N724EV

Part: UNKNOWN — WARNING MESSAGE (UNKNOWN) · airframe 38,662 hrs · 28,475 cycles

L COWL A/I CAUTION MESSAGE WHEN USING THE COWL ANTI ICE. DID THE QRH THOUGH IT CLEARED ON ITS OWN. (FILED CLOSED)UPON ARRIVAL TO AIRCRAFT FOUND L COWL A/I VALVE OPEN CAUTION MESSAGE WITHOUT VALVE BEING COMMANDED AND DURING OPERATIONAL CHECKS OF L COWL A/I VALVE PER CRJ 700 AMM 30-22-01, FOUND L COWL A/I VALVE TO BE CLOSED WHEN COMMANDED OPEN AND OPEN WHEN COMMANDED CLOSED. PERFORMED TROUBLESHOOTING OF L COWL A/I PER CRJ 700 FIM 30-22-01. UPON TROUBLESHOOTING DETERMINED THAT THE K6S RELAY WITHIN JB11 PCB 1 WAS MAJOR CAUSE OF FAULT ISSUE, REMOVED AND REPLACED PCB 1 IN JB11 PER CRJ 700 AMM 24-06-03, UPON SUBSEQUENT OPERATIONAL TESTS, L COWL A/I VALVE WORKS INTERMITTENTLY BUT STILL NO FIX. AFTER CONTINUED TROUBLESHOOTING REMOVED AND REPLACED L COWL A/I VALVE WITH A SERVICEABLE UNIT PER CRJ 700 AM 30-22-01, AFTER MULTIPLE OPERATIONAL CHECKS, L COWL A/I VALVE NOW FUNCTIONS NORMALLY AND DOES AS COMMANDED, ALL OPS CHECKS GOOD, A/C OK FOR SERVICE.

Part: WINDSHIELD — CRACKED (UNKNOWN) · airframe 37,964 hrs · 27,864 cycles

TRANSFER FROM EAML 1198898 : FORWARD RIGHT WINDSCREEN IS CRACKING FROM THE BASE TO ABOUT A THIRD OF THE WAY UP. (FLT 9913 FILED CLOSED)INSTALLED RH WINDSHIELD PER AMM 56-11-01 AND TASK CARD 56-220-1000 SKY CRJ 700 COCKPIT WINDSHIELD INSTALLATION.PERFORMED OPERATIONAL TEST OF THE WINDSHIELD TEMP CONTROLLERS IAW AMM 30-41-06. LEAK CHECK GOOD AT THIS TIME. NO DEFECTS NOTED AT THIS TIME.REFERENCE CP 27073495 FOR REMOVAL OF RH WINDSHIELD.

Part: UNKNOWN — SPARKS (UNKNOWN) · airframe 37,735 hrs · 27,635 cycles

SPARKING/ARCING AROUND LEFT WINDSHIELD HEAT. CB A11 POPPED. L WSHLD HEAT CAUTION ILLUMINATED. TURNED OFF L WINDSHIELD HEAT AND RAN QRH. (FLT 3272 FILED CLOSED)REMOVED AND REPLACED THE CAPTAINS SIDE WINDSHIELD IN REFERENCE TO AMM 56-11-01 AND COMPLIED WITH TASK CARD 56-220-1000-SKY. OPS CHECK GOOD AND NO LEAKS NOTED.TOQUE WRENCH QD1R200 S/N 0811504069

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 37,687 hrs · 27,589 cycles

TRANSFER FROM EAML 1160540 : 11 INCH CRACK ON THE CAPTAIN WIND SCREEN (FLT 3007 FILED CLOSED)REMOVED AND REPLACED PILOT SIDE WINDSHIELD PER CRJ700 AMM 56-11-01 AND TASK CARD 56-220-1000-SKY. OPS AND LEAK CHECK SATISFACTORY AT THIS TIME.TORQUE WRENCH INFO:S/N 0420502921CAL.DUE: 12/2023FORCE GAUGE: S/N U09416CAL DUE 9/30.2023MULTIMETER:S/N: 42400071CAL DUE: 12/31/2023TORQUE SCREW:S/N: 0711401160DUE: 3/2024

Part: WINDSHIELD — CRACKED · airframe 37,398 hrs · 27,333 cycles

TRANSFER FROM EAML 1114166 : LEFT WINDSHIELD CRACK BECAME VISIBLE 2 MINS PRIOR TO LANDING. ASSOCIATED L WSHLD HEAT CAUTION MESSAGE APPEARED SOON AFTER. RAN QRH AFTER LANDING.(FILED CLOSED)REMOVED AND REPLACED LH WINDSHIELD ASSEMBLY WITH A SERVICEABLE UNIT IN REF TO AMM 56-11-01. WINDSHILED HEAT OPS CHECK GOOD AT THIS TIME. NO LEAKS NOTED DURING PRESSURIZATION.

Part: NONE — ODOR · airframe 36,486 hrs · 26,525 cycles

OBVIOUS SMELL OF A BURNING ELECTRICAL ODOR INSIDE PLANE. (FLIGHT #3184 FILED CLOSED) COMPLIED WITH INSPECTIONS LISTED IN BOMBARDIER SERVICE LETTER CRJ700/705/900/1000-SL-21-028 AND FIM 21-22-00 WITH NO SMOKE SMELL OR OTHER DEFECTS NOTED AT THIS TIME. SUSPECT SMOKE SMELL MAY HAVE BEEN CAUSED BY MOISTURE INTEGRATION OF APU OR PACK DUE TO HIGH LEVEL OF PRECIPITATION IN KDRT IN PAST12 HRS. PLEASE REFERENCE AML 982651 PLEASE REFERENCE AML 982652 PLEASE REFERENCE AML 982653 PLEASE REFERENCE AML 982662 PLEASE REFERENCE AML 982669 PLEASE REFERENCE AML 982672 PLEASE REFERENCE AML 982691 FOR COMPLETE LIST OF INSPECTIONS PERFORMED.

Part: NONE — CRACKED · airframe 35,671 hrs · 25,869 cycles

CRACK LOCATED ON AVIONICS BAY DOOR HANDLE HOUSING IS CLASSIFIED AS " MAJOR REPAIR" / ***FORM M-337 INITIATED*** (FILED - CLOSED) REMOVED AND REPLACED AVIONICS BAY DOOR HANDLE HOUSING IN REFERENCE TO CRJ 700 SRM 52-42-02. COMPLIED WITH TASK CARD 51-900-1002-SKY.FORM M-337 COMPLETED. SEE CP 24593270 FOR ORIGINAL DISCREPANCY. SEE CP 24596239 FOR FPI CRACK VERIFICATION. SEE CP 24617627 FOR PRESSURIZATION CHECK.

Part: WINDOW POST — CRACKED (COCKPIT) · airframe 34,704 hrs · 25,141 cycles

COPILOTS WINDSHIELD SIDE POST WAS FOUND TO HAVE A CRACK DURING NDT (C-CHECK RO 8/19/2021) REPLACED WINDSHIELD SIDE POST (CO-PILOT) IAW CRJ700 SRM 51-40-11, 51-42-21, 51-21-11, 51-21-16, 51-42-06, 51-45-00 AND BOMBARDIER DWNG CC670-33055.

Part: WINDOW POST — CRACKED (COCKPIT) · airframe 34,704 hrs · 25,141 cycles

PILOTS WINDSHIELD SIDE POST WAS FOUND TO HAVE A CRACK DURING NDT (C-CHECK RO 8/19/2021) REPLACED WINDSHIELD SIDE POST (PILOT) IAW CRJ700 SRM 51-40-11, 51-42-21, 51-21-11, 51-21-16, 51-42-06, 51-45-00 AND BOMBARDIER DWG CC670-33055

Part: FRAME — DAMAGED (BS 333 S0-9R) · airframe 34,704 hrs · 25,141 cycles

PER CUSTOMER REQUEST, REPLACE FS 333 FRAME FROM STR 0 TO STR9R. (C-CHECK RO 8/19/2021) REPLACED FS333 FRAME STR0 TO STR9R IAW CRJ700 SRM 51-40-11,51-42-20,51-42-06 AND BOMBARDIER DRAWING SH670-31950. IAW CRJ700 AMM 20-30-00,33-51-00,33-26-00,38-10-00. ALSO CRJ700WM 24-50-11. SEE ATTACHED CONTINUE CARD FOR DETAILS, PRESSURIZATION CHECK TO BE COMPLIED WITH ON CAMP# 23231493.NO DEFECTS NOTED.

Part: INTERCOSTAL — CORRODED (BS 310-349 S20R) · airframe 34,704 hrs · 25,141 cycles

INTERCOSTAL AT STGR 20R SHOWING CORROSION. (C-CHECK RO 8/19/2021) REMOVED AND REPLACED CORRODED INTERCOSTAL/SILL AT STR20R BETWEEN FS310-FS349 IAW CRJ700 SRM 51-40-11, 51-42-06, 51-21-11, 51-25-16. NO FURTHER ACTION REQUIRED AT THIS TIME.

Part: DOOR SILL — CORRODED (AFT CARGO) · airframe 34,704 hrs · 25,141 cycles

AFT CARGO DOOR LOWER SILL AT FS 1031.00 HAS LIGGHT SURFACE CORROSION ON OUTER SURFACE REQUIRES CLEANING AND EVALUATION (C-CHECK RO 8/19/2021) REMOVED CORRODED AFT CARGO DOOR LOWER SILL PN MM670-35655-003 AND REPLACED WITH NEW AFT CARGO DOOR LOWER SILL PN MM670-35655-003 IAW CRJ700 SRM 53-61-23, 51-42-06, 51-42-13 AND 51-42-21.

Part: SEAT TRACK — CORRODED (BS 863 RBL 9) · airframe 34,704 hrs · 25,141 cycles

MAIN CABIN SEAT RAIL AT R.B.L.9 F.S. 863.00 HAS CORROSION, NICKS AND GOUGES. (C-CHECK RO 8/19/2021) REMOVED AND REPLACED SEAT TRACK AT FS836 TO 940 RBL9 IAW E 670-53-00-589

Part: BUTTSTRAP — CORRODED (BS 280-282) · airframe 34,704 hrs · 25,141 cycles

CIRCUMFERENTIAL JOINT BETWEEN FS. 280.00 TO 282.86 AND STRINGER 26LH TO 26RH IS CORRODED. (C-CHECK RO 8/19/2021) COMPLIED WITH DISPOSITION FOR BLENDED CORROSION DAMAGE TO FS280.00 BUTTSTRAP BETWEEN STR26L AND STR26R IAW MHIRJ REO 670-53-21-2014 REV.-- DATED 8/6/21. IAW CRJ700 SRM 51-42-06,51-21-06,51-25-06,51-25-16,51-21-11,51-23-00,51-42-00. CRJ700 NDTM 51-20-006. / STS-6796 CAL DATE 090921.PRESSURIZATION CHECK TO BE PERFORMED ON CAMP# 23231493 ITEM#1. SEE ATTACHED CONTINUE CARD FOR ANY ADDITIONAL INSTALLS/OPERATIONAL CHECKS.

Part: SEAT TRACK — CORRODED (BS 847-989 LBL9) · airframe 34,704 hrs · 25,141 cycles

MAIN CABIN SEAT RAILS AT LBL9 ABD RBL9 BETWEEN F.S. 847.00 TO 989.00, HAS CORROSION, NICKS AND GOUGES. (C-CHECK RO 8/19/2021) REMOVED AND REPLACED SEAT TRACK AT FS836 TO 968 LBL9 AND FS 836 TO 940 RBL9 IAW EA 670-53-00-589

Part: BOLT — CORRODED (LT WING) · airframe 34,704 hrs · 25,141 cycles

LEFT WING, OUTBOARD FLAP HINGE WS. 178.00 SUPPORT FITTING ( FWD ) HAS BOLTS CORRODED. (C-CHECK RO 8/19/2021) REMOVED AND REPLACED L/H WING O/B FLAP HINGE BOX FWD FITTING FWD BOLT'S AT WING STATION 178.00 REF. CRJ 700 AMM 57-54-02 AND ACCOMPLISHED LEAK CHECK OF THE BOLT'S REF. CRJ 700 AMM 28-11-00 (NO LEAKS NOTED AT THIS TIME)

Part: FRAME — CORRODED (BS 320-333 S21L) · airframe 34,704 hrs · 25,141 cycles

CORROSION ON FRAME GROUNDS GS1839 AND GS1841 EXTENDS ON FRAME BETWEEN FS 319.70 TO FS 333.00 LOCATED AT LEFT STRINGER 21. (C-CHECK RO 8/19/2021) REMOVED AND REPLACED CORRODED INTERCOSTAL/BACK-UP SILL AT STR21L BETWEEN FS319.70 TO FS333.00 IAW CRJ700 SRM 51-21-06, 51-42-06 AND 51-40-11. NO FURTHER ACTION REQUIRED AT THIS TIME.

Part: SEAT TRACK — GOUGED (BS 394 RBL 9) · airframe 34,704 hrs · 25,141 cycles

MAIN CABIN, SEAT TRACK, RIGHT SIDE FS. 394.00 WL 72.50 RBL 9.00 HAS GOUGES AND NICK'S (C-CHECK RO 8/19/2021) BLENDED OUT SEAT TRACK AT RBL9 FROM FS394 TO FS485, FOUND OUT OF LIMITS IAW CRJ700 SRM 53-21-49. REMOVED AND REPLACED SEAT TRACK FROM FS394 TO FS485 IAW CRJ700 AMM 53-00-49 AND REO 670-53-00-589. REV. -A DATE : 2020-07-14 / TOOL: STS-0250 CAL DUE DATE: 10 MAY 22

Part: FRAME — CRACKED (BS 333 S0-1R) · airframe 34,704 hrs · 25,141 cycles

FRAME AT FS333.00 CRACKED AT UPPER SECTION BETWEEN STRINGER 0 AND STRINGER 1 RH. (C-CHECK RO 8/19/2021) REPAIRED FRAME AT FS 333, BETWEEN STR 0 AND RH1, IAW REO 670-53-21-2051 REV --, DTD 06JUN2021. DUE TO A REQUIREMENT FOR PERIODIC RE-INSPECTIONS THE ENTIRE FRAME AT FS333 FROM STR0 TO STR9R IS BEING REPLACED ON CP 22948978. REPLACEMENT OF THE COMPLETE FRAME ELIMINATES THE NEED FOR RE-INSPECTIONS.

Part: SKIN — DENTED (BS 193-202) · airframe 34,704 hrs · 25,141 cycles

WITHIN 10 FLIGHT CYCLES, COMPLY WITH PERMANENT REPAIR OF FOUND DENT ON LH NOSE BETWEEN FS193.25 AND FS202.75 STRGR 19 LH AND 21 LH, MEASURING 7.82 IN IN LENGTH BY 4.53 IN WIDE AND .155 AT ITS DEEPEST. COMPLIED WITH TEMPORARY DISPOSITION PER REO 670-53-11-1653 REV -- DATED 2021-02-11, DUE BY TAC 25148 (C-CHECK RO 8/19/2021) REMOVED AND REPLACED L/H NOSE SKIN PANEL PN: CC670-33106-5S LOT# R00023257-0201. IAW CRJ700 SRM 51-40-11, 51-42-11, 51-40-13 AND REO 690-53-11-1215 REV. DATED 2020-01-21. AREA FREE OF FOD. NO FURTHER DEFECTS NOTED.

Part: FIRE WARNING — FALSE ACTIVATION (APU BAY) · airframe 33,172 hrs · 23,921 cycles

THE CREW REPORTED AN APU FIRE MESSAGE IN FLIGHT. THE CREW COMPLIED WITH THE QRH AND THE MESSAGE DID NOT PERSIST. THE AIRCRFT LANDED AT EVV WITHOUT INCIDENT WHERE CONTRACT MAINTENANCE INSPECTED THE AIRCRAFT WITH NO DAMAGE NOTED. MAINTENANCE OPERATIONALLY CHECKED THE APU WITH NO DEFECTS NOTED. THE AIRCRAFT WAS SUBSEQUENTLY APPROVED FOR RETURN TO SERVICE.

Part: INTERCOSTAL — CORRODED (BS 278) · airframe 32,708 hrs · 23,574 cycles

CORROSION ON RIGHT INTERCOSTAL AT NOSE JACK PAD BS 278. MAINTENANCE REPLACED THE INTERCOSTAL.

Part: INTERCOSTAL — CORRODED (BS 278) · airframe 32,708 hrs · 23,574 cycles

CORROSION ON LEFT INTERCOSTAL AT NOSE JACK BS 278. MAINTENANCE REPLACED LEFT INTERCOSTAL.

Part: FLOORBEAM — CORRODED (BS 677) · airframe 32,708 hrs · 23,574 cycles

THE FLOORBEAM CAP WAS FOUND CORRODED AT BS 677, LBL 9. MAINTENANCE REPLACED THE FLOORBEAM CAP.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 32,708 hrs · 23,574 cycles

SEAT TRACK CORRODED BS 485 - 581, LBL 9. MAINTENANCE REPLACED THE SEAT TRACK.

Part: FLOORBEAM — CORRODED (BS 554) · airframe 32,708 hrs · 23,574 cycles

THE FLOORBEAM CAP WAS FOUND CORRODED AT BS 554, LBL 9. MAINTENANCE REPLACED THE FLOORBEAM CAP.

Part: STRINGER — CORRODED (BS 310-319) · airframe 32,708 hrs · 23,574 cycles

STRINGER 27 HAS CORROSION BETWEEN BS 310 - 319. MAINTENANCE REPLACED THE STRINGER.

Part: DOOR FRAME — CORRODED (PAX DOORWAY) · airframe 32,708 hrs · 23,574 cycles

PAX DOOR FORWARD FRAME CORRODED AT UPPER CAM. MAINTENANCE REPAIRED THE DOOR FRAME IAW EC/TC EA 30-2017-128.

Part: RISER — CORRODED (PAX DOOR) · airframe 32,708 hrs · 23,574 cycles

PAX DOOR FORWARD RISER PANEL CORRODED AT TOP SECTION. REPAIRED THE RISER IAW EC/TC EA 30-2017-129.

Part: SEAT TRACK — CORRODED (BS 708-761) · airframe 32,708 hrs · 23,574 cycles

RIGHT SIDEWALL SEAT TRACK SEGMENT BS 708 - 761 HAS CORROSION. MAINTENANCE REMOVED, FABRICATED, AND INSTALLED THE SEAT TRACK IAW ECTC REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (BS 708-761) · airframe 32,708 hrs · 23,574 cycles

LEFT SIDEWALL SEAT TRACK SEGMENT AT BS 708 - 761 HAS CORROSION. MAINTENANCE REMOVED AND FABRICATED A NEW SEAT TRACK IAW ECTC REO 670-53-343 AND INSTALLED.

Part: SEAT TRACK — CORRODED (BS 785-847) · airframe 32,708 hrs · 23,574 cycles

RIGHT SIDEWALL SEAT TRACK SEGMENT BS 785 - 847 CORRODED. REMOVED AND FABRICATED A NEW SEAT TRACK IAW ECTC REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (BS 677-708) · airframe 32,708 hrs · 23,574 cycles

RIGHT SIDEWALL SEAT TRACK SEGMENT BS 677 - 708 CORRODED. MAINTENANCE REMOVED AND FABRICATED A NEW SEAT TRACK IAW ECTC REO 670-53-343.

Part: SUPPORT ANGLE — CORRODED (BS 939) · airframe 32,708 hrs · 23,574 cycles

AFT FUSELAGE FAIRING SUPPORT ANGLE CORRODED AT BS939 BL 0. MAINTENANCE REMOVED AND REPLACED THE SUPPORT ANGLE.

Part: SEAT TRACK — CORRODED (BS 485-565) · airframe 32,708 hrs · 23,574 cycles

RIGHT SIDEWALL SEAT TRACK SEGMENT, BS 485 - 565 HAS CORROSION. MAINTENANCE REMOVED AND FABRICATED A NEW SEAT TRACK IAW ECTC REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (BS 565-677) · airframe 32,708 hrs · 23,574 cycles

RIGHT SIDEWALL SEAT TRACK SEGMENT BS 565 - 677 CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK.

Part: SEAT TRACK — CORRODED (BS 485-565) · airframe 32,708 hrs · 23,574 cycles

LEFT SIDEWALL SEAT TRACK SEGMENT, BS 485 - 565 HAD CORROSION. REMOVED AND FABRICATED A NEW SEAT TRACK IAW ECTC REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (BS 565-677) · airframe 32,708 hrs · 23,574 cycles

LEFT SIDEWALL SEAT TRACK SEGMENT BS 565 - 677 HAS CORROSION. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK.

Part: SEAT TRACK — CORRODED (BS 677-708) · airframe 32,708 hrs · 23,574 cycles

LEFT SIDEWALL SEAT TRACK SEGMENT BS 677 - 708 CORRODED. MAINTENANCE REMOVED AND FABRICATED A NEW SEAT TRACK IAW ECTC REO 670-53-00-343

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 32,708 hrs · 23,574 cycles

SEAT TRACK SEGMENT BS 581 - 677, LBL 9 HAS CORROSION. FABRICATED A NEW SEAT TRACK IAW REO 670-53-00-343 AND REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 32,708 hrs · 23,574 cycles

SEAT TRACK SEGMENT BS 581 - 677, RBL 9 WAS CORRODED. FABRICATED A NEW SEAT TRACK IAW REO 670-53-00-343, AND REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (BS 364-485) · airframe 32,708 hrs · 23,574 cycles

SEAT TRACK SEGMENT BS 364 - 485, RBL 9 WAS CORRODED. REPAIRED IAW ECTC REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 32,708 hrs · 23,574 cycles

SEAT TRACK BS 485 - 581, RBL 9 WAS CORRODED. REPAIRED IAW ECTC REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (BS 349) · airframe 31,677 hrs · 22,814 cycles

DURING HEAVY CHECK, THE SEAT TRACK AT BS 349, RBL 9 WAS FOUND CORRODED. REPAIRED THE SEAT TRACK IAW REO 670-53-00-074, REV A.

Part: FLOORBEAM — CORRODED (BS 1031) · airframe 31,677 hrs · 22,814 cycles

DURING HEAVY CHECK, THE FLOORBEAM AT LBL 27, BS 1031 FOUND CORRODED BEYOND LIMITS. THE FLOORBEAM WAS REPAIRED IAW EO 700-53-10-0036, REV 0.

Part: FLOORBEAM — CORRODED (BS 1031) · airframe 31,677 hrs · 22,814 cycles

DURING HEAVY CHECK, THE FLOORBEAM AT LBL 9 AT FS 1031 FOUND CORRODED BEYOND LIMITS. FLOORBEAM REPAIRED IAW EO 700-53-10-0037, REV 0.

Part: FLOORBEAM — CORRODED (BS 1031) · airframe 31,677 hrs · 22,814 cycles

DURING HEAVY CHECK,M THE FLOORBEAM AT RBL 9, BS 1031 FOUND CORRODED BEYOND LIMITS. THE FLOORBEAM WAS REPAIRED IAW EO 700-53-10-0038, REV 0.

Part: SMOKE DETECTOR — FAULTY (ZONE 900) · airframe 31,344 hrs · 22,574 cycles

PILOT REPORTED AFT SMOKE DETECTOR WARNING MESSAGE INFLIGHT. NO SMOKE NOTED REPEAT WRITE UP. MX REMOVED AND REPLACED THE AFT LAV SMOKE DETECTOR WITH OPERATIONAL CHECK GOOD. A/C APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — LOOSE (LAVATORY) · airframe 31,343 hrs · 22,573 cycles

PILOT REPORTED AFT LAVATORY SMOKE WARNING MESSAGE ON FINAL APPROACH. CONTINUED FOR SEVERAL MINUTES. NO SMOKE DETECTED. FOUND SMOKE DETECTOR LOOSE, SECURED AND OPS CHECKED GOOD. APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (LT WING) · airframe 28,577 hrs · 20,316 cycles

LEFT WING LOWER SKIN HAS A CRACK INDICATION.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 28,577 hrs · 20,316 cycles

INTERCOSTAL CORRODED AT S27L BETWEEN BS 349-364. REMOVED INTERCOSTAL IAW SRM 51-42-06-001-001, A01 & SRM 51-42-21-001-001 A01. DRILLED NEW SERVICEABLE INTERCOSTAL AND INSTALLED IAW SRM 51-42-06-001-001 A01 AND 51-42-21-001-001 A01.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 28,577 hrs · 20,316 cycles

INTERCOSTAL CORRODED AT STR 27, RT BTW F. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23-101-003-A01. R & R INTERCOSTAL AT STR 27R BETWEEN BS 349 & 364 IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: STRIKER — CORRODED (SERVICE DOOR) · airframe 28,577 hrs · 20,316 cycles

SERVICE DOOR LOWER PRESSURE SEAL STRIKER CORRODED AROUND DRAIN HOLES. EVALUATED DAMAGE AND FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-21-23-101-002-A01. R & R SERVICE DOOR LOWER PRESSURE SEAL STRIKER REF: SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND DWG SH670-31412.

Part: ANGLE — CORRODED (SERVICE DOOR) · airframe 28,577 hrs · 20,316 cycles

SERVICE DOOR LOWER SILL ANGLE CORRODED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-42-06-001-001-A01, AND DWG II SH670-31950.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 28,577 hrs · 20,316 cycles

CRAWL WAY FLOOR PANEL 141ALF FWD FLOOR SUPPORT CORRODED. R & R ANGLE SUPPORT FOR 141ALF AT FS280 IAW SRM 51-42-21-001-001-A01, 51-42-06-001-001-A01 AND DWG CC670-34256.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 28,577 hrs · 20,316 cycles

PASSENGER DOOR LOWER SILL UPPER CAP ANGLE CORRODED. LOCATED FASTENER HOLES IN NEW SERVICEABLE LOWER KICKPLATE ANGLE AND REMOVED DISCREPANT ANGLE. INSTALLED SERVICABLE ANGLE ASSY REF SRM 51-42-06-001-001-A01, 51-42-21-000-001-A01.

Part: SKIN — CHAFED (RT WING) · airframe 28,577 hrs · 20,316 cycles

RT WING INBD L/E CHAFED. BLENDED CHAFED AREAS ON PANEL IAW SRM TR 51-00-50. BLENDED AREA IS OUT OF ALLOWABLE LIMITS IAW SRM 57-41-01-101-001-A01. RECEIVED AND COMPLIED WITH SECTION 1 PERMANENT REPAIR STS EA 32-2015-373 ALL STEPS COMPLETE. COMPLIED WITH ECTC EA 32-2015-373.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 27,122 hrs · 19,148 cycles

HOT ELECTRICAL ODOR IN COCKPIT & GALLEY DURING FLIGHT. INSPECTED COCKPIT/GALLEY AREA & PERFORMED, OPS CHECK OF ALL LIGHT/ELECTRICAL ACCESSORIES. NO ODOR OF SMOKE FOUND. EVERYTHING WORKED AS IT SHOULD WORK DONE IAW AMM 24-00-00. ALSO, OPERATED BOTH PACKS WITH NO ODOR OR PROBLEM AMM 21-00-00.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 27,021 hrs · 19,073 cycles

RT LOWER EXIT SIGN ON 12DC. TWO TOP LIGHT BULBS INSIDE EXIT SIGN BURNED. R & R BULBS IN LOWER EXIT SIGN ON 12D EXIT SIGN IAW GMM 3-8-01-03-2015.

Part: SEAL — DAMAGED (RT WING SLAT) · airframe 26,135 hrs · 18,408 cycles

RT WING INBD SLAT SEAL DAMAGED. REMOVED SEAL IAW AMM 57-42-07-000-802. INSTALLED NEW SEAL IAW AMM 57-42-07-400-802 AND SRM 51-42-13-001-001. MAJOR REPAIR.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 25,937 hrs · 18,261 cycles

PAX DOOR AFT DRAG ANGLE CRACKED NEXT TO PULLEY BRACKET. COMPLIED WITH REO 670-52-11-287, REV. C.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 25,779 hrs · 18,147 cycles

MAIN CABIN DOOR, INTERIOR OPENING HANDLE CRACKED AT MOUNT BOLT. R & R PAX DOOR PULL-IN HANDLE IAW AMM 52-11-02. MAJOR REPAIR.

Part: HINGE — GOUGED (PAX DOOR) · airframe 24,264 hrs · 17,069 cycles

GOUGES ON PAX DOOR LUGS AT NR 23, 25, 26 & 27. REMOVED GOUGES AND NDT INSPECTION PERFORMED IAW REO 670-52-11-511 AND EC/TC REO 670-52-11-511 REV A.

Part: ANGLE — CORRODED (BS 279) · airframe 24,264 hrs · 17,069 cycles

LEFT INBD SIDE OF COCKPIT DOOR CUTOUT AT FRAME BS 279 HAS A CORRODED ANGLE. REMOVED CORRODED ANGLE. FABRICATED ANGLE AND DOUBLER AND INSTALLED REPAIR PARTS IAW REO 670-53-11-745, REO DATED 20 OCT 2012.

Part: BULKHEAD — CORRODED (BS 280) · airframe 24,264 hrs · 17,069 cycles

RIGHT FS 280.0 BULKHEAD, AFT SIDE LOWER WEB IS CORRODED. R & R WEB AND SPLICE BY FABRICATING WEB AND SPLICE AND INSTALLING IAW REO 670-53-11-594, DATED 27 APR 2011 AND EC/TC REO 670-53-11-594 REV A.

Part: BULKHEAD — CORRODED (BS 280) · airframe 24,264 hrs · 17,069 cycles

LEFT FS 280.0 BULKHEAD, AFT SIDE LOWER WEB IS CORRODED. R & R WEB AND SPLICE BY FABRICATING WEB AND SPLICE AND INSTALLING IAW REO 670-53-11-594, DATED 27, APR 2011 AND ISSUED EC/TC REO 670-53-11-594, REV A.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 24,264 hrs · 17,069 cycles

RIGHT FLOOR SUPPORT AFT OF FS 280 CORRODED. R & R RT FLOOR SILL IAW SRM 51-40-11, 51-42-06, 51-42-10, 51-42-13, 51-42-15, 51-25-06, 51-25-16, 51-23-00, AND AMM 51-21-01.

Part: ANGLE — CRACKED (BS 280) · airframe 24,297 hrs · 17,094 cycles

LBL 17.46, BS 280 ANGLE CRACKED. R & R ANGLE IAW AMM 51-21-01, SRM 51-42-06, 51-40-11, AND 51-23-00.

Part: LIGHT — DAMAGED (CABIN) · airframe 24,297 hrs · 17,094 cycles

EMERGENCY LIGHTS NR 12, 9, RT 8 DAMAGED. R & R LIGHTS IAW AMM 33-51-01.

Part: ANGLE — CRACKED (BS 280) · airframe 24,297 hrs · 17,094 cycles

RBL 17.46, BS 280 ANGLE CRACKED. R & R ANGLE IAW AMM 51-21-01, 51-23-00, 51-42-06, 51-40-11.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 24,264 hrs · 17,069 cycles

LT FLOOR SEAT TRACK HAS MULTIPLE SPOTS OF CORROSION FROM BS 581 - 693. BLENDED SEAT TRACK IAW REO 670-53-00-013, REV F AND EC/TC REO 670-53-00-013, REV B.

Part: STRAP — CORRODED (BS 280) · airframe 24,297 hrs · 17,094 cycles

BS 280 FLOORBEAM, QUARTER TURN STRAP CORRODED. INSTALLED NEW STRAP IAW WITH SRM 51-42-06.

Part: BULKHEAD WEB — CORRODED (FUSELAGE) · airframe 24,297 hrs · 17,094 cycles

LEFT LOWER BULKHEAD CORRODED. R & R LT BULKHEAD WEB IAW REO 670-53-11-594.

Part: WEB — CORRODED (CABIN) · airframe 24,297 hrs · 17,094 cycles

RT WEB CORRODED AROUND FASTNERS. R & R RT WEB IAW REO 670-53-11-594.

Part: SEAT TRACK — CORRODED (BS 693-830) · airframe 24,297 hrs · 17,094 cycles

RT FLOOR SEAT TRACK HAS CORROSION IN MULTIPLE SPOTS FS 693-830. R & R SEAT TRACK IAW AMM 53-00-49.

Part: DOOR FRAME — CORRODED (COCKPIT DOOR) · airframe 24,297 hrs · 17,094 cycles

LEFT INBD SIDE OF COCKPIT DOOR CUTOUT AT FRAME 279 CORRODED. REPAIRED CORRODED AREA IAW REO 670-53-11-745.

Part: SILL — CORRODED (BS 280) · airframe 24,297 hrs · 17,094 cycles

RT SILL CORRODED, R & R RT SILL AFT AT BS 280 BEAM IAW SRM 51-42-13, 51-42-06, 51-42-15, 51-42-10, 51-40-11, 51-23-00 AMM 51-21-01.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 23,373 hrs · 16,411 cycles

NR 6 RT AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMPS IAW AMM 33-51-15, OPS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 23,153 hrs · 16,260 cycles

F/A FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW AMM 25-60-00.

Part: FLOORBEAM — CORRODED (BS 103) · airframe 19,280 hrs · 13,442 cycles

FLOORBEAM LBL 27, CORRODED AT APPROX FS 103.00. COMPLIED WITH STEPS 8-13 OF SRM CH 53-00-41-201-001, COMPLIED WITH ECTC REO 670-53-00-339 AND REO 670-53-61-782. MAJOR REPAIR

Part: BATTERY PACK — WEAK (EMERGENCY LIGHT) · airframe 19,280 hrs · 13,442 cycles

DURING OPS TEST OF THE EMERGENCY LIGHTS, FOUND THE EXIT LIGHTS TO GO DIM IN 5 SECONDS. FOUND ALL EPSU BATTERYS LOW AMPS, R & R SERVICABLE EPSU BATTERY PACK IAW AMM 33-51-17-000-801 AND 33-51-17-400-801. PERFORMED OPS TEST OF THE EMERGENCY POWER SUPPLY UNIT IAW AMM 33-51-17-710-801. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,280 hrs · 13,442 cycles

EMERGENCY LIGHTS INOPERATIVE. R & R BATTERY PACK IAW AMM TASKS 33-51-12-000(400)-801. COMPLY WITH OPS TEST OF THE EPSU IAW AMM TASK 33-51-17-710-801. DURING OPS TEST OF THE EMERGENCY LIGHT FOUND EXIT LIGHTS GO DIM IN 5 SECONDS. (CLOSED)

Part: FLOOR PANEL — CRACKED (E/E BAY) · airframe 19,268 hrs · 13,430 cycles

RIGHT FWD ELECTRICAL BAY FLOOR CRACKED JUST OTBD OF ADG STOW PUMP.

Part: FLOOR PANEL — CRACKED (E/E BAY) · airframe 19,268 hrs · 13,430 cycles

LEFT SIDE FWD ELECTRICAL BAY FLOOR CRACKED BELOW PARKING BRAKE ACCUMULATOR GAUGES FS 193. REPAIRED IAW AMM 32-43-30-400-801.

Part: INTERCOSTAL — DAMAGED (BS 364) · airframe 19,268 hrs · 13,430 cycles

INTERCOSTAL BETWEEN FS 349.00 AND 364 S26-27L HAS CORROSION DAMAGE.

Part: FLOORBEAM — CORRODED (BS 1031) · airframe 19,268 hrs · 13,430 cycles

FLOORBEAM LBL 27 CORRODED AT APPROX FS 1031. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00-101-001. REPAIRED IAW SRM 53-00-41-201-001.

Part: SILL — CORRODED (FUSELAGE) · airframe 19,268 hrs · 13,430 cycles

PAX DOOR LOWER SILL ANGLE CORRODED. REMOVED CORRODED SILL AND INSTALLED NEW IAW SRM 51-42-06-001-001.

Part: SEAT TRACK — CORRODED (BS 379-485) · airframe 19,268 hrs · 13,430 cycles

RT SIDE SEAT TRACK FROM FS 379-485 IS CORRODED. REMOVED SEAT TRACK AND INSTALLED NEW TRACK IAW AMM TASK 53-00-49-000-801.

Part: SEAT TRACK — CORRODED (BS 565-677) · airframe 19,268 hrs · 13,430 cycles

RT SIDE SEAT TRACK FROM FS 565-677 IS CORRODED. REMOVED SEAT TRACK IAW SRM 53-00-49-000-801-A03. INSTALLED NEW SEAT TRACK IAW SRM 51-41-02-001-001-A01 AND AMM 53-00-49-801-A03.

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 19,268 hrs · 13,430 cycles

FLOOR SEAT RAIL FROM FS 581.00-677.00, LBL 9.0 IS CORRODED. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801-A03.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 19,268 hrs · 13,430 cycles

STIFFNER CRACKED BOTTOM ASD MOTOR LOWER SIDE. REMOVED OLD STIFFNER IAW SRM 51-42-06. INSTALLED NEW STIFFNER IAW SRM 51-42-06-001-001-A01. MINOR REPAIR.

Part: CROSSBEAM — CORRODED (BS 280) · airframe 19,268 hrs · 13,430 cycles

LT FS280 CROSSBEAM CORRODED. CORROSION DAMAGE EXCEEDS ALLOWABLE LIMITS IAW SRM CH 53-00-00-101-001. REMOVED CROSSBEAM IAW SRM CH 51-42-06-001-001, 51-42-13-001-001, 51-42-21-001-001, 51-42-22-001-001. INSTALLED NEW CROSSBEAM IAW SRM 51-42-06, SRM 51-42-13 AND SRM 51-42-21.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 19,268 hrs · 13,430 cycles

SEAT TRACK FROM FS 485-581, RBL 9.0 IS CORRODED. REMOVED SEAT TRACK IAW AMM TASK 53-00-49-000-801. FABRICATED NEW SEAT TRACK IAW REO 670-53-00-335. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 565-677) · airframe 19,268 hrs · 13,430 cycles

LT SIDE SEAT TRACK FROM FS 565-677 IS CORRODED. REMOVED CORRODED SEAT TRACK AND INSTALLED NEW IAW AMM TASK 53-00-49-000-801.

Part: SEAT TRACK — CORRODED (BS 785.15-863) · airframe 19,268 hrs · 13,430 cycles

RIGHT SIDE SEAT TRACK FROM FS 785.15-863.00 IS CORRODED. REMOVED AND INSTALLED NEW TRACK IAW AMM 53-00-49-000-801.

Part: SEAT TRACK — CORRODED (BS 349-485) · airframe 19,268 hrs · 13,430 cycles

SEAT TRACK FROM FS 349.00-485.00 RBL 9.0 IS CORRODED. REMOVED CORRODED SEAT TRACK AND INSTALLED NEW TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 830.4-969) · airframe 19,268 hrs · 13,430 cycles

LT AFT SEAT TRACK AT APROX FS 830.4-969 CORRODED. REMOVED AND INSTALLED NEW IAW AMM 53-00-49-000-801.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 19,268 hrs · 13,430 cycles

SEAT TRACK FROM FS 485-581, RBL 9.0 IS CORRODED. REMOVED SEAT TRACK IAW AMM TASK 53-00-49-000-801. FABRICATED NEW SEAT TRACK IAW REO 670-53-00-335. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 863-977) · airframe 19,268 hrs · 13,430 cycles

LT SIDE SEAT TRACK FROM FS 863-977 IS CORRODED. REMOVED AND INSTALLED NEW TRACK IAW AMM TASK 53-00-49-000-801.

Part: FLOOR SUPPORT — CRACKED · airframe 19,268 hrs · 13,430 cycles

FLOOR SUPPORT ANGLE AT PAX DOOR IS CRACKED. FLOOR SUPPORT ANGLE BEYOND LIMITS IAW SRM. REMOVED AND REPLACED FLOOR SUPPORT MID CAP ANGLE AT PAX DOOR IAW SRM 51-41-02-001-001-A01. MINOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 785.15-863) · airframe 19,268 hrs · 13,430 cycles

LT SIDE SEAT TRACK FROM FS785.15-863.00 IS CORRODED. REMOVED AND INSTALLED NEW TRACK IAW AMM 53-00-49-000-801.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 19,268 hrs · 13,430 cycles

PAX DOOR DRAG ANGLE CRACKED AFT SIDE. INSTALLED DRAG ANGLE REPAIR IAW SRM 52-11-04-201-002-A01.

Part: SEAT TRACK — CORRODED (BS 677-708) · airframe 19,268 hrs · 13,430 cycles

LT SIDE SEAT TRACK FROM FS 677.00-708.00 IS CORRODED. REMOVED AND INSTALLED NEW TRACK IAW AMM 53-00-49-000-801.

Part: SEAT TRACK — CORRODED (BS 463.977) · airframe 19,268 hrs · 13,430 cycles

RT SIDE SEAT RAIL FROM FS 463.00-977.00 IS CORRODED. REMOVED AND INSTALLED NEW TRACK IAW AMM 53-00-49-000-801.

Part: SEAT TRACK — CORRODED (BS 708-761.85) · airframe 19,268 hrs · 13,430 cycles

LT SIDE SEAT TRACK FROM FS 708-761.85 IS CORRODED. REMOVED AND INSTALLED NEW TRACK IAW AMM TASK 53-00-49-000-801.

Part: SILL — CORRODED (FUSELAGE) · airframe 19,268 hrs · 13,430 cycles

SERVICE DOOR SILL IS CORRODED IN MULTIPLE AREAS. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION OF BLEND AREAS IAW MAC NDT INSPECTION PROCEDURE UT-3 MIN MATERIAL REMAINING IS .035". BLENDED AREA IS OUT OF LIMITS IAW SRM 53-21-23-101-002-A01. R & R SERVICE DOOR SILL ANGLE IAW SRM 51-42-06-001-001 AND 51-42-21-001-001. THIS IS A MINOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 379-485) · airframe 19,268 hrs · 13,430 cycles

LT SIDE SEAT TRACK FROM FS 379.00-485.00 IS CORRODED. REMOVED SEAT TRACK AND INSTALLED NEW TRACK IAW AMM TASK 53-00-49-000-801.

Part: SEAT TRACK — CORRODED (BS 379) · airframe 19,268 hrs · 13,430 cycles

SEAT TRACK AT FS 379.00 LBL 9.0 IS CORRODED ON FWD SIDE. REMOVED SEAT TRACK AND INSTALLED NEW TRACK IAW AMM 53-00-49-000-801.

Part: SEAT TRACK — CORRODED (BS 708-761) · airframe 19,268 hrs · 13,430 cycles

RT SIDE SEAT RAIL FROM FS 708.00-761.85 IS CORRODED. REMOVED SEAT TRACK IAW SRM 51-41-02-001-001. FABRICATED NEW SEAT TRACK IAW REO 670-53-00-335 AND INSTALLED IAW AMM 53-00-49-400-801.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 19,268 hrs · 13,430 cycles

RT FS 280 CROSSBEAM CORRODED. CORROSION DAMAGE EXCEEDS ALLOWABLE LIMITS IAW SRM 53-00-00-101-001. REMOVED CROSSBEAM IAW SRM CH 51-42-06-001-001, 51-42-13-001-001, 51-42-21-001-001, 51-42-22-001-001. AND INSTALLED NEW CROSSBEAM SRM 51-42-06, SRM 51-42-13 AND SRM 51-42-21.

Part: SEAT TRACK — CORRODED (BS 677-708) · airframe 19,268 hrs · 13,430 cycles

RT SIDE SEAT RAIL FROM FS 677.00-708.00 IS CORRODED. REMOVED SEAT TRACK IAW SRM 53-00-49-000-801-A03. FABRICATED NEW SEAT TRACK IAW REO 670-53-00-335. INSTALLED SEAT TRACK IAW SRM 51-41-02-001-001-A01 AND AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 485-565) · airframe 19,268 hrs · 13,430 cycles

LT SIDE SEAT TRACK FROM FS 485-565 IS CORRODED. REMOVED SEAT TRACK IAW IAW 51-41-02-001-001. INSTALLED SEAT TRACK SECTION IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 830.4-969) · airframe 19,268 hrs · 13,430 cycles

RT AFT SEAT TRACK AT APROX FS 830.40-969 NICKED AND CORRODED. REMOVED AND INSTALLED NEW TRACK IAW AMM 53-00-49-000-801.

Part: SEAT TRACK — CORRODED (BS 485-565) · airframe 19,268 hrs · 13,430 cycles

RT SIDE SEAT TRACK FROM FS 485-565 IS CORRODED. REMOVED SEAT TRACK AND INSTALLED NEW IAW SRM IAW AMM 53-00-49-000-801.

Part: FLOOR PANEL — CRACKED (E/E BAY) · airframe 19,268 hrs · 13,430 cycles

LT SIDE FWD ELECTRICAL BAY FLOOR CRACKED BELOW PARKING BRAKE ACCUM GAUGES FS 193. REPAIRED REO 670-53-11-509.

Part: STRUCTURE — CRACKED (BS 193) · airframe 19,268 hrs · 13,430 cycles

RT SIDE FWD ELECTRICAL BAY FLOOR CRACKED JUST OTBD OF ADG STOW PUMP AT FS 193. REPAIRED IAW REO 670-53-11-509.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 19,268 hrs · 13,430 cycles

INTERCOSTAL BETWEEN FS 349.00 AND FS364.00 FRAMES STR 26 - 27L HAS CORROSION DAMAGE. REMOVED SURFACE CORROSION IAW SRM 51-21-00. R & R INTERCOSTAL IAW 51-42-06.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 19,268 hrs · 13,430 cycles

MAIN AVIONICS BAY CRAWLWAY FLOORBOARD 141ALF FLOORBEAM ON FS 280 FRAME CORRODED. R & R WITH NEW SERVICABLE FLOORBEAM IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-45-00-001-001-A01. THIS IS A MINOR REPAIR.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 18,043 hrs · 12,584 cycles

1 INTERIOR EMERGENCY LIGHT BULBS INOP. AT ENTRY WAY AND RT EMERGENCY EXIT. RELAMPED INTERIOR EMERGENCY LIGHTS AT ENTRY WAY AND RT EMERGENCY EXIT IAW AMM 33-51-11 ITEM: 1.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 17,237 hrs · 12,027 cycles

MEGA PHONE INOP. REMOVED AND REPLACED WITH NEW MEGAPHONE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 16,977 hrs · 11,857 cycles

EXTERIOR EMERGENCY LIGHT (DS56) INOP. R & R LAMP IN EXTERIOR EMERGENCY LIGHT (DS56) IAW AMM 33-51-15.

Part: PLACARD — PEELING (CABIN) · airframe 16,643 hrs · 11,613 cycles

PAX DOOR EXIT PLACARD PEELING. R & R PAX DOOR EXIT PLACARD IAW AMM 11-30-02. R & R PAX DOOR EXIT PLACARD IAW AMM 11-30-02.

Part: SWITCH — OUT OF ADJUST (FLASHLIGHT) · airframe 16,356 hrs · 11,398 cycles

FLASHLIGHT SWITCH BROKEN, FLASHLIGHT WILL NOT STAY ON. ADJUSTED CAPT FLASHLIGHT SWITCH AS REQUIRED IAW AMM 25-61-00. OPS CHECK GOOD ACFT OK FOR SERVICE. (CLOSED)

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 15,937 hrs · 11,070 cycles

MAIN CABIN INTERIOR; LOWER OVERWING EMERGENCY RT SIDE, HAS 2 EACH BULB INOP. RELAMPED RT SIDE LOWER OVERWING EMERGENCY LIGHT, OPS CHECKED GOOD IAW AMM CHAP 33-24-07.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 15,937 hrs · 11,070 cycles

MAIN CABIN INTERIOR LOWER OVERWING EMERGENCY LIGHT, HAS 1 EACH BULB INOP. RELAMPED LT LOWER OVERWING EMERGENCY LIGHT OPS CHECKED GOOD IAW AMM CHAP 33-24-07.

Part: HEATER — SPARKS (COCKPIT WINDOW) · airframe 15,911 hrs · 11,048 cycles

F/O'S WINDSHIELD BEGAN SPARKING IN FLIGHT. TURNED OFF RT WINDSHIELD HEAT AND CONTINUED. BURN MARK VISIBLE AT CTR BOTTOM EDGE. ( WINDSHIELD AND SIDE WINDOW ANTI-ICE CONTROLLERS - ONE ) R & R F/O SIDE WINDSHIELD IAW AMM 56-11-01. OPS CHECK. NO DEFECTS NOTED. (CLOSED)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,538 hrs · 10,765 cycles

AFT MOST CABIN CEILING EMERGENCY LIGHT INOP. R & R AFT CEILING EMERGENCY FLOODLIGHT IAW AMM 33-51-09. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,753 hrs · 10,182 cycles

FORWARD MOST CABIN CEILING EMERGENCY LIGHT INOP.

Part: SIGN — DAMAGED (CABIN) · airframe 14,574 hrs · 10,045 cycles

EXIT SIGN ON AIR STAIRS UNLEDGIBLE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,479 hrs · 9,973 cycles

CEILING EMERGENCY LIGHTS DS145 AND DS146 ARE INOP.

Part: STIFFENER — CRACKED (BS 280) · airframe 14,479 hrs · 9,973 cycles

RBL 26.0 FS280 BULKHEAD WEB STIFFENER IS CRACKED AT VERY BOTTOM HOLE. CUT OUT DAMAGE TO STIFFENER PER 51-71-59-001-001-A01. FABRICATED PARTS PER SRM 51-71-59-001-001-A01 ALODINED, PRIMED & TOP COATED PER AMM 51-21-01-380-801-A01, SRM 51-25-06-001-001-A01 & 51-25-16-001-001-A01. INSTALLED REPAIR PANELS PER SRM 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 349) · airframe 14,479 hrs · 9,973 cycles

SEAT TRACK RAIL CORRODED AT NR 2 GALLEY INBD MOUNT AREA-FS 349.0.

Part: SEAT TRACK — CORRODED (BS 581-684) · airframe 14,479 hrs · 9,973 cycles

REPLACE RT CTR SEAT TRACK FROM FS 581 TO 684.00. DUE TO CORROSION ON SEAT TRACK. REMOVED RT CENTER SEAT TRACK PER MM 53-00-49-000-801. LOCATED & DRILLED RT CENTER SEAT TRACK PER SRM 51-40-11-001-001-A01. COUNTERSUNK RT CENTER SEAT TRACK PER SRM 51-40-11-001-001-A01. INSTALLED RT CENTER SEAT TRACK PER MM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 14,479 hrs · 9,973 cycles

REMOVED AND REPLACE RT CTR SEAT TRACK FROM STA485 TO FS STA581. DUE TO CORROSION ON SEAT TRACK.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 14,479 hrs · 9,973 cycles

LT FS280 FLOORBEAM HAS CORROSION AROUND NUTPLATE LOCATION AT APPROX LBL15.

Part: SEAT TRACK — CORRODED (BS 485-693) · airframe 14,479 hrs · 9,973 cycles

RIGHT CENTER SEAT TRACK HAS CORROSION FROM BS 485.00 TO BS 693.00 AREAS MARKED. WORK PERFORMED ON CARDS 7113811 OPS 75, 191, 192.

Part: FRAME — CRACKED (FUSELAGE) · airframe 14,479 hrs · 9,973 cycles

RT LWR TRANSCOWL INBD A FRAME CRACKED.

Part: SEAT TRACK — CORRODED (BS 379-693) · airframe 14,479 hrs · 9,973 cycles

LEFT CENTER SEAT TRACK HAS CORROSION FROM FS STA 379.00 TO FS 693.00 AREAS MARKED. REMOVED LT CTR SEAT TRACKS (3 EACH) FROM STA 349.00 TO STA 693.00 IAW MM 53-00-49-000-801. LOCATED, DRILLED, AND COUNTERSUNK LT CTR SEAT TRACKS NR 1 AND NR 2 IAW SRM 51-40-11-001-001-A01. LOCATED, DRILLED, AND COUNTERSUNK LT CTR SEAT TRACK NR 3 SRM 51-40-11-001-001-A01. INSTALLED LT CTR SEAT TRACKS (3 EACH) FROM BS 349.00 TO BS 693.00 IAW MM 53-00-49-400-801.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 14,479 hrs · 9,973 cycles

COCKPIT FLOORBEAM IS CORRODED AND REQUIRES REPLACEMENT. REMOVED RT & LT FS 280 DIAGONAL BRACKETS PER SRM 51-42-21-001-001-A01 & 51-42-22-001-001-A01. NO DEFECTS NOTED. REMOVED DAMAGED COCKPIT FLOORBEAM PER SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 & 51-42-22-001-001-A01. DRILLED NEW COCKPIT FLOOR SUPPORT PER 51-40-11-001-001-A01. INSTALLED NEW COCKPIT FLOORBEAM IAW SRM 51-42-21-001-001-A01 & SRM 51-42-06-001-001-A01. REINSTALLED RT FS 280 DIAGONAL BRACKET IAW SRM 51-42-21-001-001-A01 & 51-42-22-001-001-A01. REINSTALLED LT FS 280.0 DIAGONAL BRACKET IAW SRM 51-42-21-001-001-A01 & 51-42-22-001-001-A01.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,475 hrs · 9,971 cycles

SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOP.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 14,479 hrs · 9,973 cycles

RT FS 280 FLOORBEAM HAS CORROSION AROUND NUTPLATE LOCATION AT APPROX RBL 22. REMOVED AFT COCKPIT FLOORBEAM IAW SRM 51-42-21. GVI PERFORMED NO DEFECTS NOTED. LOCATED AND DRILLED NEW RT FLOORBEAM IAW REO 670-53-11-047 REV E DATED 2009-03-13. P.RICE 09-19-09. (55) 17. PERFORMED ET INSPECTION PER REO 670-53-11-047 REV E DATE 8/13/09 IAW NDTM 51-20-006. NO DEFECTS NOTED. INSTALLED RT FLOORBEAM IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 AND 51-42-13-001-001-A01.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 13,776 hrs · 9,422 cycles

LEFT FADEC CAUTION MESSAGE. DIVERTED TO SYR FROM YUL. COMPLIED WITH QRH [EMERGENCY DECLARED]. FLT 5161 DEL 352 MINS.

Part: LIGHT — UNKNOWN (CABIN) · airframe 12,444 hrs · 8,404 cycles

OVERHEAD EMERGENCY LIGHT ROW 4.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 11,244 hrs · 7,514 cycles

GALLEY/ENTRANCE HAS SEVERAL EMERGENCY LIGHT BULBS OUT. REMOVED AND REPLACED GALLEY/ENTRANCE FLOOR LEVEL EMERGENCY FLOOD LIGHT BULBS. OPS CHECK GOOD. (B)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,854 hrs · 7,236 cycles

LEFT AFT MOST EXTERNAL EMERGENCY LIGHT INOP.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 10,157 hrs · 6,755 cycles

FS 280 FWD FLOOR SUPPORT ANGLE IS CORRODED.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 10,157 hrs · 6,755 cycles

FS 280 FWD FLOOR SUPPORT ANGLE IS CORRODED.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 10,157 hrs · 6,755 cycles

FS 280 CROSSBEAM IS CORRODED. BLENDED CORROSION ON RT SIDE CROSSBEAM WITHIN LIMITS OF REO 670-53-11-046, RESTORED SURFACE FINISH PER CRJ700 SRM 51-25-00. REMOVED AND REPLACED LT SIDE 280 CROSSBEAM DUE TO OUT OF LIMITS CORROSION AS PER IS67053110026. ALL WORK ACCOMPLISHED ON ATTACHED M-234 PGS 1 THRU 4. SUPPLEMENTAL SDR CLOSED 1/4/08.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 10,127 hrs · 6,730 cycles

MOST FORWARD STRIP OF PHOTO ILLUMINICENT EMERGENCY LIGHT ON FLOOR DOES NOT ILLUMINATE (MISSING).

Part: PLATE — CRACKED (RT WING) · airframe 9,057 hrs · 5,972 cycles

LEFT TELESCOPE DUCT CLOSING PLATE CRACKED (LT OR RT WING SLAT CLOSING PLATES). 10-18-07 INSTALLED NEW ANT-ICE TELESCOPIC DUCT CLOSING PLATE IAW CRJ 700 AMM 57-40-01. OPS CK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,503 hrs · 5,584 cycles

FWD EXT EMERGENCY LIGHTS AND INTERNAL PAX DOOR AND SERVICE DOOR EMERGENCY EXIT LIGHTS INOP.

Part: STEP — CRACKED (AIRSTAIR DOOR) · airframe 8,303 hrs · 5,436 cycles

ASD BOTTOM STEP CRACKED.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 8,138 hrs · 5,330 cycles

FORWARD BULKHEAD EXIT SIGN INOP. FLTS 4536, 4781 CX.

Part: SLAT SYSTEM — FAILED (LE SLATS) · airframe 7,885 hrs · 5,152 cycles

ON APPROACH, RECEIVED SLATS FAIL MSG, EMERGENCY DECLARED, FLT 4147 DEL 26 MINS.

Part: PLACARD — WORN (AIRSTAIR DOOR) · airframe 7,410 hrs · 4,827 cycles

ASD -EXIT- PLACARD WORN.

Part: ANGLE — CRACKED (PAX DOOR) · airframe 7,410 hrs · 4,827 cycles

ASD AFT WALL LOWER ANGLE CRACKED.

Part: BULKHEAD — CORRODED (BS 280) · airframe 7,410 hrs · 4,827 cycles

THE 280 BULKHEAD WEB CORRODED - BL13-16 RT - FLOOR LEVEL. RT SIDE 280 BULKHEAD WEB ALSO FOUND CORRODED AFTER REMOVAL OF 280 FRAME, REMOVED CORROSION FROM RT AND LT WEB, REQUIRES THICKNESS CHECK. ALL WORK IAW REO 670-53-11-052 AJ21906. COMPLIED WITH EO700-53-0062 REPAIR 2: WEB REPLACEMENT.(CLOSED 11/27/06)

Part: FRAME — CRACKED (BS 280) · airframe 7,410 hrs · 4,827 cycles

UPPER LEG 280 FRAME CRACKED - RT BL9. COMPLIED WITH EO 700-53-0061. COMPLIED WITH EO700-53-0054 01 AND ISMODSUM IS67053110026 REV B-1. JOB COMPLETE.(CLOSED 11/27/06)

Part: DRAG ANGLE — CRACKED (STAB TO FUSE) · airframe 7,410 hrs · 4,827 cycles

LEFT SIDE VERTICAL STAB-TO-FUSELAGE DRAG ANGLE CRACKED (MARKED). REPAIRED IAW ALL SRM`S AND MM`S. (CLOSED)

Part: FRAME — CRACKED (BS 280) · airframe 7,410 hrs · 4,827 cycles

THE 280 FRAME CRACKED - UPPER LEG LT BL9. COMPLIED WITH EO 700-53-0061. COMPLIED WITH EO700-53-0054 01 AND ISMODSUM IS67053110026 REV B-1. JOB COMPLETE. (CLOSED 11/27/06)

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 7,294 hrs · 4,755 cycles

EMERGENCY LIGHTS CYCLE ON AND OFF SWITCH IN ARM LOCATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,148 hrs · 4,664 cycles

EMERGENCY LIGHT ABOVE ROW 2 INOP.

Part: SIGN — INOPERATIVE (CABIN) · airframe 6,345 hrs · 4,184 cycles

RIGHT OVERWING DOOR LWR EMER EXIT SIGN HAS 2 LIGHTS INOP. (CLOSED)

Part: PLACARD — WORN (CABIN) · airframe 5,690 hrs · 3,757 cycles

A/S/D EXIT AND OPEN PLACARD'S WORN

Part: UNKNOWN — ODOR

DURING CRUISE, THE CREW REPORTED A SMELL, LIKE RUBBER OR OIL, COMING FROM THE RT PACK AT ROW 1 AND 2. THE AIRCRAFT LANDED SAFELY. MAINTENANCE RAN THE RT PACK ON THE APU AND ENGINE BLEED WITH NO DEFECTS NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: STEP — CRACKED (PAX DOOR)

DURING A C-CHECK IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE BOTTOM STEP ON THE PASSENGER DOOR. (M)

Part: WARNING LIGHT — ILLUMINATED (MLG)

DURING TAKEOFF FROM SAT-DFW, THE CREW RECEIVED A GEAR DISAGREE WARNING AFTER SELECTING THE GEAR UP POSITION. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED TO SAT, LANDING SAFELY. MAINTENANCE FOUND MAINTENANCE DIAGNOSTIC COMPUTER (MDC)FAULTS FOR ALL THREE GEAR UPLOCK FAR. MAINTENANCE PERFORMED TWENTY GEAR SWINGS AND ALSO INPECTED THE DOWN AND UPLOCKS, GEAR SELECTOR VAVLE, ELECTRICAL AND HYDRAULIC CONNECTIONS FOR SECURITY. NO DEFECTS WERE NOTED. THE MDC SHOWED NO FURTHER FAULTS IN OPERATION. AIRCRAFT OK FOR SERVCE. (M)

Part: WARNING LIGHT — ILLUMINATED (MLG)

DURING TAKEOFF, THE CREW RECEIVED A GEAR DISAGREE WARNING AFTER SELECTING THE GEAR UP POSISTION. THE QRH WAS COMPLIED WITH AND AN EMERGENCY DECLARED. THE AIRCRAFT RETURNED AND LANDED SAFELY. MAINT FOUND MAINTENANCE DIAGNOSTIC COMPUTER (MDC) FAULTS FOR ALL THREE GEAR UPLOCK FAR. MAINT PERFORMED TWENTY GEAR SWINGS AND ALSO INSPECTED THE DOWN AND UPLOCKS, GEAR SELECTOR VALVE, ELECTRICAL AND HADRAULIC CONNECTIONS FOR SECURITY. NO DEFECTS WERE NOTED. THE MDC SHOWED NO FURTHER FAULTS IN OPERATION. AIRCRAFT OK FOR SERVICE.