N432SW

Part: RIB — CORRODED (LT WING) · airframe 42,603 hrs · 37,773 cycles

LH WING BATT RIB AT WS53.60 HAS CORROSION ON LOWER HALF. (FILED CLOSED) REMOVED AND REPLACED LH WING BATT RIB AT WS53.60 IN REF TO SRM 51-42-06 AND SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLETED M-337.

Part: SPAR — CORRODED (LT WING) · airframe 42,603 hrs · 37,773 cycles

LH WING AUXILIARY SPAR SPLICE PLATE, OUTBOARD OF PINTLE PIN PLUG HAS SURFAE CORROSION. (FILED CLOSED) REMOVED CORRODED LH WING AUXILIARY SPAR SPLICE PLATE (P/N 601R10009-13), OUTBOARD OF PINTLE PIN PLUG. FABRICATED NEW SPLICE PLATE IN REF DWG 601R10009. INSTALLED FABRICATED PLATE IN REF TO SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLETED M-337 AS REQUIRED.

Part: SPAR — CORRODED (RT WING) · airframe 42,603 hrs · 37,773 cycles

RH WING REAR SPAR AFT FACE AT WS53.60, INBOARD ANGLE FACE (WEB) AT THE CONNECTION OF J410 AND J412, HAS SURFACE CORROSION. (FILED CLOSED) REMOVED AND REPLACED RH WING REAR SPAR AFT FACE AT WS53.60, INBOARD ANGLE FACE (WEB) AT THE CONNECTION OF J410 AND J412 IN REF TO SRM 51-42-06 AND SRM 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY AND M-337.

Part: RETAINER — GOUGED (CARGO DOOR SEAL) · airframe 42,603 hrs · 37,773 cycles

CARGO DOOR UPPER AFT SEAL RETAINER GOUGED. (FILED CLOSED) REMOVED AND REPLACED CARGO DOOR UPPER AFT SEAL RETAINER IN REF TO SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY AND COMPLETED M-337.

Part: TRACK — GOUGED (CARGO DOOR) · airframe 42,603 hrs · 37,773 cycles

CARGO DOOR AFT TRACK GOUGED AT TOP STOP BLOCK. (FILED CLOSED) REMOVED AND REPLACED CARGO DOOR AFT TRACK IN REF TO SRM 51-42-06 AND 51-42-22. COMPLIED WITH TASK CARD 51-900-1003-SKY, COMPLETED M-337.

Part: NUT PLATE — DAMAGED (GPS ANTENNA) · airframe 42,603 hrs · 37,773 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: RA54870-601R-53-31-1063 432SW MXCODEID49947-PR - ONE SCREW STUCK IN NUT PLATE FOR #2 GPS ANTENNA (AFT OUTBOARD). INSTALLED GPS ANTENNA PER AMM 34-58-03-400-801 EXCEPT INSTALLED 1-OFF MS24694-C BOLT USING WASHER NAS1149 (OR EQUIVALENT), 0.063€™Â€™ THK (CRES OR CADMIUM PLATED STEEL) AND MS21042-3 NUT IN THE # 2 GPS AFT RIGHT MOUNTING POINT PER SRM 51-41-02. PERMANENT REPAIR DUE WITHIN 3700 FLT HRS BY 43975.5 TAT., PART NUMBER: - , SERIAL NUMBER: 7548, POSITION: (FILED CLOSED) REMOVED #2 GPS ANTENNA DOUBLER AND REPLACED 4-OFF NUTPLATES IN REF TO SRM 51-45-00. REINSTALLED DOUBLER IN REF TO DWG 601R38319 AND SRM 51-42-06. THIS IS A PERMANENT REPAIR. COMPLIED WITH TASK CARD 51-900-1003-SKY AND COMPLETED M-337.

Part: WARNING MESSAGE — ILLUMINATED (MLG) · airframe 42,189 hrs · 37,412 cycles

RECEIVED GEAR DISAGREE WARNING MSG ON DURING CLIMB, RAN QRH, PULLED RED LANDING GEAR EXENSION HANDLE, RECEIVED ASSOCIATED NOSE DOOR OPEN WARNING MSG. (FLIGHT 1369 - FILED CLOSED) JACKED ALL THREE MAIN LANGING GEARS SWUNG ALL THREE GEARS THREE TIMES, ON THE THIRD ATTEMPT WE RECEIVED GEAR DISAREE ON THE RIGHT MAIN LANDING GEAR. INTERROGATED PSEU FOUNDED ( RIGHT MAIN LANDING GEAR UPLOCK PROXIMITY SENSOR READING FAR SHOWING CODE S18 ) CHECKED TARGET CLEARENCE, FOUNDED CLEARANCE 0.055 IN REF WITH CRJ 200 AMM THE CLEARANCE SHOULD BE 0.035 TO 0.045 ADJUSTED TARGET CLEARANCE TO 0.040 / SWUNG ALL THREE MAIN LANDING GEARS THREE MORE TIMES, OPS CHECK GOOD IN REF WITH CRJ 200 AMM 32-32-05.

Part: BPSU — FAULTED (TE FLAPS) · airframe 41,320 hrs · 36,638 cycles

FLAPS FAIL MESSAGE AFTER TAKEOFF. EXECUTED ZERO FLAP LANDING. VERTICAL SPEED AT TOUCHDOWN UNKNOWN, BUT SUSPECTED <400. COMPLIED WITH AD. PERFORMED FLAP FAIL TROUBLESHOOTING PER FIM. FOUND LT BPSU FAULTED FOR FURTHER T/S AND REPLACEMENT OF LT BPSU.

Part: DOOR — GOUGED (CARGO BAY) · airframe 40,966 hrs · 36,194 cycles

GOUGE FOUND ON TOP OF CARGO DOOR 6" FWD OF FS605.00 FILED CLOSED REPAIRED CARGO DOOR AREA 6" FWD OF FS605.00 IN REF TO REO.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 40,232 hrs · 35,378 cycles

INTERCOSTAL PN# 601R31171-15 @ FS 484 RBL 28 TO RBL 36 FOUND TO BE CRACKED @ LWR OTBD CORNER. (C-CHECK) RO: 10/26/2019 REPAIRED INTERCOSTAL PN# 601R31171-15 @ FS 484 RBL 28 TO RBL 36 IAW REO.

Part: PRESSURE DECK — CRACKED (BS 460) · airframe 40,232 hrs · 35,378 cycles

PRESSURE FLOOR SKIN PANEL LOWER LEFT SURFACE CRACKED BETWEEN BL 0 AND LBL 9 AT FS 460. (C-CHECK) RO: 10/26/2019 PERFORMED MAJOR REPAIR TO PRESSURE FLOOR SKIN LOWER LEFT SURFACE BETWEEN BL 0 AND LBL 9 AT FS 460 IAW REO.

Part: POST — CRACKED (BS 409) · airframe 40,232 hrs · 35,378 cycles

FS 409+128 LBL 27.0 INBOARD HALF OF POST IS CRACKED AT BOTTOM FASTENER. (C-CHECK) RO: 10/26/2019 PERFORMED MAJOR REPAIR TO F.S. 409 POST IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 40,232 hrs · 35,378 cycles

RH FLOOR SILL HAS 2 AREAS OF CORROSION BETWEEN FS 559+12 AND FS559+20 (C-CHECK) RO: 10/26/2019 REMOVED CORROSION FROM RH FLOOR SILL BETWEEN FS 559+12 AND FS559+20 IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 409) · airframe 40,232 hrs · 35,378 cycles

FLOORBEAM CAP AT RBL9 FROM FS409 TO FS409+128 HAS NUMEROUS AREAS OF CORROSION AROUND NUTPLATE HOLES. (C-CHECK) RO: 10/26/2019 REMOVED AND REPLACED FLOORBEAM CAP AT RBL9 FROM FS409 TO FS409+128 WITH A NEW SERVICEABLE FLOORBEAM CAP IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 589-621) · airframe 40,232 hrs · 35,378 cycles

FLOORBEAM CAP AT RBL27 BEWTWEEN FS 621 AND FS 589 HAS MULTIPLE AREAS OF CORROSION (C-CHECK) RO: 10/26/2019 REPAIRED RBL 27 FLOORBEAM BETWEEN FS589 AND FS 621 AREAS A,B,C,AND F IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 559-621) · airframe 40,232 hrs · 35,378 cycles

FLOORBEAM CAP AT LBL27 IS CORRODED IN MULTIPLE AREAS FROM FS621 TO FS559+112 (C-CHECK) RO: 10/26/2019 REPAIRED FLOORBEAM CAP AT LBL27 FS 621 TO FS559+112 IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 570-618) · airframe 40,232 hrs · 35,378 cycles

FLOORBEAM CAP AT LBL9 BETWEEN FS618 AND FS 570 HAS MULTIPLE AREAS OF CORROSION (C-CHECK) RO: 10/26/2019 PERFORMED MAJOR REPAIR TO FLOOR BEAM FLANGE BETWEEN F.S 605 F.S 621 IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 449-473) · airframe 40,232 hrs · 35,378 cycles

FLOORBEAM CAP AT LBL9 IS CORRODED ON TOP SURFACE FROM FS449.85 TO FS473.15 AROUND NUTPLATE HOLES. (C-CHECK) RO: 10/26/2019 PERFORMED MAJOR REPAIR TO FLOORBEAM CAP AT LBL 9 INBOARD SIDE BETWEEN FS409.00+112 TO FS559.00 IAW REO.

Part: PRESSURE DECK — CORRODED (BS 409-559) · airframe 40,232 hrs · 35,378 cycles

LEFT PRESSURE FLOOR SILL PANEL FROM FS409.0+128 TO FS559.0, LBL36 TO LBL47 HAS NUMEROUS AREAS OF CORROSION THAT IS MARKED WITH RED SHARPIE. (C-CHECK) RO: 10/26/2019 REMOVED CORROSION IAW REO.

Part: PRESSURE DECK — CORRODED (BS 409-559) · airframe 40,232 hrs · 35,378 cycles

RIGHT PRESSURE FLOOR SILL PANEL FROM FS409.0+128 TO FS559.0, RBL36 TO RBL47 HAS NUMEROUS AREAS OF CORROSION THAT IS MARKED WITH RED SHARPIE. (C-CHECK) RO: 10/26/2019 REMOVED CORROSION IAW REO.

Part: SKIN — CHAFED (RT AILERON) · airframe 40,232 hrs · 35,378 cycles

RH AILERON UPPER LEADING EDGE CHAFED ON OB AT APPROX WS352.00. (C-CHECK) RO: 10/26/2019 REMOVED AND REPLACED RH AILERON UPPER LEADING EDGE ON OB AT APPROX WS352.00 IAW SRM.

Part: FORMER — CORRODED (PAX DOOR) · airframe 40,232 hrs · 35,378 cycles

PAX DOOR FWD FORMER AT FS 311.75 CORRODED. (C-CHECK) RO: 10/26/2019 REMOVED COROSION FROM PAX DOOR FWD FORMER AT FS 311.75 IAW SRM.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 40,232 hrs · 35,378 cycles

9EA AREAS OF CRACK INDICATIONS NOTED ON FS621 RPB WEB IN THE HEEL LINE AREA OF VERT POSTS, 1ST AREA AT RBL27 WL127-WL133 100%FSH, 2ND AREA AT RBL27 WL105-WL105.5 65%FSH, AND 3RD AREA RBL27 WL77.5-WL97.5 70%FSH, 4TH AREA AT RBL9 WL109.5-WL114 65%FSH, 5TH AREA AT BL0 WL126.5-WL124.5 60%FSH, 6TH AREA AT BL0 WL100-WL113 70%FSH, 7TH AREA AT LBL18 WL103-WL103.5 50%FSH, 8TH AREA AT LBL27 WL106.5-WL114 50%FSH, AND 9TH AREA AT LBL27 WL100-WL103 55%FSH. ALL 9EA AREAS FAILED NDT. (C-CHECK) RO: 10/26/2019 PERFORMED A MAJOR REPAIR TO THE FS 621 REAR PRESSURE BULKHEAD WEB IAW REO.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 40,232 hrs · 35,378 cycles

L/WING INBD FLAP VANE LEADING EDGE CHAFED IN 3 PLACES, I/B- 1.0 X .750 X .015, MID- 1.0 X .700 X .015, OUTBD- 1.0 X .650 X .010 (C-CHECK) RO: 10/26/2019 BLENDED I/B AND O/B CHAFES ON L/H WING I/B FLAP VANE LEADING EDGE SKIN IAW REO. REPAIRED MID LEADING EDGE SKIN ON I/B FLAP VANE LEADING EDGE IAW SRM.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 40,232 hrs · 35,378 cycles

R/WING INBD FLAP VANE LEADING EDGE CHAFED IN 3 PLACES, I/B- 1.0 X .600 X .015, MID- 1.0 X .500 X .015, O/B- 1.0 X .450 X .010 (C-CHECK) RO: 10/26/2019 BLENDED I/B AND MID CHAFES ON R/H WING I/B FLAP VANE LEADING EDGE SKIN IAW REO. REPLACED O/B LEADING EDGE SKIN ON R/H I/B FLAP VANE LEADING EDGE IAW SRM.

Part: BRACKET — FAILED (NLG) · airframe 39,259 hrs · 34,272 cycles

NOSE DOOR AND GEAR DISAGREE WARNING MESSAGE JUST AFTER TAKEOFF. PERFORMED QRH PROCEDURE AND RETURNED TO MSP. (FLT#3874) FO: 03/04/2019 CLOSED REMOVED AND REPLACED NLG OLEO PROX SENSOR BRACKED AND REINSTALLED SENSOR. OPS CHECK GOOD IAW AMM.

Part: PROXIMITY SENSOR — ICED (NLG) · airframe 39,160 hrs · 34,170 cycles

MOMENTS AFTER RETRACTING THE GEAR WE RECEIVED A STEERING INOP IMMEDIATELY FOLLOWED BY A GEAR DISAGREE WARNING. NOSE GEAR REMAINED DOWN WHILE LEFT AND RIGHT MAINS SHOWED IN TRANSIT. RAN QRH AND MANUALLY EXTENDED THE GEAR. RAN STEERING INOP QRH AND MESSAGE EXTINGUISHED. RTF. (FLT#4319) CLOSED TROUBLESHOT GEAR DISAGREE IAW FIM, FOUND ICE BUILD-UP ON NLG PROX SENSORS. REMOVED ICE, & CHECKED GAPS ON THE PROX SENSORS & INSPECTED NLG WIRING HARNESSES FOR DAMAGE, IAW AMM, NO DEFECTS NOTED. PRESSURIZED HYDRAULIC SYSTEM #3, IAW AMM, FOUND NO UNUSUAL INDICATIONS OR NOISES FROM #3A OR #3B ACMP OR #3 HYD RESERVOIR. BLED HYDRAULIC SYSTEM #3, IAW AMM. PERFORMED EXTENSION & RETRACTION OF THE NLG, IAW AMM, OPERATIONAL CHECKS SATISFACTORY. PERFORMED OPERATIONAL TEST OF THE NLG STEERING, IAW AMM, OPERATIONAL CHECKS SATISFACTORY.

Part: PRIORITY VALVE — FAILED (NLG) · airframe 39,160 hrs · 34,170 cycles

ON TAKEOFF RECEIVED A NOSEWHEEL STEERING INOP CAUTION FOLLOWED BY A GEAR DISAGREE WARNING. MAINS SHOWED IN TRANSIT, HOWEVER THE NOSEWHEEL REMAINED DOWN. COULD HEAR NOSEWHEEL DRAGGING IN SLIPSTREAM. COMPLIED WITH QRH PROCEDURE AND ALL GEAR LOCKED IN THE DOWN POSITION. ALSO COMPLIED WITH QRH PROCEDURE FOR NOSEWHEEL STEERING INOP CAUTION. MESSAGE CLEARED. RETURNED TO FIELD. REMOVED AND REPLACED NOSE LANDING GEAR PRIORITY VALVE IAW AMM. OPS CHECKED VALVE IAW AMM. PERFORMED OPS CHECK OF EXT. RETRACT ALSO MANUAL RELEASE IAW AMM. OPS CHECK GOOD AT THIS TIME. OKAY FOR SERVICE. NOSE WHEEL STEERING OPS CHECK GOOD ALSO.

Part: BRACKET — DAMAGED (NLG) · airframe 39,088 hrs · 34,086 cycles

AFTER SELECTING LANDING GEAR UP AFTER TAKE OFF, WE RECEIVED STEERING INOP FOLLOWED BY GEAR DISAGREE. THE MAIN GEAR APPEARED TO HAVE RETRACTED NORMALLY, BUT THE NOSE GEAR REMAINED DOWN OR IN TRANSIT. AFTER FOLLOWING THE QRH AND PULLING THE LANDING GEAR MANUAL RELEASE, ALL THREE GEAR WERE DOWN AND LOCKED AND THE NOSE WHEEL STEERING OPERATED NORMALLY ON LANDING AND TAXI IN. (FLT 7360) CLOSED FOUND MOUNTING BRACKET FOR THE NLG OLEO EXTENDED SENSOR TO BE DAMAGED. REMOVED AND REPLACED NLG BRACKET FOR S23 PROX SENSOR IAW AMM.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 36,601 hrs · 31,308 cycles

DOUBLERS TO UPPER AND LOWER SURFACE OF THE LT ELEVATOR DAMAGED. REMOVED THE EXISTING DOUBLERS AND PERFORMED NEW REPAIR IAW SRM.

Part: HINGE — DAMAGED (PAX DOOR) · airframe 36,601 hrs · 31,308 cycles

PASSENGER DOOR HINGE (FUSELAGE SIDE). ALL 27 LUG HOLES OBLONGED. REMOVED AND REPLACED PAX DOOR HINGE HALF ON FUSELAGE SIDE. RESTORED FINISH. PRESSURIZATION LEAK CHECK GOOD IAW SRM.

Part: WEB — CORRODED (PAX DOOR) · airframe 36,601 hrs · 31,308 cycles

PAX DOOR AFT WEB HAS CORROSION BY UPPER STEP. REPLACED THE PAX DOOR WEB IAW SRM.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 32,946 hrs · 27,406 cycles

FS 621 AFT PRESSURE BULKHEAD LBL 36.20, WL 73.50 DEFECT NOTED ON WEB. REPAIRED FS 621, BULKHEAD CRACK AT LBL36.20, WL73.50 IAW GREO. PRESSURIZATION CHECK GOOD.

Part: SKIN — DENTED (FUSELAGE) · airframe 31,236 hrs · 25,698 cycles

ONE DENT BELOW THE AFT EDGE OF THE CARGO DOOR FRAME IS OUT OF LIMITS. INSPECTED DENT AND WAS FOUND TO BE SERVICEABLE IAW REO.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 30,682 hrs · 25,157 cycles

RT EXTERIOR EMERGENCY LIGHT JUST FORWARD OF WING IS INOPERATIVE. SERVICE, R & R RT EXTERIOR EMERGENCY LIGHT JUST FWD OF WING IAW AMM.

Part: LIGHT — CRACKED (CABIN) · airframe 30,599 hrs · 25,066 cycles

EMERGENCY FLOODLIGHT BY THE MAIN CABIN DOOR IS CRACKED. RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,955 hrs · 24,410 cycles

2ND AFT EMERGENCY LIGHT INOPERATIVE. FLT 7379 REPLACED LAMP IN NR 2 POD LIGHT, PN ON OFF 1317.

Part: FRAME — CORRODED (FUSELAGE) · airframe 29,716 hrs · 24,163 cycles

CORROSION ON FRAME AT FS 333.00 BETWEEN STRINGERS 26L & 27. C-CHECK REPAIRED FRAME BY INSTALLING FRAME SECTOR PN 601R32004-55 IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 29,991 hrs · 24,456 cycles

CORROSION ON FRAME AT FS 333.00 BETWEEN STRINGERS 26L & 27. C-CHECK INSTALLED FRAME SECTOR IAW SRM PN 601R32004-55.

Part: FRAME — CORRODED (FUSELAGE) · airframe 29,716 hrs · 24,163 cycles

CORROSION ON FRAME AT FS 319.00 AT STRINGER 26L. C-CHECK REPAIRED FRAME BY INSTALLING FRAME SECTOR PN 601R32003-61 IAW SRM.

Part: SKIN — DENTED (FUSELAGE) · airframe 29,716 hrs · 24,163 cycles

REAR FUSELAGE SKIN BETWEEN FS 755.00 TO VS 67.5% STRINGERS 25R TO 26L HAS THREE DENTS. C-CHECK REPAIRED REAR FUSELAGE SKIN BETWEEN FS 755.00 TO VS 67.5% STRINGERS 24L TO 24R IAW REO.

Part: FRAME — CORRODED (FUSELAGE) · airframe 29,991 hrs · 24,456 cycles

CORROSION ON FRAME AT FS 319.00 AT STRINGER 26L. C-CHECK INSTALLED FRAME SECTOR IAW SRM PN 601R32003-61.

Part: SKIN — DENTED (FUSELAGE) · airframe 29,986 hrs · 24,446 cycles

REAR FUSELAGE SKIN BETWEEN FS 755.00 TO VS 67.5% STRINGERS 25R TO 26L HAS THREE DENTS. C-CHECK REPAIRED DENTS AT FS 755.00 TO VS 67.5% STRINGERS 24L TO 24R IAW REO.

Part: FASTENER — MISSING (LT WING) · airframe 29,986 hrs · 24,446 cycles

LT WING HAS 3 EACH FASTENERS THAT HAVE NEVER BEEN INSTALLED AT WING RIB 366.00 APPROXIMATELY 18 INCHES FROM FRONT SPAR. C-CHECK REPAIRED RIB WING PLUG WG STATION 371.00 LT SIDE IAW REO.

Part: POST — CRACKED (FUSELAGE) · airframe 29,716 hrs · 24,163 cycles

FS409+128 RBL INBD VERTICAL POST HAS AN INDICATION NOTED IN THE AFT FLANGE RADIUS AT WL. 69 APPROXIMATELY .250 INCHES LONG & 50% FSH. C-CHECK INSTALLED NEW 409+128 RBL18 POST ASSEMBLY IAW SRM & REO.

Part: POST — CRACKED (FUSELAGE) · airframe 29,716 hrs · 24,163 cycles

FS 409+128 BL 0.0 LT SIDE VERTICAL POST HAS AN INDICATION NOTED IN THE AFT FLANGE RADIUS AT WL 69 APPROXIMATELY .250 INCHES LONG X 50%FSH. C-CHECK REPLACED FS 409+128 BL 0.0 LT SIDE VERTICAL POST IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 29,716 hrs · 24,163 cycles

LT WINDSHIELD LOWER AFT SIDE POST FITTING IS CRACKED. C-CHECK REMOVED CRACKED FITTING & INSTALLED NEW LT WINDSHIELD LOWER AFT SIDE POST FITTING PN 601R33235-3 IAW SRM.

Part: HINGE — CHAFED (PAX DOOR) · airframe 29,991 hrs · 24,456 cycles

PAX DOOR HINGE ON DOOR SIDE HAS CHAFED LUGS FROM NR 6 THROUGH NR 27 APPROXIMATELY .002 INCHES DEEP & HINGE SPRING PIN HOLE ELONGATED WITH RAISED METAL AFT OF LUG NR 27. C-CHECK REPLACED PAX DOOR HINGE HALF IAW SRM PN 601R318073-5.

Part: FRAME — CORRODED (FUSELAGE) · airframe 29,991 hrs · 24,456 cycles

CORROSION ON FRAME AT FS 349.0 AT STRINGER 26L. C-CHECK REPLACED DAMAGED LOWER FRAME SECTOR AT FS 349.00 WITH NEW FRAME IAW SRM PN 601R32005-69.

Part: POST — CRACKED (FUSELAGE) · airframe 30,003 hrs · 24,470 cycles

FS 409+128 RBL 18 INBD VERTICAL POST HAS AN INDICATION NOTED IN THE AFT FLANGE RADIUS AT WL 6Y9 APPROXIMATELY .250 INCHES LONG X 50 % FSH. C-CHECK INSTALLED NEW 409+128, RBL18 POST ASSEMBLY IAW SRM & REO.

Part: POST — CRACKED (FUSELAGE) · airframe 30,003 hrs · 24,470 cycles

FS 409+128 LBL 18 INBD VERTICAL POST HAS AN INDICATION NOTED IN THE AFT FLANGE RADIUS AT WL 69 APPROXIMATELY .250 INCHES LONG X 50% FSH. C-CHECK REPLACED CRACKED POSTS FS 409+218, LBL 18 IAW SRM & REO.

Part: POST — CRACKED (FUSELAGE) · airframe 30,012 hrs · 24,481 cycles

FS 409+128 BL 0.0 LT SIDE VERTICAL POST HAS AN INDICATION NOTED IN THE AFT FLANGE RADIUS AT WL 69 APPROXIMATELY .250 INCHES LONG & 50% FSH. C-CHECK REPLACED FS 409+128 BULKHEAD VERTICAL POST AT BL0.0 IAW SRM & REO.

Part: FRAME — CORRODED (FUSELAGE) · airframe 29,716 hrs · 24,163 cycles

CORROSION ON FRAME AT FS 349.0 AT STRINGER 26L. C-CHECK REPLACED DAMAGED LOWER FRAME SECTOR AT FS 349.00 WITH NEW FRAME. PN 601R32005-69 IAW SRM.

Part: POST — CRACKED (FUSELAGE) · airframe 29,716 hrs · 24,163 cycles

FS409+128 LBL 18 INBD VERTICAL POST HAS AN INDICATION NOTED IN THE AFT FLANGE RADIUS AT WL 69 APPROXIMATELY .250 INCHES LONG X 50% FSH. C-CHECK REMOVED 409+128 LBL 18 CRACKED POSTS & INSTALLED NEW IAW SRM & REO.

Part: FITTING — CRACKED (FUSELAGE) · airframe 29,716 hrs · 24,163 cycles

RT WINDSHIELD SIDE POST LOWER AFT FITTING IS CRACKED. C-CHECK DRILLED NEW FITTING PN 601R33235-4S. INSTALLED NEW RT WINDSHIELD SIDE POST LOWER AFT FITTING IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 29,986 hrs · 24,446 cycles

LT WINDSHIELD LOWER AFT SIDE POST FITTING IS CRACKED. C-CHECK REPLACED LT WINDSHIELD LOWER AFT SIDE POST FITTING IAW SRM PN 601R33235-3.

Part: FITTING — CRACKED (FUSELAGE) · airframe 29,986 hrs · 24,446 cycles

RT WINDSHIELD SIDE POST LOWER AFT FITTING IS CRACKED. C-CHECK REPLACED RT WINDSHIELD SIDE POST LOWER AFT FITTING IAW SRM PN 601R33235-4S.

Part: BATTERY — DISCHARGED (CABIN) · airframe 29,648 hrs · 24,101 cycles

EMERGENCY LIGHT IN GALLEY DOES NOT STAY ILLUMINATED. FLT#4711 CHARGED EMERGENCY LIGHTS.

Part: COVER — MISSING (EXIT SIGN) · airframe 29,379 hrs · 23,817 cycles

EMERGENCY EXIT SIGN LIGHT COVER IS MISSING BY MAIN CABIN DOOR. FLT#4447 REPLACED.

Part: RAIL — CRACKED (APU) · airframe 29,280 hrs · 23,715 cycles

FLUID LEAKING FROM AFT EQUIPMENT BAY, APU SHUT DOWN & RECEIVED AN APU BOTTLE LOW WARNING. FLT#4570 REPLACED CRACKED, AT FLARE, PRIMARY FUEL RAIL IAW CMM. PN ON/OFF 3830155-2 & SN ON/OFF NSN.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,237 hrs · 23,679 cycles

THE FIRST OVERHEAD EMERGENCY LIGHT IS BURNED OUT. FLT#4624 RELAMPED.

Part: PAINT — LOOSE (TE FLAP) · airframe 27,708 hrs · 22,189 cycles

SELECTED FLAPS TO 45 AND FELT A BUMP IN THE CONTROL WHEEL AND PLANE WANTED TO ROLL RIGHT. (FLT 4455) CLEANED ALL FLAP SURFACES AND FOUND RIGHT OUTBOARD FLAP TO HAVE LOOSE PAINT ON LEADING EDGE. DRESSED PAINT. FUNCTIONAL FLIGHT PASSED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,571 hrs · 22,045 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4484) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,438 hrs · 21,900 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4484) RELAMPED IN REFERENCE TO AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,374 hrs · 21,839 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4719) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,307 hrs · 21,779 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4759) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,241 hrs · 21,718 cycles

OVERHEAD EMERGENCY LIGHTS NR 3 AND 4 ARE OUT. (FLT 7811) RELAMPED EMERGENCY LIGHTS.

Part: ACM — MALFUNCTIONED (AC BAY) · airframe 27,186 hrs · 21,667 cycles

A BURNING SMELL WHEN LANDING AND RECEIVED LEFT PACK HI TEMP CAUTION MESSAGE ON GROUND. (FLT 7811) REPLACED LEFT PACK AIR CYCLE MACHINE IN REFERENCE TO AMM. P/N: 782790-15 S/N OFF: 9809034

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,041 hrs · 21,522 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 7757) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,969 hrs · 21,445 cycles

FORWARD AND AFT OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 4555) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,844 hrs · 21,333 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 7768) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,689 hrs · 21,183 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4728) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,675 hrs · 21,168 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,647 hrs · 21,142 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 9 IS OUT. (FLT 4502) RELAMPED EMERGENCY LIGHT.

Part: SKIN — CRACKED (PAX DOOR) · airframe 26,553 hrs · 21,067 cycles

PASSENGER DOOR INNER SKIN AND SUPPORT ANGLE UNDER THE ACTUATOR PULLEY ASSEMBLY IS CRACKED AND TORN OFF. (SERVICE) REPAIRED PASSENGER DOOR INNER SKIN UNDER THE ACTUATOR PULLEY ASSEMBLY AND SUPPORT ANGLE IN ACCORDANCE WITH REO.

Part: SKIN — CRACKED (PAX DOOR) · airframe 26,544 hrs · 21,058 cycles

PASSENGER DOOR INNER SKIN AND SUPPORT ANGLE UNDER THE ACTUATOR PULLY ASSEMBLY IS CRACKED AND TORN OFF. REPAIRED PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,440 hrs · 20,941 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4674) RELAMPED EMERGENCY LIGHT.

Part: MOUNT — CORRODED (LT ENGINE) · airframe 26,407 hrs · 20,912 cycles

LEFT ENGINE FORWARD YOKE MOUNT UPPER AND LOWER ATTACH BOLT ASSEMBLY PITTED. (SERVICE) INSTALLED SERVICABLE YOKE MOUNT UPPER AND LOWER ATTACH BOLTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,407 hrs · 20,912 cycles

NR 1 AND 2 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 4529) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 26,361 hrs · 20,872 cycles

OVERHEAD EMERGENCY SIGN NOT FULLY ILLUMINATED. (FLT 4768) RELAMPED EMERGENCY SIGN.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 26,078 hrs · 20,613 cycles

EXTERIOR EMERGENCY LIGHTS AT SERVICE DOOR AND MCD ARE OUT. (SERVICE) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,002 hrs · 20,540 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 3 IS OUT. (FLT 4726) RELAMPED EMERGENCY LIGHT.

Part: VANE — CHAFED (TE FLAP) · airframe 25,954 hrs · 20,498 cycles

LEFT INBOARD FLAP CENTER VANE LEADING EDGE CHAFED. (C-CHECK) REPLACED LEFT INBOARD FLAP CENTER VANE LEADING EDGE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 26,991 hrs · 21,470 cycles

FS 621 BULKHEAD FORWARD FACE WEB ABOVE CARGO TRACK IS CRACKED. (C-CHECK) REPAIR PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 26,991 hrs · 21,470 cycles

FS 559 BULKHEAD CRACKED AT RIGHT SIDE. (C-CHECK) REPAIR PER REO.

Part: POST — CRACKED (FUSELAGE) · airframe 26,991 hrs · 21,470 cycles

CRACK AT RIGHT VERTICAL POST FS 409+128 IN OUTBOARD C-CHANNEL, AFT RADIUS. (C-CHECK) REPAIRED PER CRJ200 SRM.

Part: POST — CRACKED (FUSELAGE) · airframe 26,991 hrs · 21,470 cycles

CRACK AT LEFT VERTICAL POST LBL 18.0 FS 409+128 IN OUTBOARD C-CHANNEL, AFT RADIUS. (C-CHECK) REPAIRED PER CRJ200 SRM.

Part: POST — CRACKED (FUSELAGE) · airframe 26,991 hrs · 21,470 cycles

CRACK AT CENTER VERTICAL POST BL 0.0 FS 409+128 IN RIGHT C-CHANNEL, AFT RADIUS. (C-CHECK) REPAIRED PER CRJ200 SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 26,991 hrs · 21,470 cycles

CORROSION AT LBL 9 FLOORBEAM OUTBOARD SIDE AT NUTPLATE LOCATIONS FROM FS 574 TO FS 611. (C-CHECK) REPAIRED PER CRJ200 SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 26,991 hrs · 21,470 cycles

CRACK AT OUTBOARD COVER ANGLE AT OUTER SKIN TO INNER SHROUD. (C-CHECK) REPAIRED PER CRJ200 SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,937 hrs · 20,484 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS BURNED OUT. (FLT 4728) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,853 hrs · 20,411 cycles

NR 4 EXTERIOR EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,820 hrs · 20,380 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,774 hrs · 20,336 cycles

CEILING EMERGENCY LIGHT AT ROW 10 IS OUT. (FLT 4450) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,710 hrs · 20,282 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 10 IS OUT. (FLT 4697) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,635 hrs · 20,214 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4552) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,936 hrs · 19,574 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4564) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,672 hrs · 19,348 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4696) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 24,270 hrs · 19,009 cycles

LEFT TWO EXTERIOR OVERWING EMERGENCY LIGHTS ARE OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,676 hrs · 18,514 cycles

EMERGENCY LIGHT ABOVE ROW 10 INOPERATIVE. (FLT 4668) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,320 hrs · 18,208 cycles

EMERGENCY LIGHT ON CEILING AT MAIN CABIN DOOR THAT SHINES TO FLOOR IS INOPERATIVE. (FLT 4595) RELAMPED EMERGENCY LIGHT.

Part: MOUNT — CORRODED (LT ENGINE) · airframe 22,874 hrs · 17,824 cycles

LEFT ENGINE YOKE MOUNT PITTED. (ENG CHANGE) REPLACED YOKE MOUNT PER AMM.

Part: COMBUSTION LINER — CRACKED (LT ENGINE) · airframe 22,874 hrs · 17,824 cycles

LEFT ENGINE COMBUSTION LINER CRACKED BEYOND LIMITS. (BOROSCOPE INSP) REPLACED ENGINE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,598 hrs · 17,574 cycles

CEILING EMERGENCY LIGHT INOP. (FLT 4627)RELAMPED.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 22,024 hrs · 17,051 cycles

FORWARD EMERGENCY FLOOR LIGHTING INOP. (FLT 4770) REPLACED NR 1 INVERTER. P/N 5925-7.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,742 hrs · 16,838 cycles

EXTERIOR RIGHT FORWARD EMERGENCY LIGHT INOP. (FLT 4444) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,694 hrs · 16,800 cycles

CEILING LEVEL EMERGENCY FLOODLIGHT NR 3 INOP. (FLT 4749)RELAMPED.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,634 hrs · 16,748 cycles

FS 621 BULKHEAD CRACKED. (C-CHECK) DAMAGE WITHIN LIMITS. BLENDED PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,953 hrs · 16,997 cycles

FS 559 BULKHEAD CRACKED AT LBL 18 ON FRAME CAP ANGLE. (C CHECK) REPAIRED PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,634 hrs · 16,748 cycles

FS 621 BULKHEAD AT LINTEL FITTING AND ABOVE CARGO DOOR TRACK CRACKED. (C CHECK) REPAIRS PER REO.

Part: SPLICE — DAMAGED (EMERGENCY LIGHT) · airframe 21,570 hrs · 16,698 cycles

AFT FLOOR EMERGENCY EXIT LIGHTS INOP. (FLT 4723) REPLACED WIRE SPLICES.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,570 hrs · 16,698 cycles

RIGHT OVERWING MIDDLE EMERGENCY LIGHT INOP. (FLT 4723) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,403 hrs · 16,558 cycles

CEILING LEVEL EMERGENCY LIGHT NR 3 INOP. (FLT 4514) RELAMPED EMERGENCY LIGHT.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 21,229 hrs · 16,418 cycles

EMERGENCY FLOOR LIGHTING STRIP INOP. (FLT 4729) RESEATED CONNECTOR.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 21,108 hrs · 16,320 cycles

SERVICE DOOR EMERGENCY EXIT SIGNS INOP. (FLT 4892) REPLACED NR 2 ELBP.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 20,423 hrs · 15,784 cycles

FLT 4868 - FLOOR LEVEL EMERGENCY LIGHTING STRIP INOP. RESEATED CONNECTOR.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 20,423 hrs · 15,784 cycles

FLT 4683 - CAPTAINS WINDSHIELD CRACKED. REPLACED WINDSHIELD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,380 hrs · 15,752 cycles

FLT 4753 - RIGHT EXTERIOR EMERGENCY LIGHT INOP. RELAMPED.

Part: WINDOW — CRACKED (COCKPIT) · airframe 20,301 hrs · 15,692 cycles

FLT 4756 - FIRST OFFICERS SIDE WINDOW CRACKED. REPLACED WINDOW PN 601R33033-24, SN OFF 01101H5335.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 20,274 hrs · 15,671 cycles

FLT 4402 - NR 3 CEILING CABIN EMERGENCY LIGHT INOP. RELAMPED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 19,538 hrs · 15,118 cycles

FLT 4729 - NR 3 OVERHEAD EMERGENCY LIGHT INOP. RELAMPED.

Part: STRUT — DISCHARGED (NLG) · airframe 18,551 hrs · 14,357 cycles

FLT 3811 - RECEIVED A NOSE GEAR DISAGREE AND NOSE DOOR OPEN WARNING MESSAGE. RECYCLED GEAR. SERVICED NOSE GEAR STRUT IAW AMM 12-12-32. OPS CHECK GOOD.

Part: ADG — UNWANTED DEPLOY · airframe 18,497 hrs · 14,314 cycles

FLT 4006 - ADG DEPLOYED INFLIGHT. RESTOWED ADG PER CRJ MM 24-23-01.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 18,356 hrs · 14,197 cycles

FORWARD SECTION OF EMERGENCY STRIP IS INOP. (FLT 4099) RESECURED FLOOR LIGHT CONNECTION. OPS CHECK GOOD.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 18,190 hrs · 14,070 cycles

FS 280 LOWER BEAM AT LBL 9 IS CRACKED, FOUND AT C-CHECK. COMPLIED WITH REPAIRS PER CRJ200 REO601R-53-11-171.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 18,190 hrs · 14,070 cycles

FS 280 AT RBL 9 AND LBL 9 FLOOR SUPPORT ANGLE IS CRACKED, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER CRJ200 REO601R 53-11-136.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 18,190 hrs · 14,070 cycles

PAX DOOR EXTERNAL HANDLE IS CRACKED, FOUND AT C-CHECK. REPLACED PAX DOOR HANDLE IAW CRJ200 SRM 51-41-04, 51-42-06 AND 51-42-21.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 18,190 hrs · 14,070 cycles

FS 280 LOWER BEAM AT RBL 9 LOWER BEAM IS CRACKED, FOUND AT C-CHECK. COMPLIED WITH REPAIRS PER CRJ200 REO601R-53-11-171.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 18,190 hrs · 14,070 cycles

FS 280 FORWARD FLOOR SUPPORT ON LEFT SIDE IS CRACKED, FOUND AT C-CHECK. COMPLIED WITH REPAIRS PER CRJ200 SRM 51-2-06 PG 14-18.

Part: ATTACH FITTING — CORRODED (BS 615) · airframe 18,190 hrs · 14,070 cycles

CORROSION FOUND ON FLOOBEAM ATTACH FITTING AT FS 615, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER CRJ200 REO 601R53-61-2562.

Part: PSEU — MALFUNCTIONED (NLG) · airframe 17,724 hrs · 13,719 cycles

FLT 3919 - NOSE GEAR EXTENDED IN FLIGHT. REPLACED PSEU WITH A SERVICEABLE UNIT. OPS CHECKS GOOD IAW MM 32-30-00.

Part: OXYGEN MASK — UNWANTED DEPLOY (ROW 5) · airframe 17,579 hrs · 13,607 cycles

FLT 3798 - O2 MASKS INADVERTENTLY DEPLOYED AT ROW 5. RESTOWED O2 MASKS AS REQUIRED.

Part: BALLAST — ODOR (CABIN LIGHTS) · airframe 16,346 hrs · 12,656 cycles

FLIGHT NR 3968, FLIGHT ATTENDANT SMELLED ELECTRICAL SMOKE NEAR AN OVERHEAD BIN. REPLACED SIDEWALL LIGHT BALLAST IAW 33-21-10. OPS CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 16,231 hrs · 12,558 cycles

THIRD AFT CEILING LEVEL EMERGENCY FLOODLIGHT IS NOT WORKING. REPLACED LAMP. OPS CHECKS GOOD.

Part: TIRE — FAILED (MLG) · airframe 15,502 hrs · 11,985 cycles

RIGHT INBOARD MAIN TIRE BLEW OUT ON TAKEOFF WITH ASSOCIATED RIGHT ANTI-SKID LIGHT AND RIGHT INBOARD BTMS INOP. RETURNED TO SLC. REMOVED AND REPLACED NR 3 AND NR 4 WHEEL ASSEMBLY'S IAW 32-40-00PN 5010571-1 SN ON MAY03-5690 SN OFF MAR03-5540.

Part: ANGLE — CRACKED (RT WING) · airframe 13,658 hrs · 10,625 cycles

RIGHT BATT ANGLE CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS AS PER CRJ 200 REO 601R-57-51-046 REV D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 13,658 hrs · 10,625 cycles

CENTER WING BOX MAIN CABIN AT FS 484 RBL28 CLIP CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED CRACKED CLIP AT FS 484.00 AND RBL 28 PER REO 601R 53-41-059 REV 'A'.

Part: STEP — CRACKED (PAX DOOR) · airframe 13,658 hrs · 10,625 cycles

PAX DOOR NR 2 STEP BOTTOM AFT CORNER CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED 601R-52-11-702-1 DOUBLER AND REPAIR ANGLE PER CRJ200 REO 601R-52-11-702. RII 52-401 COMPLETE.

Part: FITTING — CRACKED (FUSELAGE) · airframe 13,658 hrs · 10,625 cycles

AFT SIDE OF PRESSURE BULKHEAD AT FS 625 CLIPS CRACKED ON LEFT AND RIGHT SIDES BUTT LINE 36 STRINGER 13, DISCOVERED DURING C-CHECK INSPECTION. REPLACED 2 CRACKED CLIPS; PN NR 601-35012-51 CLIP PO NR 67065-3 AT STA 625.00 AFTSIDE OF PRESSURE BULKHEAD LHS AND RHS STR 13 IAW CRJ 200 REO 601R-53-61-985.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,176 hrs · 10,257 cycles

EMERGENCY LIGHT AFT AISLE POD INOP. REPLACED LAMP. OPS CHECK GOOD.

Part: SECU — MALFUNCTIONED (NR 1 AND NR 2) · airframe 12,304 hrs · 9,603 cycles

"SPOILERON FAULT" STATUS MESSAGE ON T/O. REPLACED NR 1 AND NR 2 SECU'S. OPERATIONAL CHECK GOOD IAW MM 27-61-05 PN 49-164-05, SN 1 OFF 01280, SN 2 OFF 0478.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILERS) · airframe 12,238 hrs · 9,555 cycles

ON TAXI OUT IN SLC HAD SPOILERONS FAULT STATUS MESSAGE. REPLACED NR 2 SECU IAW 27-61-05, OPERATIONAL CHECK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 12,004 hrs · 9,375 cycles

2 OVERHEAD CABIN EMERGENCY LIGHTS INOP. RELAMPED AFT MOST AND 2ND FROM FWD CEILING EMERGENCY LIGHTS. OPERATIONAL CHECK GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 10,761 hrs · 8,411 cycles

1 BULB IN FIRST POD WILL NOT ILLUM IN EMERGENCY EXIT SIGN. REPLACED EMERGENCY LIGHT BULB AT NR 1 CEILING POSITION. OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (HORIZONTAL STAB) · airframe 10,659 hrs · 8,325 cycles

"STAB CH 2" STAB TRIM WILL NOT ENGAGE. REPLACED BOTH HSTCA AND HSTMC IAW AMM 27-40-00, 27-42-01, AND 27-42-05. OPERATIONAL CHECK GOOD, PN 7062-3, SN/OFF 799.

Part: SMOKE DETECTOR — MALFUNCTIONED (NR 1) · airframe 8,892 hrs · 6,964 cycles

RECEIVED CARGO SMOKE WARNING DURING BAGGAGE LOADING. REMOVED AND REPLACED NR 1 SMOKE DETECTOR IAW MM 26-15-00. OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,789 hrs · 6,878 cycles

EMERGENCY EXIT CEILING POD LIGHT BURNED OUT. RELAMPED , OPERATIONAL CHECK GOOD.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 8,600 hrs · 6,728 cycles

FS 625 RIGHT INTERCOSTAL ANGLE STR 14R CRACKED. ITEM FOUND AT C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40-11, 51-42-06.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 8,600 hrs · 6,728 cycles

FS 621 RIGHT HAND FLOOR SUPPORT ANGLE RBL 40 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED FLOOR SUPPORT ANGLE IAW CRJ REO 601R-53-61-117 REV "B".

Part: SILL — CRACKED (CARGO BAY) · airframe 8,600 hrs · 6,728 cycles

CARGO BAY FLOOR SILL FS 574 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED FLOOR SILL IAW REO 601R-53-61-690 REV A.

Part: DRIVE ASSY — CORRODED (TE FLAPS) · airframe 8,624 hrs · 6,750 cycles

LEFT WING NR 5 FLEX DRIVE CORRODED. ITEM FOUND AT C-CHECK INSPECTION. FLEX DRIVE REMOVED, SURFACE CORROSION ON HEX END REMOVED, POWER CORE LUBRICATED, NEW END SEAL INSTALLED, FLEX SHAFT REINSTALLED IAW 27-53-10-400-805.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 8,600 hrs · 6,728 cycles

FS 484.0 LEFT HAND INTERCOSTAL OUTBOARD FLANGE LBL 36 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED INTERCOSTAL IAW CRJ REO 601R-53-41-059 REV "A" .

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 8,600 hrs · 6,728 cycles

FS 621 LEFT HAND FLOOR SUPPORT ANGLE LBL 40 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. FLOOR SUPPORT ANGLE REPAIRED IAW CRJ REO 601R-53-61-117 REV "B".

Part: RECEPTACLE — CORRODED (FLAP DRIVE) · airframe 8,624 hrs · 6,750 cycles

LEFT WING NR 4 FLAP ACTUATOR FLAP DRIVE RECEPTICAL CORRODED. ITEM FOUND AT C-CHECK INSPECTION. LEFT NR 4 FLAP ACTUATOR REPLACED IAW CRJ AMM 27-53-05-000-801/27-53-05-400-801.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 8,600 hrs · 6,728 cycles

FS 280 RIGHT FLOORBEAM RBL 9.0 INBOARD AND OUTBOARD ANGLES CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INBOARD AND OUTBOARD ANGLES REMOVED IAW CRJ SRM 51-40-11, ANGLES REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00, 51-21-11.

Part: INTERCOSTAL — CRACKED (FUSLEAGE) · airframe 8,600 hrs · 6,728 cycles

FS 484.0 RIGHT HAND INTERCOSTAL INBOARD AND OUTBOARD FLANGE RBL 27 AND RBL 36 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED INTERCOSTAL IAW CRJ REO 601R-53-41-059 REV "A".

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 9,025 hrs · 7,070 cycles

FS 625 LT INTERCOSTAL STR 14L CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED INTERCOSTAL IAW CRJ SRM 51-40-11, 51-42-06.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 8,600 hrs · 6,728 cycles

FS 280 LT FLOORBEAM LBL 9.0 INBOARD AND OUTBOARD ANGLES CRACKED. ITEM FOUND AT C-CHECK INSPECTION. ANGLES REPLACED IAW CRJ SRM 51-40-11, 51-42-00, 51-42-21, 51-23-00, 51-21-11.

Part: ODOR — DETECTED (APU) · airframe 8,569 hrs · 6,703 cycles

STRONG SMELL OF FUEL UPON STARTING THE APU AFTER LANDING. INSPECTED APU ENCLOSURE AND ENGINE LEFT SIDE. NO FUEL LEAKING. ALL AREAS INSPECTED WERE DRY. RAN APU AND BOTH PACKS. NO FUEL SMELL NOTED. ALL CHECKS GOOD.

Part: ODOR — DETECTED (CABIN) · airframe 8,562 hrs · 6,696 cycles

A STRONG FUEL SMELL COMES INTO THE CABIN WHEN SHUTTING DOWN NR 1 ENGINE AFTER LANDING WITH THE APU RUNNING. CHECKED VENT SYSTEM. PRESSURIZED A/C WITH ALL SYSTEMS AND PERFORMED SHUTDOWN PROCEDURES. NO INDICATION OF FUEL SMELL NOTED. NO DISCREPANCIES NOTED.

Part: CONTROL KNOB — STUCK (RUDDER TRIM) · airframe 8,450 hrs · 6,607 cycles

LEFT RUDDER TRIM KNOB STICKS ALLOWING TRIM TO RUN TO FULL DEFLECTION. INSTALLED SERVICEABLE AILERON/RUDDER TRIM PANEL IAW 27-00-07, OPERATIONAL CHECK GOOD.

Part: DAMPENER — MALFUNCTIONED (AILERONS) · airframe 8,289 hrs · 6,465 cycles

LEFT FLUTTER DAMPER STATUS MESSAGE APPEARED INFLIGHT. REPLACED FLUTTER DAMPER IAW MM 27-34-05. OPERATIONAL CHECK GOOD.

Part: INDICATOR — CONTAMINATED (MACH TRIM) · airframe 7,579 hrs · 5,900 cycles

RECEIVED IAS EI MACH TRIM CAUTION MESSAGE ON DESCENT. DRAINED WATER FROM MACH SYSTEM NR 1. RESET CIRCUIT BREAKERS. OPERATIONAL CHECK OK.

Part: PCU — MALFUNCTIONED (SPOILER) · airframe 7,138 hrs · 5,553 cycles

LEFT FLIGHT SPOILER WHITE BOX W/FLIGHT SPOILERS FAULT STATUS MSG. REMOVED AND REPLACED INBOARD PCU ON LEFT SPOILER IAW MM 27-62-01. OPS CHECK AND LEAK CHECK GOOD.

Part: ADC — MALFUNCTIONED (E/E BAY) · airframe 6,709 hrs · 5,238 cycles

IN FLIGHT, RECEIVED EFIS COMP MON, STALL FAIL, MACH TRIM, IAS CAUTION MESSAGES AND ADC TEMP DISAGREE MESSAGE ON FMS. REPLACED NR 2 AIR DATA COMPUTER AND PURGED NR 1 AND NR 2 PITOT SYSTEM WITH NITROGEN. OPS AND LEAK CHECK GOOD IAW CRJ MM 34-11-00. P/N: 822-0372-154, S/N ON: 12FFG, S/N OFF: 2695

Part: PCU — MALFUNCTIONED (SPOILERONS) · airframe 6,438 hrs · 5,040 cycles

SPOILERONS FAULT STATUS MESSAGE APPEARED. REMOVED AND REPLACED RIGHT INBOARD SPOILERON PCU IAW CRJ MM 27-62-01. OPS AND LEAK CHECKS GOOD.

Part: PCU — MALFUNCTIONED (FLIGHT SPOILER) · airframe 6,269 hrs · 4,912 cycles

SPOILERONS FAULT STATUS ON TAKEOFF FROM COS, LEFT OUTBOARD SPOILERON SHOWS WHITE BOX. REMOVED AND REPLACED PCU IAW CRJ AMM 27-62-01. OPS CHECK GOOD, NO LEAKS NOTED.

Part: SHAFT — BENT (HANDLE ROLLER) · airframe 5,723 hrs · 4,479 cycles

ON ARRIVAL TO DFW, RECEIVED PAX DOOR OUT HANDLE CAUTION MESSAGE. MESSAGE INTERMITTENT, THEN ON CONTINUOUSLY TO LANDING. DOOR HARD TO OPEN. FOUND INNER DOOR HANDLE ROLLER SHAFT BENT. REMOVED AND REPLACED INNER DOOR HANDLE ROLLER ASSY WITH SERVICEABLE ONE IAW CL600 MM 52-10-00. OPS CHECKS GOOD.

Part: CONTROL PANEL — MALFUNCTIONED (RUDDER TRIM) · airframe 5,458 hrs · 4,269 cycles

RUDDER TRIM INOP NOSE LEFT. REMOVED AND REPLACED RUDDER TRIM PANEL. OPS CHECK GOOD. P/N: 601R51226-23/01

Part: SWITCH — MALFUNCTIONED (THRUST REVERSER) · airframe 4,493 hrs · 3,514 cycles

RECEIVED A RIGHT THRUST REVERSER UNLOCKED MESSAGE IN FLIGHT. NO CONTROLABILITY PROBLEMS. RAN QHR PROCEDURE. OPERATION NORMAL. MEGGED WIRES 2KE59B20 AND 2KE23N22 FROM STOW SWITCH PINS 3 & 5. CHECK OK. REPLACED STOW SWITCH PER MM 78-37-01. SYSTEM OPS CHECK OK. P/N: 228-50741-115.

Part: ATTACH FITTING — CRACKED (INTERCOSTAL) · airframe 4,666 hrs · 3,648 cycles

FS 625 RIGHT INTERCOSTAL ANGLE CRACKED STR 14R. REPLACED ANGLE IAW CRJ SRM 51-40-11.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 4,666 hrs · 3,648 cycles

FS 625 LEFT INTERCOSTAL ANGLE STRINGER 146 CRACKED. REPLACED ANGLE IAW CRJ SRM 51-40-11.

Part: CONTROL UNIT — FAILED (STALL WARNING) · airframe 3,845 hrs · 3,006 cycles

ON CLIMBOUT OF SLC AT ABOUT 700 FT AGL RECEIVED A STALL FAIL AMBER MESSAGE. PERFORMED QRH ITEMS AND RETURNED TO SLC FOR NORMAL LANDING. REMOVED AND REPLACED STALL PROTECTION UNIT. OPS CHECK GOOD IAW 27-35-01.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 3,234 hrs · 2,538 cycles

STALL FAIL CAUTION MESSAGE ILLUMINATED CLIMBING OUT OF 500 FT. RAN QRH AND MESSAGE WOULD NOT CLEAR. RETURNED TO SLC. REMOVED AND REPLACED STALL PROTECTION COMPUTER IAW CRJ MM 27-35-01. OPS CHECK GOOD.

Part: INDICATOR — MALFUNCTIONED (AIRSPEED) · airframe 3,234 hrs · 2,538 cycles

OUT OF 32,000 FT, OBSERVED STANDBY AIRSPEED INDICATOR SHOWING 450 KTS (CAPT & FO A/S = 260 KTS). AS WE DESCENDED BACK TO SLC, STANDBY AIRSPEED INDICATOR CAME DOWN WITH ALTITUDE (ACTED LIKE ALTIMETER). REMOVED AND REPLACED STANDBY DRAIN ASSY IAW 34-11-00. OPS & LEAK CHECKS GOOD.

Part: WIRE HARNESS — DAMAGED (ANTI- SKID SYS) · airframe 3,173 hrs · 2,490 cycles

ON TAKEOFF ROLL PRIOR TO V1, BOTH INBOARD AND OUTBOARD ANTI-SKID CAUTION LIGHTS ILLUMINATED. ABORTED TAKEOFF AND RETURNED TO GATE. INSPECTED ALL WHEEL SPEED TRANSDUCERS AND ANTI-SKID SUBHARNESSES. FOUND NR 1 OB SUBHARNESS BACKSHELL AND WIRING DAMAGED. REMOVED AND REPLACED NR 1 OB ANTISKID SUBHARNESS IAW TEMPCO CMM 32-61-20-00. CONDUCTED HIGH SPEED TAXI CHECK. ALL OPERATIONS NORMAL. NO DISCREPANCIES NOTED.

Part: ECU — MALFUNCTIONED (SPOILER) · airframe 2,910 hrs · 2,276 cycles

SPOILERON FAULT STATUS MESSAGE. REMOVED NR 1 & NR 2 SECU'S AND REPLACED WITH SERVICEABLE ONES IAW CL600 MM 27-61-05. REMOVED LEFT INBOARD FLIGHT SPOILER PCU & REPLACED WITH SERVICEABLE ONE IAW CL600 MM 27-62-01. OPS CHECKS GOOD.

Part: WIRE — BROKEN (ANTI SKID SYS) · airframe 2,575 hrs · 2,012 cycles

ON TAKEOFF ROLL, RECEIVED AN ANTI-SKID INBOARD CAUTION MESSAGE. ABORTED THE TAKEOFF. FOUND BROKEN WIRES ON THE TRANSDUCER CANNON PLUG RIGHT INBOARD PLUG. REMOVED AND REPLACED WITH A NEW HARNESS IAW 32-44-01. OPS CHECKS GOOD.

Part: BRAKE ASSY — MALFUNCTIONED (NR 4) · airframe 2,616 hrs · 2,046 cycles

ON TAKEOFF ROLL, RECEIVED ANTI-SKID INBOARD CAUTION MSG AND PERFORMED A LOW SPEED ABORT (60 KTS) APPLIED LITTLE BREAKING, BUT NR 4 BRAKE TEMP CLIMBED TO 7 WHILE THE REST REMAINED AT (2 OR 3 UNITS). CYCLED POWER OFF & ON. COMPLETED OPS CHECK OF ANTI-SKID. OPS CHECK GOOD AT THIS TIME. REMOVED AND REPLACED NR 4 BRAKE. LEAK & OPS CHECKS GOOD.

Part: POTENTIOMETER — TWISTED (COCKPIT) · airframe 2,575 hrs · 2,012 cycles

RUDDER TRIM WILL NOT TRIM TO THE LEFT. FOUND RUDDER TRIM POTENTIOMETER TWISTED IN THE MOUNTS, AND A WIRE LOOSE. REPLACED RUDDER TRIM PANEL WITH SERVICEABLE UNIT. OPS CHECKS GOOD IAW CRJ MM 27-00-00.

Part: WIRE — DISCONNECTED (RUDDER CONTROL) · airframe 2,449 hrs · 1,910 cycles

RUDDER TRIM WILL ONLY GO NOSE RIGHT. SOLDERED WIRE BACK ON CONTROL POTENTIOMETER. OPS CHECK GOOD.

Part: ACTUATOR — FAILED (HORIZ STAB) · airframe 2,248 hrs · 1,744 cycles

NR 2 STAB TRIM CHANNEL WILL NOT ENGAGE. REMOVED AND REPLACED HSTA. REMOVED AND REPLACED MOTOR CONTROL UNIT IAW 27-42-05. PERFORMED OPS CHECK. OPS CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB) · airframe 2,176 hrs · 1,687 cycles

STAB TRIM CHANNEL NR 2 WILL NOT ENGAGE. REMOVED AND REPLACED HSTCU IAW MM 27-41-00. OPS CHECKS GOOD.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 1,823 hrs · 1,416 cycles

AFTER TAKEOFF, STALL FAIL CAUTION MESSAGE APPEARED. RETURNED TO SLC. RESET STALL PROTECTION COMPUTER (SPC) CIRCUIT BREAKERS AND RESET SPC MEMORY. MESSAGE CLEARED. OPS CHECK GOOD.

Part: SWITCH — OUT OF ADJUST (THROTTLE LOCKOUT) · airframe 1,703 hrs · 1,323 cycles

DURING CLIMBOUT RECEIVED LEFT THRUST REVERSER UNLOCKED MESSAGE. FOLLOWED QRH AND RETURNED TO GSO. ADJUSTED THROTTLE LOCKOUT MICROSWITCH IAW CRJ MM 78-30-00. OPS CHECK GOOD.