBLESHOT PAIR AND PERFORMED AOM VOL 1. NOTHING DETECTED TO FL 210 AND EXITED IN AFTER ABOUT 5 MINUTES ICE DISAPPEARED AND AIRFRAME WAS CLEAR. IAS FLAGGED ASSOCIATED TO PROBE HEAT FAIL AFTER RESET PROCEDURE ENGINE AND STAB ICE RETURNED AND OPERATED NORMALLY WING NEVER WORKED. TURNED BACK, BOTH PFD UNRELIABLE AIRSPEED FOR 30 SEC-1 MIN ACTED LIKE ALTIMETER. DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. DURING INSPECTION, FOUND EXCESSIVE WATER ON PITOT LINES. DRAINED PITOT LINES IAW AMM 34-13-00. PERFORMED PITOT-STATIC PORTS HEATING OPS CHECK IAW AMM 30-31-00. OPS CHECKED GOOD. PERFORMED FUNCTIONAL TEST OF ADC SYSTEM IAW AMM 34-15-00. FUNCTIONAL TEST WAS GOOD AND PERFORMED OPS TEST OF ICE DETECTION SYSTEM IAW AMM 30-80-00. NO FAULTS FOUND. PERFORMED ANTI-ICING SYSTEM OPS CHECK IAW AMM 30-00-00. FOLLOWED FIM TASK 75-41-00-810-803 AND CHECKED WIRES AND CONNECTORS IAW MM 70-00-00. PERFORMED TEST OF ENGINE IAW 72-00-00. OPS CHECKED GOOD. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.
FLIGHT 4314, CREW REPORTED THE FORWARD CABIN FLASHLIGHT BRACKET BROKEN. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE CABIN FLASHLIGHT BASE IAW AMM 33-50-00. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
DURING B-INSPECTION FOUND THE RIGHT SIDE EXIT ROW EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERIVCE. REMOVED AND REPLACED RIGHT SIDE EXIT ROW EMERGENCY LIGHT IAW AMM 33-50-14. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING B-INSPECTION FOUND THE AFT FLASHLIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT FLASHLIGHT IAW EMB AMM TASKS 33-50-16-000-801-A AND 33-50-16-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING TAKEOFF ON FLIGHT 2704 CREW RECEIVED WING ANTI-ICE FAIL CAUTION MESSAGE. ON DESCENT CREW FOLLOWED AOM PROCEDURE WING ANTI-ICE FAIL CAUTION RETURNED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED RIGHT WING ANTI-ICE LOW PRESSURE SWITCH IAW AMM#30-11-02. DID NOT SOLVE THE PROBLEM TRANSFERRED TO ITEM 2 SAME LOG PAGE REMOVED AND REPLACED THE RIGHT WING ANTI-ICE VALVE IAW EMB 145 MM CH 30-10-01 OPERATIONAL CHECKS GOOD. THE AIRCRAFT RETURN TO SERVICE.
DURING MAINTENANCE RIGHT EMERGENCY EXIT CATCHES AT THE TOP. THE AIRCRAFT WAS REMOVED FROM SERVICE. ADJUSTED RIGHT EMERGENCY EXIT HATCH COVER IAW EMB 145 AMM 25-23-03. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE BASE VISIT FOUND THE RIGHT WING RIB 5 CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED RIGHT WING RIB 5 IAW EO EM-57MR-595. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE INSPECTION, FOUND THE LEFT ENGINE FORWARD LOWER MOUNT YOKE CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED CRACKED MOUNT, PREPPED AND INSTALLED SERVIABLE MOUNT IAW AEA EO EM-53MR-386. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING B-INSPECTION FOUND THE NR 4 AND NR 5 EMERGENCY LIGHT STRIP HAS BROKEN WIRES. ALSO FOUND THE EMERGENCY LIGHT ON FORWARD LOWER SERVICE DOOR SHROUD PANEL HAS BROKEN WIRES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 & NR 5 EMERGENCY LIGHT STRIP IAW EMB 145 AMM 33-50-12. REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ON THE FORWARD LOWER SERVICE DOOR SHROUD IAW EMB 145 AMM 33-50-13. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 3591 THE CREW REPORTED THE HYDRAULIC 2 PUMP FAILED/ELEC HYD 2 PUMP OPERATIONAL AT 2800 PSI IN AMBER QTY. THE CREW ELECTED TO DIVERT. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND BROKEN LINE ON ELECTRIC HYD PUMP. REMOVED AND REPLACED THE LINE 29-10-04. LEAK CHECK GOOD. ALSO AFTER RUNNING ELECTRIC PUMP MASS AMOUNT OF SMOKE FROM EXHAUST VENT. REMOVED AND REPLACED PUMP IAW EMB 145 AMM 24-10-04. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE INSPECTION FOUND THE CAPTAINS FLASHLIGHT LED CHARGING LIGHT DOES NOT ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED CAPTAINS FLASHLIGHT ASSEMBLY IAW EMB-145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
FOR FLIGHT 3358 MAINTENANCE FOUND THE CAPTIONâS FLASHLIGHT LED CHARGING LIGHT DOES NOT ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED CAPTAINâS FLASHLIGHT ASSEMBLY IAW EMB-145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
FOR FLIGHT 4068 MAINTENANCE DISCOVERED THE EMERGENCY LIGHTS WERE LEFT ON OVERNIGHT. ALL OF THE EMERGENCY LIGHT BATTERIES WERE DEAD. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1, 2, 3 AND 4 EMERGENCY BATTERY AND CHARGER IAW WC 33-700-19. PART NUMBERS AND SERIAL NUMBERS FOR NR 1: 2013-1A, 71097, BA50933901, CO1622. PART NUMBERS AND SERIAL NUMBERS FOR NR 2: 2013-1A, 84695,BA509333901, CO2469. PART NUMBERS AND SERIAL NUMBERS FOR NR 3: 2013-1A, 109778,BA509333901, CO2464 .PART NUMBERS AND SERIAL NUMBERS FOR NR 4: 2013-1A, 109789,BA509333901, CO2639. THE OPERATIONAL CHECK GOOD WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 2815 DURING THE CLIMB THE CREW REPORTED A STRONG ELECTRICAL ODOR IN THE COCKPIT AND FORWARD PORTION OF AIRCRAFT. NO VISUAL SMOKE WAS NOTED. THE CREW ELECTED TO RETURN TO DFW. THE AIRCRAFT LANDED WITHOUT INCIDENT. PERFORMED INSPECTION OF ALL ITEMS IN COCKPIT. FOUND THE NR 1 FLIGHT MANAGEMENT SYSTEM CONTROL DISPLAY UNIT OVERHEATING AND FIRST OFFICERâS FLASHLIGHT HAD ELECTRICAL BURNT SMELL. REMOVED AND REPLACED THE CAPTAINS CONTROL DISPLAY UNIT P/N OFF 1117-11 S/N OFF: 1210. REMOVED AND REPLACED THE FIRST OFFICERS FLASHLIGHT P/N OFF: P2-07-0009-520. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 3656 THE CREW REPORTED THE NR 1 MAIN LANDING GEAR FAILED TO SHOW UP AND LOCKED. AMBER IN TRANSIT INDICATION STAYED ON UNTIL THE RED LANDING GEAR LEVER DISAGREE WARNING ACTIVATTED. RECEIVED 3 DOWN GREEN WHEN SELECTED DOWN DISAGREE MESSAGE EXTINGUISHED. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR UPLOCK BOX IAW EMB AMM 32-33-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 3252 THE CREW REPORTED A SPOILER FAIL MESSAGE ON EICAS WITH THE SPOILER OPEN INDICATION WITH NO NOTICEABLE ACTUAL DEPLOYMENT IN FLIGHT. THE CAPTAIN DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. TESTED LEFT AND RIGHT INBOARD PROXIMITY SWITCHES AND OPERATED NORMALLY. REMOVED AND REPLACED THE SPOILER CONTROL UNIT IAW EMB 145 AMM 27-63-0. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE BASE VISIT FOUND THE LEFT PYLON PROFILE TO HAVE CRACKS. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED REPAIR ON THE LEFT PYLON PROFILE IAW EO EM-54MR-312. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING THE MAINTENANCE BASE VISIT FOUND THE RIGHT OMEGA BEAM AT FRAME 25 TO BE CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE RIGHT OMEGA BEAM AT FRAME 25 IAW EMB 145 SRM 53-00-10 FIGURE 203 SHEET 1. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 2735 THE CREW ABORTED THE TAKEOFF AT THE START OF THE TAKE OFF ROLL DUE TO EXCESSIVE SMOKE IN THE COCKPIT AND FRONT OF CABIN. THE AIRCRAFT RETURNED TO THE GATE WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED AN OPERATIONAL CHECK OF BOTH ENGINES IAW ETN EM-72-034R4. NO SMOKE OR SMOKE SMELL WERE FOUND. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 3526 DURING CRUISE THE CREW REPORTED THE RUDDER SYSTEM 1-2 INOPERABLE IN FLIGHT. SYSTEM 1 ACTIVATED WHEN NR 2 SYSTEM WAS SHUTOFF PER CHECKLIST. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 SYSTEM RUDDER PRESSURE SWITCH IAW AMM 27-23-04. OPERATIONAL CHECK WAS GOOD AND NO LEAKS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 3579 ON DESCENT THE CAPTAIN REPORTED THAT WHEN SELECTING FLAPS 9, RECEIVED A FLAP FAIL MESSAGE IMMEDIATELY. THE FLAPS DID NOT MOVE FROM THE ZERO POSITION. THE CAPTAIN DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. IT WAS NOT AN OVERWEIGHT LANDING. AFTER LANDING THE MESSAGE CLEARED PRIOR TO ARRIVING AT THE GATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RESET FLAPS AND PERFORMED FLAP CONTROL SYSTEM OPERATIONAL CHECK IAW AMM 27-51-00. NO PARTS REMOVED OR PLACED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 3956, CREW REPORTED ELECTRICAL BURNING ODOR AT GATE FROM COCKPIT. AIRCRAFT REMOVED FROM SERVICE. OPERATED ELECTRICAL SYSTEM AND WINDSHIELD HEAT IAW AMM 30-43-00. COULD NOT DUPLICATE. AIRCRAFT RETURNED TO SERVICE.
ON FLIGHT 4431 - CREW REPORTED ON THE GROUND, LT WING TANK FUEL CAP CAME OPEN IN FLIGHT. FUEL CAP WAS ONLY SECURED BY THE LANYARD. CREW ELECTED TO RETURNED TO THE FIELD. AIRCRAFT REMOVED FROM SERVICE. COMPLIED WITH FUEL CAP SEAL INSPECTION. RE-INSTALLED CAP, NO DEFECTS NOTED. INSPECTED SURROUNDING AREAS. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (A)
ON FLIGHT 4431, CREW REPORTED ON THE GROUND. LT WING TANK FUEL CAP CAMEO OPEN IN FLIGHT. FUEL CAP WAS ONLY SECURED BY THE LANYARD. CREW DECLARED AN EMERGENCY AND ELECTED TO RETURN TO THE FIELD. AIRCRAFT REMOVED FROM SERVICE. COMPLIED WITH FUEL CAP SEAL INSPECTION. RE-INSTALLED CAP, NO DEFECTS NOTED. INSPECTED SURROUNDING AREAS. NO DEFECTS NOTED AIRCRAFT RETURNED TO SERVICE. (A)
EMERGENCY LIGHTS INOPERATIVE DUE TO SWITCH LEFT IN ARM POSITION. REMOVED AND REPLACED BATTERY PACKS 1 THRU 4 IAW EMB AMM 33-50-04. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
BURNING SMELL IN CABIN WITH APU AND NUMBER ONE ENGINE RUNNING, FOUND BUGS IN APU INLET. CLEANED BUGS FROM APU INLET IAW EMB AMM. OPERATIONAL CHECK GOOD WITH NO SMELL DETECTED, RETURNED AIRCRAFT TO SERVICE.
DURING DEBOARDING NOISE HEARD FROM OUTSIDE OF AIRCRAFT FOLLOWED BY A SLIGHT SMOKE SMELL IN CABIN WITH APU AND NUMBER TWO PACK OPERATING, FOUND NUMBER TWO PACK SEIZED. REMOVED AND REPLACED NUMBER TWO PACK IAW EMB AMM 21-51-03. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.
DURING OVERNIGHT MAINTENANCE, CARGO DOOR AFT UPPER CORNER OF SKIN WAS FOUND CRACKED. REPLACED CARGO DOOR ASSEMBLY IAW EMB AMM 52-30-01 AND 52-31-00. AIRCRAFT WAS RETURNED TO SERVICE. (M)
EN ROUTE TO LIT AIRCRAFT EXPERIENCED DUAL PITCH TRIM FAILURE. AIRCRAFT LANDED SAFELY WITH NO FURTHER INCIDENTS. REPLACED HORIZONTAL STABILIZER CONTROL UNIT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
ABI - A 12 INCH BY 8.5 INCH DOUBLER FROM A PREVIOUS REPAIR WAS REMOVED FOR EVALUATION DUE TO PROXIMITY OF AN ADDITIONAL DENT AT FRAME 64 STRINGER 20L. RECONTOURED THE ADDITIONAL DENT AND PERFORMED AND EDDY CURRENT INSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED A NEW REPAIR DOUBLER, FILLER. REPAIR DONE IAW EMB REPAIR STATEMENT IC2004-145/4345 PARA 3 DATED SEPT 16, 2004. (M)
ABI - DURING AN MBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVD THE EXISTING CENTER SILL AND INSTALLED NEW SILL IAW EMB 145 SRM, SRM 145/1142 REV 27, CHAPTER 51-20-01-51-20-03, 51-40-02, 51-40-04 AND 51-40-06. (M)
ON CLIMB-OUT CREW NOTICED YELLOW TAB INDICATING CAPTAINS DV WINDOW OPENED. CREW RETURNED TO FIELD WITH NO FURTHER INCIDENT. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECK OF WINDOW WITH NO DEFECTS NOTED. LOCKED WINDOW AND RETURNED AIRCRAFT TO SERVICE. (M)
CREW HAD A DUAL PITCH TRIM FAILURE DURING DESCENT AT 210 KTS AND ALT OF 6,000 FT. FLAPS WERE AT 9 AND SPEED BRAKES WERE BEING DISENGAGED. REPLACED HSCU IAW MFG AMM. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (SW21200406970)
ORF - FLT 4025 - CREW REPORTED A BLEED LEAK MESSAGE ON EICAS DURING CRUISE FLIGHT. CAPTAIN DECLARED AN EMERGENCY AND CONTINUED TO ORF AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND A LOOSE V-BAND CLAMP IN THE AFT AVIONICS COMPARTMENT. CLAMP WAS TIGHTENED AND OPERATIONAL CHECK WAS COMPLIED WITH. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M)
CREW REPORTED A BRIGHT FLASH AT CAPTAINS WINDOW FOLLOWED BY AN ELECTRICAL SMOKE SMELL, LOSS OF NUMBER 4 GENERATOR. NUMBER 2 COMM, AND FMS SCREEN. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED WITHOUT FURTHER INCIDENTS. MAINTENANCE COMPLIED WITH A LIGHTENING STRIKE INSPECTION. GENERATOR WAS REPLACED. NUMBER 2 ICU WAS REPLACED, WHICH FIXED THE SMOKE SMELL. AIRCRAFT WAS RETURNED TO SERVICE.
DURING AN IMBV INSPECTION FOUND CORROSION ON GALLEY CENTER FLOOR BEAM. REMOVED CORRODED GALLEY CENTER BEAM. INSTALLED NEW FLOOR BEAM IAW SRM AND STANDARD SRM PRACTICES.
DURING IMBV INSPECTION FOUND CORROSION ON GALLEY RIGHT HAND FLOORBEAM. REMOVED CORRODED GALLEY RT BEAM. INSTALLED NEW BEAM IAW STANDARD SRM PRACTICES.
DURING IMBV INSPECTION, FOUND CORROSION ON FORWARD DIGITAL REMOVED CORROSION BY CUT OUT. FABRICATED A REPLACEMENT STRAP, TWO DOUBLERS. REPAIR DONE IAW STANDARD SRM PRACTICES.
DURING AN IMBV INSPECTION FOUND CORROSION ON SERVICE DOOR CENTER SILL. REMOVED CORROSION BY BLENDING. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW GST.
DURING IMBV INSPECTION FOUND CORROSION ON LEFT HAND BEAM AT FRAME 20. REMOVED CORROSION BY CUT OUT. FABRICATED A DOUBLER ANGLE, PLATE, FILLER, AND SHIMS. REPAIR DONE IAW AND STANDARD SRM PRACTICES.
DURING AN IMBV INSPECTION FOUND CARGO DOOR LOWER SILL CORRODED BEYOND SRM LIMITS. REMOVED CORRODED SILL. INSTALLED NEW BEAM IAW SRM.
ABI - THIS IS A LEVEL 2 FINDING. LEFT GALLEY FLOOR SILL BETWEEN FRAMES 19 AND 23 CORRODED. DAMAGE WAS BLENDED OUT AND NDT WAS PERFORMED WITH NO DEFECTS FOUND ACCEPTED AS IS IAW EMB GST-1895/02. (M)
ABI - THIS IS A LEVEL 2 FINDING, FORWARD DIAMOND GUSSET CORRODED. REMOVED AND INSTALLED SERVICEABLE FORWARD DIAMOND GUSSET IAW EMB 145 SRM 51-40-02. (M)
ABI - THIS IS A LEVEL 2 FINDING. PROFILE AT FRAME 23 CORRODED. REMOVED CORRODED PROFILE ANGLE AND INSTALLED SERVICEABLE PROFILE IAW EMB 145 SRM 51-40-02. (M)
ABI - THIS IS A LEVEL 2 FINDING, AFT DIAMOND GUSSET CORRODED. REMOVED AND INSTALLED SERVICEABLE AFT DIAMOND GUSSET IAW EMB 145 SRM 51-40-02. (M)
ABI - THIS IS A LEVEL 2 FINDING, LEFT FORWARD LOWER SEAT TRACK CORRODED. REMOVED AND INSTALLED SERVICEABLE LEFT FORWARD INBOARD SEAT TRACK IAW EMB 145 AMM 53-01-06. (M)
DURING AN IMBV INSPECTION FOUND STRINGER 19L CHAFED BETWEEN FRAMES 52 AND 53. BLENDED CHAFE. PERFORMED NDT INSPECTION NO DEFECTS. FABRICATED A DOUBLER ANGLER, AND TWO SHIMS. REPAIR DONE IAW STANDARD SRM PRACTICES.
DURING AN IMBV INSPECTION FOUND STRINGER 19R CHAFED BETWEEN FRAMES 52 AND 53. BLENDED AREA, PERFORMED NDT INSPECTION NO DEFECTS. FABRICATED A DOUBLER ANGLE, AND TWO SHIMS. REPAIR DONE IAW STANDARD SRM PRACTICES.
DENT FORWARD OF FRAME 18 BELOW STRINGER 20L. .013 X 2.0 X 1.7 (SUP) DENT ACCEPTED AS IS IAW MFG GST.
ABI - PASSENGER DOOR FORWARD LOWER EDGE IS GOUGED. PERFORMED EDDY CURRENT INSPECTION, NO DEFECTS. GOUGE ACCEPTED AS IS IAW EMB GST-1895/02. (M)
DENT INBOARD OF RIGHT WIPER MOTOR ARM. THREE DENTS ACCEPTED AS IS IAW MFG GST.
DENT AFT FRAME 19 BELOW STRINGER 13L. .006 X 2.5 X 1.1. (SUP) DENT ACCEPTED AS IS IAW MFG GST.
DENT IN PASSENGER DOOR ABOVE WINDOW, .006 X 1.0 X 1.1. (SUP) DENT ACCEPTED AS IS IAW MFG GST.
DENT ON FRAME 9 BELOW STRINGER 15R .005 X .7 X 1.0. SUP, DENT ACCEPTED AS IS IAW MFG GST.
CARGO DOOR NEAR MIDDLE HAS 3 DENTS 1).006 X 1.3 X 1.0 2).009 X 1.3 X 1.8 3) .003 X .3 X .5. (SUP) THREE DENTS FOUND TO BE WITHIN MFG SRM LIMITS.
ORD - FLT 4382 - CREW REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHTS AT ROWS 10 AND 11 TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT STRIP IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)
DFW - FLT 3759 - CREW REPORTED A NR 2 HOT BRAKE INDICATION ON TAKEOFF ROLL. TAKEOFF WAS ABORTED AND AIRCRAFT WAS RETURNED TO THE GATE. MAINTENANCE REMOVED AND REPLACED THE LEFT INBOARD BRAKE TEMP SENSOR IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)
ABI - FLT 3502 - EMERGENCY LIGHT AFT OF GALLEY DOES NOT ILLUMINATE. REMOVED AND REPLACED ASSOCIATED EMERGENCY BATTERY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
GRR - FLT 3796 - BAGGAGE SMOKE WARNING CAME ON. DEPLOYED FIRE BOTTLE. VERIFIED EVENT AS A FALSE WARNING. REMOVED AND REPLACED FORWARD AND AFT SMOKE DETECTORS IN THE AFT BAGGAGE COMPARTMENT. OPERATIONAL CHECK GOOD. REF: OPER CONTROL NR 99ZZZX4083. (X)
GRR - FLT 3796 - BAGGAGE SMOKE WARNING CAME ON. DEPLOYED FIRE BOTTLE. VERIFIED EVENT AS A FALSE WARNING. REMOVED AND REPLACED FORWARD AND AFT SMOKE DETECTORS IN THE AFT BAGGAGE COMPARTMENT. OPERATIONAL CHECK GOOD. REF: OPER CONTROL NR SIMA992593.