N431SW

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 39,568 hrs · 34,415 cycles

PAX DOOR INTERCOSTAL D3 FS347.25 CORRODED. (C-CHECK) RO: 08/29/2019 REMOVED AND INSTALLED NEW INTERCOSTAL IAW SRM. LEAK CHECK GOOD.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 39,568 hrs · 34,415 cycles

PAX DOOR INTERCOSTAL D1A FS327.763 CORRODED. REMOVED AND INSTALLED NEW INTERCOSTAL IAW SRM. LEAK CHECK GOOD.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 39,568 hrs · 34,415 cycles

PAX DOOR INTERCOSTAL D3 FS327.763 CORRODED. REMOVED AND INSTALLED NEW INTERCOSTAL IAW SRM. LEAK CHECK GOOD.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 39,568 hrs · 34,415 cycles

PAX DOOR INTERCOSTAL D5 AT F.S 347.25 WAS FOUND TO BE CORRODED. (C-CHECK) RO: 08/29/2019 REMOVED AND INSTALLED NEW INTERCOSTAL IAW SRM. LEAK CHECK GOOD.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 39,568 hrs · 34,415 cycles

PAX DOOR INTERCOSTAL D3 FS311.75 CORRODED. REMOVED AND REPLACED INTERCOSTAL IAW SRM. LEAK CHECK GOOD.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 39,568 hrs · 34,415 cycles

PAX DOOR INTERCOSTAL D4 FS347.25 CORRODED. (C-CHECK) RO: 08/29/2019 REMOVED AND REPLACED INTERCOSTAL IAW SRM. LEAK CHECK GOOD.

Part: FLOORBEAM — CORRODED (BS 559) · airframe 39,568 hrs · 34,415 cycles

CORROSION ON STRAP COMMON TO RIGHT-HAND PRESSURE FLOOR SILL AT FS 559.00 RBL 27 TO RBL 43. REMOVED AND INSTALLED NEW STRAP IAW SRM. LEAK CHECK GOOD.

Part: CROSSBEAM — CORRODED (BS 559) · airframe 39,568 hrs · 34,415 cycles

CORROSION ON CROSS BEAM PLATE COMMON TO L/H SILL AT FS 559.00 LBL 27 TO LBL 43.(C-CHECK) RO: 08/29/2019 REMOVED AND INSTALLED NEW STRAP IAW SRM. LEAK CHECK GOOD.

Part: FRAME — CORRODED (BS 605) · airframe 39,568 hrs · 34,415 cycles

CORROSION ON FRAME AT FS 605.0 IN THE AREA OF RBL 26 TO LBL 26. REMOVED AND INSTALLED NEW FRAME IAW SRM. LEAK CHECK GOOD.

Part: FRAME — CORRODED (BS 589) · airframe 39,568 hrs · 34,415 cycles

CORROSION ON FRAME AT FS 589.0 IN THE AREA OF RBL 26 TO LBL 26. REMOVED AND INSTALLED NEW FRAME IAW SRM. LEAK CHECK GOOD.

Part: DOOR SILL — CORRODED (BS 349) · airframe 39,568 hrs · 34,415 cycles

PASS DOOR SILL CORRODED AT FS 349.0. REMOVED AND INSTALLED NEW PART IAW SRM. LEAK CHECK GOOD.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 39,568 hrs · 34,415 cycles

PAX DOOR INTERCOSTOL BY VENT DOOR CORRODED FROM APPROX FS 320. TO FS 330. REMOVED AND INSTALLED NEW INTERCOSTAL IAW SRM. LEAK CHECK GOOD.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 39,568 hrs · 34,415 cycles

PASS DOOR INTERCOSTAL CORRODED FROM APPROX FS 300. TO FS 348.0. REMOVED AND INSTALLED NEW INTERCOSTAL IAW SRM. LEAK CHECK GOOD.

Part: FASTENER — CORRODED (HORIZ STAB) · airframe 40,665 hrs · 35,573 cycles

HORIZONTAL STAB STEADY FITTING HARDWARE AND FITTING TO MOUNT CORRODED. REMOVED ONE AT A TIME, 4EA SIDE TO SIDE STEADY FITTING MOUNTING BOLTS. PN: NAS 6204-(10). 2-EA NAS 6204-(11) 2-EA REF: RIL. REPLACED ONE AT A TIME, 4EA SIDE TO SIDE STEADY FITTING MOUNTING BOLTS. REF: RIL. THIS SDR FOR T/STEADY FITTING IS BEING SUBMITTED AS A PART OF VDR_2020NM064006.

Part: ACM — CONTAMINATED · airframe 38,980 hrs · 33,754 cycles

THICK SMOKE COMING OUT OF VENTS IN COCKPIT AND CABIN. RETURNED TO FIELD. LANDED WITHOUT INCIDENT. (FLT#4298) CLOSED RAN BOTH PACKS ON APU AND AS WELL AS BOTH ENGINES FOR AN EXTENDED PERIOD AT FLIGHT POWER IAW AMM. RAN ENGINES WITH DIFFERENT POWER SETTINGS, COLD, HOT AND WARM. SMOKED FOR ABOUT 5-10 MINUTES THEN WENT AWAY AND NEVER CAME BACK. NO SMOKE SMELL OF ANYTHING AFTER POWER RUN AS WELL. SMOKE WAS DUE TO GLYCOL (DE-ICE) FLUID RESIDUE.

Part: CONTROL LEVER — FAILED (MLG) · airframe 36,635 hrs · 31,181 cycles

LANDING GEAR DISAGREE MESSAGE DISPLAYED. RETURNED TO THE FIELD. REPLACED THE LANDING GEAR CONTROL LEVER IAW AMM. OPS CHECKED GOOD.

Part: SELECTOR VALVE — FAILED (MLG) · airframe 32,932 hrs · 27,152 cycles

GEAR DISAGREE BOTH MAIN GEAR WOULD NOT EXTEND UNTIL PULLED EMERGENCY EXTENSION. R & R MLG SELECTOR VALVE AND NR 3 HYDRAULIC RESERVOIR IAW AMM.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 30,920 hrs · 25,174 cycles

CARGO SMOKE WARNING MESSAGE CAME ON TWICE IN FLIGHT. MX REPLACED BOTH SMOKE DETECTOR.

Part: UNKNOWN — ODOR (A/C PACK) · airframe 30,834 hrs · 25,080 cycles

BURNING ODOR FROM PACKS AFTER TAKEOFF. ODOR WENT AWAY AFTER 3-5 MINUTES. RETURNED TO DEPARTURE. RAN PACKS FOR 3 TO 4 HOURS, COULD NOT DUPLICATE BURNING ODOR. INSPECTED ACM'S FOR OIL QUANTITY. OIL LEVEL'S GOOD. INSPECTED PACKS IAW AMM.

Part: BRACKET — FAILED (NLG) · airframe 30,099 hrs · 24,330 cycles

GEAR DISAGREE INDICATION WITH NOSE GEAR IN DOWN POSITION & NOSE DOOR OPEN WARNING MESSAGE. REPLACED NLG CENTERING PROXIMITY SENSOR BRACKET. PERFORM EXTENSION AND RETRACTION OF NLG. ALL OPS CHECKED GOOD AT THIS TIME IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 30,052 hrs · 24,287 cycles

NR 4 EXTERNAL EMERGENCY LIGHT IS BURNED OUT. SERVICE RELAMPED.

Part: BRACKET — BENT (NLG) · airframe 30,022 hrs · 24,255 cycles

GEAR DISAGREE WARNING MESSAGE AFTER TAKEOFF. NOSE GEAR DOWN WITH GEAR LEVER IN UP POSITION. FLT 4538 REPLACED NLG OLEO SENSOR BRACKET & RIGGED THE SENSOR IAW AMM.

Part: BUSHING — DAMAGED (RT ENGINE MOUNT) · airframe 29,386 hrs · 23,645 cycles

RT ENGINE YOKE LINK HAS PITTED BUSHINGS. C-CHECK REPLACED RT ENGINE YOKE LINK IN IAW AMM.

Part: POST — CRACKED (FUSELAGE) · airframe 29,386 hrs · 23,645 cycles

FOUND FS 409.0 + 128 VERTICAL POST LBL 18.0 INBD & OTBD SIDES HAVE INDICATIONS APPROXIMATELY 2 INCHES IN LENGTH 50% FSH AT AFT FLANGE RADIUS. REPLACED INBD & OTBD VERTICAL POSTS AT FS 409.0 + 128 LBL 18.0 IAW SRM & REO.

Part: FRAME — CORRODED (FUSELAGE) · airframe 29,370 hrs · 23,633 cycles

FUSELAGE FRAME AT FS 364.00 IS CORRODED ON FWD SIDE OF FRAME BETWEEN STRINGER 25L & STRINGER 26R. C-CHECK REPLACED FS 364.00 LOWER FRAME SECTOR BETWEEN STRINGER 25L & 26R IAW SRM.

Part: SILL — CORRODED (FUSELAGE) · airframe 29,370 hrs · 23,633 cycles

CARGO DOOR FLOOR SILL HAS MULTIPLE AREAS OF CORROSION AROUND NUTPLATE HOLES. DAMAGE BETWEEN FS 559.00+112 & FS 621.00. C-CHECK REPLACED CARGO DOOR FLOOR SILL IAW REO.

Part: FRAME — CORRODED (FUSELAGE) · airframe 29,370 hrs · 23,633 cycles

FS FRAME AT FS 319.70 IS CORRODED BETWEEN STRINGER 25L & 27 ON THE FWD SIDE OF FRAME. C-CHECK REPLACED FS 319.70 FROM STRINGER 23R & STRINGER 23L IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 29,370 hrs · 23,633 cycles

FUSELAGE FRAME AT FS 333.00 IS CORRODED BETWEEN STRINGER 25L & 26R ON FWD & AFT SIDE OF FRAME. C-CHECK REPLACED FS 333.00 LOWER FRAME SECTOR FROM STRINGER 23L TO STRINGER 23R IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 29,370 hrs · 23,633 cycles

FS FRAME AT FS 349.00 IS CORRODED BETWEEN STRINGER 25L & 25R ON AFT SIDE OF FRAME. C-CHECK REPLACED FS 349.00 LOWER FRAME SECTOR IAW SRM.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 29,617 hrs · 23,863 cycles

FUSELAGE FRAME AT FS 349.00 IS CORRODED AT RT OTBD EDGE AT SERVICE DOOR CUTOUT. C-CHECK REPAIRED IAW SRM.

Part: RUDDER — DENTED (TAIL) · airframe 29,370 hrs · 23,633 cycles

SMALL DENT ON RT RUDDER BETWEEN RS 78.82 & RS 85.07. C-CHECK REPAIRED SMALL DENT ON RT RUDDER BETWEEN RS 78.82 & RS 85.07 IAW REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 29,617 hrs · 23,863 cycles

INDICATION NOTED AT REAR PRESSURE BULKHEAD WEB AT RBL 18.0 WL 34.0 APPROXIMATELY 1.0 INCHES IN LENGTH. C-CHECK REPAIRED IAW SRM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 27,424 hrs · 21,725 cycles

EMERGENCY LIGHT INOPERATIVE ON EXIT SIGN BY GALLEY SERVICE DOOR. (FLT 4547) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,385 hrs · 21,683 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 7859) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,192 hrs · 21,476 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 7811) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,120 hrs · 21,403 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4532) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,638 hrs · 20,955 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 26,602 hrs · 20,923 cycles

NR 1 MAIN CABIN DOOR EXTERIOR EMERGENCY EXIT LIGHT IS OUT. (FLT 4763) RELAMPED EMERGENCY LIGHT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 26,480 hrs · 20,817 cycles

FLT 4538, NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,455 hrs · 20,791 cycles

FORWARD OVERHEAD EMERGENCY AND AFT OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 4510) RELAMPED EMERGENCY LIGHTS.

Part: FAIRING — DAMAGED (HORIZ STAB) · airframe 26,384 hrs · 20,721 cycles

LEFT HORIZONTAL STAB TIP FAIRING HAS 2 BURNT NUT PLATES ON UPPER FLANGE BL 112.00. (SERVICE) REPAIRED LIGHTNING STRIKE DAMAGE TO LEFT HORIZONTAL STAB UPPER FLANGE BL 112.00 IAW BOMBARDIER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,297 hrs · 20,635 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4539) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,259 hrs · 20,605 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4522) RELAMPED EMERGENCY LIGHT.

Part: ACTUATOR — FAILED (LANDING GEAR) · airframe 26,199 hrs · 20,555 cycles

FLT 4761, DURING GEAR RETRACTION, RECEIVED AN ANTI-SKID OUTBOARD CAUTION MESSAGE AND GEAR DISAGREE WARNING MESSAGE. REPLACED THE RIGHT SIDESTAY AND ACTUATOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,006 hrs · 20,381 cycles

NR 1 OVERHEAD EMERGENCY EXIT LIGHT IS OUT. (FLT 4825) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,954 hrs · 20,327 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4622) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,924 hrs · 20,301 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4734) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,727 hrs · 20,096 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4694) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,727 hrs · 20,096 cycles

LEFT NR 2 EXTERIOR EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: SKIN — CHAFED (RT WING) · airframe 26,791 hrs · 21,087 cycles

RIGHT WING UPPER LEADING EDGE HAS CHAFING. (C-CHECK) REPAIR PER SRM.

Part: VANE CAP — CHAFED (TE FLAP) · airframe 26,791 hrs · 21,087 cycles

LEFT INBOARD FLAP INBOARD VANE CAP CHAFED. (C-CHECK) REPAIRED PER REO.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 26,791 hrs · 21,087 cycles

CRACK IN PRESSURE FLOOR SKIN AT FS 460 BETWEEN BL 0.0 AND RIGHT BL 9.0. (C-CHECK) REPAIRED PER SRM AND REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 26,791 hrs · 21,087 cycles

CRACK ON FS 621 BULKHEAD WEB FORWARD FACE ABOVE UPPER CARGO DOOR TRACK FITTING. (C-CHECK) REPAIRED IN REFERENCE TO REO.

Part: FRAME — CORRODED (FUSELAGE) · airframe 26,791 hrs · 21,087 cycles

LOWER FRAME FORWARD OF MAIN AVIONICS BAY DOOR AT FS 333.00 HAS CORROSION ON AND AROUND GROUND TERMINAL. (C-CHECK) REPAIRED PER REO.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 26,791 hrs · 21,087 cycles

LEFT SIDE FS 559.0 PRESSURE BULKHEAD IS DAMAGED. (C-CHECK) REPAIRED PER CRJ200 SRM AND REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,598 hrs · 19,976 cycles

NR 2 AND 3 EXTERIOR EMERGENCY LIGHTS ARE OUT. (FLT 4483) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,524 hrs · 19,910 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4718) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,458 hrs · 19,849 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4593) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,344 hrs · 19,740 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4453) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,312 hrs · 19,710 cycles

RIGHT SIDE FORWARD AND AFT EXTERIOR EMERGENCY LIGHTS ARE OUT. (FLT 4709) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,312 hrs · 19,710 cycles

AFT CEILING EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,193 hrs · 19,608 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4646) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,193 hrs · 19,608 cycles

AFT CEILING EMERGENCY LIGHT BURNED OUT. (FLT 4637) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,032 hrs · 19,468 cycles

GALLEY SERVICE DOOR EXTERIOR EMERGENCY LIGHT IS OUT. (FLT 4458) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,988 hrs · 19,432 cycles

NR 3 CEILING EMERGENCY LIGHT IS OUT. (FLT 4683) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,440 hrs · 18,952 cycles

AFT OVERHEAD EMERGENCY LIGHT OUT. (FLT 4728) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 24,186 hrs · 18,741 cycles

RIGHT FORWARD EXTERIOR EMERGENCY LIGHT IS OUT. (FLT 4876) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,541 hrs · 18,203 cycles

AFT EMERGENCY LIGHT IS BURNED OUT. (FLT 4739) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,968 hrs · 16,843 cycles

NR 3 EMERGENCY CEILING LIGHT INOP. (FLT 4784) RELAMPED EMERGENCY LIGHT.

Part: WIRE — BROKEN (CABIN) · airframe 21,859 hrs · 16,757 cycles

ENTRY FLOOR EMERGENCY FLOOD LIGHT INOP. (FLT 4461) REPAIRED BROKEN WIRE.

Part: CONNECTOR — LOOSE (CABIN) · airframe 21,859 hrs · 16,757 cycles

EMERGENCY EXIT SIGN MID CABIN INOP. (FLT 4461) RESEATED LOOSE CONNECTOR.

Part: BATTERY PACK — MALFUNCTIONED (CABIN) · airframe 21,475 hrs · 16,445 cycles

EMERGENCY EXIT SIGN AT ROW 8 INOP. (FLT 4540)RESET NR 3 EMERGENCY LIGHT BATTERY PACK.

Part: FITTING — GOUGED (FUSELAGE) · airframe 21,305 hrs · 16,306 cycles

RIGHT 9G BULKHEAD LAVATORY FITTING GOUGED. (C CHECK) REPAIR PER REO IN PROGRESS.

Part: FITTING — CRACKED (FUSELAGE) · airframe 21,305 hrs · 16,306 cycles

FS 621 BULKHEAD LINTEL FITTING CRACKED. (C CHECK) REPAIRED PER REO.

Part: MOUNT BOLT — OUT OF TOLERANCE (RT ENGINE) · airframe 21,951 hrs · 16,831 cycles

RIGHT ENGINE MOUNT BOLT AND THRUST MOUNT OUT OF TOLERANCE. (C CHECK) REPLACED PER AMM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,951 hrs · 16,831 cycles

BULKHEAD WEB AT FS 559 CRACKED. (C CHECK) REPAIRED PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,951 hrs · 16,831 cycles

FS 621 BULKHEAD CRACKED AT LINTEL FITTING INTERFACE. (C CHECK) REPAIRED PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,300 hrs · 16,302 cycles

NR 1 EMERGENCY OVERHEAD LIGHT INOP. (FLT 4625) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — MISSING (CABIN) · airframe 21,300 hrs · 16,302 cycles

EMERGENCY EXIT SIGN OVER SERVICE DOOR MISSING. (FLT 4532) INSTALLED NEW EIXT SIGN LENS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,187 hrs · 16,206 cycles

SECOND TO LAST EMERGENCY CEILING LIGHT INOP. (FLT 4581) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,119 hrs · 16,151 cycles

FORWARD OVERHEAD EMERGENCY LIGHT INOP. (FLT 4950) RELAMPED EMERGENCY LIGHT.

Part: PIN — CORRODED (LT ENGINE) · airframe 21,072 hrs · 16,112 cycles

BOTH FORWARD MOUNT PINS AND YOKE BEARINGS FOR LEFT ENGINE HAVE PITTING CORROSION. (SVC CHECK) REPLACED PINS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,903 hrs · 15,984 cycles

CEILING EMERGENCY EXIT FLOODLIGHT INOP. (FLT 4515) RELAMPED EMERGENCY LIGHT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 20,755 hrs · 15,872 cycles

FLT 4480, AFT CEILING EMERGENCY LIGHT INOP. RELAMPED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 20,163 hrs · 15,427 cycles

FLT 4855 - FORWARD EMERGENCY CEILING FLOOD LIGHT INOP, RELAMPED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 19,579 hrs · 15,008 cycles

FLT 4902 - SERVICE DOOR EMERGENCY LIGHT INOP. RELAMPED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 19,291 hrs · 14,791 cycles

FLT 4757 - FORWARD EMERGENCY LIGHT INOP. RELAMPED.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 17,735 hrs · 13,585 cycles

CRACK FOUND AT STA280 AND LBL9.0 UPPER ANGLE, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER REO 601R-53-11-136 -1.

Part: LIGHT — BROKEN (CABIN) · airframe 17,735 hrs · 13,585 cycles

CABIN EMERGENCY TRACK LIGHTING IS BROKEN, FOUND AT C-CHECK. REPLACED EMERGENCY LIGHTING UPPER TRACK PER CRJ200 AMM 33-51-01-020-001 AND 33-51-01-420-001.

Part: MOUNT — CORRODED (LT ENGINE) · airframe 17,735 hrs · 13,585 cycles

LEFT ENGINE THRUST SHAFT BALL FITTING IS CORRODED, FOUND AT C-CHECK. REPLACED LEFT THRUST SHAFT FITTING PER CRJ200 AMM 71-22-01-000-801.

Part: MOUNT — CORRODED (RT ENGINE) · airframe 17,735 hrs · 13,585 cycles

RIGHT ENGINE MOUNT THRUST SHAFT BALL FITTING IS CORRODED, FOUND AT C-CHECK. REPLACED RIGHT ENGINE THRUST SHAFT PER CRJ200 AMM 71-22-01-000-801.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 17,735 hrs · 13,585 cycles

CRACK FOUND AT STA 280 AND RBL9.0 LOWER BEAM, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER REO 601R-53-11-171.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 17,735 hrs · 13,585 cycles

CRACK FOUND AT STA 280 AND LBL9.0 LOWER BEAM, FOUND AT C-CHECK. COMPLIED WITH REPAIRS PER REO 601R-53-11-171.

Part: FLEX DRIVE — CORRODED (NR 1 ACTUATOR) · airframe 16,172 hrs · 12,376 cycles

RIGHT WING NR 1 ACTUATOR NEEDS TO BE REPLACED BECAUSE OF CORROSION AT FLEX SHAFT DRIVE POINT. REPLACED NR 1 FLAP ACTUATOR IAW MM 27-53-00.

Part: FLEX DRIVE — CORRODED (TE FLAP) · airframe 16,172 hrs · 12,376 cycles

RIGHT INBOARD FLEX DRIVE SHAFT IS CORRODED AT NR 1 ACTUATOR. REPLACED RIGHT INBOARD FLEX CABLE AS REQUIRED, PN: 601R93106-107, SN OFF: 5676.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 13,399 hrs · 10,336 cycles

DURING CRUISE YD2 DISCONNECTED WITH ASSOCIATED AP DISCONNECT RE-ENGAGED. YD2 AND AP WOULD NOT ENGAGE ON EITHER SIDE. FO AND FA REPORTED A BURNING SMELL ON FLIGHTDECK. CYCLED A/C POWER YD2 MESSAGE CLEARED. RAN BOTH ENGINES AND CYCLED PACKS AND BLEEDS BUT COULD NOT DUPLICATE SMELL IN COCKPIT.

Part: UNKNOWN — UNKNOWN (SPOILERS) · airframe 12,152 hrs · 9,395 cycles

ON DESCENT ENCOUNTERED UNCOMMANDED ROLL 10 DEG TO LEFT WHEN FLIGHT SPOILERS WERE DEPLOYED. VISUALLY INSPECTED LT AND RT FLIGHT SPOILERS, NO FAULTS FOUND. MEASURED FLIGHT SPOILER TRAVEL AND BOTH FLIGHT SPOILERS WITHIN PARAMETERS PER MM 27-64-00.

Part: PCU — MALFUNCTIONED (FLT SPOILERS) · airframe 11,910 hrs · 9,202 cycles

SPOILERONS FAULT AFTER LANDING IN SLC. REPLACED OB SPOILERON NR 3 HYD PCU IAW CRJ MM 27-62-01, OPERATIONAL CHECK GOOD.

Part: WIRE — DAMAGED (ELEVATOR TRIM) · airframe 11,597 hrs · 8,961 cycles

FO TRIM SWITCH (ELEVATOR) INOP. REPAIRED WIRING AT FO'S TRIM SWITCH. OPERATIONAL CHECK GOOD.

Part: CONTROL CABLE — OUT OF RIG (AILERONS) · airframe 11,333 hrs · 8,759 cycles

AILERONS HAVE A CATCH/CLICK FEEL AFTER NEAR NEUTRAL POSITION WHEN YOKE IS TURNED LEFT AND RIGHT. CHECKED CABLE CIRCUITS. RERIGGED RIGHT AILERON FUSELAGE WING CABLES AND RETENSIONED SAME CABLES IAW 27-11-00.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 10,700 hrs · 8,279 cycles

FIVE MINS AFTER T/O REC'D SMOKE CARGO MSG. MSG WENT OUT AFTER 3 SECONDS. REPLACED NR 1 AND NR 2 CARGO SMOKE DETECTORS PER CRJ MM 26-15-01. OPERATIONAL CHECK GOOD. P/N 473597-19, S/N OFF 1747, S/N OFF 1746.

Part: SHUTOFF VALVE — MALFUNCTIONED (CABIN AIR) · airframe 10,700 hrs · 8,279 cycles

EN ROUTE TO MRY RECEIVED CARGO FAN FAIL AND CARGO SOV FAIL STATUS THEN CARGO SMOKE WARNING. REPLACED CARGO RECIRCULATED AIR SHUT OFF VALVE IAW AMM 21-55-07. REPLACED CARGO FAN AND EXHAUST SOV IAW 21-55-01. P/N VP0615E00, S/N 1888, P/N VP0615E00, S/N OFF J92345, P/N AE0607F00, S/N OFF L0250.

Part: ACTUATOR — MALFUNCTIONED (HORIZONTAL STAB) · airframe 10,675 hrs · 8,257 cycles

STAB TRIM CHANNEL ONE INOP MESSAGE ON DESCENT. REPLACED HORIZONTAL STAB TRIM ACTUATOR AND MOTOR CONTROL UNIT MM 27-42-01 AND 27-42-05, OPERATIONAL CHECK GOOD, PN 7062-3, SN OFF 1212.

Part: CABLE — MALFUNCTIONED (HORIZONTAL STAB) · airframe 10,644 hrs · 8,233 cycles

STAB 2 INOP. REPLACED HSTCA AND MCU IAW MM 27-40-00, 27-42-01, 27-42-05. OPERATIONAL CHECK GOOD, PN 7062-3, SN/OFF 329.

Part: PEDAL — BLOCKED (RUDDER) · airframe 10,530 hrs · 8,142 cycles

RUDDER ON LANDING JAMMED ON RIGHT SIDE 1/4 TRAVEL ONLY. FOUND CAMLOCK ON RT SIDE OF CENTER CONSOLE OUT AND INHIBITING RUDDER PEDAL DEFLECTION. SECURED CAMLOCK AND RAN RUDDER PEDALS IN BOTH DIRECTIONS AT FULL DEFLECTION WITH NO DEFECTS NOTED.

Part: TRIM SWITCH — STICKS (STAB) · airframe 10,281 hrs · 7,939 cycles

F/O TRIM STICKS IN DOWN POSITION. REPLACED F/O TRIM SWITCH IAW CRJ MM27-41-05. OPERATIONAL CHECK GOOD IAW CRJ MM27-40-00-710-801.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILERS) · airframe 10,008 hrs · 7,726 cycles

ON TAXI OUT THE LEFT SPOILERON RAN AWAY TO THE FULL UP POSITION. REPLACED NR 1 AND NR 2 SECU'S IAW MM 27-61-04. OPERATIONAL CHECK GOOD. P/N 49-164-06, S/N OFF 1052.

Part: ANGLE — CRACKED (AP BULKHEAD) · airframe 8,584 hrs · 6,616 cycles

FS 625 OBLIQUE ANGLE IS CRACKED APPROX .65 INCH LONG ON RT SIDE OF AFT PRESSURE BULKHEAD AT STR 14R. (ITEM FOUND AT C-CHECK INSPECTION.) INSTALLED ANGLE PN 601R-35-012-52 IAW CRJ 200 SRM 51-42-06.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 8,584 hrs · 6,616 cycles

INTERCOSTAL AD FS 484.0 RBL 36 CRACKED. (ITEM FOUND AT C-CHECK INSPECTION.) COMPLIED WITH MFG REO 601R-53-41-059. REPAIR TO INTERCOSTALS FS 484 BL 27-00-36-00.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 8,584 hrs · 6,616 cycles

FS 280.00 ANGLES AT RBL9/LBL9 IB AND OB ARE CRACKED. (ITEM FOUND AT C-CHECK INSPECTION.) INSTALLED NEW ANGLES AT RBL9/LBL9 AT FS 280.00 IAW CRJ SRM 51-42-13, 51-42-21, 51-22-00.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 8,584 hrs · 6,616 cycles

INTERCOSTAL AT FS 484 LBL 36 CRACKED. (ITEM FOUND AT C-CHECK INSPECTION.) COMPLIED WITH MFG REO 601R-53-41-059 REPAIR TO INTERCOSTALS FS 484 DL 27-00-36-00.

Part: ANGLE — CRACKED (AP BULKHEAD) · airframe 8,584 hrs · 6,616 cycles

FS 625 OBLIQUE ANGLE IS CRACKED ON LT SIDE OF AFT PRESSURE BULKHEAD, APPROX .65 INCH LONG. (ITEM FOUND AT C-CHECK INSPECTION.) INSTALLED ANGLE PN 601R-35012-51 IAW CRJ 200 SRM 51-42-06.

Part: INTERCOSTAL — CRACKED (FUSLEAGE) · airframe 8,584 hrs · 6,616 cycles

INTERCOSTAL FLOATING ANGLE AT FS 484 RBL 27 OB CRACKED. (ITEM FOUND AT C-CHECK INSPECTION.) INSTALLED NEW ANGLE IAW REO 601R-53-41-059.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 8,584 hrs · 6,616 cycles

RT AFT FLOORBOARD ATTACHMENT ANGLE CRACKED AT RIGHT OUTBOARD AT EDGE OF FRAME 621.0. (ITEM FOUND AT C-CHECK INSPECTION.) INSTALLED ALL REPAIR PARTS IAW REO NR 601R-53-61-117.

Part: LIGHT — INOPERATIVE (ROW 12) · airframe 7,534 hrs · 5,794 cycles

AFT EMERGENCY LIGHT OVERHEAD IS INOP. REMOVED AND REPLACED EMERGENCY LIGHT AT ROW 12 AS REQUIRED. OPS CHECK GOOD.

Part: SCREW — LOOSE (TERMINAL BLOCK) · airframe 7,429 hrs · 5,709 cycles

LEFT WINDSHIELD SMELLED LIKE SULFUR, PUFF OF SMOKE JUST BEFORE CIRCUIT BREAKER POPPED. FOUND LOOSE SCREW ON LEFT WINDSHIELD HEAT TERMINAL BLOCK (P1). REPLACED WIRE CONNECTOR AND HARDWARE. OPS CHECK GOOD.

Part: COMPUTER — MALFUNCTIONED (AUTOPILOT) · airframe 6,638 hrs · 5,111 cycles

EN ROUTE TO SLC AUTOPILOT FAILED FOLLOWED BY YD1, FD1, TERRAIN FAIL STATUS MSGS. LEFT SIDE WITNESS LIGHT ON FCP DO NOT ILLUMINATE. REPLACED NR 1 FCC CARD. AUTOPILOT OPS CHECK GOOD IAW 22-10-00.

Part: CONTROL UNIT — MALFUNCTIONED (STAB TRIM) · airframe 6,409 hrs · 4,940 cycles

AT 800 FT AFTER TAKEOFF, BOTH STAB TRIM CHANELS DISENGAGED (AND MACH TRIM), FOLLOWED QRH PROCEDURE, COULD NOT CLEAR MSGS. RETURNED TO DFW. PERFORM SYSTEM CHECK ON HSTCU. SYSTEM CHECK OF HSTCU, PERFORMED NORMALLY. OPERATED STAB TRIM & MACH TRIM. BOTH SYSTEMS CHECK GOOD IAW CL 600 MM 27-40-00. COULD NOT DUPLICATE SQUAWK.

Part: ACTUATOR — FAILED (SPOILER) · airframe 5,631 hrs · 4,345 cycles

RIGHT SPOILERONS FAULT STATUS MESSAGE THAT WOULD NOT CLEAR. INSTALLED SERVICEABLE PCU ACTUATOR ON RIGHT SPOILERON, INBOARD POSITION. OPS CHECK GOOD IAW 27-60-00.

Part: TIRE — SEPARATED (RT MLG) · airframe 5,361 hrs · 4,131 cycles

RIGHT INBOARD FLAP DAMAGED FROM THE NR 3 MLG TIRE TREAD CAME APART. REMOVED AND REPLACED RIGHT INBOARD FLAP WITH SERVICEABLE FLAP IAW CRJ MM 27-54-01. REMOVED AND REPLACED NR 3 WHEEL ASSY IAW CRJ MM 32-41-01. TIRE PRESSURE GOOD. S/N OFF: 4004.

Part: PCU — MALFUNCTIONED (LT SPOILER) · airframe 5,292 hrs · 4,078 cycles

FLIGHT SPOILERS FAULT MESSAGE. INSTALLED SERVICEABLE INBOARD AND OUTBOARD FLIGHT SPOILER PCU'S ON LEFT FLIGHT SPOILER IAW CRJ MM 27-62-01. OPS AND LEAK CHECKS GOOD. OB - PN OFF/ON 27000-7 SN OFF 5147. IB-PN OFF/ON 27000-7 SN OFF 3313.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 5,058 hrs · 3,889 cycles

1ST OVERHEAD EMERGENCY LIGHT IN CABIN INOP. REMOVED AND REPLACED THE LAMP. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 4,424 hrs · 3,413 cycles

FORWARD OVERHEAD EMERGENCY EXIT SIGN AT ROW 8 DOES NOT ILLUMINATE AND RIGHT OVERWING FORWARD EXTERIOR EMERGENCY LIGHT DOES NOT ILLUMINATE. REMOVED AND REPLACED TB105-3 (P/N 600-59211-1). PERFORMED OPS CHECK OF EMERGENCY LIGHTS. OPS CHECK GOOD.

Part: RIVET — CHAFED (THROTTLE ROD) · airframe 3,978 hrs · 3,073 cycles

A RIVET ON THE NR 2 ENGINE PUSH-PULL ROD FROM THE THROTTLE GEARBOX TO THE MFC WAS FOUND TO BE RUBBING ON A SCREW ON THE FACE OF THE GEARBOX WHEN THROTTLE MOVED INTO OR OUT OF FUEL SHUTOFF POSITION. RIVET BUCKED TO PROPER DIMENSIONS AND SCREW TIGHTENED. GAP FOUND TO BE AT LEAST .125 INCH AND OPS CHECK GOOD.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 4,094 hrs · 3,167 cycles

FS 621 FLOOR SUPPORT ANGLE LBL 41 FOUND CRACKED DURING C-CHECK INSPECTION. REPAIRED DAMAGE IAW CRJ REO 601R-53-61-117 REV-A. ANGLE P/N: 601R53-61-117-1. REPAIR ANGLE P/N: 601R53-61-117-3.

Part: ACTUATOR — FAILED (HORIZ STAB) · airframe 3,236 hrs · 2,513 cycles

STAB TRIM CHANNEL NR 2 WILL NOT ENGAGE. REMOVED AND REPLACED HORIZONTAL STAB TRIM ACTUATOR AND MOTOR CONTROL UNIT IAW MM 27-42-01 AND 27-42-05. OPS CHECK GOOD.

Part: TRIM SWITCH — INOPERATIVE (COCKPIT) · airframe 3,194 hrs · 2,480 cycles

AILERON SWITCH INOP. REMOVED AND REPLACED AILERON TRIM SWITCH. OPERATED AILERON TRIM. OPS CHECK GOOD.

Part: ANTI-SKID SYS — MALFUNCTIONED (MLG) · airframe 2,662 hrs · 2,075 cycles

UPON LANDING GEAR EXTENSION AT SBA RECEIVED ANTI-SKID INBOARD AND OUTBOARD EICAS MESSAGES. FOLLOWED QRH PROCEDURE. FOUND THAT AVAILABLE LANDING DISTANCE WAS VERY NEAR BOOK LIMIT WITH BOTH ANTI-SKID INOP. DIVERTED TO LAX. PULLED AND RESET BOTH ANTI-SKID CB'S. TURNED ON HYDRAULICS, SET ANTI-SKID TO ARM AND OPERATED SYSTEM SEVERAL TIMES. NO MESSAGES. OPS CHECKED GOOD.

Part: CONTROL CABLE — BINDING (ELEVATOR) · airframe 1,085 hrs · 865 cycles

CAPTAIN'S ELEVATOR CONTROL BINDING AND DIFFICULT TO MOVE FORWARD AND AFT. REMOVED AND REPLACED ELEVATOR CAPTAIN AND SERVO MOTOR IAW 27-32-00, 22-11-143. REMOVED AND REPLACED THREE CONTROL CABLES IAW 27-32-00. OPS CHECK GOOD. P/N: 622-5027-101, S/N OFF: 4AXR, P/N: 822-0260-001, S/N OFF: D18H, P/N: 601R90020-79, 601R90020-81, 601R90020-83.