N8932C

Part: PLATE — CRACKED (AFT CARGO) · airframe 31,805 hrs · 30,237 cycles

AFT CARGO STEP PLATE IS DAMAGED. REMOVED AND REPLACED WITH NEW AFT CARGO STEP PLATE IAW AMM 53-60-55.

Part: RIB — CRACKED (LWS 53.6) · airframe 31,805 hrs · 30,237 cycles

LH MLG BATT. RIB IS CRACKED W.S.53.60. REPAIRED CRACKED REFERENCING REO 601R-57-046B.

Part: HANDLE — CRACKED (PAX DOOR HANDLE) · airframe 31,805 hrs · 30,237 cycles

PAX. DOOR OUTER HANDLE IS CRACKED. J/C 52-830-300. PAX DOOR OUTER HANDLE REMOVED AND REPLACED IAW CRJ200 AMM 52-11-03.

Part: RIB — CORRODED (RWS 48.6) · airframe 31,805 hrs · 30,237 cycles

EXTENSIVE CORROSION ON RH WING BATT RIB WEB W.S 48.60. REPAIRED R/H BATT RIB @ WS 48.60 IAW EA # CRJ257-11783.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 31,805 hrs · 30,237 cycles

DENT ON L/H I/B FLAP UPPER SKIN @ W.S. 139. REPAIRED L/H I/B FLAP UPPER SKIN IAW REO#601R-57-52-058

Part: FLANGE — CRACKED (APU BAY) · airframe 31,805 hrs · 30,237 cycles

APU ENCLOSURE IS CRACKED ON UPPER AFT LH DOOR FLANGE. REPAIRED DAMAGE ON UPPER AFT L/H APU ENCLOSURE DOOR FLANGE IAW BOMBA REO 601R-49-11-071 REV NC DATED 11-22-2004. "

Part: HOUSING — CRACKED (PROXIMITY SENSOR) · airframe 31,805 hrs · 30,237 cycles

SERVICE DOOR PROX. SENSOR HOUSING IS CRACKED. J/C 52-840-503. ADJUSTED PROXIMITY SWITCH ON THE HANDLE MECHANISM TO (1.27MM) AND OPPS CHECK IAW AMM CRJ200-52-70-06-820-001. REMOVED & REPLACED SERVICE DOOR PROX. SENSOR HOUSIG IAW CRJ 200 AMM 52-41-00.

Part: HOUSING — CRACKED (GROUND POWER) · airframe 31,805 hrs · 30,237 cycles

GROUND POWER RECEPTACLE HOUSING CRACKED ON INSIDE. J/C 53-12-301. REMOVED & REPLACED GROUND POWER RECEPTACLE HOUSING, P/N 600-33283-33 IAW BOMB. REO#601R-53-11-569.

Part: RETAINER — CRACKED (PAX DOOR) · airframe 31,805 hrs · 30,237 cycles

PAX DOOR LOWER SEAL RETAINER IS CRACKED. REPAIRED PAX DOOR LOWER SEAL RETAINER IAW REO601R-52-11-915.

Part: SUPPORT — CRACKED (E/E BAY) · airframe 31,805 hrs · 30,237 cycles

AFT EQUIP. BAY DOOR CUTOUT LH SIDE SUPPORT STRUCTURE IS CRACKED. REMOVED AND REPLACED AFT EQUIPTMENT BAY DOOR CUTOUT L/H SIDE SUPPORT STRUCTURE IAW CRJ200 SRM 51-42-06.

Part: FRAME — CORRODED (BS 589) · airframe 31,204 hrs · 29,543 cycles

FRAME 589 IS CORRODED ON BOTH SIDES BETWEEN STR25R AND STR25L (C-CHECK) RO 12/27/2019 REPAIRED FRAME AT FS 589 COMMON TO STRINGERS 25R AND 25 L IAW BOMBARDIER REO.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 31,204 hrs · 29,543 cycles

LH IB FLAP VANE IS CHAFED AT ALL 3 LEADING EDGE CONTACT POINTS (C-CHECK) RO 12/27/2019 REMOVED AND REPLACED LH IB FLAP REF CAMP # 20077637 FOR REPLACEMENT.

Part: FRAME — CORRODED (BS 605) · airframe 31,204 hrs · 29,543 cycles

FRAME 605 IS CORRODED ON BOTH SIDES OF FRAME BETWEEN STR26R AND STR26L (C-CHECK) RO 12/27/2019 REPAIRED FRAME AT FS 605 IAW BOMBARDIER REO.

Part: FRAME — CORRODED (BS 574) · airframe 31,204 hrs · 29,543 cycles

FRAME 574IS CORRODED ON BOTH SIDES BETWEEN STR26L AND STR25R (C-CHECK) RO 12/27/2019 PERFORMED A MAJOR REPAIR TO FRAME 574 BETWEEN STR26L AND STR25R IAW REO. COMPLETED SKYWEST TASK CARD. FORM M-377 IS ATTACHED.

Part: BULKHEAD — CRACKED (BS 621) · airframe 31,204 hrs · 29,543 cycles

CRACK ON 621 BULKHEAD LOWER I/B CORNER OF LINTEL FITTING 0.350" 100%FSH. (C-CHECK) RO 12/27/2019 REPAIRED CRACK ON FS621 BULKHEAD COMMON TO INBD CORNER OF LINTEL FITTING IAW BOMBARDIER REO.

Part: ATTACH ANGLE — CRACKED (BS 409) · airframe 31,204 hrs · 29,543 cycles

FS409+128 BL0 L/H VERT POST HAS A CRACK INDICATION NOTED IN THE AFT FLANGE RADIUS AT WL69 .275 LONG BY 50%FSH. FAILED NDT (C-CHECK) RO 12/27/2019 PERFORMED A MAJOR REPAIR TO FS409+128 BL0 LH VERTICAL POSTS AND ATTACH ANGLES IAW BOMBARDIER REO AND CRJ200 SRM TASKS. COMPLETED SKYWEST TASK CARD.

Part: POST — CRACKED (BS 409) · airframe 31,204 hrs · 29,543 cycles

FS409+128 RBL18 I/B VERT POST HAS A CRACK INDICATION NOTED IN THE AFT FLANGE RADIUS AT WL69 .325 LONG BY 70%FSH. FAILED NDT (C-CHECK) RO 12/27/2019 PERFORMED A MAJOR REPAIR TO FS 409+128 RBL 18 I/B VERTICAL POST IAW BOMBARDIER REO. COMPLETED SKYWEST TASK CARD. FORM M-337 IS ATTACHED.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 31,204 hrs · 29,543 cycles

3EA AREAS OF CRACK INDICATIONS NOTED ON FS621 RPB WEB, 2EA IN THE HEEL LINE AREA OF VERT POSTS, 1ST AT BL0 WL108.5-WL111.5 50%FSH, 2ND AT LBL36 WL78.75-WL79.25 50%FSH, AND 3RD AT LOWER I/B CORNER OF LINTEL FITTING 0.350€? 100%FSH. MARKED ON A/C. ALL 3EA AREAS OF INDICATIONS NOTED FAILED NDT (C-CHECK) RO 12/27/2019 COMPLIED WITH 3EA AREAS OF CRACK INDICATIONS NOTED ON FS621 RPB WEB, 2EA IN THE HEEL LINE AREA OF VERT POSTS, 1ST AT BL0 WL108.5-WL111.5 50%FSH, 2ND AT LBL36 WL78.75-WL79.25 50%FSH, AND 3RD AT LOWER I/B CORNER OF LINTEL FITTING 0.350€? 100%FSH IAW REO.

Part: BULKHEAD WEB — CHAFED (BS 621) · airframe 31,204 hrs · 29,543 cycles

FS621 RPB WEB SMALL CHAFES FROM CONTACT WITH SCREWS AT WL103 IN 7EA AREAS AT RBL18, RBL27, RBL36, LBL7, LBL9, LBL18, AND LBL27 (C-CHECK) RO 12/27/2019 REPAIRED FS621 RPB WEB SMALL CHAFES FROM CONTACT WITH SCREWS AT WL103 IN 7EA AREAS AT RBL18, RBL27, RBL36, LBL7, LBL9, LBL18, AND LBL27 IAW GREO FORM 337 ATTACHED.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 30,594 hrs · 28,827 cycles

RIGHT MAIN LANDING GEAR DIDN€™T INDICATE DOWN TWENTY SECONDS AFTER SELECTING DOWN. GEAR DISAGREE. (FLT#3952) CLOSED DEFERRED LANDING GEAR RETRACTION SYSTEM IAW MEL.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 27,569 hrs · 25,439 cycles

DENTS AT APPROX FS 735 TO FS 755 BETWEEN STR 24L, 25L AND BETWEEN STR 24R, 25R. (C-CHECK) RO: 11/18/2017 REPAIRED DENT ON LT FUSELAGE IAW REO.

Part: VANE — CHAFED (TE FLAP) · airframe 27,569 hrs · 25,439 cycles

RT INBD FLAP VANE INBD VANE CAP IS CHAFED. (C-CHECK) RO: 11/18/2017 REMOVED AND REPLACED THE RT INBOARD FLAP VANE, INBOARD LEADING EDGE VANE CAP IAW SRM.

Part: PSEU — FAILED (MLG) · airframe 25,210 hrs · 22,864 cycles

GEAR DISAGREE AFTER EXTENDING THE GEAR FOR LANDING. INITIALLY ALL GEAR WERE DOWN AND GREEN BUT THEN THE NOSE GEAR GREEN INDICATION WENT OUT AND THE GEAR DISAGREE MSG WAS THEN DISPLAYED. CREW DID A GO AROUND AND CYCLED THE GEAR AND ALL GEAR STAYED GREEN. REPLACED PSEU AND PERFORMED GEAR SWINGS. ALL CHECKED GOOD.

Part: DOWNLOCK SENSOR — MALFUNCTIONED (NLG) · airframe 24,795 hrs · 22,411 cycles

GEAR DISAGREE WHEN SELECTED GEAR UP, NLG WAS HATCHED YELLOW AND MLG WERE BOTH UP. R & R NLG DOWNLOCK SENSOR NR 2 IAW AMM, ADJUSTED NLG DOWNLOCK NR 2 IAW AMM, SWUNG GEAR MULTIPLE TIMES, OPS CHECK GOOD.

Part: PROXIMITY SENSOR — FAILED (MLG) · airframe 24,396 hrs · 21,981 cycles

CREW RECEIVED A GEAR DISAGREE ON APPROACH, SHOWING THE NOSE GEAR NOT DOWN AND LOCKED. MISSED APPROACH, FOLLOWED THE QRH AND DECLARED AN EMERGENCY. THE FLIGHT LANDED WITHOUT INCIDENT AND TAXIED TO THE GATE UNDER ITS OWN POWER. R & R THE NLG DOWNLOCK PROXIMITY SENSOR, SWUNG GEAR SEVERAL TIMES IAW AMM.

Part: SEAT TRACK — CORRODED (BS 349-409) · airframe 23,968 hrs · 21,533 cycles

RIGHT CENTER CABIN SEAT TRACK AT APPROXIMATELY FS 349 TO FS 409+128 HAS EVIDENCE OF CORROSION. R & R RT CENTER SEAT TRACK FS 364.0 TO FS 399.0 IAW AMM AND R & R RT CENTER SEAT TRACK FS 399.0 TO FS 409+16 IAW AMM, AND R & R RT CENTER SEAT TRACK FS 409+16 TO FS 409+112 IAW AMM.

Part: SEAT TRACK — CORRODED (BS 349-409) · airframe 23,968 hrs · 21,533 cycles

LEFT CENTER CABIN SEAT TRACK AR APPROXIMATELY FS349 TO FS409+128 HAS EVIDENCE OF CORROSION. R & R LT CENTER SEAT TRACK FS 364.0 TO FS 399.0 IAW AMM AND R & R LT CENTER SEAT TRACK FS 399.0 TO FS 409+112 IAW AMM.

Part: FRAME — CORRODED (BS 333) · airframe 23,968 hrs · 21,533 cycles

AVIONICS BAY BELOW FLOORBOARD THERE IS CORROSION AT FS 333.0, FRAME AT STR 27. BLENDED AND REMOVED CORROSION FROM FS 333.0, STR 27 IAW SRM AND EA.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 23,968 hrs · 21,533 cycles

RIGHT INBD FLAP VANE CENTER L/E CHAFED. R & R RT INBD FLAP VANE CENTER L/E SKIN IAW SRM AND EA.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 23,968 hrs · 21,533 cycles

LEFT INBD FLAP VANE CENTER L/E CHAFED. R & R LT INBD FLAP VANE CENTER L/E SKIN IAW SRM AND EA.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 23,968 hrs · 21,533 cycles

RIGHT INBD FLAP VANE OTBD L/E CHAFED. R & R RT INBD FLAP VANE OTBD L/E SKIN IAW SRM AND EA.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 2,220,872 hrs · 19,807 cycles

TWO DENTS ON THE LT FUSELAGE TO BE OUT OF LIMITS. THE DENTS MEASURE 2.13 INCHES X 1.75 INCHES X .025 INCHES DEEP & 4.75 INCHES X 2.63 INCHES X .065 INCHES DEEP. REPAIRED IAW EA CRJ253-03067.

Part: WIRE HARNESS — DAMAGED (NLG) · airframe 22,191 hrs · 19,788 cycles

GEAR DISAGREE, NOSE GEAR DID NOT RETRACT, STEERING REMAINED ACTIVE. NO OTHER INDICATIONS NOTED BEFOREHAND. FOUND DAMAGE TO NLG HARNESS & BRACKET. R & R HARNESS & BRACKET & COMPLIED WITH SCENARIO 1 OF GEAR DISAGREE EVENT PROCEDURES. ALL CHECKED GOOD. SEE NRC CARDS N60991, N50752 & N60768 FOR WORK PERFORMED.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,748 hrs · 19,326 cycles

SERVICE DOOR EMERGENCY LIGHT HAS ONE BULB INOPERATIVE. REPLACED BULB IAW AMM 33-51-13.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 21,685 hrs · 19,259 cycles

SECTION OF EMER FLOOR LIGHT STRIP INOPERATIVE. R & R NR 2 INVERTER IAW AMM 33-51-07. OPERATIONAL CHECK GOOD.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 21,599 hrs · 19,164 cycles

EMER LIGHTS OUT FROM ROW 2 - 5. CONNECTED EMER LIGHT STRIP AT ROW 2 - 5 IAW AMM 33-51-01. NO FURTHER DISCREPANCY.

Part: BATTERY — DISCHARGED (CABIN) · airframe 21,404 hrs · 18,974 cycles

WHEN PERFORMING SERVICE CHECK FOUND FLOOR TRACK EMERGENCY LIGHTS INOPERATIVE. R & R NR 2 EMERGENCY BATTERY IAW AMM 33-51-04, OPERATIONS CHECKED GOOD.

Part: CONTROL UNIT — FAULTY (ANTI-SKID SYS) · airframe 21,345 hrs · 18,914 cycles

BRAKES FEEL LIKE THEY ARE STICKING. COULDN’T TAXI SINGLE ENG. TEMP'S APPEAR NORMAL, 3'S. TAKES MORE POWER THAN NORMAL TO GET ACFT TO MOVE. PEDAL FEEL ISN`T NORMAL. REPLACED ANTI-SKID CONTROL UNIT IAW AMM 32-44-06.

Part: HYDRAULIC SYSTEM — CONTAMINATED (NR 3) · airframe 20,927 hrs · 18,494 cycles

AFTER TAKEOFF WHILE GEAR WAS COMING UP, RECEIVED NR 3 HYD SIC LOW PRESS CAUTION, FOLLOWED BY A GEAR UP DISAGREE WARNING. THE MAIN GEAR WAS RED & THE NOSE GEAR WAS YELLOW. MX FOUND THE NR 3 HYD SYS TO BE 100% WITH THE SYS OFF. THEY BLED THE SYS IAW AMM 29-10-00-870-810 & PERFORMED A SUCCESSFUL FUNCTIONAL TEST OF THE LG IAW AMM 32-30-00-720-801.

Part: ACTUATOR — FAILED (TE FLAP) · airframe 20,927 hrs · 18,494 cycles

FLAPS FAIL AT 20 AFTER TAKEOFF WOULD NOT RETRACT. -27C CLEAR NO DE-ICE FLUID APPLIED TODAY LAND WT 41000 IAW 165 KTS 1 MIN INTO FLT. R & R ALL 8 FLAP ACTUATORS IAW AMM 27-53-05/27-53-01. RIGGING & OPERATIONS TESTED GOOD AT THIS TIME IAW SEE NON-ROUTINE WORK CARD 54109 FOR MORE DETAILS.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 20,891 hrs · 18,463 cycles

FIRST OFFICER`S FLASHLIGHT BROKEN. REPLACED FIRST OFFICER`S FLASHLIGHT BREAKAWAY STRAP, NO FURTHER DEFECTS NOTED AT THIS TIME, AMM 25-60-00.

Part: BRACKET — DAMAGED (NLG) · airframe 18,969 hrs · 16,572 cycles

NOSE GEAR WOULD NOT COME UP, GEAR DISAGREE MASTER WARNING AFTER TAKEOFF, UP, DN, UP. COMPLIED WITH PA 05-018 REV. FOUND NLG CTR EXTENDED PROXIMITY SENSOR BRACKET DAMAGED. R & R NLG CTR EXTEND BRACKET PROXIMITY SENSOR IAW CMM 32-20-04. REINSTALLED PROXIMITY SENSOR IAW AMM 32-61-05 & PERFORMED MULTIPLE GEAR SWINGS IAW AMM 32-30-00. FUNCTION TEST OF LANDING GEAR EXTENSION & RETRACTION, OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,821 hrs · 18,396 cycles

FLOOR EMERGENCY LIGHTS ARE OUT FROM ROW 9 AFT. DID OPS TEST OF THE BATTERY PACK EMERGENCY LIGHT, OPS CHECKED GOOD IAW AMM 33-51-04-740-801.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 20,788 hrs · 18,359 cycles

FS 621 BULKHEAD 29.5 INCHES ABOVE THE FLOOR HAS 6 CHAFE MARKS FROM SCREW HEADS. REPAIRED IAW REO 601R-53-61-2155.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,683 hrs · 18,255 cycles

EMERGENCY FLOOR PATH LIGHTING, ROWS 2 THRU 5 INOPERATIVE. R & R INVERTER PS2LY IAW AMM 33-51-07. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 20,434 hrs · 18,006 cycles

LEFT EMERGENCY LIGHT INOPERATIVE. CHARGED EMERGENCY LIGHT BATTERY PACK, OPS CHECKED GOOD IAW AMM 33-51-04.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 20,434 hrs · 18,006 cycles

EMERGENCY LIGHTS INOPERATIVE AT ROW 2 AND 5. CHARGED NR 2 BATTERY, LIGHTS OPS CHECKED GOOD IAW AMM 33-51-04.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,999 hrs · 17,568 cycles

EMERGENCY LIGHT OUT ON OVERHEAD PANEL. COMPLIED WITH OPS CHECK IAW AMM 33-50-04. OPS CHECKED NORMAL. OK FOR SERVICE.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 19,170 hrs · 16,764 cycles

CRACK FOUND IN FS 559 SEMI-PRESSURE BULKHEAD CAP ANGLE AT RBL 18. REPAIRED IAW BOMBARDIER REO 601R-53-41-260/601R-53-41-609 AND PA 53-025.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,093 hrs · 16,692 cycles

NR 1 CEILING EMERGENCY LIGHT INOPERABLE. REMOVED AND REPLACED LIGHT IAW AMM 33-51-00.

Part: ACTUATOR — MALFUNCTIONED (TE FLAP) · airframe 19,062 hrs · 16,665 cycles

ON FLIGHT 4280 (MSP TO CLE) RECEIVED A FLAPS FAIL CAUTION MESSAGE ON APPROACH (AT APPROX 3000FT). AIRCRAFT LANDED SAFELY IN CLE. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 44 IAW AD 2009-06-12 PARAGRAPH (H)(6)(I), AMOC DATED DECEMEBER 07 2012 AND PA 25-052J. REMOVED AND REPLACED RIGHT INBOUND AND OUTBOUND FLAP ACTUATOR DUE TO LOP TEM TORQUE CHECK REF AML. CLEANED AND LUBED LEFT AND RIGHT FLAP FLEX SHAFT ASSEMBLIES REML AML RIGGED LEFT AND RIGHT FLAP ACTUATOR REF AML 2342327. REMOVED AND REPLACED RIGHT NR 3 FLEX SHAFT REF AML 2342325. THIS CLEARS DM.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 19,061 hrs · 16,663 cycles

ON FLIGHT 3628 (CWA - MSP) ON APPROACH INTO MSP RECEIVED SMOKE TOILET MESSAGE WITH AUDIO ALARM. EMERGENCY QRH COMPLETED. NO SMOKE OR FUMES WERE IDENTIFIED. EMERGENCY WAS DECLARED AND AIRCRAFT LANDED SAFELY. FOUND MISSING SPEED TAPE ON LAVATORY VENT GRILLE. C/W PA 21-009 APPLIED SPEED TAPE. INSPECTED AIR CONDITIONING DUCTS, WATER SEPARATOR CONDENSER CHECKED AND CLEANED AS PER AMM 21-51-13. BOTH ENGINES AND APU LEAK CHECKED. NO LEAKS NOTED. OPERATED ENGINES AND APU WITH BOTH PACKS AT FULL HOT FOR OVER 30 MIN. NO SMOKE OR SMELL NOTED. REF 49-10-00/71-00-00. INFORMATION ONLY COMPLIED WITH NIN WORK SCOPE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,588 hrs · 16,205 cycles

OVER HEAD EMERGENCY LIGHT INOPERABLE. REMOVED AND REPLACED OVERHEAD EMERGENCY BULB IAW AMM 33-50-14. CHECK GOOD OK FOR SERVICE.

Part: POST — CRACKED (BS 409) · airframe 18,090 hrs · 15,715 cycles

FS 409+128 RBL18 POST CRACKED IN LOWER RADIUS. REPAIRED IAW REO 601R-53-41-056.

Part: POST — CRACKED (BS 559) · airframe 18,090 hrs · 15,715 cycles

FS 559 RBL 9 VERTICAL POST CRACKED AT BOTTOM OUTBOARD FASTENER. REPAIRED IAW REO 601R-53-41-057.

Part: BULKHEAD — GOUGED (BS 621) · airframe 18,090 hrs · 15,715 cycles

AFT PRESSURE BULKHEAD HAS MULTIPLE GOUGES. REPAIRED IAW REO 601R-53-61-2155.

Part: LIFE VEST — DAMAGED (COCKPIT) · airframe 17,869 hrs · 15,506 cycles

FLIGHT ATTENDANT’S AND CAPTAIN'S LIFE VESTS DAMAGED. REMOVED AND REPLACED FLIGHT ATTENDANT’S AND CAPTAIN’S LIFE VEST IAW AMM 25-61-03.

Part: BULKHEAD — DAMAGED (BS 621) · airframe 17,768 hrs · 15,405 cycles

FS 755 BULKHEAD AFT FACE LOWER LT WEB AND ATTACHMENT FLANGE HAS 10 AREAS OF BUCKING BAR IMPACT DAMAGE. REPAIRED IAW SRM 53-00-00.

Part: SEAT TRACK — CORRODED · corrosion level 2 · airframe 17,768 hrs · 15,405 cycles

RIGHT SIDEWALL NR 5 SEAT TRACK HAS CORROSION. REPAIRED IAW AMM 51-40-11.

Part: SEAT TRACK — CORRODED · corrosion level 2 · airframe 17,768 hrs · 15,405 cycles

RIGHT SIDEWALL NR 1 SEAT TRACK HAS CORROSION. REPAIRED IAW AMM 51-40-11.

Part: SEAT TRACK — CORRODED · corrosion level 2 · airframe 17,768 hrs · 15,405 cycles

RIGHT SIDE WALL NR 3 SEAT TRACK HAS CORROSION. REPAIRED IAW AMM 51-40-11.

Part: ACCESS PANEL — CHAFED (LT WING) · airframe 17,768 hrs · 15,405 cycles

LEFT WING FUEL PANEL HOLE NR 16 CHAFED IN NON-CRITICAL REGION. REPAIRED IAW REO 601R-57-21-030.

Part: SEAT TRACK — CORRODED · corrosion level 2 · airframe 17,768 hrs · 15,405 cycles

RIGHT SIDEWALL NR 2 SEAT TRACK HAS CORROSION. REPAIRED IAW AMM 51-40-11.

Part: SEAT TRACK — CORRODED · corrosion level 2 · airframe 17,768 hrs · 15,405 cycles

RIGHT SIDEWALL NR 4 SEAT TRACK HAS CORROSION. REPAIRED IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,768 hrs · 15,405 cycles

LEFT SIDEWALL SEAT TRACK NR 6 HAS CORROSION IN CABIN. REPAIRED IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,768 hrs · 15,405 cycles

LEFT SIDEWALL SEAT TRACK NR 1 HAS CORROSION IN CABIN. REPAIRED IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,768 hrs · 15,405 cycles

LEFT SIDEWALL SEAT TRACK NR 2 HAS CORROSION. REPAIRED IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 17,768 hrs · 15,405 cycles

RIGHT SIDEWALL SEAT TRACK CORRODED. REPAIRED IAW AMM 53-01-11.

Part: ESCAPE HATCH — OUT OF TOLERANCE (COCKPIT) · airframe 17,708 hrs · 15,350 cycles

COCKPIT ESCAPE HATCH IS PROTRUDING DOWN IN THE UPPER LEFT CORNER. INSPECTED COCKPIT ESCAPE HATCH IAW AMM 52-22-00. PERFORMED OPS CHECK AND RESECURED. OK FOR SERVICE.

Part: SELECTOR VALVE — DEFECTIVE (MLG) · airframe 17,583 hrs · 15,234 cycles

GEAR DISAGREE ON APPROACH, BOTH MAINS NOT DOWN AND LOCKED. WO#336473. PERFORMED CRJ200 LANDING GEAR HEALH CHECK FOUND MLG SELECTOR VALVE BAD. REMOVED AND REPLACED MLG SELECTOR VALVE IAW AMM 32-30-10. LEAK & OP CHECK GOOD. OK FOR SVC. THIS CLEARS WO#336473.

Part: TRIM PANEL — OUT OF ADJUST (ESCAPE HATCH) · airframe 17,217 hrs · 14,917 cycles

COCKPIT EMERGENCY HATCH FELL OPEN ON GROUND. INDICATORS WERE LINED UP BUT DOOR DOES NOT SECURE PROPERLY. ADJUSTED TRIM PIECE ON DOOR, PERFORMED OPS CHECK OF CREW ESCAPE HATCH IAW AMM 52-22-00. OPS CHECK GOOD. OK FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 17,133 hrs · 14,832 cycles

FS 280 BULKHEAD LOWER WEB CRACKED AT RBL 9 AND LBL 9. REPAIRED IAW BOMBARDIER REO 601R-53-11-171.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,133 hrs · 14,832 cycles

CARGO FLOOR SILL AT FS 574-605 LBL 36 HAS CORROSION AROUND NUT PLATES. REPAIRED IAW BOMBARDIER REO 601R-53-61-1574.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 17,133 hrs · 14,832 cycles

DOUBLE DRILLED HOLE AT FS 484, LBL 36 WHEN PERFORMING REO601R-53-41-059. REPAIRED IAW BOMBARDIER REO 601R-53-41-1530.

Part: VANE — CHAFED (TE FLAP) · airframe 17,133 hrs · 14,832 cycles

LEFT INBOARD FLAP VANE LEADING EDGE CHAFED AT WS 99.00 AND WS 139. REPAIRED IAW BOMBARDIER REO 601R-57-52-004 REV C.

Part: FAIRING — CRACKED (VERTICAL STAB) · airframe 14,566 hrs · 12,324 cycles

FLIGHT 4348, WAS PUSHED AT 19:24 OFF GATE A2 INTO AIRCRAFT 8903A. THE VERTICAL STABILIZER AFT FAIRING OF 8932C HIT THE LEFT LEADING EDGE OF 8903A. THEN, AS THE AIRCRAFT WAS BEING PUSHED FARTHER, THE LEFT HORIZONTAL STABILIZER OF 8903A WAS DRAGGED ALONG THE TOP OF THE LEFT HORIZONTAL STABILIZER OF 8932C, PERPENDICULAR TO EACH OTHER WHEN THE AIRCRAFT CAME TO A STOP. AIRCRAFT WERE LATER SEPARATED WITHOUT FURTHER DAMAGE. DAMAGE TO 8932C CONSISTED OF THE FOLLOWING: VERTICAL STABILIZER UPPER AFT FAIRING MULTIPLE DENTS AND EXTENSIVE CRACKING OVER A 23” LENGTH X 6” WIDTH X 5” HIGH ON UPPER AND LT SIDE, FS 902– FS 925.5. RT ELEVATOR UPPER SKIN PANEL AFT INBOARD CORNER BENT DOWN 0.5” X 0.5”, WL242.00, ES8.3. INSPECTED AIRCRAFT STRUCTURE AND SYSTEMS IAW BOMBARDIER MEMOS ISE-STR-10-041, CRJ200-27-217-2010-78 AND CRJ200-27-217-2010-79. REMOVED AND REPLACED VERTICAL STABILIZER UPPER AFT FAIRING. REQUESTED FLY ON FOR ELEVATOR DAMAGE AND WILL REPAIR TBD. AN AMENDMENT TO THIS SDR WILL GIVE THE FINAL REPAIR FOR ELEVATOR.

Part: AUTOPILOT SYS — MALFUNCTIONED (COCKPIT) · airframe 12,788 hrs · 10,692 cycles

AT 10,000 FT 100 FPM THRUST IDLE 250 KTS A/C ROLLED TO LEFT WITH AUTOPILOT ENGAGED A/P DISCONNECTED AND A/C STARTED ROLLING LEFT TO RIGHT AND YAWING LOSS OF CONTROL INCIDENT LASTED 30 SEC, NO MSG OR INDICATIONS. FELT LIKE A/C WAS STALLING.

Part: WARNING MESSAGE — FALSE ACTIVATION (SPOILERS)

FLIGHT SPOILER AND SPOILERON FAIL MESSAGE IN FLIGHT, QRH FOLLOWED, EMERGENCY DECLARED. LANDED WITHOUT INCIDENT. SYSTEM INSPECTED AND RESET PER FAULT ISOLATION MANUAL (FIM). (S)

Part: WARNING LIGHT — ILLUMINATED · airframe 9,428 hrs · 7,736 cycles

FLIGHT SPOILERS SPOILERON CAUTION IN FLIGHT. FOLLOWED QRH MANUAL. EMERGENCY DECLARED AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET PER CRJ FIM, MESSAGE CLEARED. OK FOR SERVICE.