N760EV

Part: WINDOW — CRACKED (ZONE 200) · airframe 39,608 hrs · 29,006 cycles

CREW REPORTS DURING DEPARTURE FO WINDOW SHATTERED. (FLIGHT 6363) REMOVED AND REPLACED THE FO SIDE WINDOW WITH A SERVICABLE UNIT IAW WORK CARD 56-220-1000 . OPS CK GOOD.

Part: WINDSHIELD — FAILED (ZONE 200) · airframe 39,461 hrs · 28,889 cycles

FO WINDSHIELD SHATTERED AT FL340, RAN QRH, NO LOSS OF CABIN PRESSURE. DIVERTED TO DEN LANDED WITH NO OTHER ISSUES (FLIGHT 6203 - FILED OPEN)

Part: WINDSHIELD — CRACKED (ZONE 200) · airframe 39,471 hrs · 28,897 cycles

FO WINDSHIELD SHATTERED AT FL340, RAN QRH, NO LOSS OF CABIN PRESSURE. DIVERTED TO DEN LANDED WITH NO OTHER ISSUES (FLIGHT 6203) REMOVED AND REPLACED FO WINDSHIELD IAW AMM 56-11-01 COMPLIED WITH TASK CARD 56-220-1000-SKY OPS CHECKS GOOD WITH NO LEAKS NOTED.

Part: SINK — CLOGGED (ZONE 900) · airframe 39,315 hrs · 28,780 cycles

LAV TOILET AND SINK STOPPED WORKING MID FLIGHT W/ASSOCIATED ELECTRICAL SMELL IN CABIN. SMELL WENT AWAY AFTER A COUPLE OF MINUTES (FLIGHT 6384) PLEASE REFERENCE AML 1734688. PLEASE REFERENCE AML 1734705.OPS CHECK OF AFT LAV TOILET PER CRJ 700 AMM 38-31-00. OPS CHECK GOOD AT THIS TIME. NO HISTORY. UNABLE TO DUPLICATE ISSUE.

Part: ANGLE — OUT OF ALIGNMENT (ZONE 100) · airframe 39,207 hrs · 28,700 cycles

WHILE PERFORMING SB 670BA-53-036/670SH53-042 FOUND PILOT HOLES IN NEW SERVICEABLE L/H 36 BEAM MISALIGN WITH EXISTING FASTENER HOLES IN L/H SEAL ANGLE AT F.S.693 REQUIRING REPLACEMENT OF SEAL ANGLE. (C-CHECK RO 10/06/2025) INSTALLED NEW SERVICEABLE SEAL ANGLE AT L/H F.S. 693 P/N SH670-35940-3 IAW CRJ 700 SRM 51-42-06-001-001-A01 LOCATED AND DRILLED UP NEW SERVICEABLE L/H F.S. 693 SEAL ANGLE P/N SH670-35940-3 IAW CRJ 700 SRM 51-40-11-001-001-A01. EDGE SEALED AND PAINTED ANGLE O/B OF LBL36 BEAM @FS693 IAW CRJ700 SRM 51-23-00-001-001-A01 AND CRJ700 SRM 51-25-16-001-001-A01. PERFORMED PRESSURE LEAK CHECK IAW CTJ 700 SRM 51-23-03-001-001-A01. LEAK CHECK GOOD AND COMPLIED WITH 51-900-1002-SKY (CL600-2C10)

Part: BEAM — DAMAGED (ZONE 200) · airframe 39,207 hrs · 28,700 cycles

WHILE PERFORMING SB 670BA-53-036/670SH53-042 WE FOUND THE LBL 9 BULKHEAD BEAM @ FS 693 TO HAVE AN EXISTING REPAIR ON BOTH THE INBOARD AND OUTBOARD FLANGES. ENGINEERING REQUIRED. (C-CHECK RO 10/06/2025)COMPLIED WITH MJIRJ REO 670-53-41-760 REPAIR FOR REDUNDANT HOLES TO LBL9.00 BULKHEAD BEAM BETWEENFS685.550-FS697.45 (DEVIATION TO SB 670SH-53-042 REV.-C) DATED 2025-09-12 AND 51-900-1002-SKY (CL600-2C10)

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 39,203 hrs · 28,696 cycles

MAIN CABIN LBL 9 SEAT TRACK SUPPORT BEAM SHOW CORROSION FROM FS 813.00 TO FS 847.00 (C-CHECK RO 08/11/2025)COMPLIED WITH REO 670-53-41-741 FOR REPAIR OF THE LBL9 SEAT TRACK SUPPORT BEAM

Part: ROLLER — OUT OF LIMITS (SLAT TRACK) · airframe 39,203 hrs · 28,696 cycles

SLAT TRAC 2-2 ROLLER OUT BOARD AND IN BOARD WERE FOUND IN BAD CONDITION. (C-CHECK RO 08/11/2025)REMOVED AND REPLACED SLAT TRACK 2-2 OUTBD FWD, AND INBD AFT ROLLERS IAW CRJ 700 AMM 27-81-44-400-802-A01 OPS CHECK GOOD. NO FURTHER ACTION IS REQUIRED.

Part: ROLLER — OUT OF LIMITS (SLAT TRACK) · airframe 39,203 hrs · 28,696 cycles

SLAT TRAC 1-2 ROLLER OUT BOARD WERE FOUND IN BAD CONDITION. (C-CHECK RO 08/11/2025)REMOVED AND REPLACED SLAT TRACK 1-2 OUTBD FWD, AND OUTBD AFT ROLLERS IAW CRJ 700 AMM 27-81-44-400-801-A01 OPS CHECK GOOD. NO FURTHER ACTION IS REQUIRED.

Part: ROLLER — OUT OF LIMITS (SLAT TRACK) · airframe 39,203 hrs · 28,696 cycles

SLAT TRAC 3-2 ROLLER OUT BOARD WERE FOUND IN BAD CONDITION. (C-CHECK RO 08/11/2025)REMOVED AND REPLACED SLAT TRACK 3-2 OUTBD FWD ROLLER IAW CRJ 700 AMM 27-81-44-400-803-A01 OPS CHECK GOOD. NO FURTHER ACTION IS REQUIRED.

Part: SLAT TRACK — CRACKED (RT WING) · airframe 35,540 hrs · 25,964 cycles

RT WING 1-3 SLAT TRACK CANISTER BRACKET IS CRACKED. C-CHECK RO 12/04/2020. REPLACED RT WING 1-3 CRACKED SLAT TRACK CANISTER BRACKET WITH A SERVICEABLE UNIT, REF REO. COMPLIED WITH TASK CARD. LEAK CHECK OF THE REPAIR AREA CHECKED GOOD, SEE CONTINUATION CARD FOR DETAILS.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 35,540 hrs · 25,964 cycles

CORROSION DETECTED ON RT SEAT SIDE RAIL "TRACK" THAT SPANS FROM FS 482.50 TO FS 572.50, IN SEVERAL PLACES, MARKED. C-CHECK RO 12/04/2020. INSTALLED NEW RT SEAT SIDE RAIL "TRACK" THAT SPANS FROM FS 482.50 TO FS 572.50, REF CRJ-700 AMM.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 35,540 hrs · 25,964 cycles

CORROSION DETECTED ON LT SEAT SIDE RAIL "TRACK" THAT SPANS FROM FS 572.50 TO FS 674.50 AT 8 EA PLACES, MARKED. C-CHECK RO 12/04/2020. REPLACED SEAT TRACK LOCATED AT APPROXIMATELY FS 572.50-FS 674.50 WITH FABRICATED, REF CRJ-700 AMM. TUC7824 30-JUN-21.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 35,540 hrs · 25,964 cycles

CORROSION DETECTED AND "GOUGES" WITH HIGH METAL ON LT SEAT SIDE RAIL "TRACK" THAT SPANS FROM FS 377.50 TO FS 482.50 IN NUMEROUS LOCATIONS. THIS SECTION OF TRACK HAS EVIDENCE OF PREVIOUS REWORK, MARKED. C-CHECK RO 12/04/2020. REPLACED WITH FABRICATED SEAT TRACK ON LT SEAT SIDE RAIL THAT SPANS FROM FS 377.50 TO FS 482.50, IAW CRJ 700 AMM. TORQUE WRENCH TUC 5658 DUE DATE 31-JUL-21.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 35,540 hrs · 25,964 cycles

CORROSION DECTECTED AND "GOUGES" WITH HIGH METAL ON RT SEAT SIDE RAIL "TRACK" THAT SPANS FROM FS 377.50 TO FS 482.50 IN NUMEROUS LOCATIONS. THIS SECTION OF TRACK HAS EVIDENCE OF PREVIOUS REWORK, MARKED. C-CHECK RO 12/04/2020. INSTALLED NEW RT SEAT SIDE RAIL "TRACK" THAT SPANS FROM FS 377.50 TO FS 482.50, REF: CRJ-700 AMM.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 35,540 hrs · 25,964 cycles

CORROSION DETECTED ON LT SEAT SIDE RAIL "TRACK" THAT SPANS FROM FS 482.50 TO FS 572.50 IN 7 PLACES, MARKED. C-CHECK RO 12/04/2020. REPLACED LT SIDE SEAT TRACK LOCATED FROM FS 482.5 TO 572.5 WITH FABRICATED TRACK, IAW CRJ 700 AMM. SEE CONTINUATION CARD FOR DETAILS.

Part: STRIKER — CORRODED (SERVICE DOOR) · airframe 35,540 hrs · 25,964 cycles

CORROSION DETECTED ON SERVICE DOOR SURROUND STRUCTURE, LOWER SEAL "STRIKER" BETWEEN FS 319.70 AND FS 349.00. AREAS ARE LOCATED AT FASTENER HOLES FOR GALLEY FLOOR PROTECTOR, MARKED. C-CHECK RO 12/04/2020. REMOVED AND REPLACED NEW FITTING SEAL STRIKE P/N SH670-31412-5 ON SERVICE DOOR SURROUND STRUCTURE, REF CRJ700 SRM AND DWG LEAK CHECK GOOD.

Part: DOOR SILL — CORRODED (ZONE 200) · airframe 35,540 hrs · 25,964 cycles

CORROSION DETECTED ON RT FLOOR SILL, JUST (AFT) OF SERVICE DOOR SURROUND STRUCTURE AT FS 349.00, MARKED. C-CHECK RO 12/04/2020. CUT OUT DAMAGED SECTION OF RT FLOOR SILL JUST AFT OF SERVICE DOOR SURROUND STRUCTURE AT FS 349.00. FABRICATED AND INSTALLED REPAIR PARTS, REF REO. COMPLIED WITH SW TASK. LEAK CHECK GOOD. SEE CONTINUE CARD FOR DETAILS.

Part: STRINGER — CRACKED (ZONE 200) · airframe 35,540 hrs · 25,964 cycles

LINTEL, STGR 3L, IS CRACKED AT FS 280-FS 282 JOINT. C-CHECK RO 12/04/2020. REPAIRED CRACKED LINTEL, STGR 3L, AT FS 280-FS 282 JOINT, REF CRJ 700 SRM. COMPLIED WITH SW TASK CARD. LEAK CHECK GOOD. SEE CONTINUE CARD FOR DETAILS.

Part: SKIN — CORRODED (LOWER FUSELAGE) · airframe 35,540 hrs · 25,964 cycles

CORROSION DETECTED ON BELLY SKIN AT LOWER TCAS OMNIDIRECTIONAL ANTENNA CUT-OUT, MARKED. C-CHECK RO 12/04/2020. CUT OUT DAMAGED AREA ON BELLY SKIN AT LOWER TCAS OMNIDIRECTIONAL ANTENNA. FABRICATED AND INSTALLED REPAIR DOUBLER, REF REO. COMPLIED WITH SW TASK CARD. LEAK CHECK GOOD. BONDING CHECK GOOD.

Part: FRAME ANGLE — CORRODED (ZONE 100) · airframe 35,540 hrs · 25,964 cycles

CLIP FOR FRAME FS 265 AT STGR 27 HAS CORROSION. C-CHECK RO 12/04/2020. REPLACED CLIP FOR FRAME FS 265 AT STGR 27, REF CRJ700 SRM.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 35,540 hrs · 25,964 cycles

COCKPIT FLOORBEAM, LBL 12, ATTACH FLANGE AT FS 280 HAS A SUSPECTED CRACK IN THE RADIUS NEAR WL 72.10. C-CHECK RO 12/04/2020. REMOVED AND REPLACED DAMAGED COCKPIT FLOORBEAM, LBL 12, APPROXIMATELY FS 272-280, WITH NEW P/N 690-53-11-228-003, IAW CRJ 700 SRM. COMPLIED WITH TASK CARD.

Part: FASTENER — DAMAGED (ZONE 100) · airframe 35,540 hrs · 25,964 cycles

EXTERNAL FASTENER DAMAGE INTO BASE METAL RESEMBLING A DRILL START IN DOUBLER REPAIR AT FS 977 AND STGR 27. C-CHECK RO 12/04/2020. REMOVED OLD REPAIR DOUBLER AND INSTALLED NEW REPAIR AT FS 977.00 STGR 27, PER REO. COMPLIED WITH TASK CARD. PRESSURIZED LEAK CHECK GOOD, REF CRJ-700 AMM.

Part: GUSSET — CORRODED (ZONE 200) · airframe 35,540 hrs · 25,964 cycles

GUSSET ON FRAME FS 349, AT THE UPPER TENSION TIE BUTTON, HAS CORROSION. C-CHECK RO 12/04/2020. REPLACED GUSSET (WITH NEW ONE) ON FRAME FS 349, AT THE UPPER TENSION TIE BUTTON LOCATION, REF CRJ-700 SRM.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 35,540 hrs · 25,964 cycles

AT FS 549, RBL 9, INBOARD ON FLOOR BEAM, BLENDED AREA, REF CAMP NR 21776576, JOB NR 4, OP NR 34. C-CHECK RO 12/04/2020. AT FS 549, RBL 9, INBOARD ON FLOOR BEAM, BLENDED AREA, REF CAMP NR 21776576, JOB NR 4, OP NR 34 HAS BEEN ADDRESSED, REF ALL APPLICABLE STEPS OF REO.

Part: FRAME SPLICE — CORRODED (ZONE 100) · airframe 35,540 hrs · 25,964 cycles

EXTERNAL FS 939 PANEL SUPPORT FRAME BUTT SPLICE DIRECTLY BELOW STGR 27 CORRODED, AS MARKED. C-CHECK RO 12/04/2020. REMOVED AND REPLACED SUPPORT FRAME BUTT SPLICE AT FS 939 BELOW STGR 27, PER CRJ700 SRM.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 35,540 hrs · 25,964 cycles

AT FS 549, LBL 9, INBOARD OF FLOOR BEAM, BLENDED AREA ON TOP OF CROSSBEAM, REF CAMP NR 21776576, JOB NR 4, PO NR 34. C-CHECK RO 12/04/2020. AT FS 549, LBL 9, INBOARD OF FLOOR BEAM, BLENDED AREA ON TOP OF CROSSBEAM, REF CAMP NR 21776576, JOB NR 4, PO NR 34 HAS BEEN ADDRESSED, REF ALL APPLICABLE STEPS OF REO. COMPLIED WITH SKYCARD.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 35,540 hrs · 25,964 cycles

AT FS 549, LBL 9, INBOARD OF SEAT TRACK RAIL. BLENDED AREA FLOOR BEAM, REF CAMP NR 21776576, JOB NR 4, OP NR 34. C-CHECK RO 12/04/2020. AT FS 549, LBL 9, INBOARD OF SEAT TRACK RAIL. BLENDED AREA FLOOR BEAM, REF CAMP NR 21776576, JOB NR 4, OP NR 34 HAS BEEN ADDRESSED, REO.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 35,540 hrs · 25,964 cycles

SURFACE CORROSION ON FLOOR STRUCTURE IN 3 SPOTS INBOARD OF RT CENTER SEAT TRACK BETWEEN FS 569R & FS 597R, MARKED. C-CHECK RO 12/04/2020. PERFORMED BEAM SPLICE REPAIR, PER CRJ700 SRM.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 35,540 hrs · 25,964 cycles

POSSIBLE CORROSION ON LT SEAT TRACK INBOARD SIDE AT FS 409L, MARKED. C-CHECK RO 12/04/2020. REMOVED AND REPLACED AND INSTALLED LT SEAT TRACK INBOARD SIDE AT FS 409L, REF CRJ 700 AMM.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 35,540 hrs · 25,964 cycles

POSSIBLE CORROSION ON RT CENTER SEAT TRACK INBOARD SIDE FS 409R, MARKED. C-CHECK RO 12/04/2020. REMOVED AND REPLACED AND INSTALLED RT CENTER SEAT TRACK INBOARD SIDE FS 409R, REF CRJ 700 AMM.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 35,540 hrs · 25,964 cycles

SURFACE CORROSION ON FS 549 FLOOR STRUCTURE BEAM BETWEEN CENTER SEAT TRACKS ON BOTH LT INBOARD SIDE AT 3 SPOTS AND RT INBOARD SIDE, MARKED. C-CHECK RO 12/04/2020. REMOVED SURFACE CORROSION ON FS 549 FLOOR STRUCTURE BEAM BETWEEN CENTER SEAT TRACKS ON BOTH LT INBOARD SIDE AT 3 SPOTS AND RT INBOARD SIDE. WORK CARRIED OUT ON TASKCARD, REF REO. BLENDED OUT PER CRJ700 SRM.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 35,540 hrs · 25,964 cycles

SURFACE CORROSION IN 2 SPOTS ON LT FLOOR SILL FS 533L, MARKED. C-CHECK RO 12/04/2020. LT FLOOR SILL FS 533.00 TO FS 581.00 HAS INTERGRANNULAR CORROSION THROUGH ENTIRE THICKNESS OF PART. OUT OF LIMITS. REMOVED CORRODED SILL AND INSTALLED NEW LT FLOOR SILL P/N: SH670-33504-3S FROM FS 533.00 TO FS 581.00, REF CRJ700 SRM DWG. RESTORED FINISH AND APPLIED CIC. COMPLIED WITH TASK CARD. PRESSURE LEAK CHECK GOOD, REF CRJ-700 AMM. SEE CONTINUATION CARD FOR DETAILS.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 35,540 hrs · 25,964 cycles

POSSIBLE CORROSION ON AVIONICS BAY FLOORBOARD MOUNTING ANGLE ON AFTER SIDE OF FS 280 BETWEEN STGR 25L TO STGR 25R, MARKED. C-CHECK RO 12/04/2020. REPLACED AVIONICS BAY FLOORBOARD MOUNTING ANGLE AFT OF FS 280.00, AS PER CRJ 700 SRM.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 35,540 hrs · 25,964 cycles

FLOOR SILL AT FS 280 FWD OF PAX DOOR HAS CORROSION IN SEVERAL SPOTS, MARKED. C-CHECK RO 12/04/2020. INSTALLED NEW LT FLOOR SILL, P/N SH670-32171-7 AT FS 280-310, IAW CRJ 700 SRM.

Part: ATTACH FITTING — CORRODED (RT WING FAIRING) · airframe 35,540 hrs · 25,964 cycles

RT WING STUB FAIRING ATTACHING GUIDE "FITTING", RT WING INBOARD TRAILING EDGE AREA, APPROXIMATELY WS 00.00, AFT OF FLAP TORQUE TUBE ANGLED GEAR BOX "CHAFED", FLAGGED. C-CHECK RO 12/04/2020. REPLACED RT WING STUB FAIRING ATTACHING GUIDE "FITTING", RT WING INBOARD TRAILING EDGE AREA, APPROXIMATELY WS 00.00, AFT OF FLAP TORQUE TUBE ANGLED GEAR BOX WITH NEW, REF CRJ-700 SRM.

Part: TORQUE TUBE — CORRODED (LT WING TE FLAP) · airframe 35,540 hrs · 25,964 cycles

CORROSION DETECTED ON LT INBOARD FLAP, OUTBOARD ACTUATOR, TORQUE TUBE SUPPORT (BEARING HOUSING), RED OXIDE DUST EXITING HOUSING, AT APPROXIMATELY WS 97.45, FLAGGED. C-CHECK RO 12/04/2020. REMOVED TORQUE TUBE WITH CORRODED BEARING HOUSING, REF CRJ700 AMM. INSTALLED NEW TORQUE TUBE P/N: 5911360-2 ON LT INBOARD FLAP, OUTBOARD ACTUATOR, TORQUE TUBE SUPPORT (BEARING HOUSING) WERE FLAGGED, REF CRJ700 AMM.

Part: RING — BROKEN (TORQUE TUBE) · airframe 35,540 hrs · 25,964 cycles

LT WING INBOARD TRAILING EDGE, LT INBOARD FLAP TORQUE TUBE (CONTAINMENT RING) AT APPROXIMATELY WS 88.00 BETWEEN THE (2) LT GROUND SPOILERS, HAS "BROKEN" FWD ATTACHING NUTPLATE, RING NOT SECURE, FLAGGED. C-CHECK RO 12/04/2020. REMOVED AND REPLACED CONTAINMENT RING MOUNTING BRACKET, REF CRJ 700 SRM AT LT WING INBOARD TRAILING EDGE, LT INBOARD FLAP TORQUE TUBE BETWEEN THE (2) LT GROUND SPOILERS AT APPROXIMATELY WS 88.00.

Part: ATTACH FITTING — CHAFED (LT WING FAIRING) · airframe 35,540 hrs · 25,964 cycles

LT WING STUB FAIRING ATTACHING LUG/PLATE, LT WING TRAILING EDGE AREA, APPROXIMATELY WS 00.00, AFT OF FLAP TORQUE TUBE SHAFT ANGLED GEAR BOX MOUNT, CHAFED, FLAGGED. C-CHECK RO 12/04/2020. REPLACED LT WING STUB FAIRING ATTACHING LUG/PLATE, LT WING TRAILING EDGE AREA, APPROXIMATELY WS 00.00, AFT OF FLAP TORQUE TUBE SHAFT ANGLED GEAR BOX MOUNT, WITH NEW, REF CRJ-700 SRM.

Part: MOUNT — CORRODED (NACELLE) · airframe 35,540 hrs · 25,964 cycles

CORRODED HARDWARE FOR LEFT AND RIGHT AFT PYLON MOUNTS UNDER PNLS 413AB AND 423AB, MARKED. C-CHECK RO 12/04/2020. REMOVED AND REPLACED 2 EA BOLTS, 4 EA WASHERS, 2 EA NUTS AND 2 EA COTTER PINS ON LEFT AND RIGHT PYLON MOUNTING HINGES UNDER PANELS 413AB AND 423AB. TORQUE WRENCH TUC8614 CAL DUE 30-NOV-20, REF CRJ 700 AMM.

Part: HINGE — GOUGED (PAX DOOR) · airframe 35,540 hrs · 25,964 cycles

PAX DOOR HINGE, FUSELAGE SIDE, LAND NR 27 IS GOUGED FROM SPRING PIN MIGRATING. C-CHECK RO 12/04/2020. REMOVED AND REPLACED PAX DOOR FUSELAGE HINGE, REF CRJ700 SRM AND DWG. COMPLIED WITH SW TASK CARD. LEAK CHECK GOOD. SEE CONTINUE CARD FOR DETAILS.

Part: LUG — DAMAGED (PAX DOOR HINGE) · airframe 35,540 hrs · 25,964 cycles

NUMEROUS PAX DOOR HINGE LUGS HAVE DAMAGE (DOOR SIDE). C-CHECK RO 12/04/2020. REPAIRED PAX DOOR HINGE LUGS, AS PER CRJ 700 SRM. REMOVED AND RE-INSTALLED PAX DOOR, REF CRJ700 AMM. CLEARANCE, FUNCTIONAL, AND OPERATIONAL TEST GOOD. C/W TASK CARD.

Part: SKIN — CORRODED (FUSELAGE BELLY) · airframe 35,540 hrs · 25,964 cycles

CORROSION DETECTED DURING EXTERNAL ZONAL INSPECTION OF CENTER WING LOWER SKIN. ON CENTER WING BELLY FAIRING "FRAME" (PN: CC670-39204-1), AT FS 794.00. DISCREPANT AREA IS ON THE (FAIRING-TO-FRAME) MATING SURFACE, AROUND ALMOST EVERY NUT PLATE HOLE BETWEEN LBL 45.00 AND RBL 45.00, FLAGGED. C-CHECK RO 12/04/2020. COMPLIED WITH ALL STEPS OF REO FOR TEMPORARY REPAIR FOR CORROSION TO WING TO FUSE FAIRING FRAME FS 797.

Part: RETAINER — BROKEN (BUTTE DOOR) · airframe 35,540 hrs · 25,964 cycles

RT BUTE DOOR HINGE PIN RETAINER (PLATE) BROKEN OFF, HINGE PIN MIGRATED OUTBOARD ACROSS HINGE BOX OPENING, AT RT OUTBOARD FLAP (CENTER) HINGE BOX LOCATION, MARKED. C-CHECK RO 12/04/2020. REMOVED CRACKED BRACKET ON RT BUTE DOOR OUTBOARD FLAP CENTER HINGE BOX, REF CRJ700 SRM. INSTALLED NEW BRACKET ON RT BUTE DOOR OUTBOARD FLAP CENTER HINGE BOX, REF CRJ700 SRM.

Part: THRESHOLD — CRACKED (FWD CARGO BAY) · airframe 35,540 hrs · 25,964 cycles

FWD CARGO DOOR THRESHOLD CRACKED AND DENTED, PANEL 151MLW. C-CHECK RO 12/04/2020. ORDERED AND RECEIVED NEW FWD CARGO DOOR THRESHOLD P/N 9846301-1 INSTALLED ON JOB 71021290 OP 7014 CAMP NR 21650120.

Part: SPRING — CORRODED (BUTTE DOOR ACT) · airframe 35,540 hrs · 25,964 cycles

EVIDENCE OF LIGHT SURFACE CORROSION ON RT OUTBOARD FLAP BUTE DOOR ACTUATOR "SPRING" AT RT FLAP (OUTBOARD) HINGE BOX LOCATION, FLAGGED. C-CHECK RO 12/04/2020. REMOVED AND REPLACED RT OUTBOARD FLAP BUTE DOOR ACTUATOR SPRING AT OUTBOARD HINGE BOX LOCATION WITH NEW PART, IAW AMM. OPERATIONS TEST GOOD.

Part: ACTUATOR — CORRODED (LT BUTTE DOOR) · airframe 35,540 hrs · 25,964 cycles

EVIDENCE OF LIGHT SURFACE CORROSION ON LT BUTE DOOR ACTUATOR "SPRING", AT LT OUTBOARD FLAP (INBOARD) HINGE BOX LOCATION, FLAGGED. C-CHECK RO 12/04/2020. REMOVED CORRODED "SPRING" AND INSTALLED NEW BUTE DOOR ACTUATOR SPRING P/N: 600-10246-1 AT LT OUTBOARD FLAP INBOARD HINGE BOX (WHERE FLAGGED), REF CRJ700 AMM. OPERATIONS TEST GOOD.

Part: ACTUATOR — CORRODED (LT BUTTE DOOR) · airframe 35,540 hrs · 25,964 cycles

EVIDENCE OF LIGHT SURFACE CORROSION ON LT BUTE DOOR ACTUATOR "SPRING", AT LT OUTBOARD FLAP (MIDDLE) HINGE BOX LOCATION, FLAGGED. C-CHECK RO 12/04/2020. REMOVED AND REPLACED LT BUTE DOOR ACTUATOR SPRING AT MIDDLE HINGE BOX LOCATION, WITH NEW PART, IAW AMM. OPERATIONS TEST GOOD.

Part: SKIN — DENTED (RUDDER) · airframe 35,540 hrs · 25,964 cycles

THE RUDDERS LT SKIN HAS 3 DENTS ABOVE A PREVIOUS REPAIR, MARKED WITH BLACK GREASE PENCIL. C-CHECK RO 12/04/2020. REMOVED RUDDER REFERENCE CRJ700 AMM. HAND DRESSED 3 EA DENTS IN RUDDER SKIN TO ORIGINAL CONTOUR, REFERENCE CRJ700 SRM AND REO. COMPLIED WITH CARD SEE JOB 71021295 OP 136 CAMP 21911725 FOR INSTALLATION OF THE RUDDER. OPERATIONS CHECKS AND TASK CARD.

Part: FADEC — FAILED (RT ENGINE) · airframe 33,348 hrs · 24,241 cycles

R FADEC CAUTION MESSAGE IN FLIGHT. (FLT#3253) CLOSED REMOVED AND REPLACED RT FADEC IAW AMM.

Part: WEB — CORRODED (PAX DOOR) · airframe 31,780 hrs · 22,972 cycles

PAX DOOR AFT WEB HAS AREA OF CORROSION NOTED ON UPPER INNER SURFACE (DOOR OPEN), ALSO PREVIOUS DRAG ANGLE REPAIR IS CRACKED. (C-CHECK) RO: 09/14/2018. INSTALLED SERVICABLE DRAG ANGLE AND AFT WEB 601R317071-11 IAW SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 31,780 hrs · 22,972 cycles

FUSELAGE EXTERNAL SKIN HAS MULTIPLE AREAS OF CORROSION AROUND NUTPLATE HOLE FOR AFT WING TO FUSELAGE FAIRINGS 195DL AND 196DR FROM FS 985.00 TO FS 1015.00 BETWEEN STR 21R AND 21L. (C-CHECK) RO: 09/14/2018. REPAIRED FUSELAGE EXTERNAL SKIN, MULTIPLE AREAS OF CORROSION AROUND NUTPLATE HOLES FOR AFT WING TO FUSELAGE FAIRINGS 195DL AND 196DR, FROM FS 985.00 TO FS 1015.00 BETWEEN STR 21R AND 21L IAW REO. LEAK CHECKS GOOD.

Part: FRAME — CORRODED (FUSELAGE) · airframe 31,780 hrs · 22,972 cycles

FOUND FS 319.70 CORRODED. (C-CHECK) RO: 09/14/2018. REMOVED AND REPLACED FRAME PORTION AT FS 319.70 IAW SRM.

Part: ANGLE — DAMAGED (FUSELAGE) · airframe 31,780 hrs · 22,972 cycles

ONE (1) FASTENER HOLE AT RBL 7.50 BELOW WL79.50 IN STIFFENER ANGLE. (C-CHECK) RO: 09/14/2018. PERFORMED REPAIR OF DAMAGED ANGLE IAW REO.

Part: WARNING MESSAGE — FALSE ACTIVATION (STALL)

STALL FAIL CAUTION MESSAGE IN FLIGHT. PERFORMED AN OPS TEST OF THE STALL PROTECTION SYSTEM IAW AMM 27-35-01. OPS CHECKED GOOD, NO FAULTS FOUND. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — NOT SEATED (EMERGENCY LIGHTS) · airframe 30,854 hrs · 22,215 cycles

RIGHT EXTERNAL OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE PERFORMED RESEAT OF THE CONNECTOR P5231 AND P876. OPS CHECKED GOOD.

Part: FAN — FAILED (RECIRCULATION) · airframe 30,310 hrs · 21,805 cycles

CREW REPORTED A RECIRCULATION FAN FAULT STATUS MESSAGE IN FLT, WITH A HEAVY ELECTRICAL ODOR. OPEN

Part: FAN — SMOKE (NR 2 RECIRC) · airframe 30,310 hrs · 21,805 cycles

CREW REPORTED A RECIRCULATION FAN FAULT STATUS MESSAGE IN FLT, WITH A HEAVY ELECTRICAL ODOR. REMOVED AND REPLACED THE NR 2 RECIRCULATION FAN IAW AMM 21-22-10.

Part: DRAG ANGLE — CRACKED (VERT - FUSE) · airframe 30,241 hrs · 21,752 cycles

LEFT REAR VERTICAL TO FUSELAGE DRAG ANGLE IS CRACKED. MAINTENANCE REPLACED CRACKED DRAG ANGLE.

Part: DRAG ANGLE — CRACKED (VERT TO FUSE) · airframe 30,241 hrs · 21,752 cycles

LEFT VERTICAL TO FUSELAGE DRAG ANGLE IS CRACKED. MAINTENANCE REPAIRED THE DRAG ANGLE IAW EC/TC REO 670-55-31-018.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 30,241 hrs · 21,752 cycles

RIGHT REAR VERTICAL TO FUSELAGE ATTACH DRAG ANGLE IS CRACKED. MAINTENANCE REPLACED CRACKED DRAG ANGLE

Part: DRAG ANGLE — CRACKED (VERT TO FUSE) · airframe 30,241 hrs · 21,752 cycles

RIGHT VERTICAL TO FUSELAGE ATTACH DRAG ANGLE IS CRACKED. REPAIRED.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 30,241 hrs · 21,752 cycles

COCKPIT FLOORBEAM ANGLE, BS 280 CORRODED. REMOVED CORROSION AND REPAIRED IAW EC/TC EA 30-2017-153.

Part: ANGLE — CORRODED (BS 939) · airframe 30,241 hrs · 21,752 cycles

WING TO FUSELAGE AFT SUPPORT AT BS 939, STRINGER 27 HAS CORROSION AT THE LOWER FLANGE. MAINTENANCE REPLACED THE ANGLE.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 30,241 hrs · 21,752 cycles

INTERCOSTAL BETWEEN BS 349 - 364, STRINGER 27L IS CORRODED. MAINTENANCE REPLACED INTERCOSTAL.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 30,241 hrs · 21,752 cycles

INTERCOSTAL BETWEEN BS 349 - 364, STRINGER 27R IS CORRODED. MAINTENANCE REPLACED THE INTERCOSTAL.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 29,656 hrs · 21,306 cycles

PILOT REPORTED EMERGENCY LIGHTS ARE NOT WORKING. MX RESET AIRCRAFT POWER. EMERGENCY LIGHTS OPS CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — FAILED (LAVATORY) · airframe 28,914 hrs · 20,757 cycles

SMOKE AFT LAV WARNING IN FLIGHT. NO VISUAL INDICATIONS OF SMOKE OR FIRE. FIRE TRUCKS CONFIRMED THE SAME FROM THE EXTERIOR. REMOVED AND REPLACED AFT LAV SMOKE DETECTOR IAW AMM 26-16-01 OPS CHECK IS GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 28,911 hrs · 20,756 cycles

FLOORBEAM AT RBL 9 BETWEEN FS 1009-1037 CORRODED BEYOND LIMITS. REPAIRED FLOORBEAM PER EO 700-53-10-0030 & REO 670-53-61-1335 IAW 670-53-00-029 AND SRM 53-00-41-201-001-A01 SPLICE REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 28,911 hrs · 20,756 cycles

FLOORBEAM LBL 27 NEAR FS 1031 CORRODED BEYOND LIMITS. REPAIRED FLOORBEAM PER EO 700-53-10-0025 AND SRM 53-00-41-201-001-A01 SPLICE REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 28,911 hrs · 20,756 cycles

FLOORBEAM AT LBL 9 BETWEEN FS 1009-1037 CORRODED BEYOND LIMITS. REPAIRED FLOORBEAM PER EO 700-53-10-0030 AND SRM 53-00-41-201-001-A01 SPLICE REPAIR.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 27,119 hrs · 19,317 cycles

REAR F/A FLASHLIGHT INOPERATIVE. R & R AFT F/A FLASHLIGHT BATTERIES, OPS CHECK GOOD AT THIS TIME IAW AMM25-61-00.

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 25,806 hrs · 18,272 cycles

FLOOR SEAT TRACK 581, LBL 9-677 HAS CORROSION THOUGHOUT TRACK. CORROSION ON FLOOR SEAT TRACK EXCEEDS THE ALLOWABLE DAMAGE LIMITS OF SRM SUPPLEMENT 53-31-49, TABLE 1 OF REO 670-53-00-013, SEAT TRACK CORRODED THROUGHTOUT COMPLETE LENGTH. R & R SEAT RAIL AT LBL 9 FS 581-677 IAW AMM 53-00-49-000-801, AO3 AND AMM 53-00-49-400-801, AO3.

Part: SEAT TRACK — CORRODED (BS 677-830) · airframe 25,806 hrs · 18,272 cycles

FLOOR SEAT TRACK 677, RBL9-830.40 CORROSION THROUGH OUT TRACK. CORROSION ON SEAT TRACK EXCEEDS THE DAMAGE LIMITS OF SRM SUPPLEMENT 53-31-49, TABLE 1 OF REO 670-53-00-013 COMPLETE LENGTH OF TRACK CORRODED. R & R SEAT TRACK IAW AMM 53-00-49-000-801, A03 & 53-00-49-400-801, AO3. COMPLIED WITH ECTC 670-53-00-343 AND GREO 670-53-00-343, REV L AS WRITTEN.

Part: ANGLE — CORRODED · airframe 25,806 hrs · 18,272 cycles

UPON REMOVAL OF DOOR SILL ANGLE ON SERVICE DOOR, FOUND ANGLE MOUNT TO BE CORRODED. REMOVED ANGLE MOUNT IAW SRM 51-42-06-001-001-A01. INSTALLED NEW ANGLE MOUNT IAW SRM 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 349-485) · airframe 25,806 hrs · 18,272 cycles

FLOOR SEAT TRACK 349 - 485 RBL9, HAS CORROSION. CORROSION EXCEEDS THE LIMITS OF SRM, SUPPLEMENT 53-21-49, TABLE 2 OF REO 670-5300-013. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801, AO3 & AMM 53-00-49-400-801, AO3.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 25,806 hrs · 18,272 cycles

FLOOR SEAT TRACK 485 - 581 LBL 9, HAS CORROSION THOUGHOUT TRACK. CORROSION EXCEEDS THE ALLOWABLE DAMAGE LIMITS OF SRM SUPPLEMENT 53-31-49, TABLE 1 OF REO 670-53-00-013. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801, AO3 & AMM 53-00-49-400-801, AO3.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 25,806 hrs · 18,272 cycles

FLOOR SEAT TRACK 485 - 581 RBL 9, HAS CORROSION THROUGHOUT TRACK. CORROSION EXCEEDS THE ALLOWABLE LIMITS OF SUPPLEMENT 53-31-49, TABLE 1 OF REO 670-53-00-013. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801, AO3 & AMM 53-00-49-400-801, AO3.

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 25,806 hrs · 18,272 cycles

SEAT TRACK BS 581- 677 RBL 9, HAS CORROSION THROUGHOUT TRACK. CORROSION EXCEEDS THE ALLOWABLE LIMITS OF SRM SUPPLEMENT 53-31-49, TABLE 1 OF REO 670-53-00-013. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801, A03 & AMM 53-00-49-400-801, AO3.

Part: STRIKER — CORRODED (SERVICE DOOR) · airframe 25,806 hrs · 18,272 cycles

SERVICE DOOR LOWER SEAL STRIKER CORRODED IN SEVERAL LOCATIONS. EVALUATED AREA AND FOUND DAMAGE OUT OF LIMITS IAW SRM 53-21-23-101-002-AO2. REMOVED SERVICE DOOR LOWER SEAL STRIKER IAW SRM TASK 51-42-06-001-001-A01. LOCATED DRILLED & INSTALLED NEW SERVICEABLE SERVICE DOOR LOWER SEAL STRIKER IN REF TO SRM 51-42-06-001-001-A01. LOCATED AND TRANSFERED DRILLED MOUNT HOLES IAW SRM 51-40-11-001-001-A01. INSTALLED DOME NUT PLATES AS NEEDED REF SRM 51-45-00-001-001-A01 & DWG SH670-31950.

Part: SEAT TRACK — CORRODED (BS 364-485) · airframe 25,806 hrs · 18,272 cycles

FLOOR SEAT TRACK 364, LBL9-485 CORRODED THROUGH OUT TRACK. FWD EDGE CORROSION ON FLOOR SEAT TRACK EXCEEDS THE ALLOWABLE LIMITS OF SRM SUPPLEMENT 53-21-49, TABLE 1 LOCATION T/E OF REO 670-53-00-013, FWD EDGE EXTREMELY EXFOLIATED. R & R SEAT TRACK LBL9 FS 364-485 IAW AMM 53-00-49-000-801-A03 AND 53-00-49-400-801-A03. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV L AS WRITTEN.

Part: SEAT TRACK — CORRODED (BS 677-708) · airframe 25,806 hrs · 18,272 cycles

RIGHT SIDEWALL SEAT TRACK BS 677-708 HAS CORROSION. OUT OF LIMITS OF REO 670-53-00-013. R & R SEAT TRACK IAW AMM 53-00-49-000-801-AO3 AND 53-00-49-400-801-AO3.

Part: SEAT TRACK — CORRODED (BS 677-708) · airframe 25,806 hrs · 18,272 cycles

LEFT SIDEWALL SEAT SEGMENT 677-708 HAS CORROSION. CORROSION ON LT SIDE SEAT RAIL EXCEEDS THE ALLOWABLE DAMAGE LIMITS OF SRM SUPPLEMENT TABLE 1 OF REO 670-53-00-013. R & R LT SIDE WALL SEAT RAIL BETWEEN F/S 677-708. REF: AMM 53-00-49-000-801-AO3 & 53-00-49-400-801-AO3 COMPLIED WITH EC/TC REO 670-53-00-343 & GREO 670-53-00-343, REV L AS WRITTEN.

Part: SEAT TRACK — CORRODED (BS 485-572) · airframe 25,806 hrs · 18,272 cycles

RT SIDEWALL RAIL SEGMENT 485-572 HAS CORROSION. CORROSION ON RT SIDE WALL SEAT RAIL EXCEEDS THE LIMITS OF SRM SUPPLEMENT TABLE 1 OF REO 670-53-00-013. REMOVED SIDE SEAT RAIL RT 485-572 IAW AMM 53-00-49-00-801-AO3. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV L AS WRITTEN. INSTALLED SEAT RAIL AT RT SIDEWALL FS 485- FS 572 IAW AMM 53-00-49-400-801-AO3.

Part: SEAT TRACK — CORRODED (BS 785-863) · airframe 25,806 hrs · 18,272 cycles

RIGHT SIDEWALL SEAT TRACK SEGMENT BS 785-863 HAS CORROSION. CORROSION ON RT SIDEWALL SEAT TRACK EXCEEDS THE LIMITS OF SRM SUPPLEMENT TABLE 1 OF REO 670-53-00-013. R & R SEAT TRACK IAW AMM 53-00-49-000-801-AO3 AND 53-00-49-400-801-AO3. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-34, REV L.

Part: SEAT TRACK — CORRODED (BS 708-761) · airframe 25,806 hrs · 18,272 cycles

RIGHT SIDEWALL SEAL TRACK SEGMENT BS 708-761 HAS CORROSION. CORROSION ON RT SIDE WALL SEAT TRACK EXCEEDS THE LIMITS OF SRM SUPPLEMENT TABLE 1 OF REO 670-53-00-013. R & R SEAT TRACK WITH A FABRICATED SEAT TRACK IN REF TO AMM 53-00-49-000-801-AO3 & 53-00-49-400-801-AO3. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV L.

Part: SEAT TRACK — CORRODED (BS 572-677) · airframe 25,806 hrs · 18,272 cycles

RIGHT SIDEWALL SEAT RAIL SEGMENT 572-677 HAS CORROSION. CORROSION ON RT SIDE WALL SEAT RAIL EXCEEDS THE LIMITS OF SRM SUPPLEMENT TABLE OK REO 670-53-00-013. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801-AO3 AND 53-000-49-400-801-AO3.

Part: SEAT TRACK — CORRODED (BS 485-572) · airframe 25,806 hrs · 18,272 cycles

LEFT SIDEWALL SEAT RAIL SEGMENT BS 485-572 HAS CORROSION. CORROSION ON LT SIDE WALL SEAT RAIL EXCEEDS THE LIMITS OF SUPPLEMENT 53-31-49, TABLE 1, OK REO 670-53-00-013. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV. L AS WRITTEN. R & R SEAT TRACK IAW AMM 53-00-49-000-801, AO3 & AMM 53-00-49-400-801- AO3.

Part: SEAT TRACK — CORRODED (BS 572-677) · airframe 25,806 hrs · 18,272 cycles

LEFT SIDEWALL SEAT TRACK, SEGMENT 572-677 HAS CORROSION. CORROSION ON LEFT SIDE WALL SEAT TRACK EXCEEDS THE LIMITS OF SRM SUPPLEMENT TABLE 1 OF REO 670-53-00-013. PARTIALY REMOVED SEAT TRACK IAW AMM 53-00-49-000-801-AO3. FINISHED REMOVAL AND INSTALATION OF SEAT TRACK IAW AMM 53-00-49-000-801-AO3 AND AMM 53-00-49-400-801-AO3. FABRICATED NEW SEAT TRACK IAW REO 670-53-00-343. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343 REV L AS WRITTEN.

Part: SEAT TRACK — CORRODED (BS 708-761) · airframe 25,806 hrs · 18,272 cycles

LEFT SIDEWALL SEAT RAIL SEGMENT 708-761 HAS CORROSION. CORROSION ON LT SIDE WALL SEAT RAIL EXCEEDS THE LIMITS OF SRM SUPPLEMENT TABLE 1 OF REO 670-53-00-013. R & R SEAT RAIL BETWEEN F/S 108-761 SIDE WALL, LT SIDE. REF: AMM 53-00-49-000-801 & 53-00-49-400-801-AO3. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV L AS WRITTEN.

Part: SEAT TRACK — CORRODED (BS 785-863) · airframe 25,806 hrs · 18,272 cycles

LEFT SIDEWALL SEAT RAIL SEGMENT 785-863 HAS CORROSION. CORROSION ON LT SIDEWALL SEAT RAIL EXCEEDS THE LIMITS OF SRM SUPPLEMENT TABLE OF REO 670-53-00-013. R & R LT SIDE SEAT RAIL FS 785- FS 863 IAW AMM 53-00-49-000-801-AO3 AND 53-00-49-400-801-AO3. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV L AS WRITTEN.

Part: ANGLE — CORRODED (DOOR SILL) · airframe 25,806 hrs · 18,272 cycles

SERVICE DOOR LOWER SILL ANGLE FROM FS 319.70-FS 349 IS CORRODED IN MULIPLE AREAS. REMOVED LOWER SILL ANGLE FROM SERVICE DOOR IAW SRM 51-42-06-001-001-A01. LOCATED AND DRILLED NEW ANGLE MOUNTING AND LOWER SILL ANGLE IAW SRM 51-40-11-001-001-A01. INSTALLED NEW LOWER SILL ANGLE ON SERVICE DOOR IAW SRM 51-42-06-001-001-A01 AND DWG SH670-31996.

Part: DOOR SILL — CORRODED (SERVICE DOORWAY) · airframe 25,806 hrs · 18,272 cycles

SERVICE DOOR SILL PLATE CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01 SILL PLATE DAMAGE OUT OF LIMITS IAW SRM 53-21-23-101-002-A01. REPLACED SILL PLATE AT SERVICE DOOR THERSHOLD REF DWG SH670-31150, REV: U, SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01. LOCATED DRILLED AND DEBURGED AND INSTALLED NUTPLATES ON WEB FLOOR PROTECTORS IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01.

Part: INTERCOSTAL — CORRODED (BS 310-349) · airframe 25,806 hrs · 18,272 cycles

INTERCOSTAL FROM FS 310-FS 349 AT STR 19, RT IS CORRODED IN MULTIPLE AREAS. REMOVED INTERCOSTAL AND STR 19 AT FS 310 TO 349 IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. INSTALLED NEW INTERCOSTAL & STR 19 IN REF TO SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. INSTALLED THE FWD MID AND AFT CLEAT ALONG WITH THE DRAIN HOSE CLAMP BRACKET TO THE INTERCOSTAL IN REF TO SRM 51-42-06-001-001-A01.

Part: PANEL — CHAFED (RT WING) · airframe 25,806 hrs · 18,272 cycles

RT WING L/E PANEL 631AR IS CHAFED. BLENDED CHAFED AREA IAW SRM 57-41-01-101-001-AO1. BLEND LENGTH 33 BY 1 MATERIAL. REMOVED .009 FOUND TO BE OUT OF ALLOWABLE DAMAGE LIMITS REF: SRM 57-41-01-101-001-AO1, TABLE 1 BLEND LENGTH IS 37 PERCENT OF THE PANEL LENGTH. SUBMITTED TO ENGINEERING FOR PERMANENT DISPOSITION. RECEIVED STS EA 32-2015-342. ECTC EA 32 2015-342 C/W THIS IS A MINOR REPAIR CH84774 8/29/15.

Part: LENS — DETERIORATED (EMERGENCY LIGHT) · airframe 25,806 hrs · 18,272 cycles

EMERGENCY FLOOR PATH MARKINGS HAS AREAS THROUGHOUT CABIN THAT ARE FADED AND DISCOLORED. REMOVED EMERGENCY FLOOR PATH MARKING IAW AMM 23-51-01-000-801, A01 & AMM SUPPLEMENT 33-51-01, REV A. INSTALLED SERVICEABLE FLOOR PATH MARKING ON IAW AMM 33-51-01-400-801 (A01) & AMM SUPPLEMENT 33-51-01, REV A.

Part: LANDING — CRACKED (STRUCTURE) · airframe 25,806 hrs · 18,272 cycles

FOUND CRACK IN LAN, SILL OF LT FWD EQUIPMENT COMPARTMENT. REMOVED DISCREPANT LANDING IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-13-001-001-A01. LOCATED FASTENER HOLES IN SERVICABLE BAY DOOR LANDING, RT SIDE AND INSTALLED ALL SOLID FASTENERS AFT OF FS 173.00. REF SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 QWL CC670-33040. INSTALLED ALL FASTENERS COMMON TO SKIN PANEL AND DOOR LANDING IAW STS EA 32-2015-356. INSTALLED, 2EA, RIVETS THRU FS 173 FRAMED CLEAT/CLIP ON DOOR LANDING & FLOOR WEB, IAW SRM 51-42-06-001-001-A01. COMPLIED WITH ECTC EA 32-2015-356.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 25,806 hrs · 18,272 cycles

RIGHT INBD FLAP HAS DENT ON LOWER SKIN JUST ABOVE MLG TIRES. COMPLIED WITH PERMANENT REPAIR OF RT INBD FLAP LOWER SKIN IAW EC/TC REO 670-57-52-160 01 AND W/O 374953, NR 00100. MFG REPAIR ITEMS -4,-20,-40 AND -52 IAW REO 670-57-52-160. MFG FILLER REPAIR ITEM NR 30 IAW REO 670-57-52-160 AND ECTC REO 670-59-52-160-01, ITEM 6. REPAIR TO THE LT/RT LOWER SKIN IS COMPLETED IAW REO 670-57-52-160 AND MEETS WITH ALL ITS REQUIREMENTS.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 21,553 hrs · 15,050 cycles

CONNECTOR FOR EMERGENCY LIGHT WIRING HAS PULLED OFF AT ENTRANCE STOWAGE COMPARTMENT. REINSTALLED CONNECTOR IAW ESPM 20-26-00 PERFORMED EMERGENCY LIGHT OPS CHECKS IAW AMM 33-51-00-710-802. OPS CHECK GOOD.

Part: GROUND STUD — CORRODED (FUSELAGE) · airframe 21,553 hrs · 15,050 cycles

FOUND CORROSION ON GROUND LUGS GS1841, GS441, GS317, GS319 BEHIND NR 1 ATL/DME EQUIPMENT RACK AT FS 324 LT SIDE. PERFORMED OPS TEST OF FMS SYS OPS TEST OF GPS SYSTEM IAW AMM 34-61-01-710-801 & 34-58-00-710-801. OPS CHECKED GOOD. PEFORMED OPS TEST OF ACARS SYS IAW AMM 23-22-00-710-801. OPS CHECKED GOOD. PERFORMED OPS TEST OF DOOR WARNING SYSTEM IAW AMM 52-70-70-710-801. OPS CHECKED GOOD.

Part: SUPPORT ANGLE — CRACKED (BS 280) · airframe 21,553 hrs · 15,050 cycles

TWO VERTICAL SUPPORT ANGLES AT FS 280 RT WEB ONE AT RBL 17.46 AND ONE AT RBL 26.00 HAVE CRACKS AT LOWER ATTACH HOLES. REMOVED VERTICAL SUPPORT ANGLES IAW SRM 51-42-06-001-001-A01. LOCATED, DRILLED AND INSTALLED VERTICAL SUPPORT ANGLE IAW SRM 51-40-06-001-001, 51-40-11-001-001 AND SRM 51-42-06-001-001.

Part: GUSSET — DAMAGED (FLOORBEAM) · airframe 21,553 hrs · 15,050 cycles

FOUND TWO FLOORBEAM GUSSETS AT FS 280 LBL & RBL 11.8 TO BE UNSERVICEABLE. REMOVED GUSSETS IAW SRM 51-42-06-001-001-A01. DRILLED AND INSTALLED NEW GUSSETS IAW SRM 51-42-06-001-001-A01, 51-40-11-001-001 & 51-42-06-001-001. MAJOR REPAIR.

Part: FLOOR SUPPORT — CRACKED (COCKPIT) · airframe 21,553 hrs · 15,050 cycles

FOUND COCKPIT FLOOR SUPPORTS CRACKED JUST FORWARD OF FS 280. REMOVED FLOOR SUPPORTS IAW SRM 51-42-06-001-001-A01. DRILLED AND INSTALLED FLOOR SUPPORTS IAW SRM 51-42-06-001-001-A01, SRM 51-40-11-001-001, SRM 51-42-06-001-001 & DWG CC670-33199.

Part: FLOORBEAM — CRACKED (COCKPIT) · airframe 21,553 hrs · 15,050 cycles

RT COCKPIT FLOORBEAM AT RBL 12.0 CRACKED AT FITTING ATTACH AREA. REPAIRED IAW REO 670-53-11-865.

Part: INTERCOSTAL — DAMAGED (BS 280) · airframe 21,553 hrs · 15,050 cycles

ON REMOVAL OF INTERCOSTAL AT FS 280 RBL 20, FOUND TOOL DAMAGE ON INBD SIDE OF INTERCOSTAL. R & R INTERCOSTAL IAW SRM 51-42-21-001-A01, 51-40-11-001-A01 AND DWG PL SH670-32150.

Part: SILL — CORRODED (BS 280-319) · airframe 21,553 hrs · 15,050 cycles

RT SILL PLATE FROM FS 280-319, RBL 45 HAS THREE CORROSION AREAS. REMOVED DAMAGED SILL PLATE IAW SRMS 51-42-06-001-001-A01, 51-42-13-001-001-A01 AND 51-42-21-001-001-A01. LOCATED AND DRILLED THE NEW SILL PLATE IAW SRM 51-40-11-001-001-A01. INSTALLED FLOOR SILL AND CONNECTOR PLUGS IAW DWG SH670-32170. MAJOR REPAIR.

Part: FRAME — CORRODED (BS 333) · airframe 21,553 hrs · 15,050 cycles

FRAME BS 333 AFT SIDE CORRODED BETWEEN S26L & 26R. REPAIRED IAW REO 670-53-21-1023.

Part: FRAME — CORRODED (BS 319.7) · airframe 21,553 hrs · 15,050 cycles

FRAME BS 319.7 FWD FACE CORRODED BETWEEN S26L AND 26R. REPAIRED FRAME IAW REO 670-53-21-799.

Part: FRAME — CORRODED (BS 295 S26R) · airframe 21,553 hrs · 15,050 cycles

FRAME BS 295, CORRODED S26R. COMPLIED WITH REO 670-53-21-1023.

Part: SKIN — CORRODED (BS 280) · airframe 21,553 hrs · 15,050 cycles

CIRCUMFERENTIAL JOINT INTERNAL SKIN CORRODED AT FS 280 BETWEEN S26L & 26R. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. COMPLIED WITH REO 670-53-21-1022.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 21,553 hrs · 15,050 cycles

FLOORBEAM AT FS 280 CORRODED. COMPLIED WITH S/B 670BA-53-041, REV C. MAJOR REPAIR.

Part: RETAINER — BENT (CARGO DOOR) · airframe 21,553 hrs · 15,050 cycles

FORWARD CARGO DOOR RT SIDE OF THE FWD & AFT CORNERS, INNER AND OUTER SEAL RETAINERS ARE BENT. REPAIRED IAW REO 670-52-35-127.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 21,522 hrs · 15,026 cycles

INTERCOSTAL CORRODED STRINGER 27RT BETWEEN FRAMES 349 & 364, REMOVED INTERCOSTAL IAW SRMS 51-42-21-001-001-A01 AND 51-42-06-001-001-A01. LOCATED AND DRILLED NEW INTERCOSTAL IAW SRM 51-40-11-001-001-A01 AND DWG SH670-32075. INSTALLED NEW INTERCOSTAL IAW SRM 51-42-21-001-001-A01 AND DWG SH670-32075. MAJOR REPAIR.

Part: FRAME — CORRODED (BS 310) · airframe 21,553 hrs · 15,050 cycles

FWD FACE OF FRAME BS 310 CORRODED BETWEEN S26L AND 26R. COMPLIED WITH REO 670-53-21-1023.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 21,553 hrs · 15,050 cycles

RT FLOORBEAM AT FS 280 CORRODED. COMPLIED WITH SB 670BA-53-041, REV C. MAJOR REPAIR.

Part: WEB — CORRODED (BS 280) · airframe 21,553 hrs · 15,050 cycles

AFT LOWER SECTION OF LT WEB AT FS 280 IS CORRODED. R & R LOWER WEB IAW REO 670-53-11-594. MAJOR REPAIR.

Part: WEB — CORRODED (BS 280) · airframe 21,553 hrs · 15,050 cycles

AFT LOWER SECTION OF RT WEB AT FS 280 IS CORRODED. R & R LOWER WEB IAW REO 670-53-11-594. MAJOR REPAIR.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 21,553 hrs · 15,050 cycles

INTERCOSTAL CORRODED S27L BETWEEN FRAMES BS 349 & 364. REMOVED INTERCOSTAL IAW SRMS 51-42-21-001-001-A01 AND 51-42-06-001-001-A01. LOCATED AND DRILLED NEW INTERCOSTAL IAW SRM 51-41-11-001-001-A01. INSTALLED THE NEW INTERCOSTAL IAW SRM 51-42-21-001-001-A01 & DWG SH670-32075. MAJOR REPAIR.

Part: FRAME — CORRODED (BS 349) · airframe 21,553 hrs · 15,050 cycles

FRAME CORRODED BS 349 AT S27. REPAIRED IAW REO 670-53-21-1023.

Part: SKIN — CORRODED (BS 295-310) · airframe 21,522 hrs · 15,026 cycles

TCAS DOUBLER INTERNAL SKIN CORRODED AROUND CONNECTOR CUTOUT BETWEEN FRAMES 295.00 & 310.00, STGR 27. REMOVED TCAS DOUBLER AND INSTALLED A NEW, SERVICEABLE, TCAS DOUBLER IAW SRM 51-42-06-001-001-A01.

Part: DOOR — LACK OF LUBE (GALLEY) · airframe 21,522 hrs · 15,026 cycles

FORWARD GALLEY SERVICE DOOR FAILED FUNCTION CHECK. FORCE GAUGE ON INTERNAL HANDLE 40LB TO UNLATCH. LUBRICATED GALLEY SERVICE DOOR IAW AMM 12-20-52-640-801. PERFORMED FUNCTIONAL CHECK ON GALLEY SERVICE DOOR IAW AMM 52-41-00-420-801, CHECK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 19,444 hrs · 13,531 cycles

INTERIOR EMERGENCY EXIT FLOOD LIGHT AT 12CD (FLOOR LEVEL) ONLY HAS ONE LAMP BURNING. LAMPED THE INTERIOR EMERGENCY EXIT FLOOD LIGHT AT 12CD AND OPS CHECK GOOD IAW AMM 33-51-00. SDR CLOSED.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 19,417 hrs · 13,508 cycles

EXTERIOR EMERGENCY LIGHTS INOPERATIVE. R & R BULBS IAW AMM 33-51-15. OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 19,417 hrs · 13,508 cycles

LEFT FWD AND RT MID EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R BULBS IAW AMM 33-51-15. OPS CHECKED GOOD WITH NO FURTHER FAULT FOUND AT THIS TIME.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 18,969 hrs · 13,163 cycles

PHOTO ILLUMINATION STRIP BY SEAT 4AB MISSING. INSTALLED PHOTO ILLUMINATION STRIP IAW AMM 33-51-01.

Part: SIGN — MISSING (EMERGENCY LIGHTS) · airframe 18,820 hrs · 13,055 cycles

EMERGENCY EXIT SIGN MISSING AT GALLEY. R & R GALLEY EXIT LIGHT HOUSING AND COVER IAW AMM 33-51-05.

Part: SHUTOFF VALVE — MALFUNCTIONED (RT ENGINE BLEED) · airframe 18,637 hrs · 12,920 cycles

RIGHT BLEED DUCT WARNING MESSAGE ON CLIMB OUT, 11000FT TO 13000FT, PRESSURE REGULATING SHUTOFF VALVE (PRSOV). EMERGENCY DECLARED, ACFT RETURNED TO DEPARTURE. OPS CHECKED RT ENGINE PRSOV IAW AMM 36-12-01. OPS CHECKED GOOD. NO FURTHER DEFECTS NOTED.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 18,565 hrs · 12,859 cycles

LEFT WINDOW AND LT WINDSHIELD CAUTION MESSAGE FOLLOWED BY SPARKS AND A PUFF OF SMOKE FROM LOWER LT WINDSHIELD CONTROLLER. R & R LT WINDSHIELD IAW AMM 56-11--01. OPS CHECKED GOOD.

Part: BULB — FAILED (COCKPIT) · airframe 18,486 hrs · 12,799 cycles

ON FINAL APPROACH, SMOKE FROM LT SIDE OF DASH NEAR NLG STEERING SWITCH. R & R BULB AT FWD SIDE PANEL FLOOD LIGHTS IAW AMM 33-11-03. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: SIGN — UNSERVICEABLE (EMERGENCY LIGHTS) · airframe 17,901 hrs · 12,389 cycles

EXIT SIGN COVER MISSING AT ENTRANCE TO FWD BOARDING DOOR. R & R EXIT SIGN IAW AMM 33-51-05.3. OPS CHECKED GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: PLACARD — MISSING (PAX DOOR) · airframe 17,852 hrs · 12,355 cycles

EXIT PLACARD MISSING ON THE STAIRS OF THE MAIN CABIN DOOR. INSTALLED NEW EXIT PLACARD IAW AMM 20-60-11.

Part: LIGHT — DAMAGED (CABIN) · airframe 17,312 hrs · 11,993 cycles

EMERGENCY LIGHT REMOVED FROM FLOOR AT ROW 12-13. REPLACED EMERGENCY FLOOR STRIPS AT ROW 12-13 IAW AMM 33-51-01.

Part: LIGHT — DAMAGED (CABIN) · airframe 17,312 hrs · 11,993 cycles

EMERGENCY LIGHT DAMAGED. R & R EMERGENCY LIGHT IAW AMM 33-51-01.

Part: LIGHT — DAMAGED (CABIN) · airframe 16,842 hrs · 11,666 cycles

EMERGENCY LIGHTING STRIP HEAVILY STAINED AT 9CD -10CD. R & R EMERGENCY LIGHT IAW AMM 33-51-01.

Part: FAN — FAILED (GALLEY/LAVATORY) · airframe 16,761 hrs · 11,616 cycles

BURNING ODOR IN COCKPIT AT CRUISE FLIGHT COMING FROM CAPTAIN'S WINDSHIELD ACFT DIVERTED. SMOKE ODOR WAS FROM THE FAILURE OF THE GALLEY/LAVATORY EXHAUST FAN. WINDSHEILD HEAT OPS CHECKED GOOD IAW AMM 30-41-01.

Part: SEAT TRACK — CORRODED (BS 683.5-836.5) · airframe 16,526 hrs · 11,458 cycles

SEAT TRACK RBL 9 BETWEEN FS 683.50 AND 836.50 CORRODED BEYOND ALLOWABLE LIMITS. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED SEAT TRACK IAW AMM TASK 53-0-49-400-801.

Part: SEAT TRACK — CORRODED (BS 683.5-836.5) · airframe 16,526 hrs · 11,458 cycles

SEAT TRACK RBL 9 BTWN FS 683.50 AND 836.50 CORRODED BEYOND ALLOWABLE LIMITS. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED SEAT TRACK IAW AMM TASK 53-0-49-400-801.

Part: SEAT TRACK — CORRODED (BS 683-836) · airframe 16,526 hrs · 11,458 cycles

SEAT TRACK AT LBL 9 FS 683 AND 836 CORRODED BEYOND ALLOWABLE LIMITS. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALL SEAT TRACK. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 16,526 hrs · 11,458 cycles

BS 280 FLOORBEAM IS CORRODED. REPAIRED IAW SRM 51-42-06, 51-42-13, 51-42-21 AND REO 670-53-11-047.

Part: SEAT TRACK — CORRODED (BS 977) · airframe 16,526 hrs · 11,458 cycles

RIGHT SIDE WALL SEAT TRACK AT FS 977.00 HAS CORROSION. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. COMPLIED WITH REO NR 670-53-00-338. INSTALLED NEW SEAT TRACK IAW AMM TASK 53-00-49-400-801.

Part: FLOOR PANEL — CRACKED (E/E BAY) · airframe 16,526 hrs · 11,458 cycles

ELECTRICAL BAY FLOOR PANEL CRACKED ON RT SIDE AT FS193. CRACK EXTENDS UNDER ADG PUMP DOUBLER. REPAIRED IAW GREO 670-53-11-509.

Part: SEAT TRACK — CORRODED (BS 836.5-977) · airframe 16,526 hrs · 11,458 cycles

SEAT TRACK AT LBL 9.00 BETWEEN FS 836.50 - FS 977.00 HAS CORROSION. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801-A03. COMPLIED WITH REO 670-53-00-338. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 836.5-977) · airframe 16,526 hrs · 11,458 cycles

SEAT TRACK AT RBL 9.00 BETWEEN FS 836.50 - FS 977.00 HAS CORROSION. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801-A03. COMPLIED WITH REO NR 670-53-00-338. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 977) · airframe 16,526 hrs · 11,458 cycles

LEFT SIDE WALL SEAT TRACK AT FS 977.00 HAS CORROSION. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. COMPLIED WITH REO 670-53-00-338. INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-00-49-400-801.

Part: FLOOR PANEL — CRACKED (E/E BAY) · airframe 16,526 hrs · 11,458 cycles

ELECTRICAL BAY FLOOR PANEL CRACKED ON LT SIDE AT FS 193. REPAIRED IAW GREO 670-53-11-509.

Part: WEB — CORRODED (BS 280) · airframe 16,526 hrs · 11,458 cycles

LT 280 WEB IS CORRODED. REPAIRED IAW REO 670-53-11-594.

Part: STRINGER — CORRODED (BS 295-319.7) · airframe 16,526 hrs · 11,458 cycles

CORROSION ON BASE OF STR 26 RT BETWEEN FRAMES 295.00 AND 319.70. CORROSION WAS FOUND OUT OF LIMITS, REMOVED, DRILLED AND INSTALLED NEW STRINGER IAW SRM 51-42-06-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 16,526 hrs · 11,458 cycles

BS 280 FLOORBEAM IS CORRODED. R & R FLOORBEAM IAW SRM CH 51-42-06-001-001 & 51-42-21-001-001 AND REO 670-53-11-047.

Part: WEB — CORRODED (BS 280) · airframe 16,526 hrs · 11,458 cycles

RT 280 WEB IS CORRODED. CORROSION EXCEEDS ALLOWABLE LIMITS IAW SRM 53-11-10-201-003-A01. PERFORMED EDDY CURRENT INSPECTION OF CUT LINE IAW REO 670-53-11-594 IAW NDTM PART 1, 51-20-006. NO INDICATIONS NOTED. REPAIRED IAW REO 670-53-11-594.

Part: SEAT TRACK — CORRODED (BS 349-477.4) · airframe 16,526 hrs · 11,458 cycles

RT SEAT TRACK, RBL 9.00, CORRODED AT FWD SECTIONS FROM FS 349.00 TO FS 477.40. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 349-477.4) · airframe 16,526 hrs · 11,458 cycles

LEFT SEAT TRACK, LBL 9.00, CORRODED AT FWD SECTIONS FROM FS349.00 TO FS 477.40. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. COMPLIED WITH REO 670-53-00-338. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 785-830) · airframe 16,526 hrs · 11,458 cycles

RIGHT SIDE SEAT TRACK JUST AFT OF OVERWING EMERGENCY EXIT AT FS 785.15 TO FS 830.40 CORRODED. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801-A03. FABRICATED NEW SEAT TRACK IAW REO 670-53-00-074. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 597-661) · airframe 16,526 hrs · 11,458 cycles

LEFT SEAT TRACK CORRODED LBL 9.00 FROM FS 597.00 TO 661.00. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. COMPLIED WITH REO 670-53-00-338. INSTALLED NEW SEAT TRACK IAW 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 785-830) · airframe 16,526 hrs · 11,458 cycles

LEFT SIDE SEAT TRACK JUST AFT OF OVERWING EMERGENCY EXIT AT FS 785.15 TO FS 830.40 CORRODED. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801-A03. FABRICATED NEW SEAT TRACK IAW REO 670-53-00-338. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-701.

Part: FLOOR SUPPORT — CORRODED (BS 280 E/E BAY) · airframe 16,526 hrs · 11,458 cycles

AVIONICS FLOOR PANEL AT FS 280.00 FWD SUPPORT ANGLE CORRODED. REMOVED FWD SUPPORT ANGLE, DRILLED NEW ANGLE AND INSTALLED IAW SRM 51-42-06-001-001, SRM 51-42-06-001-001-A01, SRM 51-42-13-001-001-A01, SRM 51-42-15-001-001-A01 AND SRM 51-42-21-001-001-A01.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 16,526 hrs · 11,458 cycles

PAX DOOR AFT DRAG ANGLE IS CRACKED. CUT OUT AND REMOVED CRACKED DRAG ANGLE SECTION IAW SRM 52-0008, PARA 4. B(1). PERFORMED T/E INSPECTION OF CUTLINE IAW SRM 52-11-04-201-002-A01, & IAW NDTM PART 1, 51-20-006. NO INDICATIONS NOTED. REPAIRED IAW SRM 52-11-04-201-002-A01.

Part: PLACARD — DETERIORATED (CABIN) · airframe 16,392 hrs · 11,362 cycles

PAX DOOR EXIT PLACARD PEELING. R & R PAX DOOR OPEN PLACARD IAW AMM 20-60-04. R & R PAX DOOR OPEN PLACARD IAW AMM 20-60-04. (CLOSED)

Part: GLOWSTRIP — MISSING · airframe 14,753 hrs · 10,269 cycles

PHOTOELUMINESENT STRIP MISSING IN FRONT OF WARDROBE AT ENTRY WAY. INSTALLED PHOTOELUMINESENT EMERGENCY FLOOR PATH MARKING IN FRONT OF WARDROBE IN ENTRY WAY IAW AMM SUPPLEMENT ASA 33-51-01. INSTALLED PHOTOELUMINESENT FLOOR PATH MARKING IN FRONT OF WARDROBE IN ENTRY WAY IAW AMM 33-51-01.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 13,313 hrs · 9,208 cycles

EMERGENCY LIGHT ON SIDEWALL AT SEAT 12CD HAS INOP LAMPS. R & R FLOOR LEVEL EMERGENCY FLOOD LIGHTS AS REQUIRED IAW AMM 33-51-05. OPS CHECK GOOD.

Part: SEAT TRACK — CORRODED (BS 379-533) · airframe 13,030 hrs · 9,005 cycles

MAIN CABIN LT SIDEWALL SEAT TRACK HAS AREAS OF CORROSION BS 379- BS 533. CLEANED MAIN CABIN LT SIDEWALL SEAT TRACK FROM BS 379-533 IAW SRM 51-21-06, REMOVED CORROSION ON MAIN CABIN LT SIDE WALL SEAT TRACK FROM BS 379-533 IAW SRM 51-21-06 ORIGINAL MAT .150 REMOVED .015 REMAINING MAT .135 FOUND IN LIMITS IAW SRM 53-21-49. APPLIED ALODINE IAW SRM 51-21-16.

Part: SEAT TRACK — CORRODED (BS 409-533) · airframe 13,030 hrs · 9,005 cycles

MAIN CABIN RT SIDEWALL SEAT TRACK HAS AREAS OF CORROSION BS 409-BS 533. CLEANED MAIN CABIN RT SIDEWALL SEAT TRACK FROM 409-533 IAW SRM 51-21-06, REMOVED CORROSION ON MAIN CABIN RT SIDEWALL SEAT TRACK FROM BS379-533 IAW SRM 51-21-06 ORIGINAL MAT .150 REMOVED .010 REMAINING MAT .140. FOUND IN LIMITS IAW SRM 53-21-49. APPLIED ALODINE IAW SRM.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 13,021 hrs · 8,996 cycles

F/A FOUND MEGA PHONE DOES NOT WORK. FLT 4957 CX / R & R OLD MEGAPHONE W/ NEW IAW 25-61-14. OPS CK GOOD. ACFT OK FOR SVC. (CLOSED)

Part: WARNING LIGHT — ILLUMINATED · airframe 11,668 hrs · 7,981 cycles

DURING FLIGHT, LT BLEED DUCT MASTER WARNING ILLUMINATED [EMERGENCY DECLARED].

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,540 hrs · 7,878 cycles

RT AFT EXTERNAL EMERGENCY LIGHT WILL NOT ILLUMINATE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,540 hrs · 7,878 cycles

ON CEILING PNL 263CLC FWD EMERGENCY EXIT LIGHT WILL NOT ILLUMINATE.

Part: SEAT TRACK — CORRODED (BS 495-555) · airframe 11,540 hrs · 7,877 cycles

CORROSION ON SEAT TRACK RT FS 555R TO APPROX FS 495R. REMOVED SEAT TRACK PER CRJ700 IAW AMM 53-00-49-000-801. REPLACED SEAT TRACK WITH NEW P/N N126-2075 PER AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 349) · airframe 11,540 hrs · 7,877 cycles

SEAT TRACK CORRODED AT NR 2 GALLEY INBD MOUNT AREA - FS349.0. REMOVED SEAT TRACK PER SRM 51-41-023-001-001-A01. 08-28-09. (32) 2. INSTALLED NEW SEAT TRACK PER SRM 51-41-02-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 11,540 hrs · 7,877 cycles

COCKPIT FLOORBEAM FS 280 LBL 11.00" TO RBL 11.00", SEVERELY CORRODED.

Part: ELEMENT — OVERHEATED (COCKPIT) · airframe 10,958 hrs · 7,432 cycles

F/O LOWER WINDSHIELD HEATING ELEMENT OVERHEATING. FLT 5007 DEL 22 MINS.

Part: WARNING SYSTEM — ACTIVATED (BLEED AIR SYS) · airframe 10,869 hrs · 7,359 cycles

LT BLEED DUCT WARNING AFTER 75 SECONDS RECEIVED LT BLEED DUCT CAUTION MSG. FOLLOWED QRH FOR BOTH MSGS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,852 hrs · 7,346 cycles

EMERGENCY EXIT LIGHT AT SERVICE DOOR FLOOR LEVEL INOP.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 10,565 hrs · 7,135 cycles

MEGAPHONE INOPERATIVE, WILL NOT WORK AT ALL (NO VOLUME).

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 10,565 hrs · 7,135 cycles

MEGAPHONE INOPERATIVE. REMOVED AND REPLACED MEGAPHONE IAW MM 25-61-14. OPS CK OK.

Part: RELAY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 8,333 hrs · 5,481 cycles

THE "EMER LTS ON" WHITE STATUS MESSAGE CONTIOUSLY CYCLING ON AND OFF. FLT 4192 DEL 136 MINS. T/S SYSTEM - FOUND RELAY 135 JB11 BAD. REMOVED AND REPLACED RELAY. PERFORMED FUNCTIONAL TEST OF EMERGENCY LIGHTS IAW AMM 33-51-01 PG 526-532. (B)

Part: PUMP — MALFUNCTIONED (HYD SYSTEM) · airframe 8,333 hrs · 5,481 cycles

RECEIVED NR 2 HYD LOW PRESS IN FLT FOLLOWED QRH OBSERVED NR 2 SYSTEM AT 0. FLT 4189 CX. EMERGENCY DECLARED. REMOVED AND REPLACED NR 2 ENGINE DRIVEN HYDRAULIC PUMP IAW AMM 29-10-01, OPS AND LEAK CK GOOD OK FOR SERVICE. (B)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,706 hrs · 5,029 cycles

THE 2 MOST AFT CEILING EMERGENCY LIGHTS INOP.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 7,042 hrs · 4,574 cycles

FOUND STA 280 FWD FLOOR SUPPORT ANGLE CORRODED AT BL 0.

Part: STEERING SYS — MALFUNCTIONED (NLG) · airframe 7,029 hrs · 4,565 cycles

AFTER TAKEOFF RECEIVED NWS INOP CAUTION MSG. FOLLOWED QRH. AFTER LANDING RESET SYS USING CIRCUIT BREAKERS. MSG EXTINGUISHED. EMERGENCY EQUIPMENT ON STANDBY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 6,734 hrs · 4,359 cycles

THE 4TH CABIN CEILING EMERGENCY LIGHT FROM ENTRY FOUND INOP.

Part: STEERING SYS — FAULTED (NLG) · airframe 6,414 hrs · 4,140 cycles

AFTER T/O FROM ATL NWS FAULTED. RESET SYSTEM C/B`S AFTER LANDING IN IAH. SYSTEM RESET. TOWER DECLARED EMERGENCY.

Part: LIGHT — WORN (CABIN) · airframe 5,812 hrs · 3,720 cycles

EMERGENCY FLOOR LIGHTING TAPE WORN AWAY NEAR GALLEY CARTS.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 5,444 hrs · 3,474 cycles

LEFT OVERWING EMERGENCY EXIT, LOWER EMERGENCY EXIT SIGN IS INOP. FOUND NR 3 BATTERY PACK VOLTS LOW. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW CRJ 200 AMM 33-00. OPS CHECK GOOD. {SDR - CLOSED}

Part: LIGHT — NO TEST (CABIN) · airframe 3,772 hrs · 2,366 cycles

EMERGENCY LIGHTS WON`T TEST. FLT 4246 DEL 40 MINS. CHARGED BATTERY PACKS FOR 45 MINUTES. OPS CHECKED GOOD. (CLOSED)

Part: LIGHT — INOPERATIVE (CABIN)

DURING A GROUND INSPECTION IN ATL, ALL OF THE EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED THE EMERGENCY EXIT LIGHTS AND NO DEFECTS WERE NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)