N656AE
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
BLD VLV FAIL MSG DISPLAYED ON T/O ROLL. NO RELEVANT CMC MESSAGES ARE PRESENT. VERIFIED E2 WAS AT FAULT C/W MX PROCEDURE. FACT 18JUN26 03:29 PHL R+R BLEED VLV #2 IAW AMM 36-11-05 REQUIRES OPS+LEAK CHECK-SS 37112 18JUN26- INSTALLED BLEED VLV 2 IRW AMM 36-11-05. PERFORMED OPS CHECK IRW 36-00-00. OPS CHECK GOOD LEAK CHECK GOOD. NO DEFECTS NOTED.
1ST ROW EMERGENCY LIGHT STRIP AND SERVICE DOOR EXIT SIGN INOP FACT 22JAN26 07:25 ROA R&R #200 INVERTER PER AMM 33-50-11 PN ON 7824-1 PN OFF 7824-1
FWD EMERGENCY LIGHT STRIP INOP. RAR STRIP IAW AMM 33-50-12. OPS CHECK GOOD.
EMERGENCY LIGHT 261BF INOPERATIVE. R & R EMERGENCY LIGHT 261BF IAW AMM 33-50-08. ACFT OK FOR SERVICE.
BAGGAGE DOOR OPEN MESSAGE DURING FLIGHT. BAGGAGE DOOR WARNING / POSITION WARNING
ROWS 8/9 AND 10/11 EMERGENCY LIGHT FLOOR PROXIMITY STRIPS INOPERATIVE. R&R #400 FLOOR PROXIMITY LIGHT IRT AMM 33-50-12 R&R#5 EMERGENCY LIGHT AC/DC INVERTER IRT AMM 33-50-11 PN ON 1013194 FLOOR PROX LIGHT PN OFF 6636-7 FLOOR PROX LIGHT PN ON 1330312 AC/DC INVERTER PN ON 1824-1 AC/DC INVERTER
LDG AIR GRND FAIL WITH E1-E2 REV DISAGREE MESSAGE IN FLIGHT MESSAGE DISAPEARED WHEN GEAR DOWN AND LOCKED. SERVICED NLG SHOCK STRUT IAW AMM 32-20-01. PERFORMED AIR/GROUND SYSTEM SIMULATION ADJUSTMENT TEST IAW 32-63-00 & SWUNG GEARS MULTIPLE TIMES. NO DEFECTS NOTED. A/C OK FOR SERVICE AT THIS TIME
FUMES NOTICED BY MAIN CABIN DOOR. FACT 29MAR25 00:41 CLT INSPECTED AND FOUND SIDEWALL LIGHT BALLAST AT 1A TO HAVE A BURNT ODOR. R+R BALLAST IAW AMM 33-21-03. OPS CHECK GOOD. NO MORE BURNING ODOR SMELT
SLIGHT SMELL OF FUMES IN FLT DECK AND CABIN AROUND 26000FT. SMELL OCCURRED WHEN F/A WAS USING TEMP CONTROL. FACT 19SEP24 07:24 CLT PERFORED FIM TASK# 21-20-00-810-801-A. BLOCKS 1-11. NO DEFECTS NOTED. PACKS 1-2 RAN FOR EXTENDED TIME WITH NO FUMES DETECTED. OK FOR SERVICE.
00179 UPON REMOVAL OF FLOOR BEAM CAP @ FRM 59 - 61 FOUND FLOOR BEAM TO HAVE EXCESSIVE CORROSION @ FRM 60 + 10" Y= + 479.0 AND REQUIRES REPAIR. COMPLETED ALL STEPS OF EMB ETD2024-145-017954 REV: / DATED 07/01/2024. REPAIR MATERIAL: 2024-T3 .08
00166 SHEAR CLIP ON FRAME 65 BETWEEN STR15L-17L REQ REPLACED/REPAIR.
00131 RH FLOOR BEAM CAP AT Y +479 AT FR20 IS CORRODED. REMOVED AND INSTALLED NEW SERVICEABLE FLOOR BEAM CAP P/N 145-22461-011 IAW EMB-145LR SRM 51-40-02-PR
00135 CORROSION FOUND ON +479.0 FLOOR BEAM CAP BETWEEN FRM 59-61. REMOVED AND INSTALLED NEW SERVICEABLE FLOOR BEAM GUSSET PN: 145-26437-001 IAW EMB-145 SRM 51-20-03-PR AND 51-40-02-PR
00133 FLOOR BEAM CAP AT FR22 AND Y +479 IS CORRODED. : REMOVED AND REPLACED DAMAGED FLOOR BEAM CAP (DOUBLER P/N 145-22461-011) IAW EMB-145LR SRM 51-40-02-PR.
00073 MULTIPLE SPOTS OF CORROSION FOUND ON BOTTOM AREA OF BAGGAGE DOOR SURROUND STRUCTURE. REMOVED AND INSTALLED BEAM ASSY PN# 145-25480-603 (CARGO DOOR SILL) @ AFT CARGO DOOR LOWER SILL IAW EMB145-LR SRM 51-40-02-PR
PITOT 2 INOP CAUTION MESSAGE DISPLAYED. FACT 20MAY24 14:22 CLT R+R # 2 PITOT SENSOR IAW AMM 34-13-01. PERFORMED PITOT/STATIC SYS 2 LEAKAGE TEST IAW AMM 34-13-00-790-803A/500 PERFORMED OPS CK IAW AMM 30-31-00-700-803A/500
IN CRUISE STRONG ELECTRICAL BURNING SMELL IN FLIGHT DECK. FACT 26JAN24 01:13 TRI RAN PACK SYSTEMS 1 AND 2 USING APU AND ENGINE BLDS, INSPECTED AND OPERATED FLIGHT DECK EQUIPMENT WITH NO SMELLS NOTED. INSPECTED PACKS 1 AND 2 AND UNDERFLOOR DUCTS FOR OBVIOUS DEFECTS, SUSPECT DETERIORATED INSULATION ON PACK 1 PIPE AS CAUSE FOR SMELL AND REMOVED LOOSE INSULATION. NO OTHER OBVIOUS DEFECTS NOTED OK FOR SERVICE.
DURING TAKE OFF WENT OFF. REVERSIONARY SWITCHED. EICAS SCREEN SHOWED PFD AND WOULD NOT RETURN. AFTER TOUCHDOWN EICAS SCREEN BLANKED OUT. R&R EICAS IAW AMM 34-22-01 AND R&R EICAS BEZEL IAW MM 31-41-02. PERFOREMD OPS CHECK IAW AMM 34-22-00. OPS CHECK GOOD. A/C OK FOR SERVICE
EXCESSIVE NOSE WHEEL SHIMMY AFTER WHICH EICAS SCREEN WENT BLANK UNTIL SPEED WAS REDUCED. R+R'D NOSE WHEEL ASSYS IAW AMM 32-49-05. GREASED TORQUE LINGS AND TAXIED A/C 20 KNOTS, NO EXCESSIVE SHIMMY NOTED. A/C OKAY FOR SERVICE.
3FLOOR STRIP EMERGENCY LIGHTS FROM LAV DOOR TO SEAT #12 ARE INOP. R & R INVERTER # 6 IAW AMM 33-50-11 OP TEST GOOD
ENGINE 2 HUNG START, AFTER START WAS ABORTED FUMES WERE NOTED IN CABIN AND FLIGHT DECK. INSPECTED #2 ENGINE FOR POSSIBLE FUEL LEAK. NONE FOUND. PERFORMED #2 ENGINE START FROM APU BLEEDS, PACKS OFF, AND #1 ENGINE BLEEDS, WITH PACKS OFF. BOTH TIMES ENGINE STARTS NORMALLY IAW RUN UP MANUAL. BOTH ENGINE 2 STARTS FROM DIFFERENT FADECS. RAN BOTH ENGINE APU AND PACKS, NO FUME SMELL OK FOR SERVICE
HUNG START OF #2 ENG FOLLOWED BY EXHAUST FUMES. OIL NOTED DRIPPING FROM #2 LOWER COWLING. RAN E2 OFF FADEC A WITH NO DEFECTS NOTED. RAN E2 OFF FADEC B WITH HUNG START MULTIPLE TIMES. R/R FADEC 2B IAW AMM 73-22-01NO FIX. NO SIGN OF OIL LEAK DURING E2 ENGINE RUN.CONTINUE T/S DISCREPANCY REF SAME LP SEQ 2. AIRCRAFT IS CURRENTLY IN WORK. WILL SUPPLY MORE INFO WHEN REPAIRS ARE MADE.
PDIS 656 27-62 2706562 09FEB22 CLT CLOSE IN FLT SPEED BRAKE HANDLE TO CLOSE, SPOILER FAIL MSG, A/C ROLLED RT AND AUTO PILOT FAILED. RAN QRH WITH SPOILERS REMAINING CLOSED REST OF THE FLIGHT DURING DECENT ABOUT 13K FT FACT 09FEB22 16:08 CLT TS USING FIM 27-63-00-810-800-A BLOCKS 1-11 AND FIM 27-63-00-810-807-A. R&R'D SPOILER CONTROL UNIT IAW 27-63-02. PERFORMED SPOILER SYSTEM OPS CHECK IAW AMM 27-63-01-700-801-A. OPS CHECK GOOD. SPOILER FAIL MESSAGE NO LONGER PRESENT. A/C OK FOR SERVICE.
E894481 - THE PASSENGER DOOR FORWARD FRAME EDGE HAS CHAFE SPOTS FROM CONTACT WITH THE LINER .... REMOVED AND REPLACED PASSENGER DOOR FORWARD FRAME IAW EMB145 SRM 51-40-02.
E894713 - LH WING RIB 21 UPPER FLANGE CRACKED .... PERFORMED REPAIR TO LH WING RIB 21 IAW EO1-57-21-0376
E894714 - RH WING RIB 21 UPPER FLANGE CRACKED .... PERFORMED REPAIR TO RH WING RIB 21 IAW EO1-57-22-0005.
E893957 - REAR ELECTRONICS DOOR HAS DENT APPROXIMATELY 3" BELOW HANDLE .... ACCOMPLISHED REPAIR OF REAR ELECTRONIC COMPARTMENT DOOR SKIN APPROX. 3 INCHES BELOW HANDLE IAW EO1-52-21-0373.
E896607 - R/H ENGINE CONTAINMENT RING GOUGED AT LOWER SURFACE .... BLENDED OUT GOUGE ON RH ENGINE CONTAINMENT RING LOWER SURFACE IAW EMB 145 SRM 51-- 10-03. NO DAMAGE LIMITS FOR THIS AREA. MAPPED DAMAGE AND SENT OUT FOR FURTHER EVALUATION IAW PIEDMONT MPPM 13.2. BLENDED AREA MEASURES 1.1"X.- 65"X.105. DEPTH GAGE #524
E894799 - LH INBD FLAP SHROUD HINGE HAS 2 FASTENERS THAT ARE PULLING THRU AT INBD END .... REMOVED LH INBOARD FLAP SHROUD HINGE SECTION WITH 2 FASTENERS PULLING THROUGH AT INBOARD END, PREPPED AND INSTALLED SERVICEABLE HINGE SECTION IAW EMB 145 SRM 51-20-03, EMB 145 SRM 51-40-06.
E894680 - STR 2L CHAFED BTW FR 20-21 .... REPAIRED STR 2L CHAFE BETWEEN FRAMES 20 - 21 IAW PIEDMONT EO1-53-22-0001.
E894621 - THE LH CENTER SEAT TRACK #3 HAS EVIDENCE OF CORROSION ON SEVERAL SPOTS ALONG ITS ENTIRE LENGTH .... REMOVED AND REPLACED THE LH CENTER SEAT TRACK #3 IAW EMB 145 AMM 53-01-06.
E894625 - THE RH WALL #1 FLOOR SUPPORT HAS CORROSION NEAR FRAME 24 AND FRAME 28 .... PERFORMED BLEND OUT OF DAMAGE ON RH WALL #1 FLOOR SUPPORT NEAR FRAME 24 AND FRAME 28 IAW EMB 145 SRM 51-10-03. REMAINING THICKNESS AT BLENDED AREAS ON THE RH WALL #1 FLOOR SUPPORT NEAR FRAME 24 AND FRAME 28 FOUND TO BE BEYOND LIMITS IAW EMB145 SRM 53-22-10AD. REQUIRES PART REPLACEMENT. REMOVED CORRODED RH WALL #1 FLOOR SUPPORT NEAR FRAME 24 AND FRAME 28 AND POSITIONED AND DRILLED SERVICEABLE RH WALL #1 FLOOR SUPPORT NEAR FRAME 24 AND FRAME 28 IAW EMB 145 SRM 51-40-02 AND SRM 51-20-03. COMPLETED INSTALLATION OF RH WALL #1 FLOOR SUPPORT NEAR FRAME 24 AND FRAME 28 IAW EMB-145 SRM 51-40-02. PAINTED FASTENER HEADS IAW EMB 145 CPM 51-21-06
PAX DOOR ENTRANCE FWD AND AFT FLOOR BOARD SUPPORT BRACKETS ARE CORRODED. RAR PAX DOOR ENTRANCE FWD AND AFT FLOOR SUPPORT BRACKETS IAW EMB-145 SRM 51-40--02.
E895312 - FRAMED CRACKED ON UNDERSIDE AT FR 72 AT STR 16L .... REMOVED AND REPLACED FRAME 72 (LH SIDE FRAME SECTION) IAW EMB145 SRM 51-40-02
E894627 - THE RH WALL #2 FLOOR SUPPORT HAS CORROSION BETWEEN FRAMES 33 AND 35 .... REMOVED AND REPLACED SERVICEABLE RH WALL #2 FLOOR SUPPORT IAW EMB 145 SRM 51-40-02.
A/C WILL NOT PRESSURIZE IN AUTO OR MANUAL MODE. MAINTENANCE FOUND GROUND AIR CONDITIONING FLAPPER VALVE BROKEN. R&R'D GROUND CONNECT VALVE IAW AMM 21-22-04 , OPS CHECK GOOD. OPS CHECKED PRESSURIZATION IAW AMM 21-31-00. OPS CHECK GOOD. A/C OK FOR SERVICE
NR BLEED VALVE FAILED AT 60-65 KNOTS. REMOVED AND REPLACED RELAY K0172 IN REF TO AMM TASK 20-13-02-000-400-801-A. OPS CHECK GOOD. NO DEFECTS NOTED. AIRCRAFT OK FOR SERVICE. OPS CHECK 36-00-00-700-803-A
BLD 2 LEAK EICAS MESSAGE AND INSCRIPTION APPEARED AT 8000 FT DURING FLIGHT. FOLLOWED QRH AND MESSAGE WENT AWAY. R&R O-RINGS ON BLEED 2 PIPES AFT COUPLING IN BAG BAY, AFT 2 COUPLINGS IN AFT CENTER WING PANEL. INSPECTED ALL #2 BLEED PIPE COUPLINGS FOR LEAKS. LEAK CHECK GOOD IAW 36-11-10. CLEAR MEL.
BLEED 2 LEAK ON CLIMB IN FLIGHT. R+R GRND AIR CHECK VLV IN REF TO AMM 36 10 02. OPS CHECK AND LEAK CHECK GOOD. GROUND RAN #2 ENG AT POWER WITH BLEEDS AND PACKS ON. NO LEAK MSG PRESENT. OK FOR SERVICE
PDIS 656 36-21 2384272 07APR21 CLT CLOSE BLD 2 LEAK DURING CLIMB. RAN QRH, RESET OK FACT 07APR21 04:14 CLT R&R'D SLEEVE AT #2 HEAT EXCHANGER TO ACM Y SLEEVE FWD OF PACK VALVE. ALSO FOUND CLAMP AT #2 ENG PRSOV LEAKING R/R'D CLAMP. RAN #2 ENG NO LEAKS FOUND AT THIS TIME OK FOR SERVICE.
FUEL 1+2 LOW LEVEL EICAS ON TAKEOFF ATTEMPT. INTERMITTANTLY LOSE #1 FUEL INDICATIONS. VISUALLY INSPECTED SPR PANEL FOR OVBIOUS DEFECTS. NO DEFECTS NOTED. CYCLED ALL SWITCHES TO ENSURE PROPER POSITIONING FOR NORMAL OPERATIONS. PERFORMED TAXI CHECK. TEXI CHECK GOOD. NO FUEL ABNORMALITIES NOTED. OK FOR SERVICE
PURPOSES. CREW CONTACTED MOC STATED ABORTED TAKEOFF DUE TO MOM ENTARY BLEED 2 VALVE FAIL MESSAGE ON TAKEOFF. MESSAGE SELF EXTINGUISHED, NO HISTORY, RECONFIG A/C, SYSTEM OPERATIONS NORMAL. CREW/MOC DETERMINED NO AIRCRAFT FAULT. HISTORY: NONE. THIS DISCREPANCY CLOSED. MIR CREATED.
PDIS 656 32-30 2415291 30OCT20 CLT. CLOSE ON GEAR RETRACTION LOUD NOISE WAS HEARD FROM NOSE GEAR AREA. NOISE WAS CONTINUOUS UNTIL GEAR WAS CYCLED, HAS HISTORY FROM 06OCT20. FACT 31OCT20 02:32 SBY. REFERRING MTL 2017-E-7. INSPECTED MLG UPLOCK BOXES AND NLG UPLOCK BOX FOUND CANNON PLUG ON THE NLG UPLOCK BOX LOOSE. REMOVED AND CLEANED CANNON PLUGS, PER SWPM 20-50-00. RECONNECTED BOTH CANNON PLUGS. PERFORMED RETRACTION AND EXTENSION. OPERATIONS CHECK, IAW AMM 32-30-00. NO THUMPING OR OTHER DEFECTS NOTED. OPERATIONS CHECK GOOD. OK FOR SERVICE AT THIS TIME.
IN FLIGHT, FA REPORTS A LOUD REVING SOUND IN CABIN, FOLLOWED BY ELECTRICAL AND DUST ODOR. AFTER LANDING PACK 2 OVHT MESSAGE ON EICAS. CHECKED THE PACK #2 AND FOUND ACM TO BE DAMAGED. R & R THE ACM IAW AMM 21-51-03. OPS CHECKED GOOD. OK FOR SERVICE.
E1 ANTI ICE VALVE INDICATED CLOSED IN FLIGHT WITH VALVE DEACTIVATED PER MEL. MAINTENANCE: VERIFIED E1 ANTI ICE VALVE IS SECURED OPEN IN LOCKED POSITION PER MEL.
DUE TO POSSIBLE ERRONEOUS INDICATIONS, VERIFICATION OF E1 ANTI-ICE VALVE DEACTIVATION IS REQUIRED.MAINTENANCE VERIFIED E1 ANTI ICE VALVE IS IN THE LOCK POSITION IAW 30-21-01-040-801-A.
ENG 1 ANTI ICE FAIL MESSAGE APPEARED IN FLIGHT. ACC OPER. PROC. MAINTENANCE R&R'D #1 ENGINE ANTI-ICEING VALVE REFERENCING AMM 30-21-05. PERFORMED OPS CHECK IAW AMM 30-00-00-700-803-A/500. OPS CHECK GOOD. CLEAR MEL.
RH OVER THE WING EMERGENCY LIGHT WONT ILLUMINATE....FIX: REPLACED LIGHT IN REFERENCE TO EMB 145 AMM 33-50-10-000/400-801-A OPS CK GOOD.OK FOR SERVICE
NDIS 656 30-21 758 04JAN20 AVP CLOSE -FOR MIR PURPOSES ONLY- FACT 04JAN20 14:22 AVP FLIGHT 4894 ABORTED TAKE OFF DUE TO ONE BRAKE ASSY TEMPERATURE GOING UP INTO THE YELLOW. AIRCRAFT TAXIED BACK TO THE GATE ALL BRAKE TEMPERATURE CAME DOWN BRAKES OPERATE NORMAL WITH NO DEFECTS NOTED.AIRCFRAT DID NOT PULLED TO THE LEFT OR RIGHT. ADVISED CREW TO RE-CONFIGURE AIRCRAFT AND WAIT FOR ALL BRAKE TEMPS
ON GEAR RETRACTION, NLG DOORS REMAINED OPEN. NORMAL GEAR INDICATION. FOUND THE LT NLG DOOR ACTUATOR TO AT FAULT. R & R THE NLG DOOR ACTUATOR IAW TASK 32-33-03, OPS CHECKED GOOD. NO DEFECTS NOTED. PERFORMED A LG RETRACTION TEST AND LEAK CHECK. OPS AND LEAK CHECKED GOOD. OK FOR SERVICE.
DURING CLIMB AFTER GEAR RETRACTION A VERY LOUD NOISE APPEARED AT ABOUT 4000 FT AS THOUGH A GEAR DOOR OPENED. PERFORMED GVI OF THE LANDING GEAR WITH NO DEFECTS NOTED. RETRACTED AND EXTENDED LANDING GEAR SEVERAL TIMES WITH NO DEFECTS NOTED IAW AMM 32-30-00-05. EVAL FLIGHT, SATISFACTORY.
PAX DOOR EMERGENCY LIGHT INTERMITTENT. FIX: REPAIRED DAMAGED WIRE AT LIGHT ASSY BY REPLACING TERMINAL END PIN.
NLG DOOR OPENED UNCOMMANDED DURING APPROACH, CREW C/W QRH, NO FURTHER DEFECTS NOTED. FIX: T/S PER FIM SHOWS TRANSITORY CONDITION. CYCLED GEAR SEVERAL TIMES OPS CHECK GOOD PER AMM 32-30-00. NLG DOORS NOT DESIGNED TO INDICATE OPEN OR CLOSE. REPLACED RELAY K0642 "DOOR CONTROL RLY ON RT AUX RLY SUPPORT, OPS CHECK GOOD. OK FOR SERVICE.
PDIS 656 32-20 1899841 08SEP19 PHL CLOSE ON GEAR RETRACTION NLG DOORS REMAINDS OPEN FACT 08SEP19 17:21 PHL PERFORMED OPS CHECK OF LANDING GEAR. OPS CHECK GOOD. NO DEFECTS NOTED. OK FOR SERVICE.
MAIN DOOR EMERGENCY LIGHT DOES NOT ILLUMINATE. R & R THE BULB IAW AMM TASK 33-50-06-000/400-801-A.OK FOR SERVICE
656 33-51 0003170 14MAY19 SBY CLOSE RT LATERAL PANEL EMERGENCY LIGHT INOP. 30100 00 CRH FACT 14MAY19 09:32 SBY R&RED RT LATERAL PANEL EMERGENCY LIGHT LIGHT BULB IAW AMM 33-50-10-000-801-A AND 33-50-01-700-801-A. P/N ON BULB 1317 P/N OFF BULB 1317.
656 30-41 1919182 01APR19 PHL CLOSE WINDSHIELD HEAT 1 INOP EICAS MSG 27626 00 RNR HISTORY: 31MAR (3X) FACT 01APR19 06:46 ALB TROUBLESHOT WS HEAT 1 INOP MSG PER EMB145 FIM TASK 30-42-00-810-801-A AND FOUND CONTATCTOR K001 TO BE FAULT. REMOVED AND REPLACED CONTACTOR -K001 PER EMB145 AMM 30-42-02. OPS CHECK GOOD.
APU FIREWALL AFT SIDE LOWER EDGE HAS NUMEROUS CHAFED AREAS. C/A-REPAIRED APU FIREWALL IAW ERS-EM-53MR-3662.
CABIN CEILING PANEL 253CLC HAS BROKEN WIRE ON BACK OF PANEL FOR EMERGENCY EXIT LIGHT. C/A-REPAIRED WIRE ON BACK OF CEILING PANEL 253CLC FOR EMERGENCY EXIT LIGHT IAW SWPM 20-21-00.
SERVICE DOOR CENTER SILL CORRODED AT FORWARD AND AFT ENDS. C/A-REMOVED AND REPLACED SERVICE DOOR CENTER SILL IAW SRM 51-40-02.
EMERGENCY LIGHT STRIP NR 6 INOP. C/A-REMOVED AND REPLACED NR 6 EMERGENCY LIGHT STRIP IAW AMM 33-50-12.
LT OMEGA BEAM SIDEWALL HAS POSSIBLE CORROSION ABOVE THE CROSSBEAM AFT OF FRAME 49. C/A-REPAIRED THE LT OMEGA BEAM CORROSION ABOVE THE CROSSBEAM AFT OF FRAME 49 IAW ERS-EM-53MR-3680.
EMERGENCY LIGHT STRIP WIRE AT 241BF IS BROKEN. C/A-REPAIRED EMERGENCY LIGHT WIRE W192-8680-22 (SP9037) AT 241BF IAW SWPM 20-21-00.
EMERGENCY LIGHT STRIP AT 231GF HAS BROKEN WIRES ON AIRCRAFT SIDE. C/A-REPAIRED EMERGENCY LIGHT WIRES (AT 231GF) W192-8630-22 (SP9019) AND W192-8631-22 (SP9020 IAW SWPM 20-21-00.
EMERGENCY LIGHT STRIP WIRE AT 251DF IS BROKEN. C/A-REPAIRED EMERGENCY LIGHT WIRE W192-8761-22 (SP9119 AT 251DF IAW SWPM 20-21-00.
EMERGENCY LIGHT STRIP WIRE AT 251DF IS BROKEN. C/A-REPAIRED EMERGENCY LIGHT WIRE W192-8761-22 (SP9119 AT 251DF IAW SWPM 20-21-00.
LT OMEGA BEAM HAS POSSIBLE CORROSION ABOVE THE CROSSBEAM AT FRAME 44. C/A-REPAIRED THE LT OMEGA BEAM CORROSION ABOVE THE CROSSBEAM AT FRAME 44 IAW ERS-EM-53MR-3679.
RT HAT BEAM INBD AND OTBD SUPPORTS ARE CRACKED FWD OF FR 48. C/A-REMOVED AND REPLACED RT HAT BEAM INBD AND OTBD SUPPORTS IAW SRM 53-23-02. ANGLE P/N 145-28364-005.
LT OMEGA BEAM FLOOR SUPPORT CORRODED BETWEEN FR58 ? 59; LT OMEGA BEAM CORRODED ON LOWER FLANGE AND WEB UNDER CROSSBEAM AT FR 59. C/A-REPAIRED THE LT OMEGA BEAM FLOOR SUPPORT CORROSION BETWEEN FR58-59, AND LOWER FLANGE AND WEB UNDER CROSS BEAM AT FR 59 IAW ERS-EM-53MR-3674.
RT MLG AFT LOWER BEARING CAP IS PITTED AND GOUGED. C/A-REMOVED AND REPLACED RT MLG AFT BEARING CAP IAW AMM 32-10-01.
RT AILERON DAMPER FITTING BOLT HOLE GOUGED. C/A-REMOVED AND REPLACED RT AILERON DAMPER FITTING IAW EM-27MR-112.
FRAME 65 SHEAR CLIP CORRODED AT CARGO DOOR LOWER SILL. C/A-REPAIRED FRAME 65 SHEAR CLIP IAW SRM 53-31-04.
LT AILERON DAMPER FITTING CHAFE. C/A-REMOVED AND REPLACED LT AILERON DAMPER FITTING IAW EM-27MR-112.
FRAME 68 CARGO DOOR CUTOUT LOWER SILL T BRACKET CORRODED. C/A-REMOVED AND REPLACED FRAME 68 CARGO DOOR CUTOUT LOWER SILL T BRACKET IAW SRM 51-40-02.
FRAME 65 CARGO DOOR CUTOUT LOWER SILL T BRACKET CORRODED. C/A-REMOVED AND REPLACED FRAME 65 CARGO DOOR CUTOUT LOWER SILL T BRACKET IAW SRM 51-40-02.
CARGO DOOR CUTOUT LOWER SILL CORRODED. C/A-REMOVED AND REPLACED CARGO DOOR CUTOUT LOWER SILL IAW SRM 51-40-02.
CARGO DOOR LOWER PROFILE IS BENT NEAR FORWARD ROLLER. C/A-REMOVED AND REPLACED CARGO DOOR LOWER PROFILE IAW SRM 51-40-02.
EXTRUSIONS FOR EMERGENCY LIGHT STRIPS #1, #4, #5, #6, #7 AND #8 ARE TORN. C/A-COMPLETE:REMOVED AND REPLACED EXTRUSIONS FOR EMERGENCY PROXIMITY LIGHTS #1,#4,#5,#6,#7 AND #8 IAW AMM 33-50-12. SEE BOW313523 FOR OPS CHECK.
SSI 53-20-11 LT OMEGA BEAM CORRODED ON LOWER FLANGE AND WEB UNDER CROSSBEAM AT FR59. C/A-COMPLETE:COMPLIED WITH ERS-EM-53MR-3674 LT OMEGA BEAM CORROSION FRAME 58 -59 - PERMANENT REPAIR.
ALL RT FLOOR SIDEWALL EXTRUSIONS ARE DAMAGED. C/A-COMPLETE:REMOVED AND REPLACED ALL RT FLOOR SIDEWALL EXTRUSIONS IAW AMM 33-50-12. SEE BOW313523 FOR INSTALLATION.
SSI 53-20-11 LT OMEGA BEAM FLOOR SUPPORT CORRODED BETWEEN FR 58/59 (MARKED). C/A-COMPLETE:FURTHER INVESTIGATION OF CORROSION ON LT OMEGA BEAM FLOOR SUPPORT BETWEEN FR 58/59 SHOWS ADDITIONAL CORROSION THAT EXCEEDS THE REPAIR LIMITS OF EM-53MR-1518. SEE NRTC E696071 FOR BEAM REPAIR.
W/S 1 HEAT FAIL ON CLIMBOUT. HEARD CLICKING NOISE. C/A-DEFERRED W/S HEAT AS PER MEL 30-24 AUTH 010172DM-C M-PROCEDURES COMPLIED WITH. REMOVED AND REPLACED LT WINDSHIELD TEMP CONTROLLER IAW AMM 30-42-01. PERFORMED OPERATIONAL TEST OF WINDSHIELD HEATING SYSTEM IAW AMM 30-42-00. OPS TEST GOOD. MEL ITEM RESTORED.
AFT FA FLASHLIGHT HOLDER ASSEMBLY BROKEN-C/A-FLIGHT CREW PLACARDED AFT FA FLASHLIGHT HOLDER REF: MEL 25- 60 AUTH: 110658-CMOC: 056020
REF AML PAGE 4419251 ITEM # 1 MEL 2553 - AUTH# 110658-C REAR FLASHLIGHT HOLDER BROKEN-C/A-RAR AFT FLASHLIGHT HOLDER IAW EMB AMM 33-50-16-000-801-A AND 33-50-16-400-801-A OPC GOOD NO DEFECTS NOTED AT THIS TIME MEL RESTORED END.
SUPPLEMENTAL BOTH AFT OVERWING EMERGENCY LIGHTS INOP. -C/A-DEFERRED PER MEL 33-29. REMOVED AND REPLACED BATTERY CHARGE ASSY PER W/C 33-700-19 NO FIX . REMOVED AND REPLACED NR 4 BATTERY CHARGER IAW AMM 33-50-04 OPS CHECK GOOD. MEL ITEM RESTORED. BATTERY CHARGER P/N 11-0049 S/N 18035 NR 4
FA WAS UNABLE TO OPEN CABIN DOOR. DOOR HAD TO BE OPENED FROM OUTSIDE. UPON INVESTIGATION FOUND INTERIOR DOOR HANDLE TO BE LOOSE. TIGHTENED DOOR HANDLE IAW AMM 52-18-05. OPC GOOD.
PTRIM MAIN INOP WARNING MSG ON EICAS WHILE CRUISING AT FL320 SPEED M .23. PERFORMED OPS CHECK IAW AMM 27-40-00-700-802-A OPS CHECK OK, NO DEFECTS NOTICED.
OVERWING EMERGENCY LIGHT AT SEAT 12A WAS FOUND INOPERATIVE. R & R THE OVERWING EMERGENCY LIGHT LAMP IAW 33-50-07-000-801-A, AND 33-50-07-400-801-A. OPS CHECKED GOOD.
OVERHEAD ENTRANCE EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED OVERHEAD ENTRANCE EMERGENCY LIGHT OPC GOOD IAW EMB AMM 33-50-06
AFT CABIN FLASHLIGHT CHARGING CRADLE CRACKED. R & R THE FLASHLIGHT CHARGING CRADLE IAW AMM 33-50-16-000-801-A, AND 33-50-16-400-801-A. OPS CHECKED GOOD.
FA INFORMED, MAIN CABIN DOOR HANDLE NEEDS TO BE FIXED DIFFICULT TO OPEN DOOR. FOUND MAIN HANDLE TO BE LOOSE AND FELL OFF. REATTACHED HANDLE IAW AMM 52-18-05. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED
FA REPORTED THE MAIN CABIN DOOR VERY HARD TO OPEN AND CLOSE. INSPECTED AND LUBRICATED THE DOOR IAW 52-00-00, OPS OK
DURING PS-2 FOUND LT AND RT OVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED LT SIDE CENTER FAIRING EXTERNAL EMERGENCY LIGHT ASSEMBLY IAW AMM 33-50-10. REMOVED AND REPLACED BATTERY POWER SUPPLY 3 AND 4 IAW AMM 33-50-04. R&R BATTERY CHARGER 4 IAW AMM 33-50-04. OPS CHECK GOOD. EMERGENCY LIGHTING BATTERY P/N 2013-1ASMI S/N 74818 3; P/N 2013-1A S/N 123941 4; LIGHT EMERGENCY LT P/N 30-2510-3
RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY IAW AMM 33-50-10. OPS CHECKED GOOD.
RIGHT AFT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED RT AFT OVERWING EMERGENCY LIGHT LAMP IAW AMM TASK 33-50-10-000-801-A, AND 33-50-10-400-801-A. OPS CHECKED GOOD.
RT EXTERNAL AFT EMERGENCY LT INOP. REMOVED AND REPLACED RT EXTERNAL AFT EMERGENCY LT LAMP IAW AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPC GOOD AT THIS TIME.
LEFT AND RIGHT OVERWING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY BATTERY PACK IAW 33-700-19. OPS CHECKED GOOD.
LT AND RT OVERWING EXTERNAL EMERGENCY LIGHTS FAIL TO ILLUMINATE. REMOVED AND REPLACED POWER SUPPLY AND BATTERY IAW AMM 33-50-04. OPS CHECKED GOOD.
OVERWING EMERGENCY AFT LIGHT INOPERATIVE. TROUBLESHOT THE EMERGENCY LIGHT IAW FIM 33-50-00-810-804-A. R & R THE BATTERY CHARGER ASSY AND BATTERY IAW AMM 33-50-04. OPS CHECKED GOOD AT THIS TIME.
FIRST INTERIOR CEILING EMERGENCY LIGHT IS INOPERATIVE. REPLACED THE BULB IN THE FIRST INTERIOR CEILING EMERGENCY LIGHT. OPS CHECKED GOOD IAW AMM 33-50-08.
BAGGAGE DOOR FWD END HAS CORROSION AROUND 4 NUTPLATES. REPAIRED BAGGAGE DOOR FWD END IAW ERS-EM-52MR-672.
BAGGAGE DOOR TRAILING EDGE IS BENT IN 2 PLACES. REPAIRED BAGGAGE DOOR TRAILING EDGE IAW ERS-EM-52MR-671.
SERVICE DOOR CUTOUT LOWER CENTER SILL CORRODED. REPAIRED SERVICE DOOR CUTOUT LOWER CENTER SILL IAW ERS-EM-53MR-2453.
LT UPPER FUSELAGE SKIN CRACKED AFT OF FRAME 75, AND ABOVE STRINGER 2L. PERFORMED REPAIR OF LT UPPER FUSELAGE SKIN CRACK AFT OF FRAME 75, AND ABOVE STRINGER 2L IAW SRM 53-31-01.
LT LATERAL UPPER MOUNT BRACKET CRACKED ABOVE LT DV WINDOW FWD UPPER CORNER. REMOVED AND REPLACED REINFORCEMENT ABOVE LATERAL POST IAW SRM 51-40-02.
LT EMERGENCY LIGHT EXTRUSION NR 1 AND NR 3 DAMAGED. R&R LT EMERGENCY LIGHT EXTRUSION NR 3 IAW AMM 33-50-12, SEE NRTC BOW233027 FOR THE INSTALLATION OF NR 1 EXTRUSION.
THE SECOND EMERGENCY LIGHT STRIP FROM THE BACK INOP. REMOVED AND REPLACED THE SECOND EMERGENCY LIGHT STRIP FROM THE BACK IAW AMM 33-50-12,AND OPS CHECKED GOOD.
LT AND RT EXTERIOR OVERWING LIGHTS INOP. REMOVED AND REPLACED EPSU NR 4 IAW W/C 33-700-19 AND OPS CHECK GOOD IAW W/C 33-700-17. BATTERY CHARGER ASSY P/N 11-0049 S/N 20114R.
SECOND AND THIRD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK. OPS CHECKED GOOD IAW AMM 33-50-12.
LT AND RT CENTER FAIRING EXTERNAL EMERGENCY LIGHT FAILS TO ILLUMINATE. REMOVED AND REPLACED THE NR 4 EPSU BATTERY CHARGER ASSY IAW AMM 33-50-04. OPS CHECKED GOOD. NO OTHER DEFECTS NOTED.
SEVERAL EMERGENCY SIGNS AND LIGHTS INOP, EXTERIOR LIGHT FWD OF LT WING, MAIN DOOR LIGHT, MAIN ENTRANCE OVERHEAD LIGHT & FWD CABIN EXIT SIGN. FOUND EMERGENCY BATTERY 1 UNINSTALLED ON COMPARTMENT FLOOR. REINSTALLED BATTERY 1 IN REFERENCE WITH 33-50-04-400-801-A. OPS CHECK NORMAL.
COCKPIT EMER LAMP INOPERATIVE. R & R COCKPIT EMER LAMP IAW AMM 33-50-05-000-801-A & 33-50-05-400-801-A. OPERATIONS CHECKED GOOD.
REAR CABIN FLASHLIGHT INOPERATIVE. R & R REAR CABIN FLASHLIGHT IAW AMM SMP. OPERATIONS CHECKED GOOD.
PASSENGER DOOR EMER LIGHT INOPERATIVE. R & R PAX DOOR EMER LIGHT LAMP IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A. OPERATIONS CHECKED GOOD.
RIGHT OVERWING EMER LIGHT INOPERATIVE. RT OVERWING EMER LIGHT LAMP R & R IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.
FORWARD PAX CABIN FLASHLIGHT CRADLE IS BROKEN. R & R FWD PAX CABIN CRADLE & FLASHLIGHT ASSEMBLY IAW MNTC WC 33-700-20. OPERATIONS CHECKED GOOD.
CAPTAIN`S EMER FLASHLIGHT CRADLE IS CRACKED. R & R REPLACED CAPTAIN`S EMER CRADLE FLASHLIGHT ASSEMBLY IAW MNTC WC 33-700-20.
RIGHT OVERWING EMER LIGHT INOPERATIVE. R & R RT OVERWING EMER LIGHT LAMP IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.
DURING FLIGHT AT FL 370 ALL COCKPIT WINDSHIELDS FROSTED OVER, STARTED DESCENT. BOTH PRIMARY AIRSPEEDS SLOWED TO UNDER 200 KTS, STDBY READ NEAR RED LINE. FOUND WATER IN NR 2 PITOT LINE, CLEANED LINES IAW AMM 34-13-00, ADC 1 & 2 OPERATIONS CHECKED GOOD IAW AMM 34-15-00 ADC 1 & 2 LEAK CHECKED GOOD IAW AMM 34-13-00, NO LEAKS NOTED. ACFT WAS STILL PRESSURIZED UPON LANDING. DELTA P WAS ABOVE 1.2. PRESSURIZATION OPERATIONS CHECKED GOOD IAW AMM CH 21-31-00, NO DEFECTS NOTED. IAW ITEM NR 1 THIS AML PAGE. PITOT STATIC LINES NEED TO BE CHECKED FOR WATER. PERFORMED PITOT STATIC SYS SERVICING IAW AMM 31-13-00. NO WATER FOUND. REQUIRES FURTHER TROUBLESHOOTING.
RIGHT AFT EMER EXTERIOR LIGHT FAILS TO ILLUMINATE. R & R BULB FOR RT AFT EMER EXTERIOR LIGHT. OPERATIONAL CHECKED GOOD.
LEFT & RIGHT OVERWING EXTERNAL EMER LIGHTS INOPERATIVE. R & R NR 4 EPSU IAW WC 33-700-19. OPERATIONS CHECKED GOOD IAW WC 33-700-17. EMER LIGHTING BATTERY PN 2013-1A & SN 108533.
FIRST OFFICER'S EMER FLASH LIGHT CRADLE BROKEN. R & R FIRST OFFICER'S EMER FLASHLIGHT ASSEMBLY IAW AMM 33-50-16-000-801-A & 33-50-16-400-801-A. OPERATIONS CHECKED GOOD.
FLOOR PROXIMITY STRIP LIGHT INOPERATIVE. R & R FLOOR PROXIMITY STRIP LIGHT IAW AMM 33-500-12. OPERATIONS CHECKED GOOD.
ON APPROACH, LOWERED LG, BRK INBD INOP MSG. MSG CLEARED WHEN GEAR WAS RAISED ON THE GO AROUND, MSG REAPPEARED ON SECOND APPROACH & LANDING & REMAINED AFTER LANDING. INBD BRK TEMPS GREEN AT THE BOTTOM OF THE SCALE. R & R BRAKE CONTROL UNIT IAW AMM 32-41-02-000-801-A & 32-41-02-400-801-A. OPERATIONS CHECKED GOOD.
DURING MBV INSPECTION, FOUND LT UPPER FUSELAGE SKIN CRACKED AT FRAME 75 STRINGER 2R. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. PERFORMED PERMANENT REPAIR IAW ERS-EM-53MR-814. REPAIR MATERIALS FILLER 2024T3 .063, REPAIR DOUBLER 2024T3 .080, REPAIR ANGLE 2024T3 .063 & ANGLE FILLER 2024T3 .032.
DURING IMBV INSPECTION, FOUND THE LT LAVATORY FLOOR OMEGA BEAM HAD A MISDRILLED HOLE AFT OF FRAME 61. ACFT WAS REMOVED FROM SERVICE FOR IMBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION. PERFORMED PERMANENT REPAIR IAW EO-EM-53MR-846. REPAIR MATERIALS FILLER AL2024-T3 0.050 INCHES, DOUBLER AL2024-T3 0.050 INCHES.
DURING IMBV INSPECTION, FOUND THE RT LAVATORY FLOOR OMEGA BEAM CRACKED NEAR A NUTPLATE CUT OUT. ACFT WAS REMOVED FROM SERVICE FOR IMBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION, PERFORMED PERMANENT REPAIR ON THE RT LAVATORY FLOOR OMEGA BEAM CRACK NEAR NUTPLATE CUT OUT IAW EO-EM-53MR-845. REPAIR MATERIALS FILLER AL2024-T3 0.050 INCHES, DOUBLER AL2024-T3 0.050 INCHES.
DURING MBV INSPECTION, FOUND RT AILERON DAMPNER FITTING GOUGED. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. R & R RT AILERON DAMPNER FITTING IAW EO EM-27MR-112.
RIGHT EXTERIOR FUSELAGE SKIN CRACKED AROUND RIVET FRAME 78 MARKED. REPAIRED RT EXTERIOR FUSELAGE SKIN AROUND RIVET FRAME 78 BY INSTALLING BUSHING IAW ERS EM-5300-822. SEE TURNOVER FOR DETAILS.
NUMBER 4 EMER LIGHT STRIP HAS BROKEN WIRE. R & R NR 4 EMER LIGHT STRIP IAW AMM 33-50-12. SEE NRTC BOW 168084 TASK NR 1 FOR OPERATIONS CHECK.
LEFT EXTERIOR FUSELAGE SKIN CRACKED AROUND 2 RIVETS FRAME 75 MARKED. REPAIRED LT EXTERIOR FUSELAGE SKIN AROUND 2 RIVETS FRAME 75 BY INSTALLING BUSHING IAW ERS EM-5300-820. SEE TURNOVER FOR DETAILS.
LEFT EXTERIOR FUSELAGE SKIN CRACKED AROUND 2 RIVETS FRAME 78 MARKED. REPAIRED LT EXTERIOR FUSELAGE SKIN AROUND 2 RIVETS FRAME 78 BY INSTALLING BUSHING IAW ERS ERS-EM-5300-820.
LEFT & RIGHT OVERWING EMER LIGHTS INOPERATIVE. R & R NR 4 EMER LIGHT POWER SUPPLY & BATTERY IAW AMM 33-50-04. OPERATIONS CHECKED GOOD.
RIGHT EXTERIOR FUSELAGE SKIN CRACKED AROUND RIVET FRAME 77 MARKED. REPAIRED RT EXTERIOR FUSELAGE SKIN AROUND RIVET FRAME 77 BY INSTALLING BUSHING IAW ERS EM-5300-822. SEE TURNOVER FOR DETAILS.
PROXIMITY LIGHT NR 1, 2 & 3 HAVE BROKEN WIRES. R & R PROX LIGHT NR 1, 2 & 3 IAW AMM 33-50-12 SEE NRTC BOW 168084 FOR FINAL INSTALLATION & OPERATIONS CHECK.
EXTERNAL FUSELAGE SKIN HAS FIVE BURN MARKS FROM FRAME 21 - 26 & BETWEEN STRINGER 19R & 21R MARKED. TWO BURN MARKS BETWEEN FRAME 25 - 26, STRINGER 20R - 19R & ONE BURN MARK BETWEEN FRAME 23 - 24, STRINGER 21R - 20R ACCEPTED IAW ERS-EM-5300-832. AFT BURN MARK BETWEEN FRAME 22 - 23, STRINGER 21R - 20R FOUND WITHIN LIMITS IAW EMB SRM 51-10-05. PERFORMED REPAIR TO FWD BURN MARK BETWEEN FRAME 22 - 23, STRINGER 21R - 20R IAW SRM 53-21-01. SEE TASK & WIP ENTRIES FOR DETAILS.
LEFT EXTERIOR FUSELAGE SKIN CRACKED AROUND 3 RIVETS FRAME 77 MARKED. REPAIRED LT EXTERIOR FUSELAGE SKIN AROUND 3 RIVETS FRAME 77 BY INSTALLING BUSHING IAW ERS EM-5300-820. SEE TURNOVER FOR DETAILS.
LEFT EXTERIOR FUSELAGE SKIN CRACKED AROUND 2 RIVETS FRAME 79 MARKED. REPAIRED LT EXTERIOR FUSELAGE SKIN AROUND 2 RIVETS FRAME 79 BY INSTALLING BUSHING IAW ERS EM-5300-820. SEE TURNOVER FOR DETAILS.
LEFT EXTERIOR FUSELAGE SKIN CRACKED AROUND RIVET FRAME 80 MARKED. REPAIRED LT EXTERIOR FUSELAGE SKIN AROUND RIVET FRAME 80 BY INSTALLING BUSHING IAW ERS EM-5300-820. SEE TURNOVER FOR DETAILS.
RIGHT EXTERIOR FUSELAGE SKIN CRACKED AROUND 3 RIVETS FRAME 79 MARKED. REPAIRED RT EXTERIOR FUSELAGE SKIN AROUND 3 RIVETS FRAME 79 BY INSTALLING BUSHING IAW ERS EM-5300-822. SEE TURNOVER FOR DETAILS.
LEVER ON DRAIN PORT OF EXTERNAL LAVATORY SERVICE DUMP VALVE IS BROKEN. REMOVED AND REPLACED LAVATORY TANK IAW 38-32-01, OPS CHECKED GOOD.
CREW UNABLE TO OPEN MAIN DOOR FROM INSIDE ACFT. DOOR HAD TO OPENED BY RAMP FROM OUTSIDE. REPEAT WRITE UP IAW PAGE 3595075. REPOSITIONED INTERNAL DOOR HANDLE ON TORQUE TUBE IAW AMM 52-11-01. NORMAL OPERATION NOTED.
ON ARRIVAL PAX DOOR COULD NOT BE OPENED FROM THE INSIDE. GND CREW OPENED DOOR FROM THE OUTSIDE. COMPLIED WITH DOOR LUBRICATION TASK 53-21-02-600-801-A. OPERATIONS CHECKED GOOD.
FORWARD CABIN EMERGENCY FLASHLIGHT INOPERATIVE. R & R FWD CABIN EMERGENCY FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.
FIRST OFFICER`S ESCAPE ROPE DOOR OPENS DURING TAKEOFF & LANDING & DURING LIGHT CHOP. RE-SECURED FIRST OFFICER`S ESCAPE ROPE IAW AMM 25-60-00, OPERATIONS CHECKED GOOD.
AFT GALLEY FLASHLIGHT INOPERATIVE. R & R AFT GALLEY FLASHLIGHT.
FORWARD GALLEY FLASHLIGHT INOPERATIVE. R & R FWD GALLEY FLASHLIGHT.
FLOOR PROXIMITY STRIP LIGHT AT SEAT 8 IS INOPERATIVE. R & R FLOOR PROXIMITY STRIP LIGHT AT SEAT 8 IAW 145 AMM 33-50-12. OPERATIONS CHECKED GOOD, NO FURTHER DEFECTS NOTED.
OVERHEAD EMERGENCY LIGHT AT MAIN DOOR INOPERATIVE. R & R BULB IAW AMM 33-50-08. OPS GOOD.
RT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R LAMP IAW AMM 33-50-10. OPS CHECKED GOOD.
FLIGHT 3051, CREW REPORTED A RAPID DECOMPRESSION AT 34000 FT. CABIN ALTITUDE CLIMBED ABOVE 10000. PERFORMED MEMORY ITEMS AND INITIATED AN EMERGENCY DESCENT. 02 MASK DEPLOYED AUTOMATICALLY. ACFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. R & R CABIN PRESSURE CONTROL SYSTEM DIGITAL CONTROLLER IAW AMM 21-31-01. THE FUNCTIONAL CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.
DURING CLIMB, RECEIVED EICAS MESSAGE HYD 1 LOW QTY. FOLLOWED AOM PROCEDURES MONITORED HYD 1 QTY INDICATION. HYD 1 QTY INDICATION BELOW AMBER RANGE AND PRESSURE DROP TO 2900 PSI. AN EMERGENCY WAS DECLARED AND DIVERTED. LANDING WAS UNEVENTFUL AND HYD 1 QTY AND HYD 1 SYS NEVER FAILED. HYD 1 SYS INDICATOR IS IN THE AMBER RANGE WITH NO PRESSURE APPLIED. CREW NOTICED A BURNING ODOR AT THE GATE DURING THE WALK AROUND AND FOUND LEAKING HYD FLUID FROM THE BOTTON OF THE NR 1 ENGINE NACELLE. ACFT REMOVED FROM SERVICE. R & R ENGINE DRIVEN PUMP 1 IAW 29-10-03. OPS AND LEAK CHECKED GOOD. ACFT RETURNED TO SERVICE.
DURING B INSPECTION, FOUND THE FWD RT PASSENGER CABIN EMERGENCY EXIT SIGN INOPERATIVE. ACFT REMOVED FROM SERVICE. TROUBLESHOT AND FOUND THE EMERGENCY LIGHT DC/AC INVERTER NR 3 THE PROBLEM. R & R THE EMERGENCY LIGHT DC/AC INVERTER NR 3 IAW AMM 33-50-11. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.
DURING MX INSP SMELLED SMOKE ODOR WHEN ENTERED INTO THE COCKPIT AND NOTICED THUR TO THE FRONT OF THE CABIN. NO SMOKE OR POPPED BREAKERS. THE ACFT WAS REMOVED FROM SERVICE. COMPLIED WITH OPS CHECK OF CONDITION AIR DISTRIBUTION SYS IAW 21-20-00.THE CHECK WAS GOOD, NO ODOR NOTED AT THIS TIME. PERFORMED ENGINE RUNS FOR ODOR EVENT TROUBLESHOOTING IAW ETN-EM-72-034. NO DEFECTS NOTED, ODOR RATING ALL CATEGORIES 1. THE ACFT WAS RELEASED FOR FUNCTIONAL CHECK FLIGHT PURPOSES ONLY. THE FUNCTIONAL CHECK FLIGHT WAS SATISFACTORY. ACFT OK FOR SERVICE.
DURING MAINTENANCE INSPECTION FOUND THAT WITH GROUND POWER APPLIED AND AIRCRAFT POWER ON, A STRONG BURNING ODOR AND SMOKE WAS OBSERVED COMING FROM UNDER COCKPIT FLOOR. THE AIRCRAFT WAS REMOVED FROM SERVICE. ACCESSED COCKPIT FLOOR PANELS, PERFORMED GENERAL VISUAL INSEPCTION FOR DAMAGE. PERFORMED OPERATIONAL CHECKS. INSPECTED EXTERNAL POWER RECEPTACLE, LEFT AND RIGHT POWER DISTRIBUTION BOXES. CHECKED TORQUE OF ELECTRICAL CABLE TO WINDSHIELD TEMPERTURE CONTROLLER. AUTOPILOT FUNCTIONAL TEST. NO EVIDENCE WAS NOTED OVER A PERIOD OF 3 DAYS. ALL SYSTEMS CHECKED GOOD. NO DAMAGE WAS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING B INSPECTION FOUND THE LEFT FAR AFT NR 8 AISLE EMERGENCY LIGHT STRIP RETAINER BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT FAR AFT NR 8 AISLE EMERGENCY LIGHT STRIP RETAINER AS REQUIRED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE INSPECTION FOUND THE CONNECTOR FOR EMERGENCY LIGHT STRIP AT PANEL 251HF MISSING. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED SERVICEABLE FOR EMERGENCY LIGHT STRIP CONNECTOR AND PIN AT FLOORBOARD 251HF AT SPLICE SP9114; IAW EMB 145 SWPM 20-50-01 AND EMB 145 SWPM 20-21-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE INSPECTION FOUND THE MAIN DOOR SEAL TORN AT THE FOLDING FLAP. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN DOOR SEAL IAW EMB 145 AMM 52-18-04 LEAK CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE INSPECTION FOUND THE AFT AISLE EMERGENCY LIGHT STRIP CONNECTOR BROKEN WIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED SERVICEABLE CONNECTOR ON THE AFT AISLE EMERGENCY LIGHT STRIP IAW EMB 145 SWPM 20-21-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
SKIN, FRAMES 22 AND 23 BELOW STRINGER 5L OIL CANNING. INSTALLED REPAIR DOUBLER AND FILLER IAW AE EO EM-53MR-2104.
DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY LIGHT STRIP NR 6 EXTRUSION BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 6 EMERGENCY LIGHT STRIP ASSEMBLY. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE INSPECTION FOUND THE AFT AISLE EMERGENCY LIGHT STRIP HAS A BROKEN WIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 8 EMERGENCY LIGHT STRIP IAW EMB-145 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE INSPECTION FOUND THE CARGO DOOR LOWER SILL CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CARGO DOOR LOWER SILL IAW EMB SRM 51-40-02 AND ETN# ETN-EM-53-224. THE AIRCRAFT WAS RETURNED TO SERVICE.
CARGO DOOR CUTOUT CORRODED JUST BELOW LT AND RT LWR STRIKER PLATES. REPAIRED STRIKER PLATE AREA IAW AEA EO EM-53MR-1129.
BOTH EXTERNAL OVERWING EMERGENCY LIGHTS INOP. RELACED LIGHT ASSY ON RIGHT SIDE DUE TO CHAFED WIRES.
LEFT EXTERNAL OVERWING EMERGENCY LIGHT INOP. REPLACED NR 4 BATTERY AND CHARGER.
ON FLIGHT 4200 THE CREW REPORTED THE CAPTAIN'S FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN'S FLASHLIGHT ASSEMBLY IAW EMB MM 25-60-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE INSPECTION FOUND THE BATTERY PACK NR 4 EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHTS BATTERY CHARGER AND BATTERY IAW EMB 145 AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING B INSPECTION FOUND THE FORWARD BULKHEAD EMERGENCY "EXIT" SIGN WILL NOT ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND LOOSE CONNECTOR ON LIGHT SECURED AS REQUIRED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING B INSPECTION FOUND THE OVERWING EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. TROUBLESHOT OVERWING EMERGENCY LIGHTS, FOUND THE PROBLEM TO BE THE NR 4 EMERGENCY LIGHTING BATTERY AND CHARGER. REMOVED AND REPLACED THE NR 4 CHARGER AND BATTERY ASSEMBLY IAW W/C 33-700-19. THE OPERATIONAL CHECK WAS GOOD IAW W/C 33-700-17. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING B INSPECTION FOUND THE FORWARD GALLEY EMERGENCY FLASHLIGHT NOT CHARGING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD FLIGHT ATTENDANT FLASHLIGHT ASSEMBLY. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 33-50-16. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING B-INSPECTION FOUND THE MAIN DOOR EMERGENCY LIGHT PANEL DAMAGED AND CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED MAIN DOOR EMERGENCY LIGHT PANEL IAW EMB AMM 25-23-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE BASE VISIT FOUND THE AFT CEILING EMERGENCY LAMP INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT AISLE EMERGENCY LAMP IAW EMB AMM TASK 33-50-08-000-801A/33-50-08-400-801A. THE OPERATIONAL TEST WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE BASE VISIT FOUND THE FLOOR PROXIMITY LIGHTING STRIP LIGHT AT ROWS 8-9 DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. THE FLOOR PROXIMITY STRIP WAS REPLACED IAW EMB 145 AMM 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 3545 AFTER PUSHBACK THE CREW RECEIVED A BAGGAGE SMOKE WARNING MESSAGE. DISCHARGED EXTINGUISHING BOTTLE AND FOLLOWED EPC & AOM PROCEDURES. INDICATIONS REMAINED UNTIL FIRE DEPARTMENT, OPENED CARGO DOOR AND THE FIRE DEPARTMENT FOUND NO INDICATION OF FIRE OR SMOKE IN CARGO COMPARTMENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FIRE EXTINGUISHER BAGGAGE PUSH BUTTON SWITCH IAW AMM 20-13-04 AND REMOVED AND REPLACED BOTH CARGO SMOKE DETECTOR AT CARGO COMPARTMENT IAW AMM 26-15-01. ALSO REMOVED AND REPLACED TEST RELAY FOR BAGGAGE SMOKE (K0629) IAW AMM STAND PRACT 20-13-02. THE OPERATIONAL CHECK FOR THE SYSTEM TEST IS OK AT THIS TIME.
DURING MAINTENANCE BASE INSPECTION FOUND THE EMERGENCY EXIT IDENTIFIER SIGN INSTALLED ON THE FORWARD CABIN SEALING PANEL INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED THE FORWARD CABIN CEILING PANEL. FOUND CONNECTOR FOR EMERGENCY LIGHT NOT CONNECTED. RECONNECTED CONNECTOR AND REINSTALLED CEILING PANEL IAW EMB AMM 25-22-04-020-001 ITEM (3) AND 25-22-04-420-001 (2). THE OPERATIONAL CHECK WAS GOOD. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE BASE VISIT FOUND THE CARGO DOOR SILL CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED CARGO SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 2731 THE CREW REPORTED A BUZZING/VIBRATION NOISE IN CLIMB FROM 8K TO 13K WITH AN ODD ODOR. THE CAPTAIN ELECTED TO RETURN TO DFW. THE NOISE RETURNED DESCENDING THROUGH 8,7K WITH AN ELECTRICAL MELTING ODOR. THE NOISE SUBSIDED AT 5K AND THE ODOR DISSIPATED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT FORWARD AVIONICS FAN PART NUMBER 526484, S/N 104407326 AND NR 2 FAN INVERTER PART NUMBER 524864, S/N E03092215. AN OPERATIONAL CHECK WAS PERFORMED ON THE LEFT AND RIGHT RAM AIR VALVE. PERFORMED GROUND RUN OF AIRCRAFT, NO ODOR OR DEFECTS NOTED AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 2920 DURING CLIMBOUT TESTING THE ANTI ICE THE CREW REPORTED, RECEIVED FUMES IN THE COCKPIT. THE CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO CLE. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. TROUBLESHOT AND FOUND A SLIGHT BURNING ODOR FROM THE COCKPIT RECIRCULATION FAN . WHEN THE FAN WAS SUPPOSE TO BE RUNNING, THE FAN BLADES WERE FROZEN IN POSITION. REMOVED AND REPLACED THE RECIRCULATION FAN IAW EMB 145 AMM 21-24-01-000-801-A AND 21-24-01-400-801-A. THE OPERATIONAL CHECK WAS GOOD AND NO ELECTRICAL ODOR WAS NOTICED. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE BASE VISIT THE OVERWING EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE BASE INSPECTION THE FORWARD SERVICE DOOR WAS FOUND TO BE CORRODED. FRAME 19 AT SILL ATTACHMENT HAS 3 MISDRILLED HOLES. FRAME 17 HAS 2 MISDRILLED HOLES JUST ABOVE STRINGER 16 AT SILL ATTACHMENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FORWARD SERVICE DOOR SILL IAW EMBRAER SRM 51-40-02. REPAIRED MISDRILLED HOLES ON FRAME 19 EO EM53MR-1375. REPAIRED MISDRILLED HOLES ON FRAME 17 IAW EO EM-53MR-1376. AIRCRAFT WAS RETURNED TO SERVICE. ALL PARTS REMOVED: FORWARD SILL PART NUMBER 145-21725-613. FRAME 19-PART NUMBER 145-24145-002. FRAME 17-PART NUMBER 145-22186-611. AIRCRAFT RETURNED TO SERVICE.
ON FLIGHT 3200: DURING A PS-2 CHECK, AN EMERGENCY EXIT SIGN ON SEAT 12A WAS FOUND INOPERABLE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED EMERGENCY EXIT SIGN ON SEAT 12A. AIRCRAFT RETURNED TO SERVICE.
DURING A HMBV INSPECTION, THE CARGO DOOR CUT OUT LOWER SILL WAS FOUND TO BE CORRODED. REPLACED LOWER SILL WITH PART NUMBER 145-25480-603 IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.
BURNING ELECTRICAL ODOR IN CABIN AND FLIGHT DECK DURING TAXI OUT, RETURNED TO BLOCK. REMOVED AND REPLACED RECIRCULATION FAN AND PACK VALVE IAW EMB AMM. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.
A DENT WITH A SCRATCH WAS DISCOVERED ON THE SKIN PANEL BETWEEN FRAMES 16 AND 17 AD BETWEEN STRINGERS 18L AND 19L. PERFORMED A CUTOUT OF THE SKIN PANEL TO REMOVE THE DAMAGE. FABRICATED A FILLER AND REPAIR DOUBLER. REPAIR DONE IAW EMB REPAIR STATEMENT IC2005-145/5137 PARA 3 DATED SEPT 15, 2003. (M)
THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. PERFORMED A CUT OUT OF LEFT OMEGA BEAM TO REMOVE CORROSION. PREPARED DOUBLER, FILLER, REPAIR PLATE AND TWO SHIMS. REPAIR DONE IAW EMB145 SRM, SRM 145/1142 REV 30 CHAPTER 53-00-10 FIG 201. (M)
CREW REPORTED THE AFT SECTION, ROW 12, FLOOR PROXIMITY, OVERHEAD EXIT LIGHT, AND SEVERAL FORWARD EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 POWER SUPPLY TO CORRECT THE PROBLEM. THE NR 1,3, AND 4 POWER SUPPLY UNITS AND ALL 4 BATTERIES WERE ALSO CHANGED AS A PRECAUTION. ALL WORK AND OPERATIONAL CHECKS WERE DONE IAW THE MM. (SW21200500265)