N684BR

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 18,115 hrs · 16,718 cycles

FLOOR EMERGENCY EXIT LIGHT BY ASD DIM. RELAMPED IAW AMM 33-50-19, OPS CHECKED GOOD.

Part: LAMP — BROKEN (EMERGENCY LIGHT) · airframe 15,979 hrs · 14,297 cycles

RT EXTERIOR NR 2 EMERGENCY LIGHT INOP. RELAMPED RT EXTERIOR NR2 EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECK GOOD. RELAMPED RT EXTERIOR NR2 EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECK GOOD.

Part: DOOR — MISINSTALLED (EMERGENCY EXIT) · airframe 15,515 hrs · 13,751 cycles

RT OVERWING EMERGENCY EXIT DOOR IS DIFFICULT TO OPEN. UPON INVESTIGATION FOUND THE OVERWING EMERGENCY EXITS TO BE INSTALLED IN THE INCORRECT POSITION. INSTALLED THE OVERWING EMERGENCY EXITS IN THE CORRECT LOCATIONS IAW AMM 52-21-00-400-801. PERFORMED OPS TEST OF THE OVERWING EMERGENCY EXITS. TESTED GOOD AT THIS TIME IAW AMM 52-21-00-710-801.

Part: FLOOR SUPPORT — CORRODED (BS 569-921) · airframe 15,505 hrs · 13,738 cycles

CARGO COMPARTMENT FLOORBEAM CAP IS CORRODED BEYOND REPAIR AT LBL 27 FROM FS 569.00 TO FS 621.00. EC/TC REQUIRED FOR REO 601R-53-61-3400 REV.H. COMPLIED WITH EC/TC REO 601R-53-61-3400 IAW REO 601R-53-61-3400 REV.H

Part: SILL — CRACKED (BS 589) · airframe 15,505 hrs · 13,738 cycles

SUPPORT ANGLE AT FS 589.00, LBL 36 UNDER CARGO DOOR FLOOR SILL IS CRACKED. LOCATED & INSTALLED NEW SUPPORT ANGLE IAW SRM 51-42-06 & 51-42-21.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 15,505 hrs · 13,738 cycles

LEFT WALL SEAT TRACK AT FS 559+75 IS CORRODED. REMOVED CORRODED SEAT RAIL SECTION ON LT WALL IAW AMM 53-01-11-000-802. INSTALLED NEW RAIL SECTION IAW AMM 53-01-11-400-802.

Part: FRAME — CORRODED (BS 513.00) · airframe 15,505 hrs · 13,738 cycles

LEFT FRAME 513.00 HAS CORROSION AT PRESSURE FLOOR. COMPLIED WITH STEP 2 OF REO 601R-53-41-1241. PERFORMED EDDY CURRENT OF LT FRAME 513 AT PRESSURE FLOOR REPAIR IAW NDTM 51-20-06. NO INDICATIONS NOTED AT THIS TIME. COMPLIED WITH STEPS 3, 4 AND 5 OF REO 601R-53-41-1241 BY ROTO PEENING, RESTORED PROTECTIVE FINISH AND APPLIED CORROSION INHIBITING COMPOUND TO THE REWORKED AREA. COMPLIED WITH EC/TC REO 601R-53-41-1241.

Part: PRESSURE PANEL — CORRODED (FLOOR) · airframe 15,505 hrs · 13,738 cycles

LEFT PRESSURE FLOOR SKIN OTBD OF LBL 36 HAS AREAS OF CORROSION. C/W REO 601R-53-41-666, REV A.

Part: SEAT TRACK — CORRODED (BS 559-567) · airframe 15,505 hrs · 13,738 cycles

CARGO COMPARTMENT SEAT RAILS AT LBL 27 BETWEEN FS 559+80 AND 567.00 ARE CORRODED. R & R SEAT RAILS IAW SRM 51-41-02.

Part: SEAT TRACK — CORRODED (BS 559-569) · airframe 15,505 hrs · 13,738 cycles

CARGO COMPARTMENT SEAT RAILS AT RBL 9 BETWEEN FS 559.00+80 AND FS 569.00 ARE CORRODED. REPLACED SEAT RAILS IAW SRM 51-41-02. FOUND FITTING BROKEN ON SEAT TRACK 601R38727-13. REPLACED FITTING IAW SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (BS 569-621) · airframe 15,505 hrs · 13,738 cycles

CARGO COMPARTMENT FLOOR SUPPORT CAP IS CORRODED BEYOND REPAIR AT LBL 27 FROM FS 569.00 TO FS 621.00. REMOVED CARGO COMPARTMENT FLOOR SUPPORT CAP IAW SRM 51-42-21 & 51-42-06. LOCATED AND DRILLED NEW FITTING & FLOOR SUPPORT CAP IAW SRM 51-40-11. COUNTERSUNK & DEBURRED FITTING & FLOOR SUPPORT IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE FLOOR SUPPORT CAP IAW REO 601-R53-61-3400. INSTALLED A NEW FLOOR SUPPORT FITTING IAW SRM 51-42-21, 51-42-02, & REO 601R-53-61-3400 REV H. APPLIED PAINT TO FLOOR SUPPORT FITTING IAW SRM 51-25-26.

Part: SEAT TRACK — CORRODED (BS 559-617) · airframe 15,505 hrs · 13,738 cycles

CARGO COMPARTMENT SEAT RAILS AT LBL 9 BETWEEN FS 559+91 AND FS 617.00 ARE CORRODED. R & R SEAT RAILS AND ANCHOR PLATES IAW SRM 51-41-02.

Part: ANGLE — CRACKED (BS 559 BULKHEAD) · airframe 15,505 hrs · 13,738 cycles

FOUND FS 559 LT CAP ANGLE HAS INDICATION NOTED, APPROX .3" IN LENGTH 60 PERCENT FSH AT LBL 18.0 AND FS 559 RT. BULKHEAD WEB HAS INDICATIONS NOTED APPROX .3" IN LENGTH 50 PERCENT FSH INBD OF RBL 18.0 WL 59.10. BOTH FAILED NDT INSPECTION. COMPLIED WITH EC/TC REO 601R-53-41-260 IAW REO 601R-53-41-260 REV D.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 15,505 hrs · 13,738 cycles

CARGO COMPARTMENT SEAT RAIL AT RBL 27 FS 559.00+80 TO 559.00+96 IS CORRODED. R & R SEAT RAIL IAW SRM 51-41-02.

Part: CHANNEL — CRACKED (BS 409 BULKHEAD) · airframe 15,505 hrs · 13,738 cycles

INDICATION NOTES AT FS 409+128 RBL 18 WL 69.0 IN RADIUS OF OTBD U CHANNEL OF THE BULKHEAD BEAM APPROX .30" LONG 50 PERCENT FULL SCREEN HEIGHT. REMOVED RBL 18 VERTICAL POST ASSY & SEPARATED INBD & OTBD HALVES IAW SRM 51-42-06. LOCATED & DRILLED NEW SERVICEABLE POST IAW SRM CH 51-40-11 & SUB ASSY INBD & OTBD POST HALVES IAW SRM CH 51-42-06. INSTALLED SERVICEABLE POST ASSY IAW SRM 51-42-06 & REO 610R-53-41-889. C/W EC/TC REO 601R-53-41-889 & MET ALL THE REQUIREMENTS OF REO 610R-53-41-889 REV A.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 15,505 hrs · 13,738 cycles

PAX DOOR AFT DRAG ANGLE IS CRACKED IN PREVIOUS REPAIR. COMPLIED WITH EC/TC REO 601R-52-11-513 IAW REO 601R-52-11-513.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 15,505 hrs · 13,738 cycles

LEFT AND RT FWD FLOOR SEAT TRACK SEGMENT IN CABIN ARE CORRODED AT THE FWD ENDS. REMOVED LT AND RT FWD SEAT TRACKS IAW AMM 53-01-11-000-802. INSTALLED NEW SEAT TRACKS LT AND RT FWD SECTION IAW AMM 53-01-11-400-802.

Part: LIGHT — BROKEN (CABIN) · airframe 15,181 hrs · 13,391 cycles

LOWER EMERGENCY LIGHT ON F/A WARDROBE BASE BROKEN. R & R FLOOR LEVEL EMERGENCY FLOOD LIGHT ON WARDROBE IAW AMM 33-51-19. OPS CHECK GOOD. R & R FLOOR LEVEL EMERGENCY FLOOD LIGHT ON WARDROBE IAW AMM 33-51-19. OPS CHECK GOOD.

Part: FLAP — FAILED (WING) · airframe 12,492 hrs · 10,613 cycles

FLAPS FAILED AT 8 WHEN SELECTING 20 ON APPROACH.

Part: SUPPORT BEAM — CRACKED (CARGO DOOR) · airframe 11,512 hrs · 9,731 cycles

CARGO DOOR SUPPORT BEAM LOWER ANGLE IS CRACKED .3" IN LENGTH. REMOVED CRACKED SUPPORT BEAM. INSTALLED NEW SERVICEABLE IAW SRM 51-42-21. (B)

Part: INTERCOSTAL — CRACKED (BS484 RBL 27-36) · airframe 11,512 hrs · 9,731 cycles

RIGHT FS 484 INTERCOSTAL AT RBL 27.00 AND RBL 36.00 IS CRACKED .25 INCH. REMOVED CLIP FROM FS 484.00, RBL 27.00 AND INSTALLED NEW SERVICEABLE CLIP ON INTERCOSTAL IAW CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-21 AND CRJ 200 SRM 51-40-11. CUT AWAY DAMAGED FLANGE AT RBL 36.00, FABRICATED NEW ANGLE FROM S MATERIAL AND INSTALLED ANGLE IAW BAS REO. (B)

Part: ATTACH FITTING — CRACKED (FS 280 LBL 9) · airframe 11,512 hrs · 9,731 cycles

BULKHEAD FS 280.00 LBL 9.0 HAS A CLIP CRACKED .5 INCH. REMOVED OLD CRACKED CLIP AT FS 280.00 LBL 9.0, INSTALLED NEW SERVICEABLE CLIP P/N 601R-31113-57 IAW CRJ 200 SRM 51-42-06 AND 51-42-21. (B)

Part: PLACARD — WORN (CABIN) · airframe 1,151,233 hrs · 9,731 cycles

CREW ESCAPE HATCH EXTERNAL PLACARDS ARE UNREADABLE. REAPPLIED SILKSCREENS ON CREW ESCAPE HATCH IAW MM 11-10-03-400-801.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 11,512 hrs · 9,731 cycles

PASSENGER DOOR STAIR AFT DRAG ANGLE IS CRACKED 1/2" REPAIRED PAX DOOR STAIR AFT DRAG ANGLE IAW REO 601R-52-11-513 AND ET/CT 601R-52-11-513. (B)

Part: HINGE FITTING — CRACKED (ESCAPE HATCH) · airframe 1,151,233 hrs · 9,731 cycles

JOB 8770831 OPERATION 152 CREW ESCAPE HATCH RIGHT HINGE ARM IS CRACKED. RESOLVED ON W/O: 91780 TASKCARD: N/R-00192. REMOVED AND REPLACED RT HINGE ARM ON CREW ESCAPE HATCH IAW CRJ 200 AMM 20-21-00-910-801. OPS TEST GOOD IAW CRJ 200 AMM 52-22-00-710-801. ASA RII C/W 5300010 [SDR CLOSED]

Part: BULKHEAD — CRACKED (BS 202) · airframe 11,512 hrs · 9,731 cycles

FS 202.75 BULKHEAD HAS A .50 INCH CRACK WHERE PARKING BRAKE CABLE GOES THROUGH. REPAIRED FS 202 BULKHEAD IAW ASA EO 600-53-217 IN ITS ENTIRETY. (B)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,735 hrs · 9,054 cycles

WHITE EMERGENCY EXIT LIGHT BY PAX DOOR INOP.

Part: SIGN — INOPERATIVE (CABIN) · airframe 9,912 hrs · 8,353 cycles

EMERGENCY EXIT SIGN AT ASD IS INOP.

Part: STEP — CRACKED (AIRSTAIR DOOR) · airframe 9,731 hrs · 8,232 cycles

ASD BOTTOM STEP CRACKED.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 9,194 hrs · 7,831 cycles

PAX DOOR AFT CABLE COUNTER BALANCE ANCHOR BRACKET CRACKED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,773 hrs · 7,510 cycles

RIGHT FWD EMERGENCY LIGHT OUT.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 8,439 hrs · 7,259 cycles

WHEN ATTEMPTING TO EXTEND FLAPS TO 8 DEG, FAILED AT 0 DEG. EN ROUTE TO ERI A/C DIVERTED TO CLE DUE TO MTC. EMERGENCY DECLARED. FLT 4266 CX & ON 02/0607 FLTS 4634, 4847 CX.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 8,246 hrs · 7,112 cycles

RT EMERG EXTERIOR OVERWING FWD LIGHT IS INOP.

Part: ANCHOR FITTING — CRACKED (AFT ASD) · airframe 8,003 hrs · 6,921 cycles

A/S/D AFT CABLE COUNTER BALANCE ANCHOR BRACKET CRACKED.

Part: BEAM — CRACKED (FUSELAGE) · airframe 8,003 hrs · 6,921 cycles

SUSPECT CRACK ON RT SIDE OF ENGINE SUPPORT BEAM. REPAIRED IAW ALL PERTINENT REPAIR INSTRUCTIONS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 8,003 hrs · 6,921 cycles

SUSPECT CRACK ON FS 640 FRAME PER INSPECTION OF TASK CARD E0600-53-69-0002. FLT 4256 CX.

Part: MASTER CAUTION — ILLUMINATED · airframe 7,862 hrs · 6,814 cycles

NOSE GEAR DISAGREE MASTER CAUTION AFTER TAKEOFF AND GEAR UNSAFE CAUTION WARNING. A/C RETURNED TO SHV AFTER T/O. EMERGENCY DECLARED. FLT 4884 CX.

Part: LANDING GEAR — INOPERATIVE (NOSE) · airframe 7,819 hrs · 6,778 cycles

NLG DID NOT RETRACT AFTER TAKEOFF, C/W QRH AND RETURNED TO OMA. FLT 4418 CX - EMERGENCY DECLARED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 6,998 hrs · 6,174 cycles

ETNRC 100-1 ANGLE CRACK AT FS260 RBL 11 UNDER FLOOR BEAM.

Part: SWITCH — FAULTY (STAB TRIM)

STABILIZER TRIM/MACH TRIM CAUTION MESSAGE. FOUND PILOT STAB DISCONNECT SWITCH FAULTED. REMOVED AND REPLACED SWITCH.

Part: ENGINE — SHUTDOWN (RIGHT)

EVENT SUMMARY STATED RIGHT ENG SHUT DOWN IN FLT DUE TO LOW OIL PRESSURE. REMOVED AND REPLACED AGB CARBON SEALS FOR IDG, ATS AND HYDRAULIC PUMP IAW AMM 72-60-00. OIL CONSUMPTION RUNS COMPLIED WITH AMM 71-00-00.

Part: WARNING LIGHT — ILLUMINATED (THRUST REVERSER)

EVENT SUMMARY STATED THRUST REVERSER UNLOCK MESSAGE IN FLIGHT. OPENED DM 3114105-1 MEL 78-30-01 CAT B. RIGHT THRUST REVERSER UNLOCK MESSAGE ON ROTATION, (M) PROCEDURES C/W, ITEM PLACARD AND TRANSFERRED TO SUMMARY OF DEF ITEMS. REMOVED AND REINSTALLED RT ENGINE COWLS REF AMM 71-10-00.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 2,947 hrs · 2,477 cycles

DURING INSPECTION THE LEFT HAND FUSELAGE EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 2,220 hrs · 1,890 cycles

DURING INSPECTION THE FORWARD OVERHEAD EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY LIGHT. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE.

Part: CONNECTOR — NOT SEATED (FA SERVICE PANEL)

DURING OVERNIGHT MAINTENANCE IT WAS DISCOVERED THAT THE FLIGHT ATTENDANT EMERGENCY LIGHT SWITCH WAS INOPERATIVE. MAINTENANCE PERSONNEL RESEATED THE CONNECTOR PLUG AT THE FLIGHT ATTENDANT SERVICE PANEL. AN OPERATIONAL CHECK OF THE EMERGENCY LIGHTS WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE.