N429SW

Part: LINE — DAMAGED (HYD SYSTEM) · airframe 40,956 hrs · 36,020 cycles

HYD 1 FAIL AFTER TAKEOFF. COMPLIED WITH QRH PROCEDURE. ON HYD SYNOPTIC PAGE, SYSTEM 1 SHOWED NO QUANTITY, NO TEMP, OR FLOW. PLEASE REFERENCE AML 328199 PLEASE REFERENCE AML 328200THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 20033850 WITH THE FOLLOWING CORRECTIVE ACTION: "TROUBLESHOT HYD 1 FAIL. FOUND #1 HYDRAULIC SYSTEM ACMP STEEL BRAIDED PRESSURE LINE DAMAGED. REMOVED AND REPLACED #1 HYDRAULIC SYSTEM ACMP STEEL BRAIDED PRESSURE LINE IAW AMM. DUE TO RETURN TO FIELD REFERENCE CAMPS CP 20035095, ML 20033851, ML 20033852 AND ML 20033853 FOR #1 HYDRAULIC SYSTEM ACMP, EDP, RESERVOIR AND ALL FILTERS CHANGED. SEE CAMP CP 20038095 FOR LEAK AND OPS CHECK."

Part: ENGINE — FAILED · airframe 40,026 hrs · 34,958 cycles

DURING CLIMB OUT, LOUD BANG FOLLOWED BY SPIKE IN ITT AND CONSTANT N2 VIB MESSAGE. (FLT#4330) REMOVED AND REPLACED RIGHT ENGINE ASSEMBLY IAW AMM. OPS AND LEAK CHECK GOOD.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 39,822 hrs · 34,716 cycles

APPROXIMATELY 8EA DENTS OR PREVIOUS BLENDS AT APPROXIMATE FS589-FS605 APPROXIMATE STR 26R TO STR 23R (C-CHECK) RO: 04/28/2019 COMPLIED WITH DENTS REPAIR IAW REO.

Part: PANEL — CORRODED (FUSELAGE) · airframe 39,822 hrs · 34,716 cycles

RT FLOOR SILL PANEL, FS409.00+128 THRU FS559.00 . BETWEEN APPROX RBL36.00 TO APPROX RBL 45.00, AREAS OF CORROSION. (C-CHECK) RO: 04/28/2019 REMOVED CORROSION ON THE RT FLOOR SILL PANEL AT LOCATIONS AT FS441 RBL45 IAW REO. PRESSURE LEAK CHECK GOOD.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 39,822 hrs · 34,716 cycles

CORROSION FOUND ALONG TOP PARTION OF PASSENGER DOOR SILL ANGLE FROM FS 312.00 THRU FS 346.00. (C-CHECK) RO: 04/28/2019 REMOVED AND REPLACED PAX DOOR SILL ANGLE ASSY WITH NEW PAX DOOR SILL ASSEMBLY IAW SRM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 39,822 hrs · 34,716 cycles

PAX DOOR LOWER FWD AND AFT SILL HAVE SPOTS OF CORROSION. (C-CHECK) RO: 04/28/2019 BLENDED CORROSION ON PAX DOOR STRAP AT LOWER LONGERON IAW SRM AND REO.

Part: SKIN — CORRODED (RT WING) · airframe 39,822 hrs · 34,716 cycles

RIGHT WING PLANK. FUEL TANK ACCESS 650HB HAS CORROSION AND FRETTING DAMAGE. (C-CHECK) RO: 04/28/2019 BLENDED, ROTOPEENED AND REPAIRED WING TANK ACCESS HOLE 650HB IAW SRM AND REO. ALL CHECKS GOOD.

Part: DOUBLER — DENTED (FUSELAGE) · airframe 39,822 hrs · 34,716 cycles

DENT LOCATED JUST AFT OF FS 589.0 JUST BETWEEN STR 21L & STR 22L. (C-CHECK) RO: 04/28/2019 PERFORMED CUT-OUT TO REPAIR AND WET INSTALLED REPAIR DOUBLER TO REPAIR AREA LOCATION ON FUSELAGE FS 589.0 BETWEEN STR 21L & STR 22L IAW SRM. PRESSURIZATION LEAK CHECK OF REPAIR AREA IAW SRM. CHECK GOOD.

Part: HINGE — WORN (PAX DOOR) · airframe 39,822 hrs · 34,716 cycles

PAX DOOR HINGE ON DOOR SIDE, PIANO HINGE PIN HOLES ARE WORN OUT OF ROUND AND SCRATCHED INTERNALLY. (C-CHECK) RO: 04/28/2019 REMOVED AND REPLACED THE PAX DOOR HINGE (DOOR SIDE) IAW SRM. PRESSURE CHECK GOOD.

Part: HINGE — WORN (FUSELAGE) · airframe 39,822 hrs · 34,716 cycles

PAX DOOR HINGE ON FUSELAGE SIDE, PIANO HINGE PIN HOLES ARE WORN OUT OF ROUND AND SCRATCHED INTERNALLY. (C-CHECK) RO: 04/28/2019 REMOVED AND REPLACED DAMAGED PAX DOOR HINGE (FUSELAGE SIDE) IAW SRM AND REO.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 39,822 hrs · 34,716 cycles

LEFT SIDE INTERNAL FUSELAGE FLOOR SILL AT APPROX LBL 42 HAS CORROSION IN VARIOUS AREAS FROM FS 559.0 TO 559.0+ 80. (C-CHECK) RO: 04/28/2019 BLENDED OUT CORROSION AT VARIOUS LOCATIONS ON FLOOR SILL AT LBL 42 BETWEEN FS 559.0 TO FS 559.0 + 80 IAW SRM AND REO.

Part: STRAP — CORRODED (FUSELAGE) · airframe 39,822 hrs · 34,716 cycles

RT SIDE FUSELAGE STRAP AT 559.0 HAS CORROSION.AT APPROX RBL 36. (C-CHECK) RO: 04/28/2019 REMOVED AND REPLACED THE RT STRAP AT FS559 RBL 27 - RBL 42 IAW SRM. ALL CHECKS GOOD.

Part: STRAP — CORRODED (FUSELAGE) · airframe 39,822 hrs · 34,716 cycles

AT FS 559.0 INTERNAL FUSELAGE LEFT SIDE UPPER STRAP (FLOOR LEVEL) HAS CORROSION. (C-CHECK) RO: 04/28/2019 REMOVED AND INSTALLED NEW LT FLOOR STRAP AT FS559 LBL 27 - LBL 42 IAW SRM. PRESSURE CHECK GOOD.

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,822 hrs · 34,716 cycles

AT FS 310 AVIONICS BAY BELOW FLOOR BOARD IN APPROX INBETWEEN STR 25L AND STR25R FRAME FLANGE HAS EVIDENCE OF CORROSION. (C-CHECK) RO: 04/28/2019 REMOVED AND REPLACED LOWER FRAME BETWEEN STR 23L AND STR 23R IAW SRM. PRESSURE LEAK CHECK GOOD.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 39,822 hrs · 34,716 cycles

AVIONICS BAY BELOW FLOOR BOARD INTERCOSTAL BETWEEN FS 349 AND FS 364 HAS EVIDENCE OF CORROSION AT STR27L. (C-CHECK) RO: 04/28/2019 REMOVED AND REPLACED INTERCOSTAL BETWEEN FS 349.0 AND FS364.0 AT STR27L IAW SRM. ALL CHECKS GOOD

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,822 hrs · 34,716 cycles

AT FS 333.0 APPROX IN BETWEEN STR 25L AND STR 25R FRME HAS EVIDENCE OF CORROSION. (C-CHECK) RO: 04/28/2019 REMOVED AND REPLACED LOWER FRAME SECTOR AT FS 333.00 BETWEEN STR 23L AND STR 23R IAW SRM. PRESSURE LEAK CHECK GOOD.

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,822 hrs · 34,716 cycles

AT FS 349.0 IN BETWEEN STR 25L AND STR 25R APPROX, THERE IS EVIDENCE OF CORROSION. (C-CHECK) RO: 04/28/2019 REMOVED AND REPLACED FRAME AT FS 349.00 LOWER SECTOR IAW SRM. ALL CHECKS GOOD.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 39,822 hrs · 34,716 cycles

AVIONIC BAY BELOW FLOOR BOARD IN BETWEEN FS 349 AND FS 364 INTERCOSTAL HAS EVIDENCE OF CORROSION.AT STR 27R (C-CHECK) RO: 04/28/2019 BLENDED OUT CORROSION FROM INTERCOSTAL AT AVIONIC BAY BELOW FLOOR BOARD IN BETWEEN FS 349 AND FS 364, STR 27R IAW SRM. PRESSURE CHECK GOOD. OPERATIONAL TEST GOOD.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 39,822 hrs · 34,716 cycles

AVIONICS BAY, BELOW FLOOR BOARD BETWEEN FS 394.0 TO FS FS 409.0 THERE IS EVIDENCE OF CORROSION AT INTERCOSTAL AT STR 27L. (C-CHECK) RO: 04/28/2019 REMOVED AND REPLACED THE LT INTERCOSTAL BETWEEN FS 394.0 AND 409 AT STR 27L IAW SRM. PRESSURE LEAK CHECK GOOD.

Part: TRACK — DAMAGED (FUSELAGE) · airframe 39,822 hrs · 34,716 cycles

AFT CARGO DOOR FWD SUPPORT TRACK STRUCTURE. U CHANNEL IS DAMAGED. APPROX FS 574.0. (C-CHECK) RO: 04/28/2019 REPAIRED AFT CARGO DOOR FWD SUPPORT TRACK STRUCTURE U CHANNEL IAW REO.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 39,822 hrs · 34,716 cycles

AFT CARGO DOOR SUPPORT STRUCTURE FWD TRACK SUPPORT AT FS 578.0 HAS CRACKED ANGLE. (C-CHECK) RO: 04/28/2019 NEW AFT CARGO DOOR FWD TRACK SUPPORT ANGLE INSTALLED IAW SRM.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 39,822 hrs · 34,716 cycles

RT SIDE FUSELAGE BELOW FLOOR LEVEL, LONGERON ASSEMBLY JUST BELOW WL 73.50 RBL 42 AT FS 513.00 VERTICAL CHANNEL HAS CORROSION. (C-CHECK) RO: 04/28/2019 REMOVED CORROSION FROM RT SIDE FUSELAGE BELOW FLOOR LEVEL, LONGERON ASSEMBLY JUST BELOW WL 73.50 RBL 42 AT FS 513.00 VERTICAL CHANNEL IAW SRM AND REO.

Part: SKIN — CORRODED (FUSELAGE) · airframe 39,822 hrs · 34,716 cycles

EXTERIOR BOTTOM SKIN FROM APPROX. FS559.0 TO FS559.0+112 AND SEVERAL INCHES EITHER SIDE OF BL 0 HAS MULTIPLE AREAS OF CORROSION AROUND FASTENERS AS WELL AS AROUND BELLY DRAINS. (C-CHECK) RO: 04/28/2019 REMOVED CORROSION UNDER FASTENERS HEAD APPROXIMATELY FROM FS559.00+80 TO FS559.00+112 BETWEEN STR 26L TO STR 26R IAW AMM. PRESSURE LEAK CHECK GOOD.

Part: SKIN — CORRODED (FUSELAGE) · airframe 39,822 hrs · 34,716 cycles

EXTERIOR BOTTOM SKIN AT APPROX. FS 559+112 EITHER SIDE OF BL 0 HAS SEVERAL AREAS OF CORROSION AROUND FASTENER HOLES FOR FAIRING 195BB AS WELL AS A DETERIORATED SEALING PAD. (C-CHECK) RO: 04/28/2019 REMOVED CORROSION FROM EXTERIOR BOTTOM SKIN AT APPROX. FS 559+112 FROM STR 21R TO STR 21L WHERE PANEL 195BB TOUCHES IAW SRM.

Part: WINDOW — DELAMINATED (COCKPIT) · airframe 39,822 hrs · 34,716 cycles

CO-PILOTS SIDE WINDOW HAS INDICATIONS OF DELAMINATION ALONG ITS BOTTOM EDGE. (C-CHECK) RO: 04/28/2019REMOVED AND REPLACED COPILOT'S SIDE WINDOW IAW AMM. OPS CHECK GOOD AT THIS TIME.

Part: PLATE — CORRODED (SERVICE DOOR) · airframe 39,822 hrs · 34,716 cycles

SERVICE DOOR PROTECTOR PLATE HAS CORROSION BEHIND SCREW HOLES. (C-CHECK) RO: 04/28/2019 RECEIVED AND INSTALLED NEW PROTECTOR PLATE IAW SRM.

Part: FITTING — CORRODED (RT AILERON) · airframe 39,822 hrs · 34,716 cycles

RIGHT AILERON. OUTBOARD PCU, FORK ATTACHMENT CORRODED. (C-CHECK) RO: 04/28/2019 REMOVED AND INSTALLED NEW SERVICEABLE RT AILERON O/B PCU IAW AMM. RIGGING AND OPERATIONAL TESTS GOOD.

Part: SKIN — DAMAGED (BS 640-700) · airframe 36,267 hrs · 30,771 cycles

MULTIPLE CREASES ON AFT FUSELAGE SKIN PANEL FROM FS 640 - 700, BETWEEN STRINGERS 20 - 22L. REPAIRED IAW REO.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 36,267 hrs · 30,771 cycles

PAX DOOR INTERCOSTAL HAS CORROSION AT DD3 CENTER. REPLACED PAX DOOR INTERCOSTAL IAW REO. PRESSURIZATION LEAK CHECK GOOD

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 36,267 hrs · 30,771 cycles

PAX DOOR AFT INTERCOSTAL AT DD4 HAS CORROSION. REPLACED PAX DOOR INTERCOSTAL IAW REO. PRESSURIZATION LEAK CHECK GOOD.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 36,267 hrs · 30,771 cycles

PAX DOOR INTERCOSTAL ABOVE PRESSURE VALVE OPENING HAS CORROSION. INSTALLED PAX DOOR INTERCOSTAL IAW REO. PRESSURE CHECK GOOD.

Part: THRESHOLD — CORRODED (SERVICE DOOR) · airframe 36,267 hrs · 30,771 cycles

SERVICE DOOR THRESHOLD HAS CORROSION. INSTALLED A NEW SERVICE DOOR THRESHOLD PANEL IAW SRM.

Part: SKIN — DENTED (BS 235-265) · airframe 36,267 hrs · 30,771 cycles

MULTIPLE DENTS ON THE LT FUSELAGE 12 TO 14 INCHES AFT OF ICE DETECTOR. PERFORMED REPAIR TO FUSELAGE SKIN BETWEEN BS 235 AND 265, STRINGER 16L IAW REO.

Part: SKIN — DENTED (BS 700) · airframe 32,773 hrs · 27,137 cycles

AFT FUSELAGE EXTERIOR SKIN DENTED FORWARD OF FS700.0 BETWEEN STR 16L AND 17L. C-CHECK, RO 3/12/15. INSTALLED NEW REPAIR DOUBLER, PN 601R-53-61-770-1, REF CRJ 200, REO. WEIGHT OF MATERIAL REMOVED 1.84 LBS, WEIGHT OF NEW REPAIR DOUBLER 2.26 LBS WEIGHT ADDED .0.42 LBS SCALE USED TUC1755 CAL DUE DATE 3 JUN 2015, COMPLIED WITH ST 51-900-1003.

Part: SKIN — CORRODED (LT WING) · airframe 32,773 hrs · 27,137 cycles

LEFT WING PLANK, TANK ACCESS CUT OUT RIM AT 510 AB, HAS PITTING CORROSION ON LOWER SURFACE, INBD AND OTBD AREAS AS MARKED, C-CHECK, RO 3/12/15, COMPLIED WITH CORROSION REMOVAL, ROTO PEEN AND RESTORED FINISH TO TANK CUTOUT, RIM AT 510AB AROUND ENTIRE CIRCUMFERENCE OF FUEL CELL CUTOUT 0A TO 360A BLEND OUT WAS IN CRITICAL AREA WITH A MATERIAL LOSS OF .001", REF REO. FOUND TO BE WITH IN LIMITS. NO LEAKS NOTED AT THIS TIME.

Part: FAIRING — CHAFED (RT WING TE FLAP) · airframe 32,773 hrs · 27,137 cycles

RIGHT STUB FAIRING CHAFED, C-CHECK, RO 3/12/15, RT FLAP STUB FAIRING CHAFE OUT OF LIMITS IAW REO. REPLACED RT FLAP STUB FAIRING IAW DWG AND SRM.

Part: WEB — CRACKED (BS 193) · airframe 32,773 hrs · 27,137 cycles

SUSPECTED CRACK IN RT TRU BAY AFT AREA, ON FLOOR WEB AT FS 193, APPROXIMATELY RBL 29, C-CHECK RO 3/12/15, REPAIRED CRACK IN RT TRU BAY FLOOR AREA AT FS 193, RBL 29, REF CRJ 200 REO .32LBS, WEIGHT ADDED COMPLETED ST 51-900-1003.

Part: FLOOR PANEL — CRACKED (BS 193) · airframe 32,773 hrs · 27,137 cycles

SUSPECTED CRACK IN LEFT TRU BAY AFT AREA, ON FLOOR WEB AT FS 193, APPROXIMATELY LBL 29, C-CHECK RO 3/12/15, NDT VERIFIED CRACK. REPAIRED LT TRU BAY FLOOR WEB AT FS 193, LBL 29, REF STS EA. COMPLIED WITH ATTACHED ST 51-900-1003.

Part: SMOKE DETECTOR — FALSE INDICATION (CARGO BAY) · airframe 31,470 hrs · 25,866 cycles

RECEIVED TWO ERRONEOUS MOMENTARY SMOKE CARGO WARNING MESSAGES. ONE DURING CRUISE AND ONE DURING TAXI TO THE GATE. NO SMOKE DETECTED BY F/A OR GROUND CREW. R & R BOTH CARGO SMOKE DETECTORS IAW AMM.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 31,470 hrs · 25,866 cycles

EMERGENCY EXIT SIGN DOES NOT ILLUMINATE. SIGN IS LOCATED NEAR MAIN CABIN DOOR. FOUND A WIRE CONNECTOR ON THE MAIN CABIN DOOR EMERGENCY EXIT SIGN BROKEN. INSTALLED NEW CONNECTOR IAW ESPM. OPS CHECKS GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 31,352 hrs · 25,734 cycles

LEFT EXTERNAL AFT EMERGENCY LIGHT INOPERATIVE. SERVICE, R & R EXTERNAL EMERGENCY LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,088 hrs · 24,452 cycles

EMERGENCY POD LIGHT INOPERATIVE. FLT#7392 RELAMPED, PN ON OFF 1317.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,960 hrs · 24,330 cycles

EMERGENCY LIGHT BY SERVICE DOOR BURNED OUT. FLT#4769 RELAMPED. PN ON OFF 1317.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 29,217 hrs · 23,585 cycles

THE 202 BULKHEAD IS CRACKED AT PARK BRAKE ROD, FWD HYDRAULIC BAY. (C-CHECK) REPAIRED LEFT FS 202 PRESSURE BULKHEAD IAW REO.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 29,217 hrs · 23,585 cycles

CARGO SEAT RAIL AT FS 559+85 TO FS 559+96 RBL 9 HAS CORROSION AROUND FASTENERS. (C-CHECK) REPLACED CORRODED SEAT RAIL WITH NEW FABRICATED RAIL P/N 601R-53-00-485-1 AT RBL 9 FS 559 +85 TO FS 559+96 IAW REO.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 29,217 hrs · 23,585 cycles

CARGO SEAT RAIL AT FS 559+96 TO FS 559+115 RBL 9 HAS CORROSION AROUND FASTENERS. (C-CHECK) REPLACED CORRODED SEAT RAIL WITH NEW FABRICATED RAIL P/N 601R-53-00-485-1 AT RBL 9 FS 559 +96 TO FS 559+115 IAW REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 29,217 hrs · 23,585 cycles

FS 621 BULKHEAD HAS A CRACK AT THE TOP OF THE LINTEL FITTING. (C-CHECK) REPAIRED LINTEL CRACK ON THE 621 BULKHEAD IAW REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,080 hrs · 22,441 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4501) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,814 hrs · 22,201 cycles

ROW 13 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4680) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,376 hrs · 21,776 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4773) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,781 hrs · 21,224 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4547) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,195 hrs · 20,665 cycles

AFT RIGHT OVERWING EMERGENCY LIGHT IS OUT. (FLT 4551) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,084 hrs · 20,568 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4450) RELAMPED EMERGENCY LIGHT.

Part: FLAP — OBSTRUCTED (WING) · airframe 25,968 hrs · 20,455 cycles

ROLL TO RIGHT OBSERVED IN FLIGHT WHEN FLAPS SELECTED FORM 30A TO 45A. (FLT 4539) REMOVED THE PAINT BUILDUP ON THE TRAILING AND LEADING EDGES OF THE FLAPS.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 25,609 hrs · 20,136 cycles

LEFT WING INBOARD FLAP CENTER VANE LEADING EDGE IS CHAFED. (C-CHECK) REPLACED FLAP VANE LEADING EDGE SKIN PER SRM.

Part: SKIN — WORN (AILERONS) · airframe 25,654 hrs · 20,174 cycles

LEFT AND RIGHT AILERON UPPER SKIN LEADING EDGES ARE WORN TO LIMITS. (C-CHECK) REPLACED BOTH AILERON LEADING EDGE SKINS.

Part: FRAME — CORRODED (FUSELAGE) · airframe 26,414 hrs · 20,889 cycles

FS 333 FRAME FLANGE IS CORRODED. (C-CHECK) REPLACED DAMAGED SECTION OF FRAME AT FS 330.0 BETWEEN RBL 32.0 AND LBL 32.0 AS PER SRM.

Part: YOKE — GALLED (ENGINE MOUNT) · airframe 25,487 hrs · 20,024 cycles

LEFT ENGINE FORWARD MOUNT YOKE ASSEMBLY HAVE GALLING. (ENGINE CHANGE) REPLACED LEFT ENGINE FORWARD MOUNT YOKE ASSEMBLY.

Part: WIRE — BROKEN (CABIN) · airframe 25,038 hrs · 19,616 cycles

FLOOR EMERGENCY LIGHT FROM EXIT ROW TO REAR OF CABIN IS OUT. (FLT 4742) REPAIRED FLOOR EMERGENCY LIGHT STRIP WIRE AS NECESSARY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,825 hrs · 17,734 cycles

EMERGENCY OVERHEAD LIGHT IN CABIN INOP. (FLT 4670) RELAMPED EMERGENCY LIGHT.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 22,133 hrs · 17,153 cycles

CABIN PRESSURIZATION RATE UNCONTROLLABLE. (FLT 4603)REPLACED RIGHT PACK PRSOV AND CONTROLLER.

Part: CABLE — SHORTED (CABIN) · airframe 22,100 hrs · 17,120 cycles

EMERGENCY EXIT LOWER LIGHT INOP. (FLT 4685) REPLACED CABLE ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,100 hrs · 17,120 cycles

FORWARD EMERGENCY FLOOR TRACK LIGHTING INOP. (FLT 4685) REPLACED FLOOR STRIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,558 hrs · 16,682 cycles

EMERGENCY EXIT LIGHT NEXT TO MAIN CABIN DOOR INOP. (FLT 4421) RELAMPED EMERGENCY LIGHT.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,518 hrs · 16,652 cycles

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

Part: STRUCTURE — GOUGED (FUSELAGE) · airframe 21,518 hrs · 16,652 cycles

FS 280 GOUGED. (C CHECK) REPAIRED PER SRM.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 19,999 hrs · 15,500 cycles

FLT 4559 - FIRST EMERGENCY LIGHT INOP. RELAMPED.

Part: SIGN — BROKEN (EMERGENCY LIGHT) · airframe 19,211 hrs · 14,897 cycles

LOWER EMERGENCY LIGHT BY MAIN CABIN DOOR IS BROKEN. (FLIGHT NR 3810) REPLACED EXIT SIGN ASSEMBLY IAW CRJ 33-51-19. OPS CHECK OK.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 17,313 hrs · 13,460 cycles

FLT NR 3916 - OVERHEAD CEILING EMERGENCY FLOODLIGHT IS INOP. RELAMPED EMERGENCY LIGHT AS REQUIRED.

Part: SKIN — DENTED (FUSELAGE) · airframe 17,172 hrs · 13,348 cycles

BIRDSTRIKE INDUCED DENT JUST AFT OF LEFT TRU DOOR. REPLACED SKIN PANEL AND TWO DAMAGED INTERCOSTALS IAW CRJ SRM 51-23-00, 51-40-11, 51-42-06, 51-42-13, AND 51-42-21.

Part: DOOR — CORRODED (EMERGENCY EXIT) · airframe 17,624 hrs · 13,702 cycles

AREAS OF CORROSION FOUND AT BOTTOM OF LEFT OVERWING EMERGENCY EXIT DOOR, FOUND AT C-CHECK. REMOVED CORROSION PER CRJ200 SRM 52-00-00 FIG 102.

Part: UNKNOWN — SMOKE (CABIN) · airframe 15,044 hrs · 11,739 cycles

PASSENGERS REPORTED SEEING SMOKE IN THE AREA AROUND ROW 10. RAN AC PACKS AND CHECKED ALL LEFT AND RIGHT COMPARTMENTS UNABLE TO DUPLICATE COMPLAINT. OPERATIONAL CHECKS GOOD.

Part: ADC — MALFUNCTIONED (NR 2) · airframe 14,055 hrs · 10,983 cycles

ADC, NR 2 DROPPED OFF LINE WITH ASSOCIATED MACH TRIM CAUTION. LOST PFD NR 2 AIRSPEED, ALT AND VSI WITH WARNING. REPLACED ADC IAW 34-13-01. OPERATIONAL AND LEAKS CHECKS GOOD PER ST34-406. PN: 822-0372-445, SN ON: 1GKCG SN OFF: 13KRR.

Part: ACTUATOR — MALFUNCTIONED (STAB TRIM) · airframe 13,183 hrs · 10,326 cycles

STAB TRIM CHANNEL 2 INOP. REPLACED STAB TRIM ACTUATOR AND MCU IAW MM 27-41-00 AND 27-42-00. OPERATIONAL CHECK GOOD. P/N ON 8396-3, S/N OFF 887, P/N ON 7067-3, S/N OFF 789.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 13,110 hrs · 10,271 cycles

FUSELAGE, TRANSVERSE BEAM LOWER FLANGE IS CRACKED, FS 280.0, LBL 11.0, ITEM FOUND AT C CHECK INSPECTION. TRANSVERSE BEAM REPAIRED REF REO 601R-53-11-171 REV C.

Part: BULKHEAD — CRACKED (BS 621) · airframe 13,110 hrs · 10,271 cycles

AFT PRESSURE BULKHEAD WEB FS 621 LBL 27.5 WL 130 CRACKED ITEM FOUND AT C CHECK INSPECTION. REPAIRED WEB IAW CRJ REO 601R-53-61-1541.

Part: INTERCOSTAL — CRACKED (BS 625 S14L) · airframe 13,110 hrs · 10,271 cycles

FOUND FS 625 LT INTERCOSTAL AT STR 14 LT CRACKED, ITEM FOUND AT C CHECK INSPECTION. REPLACED IAW CRJ REO 601R-53-61-100 AND 601R-53-61-422 REV NC.

Part: ATTACH ANGLE — CRACKED (BS 280) · airframe 13,110 hrs · 10,271 cycles

FUSELAGE, TRANSVERSE BEAM TO FLOORBEAM ATTACH CLIP IS CRACKED FS 280.0, RBL 8.0, ITEM FOUND AT C CHECK INSPECTION. TRANSVERSE BEAM TO FLOORBEAM ATTACH CLIP REPLACED.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 13,110 hrs · 10,271 cycles

FUSELAGE, TRANSVERSE BEAM LOWER FLANGE IS CRACKED, FS 280.0, RBL 11.0, ITEM FOUND AT C CHECK INSPECTION. TRANSVERSE BEAM LOWER FLANGE REPAIRED REF REO 601R-53-11-171 REV C.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 10,539 hrs · 8,258 cycles

FO SIDE WINDSHIELD SHATTERED IN FLIGHT. REPLACED RIGHT WINDSHIELD IAW 56-11-01. P/N OFF 601R33033-14 S/N OFF 01046H1005.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 10,539 hrs · 8,258 cycles

LEFT WINDSHIELD STARTING TO CRACK IN 3 PLACES. FOUND ON GROUND AFTER RIGHT WINDSHIELD CRACKED/SHATTERED INFLIGHT. REPLACED LEFT WINDSHIELD IAW 56-11-01, P/N OFF NP-139321-9 S/N OFF 01199H3456.

Part: WINDOW — CRACKED (COCKPIT) · airframe 10,065 hrs · 7,890 cycles

WHILE ON SHORT FINAL INTO FCA, THE CAPTAINS SIDE WINDOW DEVELOPED 3 LARGE CRACKS IN IT. REPLACED CAPTAINS SIDE WINDOW PER MM 56-12-01. OPERATIONAL CHECK GOOD. P/N NP-139322-5, S/N OFF 02164H8144.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 9,588 hrs · 7,513 cycles

STALL FAIL CAUTION MESSAGE. REPLACED STALL COMPUTER IAW 27-35-00. OPERATIONAL CHECK GOOD. S/N OFF 589.

Part: LIGHT — BURNED OUT (ROW 5) · airframe 9,258 hrs · 7,248 cycles

CEILING EMERGENCY LIGHT POD AT ROW 5 INOPERATIVE. RELAMPED EMERGENCY LIGHT CEILING POD AT ROW 5. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (STALL PROTECTION) · airframe 9,174 hrs · 7,185 cycles

STALL FAIL CAUTION MESSAGE AFTER TAKEOFF. REMOVED AND REPLACED STALL PROTECTION COMPUTER PER M/M 27-35-01. OPERATIONAL CHECK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 9,110 hrs · 7,135 cycles

DURING PREFLIGHT FOUND FORWARD CEILING EMERGENCY LIGHT INOPERATIVE. RELAMPED FORWARD CEILING EMERGENCY LIGHT. OPERATIONAL CHECK GOOD.

Part: ENGINE — SEIZED (NR 2) · airframe 8,945 hrs · 7,006 cycles

AFTER TAKEOFF (ABOUT 500FT), ENGINE NR 2 FAILED. NR 2 STOPPED, AND ITT PEGGED. OIL PRESSURE DROPPED TO ZERO. REMOVED AND REPLACED NR 2 ENGINE IAW AMM 71-00-00. OPERATIONAL CHECK GOOD.

Part: BEAM — CRACKED (FUSELAGE) · airframe 8,475 hrs · 6,642 cycles

FUSELAGE VERTICAL BEAM LOWER FLANGE CRACKED FS 559 LBL 9 O/B. ITEM FOUND AT C-CHECK. REPAIRED IAW CRJ REO 601R-53-41-057 REV. NC.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 8,475 hrs · 6,642 cycles

FUSELAGE FLOORBEAM TO TRANSVERSE BEAM ATTACH CLIPS ARE CRACKED I/B LOCATION. ITEM FOUND AT C-CHECK. REPLACED CLIPS IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-21-11, 51-25-16, AND 51-23-00.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 8,475 hrs · 6,642 cycles

FUSELAGE PULLEY INTERCOSTAL HAS A CRACKED ANGLE FS 484.00 RBL 27.0 O/B LOCATION. ITEM FOUND AT C-CHECK. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-21-11, AND 51-25-16.

Part: FITTING — CRACKED (FUSELAGE) · airframe 8,475 hrs · 6,642 cycles

FUSELAGE FITTING CRACKED AT FS 461 RBL 9 O/B. ITEM FOUND AT C-CHECK. FITTING REPLACED IAW CRJ SRM 51-40-11, 51-23-00, 51-42-06, 51-42-21, 51-25-16, 51-21-11.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 8,475 hrs · 6,642 cycles

RIGHT HAND WHEEL WELL HAT ANGLE AT FS 530.00 ON UNDERSIDE OF PRESSURE FLOOR IS CRACKED. ITEM FOUND AT C-CHECK. REPLACED HAT ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-23-00, 51-25-16, 51-21-11.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 8,475 hrs · 6,642 cycles

FUSELAGE FLOORBEAM TO TRANSVERSE BEAM ATTACH CLIP IS CRACKED O/B LOCATION FS 280.00 LBL 9.0. ITEM FOUND AT C-CHECK. REPLACED CLIP IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00, 51-25-16, AND 51-21-11.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 8,475 hrs · 6,642 cycles

FUSELAGE PULLEY INTERCOSTAL FLANGE CRACKED FS 484 LBL 36 PREVIOUS REPAIR ANGLE. ITEM FOUND AT C-CHECK. REPAIRED IAW CRJ REO 601R-53-41-059 REV. A

Part: ANGLE — CRACKED (FUSELAGE) · airframe 8,475 hrs · 6,642 cycles

LEFT HAND WHEEL WELL HAT ANGLE AT FS 530.00 ON UNDERSIDE OF PRESSURE FLOOR IS CRACKED. ITEM FOUND AT C-CHECK. REPAIRED IAW CRJ SRM 51-31-00, 51-24-21, 51-24-36, 51-40-11, 51-21-11, 51-25-06, 51-25-16, 51-42-06, AND 51-23-00.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 8,689 hrs · 6,810 cycles

CARGO PIT FLOOR SUPPORT ANGLE FS 621.00 RBL 36 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-61-007 REV B.

Part: CLIP — CRACKED (INTERCOSTAL) · airframe 8,689 hrs · 6,810 cycles

AFT EQUIPMENT COMPARTMENT INTERCOSTAL CLIP IS CRACKED; FS 625.00, STR 14R. ITEM FOUND AT C-CHECK INSPECTION. CLIP REPLACED AT FS 625 STR 14R IAW CRJ SRM 51-40-11, 51-42-06, AND 51-25-16.

Part: ANGLE — CRACKED (PAX DOOR) · airframe 8,475 hrs · 6,642 cycles

PASSENGER DOOR; STAIRS AFT DRAG ANGLE IS CRACKED BY DOOR ASSIST PULLEY BRACKET. ITEM FOUND AT C-CHECK. PASSENGER DOOR DRAG ANGLE REPAIRED IAW CRJ REO 601R-52-11-513 REV. NC.

Part: PCU — MALFUNCTIONED (SPOILER) · airframe 8,394 hrs · 6,576 cycles

LEFT OUTBOARD SPOILERON FAULT, WILL NOT CLEAR. INSTALLED SERVICEABLE PCU ON LEFT SPOILERON OUTBOARD POSITION. OPERATIONAL CHECK GOOD IAW 27-62-01. P/N: 27000-7, S/N OFF: 4403.

Part: ELEMENT — BROKEN (MLG WW) · airframe 8,075 hrs · 6,333 cycles

RECEIVED MULTIPLE NUISANCE AMBER MLG OVERHEAT FAIL MESSAGES. UPON TOUCHDOWN, RECEIVED MASTER WARNING MLG BAY OVERHEAT WITH AURAL GEAR BAY OVERHEAT. REMOVED AND REPLACED BROKEN LT WHEEL BIN ELEMENT PER CRJ MM 26-14-01. OPS CHECK GOOD.

Part: COMPUTER — MALFUNCTIONED (FLIGHT CONTROL) · airframe 7,121 hrs · 5,582 cycles

YAW DAMP NR 2 DISENGAGED ON THE GROUND AT SLC AND WOULD NOT RE-ENGAGE. REMOVED AND REPLACED NR 2 FCC CARD PER CRJ MM 22-12-14. OPS CHECKS GOOD.

Part: CONTROL PANEL — MALFUNCTIONED (YAW DAMPER) · airframe 7,106 hrs · 5,570 cycles

YAW DAMPER 2 WOULD NOT ENGAGE. REMOVED AND REPLACED YAW DAMPER PANEL. OPS CHECK GOOD AT THIS TIME. P/N OFF: 601R51594-1.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 4,441 hrs · 3,526 cycles

FS 625 STR 14L LT INTERCOSTAL ANGLE FOUND CRACKED. FOUND DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11 & 51-42-06. P/N: 601-35012-51.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 4,441 hrs · 3,526 cycles

FS 280 LBL 9.0 FLOORBEAM I/B & O/B ANGLES CRACKED. FOUND DURING C-CHECK INSPECTION. ANGLES REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13, AND 51-42-21. P/N: 601R3113-57.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 4,441 hrs · 3,526 cycles

FS 621 LT FLOOR SUPPORT ANGLE CRACKED. FOUND DURING C-CHECK INSPECTION. REPAIRED DAMAGED AREA IAW CRJ REO 601R-53-61-117. ANGLE P/N: 601R-53-61-117-1 REP, ANGLE P/N: 601R-53-61-117-3.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 4,404 hrs · 3,494 cycles

FS 280 RBL 9.0 FLOORBEAM I/B ANGLE CRACKED. FOUND DURING C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40-11, 51-42-06 AND 51-42-21. P/N: 601R3113-58.

Part: SCISSORS — DISCONNECTED (NLG) · airframe 4,203 hrs · 3,340 cycles

NOSE WHEEL GEAR DISAGREE MESSAGE WHEN GEAR RETRACTED. RETURNED TO AUS. FOUND NOSE WHEEL STEERING LINKS (SCISSORS) DISCONNECTED. RECONNECTED, INSPECTED NOSE GEAR TIRES. NO VISUAL DAMAGE NOTED.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB) · airframe 3,741 hrs · 2,973 cycles

STAB TRIM CHANNEL 1 STATUS MESSAGE. COULD NOT ENGAGE STAB TRIM CHANNEL 1. MOTOR 1 FAILURE ON HSTCU ON GROUND TEST. REPLACED HSTA ACTUATOR IAW 27-40-00 AND REPLACED MOTOR CONTROL UNIT IAW 27-42-05. OPS CHECK GOOD.

Part: SPRING — OUT OF ADJUST (PAX DOOR) · airframe 3,687 hrs · 2,926 cycles

CABIN DOOR DIFFICULT TO OPEN. ADJUSTED SPRING ROD ASSEMBLY IAW CRJ MM 52-11-02. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 3,660 hrs · 2,903 cycles

CEILING EMERGENCY LIGHT INOP AT ROW 2. REMOVED THE INOP BULB AND INSTALLED A NEW BULB. OPERATIONAL CHECK GOOD.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 3,660 hrs · 2,903 cycles

LOSS OF ALL NR 3 SYSTEM HYDRAULIC FLUID. REMOVED AND REPLACED ELECTRIC HYDRAULIC PUMP 3A WITH SERVICEABLE UNIT IAW MM 29-12-03. OPS AND LEAK CHECK GOOD.

Part: DOOR — OPEN (OXYGEN SERVICE) · airframe 1,856 hrs · 1,457 cycles

STALL FAIL MESSAGE AFTER TAKEOFF. RETURNED TO SLC. FOUND OXYGEN SERVICE DOOR OPEN, CLOSED DOOR. OPS CHECK GOOD.