N860AS

Part: FRAME SPLICE — CRACKED (BS 409) · airframe 34,267 hrs · 31,780 cycles

CRACKED FRAME SPLICE AT FRAME BS 409+32 AND STR 6R. RECEIVED AND COMPLIED WITH SNIEO 601R32202 501, REV: B. COMPLIED WITH ECTC SNIEO 601R-32202 501 AND SNIEO 601R32202 501. COMPLIED WITH EC/TC SNIEO 601R32201501 AND SNIEO 601R32201501.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 34,267 hrs · 31,780 cycles

CARGO TRACK CORRODED AT LBL 9, FS 559+80 - 559+96. R & R THE CARGO TRACK IAW AMM 53-00-49-000-801, & 53-00-49-400-801.

Part: FLOORBEAM — CORRODED (BS 605) · airframe 34,267 hrs · 31,780 cycles

SCREW HOLE CORRODED ON FLOORBEAM RBL 9 AT FS 605.00. COMPLIED WITH ECTC REO 601-53-00-005.

Part: SEAT TRACK — CORRODED (BS 559-574) · airframe 34,267 hrs · 31,780 cycles

CARGO TRACK CORRODED RBL 9 BS 559+112 - 574. R & R THE CARGO TRACK IAW AMM 53-00-49-000-801, & 53-00-49-400-801.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 34,267 hrs · 31,780 cycles

CARGO TRACK CORRODED AT LBL 9. R & R IAW AMM 53-00-49-000-801, & 53-00-49-400-801.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 34,267 hrs · 31,780 cycles

MULTIPLE SCREW HOLES CORRODED ON CARGO TRACK BS 559+80 - 559+112 RBL9. REMOVED CORROSION IAW SRM 51-21-06. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00, FIG 101. REMOVED AND REPLACED THE CARGO TRACK IAW AMM 53-01-11.

Part: CARGO TRACK — CORRODED (BS 621) · airframe 34,267 hrs · 31,780 cycles

CARGO TRACK CORRODED AT LBL 9, FWD OF BS 621. R & R THE CARGO TRACK IAW AMM 53-00-49-000-801, & 53-00-49-400-801.

Part: CARGO TRACK — CORRODED (BS 559-574) · airframe 34,267 hrs · 31,780 cycles

CARGO TRACK CORRODED AT LBL 9, FS 559+112 - 574. R & R THE CARGO TRACK IAW AMM 53-00-49-000-801, & 53-00-49-400-801.

Part: FLOOR SUPPORT — CORRODED (BS 589-605) · airframe 34,267 hrs · 31,780 cycles

MULTIPLE SCREW HOLES CORRODED ON FLOORBEAM AT LBL 27 AT CARGO DOOR FS 589-FS 605. DAMAGE IS OUT OF LIMITS IAW GREO 601R-53-00-0005, REV B. FOUND NUMEROUS AREAS ON SECTION OF FLOORBEAM FS 589-605.00 TO BE EXFOILATED AND BEYOND LIMITS IAW REO 601R-53-00-005. DRILLED AND LOCATED NEW SERVICEABLE SEAT RAIL BEAM FS 589-605, LBL 27 IAW DWG NR 601R35031 AND SRM 51-40-06 AND 51-40-11-00. STARTED INSTALLTION OF SEAT RAIL BEAM ASSY AT LBL27, FS561-FS621 IAW SRM 51-42-21. COMPLETED INSTALLTION OF SEAT RAIL BEAM, EXCEPTS NOTED BELOW IAW REO 601R-53-61-3778. SEAT RAIL FITTING DOES NOT REQUIRE A REPLACEMENT FOUND SURFACE CORROSION AND BLENDING IAW SRM 51-21-06. MECHANICALLY MEASURED DEPTH WITH TOOL ITEM MACT 2886 AND VERIFIED NO MATERIAL LOSS IAW DWG 601-35017. REPLACED SURFACE FINISH IAW SRM 51-21-16. COMPLIED WITH ECTC REO 601R-53-61-3778 AND GREO 601R-5361-3778, REV A.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 34,267 hrs · 31,780 cycles

SEAT TRACK RBL 9, BS 559 - 559+80 IS CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802, & AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 34,267 hrs · 31,780 cycles

SEAT TRACK, RBL 9, BS 559+86 - 559+92 CORRRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11, & AMM 53-01-00-400-02.

Part: SKIN — CRACKED (BS 192) · airframe 34,267 hrs · 31,780 cycles

LEFT FWD FUSELAGE SKIN CRACKED BELOW AFT TRU DOOR LATCH AT APPROXIMATELY FS 192.00. REMOVED CRACKED DOOR LAND AND INSTALLED NEW SERVICEABLE DOOR LAND ON LT FWD FUSELAGE BELOW TRU DOOR IAW DWG 600-33052 AND SRM 51-42-06-00 AND 51-42-12-00. LOCATED AND DRILLED NEW SERVICEABLE DOOR LAND WHEN RECEIVED. COMPLIED WITH REO 601R-53-11-2908. RECEIVED AND COMPLIED EC/TC REO 601R-53-11-2908.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 34,267 hrs · 31,780 cycles

LT INBD FLAP LOWER SHIN DENTED AT APPROXIMATELY WS 76.00, 13" T/E OF FLAP. REPAIRED LT INBD FLAP IAW EO EC/TC EO 60057-0483.

Part: LIGHT — DAMAGED (CABIN) · airframe 33,030 hrs · 30,438 cycles

FLOOR-LEVEL EMERGENCY FLOODLIGHT AT ENTRANCE AREA DAMAGED. R & R FLOODLIGHT IAW AMM 33-51-19. SYSTEM OPS CHECKED GOOD. NO FURTHER ACTION.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 31,813 hrs · 29,145 cycles

EXIT SIGN MISSING AT ROW 7. FOUND EXIT SIGN COVER ON ACFT AND SECURED IAW AMM 33-51-14.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 31,797 hrs · 29,128 cycles

EMERGENCY LIGHT LEFT ON TO OUTSIDE FWD FUSELAGE LIGHTS GLOWING FAINTLY, LIGHT WOULD NOT ILLUMINATE WITH SWITCH ON . OPS TEST OF THE EMERGENCY LIGHT IAW AMM 33-51-00, OPS CHECK IS GOOD, ACFT BACK TO SERVICE.

Part: SKIN — DAMAGED (PAX DOOR) · airframe 30,507 hrs · 27,859 cycles

TWO FASTENERS BACKED OUT OF SKIN ON PAX DOOR. REPAIRED IAW REO 601R-52-11-2236. REPAIR CLASSIFIED AS MAJOR IAW GMM 5-3.

Part: SKIN — DENTED (RUDDER) · airframe 30,480 hrs · 27,831 cycles

DURING REMOVAL OF RUDDER, FOUND DENT ON LOWER LT SIDE OF RUDDER. FOUND OUT OF LIMITS IAW SRM 55-40-00. MAJOR REPAIR IAW SOP 5702. COMPLIED WITH REO 601R-55-41-105 P1.

Part: SKIN — CORRODED (RT WING) · airframe 30,480 hrs · 27,831 cycles

RT WING LOWER WING PLANK ACCESS HOLE 64B LAND CORRODED. COMPLIED WITH EC/TC EO 600-57-81 C/W IAW REO 601R-57-21-030, REV L. MAJOR REPAIR.

Part: FITTING — CORRODED (DOOR SEAL) · airframe 30,480 hrs · 27,830 cycles

THE LOWER SERVICE DOOR SEAL FITTING AT FS 329.00 IS CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-00-00-01, FIG 101, SHEET 1 (TR 53-27). LOCATED & DRILLED NEW SERVICE DOOR SEAL FITTING IAW SRM 51-40-11 & DWC 601R38533. INSTALLED NEW SERVICE DOOR SEAL FITTING IAW SRM 51-41-02 & DWG 601R38533.

Part: SKIN — CORRODED (RT WING) · airframe 30,480 hrs · 27,831 cycles

RT WING LOWER WING PLANK ACCESS HOLE FUEL PANEL 650EB LAND CORRODED. COMPLIED WITH EC/TC EO 600-57-81 C/W IAW REO 601R-57-21-030, REV L. MAJOR REPAIR.

Part: BEARING — WORN (RUDDER) · airframe 30,480 hrs · 27,831 cycles

RUDDER CENTER ATTACHMENT UPPER BEARING HAS EXCESSIVE PLAY. COMPLIED WITH EC/TC RIL 0602. MAJOR REPAIR.

Part: ANGLE — CRACKED (BS 625) · airframe 30,480 hrs · 27,830 cycles

ANGLE CRACKED ON RT SIDE OF REAR PRESSURE BULKHEAD AFT FACE FS 625.00. R & R ANGLE IAW SRM 51-42-20.

Part: FITTING — DAMAGED (VERTICAL STAB) · airframe 30,480 hrs · 27,831 cycles

DAMAGE TO LOWER RT FITTING ON VERTICAL STAB FRONT SPAR. REMOVED DAMAGED LOWER RT FITTING IAW SRM 51-92-21. INSTALLED NEW SERVICEABLE LOWER RT FITTING IAW SRM 51-42-21. MAJOR REPAIR.

Part: FITTING — DAMAGED (VERTICAL STAB) · airframe 30,480 hrs · 27,831 cycles

DAMAGE TO LOWER LT FITTING ON VERTICAL STAB FRONT SPAR. REMOVED DAMAGED LOWER LT FITTING IAW SRM 51-42-21. INSTALLED NEW SERVICEABLE LT LOWER FITTING IAW SRM 51-42-21. MAJOR REPAIR.

Part: SUPPORT ANGLE — CORRODED · airframe 30,480 hrs · 27,830 cycles

LEFT SIDE WINDSCREEN SUPPORT ANGLE IS CORRODED. R & R RT SIDE WINDSCREEN SUPPORT ANGLE AND CAP IAW SRM 51-42-21 AND 51-42-06.

Part: ANGLE — CRACKED (BS 625) · airframe 30,480 hrs · 27,830 cycles

ANGLE CRACKED ON LT SIDE OF REAR PRESSURE BULKHEAD AFT FACE BS 625. R & R CRACKED ANGLE IAW SRM 51-42-28.

Part: SKIN — CHAFED (LT AILERON) · airframe 30,480 hrs · 27,831 cycles

LT AILERON UPPER L/E CHAFED. BLENDED AREAS IAW SRM 57-60-00. BLENDED AREA OUT OF LIMITS IN PAD UP AREA AT INBD IAW SRM 51-60-00. COMPLIED WITH EC/TC 601R-57-60-013 IAW REO 601R-57-60-013, REV A.

Part: FRAME — CORRODED (BS 349) · airframe 30,480 hrs · 27,831 cycles

FS 349 FRAME AT SERVICE DOOR CORRODED. BLENDED CORROSION IAW SRM 51-21-06. MAJOR REPAIR.

Part: FAIRING — DAMAGED (LT WING) · airframe 30,480 hrs · 27,830 cycles

LT WING FLAP CANOE FAIRING 586AB HAS COMPOSITE DAMAGE ON L/E. REPAIRED PANEL 586AB IAW SRM 51-74-00.

Part: HINGE — GOUGED (PAX DOOR) · airframe 30,480 hrs · 27,831 cycles

PAX DOOR HINGE ON DOOR SIDE GOUGED. BLENDED GOUGES IAW SRM 51-12-00.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 30,480 hrs · 27,831 cycles

CORROSION ON FLOOR SUPPORT AFT OF SERVICE DOOR. REPAIRED IAW REO601R-53-21-2539 AND REO 601R-53-21-2544. MAJOR REPAIR.

Part: BULKHEAD — CHAFED (BS 280) · airframe 30,480 hrs · 27,831 cycles

TWO CHAFE SPOTS ON AFT SIDE OF BS 280 BULKHEAD APPROXIMATELY 24 INCHES ABOVE FLOOR RT SIDE. BLENDED CHAFE SPOTS IAW SRM 51-12-00 AND 53-00-31. MAJOR REPAIR.

Part: FRAME — CRACKED (PAX DOOR) · airframe 30,480 hrs · 27,831 cycles

FRAME CRACKED IN PAX DOOR AT BS 338.00. COMPLIED WITH ECTC REO 601R-52-11-402 AND GREO 601R-52-11-402. MAJOR REPAIR.

Part: ANGLE — CRACKED (BS 280) · airframe 30,480 hrs · 27,830 cycles

FS 280 ANGLE CRACKED AT LBL 9.00. REMOVED CRACKED ANGLE IAW SRM 52-42-20. FABRICATED NEW REPAIR ANGLE IAW REO 601R-53-11-926.

Part: HINGE — GOUGED (PAX DOOR) · airframe 30,480 hrs · 27,831 cycles

PAX DOOR HINGE HALF ON FUSELAGE IS GOUGED. BLENDED GOUGES IAW SRM 51-12-00.

Part: ANGLE — CRACKED (BS 280) · airframe 30,480 hrs · 27,830 cycles

FS 280, ANGLE CRACKED AT RBL 9.00. REMOVED CRACKED ANGLE IAW SRM 52-42-20. FABRICATED NEW REPAIR ANGLE IAW REO 601R-53-11-926. COMPLIED WITH EC/TC REO 601R-53-11-926-01 AND COMPLIED WITH EC/TC REO 601R-53-11-926 01.

Part: SPAR — CRACKED (RT WING) · airframe 30,480 hrs · 27,830 cycles

RT WING SPAR CRACKED AT WS 148.019. COMPLIED WITH ECTC REO 601R-57-21-130-01.

Part: COVER — MISSING (RUDDER) · airframe 30,480 hrs · 27,831 cycles

LIGHTNING HOLE MISSING COVER ON RUDDER IAW REO 601R-55-41-018. REPAIRED IAW REO 601R-55-41-018. MAJOR REPAIR.

Part: SIGN — DAMAGED (EMERGENCY LIGHT) · airframe 28,693 hrs · 26,032 cycles

F/A REPORTS EXIT SIGN/LIGHT ON LT BULKHEAD ADJACENT TO PAX DOOR IS DAMAGED. OPEN.

Part: WINDOW — ARCED (COCKPIT) · airframe 27,345 hrs · 24,634 cycles

NOTICED ARCING AT LOWER REAR SIDE OF RT WINDOW AFTER TAKE OFF. SHORTLY AFTER RT WINDOW SHATTERED. R & R RT WINDOW IAW AMM 56-12-01. OPS TEST OF SIDE WINDOW TEMP CONTROLLERS ARE GOOD IAW AMM 30-41-01.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 26,616 hrs · 23,875 cycles

CABIN SECOND EMERGENCY CEILING LIGHT IS INOPERATIVE. R & R SECOND EMERGENCY CEILING LIGHT BULB IAW AMM 33-51-16. OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 26,616 hrs · 23,875 cycles

RT AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R EXTERNAL EMERGENCY LIGHT BULB. OP'S CHECKED GOOD.

Part: SEAT TRACK — CORRODED (BS 444-495) · airframe 26,418 hrs · 23,646 cycles

RT SIDE SEAT TRACK IS CORRODED FROM FS 444 - 495. REMOVED CORROSION AND MEASURED MAT LOSS AT .007". FOUND TO BE OUT OF LIMITS IAW SRM 58-31-49. REPAIRED IAW REO 601R-53-00-468.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 26,418 hrs · 23,646 cycles

LEFT SIDE SEAT TRACK IS CORRODED FROM FS 409+18 - 409+111. FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49. REPAIRED IAW 601R-53-00-468.

Part: SEAT TRACK — CORRODED (BS 409-444) · airframe 26,418 hrs · 23,646 cycles

RT SIDE SEAT TRACK IS CORRODED FROM FS 409 - 444. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49. REPAIRED IAW REO 601R-53-00-468.

Part: SEAT TRACK — CORRODED (BS 535-559) · airframe 26,418 hrs · 23,646 cycles

LEFT SIDE SEAT TRACK IS CORRODED FROM FS 535 - 559+79. REMOVED CORROSION AND MEASURED MAT LOSS AT .007". FOUND TO BE OUT OF LIMITS IAW SRM 58-41-49. REPAIRED IAW REO 601R-53-00-468.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 26,418 hrs · 23,646 cycles

CARGO LT FLOOR SILL HAS CORROSION AROUND NUTPLATE AT FS559.00+112. REMOVE CORROSION SRM 51-26-06. CORROSION WITHIN ALLOWABLE LIMITS IAW SRM 53-00-00, FIG 102. REMOVED LIGHT SURFACE CORROSION IAW SRM 51-21-06 AND RESTORED FINISH AS REQUIRED. THIS REPAIR REQUIRES MAJOR/MINOR CLASSIFICATION IAW ASA SOP 5702. THIS REPAIR IS CLASSIFIED AS A MAJOR/MINOR REPAIR IAW ASA SOP 5702. (SDR CLOSED)

Part: SEAT TRACK — CORRODED (BS 444-495) · airframe 26,418 hrs · 23,646 cycles

LEFT SIDE SEAT TRACK IS CORRODED FROM FS 444 - 495. REMOVED CORROSION AND MEASURED MAT LOSS AT .005". FOUND TO BE OUT OF LIMITS IAW SRM 58-41-49. REPAIRED IAW REO 601R-53-00-468.

Part: SEAT TRACK — CORRODED (BS 535-559) · airframe 26,418 hrs · 23,646 cycles

RT SIDE SEAT TRACK IS CORRODED FROM FS 535 - 559+79. REMOVED CORROSION AND MEASURED MAT LOSS AT .005. FOUND TO BE OUT OF LIMITS IAW SRM 53-51-49. REPAIRED IAW REO 601R-53-00-468.

Part: SEAT TRACK — CORRODED (BS 409-444) · airframe 26,418 hrs · 23,646 cycles

LEFT SIDE SEAT TRACK IS CORRODED FROM FS 409+111- 444. REMOVE CORROSION AND MEASURED MAT LOSS AT .008. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49. REPAIRED IAW REO 601R-53-00-468.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 26,418 hrs · 23,646 cycles

CARGO TRACK CORRODED LBL 9 BETWEEN FS 559+80 - 559+96. REMOVED CORROSION DAMAGE ON CARGO TRACK IAW SRM 51-21-06. FOUND TO BE OUT OF LIMITS IAW SRM 53-61-49. REMOVED DAMAGED CARGO TRACK IAW AMM 53-01-11-000-802. INSTALLED NEW SERVICEABLE CARGO TRACK IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 26,418 hrs · 23,646 cycles

RT SIDE SEAT TRACK IS CORRODED FROM FS 409+18 - 409+111. REMOVED CORROSION AND MEASURED MAT LOSS AT .005. FOUND TO BE OUT OF LIMITS IAW SRM 58-31-49. REPAIRED IAW REO 601R-53-00-468.

Part: SEAT TRACK — CORRODED (BS 495-535) · airframe 26,418 hrs · 23,646 cycles

LEFT SIDE SEAT TRACK IS CORRODED FROM FS 495 - 535. REMOVED CORROSION AND MEASURED MAT LOSS AT .008". FOUND TO BE OUT OF LIMITS IAW SRM 58-41-49. REPAIRED IAW REO 601R-53-00-468.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 26,418 hrs · 23,646 cycles

CARGO TRACK CORRODED AROUND NUTPLATE RBL 9 AT FS 559+96. REMOVED CORROSION BY BLENDING IAW STEP (1) OF GREO 601R-53-00-005. PERFORMED UT-THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT PROCEDURE UT-3. MIN MATERIAL REMAINING IS .048", ORIGINAL IS .050" MATERIAL REMOVED IS .002" WITHIN LIMITS IAW REO 601R-53-00-005.

Part: SKIN — CORRODED (SERVICE DOOR) · airframe 26,418 hrs · 23,646 cycles

CORROSION ON SERVICE DOOR INNER SKIN AROUND SCREW HOLES. REMOVED CORROSION, NO MATERIAL LOSS FOUND IAW SRM 51-21-06. TREATED PRIMED AND PAINTED IAW IAW SRM 51-21-11.

Part: SUPPORT BRACKET — CRACKED · airframe 26,418 hrs · 23,646 cycles

TWO SUPPORT BRACKETS CRACKED ON NOSE INLET COWLING OTBD SIDE. R & R SUPPORT BRACKETS IAW SRM 51-21-06 AND CMM 71-61-01-400-001-A01.

Part: COALESCER BAG — ODOR (LT A/C PACK) · airframe 26,343 hrs · 23,555 cycles

LEFT PACK EMITTING A MOLDY ODOR THAT IRRITATES THE NOSE THROAT. R & R THE COALESCER BAG IAW AMM 24-51-13. OPS CHECKED GOOD NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: PRESSURE VALVE — OUT OF ADJUST (PAX DOOR) · airframe 25,562 hrs · 22,715 cycles

UNABLE TO OPEN MAIN DOOR FROM INSIDE BECAUSE OUTER DOOR HANDLE WILL NOT RELEASE. ADJUSTED PAX DOOR PRESSURE VALVE IAW AMM 52-11-15. OPS CHECKED GOOD.

Part: PUSHROD — OUT OF RIG (PAX DOOR HANDLE) · airframe 25,562 hrs · 22,715 cycles

UNABLE TO OPEN MAIN DOOR FROM INSIDE. FOUND PAX DOOR OUT OF RIG. ADJUSTED PAX DOOR OUTER HANDLE PUSHROD ASSY IAW AMM 52-11-03.

Part: DOOR — BINDING (MAIN PAX) · airframe 25,548 hrs · 22,699 cycles

MAIN PAX DOOR WILL NOT OPEN FROM THE INSIDE. COMPLIED WITH RIGGING, FUNCTIONAL AND SYS TEST IAW AMM 52-11-00. OPS CHECKED GOOD.

Part: DOOR — BINDING (MAIN PAX) · airframe 25,547 hrs · 22,698 cycles

PASSENGER DOOR WILL NOT OPEN FROM INSIDE. PERFORMED OPS CHECK OF PAX DOOR IAW AMM 52-11-00, OPS CHECKED GOOD.

Part: COALESCER BAG — CONTAMINATED · airframe 25,433 hrs · 22,576 cycles

BURNING ELECTRICAL ODOR IN FLIGHT. ACFT DIVERTED, EMERGENCY DECLARED. ON INSPECTION, FOUND LT & RT COALESCERS BAD. R & R COALESCERS IAW AMM 21-51-13. OPS CHECKED GOOD IAE AMM 21-51-13.

Part: PLACARD — MISSING (CABIN) · airframe 24,890 hrs · 21,978 cycles

CABIN EMERGENCY EXIT SIGN MISSING "EXIT" PLACARD. RE-INSTALLED EMERGENCY EXIT SIGN LIGHT CASE IAW AMM 11-30-00. (CLOSED)

Part: SELECTOR VALVE — UNSERVICEABLE (MLG) · airframe 24,245 hrs · 21,255 cycles

DURING DECENT 5000 FT 240KNTS SELECTED GEAR HANDLE DOWN. NOSE EXTENDED NORMALLY. BOTH MAINS REMAINED UP WITH WHITE INDICATION. GEAR DISAGREE WARNING AND ORAL WARNING COMPLIED WITH QRH CYCLED GEAR 3 TIMES DURING MANUAL EXT BOTH MAINS EXTENDED. R & R MLG SELECTOR VALVE IAW 32-32-10. OPS CHECKED GOOD, ACFT GOOD TO RETURN SERVICE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 23,922 hrs · 20,889 cycles

CABIN CEILING EMERGENCY LIGHT SECOND FROM FRONT INOP. RELAMPED CABIN CEILING EMERGENCY LIGHT SECOND FROM FRONT IAW AMM 33-51-16, OP'S CHECK GOOD.

Part: TAPE — LOOSE (NLG) · airframe 23,250 hrs · 20,112 cycles

OBSERVIVED NOISE AND VIBRATION IN THE NOSE GEAR AREA DURING LEVEL CRUISE. ACFT WAS AT 10000 MSL AND 300 KTS, SLOWING TO 250 KAIS REDUCED VIBRATION SLIGHTLY (EMERGENCY DECLARED). FOUND NOSE GEAR TAPE FLAPPING ON THE RT FWD DOOR REINSTALLED TAPE, NO OTHER DEFECT NOTED. REF AMM 32-12-05. (CLOSED)

Part: UPLOCK — FAILED (RT MLG) · airframe 23,250 hrs · 20,112 cycles

GEAR UP DISAGREE MSG RT MAIN GEAR (A/C RETURNED TO DEPARTURE AFTER T/O -- EMERGENCY DECLARED] R & R RT MLG UPLOCK ASSY IAW AMM 32-32-05. LEAK AND OPS CHECK GOOD. (CLOSED)

Part: INTERCOSTAL — CRACKED (BS 625) · airframe 22,898 hrs · 19,705 cycles

FS 625 INTERCOSTAL CLIP AT LBL 45 WL 97.5 IS CRACKED. R & R INTERCOSTAL CLIP IAW REO 601R-53-61-422. REPAIRED INTERCOSTAL CLIP IAW ECTC 601R-53-61-422.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 22,898 hrs · 19,705 cycles

FS 484, LBL 36 INTERCOSTAL CLIP IS CRACKED. REMOVED DAMAGED REPAIR ANGLE IAW SRM 51-42-21. FABRICATED NEW SERVICEABLE REPAIR ANGLE IAW REO 601R-53-41-059, STEP 13. C/W LPIP OF FS 484, LBL 36 FABBED CLIP IAW NDTM PT 1 51-20-08. NO INDICATIONS NOTED AT THIS TIME. INSTALLED 601R31171-9 IAW REO 601R-53-41-059 ITEM 10. REPAIR OF THE INTERCOSTALS AT FS 484 BETWEEN BL 27, AND BL 36 IS COMPLETE IAW REO 601R-53-41-059 AND MEETS WITH ALL THEIR REQUIREMENTS.

Part: FLOOR SUPPORT — CORRODED (BS 621-574) · airframe 22,898 hrs · 19,705 cycles

FLOOR SUPPORT CAP AT LBL 27 FS 621 TO FS 574 HAS CORROSION. REMOVED FLOOR SUPPORT CAP IAW SRM 51-42-05, 51-42-21 AND 51-42-13. INSTALLED NEW SERVICEABLE FLOOR SUPPORT CAP IAW SRM 51-30-11, 51-42-21 & 51-42-22. ALSO COMPLIED WITH STEPS 1 THRU 7 OF REO 601R-35-61-3703. COMPLIED WITH ASA EC/TC REO 601R-53-61-3703, STEPS 1 THRU 7.

Part: PLACARD — TORN (PAX DOOR) · airframe 22,898 hrs · 19,705 cycles

PAX DOOR STEPS ARROW, EXIT AND OPEN PLACARDS ARE TORN. R & R ARROW, EXIT, AND OPEN PLACARDS ON PAX DOOR STEPS IAW AMM 11-20-00-000-801 AND 11-20-00-400-801.

Part: FLOOR SUPPORT — CRACKED (BS 280) · airframe 22,898 hrs · 19,705 cycles

FS 280 FLOOR SUPPORT CLIP AT RBL 18 INBD IS CRACKED. AFTER CLEANING AREA FOUND NO CORROSION. RETREATED AREA IAW SRM 51-21-11.

Part: SILL — CORRODED (BS 589-559) · airframe 22,898 hrs · 19,705 cycles

RIGHT FUSELAGE FLOOR SUPPORT SILL AT LBL 36 FASTENER HOLES HAVE CORROSION FROM FS 589 TO 559+112. AFTER CLEANING AREA FOUND NO CORROSION. RETREATED AREA IAW SRM 51-21-11. REMOVED FLOOR SILL IAW SRM 51-42-06 AND 51-42-21. FABRICATED REPLACEMENT LIPPED PLATE FOR SILL USING 7075-0 .050" IAW SRM 51-24-21. LOCATED AND DRILLED LIP PLATE AND SILL WEB IAW SRM 51-42-06, 51-42-21. TREATED, PRIMED AND PAINTED LIP PLATE IAW SRM CH 51-25-16. REPAIRED SILL WEB IAW REO 601R-53-51-119 STEPS 1-8.

Part: SEAT TRACK — CORRODED (BS 559-569) · airframe 22,898 hrs · 19,705 cycles

AFT CARGO COMPARTMENT SEAT RAILS AT LBL 9 BETWEEN FS 559+110 AND FS 569.00 BETWEEN FS 612.00 AND FS 617.00 ARE CORRODED. REMOVED AFT CARGO COMPARTMENT SEAT RAILS AT LBL 9 BETWEEN FS 559+110 AND 569.00, FS 612 - FS 617.00 AND INSTALLED SERVICEABLE SEAT RAILS BY DRILLING AND COUNTERSINKING SCREW HOLES IAW SRM 51-40-11. INSTALLED SCREWS IAW AMM 20-21-00-910-801. (CLOSED)

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 22,898 hrs · 19,705 cycles

AFT EQUIPMENT COMPARTMENT FS 621.00 TO 625.00 ANGLE AT STR 14R IS CRACKED. REMOVED DAMAGED ANGLE AT FS 621.00 - 625.00 AT STR 14R AND INSTALLED SERVICEABLE ANGLE (INTERCOSTAL) IAW SRM 51-42-21.

Part: BULKHEAD — CRACKED (BS 559) · airframe 22,898 hrs · 19,705 cycles

FOUND FS 559 RT BULKHEAD WEB HAS INDICATION NOTED OTBD OF RBL 9.0 WL 54.10 APPROX .4" IN LENGTH 80 PERCENT FSH. FAILED NDT INSPECTION. C/W EC/TC REO 601R-57-41-260 IAW REO 601R-53-41-260 REV D.

Part: SEAT TRACK — CORRODED (BS 559-569) · airframe 22,898 hrs · 19,705 cycles

AFT CARGO COMPARTMENT SEAT RAILS AT RBL 9 BETWEEN FS 559+91 AND FS 559+96 BETWEEN FS 559+110 AND FS 569.00 ARE CORRODED. REMOVED AFT CARGO COMPARTMENT SEAT RAILS AT RBL 9 BETWEEN FS 559+91 AND 559+96, ALSO BETWEEN FS 559+110 - FS 569.00. DRILLED/COUNTERSUNK HOLES IAW SRM 51-40-11 AND INSTALLED SERVICEABLE SEAT RAILS IAW AMM 20-21-00-900-801. (CLOSED)

Part: SEAT TRACK — CORRODED (BS 559) · airframe 22,898 hrs · 19,705 cycles

AFT CARGO COMPARTMENT SEAT RAILS AT RBL 27 BETWEEN FS 559+80 AND FS 559+96 IS CORRODED. REMOVED AFT CARGO COMPARTMENT SEAT RAIL AT RBL 27 BETWEEN FS 559+80 AND FS 559+96. DRILLED AND COUNTERSUNK SCREW HOLES IN SERVICEABLE RAIL IAW SRM 51-40-11 AND INSTALLED IAW AMM 20-21-00-910-801.

Part: CHANNEL — CRACKED (BS 409) · airframe 22,898 hrs · 19,705 cycles

INDICATION NOTED AT FS 409+128 RBL 18 WL 69.00 VERTICAL POST OUTBD U-CHANNEL IN RADIUS VERTICALLY APPROX .30 IN LENGTH 55 PERCENT FSH. REMOVED OTBD POST IAW SRM 51-42-06 AND 51-42-21. LOCATED AND DRILLED NEW OTBD POST IAW SRM 51-40-11. ASSEMBLED NEW OTBD POST WITH NEW INBD POST IAW SRM 51-42-06. INSTALLED ASSEMBLED POST IAW SRM 51-42-06 AND COMPLIED WITH STEP 1 OF REO 601R-53-41-889. COMPLIED WITH EC/TC REO 601R-53-41-889 AND MET ALL THE REQUIREMENTS OF REO 601R-53-41-889, REV A.

Part: LIGHT — LOOSE (ROW 8AB) · airframe 22,814 hrs · 19,609 cycles

BURNING SMELL FROM OVER HEAD ON ROW EIGHT. INSPECTED ACFT , NO SMELL NOTED. FOUND CEILING LIGHT AT ROW 8AB LOOSE, REINSTALLED AND FOUND BULBS INOP. REF AMM 33-21-01, REFER TO AFDL 535230-1.

Part: WARNING MESSAGE — ILLUMINATED (CABIN COOLING) · airframe 22,274 hrs · 18,978 cycles

IN FLIGHT GOT DISPLAY COOL CAUTION MESSAGE COMPLIED WITH QRH MESSAGE DID NOT EXTENGUISH, LANDED AS DIRECTED BY QRH. JUST PRIOR TO LANDING PFD1 MFD1 AND PFD 2 HAD DISPLAY TEMP MESSAGE ILLUMINATED ON THEM. ACFT RETURNED TO DEPARTURE AFTER T/O -- EMERGENCY DECLARED. FOUND THAT PREVIOUS CREW DEFERED THE WRONG FAN. REMOVED & REPLACED GROUND FAN ASSY.OPS CHECK GOOD.IAW AMM 21-24-19. DEFER CLEARED & PLACARD REMOVED.

Part: THRUST REVERSER — MALFUNCTIONED (LT ENGINE) · airframe 22,181 hrs · 18,873 cycles

AMBER L REV UNLOCKED MESSAGE AT FL230 DURING CRUISE. PRESSED LT EMERGENCY STOW AND SHUTDOWN ENGINE IAW QRH, DIVERTED. DIVERTED TO DUE TO MX-- EMERGENCY DECLARED -- OPEN (THRUST REVERSER SYSTEMS )

Part: PDU — FAILED (THRUST REVERSER) · airframe 22,181 hrs · 18,873 cycles

R & R LT THRUST REVERSER PDU IAW AMM 78-32-03. OPS CK GOOD, DEFER CLEARED PLACARD REMOVED. (CLOSED)

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,883 hrs · 18,545 cycles

FOUND 202 BULKHEAD CRACKED BETWEEN 12 AND 1 O`CLOCK.

Part: LIGHT — INOPERATIVE (RT EXTERIOR) · airframe 21,867 hrs · 18,527 cycles

RT SIDE EXTERIOR EMERGENCY LIGHT INOP.

Part: DOOR — JAMMED (CABIN) · airframe 21,126 hrs · 17,788 cycles

MAIN CABIN DOOR IS HARD TO OPEN AND CLOSE, IT JAMS WHEN OPENING AND THE HANDLE DOES NOT STOW WHEN SHUTTING.

Part: DOOR — MALFUNCTIONED (CABIN) · airframe 21,118 hrs · 17,781 cycles

PAX DOOR IS HARD TO OPEN AND CLOSE.

Part: DOOR — BINDING (CABIN) · airframe 21,081 hrs · 17,747 cycles

PASSENGER DOOR NEED FURTHER TROUBLESHOOTING DUE DOOR HARD TO OPEN AND HARD TO CLOSE.

Part: DOOR — STIFF (CABIN) · airframe 21,062 hrs · 17,728 cycles

PAX ENTRY DOOR VERY DIFFICULT TO OPEN. REQUIRES 2 CREW MEMBERS TO OPEN FULLY.

Part: DOOR — BINDING (PAX DOOR) · airframe 21,007 hrs · 17,674 cycles

MAIN PAX DOOR IS VERY DIFFICULT TO OPEN.

Part: DOOR — BINDING (PAX DOOR) · airframe 21,007 hrs · 17,674 cycles

PAX DOOR WOULD NOT OPEN FROM INSIDE. OUTSIDE HELP AND INSIDE FORCE REQUIRED. FLT 5587 DEL 80 MINS.

Part: DOOR — STUCK (MAIN PAX) · airframe 20,998 hrs · 17,663 cycles

MAIN PAX DOOR UNABLE TO BE OPENED WITHOUT EXCESSIVE FORCE.

Part: DOOR — BINDING (MAIN CABIN DOOR) · airframe 20,990 hrs · 17,656 cycles

PREVIOUS FA REPORTS MAIN CABIN DOOR IS DIFFICULT TO OPEN/ CLOSE. FLT 5587 DEL 51 MINS.

Part: DOOR — BINDING (PAX DOOR) · airframe 20,914 hrs · 17,582 cycles

PAX DOOR IS VERY HARD TO OPEN. F/A WAS UNABLE TO OPEN IT. CAPTAIN HAD TO PUSH VERY HARD FOR IT TO OPEN.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,869 hrs · 17,544 cycles

NR 2 CEILING EMERGENCY LIGHT INOP.

Part: DOOR — BINDING · airframe 20,571 hrs · 17,251 cycles

BOARDING DOOR VERY DIFFICULT TO OPEN. FLT 5567 DEL 28 MINS.

Part: DOOR — BINDING · airframe 20,571 hrs · 17,251 cycles

FLIGHT ATTENDANT REPORTS BOARDING DOOR STILL VERY DIFFICULT TO OPEN. FLT 4983 DEL 89 MINS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 19,894 hrs · 16,640 cycles

RT BS 210 FRAME CRACKED. REMOVE FRAME AND INSTALLED NEW FRAME P/N 600-34011-1 PER SRM 51-42-06.

Part: DOOR — STUCK (PAX DOOR) · airframe 19,801 hrs · 16,545 cycles

PAX DOOR WILL NOT OPEN.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 19,689 hrs · 16,432 cycles

PAX DOOR HARD TO OPEN. LUBRICATED PAX DOOR. CHECKS GOOD. REF AMM 52-11-13. PAX DOOR WHEEL WAS STIFF. CKS GOOD AT THIS TIME.

Part: ECU — LOOSE (E&E BAY) · airframe 19,562 hrs · 16,302 cycles

FLAP FAILURE CAUTION MSG ON 4 MILE FINAL. FLAPS FAILED AT 30`. VERIFIED ON SYNOPTIC PAGE. EMERGENCY VEHICLES ROLLED AS A PRECAUTION. T/S SYSTEM FOUND FECU LOOSE IN RACK. PERFORMED FECU TEST AFTER TIGHTENING KNOBS. IAW AMM 27-51-05 PG 501-504. SYSTEM OP CHECKED OK. A/C OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 19,517 hrs · 16,259 cycles

SERVICE DOOR EXTER. EMER. LIGHT INOP. RELAMPED SERVICE DOOR EXTER. EMER. LIGHT IAW CRJ200AMM 33-51-21. OP CHECK GOOD AT THIS TIME.

Part: MECHANISM — DIRTY (PAX DOOR LOCK)

MAIN ENTRY DOOR VERY DIFFICULT TO OPEN. CLEANED LOCKING MECHANISM ON PAX DOOR, CYCLED PAX DOOR, NO FURTHER DEFECTS NOTED. (A)

Part: DOOR — STIFF (MAIN PAX)

F/A REPORTS THAT MAIN ENTRY DOOR IS DIFFICULT TO OPEN. PERFORMED OPERATIONAL TEST OF PAX DOOR IAW CRJ200 AMM 52-11-00-710-801. NO DIFFICULTY OPENING OR CLOSING DOOR. OPS CHECKS GOOD. OK FOR SERVICE. (A)

Part: HINGE — FOD (PAX DOOR) · airframe 19,107 hrs · 15,910 cycles

ACFT PASSENGER DOOR DIFFICULT TO OPEN AFTER FLIGHT. REMOVED DEBRIS FROM PASSENGER DOOR HINGE TRACK. PERFORMED OPS CHECK OF MAIN PASSENGER DOOR IAW AMM 52-11-00. NO DEFECTS NOTED. (S)

Part: HANDLE — LACK OF LUBE (PAX DOOR) · airframe 19,107 hrs · 15,910 cycles

F/A REPORTS MAIN DOOR HARD TO OPEN. CLEANED AND LUBED DOOR HANDLE AMM 52-11. (S)

Part: HANDLE — LACK OF LUBE (PAX DOOR) · airframe 19,061 hrs · 15,870 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN, RAMP CREW COULD NOT OPEN FROM THE OUTSIDE. COMPLIED WITH CABIN HANDLE INSP, CLEANED AND LUBE, OK FOR SERVICE PER CRJ200AMM52-10.

Part: STRIKER — GOUGED (PAX DOOR) · airframe 1,906,107 hrs · 15,870 cycles

ASD HARD TO OPEN FOUND ASD FORWARD TOP ROLLER STRIKER PLATE GOUGED. UPON INSPECTION OF DOOR FOUND UPPER FORWARD ROLLER DRAGING ON CAM. CHECKED RIGGING ON CONTROL RODS IAW AMM 52-11-21. ADJUSTED UPPER LINK TO CAM AND ADJUSTED SHIMS AT FWD UPPER CAM IAW AMM 52-11-21. DOOR STILL NEEDS CHECKED FOR RIGGING OF THE CAM ASSY AND THE ICE BREAKER (B)

Part: SUPPORT ANGLE — CRACKED (BS 621) · airframe 19,043 hrs · 15,854 cycles

LINTEL SUPPORT ANGLE PN 601R35050-109 CRACKED AT PRESSURE BULKHEAD WEB BS 621 . REMOVED LINTEL SUPPORT ANGLE. FABRICATED NEW LINTEL SUPPORT ANGLE PER EO 600-53-0346. INSTALLED FABRICATED LINTEL SUPPORT ANGLE IAW SRM 51-42-20. AWAITING EC/TC 7025126. (B)

Part: SILL — CORRODED (BS 473) · airframe 19,043 hrs · 15,854 cycles

CORROSION DAMAGE ON LT PRESSURE FLOOR SILL FS 473.15 AT RBL 43 (MARKED). REMOVED MINOR SURFACE CORROSION DAMAGE ON PRESSURE FLOOR SILL ASSEMBLY REINFORCING ANGLE AT FS 473.15 AT RBL 43. BLENDED AREA DIMENSIONS ARE 1"X1.5"X.004"MAX DEPTH. MAXIMUM MATERIAL REMOVAL ALLOWED IS .008". BLENDED AREA IS WITHIN LIMITS PER CRJ 200 SRM 53-41-45 FIGURE 101. WORK COMPLETED. (B)

Part: SILL — CORRODED (BS 574-589) · airframe 19,043 hrs · 15,854 cycles

AFT CARGO COMP FLOOR SILL CORRODED LT SIDE BETWEEN FS 574 AND 589 AT LBL 45 (MARKED). REMOVED LIGHT SURFACE CORROSION ON CARGO FLOOR SILL AT FS 574 AND 589 IAW SRM 51-21-06. REMOVED .002 MATERIAL WITHIN LIMITS. ALODINE, PRIMED, AND PAINTED IAW CRJ 200 SRM 51.00.00. (B)

Part: SILL — CORRODED (BS 424) · airframe 19,043 hrs · 15,854 cycles

CORROSION DAMAGE ON LT PRESSURE FLOOR SILL FS 424.00 AT LBL 36.0 TO LBL 45.0 (MARKED). JOB COMPLETE REMOVED MINOR SURFACE CORROSION DAMAGE ON PRESSURE FLOOR SILL ASSEMBLY REINFORCING ANGLE AT FS 424.00 AT LBL 36. BLENDED AREA DIMENSIONS ARE 1"X.5"X.002"MAX DEPTH, 1.5"X1.5"X.006", 5"X.5"X.002". MAXIMUM MATERIAL REMOVAL ALLOWED IS .008". BLENDED AREA IS WITHIN LIMITS PER CRJ 200 SRM. (B)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 19,043 hrs · 15,854 cycles

FLOOR SUPPORT STRINGER CORRODED AT PAX DOOR SILL (MARKED). JOB COMPLETE REMOVED CORROSION PER CRJ 200 SRM 51-21-06. MATERIAL REMOVED .004", WITHIN LIMITS. REMOVED UPPER FLOORBOARD ATTACH ANGLE AND AFT PAX DOOR ARM FITTING FOM. (B)

Part: ATTACH FITTING — CRACKED (BS 625) · airframe 19,043 hrs · 15,854 cycles

AFT PRESSURE BULKHEAD, AFT FACE LEFT SIDE CLIP IS CRACKED. JOB COMPLETE REMOVED AND REPLACED LT 625 CLIP IAW SRM 51-42-21. JOB COMPLETE. DB7020877. (B)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,315 hrs · 14,405 cycles

THE 2ND FROM FRONT CEILING EMERGENCY LIGHT INOP.

Part: LIGHT — INOPERATIVE (RT WING) · airframe 17,034 hrs · 14,198 cycles

RIGHT WING EMERGENCY LIGHT IS INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,536 hrs · 13,799 cycles

AFT FLOOR LEVEL EMERGENCY LIGHTS INOP.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 16,431 hrs · 13,716 cycles

AFT EMERGENCY FLOOR TRACK LIGHTING IS INOP. PERFORMED OPS TEST OF THE EMERGENCY FLOOR TRACK LIGHTING SYSTEM IAW CRJ200 AMM 33-50. OPS TEST GOOD. COULD NOT DUPLICATE PROBLEM. {SDR - CLOSED}

Part: HOSE — TWISTED · airframe 15,877 hrs · 13,313 cycles

BWO 6042035-790 SNAG SHEET C-1026405 NR 2 BRADED STEEL HOSE ON LEFT COLLECTOR TANK FOUND FOULING ON RIB STIFFENER P/N 600-10221-1. RIB BLENDED IAW SRM 57-00-00 SERVICABLE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 15,874 hrs · 13,311 cycles

UPON WALK AROUND, FOUND LARGE HOLE IN BELLY OF A/C.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,498 hrs · 13,038 cycles

FWD EMERGENGY CEILING LIGHT INOP.

Part: STEP — BROKEN (AIRSTAIRS) · airframe 15,032 hrs · 12,674 cycles

ASD LWR STEP IS BROKEN.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 14,870 hrs · 12,544 cycles

CRACKED STIFNER ON 409 + 128 BULKHEAD RBL27. REPAIRED IAW REO 601R-53-41-056. (CLOSED)

Part: STRUCTURE — CORRODED (RT WING) · airframe 14,870 hrs · 12,544 cycles

FOUND CORROSION ON RT WING FUEL TANK ACCESS LANDS FROM BL 0.00 TO WS 314.50. REPAIRED IAW REO 601R-57-21-030. (CLOSED)

Part: STRUCTURE — CORRODED (LT WING) · airframe 14,870 hrs · 12,544 cycles

FOUND CORROSION ON LT WING FUEL TANK ACCESS LANDS FROM BL 0.00 TO WS 314.50. REPAIRED IAW REO 601R 57-21-030. (CLOSED)

Part: SEAT TRACK — CORRODED (CARGO BAY) · airframe 14,870 hrs · 12,544 cycles

ALL SEAT TRACKS CORRODED IN CARGO COMPT.

Part: SILL — CORRODED (FUSELAGE) · airframe 14,870 hrs · 12,544 cycles

FOUND SERVICE DOOR SILL AREA CORRODED.

Part: PRESSURE BLKHD — CRACKED (FUSELAGE) · airframe 14,870 hrs · 12,544 cycles

SUSPECTED CRACK ON IB SIDE OF RBL 18 AND STR 24 AFT CORNER ON PRESSURE BULKHEAD 409+128.

Part: PRESSURE BLKHD — CRACKED (FUSELAGE) · airframe 14,870 hrs · 12,544 cycles

SUSPECTED CRACK ON IB SIDE OF LBL18 AND STR 24 AFT CORNER ON PRESSURE BULK HEAD 409+128. REPAIRED IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 14,870 hrs · 12,544 cycles

AFTER REMOVAL FS 280 FWD FLOOR SUPPORT SUPPORT ANGLE, FOUND 280 WEB CORRODED ON THE FWD AND AFT SIDES.

Part: ANCHOR FITTING — CRACKED (AIR STAIR DOOR) · airframe 14,870 hrs · 12,544 cycles

ASD FWD ANCHOR MOUNT CRACKED (MTC).

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 14,870 hrs · 12,544 cycles

FOUND FLOOR SUPPORT BY AFT SERVICE DOOR SILL AND DOOR FRAME CORNER CORRODED AT FS 349 AND FLOOR STR.

Part: FLOOR SUPPORT — CORRODED (DOOR SILL) · airframe 14,870 hrs · 12,544 cycles

FLOOR SUPPORT ON THE AFT CORNER OF ASD SILL AND DOOR FRAME CORRODED AT FS 349 AND FLOOR STR. REMOVED CORROSION ON THE CORNER OF ASD SILL , DOOR FRAME AT FS 349 AND FLOOR STR , PRIMED AND PAINTED IAW SRM 51-21-06, 51-21-16 CB 7015474. (CLOSED)

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 14,870 hrs · 12,544 cycles

FOUND CORRISION ON TOP OF FLOOR SUPPORT ANGLE ON FWD SIDE OF FS 280 TRANSVERSE BEAM. REMOVED FLOOR SUPPORT ANGLE FROM THE FWD SIDE OF THE BS 280. ANGLE NEEDS REPLACED. DRILLED ANGLE, DEBURRED AND INSTALLED REF: CRJ200 SRM 51-42-06 PSP19749 (CLOSED)

Part: PRESSURE BLKHD — CRACKED (FUSELAGE) · airframe 14,870 hrs · 12,544 cycles

SUSPECTED CRACK ON ANGLE AT WL 48.95 AND STR 26R ON THE PRESSURE BULK HEAD OF 409+128.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 14,870 hrs · 12,544 cycles

SUSPECTED CRACK ON ANGLE AT WL 48.95 AND STR 26L ON THE PRESSURE BULK HEAD OF 409+128.

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 14,870 hrs · 12,544 cycles

FOUND LBL 9 FLOORBEAM ATTATCH CLIPS I/B AND O/B CRACKED AT FS 280. FLOORBEAM ATTACH CLIPS WERE REPLACED DURING REPAIR ON F/S 280 WORK ACCOMPLISHED ON N/R-280 W/O 25868. (CLOSED)

Part: RIB — CRACKED (FUSELAGE) · airframe 14,870 hrs · 12,544 cycles

LT BAT RIB CRACKED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 14,870 hrs · 12,544 cycles

RT 718 FRAME CRACKED AT STRINGER 12. REPAIRED RT 718 FRAME CRACK AT STRINGER 12 IAW REO 601R-53-61-193. (CLOSED)

Part: BEAM — CRACKED (FUSELAGE) · airframe 14,870 hrs · 12,544 cycles

TRANSVERSE BEAM CRACKED JUST O/B OF RBL 9 AT FS 280. CLEANED AREA NEED NDT TO CONFIRM CRACK. PERFORMED ET INSPECTION OF THE FLOOR SUPPORT BEAM BETWEEN AT FS280.00 RBL9 AND 27 IAW CRJ 200 NDT MANUAL PART 1 CHAPTER 51-20-06. BEAM CRACKED AT LOWER RADIUS JUST OTBD OF RBL 9 AT VERTICAL SUPPORT BEAM ATTACHMENT. CRACKED SECTION OF TRANSVERSE BEAM WAS CUT OUT AND REPLACED DURING REPAIR ON F/S 280 WORK ACCOMPLISHED ON N/R-280 W/O 25868 PSP19749 (CLOSED)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,776 hrs · 12,465 cycles

AFT SECTION OF THE EMERGENCY FLOOR LIGHTS INOP.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 14,753 hrs · 12,445 cycles

ON DESCENT FROM FL290, LT THRUST LEVER LOCKED AND WOULD NOT RETARD WITH N1 90% ENGINE SECURED VIA LT ENGINE FIRE PUSH, AN EMERGENCY WAS DECLARED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,604 hrs · 12,332 cycles

EMERGENCY FLOOR TRACK LIGHTING INOP FROM ROW 9 TO ROW 12

Part: A/C PACK — ODOR · airframe 14,578 hrs · 12,311 cycles

BOTH PACKS EMIT FOUL ODOR... FLT 4576 DEL 39 MINS

Part: LAMP — BURNED OUT (CABIN)

DURNG HANGAR INSPECTION, THE CEILING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE CEILING EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: LIGHT — INOPERATIVE (CABIN)

DURING A HANGAR INSPECTION, THE AFT SECTION OF THE EMERGENCY FLOOR LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED THE AFT SECTION OF THE EMERGENCY FLOOR LIGHTS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: LIGHT — INOPERATIVE (CABIN)

DURING A GROUND INSPECTION IN SHV, THE EMERGENCY FLOOR LIGHT STRIP, FROM ROW 9 TO THE LAVATORY, WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF EMERGENCY FLOOR LIGHT STRIP, FROM ROW 9 TO THE LAVATORY, WITH NO DEFECTS NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT)

DURING A GROUND INSPECTION IN CVG, THE EMERGENCY FLOOR STRIP LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE RECONNECTED THE CONNECTORS TO THE EMERGENCY FLOOR STRIP LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS)

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

Part: DOUBLER — CRACKED (BS 640)

DURING A HANGAR INSPECTION IN BTR, THE RIGHT SIDE FS 640, AT STRINGER 10, DOUBLER WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT SIDE FS 640, AT STRINGER 10, DOUBLER IAW CRJ 200 SRM 51-40. (M)

Part: LAMP — BURNED OUT (CABIN)

DURING A GROUND INSPECTION, THE EMERGENCY LIGHT ASSY, NEAR THE PASSENGER DOOR, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMPS IN THE EMERGENCY LIGHT ASSY, NEAR THE PASSENGER DOOR. (K)

Part: DOOR — STICKING (MAIN PAX)

DURING AN OVERNIGHT INSPECTION, THE MAIN CABIN DOOR WOULD NOT OPEN FROM THE INSIDE OR OUTSIDE. MAINTENANCE REMOVED EXCESS GREASE FROM THE MAIN CABIN DOOR HANDLE. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — BROKEN (PAX DOOR)

DURING AN A-CHECK, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN AND MATERIAL MISSING. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. (K)

Part: LAMP — BURNED OUT (FUSELAGE)

DURING OVERNIGHT MAINTENANCE IN SHV, THE LEFT FORWARD EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE LEFT FORWARD EXTERIOR EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. (M)

Part: MECHANISM — CONTAMINATED (PAX DOOR) · airframe 12,131 hrs

DURING A GROUND INSPECTION, THE PASSENGER DOOR WOULD NOT CLOSE AND A PASSENGER DOOR LATCH CAUTION MESSAGE WAS RECEIVED. MAINTENANCE REMOVED SAND AND GRIT FROM ALL THE ROLLING COMPONENTS ON THE PASSENGER DOOR AND CHECKED THE ADJUSTMENT ON THE LINKAGES. MAINTENANCE ALSO CLEANED ALL THE MOVING PARTS WITH NO DEFECTS NOTED. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: STEP — CRACKED (PAX DOOR)

DURING HANGAR MAINTENANCE, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. (K)

Part: PSEU — MALFUNCTIONED (MLG)

DURING CLIMB OUT FROM DEPARTURE, UPON SELECTING GEAR UP, ALL 3 GEARS REMAINED DOWN AND THE CREW RECEIVED AN ANTI-SKID IB MESSAGE ACCOMPANIED BY A PARK BRAKE SOV MESSAGE. THE TOWER DECLARED AN EMERGENCY AS A PRECAUTION AND THE AC RETURNED TO DEPARTURE, LANDING SAFELY. MAINT REMOVED AND REPLACED THE PROXIMITY SENSOR ELECTRONIC UNIT (PSEU); AND ALSO CYCLED THE GEARS SEVERAL TIMES. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: STEP — BROKEN (PAX DOOR)

DURING A GROUND INSPECTION, THE PASSENGER DOOR BOTTOM STEP WAS FOUND BROKEN AT THE FORWARD ATTACH ROD. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP WAS FOUND BROKEN AT THE FORWARD ATTACH ROD. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: RIB — CRACKED (RT WING)

DURING A C-CHECK IN MCN, THE RIGHT WHEEL WELL BATT RIB AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE RIGHT WHEEL WELL BATT RIB AT WS 53.60 IAW ASA EO 600-57-039A. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE FLOOR SUPPORT ANGLES AT FS 621 LT/RT WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FLOOR SUPPORT ANGLES AT FS 621 LEFT/RIGHT IAW ASA EO 600-53-0105. (M)

Part: SUPPORT BEAM — CRACKED (CENTER ENGINE)

DURING A C-CHECK IN MCN, THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 UNDER THE FIRE LOOP CLIP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 IAW ASA EO 600-53-0072. (M)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE LEFT AND RIGHT INBOARD AND OUTBOARD CLIPS AT FS 280 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LEFT AND RIGHT INBOARD AND OUTBOARD CLIPS AT FS 280. (M)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE AFT EQUIPMENT BAY CLIP AT FS 625 LEFT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE AFT EQUIPMENT BAY CLIP AT FS 625 LEFT. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE INTERCOSTAL AT FS 484, LBL 36, RBL 36 AND RBL 27 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE INTERCOSTALS AT FS 484, LBL 36, RBL 36 AND RBL 27 IAW ASA EO 600-53-0098. (M)

Part: PLATE — CRACKED (CARGO DOOR SILL)

DURING A C-CHECK IN MCN, THE CARGO DOOR FLOOR SILL PLATE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO DOOR FLOOR SILL PLATE IAW ASA EO 600-53-0117. (M)

Part: RIB — CRACKED (RT WING)

DURING AN A-CHECK IN MCN, THE RIGHT BATTERY RIB ASSEMBLY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE PERFORMED A TEMPORARY REPAIR TO THE RIGHT BATTERY RIB ASSEMBLY AT WS 53.60 IAW BOMBARDIER REO 601R-57-51-195. THIS IS A TEMPORARY REPAIR IS VALID FOR 500 FLIGHT HOURS FROM THE TIME OF INCORPORATION AND IS TO BE INSPECTED AT EVERY SERVICE CHECK. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: RIB — CRACKED (RT WING)

DURING AN A-CHECK, THE RT BATT RIB ASSEMBLY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RT BATT RIB ASSY AT WS 53.60 IAW EO. (K)

Part: SHUTOFF VALVE — INOPERATIVE (FUSELAGE)

FLT 4749 - DURING DESCENT FROM SRQ-ATL, A STRONG BURNING ODOR OCCURRED FOR APPROXIMATELY ONE MINUTE WHEN THE POWER WAS BROUGHT FROM IDLE TO CRUISE WITH THE ENGINE BLEEDS ON. THE ODOR DID NOT OCCUR WHEN THE BLEEDS WERE SELECTED TO THE AUXILIARY POWER UNIT. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE PRESSURE REGULATING SHUTOFF VALVE ON THE TENTH STAGE BLEED AIR SYSTEM. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: ODOR — DETECTED (COCKPIT)

DURING DESCENT INTO SHV FROM DFW, THE CREW NOTICED A BURNING ODOR COMING FROM THE LT PACK. THE AIRCRAFT LANDED SAFELY IN SHV. MAINTENANCE TESTED AND INSPECTED THE LEFT PACK SYSTEM OPERATING THE PACK THROUGH ALL TEMPERATURE RANGES FOR AN EXTENDED PERIOD OF TIME WITH NO ODOR NOTED. AIRCRAFT OK FOR SERVICE. (M)

Part: FITTING — CRACKED (PAX DOOR)

DURING HANGAR MAINTENANCE IN MCN, THE AFT ANCHOR ON THE PASSENGER DOOR WAS FOUND TO BE CRACKED. MAINTENANCE WILL MONITOR THE CRACK AND REPLACE THE ANCHOR WITHIN 100 FLIGHT HOURS PER REO 601R-52-11-272. (M)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

FLT 4382 - DURING A GROUND INSPECTION IN MGM, THE EMERGENCY CEILING LIGHT AT ROW FIVE WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY CEILING LIGHT LAMP AT ROW FIVE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: ODOR — DETECTED (CABIN)

FLT 4736 - DURING DESCENT INTO MYR FROM ATL, THE CREW RECEIVED A SMOKE TOILET AMBER MESSAGE ALONG WITH A NOTICEABLE ODOR OF SMOKE IN THE COCKPIT AND CABIN. A THIN HAZE OF SOME OCCURRED IN THE CABIN AND DISSIPATED ALONG WITH THE ODOR SHORTLY AFTERWARDS. THE RIGHT PACK OUTLET TEMPERATURE SPIKED TO 79 DEGREES CELSIUS SHORTLY AFTER TRANSFERRING THE BLEEDS TO THE AUXILIARY POWER UNIT. QRH PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE RAN THE ENGINES SWITCHING THE PACKS BETWEEN THE AUXILIARY POWER UNIT AND THE ENGINES WITH NO SMOKE OR ODOR RE-OCCURRING. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT)

DURING A GROUND INSPECTION IN DFW, THE MID AND AFT CABIN EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 3 BATTERY CHARGER AND BATTERY PACK (S/N 20131A). OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT)

FLT 4711 - DURING A GROUND INSPECTION IN DFW, THE RIGHT OVERWING EMERGENCY EXIT AND THE FORWARD CEILING EXIT SIGNS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT POWER SUPPLY UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: WINDSHIELD — CRACKED (COCKPIT)

WHILE DESCENDING INTO DSM, AT 17,000 FEET, THE CAPTAIN FORWARD WINDSHIELD CRACKED. AIRCRAFT LANDED SAFELY IN DSM. MAINTENANCE REMOVED AND REPLACED THE LEFT MAIN WINDSHIELD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: WIRE — DEFECTIVE (CABIN)

DURING GROUND INSPECTION IN ATL, CREW REPORTED EMERGENCY LIGHT ON DECK FROM ROW 6 AND FORWARD WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED POWER STRIP CABLE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CONTROL HANDLE — MALFUNCTIONED (COCKPIT)

FLT 4528 - AFTER DEPARTURE FROM ATL, WHEN GEAR WAS SELECTED UP, GEAR DID NOT COME UP, AND IT STAYED LOCKED THE ENTIRE FLIGHT. CAPTAIN ALSO RECEIVED A PARKING BRAKE SHUTOFF VALVE AND AN INBOARD ANTI-SKID CAUTION MESSAGE ON EICAS. CREW DECLARED AN EMERGENCY. AFTER PUTTING THE GEAR HANDLE IN THE DOWN POSITION ALL EICAS CAUTION MESSAGES WENT OUT. AIRCRAFT RETURNED AND LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED GEAR HANDLE ASSEMBLY. OPERATIONAL CHECK GOOD. NO OTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M)