N414ZW

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 41,099 hrs · 39,292 cycles

CAP STRIP CORRODED ON CROSS BEAM 62, FS 589 BETWEEN LBL 9 AND LBL 27. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED CAP STRIP ON CROSS BEAM 62 FS 589 BETWEEN LBL 9 AND LBL 27, IAW CRJ200 SRM 51-42-06.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 41,099 hrs · 39,292 cycles

FOUND CORRODED SEAT TRACK AT LBL 9 FS 379 TO FS 409+128. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK, IAW BOMBARDIER ERO 601R-53-00-764 AND CRJ-2OO SRM 51-41-02.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 41,099 hrs · 39,292 cycles

FOUND SEAT TRACK CORRODED AT FS 559+80 AT LBL 9. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK, IAW BOMBARDIER REO 601R-53-00-764 AND CRJ-200 SRM 51-41-02.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 41,099 hrs · 39,292 cycles

FOUND CORRODED SEAT TRACK AT RBL 9 FS 409+128 TO FS 559+32. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK, IAW BOMBARDIER REO 601R53-00-764 AND CRJ-200 SRM 51-41-02.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 41,099 hrs · 39,292 cycles

FOUND SEAT TRACK CORRODED AT FS 559+64 TO FS 559+80. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK, IAW BOMBARDIER REO 601R-53-00-764 AND CRJ-200 SRM 51-41-02.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 41,099 hrs · 39,292 cycles

FOUND SEAT TRACK CORRODED AT FS 559+64 TO FS 559+80. REMOVED AND REPLACED SEAT TRACK. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK, IAW BOMBARDIER REO 601R-53-00-764 AND CRJ-200 SRM 51-41-02.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 41,099 hrs · 39,292 cycles

FOUND CORRODED SEAT TRACK AT LBL 9 FS 409+128 TO FS 559+32. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK, IAW BOMBARDIER REO 601R-53-00-764 AND CRJ-200 SRM 51-41-02.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 41,099 hrs · 39,292 cycles

FOUND CORRODED SEAT TRACK AT LBL 9 FS 559+32 TO 559+80. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK, IAW BOMBARDIER REO 601R-53-00-764 AND CRJ-200 SRM 51-41-02.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 41,099 hrs · 39,292 cycles

FOUND SEAT TRACK CORRODED AT FS 559 + 80. REMOVED AND REPLACED SEAT TRACK, IAW BOMBARDIER REO 601R-53-00-764 AND CRJ-200 SRM 51-41-02. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK, IAW BOMBARDIER REO 601R-53-00-764 AND CRJ-200 SRM 51-41-02.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 41,099 hrs · 39,292 cycles

FOUND CORRODED SEAT TRACK AT RBL 9 FS 559+32 TO 559+80. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK, IAW BOMBARDIER REO 601R-53-00-764 AND CRJ-200 SRM 51-41-02.

Part: STRUCTURE — CORRODED (CABIN) · corrosion level 2 · airframe 41,099 hrs · 39,292 cycles

FOUND CORROSION ON T-CAP AT FS 559+80 TO FS 621 LBL 27. REMOVED AND REPLACED T-CAP, IAW BOMBARDIER DRAWING 601R35031 AND CRJ-200 SRM 51-42-21. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED T-CAP, IAW BOMBARDIER DRAWING 601R35031 AND CRJ-200 SRM 51-42-21.

Part: LANDING — CRACKED (FUSELAGE) · airframe 38,543 hrs · 36,822 cycles

LT AFT LATCH AREA ON TRU DOOR HAS A CRACK. REPLACED LT TRU DOOR LAND SKIN IAW SRM 51-42-06, 51-42-13.

Part: RIB — CRACKED (RT EXHAUST) · airframe 38,543 hrs · 36,822 cycles

RT EXHAUST FAIRING 446AL SECOND RIB FROM FWD IS CRACKED. REPLACED

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 38,543 hrs · 36,822 cycles

CARGO DOOR BEAM AFT LOWER ATTACH ANGLE AT 621 IS CRACKED. REPLACED

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 38,543 hrs · 36,822 cycles

REAR PRESSURE BULKHEAD HAS A 1" CRACK EXTENDING FROM THE UPWARD END OF THE CARGO DOOR TRACK. REPAIR INCORPORATED IN BULKHEAD MOD DOCUMENTED ON W/O 1016221-2000-0050 SN: 6576339. (PICKET FENCE MOD)

Part: FITTING — CRACKED (FUSELAGE) · airframe 38,543 hrs · 36,822 cycles

RIGHT WINDSHIELD SIDE POST LOWER AFT FITTING IA CRACKED. REPLACED FITTING IAW SRM 51-42-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 38,543 hrs · 36,822 cycles

LEFT HAND WINDSHIELD SIDE POST LOWER AFT FITTING HAS A CRACK. REPLACED LT LOWER AFT FITTING IAW SRM 51-42-21.

Part: SKIN — GOUGED (TE FLAP VANE) · airframe 38,543 hrs · 36,822 cycles

LEFT HAND, OUT BOARD FLAP VANE, O/B END OF VANE HAS A GOUGE. REPLACED LT, O/B FLAP VANE LEADING EDGE SKIN IAW SRM 57-53-00, 51-42-13, 51-24-36, TR-51-42.

Part: ATTACH BRACKET — CRACKED (BS 449-473) · airframe 38,543 hrs · 36,822 cycles

LEFT SIDE LONGERON ATTACH BRACKETS CRACKED (4 EACH) FROM FS 449.85 TO 473.15. REPLACED 4 EACH LONGERON ATTACH BRACKETS IAW CRJ200 SRM 53-82-83, TR51-42, 51-42-06, 51-42-15, 51-24-21.

Part: BRACKET — CRACKED (BS 473) · airframe 38,543 hrs · 36,822 cycles

RIGHT SIDE LONGERON ATTACH BRACKET CRACKED AT FS 473.15. REPLACED BRACKET IAW CRJ200 SRM 51-42-06, 51-42-21, 51-45-00.

Part: RETAINER — CRACKED (PYLON) · airframe 38,543 hrs · 36,822 cycles

PNL 422DB SEAL RETAINER CRACKED. REPLACED SEAL RETAINER IAW SRM 54-42-06.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 38,468 hrs · 36,761 cycles

AT FL300 LT REV UNLOCK CAUTION. NO ADVERSE A/C INDICATIONS. PER IAC LT REV LEVER IDLE, LT THRUST REV EMER STOW. MSG REMAINED HOWEVER WE HAD POSITIVE CONTROL OF LT THRUST AND A/C. DEFERRED PER THE MEL

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,358 hrs · 35,614 cycles

FLOOR LEVEL EMERGENCY FLOOD LIGHT AT PAX DOOR ENTRY INOPERATIVE. ON FURTHER TROUBLESHOOTING, FOUND CEILING EMERGENCY EXIT SIGN FWD SIDE AT ROW 8 AND EMERGENCY EXIT EXTERIOR LIGHTS JUST FWD OF THE LEFT AND RIGHT OVERWING EXIT LIGHTS ALSO INOPERATIVE. REMOVED AND REPLACED THE NR 2 BATTERY PACK IAW AMM 33-51-01. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,165 hrs · 35,424 cycles

BOTH FORWARD OUTSIDE EMERGENCY LIGHTS FWD AND GALLEY FLOOR LIGHTS. REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY PACK IAW AMM 33, OPS CHECKED GOOD.

Part: CONNECTOR — DIRTY (EMERGENCY LIGHTS) · airframe 36,529 hrs · 34,801 cycles

FLOOR EMERGENCY LIGHTS ROWS 6-8 INOPERATIVE. FOUND CONNECTORS TO BE DIRTY, CLEANED THE CONNECTORS, OPS CHECKED GOOD.

Part: DOOR — DAMAGED (SERVICE) · airframe 36,087 hrs · 34,384 cycles

SERVICE DOOR WILL NOT OPEN FROM THE OUTSIDE. PLUNGER APPERATUS TO BE INOPERABLE AS WELL

Part: SKIN — PUNCTURED (RT SPOILER) · airframe 34,975 hrs · 33,379 cycles

RT WING OTBD GROUND SPOILER LOWER SURFACE PUNCTURED.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 34,975 hrs · 33,379 cycles

PASSENGER DOOR AFT DRAG ANGLE IS CRACKED.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 34,975 hrs · 33,379 cycles

C/W JOB CARD 4DMI19668, PERFORMED PERMANENT REPAIR OF RT ACMP OTBD INTERCOSTAL.

Part: SKIN — DAMAGED (TE FLAP) · airframe 34,975 hrs · 33,379 cycles

LEFT WING INBD FLAP LOWER SKIN HAS 2 LARGE AREAS WITH GOUGES PITTING AND DENTS FROM DEBRIS.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,675 hrs · 33,379 cycles

SERVICE DOOR LOWER SILL ANGLE IS CORRODED AT FS 325.

Part: SKIN — GOUGED (TE FLAP) · airframe 34,975 hrs · 33,379 cycles

RIGHT WING INBD FLAP LOWER SKIN HAS 2 LARGE AREAS WITH GOUGES, PITTING AND DENTS FROM DEBRIS.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,975 hrs · 33,379 cycles

PASSENGER DOOR OPENING LOWER SILL, LOWER ANGLE HAS CORROSION BETWEEN FS 310 AND FS 349.

Part: SKIN — CHAFED (LT AILERON) · airframe 34,975 hrs · 33,379 cycles

LEFT AILERON UPPER LEADING IS CHAFED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,975 hrs · 33,379 cycles

LEFT SIDEWALL SEAT TRACK STICK 7 HAS CORROSION BETWEEN FS 544 AND FS 559+80 IN CABIN.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 34,975 hrs · 33,379 cycles

PASSENGER DOOR LOWER CLOSEOUT PANEL AFT BRACKET IS CRACKED.

Part: RETAINER — CRACKED (PYLON) · airframe 34,975 hrs · 33,379 cycles

PYLON PANEL NR 421AL UPPER AND LOWER SEAL RETAINERS ARE CRACKED.

Part: WEB — CRACKED (PAX DOOR) · airframe 34,975 hrs · 33,379 cycles

PASSENGER ENTRY DOOR AFT WEB IS CRACKED UNDER AFT TENSION REGULATOR SUPPORT BEAM.

Part: WEB — CRACKED (PAX DOOR) · airframe 34,975 hrs · 33,379 cycles

PASSENGER DOOR FORWARD WEB CRACKED AT LOWER CORNER COMMON TO STEP 832 AT.

Part: FITTING — CRACKED (RT MLG WW) · airframe 34,975 hrs · 33,379 cycles

CLIP AT RBL 6, FS 202 INSIDE WHEEL WELL CRACKED, REPLACED.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 34,975 hrs · 33,379 cycles

INTERCOSTAL MEMBER BETWEEN FRAMES AT FS 654 AND 672 STR 4, FWD END LOWER RADIUS CRACKED, REPLACED.

Part: FITTING — CRACKED (LT MLG WW) · airframe 34,975 hrs · 33,379 cycles

CLIP AT LBL6, FS 202 INSIDE WHEEL WELL CRACKED, REPLACED.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,975 hrs · 33,379 cycles

RIGHT FLOOR SILL INTERCOSTAL BETWEEN FS 559 AND 559+16 CORRODED, REPAIRED

Part: ATTACH BRACKET — CRACKED (RT WING) · airframe 34,975 hrs · 33,379 cycles

RIGHT WING CENTER L/E INBD ATTACH BRACKET CRACKED, REPLACED.

Part: BRACKET — CRACKED (COCKPIT) · airframe 34,975 hrs · 33,379 cycles

LEFT CENTER WINDSHIELD LOWER POST BRACKET CRACKED, REPLACED.

Part: SUPPORT BRACKET — CRACKED (COCKPIT) · airframe 34,975 hrs · 33,379 cycles

RT CENTER WINDSHIELD POST LOWER SUPPORT BRACKET CRACKED, REPLACED.

Part: GUTTER — CRACKED (PAX DOOR) · airframe 34,975 hrs · 33,379 cycles

PASSENGER DOOR GUTTER FORWARD HALF IS CRACKED, REPLACED.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 34,975 hrs · 33,379 cycles

FS 280, FWD FLOORBOARD SUPPORT ANGLE CRACKED AT RBL 9.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,975 hrs · 33,379 cycles

FLOORBEAM FS 280 AFT ANGLE IS CORRODED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,975 hrs · 33,379 cycles

RIGHT AISLE SEAT TRACK STICK 1 HAS CORROSION BETWEEN FS 364 AND 394.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 34,975 hrs · 33,379 cycles

INTERCOSTAL ATTACHMENT CLIP CRACKED AT FS 484 AND LBL 27.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,975 hrs · 33,379 cycles

LEFT AISLE SEAT TRACK STICK NR 1 HAS CORROSION BETWEEN FS 364 AND FS 394.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,975 hrs · 33,379 cycles

RIGHT AISLE SEAT TRACK STICK 2 HAS CORROSION BETWEEN FS 394 AND 409+128.

Part: RIVET — BROKEN (FUSELAGE) · airframe 34,975 hrs · 33,379 cycles

ANGLE CAP AT THE OTBD SIDE OF RBL 9 AND AFT SIDE OF 280 FRAME CRACKED AND HAS A BROKEN RIVET, REPLACED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 34,975 hrs · 33,379 cycles

ANGLE CLIP ON THE INBD SIDE OF RBL 9 AND THE AFT SIDE OF THE 280 FRAME CRACKED, REPLACED

Part: BEAM — CRACKED (FUSELAGE) · airframe 34,975 hrs · 33,379 cycles

VERTICAL BEAM AT RBL 27, FS 409+128 IS CRACKED AT INBD LWR CORNER.

Part: BEAM — CRACKED (FUSELAGE) · airframe 34,975 hrs · 33,379 cycles

VERTICAL BEAM LBL 27, FS 409+128 IS CRACKED AT LBL LWR CORNER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,975 hrs · 33,379 cycles

FLOORBEAM 589 MIDDLE CAP BETWEEN LBL 9 AND RBL 9 CORRODED, REPLACED.

Part: COALESCER BAG — DIRTY (AC BAY) · airframe 34,755 hrs · 33,166 cycles

F/A REPORTS STRONG SMOKE ODOR IN CABIN. ODOR STARTED 2-3 MINS AFTER APU START, BLEEDS STILL ON ENGINES. PERFORMED PACK BURNOUT IAW AMM SUP 09-037A, NO SMOKE SMELLS NOTED IN CABIN OR COCKPIT. INSPECTED APU FOR FUEL & OIL LEAKS, NO LEAKS NOTED. R & R BOTH COALESCER SOCKS IAW SUP 09-037A.

Part: UNKNOWN — ODOR (CABIN) · airframe 34,755 hrs · 33,166 cycles

FA REPORTED STRONG SMOKE ODOR IN THE CABIN. ODOR STARTED 2-3 MINUTES AFTER APU START, BLEEDS STILL ON ENGINES.

Part: ROD — OUT OF ADJUST (SERVICE DOOR) · airframe 32,799 hrs · 31,302 cycles

SERVICE DOOR HARD TO CLOSE FROM OUTSIDE, TOP OF DOOR DOES NOT LINE UP, MUST BE PULLED FROM TOP HANDLE. CYCLED SERVICE DOOR, FOUND DOOR NEEDS TO BE ADJUSTED, GREEN WITNESS MARKS LINE UP WITH DOOR CLOSED IAW 260316 1 FOR MEL. ADJUSTED UPPER STABILIZER ROD IAW AMM 51-41-00, ALSO LUBED IAW AMM 12-20-52. OPERATIONS CHECKED GOOD. REMOVED PLACARD & REMOVED MEL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,179 hrs · 30,692 cycles

FLIGHT 3826, EMERGENCY EXIT ON WINDSCREEN ROW 1DF WILL NOT ILLUMINATE.

Part: VALVE — MALFUNCTIONED (NLG STEERING) · airframe 31,566 hrs · 30,096 cycles

DURING IN ROUTE CLIMB RECEIVED STEERING INOPERATIVE CAUTION. COMPLIED WITH QRH, MSG PERSISTS. R & R NWS EHSV. OPS CHECKED GOOD.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 31,539 hrs · 30,068 cycles

GEAR DISAGREE WARNING AFTER GEAR LEVER UP. RAN QRH, MSG CLEARED. RT MLG SHOWED UNSAFE. EXTENDED GEAR MANUALLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,331 hrs · 28,930 cycles

LAST FOUR SECTIONS OF EMER FLOOR LIGHTS INOPERATIVE.

Part: FITTING — DAMAGED (LT FLAP) · airframe 30,265 hrs · 28,839 cycles

LEFT OTBD FLAP CTR HINGE ARM FLAP LUG HAS TOOLING MARK ON LUG.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 30,235 hrs · 28,839 cycles

EXTERNAL AC POWER RECEPTACLE BRACKET CRACKED.

Part: BRACKET — CRACKED (LT EXHAUST)

LEFT EXHAUST FAIRING STANDOFF BRACKET IS CRACKED.

Part: STRUT — CHAFED (NLG) · airframe 30,235 hrs · 28,839 cycles

NLG STRUT ASSEMBLY CHAFED BY TORQUE LINK PROX SWITCH.

Part: DRAG ANGLE — CRACKED (RT MLG) · airframe 30,235 hrs · 28,839 cycles

RIGHT MLG DRAG ANGLE COMMON TO BATTERY RIB CRACKED.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,235 hrs · 28,839 cycles

RIGHT FLOOR SILL AT FS 319.00 IS CORRODED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,235 hrs · 28,839 cycles

RIGHT NR 3 SEAT TRACK HAS MULTIPLE GOUGES & CORRODED AT FS 409+128 TO FS 559.00.

Part: SEAL — CRACKED (RT SPOILER) · airframe 30,235 hrs · 28,839 cycles

RIGHT FLIGHT SPOILER INBD SPRING SEAL CRACKED.

Part: SKIN — DENTED (FUSELAGE) · airframe 30,235 hrs · 28,839 cycles

EXT SKIN DENTED AT FS 605 & LT STRINGER 19.

Part: RIB — CRACKED (LT WING) · airframe 30,235 hrs · 28,839 cycles

LEFT MLG BATTERY RIB CRACKED.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 30,235 hrs · 28,839 cycles

ELONGATED SCREW HOLE UNDER BELLY FAIRING.

Part: SKIN — DENTED (FUSELAGE) · airframe 30,235 hrs · 28,839 cycles

EXT SKIN HAS PROTRUDING DENT AT FS 672.20 & LT STRINGER 21.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 30,235 hrs · 28,839 cycles

CARGO BAY TRACK AT RBL 27 & FS 559.80 CORRODED.

Part: RETAINER — CRACKED (RT PYLON) · airframe 30,235 hrs · 28,839 cycles

SEAL RETAINER ON RT UPPER PYLON PANEL 422BT IS CRACKED.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 30,235 hrs · 28,839 cycles

CARGO BAY TRACK AT RBL 9 & FS 559.112 CORRODED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 30,235 hrs · 28,839 cycles

CLIPS AT LT STRINGER 3 & FS 280 ARE CRACKED.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 30,235 hrs · 28,839 cycles

CARGO BAY TRACK AT FS 559.80 & LBL 27 IS CORRODED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 30,235 hrs · 28,839 cycles

LEFT 484 CLIP CRACKED AT BL 36.00.

Part: BRACKET — CORRODED (CABIN) · corrosion level 2 · airframe 30,235 hrs · 28,839 cycles

PAX DOOR AFT HANDRAIL STOW CUP ON FLOOR CORRODED.

Part: DRAG ANGLE — CRACKED (LT WING) · airframe 30,235 hrs · 28,839 cycles

LEFT MLG WW BATTERY RIB DRAG ANGLE CRACKED.

Part: MOUNT BRACKET — CRACKED (NR 3 BRAKE) · airframe 30,235 hrs · 28,839 cycles

NUMBER 3 BRAKE ACCUMULATOR FWD MOUNT BRACKET CRACKED.

Part: SEAL — CRACKED (RT SPOILER) · airframe 30,235 hrs · 28,839 cycles

RIGHT WING FLIGHT SPOILER OTBD SPRING SEAL CRACKED.

Part: BALLAST — DEFECTIVE (CABIN) · airframe 29,757 hrs · 28,372 cycles

ACRID BURNING SMELL IN VICINITY OF ROW 10 & 11, UNABLE TO IDENTIFY SOURCE. ONLY OCCURRED ON GND DURING BOARDING. BOTH BALLAST ROW 10 RT SIDE DISCONNECTED. RAN APU WITH BOTH PACKS ON FOR 10 MINUTES & ALL CABIN LIGHTS ON, NO MORE BURNING SMELL. RT SIDE CTR AISLE & SIDEWALL LIGHT BALLASTS DISCONNECTED, ROW 10 & 11 FLUORESCENT LIGHTS INOPERATIVE, PLACARDED & PLACED ON MEL. MC IAW LP 267086 3 ACRID SMELL FROM ROWS 10 & 11 ON GND, DETERMINED 1 OF THESE 2 BALLASTS BAD.

Part: CARBON SEAL — BLOWN (LT ENGINE) · airframe 27,741 hrs · 26,402 cycles

SMOKE IN FLIGHT DECK FOLLOWED BY LEFT ENGINE OIL PRESSURE WARNING MESSAGE. COMPLIED WITH QRH. BROUGHT LT ENGINE TO IDLE FOR REMAINDER OF FLIGHT AFTER LANDING LT ENGINE WAS SHUTDOWN AND SMOKE CLEARED. R & R LT ENGINE NR 1 CARBON SEAL IAW 72-00-00. LEAK AND OPS CHECKED GOOD.

Part: DRAG BRACE — DAMAGED (NLG) · airframe 27,109 hrs · 25,801 cycles

AFTER TAKEOFF UPON SELECTION OF LANDING GEAR TO THE UP POSITION RECEIVED A GEAR DISAGREE WARN MSG WITH A NOSE GEAR INDICATION OF RED. RAN QRH AND PULLED MAIN GEAR EXTENSION HANDLE- NOSE INDICATION THEN TURNED GREEN AND SHOWED ALL 3 DOWN AND LOCKED. FOUND PSEU CODES DOWNLOCK 1 NEAR AND DOWNLOCK 2 FAR REPLACED NLG DRAG BRACE AND UPLOCK ASSY PER AMM 32-33-05 AND 32-21-05. NLG EXTENDS AND RETRACTS AND INDICATES NORMALLY RII-185.

Part: SENSING ELEMENT — FAULTY (LT ENGINE) · airframe 26,920 hrs · 25,625 cycles

LEFT 14TH DUCT WARNING MSG + AURAL AT 24,000 FT. C/W QRH, WARNING PERSISTED TO THE GROUND. DECLARED EMERGENCY, UNEVENTFUL LANDING. REMOVED AND REPLACED LEFT ENGINE PYLON SENSE ELEMENT (A58WK) IAW AMM: 36.21.04, OPS CHECKS GOOD.

Part: HINGE FITTING — GOUGED (R SPOILER) · airframe 25,544 hrs · 24,255 cycles

RIGHT FLIGHT SPOILER CENTER O/B HINGE FITTING IS GOUGED. REMOVED AND REPLACED RIGHT FLIGHT SPOILER O/B CENTER HINGE FITTING IAW CRJ SRM 51-42-21. P/N 601R10086-24PE

Part: ACTUATOR — CHAFED (TE FLAP VANE) · airframe 25,544 hrs · 24,255 cycles

RIGHT I/B FLAP VANE ACTUATOR TUBE ARE CHAFED FROM ROLLERS. REPAIRED DAMAGE IAW REO 601R-57-52-1962.

Part: ACTUATOR — CHAFED (TE FLAP VANE) · airframe 25,544 hrs · 24,255 cycles

LEFT I/B FLAP VANE ACTUATOR TUBES ARE CHAFED FROM ROLLERS. REPAIRED DAMAGE IAW REO 601R-57-52-1961.

Part: CAM — WORN (PAX DOOR) · airframe 25,544 hrs · 24,255 cycles

PAX DOOR FWD AND AFT LATCH CAMS HAVE WEAR MARKS. BLENDED OUT DAMAGE TO SMOOTH CONTOUR AND PASSIVATED LATCH CAMS IAW REO 601R-52-11-2699.

Part: DIAPHRAGM — DAMAGED (RT WING) · airframe 25,544 hrs · 24,255 cycles

TOOLING MARKS ON RIGHT O/B LEADING EDGE UPPER AND LOWER RADIUS OF THE DIAPHRAM ENTINRE LENGTH OF THE LEADING EDGE. REMOVED AND REPLACED SHROUD EDGING, INBOARD AND OUTBOARD UPPER, INBOARD LOWER.

Part: VANE — CHAFED (TE FLAP) · airframe 25,544 hrs · 24,255 cycles

RIGHT I/B FLAP VANE CHAFED ON LEADING EDGE WHERE VANE HITS STOPS. REMOVED AND REPLACED CTR VANE LEADING EDGE P/N 601R14303-52 IAW CRJ 51-40-11 AND 51-42-13, I/B AND O/B VANE LEADING EDGE BLENDED OUT DAMAGE AND FOUND TO BE WITHIN LIMITS IAW REO 601R-57-52-004 REV C.

Part: TRUNNION — DAMAGED (LT MLG) · airframe 25,544 hrs · 24,255 cycles

DURING INCORPORATION OF MLG TRUNNION LOWER FLANGE COLD WORKING, EO E10/016/457 FOUND 1 OVERSIZED HOLE ON LEFT SIDE AFT HOLE IN DOUBLER. REPAIRED 1 EA OVERSIZED HOLE ON LEFT LOWER MLG TRUNNION FLANGE IAW BOMBARDIER REO 601R-57-21-1742 REV- .

Part: SEPARATOR — DAMAGED (LT PYLON) · airframe 25,544 hrs · 24,255 cycles

LEFT ENGINE PYLON PANEL 412DB INNER SKIN SEPARATOR HAS WEAR DAMAGE. REMOVED DAMAGED SEPARATORS LOCATED AND DRILLED NEW SERVICEABLE SEPARATORS & RUB STRIP: P/N: 601R37138-27, 601R37138-25 & 601R37138-21) INSTALLED SEPARATORS AND RUB STRIPS TO PANEL 412DB IAW CRJ 200 CMM 20-40-11, 20-40-06, 20-42-13, 20-25-11.

Part: PANEL — DAMAGED (LT PYLON) · airframe 25,544 hrs · 24,255 cycles

PANEL 412BT PYLON PANEL LEADING EDGE INNER SIDE HAS GROOVES. PANEL 412BT LEFT PYLON FOUND TO BE OUT OF LIMITS, LOCATED, DRILLED & INSTALLED NEW SERVICEABLE PANEL. P/N 601-37003-159

Part: HOUSING — CRACKED (CARGO DOOR) · airframe 25,544 hrs · 24,255 cycles

CARGO BAY DOOR HANDLE HOUSING CRACKED. REMOVED AND REPLACED CARGO BAY DOOR HANDLE HOUSING WITH SERVICEABLE P/N H3415-31 IAW CRJ 200 SRM 51-42-21.

Part: STRUCTURE — CHAFED (FUSELAGE) · airframe 25,544 hrs · 24,255 cycles

RIGHT FUSELAGE CHAFED AT INTERSECTION OF RIGHT I/B TRAILING EDGE AND FUSELAGE. REPAIR AREA PER REO 601R-53-41-610.

Part: PANEL — DAMAGED (HORIZ STAB) · airframe 25,544 hrs · 24,255 cycles

PANEL 332AB HAS FINE DAMAGED SCREW HOLES. REPAIRED HOLES REO 601R-55-11-428.

Part: FITTING — CRACKED (FUSELAGE) · airframe 25,544 hrs · 24,255 cycles

CLIP ON FLOOR CROSS BEAM AT FS 589.00 IS CRACKED LOCATED UNDER CARGO DOOR CUTOUT LOWER SILL. REPLACED UNSERVICEABLE CLIP ANGLE WITH SERVICEABLE IAW CRJ 200 SRM 51-24-16.

Part: SKIN — CHAFED (RT MLG DOOR) · airframe 25,544 hrs · 24,255 cycles

CHAFE ON INNER SKIN OF RIGHT MLG DOOR. REMOVED AND REPLACED INNER SKIN ON RIGHT MLG DOOR IAW CRJ 200 SRM 51-24-16, 51-42-13, 51-40-11, 51-42-22.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 25,544 hrs · 24,255 cycles

BULKHEAD AT FS 169.0 IS CHAFED AT THE 3 O'CLOCK AND 9 O'CLOCK POSITION. BLENDED OUT CHAFES AT BULKHEAD 169.0 IAW BOMBARDIER REO 601R-53-11-2377 DATED 09/5/12, CRJ SRM 51-12-00, CRJ 200 TR 53-27.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,544 hrs · 24,255 cycles

SEAT TRACK IN CARGO COMPARTMENT LBL 9 & RBL 9 AT FS 559+88 ARE CORRODED. REMOVED CORRODED SEAT TRACKS FROM RBL 9 & LBL 9 AT FS 559+88 FABRICATED AND INSTALLED NEW SERVICEABLE SEAT TRACKS FROM P/N N126-2075 IAW CRJ 200 AMM 53-01-11.

Part: SKIN — CORRODED (RT SPOILER) · airframe 25,544 hrs · 24,255 cycles

SMALL FOUND ON RIGHT I/B GROUND SPOILER ON THE UPPER SURFACE. MEASURED FOUND TO BE WITHIN LIMITS & COMPLIED WITH THE STEPS OF REO 601R-57-71-355.

Part: STRUCTURE — DAMAGED (STABILIZER) · airframe 25,544 hrs · 24,255 cycles

STRUCTURE UNDER PANEL 332AB QTY 5 DAMAGED SCREW HOLES AND SCREW SHANKS. REPAIRED STRUCTURE UNDER PANEL 332AB IAW REO 601R-55-11-428.

Part: SKIN — CHAFED (LT MLG DOOR) · airframe 25,544 hrs · 24,255 cycles

LEFT MLG DOOR LEADING EDGE HAS CHAFING. CHAFING ON LEADING EDGE INNER SKIN FOUND TO BE .022 OUT OF LIMITS, ORIGINAL SKIN IS .051. REPAIR DONE IAW REO 601R-52-82-102.

Part: SUPPORT — CRACKED (RT WING) · airframe 25,544 hrs · 24,255 cycles

RIGHT WING PICCOLO TUBE SUPPORT FOR INBOARD AND CENTER TUBE JOINT IS CRACKED IN THE UPPER OUTBOARD CORNER. REMOVED AND REPLACED SUPPORT WITH SERVICEABLE PART IAW CRJ 200 SRM 57-41-12 AND 51-24-16.

Part: SKIN — GOUGED (LT MLG DOOR) · airframe 25,544 hrs · 24,255 cycles

LEFT MAIN LANDING GEAR DOOR IS GOUGED IN 3EA SPOTS ON INSIDE SKIN JUST AFT OF THE DATA PLATE. REMOVED AND REPLACED INNER SKIN & INSTALLED IAW CRJ 200 SRM 51-24-16 & 51-42-10.

Part: HINGE FITTING — GOUGED (TE FLAP) · airframe 25,544 hrs · 24,255 cycles

GOUGE ON RIGHT I/B FLAP, I/B HINGE ARM FWD SIDE. REPAIRED THE GOUGE ON RIGHT I/B FLAP HINGE ARM FWD SIDE IAW BOMBARDIER REO 601R-57-54-226.

Part: ANGLE — CRACKED (PAX DOOR) · airframe 25,544 hrs · 24,255 cycles

PAX DOOR POWER ASSIST MOTOR ANGLE HAS A CRACK. ALSO GOUGED AND HAS 2 BAD RIVET BUCKTAILS. (ANGLE CLOSEST TO THE CABLE DRUM). LOCATED FASTENER HOLES, AND INSTALLED SERVICEABLE ANGLE P/N 601R317745-7.

Part: SILL — CORRODED (FUSELAGE) · airframe 25,544 hrs · 24,255 cycles

PAX DOOR CUTOUT LOWER SILL HAS EXFOILIATED CORROSION IN MULTIPLE AREAS. CORROSION IS AT AND EXTENDING UNDER J1MB AND J2MB CONNECTOR MOUNT BLOCKS. ALSO PROX SWITCH AND AT AFT LOWER CORNER OF CUTOUT. REMOVED AND REPLACED PAX DOOR CUTOUT LOWER SILL IAW CRJ 200 SRM 51-42-06, 51-42-21 AND SRM TR#53-23.

Part: FITTING — CRACKED (CARGO BAY) · airframe 25,544 hrs · 24,255 cycles

CLIP IS CRACKED AT AFT CARGO DOOR TRACK. REMOVED & REPLACED CLIP AT FS 621, LBL 36, WL 114 NEAR CARGO DOOR AFT TRACK IAW CRJ 200 SRM 51-42-21.

Part: HEAT SHIELD — CHAFED (RT COWLING) · airframe 25,544 hrs · 24,255 cycles

RIGHT LOWER CORE COWL LEADING EDGE OF HEAT SHIELD IS CHAFED THROUGH SKIN. REPAIRED HEAT SHIELD IAW BOMBARDIER REO 601R-71-12-4130.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 25,544 hrs · 24,255 cycles

LOWER BRACKET CRACKED AT FS 574.00. REMOVE & REPLACE LOWER BRACKET AT FS 574.00 WITH SERVICEABLE P/N 601R35050-25 IAW CRJ 200 SRM 51-42-06.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 25,544 hrs · 24,255 cycles

FLOORBEAM AT FS 280 IS CRACKED IN UPPER CAP RADIUS AT LBL 12 AND RBL 12. REPAIR AREA IAW BOMBARDIER REO 601R-53-11-126 REV A.

Part: VANE — CHAFED (TE FLAP) · airframe 25,544 hrs · 24,255 cycles

RIGHT I/B FLAP VANE WORN AND CHAFED IN THREE PLACES ON THE LEADING EDGE. BLENDED O/B AND CENTER LEADING EDGE. REMOVED 0.008" FROM O/B LEADING EDGE. REMOVED 0.010" FROM CENTER LEADING EDGE. OUTBOARD AND CENTER LEADING EDGE ARE WITHIN ALLOWABLE DAMAGE LIMITS. REMOVED UNSERVICEABLE INBOARD LEADING EDGE INSTALLED SERVICEABLE INBOARD LEADING EDGE IAW REO 601R-53-52-004 REV C.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 25,544 hrs · 24,255 cycles

RIGHT AND LEFT OBLIQUE ANGLES ON AFT SIDE OF BULKHEAD FS 621 ARE CRACKED. REMOVED AND REPLACED RIGHT AND LEFT OBLIQUE ANGLES IAW REO 601R-53-61-100 AND 601R-53-61-422.

Part: FITTING — CRACKED (FUSELAGE) · airframe 25,544 hrs · 24,255 cycles

RIGHT FS 484.00 BL 27 CLIP IS CRACK. REMOVED UNSERVICEABLE CLIP AND REPLACED WITH SERVICEABLE CLIP IAW BOMBARDIER REO 601R-53-41-059.

Part: BULKHEAD — GOUGED (FUSELAGE) · airframe 25,544 hrs · 24,255 cycles

RIGHT AFT FS 280.00 BULKHEAD GOUGED ON PREVIOUS REPAIR. REMOVED & REPLACED PREVIOUS REPAIR ON RIGHT AFT FS 280 BULKHEAD IAW REO 601R-53-11-1727 REV E. 01/14/11 STARTING AT STEP 4.

Part: UNKNOWN — ODOR (CABIN) · airframe 22,922 hrs · 21,522 cycles

SMELLED LIKE BURNING RUBBER IN COCKPIT AND CABIN DURING DESCENT. VISUALLY INSPECTED BOTH PACKS, NO DEFECTS NOTED. OIL QTY GOOD IN BOTH PACKS. RAN SYS IN BOTH APU & ENG AIR NO ODOR OR DEFECTS NOTED AT THIS TIME. ACFT AWAC SUPP 09-037A.

Part: LIGHT — FAILED (CABIN) · airframe 22,254 hrs · 20,831 cycles

SIDEWALL LIGHT OVER SEAT 11F EXPLODED. R & R FLOURESCENT LIGHT OVER SEAT 11F IAW AMM 33-20-00. OPS CHECK GOOD. CLEANED UP BROKEN GLASS.

Part: ACTUATOR — INOPERATIVE (LT MLG) · airframe 21,648 hrs · 20,191 cycles

AFTER GEAR LEVER SELECTED UP GOT ANTI-SKID INBD CAUTION FOLLOWED BY GEAR DISAGREE MESSAGE LEFT MLG DOWN AND LOCKED. R & R LT SIDESTAY ACTUATOR.

Part: ANGLE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 21,349 hrs · 19,898 cycles

PAX DOOR LOWER ANGLE CLIPS CORRODED AT FS 320.10 AND B 338.00 (4 EA) R & K CLIPS IAW SRM 57-42-06.

Part: BRACKET — CRACKED (RT NACELLE) · airframe 21,349 hrs · 19,898 cycles

RT ENG NOSE COWL ALIGNMENT BRACKET IS CRACKED. R & R BRACKET IAW AMM 71-14-07.

Part: SKIN — CHAFED (RT MLG DOOR) · airframe 21,349 hrs · 19,898 cycles

RT MLG DOOR INNER SKIN IS CHAFED NEXT TO PLACARD. R & R RT MLG DOOR INNER SKIN IAW SRM 51-42-13, 51-40-11.

Part: BRACKET — CHAFED (TE FLAP) · airframe 21,349 hrs · 19,898 cycles

RT FLAP STUB FAIRING FWD BRACKET CHAFED AND BUTTPLATE BROKEN. REMOVED UNSERVICEABLE FAIRING (STUB RT) REC SERVICEABLE STUB FAIRING ( RT) FROM STOCK INSTALLED.

Part: SWITCH — CORRODED (PAX DOOR) · corrosion level 2 · airframe 21,349 hrs · 19,898 cycles

PAX DOOR TARGET SWITCH CORRODED. R & R WITH NEW TARGET PN 601R31902-349.

Part: PRESSURE BLKHD — CRACKED (BS 202.75) · airframe 21,349 hrs · 19,898 cycles

PRESSURE BULKHEAD CRACKED WHERE BRAKE CABLE PASSES THROUGH. REPAIRED FS202.75 BULKHEAD AT LBL 23.71, IAW REO 601R-53-11-2021, DATED 2010-11-30.

Part: ACCESS PANEL — CRACKED (LT PYLON) · airframe 21,349 hrs · 19,898 cycles

LT JETPIPE FAIRING CRACKED NEXT TO LOWER BOLT ACCESS PANEL CRACKED. REPAIRED LT JETPIPE FAIRING CRACK NEXT TO LOWER BOLT ACCESS PANEL BY CALLING OUT DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW CMM 78-11-50 REPAIR.

Part: SKIN — CHAFED (CARGO DOOR) · airframe 21,349 hrs · 19,898 cycles

CARGO DOOR EXTERIOR SKIN CHAFED AT TOP CENTER .760 LONG, .350 WIDE AND .032 DEEP. BLENDED DAMAGED AREA IAW REO 601R-52-30-023 REV NC, TREATED AREA IAW SRM 51-21-11, SRM 51-25-06 AND SRM 51-25-16.

Part: LATCH — BROKEN (BAGAGE DOOR) · airframe 21,349 hrs · 19,898 cycles

CARGO DOOR HOLD OPEN LATCH ON TOP OF FWD DOOR TRACK IS BROKEN OFF. REMOVED DAMAGED CARGO DOOR HOLD OPEN LATCH AND INSTALLED SERVICEABLE PN 600-35166-3 LATCH IAW AMM 52-31-00.

Part: SKIN — CHAFED (CARGO DOOR) · airframe 21,349 hrs · 19,898 cycles

CARGO DOOR EXTERIOR HANDLE CUTOUT CHAFED IN 3 PLACES BLENDED DAMAGED AREAS IAW REO 601R-52-31-086, REV NC, TREATED AREAS IAW SRM 51-21-11, SRM 51-25-06 AND SRM 51-25-16.

Part: FRAME — DAMAGED (BS 559) · airframe 21,349 hrs · 19,898 cycles

SCREW HOLE FOR CONNECTOR PLUG 1J6CE ON FS 559 HAS 2 DRILL STARTS. REPAIRED 2 EA DRILL STARTS NEX TO CONNECTOR PLUG 1J6CE AT FS559 BY BLENDING DAMAGE SMOOTH TO CONTOUR WITHOUT DEEPING DAMAGE IAW REO 601R-53-41-1316 AND SRM 51-12-00.

Part: BRACKET — BENT (PAX DOOR) · airframe 21,349 hrs · 19,898 cycles

BOTH PAX DOOR HANDRAIL SPRING CLIPS BRACKETS ARE BENT. REMOVED BOTH PAX DOOR HANDRAIL CLIPS AND INSTALLED SERVICEABLE PN 601R38587-17 (2 EA) CLIPS IAW SRM 51-42-06.

Part: RETAINER — CRACKED (LT PYLON SEAL) · airframe 21,349 hrs · 19,898 cycles

PANEL (412DB) HAS CRACK IN EDGE OF SEAL RETAINER 63 LONG. REMOVED SEAL RETAINER PN 601-37003-303 IAW SRM 51-23-00 AND SRM 51-42-06.

Part: SKIN — CHAFED (SERVICE DOOR) · airframe 21,349 hrs · 19,898 cycles

SERVICE DOOR OUTER HANDLE CUT-OUT IS CHAFED. REPAIRED 3 EA CHAFED AREAS ON SERVICE DOOR EXTERNAL HANDLE CUT OUT IAW REO 601R-52-41-157.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 21,349 hrs · 19,898 cycles

L/E OF FLAP FAIRING 697BB IS CHAFED. BLENDED AREA IAW SRM 51-12-00.

Part: SKIN — CHAFED (RT NACELLE) · airframe 21,349 hrs · 19,898 cycles

RT UPPER NOSE COWL AFT EDGE STRIP IS CHAFED. R & R RT UPPER NOSE COWL AFT EDGE STRIP IAW AMM 51-42-06.

Part: PLATE — CHAFED (RT PYLON) · airframe 21,349 hrs · 19,898 cycles

RT PYLON PANEL 422DB PLATES ON KNIFE EDGES. R & R (2 EA) PLATES IAW SRM 200-51-42-06.

Part: SKIN — CHAFED (RT WING AILERON) · airframe 21,349 hrs · 19,898 cycles

RT AILERON UPPER CTR L/E HAS CHAFE DAMAGE. REPAIRED RT AILERON UPPER CENTER L/E IAW REO 601R-57-60-013 REV NC.

Part: SKIN — GOUGED (RT WING TE FLAP) · airframe 21,349 hrs · 19,898 cycles

LT INBD FLAP L/E PANELS 584AB AND 584BB ARE GOUGED, BLENDED OUT GOUGES ON FLAP PANELS IAW SRM 51-21-00.

Part: HINGE — CHAFED (PAX DOOR) · airframe 21,349 hrs · 19,898 cycles

FUSELAGE HALF OF PAX DOOR PIANO HINGE IS CHAFED ON AFT END ON THE LAND OF THE HINGE. REPAIRED DAMAGED HINGE IAW REO 406R-53-21-814 TYPE IV REPAIR.

Part: PANEL — CHAFED (LT WING) · airframe 21,349 hrs · 19,898 cycles

LT WING PANEL 599BB HAS CHAFING DAMAGED ON LOWER SIDE. REPAIRED LT WING PANEL 599BB IAW REO 601R-57-60-013.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 21,349 hrs · 19,898 cycles

PAX DOOR STAIR STRUCTURE IS CRACKED NEXT TO FWD HANDRAIL 1 BRACKET CUT OUT CRACKED SECTION AND FABRICATED NEW SECTION IAW REO 601R-52-11-702, REV C, REPAIR Z.

Part: ANGLE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 21,349 hrs · 19,898 cycles

PAX DOOR LWR ANGLE CLIPS AT FS 320.10 AND FS338.00 CORRODED. REMOVED CORRODED CLIPS AND FABRICATED NEW SERVICEABLE CLIPS AND INSTALLED.

Part: SKIN — MISREPAIRED (PAX DOOR) · airframe 21,349 hrs · 19,898 cycles

PAX DOOR INNER SKIN AND SUB STRUCTURAL HAS 2EA MISLOCATED HOLES NEAR HINGE AT PAX DOOR FRAME STATION 320.10. CUT OUT DAMAGE AT FS320.00 AND PLUGGED HOLES ON INNER SKIN AND FRAME AT FS 320.163.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 21,349 hrs · 19,898 cycles

PAX DOOR AFT DRAG ANGLE CRACKED. REMOVED CRACKED SECTION OF AFT DRAG ANGLE, THE INSTALLED NEW SERVICEABLE SECTION IAW B/A REO 601R-52-11-513, REV A.

Part: ANCHOR FITTING — CORRODED (RT WINDSCREEN) · airframe 21,349 hrs · 19,898 cycles

RT WINDSCREEN ANCHOR FITTING IS CORRODED. R & R TR WINDSCREEN ANCHOR FITTING IAW AMM 20-21-07.

Part: SKIN — CHAFED (LT NACELLE) · airframe 21,349 hrs · 19,898 cycles

LT LOWER CORE COWL CHAFED FROM BLOCKER DOOR NEXT TO FWD LATCHES BLENDED DAMAGE IAW REO 601R-71-12-232, REV D AND WAS FOUND TO BE WITHIN ALLOWABLE LIMITS. DAMAGE MEASURES 4.00 LONG, 0.25 WIDE AND .007 DEEP. TREATED AREA IAW CMM 20-01-11 AND SRM 51-25-06.

Part: CARGO TRACK — CORRODED (BS 574-605) · airframe 21,349 hrs · 19,898 cycles

BAGGAGE COMPARTMENT TIE DOWNS NR2 AND NR3 ON LBL 27 AND NR1 AND NR2 ON LBL9 ARE CORRODED. R & R 2EA TIE DOWNS ON LBL 9.0 & 2 EA TIE-DOWNS ON LBL 27.0 IAW SRM 51-41-02.

Part: HINGE — DAMAGED (LT ELEVATOR) · airframe 21,349 hrs · 19,898 cycles

LT NR2 ELEVATOR HINGE ON BOTH ELEVATOR AND HORIZ STABILIZER HAVE MINOR TOOLING DAMAGE. B.ENDED OUT MINOR TOOLING DAMAGE IAW REO 601R-55-11-061, REO 601R-55-21-080.

Part: BULKHEAD — CHAFED (BS 280) · airframe 21,349 hrs · 19,898 cycles

AFT SIDE OF RT 280 BULKHEAD CHAFED FROM GALLEY ACCESS DOOR. CUT OUT DAMAGE FROM AFT RT SIDE 280 BULKHEAD, BLENDED CHAFED AREA ON CHANNEL IAW REO 601R-53-11-1727 FAB, WEB FILLER AND WEB DOUBLER PRIMED TOP COAT INSTALLED PART IAW REO 601R-11-1727, REV D.

Part: FRAME — CRACKED (BS 484) · airframe 21,349 hrs · 19,898 cycles

FRAME STA 484, LBL27 INBD CLIP IS CRACKED IN UPPER CORNER. REMOVED UNERVICEABLE CLIP, DUPLICATED AND INSTALLED SERVICEABLE CLIP IAW SRM 51-42-00, 51-42-21, 53-41-43.

Part: OVERHEAT LOOP — MALFUNCTIONED (ANTI ICE DUCT) · airframe 21,146 hrs · 19,685 cycles

GOT ANTI-ICE DUCT WARNING MESSAGE RT AFTER TAKEOFF. RAN QRH. ANTI-ICE SELECTED OFF AND SYNOPTIC PAGE SHOWED RT FUSELAGE RED. R & R BLEED LEAK DETECTOR LOOP A15WK IAW 36-21-04. OPS CK OF BLEED AIR LEAK DETECTION SYS GOOD AT THIS TIME.

Part: VANE — GOUGED (LT WING TE FLAP) · airframe 16,824 hrs · 15,828 cycles

LT WING INBD FLAP, VANE LEADING EDGE GOUGED AT 3 PLACES. 1ST GOUGE AT FLAP STA 57.00 WIDTH .500", LENGTH 1", DEPTH .030". 2ND GOUGE AT FLAP STA 105 WIDTH .500", LENGTH 1.00", DEPTH .007". 3RD GOUGE AT FLAP STA 141 WIDTH .500" LENGTH 1.00", DEPTH .010". LT WING INBD FLAP VANE L/E AT FLAP STA 57 FOUND OUT OF LIMIT IAW REO 601R-57-52-004 REV C AND REPLACED IAW SRM 51-42-13. FLAP VANE L/EDGE AT FLAP STA 105 AND 141. PERMANENT REPAIR PERFORMED IAW REO 601R-57-52-004 REV C.

Part: STOP — CRACKED (DOOR) · airframe 16,824 hrs · 15,328 cycles

BUTE DOOR HINGE PANEL 694KB STOP ASSY CRACKED. .550" L X .300 W X .090 D STOP ASSY ON BUTE DOOR HINGE PANEL 694KB R&R IAW CRJ200 SRM 51-42-06 AND 51-23-00.

Part: STRINGER — CORRODED (BS 333-349 S27) · airframe 16,824 hrs · 15,328 cycles

STRINGER 27 FOUND CORRODED BTW FS 333. TO FS 349. CORROSION ON STR 27 BTW FS 333 TO FS 349. REMOVED IAW SRM 51-12-00. EDDY CURRENT PERFORMED ON BLEND OUT AREA, NO CRACKS FOUND. SURFACE FINISH RESTORED.

Part: VISOR — CRACKED (HORIZONTAL STAB) · airframe 16,824 hrs · 15,328 cycles

VERTICAL STAB. LT UPPER VISOR CRACKED AND BENT. CRACK .250 LONG. VERTICAL STAB LT UPPER VISOR REPLACED IAW CRJ 200

Part: SKIN — GOUGED (RT WING TE FLAP) · airframe 16,824 hrs · 15,328 cycles

RT WING INBD FLAP VANE L/E SKIN AT STA 57.00 GOUGED OVER LIMITS IAW REO 601R-57-52-004. RT WING INBD FLAP VANE LEADING EDGE AT STA 57.00 REPLACED IAW SRM 51-42-13.

Part: STIFFENER — CRACKED (PAX DOOR) · airframe 16,824 hrs · 15,328 cycles

CRACK FOUND ON PAX DOOR MOTOR ASSIST STIFFENER AFT WEB. PAX DOOR MOTOR ASSIST STIFFENER AFT WEB REPLACED IAW SRM 51-42-06 AND 51-42-13.

Part: BRACKET — CRACKED (BS 280) · airframe 16,824 hrs · 15,828 cycles

CRACK FOUND ON BRACKET FS 280 RBL 9 INBD CRACK LENGTH IS .200. BRACKET AT FS 280 RBL 9 REMOVED IAW SRM 51-42-13 AND 51-42-21. NEW BRACKET AT FS RBL 9 INSTALL IAW 51-42-20.

Part: BULKHEAD — CRACKED (BS 280) · airframe 16,824 hrs · 15,328 cycles

CRACK FOUND ON PILOT BULKHEAD FS 280 RBL 9. CRACK LENGTH IS .500. PILOT BULKHEAD FS 280 RBL 9 REPAIRED IAW CRJ 200 REO 601R-53-11-171 REV D.

Part: BRACKET — CRACKED (BS 280) · airframe 16,824 hrs · 15,828 cycles

CRACK FOUND ON BRACKET FS 280 LBL 9 INBD CRACK LENGTH IS .250. BRACKET AT FS 280 LBL 9 REMOVED IAW SRM 51-54-13 AND 51-42-21. NEW BRACKET ST FS 280 LBL INSTALL IAW SRM 51-42-20.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 16,824 hrs · 15,328 cycles

CRACK FOUND ON INTERCOSTAL CLIP AT FS 484 RBL 27. CRACK LENGTH IS .400. INTERCOSTAL CLIP AT FS 484 RBL 27 R&R.

Part: LEVER — GOUGED (PAX DOOR) · airframe 16,824 hrs · 15,328 cycles

GOUGE FOUND ON PAX DOOR PULL IN LEVER, FWD UPPER PACK DOOR PULL IN LEVER REPLACED IAW AMM 20-21-00-910-801.

Part: SCUFF PLATE — CORRODED (FUSELAGE) · airframe 16,824 hrs · 15,328 cycles

SERVICE DOOR LOWER SCUFF PLATE FOUND CORRODED, 3 PLACES APPROX .500 X .500, .026 DEEP. CORROSION REMOVED IAW SRM 51-21-26 AND FOUND OUT OF LIMITS IAW SRM 53-00-00. LOWER SERVICE DOOR SCUFF PLATE REPLACED IAW SRM 51-41-02.

Part: REGULATOR — OUT OF RIG (AILERON) · airframe 15,636 hrs · 14,187 cycles

AIRCRAFT REQUIRES 50% LT AILERON TRIM FOR LEVER FLIGHT, THE YOKE HAS LT TO RT SLOP FEEL ON FINAL APPROACH. THE YOKE HAD TO BE MOVED APPROXIMATELY 2-3 INCHES BEFORE RESPONSE. (A) RIGGED LT AND RT AILERON TENSION REGULATORS & RIGGED LT AND RT AILERON OUTBOARD PCU`S IAW AMM CHP 27-11. OPS & RIG CK GOOD AT THIS TIME. RII YES 1-42. (A)

Part: AILERON — RATCHETING

NOTICEABLE HANGUP/LATCH IN AILERON ROLL CONTROL ON BOTH YOKES NEAR NEUTRAL POSITION, NOTICED IN FLIGHT, 6000-7000 FT WHILE HAND FLYING. (M)

Part: CHANNEL — CRACKED (RT MLG WW)

RIGHT MLG WHEEL WELL HYDRAULIC TRANSDUCER HAT CHANNEL P/N 601R75262-157 CRACKED APPROX .2 INCH LONG. MAINTENANCE REPAIRED IAW BSC EO 601R-53-0044E BY REMOVING DAMAGED BRACKET FABRICATING NEW BRACKET AND INSTALLING. (M)

Part: CHANNEL — CRACKED (LT MLG WW)

LEFT MLG WHEEL WELL HYDRAULIC TRANSDUCER HAT CHANNEL P/N 601R75262-159 CRACKED APPROX .2 INCHE LONG. MAINTENANCE REMOVED AND REPLACED CHANNEL IAW BSC SR 601R-53-0044E. (M)

Part: SHUTOFF VALVE — MALFUNCTIONED (LT, RT PRESS REG) · airframe 11,781 hrs · 10,471 cycles

ON TAKEOFF ROLL CAUTION MESSAGE FOR LT AND RT HIGH PACK PRESSURE, ABORT TAKEOFF. C/W QRH. RAN UP 2ND TIME AND BOTH HI PRESS CAUTION MESSAGE AGAIN. REMOVED AND REPLACED BOTH PRSOV VALVES IAW AMM, OPS CHECK GOOD. REMOVED PN 32156222, RT SN 1319 (TT 9618 HRS) AND LT SN 957 (TT - 11764 HRS) (K)

Part: STRINGER — DAMAGED (BS 409 S7L)

PIT DAMAGE ON STRINGER NR 7L OF FS 409 DAMAGE IS .011 DEEP LOCATED .250 BELOW RIVET ROW. MAINTENANCE REPAIRED DAMAGE IAW SRM 53-00-31, 51-12-00 AND EO 601R-53-9798. (M)

Part: SELECTOR VALVE — INOPERATIVE (NLG) · airframe 8,658 hrs · 7,502 cycles

ON APPROACH, WHEN SELECTED GEAR DOWN GOR (GEAR DISAGREE AND NOSE DOOR) MASTER WARNING. NLG INDICATED UP AND LOCKED MLG DOWN. CYCLED GEAR WITH SAME INDICATIONS. PERFORMED QRH AND OBTAINED 3 GREEN. REMOVED AND REPLACED NLG SELECTOR VALVE AMM. OPS CHECK GOOD. LEAK CHECK GOOD. (K)

Part: LINE — CHAFED (HYDRAULIC SYS) · airframe 7,707 hrs · 6,654 cycles

HYDRAULIC NR 1 LOW PRESSURE MESSAGE INFLIGHT ON CLIMBOUT. QUANTITY INDICATES ZERO. REMOVED AND REPLACED HYDRAULIC SUPPLY LINE TO CASE DRAIN ASSY REF 29-11-02, RAN ENGINE LEAK CHECK. OPS CHECK GOOD. (K)

Part: FASTENER — MISLOCATED (WING) · airframe 7,269 hrs · 6,334 cycles

UNABLE TO ACHIEVE EDGE DISTANCE ON JOINT STRAP (PN 601R1004654) WHILE COMPLYING WITH SB 601R57037 DUE TO EXISTING FASTENER BEING MISLOCATED. PERFORMED A MAJOR ALTERATION TOO, BY SHIFTING THE CUTLINE TO PROVIDE MINIMUM EDGE DISTANCE ON THE EXISTING FASTENERS, FABED NEW DOUBLE IAW EO. (K)

Part: SKIN — DENTED (RUDDER) · airframe 7,269 hrs · 6,334 cycles

SKIN IS DENTED ON THE LT SIDE SKIN PANEL BETWEEN RS 108.25 AND 113.98 THE DENT MEASURES 2.2 INCHES LONG X 2 INCHES WIDE. PERFORMED A MAJOR REPAIR TO THE RUDDER SKIN ON LT SIDE BY TRIMMING OUT DAMAGE, LPI, FABED DOUBLER AND INSTALLED IAW EO. (K)

Part: ANGLE — CRACKED (FUSELAGE)

FOUND RT FS 621 ANGLE IS CRACKED. REPAIRED RT FS 621 ANGLE IAW BOMBARDIER REO 601-53-61-117 REV A. (M)

Part: ANGLE — CRACKED (FUSELAGE)

FOUND LEFT FS 621 ANGLE IS CRACKED. REPAIRED LEFT FS 621 ANGLE IAW BRAS EO 601R-53-61-117. (M)

Part: ANGLE — CRACKED (FUSELAGE) · airframe 7,369 hrs · 6,334 cycles

LT FS 621.00 ANGLE IS CRACKED. CUT AWAY DAMAGED SECTION OF ANGLE AND INSTALLED A REPAIR ANGLE IAW REO. (K)

Part: ANGLE — CRACKED (PAX DOOR)

PAX DOOR AFT DRAG ANGLE IS CRACKED 2 INCHES LONG JUST FORWARD OF DOOR ASSIST PULLEY MOUNT. REPAIRED ANGLE BY INSTALLING SPLICE ANGLE P/N 601R31772-5 AND IAW BOMBARDIER, INC REO 601R-52-11-513. (M)

Part: ANGLE — CRACKED (FUSELAGE)

LEFT FS 484 ANGLE AT LBL 36 IS CRACKED. REPAIRED LEFT FS 484 ANGLE IAW BRAS REO 601R-53-41-059. (M)

Part: ANGLE — CRACKED (FUSELAGE)

FOUND RT FS 484 ANGLE AT RBL 27 IS CRACKED. REPAIRED RT FS 484 ANGLE IAW BRAS EO 601R-53-41-059. (M)

Part: ANGLE — CRACKED (FUSELAGE)

RT FS 484 ANGLE AT RBL 36 IS CRACKED. REPAIRED RT FS 484 ANGLE IAW BRAS EO 601R-53-41-059. (M)

Part: SKIN — CORRODED (WING) · corrosion level 1 · airframe 7,369 hrs · 6,334 cycles

MWC 170 CORROSION EXISTS ON LOWER WING PLANK UNDER FUEL PANEL 510AB. PERFORMED A MAJOR REPAIR BY REMOVING CORROSION IAW REO. (K)

Part: SKIN — CORRODED (RT WING) · airframe 7,369 hrs · 6,334 cycles

FOUND CORROSION ON RT LOWER WING PLANK UNDER THE FOLLOWING FUEL PANELS 640BB AND 650GB. PERFORMED A MAJOR REPAIR BY REMOVING CORROSION IAW REO. (K)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

FOUND CABIN FLOOR SUPPORT STRUCTURE AT FS 280, RBL 9 BOTH CLIPS ARE CRACKED IN RADIUS AT TOP. REPAIRED CABIN FLOOR SUPPORT STRUCTURE AT FS 280 RBL 9 IAW BRAS EO 601R-53-5924. (M)

Part: BUSHING — MIGRATED (RT MLG TRUNNION) · airframe 7,369 hrs · 6,334 cycles

RT MLG AFT TRUNNION BUSHING IS MIGRATED .046 INCH. REMOVED MIGRATED BUSHING AND INSTALLED 2ND OVERSIZED BUSHING MODIFIED TO A 1ST OVERSIZED IAW EO.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 7,539 hrs · 6,334 cycles

CABIN FLOOR SUPPORT STRUCTURE AT FS280, LBL 9.0. THE OB CLIP IS CRACKED IN RADIUS AT TOP. (K) REMOVED CRACKED CLIP AND INSTALLED NEW FABRICATED CLIP IAW BRAS EO 601R-53-5924. (M)

Part: BUSHING — MIGRATED (LT MLG)

LT MAIN LANDING GEAR AFT TRUNNION BUSHING IS MIGRATED .007 INCH. REMOVED MIGRATED BUSHING AND INSTALLED A 2ND OVERSIZED BUSHING MODIFIED TO A 1ST OVERSIZED BUSHING IAW BOMBARDIER EO 601R-57-21-003 REV B AND EO 601R-57-5907A. (M)

Part: SILL — CRACKED (FUSELAGE)

FOUND CARGO DOOR SILL PLATE AT FS 589 CRACKED. REPAIRED CARGO DOOR SILL PLATE IAW BOMBARDIER REO 601R-53-61-433. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

RT SIDE FS621 THROUGH FS623.3 INTERCOSTAL AT STR 14R IS CRACKED IN RADIUS APPROXIMATELY 1.1 INCH LONG. REMOVED AND REPLACED FS 621-625.3 INTERCOSTAL ANGLE AT STRINGER 14R IAW BRAS EO 601R-53-5933. (M) (K)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 7,369 hrs · 6,334 cycles

LT SIDE FS621 THROUGH FS 625.3 INTERCOSTAL AT STR 14L IS CRACKED IN RADIUS APPROXIMATELY 1.0 INCH LONG. (K) REMOVED AND REPLACED FS 621-625.3 INTERCOSTAL ANGLE AT STRINGER 14L IAW BRAS EO 601R-53-5933. (M)

Part: BPSU — OUT OF RIG (RT AND LT) · airframe 7,065 hrs · 6,074 cycles

FLAPS FAIL AT 20 DEGREES. 49700 LBS. LANDING WEIGHT LIGHT BREAKING. 5 MAX BTMS READING, LIGHT TOUCHDOWN. FOUND LT AND RT BRAKE POSITION SENSOR UNITS (BPSU) BOTH OUT OF RIG. RIGGED LT AND RT BPSU`S REF AMM, FLAPS OPS GOOD.

Part: TUBE — FAILED (HYD SYSTEM)

NR 2 HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED, FLUID INDICATES ZERO. REMOVED AND REPLACED HYDRAULIC TUBE ASSEMBLY. (M)

Part: STRIKER — DAMAGED (FUSELAGE)

PASSENGER DOOR SEAL STRIKER IS DAMAGED AT FS 349 MIDWAY TOP TO BOTTOM. REPAIRED DAMAGE TO PASSENGER DOOR SEAL STRIKER FS 349 IAW BOMBARDIER REO 601R-52-11-008 REV B. (M)

Part: STRIKER — DAMAGED (PAX DOOR SEAL)

PASSENGER DOOR SEAL STRIKER AT FS 310 IS DAMAGED MIDWAY TOP TO BOTTOM. REPAIRED DAMAGED PASSENGER DOOR SEAL STRIKER AT FS 310 IAW BOMBARDIER REO 601R-52-11-008 REV B. (M)

Part: STRIKER — DAMAGED (DOOR SEAL)

PASSENGER DOOR SEAL STRIKER AT FS 310 IS DAMAGED MIDWAY TOP TO BOTTOM. REPAIRED DAMAGED PASSENGER DOOR SEAL STRIKER AT FS 310 IAW BOMBARDIER REO 601R-52-11-008 REV B. (M)

Part: IDG — UNDERSERVICED (RT GENERATOR)

RT IDG CAUTION FOLLOWED BY RT GEN OFF LINE ON TAKEOFF SERVICED IDG. OPS CHECK GOOD. (M)