N861AS

Part: INTERCOSTAL — CRACKED (PAX DOOR AREA) · airframe 37,420 hrs · 34,994 cycles

PAX DOOR LOWER FWD INTERCOSTAL HAS CRACK IN RADIUS. REPAIRED IAW WITH REO 601R-52-11-402 REV-H DATED 2007-11-01

Part: INTERCOSTAL — CRACKED (PAX DOOR AREA) · airframe 37,420 hrs · 34,994 cycles

PAX DOOR LOWER AIRCRAFT INTERCOSTAL HAS CRACK IN RADIUS. REPAIRED IAW WITH REO 601R-52-11-402 REV-H DATED 2007-11-01

Part: SKIN — CORRODED (LT WING) · airframe 37,420 hrs · 34,994 cycles

RH WING LOWER WING PLANK ACCESS HOLE 640BB LANDING HAS EVIDENCE OF CORROSION ON INBD AND OUTBD END. REPAIRED WING PLANK ACCESS HOLE 640BB I.A.W BOMBARDIER REO 601R-57-21-030 REV. L

Part: SKIN — CORRODED (RT WING) · airframe 37,420 hrs · 34,994 cycles

RH WING LOWER WING PLANK ACCESS HOLE 650HB LANDING HAS EVIDENCE OF CORROSION ON OUTBD END. REPAIRED WING PLANK ACCESS HOLE 640BB I.A.W BOMBARDIER REO 601R-57-21-030 REV. L

Part: SKIN — CORRODED (LT WING) · airframe 37,420 hrs · 34,994 cycles

LH WING LOWER WING PLANK ACCESS HOLE 640BB LANDING HAS EVIDENCE OF CORROSION ON INBD AND OUTBD END. REPAIRED WING PLANK ACCESS HOLE 640BB I.A.W BOMBARDIER REO 601R-57-21-030 REV. L

Part: SKIN — CORRODED (LT WING) · airframe 37,420 hrs · 34,994 cycles

LH WING LOWER WING PLANK ACCESS HOLE 650HB LANDING HAS EVIDENCE OF CORROSION ON INBD AND OUTBD ENDS. REPAIRED I.A.W BOMBARDIER REO 601R-57-21-030 REV. L DATED 2014-02-05

Part: SKIN — DENTED (BS 250-265) · airframe 37,420 hrs · 34,994 cycles

DENT ON LH FUSELAGE FS265-250 BETWEEN STR 24L-25L. REPAIRED PER STS EA 30-2018-196 REV --DATED 12/06/2018.

Part: INDICATOR — FAILED (COCKPIT) · airframe 36,580 hrs · 34,054 cycles

STBY AIRSPEED INDICATOR DID NOT COME ALIVE ON TAKE OFF ROLL, ABORTED APPROXIMATELY 80 KNOTS. REMOVED AND REPLACED STBY ISI, OPS CHECKED GOOD IAW AMM 34-14-01 (34-12-01 - IPC ITEM 5).

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 35,375 hrs · 32,685 cycles

FOUND EMERGENCY LIGHTS INOPERATIVE, TWO IN THE CABIN & TWO EXTERNAL EMERENCY LIGHTS. TROUBLESHOT IAW WDM 33-52-00 AND 33-51-00 AND FOUND BATTERY PACK NR 4 TO BE BAD. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-51-04-000-801, AND AMM 33-51-04-400-801. SELF TEST OF BATTERY PACK AND CHARGER ASSEMBLY TESTED GOOD IAW AMM 33-51-04-740-005. ALL LIGHTS WORKING.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 35,375 hrs · 32,685 cycles

FOUND LBL 9 SEAT TRACK FROM BS 409+128 - 559 CORRODED OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802, AND AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 35,375 hrs · 32,685 cycles

FOUND RBL 9 SEAT TRACK FROM BS 409+128 - 559 CORRODED OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802, AND AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 35,375 hrs · 32,685 cycles

FOUND RBL 9 SEAT TRACK FROM BS 559 - 559+86 CORRODED OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802, AND AMM 53-01-11-400-802.

Part: BUSHING — DAMAGED (RT MLG TRUNNION) · airframe 35,375 hrs · 32,685 cycles

RIGHT FWD TRUNNION BUSHINGS DAMAGED. REMOVED TRUNNION AND INSTALLED FIRST OVERSIZE BUSHING AND FINAL REAMED PER REO601R-57-21-003.

Part: STRAP — DAMAGED (LEFT) · airframe 35,375 hrs · 32,685 cycles

WHILE PERFORMING SB601R-57-046 REV C FOUND AFT HOLE ON LT STEEL STRAP AT OVERSIZED. REPAIRED IAW REO 601R-57-21-2476.

Part: STRAP — DAMAGED (RIGHT) · airframe 35,375 hrs · 32,685 cycles

WHILE PERFORMING SB601R-57-046 REV C, FOUND AFT HOLE ON RT STEEL STRAP OVERSIZED. REPAIRED IAW REO 601R-57-21-2476.

Part: BUSHING — DAMAGED (RT MLG TRUNNION) · airframe 35,375 hrs · 32,685 cycles

RT AFT TRUNNION BUSHING DAMAGED. REAMED THE TRUNNION AND INSTALLED A FIRST OVERSIZE BUSHING AND FINAL REAMED IAW SB 601R-57-21-003.

Part: BUSHING — DAMAGED (LT MLG) · airframe 35,375 hrs · 32,685 cycles

LEFT AFT TRUNNION BUSHING DAMAGED. REAMED THE TRUNNION AND INSTALLED A FIRST OVERSIZED BUSHING AND FINAL REAMED IAW REO601R-57-21-003.

Part: SEAT TRACK — CORRODED (BS 559-574) · airframe 35,375 hrs · 32,685 cycles

SEAT TRACK BS 559+112 - 574, LBL 9 IS CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-61-49. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, AND AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 35,375 hrs · 32,685 cycles

SEAT TRACK BS 559+80 - 559+96, LBL 27 IS CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-61-49. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, AND AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 35,375 hrs · 32,685 cycles

SEAT TRACK BS 559+80 - 559+96, LBL 9 IS CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-61-49. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, AND AMM 53-00-49-400-801.

Part: FLOORBEAM — CORRODED (BS 589) · airframe 35,375 hrs · 32,685 cycles

FLOORBEAM TEE BS 589 BETWEEN RBL 27 - 43 IS CORRODED. REMOVED CORROSION IAW SRM 51-21-06 AND FOUND OUT OF LIMITS IAW SRM 53-00-00. REMOVED AND REPLACED THE FLOORBEAM TEE IAW SRM 51-42-06.

Part: FLOOR SUPPORT — CORRODED (BS 449-529) · airframe 35,375 hrs · 32,685 cycles

RIGHT FLOOR SUPPORT BS 449.85 - 529 HAS SEVERAL SPOTS OF CORROSION, FOUND TO BE OUT OF LIMITS IAW ECTC REO 601R-53-41-666-01 REV A, TABLE 1, INSTALLED REPAIR I IAW REO 601R-53-41-2074.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 35,375 hrs · 32,685 cycles

FLOOR SUPPORT RBL 9, BS 574-621 CORRODED IN MULTIPLE AREAS. REMOVED CORROSION IAW SRM 51-21-06, AND FOUND OUT OF LIMITS IAW GREO 601R-53-00-005. REPAIRED IAW ECTC REO 601R-53-61-3780 & REO 601R-53-61-3780 REV A & IAW SRM 51-42-13.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 35,375 hrs · 32,685 cycles

SEAT TRACK BS 559+96 - 559+112, RBL 9 IS CORRODED, FOUND TO BE OUT OF LIMITS IAW SRM 53-61-49. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, AND AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 559-574) · airframe 35,375 hrs · 32,685 cycles

SEAT TRACK RBL 9, BS 559+112 - 574 CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-61-49. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, AND AMM 53-00-49-400-801.

Part: FLOORBEAM — CORRODED (BS 565) · airframe 35,375 hrs · 32,685 cycles

FLOORBEAM AT RBL 9, BS 565 IS CORRODED. CORROSION REMOVED IAW SRM 51-21-06, AND FOUND OUT OF LIMITS IAW GREO 601R-53-00-0005. REPAIRED IAW SRM 53-00-43. .

Part: SEAT TRACK — CORRODED (BS 559) · airframe 35,375 hrs · 32,685 cycles

SEAT TRACK BS 559+96 - 559+112 AT RBL 27 CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-61-49. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, AND AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 35,375 hrs · 32,685 cycles

LEFT SEAT TRACK, BS 364 TO 409+16 CORRODED AT NUMEROUS LOCATIONS, OUT OF LIMITS. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. REMOVED AND REPLACED IAW AMM 53-01-11-000-802, AND AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 460 & 473) · airframe 35,375 hrs · 32,685 cycles

LEFT SEAT HAS CORROSION IN 2 SPOTS, BS 460 AND 473.15. REMOVED AND REPLACED THE SEAT TRACK IAW AMM TSK 53-01-11-000-802, EC/TC REO 601R-53-00-633 REV O, AND AMM TASK 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 473) · airframe 35,375 hrs · 32,685 cycles

RIGHT SEAT TRACK IS CORRODED AT BS 473.15. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11, REO 601R-53-00-633. REV -- B, AMM 53-01-114, AND REO 601R-53-00-633 REV--, B STEPS 6-7.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 35,375 hrs · 32,685 cycles

LEFT SEAT TRACK CORRODED BS 559+70. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802.

Part: SEAT TRACK — CORRODED (BS 385) · airframe 35,375 hrs · 32,685 cycles

RIGHT SEAT TRACK CORRODED BS 385. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802, AND AMM 53-01-1-400-802.

Part: HINGE FITTING — GOUGED (PAX DOOR) · airframe 35,375 hrs · 32,685 cycles

HINGE ON FUSELAGE NR 4 LUG IS GOUGED. REPAIRED IAW ECTC 601R-53-21-814 TUPE 1. MAJOR REPAIR.

Part: UPLOCK SENSOR — OUT OF ADJUST (RT MLG) · airframe 33,817 hrs · 30,992 cycles

AFTER TAKEOFF, RECEIVED A GEAR DISAGREE WARNING WITH ROD RT MAIN GEAR INDICATION ON EICAS. RAN QRH WITH MANUAL GEAR RELEASE, GEAR CAM DOWN AND LOCKED NORMALLY, ACFT RETURNED TO DEPARTURE AFTER T/O. RESET RT MLG UPLOCK TARGET AND ADJUST UPLOCK SENSOR IAW AMM 32-32-05 AND SWING GEAR IAW AM 32-30-00. OPS CHECK GOOD. ACFT OK FOR SERVICE.

Part: PIN — OUT OF POSITION (PAX DOOR) · airframe 33,252 hrs · 30,401 cycles

F/A REPORTS PASSENGER DOOR HARD TO OPEN AND CLOSE. FOUND PIN AT BOTTOM STEP OUT APPROXIMATELY 2". PUSH IN PIN FLUSH WITH STEP. PERFORMED OPS TEST ON PASSENGER DOOR IAW AMM 52-11-00. OPS TEST GOOD. NO FURTHER DEFECT NOTED AT THIS TIME.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 33,214 hrs · 30,367 cycles

NR 4 EMERGENCY FLOOD LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM 33-51-16. OPS CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 32,690 hrs · 29,842 cycles

LEFT NR 1 EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED LEFT NR 1 EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECK GOOD.

Part: WINDOW — FAILED (COCKPIT) · airframe 32,651 hrs · 29,801 cycles

LT WINDOW SHATTERED DURING CLIMBOUT. COMPLIED WITH QRH, RETURNED TO DEPARTURE AFTER T/O. EMERGENCY DECLARED. R & R LT WINDOW IAW AMM 56-12-01, APC 56-12-00, FIG 11, ITEM 10C.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 31,405 hrs · 28,553 cycles

FLASHLIGHT AT F/A STATION NOT WORKING. R & R FLASHLIGHT BATTERIES IAW AMM 25-61-00. OPS CHECKED GOOD.

Part: ANGLE — CORRODED (BS 333) · airframe 31,365 hrs · 28,509 cycles

ANGLE AT BS 333 ON LOWER SERIVCE DOOR SILL IS CORRODED. REPLACED ANGLE IAW DWG 601R38303. MAJOR REPAIR.

Part: ANGLE — CORRODED (BS 319) · airframe 31,365 hrs · 28,509 cycles

ANGLE AT BS 319 ATTACHED TO UPPER SERIVCE DOOR SILL IS CORRODED. REMOVED AND REPLACED ANGLE IAW SRM 51-42-21 & SRM 51-40-11.

Part: SEAT TRACK — CORRODED (BS 394-409) · airframe 31,365 hrs · 28,509 cycles

LBL 9 SEAT TRACK SEGMENT BS 394-409+128 CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49 AND 53-21-49. REMOVED SEAT TRACK IAW 53-01-11. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.

Part: BRACKET — CORRODED (BS 319) · airframe 31,365 hrs · 28,509 cycles

LOWER FWD BRACKET AT SERVICE DOOR BS 319 IS CORRODED OUT OF LIMITS IAW SRM TR53-27. REMOVED AND REPLACED THE BRACKET IAW SRM 51-42-21.

Part: FRAME — CORRODED (BS 349) · airframe 31,365 hrs · 28,509 cycles

FRAME BS 349 CORRODED AT SERVICE DOOR AFT SECTION RBL 42. BLENDED CORROSION IAW SRM 51-21-06. MAJOR REPAI. REPAIRED IAW REO NR 601R-53-21-2554.

Part: ANGLE — CORRODED (BS 349) · airframe 31,365 hrs · 28,509 cycles

SERVICE DOOR UPPER FRAME ANGLE CORRODED AT FS 349. REMOVED UPPER FRAME ANGLE IAW SRM 51-40-11 AND INSTALLED IAW DWG 601R38303.

Part: ANGLE — CORRODED (DOOR SILL) · airframe 31,365 hrs · 28,509 cycles

SERVICE DOOR LOWER SILL ANGLE CORRODED AT SEVERAL AREAS. REMOVED SERVICE DOOR LOWER SILL ANGLE IAW SRM 51-42-21. DRILLED AND LOCATED NEW LOWER SILL ANGLE IAW SRM 51-40-11. INSTALLED LOWER SILL ANGLE ON SERVICE DOOR SURROUND IAW SRM 51-42-06 AND DWG 601R38303.

Part: FLOOR SUPPORT — CORRODED (BS 473) · airframe 31,365 hrs · 28,509 cycles

CORROSION ON RT FLOOR SUPPORT BS 473.15 UNDER THE OVERWING EMERGENCY EXIT. REPAIRED IAW EC/TC REO 601R-53-41-666-01 AND REO 601R-53-41-666, REV C. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 364-394) · airframe 31,365 hrs · 28,509 cycles

LBL 9, SEAT TRACK SEGMENT BS 364-394 CORRODED. R & R SEAT TRACK IAW AMM 53-01-11.

Part: FLOOR SUPPORT — CORRODED (BS 349) · airframe 31,365 hrs · 28,509 cycles

RT CABIN FLOOR SUPPORT CORRODED AT FS 349. REPAIRED IAW REO/ ECTC 601R-53-00-530.

Part: INTERCOSTAL — CRACKED (CARGO DOOR) · airframe 31,365 hrs · 28,509 cycles

CARGO DOOR INTERCOSTAL CRACKED INSIDE LOWER AFT INSPECTION HOLE. R & R INTERCOSTAL IAW SRM 51-42-21-00, 51-42-06-00 & DWG 601R35027. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (BS 449-484) · airframe 31,365 hrs · 28,509 cycles

LT FLOOR SUPPORT BETWEEN BS 449.85-484 HAS SEVERAL SPOTS OF CORROSION UNDER THE OVERWING EMERGENCY EXIT. REPAIRED IAW EC/TC REO 601R-53-41-666-01 AND REO 601R-53-41-666, REV C. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 364-394) · airframe 31,365 hrs · 28,509 cycles

SEAT TRACK SEGMENT BS 364-394 CORRODED. R & R SEAT TRACK IAW AMM 53-01-11-000-802.

Part: DOOR SILL — CORRODED (CARGO DOORWAY) · airframe 31,365 hrs · 28,509 cycles

AFT CARGO DOOR SILL HAS CORROSION AROUND NUT PLATE REMOVED CORROSION IAW SRM 51-21-06 AND COMPLIED WITH REO 601R-53-00-526. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 31,365 hrs · 28,509 cycles

CORROSION RT FLOOR SUPPORT BETWEEN BS 559+96-559+112. REMOVED CORROSION IAW SRM 51-21-06. REPAIRED IAW REO 601R-53-00-526. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 394-409) · airframe 31,365 hrs · 28,509 cycles

RBL 9 SEAT TRACK SEGMENT BS 394-409+128 CORRODED. REMOVED CORRRODED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.

Part: SHROUD — GOUGED (RT AILERON) · airframe 31,386 hrs · 28,533 cycles

RT AILERON SHROUD 698BB HAS TOOLING DAMAGE. BLENDED AND EVALUATED AILERON SHROUD IAW SRM 57-00-00. BLEND AREA OUT OF LIMITS IAW SRM 57-51-31. RECEIVED AND COMPLIED WITH EA 25-2014-179, SECTION 1 PERMENENT REPAIR.

Part: BULKHEAD — GOUGED (BS 621) · airframe 31,365 hrs · 28,509 cycles

FIVE SPOTS WITH DAMAGE FROM SCREWS ON FWD SIDE OF AFT PRESSURE BULKHEAD AT BS 621. REPAIRED IAW REO 601R-53-61-2155, REV A. MAJOR REPAIR.

Part: ANGLE — CRACKED (BS 625) · airframe 31,365 hrs · 28,509 cycles

LEFT BS 625 ANGLE CRACKED. R & R ANGLE IAW SRM 51-42-20, FIG 14.

Part: ANGLE — CRACKED (BS 625) · airframe 31,365 hrs · 28,509 cycles

RIGHT BS 625 ANGLE CRACKED. R & R ANGLE IAW SRM 51-42-20, FIG 14.

Part: INSULATION — TORN (WIRE BUNDLE) · airframe 31,365 hrs · 28,509 cycles

TORN PROTECTIVE SHEATHING ON WIRE BUNDLES INSIDE LT PYLON ZONE 412. REPAIRED WIRES IAW REO 601R-20-12-001.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 31,365 hrs · 28,509 cycles

THE MID FWD SERVICE DOOR EMERGENCY LIGHT AND BOTH PAX DOOR EMERGENCY LIGHTS FAILED OPS TEST. REMOVED AND REPLACED NR 2 EMERGENCY BATTERY PACK IAW AMM 33-51-04-000-801 AND AMM 33-51-04-400-801. PERFORMED OPS TEST OF THE EMERGENCY EXIT LIGHTS IAW IAW AMM 33-51-00-710-801. OPS TESTED GOOD.

Part: SKIN — DENTED (BS 283) · airframe 31,365 hrs · 28,509 cycles

DENT ON LOWER FWD FUSLAGE EXTERNAL AT BS 283 BETWEEN S24-25R. EVALUATED DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM TR 53-33. REPAIRED IAW REO 601R-53-21-2547. MAJOR REPAIR.

Part: LATCH — OUT OF ADJUST · airframe 30,666 hrs · 27,824 cycles

PASSENGER DOOR BINDING CLOSED WHEN F/A TRIED TO OPEN IT. EVENTUALLY LET LOOSE AND OPENED. INSPECTED AND ADJUSTED BOTH LOWER LATCHES IAW IAW AMM 52-11-23, AND LATCH ASSY IAW AMM 52-11-23. OPS CHECKED GOOD. ALL INDICATIONS NORMAL.

Part: HANDLE — BINDING (PAX DOOR) · airframe 30,666 hrs · 27,824 cycles

WHEN CLOSING PAX DOOR, TEE HANDLE WILL NOT STAY IN UNLESS PULLED HARD. WHEN OPENING PAX DOOR, LEVER JAMMED. JIGGLING TEE HANDLE FREED LEVER AND DOOR OPENED. R & R PAX DOOR PULL IN HANDLE ASSY IAW AMM 52-11-03. OPS TEST GOOD. NO DEFECTS NOTED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,272 hrs · 27,415 cycles

NR 3 CEILING EMERGENCY FLOOD LIGHT INOPERATIVE. REPLACED LAMPS IAW AMM 33-51-16. OPS CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 28,765 hrs · 25,857 cycles

NR 7 EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: SEAT TRACK — CORRODED · airframe 27,584 hrs · 24,614 cycles

THE RT SIDE PASSENGER SEAT TRACK IS BADLY CORRODED. R & R SEAT TRACK SECTIONS AT RBL 9 FROM FS 364 TO FS 409+128 IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.

Part: STRUCTURE — CORRODED (PAX DOOR) · airframe 27,584 hrs · 24,614 cycles

PAX DOOR UPPER AFT CORNER CORRODED BEYOND LIMITS AND OTBD ATTACH ANGLE AT FS 338.00. REMOVED PAX DOOR UPPER AFT CORNER IAW SRM 51-42-06 AND 51-42-21. INSTALLED THE UPPER AFT CORNER ON PAX DOOR USING PN 601R319983-4S AND OTBD ANGLE IAW SRM 51-42-06 AND SRM 51-42-21.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 27,584 hrs · 24,614 cycles

SEAT TRACK CORRODED AT BS 559+96, LBL 9, . REMOVED SEAT TRACK IAW SRM 51-41-02. REPLACED CORRODED SEAT TRACK IAW SRM 51-41-02.

Part: FLOORBEAM — CORRODED (BS 559) · airframe 27,584 hrs · 24,614 cycles

FLOORBEAM FS 559.00, LBL 27 - 43 CORRODED. REMOVED FLOORBEAM STRAP, LOCATED, DRILLED NEW STRAP, IAW SRM 51-42-06 AND SRM 51-40-11. REQUIRES INSTALL OF STRAP. INSTALLED NEW STRAP IAW SRM 51-42-06.

Part: BULKHEAD — CRACKED (BS 621) · airframe 27,591 hrs · 24,622 cycles

FS 621 BULKHEAD FAILS NDT WITH AN INDICATION AT TOP OF CARGO TRACK LBL 27.50. FULL SCREEN HEIGHT. REPAIRED IAW REO 601R-53-61-1541 AND SRM 51-42-06.

Part: STRUCTURE — CORRODED (BS 409-559) · airframe 27,584 hrs · 24,614 cycles

ANGLE HAS MULTIPLE AREAS OF CORROSION FROM FS 409.00+128 THRU 559.00 AT LBL 36-45 IN PASSENGER COMPARTMENT UNDER FLOORBOARDS. REMOVED SURFACE FINISH FROM AREAS OF CORROSION IAW SRM 51-20-00. PREPPED AND PAINTED REPAIR AREA IAW CORROSION AT FS 449.85 FLOOR SILL PANEL FOUND TO BE OUT OF LIMITS IAW REO 601R-53-41-666, REV B. COMPLIED WITH STEP NR 1 OF REO 601R-53-41-1593, STEPS 1-3. COMPLIED WITH EC/TC REO 601R-53-41-666 AND REO 601R-53-41-666, REV B.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 27,584 hrs · 24,614 cycles

CARGO TRACK AT RBL 9 FS 559+12 IS CORRODED. REMOVED CORRODED CARGO TRACK. LOCATED & DRILLED NEW CARGO TRACK IAW SRM 51-40-11. INSTALLED NEW CARGO TRACK IAW SRM 51-41-04.

Part: ISOLATOR — CRACKED (BULKHEAD) · airframe 27,584 hrs · 24,614 cycles

BULKHEAD WEB FWD FACE HAS FIVE CRACKED ISOLATORS. REMOVED DAMAGED ISOLATORS AND INSTALLED NEW ISOLATORS IAW SRM 51-42-13.

Part: FLOORBEAM — CORRODED (BS 559) · airframe 27,591 hrs · 24,622 cycles

FLOORBEAM STRAP FS 559.00, RBL 27 - 43 IS CORRODED. REMOVED CORRODED STRAP IAW SRM 51-42-06. LOCATED AND DRILLED NEW SERVICEABLE FLOORBEAM STRAP IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE FLOORBEAM STRAP IAW SRM 51-42-06.

Part: SMOKE DETECTOR — FALSE INDICATION (LAVATORY) · airframe 24,643 hrs · 21,284 cycles

SMOKE TOILET CAUTION MSG ILLUMATED MOMENTARLY IN FLIGHT. R & R LAV SMOKE DETECTOR, OPS CK GOOD REF AMM 26-16-01.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 24,634 hrs · 21,273 cycles

FAINT ELECTRICAL BURNING ODOR EMANATING OCCASSIONALLY FOR BREIF PERIODS BY FOS DCU SWITCHES. INSPECTED WIRING AND ALL ELECTRICAL COMPONENTS IN THE FOS AREA AND FOUND NO DEFECTS OR EVIDENCE THERE OF IAW ESPM 20-12-00.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 24,518 hrs · 21,130 cycles

FIRST OFFICER FLASHLIGHT INOP. REPLACED FIRST OFFICERS FLASHLIGHT IAW CRJ 200 AMM 25-60-00. A/C OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 23,860 hrs · 20,374 cycles

EMERGENCY LIGHT BATTERY PACK AT CHARGER ASSY NR 2 IS INOP. R & R NR 2 EMERGENCY EXIT LIGHT BATTERY PACK IAW IAW AMM 33-51-04-000/400-801. NR 2 E&E BATTERY PACK SELF TEST CHECKS GOOD IAW AMM 33-54-04-400-810, SUBTASK 33-51-04-740-005.

Part: ATTACH FITTING — CRACKED · airframe 23,860 hrs · 20,374 cycles

FOUND ENGINE SUPPORT BEAM FWD CLIP AT LBL 9.5 HAS A CRACK APPROX .5" IN LENGTH NEAR LOWER FASTENER. R & R CLIP AT ESB AT LBL 9.5 FWD WEB IAW SRM 51-42-06 AND 51-42-22.

Part: ATTACH FITTING — CRACKED · airframe 23,860 hrs · 20,374 cycles

FOUND ENG SUPPORT BEAM FWD CLIP AT RBL 27.50 HAS A CRACK APPROX .5" IN LENGTH NEAR TOP FASTENER. R & R CLIP AT ESB AT RBL 27.5 FWD WEB IAW SRM 51-42-06 AND 51-42-22.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 23,860 hrs · 20,374 cycles

CONTINUATION FROM MWC 255 FLOOR SUPPORT AT LBL 9 FS 621.00 TO 574.00 IS CORRODED. REO 601R-53-61-3729 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUTINE WORK CARD. ALL RIIS HAVE BEEN ACCOMPLISHED BY A TRAINED, QUALIFIED AND AUTHORIZED RII INSPECTOR IAW ASA GMM 5-2 PROCEDURES, PRIOR TO THE ACFT BEING RETURNED TO SERVICE.

Part: SILL — CORRODED (BS 621) · airframe 23,860 hrs · 20,374 cycles

SPLICE FITTING COMMON TO CARGO DOOR SILL AT FS 621 IS CORRODED. BLENDED CORROSION ON SPLICE FITTING COMMON TO CARGO DOOR SILL AT FS 621 MAT. REMOVED 4" X 1.5" X .015". FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00, FIG 101. REMOVED SPLICE, LOCATED AND DRILLED UP NEW SPLICE FITTING IAW SRM 51-42-00, 51-42-21. FITTING REQUIRES INSTALLATION. INSTALLED SPLICE FITTING IAW SRM 51-42-06, 51-42-21.

Part: ANGLE — CRACKED · airframe 23,860 hrs · 20,374 cycles

REAR PRESSURE BULKHEAD AFT SIDE BL 45 STRINGER 14, OBLIQUE ANGLES ARE CRACKED LT AND RT SIDE.

Part: FLOORBEAM — CORRODED (BS 574-621) · airframe 23,860 hrs · 20,374 cycles

FLOORBEAM CAP AT LBL 27 FS 621.00 TO FS 574.00 IS CORRODED. REMOVED FLOORBEAM CAP AT LBL 27 FS 621-574 BY REMOVING ALL FASTENERS IAW SRM 51-42-06 AND 51-42-21. LOCATED AND DRILLED NEW SERVICEABLE CAP IAW SRM 51-40-11. INSTALLED BEAM CAP IAW SRM 51-42-21 AND 51-42-06. COMPLIED WITH REO 601R-53-61-3400.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 23,860 hrs · 20,374 cycles

FS 280.00 FLOOR SUPPORT CLIPS AT RBL & LBL 9 INBD & OTBD ARE CRACKED. REMOVED CLIPS (4 EA) IAW SRM 51-42-21. LOCATED AND DRILLED FS 280, LBL 9 INBD AND OTBD CLIPS AND RBL 9 INBD CLIP IAW SRM 51-40-11. INSTALLED CLIPS IAW SRM 51-42-21. FOUND FS 280, RBL 9 OTBD CLIP CRACKED FROM PREVIOUS REPAIR IAW REO 601R-53-11-171. FABRICATED CLIP AND FILLER IAW REO 601R-53-11-171, STEP 9 AND INSTALLED STEP 13 IAW SRM 51-42-21. COMPLIED WITH EC/TC REO 601R-53-11-171.

Part: CARGO TRACK — CORRODED (BS 559-621) · airframe 23,860 hrs · 20,374 cycles

BAGGAGE RAILS AND ANCHOR PLATES ARE SEVERLY CORRODED AND REQUIRE REPLACEMENT FROM FS 559+112 TO FS 621.00, LBL 9. REMOVED (2 EA) BAGGAGE RAILS AND (2 EA) ANCHOR PLATES FROM LBL 9 FS 559+112 TO FS 621.00 AND DRILLED TO FINAL SIZE. (2 EA) NEW SERVICEABLE BAGGAGE RAILS IAW SRM 51-41-02. INSTALL (2 EA) BAGGAGE RAILS AND (2 EA) ANCHOR PLATES. INSTALLED (2 EA) BAGGAGE RAILS AND (2 EA) ANCHOR PLATES WITH (12 EA) SCREWS IN FWD BAG RAIL SCREWS IN AFT BAG RAIL (4 EA) SCREWS IN ANCHOR PLATES IAW AMM 20-21-00-910-801.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 23,860 hrs · 20,374 cycles

LEFT FLOOR SUPPORT SILL IS CORRODED FROM FS 559.00 TO JUST AFT OF FS 559+48. COMPLIED WITH STEPS 1, 2 OF REO 601R-53-51-125. PERFORMED EDDY CURRENT IAW REO 601R-53-51-125, STEP 3. NO INDICATIONS NOTED. COMPLIED WITH STEPS 4 AND 5 OF REO 601R-53-51-125. COMPLIED WITH EC/TC REO 601R-53-51-125.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 23,860 hrs · 20,374 cycles

LEFT FLOOR SUPPORT SILL IS CORRODED FROM FS 559+48 TO FS 574. COMPLIED WITH STEPS 1, 2 OF REO 601R-53-51-125. PERFORMED EDDY CURRENT IAW STEP 3 OF REO 601R-53-51-125. NO INDICATIONS NOTED. COMPLIED WITH STEPS 4 AND 5 OF REO 601R-53-51-125. ECTC REQUIRED. COMPLIED WITH EC/TC REO 601R-53-51-125.

Part: FLOORBEAM — CORRODED (BS 574-621) · airframe 23,860 hrs · 20,374 cycles

FLOORBEAM CAP AT LBL 9 FS 621.00 TO FS 574.00 IS CORRODED. FOUND 80 PERCENT MATERIAL LOSS ON FLOORBEAM CAP AT LBL 9, FS 589 BRINGING CAP OUT OF LIMITS IAW IAW SRM 53-61-43. REMOVED MS20470AD RIVETS FROM FLOORBEAM CAP AT LBL 9, FS 574 TO 621 IAW SRM 51-42-06. CONTINUE REMOVING BEAM CAP. REMOVED BEAM CAP IAW SRM 51-42-06 AND 51-42-21. INSTALLED BEAM CAP IAW SRM 51-42-21 AND 51-42-06. COMPLIED WITH REO 601R-53-61-3729.

Part: POST — CRACKED (BS 409) · airframe 23,860 hrs · 20,374 cycles

FOUND FS 409+128 VERTICAL POST LBL 18.0 OTBD SIDE HAS INDICATION NOTED APPROX .3" IN LENGTH 70 PERCENT FSH AFT FLANGE RADIUS WL 69.0. FAILED NDT INSP. REMOVED 409+128 LBL 18 POST ASSY. LOCATED AND DRILLED A NEW SERVICEABLE 409+128 LBL 18 OTBD POST IAW SRM 51-42-06. 409+128 LBL 18 POST ASSY REQUIRES INSTALL. DERIVETED POST ASSY. STARTED RIVETING POST ASSY WITH OLD SERVICEABLE INBD POST AND NEW SERVICEABLE OTBD POST IAW SRM 51-42-06. REMAINING RIVETS IN POST ASSY REQUIRE INSTALL. INSTALLED POST ASSY IAW SRM 51-42-06 REO 601R-53-41-889. REQUIRES DINITROL. COMPLIED WITH EC/TC REO 601R-53-41-889 AND MET ALL THE REQUIREMENTS OF REO 601R-53-41-889, REV A.

Part: POST — CRACKED (BS 409) · airframe 23,860 hrs · 20,374 cycles

FOUND FS 409.0+128 VERTICAL POST RBL 18.0 OTBD SIDE HAS INDICATION NOTED APPROX .3" IN LENGTH 80 PERCENT FSH AFT FLANE RADIUS WL 69.0. FAILED NDT INSPECTION. REMOVED VERTICAL POST AT FS 409.0+128, RBL 18 IAW SRM 51-42-06. WHILE WORKING POST REMOVAL NOTICED FACTORY HOLE ON INBD POST TO BE CROOKED AND ELONGATED FOUND TO BE OUT OF LIMITS IAW SRM 51-42-06, FIG 3. LOCATED AND DRILLED INBD TO OTBD POST AT 409+128 RBL 18 IAW SRM 51-42-06. INSTALLED POST AT 409+128, RBL 18 IAW 601R-53-41-889, REV A. COMPLIED WITH EC/TC REO 601R-53-41-889 AND MET ALL THE REQUIREMENTS OF REO 601R-53-41-889 REV.

Part: ISOLATOR — BROKEN (REAR BLKHD) · airframe 23,860 hrs · 20,374 cycles

THERE ARE SEVERAL BROKEN ISOLATORS ON THE REAR PRESSURE BULKHEAD. INSTALLED NEW SERVICEABLE ISOLATORS IAW SRM 51-42-06.

Part: SEAT TRACK — CHAFED (BS 409) · airframe 23,860 hrs · 20,374 cycles

LT & RT FLOOR LEVEL SEAT TRACKS FROM FS 409 TO FS 409+128 ARE CHAFED AND CORRODED AT SEVERAL LOCATIONS. REMOVED FLOOR SEAT TRACK AT LBL 9.0 IAW AMM 53-01-11-000-802. LOCATED AND DRILLED FASTENER HOLES IN FLOOR SEAT TRACK IAW SRM 51-40-11. PARTIALLY INSTALLED SEAT TRACK IAW AMM TASK 53-01-11-400-802. INSTALLED THE REMAINDER OF SEAT TRACK AT LBL 9.00 FROM FS 409-FS 409+128 IAW AMM 53-01-11-400-802.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 23,860 hrs · 20,374 cycles

PAX DOOR AFT DRAG ANGLE IS CRACKED. REPAIRED PAX DOOR AFT DRAG ANGLE IAW EC/TC REO 601R-52-11-513 AND ALL REQUIREMENTS OF REO 601R-52-11-513 ARE MET.

Part: COVER — CRACKED (EXIT SIGN) · airframe 23,860 hrs · 20,374 cycles

EXIT SIGN COVER CRACKED ON PANEL 231BLC. REMOVED EXIT SIGN COVER ON PANEL 231BLC IAW AMM 33-51-14-000-801 STEP 3,A,1 & INSTALLED NEW SERVICEABLE EXIT SIGN COVER ON PANEL 231BLC IAW AMM 33-51-14-400-801 STEP 3,A,1.

Part: ANGLE — CRACKED (BS 621-625) · airframe 23,860 hrs · 20,374 cycles

LT & RT FS 621-FS 625 OBLIQUE ANGLE IS CRACKED. REMOVED CRACKED OBLIQUE ANGLES, LT & RT AT FS 621- FS 625 IAW SRM 51-42-21. FABRICATED NEW OBLIQUE ANGLES ON RT AT FS 621 - FS 625 IAW REPAIR EO 601R-53-61-100. INSTALLED NEW OBLIQUE ANGLES LT & RT AT FS621-FS625 IAW SRM 51-42-21. COMPLIED WITH EC/TC EO 600-53-174 C/W.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,841 hrs · 20,351 cycles

REF DMIL 529916-2. RT AFT EMERGENCY LIGHT INOP. R & R RT AFT EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21. DEFER CLEARED. (CLOSED)

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,841 hrs · 20,351 cycles

RT NR 4 AFT MOST EXTERIOR EMERGENCY LIGHT INOP. R & R RT AFT EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21. DEFER CLEARED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 23,247 hrs · 19,653 cycles

CRACK FOUND ON NDT INSP AT LBL18 APPROX A/4 INCH IN THE FRAME RADIUS. COMPLIED WITH EDDY CURRENT INSP OF THE LBL18 FRAME CUT LINE IAW NDTM 51-20-06 PART 1 AND IAW EC/TC REO601R-53-41-260 AND EC/TC REO601R-53-41-609 NO DEFECTS WERE NOTED. REPAIRED IAW EC/TC REO 601R-53-41-609 REV A AND EC/TC REO 601R-53-41-260 REV D.

Part: BULKHEAD — CRACKED (BS 559) · airframe 23,246 hrs · 19,653 cycles

COMPLIED WITH A SPECIAL DETAILED INSP OF FS559.0 PRESSURE BULKHEAD WEB AND CAP ANGLE LOCAL TO BL9.0 AND BL18.0 LT AND RT IAW NDT MANUAL, PART 6, 53-41-201. (3) CRACKS NOTED LBL18 APPROX .2500" IN THE FRAME RADIUS, RBL18 APPROX .5" IN THE FRAME RADIUS AND RBL18, WL 59.10. DEFECTS NOTED ON SEPARATE N/R CARD IN THIS W/O.

Part: UNKNOWN — CRACKED · airframe 23,247 hrs · 19,653 cycles

CRACK FOUND ON NDT INSP AT RBL18 WL 59.10 1/4 LENGTH. REPAIRED IAW EC/TC REO 601R-53-41-260 AND EC/TC REO601R-53-41-609.

Part: FRAME — CRACKED (FUSELAGE) · airframe 23,247 hrs · 19,653 cycles

CRACK FOUND ON NDT INSP AT RBL18 APPROX 1/2 INCH IN THE FRAME RADIUS. REPAIRED IAW EC/TC REO 601R-53-41-260 AND EC/TC REO 601R-53-41-609.

Part: SWITCH — MALFUNCTIONED (THRUST REVERSER) · airframe 23,149 hrs · 19,548 cycles

CLIMBING THROUGH FL220, REV CAUTION ICON ON LT N1 AND L REV UNLOCKED CAUTION CAME ON INTERMEDIATLEY THEN WENT AWAY. ABOUT 10 SEC LATER MSG RETURNED AND STAYED ON. AIRPLANE YAWED TO THE LT AND WE RAN THE QRH PROCEDURE- WHICH LED TO ENG SHUTDOWN. F/A NOTICED YAW AND VIBRATION. VIBRATION CONTINUED UNTIL SHUTDOWN. EMERGENCY DECLARED. REMOVED AND REPLACED LT T/R SWITCH AND AFDL 537960-1 LT T/R STOW SWITCH RIGGING AND OPS CKS. ACFT OK FOR SERVICE AT THIS TIME.

Part: DOOR — STUCK (MAIN PAX) · airframe 22,529 hrs · 18,853 cycles

NOTICED THE VENT FLAP ON PAX DOOR OPEN WITH THE HANDLE FLUSH. PAX DOOR WILL NOT OPEN.

Part: TRU — MALFUNCTIONED (NR 2) · airframe 22,195 hrs · 18,515 cycles

TRU 2 WOULD SPIKE TO 100A AND A HEAVY ELECTRICAL (BURNING) SMELL WOULD FOLLOW. FLT 5297 DEL 24 MINS.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 22,127 hrs · 18,448 cycles

RT EMERGENCY LIGHT MOST AFT LIGHT (EXT) IS INOP.

Part: UNKNOWN — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 21,425 hrs · 17,756 cycles

EMERGENCY LIGHTS TURN ON IN ARM POSITION.

Part: DOOR — BINDING (PAX DOOR) · airframe 20,591 hrs · 16,981 cycles

PAX DOOR WOULD NOT CLOSE.

Part: STEP — BROKEN (PAX DOOR) · airframe 20,587 hrs · 16,977 cycles

PAX DOOR BOTTOM STEP BROKEN.

Part: FLOORBEAM — CRACKED (BS 621) · airframe 20,075 hrs · 16,484 cycles

LT SIDE FS 621 FLOORBEAM ON FWD SIDE OF AFT PRESSURE BULKHEAD IS CRACKED. (B)

Part: STRUCTURE — CORRODED (AILERON) · airframe 20,075 hrs · 16,484 cycles

CORROSION FOUND IN LEFT AILERON AROUND THE HINGE INTERNAL AREA. OPEN (B)

Part: CHANNEL — CRACKED (CARGO DOOR TRACK) · airframe 20,075 hrs · 16,484 cycles

CARGO DOOR FWD TRACK LWR ATTACH STRUCTURE CHANNEL CRACKED. (MARKED) REMOVED AND REPLACED BAD CHANNEL BRACKET PER SRM 51042-06 .

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 20,075 hrs · 16,484 cycles

CARGO DOOR TRACK SUPPORT TO AFT PRESSURE BULKHEAD LWR ATTACH ANGLE IS CRACKED. REMOVED AND REPLACED ATTACH ANGLE IAW SRM 51-42-21.

Part: BULKHEAD — CRACKED (BS 621) · airframe 20,075 hrs · 16,484 cycles

AFT PRESSURE BULKHEAD FS 621 IS CRACKED AT THE LINTEL FITTING AREA. OPEN (B)

Part: SEAT TRACK — CORRODED (BS 559) · airframe 20,075 hrs · 16,484 cycles

RIGHT SIDE FLOOR SEAT TRACK FORWARD OF LAV AT FS559+112 HAS SEVERE CORROSION. REMOVED DAMAGE BY BLENDING PER SRM 51-12-00, REMOVED DAMAGE FOUND TO BE WITHIN ALLOWABLE DAMAGE LIMITS PER SRM 53-51-49 AND 51-21-49 FIG 101, APPLIED FINISH PER SRM 51-21-16 SG7021421 JOB COMPLETE. (B)

Part: BULKHEAD — CRACKED (BS 202) · airframe 20,075 hrs · 16,484 cycles

SUSPECT CRACK AT FWD PRESSURE BULKHEAD FS 202.75 AT THE PILOTS BRAKE CONTROL PUSH/PULL CABLE LOCATION. THIS SDR WILL REMAIN OPEN PENDING MAINTENANCE DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION. (B)

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 20,075 hrs · 16,484 cycles

FS 280 CLIPS ARE CRACKED AT RBL 9. REMOVED AND REPLACED I/B CLIP AT RBL 9 IAW CRJ200 REO 601R-53-11-136. FABRICATED O/B CLIP FROM 2024-T3 .050" BATCH 845191 SAME AS 601R31113-58 AS INDICATED IN REO 601R-53-11-136 EXCEPT AS NEEDED TO CONFORM TO EXISTING REPAIR DOUBLER CONTOUR. JOB COMPLETE RAP 7025969. (B)

Part: STRUCTURE — CORRODED (PAX DOOR) · airframe 20,075 hrs · 16,484 cycles

PAX DOOR HANDLE SUPPORT WELLS ARE CORRODED AT FS 319 AND FS 33, LBL 45. REMOVED PAX DOOR HANDLE SUPPORT WELLS. STARTED PICKING UP EXISTING HOLES IN NEW PAX DOOR HANDLE SUPPORT WELLS IAW CRJ 200 SRM 51-42-06 SP7025126 7/02/08. (B)

Part: FLOORBEAM — CRACKED (BS 280) · airframe 20,075 hrs · 16,484 cycles

FS 280 CLIPS ARE CRACKED AT LBL 9. REMOVED AND REPLACED FS 280 CLIPS AT LBL 9 IAW CRJ200 REO 601R-53-11-136 JOB COMPLETE RAP 7025969. (B)

Part: DOOR — BINDING (PAX DOOR) · airframe 19,721 hrs · 16,173 cycles

MAIN PAX DOOR HARD TO CLOSE HAD TO GET GROUND PERSONNEL TO CLOSE IT FROM OUTSIDE.

Part: UNKNOWN — ODOR (CABIN) · airframe 19,422 hrs · 15,946 cycles

BURNING PLASTIC SMELL COMING FROM APU BLEED. FLT 4566 DEL 21 MINS.

Part: GATE — STIFF (PAX DOOR) · airframe 19,355 hrs · 15,891 cycles

DIFFICULT CLOSING MAIN DOOR VENT FLAP WOULD NOT PULL SHUT.

Part: DOOR — MALFUNCTIONED (PAX DOOR) · airframe 19,113 hrs · 15,688 cycles

DOOR WILL NOT CLOSE/LOCK, INDICATES AMBER PAX OUTER HANDLE CAUTION MSG.

Part: DOOR — MALFUNCTIONED · airframe 19,113 hrs · 15,688 cycles

DOOR WILL NOT CLOSE/LOCK INDICATES PAX DOOR CAUTION MESSAGE PREVIOUS WRITE-UP. TAKES MULTIPLE ATTEMPTS TO CLOSE PROPERLY.

Part: UNKNOWN — ODOR (CABIN) · airframe 18,570 hrs · 15,240 cycles

FA REPORTS STRONG ELECTRICAL ODOR BETWEEN ROW 9 AND 11 OUT BOUND FROM ATL. EN ROUTE TO BTR A/C DIVERTED TO JAN DUE TO MTC. EMERGENCY DECLARED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,273 hrs · 14,990 cycles

DOING FIRST FLIGHT CHECKS FOUND FLOOR EMERGENCY LIGHTS OUT FROM ROW 8 BACK.

Part: LANDING GEAR — MALFUNCTIONED (NLG) · airframe 18,273 hrs · 14,990 cycles

GEAR DISAGREE MSG ON TAKEOFF - NOSE GEAR REMAINED OUT. FOLLOWED QRH. A/C RETURNED TO ATL AFTER T/O. EMERGENCY DECLARED.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 18,245 hrs · 14,970 cycles

LEFT BONDED SKIN DOUBLER IS CRACKED. IN REFERENCE TO EO 600-53-81 REP. 10-18-07 PREFORMED LT BONED SKIN DOUBLER REPAIR ALL WORK DONE IAW WITH REO 601R-53-61-506. REFERENCE JOB SIGN OFF INCLUDED IN TASK CARD REO 601R-53-61-506.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,625 hrs · 14,459 cycles

SECOND LAST CEILING EMERGENCY LIGHT INOP.

Part: STEP — CRACKED (AIRSTAIR DOOR) · airframe 17,347 hrs · 14,238 cycles

ASD BOTTOM STEP CRACKED.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 16,717 hrs · 13,764 cycles

FLAPS FAULT AT 8 DEGREES. EMERGENCY EQUIPMENT ON STANDBY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,308 hrs · 13,470 cycles

MIDDLE WING EMERGENCY LIGHT OUT LEFT AND RIGHT SIDE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,257 hrs · 12,663 cycles

RT EXT EMERG LIGHT FWD OF WING L/E INOP.

Part: SKIN — CORRODED (WING) · airframe 15,211 hrs · 12,624 cycles

SOME WING FUEL TANK ACCESS OPENINGS HAVE PITTING CORROSION. (MARKED)

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 15,211 hrs · 12,624 cycles

STATION 280 BULKHEAD CRACKED AT RBL9 BEFORE FLOOR LEVEL.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 15,211 hrs · 12,624 cycles

CORROSION ON CENTER FS 280 FLOOR SUPPORT.

Part: HANDLE — CRACKED (E/E BAY DOOR) · airframe 15,211 hrs · 12,624 cycles

AVIONICS DOOR HANDLE CRACKED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 15,211 hrs · 12,624 cycles

RIGHT 625 ANGLE CRACKED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 15,211 hrs · 12,624 cycles

LEFT 625 ANGLE CRACKED.

Part: RIB — CRACKED (RT MLG WW) · airframe 15,212 hrs · 12,624 cycles

RIGHT WHEEL WELL BATT RIB CRACKED.

Part: WARNING MESSAGE — ACTIVATED (LAVATORY SMOKE) · airframe 14,942 hrs · 12,398 cycles

AFTER T/O, GOT "SMOKE TOILET" EICAS INDICATION WENT OUT. A/C RETURNED TO ATL AFTER T/O. FLT 4547 CX AND 4690 CX 5/8/06 AS A C/O.

Part: LAMP — BURNED OUT (CABIN)

DURING A GROUND INSPECTION, THE OVERHEAD EMERGENCY LIGHT AT ROW 5 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE OVERHEAD EMERGENCY LIGHT AT ROW 5. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: LAMP — BURNED OUT (FUSELAGE)

DURING A HANGAR INSPECTION, THE NR 2 LT SIDE EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE NR 2 LT SIDE EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: CONNECTOR — DISCONNECTED (CABIN)

FLT 4578 - DURING A HANGAR INSPECTION IN BTR, THE FORWARD MOST EMERGENCY FLOOR LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE RECONNECTED THE FORWARD MOST EMERGENCY FLOOR LIGHT STRIP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — BROKEN (PAX DOOR)

DURING AN A-CHECK IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND BROKEN AT THE ATTACH POINT. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. (M)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DURING AN A-CHECK IN BTR, THE EXTERIOR EMERGENCY LIGHT ON THE RIGHT SIDE IN THE FORWARD MOST POSITION WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EXTERIOR EMERGENCY LIGHT ON THE RIGHT SIDE IN THE FORWARD MOST POSITION. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (FUSELAGE) · airframe 11,300 hrs

DURING A C-CHECK, THE EMERGENCY EXIT LIGHT BY THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE IS REMOVING AND REPLACING THE EMERGENCY EXIT LIGHT LAMP BY THE SERVICE DOOR. (K)

Part: LIGHT — BURNED OUT (CABIN)

DURING OVERNIGHT MAINTENANCE IN SHV, THE FIRST SECTION OF THE EMERGENCY FLOOR LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY FLOOR LIGHT TRACK. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: DOUBLER — CRACKED (FUSELAGE)

DURING AN A-CHECK IN BTR, THE RT SIDE FS 640 DOUBLER BETWEEN STRINGERS 9 AND 12 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RT SIDE FS 640 DOUBLER BETWEEN STRINGERS 9 AND 12 IAW SRM 51-00. (M)

Part: DOUBLER — CRACKED (FUSELAGE)

DURING AN A-CHECK IN BTR, THE DOUBLER ON FS 640 BETWEEN STRINGERS 9 AND 12 ON THE RIGHT SIDE WAS FOUND CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE DOUBLER ANGLE ON FS 640 BETWEEN STRINGERS 9 AND 12 ON THE RIGHT SIDE IAW SRM 51-00-00 AND 51-42-06. (M)

Part: ACM — INOPERATIVE (FUSELAGE)

DURING APPROACH INTO DFW FROM DTW, THE CREW NOTICED A BURNING SMELL IN THE CABIN. THE AIRCRAFT LANDED SAFELY IN DFW. MAINTENANCE REMOVED AND REPLACED THE AIR CYCLE MACHINE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: ANGLE — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CARGO COMPARTMENT FLOOR SUPPORT ANGLE BRACKETS AT FS 621, ON THE LEFT AND RIGHT SIDES, WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO COMPARTMENT FLOOR SUPPORT ANGLE AT FS 621 ON THE LEFT AND RIGHT SIDES IAW ASA EO 600-53-0105. (M)

Part: DOOR FRAME — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE RIGHT AFT FUSELAGE CABIN AIR HOOKUP DOOR FRAME WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACD THE CRAFTED DOOR LAND IAW SRM 51. AIRCRAFT OK FOR SERVICE. (M)

Part: PLATE — CRACKED (DOOR SEAL)

DURING A C-CHECK IN MCN, THE CARGO DOOR CUT OUT LOWER SEAL PLATE WAS FOND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CARGO DOOR CUTOUT LOWER SEAL PLATE IAW SRM 51-00. AIRCRAFT OK FOR SERVICE. (M)

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS)

DURING APPROACH FROM RDU-DFW, THE FLAPS FAILED AT ZERO DEGREES. THE AIRCRAFT LANDED SAFELY IN DFW. MAINTENANCE COMPLIED WITH AD 98-20-01 AND RESET THE FLAPS SYSTEM. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CONTROLLER — MALFUNCTIONED (TE FLAPS)

DURING APPROACH INTO ATL FROM SWF,WITH THE FLAPS SELECTED TO 8 DEGREES, THE CREW RECEIVED A FLAPS FAILED MESSAGE. EMERGENCY EQUIPMENT WAS REQUESTED AND THE AIRCRAFT LANDED SAFELY IN ATL WITH THE FLAPS TO ZERO. MAINTENANCE COMPLIED WITH AD 98-20-01 AND RESET THE FLAPS SYSTEM. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: COVER — MISSING (EXIT SIGN)

FLT 4479 - DURING A GROUND INSPECTION AT CHS, A LIGHTED EXIT SIGN COVER WAS FOUND TO BE MISSING. MAINTENANCE INSTALLED A LIGHTED EXIT SIGN COVER. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: BULB — BURNED OUT (CABIN)

FLT 4505 - DURING A SCHEDULED INSPECTION IN XNA, THE FORWARD CABIN OVERHEAD EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT OVERHEAD EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (EXTERIOR)

DURING A SCHEDULED INSPECTION IN XNA, THE LEFT FORWARD EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT LEFT FORWARD EXTERIOR EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)