N650AE
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 |
|---|---|---|---|
| PIEDMONT AIRLINES (HNAA) | Operator | 2021-03-28 – 2021-03-28 | Operator named in NTSB report |
| Piedmont Airlines | Operator | 2021-03-28 – 2021-03-28 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
NOSE GEAR SHAKING AT 115KNTS (PRIOR TO ROTATION) CLEANED AND GREASED NOSE GEAR TORQUE LINKS IAW AMM 32-34-00. OK FOR SERVICE. LG AIR/GND FAIL AFTER TAKEOFF (MSG CLEARED ON LANDING) FACT 01MAY26 11:32 ALB ADJUSTED NOSE GEAR PROX SWITCH TARGET IAW AMM 32-63-05. OPS CHECK GOOD.
AT ABOUT 85 TO 90 KTS, BRAKE OVER HEAT EICAS MESSAGE WITH LEFT INBD BRAKE INDICATION HIGHER. ON GROUND LEFT INBD TEMP FLUXUATES MEL 10AUG25 12:12 PHL C22214 32-2-2 BRAKE TEMPERATURE INDICATIONS FACT 12AUG25 12:37 SBY RAR BRAKE TEMP SENSOR #200 IAW AMM 32-47-01. OPS CHECK GOOD.
AT LEAST TWO LIGHTNING STRIKES IN FLIGHT, FLIGHT CREW AND CABIN BOTH REPORTED ELECTRICAL FUMES. (NO LOSS OF AVIONICS, NO EICAS MSGS) FACT 15MAY25 03:04 PHL PERFORMED LIGHTNING STRIKE INSPECTION IAW AMM REF. 05-50-01 AND FOUND NO DEFECTS NOTED AT THIS TIME. A/C OKAY FOR SERVICE.
AT LEAST TWO LIGHTNING STRIKES IN FLIGHT FLIGHT CREW AND CABIN BOTH REPORTED ELECTRICAL FUMES(NO LOSS OF AVIONICS, NO EICAS MSGS) FACT 15MAY25 03:04 PHL PERFORMED LIGHTNING STRIKE INSPECTION IAW AMM REF. 05-50-01 AND FOUND NO DEFECTS NOTED AT THIS TIME. A/C OKAY FOR SERVICE.
ON DESCENT BURNING SMELL NOTICED IN FLT DECK FOR APROX 1 MIN BEFORE SMELL DISSIPATED. DU 4 O/H MSG DISPLAYED FOR APROX 3SECS. ENGINE BLEEDS AND PACK NORMAL OPERATION FACT 13FEB25 09:12 CLT R/R DISPLAY UNIT 4 IAW AMM 34-22-01. EFIS OPS CHECK GOOD. NO ABNORMAL SMELLS NOTED. AIRCRAFT GOOD FOR SERVICE.
E2 THRUST REVERSER REVERSE DISAGREE REJECTED TAKE OFF 80 KNOTS. FACT 04DEC24 05:21 PHL COULD NOT DUPLICATE. R/R RELAY K0378 K0264 K0400 IRW AMM 20-13-02 FOR POSITIVE MAINTENANCE. OPS CHECK GOOD IRW AMM 78-31-01. OK FOR SERVICE AT THIS TIME.
CLIMBING THROUGH 3000FT HEARD A BANG AND NO. 1 ENGINE SUDDENLY FAILED. LOST ITT INDICATION. N1 CONTINUED TO SPIN AT 13 PRESENT. OIL PRESSURE ZERO. FACT 04NOV24 08:34 PHL R/R #100 ENGINE PER W/C 71-00-00
00153 L/H STUB FRAME ABOVE WINDSHIELD POST CRACK AT LOWER CORNER. RAR L/H STUB FRAME PN: 123-07751-005 ABOVE WINDSHIELD POST IAW EMB 145 SRM 51-40-02
00154 R/H STUB FRAME ABOVE WINDSHIELD POST CRACK AT LOWER CORNER. RAR R/H STUB FRAME PN: 123-07751-006 ABOVE WINDSHIELD POST IAW EMB 145 SRM 51-40-02
00161 RH FLOOR SILL IS CORRODED AT FS. 20. REPAIRED IAW PIEDMONT EO1-53-24-0320.
00139 CENTER FUSELAGE I - SMALL DENT LOCATED AFT OF MAIN DOOR REQUIRES PERMANENT REPAIR. PAIRED PERMANENTLY ON CENTER FUSELAGE 1 - SMALL DENT LOCATED AFT OF MAIN DOOR IAW EMB 145 SRM 53-21-01
00105 TOP RH AFT CORNER OF RUDDER 1 DAMAGED. REMOVED DAMAGE IAW EMB 145 51-10-05 STEP #3 DAMAGE DID NOT PENETRATE CLAD LAYER.
00105 CENTER FUSELAGE I - SMALL DENT LOCATED AFT OF MAIN DOOR REQUIRES PERMANENT REPAIR. REPAIRED PERMANENTLY ON CENTER FUSELAGE 1 - SMALL DENT LOCATED AFT OF MAIN DOOR IAW EMB 145 SRM 53-21-01
DURING CLIMB AT 16,000 FT F/A REPORTED LOUD AIR RUSHING NOISE AND BURNING SMELL. FACT 09MAY23 00:57 CLT R&R RECIRC FAN #1 IAW AMM 21-24-01 (SHORT SIGN) R&R FUSE F0059 AND CONTACTOR K0189. FAN BLEW NEW FUSE. SEE LP 286540-1 FOR FUSE REPLACEMENT AND FAN OPS CHECK
LOUD NOISE FROM NLG AREA FLY BY TOWER SHOWED NLG DOOR OPEN. UNSURE OF NLG POSITION. FLIGHT WAS AT 310K WHEN NOISE ORIGINATED. HISTORY: NO FACT 25APR23 16:38 MDT R&R NLG DOOR SOLENOID VALVE OPS CHECK GOOD. OK FOR SERVICE. REF AMM 32-33-02.......NOTE: FAULT DUPLICATED ON GROUND MULTIPLE TIMES AND ONCE REPAIRED. OPS CHECK GOOD MULTIPLE TIMES
MDIS 650 26-15 2594831 18FEB22 RIC CLOSE BAGGAGE BAY FIRE PUSHBUTTON DOES NOT ILLUMINATE WHILE PRESSING FIRE DET PUSH BUTTON FACT 18FEB22 08:49 RIC R+R'D #200 BAG BAY SMOKE DETECTOR IN REF. TO AMM TASK 26-15-01-000/400-801-A OPS CHECK GOOD OK FOR SERVICE
PDIS 650 78-30 2594602 24JAN22 CHO CLOSE E2 REV DISAGREE MSG ON EICAS DURING TAKEOFF ROLL FACT 26JAN22 16:45 ROA REMOVED AND REPLACED #2 THRUST REVERSER ASSY PER W/C 78-31-01. REMOVED AND REPLACED WIRING HARNESS W408 PER AMM 78-35-01. SEE HA-300 SEQ# 4, 9 & 10 FOR SIGN OFFS. OPS & LEAK CHECKS GOOD, CLEAR MEL. RE-ACTIVATED #2 T/R PER AMM 78-31-01. P/N ON/OFF 145-77751-615 S/N ON TR0360, S/N OFF TR136.
PDIS 650 78-33 2598492 12JAN22 CLT ASSGN ENG 2 REV DISAGREE ON TAKE OFF ROLL. 31933 00 AKR HISTORY: . MEL 12JAN22 19:07 CLT C01206 78-2 ENG 1(2) REV DISAGREE MESS CURRENTLY ON THE MEL R&R RELAY K0640 AS REQ OPS CHECK GOOD NO CMC OR EICAS MSG OK FOR SERVICE AT THIS TIME.REACTIVATED #2 T/R.NO FADEC MSG.
PDIS 650 78-33 2598471 10JAN22 PHL CLOSE ENG 2 REV DISAGREE ON TAKEOFF ROLL FACT 11JAN22 07:10 PHL REMOVED AND REPLACED #2 TR ICU IAW AMM 78-33-01 OPS CHECK LEAK CHECK GOOD OK FOR SERVICE
E893076 - CENTER CABIN FLOOR BEAM SEAT TRACK #3 IS CORRODED ... REMOVED CORRODED SEAT TRACK AND INSTALLED SERVICEABLE CENTER SEAT TRACK #3 IAW EMB 145 AMM 53-01-06
E893014 - CORROSION ON LH OTBD #5 SEAT TRACK ... REMOVED AND REPLACED LH OTBD #5 SEAT TRACK IAW EMB 145 AMM 53-01-06
E893012 - CORROSION ON LH OTBD #6 SEAT TRACK ... REMOVED CORROSION ON LH OUTD #6 SEAT TRACK IAW EMB145 SRM 51-10-03, FOUND TO BE OUTSIDE ALLOWABLE LIMITS IAW EMB145 SRM 53-00-11. CALIPERS EASI# 7496. REMOVED AND INSTALLED SERVICEABLE LH OTBD #6 SEAT TRACK IAW EMB 145 53-01-06.
E892969 - CORROSION ON RH OTBD #1 SEAT TRACK ... REMOVED AND REPLACED R/H OUTBD #1 SEAT TRACK IAW EMB 145 AMM 53-01-06, REINSTALLED RISER DUCT BETWEEN FR 29 AND FR 30 AFTER MTX IAW EMB 145 AMM 21-20-04
E892968 - CORROSION ON RH OTBD #2 SEAT TRACK ... RAR RH OTBD #2 SEAT TRACK DUE TO CORROSION IAW EMB-145 AMM 53-01-06.
E892967 - CORROSION ON RH OTBD #3 SEAT TRACK ... RAR RH OUTBD #3 SEAT TRACK IAW EMB 145 AMM 53-01-06. TORQUE WRENCH #4401
E892937 - RH AILERON INBD HINGE ATTACHMENT BOLT HOLE GOUGED ... REMOVED AND INSTALLED SERVICEABLE RH AILERON INBD HINGE FITTING IAW EMB145 SRM 51-40-02 AND ETD2021-145-040901 AND PIEDMONT EO1-05-21-0365.
E892915 - LH FLOOR SEAT TRACK PITTED BETWEEN FR29-30 ... REMOVED AND REPLACED LH FLOOR SEAT TRACK AT FR 29-30 IAW EMB 145 AMM 53-01-06. TQW USED EASI# 4401.
E892912 - LH CABIN #3 FLOOR SILL CORRODED. ... RAR LH #3 CABIN FLOOR SILL IAW EMB 145 SRM 51-40-02
E892911 - LH CABIN #2 FLOOR SILL CORRODED ... REMOVED AND REPLACED LH CABIN #2 FLOOR SILL IAW EMB 145 SRM 51-40-02
E892910 - RH CABIN #2 FLOOR SILL CORRODED ... REMOVED AND REPLACED RH CABIN #2 FLOOR SILL IAW EMB 145 SRM 51-40-02
E892909 - RH CABIN #1 FLOOR SILL CORRODED. ... RAR RH CABIN #1 FLOOR SILL IAW EMB1145 SRM 51-40-02
E892893 - CARGO DOOR SILL CORRODED ...REMOVED DRILLED AND INSTALLED SERVICEABLE CARGO DOOR LRW CENTER SILL IAW EMB 145 SRM 51-20-03 AND SRM 51-40-02.
E892891 - FR 68 SHEAR CLIP CRACKED BETWEEN STGRS 06L/07L .... COMPLETED INSTALLATION OF SHEAR CLIPS REPAIR FOR FR 68 BETWEEN STGRS 06L/07L IAW EMB 145 SRM 53-31-04-RE, ITEM #2 AND TABLE 203 AND TABLE 205 AND PIEDMONT EO1-53-21-0367.
E892890 - CARGO FR 68 GOUGED AT NUTPLATE HOLES (6EA) BETWEEN STGRS 01L/08L .... INSTALLED 3 EA DOUBLER REPAIRS FOR FR 68 NUTPLATE REPAIR POSITION #3, #4 AND #6 IAW ETD2021-145-042792 REV. B AND PIEDMONT EO1-53-21-0366.
E892866 - R/H WING RIB 21 IS CRACKED. ... COMPLETED FABRICATION, POSITIONING, AND DRILLING OF REPAIR DOUBLER, FILLER, AND SHIM FOR RH WING RIB 21 REPAIR IAW EMB145 SRM 57-20-07 AND PIEDMONT EO1-57-21-0358
E892865 - L/H WING RIB 21 IS CRACKED ...INSTALLED SERVICEABLE REPAIR DOUBLER, FILLER, AND SHIM ON LH WING RIB 21 IAW EMB145 SRM 57-20-07 AND PIEDMONT EO1-57-21-0357.
E892657 - BAGGAGE DOOR WEBBING IS GOUGED 5 EACH ONE ON PREVIOUS REPAIR ... NO. 4 AND 5 GOUGES FOUND TO BE WITHIN ALLOWABLE LIMITS, MATERIAL REMAINING AFTER BLEND OUT IAW EMB 145 SRM 52-30-01. REPAIRED 1, 2 AND 3 DOUBTERS ON CARGO DOOR INNER WEB IAW ETD2021-145-041226 AND PIEDMONT EO1-52-21-0353
E892626 - DENT ON BAGGAGE DOOR LOWER FRAME ... UPON FURTHER INVESTIGATION FOUND DENT TO BE ON BAGGAGE DOOR LOWER OUTBD "L" PROFILE. RAR "L" PROFILE ON LOWER BAGGAGE DOOR IAW EMB 145 SRM 51-40-02
E892012 - LH SIDE FUSELAGE SKIN HAS POSSIBLE CRACKS AROUND FASTENERS ON FRAME 79 (1) EA ... REPAIRED LH SIDE FUSELAGE SKIN AROUND FASTENERS ON FRAME 79 (1) EA IAW EMB 145 SRM 53-32-01-RE, ITEM 9, FIG 213 AND PIEDMONT EO1-53-21-0360.
E891811 - LIGHTNING STRIKE ON FUSELAGE SKIN AT FR 26-27 AND STR 17R-16R ... ACCOMPLISHED RIVET REPAIR OF LIGHTNING STRIKE ON FUSELAGE SKIN AT FR 26-27 AND STR 17R-16R IAW EMB 145 SRM 53-00-01 ITEM 2B AND PIEDMONT EO1-53-21-0368.
E891808 - LIGHTNING STRIKE ON FUSELAGE SKIN AT FR 24-25 AND STR 17R-18R ... PERFORMED REPAIR ON FUSELAGE SKIN AT FR 24-25 AND STR 17R-18R. IAW EMB 145 SRM 53-22-01 FIG 204 SHEET 1 AND PIEDMONT EO1-53-21-0369.
E893519 - CORROSION ON LH OTBD #1 SEAT TRACK - RAR LH OUTBD#1 SEAT TRACK IAW EMB 145 AMM 53-01-06
E892916 - RH FLOOR SEAT TRACK PITTED BETWEEN FR27-28 ... RAR RH FLOOR SEAT TRACK IAW EMB 145 AMM 53-01-06.
E893576 - LH AILERON TO DAMPER FITTING OTBD HAT BUSHING MIGRATED ... RAR LH AILERON DAMPER FITTING IAW EMB 145 SRM 51-40-02, ETD2021-145-041146 AND PIEDMONT EO1-05-21-0365
E893017 - CORROSION ON LH OTBD #3 SEAT TRACK ... RAR LH OTBD #3 SEAT TRACK IAW EMB 145 AMM 53-01-06
E895330 - LH PLYON YOKES SPAR II UPPER FLANGE FASTENER HOLE PREVIOUSLY OVERSIZED ... ACCOMPLISHED REPAIR OF LH PYLON YOKE SPAR II UPPER FLANGE FASTENER HOLE IAW ETD# ETD-2021-145-042799 REV. A. AND PIEDMONT EO1-54-21-0364
E894729 - #3 R/H OVER WING BRACKET HAS MISSED DRILLED HOLE ON SKIN BETWEEN FR 49-50 STRINGER 14R-13R ... REPAIRED #3 R/H OVER WING BRACKET HOLE ON SKIN BETWEEN FR 49-50 STRINGER 14R-13R BY INSTALLING BUSHING IAW ETD2021-145-042169 AND PIEDMONT EO1-53-21-0354.
E893647 - FR 73 CRACKED AT STR 17R ... REMOVED AND REPLACED FR-73 (LWR SECTION) IAW EMB 145 SRM 51-40-02.
E893582 - RH AILERON TO DAMPER FITTING LUG WORN ... REMOVED AND INSTALLED SERVICEABLE RH AILERON DAMPER FITTING IAW EMB145 SRM 51-40-02 AND ETD2021-145-041149 AND PIEDMONT EO1-05-21-0365
E893451 - FUSELAGE SKIN IS CRACKED BETWEEN FR 80-81 NEAR STR 13R ... COMPLETED REPAIR OF FUSELAGE SKIN BTW FR 80-81 STGR 13R-15R IAW ETD# ETD2021-145-041044 AND PIEDMONT EO1-53-21-0356.
E893326 - RH FUSELAGE DRAG ANGLE FWD SECTION AFT AREA HAS POSSIBLE CRACKS AT FASTENER HOLE AREAS MARKED ... COMPLETED INSTALLATION OF SERVICEABLE FWD DRAG ANGLE, AND PREVIOUS REPAIR ANGLE AND SHIMS AT FRAME 75 STRINGER 2R IAW EMB145 SRM 51-40-02, 53-31-01 ITEM 11, FIGURE 219, SHEETS 1-2 AND PIEDMONT EO1-53-21-0372.
E893075 - L/H CABIN FLOOR BEAM SEAT TRACK #4 IS CORRODED ... RAR L/H CABIN FLOOR BEAM SEAT TRACK #4 IAW EMB 145 AMM 53-01-06
E893073 - L/H FLOOR BEAM SEAT TRACK GUESSET #4 IS CORRODED ... REMOVED AND REPLACED L/H FLOOR BEAM SEAT TRACK GUSSET #4 IAW EMB-145 SRM 51-40-02.
E893072 - CENTER FLOOR BEAM SEAT TRACK GUESSET #3 IS CORRODED. ... REMOVED AND INSTALLED SERVICEABLE CENTER FLOOR BEAM SEAT TRACK GUSSET #3 IAW EMB145 SRM 51-40-02.
E893071 - L/H CABIN FLOOR SILL #4 IS CORRODED ... RAR LH #4 CABIN FLOOR SILL IAW EMB 145 SRM 51-40-02
E893044 - CORROSION IN GALLEY AREA ON CROSS FLOOR BOARD SUPPORT AT FRAME 19 ... REMOVED AND REPLACED CROSS FLOOR BOARD SUPPORT AT FRAME 19 IN GALLEY AREA IAW EMB145 SRM 51-40-02.
E893043 - CORROSION IN GALLEY AREA ON HAT BEAM AT FRAME 18 PREVIOUS REPAIR ... ACCOMPLISHED REPAIR DOUBLER ON R/ H HAT BEAM AT FRAME 18 IAW ETD2021-145-041321 AND PIEDMONT EO1-53-21-0348.
E893042 - CORROSION ON PASSENGER DOOR ENTRY AFT FLOOR BOARD SUPPORT ... REMOVED DAMAGED SUPPORT AND INSTALLED SERVICEABLE PASSENGER DOOR ENTRY AFT FLOOR BOARD SUPPORT IAW EMB 145 SRM 51-40-02.
E893041 - CORROSION ON PASSENGER DOOR ENTRY FWD FLOOR BOARD SUPPORT ... REMOVED DAMAGED SUPPORT AND INSTALLED SERVICEABLE PASSENGER DOOR ENTRY FWD FLOOR BOARD SUPPORT IAW EMB 145 SRM 51-40-02.
E893033 - CORROSION IN GALLEY AREA ON CENTER GUSSET AT FRAME 22 ... REMOVED AND REPLACED CENTER GUSSET AT FRAME 22 IAW EMB 145 SRM 51-40-02
E893029 - CORROSION IN GALLEY AREA ON SERVICE DOOR CENTER SILL ... INSTALLED INTERNAL DOUBLER AT GALLEY SERVICE DOOR CENTER SILL AT FWD NUTPLATE HOLE IAW EMB 145 SRM 53-21-02 RE, ITEM 2, FIG. 201 AND PIEDMONT EO1-53-21-0362.
E893018 - CORROSION ON LH OTBD #2 SEAT TRACK ... RAR LH OUTBD#2 SEAT TRACK IAW EMB 145 AMM 53-01-06.
E893015 - CORROSION ON LH OTBD #4 SEAT TRACK ... COMPLETED INSTALLATOIN OF LH OUTB #4 SEAT TRACK IAW EMB 145 AMM 53-01-06.
E893034 - CORROSION IN GALLEY AREA ON CROSS BEAM AT FRAME 20 ... REMOVED CORRODED CROSSBEAM, DRILLED UP AND INSTALLED NEW FLOOR CROSS BEAM AT FRAME 20 IN GALLEY AREA IAW EMB 145 SRM 51-40-02.
E893062 - L/H CABIN FLOOR SILL #7 IS CORRODED ... RAR CABIN FLOOR SILL #7 IAW EMB 145 SRM 51-40-02.
ON REJECTED T/O EICAS WARNING T/O NO CONFIG APPEARED WITH NO AURAL CALLOUT. T/S PERFORMED FIM TASK 31-51-00-810-804-A BLOCK 1 THROUGH BLOCK 7 R&R RELAY K0212 IAW AMM 20-13-02 OPS CHECK PERFORMED IAW AMM 31-51-00 OPS CHECK GOOD A/C OK FOR SERVICE AT THIS TIME.
HYD SYS 1 LOW QTY IN FLT ( HYD SYS 2 REMAIN FULL) R&R NR 1 ENG DRIVEN PUMP IAW EMB 145 AMM 29-10-03. OPS CHECK GOOD NO FURTHER LEAKS DETECTED A/C OK FOR SERVICE
PDIS 650, 31-41, 13APR21 PHL CLOSE, 300 FEET AFTER ROTATION, EICAS DISPLAY FLASHED BRIGHTLY AND WENT BLANK MOMENTARILY FOLLOWED BY AN ELECTRICAL ODOR. R&R'D EICAS DISPLAY UNIT AS REQUIRED PER AMM 34-22-01-400-801-A, OPS CHECK IAW 34-22-00-700-801A GOOD ON GROUND AT THIS TIME, OK FOR SERVICE.
AFTER T/O FUMES WERE SMELLED, SIMILAR TO A WET MUSTY SOCK ODOR. GROUND RAN AIRCRAFT ENGINE NR 1 AND NR 2 ALSO OPERATIONS CHECKED AIRCRAFT AIR CONDITION SYSTEM. NO DEFECTS OR ABNORMAL SMELLS FOUND, IN REF TO FIM TASK 21-20-00-810-801-A. A/C OK FOR SERVICE.
SPOILER FAIL EICAS MESSAGE DISPLAYED ON TAKE OFF.CW FIM 27-63-00-810-802A STEPS 1-9, DETERMINED TO BE TRANSITORY. R+R SCU IAW 27-63-02 AND 27-63-01 FOR POSITIVE MAIN ACTION . OPS CHECK GOOD. OK FOR SERVICE
SPOILER FAIL EICAS MESSAGE DISPLAYED ON TAKE OFF. CW FIM 27-63-00-810-802A STEPS 1-9, DETERMINED TO BE TRANSITORY. R & R SCU IAW 27-63-02 AND 27-63-01 FOR POSITIVE MAIN ACTION . OPS CHECK GOOD. OK FOR SERVICE.
PDIS 650 21-01 2289391 11FEB20 PHL CLOSE CREW NOTICED FUMES DURING TAKE OFF. THEN WENT AWAY. FUMES CAME BACK IN CRUISE FLIGHT AND GOT STRONGER TH ROUGH DESCENT FACT 11FEB20 18:43 PHL EVALUATION FLIGHT REQUIRED. RAN BOTH PACKS TOGETHER AND SEPERATELY ON FULL COLD AND FULL HOT IN AUTO AND MANUAL MODE. DID SAME SEQUENCE WITH APU BLEED AND ENGINE BLEED. RAN HYD PUMPS AS WELL TO SEE IF A SMELL COULD BE SMELT IN COCKPIT. ACFT WAS AT 90% N2 FOR AFEW MOMENTS AS WELL. NO SMELL EVER NOTED
OIL FUME SMELL-VERY APPARENT IN COCKPIT- WHEN BOTH PACKS ARE ACTIVATED THROUGHOUT WHOLE FLIGHT. FOUND LOOSE DUCT IN #1 PACK. OPERATED APU AND BOTH ENGINES AFTER TIGHTENING DUCTS WITH BOTH PACKS ON AND FULL HEAT, NO SMELL PRESENT. OK FOR SERVICE AT THIS TIME.
EICAS CT MESS, RUDDER SYS 2 INOP, IN FLT (TAKE-OFF). R+R RUDDER #2 PRESSURE SWITCH IAW AMM 27-23-04. OPS CHECK GOOD OK FOR SERVICE. EICAS MESS, RUDDER SYS 2 INOP, IN FLT. T/S IAW FIM TASK 27-23-00-810-802-A. FOUND RUDDER PRIORITY RELAY K0384 TO AT FAULT. R/R'D RELAY IAW MM 20-13-02/400, OPS CK GOOD TO 160 KTS.
STRONG FUMY SMELL IN FLT DECK DURING ALL PHASES OF FLIGHT.MORE NOTICEABLE ON GROUND....FIX:PERFORMED HIGH POWER ENGINE RUNS WITH CREW. COULD NOT DUPLICATE ANY SMELLS WHILE ON APU,ENGINES AND WITH BOTH PACKS ON. A/C OK FOR SERVICE AT THIS TIME
PDIS 650 27-36 2289051 05JAN20 PHL CLOSE SPS 2 INOP AND SPS ADVANCED DURING REJECTED TAKEOFF FACT 05JAN20 20:15 PHL PERFORMED OPS CHECK IAW AMM 27-26-00. DETERMINED FAU LT ON STALL PROTECTION COMPUTER. R&R SPC COULDN'T DU PLICATE FAULT ON GROUND. A/C OK FOR SERVICE.
PDIS 650 21-50 1891911 27OCT19 DCA CLOSE BURNING RUBBER SMELL NOTICED IN CABIN AND COCKPIT. S MELL WENT WHEN PACK 1 WAS TURNED OFF. FACT 27OCT19 02:33 ALB MX INSP AND DETERMINED SMELL IS ONLY ASSOCIATED WITH PACK 1. OPERATED BOTH PACK SYSTEMS FOR 30 MINUTES FROM COLD TO HOT AND FOUND NO IRREGULAR SMELLS. WORK WAS DONEIAW E145 AMM 21-00-00 OPS CHECK GOOD MEL 21-13-2 CLOSED.
SMOKE FOUND IN CABIN DURING FLIGHT....FIX: R&RD RH ACM, MAINT FOUND FROZEN, IAW AMM 21-51-03. OPS AND LEAK CHECK GOOD.OK FOR SERVICE. NO SMOKE FOUND WITH ENGINES RUNNING. NOTE: CREW REPORTED EMERGENCY, NO EVACUATION, NO EMERGENCY EQUIPMENT USED
NDIS 650 05-50 0001550 24APR19 RIC CLOSE PITOT NR 3 RELAY K0058 AND BASE VISIBLY BURNT AND DEFORMED RELAY K0057 WAS PHYSICALLY DAMAGED AND SILICONE GASKET WAS STICKING AND NOT RETAINING ORIGINAL FORM 34793 00 SJU FACT 24APR19 10:50 RIC RR RELAY K0058 AND K0057 AND RELAY BASE K0058 IAW FCD 1-30-16-0276 PITOT NR 3 RELAYS CONFORMITY.
DENT ON RH OMEGA BEAM BETWEEN FR. 49-50-C/A-ACCOMPLISHED REPAIR ON RH OMEGA BEAM BETWEEN FR49 AND 50 IAW ERS-EM-5300-3734 AND EMB145 SRM 53-23-10
SERVICE DOOR CUT-OUT FRAME 22 AFT LOWER CORNER OUT OF LIMITS.-C/A-ACCOMPLISHED SERVICE DOOR CUTOUT FR22 REPAIR IAW ERS-EM-53MR-3728
APU FIREWALL AT RH UPPER CORNER IS OIL CANNING-C/A-REPAIRED APU FIREWALL IAW ERS-EM-49MR-141
#8 EMERGENCY LIGHT STRIP WIRE BROKEN-C/A-REMOVED AND REPLACED # 8 EMERGENCY LIGHT STRIP IAW EMB 145 AMM 33-50-12.
PREVIOUS REPAIR IS CORRODED ON CENTER OMEGA BEAM BETWEEN FRAMES 24-25. C/A-COMPLETE:REMOVED CORROSION ON PREVIOUS REPAIR ON CENTER OMEGA BEAM BETWEEN FRAMES 24-25 VIA BLENDING IAW SRM 51-10-03.
CENTER AISLE CROSSMEMBER AT FRAME 25 IS CORRODED. C/A-COMPLETE:REMOVED AND REPLACED CENTER AISLE CROSSMEMBER AT FRAME 25 IAW SRM 53-22-10, ETN-EM-53-139R4, AND ETN-EM-53-150R2.
DIVR STL E2 A/I ICE FAIL IN ICING CONDITIONS / EMER DECL. DEFERRED E2 A/I VLV M PROCEDURES C/W. FOUND CMC MSG E2 A/ICE VALVE FAIL, E2 A/ICE LOW PRESS, AND A/ICE OVERPRESS REMOVED AND REPLACED RT A/ICE VALVE IAW AMM 30-21-01 AND REMOVED AND REPLACED TRANSDUCER IAW AMM 30-21-06 OPC GOOD NO DEFECTS NOTED AT THIS TIME MEL RESTORED END. ENGINE ANTICE/VALVE P/N C146009-4 S/N 1397.
ON DESENT TO LANDING PASSING THROUGH FL 240, AURAL ALERT CABIN AND CABIN ALT REACHED 11,000 FT. TS PRESN AUTO FAIL MSG PER FIM 21-31-00-810-801-Z. R&R DIGITAL CONTROLLER IAW AMM 21-31-01-000-801-A/21-31-01-400-801-A FNC TASK 21-31-00-700-802-A GOOD.
ON DESCENT TO LANDING AUTO MODE PRESS FAIL. TS PRESN AUTO FAIL MSG PER FIM 21-31-00-810-801-Z. REMOVED AND REPLACED DIGITAL CONTROLLER IAW AMM 21-31-01-000-801-A/21-31-01-400-801-A FNC TASK 21-31-00-700-802-A.
AFT FA FLASHLIGHT HOLDER BROKEN. R&R AFT FA'S FLASHLIGHT HOLDER BRACKET IAW AMM 33-50-16 OPS CHK GOOD AT THIS TIME LED LIGHT IS ON.
ELECTRICAL BURNING ODOR ENROUTE, DESCENT & LANDING, ODOR IN COCKPIT AND NEAR F/A JUMPSEAT. INSPECTED AND FOUND THE CAPTAIN'S FLOODLIGHT RHEOSTAT TO BE AT FAULT. REMOVED AND REPLACED THE INSTRUMENT AND CONTROL PANEL LIGHT PANEL ASSEMBLY IAW AMM 20-13-10 AND OPS CHECKED GOOD IAW 33-12-00, RAN BOTH BLEEDS, PACKS, WINDSHIELD HEAT, ALL COCKPIT LIGHTS & SYSTEMS, NO SMOKE OR BURNING ELECTRICAL ODOR NOTED.
SERVICE DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. R & R THE LAMP IAW AMM 33-50-10-000-801-A, & 33-50-10-400-801-A. OPS CHECKED GOOD.
MAIN DOOR HARD TO OPEN AND CLOSE. REMOVED BRACKET AND BELLCRANK BOLT IAW AMM 52-18-02 ALL WORK ACCOMPLISHED ON NRWC 650-DFW-03000, 03001, AND 03002. PERFORMED OPERATIONAL CHECK IAW AMM 52-18-00 ON MAIN CABIN DOOR. OPS CHECKED GOOD.
FLIGHT ATTENDANT FORWARD FLASHLIGHT RED CHARGING LIGHT NOT ILLUMINATING. REMOVED AND REPLACED THE FLASHLIGHT IAW AMM 33-50-16 OPS CHECKED GOOD.
NR 3 FLOOR PROX LIGHT STRIP BROKEN. REMOVED AND REPLACED NR 3 FLOOR PROX LIGHT STRIP IAW AMM 33-50-12. OPS CHECK GOOD.
LT NR 5 EMERGENCY LIGHT STRIP BROKEN. REMOVED AND REPLACED LT NR 5 EMERGENCY LIGHT STRIP IAW AMM 33-50-12. OPS CHECK GOOD.
WHILE PERFORMING HFEC INSPECTION ON LT MLG AFT UPPER TRUNNION, FOUND TRUNNION TO BE CRACKED. FREQUENCY 400KHZ,ANGLE 130 DEGREES, H-GAIN 63.6,V-GAIN 77.6. USED EASI 6581. INSTALLED SERVICEABLE LT MLG AFT UPPER TRUNNION IAW ERS-EM-57MR-722.
RT AFT UPPER TRUNNION CRACKED. INSTALLED SERVICEABLE RT MLG AFT UPPER TRUNNION IAW ERS-EM-57MR-731.
CHAFE ON FR 61 BETWEEN STGRS 4R-5R. PERFORMED PERMANENT REPAIR IAW ERS-EM-53MR-2442. DOUBLER P/N 145-64146-001.
POSSIBLE CRACK LOCATED APPROX 1" BELOW CARGO DOOR HANDLE CUTOUT. INSTALLED REPAIR DOUBLER, CARGO DOOR IAW ERS-EM-52MR-661.
CARGO DOOR ENTRANCE SILL CORRODED. R&R CARGO DOOR SILL IAW SRM 51-40-02.
CORROSION IN GALLEY AREA ON RT OMEGA BEAM FRAME 23 AT PREVIOUS REPAIR. INSTALLED DOUBLER AT RT OMEGA BEAM AT FR 23 IAW ERS-EM-53MR-2447.
LT ENGINE FWD LOWER YOKE CRACKED. REMOVED AND REPLACED LT FWD PYLON LOWER YOKE IAW EO EM-54MR-386.
UNDER FLOOR BOARD PANEL 251DF BROKEN OFF SPLICE ON AIRCRAFT SIDE FOR LIGHT STRIP. REPLACED CONNECTOR ON AIRCRAFT SIDE FOR LIGHT STRIP UNDER FLOOR BOARD PANEL 251DF IAW SWPM 20-21-00.
RT UPPER FUSELAGE SKIN CRACKED AFT OF FRAME 75 AND ABOVE STRINGER 2R, APPROX 3/8' LONG. INSTALLED REPAIR DOUBLER, FILLER, SHIM DRAG ANGLE ON RT UPPER FUSELAGE AFT OF FRAME 75 AND ABOVE STRINGER 2R IAW SRM 53-31-01. SEE WIPS AND TASKS FOR DETAILS.
POSSIBLE CRACK LOCATED APPROX 1'' BELOW CARGO DOOR HANDLE CUTOUT. INSTALLED REPAIR DOUBLER, CARGO DOOR IAW ERS-EM-52MR-661. SEE TASKS AND WIPS FOR DETAILS.
EMERGENCY MAIN DOOR LIGHT INOPERATIVE. R & R EMER MAIN DOOR LAMP IAW AMM 33-50-10. OPERATIONS CHECK WAS GOOD AT THIS TIME.
CABIN COVE LIGHTS WILL NOT TURN ON. FLIGHT ATTENDANT SMELLED SOMETHING. R & R WITH SERVICEABLE SIDEWALL LIGHT CONTROL MODULE IAW AMM 33 21 01. OPERATIONS CHECKED OK.
MAIN DOOR EMER LIGHT INOPERATIVE. RELAMPED MAIN DOOR EXTERNAL EMER LIGHT IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.
AFTER TAKEOFF & AFTER LG AIR & GND FAIL MSG RECEIVED, THRUST 1 - 2 REVERSER DISAGREE CAUTION MSG ON EICAS. AFTER LANDING MSG WENT AWAY, FOUND MSG RELATED TO AFOREMENTIONED NLG WOW SWITCH TARGET ADJUSTMENT, REF THIS AML PAGE ITEM 1. MSG NO LONGER IN VIEW AFTER NLG WOW TARGET WAS ADJUSTED. COMPLIED WITH OPERATIONS CHECK OF THRUST REVERSERS IAW AMM 78-31-01-700-801-A. NO DEFECTS NOTED.
MAIN DOOR HINGE, EMER LIGHT INOPERATIVE. R & R EMER LIGHT IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.
LEFT FWD LOWER FAIRING, EMER LIGHT INOPERATIVE. R & R LT FWD LOWER FAIRING EMER LIGHT LAMP IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.
INITIALLY AFTER TAKEOFF VERY LOUD NOISE COMING FROM FWD NOSE SECTION, ACCESS DOOR OPEN ON EICAS. PERFORM APPROPRIATE CHECKLIST, DECLARED EMER. PERFORMED GEAR SWING & FOUND NOSE GEAR DOORS DID NOT CLOSE. FOUND BAD NOSE GEAR SEQUENCE PROX SWITCH WITH GSE212. R & R NOSE GEAR DOOR SEQUENCE PROX SWITCH IAW AMM 32-63-03. OPERATIONS CHECKED GOOD. SEE ITEM 2 BELOW FOR ACCESS DOOR OPEN. FWD ELEC COMPARTMENT DOOR INDICATION CHECKED GOOD IAW AMM 52-71-00.
AFT EMER FLASHLIGHT STAYS ON ALL THE TIME. R & R AFT EMER FLASHLIGHT IAW AMM 33-50-16 STEPS 2 J 1, 3 I 4. OPERATIONS CHECKED GOOD.
AFT FLIGHT ATTENDANT EMER FLASHLIGHT INOPERATIVE. REPLACED AFT FLIGHT ATTENDANT EMER FLASHLIGHT IAW AMM 25-60-01. CHECKED GOOD.
ON TAXI OUT SMOKE IN COCKPIT & CABIN FOLLOWED BY APU FAIL CAUTION ON EICAS. INSPECTED & COMPLIED WITH ETN-EM-72-034. FOUND APU TO BE SOURCE FOR THE SMELL. DEFERRED APU IAW MEL 49-1. R & R APU REF WC 49-800-05. OPERATIONS CHECKED GOOD AT THIS TIME & MEL RESTORED.
FLIGHT ATTENDANT`S EMER FLASHLIGHT INOPERATIVE. R & R FLIGHT ATTENDANT`S EMER FLASHLIGHT IAW AMM 33-50-16-000-801-A & 33-50-16-400-801-A. OPERATIONS CHECKED GOOD AT THIS TIME.
RIGHT AFT OVERWING EXTERNAL EMER LIGHT INOPERATIVE. R & R RT AFT OVERWING EXTERNAL EMER LIGHT LAMP IAW AMM 33-50-07-000-801-A & 33-50-07-400-801-A. OPERATIONS CHECKED GOOD.
RIGHT EXTERNAL OVERWING EMER LAMP INOPERATIVE. R & R RT EXTERNAL OVERWING EMER LIGHT LAMP IAW AMM 33-50-07-000-801-A & 33-50-07-400-801-A. OPERATIONS CHECKED GOOD. NO DEFECTS NOTED AT THIS TIME.
AFTER ENG'S WERE AT IDLE FOR A LONG PERIOD, THE THRUST WAS BROUGHT UP & WE SMELLED AN OIL BURNING SMELL. REPEAT WRITE UP TRANSFERRED TO NRWC 650-DFW-01922. IAW NRWC 650-DFW-01922, R & R LT ENG IAW WC 71-000-00. OPERATIONS CHECKED GOOD. NO LEAKS DETECTED.
OILY BURNING SMELL COMING THRU PACK SYS WITH TAKEOFF THRUST & CLIMB THRUST SET. SEEMED TO GET WORSE IN THE DESCENT WITH LOW THRUST SETTINGS. NO VISIBLE SMOKE. SUSPECT PACK NR 1 SYS. TRANSFERRED TO NRWC 650-DFW-01912. IAW NRWC 650-DFW-01917, COMPLIED WITH. R & R E1 NR 0 CARBON SEAL. ENG RUN PERFORMED FOR ODOR CONFIRMATION, NO SMELL NOTED IAW ETN-EM-72-034.
LEFT UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 & ABOVE STRINGER 2L. INSTALLED FILLER, REPAIR DOUBLER, REPAIR ANGLE & REPAIR ANGLE FILLER IAW ERS -EM-53MR-712.
COCKPIT UNDERFLOOR ACCESS HATCH 123BL FRAME IS CRACKED UNDER THE RETAINER RING EYELET. PERFORMED REPAIR TO COCKPIT UNDERFLOOR ACCESS HATCH IAW ERS EM-5200-199.
LEFT MLG WW AFT LOWER BULKHEAD CRACKED INBD OF PREVIOUS REPAIR. R & R LT MLG WW AFT BULKHEAD IAW SRM 51-20-03, 51-40-06, 51-40-02 & 51-40-09. SEE WIP ENTRIES FOR DETAILS.
APU FIREWALL CRACKED AT APPROX 6 O'CLOCK POSITION. REPAIR IAW EO EM-53AD-1883 PART C, REPAIRED APU FIREWALL.
NUMBER 2 MAIN BRAKE SYS RETURN LINE CHECK VLV FAILED OPERATIONAL CHECK. R & R NR 2 MAIN BRAKE SYS RETURN LINE CHECK VLV IAW AMM 32-41-09. LEAK & OPERATIONAL CHECKED GOOD.
LEFT FUEL SOV PRESS REFERENCE LINE CRACKED. R & R CRACKED LT FUEL SOV PRESS IAW EMB 145 AMM 28-00-01.
FLIGHT ATTENDANTS FLASHLIGHT CRADLE IS LOOSE. FLASHLIGHT WILL NOT CHARGE. REPLACED FLIGHT ATTENDANT FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.
DURING PS 1 INSPECTION FOUND SECTION 4 FLOOR PROXIMITY EMER LIGHT ASSEMBLY INOPERATIVE. ITEM DEFERRED IAW MEL 33-30. INSTALLED NEW SPLICES AT SECTION 4 FLOOR STRIP IAW WM CH 20-50-01. OPERATIONS CHECKED GOOD IAW MM CH 33-50-00. MEL ITEM RESTORED.
CARGO SMOKE WARNING DURING CRUISE AT FL 250. FIRE BOTTLE FIRED, CFR REPORTED NO FIRE. CVR PULLED DUE TO POSSIBLE FIRE.
CLIMBING THROUGH FL 180, WHILE PERFORMING THE ANTI-ICE TEST, BLD 1 LEAK WARNING. EA PROCEDURE COMPLIED WITH & RESOLVED ISSUE. DURING TROUBLESHOOTING, FOUND LEAK AT O & L ABOVE NR 1 BLEED AIR CHECK VLV. R & R BLEED AIR CHECK VLV & UPPER DUCT ASSEMBLY. ADJACENT TO CHECK VLV IAW AMM 36-11-09-000-002-A & 36-11-09-400-802-A. LEAK CHECKED & PERFORMED OPERATIONAL TEST OF THE BLEED AIR SYS IAW AMM 36-00-00-700-803A. NO LEAKS NOTED & NO FAULTS INDICATED. ACFT OK FOR SERVICE.
TRANSFERRED FROM AML PAGE 3527007 ITEM 1, BLEED 1 LEAK EICAS WARNING & BUTTON INSCRIPTION DURING CLIMB FL 190. EPC & AOM PROCEDURES COMPLIED WITH. EICAS MSG & BUTTON INSCRIPTION EXTINGUISHED WITH CLOSURE OF ASSOCIATED BLEED VLV & CROSSBLEED CLOSED. REMAINED BELOW FL 250, NO FURTHER INDICATIONS PRESENTED. R & R AIR BLEED LINE O RINGS JOINT NR 28 AFT PRESS BULKHEAD IAW AMM 36-11-10. OPERATIONS CHECKED LEAK, CHECKED GOOD. NO OTHER DEFECTS NOTED.
PAX DOOR EMERGENCY LIGHT, OVERHEAD BY COCKPIT DOOR EMERGENCY LIGHT & LT WING LATERAL PANEL EMERGENCY LIGHT INOPERATIVE. R & R BATTERY POWER SUPPLY & BATTERY FOR NR 1 EMERGENCY SYS IAW AMM 33-50-04 & REPLACED LT WING EMERGENCY LIGHT BULB IAW AMM 33-50-10. OPERATIONS CHECKED GOOD IAW AMM 33-50-00.
FDR PARAMETERS REPORTED OUT OF LIMITS. NR 2 ELEVATOR FAILED OUT OF TOLERANCE. ADJUSTED ELEVATOR NR 2 RVDT IAW AMM 31-31-06 OPS CHECKED GOOD.
WHEN ON THE APPROACH THE AP DID A HARD RT TURN & THEN A HARD LT TURN. FLIGHT CREW PLACARDED IAW MEL 22-01.
EXIT SIGN ON GALLEY BULKHEAD IN FRONT OF SEAT 3BC IS INOPERATIVE. R & R NR 3 DC/AC INVERTER IAW EMB 145 AMM 33-50-11. R & R EMERGENCY LIGHTS BATTERY SUPPLY NR 2 IAW EMB 145 AMM 33-50-04, OPERATION CHECKED GOOD.
F/O FLASHLIGHT HOLDER BROKEN. R & R F/O FLASHLIGHT HOLDER IAW AMM 33-50-16.
MAIN DOOR EMERGENCY LIGHT INOPERATIVE. R & R BULB IAW AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECKED GOOD END.
MAIN CABIN DOOR INTERIOR HANDLE IS DIFFICULT TO OPERATE. WHEN CLOSING HANDLE DOES NOT COMPLETELY LATCH DOWN. CLEANED DOOR SEAL AND LUBED TOP ROLLERS IN REF TO AMM 52-18-06. OPS CHECKED GOOD IAW AMM 52-18-00.
MAIN DOOR EMERGENCY LIGHT INOPERATIVE. R & R LAMP IAW AMM TASK 33-50-06-000-801-A AND 33-50-06-400-801-A. OPS CHECKED GOOD.
DURING CRUISE, RECEIVED AN EICAS BAGGAGE SMOKE INDICATION AND OVERHEAD, AUROL WARNING. PERFORMED THE EMERGENCY CHECKLIST AND THE BAGGAGE SMOKE LIGHT EXTINGUISHED & THEN CAME BACK ON. BOTTLE WAS DISCHARGED. THE CREW DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. THE ACFT LANDED WITHOUT INCIDENT. THE ACFT WAS REMOVED FROM SERVICE. R & R CARGO REAR SMOKE DETECTOR IAW MM 26-15-01. OPT CHECK FOUND SATISFACTORY IAW MM 26-15-00. PERFORMED CARGO SMOKE DETECTOR, INSPECTION CHECK IAW AMM 26-15-01. FOUND OK. NO EVIDENCE OF SMOKE. FOUND BAGGAGE TEST SWITCH S7265 ON MAINT PANEL BAD. CARTRIDGE LOWER, PN: M30903870. CARTRIDGE UPPER, PN: M30903870. FIREX BOTTLE-630 CU. IN., PN: 346000731, SN: 1959F1. FIREX BOTTLE-630 CU.IN., PN: 346000731. SN: 1959F1. SWITCH, PN: M83731/10-271. CARGO AREA SMOKE DETECTOR, PN: 473597-13. SN: 1059. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.
DURING B INSPECTION, FOUND THE 12C INTERIOR OVERWING EMERGENCY LIGHT INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE RT OVERWING EMERGENCY LIGHT LAMP IAW AMM 33-50-07-000-801-A AND 33-50-07-400-801-A. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.
ON FLIGHT 3996 THE CREW REPORTED THAT AFTER TAKEOFF THEY COULD NOT RAISE THE LANDING GEAR NORMALLY, RECEIVED NUMEROUS CONFIG WARNINGS FOR FLAPS & TRIM VIA AURAL WARNING- NO EICAS MESSAGES DISPLAYED. THE CREW PERFORMED AOM VOL 1 PROCEDURE FOR LANDING GEAR AND IT COULD NOT BE RAISED. GOT GEAR UP AND MOC ADVISED AND TOLD THEM TO RETURN TO ORD. THE CREW DECLARED AN EMERGENCY AND LANDED NORMALLY. DURING THE ROLLOUT THE CREW BEGAN TO RECEIVE MANY EICAS WARNING AND CAUTIONS INCLUDING LG. AIR/GND FAIL AND IC 1-2 WOW INOP. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED RELAYS K0025, K0024, AND K0453. NO DEFECTS NOTED. GEAR SWING GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE INSPECTION NOTICED A STRONG FUEL SMELL AFTER APU START-UP REF LOG PAGE 3199769. COMPLIED WITH ETN-EM-72-034 PERFORMED PACKS WITH ENGINES AND APU RUNS. THE OPERATIONAL CHECK WAS GOOD NO FUEL SMELL NOTED DURING ECF FLIGHT 9808. THE AIRCRAFT WAS RETURNED TO SERVICE.
FLIGHT 9806. CREW REPORTED ACFT BANKS HARD TO RIGHT WITH AILERON TRIM AT ZERO. TO KEEP WINGS LEVEL 1/4 ROLL TRIM IS REQUIRED. ACFT REMOVED FROM SERVICE. REMOVED AND REPLACED LEFT AND RIGHT AILERON ACTUATORS IAW AMM 27-21-01. OPS AND & LEAK CHECKED GOOD. ACFT RETURNED TO SERVICE.
FOR FLIGHT 9806 THE CREW REPORTED STRONG FUEL SMELL AFTER STARTING APU. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH ETN-EM-72-034. PERFORMED ENGINE RUNS AND APU RUNS NO FUEL SMELL NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 3596 THE CREW REPORTED THAT WHILE DOING HIGH SPEED TAXI THE AIRCRAFT OCCASIONALLY JERKS TO THE LEFT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND INSTALLED LOAD POTENTIOMETER IAW EMB 145 AMM 32-00-00. THE AIRCRAFT WAS RETURNED TO SERVICE.
FWD CABIN FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT AREA 2 BATTERY AND CHARGER ASSEMBLY.
DURING B INSPECTION FOUND THE MAIN DOOR CEILING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN DOOR CEILING EMERGENCY LIGHT IAW EMB AMM TASK 33-50-06-000-801-A AND 33-50-06-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING B INSPECTION FOUND THE ROW 3 EMERGENCY EXIT SIGN INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. TROUBLESHOT AND FOUND CONNECTORS LOOSE. RECONNECTED LAMP IAW EMB AMM 33-50-14-000-801-A AND 33-50-14-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING B INSPECTION FOUND THE EMERGENCY LIGHT AT MID-CABIN LEFT SIDE EMERGENCY EXIT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAMP AT THE LEFT EMERGENCY EXIT PER EMB AMM 33-50-07-000-801-A AND 33-50-07-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING B INSPECTION FOUND THE RIGHT BEAM GUSSET CORRODED BETWEEN FRAMES 60-61. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT BEAM GUSSET BETWEEN FRAMES 60-61 IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.
BACKSIDE FRAME 80 BURNED/CORRODED. ACCOMPLISHED EM-53MR-2024.
LEFT OMEGA BEAM IS CORRODED BETWEEN FRAMES 58-59. REPAIRED LEFT OMEGA BEAM CORROSION BETWEEN FR 58-59 IAW AEA EO-EM-53MR-2027.
BACK SIDE OF FRAME 80 IS BURNED/CORRODED WHERE APU SHUNT IS ATTACHED. REPAIRED BACK SIDE OF FR 80 BURNED/CORRODED WHERE APU SHUNT IS ATTACHED IAW AEA EO-EM-53MR-2024.
DURING B INSPECTION FOUND THE RIGHT CROSS MEMBER OUTBOARD GUSSET CORRODED AT FRAME 23. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT CROSS MEMBER OUTBOARD GUSSET IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING B INSPECTION FOUND THE SERVICE DOOR CENTER SILL CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SERVICE DOOR CENTER SILL IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING B INSPECTION FOUND THE RIGHT BEAM GUSSET CORRODED AT FRAME 31. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT BEAM GUSSET IAW EMB SRM 51-40-02, EMB SRM 51-20-03, EMB SRM 51-40-06 AN EMB SRM 51-40-09. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING B INSPECTION FOUND THE RIGHT BEAM GUSSET CORRODED AT FRAME 28. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT BEAM GUSSET IAW EMB SRM 51-40-02, EMB SRM 51-20-03, EMB SRM 51-40-06 AN EMB SRM 51-40-09. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING B INSPECTION FOUND THE CENTER BEAM GUSSET CORRODED BETWEEN FRAMES 59-61. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CENTER BEAM GUSSET BETWEEN FRAMES 59-61 IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING B INSPECTION FOUND THE MAIN CABIN DOOR SEAL TORN IN TWO PLACES ON DOOR FLAP. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN CABIN DOOR SEAL IAW EMB 145 AMM 52-18-04. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING B INSPECTION FOUND THE CARGO DOOR SILL CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CARGO DOOR SILL IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 3266 THE CREW REPORTED THE FLASHLIGHT CRADLE BEHIND THE CAPTAIN SEAT WAS BROKEN. (FLASHLIGHT FALLS OUT) DEFERRED PER MEL 25-53 AUTH 090679-C FOR CAPT'S FLASHLIGHT. SECURED IN PLACE. COMPLIED WITH (M) PRODGERS FOR MEL. REMOVED AND REPLACED THE CAPTAINâS EMERGENCY FLASHLIGHT ASSEMBLY. THE OPERATIONAL CHECK WAS GOOD IAW AMM 33-50-16. MEL RESTORED. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 3401 THE CREW REPORTED THE CAPTAINâS FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAINâS FLASHLIGHT IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE INSPECTION, FOUND THE ROW NR 8 FLOOR EMERGENCY LIGHT CONNECTOR WIRE BROKEN. AIRCRAFT REMOVED FROM SERVICE. REPAIRED ROW NR 8 FLOOR EMERGENCY LIGHT CONNECTOR IAW WM 20-50-00. AIRCRAFT RETURNED TO SERVICE.
DURING B INSPECTION, FOUND THE FLIGHT ATTENDANT STATION EMERGENCY FLASHLIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FLIGHT ATTENDANT FLASHLIGHT BATTERY. OPS CHECKED GOOD IAW CMM 25-60-11. AIRCRAFT RETURNED TO SERVICE.
FLIGHT 4050 - ON ARRIVAL AT GATE WITH NR 2 ENGINE RUNNING, PARKING BRAKE ON, NO APU OR GPU, HAD NR 2 ENGINE FLAMEOUT, SHUTDOWN UNCOMMANDED WITH ECAS MESSAGE. AIRCRAFT REMOVED FROM SERVICE. PERFORMED CMC AND FDR DOWNLOAD, FOUND THAT NR 2 ENGINE FUEL PUMP WAS TURNED OFF PRIOR TO ENGINE SHUTDOWN CAUSING FLAMEOUT. GROUND RAN AIRCRAFT IAW FIM TASK 72-00-00. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
ON FLIGHT 4291 THE CREW REPORTED THE MAIN CABIN DOOR WAS HARD TO OPEN FROM THE INSIDE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN CABIN DOOR HANDLE COVER PER STANDARD MTX PROCEDURES. THE OPERATIONAL CHECK WAS GOOD PER EMB-145 MM 52-18-00. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 4200 THE LIGHT ATTENDANT REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBRICATED MAIN CABIN DOOR FRAME ROLLERS IAW EMB MM 53-21-00. NO DEFECTS NOTED, DOOR OPENING WITH NO DIFFICULTY. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING B-INSPECTION FOUND THE MAIN DOOR MOUNTED EMERGENCY LIGHT INOP. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED MAIN CABIN DOOR MOUNTED EMERGENCY LAMP IAW EMB 145 AMM TASK 33-50-10-000-801-A & 33-50-10-400-801-A OPERATIONAL CHECK GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 4391 THE CREW REPORTED AN UNCOMMANDED ROLL TO THE RIGHT AFTER TAKEOFF. THE FLAPS WERE AT 9 DEGREES. THE CREW RETURNED TO ORD AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND AILERON CONTROL CABLES BELOW SPECIFICATION. ADJUSTED THE WING AND FUSELAGE SECTORS OF THE AILERON CONTROL SYSTEM IAW EMB-145 AMM 27-11-01. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE INSPECTION FOUND THE FORWARD BAGGAGE SMOKE DETECTOR INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED FORWARD BAGGAGE SMOKE DETECTOR IAW EMB AMM 26-15-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
FOR FLIGHT 3541 THE CREW REPORTED THE AFT CABIN FLASHLIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT CABIN FLASHLIGHT AND CHARGER ASSY IAW EMB AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE INSPECTION FOUND THE AFT CABIN FLASHLIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT CABIN FLASHLIGHT IAW EMB MM 33-50-16. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE CHECK FOUND EMERGENCY LIGHT STRIPS 4 AND 5 INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE DC/AC INVERTER NR 5 IAW EMB 145 AMM 33-50-11. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE BASE VISIT FOUND THE RIGHT OVERWING EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVERWING EMERGENCY LIGHT LAMP IAW EMB 145 AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 3209 THE CREW REPORTED UPON DESCENT TO LANDING SMELLED A BURNING ODOR IN THE COCKPIT ONLY. DETECTED FUMES ONLY, NO SMOKE. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED GENERAL VISUAL INSPECTION OF THE COCKPIT AND HAD CREW RUN ENGINES WITH PACKS ON WITH MAINTENANCE PRESENT. NO FURTHER ODORS WERE NOTED. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.
FOR FLIGHT 2875 DURING MAINTENANCE CHECK FOUND THE LIGHT STRIP FOR EMERGENCY LIGHTING ON THE LEFT OVERWING EMERGENCY EXIT WILL NOT ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LIGHT STRIP ON THE LEFT SIDE OVERWING EMERGENCY EXIT IAW AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 4318 CREW REPORTED ON LANDING, RECEIVED A "BRAKE DEGRADED" & FELT ASYMMETRIC THRUST ON LAST PORTION OF LANDING ROLLOUT. TOWER REPORTED SMOKE COMING FROM LT MLG. ON TURN INTO GATE TOWER REPORTED MORE SMOKE FROM LT MLG AND FLUID SPILLING OUT, AT THAT MOMENT LOST HYD NR 2 QTY & PRESSURE. HAD MINIMAL BRAKING. POST FLT INSPECTION REVEALED HYD FLUID LEAKING FROM LT MLG & INBOARD BRAKE PIN MISSING. NO FIRE AT ANYTIME. ACFT REMOVED FROM SERVICE. INSPECTED LT MLG ASSY. FOUND NR 2 HYD BRAKE LINE DISCONNECTED CAUSING HYD NR 2 QTY DEPLETION & SUBSEQUENT BRAKE DEGRADING & EMERGENCY LOW PRESSURE MESSAGE ON EICAS. NO CMC MSG. R & R NR 2 MLG BRAKE ASSY IAW W/C 32-600-14. ALSO R & R NR 2 BRAKE TEMP SENSOR IAW AMM 32-47-01. OPS & LEAK CHECK GOOD. ACFT RETURNED TO SERVICE.
ON FLIGHT 3648 THE CREW REPORTED AN ELECTRICAL BURNING SMELL IN THE GALLEY. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND BURNED LIGHT BALLAST AT SEAT 3 B & C. REPLACED THE BALLAST IAW EMB AMM 33-21-04. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE BASE VISIT FOUND THE GALLEY EMERGENCY EXIT LIGHTS TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BATTERY AND BATTERY CHARGER ASSEMBLY ASSY IAW EMB AMM TASK 33-50-04-000-801-A & 33-50-04-400-801-A . THE OPERATIONAL CHECK WAS NORMAL AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE BASE VISIT FOUND THE RIGHT EXIT EMERGENCY OVERWING LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED RIGHT OVERWING EMERGENCY LIGHT ASSEMBLY IAW EMB SB 145-33-0013R1. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE BASE VISIT FOUND THE PASSENGER DOOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BULB IAW EMB 145 AMM 33-50-10. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING P2-2 CHECK THE FORWARD CENTER OVERWING INTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 INVERTER FOR THE EMERGENCY LIGHT IAW EMB145 AMM 33-50-11. THE OPERATIONAL CHECK WAS GOOD IAW 33-50-00-700-801-A. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 3892 THE CREW REPORTED, RECEIVED A MESSAGE THAT NR 1 ENGINE FIRE BOTTLE WAS INOPERABLE. THE CREW ELECTED TO RETURN TO MIA. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. RESET SYSTEM. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD PER AMM 26-21-00. NO DEFECTS NOTED, OK FOR SERVICE. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 4348, CREW REPORTED THAT ATOMIZED TURBINE OIL FUMES WERE INTRODUCED INTO THE CABIN CONDITIONED AIR WHEN USING ENG 1 BLEED AS SUPPLY SOURCE. WHEN USING BLEED 2 OR APU TO SUPPLY A/C PACKS CONDITIONED AIR IS GOOD. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR1 ENGINE IAW WORK CARD 71-00-00. AIRCRAFT RETURNED TO SERVICE.
EMERGENCY LIGHTS IN FORWARD CABIN INOPERATIVE. REMOVED AND REPLACED NUMBER TWO BATTERY PACK AND CHARGER IAW EMB AMM. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.
CID - FLT 3570 - FLOOR EMERGENCY LIGHTS FROM ROW 8 TO 12 OUT AND OVERWING EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED NR 3 BATTERY PACK, IAW EMB 145, AMM 33-50-04. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
CMH - FLT 3589 - ON TAKEOFF, FIRST OFFICERS TRIM SWITCH WAS IN USE AND IT STARTED TO SMOKE. STOP USING THE FIRST OFFICERS TRIM SWITCH AND CAPTAIN TRIM WORKED NORMAL, RETURNED TO FIELD NO OTHER PROBLEMS NOTED. RAI FIRST OFFICERS TRIM SWITCH, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
MKE - FLT 4095 - ABORTED TAKEOFF FOR TAKEOFF CONFIGURATION WARNING WITH SPOILER OPEN EICAS MESSAGE. RAI RELAY K0212, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
ALL EMERGENCY LIGHTS FAILED TO TEST DURING PREFLIGHT. REPLACED NR 2 BATTERY PACK. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (K)
ORD - FLT 4435 - FOUND EMERGENCY LIGHT CIRCUIT BREAKER POPPED. WOULD NOT RESET. EMERGENCY LIGHT NO ARMED EICAS MESSAGE ILLUMINATED. REPLACED NR 3 EMERGENCY BATTERY AND CHARGER IAW EMB 145 MM 33-50-04. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. CHARGER P/N OFF 11-0049 S/N OFF 14855, BATTERY P/N OFF 20131 S/N OFF 67338. (M)
EMERGENCY LIGHTS WILL NOT EXTINGUISH. REPLACED NR 1, 2, 3 AND 4 EMERGENCY LIGHT BATTERY POWER SUPPLIES AND NR 2 EMERGENCY LIGHT CHASSIS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. EMERGENCY LIGHT BATTERIES OFF P/N 2-131A. POWER SUPPLY SERIAL NUMBERS OF AS FOLLOWS 1-66089, 2-69701, 3-67880, 4-74123. (M)
CVG - FLT 3971 - EMERGENCY LIGHTING CIRCUIT BREAKER POPPED. REPLACED CIRCUIT BREAKER 8500 AND RELAY K0275. OPERATIONAL CHECK OF EMERGENCY LIGHTING SYSTEM GOOD PER EMB AMM 33-50-00. AIRCRAFT RETURNED TO SERVICE. C/B PN IS REBC4105-200003. (M)
EMERGENCY LIGHT ARM CIRCUIT BREAKER POPPED. FOUND LOOSE CONNECTOR ON BATTERY PACK. RESECURED CONNECTOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
THE EMERGENCY LIGHTS ILLUMINATED IN THE COCKPIT AND CABIN. SHORTLY AFTERWARDS THE EMERGENCY LIGHTS NOT ARMED MESSAGE APPEARED ON THE EICAS. REPLACED EMERGENCY BATTERIES NR 1 AND NR 3 IAW EMB 145 MM 33-50-04. BOTH BATTERIES HAD LOW VOLTAGE. PERFORMED EMERGENCY LIGHTING TEST IAW EMB-145 MM 33-50-00. NO DEFECTS NOTED. A/C RETURNED TO SERVICE. (M)
DURING MBV INSPECTION, A DENT WAS FOUND AFT OF RADOME FRAME 1 AND STRINGER 13 R. REPLACED DAMAGED SECTION OF SKIN IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501985) (K)
DURING CPCP INSPECTION FOUND ANGLE CORRODED THROUGH AFT END. REMOVED AND REPLACED FORWARD CABIN FLOOR ANGLE WITH A NEW ANGLE IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501) (K)
DURING CPCP INSPECTION, FOUND THE FORWARD CABIN FLOOR RT SILL HAS CORROSION AROUND NUTPLATE. REMOVED AND REPLACED SILL ASSY IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501985) (K)
DURING CPCP INSPECTION FOUND FORWARD CABIN LT SILL CORRODED. REMOVED AND REPLACED SILL IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501985) (K)
DURING CPCP INSPECTION, FOUND THE FLOOR DIGITAL CORRODED IN SEVERAL AREAS REMOVED AND REPLACED FLOOR DIGITAL IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501985) (K)
DURING CPCP INSPECTION, FOUND THE MAIN DOOR SILL ANGLES ARE CORRODED. REMOVED AND REPLACED MAIN DOOR SILL ANGLES IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501985) (K)
DURING CPCP INSPECTION, FOUND THE SUPPORT CORRODED UPPER AFT END. REMOVED AND REPLACED FLOOR SUPPORT BETWEEN FRAME 19 AND FRAME 20 IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE.
DURING CPCP INSPECTION FOUND THE FORWARD CABIN FLOOR OMEGA SHAPE CORRODED. REPAIRED FORWARD LT CABIN OMEGA SHAPE AT FRAME 20 CROSSBEAM ATTACH JUNCTION IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501985) (K)
DURING CPCP INSPECTION, FOUND THE SERVICE DOOR SILL CORRODED AROUND NUTPLATES UPPER SURFACE. REMOVED AND REPLACED SERVICE DOOR SILL PLATE IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501985) (K)
DURING CPCP INSPECTION FOUND THE FORWARD CABIN FLOOR DOUBLERS HAVE CORROSION ON UPPER SURFACE. REMOVED AND REPLACED THE FLOOR DOUBLERS IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501985) (K)
DURING CPCP INSPECTION FOUND THE FORWARD CABIN FLOOR SILL ASSEMBLY HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED FORWARD SILL ASSEMBLY IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501985) (K)
DURING CPCP INSPECTION FOUND THE FORWARD CABIN FLOOR GUSSET HAS CORROSION ON UPPER SURFACE. INSTALLED NEW GUSSET IAW SRM. AC RETURNED TO SERVICE. (SW21200501985) (K)
ON FINAL APPROACH, FLAPS SELECTED TO MOVE FROM 22 TO 45 DEGREES. FLAPS STUCK AT 41 DEGREES WITH ACCOMPANYING FLAP FAIL AND FLAP CAUTION MESSAGES ON EICAS. REPLACED PDU. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
ORD - FLT 4431 - CREW REPORTED A HEAVY OZONE ODOR IN COCKPIT AFTER LIGHTNING STRIKE. MAINTENANCE PERFORMED LIGHTNING STRIKE INSPECTION IAW WORK CARD 05-200-00. NO DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M)
ORD - FLT 4333 - DURING CLIMB, CREW REPORTED HYDRAULIC 1 QTY MESSAGE ON EICAS. QUANTITY DROPPED TO BOTTOM OF GAUGE AND A E1 HYDRAULIC PUMP FAIL MESSAGE SHOWED ON EICAS. CREW DECLARED AN EMERGENCY. AFTER GEAR WAS SELECTED DOWN PUMP FAIL MESSAGE WENT AWAY. AIRCRAFT WAS LANDED AND TAXIED WITH NO FURTHER INCIDENTS REPORTED. MAINTENANCE FOUND AND REPLACED A SPOILER ACTUATOR FOR THE RIGHT SPOILER IAW EMB MM. OPERATIONAL AND LEAK CHECK WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M)
ABI - DURING AN MBV INSPECTION, THE RIGHT STRINGER 19 WAS FOUND TO BE CHAFED AT FRAME 52. BLENDED THE CHAFED AREA AND PERFORMED NDT INSPECTION WITH NO DEFECTS NOTED. FABRICATED A REPAIR ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB SRM (EMB 145/1142 REV 20) CHAPTER 53-24-02. (M)
ABI - DURING AN MBV INSPECTION LEFT STRINGER 19 WAS FOUND TO BE CHAFED AT FRAME 52. BLENDED THE CHAFED AREA AND PERFORMED NDT INSPECTION WITH NO DEFECTS NOTED. FABRICATED A REPAIR ANGLE AND SHIMS. REPAIR DONE IAW EMB SRM (EMB SRM 145/1142 REV 20) CHAPTER 53-24-02. (M)
ABI - DURING AN MBV INSPECTION, THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED BELOW SRM LIMITS. PERFORMED A CUT OUT OF THE DAMAGED SECTION OF THE LEFT FLOORBEAM. FABRICATED AN EXTERNAL ANGLE, FILLER AND SHIMS. REPAIR DONE IAW EMB 145 SRM (SRM 145/1142 REV 20) CHAPTER 53-21-10 FIGURE 201 SHEET 1. (M)
ABI - THIS LEVEL 2 FINDING FOUND DURING MBV INSPECTION REFERENCE CRIC NR 27875, CENTER BEAM GUSSET CORRODED. REMOVED AND INSTALLED SERVICEABLE CENTER BEAM GUSSET IAW EMB 145 SRM 51-40-02. (M)
ABI - THIS LEVEL 2 FINDING FOUND DURING MBV INSPECTION REFERENCE CRIC NR 27870. FORWARD DIAMOND GUSSET CORRODED. REMOVED AND INSTALLED SERVICEABLE GUSSET IAW EMB 145 SRM 51-40-02. (M)
ABI - THIS LEVEL 2 FINDING FOUND DURING MBV INSPECTION REFERENCE CRIC NR 27871, AFT DIAMOND GUSSET CORRODED. REMOVED CORRODED GUSSET AND INSTALLED SERVICEABLE GUSSET IAW EMB 145 SRM 51-40-02. (M)
ABI - THIS LEVEL 2 FINDING WAS FOUND DURING AN MBV INSPECTION REFERENCE CRIC NR 27872 SERVICE DOOR AFT SILL CORRODED. INSTALLED NEW AFT SERVICE DOOR SILL IAW EMB 145 SRM 51-40-02. (M)
ABI - THIS LEVEL 2 FINDING FOUND DURING MBV INSPECTION REFERENCE CRIC NR 27873. SERVICE DOOR FORWARD SILL CORRODED. REMOVED AND INSTALLED SERVICEABLE SILL IAW EMB 145 SRM 51-40-02. (M)