N903SW

Part: WINDOW — BROKEN (SEAT 11A) · airframe 48,900 hrs · 40,933 cycles

OUTSIDE WINDOW BROKEN AT 11A. FLIGHT 5141. REMOVED AND REPLACED LT SIDE PASSENGER WINDOW 11A OUTER PANE WITH NEW IAW AMM 56-21-01.

Part: ANGLE — CRACKED (BS 621 BULKHEAD) · airframe 47,300 hrs · 39,489 cycles

CRACKED ANGLE AT THE FS621 BULKHEAD COMMON TO THE CARGO DOOR BEAM LOWER ANGLE. REMOVED AND REPLACED THE CRACKED ANGLE AT FS621 BULKHEAD CARGO DOOR BEAM LOWER ANGLE IAW SRM. LEAK CHECKS GOOD.

Part: FLOOR SUPPORT — CORRODED (BS 460-473.15) · airframe 47,300 hrs · 39,489 cycles

FLOORBEAM FS460.00 - FS473.15 RBL9 HAS CORROSION AROUND NUTPLATES (C-CHECK) RO: 08/01/2019 BLENDED CORROSION ON FLOORBEAM FS460.00-FS473.15 RBL9 IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 484-499) · airframe 47,300 hrs · 39,489 cycles

FLOORBEAM FS484 - FS499 RBL9 HAS CORROSION AROUND NUTPLATES. (C-CHECK) RO: 8/01/2019 REPAIRED FLOORBEAM FS484-FS499 RBL9 IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 439-460) · airframe 47,300 hrs · 39,489 cycles

FLOORBEAM FS439 - FS460 RBL9 HAS CORROSION AROUND NUTPLATES. (C-CHECK) RO: 8/01/2019 / BLENDED CORROSION ON FLOORBEAM FS439 - FS460 RBL9 IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 529-544) · airframe 47,300 hrs · 39,489 cycles

FLOORBEAM FS529 -FS544 RBL9 HAS CORROSION AROUND NUTPLATES. (C-CHECK) RO: 8/01/2019 REPAIRED FLOORBEAM FS529-FS544 RBL9 IAW REO.

Part: CLEAT — CORRODED (PAX DOOR AREA) · airframe 47,300 hrs · 39,489 cycles

PAX DOOR SURROUND FWD SND AFT UNDER FLOOR CLEAT ASSY HAS CORROSION. REMOVED AND REPLACED FWD AND AFT UNDER FLOOR CLEAT ASSY IAW SRM.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 47,300 hrs · 39,489 cycles

CORRODED FLOOR BEAM AT SERVICE DOOR, FS349 AND RBL42. INSTALLED ALL REPAIR PARTS TO FS349 RBL 42 FLOOR BEAM IAW REO.

Part: VERTICAL BEAM — CRACKED (BS 409) · airframe 47,300 hrs · 39,489 cycles

F.S. 409+128 BL 0.00 LH VERTICAL POST AFT RADIUS DEFECT NOTED. (C-CHECK) RO: 08/01/2019 REMOVED AND REPLACED 2EA FS409+128 BL0 VERTICAL POSTS IAW REO AND SRM, LEAK CHECKS GOOD.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 47,300 hrs · 39,489 cycles

AVIONICS BAY FLOOR SUPPORT ANGLE AT FS 349.00 HAS CORROSION. INSTALLED NEW AVIONICS BAY FLOOR SUPPORT ANGLE AND INSTALLED 2EA NEW REINFORCING ANGLES AT FS349 STR26R - STR26L IAW SRM AND REO. LEAK CHECKS GOOD.

Part: STRAP — CORRODED (BS 319) · airframe 47,300 hrs · 39,489 cycles

STRAP CORRODED ON FRAME FS319 RBL43. (C-CHECK) RO: 08/01/2019 REMOVED AND INSTALLED NEW STRAP P/N AT FS319 RBL43 IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 409) · airframe 47,300 hrs · 39,489 cycles

FLOOR BEAM CORRODED LEFT BL9 FS409+6 €“ FS409+118. REMOVED AND REPLACED FLOOR BEAM CAP IAW REO.

Part: DOOR FRAME — CRACKED (BS 379) · airframe 47,300 hrs · 39,489 cycles

PASSENGER DOOR UPPER SILL STGR3 L/H AT FS379.0 CLIP HAS CRACKED. REMOVED AND REPLACED THE PASSENGER DOOR UPPER SILL STGR3 L/H IAW REO AND SRM. LEAK CHECKS GOOD.

Part: DOOR SILL — CORRODED (SERVICE DOOR) · airframe 47,300 hrs · 39,489 cycles

SERVICE DOOR CUTOUT LOWER SILL HAS MULTIPLE AREAS OF CORROSION. REMOVED AND REPLACED SVC DOOR LOWER SILL ANGLE IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 47,300 hrs · 39,489 cycles

LH PRESSURE FLOOR ANGLE FS409+128 - FS559 HAS CORROSION IN MULTIPLE AREAS. REMOVED CORROSION FROM LH PRESSURE FLOOR ANGLE FS409+128 - FS559 IAW REO AND SRM. LEAK CHECKS GOOD.

Part: DOOR SILL — CORRODED (BS 295-310) · airframe 47,300 hrs · 39,489 cycles

FLOOR STRUCTURE (SILL PLATE) CORRODED LBL41 FS310 - FS295. REMOVED AND REPLACED FLOOR STRUCTURE SILL PLATE IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 47,300 hrs · 39,489 cycles

RH PRESSURE FLOOR ANGLE FS409+128 - FS559 HAS CORROSION IN MULTIPLE AREAS. COMPLIED WITH ALL STEPS OF REO.

Part: FLOOR SUPPORT — CORRODED (BS 409) · airframe 47,300 hrs · 39,489 cycles

FLOOR BEAM CORRODED RIGHT BL9 FS409+6 €“ FS409+118. REMOVED CORROSION ON R/H FLOOR BEAM, BL9, FS409+6 -FS409+118 IAW SRM AND REO.

Part: SEAT TRACK — GOUGED (BS 621) · airframe 47,300 hrs · 39,489 cycles

FLOOR RAIL FITTING AT RBL 9 FS 621 HAS DEEP GOUGE. (C-CHECK) RO: 08/01/2019 REMOVED AND REPLACED FITTING IAW REO.

Part: SKIN — CORRODED (BS 409) · airframe 47,300 hrs · 39,489 cycles

FRETTING CORROSION ON AIRCRAFT SKIN AROUND FASTENERS LH FS 409.00+80 TO 409.00+112 STR 20L (C-CHECK) RO: 08/01/2019 REMOVED DAMAGE, ON AIRCRAFT SKIN AROUND FASTENERS LH FS 409.00+80 TO 409.00+112 STR 20L IAW REO.

Part: SKIN — CORRODED (BS 409) · airframe 47,300 hrs · 39,489 cycles

FRETTING CORROSION ON AIRCRAFT SKIN AROUND FASTENERS RH FS 409.00 TO 409.00+96 STR 20R. REMOVED DAMAGE IAW REO.

Part: SKIN — CORRODED (BS 755) · airframe 47,300 hrs · 39,489 cycles

CORROSION ON THE EXTERNAL SKIN AT FS755.0, AT APPROXIMATELY STRINGER 18R. BLENDED OUT CORROSION ON EXTERNAL SKIN AT F/S 775.0 AT STR. 18R.IAW SRM. C/W REO ALL STEPS COMPLETED OF PERMANENT REPAIR.

Part: SHROUD — CHAFED (LT AILERON) · airframe 47,300 hrs · 39,489 cycles

LEFT AILERON. UPPER LEADING EDGE SHROUD CHAFED, OUTBOARD SIDE APPROXIMATELY AS354 TO AS375. REMOVED AND REPLACED AILERON L/E SKIN IAW SRM.

Part: BRACKET — BENT (WOW SENSOR) · airframe 45,480 hrs · 37,863 cycles

AFTER TAKEOFF, AND GEAR RETRACTION, RECEIVED A GEAR DISAGREE AND NOSE DOOR OPEN CAUTION MESSAGES. LANDING GEAR INDICATIONS SHOWED MAIN GEAR UP AND NOSE GEAR DOWN, WITH GEAR HANDLE IN THE UP POSITION. AFTER RUNNING QRH, RECEIVED THREE GREEN IN THE DOWN POSITION. LANDED WITHOUT INCIDENT. FOUND NLG WOW SENSOR BRACKET BENT. REMOVED AND REPLACED BRACKET IAW CMM. ADJUSTED THE WOW SENSOR IAW AMM. OPS CHECK GOOD.

Part: BPSU — FAILED (TE FLAP) · airframe 45,409 hrs · 37,791 cycles

FLAPS FAIL AT 10 DEGREE ON RETRACTION DURING DEPARTURE. (FLT 5068) CLOSED REMOVED AND REPLACED RT BPSU IAW AMM. OPS CHECK GOOD.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 42,779 hrs · 35,386 cycles

PAX DOOR INTERCOSTAL DD7 HAS CORROSION. REPLACED PAX DOOR INTERCOSTAL IAW SRM AND PERFORMED A PRESSURIZATION CHECK IAW AMM, CHECK GOOD.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 42,779 hrs · 35,386 cycles

CORROSION DETECTED ON INTERCOSTAL LOCATED ON AFT SIDE OF PAX DOOR BETWEEN BS 338.0 AND 347.25.REPLACED INTERCOSTAL DESIGNATED IAW SRM. PERFORMED PRESSURE CHECK IAW AMM CHECK GOOD.

Part: DOOR SILL — CORRODED (CARGO BAY) · airframe 42,779 hrs · 35,386 cycles

CARGO DOOR SILL RIGHT INSIDE DOOR HAS CORROSION AROUND NUTPLATE HOLES. INSTALLED NEW CARGO DOOR SILL IAW SRM.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 42,779 hrs · 35,386 cycles

RIGHT WING INBOARD FLAP L/E VANE SKIN CHAFED AT INBOARD SECTION. REMOVED AND REPLACED IAW SRM.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 42,779 hrs · 35,386 cycles

LEFT WING INBOARD FLAP L/E VANE SKIN IS CHAFED AT OTBD SECTION. REMOVED AND REPLACED IAW SRM.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 42,779 hrs · 35,386 cycles

RIGHT WING INBOARD FLAP L/E VANE SKIN CHAFED AT CENTER SECTION. REMOVED AND REPLACED IAW SRM.

Part: STRUCTURE — DENTED (BS 718-736) · airframe 42,779 hrs · 35,386 cycles

DENT FOUND BETWEEN BS 718 AND 736. REPAIRED THE DENT IAW REO.

Part: SKIN — DAMAGED · airframe 39,052 hrs · 32,023 cycles

DURING BIRD STRIKE INSPECTION, FOUND GOUGE IN FUSELAGE SKIN AFT OF NLG CUTOUT. COMPLIED WITH SRM.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 38,251 hrs · 31,319 cycles

CRACKS NOTED ON FS 621 BULKHEAD WEB FWD FACE AT BL0.0, WL 125 AND WL 92.5. C-CHECK, REPAIRED CRACKS ON FS 621 BULKHEAD WEB FWD FACE AT BL0.0, WL 125 AND WL 92.5 IAW REO.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 38,251 hrs · 31,319 cycles

CRACK NOTED ON FS 621 BULKHEAD WEB, FWD FACE, AT LBL18 APPROXIMATELY WL125. REPAIRED THE BULKHEAD WEB IAW REO.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 38,251 hrs · 31,319 cycles

CRACK NOTED ON BS 621 BULKHEAD WEB, FWD FACE, AT LBL18 APPROXIMATELY WL105. REPAIRED THE BULKHEAD WEB IAW REO.

Part: SKIN — DENTED (BS 605-621) · airframe 38,251 hrs · 31,319 cycles

DENTS IN FUSELAGE SKIN PANEL. UPPER DENT IS BETWEEN FS 605-621 AND STR 22-24L. REPAIRED SKIN IAW EA.

Part: SKIN — DENTED (BS 605-621) · airframe 38,025 hrs · 31,108 cycles

FOUND DENT IN FUSELAGE SKIN PANEL UPPER DENT IS BETWEEN BS 605-621 STRINGERS 22-24L. COMPLIED WITH REPAIR IAW REO.

Part: BATTERY PACK — FAILED (FLASHLIGHT) · airframe 36,264 hrs · 29,662 cycles

F/A FLASHLIGHT RED LIGHT NOT BLINKING. REPLACED F/A FLASHLIGHT BATTERY IAW AMM.

Part: COVER — CRACKED (APU) · airframe 36,195 hrs · 29,608 cycles

APU COVER IS CRACKED ON TOP CORNER. REPAIRED CRACK ON THE TOP CORNER OF THE APU COVER IAW REO.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 36,013 hrs · 29,470 cycles

NR 3 RT EXTERNAL EMERGENCY LIGHT INOPERATIVE. R & R EXTERNAL EMERGENCY LIGHT IAW AMM.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 35,250 hrs · 28,906 cycles

EMERGENCY LIGHT BY MAIN CABIN DOOR HAS BULB BURNED OUT, REPLACED BULB.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 35,223 hrs · 28,888 cycles

EMERGENCY EXIT SIGN BY GALLEY SERVICE DOOR COVER MISSING. REPLACED MISSING COVER FOR SERVICE DOOR EMERGENCY EXIT SIGN.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,438 hrs · 28,310 cycles

EMERGENCY EXIT LIGHT NEAR MCD ON WALL HAS ONE LIGHT BURNED OUT. FLT 6421 RELAMPED.

Part: SILL — CORRODED (FUSELAGE) · airframe 34,099 hrs · 28,071 cycles

AFT CARGO COMPARTMENT RT FLOOR SILL HAS CORROSION. C-CHECK REMOVED CORROSION FROM FS589.00 TO FS621.00 IAW REO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 34,099 hrs · 28,071 cycles

LT TRU SURROUND SKIN CRACKED AT AFT LATCH CUT OUT. C-CHECK REPLACED WITH NEW LT TRU SKIN IAW SRM.

Part: SKIN — CHAFED (RT AILERON) · airframe 34,099 hrs · 28,071 cycles

RT AILERON UPPER LE REQUIRES REPLACEMENT DO TO CHAFING. C-CHECK REPLACED RT AILERON UPPER LE SKIN PN 601R13031-166 IAW CRJ-200 IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 34,099 hrs · 28,071 cycles

AFT CARGO COMPARTMENT OTBD LT FLOOR PANEL FRAME CORRODED AROUND NUTPLATES FS 559.00+16 TO FS 625.30. C-CHECK COMPLIED IAW REO.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 34,099 hrs · 28,071 cycles

FS 280 NEAR BL 0, CORROSION AROUND NUT PLATES. C-CHECK REPLACED CORRODED REPAIR FILLER SECTION ON FS 280 UPPER ANGLE IAW REO & SRM.

Part: SKIN — CHAFED (RT AILERON) · airframe 34,099 hrs · 28,071 cycles

RT AILERON LOWER LE HAS A SPOT OF CHAFFING. C-CHECK BLENDED IAW REO.

Part: SKIN — CHAFED (RT AILERON) · airframe 34,099 hrs · 28,071 cycles

RT AILERON UPPER LE HAS NUMEROUS SPOTS OF CHAFFING. C-CHECK CHAFFING ON THE RT AILERON UPPER LE WAS BLENDED IAW REO.

Part: SKIN — CHAFED (LT AILERON) · airframe 34,099 hrs · 28,071 cycles

LT AILERON UPPER LE HAS NUMEROUS SPOT OF CHAFFING. C-CHECK REMOVED CHAFFING ON THE LT AILERON UPPER LE BY BLENDING IAW REO.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 34,099 hrs · 28,071 cycles

AFT CARGO COMPARTMENT OTBD RT FLOOR PANEL FRAME CORRODED AROUND NUTPLATES FS 559.00+16 TO FS 589.00. C-CHECK REMOVED CORROSION IAW REO.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 34,099 hrs · 28,071 cycles

FS 483 CABLE PULLEY GANG CHANNEL HAS CRACKED ATTACH ANGLE AT FLOOR BEAM RBL35. C-CHECK FABRICATED NEW CLIP IAW REO.

Part: SKIN — CHAFED (LT WING) · airframe 34,099 hrs · 28,071 cycles

LT WING LOWER WING PLANK HAS CHAFE AT TE, FWD 1.5 INCHES FROM CONTACT WITH PANEL 193AB. C-CHECK BLENDED IAW REO.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 34,099 hrs · 28,071 cycles

FS 483 CABLE PULLEY GANG CHANNEL HAS CRACKED ATTACH ANGLE AT FLOOR BEAM RBL 29. C-CHECK REMOVED CRACKED CLIP & INSTALLED NEW CLIP PN 601R31171-9 IAW SRM.

Part: LINK ASSY — CORRODED (FLIGHT CONTROL) · airframe 34,099 hrs · 28,071 cycles

THE RT FLUTTER DAMPNER LINK ASSEMBLY IS HEAVILY CORRODED & PITTED ALONG WITH THE LINK ASSEMBLY HARDWARE. C-CHECK INSTALLED NEW RT FLUTTER DAMPENER LINK ASSEMBLY & HARDWARE IAW AMM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 34,099 hrs · 28,071 cycles

FS 483 CABLE PULLEY GANG CHANNEL HAS CRACKED ATTACH ANGLE AT FLOOR BEAM LBL 29. C-CHECK REMOVED CRACKED CLIP ON FS 483 AT LBL 29 IAW SRM.

Part: VANE — CHAFED (TE FLAP) · airframe 34,099 hrs · 28,071 cycles

RT INBD FLAP VANE HAS 1" AREA CHAFFED ON LE INBD SIDE. C-CHECK BLENDED CHAFFING IAW SRM & REO.

Part: VANE — CHAFED (TE FLAP) · airframe 34,099 hrs · 28,071 cycles

LT INBD FLAP LE VANE IS CHAFFED ON INBD SECTION. C-CHECK BLENDED LT INBD FLAP VANE LE INBD SECTION IAW SRM & REO.

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,099 hrs · 28,071 cycles

RBL 9 FS 280 OTBD CLIP IS CRACKED. C-CHECK REPLACED FS 280.0 RBL 9.0 OTBD FLOOR BEAM CLIP IAW REO.

Part: FLOOR PANEL — CRACKED (E&E BAY) · airframe 34,099 hrs · 28,071 cycles

LT FWD EQUIPMENT COMPARTMENT FLOOR PANEL HAS CRACK AT LOWER CORNER. C-CHECK REPAIRED LT FWD EQUIPMENT COMPARTMENT FLOOR PANEL IAW REO.

Part: FLOOR PANEL — CRACKED (E&E BAY) · airframe 34,099 hrs · 28,071 cycles

RT FWD EQUIPMENT COMPARTMENT FLOOR PANEL HAS POSSIBLE CRACK AT CORNER. C-CHECK CUT OUT DAMAGED AREA ON RT TRU BAY FLOOR, FABRICATED & INSTALLED DOUBLER IAW REO.

Part: SILL — CORRODED (FUSELAGE) · airframe 34,099 hrs · 28,071 cycles

SERVICE DOOR AT LOWER SILL CORRODED. C-CHECK REPLACED LOWER SILL PN 601R38303-253 AT SERVICE DOOR IAW SRM.

Part: POST — CRACKED (FUSELAGE) · airframe 34,099 hrs · 28,071 cycles

CRACK ON FS 409+128 VERTICAL POST OTBD AFT RADIUS AT LBL 18.00 WL 71.00. C-CHECK REPLACED VERTICAL POST PN S6144-14 IAW SRM & REO.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 34,099 hrs · 28,071 cycles

SERVICE DOOR JUST FWD OF THE LOWER SILL, AT FS 310, STRINGER 19R ANGLE SUPPORT IS CORRODED. C-CHECK REPLACED ANGLE SUPPORT BY SERVICE DOOR JUST FWD OF THE LOWER SILL, AT FS 310, STRINGER 19R IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,099 hrs · 28,071 cycles

LBL 9 FS 280 OTBD CLIP IS CRACKED. C-CHECK REPLACED FS 280.0 LBL 9.0 OTBD FLOOR BEAM CLIP IAW REO.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 33,533 hrs · 27,660 cycles

EMERGENCY EXIT SIGN IN PASSENGER ENTRY IS BURNED OUT. FLT#5241 RELAMPED.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 33,452 hrs · 27,608 cycles

FLT 6256. EMERGENCY EXIT OVERWING SIGN LENS MISSING. REPLACED LENS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,237 hrs · 27,454 cycles

TWO LAMPS BURNED OUT ON LOWER FLOOR LEVEL EMERGENCY EXIT LIGHT AT PASSENGER ENTRY WAY. RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,057 hrs · 27,310 cycles

EMERGENCY OVERHEAD AFT LIGHT IS BURNED OUT. RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,620 hrs · 26,986 cycles

NR 1 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. (FLT 5435) RELAMPED EMERGENCY LIGHT.

Part: BATTERY PACK — MALFUNCTIONED (CABIN) · airframe 32,510 hrs · 26,903 cycles

FRONT RIGHT SECTION OF EMERGENCY LIGHTING COMES ON RANDOMLY. (FLT 6496) DISCONNECTED AND RESET NR 1 EMERGENCY BATTERY PACK. OPERATED EMERGENCY LIGHTS SEVERAL TIMES. WITH NO DEFECTS NOTED.

Part: BRACKET — BENT (NLG) · airframe 32,189 hrs · 26,631 cycles

NOSE GEAR DISAGREE. NOSE GEAR DID NOT COME UP. INDICATIONS SHOWED MLG UP & NOSE GEAR DOWN. (FLT 5364) REPLACED NLG CENTERING PROX SENSOR BRACKET WITH A SERVICEABLE BRACKET. ADJUSTED CENTERING PROX SENSOR ON NLG. PERFORMED OPS CHECK OF LANDING GEAR EXTENSION AND RETRACTION SYSTEM AND OPERATIONAL TEST OF THE LANDING GEAR MANUAL RELEASE SYSTEM IAW AMM. OPS CHECK NORMAL. NO OTHER FAULTS NOTED AT THIS TIME.

Part: PROXIMITY SWITCH — OUT OF RIG (NLG) · airframe 32,148 hrs · 26,592 cycles

NOSE GEAR DID NOT COME UP. (FLT 5526) RE-RIGGED AND ADJUSTED NLG EXTENSION PROX SWITCH IAW AMM. PERFORMED GEAR SWING. OPS CHECKS GOOD.

Part: PROXIMITY SENSOR — OUT OF ADJUST (NLG) · airframe 31,930 hrs · 26,413 cycles

ON CLIMBOUT AFTER BRINGING THE GEAR LEVER UP, RECEIVED A NOSE GEAR DOOR OPEN AND GEAR DISAGREE WARNNG MESSAGES. NOSE GEAR SYNOPTIC SHOWED DN AND GREEN WHILE MAINS WERE UP. CYCLED THE GEAR ONCE WITH NO RESOLUTION TO THE PROBLEM. RETURNED TO FIELD. (FLT 6463) INSPECTED AND FOUND OLEO CENTERING/EXTENDED PROXIMITY SENSOR MISALIGNED. ADJUSTED PROXIMITY SENSOR.

Part: SKIN — DENTED (FUSELAGE) · airframe 31,134 hrs · 25,785 cycles

SMALL DENTS ON BELLY OF AIRCRAFT NEAR THE NOSE GEAR. ONE APPEARED TO BE A PUNTCURE. (FLT 6221) REMOVED DAMAGED AREA AND INSTALLED DOUBLER REPAIR IN REFERENCE TO CRJ REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,878 hrs · 25,593 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6217) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,037 hrs · 24,916 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 2 IS OUT. (FLT 6410) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,652 hrs · 24,612 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6475) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,652 hrs · 24,612 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6382) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,490 hrs · 24,456 cycles

NR 1 EMERGENCY OVERHEAD LIGHT INOPERATIVE. (FLT 6205) RELAMPED EMERGENCY LIGHT.

Part: CONNECTOR — DAMAGED (AC BAY) · airframe 29,461 hrs · 24,428 cycles

RIGHT HIGH TEMP CAUTION MESSAGE. THIS WAS FOLLOWED BY SOME SMELL OF SMOKE IN CABIN. (FLT 5327) REPLACED CONNECTOR AND COMPRESSOR OVER TEMP SWITCH. PN OFF AD-750659-17, SN OFF 000215

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,432 hrs · 24,397 cycles

FLOOR EMERGENCY LIGHTS ARE OUT. (FLT 5538) REPLACED THE FLOOR LIGHTING STRIP AND BOTH BAD CONNECTORS AT THE NR 1 AND NR 3 POSITIONS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,432 hrs · 24,397 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6459) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,392 hrs · 24,364 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6307) RELAMPED EMERGENCY LIGHT.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 30,815 hrs · 25,539 cycles

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

Part: POST — CRACKED (FUSELAGE) · airframe 30,815 hrs · 25,539 cycles

CRACK AT FS 409+128 VERTICLE POST AT RBL 18 OUTBOARD C-CHANNEL AFT RADIUS. (C-CHECK) REPLACED VERTICLE POST RBL 18 AT FS 409+128 IN REFERENCE CRJ200 SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 30,815 hrs · 25,539 cycles

INTERCOSTAL CRACKED AT FS 621-FS 625 LEFT STRINGER 16. (C-CHECK) REPAIRED IN REFERENCE TO CRJ200 SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,983 hrs · 24,027 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6452) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,911 hrs · 23,969 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5575) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,844 hrs · 23,914 cycles

AFT OVERHEAD EMERGENCY LIGHT IS INOPERATIVE. (FLT 6498) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,788 hrs · 23,872 cycles

AFT OVERHEAD EMERGENCY LIGHT NR 4 INOPERATIVE. (FLT 5372) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,666 hrs · 23,769 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS BURNED OUT. (FLT 6243) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,528 hrs · 23,646 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6365) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,419 hrs · 23,555 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6336) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 28,349 hrs · 23,507 cycles

RIGHT EXTERIOR AFT EMERGENCY LIGHT IS OUT. (FLT 5844) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,304 hrs · 23,478 cycles

NR 1 CEILING EMERGENCY LIGHT IS OUT. (FLT 6400) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 28,287 hrs · 23,466 cycles

LEFT WING AFT EXTERIOR EMERGENCY EXIT LIGHT IS OUT. (FLT 6521) RELAMPED EMERGENCY LIGHT.

Part: PUMP — FAULTY (HYDRAULIC SYS) · airframe 27,841 hrs · 23,109 cycles

GEAR DOWN DISAGREE WARNING MESSAGE. (FLT 6804) REPLACED 3B HYDRAULIC ACMP, MLG SELECTOR VALVE, REPLACED LT MLG UPLOCK LOCK. P/N: 17051-101, S/N OFF: NGL/1434/03, P/N: 750005000, S/N OFF: 0619, P/N: 848847, S/N OFF: MX657967.

Part: ACTUATOR — FAILED (LT MLG) · airframe 27,828 hrs · 23,098 cycles

"GEAR DISAGREE" MESSAGE WITH LEFT LANDING GEAR SHOWING RED. (FLT 6726) REPLACED LEFT MLG SIDESTAY ACTUATOR. P/N OFF 17008-115 S/N OFF 01207.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,617 hrs · 22,932 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6738) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,498 hrs · 22,834 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 7022) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,122 hrs · 22,502 cycles

NR 1 CEILING EMERGENCY LIGHT IS OUT. (FLT 6655) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,473 hrs · 21,966 cycles

NR 1 CEILING EMERGENCY LIGHT INOPERATIVE. (FLT 6471) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,433 hrs · 21,941 cycles

CENTER AISLE EMERGENCY LIGHT AT THIRD POSITION INOPERATIVE. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,145 hrs · 21,684 cycles

AFT CEILING POD LIGHT INOPERATIVE. (FLT 6540) RELAMPED CEILING POD LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,126 hrs · 21,668 cycles

REAR MOST EMERGENCY LIGHT INOPERATIVE. (FLT 6303) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,036 hrs · 21,596 cycles

TWO OVERHEAD EMERGENCY LIGHTS OUT. (FLT 6774) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,248 hrs · 20,939 cycles

NR 3 EMERGENCY CEILING LIGHT INOP. (FLT 6729) RELAMPED EMERGENCY LIGHT.

Part: UNKNOWN — BINDING (RUDDER SYSTEM) · airframe 24,928 hrs · 20,666 cycles

AT HALF TRAVEL, BINDING IS FELT IN RUDDER PEDALS. (FLT 6771) INSPECTION FOUND NO CABLE RUN OBSTRUCTIONS. NO OBSTRUCTIONS NOTED IN RUDDER PEDAL AREA. COULD NOT DUPLICATE FROM CAPTAIN OR F/O'S PEDALS ON EACH INDIVIDUAL HYDRAULIC SYSTEM. RUDDER SYSTEM OPS CHECKS NORMAL.

Part: BULKHEAD — CRACKED (BS 621) · airframe 24,843 hrs · 20,588 cycles

FS 621 PRESSURE BULKHEAD CRACKED AT TOP OF CARGO DOOR TRACK. (C CHECK) REPAIR PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,355 hrs · 21,027 cycles

AT FS 559.0 RBL 18.0 WL 59.10 PRESSURE BULKHEAD CRACKED. (C-CHECK) REPAIRED PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,355 hrs · 21,027 cycles

FS 621 BULKHEAD CRACKED. (C-CHECK) REPAIRED PER SRM AND REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,732 hrs · 20,503 cycles

AFT EMERGENCY CEILING LIGHT INOP. (FLT 6031) RELAMPED EMERGENCY LIGHT.

Part: BUSHING — LACK OF LUBE (CABIN DOOR) · airframe 24,673 hrs · 20,458 cycles

MAIN CABIN DOOR HANDLE STUCK. (FLT 6271) DISASSEMBLED DOOR UPPER BELL CRANK ASSEMBLY AND LUBED THRU BOLT AND BUSHING.

Part: DOOR — MALFUNCTIONED (CABIN) · airframe 24,601 hrs · 20,390 cycles

COULD NOT OPEN MAIN CABIN DOOR FROM OUTSIDE. (FLT 6045) OPERATION CHECKS NORMAL.

Part: HINGE — LACK OF LUBE (PAX DOOR) · airframe 24,530 hrs · 20,328 cycles

PASSENGER DOOR DIFFICULT TO OPEN. (FLT 6125) LUBED DOOR HINGE AND MECHANISM, CYCLED DOOR SEVERAL TIMES.

Part: ADC — MALFUNCTIONED (NR 2) · airframe 24,360 hrs · 20,198 cycles

LOSS OF FIRST OFFICER INSTRUMENTATION AFTER AUTO PILOT DISENGAGED. (FLT 6587) REPLACED NR 2 ADC AND NR 2 AHRS.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 24,215 hrs · 20,072 cycles

FLT 5955 - MOST AFT CEILING EMERGENCY LIGHT INOP. RELAMPED.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 24,166 hrs · 20,029 cycles

FLT 6631 - CABIN DOOR FLOOR EMERGENCY EXIT SIGN AND OVERHEAD EXIT SIGN AT ROW 8 INOP. REPLACED NR 2 BATTERY CHARGER.

Part: FUEL CONTROL — FAILED (ENGINE) · airframe 24,120 hrs · 19,983 cycles

ENGINE OIL WARNING WITH ENGINE SPOOLING DOWN. (FLT 6044) REPLACED FUEL CONTROL AND FUEL PUMP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,680 hrs · 19,623 cycles

EMERGENCY FLOOD LIGHT NR 3 INOP. (FLT 6129) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,555 hrs · 19,518 cycles

AFT EMERGENCY EXIT CEILING LIGHT INOP. (FLT 5782) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,413 hrs · 19,402 cycles

NR 3 CEILING LEVEL EMERGENCY FLOODLIGHT INOP. (FLT 6562) REPLACED THE NR 3 CEILING EMERGENCY FLOOD LIGHT IAW AMM 33-51-16.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,362 hrs · 19,354 cycles

THE OVERHEAD EMERGENCY LIGHT INOP. (FLT 6757) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,115 hrs · 19,164 cycles

CEILING LEVEL EMERGENCY FLOOD LIGHT INOP. (FLT 6259) RELAMPED EMERGENCY LIGHT.

Part: CONTROL UNIT — FALSE INDICATION (TE FLAP) · airframe 22,651 hrs · 18,804 cycles

FLAPS APPEARED TO MOVE UNCOMMANDED. (FLT 6724) REPLACED FECU.

Part: WINDOW — CRACKED (COCKPIT) · airframe 22,345 hrs · 18,577 cycles

FLT 6038 - RIGHT WINDOW CRACKED. REPLACED WINDOW.

Part: MECHANISM — OUT OF ADJUST (CABIN DOOR) · airframe 22,235 hrs · 18,492 cycles

FLT 6509 - MAIN CABIN DOOR WILL NOT OPEN FROM THE OUTSIDE. ADJUSTED AND LUBED DOOR MECHANISMS.

Part: DOOR — STICKING (MAIN PAX) · airframe 22,177 hrs · 18,440 cycles

FLT 6633 - MAIN CABIN DOOR DIFFICULT TO OPEN. OPERATIONAL CHECK ACCOMPLISHED, NO DEFECTS NOTED.

Part: HANDLE — LACK OF LUBE (PAX DOOR) · airframe 22,177 hrs · 18,440 cycles

FLT 6694 - MAIN CABIN DOOR WOULD NOT OPEN FROM OUTSIDE. LUBRICATED INTERNAL HANDLE.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 22,050 hrs · 18,342 cycles

FLT 60770 - LEFT WINDSHIELD CRACKED. REPLACED WINDSHIELD.

Part: DOOR — STUCK (MAIN PAX) · airframe 21,918 hrs · 18,238 cycles

FLT 6014 - MAIN CABIN DOOR DIFFICULT TO OPEN FROM OUTSIDE. OPS CHECKS GOOD.

Part: MECHANISM — FROZEN (PAX DOOR) · airframe 21,581 hrs · 17,984 cycles

FLT 5945 - CABIN DOOR WILL NOT OPEN FROM EXTERIOR OF AIRCRAFT. LUBRICATED ACTUATOR MECHANISM AND ADJUSTED STEP ON DOOR HANDLE.

Part: HANDLE — BINDING (PAX DOOR) · airframe 21,304 hrs · 17,773 cycles

FLT 5827 - MAIN DOOR OUTER HANDLE DIFFICULT TO STOW AND OPERATES ABNORMAL. REPLACED PAX DOOR HANDLE.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 21,033 hrs · 17,562 cycles

DURING C-CHECK, FS 280 RBL9 UPPER FLOOR SUPPORT CRACKED. REPAIRED PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,033 hrs · 17,562 cycles

DURING C-CHECK, FS 621 BULKHEAD WEB CRACKED ABOVE LINTEL FITTING. REPAIRED PER REO.

Part: FITTING — CRACKED (FUSELAGE) · airframe 21,033 hrs · 17,562 cycles

DURING C-CHECK, REAR PRESSURE BULKHEAD LINTEL FITTING UPPER AND LOWER INBOARD CORNERS CRACKED. REPAIRED PER REO.

Part: FITTING — CRACKED (FUSELAGE) · airframe 21,033 hrs · 17,562 cycles

DURING C-CHECK, FS 280 RBL9 INBOARD AND OUTBOARD CLIPS CRACKED. REPLACED PER SRM.

Part: WINDOW — CRACKED (COCKPIT) · airframe 20,556 hrs · 17,180 cycles

CAPTAIN'S WINDOW CRACKED AT 35000 FT (6307 09-11-08). REMOVED AND REPLACED LT SIDE WINDOW (CAPTAIN SIDE WINDOW) IAW CRJ MM 56-12-01 AND P/N, NP-139322-11 S/N ON, 08025H1360, S/N OFF: 00031H8684.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 20,526 hrs · 17,156 cycles

CORROSION FOUND ON PAX DOOR LOWER ANGLE. REPLACED LOWER PAX DOOR ANGLE IAW SRM 53-21-13.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 19,591 hrs · 16,319 cycles

FLT 6603 - FIRST OFFICERS WINDSHIELD BROKE ON CLIMB-OUT. REPLACED RIGHT WINDSHIELD IAW MM 56-11-01, P/N OFF 601R33033-10, S/N OFF 00080H3197.

Part: PRIORITY VALVE — MALFUNCTIONED (NLG) · airframe 18,466 hrs · 15,407 cycles

FLT 6650 - NOSE GEAR DISAGREE ON FINAL. REPLACED NLG PRIORITY VALVE IAW AMM 32-33-00. OPS AND LEAK CHECKS GOOD.

Part: ACTUATOR — MALFUNCTIONED (NLG) · airframe 18,466 hrs · 15,407 cycles

FLT 6675 - ON APPROACH, RECEIVED NOSE GEAR DISAGREE AND NOSE GEAR DOOR OPEN WARNING MESSAGES BEFORE NOSE GEAR LOCKED DOWN IN PLACE WITH THREE GREENS. REPLACED NLG EXTEND/RETRACT ACTUATOR IAW CRJ 200 MM 32-33-01. OPS CHECK GOOD.

Part: PRIORITY VALVE — MALFUNCTIONED (MLG) · airframe 18,466 hrs · 15,407 cycles

FLT 5851 - "GEAR DISAGREE" ON TAKEOFF AFTER SELECTING GEAR UP. NO PROBLEMS WITH GEAR ON EXTENSION. REPLACED MLG PRIORITY VALVE IAW CRJ 200 MM 32-32-15.

Part: SKIN — CRACKED (BS 202) · airframe 17,461 hrs · 14,509 cycles

FOUND POSSIBLE CRACK ON UPPER NOSE AREA AT FS 202.75.DAMAGE FOUND TO BE A MAJOR REPAIR. REPAIRED FUSELAGE SKIN IN ACCORDANCE WITH CRJ REO 601R-53-11-1212.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 17,461 hrs · 14,509 cycles

LEFT HORIZONTAL STABILIZER HAS LEADING EDGE DENT AT SECTION 10.91.DAMAGE FOUND TO BE A MAJOR REPAIR. C/W REO 601R-55-12-349. OK FOR SERVICE.

Part: STRUCTURE — DAMAGED (HORIZONTAL STAB) · airframe 17,461 hrs · 14,509 cycles

RIGHT HORIZONTAL STABILIZER HAS A DENT ON THE LEADING EDGE AT SECTION 10.91. DAMAGE FOUND TO BE A MAJOR REPAIR. C/W REO 601R-55-12-348. OK FOR SERVICE.

Part: SKIN — DENTED (BS 169-210) · airframe 17,461 hrs · 14,509 cycles

UPPER FORWARD FUSELAGE BETWEEN FS 169.00 AND FS 210.00 HAS SEVERAL DENTS. DAMAGE FOUND TO BE A MAJOR REPAIR. REPLACED FUSELAGE SKIN BETWEEN FS 169.00 AND FS 193 IAW CRJ SRM 51-42-06 AND REO 601R-53-11-1207.

Part: MOTOR — DEFECTIVE (HYD SYSTEM) · airframe 17,256 hrs · 14,333 cycles

SELECTED GEAR UP AFTER TAKEOFF AND RECEIVED A GEAR DISAGREE AND A NOSE GEAR DOOR OPEN MESSAGE. RAN QRH AND PROBLEM CORRECTED ITSELF. RETURNED TO DEN. REMOVED AND REPLACED THE NR 3A AC MOTOR PUMP IAW CRJ 200 MM 29-12-03. OPS CHECK GOOD WITH NO DEFECTS NOTED, P/N:848847, S/N OFF: MX677647.

Part: MECHANISM — CONTAMINATED (PAX DOOR) · airframe 16,679 hrs · 13,841 cycles

FOUND MAIN CABIN DOOR WILL NOT OPEN FROM INSIDE/OUTSIDE. REMOVED EXCESSIVE LUBRICATION FROM HANDLE MECHANISM. OPERATIONAL CHECKS GOOD.

Part: ANGLE — CRACKED (BS 480) · airframe 16,052 hrs · 13,273 cycles

FS 480 LBL 27 INBOARD ANGLE IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLE PER CRJ200 SRM 51-42-06/51-23-00.

Part: STEP — CRACKED (PAX DOOR) · airframe 16,052 hrs · 13,273 cycles

BOTTOM FOLDING STEP PAX DOOR HAS CRACK JUST ABOVE ACCESS PLATE. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED CRACK IN BOTTOM FOLDING STEP ON PAX DOOR IAW CRJ 200 REO 601R-52-11-1145

Part: INTERCOSTAL — CRACKED (BS 625) · airframe 16,052 hrs · 13,273 cycles

STA 625 RT INTERCOSTAL HAS CRACK IN RADIUS. DISCOVERED DURING C-CHECK INSPECTION. REPLACED INTERCOSTAL CLIP RT STA 625 PER CRJ 200 SRM 51-42-21 PG 3-21.

Part: FRAME — CRACKED (BS 280) · airframe 16,052 hrs · 13,273 cycles

FS 280 WL 79 RBL 9 FRAME LOWER HAS CRACK. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW PART PER CRJ200 REO 601R 53-11-171. ON RBL 9 FS 280.

Part: FRAME — CRACKED (BS 280) · airframe 16,052 hrs · 13,273 cycles

FS 280 WL 79 LBL 9 FRAME/CRACK LOWER. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW ANGLE FILLER PER CRJ200 REO 601R 53-11-171, ON RBL 9 FS 280.

Part: FRAME — CRACKED (BS 280) · airframe 16,052 hrs · 13,273 cycles

FS 280 WL 79 LBL 9 OUTBOARD FRAME CLIP CRACKED. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED FABRICATED INBOARD AND OUTBOARD CLIPS AND 2EA FILLER STRIPS P/N 601R 53-11-171-2/-3 PER CRJ200 REO 601R 53-11-171 REV C AND FULLY COMPLIED WITH SKYWEST FUSELAGE STRUCTURE REPAIR RII 53-900-1001.

Part: INTERCOSTAL — CRACKED (BS 625) · airframe 16,052 hrs · 13,273 cycles

STA 625 LT INTERCOSTAL CRACKED IN RADIUS. DISCOVERED DURING C-CHECK INSPECTION. REPLACED LT INTERCOSTAL AT STATION 625 PER CRJ 200 51-42-21 PG 1-24 PART 601-35012-50 PO 71471.

Part: FRAME — CRACKED (BS 280) · airframe 16,052 hrs · 13,273 cycles

FS 280 WL 79 LBL 9 FRAME CRACKED UPPER. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED PARTS P/N 601R 53-11-138-1 PER CRJ200 REO 601R 53-11-138 AT STA 280 LBL 9 UPPER.

Part: LATCH — LACK OF LUBE (PAX DOOR) · airframe 12,978 hrs · 10,527 cycles

UNABLE TO TURN ON MCD TO OPEN IT. LUBED CABIN DOOR LATCH PINS AS NEEDED. OPERATIONAL CHECK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 12,096 hrs · 9,844 cycles

EXTERIOR EMERGENCY LIGHT JUST FORWARD OF LEFT OVERWING EXIT INOP. RELAMPED EMERGENCY EXTERIOR LIGHT AS NEEDED. OPERATIONAL CHECK GOOD.

Part: SENSOR — MALFUNCTIONED (RT T/E FLAP) · airframe 11,929 hrs · 9,693 cycles

FLAPS FAIL CAUTION MESSAGE AFTER LANDING. REPLACED THE RIGHT WING INBOARD AND OUTBOARD FLAP SKEW DETECTION SENSORS IAW CRJ 200 MM 27-51-15. OPERATIONAL CHECK GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 11,892 hrs · 9,667 cycles

CABIN EMERGENCY LIGHTS, CEILING LIGHTS THE ONE MOST FORWARD IS INOPERATIVE. REPLACED FORWARD ELBP CHANGING ASSY. OPERATIONAL CHECK GOOD.

Part: PCU — MALFUNCTIONED (FLIGHT SPOILERS) · airframe 11,834 hrs · 9,616 cycles

FLT SPOILERONS FAULT MESSAGE. REMOVED AND REPLACED LT INBOARD SPOILERON PCU IN OF WITH AMM 27-62. OPERATIONAL CHECK GOOD.

Part: STRINGER CLIP — CRACKED (BS 280) · airframe 13,185 hrs · 10,705 cycles

STATION 280 LBL 9.00' INBOARD CLIP CRACKED AT TOP RADIUS; RBL 9.00' INBOARD AND OUTBOARD CLIP CRACKED AT TOP RADIUS, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW CLIPS AT STA 280 RBL 9.0 INBD SIDE AND AT STA 280 RBL 9.0 INBD AND OTBD IAW CRJ200 SRM 51-10-06 PG 3 51-42-06 PG 15 AND 51-42-20 PG 1.

Part: CLIP — CRACKED (BS 625) · airframe 13,185 hrs · 10,705 cycles

LT AND RT SUPPORT CLIPS ON AFT SIDE OF REAR PRESSURE BULKHEAD AT FS 625.00 ARE CRACKED, ITEM FOUND AT C-CHECK INSPECTION. NEW CLIPS INSTALLED IAW CRJ 200 SRM 51-42-06; 51-42-21 AND REO601R-53-61-985.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 11,826 hrs · 9,609 cycles

CAPTAIN'S WINDSHIELD SHATTERED WHILE AT FL340. REPLACED CAPTAIN'S WINDSHIELD ASSY PER CRJ MM 56-00-00, 56-11-01, 56-12-01. OPERATIONAL CHECK GOOD. P/N NP139321-11, S/N OFF 01043H9715.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 11,597 hrs · 9,423 cycles

RECEIVED SMOKE TOILET MESSAGE DURING INITIAL CLIMBOUT. F/A VERIFIED NO SMOKE IN LAV. REMOVED AND REPLACED LAV SMOKE DETECTOR IAW CRJ AMM 26-16-01, OPERATIONAL CHECK GOOD. P/N OFF P90-421R3, S/N OFF 07589.

Part: ENGINE — SMOKE (RIGHT) · airframe 11,526 hrs · 9,361 cycles

AFTER APPLYING TAKEOFF THRUST, NOTICED A STRONG OIL SMOKE SMELL IN THE AIRCRAFT. SMELL DISAPPEARED AFTER SEVERAL MINUTES IN FLIGHT. RECEIVED SMOKE TOILET MESSAGE DURING INITIAL CLIMBOUT. REMOVED AND REPLACED RIGHT ENGINE. OPERATIONAL CHECK GOOD.

Part: LIGHT — SMOKE (CABIN) · airframe 11,510 hrs · 9,351 cycles

ON CLIMBOUT SMOKE TOILET CAUTION MESSAGE ILLUMINATED. SMOKE ALARM SOUNDED AND SMOKE VISIBLE IN LAV AREA. RETURNED TO KCRW. REPLACED LAV OVERHEAD LIGHT ASSY PER CRJ MM CH 33. OPERATIONAL CHECK GOOD.

Part: TRIM SWITCH — STUCK (COCKPIT) · airframe 11,351 hrs · 9,224 cycles

CAPTAINS SIDE YOKE STAB TRIM STICKY DURING OPERATIONS. REMOVED AND REPLACED CAPTAINS SIDE STAB TRIM SWITCH, OPERATIONAL CHECK GOOD IAW CRJ MM 27-41-05.

Part: PIN — BROKEN (PAX DOOR) · airframe 11,351 hrs · 9,224 cycles

MAIN CABIN DOOR WILL NOT OPEN FROM THE INSIDE WHEN CLOSED. REPLACED BROKEN PIN INSIDED THE INNER/OUTER DOOR HANDLE MECHANISM PER CMM 52-11-03 AND AMM 52-11-02. DOOR OPERATION CHECKS GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 11,318 hrs · 9,196 cycles

OUTBOARD AND INBOARD SPOILER FAULT STATUS. REPLACED NR 2 SECU IAW CRJ AMM REF CHAP 27-60-00. OPERATIONAL CHECK GOOD.

Part: TRIM SWITCH — MALFUNCTIONED (COCKPIT) · airframe 10,789 hrs · 8,768 cycles

F/O'S TRIM SWITCH WILL NOT ADVANCE TRIM NOSE UP. REMOVED AND REPLACED F/O'S TRIM SWITCH, OPERATIONAL CHECK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 10,615 hrs · 8,605 cycles

REAR RIGHT EMERGENCY LIGHTS INOPERATIVE. RELAMPED AFT EMERGENCY INTERIOR OVERHEAD LIGHT IAW CRJ AMM REF CHAP 33-50-00, OPERATIONAL CHECK GOOD.

Part: STICK SHAKER — INTERMITTENT (CAPTAINS) · airframe 10,576 hrs · 8,575 cycles

CAPTAINS STICK SHAKER INTERMITTENT. REPLACED CAPTAINS STICK SHAKER CONNECTOR. OPERATIONAL CHECK GOOD.

Part: CONNECTOR — DAMAGED (TE FLAP IND) · airframe 9,047 hrs · 7,274 cycles

FLAPS EICAS PAGE (FLT CTRL) SHOWS FLAP DISCREP F20 INDICATES = 20 LT, 16 RT, F8 = 8 LT, 4 RT, F45 = 45 LT, 41 RT, F30 = 30 LT, 26 RT. NO ABNORMAL MSGS. A/C FLIES STRAIGHT. NO HANDLING PROBLEMS. FOUND CONNECTOR PIN HOLE 40 ON PLUG 211 WORN AND WILL NOT RETAIN PIN PROPERLY, CAUSING ERRATIC FLAP INDICATION (POSITION). REPLACED PLUG CONNECTOR P211 IAW WM 27-17-10. ACCOMPLISHED OPS, CHECK OF FLAP POSITION TRANSMITTER IAW MM 27-55-01 AFTER REPLACEMENT OF CANNON PLUG P11 ON JB9.

Part: HANDLE — CORRODED (ESCAPE HATCH) · airframe 8,044 hrs · 6,340 cycles

CREW ESCAPE HATCH OUTER HANDLE SHAFT CORRODED. DISCOVERED DURING C-CHECK INSPECTION. CREW ESCAPE HATCH OUTER HANDLE REPLACED, REF. CMM 52-22-03. PN: H3419-33

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 8,044 hrs · 6,340 cycles

FS 484 RT INTERCOSTAL IB ANGLE RBL 27 CRACKED. (DISCOVERED DURING C-CHECK INSPECTION). ANGLE REPLACED IAW CRJ REO 601R-53-41-059 REV ''A''.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 8,044 hrs · 6,340 cycles

FS 484 LT INTERCOSTAL OB FLANGE LBL 36 AND ANGLE LBL 27 CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) REPAIRED INTERCOSTAL IAW CRJ REO 601R-53-41-059 REV. ''A''. REPAIR ANGLE P/N: S6144-14

Part: FLOOR SUPPORT — DAMAGED (CARGO BAY) · airframe 8,044 hrs · 6,340 cycles

CARGO PIT; STEP SUPPORT IS CRACKED AND BROKEN OUT ALONG LENGTH OF IB SIDE. (DISCOVERED DURING C-CHECK INSPECTION) NEW CARGO PIT STEP PLATE SUPPORT INSTALLED IAW CRJ AMM 20-21-00 AND CRJ SRM 51-41-02. PN: 601R35205-37

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 8,044 hrs · 6,340 cycles

FS 280 RT FLOORBEAM RBL 9.0 IB AND OB ATTACH ANGLES CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) INBOARD AND OUTBOARD ANGLES AT FS 280 RT RBL 9.0 FLOORBEAM REPLACED IAW CRJ SRM 51-40-11. P/N: 601R31113-58

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 8,044 hrs · 6,340 cycles

FS 621 RT FLOOR SUPPORT ANGLE CRACK. (DISCOVERED DURING C-CHECK INSPECTION) REPAIRED ANGLE IAW CRJ REO 601R-53-61-117 REV ''A'' & RII 53-401.PN: 601R-53-61-117-2

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 8,044 hrs · 6,340 cycles

FS 280 LT FLOORBEAM LBL 9.0 IB AND OB ATTACH ANGLES CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) INBOARD AND OUTBOARD ANGLES AT FS 280 LBL 9 FLOORBEAM REPLACED IAW CRJ SRM 51-40-11. P/N: 601R31113-57

Part: SWITCH — MALFUNCTIONED (STAB TRIM) · airframe 8,003 hrs · 6,300 cycles

STAB TRIM CHANNEL 1 INOPERATIVE. REMOVED AND REPLACED FO'S STAB TRIM DISCONNECT SWITCH AND STAB TRIM PANEL IAW CRJ MM 27-41-15. OPS CHECKS GOOD. PANEL PN: 601R51707-9 SWITCH PN: 996-0013

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,477 hrs · 5,834 cycles

CENTER ROW MID EMERGENCY LIGHT INOP. RE-LAMPED CENTER ROW MID EMERGENCY LIGHT AS REQUIRED. OPS CHECK GOOD.

Part: CONTROL UNIT — FAILED (SPOILERS) · airframe 7,399 hrs · 5,768 cycles

ON TAXI OUT OUTBOARD GROUND SPOILERS, FLIGHT SPOILERS, SPOILERONS CAUTION MESSAGES. REMOVED AND REPLACED NR 1 SECU. OPS CHECKS GOOD. S/N OFF 1254.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZONTAL STAB) · airframe 7,082 hrs · 5,468 cycles

STAB FAIL MESSAGE RECEIVED ON EICAS. REMOVED AND REPLACED HSTCU WITH SERVICEABLE UNIT. S/N OFF 865.

Part: TRIM SWITCH — MALFUNCTIONED (CAPTAIN'S) · airframe 6,030 hrs · 4,613 cycles

MACH TIRM/STAB TRIM DISCONNECTED IN FLIGHT. REPLACED CAPTAIN'S TRIM SWITCH. DISCONNECT SWITCH OPS CHECKS GOOD IAW CRJ 27-41-30. PN OFF 996-0013.

Part: SMOKE — DETECTED (CABIN) · airframe 5,988 hrs · 4,591 cycles

ON CLIMB OUT OF FAT, THE FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN. RETURNED TO FAT. CHECKED ENGINE OIL SERVICE, FOUND SATISFACTORY. RAN ENGINES AT CRUISE FOR 5 MIN AT RUN-UP AREA AND COULD NOT FURTHER DUPLICATE, FOUND SATISFACTORY.

Part: ECU — MALFUNCTIONED (SPOILER) · airframe 5,420 hrs · 4,097 cycles

SPOILER FAULT STATUS MESSAGE AND INBOARD GROUND SPOILER FAULT STATUS MESSAGE ON TAXI OUT. RESET CIRCUIT BREAKERS 1N8, 2N8, 4A3 AND 4A2. DID NOT RESET. RETURNED TO THE GATE. REPLACED SECU IAW 27-61-05. OPS CHECK GOOD.

Part: PRESSURE SWITCH — DIRTY (APU) · airframe 4,433 hrs · 3,234 cycles

APU OIL PRESSURE MESSAGE IN FLIGHT. DIVERTED TO FAT. CHANGED OIL AND FILTER AND CLEANED PRESSURE SWITCH. OPS CHECKED GOOD.

Part: CONTROL UNIT — OUT OF RIG (NLG STEERING) · airframe 3,816 hrs · 2,654 cycles

LOST NOSE WHEEL STEERING AND STEERING INOP CONDITION MESSAGE ILLUMINATED DURING TAKEOFF ROLL. ABORTED TAKEOFF AT APPROXIMATELY 60 KTS AND RETURNED TO GATE. PERFORMED RIGGING OF ECU AS PER MM 32-51-10. SYSTEM OPS CHECKS GOOD ON TAXI TEST.

Part: IDG — FAILED (NR 2 ENGINE) · airframe 3,816 hrs · 2,654 cycles

IDG NR 2 CAUTION MESSAGE. TAKEOFF DISCONTINUED. REMOVED AND REPLACED RT IDG. NO LEAKS NOTED. OPS CHECKS GOOD. S/N ON 1248GEN3627, S/N OFF 0812GEN1261.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILERON) · airframe 3,489 hrs · 2,311 cycles

O/B GND SPLR FAULT ADVISORY MESSAGE ACCOMPANIED BY SPOILERONS, FLT SPOILERS AND GND SPOILERS CAUTION MESSAGES. RETURNED TO GAT. SWAPPED NR 1 AND NR 2 SECU'S FROM SIDE TO SIDE. PERFORMED BIT TEST AND SYSTEM RESET TEST. GROUND OPS CHECK GOOD AT THIS TIME.

Part: WIRE — BROKEN (CARGO BAY) · airframe 3,489 hrs · 2,311 cycles

STAB TRIM CH2 WILL NOT ENGAGE. REPAIRED WIRE CD91A22 AT CONNECTOR J6CD IN CARGO BAY. STAB TRIM OPS CHECK GOOD IAW AMM 27-41-00.

Part: ECU — MALFUNCTIONED (SPOILER) · airframe 3,276 hrs · 2,111 cycles

OUTBOARD GROUND SPOILER FAULT STATUS MESSAGE ON EICAS. INSPECTED LEFT AND RIGHT OUTBOARD SPOILERON PCU. OHMS CHECK NORMAL. CLEARED FAULTS. GROUND CHECKS NORMAL. AS A PRECAUTION (FAULT CODE 05, 04, FF, 13) REPLACED SECU NR 1 IAW 27-61-05. GROUND CHECK NORMAL.

Part: CONTROL HANDLE — FAULTY (COCKPIT) · airframe 3,263 hrs · 2,097 cycles

ON TAKEOFF, FLAPS FAIL CAUTION MESSAGE APPEARED WHEN ATTEMPTING TO RETRACT FLAPS FROM 20 DEGREES TO 8 DEGREES. VISUAL INSPECTION SHOWS FLAPS AT 20 DEGREES. COMPLIED WITH AD 98-20-01 PER AD COMPLIANCE FORM. FOUND FAULT CODE ON FLAP CONTROL LEVER. REMOVED AND REPLACED FLAP CONTROL LEVER IAW CRJ 27-51-01. OPS CHECK GOOD. P/N ON 7-45500-1, S/N ON 0067, S/N OFF 0054.

Part: FLAP — MALFUNCTIONED (WING) · airframe 3,236 hrs · 2,075 cycles

AFTER LANDING, DURING RETRACTION OF FLAPS, RECEIVED FLAPS FAIL CAUTION MESSAGE WHEN FLAP HANDLE WAS MOVED FROM 20 DEGREES TO 8 DEGREES. FLAPS WOULD NOT GO OUT OF 20 DEGREES. VISUAL INSPECTION CONFIRMS FLAPS AT 20 DEGREES. COMPLIED WITH AD 98-20-01. ALL CHECK GOOD. NO DEFECTS NOTED.

Part: COMPUTER — MALFUNCTIONED (COCKPIT) · airframe 2,515 hrs · 1,571 cycles

WITH AUTOPILOT ENGAGED (INFLIGHT OPERATIONS) BOTH CONTROL COLUMNS JERK FORWARD AND BACK INTERMITTENTLY DURING FLIGHT. THE FO'S INCLINOMETER WOULD ALSO DEFLECT QUICKLY LEFT AND RIGHT THEN RETURN TO CENTER POSITION. THEN IT WOULD REPEAT. REMOVED AND REPLACED NR 1 AHC-85E. AP SYSTEM OPS CHECK GOOD IAW MM 22-10-00 AND AHC OPS CHECK GOOD IAW 34-21-00. COMPLIED WITH CAT II AS REQUIRED. P/N: 622-9336-402 S/N ON: 5GNX P/N OFF: 622-9336-400 S/N OFF: 468L

Part: BPSU — DEFECTIVE (T/E FLAP) · airframe 2,443 hrs · 1,528 cycles

FLAPS FAIL CAUTION MESSAGE WHEN SELECTING FLAPS OUT OF ZERO. LEFT SIDE FAILED AT 4 DEGREES, RIGHT SIDE FAILED AT 3 DEGREES.REPLACED RIGHT BRAKE POSITION SENSING UNIT IAW 27-51-10. OPS CHECK GOOD.

Part: BPSU — DEFECTIVE (T/E FLAP) · airframe 2,558 hrs · 1,597 cycles

ON FINAL APPROACH WHILE SELECTING FLAPS FROM 20 TO 30 DEGREES "FLAPS HALF SPEED" STATUS MESSAGE ILLUMINATED.PULLED CB F4 ON CB PANEL 1 AND 2, RESET AND CYCLED FLAPS SEVERAL TIMES. OPS CHECKS GOOD. "FLAPS HALF SPEED" STATUS MESSAGE ILLUMINATED AGAIN ON FINAL APPROACH. REPLACED RIGHT BPSU IAW 27-51-10. OPS CHECK GOOD.

Part: PUMP — FAILED (RT ENG HYD SYS) · airframe 2,140 hrs · 1,343 cycles

30 SECONDS AFTER GEAR WAS SELECTED DOWN, NR 2 HYDRAULIC PRESSURE MESSAGE HYDRAULIC LEVEL IN NR 2 INDICATED 0 PERCENT FLUID. AFTER SHUTDOWN LEVEL ROSE TO 15 PERCENT. EDP RUNNING DRY FOR 5 MINUTES. REPLACED RIGHT ENGINE HYDRAULIC PUMP IAW MM 29-11-01. PN ON 887055 SN ON MX625954 SN OFF MX555746. SERVICED WITH 4 QTS SKYDROL. RAN RIGHT ENGINE AND CYCLED HYDRAULIC COMPONENTS. NO LEAKS NOTED. OPS CHECK GOOD.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 1,873 hrs · 1,175 cycles

ON DESCENT INTO DEN CAPTAINS WINDSHIELD SHATTERED, APPEARED TO BE MIDDLE LAYER. REPLACED CAPTAINS WINDSHIELD IAW CRJ MM 56-11-01 AND SKYWEST CARD RII 56-401. OPS CHECK GOOD ON GROUND. P/N ON: NP-139321-9 S/N ON: 01043H9715 P/N OFF: 601R33033-9 S/N OFF: 00111H5787.

Part: WARNING SYSTEM — ACTIVATED (STALL WARNING) · airframe 794 hrs · 488 cycles

STALL FAIL MESSAGE ON TAKEOFF ROLL. ABORTED TAKEOFF. PERFORMED STALL WARNING TEST AND CHECK STALL VANES. OPS CHECK GOOD. COULD NOT DUPLICATE.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 479 hrs · 284 cycles

ON TAKEOFF ROLL, RECEIVED A STALL FAIL CAUTION MESSAGE AND CONFIG SPOILERS WARNING. EXACTLY SAME THING OCCURRED ON SECOND TAKEOFF ATTEMPT. RESET SECUS AND POWERED DOWN AIRCRAFT. OPS CHECKED SPOILERS, ALL SYSTEMS CHECK GOOD.AFTER SECOND ATTEMPT, CLEARED MEMORY IN STALL WARNING COMPUTER. PERFORMED TWO HIGH SPEED TAXIS WITH NO FURTHER DISCREPANCIES. PERFORMED A TEST FLIGHT WITH NO DISCREPANCIES.