N8698A

Part: SEAL — BROKEN (CABIN) · airframe 23,349 hrs · 21,047 cycles

FIRST AID KIT SEAL BROKEN. RESEALED FIRST AID KIT IAW AMM 25-60-00.

Part: STOWAGE BOX — BROKEN (COCKPIT OXYGEN) · airframe 22,545 hrs · 20,242 cycles

FIRST OFFICER OXYGEN STOWAGE BOX BROKEN. R & R STOWAGE BOX IAW AMM 35-11-04. CHECKED GOOD.

Part: VANE — CHAFED (TE FLAP) · airframe 22,186 hrs · 19,896 cycles

FLAP VANE LEADING EDGE CHAFED OUTBOARD OF THE OUTBOARD ACTUATOR. REPAIRED IAW BOMBARDIER REO 601R-57-52-004.

Part: VANE — CHAFED (TE FLAP) · airframe 22,186 hrs · 19,896 cycles

INBOARD FLAP VANE LEADING EDGE IS CHAFED INBOARD OF THE INBOARD ACTUATOR. REPAIRED IAW SRM 51-24-28.

Part: SKIN — CHAFED (LT AILERON) · airframe 22,186 hrs · 19,896 cycles

LEFT AILERON UPPER LEADING EDGE SKIN CHAFED OUT OF LIMITS. REPLACED IAW SRM 51-42-21.

Part: VANE — CHAFED (TE FLAP) · airframe 22,186 hrs · 19,896 cycles

FLAP VANE LEADING EDGE CHAFED OUTBOARD OF THE MIDDLE ACTUATOR. REPAIRED IAW BOMBARDIER REO 601R-57-52-004.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 22,186 hrs · 19,896 cycles

FORWARD RIGHT ACCESS PANEL DOOR SURROUND DOUBLER AT FS 235 HAS DAMAGED HOLES. REPAIRED IAW BOMBARDIER REO 601R-53-11-162.

Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 21,879 hrs · 19,595 cycles

1 INFANT LIFE VEST BAG TORN. REMOVED AND REPLACED INFANT LIFE VEST IAW PA 25-096A.

Part: FLEX DRIVE — FAULTY (TE FLAP) · airframe 21,820 hrs · 19,543 cycles

ON FLIGHT 4099 (BTV TO DTW) CREW RECEIVED FLAP FAIL AT 0 DEGREE. AIRCRAFT LANDED IN DTW SAFELY. REMOVED AND REPLACED NR 1, 2 & 3 FLEX SHAFT IAW AMM 27-53-10. REMOVED AND REPLACED NR 3 LEFT ACT IAW CRJ 200 AMM 27-53-05. PERFORMED TORQUE CHECK OF LEFT AND RIGHT FLAPS IAW CHECKLIST PROVIDED. LEFT -15INLB RIGHT -14INLB.

Part: STOWAGE BOX — DAMAGED (COCKPIT) · airframe 21,643 hrs · 19,381 cycles

O2 BOX DOOR BROKE. REMOVED AND REPLACED O2 STORAGE BOX IAW AMM 35-11-15. LEAK AND OPS CHECK GOOD. OK FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 21,438 hrs · 19,184 cycles

SMOKE TOILET MASTER CAUTION AFTER TAKEOFF. A/C WAS DEICED BEFORE FLIGHT WITH ALL TIMES ADHERED TO, APU OFF, BLEEDS ON THE ENGINES, AND OAT 1C ORH COMPLETE. COMPLIED WITH SMOKE/FUMES IN CABIN/FLIGHT DECK/SMOKE TOILET MSG WORKS COPE, NO DISCREPANCY NOTED. COULD NOT DUPLICATE ON GROUND, IAW CHECKLIST PROVIDED, SEE AML PAGE'S 2368803, 2368804 FOR CORRECTIVE ACTIONS.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 21,416 hrs · 19,160 cycles

PILOT LIFE VEST BAG TORN. REMOVED AND REPLACED PILOTS LIFE VEST IAW AMM 25-61-03.

Part: SHUTOFF VALVE — FAILED (CABIN PRESSURE) · airframe 20,926 hrs · 18,677 cycles

FLIGHT 4285, RIGHT PACK DROPPED OFF LINE ON CLIMB THRU 15000. RESET PACK, PACK CLOSED WITH TEMP THRU 20000. RESET PACK, PACK CLOSED HIGH TEMP CAUTION SECOND TIME WITHIN 90 SECONDS OF PREVIOUS RESET AT 23000. EXECUTED EMERGENCY DESCENT TO 10000. FLIGHT COMPLETED UNPRESSUREIZED. PERFORMED AIR RETURN. REMOVED AND REPLACED RIGHT PRESSURE REGULATING SHUTOFF VALVE PER AMM 21-51-43. OPS CHECKED GOOD. PERFORMED HIGH POWER ENGINE RUNS PER 71-00-00. OPS CHECKED GOOD.

Part: ISIS — ACTIVATED (COCKPIT) · airframe 20,064 hrs · 17,855 cycles

AIR RETURN FOR ISIS UNRELIABLE- SHOWING AS MUCH AS 30 DEGREE NOSE DOWN WHILE STRAIGHT AND LEVEL AND UP TO 90 DEGREE BANKS L/R WHEN STRAIGHT. ATTITUDE INDICATION AFFECTED ONLY. SPEED AND ALTITUDE OK. REMOVED AND REPLACED ISIS IAW AMM 34-14-01. A/C OK FOR SERVICE, OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 19,690 hrs · 17,539 cycles

FIRST OFFICER FLASHLIGHT DOES NOT BLINK. REMOVED AND REPLACED BATTERY IN F/O'S FLASHLIGHT IAW CRJ AMM 25-61-01. OPS CHECKS GOOD. PART EFFECTIVITY VERIFIED.

Part: VALVE — MALFUNCTIONED (FUEL SYSTEM) · airframe 19,514 hrs · 17,329 cycles

FUEL GRAVITY X-FLOW VALVE WILL NOT OPEN INOP. PERFORMED OPERATIONAL TEST OF GRAVITY X FLOW VALVE IAW AMM 28-13-16. OP CHECK GOOD. OK FOR SERVICE.

Part: AUTOPILOT SYS — MALFUNCTIONED · airframe 19,352 hrs · 17,184 cycles

AUTOPILOT PITCH TRIM CAUTION IN FLIGHT QRH COMPLETE. OPS CHECK AFTER RESET OPS CHECKED GOOD IAW AMM 27-41-15, OPS CHECK GOOD. A/C OK FOR SERVICE.

Part: WEB — DAMAGED (FUSELAGE) · airframe 18,933 hrs · 16,773 cycles

FS 559.0 RT WEB HAS INDICATION NOTED I/B OF RBL 18.0 WL 59.10 APPROX .2" IN LENGTH 50 PERCENT FSH AND O/B OF RBL 9.0 WL 58.7 APPROX .3" IN LENGTH 80 PERCENT FSH FAILED NDT INSPECTION. REPAIRED IAW BOMBARDIER REO 601R-53-41-260 REV E AND REO 601R-53-41-609 REV B, DEVIATION "E".

Part: WEB — DAMAGED (FUSELAGE) · airframe 18,933 hrs · 16,773 cycles

FOUND FS 559.00 RT SIDE WEB HAS INDICATIONS NOTED I/B OF RBL 18.0 WL 59.10 APPROX .2 INCH IN LENGTH 50 PERCENT FSH AND O/B OF RBL 9.0 WL 58.70 APPROX .3 INCH IN LENGTH 80 PERCENT FSH. FAILED NDT. REPAIRED IAW BOMBARDIER REO 601R-53-41-260 REV E; REO 601R-53-41-609 REV B; & BOMBARDIER SERVICE CORPORATION STANDARD REPAIR 601R-53-0114.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 18,391 hrs · 16,280 cycles

NWS INOP CAUTION MSG AFTER GEAR RETRACTION IN WORK JFK, REPEAT ISSUE FROM 4-11-11.

Part: HINGE FITTING — DAMAGED (TE FLAP) · airframe 18,029 hrs · 15,947 cycles

LIGHTENING STRIKE DAMAGE WAS FOUND ON THE LEFT OUTBOARD FLAP CENTER HINGE BOX FITTING (P/N 601R10119-95). ONE OF THE DAMAGE LOCATIONS SHOWED SIGNS OF MELTING AND IT MEASURED 0.311 X 0.144 X 0.045. REPAIRED IAW STS ENGINEERING EA 09-2011-031.

Part: DOUBLER — LEAKING (FUSELAGE) · airframe 17,504 hrs · 15,453 cycles

PREVIOUS FUSELAGE SKIN REPAIR PATCH PERFORMED AT WVAV IAW REO 601R-53-19698 AT FS 409+64 - FS 409+96 AND STR 1L - 1R WAS FOUND LEAKING UNDER PRESSURE CAUSING A HIGH PITCHED NOISE UNDER PRESSURE IN RDU. FERRY FLY FROM RDU TO CKB (WVAC) IAW BOMBARDIER REO 601R-53-707 WHERE THE PATCH WAS PROPERLY SEALED IAW APPLICABLE AMM 51-23-00 PROCEDURES.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,410 hrs · 15,352 cycles

CARGO SILL PLATE FS 574 TO FS 621 IS CORRODED. REPLACED AS PER REO 601R-53-61-1574.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,410 hrs · 15,352 cycles

FUSELAGE SKIN HAS MINOR CORROSION AROUND DRAIN HOLE AT FS 559+64 BETWEEN STR 26L AND 27. REPAIRED IAW BOMBARDIER REO 601R-53-19685A.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,410 hrs · 15,352 cycles

RT CABIN SIDE SEAT TRACKS CORRODED FROM FS 409+18.02 TO 559+80. REMOVED AND REPLACED RT CABIN SIDE SEAT TRACKS FROM FS 409+18.02 TO FS 559+80 IAW CRJ 200 SRM 51-40-11, CRJ 200 AMM 53-01-11-000-802 AND 53-01-11-400-802.

Part: SKIN — GOUGED (FUSELAGE) · airframe 17,410 hrs · 15,352 cycles

DURING REMOVAL OF ADF ANTENNA FOUND BAD NUT PLATES AND FUSELAGE SKIN GOUGED. PERFORMED A MAJOR REPAIR TO THE EXTERNAL FUSELAGE SKIN AT FS 409.00+64 TO FS 409.00+96 BETWEEN STRINGERS 1R TO 1L AFT OF ADF ANTENNA BY CUTTING AWAY THE DAMAGE, FABRICATING REPAIR PARTS, AND INSTALLING REPAIR PARTS IAW BSC EO 601R-53-19610.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,410 hrs · 15,352 cycles

FUSELAGE SKIN HAS MINOR CORROSION AT FS 559+80 AT STR 27. REPAIRED IAW BOMBARDIER REO 601R-53-19685A.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,410 hrs · 15,352 cycles

RT CABIN FLOOR SIDE SILL HAS AREAS OF MINOR CORROSION AT FS 506.00 AND FS 559.00. REPAIRED RT CABIN FLOOR SIDE SILL AT FS 506.00 AND FS 559.00 IAW BOMBARDIER REO 601R-53-41-666.

Part: FRAME — WORN (FUSELAGE) · airframe 17,410 hrs · 15,352 cycles

THE FUSELAGE FRAME AT FS 718.00 HAS WEAR DAMAGE AND A HOLE BETWEEN STRINGER 16L AND 17L. REPAIRED THE FRAME AT FS 718.00 BETWEEN STRINGER 16L AND 17L IAW BOMBARDIER SERVICES CORPORATION EO 601R-53-19680.

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,410 hrs · 15,352 cycles

CONNECTORS BRACKETS (2) ATTACHED TO PAX DOOR SILL ANGLE CORRODED AT PAX DOOR ENTRANCE. REMOVED AND REPLACED CONNECTORS BRACKETS IAW CRJ 200 SRM 51-40-06 AND 51-42-06.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,410 hrs · 15,352 cycles

FUSELAGE SKIN HAS MINOR CORROSION AT FS 559+64 BETWEEN STR 23R AND 24R. REPAIRED IAW BOMBARDIER REO 601R-53-19685A.

Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,410 hrs · 15,352 cycles

FS 280.00 BULKHEAD WEB CORRODED AND FLOOR SUPPORT ANGLE BETWEEN LBL 9 AND RBL 9, ALSO CRACKED O/B OF LBL 9 AND RBL 9, ALONG WITH FLOOR SUPPORT CLIPS LBL 9 I/B AND O/B. REPAIRED FS 280.00 BULKHEAD WEB, ANGLES AND CLIPS IAW BOMBARDIER REO 601R-53-11-926 REV B. BSC EO 601R-53-19702 AND BSC SR 601R-53-0110.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,410 hrs · 15,352 cycles

FS 280.00 FWD FLOOR SUPPORT J-ANGLE IS CORRODED BETWEEN LBL 9 AND RBL 9. REMOVED AND REPLACED FS 280.00 FWD FLOOR SUPPORT J-ANGLE BETWEEN LBL 9 AND RBL 9 IAW CRJ 200 SRM 51-40-11 AND 51-42-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,410 hrs · 15,352 cycles

LT CABIN SIDE SEAT TRACK CORRODED FROM FS 484 TO 559+80. REMOVED AND REPLACED SEAT TRACK IAW CRJ AMM 53-01-11-400-802.

Part: PRESSURE PANEL — DAMAGED (FUSELAGE) · airframe 17,404 hrs · 15,346 cycles

OUTBOARD FLANGE AT FS 529.00 RBL 27.00 HAS MISS-DRILLED/ DOUBLE DRILLED HOLES THROUGH THE PRESSURE FLOOR AND FLOORBEAM FLANGE INBOARD FLANGE. THE HOLE IS 0.35" (EDGE TO EDGE ) X 0.2. COMPLIED WITH BSC EO 601R-53-19683.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 17,404 hrs · 15,346 cycles

S 202.75 PRESSURE BULKHEAD IS CRACKED AT BRAKE CABLE PASS-THRU HOLE. C/W REO 601R-53-11-563 AND BSC STANDARD REPAIR 601R-53-0101A.

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,410 hrs · 15,352 cycles

CONNECTOR BRACKETS P/N 601R31771-1 (2 EACH) ATTACHED TO PASSENGER DOOR SILL BETWEEN FS 319 AND FS 349 ARE CORRODED. REMOVED AND REPLACED CONNECTOR BRACKETS IAW CRJ 200 SRM 51-40-06 AND 51-42-06.

Part: FAIRING — CHAFED (TE FLAP) · airframe 17,353 hrs · 15,297 cycles

RT WING FLAP STUB FAIRING ASSEMBLY (P/N 601R31199) WAS FOUND WITH CHAFE DAMAGE. THE DAMAGE IS THE RESULT OF A FASTENER / PACKER THAT SECURES THE P/N 601R14016 SEAL TO THE INBOARD FLAP PROTRUDING AND CONTACTING THE STUB FAIRING DURING NORMAL FLAP MOVEMENT. CHAFE DAMAGE IS PRESENT OVER A 9.25 INCH LENGTH WITH A MAXIMUM DEPTH OF 0.035 INCH. AT THE LOWER AFT END OF THE CHAFE DAMAGE, THE FAIRING SKIN IS PENETRATED OVER A 0.60 INCH BY 0.312 INCH AREA. TEMPORARY REPAIR AND FLY ON NOT TO EXCEED 100 FH PER STS ENGINEERING EA 5-2010-177 WITHIN WHICH TIME RT WING FLAP STUB FAIRING ASSEMBLY WILL BE REMOVED AND REPLACED.

Part: FCU — FAILED (TE FLAPS) · airframe 14,578 hrs · 12,581 cycles

FLIGHT 2453 ICT/MSP CREW RECEIVED FLAP FAIL CAUTION MESSAGE WHILE BOARDING PASSENGERS. MAINTENANCE PERFORMED FIM TROUBLES SHOOTING PER AD 2009-06-12 FOUND FLAP ELECTRONIC CONTROL UNIT (FECU) SHOWING CODE FOR INTERNAL FAILURE. FECU REMOVED AND REPLACED PER AMM.

Part: SCAVENGE PUMP — DEFECTIVE (RT ENGINE)

IN CRUISE FLIGHT, THE FLIGHT CREW NOTICED A LOSS OF RT ENGINE OIL PRESSURE AND THE ASSOCIATED WARNINGS. THE FLIGHT CREW EXECUTED THE QRH, SHUTDOWN THE ENGINE AND DECLARED AN EMERGENCY. AN OTHERWISE NORMAL APPROACH AND LANDING WAS MADE. MX INSPECTED THE ENGINE AND DISCOVERED THERE WAS A SMALL AMOUNT OF OIL LEAKING FROM THE AXIS D AND F AGB CARBON SEALS, BUT THAT THE OIL PRESSURE LOSS WAS DUE TO A DEFECTIVE LUBE AND SCAVENGE OIL PUMP. THE CARBON SEALS AND PUMP WERE REPLACED. THE ENGINE WAS RUN UP AND FOUND TO HAVE TO HAVE GOOD OIL PRESSURE AND NO LEAKS. THE ACFT WAS RELEASED FOR SERVICE. (K)

Part: TIRE — FAILED (MLG) · airframe 12,963 hrs · 11,150 cycles

UPON ROTATION DEPARTING KJAN CREW NOTICED SUDDEN AND SHARP ROLLING MOTION AND TUG TO THE LEFT. SUSPECTED TO BE BLOWN TIRE. NO OTHER INDICATIONS NOTED. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. NO DAMAGE OR DEFECTS NOTED AND A/C HANDLED NORMALLY. MAINTENANCE FOUND NO DAMAGE OF DEFECTS NOTED.

Part: FLAP SYSTEM — UNKNOWN · airframe 9,862 hrs · 8,563 cycles

FLAP FAIL, SECOND OCCURNACE WITHIN 72 HOURS.

Part: ACM — INOPERATIVE (RIGHT)

(REF NR: 05-094) IN FLIGHT CABIN HAD FUMES AND POSSIBLE SMOKE. QRH FOLLOWED DIVERTED WITH UNEVENTFUL LANDING. TROUBLESHOT AIRCRAFT AND ENGINES DOWN TO THE RT AIR CYCLE MACHINE (ACM). REMOVED AND REPLACED RT ACM IAW AMM. OPS CHECKED GOOD. (K)

Part: PROXIMITY SENSOR — OUT OF ADJUST (NLG)

GEAR DISAGREE LIGHT ON SHORT FINAL. UNEVENTFUL LANDING. ADJUSTED NLG OLEO PROX SENSOR IAW AMM. PERFORMED GEAR SWING, OPS CHECKED GOOD IAW AMM. OK FOR SERVICE. (K)

Part: INDICATION SYS — MALFUNCTIONED (NLG)

UPON GEAR EXTENSION FOR LANDING, NOSE LANDING GEAR WOULD NOT SHOW DOWN. DECLARED EMERGENCY, FOLLOWED QRH WITH UNEVENTFUL LANDING. PERFORMED GEAR SWING IAW AMM. NO DEFECTS NOTED, OK FOR SERVICE. (K)