N698CB
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 | 2015-02-17 – 2015-02-17 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
RUDDER SYS 1 INOP MESSAGE ON T/O ROLL AND REJECTED T/O. PERFORMED RUDDER SYSTEM OPERATIONAL TEST IAW AMM 27-23-00. OPS CHECK GOOD. A/C OK FOR SERVICE
ENG 1 ANTI-ICE VALVE FAILED DURING TAKE OFF ROLL. R & R NR 100 ENGINE ANTI-ICE VALVE IRT AMM 30-21-01. OPS CHECKED GOOD. A/C OK FOR SERVICE.
RH OVERWING EMERGENCY EXIT LIGHT INOP. R&R EMERGENCY EXIT SIGN IRT AMM 33-50-14 PN ON EXIT SIGN 7444-36 PN OFF EXIT SIGN 7444-36
EMERGENCY EXIT LIGHT BELOW FLIGHT DECK DOOR INOP. INSTALLED NEW INVERTER P/N 1330212 IAW AMM 33-50-11 INSTALLED NEW EXIT INDENTIFER IAW AMM 33-50-13.
E052528 CARGO DOOR INTERNAL LOWER WEB IS CHAFED IN THREE (3) AREAS. INSTALLED FABRICATED REPAIR DOUBLER AT INTERSECTION OF HB3-BV2 ON LOWER CARGO DOOR INTERNAL WEB IAW EMBRAER ETD2024-145-023066 AND PIEDMONT EO1-52-24-0525.
E051429 CABIN CENTER AISLE CROSSBEAM AT FRAME 25 CORRODED. REMOVED AND REPLACED CABIN CENTER AISLE CROSSBEAM AT FR 25 IAW EMB 145 SRM 51-40-02.
E051424 LH CABIN OMEGA BEAM #2 GUSSETT IS CORRODED. : RAR THE LH CABIN OMEGA BEAM #2 GUSSET IAW EMB 145 SRM 51-40-02.
E051425 LH CABIN OMEGA BEAM #3 GUSSETT IS CORRODED. RAR LH CABIN OMEGA BEAM #3 GUSSET IAW EMB 145 SRM 51-40-02.
E051313 SHEAR CLIP ON FRAME 25 CRACKED AT STRINGER 15R. REMOVED AND INSTALLED SERVICEABLE SHEAR CLIP ON FRAME 25 AT STRINGER 15R IAW EMB 145 SRM 51-40-02.
E051309 SHEAR CLIP ON FRAME 24 CRACKED AT STRINGER 15R. REMOVED AND INSTALLED SERVICEABLE SHEAR CLIP ON FRAME 24 AT STRINGER 15R IAW EMB 145 SRM 51-40-02
E050582 RH FLOOR SILL CORRODED BTWN FR 54-55. REMOVED AND REPLACED RH FLOOR SILL BTW FR 52-60 IAW EMB 145 SRM 51-40-02
E051427 CABIN LH #3 FLOOR SILL CORRODED. RAR LH CABIN FLOOR SILL #3 IAW EMB 145 SRM 51-40-02.
E050581 RH FLOOR SILL CORRODED BTWN FR 53-54. BLENDED TO REMOVE CORROSION ON R/H FLOOR SILL BETWEEN FR 53-54 IAW EMB 145 SRM 51-10-03. REMAINING THICKNESS OF BLENDED AREA FOUND TO BE WITHIN ALLOWABLE LIMITS IAW EMB 145 SRM 53-24-02.
E050583 LH OMEGA BEAM GUSSET CORRODED BTWN FR 50-51. RAR THE LH OMEGA BEAM GUSSET BTWN FR 45-53 IAW EMB 145 SRM 51-40-02.
E050234 CORROSION IN CARGO ON LOWER SKIN PLATE BETWEEN FRAMES 61-62 STRINGERS 19L-20L. RAR THE CARGO UNDERFLOOR LOWER SKIN PLATE BETWEEN FRAMES 61-62 STRINGERS 19L-20L IAW EMB 145 SRM 51-40-02.
E050232 CORROSION ON CARGO DOOR LOWER SILL. RAR CARGO DOOR LOWER SILL IAW EMB 145 SRM 51-40-02
E050150 CARGO DOOR INTERNAL UPPER AND LWR WEB IS CHAFED IN MULTIPLES AREAS. FABRICATED DOUBLERS FOR TWO (2) PREVIOUS REPAIRS. INSTALLED DOUBLERS FOR TWO (2) PREVIOUS REPAIRS ON LOWER CARGO DOOR INTERNAL WEB IAW EMB145 SRM 51-40-02RE, AND SRM 52-30-01RE ITEM 12, FIGURE 213 AND PIEDMONT EO1-52-24-0526.
E050029 CRACKED SHEAR CLIP AT FR80, BETWEEN STRG 07L-05L. RAR SHEAR CLIP AT FR80, BETWEEN STRG 07L-05L IAW EMB 145 SRM 51-40-02.
E050238 CORROSION ON FRAME 65 SHEAR CLIP BAGGAGE DOOR CUT-OUT. : RE-ACCOMPLISHED FR65 SHEAR CLIP REPAIR IAW EMB 145 SRM 53-31-04 ITEM 4.D FIGURE 212.
E050028 CRACKED SHEAR CLIP AT FR80, BETWEEN STRG 09R-07R. : RAR SHEAR CLIP AT FR80, BETWEEN STRG 09R-07R IAW EMB 145 SRM 51-40-02.
E049491 SCRATCH ON REAR FUSELAGE SKIN BETWEEN FR79-FR80 AND STRG 03L-04L. RFORMED CUTOUT, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER AND APPLIED EDGE SEALANT FOR REPAIR OF DAMAGED SKIN BTW FR79-80, STGR 3L-4L IAW EMB 145 SRM 53-32-01 ITEM 2 FIGURE 201 SHEET 3 AND EO1-53-24-0530
AFT EMERGENCY FLASHLIGHT MISSING-C/A-FLIGHT CREW PLACARDED AFT EMERGENCY FLASHLIGHT MISSING M PROC. C/W MEL 25-32 AUTH 050146M-C MOC ID 373623. PENDING CA
AFT EMERGENCY FLASHLIGHT HOLDER BROKEN-C/A-RAR AFT EMERGENCY FLASHLIGHT HOLDER IAW AMM 33-50-16, OPS CHECK GOOD
MAIN DOOR EMERGENCY LIGHT INOP-C/A-RAR MAIN DOOR EMERGENCY LIGHTBULB. OPC GOOD IAW AMM 33-50-06.
RH AFT OVERWING EMERGENCY LIGHT INOP REF MEL 33-22 LG PG 4589780 ITEM 3-C/A-RAR OVERWING EMERGENCY LIGHT ASSY IAW AMM 33-50-10 OPC GOOD MEL RESTORED
RH AFT OVERWING EMERGENCY LIGHT INOP-C/A- "TRANSFERRED TO AML PAGE 4589780 ITEM 3" -RAR RH AFT OVERWING EMERGENCY LIGHT LAMP IAW EMB145 AMM 33-50-07. NO FIX. PERFORMED TROUBLESHOOTING IAW EMB145 FIM TASK 33-50-00-810-804-A. FOUND PROPER VOLTAGE AT CANNON PLUG. DETERMINED LIGHT ASSY TO BE INOP.
EMERGENCY LIGHT OVER R/H WING INOP-C/A-RAR R/H OVERWING EMERGENCY LIGHT IAW EMB145 AMM 33-50-10
RH UPPER EXTERNAL EMERGENCY LIGHT INOP-C/A-RAR RH UPPER EXTERNAL EMERGENCY LIGHT BULB IAW AMM 33-50-10. OPC GOOD.
RH OVERWING EMERGENCY LIGHT INOP.-C/A-RAR RH OVERWING EMERGENCY LIGHT BULB IAW AMM 33-50-10. OPC GOOD.
REAR EMREGENCY FLASHLIGHT NOT WORKING PROPERLY-C/A-RAR EMERGENCY FLASHLIGHT ASSY IAW EMB 145 AMM 33-50-16. NO FURTHER DEFECTS NOTED AT THIS TIME.
PILOT REPORTS BURNING SMELL IN COCKPIT. PERFORMED ENGINE RUNS IAW ETN-EM-72-034. NO ODORS NOTED. NO DEFECTS NOTED.REF NRWC 698-ORD-05499 FOR COMPLETION OF TECH SUPPORT WORKSCOPE REV.1 FOR BURNING SMELL IN COCKPIT. NO ODOR NOTED AT THIS TIME.
EMERGENCY GALLEY LIGHT PLACARD INOP-C/A-T/S IAW EMB WM 33-50-50-005. RAR #2 EMERGENCY LIGHT DC INVERTER IAW EMB AMM 33-50-11-000-801-A AND 33-50-11-400-801-A. OPC GOOD.
CABIN EMERGENCY FLOOR LIGHT WIRE BROKEN AT SEAT 11A. C/A-REMOVED AND REPLACED FLOOR EMERGENCY LIGHT SPLICE SP9115 IAW EMB 145 SWPM 20-21-00. OPERATIONAL CHECK GOOD.
MECH SMOKE IN CABIN AND COCKPIT IN CRUISE LEVEL FLIGHT AT FL240 NOTICED SMOKE FROM CAPTAIN SIDE VENTS AND THROUGT THE CABIN DECLARED EMERGENCY RESCUE SENT, FLT CONT.-C/A-PERFORMED FIM TASK 21-20-00-810-801-A PACK OVERHEAT AND FOUND ACM ON PACK 2 TO BE SEIZED REF ITEM 1 ON LG PG 4635121
RT OVERWING EMERGENCY LIGHT INOPERABLE. C/A: R & R RT OVERWING EMERGENCY LIGHT LAMP, IAW WMB AMM TASK 33-50-07-000-801-A AND 33-50-07-400-801-A. OPERATIONS CHECK GOOD.
FWD F/A EMERGENCY FLASHLIGHT INOPERABLE MEL 2553, AUTH 10-280-C LOGPAGE: 4681588. C/A: R & R FWD F/A EMERGENCY FLASHLIGHT SYSTEM ASSEMBLY, IAW EMB 145 AMM 33-50-16-04. OPERATIONS CHECK GOOD. M PROCEDURES REVERSED. MEL RESTORED.
FWD F/A EMERGENCY FLASHLIGHT INOPERABLE. C/A: FLIGHT CREW PLACARD FWD F/A FLASHLIGHT AUTH 100280-C, REF 25-53 MOC 864015.
FA REPORTS LOUD WHISTLING FROM SERVICE DOOR DURING CLIMB STOPED AT CRUISE ALT 37000 "TRANSFERRED FROM LOG PAGE #4676996"-C/A-PERFORMED PRESSURIZATION CONTROL SYSTEM TEST AS PER AMM 21-31-00. CHECKED OK. PRESSURIZATION NORMAL . NO FURTHER DEFECTS. SEE NRWC# 698-MIA-0548 FOR ADDITIONAL WORK PERFORMED.
DURING PS-2 CHECK, FOUND RH AFT EXTERNAL EMERGENCY LIGHT TO BE INOPERATIVE. R & R RT AFT EMERGENCY LIGHT IAW AMM 33-50-10. NO FURTHER DEFECTS NOTED.
DURING PS-1 CHECK, FOUND THE RT OVERWING EMERGENCY LIGHT TO BE INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW AMM 33-50-10. OPS CHECKED GOOD.
SERVICE DOOR OVERHEAD EMERGENCY EXIT SIGN INOP-C/A-TS IAW EMB AMM 33-50-00-810-804-A EMOVED AND REPLACED POSITION 2 BACK BATTERY PACK IAW EMB AMM 33-50-04-000-802-A AND 33-50-04-400-802-A AND CHARGER ASSY IAW EMB AMM 33-50-04-000-801-A AND 33-50-04-400-801-A OPS CHECK GOOD NO FURTHER DEFECTS NOTED AT THIS TIME, BATTERY CHARGER ASSY P/N 11-0049 S/N 11652
DURING HMBV INSPECTION, QC FOUND PAX DOOR LOWER FRAME CORRODED AT LINER NUT PLATE HOLES.-C/A-PERFORMED PERMANENT REPAIR TO CORRODED AREAS ON PAX DOOR LOWER FRAME AT NUT PLATE HOLES IAW EMB 145 SRM 52-10-04RE AND ETN-EM-52-041.
DURING HMBV INSPECTION, QC FOUND LAV BUCKET CORRODED AROUND TOILET WASTE VALVE MOUNTING FLANGE.-C/A-REMOVED AND REPLACED LAV BUCKET IAW EMB 145 SRM 51-40-02.
DURING HMBV INSPECTION, QA FOUND THE LH WING RIB 21 CRACKED INSIDE 551CB-C/A-PERFORMED PERMANENT REPAIR ON LH WING RIB 21 IAW EMB 145 SRM 57-20-07-RE ITEM 4
DURING HMBV INSPECTION, QC FOUND CORROSION ON FR 22 AT SERVICE DOOR LOWER CUT-OUT.-C/A-PERFORMED PERMANENT REPAIR TO FR 22 AT SERVICE DOOR CUT-OUT IAW EMB 145 SRM 53-00-04RE.
DURING HMBV INSPECTION, QC FOUND RUDDER II TRAILING EDGE LOWER LH SKIN PUNCTURED.-C/A-REPAIRED RUDDER II LOWER LH SKIN IAW ERS-EM-55MR-841.
DURING HMBV INSPECTION, QC FOUND PAX DOOR HANDLE BOX SUPPORT ASSY BRACKET CRACKED.-C/A-REMOVED AND REPLACED PAX DOOR HANDLE BOX SUPPORT BRACKET IAW EMB 145 SRM 51-40-02.
DURING HMBV INSPECTION, QC FOUND FR 72 CRACKED BETWEEN STGR 16L-17L.-C/A-PERFORMED PERMANENT REPAIR TO CRACK ON FR 72 IAW EMB 145 SRM 53-00-04RE.
DURING HMBV INSPECTION, QC FOUND A RH AILERON DAMPER FITTING BUSHING HOLE ELONGATED. -C/A-REMOVED AND REPLACED RH AILERON DAMPER FITTING IAW EO EM-27MR-112.
DURING HMBV INSPECTION. QC FOUND THE SERVICE DOOR CENTER SILL CORRODED.-C/A-REMOVED AND REPLACED SERVICE DOOR CENTER SILL IAW EMB 145 SRM 51-40-02.
LH AILERON DAMPNER BRACKET GOUGED. -C/A-REMOVED AND INSTALLED SERVICABLE DAMPNER FITTING IAW EO EM-27MR-112
RH FWD PYLON LWR YOKE CRACKED-C/A-REMOVED AND INSTALLED SERVICABLE YOKE IAW ERS-EM-54MR-698
CARGO DOOR LWR SILL IS CORRODED-C/A-REMOVED AND REPLACED THE CARGO DOOR SILL IAW EMB SRM 51-40-02
LH ENGINE FWD YOKE LWR FWD FITTING CRACKED-C/A-REMOVED AND INSTALLED SERVICABLE LH FWD YOKE LWR FWD FITTING IAW EO ERS-EM-54MR-698
L/H # 1 EMERGENCY LIGHT INOP .-C/A-COMPLETE:REMOVED AND REPLACED L/H # 1 EMERGENCY LIGHT IAW EMB 145 AMM 33-50-12. OPS CHECKED GOOD .
L/H #8 EMERGENCY LIGHT STRIP HAS A BROKEN WIRE .-C/A-COMPLETE:REMOVED AND REPLACED CORRECTART # FOR L/H #8 LIGHT STRIP IAW EMB 145 AMM 33-50-12. OPS CHECKED GOOD .
L/H #8 EMERGENCY LIGHT STRIP PANEL BROKEN .-C/A-COMPLETE:REMOVED AND REPLACED BROKEN L/H #8 LIGHT STRIP PANEL IAW EMB 145 AMM 33-50-12. SEE BOW341052 FOR RE-INSTALLATION.
R/H #5 EMERGENCY LIGHT STRIP PANEL BROKEN-C/A-COMPLETE:REMOVED AND REPLACED BROKEN R/H #5 EMERGENCY LIGHT STRIP PANEL IAW EMB 145 AMM 33-50-12. SEE BOW341052 FOR RE-INSTALLATION.
CABIN FLOOR PROXIMITY LIGHT STRIP HAS BROKEN WIRE/MISSING CONNECTOR AT FR 38-C/A-COMPLETE:REPAIRED EMERGENCY LIGHT STRIP AT FR 38 IAW EMB 145 SWPM 20-21-00. EASI #6277 AND #6224H.. SEE THIS NRTC FOR ALL WIP AND TASK DETAILS
L/H #6 EMERGENCY LIGHT STRIP BROKEN .-C/A-COMPLETE:REMOVED AND REPLACED BROKEN L/H #6 EMERGENGY LIGHT STRIP IAW EMB 145 AMM 33-50-12. SEE BOW341052 FOR RE-INSTALLATION AND OPS CHECK .
R/H #2 EMERGENCY LIGHT STRIP PANEL BROKEN-C/A-COMPLETE:REMOVED AND REPLACED BROKEN R/H #2 LIGHT STRIP PANEL IAW EMB 145 AMM 33-50-12. SEE BOW341052 FOR RE-INSTALLATION .
L/H #5 LIGHT STRIP PANEL BROKEN .-C/A-COMPLETE:REMOVED AND REPLACED BROKEN L/H #5 LIGHT STRIP PANEL IAW EMB 145 AMM 33-50-12. SEE BOW341052 FOR RE-INSTALLATION
SERVICE DOOR EMERGENCY EXIT LIGHT INOP-C/A- T/S FOUND EMERGENCY BATTERY NOT WORKING REMOVED AND REPLACED EMERGENCY BATTERY #2 AND CHARGER IAW ENVOY W/C 33-700-19 OPC GOOD. EMERGENCY LIGHTING BATTERY P/N 2013-1A S/N 104854
AFT OVERWING EMERGENCY LIGHTS INOP-C/A-REMOVED AND REPLACED #4 EMERGENCY BATTERY AND CHARGER IAW EMB 145 AMM 33-50-04 OPC GOOD. BATTERY CHARGER ASSY P/N 11-0049 S/N 11448 / +
FA AND GATE AGENT REPORTED 'BURNING SMELL" IN FORWARD CABIN TAXIING UP TO THE GATE.-C/A-FOUND STRONG ELECTRICAL SMELL COMING FROM FLIGHT GUIDANCE CONTROLLER (FGC). REMOVED AND REPLACED FGC IAW AMM 22-11-01. OPERATIONAL CHECKS GOOD.
DENT AND SCRATCH LH REAR FUSELAGE II BETWEEN FR 78 AND FR 79 AND STR 5L AND 7L-C/A-PERFORMED PERMANENT REPAIR IAW ERS-EM-53MR-3952
PTRIM MAIN INOP "TRANSFERRED TO NRWC 698-ORD-04545". WLS 1 HEAT FAIL. C/A-REMOVED AND REPLACED HORIZONTAL-STABILIZER ACTUATOR IAW AMM 27-40-02 PERFORMED ELECTRICAL ZERO POSITION OF THE HORIZONTAL STABILIZER IAW AMM 27-40-02. OPS CHECK GOOD. PERFORMED OPERATIONAL CHECK IAW 30-42-00 COULD NOT DUPLICATE. OPS CHECK GOOD.
PTRIM MAIN INOP FL 270, BACKUP PTRIM OPERATED NORMALLY. "TRANSFERRED TO NRWC 698-ORD-04543" PTRIM MAIN INOP. C/A-REMOVED AND REPLACED HSCU IAW AMM 27-40-01. OPC GOOD.
FWD CABIN FLASHLIGHT CRADLE BROKEN-C/A-REMOVED AND REPLACED FWD CABIN FLASHLIGHT ASSY, OPC GOOD IAW EMB AMM 33-50-16
AISLE EMERGENCY LIGHT ROW 3 INOP-C/A-REMOVED AND REPLACED AISLE EMERGENCY LIGHT ROW 3 LAMP, OPC GOOD IAW EMB AMM 33-50-08
FA REPORTS EMERG LIGHTS WOULD NOT TEST. REINITIALIZED POWER TO A/C EMERG LIGHTS OPS CK GOOD IAW AMM 33-50-00.
INBD BRAKE INOPERATIVE ON FINAL.. CREW REPORTED INDICATIONS NORMAL ON TAXI TO GATE AFTER LANDING. PERFORMED GVI OF BOTH MLG AND BOTH INBD AND OTBD BRAKES, NO DEFECTS NOTED. BRAKE SYSTEM OPERATES NORMAL IAW AMM 32-41-00 PAR J .(2.). NO CMC MESSAGES DISPLAYED, NO FAULTS FOUND.
DURING CRUISE AT 19000 FT, ODOR ELECTRICAL WHILE IN VMC. COMPLIED WITH FIM 1-20-00-810-801. INSPECTED & OPERATED THE SENSOR, HEATING PACKS, RECIRCULATION, GASPERS, WINDSHIELD HEAT, COCKPIT LIGHTING & DISPLAYS. NO DEFECTS OR ODORS NOTED.
ON GROUND POWER, APU PNEUMATICS, PACK 2 ON, GROUND RAMPERS REPORTED SMOKE OUT OF APU STARTER OUTFLOW EXHAUST. SMELL OF SMOKE IN THE FLIGHT DECK-C/A-FLIGHT CREW PLACARDED APU GEN FUNCTION MEL 2408 AUTH 060363-D MOC 056048. DEFERRAL PER MEL 49-1 AUTH # 060368DM-C (M) PRECEDURES C/W. REMOVED AND REPLACED APU START GEN IAW AMM 24-34-01. MEL ITEM RESTORED.
SERVICED DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW AMM 33-50-06-000-801-A, AND 33-50-06-400-801-A. OPS CHECKED GOOD.
DURING APPROCH, AT POWER IDLE, AN ODOR OF SOMETHING BURNING. STARTED IN COCKPIT AND WORKED ITS WAY THROUGH THE CABIN. ONLY LASTED 30 SECONDS IN COCKPIT. PERFORMED ENGINE ODOR EVENT TROUBLESHOOTING IAW ETN-EM-72-034. PERFORMED ENGINE RUNS IAW ETN-EM72-034. COULD NOT DUPLICATE THE BURNING ODOR. NO FURTHER DEFECTS NOTED.
CRACKED LT SHEAR CLIP AT FRAME 25 STRINGER 15L. REMOVED SHEAR CLIP AT FRAME 25 STRINGER 15L, FABRICATED AND INSTALLED NEW SHEAR CLIP IAW SRM 51-40-02 AND 51-30-01. RESTORED PROTECTIVE COATING IAW CPM 51-21-03, 51-21-04 AND 51-21-05 FABRICATED FROM 7475-T761 0.032 NDT'D IAW NDTM INTRODUCTION SECTION D.
MULTIPLE EMERGENCY LIGHTS, SIGNS AND FLOOR STRIPS NOT ILLUMINATING. REMOVED AND REPLACED NUMBER 2 BATTERY POWER SUPPLY AND CHARGER IAW WORK CARD 33-700-19 OPS CHECK GOOD. EMERGENCY LIGHTING BATTERY P/N 2013-1A S/N 71928.
CRACK IN SHEAR CLIP FRAME 68 BETWEEN STRINGER 6R AND 7R. REMOVED CRACKED SHEAR CLIP LOCATED DRILLED ALODINED NEW CENTER AND UPPER CLIP IAW SRM 51-20-03 AND CPM 51-21-04 FABRICATED LOWER CLIP WITH 7475-T761 0.050 IAW DRAWING 140-04102 NDT'D IAW NDTM INTRODUCTION SECTION D INSTALLED IAW SRM 53-31-04 AND RESTORED PROTECTIVE COATING IAW CPM 51-21-04, 51-21-05 51-21-06. SHEAR CLIP P/N 140-04102-607.
CORROSION ON LH/SIDE OF CENTER OMEGA AT CARBON CROSS MEMBER BETWEEN FRAME 58-59-C/A-REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW EMB 145 SRM 53-24-10, REMOVED CARBON CRESS BEAM AND OMEGA BEAM BETWEEN FRM 53-59 IAW EMB 145 SRM 51-40-02.LOCATED, DRILLED, ALODINED, PRIMED AND INSTALLED NEW BEAM BETWEEN FRAME 53-59 IAW EMB 145 SRM 51-20-03, 51-40-02 AND CPM 51-21-04 AND 51-21-05 REINSTALLED CROSSBEAM IAW EMB 145 SRM 51-40-02
CRACKED SHEAR TIE AT FRAME 65, BETWEEN STRINGERS 7L AND 9L. LOCATED, DRILLED, ALODINED, PRIMED AND INSTALLED A NEW SHEAR TIE IAW ARM 51-20-03, 51-40-02, CPM 51-21-04, 51-21-05, AND 51-21-06
CRACKED SHEAR TIE AT FRAME 68, BETWEEN STRINGERS 6L AND 7L. REMOVED, FABRICATED, AND INSTALLED A NEW SHEAR TIE IAW SRM 53-31-04, 51-40-02, CPM 51-21-04, 51-21-05, AND 51-21-06.
CORROSION IN LATERAL L SHAPE AT FRAME 65, DOOR STOP. REMOVED CORROSION, FOUND OUT OF LIMITS, REMOVED DAMAGED AREA, LOCATED , DRILLED AND INSTALLED A SPLICE. ALODINED, PRIMED, AND PAINTED IAW SRM 53-31-04, 51-20-03, 51-40-02, CPM 51-21-04, 51-21-05, AND 51-21-06
CORROSION ON INBD SIDE OF THE LT OMEGA AT CARBON CROSS MEMBER BETWEEN FRAME 53 - 59. REMOVED THE OMEGA BEAM, DISCONNECTED BONDING JUMPER, REMOVED DOUBLER SND SUPPORT IAW AMM 51-40-02, AND 20-13-21. FABRICATED A DOUBLER AND SUPPORT IAW SRM 51-20-03, AND ENGINEERING DRAWING 145-01079. APPLIED ALODINE, PRIMER AND PAINT IAW CPM 51-21-03, 51-21-04, AND 51-21-05. LOCATED DRILLED AND INSTALLED THE NEW OMEGA BEAM BETWEEN FRAMES 53-59 IAW SRM 51-40-02. REINSTALLED BONDING JUMPER AND CROSSBEAM IAW AMM 20-13-21, AND SRM 51-40-02
CARGO DOOR HAS A GOUGE AROUND NUTPLATE HOLE ON AFT FRAME SIDE. REMOVED DAMAGE, PERFORMED HFEC INSPECTION, NO DEFECTS NOTED, FABRICATED AND INSTALLED A FILLER AND DOUBLER. INSTALLED THE DOUBLER AND FILLER IAW SRM 52-30-04, NDTM 51-00-00-916-801-00, CPM 51-21-04, 51-21-05 51-21-06, AND NCR EM-52-048.
RT OMEGA BEAM CORRODED AT FRAME 23. REMOVED CORROSION FROM RT OMEGA BEAM AT FRAME 23 REPAIR DOUBLER. NO DAMAGE ALLOWED. FABRICATED .LOCATED AND DRILLED REPLACEMENT DOUBLER. PERFORMED NDT NO DEFECTS NOTED, ALODINED PRIMED, AND INSTALLED IAW SRM51-10-03, 51-40-02,CPM 51-21-04, 51-21-05 AND NDTM 51-00-00-918-803 TYPE 1 METHOD C, SENSITIVITY LEVEL 3.
CRACKED LT SHEAR CLIP AT FRAME 27 STRINGER 15L. REMOVED AND REPLACED SHEAR CLIP AT FRAME 26 STR 15L-16L IAW SRM 51-40-02.
CRACK IN SHEAR CLIP AT FRAME 27 BETWEEN STRINGER 15R -16R. REMOVED AND REPLACED SHEAR CLIP AT FRAME 27 BETWEEN STRINGER 15R-16R IAW SRM 51-40-02.
CRACK IN SHEAR CLIP AT FRAME 65 BETWEEN STRINGERS 18L-19L. REMOVED AND REPLACED SHEAR CLIP AT FRAME 65 BETWEEN STRINGER 18L-19L IAW SRM 51-40-02.
CRACK IN SHEAR CLIP AT FRAME 24 BETWEEN STRINGER 16R-17R. REMOVED AND REPLACED SHEAR CLIP AT FRAME 24 BETWEEN STRINGERS 16R-17R IAW SRM 51-40-02.
CRACK IN SHEAR CLIP AT FRAME 67 BETWEEN STRINGERS 6L-7L. REMOVED AND REPLACED SHEAR CLIP AT FRAME 67 BETWEEN STRINGERS 6L-7L IAW SRM 51-40-02.
CORROSION IN CENTER OMEGA BEAM AT FRAME 59. CORROSION IN CENTER OMEGA BEAM AT FRAME 59 NUT PLATE HOLE FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGE AND PERFORMED NDT INSPECTION, NO DEFECTS NOTED . FABRICATED, LOCATED AND DRILLED DOUBLER FROM 2024TS 0.080. APPLIED ALODINE, PRIMER, TOP COAT AND INSTALLED DOUBLER TO CENTER OMEGA BEAM IAW SRM 53-24-10, NDTM 51-00-00-916-801-A00 AND CPM 51-21-04,51-21-05 AND 51-21-06.
CRACK IN SHEAR CLIP AT FRAME 72 BETWEEN STRINGER 17L-18L. REMOVED CRACKED SHEAR CLIP, FABRICATED NEW CLIP FROM 7075-T761 0.032, LOCATED AND DRILLED HOLES AND ALODINED AND PRIMED THEN INSTALLED CLIP IAW SRM 51-40-02, 51-30-01, CPM 51-21-04, 51-21-05 AND ENGINEERING DRAWING 145-44878-010.
AFT FLASHLIGHT CRADLE BROKEN. REMOVED AND REPLACED THE AFT FLASHLIGHT CRADLE IAW AMM 33-50-16-000-801-A, AND 33-50-16-400-801-A. OPS CHECKED GOOD.
AFT FACING EXIT LOCATOR SIGN AT ROW 12 WILL NOT ILLUMINATE. REMOVED AND REPLACED BATTERY AND BATTERY CHARGER NR 3 IAW AMM 33-50-04 AND INVERTER NR 4 IAW AMM 33-50-11 OPS CHECKED GOOD AT THIS TIME.
CAPTAIN SIDE FLASHLIGHT INOPERATIVE. R & R LIGHT BULB FOR CAPTAINS FLASHLIGHT IAW STD MX. OPERATIONS CHECKED GOOD.
DURING PS 1 CHECK, FOUND AFT CEILING EMER EXIT LIGHT STRIP INOPERATIVE. R & R AFT CEILING EMER EXIT LIGHT STRIP IAW MM 33-50-15. OPERATIONS CHECKED GOOD.
TRIM PIECE ON MAIN CABIN DOOR IS LOOSE & MAKING DOOR DIFFICULT TO OPEN. TRIM PIECE WAS REMOVED & DEFERRED MAIN PAX DOOR TRIM.
EMERGENCY LIGHT STRIP NR 8, PANEL 261 BF, HAS BROKEN CONNECTOR. REPAIRED SPLICE CONNECTOR ON PLANE SIDE FOR EMER LIGHT STRIP NR 8 IAW SWPM 20-21-00.
LEFT FWD CARGO FLOOR SUPPORT, FWD OF CROSSBEAM HAS CORROSION AROUND NUTPLATE. REMOVED THE CORRODED LT FWD CARGO FLOOR SUPPORT & INSTALLED THE NEW SERVICEABLE FLOOR SUPPORT IAW SRM 51-40-02.
TOP OF FRAME 66 CRACKED, BETWEEN RIVET HOLES FOR LOWER LT BRACKET FOR CARGO DOOR RAMP SUPPORT. REPAIRED LOWER LT BRACKET FOR CARGO DOOR RAMP SUPPORT AT FRAME 66 IAW ERS-EM-53MR-1837. SEE WIPS & TASKS FOR DETAILS OF WORK PERFORMED.
TOP OF FRAME 67 CRACKED, BETWEEN RIVET HOLES FOR LOWER LT BRACKET FOR CARGO DOOR RAMP SUPPORT. REPAIRED LOWER LT BRACKET FOR CARGO DOOR RAMP SUPPORT AT FRAME 67 IAW ERS-EM-53MR-1837. SEE WIPS & TASKS FOR DETAILS OF WORK PERFORMED.
RIGHT UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 & ABOVE STRINGER 2R. CRACK IS APPROX 1/4" LONG. REPAIRED RT UPPER FUSELAGE SKIN CRACK IAW ERS-EM-53MR-1840. SEE WIPS & TASKS FOR DETAILS OF WORK PERFORMED.
CORROSION FOUND ON LT UNDER THE GUSSET, ON BEAM AT FRAME, BETWEEN 59 & 60. REPAIRED THE LT BEAM UNDER THE GUSSET IAW ERS-EM-53MR-1839. SEE WIPS & TASKS FOR DETAILS OF WORK PERFORMED.
LEFT UPPER FUSELAGE SKIN CRACKED 2 PLACES. CRACK 1= 1/4"CRACK JUST AFT OF FRAME 75 & ABOVE STRINGER 2L, CRACK 2 =1/4" CRACK ON FRAME 75, AT FIRST FASTENER BELOW STRINGER 2L. REPAIRED LT UPPER FUSELAGE SKIN IAW ERS-EM-53MR-1840. SEE WIPS & TASKS FOR DETAILS OF WORK PERFORMED.
PACK 2 OVLD IN CRUISE FLIGHT AT FL 300 MEL 21-29. R & R NR 2 PACK OVERPRESSURE SWITCH IAW AMM-21-51-06. OPERATIONS CHECKED GOOD AT THIS TIME, MEL RESTORED.
AFT CABIN EMER FLASHLIGHT WILL NOT CHARGE. R & R AFT CABIN EMER FLASHLIGHT IAW AMM 33-50-16-000-801-A & 33-50-16-400-801-A. OPERATIONS CHECKED GOOD AT THIS TIME.
LANDING GEAR LEVER DISAGREEMENT, AIR TURN BACK. LG DID NOT RETRACT AFTER TAKEOFF. GEAR IN TRANSIT ALL THREE GEARS CAME ON & STAYED ON WITH GEAR HANDLE UP. LG DISAGREE EICAS MSG CAME ON AFTER 10 SECS. GEAR HANDLE MOVED TO DOWN & ALL THREE GEAR DOWN INDICATION DISPLAYED. ABNORMAL GEAR EXTENSION PROCEDURE WAS ACCOMPLISHED IAW AOM VOL 1. NORMAL RATE OF DECENT FOR LANDING. R & R LG CONTROL LEVER. PERFORMED OPERATIONAL CHECK OF THE LG EXTENSION & RETRACTION CYCLE & PERFORMED GVI OF NLG & MLG COMPONENTS & WW WITH NO DEFECTS NOTED. LG OPERATIONS CHECKED GOOD IAW AMM 32-32-02 & 32-30-00 EMB AMM.
ON INITIAL CLIMB OUT WE GOT BLEED 2 OVERTEMP. CONFIRMED OPERATIONS OF FAN AIR VLV 2. NO LEAKS AT PRE COOLER 2. R & R WITH SERVICEABLE PRE COOLER 2 OUTLET TEMP SENSOR IAW EMB AMM 36 20 01, OPERATIONS CHECKED IAW AMM 36 00 00, 700 - 803A.
FLAP LOW SPEED ADVISORY MSG ON EICAS AFTER LANDING. ITEM DEFERRED IAW MEL 27-9. FLAP LT MOTOR BRAKE FAIL M PROCEDURE COMPLIED WITH.
LEFT OVERWING AFT EMER LIGHT INOPERATIVE. R & R LT OVERWING AFT EMER LIGHT ASSEMBLY IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A. OPERATIONS CHECKED GOOD.
PNEUMATIC ICE TEST INFLIGHT DID NOT SHOW OPEN INSCRIPTION ON WING. ALL OTHER INDICATES NORMAL. R & R LIGHT BULBS IAW AMM 20-13-04. OPERATIONS CHECKED IAW AMM 30-00-00. OPERATIONS CHECKED GOOD.
PARKING BRAKE LIGHT INOPERATIVE. R & R THE LAMPS IAW AMM 20-13-04. OPS CHECKED GOOD.
RAM AIR VLV FAIL. DURING CLIMB CREW RECEIVED EICAS PACK 2 VLV CLSD & RAM AIR VLV FAIL MSG. CREW COMPLIED WITH AOM VOL 1 PROCEDURES & WAS ABLE TO RESET THE NR 2 PACK, HOWEVER THE RAM AIR VLV FAIL MSG REMAINED. CREW ELECTED TO RETURN & LANDED WITHOUT INCIDENT. PERFORMED RAM AIR VLV ADJUSTMENT & TEST IAW AMM 21-25-01. BOTH VLVS REMAIN CLOSED. R & R RELAY K0804 IAW AMM 21-13-02. OPERATIONS CHECKED GOOD IAW AMM 21-25-01 & 21-60-00.
RIGHT OMEGA BEAM AT FRAME 23 CORRODED ON PREVIOUS BLEND. REPAIRED CORRODED AREA IAW ERS-EM-53MR-231.
FRAME 20 CTR ALUMINUM CROSS BEAM IS CORRODED. INSTALLED SERVICEABLE FRAME 20 ALUMINUM CROSS BEAM IAW AEA ETN EM 53-139 R3.
SHEAR CLIP ON FRAME 65 CRACKED BETWEEN 6L - 8L. REMOVED CRACKED SHEAR CLIP ON FRAME 65 BETWEEN 6L - 8L. PREPPED & INSTALLED SERVICEABLE SHEAR CLIPS IAW SRM 53-31-04.
FOUND CORROSION IN LT & RT HORIZONTAL STABILIZER SPHERICAL BEARING HOUSING. REWORKED BOTH LT & RT HORIZONTAL STABILIZER SPHERICAL BEARING HOUSINGS TO THE FIRST OVER SIZE TO REMOVE ALL CORROSION IAW SRM 55-30-02. SEE NRTC E363658 FOR HORIZONTAL STAB INSTALLATION & SEE NRTC E365978 FOR DIHEDRAL & INCIDENCE CHECK.
BLEED 2 OVER TEMPERATURE CLIMBING THROUGH FL 220. REPLACE FAN AIR VLV FILTER IAW FIM 36-11-00-810-804A. FAN ACFT OPERATIONS CHECKED GOOD 72-00-00.
CA FLASHLIGHT INOPERATIVE. REPLACED CA FLASHLIGHT IAW 33-50-16.
AFT AISLE CEILING EMERGENCY LIGHT INOPERATIVE. R & R AFT AISLE CEILING EMERGENCY LIGHT BULB IAW AMM 33-50-08.
DRING COURTESY CHECK FOUND NR 4 EMERGENCY LIGHT TO BE INOPERATIVE. R & R NR 4 EPSU BATTERY IAW AMM 33-50-04, OPS CHECK GOOD EMERGENCY LIGHT OPERABLE.
DURING B INSPECTION FOUND THE MAIN-DOOR EMERGENCY LIGHT COVER HAS MULTIPLE HOLES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN-DOOR EMERGENCY LIGHT ASSEMBLY IAW EMB AMM 25-23-04 STEPS 2(J)3 AND 3(I)3. EMERGENCY LIGHTS OPERATIONAL CHECK WAS GOOD IAW EMB AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 3402 THE CREW REPORTED THE REAR CABIN FLASHLIGHT HOLDER HAS A BROKEN CLIP AND WOULD NOT HOLD FLASHLIGHT IN PLACE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE REAR CABIN FLASHLIGHT HOLDER IAW AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
FOR FLIGHT 2840 THE CREW REPORTED THAT ON TAXI IN ON ENGINE NR 2 OPERATING ADVANCED NR 2 THRUST LEVER THE NR 2 GEN OVERLOADED AND THEN THE NR 2 ENGINE SHUT DOWN. STARTED THE NR 1 ENGINE WITH APU ASSISTING THE ENGINE START. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH RR FIM TASK 72-00-00-810-815 WITH NO DEFECTS NOTED. FDR DOWNLOAD SHOWS NR 2 ENGINE HAD NORMAL SHUT DOWN AFTER NR 1 ENGINE WAS RESTARTED. PERFORMED ENGINE RUNS IAW RR MM 72-00-00 NO DEFECTS NOTED. THE NR 2 ENGINE OPERATIONAL CHECKS WERE GOOD. REMOVED AND REPLACED THE NR 2 GENERATOR IAW EMB145 MTX W/C 24-800-00. THE OPERATIONAL & LEAK CHECKS WERE GOOD. REMOVED AND REPLACED NR 2 GENERATOR CONTROL UNIT IAW EMB 145 AMM 24-31-02. THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING B INSPECTION FOUND THE FORWARD CEILING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD 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.
ON FLIGHT 2977 THE CREW REPORTED THE COCKPIT FLASHLIGHT BRACKET WAS LOOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. SECURED COCKPIT FLASHLIGHT BRACKET IAW EMB-145 MM 25-60-00. OK FOR SERVICE. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 4306 THE FLIGHT ATTENDANT REPORTED THAT UPON DESCENT TO ORD SHE NOTICED THE AFT CABIN GOT HOT AND SAID SHE DETECTED A FAINT BURNING ELECTRICAL ODOR. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED GENERAL VISUAL INSPECTION OF CABIN COMPARTMENT LIGHTS. CYCLED ELECTRICAL POWER. RAN APU WITH BOTH PACKS ON. COULD NOT DUPLICATE. NO DEFECTS FOUND. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING PS2 INSPECTION FOUND THE RIGHT EMERGENCY LIGHT OVER WING BURNT OUT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BURNT EMERGENCY BULB OVER RIGHT WING IAW EMB145 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE INSPECTION, FOUND THE MAIN DOOR EXIT EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN DOOR EXIT EMERGENCY LIGHT LAMP IAW AMM 33-50-10. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
DURING B INSPECTION, FOUND THE NR 4 CABIN PROXIMITY LIGHT CRACKED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 CABIN PROXIMITY LIGHT IAW AMM 33-50-12, NRTC BOW93438. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
LEFT OVERWING EMERGENCY ESCAPE HATCH SKIN GOUGED AT LOWER FWD END NEAR METAL CLIP.(MARKED) REPAIRED LT OVERWING EMERGECY ESCAPE HATCH SKIN GOUGE AT LOWER FWD END NEAR METAL CLIP IAW EO EM-52MR-310.
DURING B INSPECTION, FOUND THE SERVICE DOOR CUTOUT FORWARD FRAME HAS CORROSION AT LOWER AREA. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SERVICE DOOR CUTOUT FORWARD FRAME IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.
DURING B INSPECTION, FOUND THE LEFT OVERWING EMERGENCY EXIT HATCH CATCHES AT UPPER END WHILE OPENING. AIRCRAFT REMOVED FROM SERVICE. ADJUSTED LEFT OVERWING EMERGENCY EXIT HATCH LINING IAW AMM 52-21-00. AIRCRAFT RETURNED TO SERVICE.
DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY LIGHT STRIP 2 & 3 ARE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 INVERTER IAW EMB-145 AMM 33-50-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 2836 THE CREW REPORTED THE EMERGENCY LIGHT PROXIMITY STRIP AT 6-8A AND THE EMERGENCY EXIT LIGHTS FROM ROW 3 THRU 8 TO BE INOPERABLE (FLOOR STRIP LIGHTS). THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED EMERGENCY LIGHT PROXIMITY STRIP AT ROW 6-8A. THE OPERATIONAL CHECK WAS GOOD IAW 33-50-12. REMOVED AND REPLACED THE EMERGENCY PROXIMITY STRIP AT ROW 3-8A. THE OPERATIONAL CHECK WAS GOOD IAW 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 3275 THE CREW REPORTED A BURNING ODOR IN THE COCKPIT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FIRST OFFICERâS MULTI FUNCTION DISPLAY UNIT IAW EMB-145 AMM 34-22-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 3302 THE CREW REPORTED THAT ON APPROACH THEY DECLARED AN EMERGENCY FOR A WING ANTI-ICE FAIL FOLLOWED BY A BLEED 2 VALVE FAIL. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. CMC POSTED WING 1 LEAK REPLACED COUPLINGS AT LEFT DUAL TEMP CONTROL VALVE NORMAL PACK OPERATION EMB 145 AMM 21-51-00. OPERATIONAL TEST OF ANTI-ICING SYSYTEM IAW EMB 145 AMM 30-00-00 CHECKS GOOD. BLEED 2 VALVE CHECKS GOOD EMB AMM 36-11-05. REMOVED AND REPLACED COUPLING GOING TO HEAT EXCHANGER IAW EMB 145 AMM 21-51-00. THE OPERATIONAL CHECK WAS GOOD IAW EMB 145 AMM 21-00-00. THE AIRCRAFT WAS RETURNED TO SERVICE.
LT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED NR 4 BATTERY PACK AND CHARGER.
ON FLIGHT 4319 THE CREW REPORTED THAT THE GUST LOCK DID NOT FULLY RELEASE ON TAKEOFF. THE CREW ELECTED TO ABORT THE TAKEOFF. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED BOTH GUST LOCK SPRING CARTRIDGES IAW EMB 145 AMM 27-71-03. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 3992 AFTER TAKEOFF DURING GEAR RETRACTION CREW RECEIVED A L/G DISAGREE AND RIGHT L/G RED. CREW RAN CHECKLIST AND NOTED NORMAL ONLY WHEN GEAR DOWN. CREW RETURNED FOR LANDING AND WAS ADVISED BY CONTROL TOWER THAT THE NR 3 TIRE WAS BLOWN. AFTER LANDING CREW RECEIVED L/G AIR/GND FAIL, BRAKE DISAGREE, PITOT 3 INOP, E1/2 IDLE STOP FAIL MESSAGES. ALSO WASNâT ABLE TO PUT GUST LOCK ON. A/C TOWED TO GATE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 3 WHEEL/TIRE ASSEMBLY, RT GEAR BRAKE TEMP HARNESS, WOW HARNESS REPLACED SEVERAL HARNESS CLAMPS, RT MLG WHEEL SPEED TRANSDUCER HARNESS, NUMBER 3 BRAKE LINES. RETRACTION CHECK COMPLETED. OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
ON FLIGHT 3484 DURING CLIMB AT 280, CREW REPORTED SERVICE DOOR WARNING INDICATION ILLUMINATED. PRESSURIZATION HELD. CREW DECLARED EMERGENCY. AIRCRAFT REMOVED FROM SERVICE. MAINTENANCE MEASURED GAPS AROUND SERVICE DOOR AND OPERATIONAL CHECKED THE DOOR, ISSUED MEL 52-04. ADJUSTED MICROSWITCH S7246 IAW EMB 145 AMM 52-74-01. OPERATIONAL TEST GOOD. THIS RESTORES MEL 52-04. AIRCRAFT RETURNED TO SERVICE.
HEARD CIRCUIT BREAK EBV-2(C-21) POP OUT. REPAIRED CHAFED WIRE AT RELAY K0542 IAW EMB AMM 20-10-00. OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
CLIMBING THROUGH 36,000 FEET, THE NR 2 ENGINE OIL QUANTITY STARTED DROPPING AT A STEADY RATE, DIVERTED TO NEAREST SUITABLE AIRPORT. DURING DESCENT OIL LEVEL GOT DOWN TO 3 QUARTS AND OIL PRESSURE WAS FOLLOWING LOWEST PRESSURE NOTED WAS 15 POUNDS PER SQUARE INCH BEFORE SHUTTING DOWN ENGINE. (M)
DFW - FLT 3788 - SULFUR INSULATION SMELL IN FLIGHT ACCOMPANIED BY WINDSHIELD FOGGING OVER. NO EICAS MSG RECEIVED. DISCOVERED LARGE BLEED AIR LEAK FROM THE PACK VALVE, PACK INLET BLEED TUBE. REMOVED AND INSTALLED BLEED TUBE IAW EMB145 AMM 31-51-01 AND PACK INLET PRESSURE SENSE LINE IAW EMB 145 AMM 21-80-01. NO LEAKS NOTED. RAN A/C PACK COOLING SYSTEM OPERATING TESTS. NO FAULTS NOTED OR ODORS DETECTED. AIRCRAFT RETURNED TO SERVICE. (M)