N905JH
Registered owner: AMERICAN AIRLINES INC, TX (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
AIRCRAFT WILL NOT PRESSURIZE DURING FLIGHT. AUTO & MANUAL PRESSURIZATION C/W MAINT AND FLIGHT CREW PROCEDURES. DUMP BUTTON SELECTED. PERFORMED OPERATIONAL CHECK OF BOTH MANUAL & AUTO PRESSURIZATION CONTROL SYSTEMS IAW AMM 21-31-00. OPS CHECK GOOD. DETERMINED TO BE TRANSITORY CONDITION.
FO AIRSPEED REMAINS AT ZERO DURING TAKEOFF ROLL. ON TAKEOFF ROLL SPS ADV MESSAGE ON EICAS. ABORTED TAKEOFF TWICE. PERFORMED ADC 1 AND ADC 2 LEAK CHECK IAW AMM 34-13-00-790-802-A MULTIPLE TIMES. NO DEFECTS NOTED. AIRSPEED AND ALT INDICATIONS CHECKED GOOD ON PFD 1 AND 2 USING BOTH ADCS COULD NOT DUPLICATE DISCREPACY ACFT GOOD FOR SERVICE
F111356 LH AILERON DAMPER ATTACHMENT FITTING IS GOUGED 2 EACH. RAR LH AILERON DAMPER ATTACHMENT FITTING IAW EMB 145 SRM 51-40-02
LEFT CARGO FLOOR SILL CORRODED BTWN FR 60-61. R & R LT CARGO FLOOR SILL IAW EMB 145 SRM 51-40-02.
CENTER OMEGA BEAM IS CRACKED AT THE FR25 STANTION. REPAIRED THE CENTER OMEGA BEAM AT THE FR. 25 STANTION IAW SRM 51-40-02, ETD2026-145-005274A AND PIEDMONT EO1-53-26-0154.
LH OMEGA BEAM IS CRACKED AT THE FR35 STANTION. ACCOMPLISHED REPAIR TO LH OMEGA BEAM AT THE FRAME 35 STATION IAW EMB 145 SRM 51-75-00, ETD2026-145-005461 AND EO1-53-26-0150.
LEFT OMEGA BEAM IS CRACKED AT THE FR 27 STANTION. REPAIRED THE LH OMEGA BEAM AT FR. 27 STANTION IAW EMB ETD2026-145-005372 REV A AND PIEDMONT EO1-53-26-0151
LH OMEGA BEAM IS CRACKED AT THE FR26 STANTION. ACCOMPLISHED REPAIR ON LH OMEGA BEAM AT FR 26 STANCHION IAW ETD 2026-145-005348 AND PIEDMONT EO1-53-26-0172.
CENTER OMEGA BEAM IS BLENDED BEYOND ALLOWABLE LIMITS JUST FWD OF THE FR29 CENTER AISLE CROSSBEAM
CENTER OMEGA BEAM IS CRACKED AT THE FR27 STANTION. ACCOMPLISHED PERMANENT REPAIR TO CRACKED CENTER OMEGA BEAM AT FR 27 STATION IAW ETD2026-145-005460 AND EO-1-53-26-0162.
CENTER FUSELAGE 1 EXTERNAL SKIN HAS DAMAGE AREA FROM PREVIOUS BLEND OUT BETWEEN FR22 AND FR23 AND BETWEEN STGR 19R AND STGR 20R. INSTALLED FABRICATED DOUBLER AND FILLER FOR REPAIR ON CENTER FUSELAGE 1 EXTERNAL SKIN FROM PREVIOUS BLEND OUT BETWEEN FR22 AND FR23 AND BETWEEN STGR 19R AND STGR 20R. IAW EMB 145 SRM 53-21-01RE FIGURE 204 AND PIEDMONT EO1-53-26-0173.
HORIZONTAL STABILIZER HINGE FITTING SLEEVE BUSHINGS 3 AND 4 ARE SCORED AND PITTED. REMOVED & REINSTALLED NR 3 AND 4 SLEEVE BUSHINGS, REWORKED #3 AND #4 HINGE FITTINGS TO 2ND OVERSIZE AND INSTALLED OVERSIZE #2 SLEEVE BUSHINGS. IAW EMB 145 SRM 55-10-02-RE FROM STEPS 2A UP TO AND INCLUDING 2F, AND FROM 2H UP TO AND INCLUDING STEP 2K AND EO1-55-26-0146.
SHEAR CLIP IS CRACKED AT FRAME 15 BETWEEN STRINGERS 15R-16R. R & R SHEAR CLIP AT FR 15 BETWEEN STRINGERS 15R-16R IAW EMB 145 SRM 51-40-02.
FRAME 80 SHEAR CLIP BETWEEN STR 5L/7L CRACKED. REMOVED AND REPLACED FRAME 80 SHEAR CLIP BETWEEN STR 5L - 7L IAW EMB 145 SRM 51-40-02.
CORROSION ON FRAME 20 SERVICE DOOR LOWER FWD CUT-OUT. ACCOMPLISHED REPAIR ON FR 20 SERVICE DOOR LOWER FWD CUT-OUT IAW EMB 145 SRM 53-00-04-RE, ITEM 16, FIGURE 208 AND EO1-53-26-0149.
FRAME 80 SHEAR CLIP BETWEEN STR 5L/7L CRACKED.. REMOVED AND REPLACED FRAME 80 SHEAR CLIP BETWEEN STR 5L - 7L IAW EMB 145 SRM 51-40-02.
AFT PRESSURE BULKHEAD AFT SIDE HAS A DENT WITH SCRATCH AT LT LOWER AREA. R & R AFT PRESSURE BULKHEAD LH LOWER AREA IAW EMB 145 SRM 51-40-02, ETD2026-145-006130 AND PIEDMONT EO1-05-26-0185.
CORROSION ON SERVICE DOOR CUT-OUT AFT SILL. R & R SERVICE DOOR CUT-OUT AFT SILL IAW SRM 51-40-02.
F111817 LAV. CENTER FLOOR SUPPORT IS CORRODED. RAR LAV CENTER FLOOR SUPPORT IAW EMB 145 SRM 51-40-02.
F111816 LAV. L/H FLOOR SUPPORT IS CORRODED. RAR LAV L/H FLOOR SUPPORT IAW EMB 145 SRM 51-40-02.
F111815 LAV. R/H FLOOR SUPPORT IS CORRODED. RAR LAV R/H FLOOR SUPPORT IAW EMB 145 SRM 51-40-02.
LAV. RT FLOOR SUPPORT CORRODED. RAR LAV RT FLOOR SUPPORT IAW SRM 51-40-02.
R/H SHEAR CLIP AT FR-26 BETWEEN STGRS 15R/16R HAS A CRACK. REMOVED AND REPLACED THE RH SHEAR CLIP AT FR. 26 BETWEEN STGRS. 15R-16R IAW EMB 145 SRM 51-40-02.
F111971 R/H SHEAR CLIP AT FR-25 BETWEEN STGRS 15R/16R HAS A CRACK. REMOVED AND REPLACED THE RH SHEAR CLIP AT FR. 25 BETWEEN STGRS. 15R-16R IAW EMB 145 SRM 51-40-02.
R/H SHEAR CLIP AT FR-24 BETWEEN STGRS 16R/17R HAS A CRACK. RAR R/H SHEAR CLIP AT FR-24 BETWEEN STGRS 16R/17R IAW EMB 145 SRM 51-40-02
F111866 CENTER OMEGA BEAM GUSSET #4 HAS NUMEROUS AREAS OF CORROSION. REMOVED AND INSTALLED NEW CENTER OMEGA BEAM GUSSET #4 IAW EMB 145 SRM 51-40-02.
F111864 LH OMEGA BEAM GUSSET #6 HAS NUMEROUS AREAS OF CORROSION. LH OMEGA BEAM GUSSET, REMOVED AND REPLACED LH OMEGA GUSSET #6 IAW EMB 145 SRM 51-40-02.
F111865 CENTER OMEGA BEAM GUSSET #3 HAS NUMEROUS AREAS OF CORROSION. R & R CENTER OMEGA BEAM GUSSET #3 IAW EMB 145 SRM 51-40-02.
R/H SHEAR CLIP AT FR-24 BETWEEN STGRS 15R/16R HAS A CRACK. RAR RH SHEAR CLIP AT FR 24 BETWEEN STGRS 15R-16R IAW EMB 145 SRM 51-40-02.
F111863 LH OMEGA BEAM GUSSET #5 HAS NUMEROUS AREAS OF CORROSION. RAR LH OMEGA BEAM GUSSET #5 IAW EMB 145 SRM 51-40-02.
F111860 LH CABIN FLOOR SILL #5 HAS NUMEROUS ARES OF CORROSION. RAR CABIN FLOOR SILL #5 IAW EMB 145 SRM 51-40-09, 51-40-02.
F111858 RH CABIN FLOOR SILL #5 HAS NUMEROUS ARES OF CORROSION. REMOVED AND REPLACED RH CABIN FLOOR SILL #5 IAW EMB 145 SRM 51-40-02.
F111856 RH CABIN FLOOR SILL #3 HAS NUMEROUS ARES OF CORROSION. REMOVED AND REPLACED RH CABIN FLOOR SILL #3 IAW EMB 145 SRM 51-40-02
F111828 CABIN L/H CENTER FLOOR SUPPORT IS CORRODED BETWEEN FR 52-53. PREPPED PRIMED AND PAINTED CABIN LT CENTER FLOOR SUPPORT BETWEEN FR 52-53 IAW EMB 145 51-21-05 AND PIEDMONT BULLETIN CPM 51-02 AND PIEDMONT BULLETIN SRM 51-03.
F111826 CABIN L/H LOWER SEAT TRACK SUPPORT IS CORRODED AT FR 53. RAR CABIN L/H LOWER SEAT TRACK SUPPORT BETWEEN FR 52-59 IAW EMB145 SRM 51-40-02.
LEFT FLOOR OMEGA BEAM GUSSET AT AFT END BETWEEN FR-34/36 HAS CORROSION. RAR L/H FLOOR OMEGA BEAM GUSSET BETWEEN FR 29 TO FR 36 IAW EMB 145 SRM 51-40-02.
LT FLOOR SILL NR 3 HAVE CORROSION IN MULTIPLE AREAS. R & R LT FLOOR SILL NR 3 IAW SRM 51-40-02
LEFT FLOOR SUPPORT NR 2 HAVE CORROSION IN MULTIPLE AREAS. RAR L/H FLOOR SILL # 2 IAW EMB 145 SRM 51-40-02.
CORROSION ON SERVICE DOOR CUT-OUT FWD SILL. R & R SERVICE DOOR CUT-OUT FWD SILL IAW SRM 51-40-02.
F111821 CABIN L/H FLOOR SILL #7 IS CORRODED. RAR CABIN L/H FLOOR SILL #7 IAW EMB 145 SRM 51-40-02.
CENTER OMEGA BEAM GUSSET #5 HAS NUMEROUS AREAS OF CORROSION. REMOVED AND REPLACED CENTER OMEGA BEAM GUSSET #5 IAW EMB 145 SRM 51-40-02.
R/H SHEAR CLIP AT FR-26 BETWEEN STGRS 16R/17R HAS A CRACK. RH SHEAR CLIP AT FR. 26, REMOVED AND REPLACED THE RH SHEAR CLIP AT FR. 26 BETWEEN STGRS 16R AND 17R IAW EMB 145 SRM 51-40-02.
F111743 CARGO SHEAR CLIP CRACKED AT FR 67 BTWN STGRS 6L-7L. REMOVED AND REPLACED CARGO SHEAR CLIP AT FR 67 BTWN STGRS 6L-7L IAW EMB 145 SRM 51-40-02.
F111689 CARGO DOOR CUTOUT LWR SILL CORRODED IN NUMEROUS AREAS. RAR CARGO DOOR CUTOUT LWR SILL IAW EMB 145 SRM 51-40-02.
CARGO DOOR CUTOUT LWR SILL CORRODED IN NUMEROUS AREAS. RAR CARGO DOOR CUTOUT LWR SILL IAW EMB 145 SRM 51-40-02.
LH CARGO FLOOR SILL CORRODED IN NUMEROUS AREAS BTWN FR 70-72. R & R LT CARGO FLOOR SILL BTWEEN FR 70-72 IAW EMB 145 SRM 51-40-02.
RIGHT CARGO FLOOR SILL CORRODED IN NUMEROUS AREAS BTWN FR 71-73. RAR R/H CARGO FLOOR SILL #4 IAW SRM 51-40-02.
RIGHT CARGO FLOOR SILL CORRODED IN NUMEROUS AREAS BTWN FR 65-68. RAR RH CARGO FLOOR SILL BTWN FR 65-68 IAW EMB 145 SRM 51-40-02.
F111352 HAT BUSHING IS MIGRATING ON LH AILERON PCA OTBD HINGE. REMOVED AND REPLACED LH AILERON PCA ATTACHMENT HINGE FITTING IAW EMB 145 SRM 51-40-02.
BAGGAGE DOOR LWR EDGE OTBD ANGLE SUPPORT BRACKET HAS MULTIPLE GOUGES. BAGGAGE DOOR LWR EDGE OUTBD ANGLE SUPPORT BRACKET. INSTALLED SERVICEABLE BAGGAGE DOOR LOWER OUTBD ANGLE SUPPORT IAW EMB 145 SRM 51-40-02.
LEFT WING RIB 21 IS CRACKED UNDER ACCESS PANEL 551CB. ACCOMPLISHED LH RIB 21 REPAIR IAW EMB 145 SRM 57-20-07 ITEM 4 FIGURE 203 AND PIEDMONT EO1-57-26-0174.
BAGGAGE DOOR LWR EDGE INBD ANGLE SUPPORT BRACKET CORRODED AROUND NUT PLATE HOLES. R & R ANGLE IAW SRM 51-40-02
BAGGAGE DOOR INTERNAL LWR SKIN CHAFED BETWEEN VB3AND HB4. ACCOMPLISHED PERMANENT REPAIR OF BAGGAGE DOOR INTERNAL LOWER SKIN CHAFE BETWEEN VB3 AND HB4 IAW EMB 145 SRM 52-30-01, ITEM #12 AND EO1-52-26-0145.
PASSENGER DOOR INTERNAL LWR EDGE NUT PLATE HOLES ARE CORRODED. ACCOMPLISHED REPAIIR OF PASSENGER DOOR INTERNAL LWR EDGE NUT PLATE HOLE IAW EMB 145 SRM 52-10-04 ITEM #3 FIG. 201, SHEET 3 AND PIEDMONT EO1-52-26-0153.
FWD FUSELAGE, THERE ARE 9 LIGHTNING STRIKES ON EXTERIOR SKIN FROM FR1A-9, STGR 14R-17R. INSTALLED DOUBLER REPAIR ON FORWARD FUSELAGE - SKIN BETWEEN FR.1A-2 AND STRG. 14R -17R. IAW EMB 145 ETD-2026-145-005225 AND PIEDMONT EO1-53-26-0159.
HEAVY NOSE WHEEL SHIMMY AROUND 35 TO 100 KNTS. R & R 100 & 200 NLG TIRE ASSY IAW AMM 32-49-05. NO FURTHER DEFECTS FOUND AT THIS TIME #1,#2 PN:3-1551, #1 SN:04530453 TAT:36464.1 TAC:34125 TSO:683.1; #2 SN:23092309 TAT:24768.6 TAC:23012 TSO:924.7
AFTER T/O EXTREME STATIC ON COMM AND INTERPHONES. ON COMM 1, 2 & 3. STATIC CLEARED ON GROUND. R & R #100 INTEGRATED COMMUNICATIONS UNIT ITW AMM 23-00-01. OPS CHECK GOOD. A/C OK FOR SERVICE AT THIS TIME
CABIN ALTITUDE WAS AT 300 CABIN RATE DIDNT INCREASE IN CLIMB IN AUTO MODE. PERFORMED FUNCTIONAL TEST OF PRESSURE CONTROL SYSTEM IN AUTOMATIC MODE PER AMM 21-31-00. CHECKED GOOD, NO DEFECTS NOTED AT THIS TIME. CLEAR MEL 21-12-3. PRESS CONTROL AUTO AND MANUAL
IN FLIGHT HAD A BURNING PLASTIC SMELL FOR ABOUT 4 MINUTES THEN DISSAPATED. PERFORMED GVI OF ICU PANEL WIRING AS REQ'D. NO DEFECTS NOTED OR SMELL OF BURNING PLASTIC PRESENT AT THIS TIME. OK FOR SERVICE.
AFTER T/O SMOKE IN FLT DECK WITH PACK 1 SELECTED, SMOKE CLEARED WHEN PACK 1 DESELECTED AIR CONDITIONING PACKS R & R HEAT EXCHANGER,CONDENSOR MIXER, AND WATER COLLECTOR. OPS CHECK GOOD WITH APU AND ENGINES PACK 1 SELECTED NO SMOKE IN COCKPIT.
SMOKE IN RHE CABIN DURING TAKEOFF. PACK 1 OVERHEAT MSG NOTICED AFTER LANDING. FACT 11AUG25 00:37 CLT RAN PACKS FOUND PACK 1 TO CONSTANTLY OVERHEAT AFTER 30 SECS AND COCKPIT RECIRC SMOKING WHILE TRYING TO RUN PACK 1 SOUNDS VERY WEAK AND ONLY BLOWS SUPER HOT AIR. REF LP 330173 SEQ 3 AND 330174 SEQ 1 FOR PACK 1 AND RECIRC 1 MEL. RAN PACK 2 AND CABIN RECIRC FAN NO SMOKE OR DEFECTS NOTED. FOUND COCKPIT RECIRC FAN TO BE PULLING INSUFFICIENT VOLTAGE AND SMOKING WHEN TRYING TO RUN FAN. R/R'D COCKPIT RECIRC FAN IRT AMM 21-24-01, OPS CHECK GOOD. A/C GOOD FOR SERVICE AT THIS TIME.
BLACK SMOKE REPORTED IN CABIN AFTER GRINDING SOUND COMING FROM NR 2 ENG. BURNT RUBBER SMELL IN FLIGHT DECK. OXYGEN MASKS IN FLIGHT DECK DEPLOYED. FOUND ACM TO BE FAULTY. R & R #100 ACM IAW AMM 21-51-03. AC OK FOR SERVICE
AT 33000 FEET UNTIL 20000 ELECTRICAL BURNING FUMES CAUSING LIGHT HEADEDNESS IN FLIGHT DECK. INSPECTED AND FOUND NR 200 DAU INOPERATIVE. R & R NR 200 DAU IAW AMM 31-41-01-000-801-A AND 31-41-01-400-801-A. OPS CHECK GOOD. NO SMELLS NOTED AT THIS TIME. OK FOR SERVICE.
FLAP LOW SPEED DISPLAYED AFTER TAKE OFF. CW MX PROCEDURE FOR FLAP CHANNEL 2 FACT 20JUL25 06:15 SBY T/S USING FIM 27-51-00-810-801 R&R'D LH FLAP TRANSMISSION BRAKE IAW AMM 27-51-01. OPS CHECK GOOD
LOW SPEED REJECTED TAKEOFF AT 20 KNOTS DUE TO OPEN SPOILER INDICATION ON EICAS AND UNCOMMANDED PITCH TRIM MOVEMENT, UP 9 DOWN 4 FACT 23JUN25 23:04 CLT INSPECTED SPOILER SYSTEM AND FOUND LH OB SPOILER PROX SWITCH CONNECTOR PLUG LOOSE AND WOULD NOT STAY TIGHTENED. R&R'D CANNON PLUG & BACKSHELL IRT EMB SWPM 20-50-00. ALSO R&R'D LH OB SPOILER PROXIMITY SENSOR IRT EMB AMM 27-63-04. OPS CHECK GOOD, AC OK FOR SERVICE
TAT 1 HT INOP MSG DISPLAYED AFTER TAKEOFF EXTINGUISHED AFTER LANDING. FACT 18FEB25 06:55 PHL T/S USIING FIM TASK 30-33-00-810-801-A FROM STEP 1-8 FAILURE OF TAT SENSOR 1 (PROBE). R/R TAT SENSOR 1 PROBE IAW AMM 34-15-03. OPS CHECK GOOD ALL OK FOR SERVICE.
DURING CLIMB INTO ICING CON. BLEED 2 OVERTEMP. FACT 26DEC24 07:02 MDT REMOVED PRECOOLER PANELS FOR INSP, FOUND HOLE IN RH BLEED AIR SERVO LINE GOING TO FAN AIR VALVE. RR SERVO LINE SECTION IRT AMM 36-11-11. OPS AND LEAK CHK GOOD. REINSTALLED ALL REMOVED PANELS. OK FOR SERVICE AT THIS TIME.
ON CLIMB OUT BLEED 2 OVERTEMP DISPLAYED WHENEVER ENGINE,WING, STAB OPEN LIGHT ON PB. FOLLOWED BY WING A/I FAIL IN ICING CONDITION. REMOVED AND REPLACED INLET AND OUTLET BLEED TEMP SENSORS IAW AMM 36-20-01. PERFORMED AMM 36-00-00. OPS AND LEAK CHECK GOOD. A/C OK FOR SERVICE AT THIS TIME
FLAP FAIL AT 4 DEG. FLAPS STUCK 4 DEGS. L/H TRANSMISSION FAIL. FACT 27OCT24 06:34 MDT T/S IRT FIM TASK 27-51-00-810-816A. INSPECTED LH FLAP FLEXIBLE SHAFTS IRT AMM 27-51-00. NO DEFECTS NOTED R/R'D L/H FLAP TRANSMISSION BRAKE IRT AMM 27-51-01. OPS CHECK GOOD. RAN FLAPS THROUGH MULTIPLE CYCLES. NO DEFECTS NOTED. OK FOR SERVICE AT THIS TIME.
AFTER T/O AND FLAP RETRACTION RESULTED IN FLAP FAIL MESSAGE ON EICAS AT 4 DEGREES WITH HANDLE IN UP POSITION, CMC MESSAGE OF L/H FLAP TRANSMISSION FAIL FACT 16OCT24 14:44 CLT PERFORMED FIM TASK 27-51-00-810-816-A BLOCKS 1 TO 12 FIM TASK INDICATED TRANSITORY CONDITION. PER DIRECTIVE OF MOC, R&R'D L/H FLAP VELOCITY SENSOR IAW AMM 27-51-12 FLAP CONTROL SYSTEM OPS CHECK GOOD. OK FOR SERVICE
FLAPS 9 DEGRESS IAS 270 FOR FIVE MINUTES. PERFORMED INSPECTION OF THE LH WING IB/OB FLAP TRACK IRT AMM 05-50-07 TABLE 603 NO DEFECTS NOTED PERFORMED INSPECTION OF THE FLAP INBD AND OUTBD. FLAP TRACKS ON THE RH FLAPS IRT E145 AMM 05-50-07 TABLE 603 NO DEFECTS NOTED.
PHOTOLUMINESCNET LIGHT INOP MAIN CABIN DOOR LINER, EMERGENCY LIGHT ASSY, DAMAGED-C/A-RAR MAIN CABIN DOOR LINER, EMERGENCY LIGHT ASSY OPC GOOD IAW AMM 25-23-04
MAIN DOOR EMERGENCY LIGHT INOP-C/A-RAR MAIN DOOR EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-06-000-801-A AND 33-50-06-400-801-A. OPC GOOD. END.
LAVATORY EMERGENCY FLASHLIGHT HOLDER BROKEN-C/A-REMOVED AND REPLACED BROKEN EMERGENCY FLASHLIGHT HOLDER AT LAVATORY IAW EMB 145 AMM 33-50-16 AND ETN-EM-33-059 R1. OPC GOOD.
AFT FLASHLIGHT INOP-C/A-RAR AFT FLASHLIGHT IAW EMB AMM 33-50-16-000-801-A AND 33-50-16-400-801-A. OPC GOOD. END.
ON APPROACH ICE COND - A/I INOP MESSAGE DISPLAYED DECLARED EMERGENCY-C/A-TROUBLESHOOTED IAW FIM TASK 30-80-00-810-801-A PERFORMED OPERATIONAL CHECK IAW AMM 30-00-00-700-803-A/500 FOUND TRANSITORY CONDITION OF A/I SYS NO DEFECTS NOTED AT THIS TIME.
DURING PS-1 CHECK FOUND LH OVER WING EMERGENCY LIGHT INOP-C/A-RAR L/H OVERWING EMERGENCY LIGHT ASSY. IAW EMB-145MM 33-50-10 - OPS CHECK GOOD
DURING PS-1 CHECK FOUND EMERGENCY LIGHT LEFT SIDE EXTERIOR AFT LIGHT INOP .-C/A-R&R EMERGENCY LIGHTI IAW AMM 33-50-10 OP'S GOOD NO OTHERE DEFECT NOTED AT THIS TIME
FLT ENCOUNTERED SVR ICING FROZEN PITOT TUBES. AT 36,000 FEET, AIRCRAFT ENCOUNTERED SEVERE ICING. CAPTAIN'S IAS COMPARATOR ILLUMINATED ON CA'S PFD. CA'S AIRSPEED STAGNANT AND INITIALLY READ 9 KTS SLOWER. FO AND STBY AIRSPEED CONSISTANT. CA SIRSPEEED LOWER AS WE DESCENDED.-C/A-ADC SYSTEM OPS GOOD. IAW AMM 34-15-00-200-80. PITOT/STATIC SYSTEM LEAK CHECK GOOD IAW AMM 34-15-00-790-802/803. DURING LEAK CHECK STOPPED EVERY 50 FT TO COMPARE AIRSPEED INDICATIONS. CA AND FO AIRSPEED WERE THE SAME UP TO 300 KNOTS WITH AND WITHOUT ALTITUDE ADDED. PITOT TUBE AND STATIC PORT HEATING OPC GOOD IAW AMM 30-31-00-700-801.
SMOKE IN CABIN/COCKPIT - FUMES IN COCKPIT AFTER TAKEOFF DECLARED EMEREGNCY-C/A-PERFORMED ENG ODOR EVENT TROUBLESHOOT IAW ETN-EM-72-034. FOUND FUMES TO BE FROM PACK 1. SEE ITEM 3 THIS LOG PAGE FOR DEFERAL OF PACK 1
FOUND SIDE HINGED MIAN DOOR EXTERNAL EMERGENCY LIGHT LENS BROKEN-C/A-RAR SIDE HINGED MAIN DOOR EXTERNAL EMERGENCY LIGHT LENS IN REF WITH EMB 145 AMM 33-50-10.
LEFT AILERON FITTING FOR DAMPER ATTACH IS CHAFED.-C/A-RAR'D LH AILERON FITTING IAW EO# EM-27MR-112.
RIGHT AILERON PCA FITTING HAS MIGRATING BUSHINGS. -C/A-RAR RH AILERON PCA FITTING IAW EO-EM-27MR-112.
FRAME 15 HAS A CHAFE AT STR 2R. -C/A-C/W REPAIR AT FRAME 15 AND STR 2R IAW ERS-EM-53MR-4279.
SSI 53-10-27 DOUBLER UNDER CAPT RT SEAT TRACK IS CORRODED AND GOUGED (LEVEL 1 CORROSION)-C/A-REPAIRED DAMAGE IAW ERS-EM-5300-4282.
CPCP SSI ITEM. FWD SERVICE DOOR SILL IS CORRODED FROM FR 18 TO FR 20 AT THE FLOOR LEVEL. (LEVEL 1 CORROSION)-C/A-INSTALLED NEW FWD SERVICE DOOR SILL IAW SRM 51-40-02.
LEFT FUSELAGE SKIN HAS A CRACK JUST AFT OF FRAME 75 BETWEEN STRS 1L AND 2L.(CRACK APROX 1/2 " LONG )-C/A-REPAIRED LT FUSELAGE SKIN AT FRAME 75 IAW EMB-145 SRM CH. 53-31-01.
CARGO DOOR SILL AREA IS CORRODED BETWEEN FRAMES 60-64. (LEVEL1 CORROSION)-C/A-REPLACED CARGO SILL IAW SRM 51-40-02.
R/H FUSELAGE SKIN HAS A CRACK JUST AFT OF FRAME 75 BETWEEN STRS 1R AND 2R.(CRACK APROX 1/2 " LONG )-C/A-REPAIRED R/H FUSELAGE SKIN AFT OF FRAME 75 BETWEEN STRS 1R AND 2R IAW SRM 53-31-01.
EXTRUSION FOR #6 AND #8 FLOOR EMERGENCY LIGHT STRIP IS BROKEN.-C/A-COMPLETE:RAR EXTRUSION IAW AMM 33-50-12.
ALL BLACK ADHESIVE SPLICES BETWEEN FLOOR EMERGENCY LIGHT STRIPS REQUIRE REPLACEMENT.-C/A-COMPLETE:INSTALLED ALL SPLICES BETWEEN FLOOR EMERGENCY LIGHT STRIPS IAW AMM 33-50-12.
#1 FLOOR EMERGENCY LIGHT STRIP WIRES (ON AIRCRAFT SIDE) ARE EXPOSED.-C/A-COMPLETE:REPLACED EXPOSED CONNECTOR IAW SWPM 20-21-00
DURING BOARDING A BUNCH OF SMOKE CAME INTO CABIN & FLIGHT DECK. APU FAIL CAUTION SHORTLY AFTER & IT SHUT ITSELF DOWN. APU WAS RUNNING WHEN ARRIVED AT AIRCRAFT. C/A: C/W WORKSCOPE, REF NRWC 905-ORD-05100,905-ORD-05101,AND 905-ORD-05104 REF NRWC 905-ORD-05098 FOR APU RAR, OPERATIONS CHECK LEAK CHECK GOOD. NO SMOKE OR ORDER NOTED IN CABIN OR FLIGHT DECK AT THIS TIME END.
FOUND FWD F/A FLASHLIGHT INOPERABLE DURING PS-2. C/A: R & R FWD F/A FLASHLIGHT, IAW AMM TASK 33-50-16. OPERATIONS CHECK GOOD.
LT EXTERIOR EMERGENCY EXIT LIGHT OVER WING INOPERABLE. C/A: R & R LT EXTERIOR EMERGENCY EXIT LIGHT BULB, IAW EMB145 AMM TASK 33-50-10-400-801.
OVERWING EMERGENCY RT SIDE INOPERATIVE. R & R THE OVERWING EMERGENCY LIGHT LAMP IAW AMM 33-50-10. OPS CHECKED GOOD.
GALLEY SERVICE DOOR LOWER EMERGENCY MARKER AND FIRST EMERGENCY FLOOR STRIP DID NOT ILLUMINATE. R & R EMERGENCY LIGHT DC/AC INVERTER NR 2 IAW AMM 33-50-11 WITH WM 33-50-50. OPC GOOD IAW AMM 33-50-00-700-801-A. NO OTHER DEFECTS NOTED.
LG AIR/GND FAIL CAUTION MESSAGE DURING TAKEOFF LANDING GEAR LEVER LOCKED INTO DOWN POSITION AND GEAR WOULD NOT RETRACT. ALL INDICATIONS INDICATED DOWN AND LOCKED. RESTORED LATERAL PLAY IN NLG TRUNNION REPLACED NLG WOW PROX SENSOR AND HARNESS. REF NRWC 942-ORD-04796 THUR 942-ORD-04804 FOR WORK PREFORMED. REF LOG PAGE 4667438 ITEM NR 1 FOR FCF.
LAND GEAR EICAS MSG, FLT DECLARED EMERGENCY. LG AIR/GND FAIL REPEAT WRITE-UP, TRANSFERRED TO NRWC 905-ORD-04793. SERVICED NOSE STRUT. PERFORMED OPS OF NOSE PROX SWITCH. PERFORMED PROX SWITCH CLEARANCE GAP ADJUSTMENT. PERFORMED RETRACTION AND EXTENSION OF LANDING GEAR. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME.
L/H OVERWING EXTERIOR EMERGENCY LIGHT INOP.-C/A-REMOVED AND REPLACED L/H OVERWING EXTERIOR EMERGENCY LIGHT BULB IAW AMM 33-50-10. OPS CHECK GOOD.
HYD SYS 1 FAILED, HYD 1 LOW QTY, E1 HYD PUMP FAIL. EMERGENCY DECLARED. REMOVED AND REPLACED THE NR 1 HYD MANAFOLD IAW AMM 29-10-07, TEPS K-1 TO 8, OPS TESTED GOOD, NO LEAKS NOTED.
FOUND L/H WING EMERGENCY LIGHT INOP-C/A-RELAMPED L/H WING EMERGENCY LIGHT IAW EMB145 AMM 33-50-10. OPS CHECK GOOD
RH OVERWING EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED RH OVERWING EMERGENCY LIGHT ASSEMBLY IAW AMM TASK 33-50-10-000-801-A AND 33-50-10-400-801-A. OPC GOOD. END.
PAX EMERGENCY GROUND ILLUMINATION LIGHT INOPERATIVE. INSPECTED AND CORRECTLY REASSEMBLED PAX EMERGENCY GROUND ILLUMINATION LIGHT ASSY IAW EMB 145 AMM 33-50-10, OPC GOOD.
MAIN DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED MAIN DOOR EMERGENCY LIGHT LAMP IAW AMM 33-50-06-000-801-A, AND 33-50-06-400-801-A. OPS CHECKED GOOD.
ROW 17 AISLE EMERGENCY LIGHT INOP. C/A-REMOVED AND REPLACED ROW 17 AISLE EMERGENCY LIGHT LAMP. OPS CHECK GOOD. NO FURTHER DEFECTS FOUND.
MAIN DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED MAIN DOOR EMERGENCY LIGHT IAW AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPC GOOD, NO DEFECTS NOTED AT THIS TIME. END.
PAX DOOR EMERGENCY LIGHT INOP. PAX DOOR EMERGENCY LIGHT LAMP REMOVED AND REPLACED IAW AMM 33-50-10. OPS CHECKED GOOD.
RT EXTERIOR OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED RT EXTERIOR OVERWING EMERGENCY LIGHT LAMP IAW AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECK GOOD.
TDMI 905T3354 PERFORME PERMANENT REPAIR OF RH OVERWING EMERGENCY LIGHT N/P BROKEN-C/A-RAR RH OVERWING EMEGENCY LIGHT ASSEMBLY IAW ERS-EM-33DF-024 AND EMB145 AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.
TDMI 905T3354 C/W REINSP OF RH OVERWING EMERGENCY LIGHT N/P BROKEN PER ERS-EM-33DF-024 PTB-C/A-PERFORMED GVI OF SPEED TAPE ON RH OVERWING EMERGENCY LIGHT IAW ERS-EM-33DF-024 NO DEFECTS NOTED TDMI REMAINS OPEN
ROW 12 CEILING EMERGENCY LT INOP-C/A-RAR ROW 12 CEILING EMERGENCY LT IAW 33-50-08-000-801-A AND 33-50-08-400-801-A OPS CHECK GOOD END
AFT CABIN FLASHLIGHT CRADLE CRACKED-C/A-REMOVED AND REPLACED AFT CABIN FLASHLIGHT CRADLE BASE IAW GENERAL MAINTENANCE KNOWLEDGE OPS CHECK GOOD AT THIS TIME END
RIGHT OTBD FLAP, OTBD ROLLER BUSHING BORE WAS SCORED. REMOVED AND REPLACED THE RT RIB 19 IAW ERS-EM-57MR-1001 R1.
FWD AVIONICS BAY FLOOR PAN IS CRACKED AT FRAME 5 CROSSBEAM. (CROSSBEAM JUST AFT OF THE NLG UPLOCK BOX.) REPAIRED FWD AVIONICS BAY FLOOR PAN AT FRAME 5 CROSSBEAM IAW SRM 53-11-10 AND ERS-EM-5300-3340.
LT AILERON, PCU FITTING, OUTBOARD HAT BUSHING IS MIGRATED. REMOVED AND REPLACED AILERON PCU FITTING IAW EO EM-27MR-112.
LT AILERON DAMPER FITTING HAS WORN BORES / NICKS AND GOUGES. REMOVED AND REPLACED LT AILERON DAMPER FITTING IAW EO EM-27MR-112.
CARGO DOOR FUSELAGE FWD ANGLE SUPPORT HAS AREAS OF CORROSION BOTTOM AREA. REPAIRED CARGO DOOR FUSELAGE FWD ANGLE SUPPORT IAW SRM 53-31-04-RE.
CARGO DOOR SILL HAS AREAS OF CORROSION. REMOVED AND REPLACED CARGO DOOR SILL IAW SRM 51-40-02.
CENTER CROSS BEAM AT FRAME 20 IS CORRODED. C/A-COMPLETE:REPAIRED CENTER CROSS BEAM AT FRAME 20 IAW ETN-EM-53-241.
LT AILERON DAMPER FITTING HAS WORN BORES/NICKS AND GOUGES. REMOVED AND REPLACED DAMPER FITTING IAW EO EM-27MR-112.
CENTER HAT BEAM HAS AN ELONGATED NUT PLATE HOLE AFT OF FRAME 59. REPAIRED CENTER HAT BEAM IAW SRM 53-24-10.
LT #8 PROXIMITY FLOOR LIGHT STRIP HAS DAMAGED WIRES. C/A-COMPLETE:REPLACED LT #8 PROXIMITY FLOOR LIGHT STRIP IAW 33-50-12.
CABIN FLOOR LT #7 EMERGENCY LIGHT STRIP DAMAGED AT FWD END. C/A-COMPLETE:INSTALLED EXISTING LIGHT STRIP IN NEW EXTRUSION IAW 33-50-12.
CENTER CROSS BEAM BETWEEN FRAMES 24/25 IS CORRODED. C/A-COMPLETE:REPAIRED CENTER CROSS BEAM BETWEEN FRAMES 24/25 IAW ETN-EM-53-241.
CENTER OMEGA BEAM HAS SPOTS OF CORROSION AT FRAMES 27 AND 28. (MARKED IN RED)-C/A-COMPLETE:REPAIRED CENTER OMEGA BEAM AT FRAMES 27 AND 28 IAW SRM 53-22-10.
CABIN FLOOR LT #6 EMERGENCY LIGHT STRIP DAMAGED AT FWD AND AFT END. C/A-COMPLETE:INSTALLED EXISTING LIGHT STRIP IN NEW EXTRUSION IAW 33-50-12
CABIN FLOOR LT #4 EMERGENCY LIGHT STRIP DAMAGED AT AFT END. C/A-COMPLETE:INSTALLED EXISTING LIGHT STRIP IN NEW EXTRUSION IAW 33-50-12.
RT #4 PROXIMITY FLOOR LIGHT STRIP HAS DAMAGED WIRES. C/A-COMPLETE:REPLACED LT #4 PROXIMITY FLOOR LIGHT STRIP IAW 33-50-12.
LT #2 EMERGENCY FLOOR LIGHT STRIP HAS BROKEN WIRE (BROKE FLUSH WITH LIGHT UNREPAIRABLE). C/A-COMPLETE:REPLACED LIGHT STRIP AND EXTRUSION IAW 33-50-12.
LEFT AFT EMERGENCY EXTERIOR LIGHT INOPERATIVE. REMOVED AND REPLACED THE LIGHT IAW AMM 33-50-10. OPS CHECKED GOOD IAW 33-50-00.
LG AIR/GRD FAIL EICAS CLIMBING OUT OF FL180. DID NOT CLEAR. FOLLOWED FIM 32-63-00, CLEANED CONNECTORS AND REPLACED AD TAPE ON ALL MLG WOW SWITCH IAW SWPM 20-50-00. PERFORMED A FUNCTIONAL CHECK IAW AMM 32-63-05 AND OPS TESTED IAW W/C 32-700-16. OPS CHECKED GOOD, NO FURTHER DEFECT NOTED
DURING PS-2 INSPECTION FOUND LT EXTERIOR AFT OVERWING LIGHT INOPERATIVE. REMOVED AND REPLACED NR3 BATTERY AND CHARGER IAW AMM 33-50-04. REMOVED AND REPLACED LT EXTERIOR AFT OVERWING LIGHT BULB IAW AMM 33-50-10. OPS CHECKED GOOD.
EMERGENCY LIGHT AT ROWS 17 AND 18 INOPERATIVE. INSTALLED PIN ON WIRE SPLICE SP9213 FOR THE EMERGENCY LIGHT IAW SWPM 20-51-01. OPS CHECKED GOOD.
FOUND FWD FA FLASHLIGHT MISSING. NSTALLED FWD FA FLASHLIGHT IAW AMM 33-50-16.
FUMES IN CABIN AND COCKPIT AT ALTITUDE STRONG ODOR OF ELEECTICAL EMERGENCY LANDING. REMOVED AND REPLACED THE FLASHLIGHT ASSY IAW 33-50-16 CHECKED GOOD.
BLD 2, LEAK AFTER TAKEOFF. R & R BLEED LINE O-RINGS AT 18 AND 23 IAW AMM 36-11-10, 36-11-09. CHECK GOOD, NO LEAKS NOTED.
CARGO DOOR AFT FRAME ANGLE NUTPLATE CORRODED. REPAIRED CARGO DOOR AFT FRAME ANGLE NUTPLATE CORRODED IAW ENVOY ERS-EM-52MR-576
CARGO DOOR SILL CORRODED AROUND FASTENER ART FR 66. PERFORMED PERMANENT REPAIR ON CARGO DOOR SILL IAW SRM 53-31-15 ITEM #
ABOUT 5 SECONDS AFTER SELECTING ENG 1 TO STOP WHILE PULLING INTO GATE SAW & HEARD ELEC ARCHING THOUGH SCREEN PANEL DIRECTLY BEHIND FIRST OFFICERS SEAT. ELEC BURNING SMELL FOLLOWED, NO ABNORMAL MSGS OR INDICATIONS ON EICAS OR ELEC PAGE ON MFD. R & R CONTACTOR K0190 IAW AMM 21-24-03. OPERATIONS CHECKED GOOD. NO DEFECTS NOTED.
CAPTAINS FLASHLIGHT INOPERATIVE. R & R CAPTAINS FLASHLIGHT AS REQUIRED. OPERATIONS CHECKED GOOD.
LEFT WING AFT EMERGENCY LIGHT INOPERATIVE. R & R LAMP. OPS GOOD IAW AMM 33-50-10.
FLIGHT OFFICERS EMER FLASHLIGHT INOPERATIVE. R & R FLIGHT OFFICERS EMER FLASHLIGHT IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.
CAPTAIN`S FLASHLIGHT HOLDER BROKEN. R & R CAPTAIN`S FLASHLIGHT HOLDER IAW AMM 33-50-16-000-801-A & 33-50-16-400-801-A. OPERATIONS CHECKED GOOD.
AFT FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. DEFERRED AFT FLIGHT ATTENDANT FLASHLIGHT IAW MEL 25-53. R & R FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPERATIONS CHECKED GOOD. MEL ITEM RESTORED. FLASHLIGHT OPERATIONS CHECKED GOOD.
COCKPIT STEP & FIRST OVERHEAD CEILING LONG EMER LIGHTS INOPERATIVE. R & R IAW AMM 33-50-11. PERFORMED OPERATIONS CHECK IAW AMM 33-50-00. OPERATIONS CHECKED GOOD.
FLIGHT ATTENDANT REPORTS THAT AFT CABIN FLASHLIGHT CRADLE IS BROKEN & WILL NOT CHARGE UNLESS HELD IN PLACE. R & R IAW AMM-33-51-01. OPERATIONS CHECKED GOOD.
RIGHT AISLE OVERWING EMER LIGHT INOPERATIVE. R & R RT AISLE OVERWING EMER LIGHT BULB IAW AMM 33-50-07.
AFTER TAKEOFF, MAIN ALT HAD YELLOW DASHES ON EICAS. DEFERRED IAW MEL 21-18. PERFORMED OPERATIONS CHECK OF PRESSURIZATION CONTROL SYS IN BOTH MANUAL & AUTO MODES IAW AMM 21-31-00. OPERATIONS CHECKED GOOD, NO DEFECTS NOTED. MEL RESTORED.
DURING FLIGHT GOT E-2 ANTI-ICE FAIL ON EICAS. DEFERRED E-2 ANTI-ICE M PROCEDURE. COMPLIED WITH MEL 30-11. R & R ENG 2 ANTI-ICE VLV. OPERATIONS CHECKED GOOD IAW AMM 30-21-01. MEL ITEM RESTORED.
ADC 1 & 2 FAIL WITH AP FAIL & AIRSPEED & ALT PRESELECT FAIL VERT SLOPE OFF. R & R REPLACED 2 ICU IAW AMM 23-00-01. OPERATIONS CHECKED GOOD & PERFORMED FNC OF ADC 1 & 2 IAW AMM 34-15-00. OPERATIONS CHECKED GOOD.
NUMBER 1 FUEL QTY INDICATIONS ON EICAS & MFD WENT OUT SHOWING DASHES DURING FLIGHT, INDICATIONS CAME BACK SEVERAL TIMES DURING FLIGHT SHOWING DIFFERENT LEVELS.
ALL EMER LIGHTS INOPERATIVE. R & R NR 1, 2, 3 & 4 EMER LIGHT BATTERIES IAW MM 33-50-04. OPERATIONS CHECKED GOOD. PN 2013-1A, SN 112892 NR 2, SN 114996 NR 3 & SN 104852 NR4.
FWD GALLEY EMERGENCY LIGHT STRIP WIRES BROKE. R & R FWD GALLEY EMERGENCY LIGHT STRIP IAW EMB 145 AMM 33-50-12.
GALLEY RT HAT BEAM HAS CORROSION AT NUTPLATE HOLE AT FRAME 23. REPAIRED IAW ERS-EM-53MR-407.
PAX DOOR EMERGENCY LIGHT INOPERATIVE ON DOOR HINGE. REMOVED & INSTALLED NR 1 EMERGENCY BATTERY POWER SUPPLY IAW WORK CADR 33-700-17 & 33-700-19, OPERATIONAL CHECKED GOOD.
LT & RT OVERWING EMERGENCY LIGHTS INOPERATIVE. R & R RT & LT OVERWING EMERGENCY BULBS IAW AMM 33-50-07, OPERATIONS CHECKED GOOD.
DURING MAINTENANCE INSPECTION ON AC905 FOUND LT LATERAL PANEL EMERGENCY OVERWING LIGHT INOPERABLE. R & R THE LT LATERAL PANEL EMERGENCY OVERWING LIGHT ASSEMBLY IAW 145 AMM 33-50-10, CHECKED GOOD.
EMERGENCY LIGHT STRIP AT ROW 11 & 12 IS INOPERATIVE. R & R FLOOR PROXIMITY LIGHT AT ROW 11 & 12 IAW EMB-145 AMM 33-50-12, OPERATIONS CHECKED GOOD.
GEAR WOULD NOT RETRACT AFTER TAKEOFF. DURING RETURN TO DEPARTURE, RECEIVED "TAKEOFF, FLAPS, GEAR, TRIM" AURAL WARNING. EXECUTED A NORMAL LANDING AND IMMEDIATELY AFTER TOUCHDOWN RECEIVED LG AIR/GROUND FAIL AND IC 1-2 WOW INOP EICAS MESSAGES. AFTER PARKING TRIED TO CONNECT GPU BUT PLANE WASN'T SEEING IT ON ELECTRIC PAGE - SHUTDOWN NR 1 ENGINE AND LOST CAPT PFD + FO MFD. ON SHUTTING DOWN NR 2 ENGINE THE F/O PFD. R & R LANDING GEAR ELECTRONIC UNIT IAW AMM 32-32-01. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED.
COCKPIT STEP EMERGENCY LIGHT INOP. FOUND CONNECTORS DIRTY. CLEANED CONNECTORS AS REQUIRED. OPS GOOD AT THIS TIME, NO OTHER DEFECTS NOTED.
FWD CEILING EMERGENCY LIGHT INOPERATIVE. FOUND CONNECTORS DIRTY, CLEANED CONNECTORS AS REQUIRED. OPS GOOD AT THIS TIME, NO OTHER DEFECTS NOTED.
LEFT OVERWING UPPER EMERGENCY LIGHT INOPERATIVE. R & R NR 4 EMERGENCY LIGHT INVERTER IAW AMM 33-50-11, OPS CHECKED GOOD IAW WC 33-700-17.
EMERGENCY EXIT SIGN BEHIND GALLEY AT PAX SEAT 3 INOPERTIVE. R & R NR 3 INVERTER IAW AMM 33-50-11. OPS CHECKED GOOD.
FLOOR EMERGENCY LIGHT FROM SEAT 8 TO 10 INOPERATIVE. R & R NR 3 EPSU BATTERY AND CHARGER OPS CHECKED GOOD IAW AE WC 33-700-19.
THE F/A REPORTED THE PASSENGER DOOR WAS DIFFICULT TO OPEN AND CLOSE. THE ACFT WAS REMOVED FROM SERVICE. CLEANED AND LUBED MAIN DOOR AND ROLLERS IN REF TO AMM 52-18-00 AND 52-21-02. THE OPS CHECK OF THE OPEN AND CLOSED DOOR IS GOOD AT THIS TIME. THE ACFT WAS RETURNED TO SERVICE.
DURING MX INSPECTION, FOUND LIGHTED EMERGENCY "EXIT" SIGN ON THE AFT SIDE OF THE AFTER GALLEY WALL IN FRONT OF ROW 3 BC, DID NOT ILLUMINATE. ACFT REMOVED FROM SERVICE. FOUND BACK SHELL LOOSE ON CONNECTER P8003, TIGHTENED CONNECTER IAW SWPM 20-50-00. OPS CHECKED GOOD IAW AMM 33-50-00. ACFT RETURNED TO SERVICE.
DURING MX INSPECTION FOUND CAPTAINâS FLASHLIGHT SWITCH BROKEN. ACFT REMOVED FROM SERVICE. R & R FLASHLIGHT ASSY IAW AMM 33-50-16. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.
ON FLIGHT 2888 THE CREW REPORTED THE FIRST OFFICERâS FLASHLIGHT REAR BRACKET WAS BROKEN. REMOVED AND REPLACED THE FIRST OFFICERâS FLASHLIGHT ASSEMBLY IAW EMB-145 AMM 33-50-16. THE AIRCRAFT WAS RETURNED TO SERVICE.
FLIGHT 3916, FLIGHT ATTENDANT REPORTED SMOKE IN CABIN IMMEDIATELY AFTER PUSHBACK FROM GATE. AIRCRAFT REMOVED FROM SERVICE. FOUND NR 2 PACK BLOWING DUST & DIRT. NO EVIDENCE OF SMOKE OR OIL ODOR. REMOVED AND REPLACED THE NR 1 PACK VALVE IAW AMM 21-51-01. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
ON FLIGHT 2897 THE CREW REPORTED THE MAIN CABIN DOOR WAS HARD TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBE MAIN DOOR ROLLER BEARING, DOOR OPEN /CLOSE CHECK WAS GOOD IAW EMB 145 52-18-00 AMM. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE INSPECTION FOUND THE LEFT ENGINE LOWER FORWARD YOKE CRACKED FORWARD OF ENGINE MOUNT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED LEFT ENGINE LOWER FORWARD YOKE FORWARD OF ENGINE MOUNT IAW EO EM-54MR-386. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING B INSPECTION FOUND THE SERVICE DOOR FORWARD SILL CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SERVICE DOOR FORWARD SILL IAW EMB145 SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING B INSPECTION FOUND THE SERVICE DOOR AFT SILL CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SERVICE DOOR AFT SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING B INSPECTION FOUND THE DIAMOND GUSSET AT FRAME 20 CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE DIAMOND GUSSET AT FRAME 20 IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING B INSPECTION FOUND THE GALLEY CEILING PANEL 233BLC EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RECONNECTED GALLEY CEILING PANEL 233BLC EMERGENCY LIGHT CONNECTOR IAW EMB 145 AMM 25-22-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
LEFT ENGINE LOWER FWD YOKE CRACKED FWD OF ENGINE MOUNT. R & R LT ENGINE LOWER FWD YOKE FITTING IAW AEA EO EM-54MR-386.
FLT 4038, CREW REPORTED PITCH TRIM BACKUP INOPERATIVE MASTER WARNING AND EICAS MESSAGE PRESENTED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED HSCU IAW AMM 27-40-01. OPS CHECKED GOOD. AIRCRAFT RETURN TO SERVICE.
ON FLIGHT 3909 THE CREW REPORTED THE SWITCH ON THE CAPTAINâS FLASHLIGHT WAS BROKEN. 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 B-INSPECTION, FOUND THE FIRST FLOOR EMERGENCY LIGHT STRIP AND SERVICE DOOR LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 EMERGENCY INVERTER. THE OPERATIONAL CHECK WAS GOOD IAW AMM 33-50-11. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING B-INSPECTION FOUND THE FLASHLIGHT HOLDER BEHIND CAPTAINâS SEAT BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLASHLIGHT HOLDER IAW EMB AMM 33-50-16-000-801-A AND 33-50-16-400-801-A NO FURTHER DEFECTS NOTED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 3249 THE CREW REPORTED THE CABIN ENTRY DOOR HANDLE OPERATION IS DIFFICULT AND PRODUCES A SNAPING SPRING EFFECT WHEN LOCKING -REPEAT WRITE UP PAGE 3160411. THE AIRCRAFT WAS REMOVED FROM SERVICE. MAIN ENTRY DOOR ROLLERS SERVICED IAW AMM 52-18-00. THE OPERATIONAL CHECK WAS GOOD NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 3959 THE FLIGHT ATTENDANT REPORTED THE MAIN ENTRY DOOR WAS DIFFICULT TO OPERATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. CONDUCTED AN OPERATIONAL CHECK OF THE MAIN PAX DOOR IAW EMB-145 AMM 52-18-00. THE PASSENGER DOOR CHECKED AS GOOD. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENACE BASE VISIT FOUND THE SERVICE DOOR SILL HAS CORROSION. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED THE SERVICE DOOR SILL IAW EMBRAER SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.
FOR FLIGHT 4224 MAINTENANCE FOUND THE EMERGENCY LIGHT STRIP AT ROW 8 AND 9 TO HAVE BROKEN WIRES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT STRIP AT ROW 8 AND 9. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.
FOR FLIGHT 4090 DURING INSPECTION FOUND THE HALON FIRE EXTINGUISHER IN AFT CABIN MISSING A SAFETY PIN AND WIRE (YELLOW BUTTON STILL PRESENT). THE AIRCRAFT WAS REMOVED FROM SERVICE. RE-SECURED SAFETY PIN AFTER LOCATING IT IAW ETN GN-26-001R1. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE BASE VISIT FOUND THE FLOOR EMERGENCY LIGHTS FROM ROW 12 AFT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 INVERTER. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING PS2 INSPECTION FOUND THE REAR CABIN EMERGENCY FLOOR PROXIMITY FLOOR LIGHT STRIP TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHT SYSTEM FLOOR STRIPS IAW EMS AMM 33-50-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
AIRCRAFT ARRIVED FOR REPAIR OF ACCIDENTAL DAMAGE THAT OCCURRED TO RT AFT FUSELAGE BETWEEN FR 61 AND 62 AND BETWEEN STR 13R AND 14R. PERFORMED A CUT OUT OF THE FUSELAGE SKIN TO REMOVE THE DAMAGE. FAB A FILLER, DOUBLER FOR REPAIR. DRILLED, CLEANED, TREATED AND INSTALLED REPAIR PARTS. REPAIR DONE IAW EMBRAER 145 SRM (SRM EMB-145/1142 REV 40) CHAPTER 53-31-01. AIRCRAFT RETURNED TO SERVICE.
ON FLIGHT 4200, CREW REPORTED A ABORTED TAKEOFF AT 100 KNOTS AFTER F/O NOTICED EVIDENCE OF SMOKE IN THE COCKPIT. THE F/A ALSO REPORTED VISIBLE SMOKE AROUND GALLEY AREA AND AFTER SHUTDOWN THE PACKS THE SMOKE WENT AWAY. THE SMOKE DID NOT HAVE A ODOR OF ELECTRICAL OR OIL ODOR LIKE. THE SMOKE ODOR LIKE BURNING PAPER AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NUMBER ONE ENGINE. REMOVED AND REPLACED THE NR 4 CARBON SEAL PER SERVICE BULLETIN 72-348. THE OPERATIONAL CHECKS WERE GOOD.
PTRIM MAIN INOP MESSAGE FOLLOWED BY PTRIM BACKUP INOP MESSAGE. FOUND PILOTS AUTO PILOT/TRIM/PUSHER DISCONNECT SWITCH PINCHED. REPOSITIONED WIRES. SYSTEM OPERATIONAL CHECK GOOD IAW EMB 27-11-00-700-803A AND AMM 27-40-00. AIRCRAFT RETURNED TO SERVICE.
SERVICE DOOR CENTER SILL FOUND CORRODED. FABRICATED REPAIR DOUBLER, INSTALLED AND RESTORED PROTECTIVE FINISH IAW EMB SRM 53-21-02. RETURNED AIRCRAFT TO SERVICE.
AIRCRAFT LIGHTNING STRIKE. ACCOMPLISHED LIGHTNING STRIKE INSPECTION IAW AMERICAN EAGLE WORK CARD 05-200-00. REPAIRED RIGHT TRAILING EDGE OF WING TIP IAW 51-21-07 WORK CARD 05-200-00. REPAIRED RIGHT TRAILING EDGE OF WING TIP IAW 51-21-07. RETURNED AIRCRAFT TO SERVICE. (M)