N639AE
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 | 2012-01-24 – 2012-01-24 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
HS VLV 2 FAIL APPEARED BEFORE TAKEOFF, CLEARED AFTER CYCLING BLEED 2 PB FACT 07APR23 21:01 PHL INSPECTED RELAY CONTACT/PINS FOR RELAYS K0528 AND K0552. REINSTALLED RELAYS, NO DEFECTS NOTED. RERACKED DAU1 AND DAU2. REMOVED AND REINSTALLED RH HIGH STAGE VALVE FILTER FOR INSPECTION IN REF WITH AMM 36-11-02. OPS CHECK GOOD, A/C OK FOR SERVICE AT THIS TIME
PACK 2 OVRTEMP FOLLOW PACK SHUTDOWN MULTIPLE TIMES INFLIGHT. FOLLOWED FIM TASK 21-51-00. PERFORMED OPS CHECK IAW EMB 145 AMM 21-5-00. OPS CHECK GOOD. NO DEFECTS OR FAULT MESSAGES NOTED. THIS CLEARS MEL 21-15-1. OK FOR SERVICE.
CORROSION BETWEEN STRINGER 17L AT FRAME 60-61. REPARIED IAW EO1-53-23-0043 DAMAGE WAS ON STRINGER SECTION THAT WAS REPLACED
PDIS 639 36-11 2907393 14FEB23 CLT CLOSE ON TAKE OFF ROLL RECIEVED HS VLV FAIL ON EICAS. DID NOT KNOW WHICH SIDE SUSPECT ENGINE 2. 30123 00 AKR FACT 14FEB23 19:29 CLT UPON ARRIVAL TO AIRCRAFT NO CMC OR RELATING FAILURE EICAS MSGS WERE DISPLAYED. PERFORMED OPS CHECK ON 1 AND 2 ENG IAW AMM 36-11-07-700-801-A OPS CHECK GOOD. A/C OK FOR SERVICE.
PDIS 639 05-50 2662134 28AUG22 CLT ASSGN ENG 1 SHUTDOWN UNCOMMANDED IN FLIGHT. 22-26K FT. (NO ROTATION WITH ATTEMPTED RESTART, CREW SAID DURING CLIMB THE VERTICAL POWER FELT WEAKER THAN USUAL BUT ENG1 N2 INDICATION NORMAL) ORIGINAL LOG PAGE 266213 SEQ 2 .... AIRCRAFT CURRENTLY IN WORK. ENGINE CHANGE IS EXPECTED. MORE INFO WILL BE PROVIDED THROUGH SUPPLEMENTAL INFORMATION WHEN AVAILABLE.
CAPTAIN'S RUDDER PEDAL EASILY COMES OFF TRACK. FOUND 2 BOLTS SHEARED FROM RUDDER PEDAL GUIDE REGULATOR. REMOVED SHEARED BOLTS AND INSTALLED NEW BOLTS IN REF TO AMM 20-10-01 AND SAFETIED IN REF TO AMM 20-10-02. PERFORMED OPS CHECK TO THE PEDAL ACTUATOR IN REF TO AMM 27-21-07-400-801-A SUBTASK 842-002-A. OPS CHECK GOOD.
EMERGENY LIGHT ABOVE FLIGHT ATTENDANT SEAT AND MAIN DOOR INOPERATIVE. REMOVED AND REPLACED BATTERY POWER SUPPLY IRT F EMB 145 AMM 33-50-04 OPS CHECK GOOD OK FOR SERVICE
BLEED 2 VALVE FAILED AT 40 KNOTS ON TAKEOFF, FAILED FOR THE SECOND TIME. R & R BLEED VALVE ON #2 ENGINE PER FIM 36-11-00,AND AMM 36-11-05. NO FIX, LEAK CHECK GOOD. R & R HIGH STAGE PRESSURE SWITCH IN REF TO 36-11-20. OPS CHECKED GOOD. AC OK FOR SERVICE.
ON TAKE OFF ROLL W/ THRUST LEVERS ADVANCED BLEED 2 VLV FAIL APPEARS ON EICAS. R&R'D #2 ENGINE BLEED VALVE IAW EMB AMM 36-11-05-000-801-A AND 36-11-05-400-801-A. OPS AND LEAK CHECK GOOD. AC OK FOR SERVICE.
FOUND MULTIPLE V BAND CLAMPS IN LH PYLON AROUND PRECOOLER AND MULTIPLE CLAMPS IN LH PACK AREA TO BE LOOSE. RE TORQUED CLAMPS IRW E145 AMM 20-10-01. OPS CHECK IRW E145 AMM 36-00-00. NO LEAKS OR MESSAGES. OPS CHECK GOOD.
BLEED 1 LEAK EICAS MSG DISPLAYED C/W RMM 36-11-05. LEFT ENG BLEED INOP WITH APU BLEED AIR CURRENTLY ON THE MEL. OPEN
HEAVY CHECK - CARGO DOOR AFT FRAME BENT AT LOWER END...REMOVED BENT CARGO DOOR LOWER AFT FRAME CONTINUOUS STOP AND INSTALLED SERVICEABLE CONTINUOUS STOP IAW EMB 145 SRM 51-40-02.
HEAVY CHECK - EXTERIOR SKIN CORRODED BTW FR 66-67 STR 21L-21R...ACCOMPLISHED REPAIR OF EXTERIOR SKIN CORROSION BTW FR 66-67 STGR 21L-21R IAW ETD# ETD2020-145-020488.
HEAVY CHECK - CARGO DOOR HANDLE CUTOUT CRACKED AT AFT UPPER END. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER ON CARGO DOOR IAW ETD2020-145-020134 AND EO1-52-20-0259.
HEAVY CHECK - CARGO DOOR HANDLE CUTOUT CRACKED AT AFT UPPER END. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER ON CARGO DOOR IAW ETD2020-145-020134 AND EO1-52-20-0259.
DURING HEAVY CHECK, RIGHT MLG AFT UPPER TRUNNION HAS A RELEVANT INDICATION OUTBD AREA. R & R THE RT MLG UPPER AFT TRUNNION IAW EO1-57-20-0253.
DURING HEAVY CHECK, RIGHT WING RIB 21 HAD A POSSIBLE CRACK. PERFORMED HFEC INSPECTION IAW EASI NDTM RELEVANT INDICATION NOTED. PERFORMED A CUT-OUT OF CRACKED AREA ON THE RT WING RIB IAW SRM 57-20-07, ITEM 4, FIG 203. FABRICATED AND DRILLED A DOUBLER, FILLER, AND SHIM IAW SRM 57-20-07, ITEM 4, FIG 203.
DURING HEAVY CHECK, LEFT WING RIB 21 WAS CRACKED. PERFORMED A CUT-OUT OF CRACKED AREA IAW SRM 57-20-07, ITEM 4, FIG 203. FABRICATED AND DRILLED A DOUBLER, FILLER, AND SHIM FOR REPAIR OF LH WING RIB 21 IAW SRM 57-20-07, ITEM 4, FIG 203.
DURING HEAVY CHECK, FRAME 81 WAS CHAFED THROUGH AT THE 6 O'CLOCK POSITION. R & R THE LOWER SECTION OF THE FRAME IAW SRM 51-40-02.
DURING HEAVY CHECK, CARGO DOOR CUT-OUT LOWER SILL CORRODED. REMOVED AND INSTALLED A SERVICEABLE CARGO DOOR CUT-OUT LOWER SILL IAW SRM 51-40-02.
DURING HEAVY CHECK, THE SERVICE DOOR LOWER CENTER SILL WAS CORRODED. FABRICATED AND INSTALLED A DOUBLER IAW SRM 53-21-02 RE ITEM 2.
DURING HEAVY CHECK, LEFT WING WING SPAR I LOWER FLANGE AT RIB 9 WAS FOUND TO BE CRACKED. FOUND DURING HFEC INSPECTION. REPAIRED THE LT WING SPAR I LOWER FLANGE IAW SRM 57-20-05, AND CW EO1-57-20-0252.
HEAVY CHECK - PAX DOOR LOWER FRAME CRACKED INSIDE THE LOWER AFT CORNER BAY BELOW THE AFT LOWER DOOR STOP. REMOVED AND REPLACED PAX DOOR LOWER FRAME AFT FRAME SECTION IAW SRM 51-40-02
HEAVY CHECK - PAX DOOR LOWER FRAME CRACKED INSIDE THE LOWER AFT CORNER BAY BELOW THE AFT LOWER DOOR STOP...REMOVED AND REPLACED PAX DOOR LOWER FRAME AFT FRAME SECTION IAW EMB 145 SRM 51-40-02
DURING HEAVY CHECK, THE LT OMEGA BEAM SUPPORT COLUMN AT FRAME 25 WAS CRACKED. REMOVED AND REPLACED THE LT OMEGA BEAM SUPPORT COLUMN AT FRAME 25 IAW SRM 51-40-02.
HEAVY CHECK - 2 POSSIBLE SKIN CRACK AROUND RIVETS AT FR 80 BTW STR 6L-7L....CUT OUT DAMAGED SKIN AROUND LOWER FASTENER AT FR80 BTW STGR 6L-7L IAW EMB 145 SRM 53-32-01. MADE REPAIR BUSHING IAW EMB 145 SRM 53-32-01 9,H,1-7.
HEAVY CHECK - CARGO DOOR INTERNAL HANDLE BUCKET CRACKED (AFT)...REMOVED AND INSTALLED AND EDGE SEALED CARGO DOOR INTERNAL HANDLE BUCKET IAW ETD2020-- 145-021325, EMB 145 SRM 51-40-02 AND EMB 145 SRM 51-20-01. AND EO1-05-20-0264
HEAVY CHECK - 2 POSSIBLE SKIN CRACK AROUND RIVETS AT FR 78 BTW STR 4R-5R...CUT OUT DAMAGED SKIN AROUND UPPER FASTENER AT FR78 BTW STGR 4R-5R IAW EMB 145 SRM 53-32-01.MADE REPAIR BUSHING IAW EMB 145 SRM 53-32-01 9,H,1-7.
HEAVY CHECK - 2 POSSIBLE SKIN CRACK AROUND RIVET AT FR 77 BTW STR 5R-6R...CUT OUT DAMAGED SKIN AROUND RIVET IAW SRM 53-32-01. MADE REPAIR BUSHING IAW SRM 53- 32-01 9,H,1-7.
HEAVY CHECK - 2 POSSIBLE SKIN CRACK AROUND RIVETS AT FR 77 BTW STR 7R-8R...CUT OUT DAMAGED SKIN AT UPPER FASTENER IAW SRM 53-32-01. MADE REPAIR BUSHING IAW SRM 53-32-01 9,H,1-7.
PDIS 639 27-41 2161322 18MAR20 PHL CLOSE MAIN PITCH TRIM INOP ON EICAS DURING FLIGHT 24848 00 MDC FACT 18MAR20 11:34 PHL REMOVED AND REPLACED HORIZONTAL STAB CONTROL UNIT IA W EMB 145 AMM 27-40-01 OPERATIONAL TEST SATISFACTORY OK FOR SERVICE
#1 HIGH STAGE VALVE FAILURE INDICATED DURING TAKE OFF ERROR MESSAGE EXTINGUISHED. MAINTENANCE PERFORMED OPS CHECK ON #1 HIGH STAGE VALVE WITH CREW OPS CHECK GOOD OPS CHECK DONE IAW AMM 36-11-02. OK FOR SERVICE.
PDIS 639 36-21 2095942 26SEP19 PWM CLOSE ON TAKEOFF ROLL BLD 1 VLV FAIL MESSAGE APPEARED ON E ICAS. FACT 27SEP19 03:49 MDT R&R'D #1 BLEED VALVE & REACTIVATED IRT EMB MM 36-11-05. GROUND RUN OPS CHECK GOOD AT THIS TIME.
RTO AT 40KTS DUE CAUTION LIGHT ILLUMINATED. NO EMERGENCY. ISSUE WAS FIXED ITSELF SOON AFTER EXITING THE RUNWAY. FLT CONTINUE ON TO OAJ LOCATION.
PDIS 639 36-21 2095731 05SEP19 RIC CLOSE #1 BLEED VLV EICAS MSG ON TAKEOFF FACT 05SEP19 04:36 RIC REMOVED AND REPLACED #1 ENG BLEED VALVE IN REF TO AMM 36-11-05-000/400-801A. OPS CHECK #1 BLEED SYSTEM O IN REF TO AMM 36-00-00-700-803A OPS CHECK GOOD AT THIS TIME OK FOR SERVICE CLEAR MEL 36-21.
#1 BLEED VALVE EICAS MESSAGE ON TAKE-OFF. REMOVED AND REPLACED NR 1 BLEED VALVE IN IAW AMM 36-11-05-000/400-801A. OPS CHECK NR 1 BLEED IAW AMM 36-00-00-700-803A. OPS CHECK GOOD AT THIS TIME.OK FOR SERVICE
UPON T/O ROLL, A BLEED CAUTION LIGHT APPEARED FOLLOWED BY BLD WARNING LIGHT. T/O ABORTED. NO CMC RELATED MESAGES FOUND ON MFD DOWNLOAD. FIX: PERFORMED AIR BLEED SYS OPS CHECK/TEST IAW AMM 36-00-00-700-803-A. OPC CHECK GOOD. NO MESSAGES FOUND. OK FOR SERVICE AT THIS TIME.
NDIS 639 33-51 0011920 25MAY19 RIC CLOSE EMER FLOOR STRIP @ SEAT 14 & 15A INOP 32622 00 BRA ACT 25MAY19 11:39 RIC R/R THE EMERGENCY FLOOR PROXIMITY STRIP AT SEAT 14 &15A IN REF TO AMM 33-50-12-000/400-801-A OPS CHECK GOOD OK FOR SERVICE P/N LIGHT 1250613 P/N OFF LIGHT 1250615.
PDIS 639 32-10 1689331 24NOV18 MDT CLOSE NLG DOOR STUCK OPEN. DFRL 25NOV18 06:25 MDT REF:EMB FIM 32-32-00-810-802,DOWNLOADED CMC IN REF TO W/C 45-90-00-NO ASSOCIATED MESSAGES. MERLIN HISTORY INDICATED NLG DOOR SOLIENIOD VALVE WAS R&R'D. FACT 25NOV18 06:29 MDT FOUND UPLOCK PROXIMITY SWITCH BAD.R&R'D UPLOCK PROX SWITCH IN REF TO AMM 32-63-03/GAP REF AMM 32-63-05.SWUNG GEAR SEVERAL TIMES.LANDING GEAR OPS CHECKED GOOD IN REF TO AMM 32-30-00. OK FOR SERVICE @ THIS TIME.
PDIS 639 30-21 1689141 05NOV18 PIT CLOSE E1 ANTI ICE VALVE FAIL MESSAGE DISPLAYED ACFT WAS IN ICING IN CLIMB. ALSO ADVISORY MSG E-ANTI ICE OVER PRESS DISPLAYED. C/W MX PROCEDURE FACT 05NOV18 06:04 ROA REACTIVATED E1 ANTI-ICE VALVE PER AMM TASK 30-21-440-801-A. R/R'D RELAY K0534 IAW AMM TASK 20-13-02-04, PERFORMED A-ICE OPERATIONAL TEST TASK 30-00-00-700-802-A OPS CK GOOD CLEAR MEL.
PDIS 639 21-30 1698241 27SEP18 IAD CLOSE IN CLIMB AT APROZ 15000 FEET CABIN ALTITUDE REACHED ORANGE. HANUAL IMPUT HAD ON EFFECT ALL PRESSURIZATION INDICATIONS WERE DASHES ONCE ON GROUND CREW WAS UNABLE TO OPEN PAX DOOR. CB F8 WAS CYCLED WHICH RELEASED PRESSURIZATION HISTORY: NO, ACFT DIVERTED AND DECLARED EMERGENCY MEL 27SEP18 08:00 IAD C27005 21-10-3 PRESS CONTROL AUTO MANUAL FACT 28SEP18 09:32 MDT REACTIVATED PRES. CONTROL SYSTEM REF 21-31-03.OPS CHECKED IN MAN AND AUTO MODE REF 21-31-00 OPS CHECK FAILED.TROUBLESHOT REF FIM 21-31-00-810-803A TO BLOCK 14.R&RD ELEC. OUTFLOW VALVE OPS/LEAK CHECK GOOD.AUTO PASSED MAN FAILED.R&RD PNEUMATIC OUT FLOW VALVE.OPS/LEAK CHECK GOOD.AUTO PASSED.MAN PASSED.REF 21-30-04&21-31-03 PER EMB145 AMM.OK FOR SERVICE
FWD SEAT EMERGENCY LIGHT UNDER COCKPIT DOOR WAS INOPERATIVE. R & R THE EMERGENCY LIGHT.
BATTERY 1 OVER TEMP CONTINUED THERMAL RUNAWAY. BATTERY REACHED 82 DEGREES C BEFORE ARFF DISCONNECTED IT. NO FIRE OR IGNITION NOTED. R&R BATTERY ONE AND TWO IAW AMM24-36-01. OPS CK GOOD OK FOR SERVICE.
ALL 4 FLANGED BUSHINGS FOR RIGHT HAND AILERON TO PCA ATTACH POINTS ARE DAMAGED. -C/A-INSTALLED NEW PCA FITTING ON THE RIGHT HAND AILERON IAW EO WORK CARD EM-27M2-112.
APU FIREWALL ANGLE AT FRAME 80 STR 9L IS CRACKED.
RT. OVERWING PANEL, #2 LOWER ATTACHMENT BRACKET CRACKED. -C/A-REMOVED, FABRICATED AND INSTALLED NEW ATTACHMENT BRACKET IAW ETN-EM-53-142.
RIGHT CABIN OUTBRD OMEGA BEAM SUPPORT, CRACKED BETWEEN FRAMES 47-48.-C/A-COMPLETED REPAIR IAW SRM 53-23-02.
LEFT CABIN OMEGA BEAM SUPPORT, CRACKED AT FRAME 50. -C/A-REMOVED AND REPLACED INDICATED L/H CABIN OMEGA BEAM SUPPORT IAW SRM 51-40-02.
BAGGAGE DOOR FORWARD FRAME BOX FOR LIFT/LOERING MECHANISM HAS CRACK AT FORWARD LOWER END.-C/A-COMPLETED REPAIR IAW SRM 53-23-02.
SHEAR CLIP AT FRAME 80, BETWEEN STRINGERS 05R AND 07R IS CRACKED.-C/A-REMOVED AND REPLACED SHEAR CLIP AT FRAME 80 BETWEEN STRINGERS 5R AND 7R IAW SRM 51-40-02.
DURING POST FLIGHT INSPECTION, SMOKE COMING OUT OF THE NR 1 ENGINE. PERFORMED AN INSPECTION OF THE NR 1 ENGINE. NO LEAKS FOUND AT THIS TIME. ENGINE OK TO RETURN TO SERVICE IAW ETN-EM-79-015.
SPS ADVANCE ILLUMINATED WITHOUT ICE CONDITIONS, FLAP LOW SPEED ILLUMINATED WITH SPS ADVANCE. REMOVED AND REPLACED FECU IAW AMM 27-53-02, OPS CHECKED GOOD.
FWD FUSELAGE SKIN CRACKED. REPAIRED THE SKIN IAW ERS-CR-53MR-2541
CREW REPORTED THAT THE NR 2 TIRE HAD A THROWN TREAD FAILURE. PERFORMED TASK CARD 05-50-15-200-801-A . REMOVED AND REPLACED NUM 1 MLG TIRE IAW WORK CARD 32-700-11 ALL CHECK SGOOD A/C OK FOR SERVICE. REMOVED AND REPLACED NUM 2 MLG TIRE IAW WORK CARD 32-700-11. ALL CHECKED GOOD. ACFT OK FOR SERVICE.
SEVERAL EMER LIGHTS INOPERATIVE. R & R NR 2 EMER BATTERY & CHARGER. OPERATIONS CHECKED GOOD IAW AMM 33-50-04. BATTERY CHARGER ASSEMBLY, PN 11-0049 & SN 18196.
EMERGENCY LIGHTS AT ROWS 1 - 5 DO NOT ILLUMINATE. RESET EMER LIGHTS & OPERATIONS CHECKED GOOD IAW AMM 33-50-00.
DURING MBV INSPECTION, A DENT WAS FOUND, BETWEEN FRAME 25 & 26, BETWEEN STRINGERS 20R & 21R. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. REPAIRED DENT IAW ERS-EM-53MR-1993. REPAIR MATERIALS, FILLER 2024-T3 .032 & DOUBLER 2024T3 .050.
DURING MBV INSPECTION, QA FOUND A CRACK ON THE LT WING RIB 5. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. R & R LT WING RIB 5 IAW ERS-EM-57MR-592. REPAIR MATERIALS, RIB 5 PN 145-67083-601.
DURING MBV INSPECTION, QA FOUND A CRACK AT A FASTENER HOLE ON FRAME 75, BETWEEN STRINGERS 2R & 3R. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. PERFORMED PERMANENT REPAIR ON CRACK AT FASTENER HOLE IAW ERS-EM-53MR-1980. REPAIR MATERIALS, DOUBLER 2024T3 .080, FILLER 2024T3 .063, REPAIR ANGLE 2024T3 .050, REPAIR ANGLE FILLER 2024T3 .032.
DURING MBV INSPECTION, QA FOUND 3 CRACKED AT FASTENER HOLES ON FRAME 75, BETWEEN STRINGERS 1L & 3L. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. PERFORMED PERMANENT REPAIR ON CRACKED FASTENER HOLES IAW ERS-EM-53MR-1980. REPAIR MATERIALS, DOUBLER 2024T3 .080, FILLER 2024T3 .050, REPAIR ANGLE 2024T3 .063, REPAIR ANGLE FILLER 2024T3 .032.
DURING MBV INSPECTION, QA FOUND RT WING SPAR 1 LOWER LE FLANGE CRACKED AT RIB 9. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. REPAIRED RT SPAR I CRACK AT RIB 9 IAW ERS-EM-57MR-593. REPAIR MATERIALS REINFORCEMENT ANGLE, PN TI-145-16-042-001 MADE FROM AL 7475-T7351, 1.750, FILLER AL 7075-T6, .125, INBD SPACER AL7075-T6, .043, OTBD SPACER AL7075-T6, .043.
DURING MBV INSPECTION, QA FOUND FRAME 68 SHEAR CLIP CORRODED AT LOWER END, BETWEEN STRINGERS 15L & 16L. ACFT WAS REMOVED FROM SERVICE & WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. REPAIRED IAW SRM 53-31-04 SECTION 4 F. REPAIR MATERIALS, SHEAR CLIP 145-25369-603.
DURING MBV INSPECTION, QA FOUND FRAME 70 RT SIDE GOUGED AT PREVIOUS REPAIR. ACFT WAS REMOVED FROM SERVICE & WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. REPAIRED IAW ERS EM-53MR-1941. REPAIR MATERIALS, EA9394 RESIN, SS301 SHEET 0.016" THICK.
DURING MBV INSPECTION, A DENT WAS FOUND BETWEEN FRAME 7 & 8, BETWEEN STRINGER 13R & 15R. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. REPAIRED DENT IAW ERS-EM-53MR-1954. REPAIR MATERIALS DOUBLER 2024T3 0.040", FILLER 2024T3 0.032".
DURING MBV INSPECTION, A DENT WAS FOUND, BETWEEN FRAME 7 & 8, BETWEEN STRINGERS 13R & 15R. ACFT WAS REMOVED FROM SERVICE & WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. REPAIRED DENT IAW ERS-EM-53MR-1954. REPAIR MATERIALS, DOUBLER 2024T3 0.040", & FILLER 2024T3 0.032".
DURING PNEUMATIC ANTI-ICE TEST, RECEIVED EICAS WG ANTI-ICE FAIL MSG. COMPLIED WITH AOM VOL 1 PROCEDURES & RETURNED WITHOUT INCIDENT. R & R WING ANTI-ICING ASYMMETRY PRESS TRANSDUCER IAW MM 0-11-13. OPERATIONS CHECK OF ANTI-ICING SYS GOOD IAW MM 30-00-00. MEL ITEM IS RESTORED.
AFTER TAKEOFF RT MLG DID NOT RETRACT. YELLOW IN TRANSIT LIGHT CAME ON & THERE WAS A SLIGHT YAW ASSOCIATED. ANTI-ICE ACCT MECH GEAR PROBLEM. FLIGHT DECLARED EMER. R & R RT MLG UNLOCKING ACTUATOR IAW AMM 32-33-09. LEAK & OPERATIONS CHECKED GOOD.
LEFT OTBD TIRE DAMAGE? NR 1 MLG OTBD TIRE MISSING TREAD? R & R NR 1 MLG TIRE ASSEMBLY. PERFORMED BRAKE ASSEMBLY CARBON INSPECTION IAW WC 32-700-11 & 32-700-18.
AFT CEILING EMER LIGHT INOPERATIVE. R & R AFT CEILING EMER LIGHT BULB IAW AMM 33-50-08-000-801-A & 33-50-08-400-801-A. OPERATIONS CHECKED GOOD END.
REAR FLASHLIGHT WILL NOT CHARGE. R & R REAR FLASHLIGHT ASSEMBLY. OPERATIONS CHECKED GOOD IAW 33-50-16.
AT FL 350 NR 2 HAD A SUDDEN POWER LOSS OF AROUND 15 PERCENT, N1 CAME BACK TO NORMAL FEW SECONDS LATER. TROUBLESHOOT RT ENGINE AND FOUND FAULTY FADEC 2B. REMOVED AND REPLACED THE FADEC 2B IAW AMM 73-22-01. RESET FADECS AND INSPECTED LABELS IAW AMM 73-22-01-700-801-A AND OPERATED ENGINES IAW ROLLS ROYCE MM 72-00-00. NO DEFECTS NOTED.
FLIGHT ATTENDANT FLASHLIGHT SWITCH IS BROKEN. R & R FLIGHT ATTENDANTS FLASHLIGHT IAW AMM 33-50-16. OPERATIONAL CHECKED GOOD.
EMERGENCY LIGHT IN AFT CABIN, LAST ROW, INOPERATIVE. R & R THE LIGHT AT ROWS 17 & 18 IAW AMM 33-50-12. OPS CHECKED GOOD.
MAIN DOOR EMER LIGHT INOPERATIVE. R & R LAMP FOR THE MAIN DOOR LINING EMER LT IAW AMM TASKS 33-50-10-000-801-A & 33-50-10-400-801-A. OPERATIONS CHECKED GOOD.
RT ENG PYLON FWD YOKE CRACKED AT LOWER ENG MOUNT. R & R RT LOWER FWD YOKE IAW EO EM-54MR-386.
FRAME 73 SHEAR CLIP BETWEEN STRINGER 8L & 10L CRACKED. R & R FRAME 73 SHEAR CLIP BETWEEN STRINGER 8L & 10L IAW SRM 53-31-04.
RIGHT ENG STARTER CONTROL VLV OTBD SUPPORT BRACKET CRACKED. R & R RT ENG STARTER CONTROL VLV OTBD SUPPORT BRACKET IAW AMM 80-10-02.
LEFT NR 1 EMERGENCY LIGHT STRIP IS CRACKED. REMOVED & ACQUIRED LT NR 1 EMERGENCY LIGHT STRIP SEE BOW 150844 FOR INSTALLATION IAW AMM 33-50-12.
LEFT NR 7 EMERGENCY LIGHT STRIP IS CRACKED. R & R LT NR 7 EMERGENCY LIGHT STRIP IAW AMM 33-50-12 SEE BOW 150877 FOR OPERATIONAL CHECK.
LAVATORY CTR BEAM GUSSET IS CORRODED AT CARBON CTR BEAM. R & R LAVATORY CTR BEAM GUSSET IAW SRM 51-40-02.
CARGO UNDERFLOOR LT BLEED AIR TUBE SUPPORT BETWEEN FRAME 68 & 69 CRACKED. REMOVED & INSTALLED LT BLEED AIR TUBES UNDER & ABOVE BLEED AIR TUBE SUPPORT BETWEEN FRAME 66 & 69 IAW AMM 36-11-09, LEAK CHECKED GOOD.
LEFT CARGO FLOOR SILL IS CORRODED FWD OF FRAME 61 & LAVATORY CARBON BEAM. R & R LT CARGO FLOOR SILL FWD OF FRAME 61 IAW SRM 51-40-02.
CARGO DOOR CUT OUT RAMP SUPPORT ANGLE AT FRAME 66 CRACKED. REMOVED & INSTALLED NEW CARGO DOOR CUT OUT RAMP SUPPORT ANGLE AT FRAME 66 IAW SRM 51-40-02.
RIGHT CARGO FLOOR SILL IS CORRODED FWD OF FRAME 61 & LAVATORY CARBON BEAM. R & R RT FLOOR SILL AT FRAME 61 IAW SRM 51-40-02.
BAGGAGE DOOR LOWER NUTPLATE HOLES HAVE SURFACE CORROSION. REPAIRED BAGGAGE DOOR LOWER NUTPLATE HOLES IAW ERS-EM-5200-104.
RIGHT OVERWING FAIRING UPPER ATTACHMENT FLANGE SUPPORT BRACKET BETWEEN FRAME 48 & 49 CRACKED. R & R RT OVERWING FAIRING UPPER ATTACHMENT FLANGE SUPPORT BRACKET BETWEEN FRAME 48 & 49 IAW SRM 51-40-02.
LEFT NR 2 EMERGENCY LIGHT STRIP WIRE UNDER FLOOR IS BROKEN. REPAIRED LT NR 2 EMERGENCY LIGHT STRIP WIRE UNDER FLOOR IAW SWPM 20-21-00 STEP 5 & WM 20-00-03. REFER TO BOW 150877 FOR OPERATIONS CHECK.
APU FIREWALL CRACKED ON RT SIDE AT 3 O'CLOCK POSITION, REPAIR IAW EO EM-53AD-1883 PART C. FABRICATED & INSTALLED FILLER & DOUBLER FOR CRACKED RIVET HOLES & CRACK THAT WAS PREVIOUSLY STOP DRILLED AT THE 3 O'CLOCK POSITION ON THE APU FIREWALL IAW AMM 53-32-13, SRM 51-40-02, SRM 51-20-03 & ETN'S EM-53-244 R1, EM-53-242.
CENTER BEAM NR 1 SEAT TRACK IS CORRODED. R & R CTR BEAM NR 1 SEAT TRACK IAW AMM 53-01-06.
SHEAR CLIP CRACKED ON FRAME 24 BETWEEN STRINGERS 15R - 16R. R & R SHEAR CLIP ON FRAME 24, BETWEEN STRINGER 15R & 16R IAW SRM 51-40-02.
SHEAR CLIP CRACKED ON FRAME 26 BETWEEN STRINGERS 15R - 16R. R & R SHEAR CLIP AT FRAME 26, BETWEEN STRINGER 15R & 16R IAW SRM 51-40-02.
LEFT OVERWING PANEL LOWER BRACKET NR 2 IS CRACKED. LT OVERWING PANEL LOWER BRACKET NR 2 CRACKED HAS BEEN REMOVED & INSTALLED SERVICEABLE LT NR 2 LOWER BRACKET IAW ETN-EM-53-142.
RIGHT OVERWING PANEL LOWER BRACKET NR 2 IS CRACKED. RT OVERWING PANEL LOWER BRACKET NR 2 CRACKED HAS BEEN REMOVED & REPLACED WITH SERVICEABLE NR 2 BRACKET IAW ETN-EM-53-142.
DURING TAKEOFF ROLL WE HAD A NO TAKEOFF CONFIG WARNING ON EICAS WITH NO AURAL WARNING. TAKEOFF OK WAS HEARD PRIOR TO TAKEOFF & AFTER ABORTED TAKEOFF. R & R RELAY K0212 IAW AMM 20-13-02. R & R AURAL WARNING UNIT IAW AMM 31-51-01. OPERATIONS CHECKED IAW AMM 31-51-00. OPERATIONS CHECKED GOOD.
DURING MAINTENANCE INSPECTION ON FLIGHT 3496 FOUND MAIN CABIN DOOR HARD TO OPEN. LUBRICATED MAIN CABIN ENTRY DOOR MECHANISM IAW AMM 52-18-00, OPERATIONS CHECKED GOOD.
AFTER TAKEOFF HAD ENG 1 LOW PRESS INDICATION. THE RELAY COULD BE HEARD BEHIND CAPTAIN SEAT GOING ON & OFF CONSTANTLY. PROBLEM WAS FOUND WHEN USING PUMP 1B ON NR 1 ENG. AIRCRAFT WAS REMOVED FROM SERVICE. R&R FUEL PUMP 1B IAW EMB 145 AMM 28-21-01. OPC AND LEAK CHECK GOOD MEL RESTORED.
F/A EMERGENCY FLASHLIGHT INOPERAITVE. R & R F/A EMERGENCY FLASHLIGHT.OPS CHECKED GOOD.
F/A FORWARD FLASHIGHT HOLDER IS COMING LOOSE. SECURED F/A FLASHLIGHT, AMM 20-10-05.
CREW REPORTED EMERGENCY FLASHLIGHT ASSY ABOVE F/A CHAIR WAS DETACHED FROM THE WALL. INSTALLED MISSING SCREW IN FLASHLIGHT ASSEMBLY. IAW AMM 20-00-00. ACFT RETURNED TO SERVICE.
LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R LAMP IAW AMM 33-50-10-000-801-A AND 33-50-10-400-801-A, OPS CHECKED GOOD.
ON FLIGHT 3574 THE CREW REPORTED THE CAPTAINâS FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN'S FLASHLIGHT IAW/CMM 25-60-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 3216 THE CREW REPORTED THE EMERGENCY FLASHLIGHT ABOVE FLIGHT ATTENDANT JUMPSEAT WON'T STAY IN CRADLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLASHLIGHT IAW AMM# 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 3439 THE FLIGHT ATTENDANT REPORTED THE FLOOR LIGHTING AFT OF OVERWING EXIT ON THE LEFT SIDE OF AIRCRAFT DOES NOT HAVE DIRECTIONAL ARROWS POINTING FORWARD. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED EMERGENCY LIGHT STRIP IN FRONT OF LAV IAW EMB-145 AMM 33-50-12. THE OPERATIONAL TEST WAS GOOD IAW EMB-145 AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 3439 THE CREW REPORTED THE NOSEWHEEL STEERING HAS PRONOUNCED VIBRATION AT LOW SPEED AND AIRCRAFT PULLS RIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NOSE LANDING GEAR WHEEL ASSEMBLIES WC 32-700-17 TAXI CHECK IAW GHC. NO DISCREPANCY FOUND. THE AIRCRAFT WAS RETURNED TO SERVICE.
FOR FLIGHT 4128 THE FLIGHT ATTENDANT REPORTED AFTER LANDING SHE NOTICED AN ELECTRICAL ODOR EMITTING FROM THE TOILET SECTION (ELECTRICAL BURNING SMELL). THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED GENERAL VISUAL INSPECTION OF LAV LIGHTS /BALLAST AND LAV MOTOR. FOUND UPPER LAV LIGHT BALLAST BLOWN. REMOVED AND REPLACED BALLAST IAW EMB 145 AMM 33-28-02 COULD NOT REPRODUCE ODOR. NO DEFECTS NOTED. THE LAV LIGHT OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 3560 THE FLIGHT ATTENDANT REPORTED THE PASSENGER DOOR WAS DIFFICULT TO OPERATE WHEN OPENING. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED AND LUBED PASSENGER DOOR IAW EMB AMM 52-18-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 4152 THE CREW REPORTED THE FIRST OFFICERâS FLASHLIGHT CRADLE RETENTION CLIP WAS BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICERâS FLASHLIGHT CRADLE IAW EMB-145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 3908 THE CREW REPORTED THE AFT SECTION OF THE FLOOR EMERGENCY LIGHTS WERE NOT ILLUMINATING. DEFERRED PER MEL 33-30 AUTH 101342-C. REMOVED AND REPLACED THE NR 4 PROXIMITY STRIP IAW EMB-145 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. INSTALLED NEW CONTACT PIN ON STRIP 6 WIRE LEADING TO SPLICE SP9210 IAW WM 20-50-01. WIRE WAS BROKEN. THE OPERATIONAL CHECK WAS GOOD. MEL RESTORED. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 4199 THE CREW REPORTED, DURING TAKEOFF RECEIVED A LANDING AIR/GROUND FAIL MESSAGE ON EICAS. THE MESSAGE WENT AWAY AFTER APPROX 3 MINUTES. THE CREW DECLARED AN EMERGECNY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NOSE LANDING GEAR WEIGHT ON WHEELS HARNESS W019 REF EMB AMM 32-00-03. PERFORMED GEAR EXTENSION/RETRACTION CHECK IAW EMB AMM 32-30-00. THE OPERATIONAL CHECK WAS GOOD. NO RELATED MAINTENANCE OR CMC MESSAGES NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 4352, DURING CLIMB-OUT AIRCRAFT FAILED TO PRESSURIZE IN THE AUTO MODE. THE AIRCRAFT WAS REMOVE FROM SERVICE. REMOVED AND REPLACED AUTO PRESSURIZATION DIGITAL CONTROLLER IAW EMB 145 AMM 21-31-01. OPS CHECK GOOD. ALSO PERFORMED MANUAL PRESSURIZATION CONTROL OPS CHECK IAW EMB 145 AMM 21-31-01. OPS CHECK GOOD. ALL PANELS VERIFIED AS SECURE. THE AIRCRAFT RETURN TO SERVICE.
DURING MAINTENANCE INSPECTION, FOUND THE EMERGENCY LIGHT CONNECTOR BROKEN AT FLOOR PANEL 241BF. AIRCRAFT REMOVED FROM SERVICE. REPAIRED THE EMERGENCY LIGHT STRIP MALE CONNECTOR ON AIRCRAFT SIDE IAW WM 20-21-00. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
DURING MAINTENANCE INSPECTION, FOUND THE NR 1 EMERGENCY LIGHT STRIP HAS BROKEN WIRES. AIRCRAFT REMOVED FROM SERVICE. REPAIRED EMERGENCY LIGHT STRIP FEMALE CONNECTOR ON AIRCRAFT SIDE IAW WM 20-21-00. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
DURING MAINTENANCE INSPECTION, FOUND THE CABIN CEILING PANEL 253CLC EMERGENCY LIGHT WIRE BROKEN. AIRCRAFT REMOVED FROM SERVICE. REPAIRED EMERGENCY LIGHT WIRE ON CABIN CEILING PANEL 253CLC IAW WM 20-21-00. EMERGENCY LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
DURING B INSPECTION, FOUND THE GALLEY CROSSBEAM CORRODED BETWEEN FRAMES 24-25. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND INSTALLED NEW SERVICEABLE GALLEY CROSSBEAM BETWEEN FRAMES 24-25 IAW SRM. 51-40-02,51-40-09,51-20-03,51-20-01. AIRCRAFT RETURNED TO SERVICE.
DURING MAINTENANCE INSPECTION FOUND THE LEFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LIGHT IAW EMB 145 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY LIGHT ON LEFT OVER WING INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT ON LEFT OVER WING IAW EMB-145 AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING B-INSPECTION FOUND THE MAIN DOOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND LOOSE GROUND TERMINAL ON LIGHT ASSEMBLY. RE-SECURED GROUND TERMINAL IN REFERENCE WITH EMB 145 AMM TASKS 33-50-06-000-802-A & 33-50-06-400-802-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 3376 THE CREW REPORTED A LIGHTING STRIKE. THE CREW DIVERTED TO LIT AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED LIGHTNING STRIKE INSPECTION IAW WC 05-200-00. PERFORMED PERMANENT REPAIR TO 12 EACH LIGHTNING STRIKE DAMAGES BETWEEN FR1L AND FR6L AND STRS 11L AND 17L IAW EMB 145 SRM 53-00-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 2944 DURING TAKEOFF THE CREW REPORTED, RECEIVED A NR 1 HYDRAULIC PUMP FAIL EICAS MESSAGE AT GEAR RETRACTION. THE CAPTAIN ELECTED TO RETURN TO MAF. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1 HYDRAULIC PUMP IAW EMB 145 AMM 29-10-04 LEAK CHECK OK AT THIS TIME. PART NUMBER 971808. SERIAL NUMBER MX600080. REMOVED AND REPLACED NR 1 HYDRAULIC ELECTRIC MOTOR DRIVEN PUMP IAW EMB 145 AMM 29-10-03. PART NUMBER MPEV30086. SERIAL NUMBER MX642084. LEAK CHECK GOOD AT THIS TIME. REMOVED AND REPLACED HYDRAULIC LINES AT LMLG ACTUATOR IAW EMB 145 AMM 32-10-01. LEAK CHECK GOOD AT THIS TIME. SYS BLEED C/W IAW AMM 29-10-00. REMOVED AND REPLACED HYDRAULIC LINES AT LMLG ACTUATOR IAW EMB 145 AMM 32-10-01, LEAK CHECK GOOD AT THIS TIME. SYS BLEED C/W IAW AMM 29-10-00. REMOVED AND REPLACED NR 1 HYDRAULIC SYSTEM PRESSURE, CASE AND RETURN FILTERS IAW EMB 145 AMM 29-10-08. NO CONTAMINATION FOUND. THE LEAK CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 4061 THE CREW REPORTED THE AFT CABIN EMERGENCY FLASHLIGHT CRADLE SHOWS SIGNS OF OVERHEATING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT CABIN EMERGENCY FLASHLIGHT CRADLE. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 33-50-16. THE AIRCRAFT WAS RETURNED TO SERVICE.
FLT 4076 AT FLT LEVEL 330, CREW REPORTED AT CRUISE CABIN PRESSURE WENT UP & WOULD NOT COME BACK DOWN. CREW BEGAN TO DESCEND TO FLT LEVEL 140 WHEN CABIN OXYGEN MASKS AUTO DEPLOYED. CREW FOLLOWED ACFT OPS MANUAL PROCEDURES. ACFT LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. R & R PRESSURIZATION CONTROLLER IAW MM 21-31-01, NO FIX. PRESSURIZATION PROBLEM STILL EXISTS. OPS CHECK WAS GOOD IN AUTO MODE AS WELL AS MANUAL MODE IAW MM 21-31-00. R & R GASPER FAN IAW AMM 21-23-03. THE OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.
DURING MAINTENANCE BASE VISIT FOUND THE UPPER LEFT EXTERIOR EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT EXTERIOR UPPER EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
FOR FLIGHT 2917 DURING INSPECTION FOUND THE NR 3 FLOOR EMERGENCY LIGHTING STRIP WILL NOT ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 3 EMERGENCY FLOOR LIGHT STRIP IAW EMB 145 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE BASE VISIT FOUND THE PREVIOUS REPAIR CHAFED ON STRINGER 19 LEFT AFT OF FRAME 52. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED PREVIOUS REPAIR ON STRINGER 19L AFT OF FRAME 52. FABRICATED NEW REPAIR AND INSTALLED IAW EMB SRM 53-24-02. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE BASE VISIT FOUND A CRACK ON THE LEFT FORWARD LOWER PYLON ENGINE YOKE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FITTING IAW EO EM-54MR-354. THE AIRCRAFT WAS RETURNED TO SERVICE.
FOR FLIGHT 2720 THE CREW REPORTED THE CABIN DOOR IS DIFFICULT TO CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBED THE MAIN CABIN DOOR IAW EMB-145 MM 52-10-00 AND CLEANED ROLLERS. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE BASE VISIT FOUND THE EMERGENCY EXIT SIGN LOCATED AT THE MAIN ENTRANCE DOOR TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE INVERTER IAW EMB AMM 33-50-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
FOR FLIGHT 3606 EN ROUTE THE CREW REPORTED, RECEIVED AN EICAS MESSAGE FOR HYDRAULIC 1 LOW AND A FEW MINUTES LATER ENGINE 1 HYDRAULIC PUMP FAIL MESSAGE AND A FEW MINUTES LATER HYDRAULIC 1 SYSTEM FAIL. THE CREW COMPLIED WITH THE AIRCRAFT OPERATIONS MANUAL. THE FLIGHT ATTENDANT ALSO REPORTED A VERY LOUD SQUEAL FROM THE SERVICE DOOR. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE ENGINE DRIVEN PUMP IAW EMB AMM 29-10-03. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 3897 THE CREW REPORTED AT LIFT OFF RECEIVED A CAUTION LANDING GEAR AIR/GROUND FAIL MESSAGE ON EICAS. THE CREW ELECTED TO RETURN TO CMH AND LANDED OVERWEIGHT WITH A NORMAL LANDING WITH A DESCENT RATE AT 100` PER MINUTE. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSPECTED AND FOUND NOSE LANDING GEAR WEIGHT ON WHEELS HARNESS WOI9 DAMAGED. PERFORMED LANDING GEAR EXTENSION/RETRACTION TEST WITH NO FAULTS NOTED IAW EMB 145 AMM 32-003. NO INSPECTION REQUIRED FOR OVERWEIGHT LANDING DUE TO SINK RATE WITHIN LIMITS IAW AE ETN EM-05-009. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 4118 - CREW REPORTED EMERGENCY EXIT SIGN ON STEP UNDER COCKPIT WILL NOT ILLUMINATE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED INVERTER NR 1 IAW EMB 145 AMM 33-50-11, OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
ON FLIGHT 3448 CREW REPORTED ODD ODOR COMING FROM LAST 2 ROWS OF CABIN. ACFT REMOVED FROM SERVICE. INSPECTED AND FOUND BALLAST AT 16A CEILING BURNED. REMOVED AND REPLACED BALLAST ABOVE ROW 16A IAW EMB 145 AMM 33-21-05 OPERATIONAL CHECKED GOOD. NO FURTHER ODOR NOTED. (K)
ENGINE TWO ON START VIBRATIONS INCREASED BETWEEN 35 TO 40 PERCENT, N1 REMAIN IN GREEN BAND. REMOVED AND REPLACED NUMBER TWO ENGINE IAW AMERICAN EAGLE WORK CARD. OPERATIONAL AND LEAK CHECK GOOD. RETURNED TO SERVICE.
LOUD THUMP HEARD FROM NOSE WHEEL WELL AREA DURING CLIMB AND CRUISE, THUMPS FELT IN FIRST OFFICER'S LEFT RUDDER PEDAL, SOUNDS LIKE NOSE WHEEL STEERING IS ACTIVATED. REMOVED AND REPLACED NOSE GEAR PROXIMITY SWITCH IAW EMB AMM 32-61-01. OPERATIONAL CHECK GOOD, FUNCTIONAL CHECK FLIGHT PERFORMED WITH NO DEFECTS NOTED. RETURNED AIRCRAFT TO SERVICE.
HYD 1 LOW QUANTITY IN FLIGHT, QTY REMAINED STABLE BUT LOW FOR 45 MINUTES. ENGINE 1 HYD PUMP FAIL IN FLIGHT ASSOCIATED WITH LOUD SQUEAL NOISE REPORTED BY F/A IN REAR CABIN. CREW DECLARED EMERGENCY AIRCRAFT LANDED SAFELY. RAI EMERGENCY/PARKING BRAKE THERMAL RELIEF VALVE, OPS CHECK GOOD IAW EMB145 AMM 32-44-06, RETURNED AIRCRAFT TO SERVICE. (M)
DURING TAXI CREW REPORTED FUEL SMELL IN THE CABIN AND COCKPIT. PASSENGER REPORTED THE SMELL AT ROW 8. MAINTENANCE GROUND RUN ENGINES TO CHECK AIR CONDITION SYSTEM FOR FUEL ODOR. NONE WAS DETECTED AT THIS TIME. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200503049) (K)
ORD - FLT 4057 - DURING CLIMB, CREW REPORTED A PITCH TRIM 1 INOPERATIVE MESSAGE ON EICAS. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT, IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)
CREW A FLAP FAIL MESSAGE WHEN FLAPS WERE RETRACTED AFTER TAKEOFF. FLAPS REMAINED AT 9 DEGREES. FOLLOWED AOM PROCEDURES AND LANDED WITH FLAPS AT 9 DEGREES AND OVERWEIGHT AT 42,800 AND 300 FPM. MAINTENANCE REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT IAW MFG MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE.
ON APPROACH, CREW SELECTED FLAPS TO 9 DEGREES AT WHICH POINT THEY RECEIVED FLAPS FAIL MSG AND FLAPS FAILED TO MOVE. DECLARED EMERGENCY AND LANDED SAFELY WITH 0 FLAPS. FPDU OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (SW21200406985)
EMERGENCY LIGHTS WILL NOT WORK FROM THE FLIGHT ATTENDANTS PANEL. REPLACED FLT ATTENDANT CONTROL PANEL IAW EMB 145 AMM 33-21-00. OPS CHECKED GOOD. (M)
EMERGENCY EXIT SIGN ABOVE GALLEY SERVICE DOOR INOPERATIVE AND EMERGENCY EXIT SIGN ON RT FW BULKHEAD IN FRONT OF SEATS 2 B,C INOPERATIVE. FOUND CONNECTOR P8530 OFF, RECONNECTED P8530. AC GOOD IAW MFG AMM. (SW21200406975)
ABI - DURING A IMBV INSPECTION STRINGER 19L WAS FOUND CHAFED BETWEEN FRAMES 52 AND 53. PERFORMED EDDY CURRENT INSPECTION NO DEFECTS NOTED. FABRICATED A REPAIR ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM 145/1142 REV 20, 53-24-02. (M)
ABI - DURING AN IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED DAMAGED BY BLENDING. CUT OUT A 1.062 INCH BY .562 INCH PORTION NEAR THE AFT END. PERFORMED EDDY CURRENT INSPECTION NO DEFECTS NOTED. FABRICATED TWO DOUBLERS FOR THE REPAIR TO THE CUTOUT AREAS. REPAIR DONE IAW EMB REPAIR STATEMENT 1C2003-145/0562 AND STANDARD SRM, SRM 145/1142 REV 20 PRACTICES. (M)
ABI - DURING A IMBV INSPECTION, THE CARGO DOOR CENTER SILL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED DAMAGED CENTER SILL AND INSTALLED SERVICEABLE SILL IAW EMB 145 SRM (SRM 145/1142 REV 20) CHAPTERS 51-20-01, 51-40-02, 51-40-04, 51-40-06 AND EMB 145 CPM 51-21-04 AND 51-21-05. (M)
ABI - THIS IS A LEVEL FINDING. RIGHT MAIN LANDING GEAR FORWARD MAIN BEARING CAP IS CORRODED. INSTALLED NEW CAP IAW EMB145 AMM 32-10-01 AND 32-10-03. (M)
FLT 3570 - CRP - CREW REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHTS FROM ROW 12 AFT WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FLOOR LIGHTING STRIP IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)
CID - FLT 3954 - ON TAKEOFF ROLL HAD NR 1 THRUST REVERSER DISAGREE AND THAN NR 2. ABORTED TAKEOFF AND RETURNED TO GATE. ADJUSTED LEFT AND RIGHT THRUST REVERSE ACTUATOR DOORS IAW AMM. OPS CHECK GOOD. (M)
ABI - DURING MBV INSPECTION UNDER FLOOR OF AIRCRAFT, THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED BEYOND SRM LIMITS AT FRAME 20. REMOVED AND REPLACED CORRODED AREA. WORK DONE IAW EMB SRM 145/1142 REV 12 CHAPTER 53-21-10 PATE 201 THROUGH PAGE 204. (M)
GRB - FLT 4200 - BAGGAGE COMPARTMENT SMOKE DETECTOR OVERHEAD WARNING LIGHT INOPERATIVE ISSUED CP MEL 26-09 AUTH 030152D CAT C. REMOVED AND REPLACED PUSH BUTTON OVERHEAD SWITCH IAW 20-13-04. OPS CHECK GOOD IAW EMB 145 AMM 26-10-00. (M)
CID - FLT 4463 - DURING CLIMB-OUT, CREW HAD BAGGAGE SMOKE WARNING. BOTTLES WERE USED. CREW RETURNED TO CID. DECLARED EMERGENCY. CFR MEET A/C AND NOTED NO EVIDENCE OF FIRE. A/C LANDED SAFELY, BUT HAD AN OVERWEIGHT LANDING. NO FURTHER INCIDENTS WERE REPORTED. BAGGAGE COMPT WAS MEL''''''''D DUE TO NO EXTINGUISHING SYSTEM. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. FIRE BOTTLES WERE REPLACED AND A OVERWEIGHT INSPECTION WAS COMPLIED WITH. (M)
DFW - FORWARD EMERGENCY EXIT LIGHT IN CABIN CAME ON BRIGHT BUT DIM VERY FAST. REMOVED AND REPLACED POWER SUPPLY AND REINSERTED LOOSE CONTROL WIRE. OPS CHECK GOOD. (M)
CLE - FLIGHT 4348 - CABIN ENTRY DOOR EMERGENCY FLOOD LIGHT INOPERATIVE. REMOVED AND INSTALL NR 1 EMERGENCY BATTERY CHARGER. OPS CHECK GOOD. (M)
ORD - FLT 4114 - ROW 12B EMERGENCY LIGHTS INOPERABLE. FOUND GROUNDING POINT DISCONNECTED, RECONNECTED AT GS8522DL. OPS CHECKED GOOD. (X)
ORD - FLT 4245 - LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. REMOVED AND REPLACED LANDING GEAR VALVE UP SOLENOID. AIRCRAFT RETURNED TO SERVICE. (X)