N696AE
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
ON APU START UP A BURNING FUMES WERE SMELT IN FLIGHT DECK. INSPECTED FWD AVIONICS BAY AND APU NO DEFECTS NOTED. STARTED APU NO SMELL NOTED. A/C OK FOR SERVICE.
BLEED 1 LEAK MESSAGE IN FLIGHT. FACT 17MAY26 00:12 CLT TIGHTENED 2 V-BAND CLAMPS IN LH PYLON IRT AMM 36-11-09. C/W OPS CK IRT AMM 36-00-00. NO FIX, "BLEED 1 LEAK" ON EICAS AFTER 3 MINS. DISCOVERED LOOSE WORM CLAMP ON LH PACK EXHAUST. TIGHTENED WORM CLAMP A/R. FOUND LEAK ON LH VALVE REGULATOR. R&R'D LH VALVE REGULATOR IRW AMM 36-11-05. LEAK CHECK GOOD.
FA FWD FLASHLIGHT CLIP HOLDER BROKEN. FLIGHT DECK FA FLASHLIGHT HOLDER. R & R BROKEN FLASHLIGHT CLIP IAW CMM 25-60-14. OPS CHECKED GOOD,
FORWARD 4 ROWS FLOOR LIGHTS-EMERGENCY LIGHTS INOP.R&R #300 INVERT PER AMM 33-50-11 NO FIX R&R #200 BATTERY PER AMM 33-50-04 OPS CHECK GOOD PN ON 7824-1 PN OFF 7824-1 PN ON BATTERY 2013-1ASMI CC1463 PN OFF 2013-1A 67196
DESCENDING AROUND 22000FT , A LOT OF STATIC AND TURBULANCE. SMELL AS IF IT WERE A LIT MATCH AND STRONG SMELL FOR ABOUT 90 SECONDS FACT 31MAR25 20:17 PHL COULD NOT DUPLICATE SMELL RAN PACKS INSPECTED PLANE FOR DAMAGE. NO DEFECTS FOUND. OK FOR SERVICE AT THIS TIME
IN FLIGHT STRONG ELECTRICAL BURNING SMELL IN COCKPIT AND FWD CABIN FACT 05MAR25 22:13 ORF REMOVED AND INSPECTED RELAY PANELS NO DEFECTS NOTED. RAN PACK ON ENGINES AND APU 15 MIN IDLE/15MINUTES 63% N1 NO DEFECTS NOTED AC OK FOR SERVICE
WHILE AT GATE GPU CONNECTED SAW GPU SMOKING. DESELECTED GPU AND AFTER A/C SHUT DOWN AND POWERED UP. FOUND SOMEBODY TO DISCONNECT GPU AND NOTICED STRONG SMOKE SMELL IN A/C. PERFORMED EXTERNAL POWER TEST IAW 24-40-00-700-801-A OPS CHECK'D OK. VISUALLY INSP GROUND POWER AREA, NO DAMAGE NOTED. OK FOR SERVICE
E050565 RH SIDE FUSELAGE UPPER SKIN HAS POSSIBLE CRACK AROUND (1) FASTENER AT FRAME 78. REPAIRED IAW EO1-53-24-0571.
E052117 L/H OMEGA BEAM GUSSET #7 HAS CORROSION IN MULTIPLE AREAS. RAR L/H OMEGA BEAM GUSSET #7 IAW EMB 145 SRM 51-40-02
E052222 CENTER OMEGA BEAM #5 GUSSET HAS CORROSION. REMOVED AND REPLACED CENTER OMEGA BEAM #5 GUSSET IAW EMB 145 SRM 51-40-02.
E053208 RH SHEAR CLIP AT FR 13 BETWEEN STGR 06R AND STGR 07R CRACKED. REMOVED AND REPLACED RH SHEAR CLIP AT FR 13 BETWEEN STGR 06R AND STGR 07R IAW EMB-145 SRM 51-40-02.
E052082 L/H UPPER SEAT TRACK #6 HAS CORROSION, NICKS AND GOUGES IN MULTIPLE AREAS. REMOVED AND REPLACED L/H UPPER SEAT TRACK #6 IAW EMB 145 AMM 53-01-06.
E052289 AFT FUSELAGE 1, FWD LOWER CORNER OF THE CARGO DOOR CUTOUT, THERE IS CORROSION IN THE CORNER. REPAIRED FWD LOWER CORNER OF CARGO DOOR CUTOUT (FR65 SHEAR CLIP LOWER SECTION) IAW EMB145 SRM 53-31-04RE, ITEM 4D, FIG 212 AND PDT EO-53-24-0531
E052237 LH OMEGA BEAM #6 GUSSET HAS CORROSION. REMOVED AND REPLACED LH OMEGA BEAM #6 GUSSET IAW EMB 145 SRM 51-40-02
E052163 LH FLOOR SILL #4 HAS CORROSION IN MULTIPLE AREAS. REMOVED AND REPLACED LH FLOOR SILL #4 IAW EMB 145 SRM 51-40-02
E052079 LAV POTABLE WATER DRAIN CABLE SUPPORT BRACKET HAS CORROSION. REMOVED AND REPLACED LAV POTABLE WATER DRAIN CABLE SUPPORT BRACKET IAW EMB145 SRM 51-40-02.
E052355 LH FLOOR SILL #3 HAS CORROSION IN MULTIPLE AREAS. REMOVED CORRODED LH FLOOR SILL #3 AND INSTALLED SERVICEABLE FLOOR SILL IAW EMB 145 SRM 51-40-02.
E052180 CENTER OMEGA BEAM #3 GUSSET HAS CORROSION. REMOVED AND REPLACED CENTER OMEGA BEAM #3 GUSSET IAW EMB 145 SRM 51-40-02
E052164 LH OMEGA BEAM #4 GUSSET HAS CORROSION IN MULTIPLE AREAS. REMOVED AND REPLACED LH OMEGA BEAM #4 GUSSET IAW EMB 145 SRM 51-40-02
E053099 LH OMEGA BEAM SIDEWALL CRACKED AT FR 26. PERFORMED DOUBLER AND FILLER REPAIR ON LH OMEGA BEAM AT FR26 IAW ETD2024-145-023732 REV "B" AND EO1-53-24-0566
E053101 LH OMEGA BEAM SIDEWALL CRACKED AT FR 28. PERFORMED DOUBLER, FILLER REPAIR FOR L/H OMEGA BEAM SIDEWALL AT FRAME 28 IAW ETD2024-145-023732, REV B AND EO1-53-24-0568.
E053100 LH OMEGA BEAM SIDEWALL CRACKED AT FR 27. PERFORMED DOUBLER, FILLER REPAIR FOR L/H OMEGA BEAM SIDEWALL AT FRAME 27 IAW ETD2024-145-023732, REV B AND EO1-53-24-0567.
E053098 CENTER OMEGA BEAM SIDEWALL CRACKED AT FR 27. PERFORMED CUTOUT AS REQUIRED TO REMOVE DAMAGE FROM CENTER OMEGA BEAM SIDEWALL AT FR 27 AND FABRICATED AND INSTALLED FILLER AND DOUBLER IAW ETD2024-145-023735 REV. C AND EO1-53-24-0569.
E052973 LAV POTABLE WATER FILL/DRAIN EXTERNAL REINFORCEMENT PLATE HAS CORROSION. REMOVED AND INSTALLED NEW LAV POTABLE WATER FILL/DRAIN EXTERNAL REINFORCEMENT PLATE IAW EMB 145 SRM 51-40-02.
E052562 LH OMEGA BEAM #2 GUSSET HAS CORROSION. RAR LH OMEGA BEAM #2 GUSSET IAW EMB 145 SRM 51-40-02.
E052588 SHEAR CLIP AT FR24, BETWEEN STR15R-STR16R IS CRACKED. RAR SHEAR CLIP AT FR24, BETWEEN STR15R-STR16R IAW EMB I45 SRM 51-40-02
E052521 RH FLOOR SILL #2 HAS CORROSION. REMOVED AND INSTALLED SERVICEABLE R/H # 2 FLOOR SILL IAW EMB 145 SRM 51-40-02
E052532 RH LOWER SEAT TRACK #2 HAS CORROSION. REMOVED AND REPLACED RH LOWER SEAT TRACK #2 AND TORQUED SCREWS IAW EMB 145 AMM 53-01-06.
E052533 CENTER OMEGA BEAM #2 GUSSET HAS CORROSION. REMOVED AND REPLACED CENTER OMEGA BEAM GUSSET #2 IAW EMB 145 SRM 51-40-02
E052544 RH FLOOR SILL #1 HAS CORROSION AT FR25. RAR RH FLOOR SILL #1 IAW EMB 145 SRM 51-40-02.
LH OMEGA BEAM #3 GUSSET HAS CORROSION. REMOVED AND REPLACED LH OMEGA BEAM #3 GUSSET IAW EMB 145 SRM 51-40-02
E052555 CENTER OMEGA BEAM #1 GUSSET HAS CORROSION. RAR CENTER OMEGA BEAM #1 GUSSET IAW EMB 145 SRM 51-40-02
E052531 RH UPPER SEAT TRACK #2 HAS POSSIBLE CORROSION AT FR31. RAR RH UPPER SEAT TRACK #2 IAW EMB 145 AMM 53-01-06
E052290 AFT FUSELAGE 1, ON THE LOWER EDGE OF THE CARGO DOOR CUT OUT THERE IS CORROSION. AT FR 65-66, STGR 16L-17L. REMOVED AND REPLACED AFT FUSELAGE1 CARGO DOOR CUTOUT LOWER CENTER SILL IAW EMB145 SRM 51-40-02.
E052415 SERVICE DOOR LWR CENTER SILL HAS CORROSION. REMOVED AND INSTALLED SERVICEABLE SERVICE DOOR LOWER CENTER SILL IAW EMB145 SRM 51-40-02.
E052167 LH LOWER SEAT TRACK #4 HAS CORROSION AT FR38. REMOVED, AND REPLACED THE LH LOWER SEAT TRACK #4 THAT WAS CORRODED AT FR38 IAW EMB 145 AMM 53-01-06.
E052428 L/H LWR SEAT-TRACK #1 HAS CORROSION, NICKS AND GOUGES IN MULTIPLE AREAS. REMOVED CORRODED, NICKED, GOUGED L/H LWR SEAT TRACK #1 AND INSTALLED SERVICEABLE #1 SEAT TRACK IAW EMB 145 AMM 53-01-06.
E052161 LH FLOOR SILL #5 HAS CORROSION IN MULTIPLE AREAS INCLUDING PREVIOUSLY BLENDED AREA. REMOVED CORRODED LH FLOOR SILL #5 AND INSTALLED SERVICEABLE FLOOR SILL IAW EMB 145 SRM 51-40-02
E052160 LH UPPER SEAT TRACK #5 HAS CORROSION AT FR48. REMOVED AND REPLACED LH UPPER SEAT TRACK #5 AT FR48 IAW EMB 145 AMM 53-01-06.
E052154 LH FLOOR SILL #6 HAS CORROSION IN MULTIPLE AREAS. REMOVED CORRODED LH FLOOR SILL #6 AND INSTALLED SERVICEABLE FLOOR SILL IAW EMB 145 SRM 51-40-02.
E052107 CENTER OMEGA BEAM GUSSET #6 HAS CORROSION IN MULTIPLE AREAS. RAR CENTER OMEGA BEAM GUSSET #6 IAW EMB 145 SRM 51-40-02.
E052092 R/H UPPER SEAT TRACK #5 HAS CORROSION, NICKS AND GOUGES IN MULTIPLE AREAS. REMOVED AND REPLACED R/H UPPER SEAT TRACK #5 IAW EMB 145 AMM 53-01-06.
E052089 L/H LWR SEAT TRACK #6 HAS CORROSION NICKS AND GOUGES IN MULTIPLE AREAS. REMOVED AND REPLACED L/H LWR SEAT TRACK #6 AND TORQUED SCREWS IAW EMB 145 AMM 53-01-06.
E052093 R/H LWR SEAT TRACK #5 HAS CORROSION, NICKS AND GOUGES IN MULTIPLE AREAS. RAR THE R/H LWR SEAT TRACK #5 IAW EMB 145 AMM 53-01-06.
E051650 CORROSION AROUND NUT PLATE HOLES ON LH WING AT AFT BELLY PANEL LH LOWER ATTACHMENT FLANGES. RAR LH WING AFT BELLY PANEL LOWER ATTACHMENT FLANGE IAW EMB-145 SRM 51-40-02
E051821 HORIZONTAL STABILIZER L/H AND R/H SPHERICAL BEARING HOUSINGS WORN OUT OF LIMITS. REPAIRED IAW EO1-53-24-0548
E050563 LH SIDE FUSELAGE UPPER SKIN HAS POSSIBLE CRACK AROUND (2) FASTENERS AT FRAME 78. REPAIRED IAW EO1-53-24-0570
RH OVERWING EMERGENCY LIGHT INOP.-C/A-RAR RH OVERWING LIGHT LAMP IAW 145 AMM 33-50-07. OPC GOOD. MEL ITEM RESTORED.
RH OVERWING EMERGENCY LIGHT INOP-C/A-RAR RH OVERWING EMERGENCY LIGHT LAMPIAW EMB AMM 33-50-07-000-801-A AND 33-50-07-400-801-A. OPC GOOD. END.
ICE COND-A/I INOP WARNING AND WG A/ICE FAIL CAUTION ILLUNINATED IN CLIMB FL 200 , TEMP-13 SAT TAT WING ICE PROTECTION PUSHBUTTON DID NOT ILLUMINATE . EXITED ICE CONDITION IN FLIGHT AND RAN QRH WITH NO EFFECT. "TRANSFERRED FROM AML PAGE 4922319 ITEM 1"-C/A-RAR DUAL HEAT EXCHANGER OUTLET GRATE AND RUBBER SLEEVE IAW EMB 145 AMM 21-51-02. LEAK CHECKS GOOD NO DEFECTS NOTED.
AFT CABIN EMERGENCY FLASHLIGHT HOLDER BROKEN.MEL 25-32 AUTH. #110172M-C ORIGINAL AML P. 4590238 ITEM #1.-C/A-RAR AFT CABIN EMERGENCY FLASHLIGHT ASSY.IAW AMM 33-50-16 OPC CHECK GOOD MEL 25-32 RESTORED
# 1 AFT EMERGENCY CABIN FLASHLIGHT HOLDER BROKEN IN REF LG PG 4590238 ITEM-C/A-AFT EMERGENCY CABIN FLASHLIGHT DEFERRED (M) PROCEDURE C/W
AFT EMERGENCY CEILING LIGHT, AFT FACING LIGHT INOP.-C/A-RAR'D LIGHT ASSY PER AMM 33-50-15, AND RAR'D INVERTER PER AMM 33-50-11. OPS CHECK IS GOOD
AVIONICS ISSUES TRANSPONDER 1 FAIL NO FMS GS AFTER ROTATION FD WENT AWAY MFD TRACKING INCORRECTLY NO EICAS MESSAGE EMERGENCY NOT DECLARED. -C/A-INSPECTED FMS 1 AND 2 AND FOUND BOTH GPS 1 AND 2 FAIL ON CAPT'S SIDE PERFORMED RESET OF ELECTRICAL SYSTEM AS PER AMM 24-60-00 AND AMM 34-62-00
BLEED 1 LIEAK ENROUTE CLIMBING THROUGH FL210. QRH PROCEDURE COMPLIED WITH, MESSAGE EXTINGUISHED, DECLARED EMERGENCY CHG EQ FLT CONT. C/A: GROUND FOUND NR 7 JOINT LEAKING AIR. R & R NR 7 O-RINGS IN REF TO AMM 36-11-10 AND RE-CONNECTED NR 7 COUPLER. PERFORMED LEAK CHECK ABOUT 15 MINS, IN REF TO AMM 36-11-09. NO LEAKING FOUND AT THIS TIME & NO MESSAGE NOTED.
BROKEN EMERGENCY LIGHT STRIP WIRE AT FLOOR PANEL 231GL. C/A UPON FURTHER INVESTIGATION FOUND PANEL NUMBER TO BE 231GF. REPAIRED EMERGENCY LIGHT STRIP WIRE AT FLOOR PANEL 231GF, IAW EMB 145 SWPM 20-21-00 AND SYS CHK IAW EMB 145 AMM 33-50-00. CHECK GOOD.
LT WING SPAR 1 LOWER FLANGE CRACKED AT SCREW HOLE JUST OUTBOARD OF RIB 9 THRU TO THE RADIUS OF THE SPAR FACE. C/A PERFORMED REPAIR OF LT WING SPAR 1, IAW EMB 145 SRM 57-20-05 STEP 3X.
EMERGENCY LIGHT STRIP NR 4 WIRE DAMAGED, ON LIGHT STRIP. FOUND ON OPEN UP. C/A, REMOVED AND REPLACED EMERGENCY LIGHT STRIP NR 4, IAW EMB 145 AMM 33-50-12. PERFORMED OPC, IAW EMB145 AMM 33-50-00. SYS CKS GOOD.
LT OMEGA BEAM CRACKED AT LOWER INBOARD RIVET AT FR 23. C/A PERFORMED REPAIR FOR LT OMEGA BEAM CRACKED AT LOWER INBOARD RIVET AT FR 23, IAW EMB ERS-EM-53MR-4187.
THE LT WING LEADING EDGE 2 IS DENTED IN THE POLISHED AREA 38" FROM THE OUTBOARD END, AS MARKED. C/A-ACCOMPLISHED PERMANENT REPAIR TO LT LEADING EDGE 2, IAW ENVOY ERS-EM-57MR-1264.
FR 72 CRACKED STGR 16L AT RIVET BUCKTAIL. C/A PERFORMED REPAIR TO FR72 LT SECTION, IAW ERS-EM-5300-4180 AND EMB 145 SRM 53-00-04, ITEM 3, FIG.201.
SSI 52-30-08 CORROSION ON BAGGAGE DOOR FWD FRAME. C/A INSTALLED FABRICATED LOWER BAGGAGE DOOR FWD FRAME DOUBLER & FILLER, IAW EMB145 SRM 52-30-04RE.
CORROSION ON BAGGAGE DOOR LOWER FWD WEBBING. C/A INSTALLED REPAIR DOUBLER AND NUTPLATE ON BAGGAGE DOOR LOWER FWD WEBBING, IAW EMB145 SRM 51-40-02.
RH OMEGA BEAM INBD SUPPORT IS CRACKED BETWEEN FRAMES 47-48-C/A-REMOVED UNSERVICEABLE RH OMEGA BEAM INBD SUPPORT BETWEEN FRAMES 47-50 IAW EMB 145 SRM 51-40-02 AND INSTALLED SERVICEABLE RH OMEGA BEAM SUPPORT FROM FR 47-50 IAW EMB 145 SRM 51-40-02 AND EMB 145 SRM 53-23-02.
LT OMEGA BEAM SUPPORT COLUMN AT FRAME 29 IS CRACKED MARKED. C/A REMOVED AND REPLACED LT OMEGA BEAM SUPPORT COLUMN AT FRAME 29, IAW EMB 145 SRM 51-40-02.
SSI 53-30-48 CARGO DOOR CUTOUT LOWER DOOR SILL CORRODED.-C/A-REMOVED CORRODED CARGO DOOR CUTOUT LOWER DOOR SILL IAW EMB 145 SRM 51-40-02.INSTALLED SERVICEABLE CARGO DOOR CUTOUT LOWER SILL IAW EMB 145 SRM 51-40-02.
FR 73 CRACKED STGR 16R-17R. C/A REMOVED AND INSTALLED FR 73 SECTION, IAW EMB 145 SRM 51-40-02.
LT OMEGA BEAM SUPPORT COLUMN AT FRAME 25 IS CRACKED. REMOVED AND REPLACED LT OMEGA BEAM SUPPORT COLUMN AT FRAME 25 IAW EMB 145 SRM 51-40-02.
WASTE SERVICE DUMP VALVE HAS CORROSION BETWEEN VALVE AND BUCKET-C/A-RAR LAV WASTE BUCKET IAW EMB 145 SRM 51-40-02
LH AILERON PCA ATTACHMENT FITTING LUGS HAVE EDGE DAMAGE 3EA.-C/A-ACCOMPLISHED EO EM-27MR-112 ON LH AILERON PCA FITTING TORQUE WRENCH 7381
RH AILERON DAMPER FITTING GOUGED.-C/A-ACCOMPLISHED EO# EM-27MR-112 TO RH AILERON DAMPER FITTING
LT NR 1,NR 2, AND NR 3 EMERGENCY LIGHT STRIP EXTRUSIONS BROKEN. C/A COMPLETE: REMOVED AND REPLACED LT NR 1, NR 2, AND NR 3 EMERGENCY LIGHT STRIP EXTRUSIONS, IAW EMB 145 AMM 33-50-12.
LT NR 1 EMERGENCY LIGHT STRIP WIRE HARNESS DISBONDED. C/A COMPLETE: DUPLICATE DISCREPENCY, SEE NRWC NR E808485 FOR SIGN OFF AND DETAILS.
LT NR 5 EMERGENCY LIGHT STRIP EXTRUSION BROKEN. C/A COMPLETE: REMOVED AND REPLACED LT NR 5 EMERGENCY LIGHT STRIP EXTRUSION, IAW EMB 145 AMM 33-50-12.
LT NR 4 EMERGENCY LIGHT STRIP EXTRUSION SCREW HOLE ELONGATED. C/A COMPLETE: REMOVED AND REPLACED LT NR 4 EMERGENCY LIGHT STRIP EXTRUSION, IAW EMB 145 AMM 33-50-12.
PARKING BRAKE STICKY TO SET IT RELEASE.-C/A-LUBED PARKING BRAKE ACTUATOR IAW EMB 145MM 32-44-10.
SUPPLEMENTAL AFT FLIGHT ATTENDEANT FLASHLIGHT INOP.-C/A-DEFERRED PER MEL 25-53. AUTH #030415-C. REMOVED AND REPLACED AFT FA FLASHLIGHT IAW AMM 33-50-16 AND ETN- EM-33-059. OPS CHECK GOOD. MEL ITEM RESTORED
FWD CABIN EMERGENCY FLASHLIGHT BRACKET ASSEMBLY BROKEN.-C/A-REMOVED AND REPLCED FWD CABIN EMERGENCY FLASHLIGHT ASSEMBLY. OPS CHECKED GOOD IAW AMM 33-50-16.
DURING PS-1 CHECK, FOUND LH OVERWING EXTERNAL EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED OVERWING EXTERNAL EMERGENCY LIGHT LAMP IAW AMM 33-50-10. OPERATIONAL CHECK GOOD. NO DEFECTS NOTED AT THIS TIME.
SMOKE REPORTED COMING FROM GPU CONNECTOR UPON DISCONNECTING FROM AIRCRAFT PORT NEEDS INSPECTION-C/A-INSP GPU CONNECTOR NO DEFECT FOUND IAW EMB 145 AMM 20-40-01 & 24-40-01 AC OK FOR SERVICE
R/H EXT UPPER EMERGENCY LIGHT INOP-C/A-ADJUSTED EMERGENCY LIGHT IAW EMB 145 AMM 33-50-00. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED.
RIGHT SIDE OVER WING EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED RIGHT SIDE OVER WING EMERGENCY LIGHT BULB IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD NO FURTHER DEFECTS NOTED.
REMOVED LH EXTERIOR EMERGENCY LIGHT ASSEMBLY AND SPACER PLATE ON FWD BELLY FAIRING TO FOM (REPAIR)-C/A-INSTALLED LH EXTERIOR EMERGENCY LIGHT ASSEMBLY AND SPACER PLATE ON FWD BELLY FAIRING IAW EMB145 AMM 33-50-10. OPC GOOD. SEE NRWC3 696-MQT-04135 FOR COMPLETION OF REPAIR MENTIONED IN TURNOVER.
COCKPIT STEP RED EMERGENCY LIGHT IS BROKEN.-C/A-REPOSITIONED AND INSTALLED MISSING HARDWARE ON THE COCKPIT STEP COURTESY LIGHT IAW AMM33-26-06 OPS CHECK GOOD
EXT OVER WING EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED NR 4 BATTERY CHARGER ASSEMBLY. OPS CHECK FAILED. DEFERRED AFT EXTERNAL EMERGENCY LIGHTS AS PER MEL 33-29 AUTH# 030740D-C. REMOVED AND REPLACED BATTERY CHARGER NR 4 DID NOT FIX. REMOVED AND REPLACED RT EXTERNAL EMERGENCY LIGHT ASSEMBLY, OPS CHECK GOOD IAW 33-50-10 MEL ITEM RESTORED. BATTERY CHARGER ASSY NR 4 P/N 11-0049 S/N 12569 S/N 15038.
DURING PS-1 CHECK FOUND BOTH AFT OVER THE WING EMERGENCY LIGHTS NOT WORKING. C/A-REMOVED AND REPLACED NR 4 EMERGENCY BATTERY PACK AND POWER SUPPLY IAW AMM 33-50-04, OPS CHECK IAW AMM 33-50-00-700-801-A. OPS CHECK GOOD. EMERGENCY LIGHTING BATTERY P/N 2013-1ASMI S/N 798326.
EMERGENCY EXIT SIGN LEFT SIDE INOP (UPPER SIGN). C/A-REMOVED AND REPLACED #3 EMERGENCY LIGHTING BATTERY AND POWER SUPPLY IAW AMM 33-50-04 OPS CHECK GOOD. BATTERY CHARGER ASSY P/N 11-0049 S/N 15185
FOUND RT EMERGENCY OVER WING LIGHT INOP PER PS-2 CHECK. REMOVED AND REPLACED BATTERY CHARGER FOR BATTERY POWER SUPPLY 4 IAW AMM 33-50-04. OPS CHECK GOOD
LT OVER WING EMERGENCY LIGHT INOP. C/A-REMOVED AND REPLACED BULB ON LT OVERWING EMERGENCY LIGHT IAW AMM 33-50-10. OCK GOOD.
RT OVER WING EMERGENCY LIGHT INOP. C/A-REMOVED AND REPLACED BULB ON RT OVERWING EMERGENCY LIGHT IAW AMM 33-50-10. OCK GOOD.
REAR EXTERNAL EMERGENCY LIGHTS INOP. C/A-RAR EXTERNAL EMERGENCY LIGHT IAW AMM 33-50-10. REMOVED AND REPLACED NR 4 BATTERY POWER SUPPLY IAW AMM 33-50-04 AND 33-50-00. OPS CHECKS GOOD.
TRANSFER FROM LOG PG 4294014 ITEM #1 EMERGENCY LIGHTS FLICKERING + GALLEY LIGHTS WOULD NOT OFF IN FLIGHT ACCORDING TO FA-C/A-PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHTS IAW AMM 33-50-00. OPS CHECK GOOD. PERFORMED OPERATIONAL CHECK OF GALLEY LIGHT IAW AMM 33-29-00. OPS CHECK GOOD.
DURING PS-1 CHECK FOUND LH AND RH OVERWING EMERGENCY LIGHTS INOP-C/A-REMOVED LH AND RH O/W SIDE CENTER FAIRING EMERGENCY LIGHT IAW 33-50-10 SUBTASK 020-004-A AND TROUBLE SHOT LIGHTS IAW EMB-145 AMM 20-20-03. FOUND LH O/W EMERGENCY LIGHT TO BE SHORTED. RAR LH O/W EMERGENCY LIGHT AND REINSTALLED RH O/W EMERGENCY LIGHT IAW EMB-145 AMM 33-50-10 SUBTASK 020-004-A AND 420-004-A. OPS CHECK GOOD IAW 33-50-00-700-801.
STALL PROTECTION TEST LIGHT STAYS ILLUMINATED AFTER TEST. NO AURAL WARNING DURING TEST. C/A-FOUND CMC MESSAGE SPC FAIL. REPLACED STALL PROTECTION COMPUTER IAW AMM 27-36-02-000-801-A & 27-36-02-400-801-A. OPERATIONAL TEST IAW WORK CARD 27-700-20 GOOD. NO FURTHER DEFECTS NOTED.
SMOKE COMING OF BAG EXTINGISHER SYSTEM "TRANSFERRED TO NRWC 696-MIA-03681". C/A-REMOVED AND REPLACED BOTH BAGGAGE COMP EXT BOTTLES IAW AMM 26-23-04 OPT FOUND OK REFER NRWC 696-MIA-03681 FOR WORK PERFORMED. FIREEX BOTLE-630 CU.IN P/N 34600073-1 S/N 16935F1 LWR.
FOWARD CABIN FLASHLIGHT HAD WATER INSIDE LED AND MUST BE THUMPED TO GET IT TO WORK. R & R THE FWD FLASHLIGHT ASSY IAW AMM 25-60-00 OPS CHECKED GOOD.
DURING PS-1 INSPECTION, FOUND THE LEFT & RIGHT EXTERNAL OVERWING EMERGENCY LIGHTS INOPERATIVE. REMOVED & REPLACED THE NR 4 EMERGENCY LIGHT POWER SUPPLY & BATTERY, OPS OK.
PITCH MAIN TRIM EICAS AT 36000 FT, RMR6 PROCEDURES FOLLOWED. RESET SYSTEM AND PERFORMED AN OPS CHECK OF PITCH TRIM SYSTEM IAW AMM 27-40-00-700-802-A. OPS CHECKED GOOD. REMOVED HORIZONTAL STABILIZER ACTUATOR IAW AMM 27-40-02-000-801-A. REPLACED THE HORIZONTAL STABILIZER ACTUATOR IAW AMM 27-40-02-400-801-A. OPS CHECKED GOOD IAW AMM 27-40-02.
CRACK IN THE SHEAR TIE AT FRAME 66, BETWEEN STRINGERS 6L AND 7L. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, CPM 51-21-04, 51-21-05, AND 51-21-06.
CRACKED SHEAR TIE AT FRAME 68, BETWEEN STRINGERS 6R AND 7R. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, CPM 51-21-04, 51-21-05, AND 51-21-06
SERVICE DOOR FORWARD TRIM EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE EMEGENCY LIGHT IAW AMM 33-50-09, OPS CHECKED GOOD.
FLOOR EMERGENCY LIGHT SPLICE AT FRAME 58 IS MISSING . REPLACED THE SPLICE IAW SWPM 20-21-00. OPS CHECKED GOOD.
FUSELAGE SKIN UNDER FWD GPS ANTENNA FOUND GOUGED, AFTER ANTENNA REMOVAL. BLENDED THE GOUGES, FOUND TO BE OUT OF LIMITS IAW SRM 53-21-01, AND 53-10-03, TABLE 101. REMOVED DAMAGED MATERIAL, AND PERFORMED HFEC INSPECTION IAW NDTM 51-00-00-916-801-A NO DEFECTS NOTED. FABRICATED, LOCATED, AND INSTALLED A FILLER AND DOUBLER IAW ETD-2018-145-013915, AND EM-53-071.
CORROSION ON INBD SIDE OF THE LT OMEGA BEAM AT CARBON CROSS MEMBER, FRAME 38. REMOVED CORROSION, PERFORMED HFEC INSPECTION, NO DEFECTS NOTED IAW SRM 51-10-03, AND NDTM 51-00-00-916-803-A, FABRICATED, LOCATED, DRILLED AND INSTALLED A REPAIR FILLER AND EXTERNAL ANGLE IAW SRM 53-00-00.
CORROSION ON INBD SIDE OF THE LT OMEGA BEAM AT CARBON CROSSBEAM MEMBER AT FRAME 29. BLENDED CORROSION AND REMOVED DAMAGE IAW SRM 53-22-10, AND 53-00-10. PERFORMED NDT OF CUT OUT AREA IAW NDTM 51-00-00-916-801-A00 NO DEFECTS NOTED. FABRICATED A FILLER AND SHIMS, PERFORMED FPI OF REPAIR PARTS, NO DEFECTS NOTED, INSTALLED THE REPAIR AND APPLIED PROTECTIVE COATINGS IAW SRM 53-00-10, CPM 51-20-04, 51-20-05, AND 51-20-06
TEAR STRAP AT FR73 BETWEEN STR21L AND 21R CHAFED THROUGH. COMPLIED WITH ERS-EM-53MR-2877.
AISLE FLOOR LIGHT STRIPS NR 2 AND 3 INOPERATIVE. REMOVED AND REPLACED THE AC/DC INVERTER IAW AMM 33-50-11. OPS CHECKED GOOD.
EMERGENCY FLOOR LT STRIPS 2 AND 3 INOP. EMERGENCY BATTERIES CHARGED WITH GPU PER AMM 20-40-01-860-801-A. PERFORMED OPC OF EMERGENCY LIGHTING SYSTEM IAW AMM 33-50-00-700-801-A NO FAULTS FOUND.
LAV SMOKE WARNING ON EICAS AND SMOKE ALARM TONE IN GALLEY AT THE GATE. PERFORMED A LAV SMOKE TEST IAW AMM 26-14-00. OPS CHECKED GOOD WITH NO DEFECTS NOTED. NO ODORS OR SIGNS OF SMOKE. SUSPECT HIGH HUMIDITY.
DISCOVERED EMERGENCY AISLE LIGHTS ON ROWS 3-6, DO NOT OPERATE. REMOVED AND REPLACED BATTERY POWER SUPPLY AND CHARGER IAW W/C 33-700-19. OPS CHECKED GOOD.
AT 35,000 FT LOSS OF CA'S AIRSPEED INDICATOR, ALTIMETER, AND VERTICAL SPEED INDICATOR. RED X'S ON ALL SPS ADVANCED ON EICAS. TROUBLESHOT IAW FIM 34-22-00-810-812, AND FIM 34-22-00-810-813. R & R THE NR 1 AIR DATA COMPUTER IAW AMM 34-15-01. OPS CHECKED GOOD. ALSO, SPS ADVANCE MESS RELATED TO ADC FAIL IAW FIM 27-36-00-810-804. OPS CHECKED GOOD
ON GEAR RETRACTION, HAD A LANDING GEAR LEVER DISAGREE WARNING ON THE EICAS. FOLLOWED AOM -1 LIST, CYCLING GEAR WITH THE SAME RESULTS. RETURNED TO DEPARTURE. REMOVED AND REPLACED LGEU IAW AMM TASK 32-32-01. OPS CHECKED GOOD.
NR 1 ENGINE ANTI ICE FAIL MESSAGE DURING PNEUMATIC INFLIGHT TEST. TURNED ICE DETECTION KNOB TO AUTO AND THE NR 1 ANTI ICE VALVE REMAINED OPEN. VALVE CLOSED AFTER SECOND ATTEMPT. SWITCHING ALL TO AUTO. PERFORMED CONTINUITY AND VOLTAGE TEST AND FUNCTIONAL TEST OF PRESSURE TRANSDUCER OF NR 1 ANTI-ICE SYSTEM IAW WM 30-20-50 AND AMM 30-21-00-700-801. NO DEFECTS NOTED. REMOVED AND REPLACED THE NR 1 ANTI ICE VALVE IAW AMM 30-21-01. OPS TESTED GOOD.
WHILE SITTING AT GATE ON APU PWR STRONG ELEC SMELL FROM CA SIDE THEN CA PFD WENT OFF. FEW MINUTES LATER PFD CAME BACK ON STRONG ODOR. SHUT OFF AC POWER TO AIRCRAFT. SWAPPED FO'S MFD AND CA PFD BACK TO ORIGINAL LOCATIONS. REMOVED AND REPLACED CA PFD IAW AMM 34-22-01. OPC GOOD. MEL RESTORED
MAIN PAX DOOR EMER EXIT LIGHT INOPERATIVE. R & R PAX DOOR HINGE EMER LIGHT SHROUD IAW AMM 25-23-04 STEPS 3 I 1 F-I. OPERATIONS CHECKED GOOD IAW AMM 33-50-00.
DURING DESCENT IN ICING CONDITIONS, WING ANTI-ICE FAIL CAUTION MSG & ICE CONDITIONS, ANTI-ICE INOPERATIVE. WARNING MSG PRESENTED ON EICAS. WING ANTI-ICE SELECTION BUTTON SHOWED OPEN INSCRIPTION. R & R PITOT CURRENT SENSOR IAW AMM 30-31-00. OPERATIONS CHECKED GOOD.
AT 28000 RUDDER 1 & 2 BECAME INOPERATIVE ON EICAS MSG ON & OFF, 25000 MSG REMAINED. TRANSFERRED TO NRWC 696-MIA-02571. REMOVED & INSTALLED BOTH RUDDER PRESS SWITCHES & OPERATIONS CHECKED. ALL CHECKS PASSED IAW 27-23-04.
AFT CABIN EMER FLASHLIGHT INOPERATIVE. R & R AFT CABIN FLASHLIGHT IAW AMM 25-60-00. OPERATIONS CHECKED GOOD AT THIS TIME. FLASHLIGHT BATTERY PN P4-01-1003-001.
AFT FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW EEL. OPERATIONS CHECKED GOOD.
LEFT ENG FWD LOWER YOKE CRACKED BEHIND ENG MOUNT. R & R LT ENG LOWER FWD YOKE IAW EO EM-54MR-386.
RIGHT OMEGA BEAM INBD SUPPORT IS CRACKED ON AFT END & NEAR FWD END. INSTALLED NEW SERVICEABLE RT OMEGA BEAM INBD SUPPORT, TWO PIECES, OVER WINGBOX AREA IAW SRM 51040-02 & SRM 53-23-02.
FUSELAGE SKIN CRACK ON FRAME 78, BETWEEN STRINGERS 6R - 7R. FABRICATED & INSTALLED DOUBLER AT FRAME 78, BETWEEN STRINGER 6R & 7R IAW SRM 53-32-01.
ENGINE FWD LOWER YOKE REPAIR & REPLACEMENT. INSTALL OVERSIZE BUSHINGS, INSTALL GUSSET PLATE IAW EO-EM-54MR-386.
FRAME 65 IS CORRODED NEAR CARGO DOOR LOWER STOP. REMOVED & INSTALLED NEW HALF FRAME & SHEAR CLIP AT FRAME 65 NEAR CARGO DOOR LOWER STOP IAW SRM 53-31-04 PG 204.
LEFT SPOILER CTR HINGE FITTING ON WING IS CORRODED. R & R LT SPOILER CTR HINGE FITTING ON WING IAW AMM 57-51-02.
MAIN PAX DOOR HAS A DENT, LOCATED 16" AFT OF DOOR FWD EDGE & 13.5" UP FROM LOWER EDGE. DENT IS 1" L X 1.75" W X .012" D. ACCOMPLISHED PERMANENT REPAIR TO MAIN PAX DOOR DENT IAW ERS-EM-5200-468. DENT ENTERED INTO ADL 6960035.
AFTER TAKEOFF LOUD BANGING NOISE HEARD IN ACFT RT MLG CYCLED FROM UP TO AMBER. GEAR EXTENDED NORMALLY. R & R RT UPLOCK BOX UPPER PROX SWITCH IAW AMM 32-61-01. PERFORMED GEAR EXTENSION & RETRACTION OPERATIONAL CHECK IAW AMM 32-30-00. OPERATIONS CHECKED SATISFACTORY.
CEILING EMER LIGHT AT EMER EXIT ON FWD SIDE INOPERATIVE. R & R BATTERY & POWER UNIT NR 4 IAW AMM 33-50-04, DID NOT FIX. REFER TO NRWC 696-DFW-02268. EMER LIGHTING BATTERY PN 2013-1ASMI SN 74445. R & R EMER LIGHT INVERTER AT NR 6 POSITION IAW AMM 33-50-11. OPERATIONS CHECKED GOOD. INVERTER PN 7824-1.
RIGHT WING AFT EMER LIGHT INOPERATIVE. R & R RT WING AFT EMER LIGHT BULB IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.
EMERGENCY FLOOR LIGHT STRIPS 4 & 5 & LT & RT SERVICE DOOR EXIT SIGNS INOPERATIVE. R & R EMER LIGHT AC DC INVERTOR NR 5. FLOOR STRIPS 4 & 5 & LT & RT SERVICE DOOR EXIT SIGNS. OPERATIONS CHECKED GOOD IAW AMM 33-50-11.
DURING PS 1 INSPECTION FOUND MAIN DOOR EXIT SIGN INOPERATIVE. R & R NR 1 BATTERY & NR 1 CHARGER IAW AMM 33-50-04. OPERATIONS CHECKED GOOD. BATTERY CHARGER ASSEMBLY PN 11-0049 SN 14895.
DURING PS 1 INSPECTION FOUND EMER LIGHT AT MAIN ENTRANCE DOOR INOPERATIVE. R & R NR 1 INVERTER IAW AMM 33-50-11. OPERATIONS CHECKED GOOD.
RMU NR 1 FROZE THEN WENT BRIGHT WHITE. IN CRUISE RMU NR 2 GOES TO COMPLETELY ALL DASHES, KICKED OFF NR 1 TRANSPONDER. REMOVED RMU NR 1 CLEANED CONNECTOR & REINSTALLED IAW AMM 23-81-01. OPERATIONS CHECKED GOOD AT THIS TIME IAW AMM 23-81-00-700-801-A. NO DEFECTS NOTED. REMOVED RMU NR 2, CLEANED CONNECTOR & REINSTALLED IAW AMM EMB 23-81-01. OPERATIONS CHECKED GOOD AT THIS TIME IAW AMM 23-81-00-700-801-A. NO DEFECTS NOTED.
AFT CABIN FLASHLIGHT INOPERATIVE. R & R AFT CABIN FLASHLIGHT IAW AMM 33-50-16-000-801-A & 33-50-16-400-801-A. OPERATIONS CHECKED GOOD.
WHILE AIRBORNE APU GEN OFF BUS EICAS MSG OCCURRED. IAW MEL 24-5 FLIGHT REQUIRED AN APU GEN TO BE OPERATOR TO CONTINUOUS FLIGHT, RETURNED. APU GEN FUNCTION DEFERRED IAW MEL 24-8. R & R NR 4 ENG GEN IAW WC 24-800-00. OPERATIONS CHECKED GOOD. NO LEAKS NOTED. MEL RESTORED.
EMERGENCY LIGHTING STRIPS FROM 3A TO 7A INOPERATIVE. SECURED CONNECTOR FOR EMER LIGHTS IAW AMM 33-50-08.
OVERHEAD CEILING FWD EMER LIGHT BY EMER EXIT INOPERATIVE. REMOVED ELEC CONNECTIONS, CLEANED & REATTACHED CONNECTORS. OPERATIONS CHECKED GOOD IAW AMM 33-50-15.
LT & RT SIDE CTR FAIRING EMER LIGHTS ARE INOPERATIVE. R & R NR 4 BATTERY & CHARGER ASSEMBLY IAW AMM 33-50-04. OPERATIONS CHECKED GOOD AT THIS TIME. BATTERY CHARGER ASSEMBLY PN 11-0049 SN 15916.
LEFT EXTERNAL OVERWING EMERGENCY LAMP INOPERATIVE. R & R NR 4 BATTERY POWER SUPPLY & CHARGER IAW AE WC 33-700-17 & 33-700-19, OPERATIONS CHECKED GOOD.
AFT LT & RT OVERWING EMERGENCY LIGHTS INOPERATIVE IAW PS-1 INSPECTION. R & R LT & RT OVERWING EMERGENCY LIGHTING BULBS IAW AMM 33-50-07, NO FIX. R & R NR 4 EMERGENCY BATTERY & POWER PACK IN OVERHEAD LT PAX COMPARTMENT. CLEANED LIGHT BULB CONTACTS, OPERATIONS CHECKED GOOD, NO FURTHER DEFECTS.
FOUND LT & RT EXTERIOR OVERWING EMERGENCY LIGHT NOT ON. R & R NR 4 EMERGENCY LIGHT BATTERY CHARGER & BATTERY PACK IAW AMM 33-50-04. R & R RT EXTERIOR OVERWING EMERGENCY LIGHT ASSEMBLY IAW AMM 33-50-10, OPERATIONS CHECKED GOOD.
CAPTAIN'S FLASHLIGHT BRACKET CRACKED. R & R CAPTAIN'S FLASHLIGHT IAW AMM 33-50-16, OPERATIONS CHECKED GOOD.
RT EMERGENCY EXIT LOWER RECESS CUP DAMAGED. INSTALLED NEW RT EMERGENCY EXIT LOWER RECESS CUP IAW SUB TASK 25-23-03-420-001 STEP I 1 D PART TASK.
RT OVERWING EMERGENCY EXIT HAS SURFACE SCRATCHES ALONG UPPER OUTER SURFACE & AFT EDGE OUTER SURFACE. INNER LOWER OBSCURED HANDLE HAS LOWER SECTION BROKEN. REPAIRED OUTER SURFACE SCRATCHES OF RT EMERGENCY EXIT IAW CPM 51-21-07. NO FURTHER DEFECTS NOTED IAW NRWC 696-DFW-01736 FOR DAMAGED OBSCURED HANDLE, RECESS CUP.
FLIGHT CREW DECLARED EMERGENCY LANDING FOR ELEC SMELL WITH SMOKE IN COCKPIT. FOUND COCKPIT RECIRCULATION FAN BURNED. R & R NR 1 RECIRCULATION FAN IAW AMM 21-24-01 & OPERATIONS CHECKED GOOD. PERFORMED ETN-EM-72-034 & NO ELEC SMELL OR SMOKE WAS FOUND.
MAIN CABIN AFT EMERGENCY FLASHLIGHT MISSING. DEFERRED AFT EMERGENCY LIGHT FLASHLIGHT IAW MEL 25-53 AUTH 030253-C. REINSTALLED AFT FLASHLIGHT & OPERATIONS CHECKED GOOD IAW AMM 33-51-01. MEL ITEM IS RESTORED.
ON SHORT FINAL APPROXIMATELY 30 SEC AFTER WE PUT THE GEAR DOWN WE STARTED SMELLING WHAT WE THOUGHT WAS ELEC SMOKE, BUT WE WERE NOT SURE ON THE LANDING ROLL OUT. THE FLIGHT ATTENDANT CALLED & SAID SHE SMELLED IT. NO SMELL WAS NOTED IN THE AFT CABIN AT ANY POINT. THE SMELL SUBSIDED SUBSTANTIALLY ON THE LANDING ROLL OUT. PERFORMED FIM TASKS IAW 21-20-00-810-803A. FOUND NO DEFECTS ALL LIGHTS WORK & ALL AVIONICS OPERATE NORMAL. PERFORMED ETN EM-72-034, FOUND NO DEFECTS & NOTICED NO SMELL IN COCKPIT OR CABIN.
DURING MBV INSPECTION FOUND FRAME SUPPORT CLIP AT FRAME 72, STRINGER 16L IS CRACKED. REMOVED AND REPLACED CRACKED FRAME SUPPORT CLIP AT FRAME 72, STRINGER 16L IAW SRM 51-40-02. RESTORED SURFACE FINISH TO AFFECTED AREA OF EXTERNAL FUSELAGE IAW CPM 51-21-07 AND ETN-EM-51-091.
DURING MBV INSPECTION FOUND FRAME SUPPORT CLIP AT FRAME 71, STRINGER 16L IS CRACKED. REMOVED AND REPLACED CRACKED FRAME SUPPORT CLIP AT FRAME 71, STRINGER 16L IAW SRM 51-40-02. RESTORED SURFACE FINISH TO AFFECTED AREA OF EXTERNAL FUSELAGE IAW CPM 51-21-07 AND ETN-EM-51-091.
DURING MBV INSPECTION FOUND APU FIRE WALL IS CRACKED AT THE UPPER RT ATTACHMENT POINT AS VIEWED FROM THE AFT SIDE. REPAIRED AS PER PART C OF EO EM-53AD-1883.
LEFT NR 7 EMERGENCY PROXIMITY LIGHT HAS A BROKEN WIRE. R & R LT NR 7 EMERGENCY PROXIMITY LIGHT IAW AMM 33-50-12.
LEFT NR 1 & LEFT NR 2 EMERGENCY LIGHT STRIPS ARE CRACKED. R & R LT NR 1 & LT NR 2 EMERGENCY LIGHT STRIPS IAW AMM 33-50-12.
DURING CLIMB ABOUT FL260 NI & ITT SPUN DOWN THEN INTERMITTENTLY WIND UP & DOWN. N1 APPEARED NORMAL AFTER IGNITERS ON BUT ITT STAYED LOW 300 ENG 1. PERFORMED ENG RUNS IAW RR MM 72-00-00. COULD NOT DUPLICATE THIS PROBLEM AT THIS TIME.
BOTH RT & LT EXTERIOR OVERWING EMERGENCY LIGHTS INOPERATIVE. R & R NR 4 EMERGENCY BATTERY & CHARGER ASSEMBLY IAW AMM 33050--04. OPERATIONS CHECKED GOOD.
BOTH OVERWING EMERGENCY LIGHTS INOPERATIVE. R & R BOTH OVERWING EMERGENCY LIGHTS BATTERY CHARGER IAW AMM 33-50-04, OPERATIONS CHECKED GOOD.
DURING MAINTENANCE INSPECTION ON FLIGHT 3005 FOUND LT & RT WING UPPER EMERGENCY LIGHTS INOPERATIVE. THE ACFT WAS REMOVED FROM SERVICE. R & R NR 4 BATTERY CHARGER IAW EMB 145 AMM 33-50-04. OPERATIONS CHECKED GOOD MEL 33-50-04 AUTH 120368D-C IS RESTORED. THE ACFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE INSPECTION ON FLIGHT 3005 FOUND FLIGHT ATTENDANT`S EMERGENCY FLASHLIGHT MISSING. THE ACFT WAS REMOVED FROM SERVICE. R & R FLIGHT ATTENDANT`S EMERGENCY FLASHLIGHT IAW EMB 145 AMM 25-51-00 & OPERATIONAL CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.
RIGHT EXTERIOR EMERGENCY OVERWING EMERGENCY LIGHT HAS A BROKEN NUTPLATE. R & R RT OVERWING EXTERIOR EMERGENCY LIGHT ASSEMBLY IAW AMM 33-50-10. CANNOT PERFORM OPERATIONS CHECK LIGHT IS MEL IAW AML.
NR 1 EMERGENCY LIGHT BATTERY INOPERATIVE. R & R BATTERY IAW MAINTENANCE W/C 33-700-19, OPS CHECKED GOOD.
EMERGENCY LIGHT ABOVE SERVICE DOOR INOPERATIVE. R & R NR 2 EMERGENCY LIGHT INVERTER IAW AMM 33-50-11. OPS CHECKED GOOD IAW WC 33-700-17.
CREW REPORTED THAT ON FINAL APPROACH, SELECTED FLAP 9 DEGREES. RECEIVED A FLAP FAIL MESSAGE ON EICAS AND THE FLAPS REMAINED AT 0 DEGREES. RAN THROUGH FLAP FAIL CHECKLIST AND DECLARED AN EMERGENCY . LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. ACTIVATED FECU IAW AMM 27-53-00. OPS CHECKED IAW AMM 27-53-00-700-801-A. R & R THE FLAP ELECTRONIC CONTROL UNIT IAW AMM 27-53-02. OPS CHECK GOOD. NO DEFECTS NOTED. PERFORMED FLAP FAIL/FLAP LOW SPEED OPS CHECK IAW WC 27-700-28. OPS CHECK GOOD. NO DEFECTS NOTED. MEL RESTORED. THE ACFT WAS RETURNED TO SERVICE.
DURING B INSPECTION FOUND THE COPILOTS FLASHLIGHT INTERMITTENTLY CHARGING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICERâS FLASHLIGHT CRADDLE ASSEMBLY AND REMOVED AND REPLACED THE FLASHLIGHT BATTERY UNIT IAW EMB145 AMM 33-50-16-000-801A AND 33-50-16-400-801A AND 33-51-01-700-802A. PART # P4-01-1003-001. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING B INSPECTION FOUND THE CAPTAINâS FLASHLIGHT WILL NOT TURN ON. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAINâS EMERGENCY FLASHLIGHT IAW EMB AMM 33-50-16-00-801-A AND 33-50-16-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY LIGHT AT FORWARD CEILING PANEL INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT AT FORWARD CEILING PANEL IAW AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 3307 THE CREW REPORTED THAT ON FINAL APPROACH THEY NOTICED STRONG ELECTRICAL FUMES IN THE COCKPIT. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND ELECTRICAL SMELL COMING FROM AUTOFLIGHT GUIDANCE CONTROLLER. REMOVED AND REPLACED THE AUTOFLIGHT GUIDANCE CONTROLLER IAW AMM 22-11-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
LEFT AND RIGHT OVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED NR 4 EMERGENCY BATTERY PACK AND CHARGER ASSY.
ON FLIGHT 4009 THE CREW REPORTED THEY WERE CLEARED FOR AN ILS 27L INTO ORD AND RECEIVED A FLAP FAIL MESSAGE WHEN TRYING TO DEPLOY FLAPS 9, FLAPS STAYED AT 0. THE CREW PERFROMED THE AOM CHECKLIST AND ASKED FOR VECTORS OFF THE APPROACH AND DECLARED AN EMERGENCY. THE CREW RETURNED TO PIT AND LANDED WITHOUT INCIDENT. THE FLAPS NEVER DEPLOYED PAST 0. THE AIRCRAFT WAS REMOVED FROM SERVICE. TROUBLESHOT AND FOUND LEFT NR 3 FSA LEAKING. REMOVED AND REPLACED THE LEFT NR 3 ROOT FLAP ACTUATOR IAW EMB 145 AMM 27-51-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 4350 THE CREW REPORTED THAT ON APPORACH THE FLAPS FAILED IN THE ZERO POSITION. THE CREW COULD NOT OBTAIN ANY FLAPS ON LANDING. THE CREW DECLARED AN EMERGENCY AND RAN THE APPROPRIATE CHECKLIST. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. TROUBLESHOT FLAP SYSTEM IAW EMB 145 AMM 27-51-00. REMOVED AND REPLACED THE FLAP POWER DRIVE UNIT IAW EMB 145 AMM 27-53-04. THE OPERATIONAL CHECK WAS GOOD, NO FURTHER DISCREPANCIES FOUND AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 4018 THE CREW REPORTED THAT THE FLAP FAILED WHEN SELECTING FLAP 9 ON APPROACH INTO ORD. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED FLAP SCREW JACK ACTUATOR GEAR - LUBRICATION IAW FIN REF 27-51-00. FOLLOWING FIM REF 27-51-00. FILLED ALL ACTUATORS. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING B INSPECTION FOUND THE CAPTAIN'S FLASHLIGHT CRADLE BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAINâS FLASHLIGHT CRADLE IAW EMB 145 AMM 33-50-16-000-801-A AND 33-50-16-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING COURTESY CHECK, FOUND THE FORWARD FLIGHT ATTENDANTâS FLASH LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLASH LIGHT AS REQUIRED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE INSPECTION FOUND FRAME 65 HAS OUT OF LIMITS WITH CORROSION AT LOWER STIKER PLATE NUTPLATES. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION, FABRICATED AND INSTALLED DOUBLER PER ETD 2012-145-006915. AIRCRAFT RETURNED TO SERVICE.
DURING SCHEDULED MAINTENANCE FOUND THE RIGHT OUTBOARD OMEGA BEAM SUPPORT CRACKED AT FR47 AS MARKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED OUTBOARD OMEGA BEAM SUPPORT REF 51-40-02. LOCATED AND DRILLED NEW OUTBOARD OMEGA SUPPORT AT FRAME 47. INSTALLED NEW OUTBOARD OMEGA BEAM SUPPORT RIGHT SIDE FR47 REF SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING SCHEDULED MAINTENANCE FOUND THE BAGGAGE DOOR CUTOUT FORWARD LOWER CORNER CORRODED AT NUT PLATE FOR TRIM. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED RIB DUE TO OUT OF LIMIT CORROSION. LOCATED & DRILLED NEW RIB IAW SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING SCHEDULED MAINTENANCE FOUND THE BAGGAGE DOOR SILL HAS CORROSION AT NUT PLATE (4 EACH). THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED CARGO DOOR SILL, LOCATED & DRILLED NEW SILL BLENDED CORROSION ON EXISTING SILL REF SRM 51-10-03, 100 PERCENT MATERIAL LOSS, OUT OF LIMITS. INSTALLED NEW SILL PER SRM 51-40-02. PAINT: RE-STORED FINISH IAW SRM 51-21-06. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING SCHEDULED MAINTENANCE FOUND THE EMERGENCY LIGHT STRIP WIRES PULLED/BROKEN AT FERRULE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RESOLDERED LEFT NR 1 EMERGENCY LIGHT WIRES REFERENCING EMB 145 SWPM 20-30-00. THE AIRCRAFT WAS RETURNED TO SERVICE.
CARGO DOOR CUT OUT FWD LOWER CORNER CORROSION AT LOWER STRIKER PLATE AND RIVETS. REMOVED CORROSION ON FWD STRIKER PLATE REF SRM 51-20-00. REMOVED STRIKER PLATE FOM.
DURING MAINTENANCE INSPECTION, FOUND THE RIGHT FLOOR SILL CORRODED BETWEEN FRAMES 39 AND 44. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED CORROSION REF SRM 51-10-03 NOMINAL .050 INCH REMAINING MATERIAL .032" OUT OF LIMITS OF SRM 53-23-10 FIGURE 101. REMOVED CORRODED SILL REF SRM 51-40-02, TRANSFERRED HOLES TO NEW SILL REF SRM 51-20-03 AND INSTALLED NEW SILL USING REF SRM 51-40-02. REMOVED FLOOR SILL FROM FR 36-41 REF SRM 51-410-02 LOCATED AND DRILLED NEW SILL USING REF SRM 51-20-03. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE INSPECTION, FOUND A CRACK ON RIGHT BELLY PANEL SUPPORT FORWARD OF RIGHT INBOARD FLAP TQ BOX. AIRCRAFT REMOVED FROM SERVICE. REMOVED CRACKED BELLY PANEL SUPPORT RIGHT USING REF SUM 51-40-00. FABRICATED NEW ANGLE IAW SRM 51-40-02. TREATED AND PRIMED IAW CPM 51-23-04 AND CPM 51-28-05. INSTALLED NEW BELLY PANEL SUPPORT IAW SRM 51-40-02 AND TOP COATED IAW CPM 51-23-06. AIRCRAFT RETURNED TO SERVICE.
DURING MAINTENANCE INSPECTION, FOUND THE LEFT OUTBOARD OMEGA BEAM SUPPORT CRACKED AT FR47. AIRCRAFT REMOVED FROM SERVICE. REMOVED LEFT OUTBOARD OMEGA BEAM SUPPORT, LOCATED AND DRILLED NEW PART AND INSTALLED REF SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.
CORROSION ON FR68 "L" SHAPE AT THRESHOLD. REPAIRED FR 68 "L" SHAPE IAW EM-53MR-1129.
DURING B-INSPECTION FOUND THE RIGHT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVERWING EMERGENCY LIGHT IAW AMM TASKS 33-50-07-000-801-A AND 33-50-07-400-801-A. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE INSPECTION FOUND THE FUSELAGE AFT OVERWING EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT CHARGER AND BATTERY IAW EMB WC 33-700-19. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 3933 THE CREW REPORTED THE REAR FLASHLIGHT HOLDER CLIP WAS BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT FLASHLIGHT HOLDER IAW EMB 145 AMM 33-50-16. THE OPERATIONAL TEST WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 2705 THE CREW REPORTED THAT DURING THE CLIMB AFTER TAKEOFF, RECEIVED A LAVATORY SMOKE WARNING. THE FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN. THE PACKS BLEEDS AND RECIRCULATION FANS WERE TURNED OFF AND THE SMOKE CLEARED. THE CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO DFW. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT ENGINE IAW W/C 71-000-00. THE OPERATIONAL CHECK WAS GOOD. NO LEAKS NOTED. NO SMOKE IN CABIN NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.
FOR FLIGHT 3637 IT WAS DISCOVERED THAT THE EMERGENCY LIGHTS AT ROW 8-12 AND THE OVERWING EMERGENCY LIGHTS WERE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BATTERY POWER SUPPLY AND BATTERY HOLDER ASSEMBLY AT LOCATION NR 3. THE OPERATIONAL CHECK WAS NORMAL IAW AMM 33-50-04 AND WORK CARD 33-700-17. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE BASE VISIT FOUND THE EMERGENCY FLOOR PROXIMITY LIGHT NUMBER 4 HAS A BROKEN WIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED NEW SOCKET ON FLOOR PROXIMITY LIGHT NR 4 IAW EMB SWP 20-50-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 3444 THE CREW REPORTED AN ODOR IN THE COCKPIT DURING TAKEOFF WITH THE PACKS ON. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NUMBER 1 ENGINE. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 4287 DURING CRUISE THE FLIGHT ATTENDANT REPORTED A BURNING ODOR FROM THE CD PLAYER. THE CREW PULLED CIRCUIT BREAKER J15AND THE ODOR WAS GONE. THE AIRCRAFT CONTINUED TO CMH AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CD PLAYER IAW EMB AMM 23-32-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 3505, CREW REPORTED THEY DECLARED AN EMERGENCY DUE TO ELECTRICAL ODOR IN THE COCKPIT DURING CRUISE. ODOR DISSIPATED DURING DECENT ACFT REMOVED FROM SERVICE. REMOVED AND REPLACED CAPTS CHART HOLDER DUE TO LIGHT STAYS ON WHEN CLOSED AND MELTED AREA AROUND LIGHT BULB. IAW MM 25-12-11 CHART HOLDER OPS CHECK GOOD. NO BURNING SMELLS. ACFT RETURNED TO SERVICE.
DURING MBV INSPECTION, FOUND CARGO DOOR SILL UPPER AND LOWER SURFACES CORRODED. MAINT REPLACED CARGO DOOR SILL IAW SRM 51-40-02. ACFT WAS RETURNED TO SERVICE. (K)
ON FLIGHT 3799, CREW REPORTED SMOKE IN CABIN AND COCKPIT WHEN POWER WAS APPLIED FOR TAKEOFF. ABORTED TAKEOFF AND EMERGENCY WAS DECLARED. AIRCRAFT RETURNED TO GATE UNEVENTFULLY. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1 ENGINE ASSEMBLY IAW WORK CARD 71-000-00. REMOVED AND REPLACED THE NR 4 CARBON SEAL. UPON DISASSEMBLY THE NR 4 CARBON SEAL WAS NOTED WITH SEVERAL INDICATIONS IN THE CARBON SEALS. THE OUTER CARBON SEAL HOUSING WAS ALSO NOTED WITH OIL STAINING AND COKING DUE TO OIL LEAKING PAST THE CARBON SEAL SEGMENTS. OPERATIONAL CHECKS GOOD AT THIS TIME. AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 3731, CREW REPORTED UPON REACHING TAKEOFF SPEED NOTED SMOKE SMELL IN THE COCKPIT. CREW ABORTED TAKEOFF AND RETURNED TO GATE.
IN CLOUDS COMM 1 AND 2 BECOMES UNREADABLE AND UNLINK GOES NO COMM CREW ELECTED TO RETURN TO MQT. FOUND COMM 3 ANTENNA UNBOUNDED REBOUNDED COMM 3 ANTENNA. AIRCRAFT RETURNED TO SERVICE.
LAVATORY SMOKE WARNING AFTER TAKEOFF. REMOVED AND REPLACED NUMBER TWO ENGINE IAW EMB AMM 72-00-00. PERFORMED OPERATIONAL CHECKS WITH NO DEFECTS, RETURNED AIRCRAFT TO SERVICE.
AIRCRAFT RETURNED TO FIELD FOR SMOKE SMELL IN COCKPIT COMING FROM CAPTAINS YOKE AREA. RAI CAPTAIN YOKE CHART HOLDER, IAW EMB 145 AMM 25-12-11, OPS CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. (M)