N935SW

Part: VANE — CHAFED (TE FLAP) · airframe 37,681 hrs · 32,822 cycles

RT INBD FLAP CENTER OUTBD FLAP VANE CAP IS CHAFED. (C-CHECK) RO: 07/29/2018 REMOVED AND REPLACED RT INBOARD FLAP CENTER VANE CAP IAW SRM.

Part: VANE — CHAFED (TE FLAP) · airframe 37,681 hrs · 32,822 cycles

RT INBD FLAP OUTBD FLAP VANE CAP IS CHAFED. (C-CHECK) RO: 07/29/2018. REMOVED AND REPLACED RT INBOARD FLAP OUTBOARD VANE CAP IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,681 hrs · 32,822 cycles

FRAME FS333 CRACKED LOCATED BETWEEN STR 0 AND STR 1L. (C-CHECK) RO: 07/29/2018. REMOVED AND INSTALLED NEW REPLACEMENT FRAME, P/N: 601R32004-41 AT LT FS 333.00 FRAME FROM STR 0 TO APPROXIMATELY STR 3 IAW SRM. COMPLIED WITH THE PRESSURIZATION OF THE AIRCRAFT IAW AMM. NO LEAKS NOTED.

Part: PANEL — CORRODED (FUSELAGE) · airframe 37,681 hrs · 32,822 cycles

THE LT FLOOR SILL PANEL HAS MULTIPLE SPOTS OF CORROSION AROUND NUTPLATE HOLES FROM APPROX FS 424.00 TO APPROX FS 529. (C-CHECK) RO: 07/29/2018 BLENDED CORROSION TO A SMOOTH CONTOUR ON THE LT FLOOR SILL PANEL AROUND NUTPLATE HOLES FROM APPROX FS 424.00 TO APPROX FS 529 IAW REO. PRESSURE CHECK GOOD.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 37,681 hrs · 32,822 cycles

FS559.00 +80 TO FS559.00+112 APPROX. RIGHT SIDE SILL HAS CORROSION. (C-CHECK) RO: 07/29/2018 REMOVED CORROSION ON RT FLOOR SILL AT FS 559.00+80 TO FS559+112 IAW SRM AND REO.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 37,681 hrs · 32,822 cycles

FS 280.00 BETWEEN LBL 9.00 AND RBL 9.00 SUPPORT ANGLE PANEL HAS CORROSION. (C-CHECK) RO: 07/29/2018 REMOVED AND REPLACED FLOOR SUPPORT ANGLE BETWEEN FS 280.00 BETWEEN LBL 9.00 AND RBL 9.00 IAW SRM.

Part: VANE — DENTED (TE FLAP) · airframe 33,968 hrs · 28,703 cycles

RIGHT OTBD FLAP VANE WAS DENTED AT WING STA 178.00. R & R OTBD RT FLAP VANE.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 33,968 hrs · 28,703 cycles

AVIONICS BAY INTERCOSTAL FWD OF FS 349.00 AT STR 25L HAS CORROSION. R & R INTERCOSTAL ON STR 25 LT BETWEEN FS 333.00-FS349.00. WITH NEW PART, PN: 601R31049-105 IAW SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 33,968 hrs · 28,703 cycles

AVIONICS BAY, U CHANNEL, LOCATED BETWEEN FS 349.0-FS 333.0 AND STR 25R-STR 24R HAS CORROSION. REPLACED, INSTALLED U-CHANNEL WITH NEW PART, PN: 601R43210-19 IAW SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 33,968 hrs · 28,703 cycles

CORROSION FOUND ON FLOOR STRAP AT FS 589 FROM LBL 8-LBL 26. INSTALLED NEW STRAP IAW SRM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 33,968 hrs · 28,703 cycles

CARGO DOOR OPENING FLOOR SILL HAS CORROSION AROUND NUT PLATE HOLES. R & R CARGO DOOR LOWER FLOOR SILL IAW REO.

Part: SKIN — CHAFED (LT AILERON) · airframe 33,968 hrs · 28,703 cycles

LEFT AILERON OTBD LOWER L/E SKIN CHAFED. R & R LT AILERON OTBD LOWER L/E SKIN PN CC670-13054-1 IAW SRM.

Part: SHROUD — CHAFED (RT AILERON) · airframe 33,968 hrs · 28,703 cycles

RT AILERON LOWER CENTER L/E CHAFED. R & R RT AILERON LOWER CENTER L/E SHROUD, PN 601R13031-148 IAW SRM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,735 hrs · 27,439 cycles

VARIOUS CABIN EMERGENCY LIGHTS ARE INOPERATIVE. R & R BATTERY PACK NR 2 IAW AMM. OPS CHECKED GOOD AT THIS TIME. PN ON AD-2013-1A, SN ON 84021; PN OFF AD-2013-1A, SN OFF 72083.

Part: STRUCTURE — DEFORMED (RT NACELLE) · airframe 31,721 hrs · 26,408 cycles

DEFORMATION IN THE L/E OF THE STARBOARD ENGINE PYLON. SOME PAINT MISSING, CAUSE UNKNOWN. COMPLIED WITH AND REPAIRED IAW REO.

Part: THRUST REVERSER — OUT OF ADJUST (RIGHT) · airframe 31,080 hrs · 25,792 cycles

RIGHT THRUST REVERSER UNLOCK CAUTION FAILED. ADJUSTED THE TWO THRUST REVERSER ALIGNMENT HOLES IAW AMM AND THEN LUBRICATED THE BALLSCREW ACTUATORS IAW AMM. OPS CHECKED GOOD AT THIS TIME

Part: ADG — UNWANTED DEPLOY · airframe 30,394 hrs · 25,272 cycles

THE ADG DEPLOYED IN FLIGHT. THE AC ELECTRICAL SYSTEM DID NOT FAIL. F/O REPLACED ADG CONTROL PANEL AND RESTOWED ADG.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 30,444 hrs · 25,308 cycles

F/A'S EMERGENCY FLASHLIGHT IS INOPERATIVE. R & R THE FLASHLIGHT BATTERY IAW CMM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,124 hrs · 25,067 cycles

FOUR BULBS IN FRONT OVERHEAD EMERGENCY EXIT LOCATOR SIGN AND BULBS IN AFT SIGN ARE INOPERATIVE. REPLACED WITH NEW BULBS IN FRONT OVERHEAD EMERGENCY EXIT LOCATOR SIGN IAW AMM.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,021 hrs · 24,973 cycles

AFT AND ROW 5 CEILING EMERGENCY LIGHT INOPERATIVE. C-CHECK, R & R NR 4 EMERGENCY BATTERY PACK FUSE IAW AMM.

Part: CONNECTOR — OUT OF POSITION (EMERGENCY LIGHT) · airframe 30,021 hrs · 24,973 cycles

EMERGENCY LIGHTS EXIT SIGN ON THE GALLEY TRIM PANEL DOES NOT WORK. C-CHECK, REPOSITION WIRE CONNECTORS TO PROPER LOCATION IAW AMM.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 30,021 hrs · 24,973 cycles

EMERGENCY LIGHTS RIGHT EMERGENCY DOOR AFT EXTERIOR LIGHT DOES NOT WORK. C-CHECK, RESEATED CONNECTORS, OPS CHECK GOOD IAW AMM.

Part: CONNECTOR — OUT OF POSITION (EMERGENCY LIGHT) · airframe 30,021 hrs · 24,973 cycles

EMERGENCY LIGHT EXIT SIGN ON THE SERVICE DOOR TRIM PANEL DOES NOT WORK. C-CHECK, REPOSITION WIRE CONNECTORS TO PROPER LOCATION IAW AMM.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 30,021 hrs · 24,973 cycles

EMERGENCY LIGHT EXIT SIGN ON THE WARDROBE DOES NOT WORK. C-CHECK, RESEATED CONNECTORS OP CHECKED GOOD IAW AMM.

Part: HINGE — GOUGED (PAX DOOR) · airframe 30,021 hrs · 24,973 cycles

PASSENGER DOOR HINGE HALF, DOOR SIDE, LUG 21, FROM THE AFT END GOUGED. C-CHECK, BLENDED GOUGE ON PAX DOOR HINGE IAW REO.

Part: HINGE — GOUGED (PAX DOOR) · airframe 30,021 hrs · 24,973 cycles

PASSENGER DOOR HINGE HALF, DOOR SIDE, LUG 8 FROM AFT END, GOUGED. C-CHECK, BLENDED GOUGE ON PAX DOOR HINGE IAW REO.

Part: HINGE — GOUGED (PAX DOOR) · airframe 30,021 hrs · 24,973 cycles

PASSENGER DOOR HINGE HALF, DOOR SIDE, LUG 20, FROM THE AFT END GOUGED. C-CHECK, BLENDED GOUGE ON PAX DOOR HINGE IAW REO.

Part: HINGE — GOUGED (PAX DOOR) · airframe 30,021 hrs · 24,973 cycles

PASSENGER DOOR HINGE HALF, DOOR SIDE, LUG 2, FROM AFT, END GOUGED. C-CHECK, BLENDED GOUGE ON PAX DOOR HINGE IAW REO.

Part: HINGE — GOUGED (PAX DOOR) · airframe 30,021 hrs · 24,973 cycles

PASSENGER DOOR HINGE HALF, DOOR SIDE, LUG 27, FROM AFT END, GOUGED. C-CHECK, BLENDED GOUGE ON PAX DOOR HINGE IAW REO.

Part: HINGE — GOUGED (PAX DOOR) · airframe 30,021 hrs · 24,973 cycles

PASSENGER DOOR HINGE HALF, DOOR SIDE, LUG 18, FROM THE AFT END GOUGED. C-CHECK BLENDED GOUGE ON PAX DOOR HINGE IAW REO.

Part: HINGE — GOUGED (PAX DOOR) · airframe 30,021 hrs · 24,973 cycles

PASSENGER DOOR HINGE HALF, DOOR SIDE, LUG 15, FROM AFT END, GOUGED. C-CHECK, BLENDED GOUGE ON PAX DOOR HINGE IAW REO.

Part: HINGE — GOUGED (PAX DOOR) · airframe 30,021 hrs · 24,973 cycles

PASSENGER DOOR HINGE HALF, DOOR SIDE, LUG 17, FROM AFT END, GOUGED. C-CHECK, BLENDED GOUGE ON PAX DOOR HINGE IAW REO.

Part: HINGE — GOUGED (PAX DOOR) · airframe 30,021 hrs · 24,973 cycles

PASSENGER DOOR HINGE HALF (DOOR SIDE) LUG 10, FROM AFT END, GOUGED. C-CHECK, BLENDED GOUGE ON PAX DOOR HINGE IAW REO.

Part: HINGE — GOUGED (PAX DOOR) · airframe 30,021 hrs · 24,973 cycles

PASSENGER DOOR HINGE HALF, DOOR SIDE, LUG 11, FROM THE AFT END GOUGED. C-CHECK, BLENDED GOUGE ON PAX DOOR HINGE IAW REO.

Part: HINGE — GOUGED (PAX DOOR) · airframe 30,021 hrs · 24,973 cycles

PASSENGER DOOR HINGE HALF, DOOR SIDE, LUG 12, FROM THE AFT END GOUGED. C-CHECK, BLENDED GOUGE IAW REO.

Part: HINGE — GOUGED (PAX DOOR) · airframe 30,021 hrs · 24,973 cycles

PASSENGER DOOR HINGE HALF, DOOR SIDE, LUG 3, FROM THE AFT END GOUGED. C-CHECK, BLENDED GOUGE ON PAX DOOR HINGE IAW REO.

Part: HINGE — GOUGED (PAX DOOR) · airframe 30,021 hrs · 24,973 cycles

PASSENGER DOOR HINGE HALF, DOOR SIDE, LUG 4, FROM THE AFT END GOUGED. C-CHECK, BLENDED GOUGE ON PAX DOOR HINGE IAW REO.

Part: HINGE — GOUGED (PAX DOOR) · airframe 30,021 hrs · 24,973 cycles

PASSENGER DOOR HINGE HALF (DOOR SIDE) LUG 19, FROM AFT END, GOUGED. C-CHECK, RO: BLENDED GOUGE ON PAX DOOR HINGE IAW REO.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 30,021 hrs · 24,973 cycles

FS 280 FLOORBEAM ANGLE CRACKED AT LBL 9 AND RBL 9. C-CHECK, REPLACED AFT FLOOR ANGLE IAW SRM.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 30,021 hrs · 24,973 cycles

FS 280, AFT LOWER REPAIR ANGLE OTBD OF RBL 9 IS CRACKED. C-CHECK, REPLACED, FS 280 AFT LOWER REPAIR ANGLE OTBD OF RBL 9 IAW SRM.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 30,021 hrs · 24,973 cycles

FS 280, AFT UPPER SPLICE ANGLE OTBD OF RBL 9 IS CRACKED. C-CHECK, R & R FS 280 UPPER SPLICE ANGLES 601R-53-11-136-4 AND 601R-53-11-136-1 OTBD OF RBL 9 IAW SRM.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 30,021 hrs · 24,973 cycles

FS 280 COCKPIT FLOORBEAM ANGLE CRACKED. C-CHECK, INSTALLED NEW FLOORBEAM ANGLE IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 409) · airframe 30,021 hrs · 24,973 cycles

CORROSION AROUND FASTENER HOLE ON FLOOR SUPPORT BS 409, LBL36. C-CHECK, BLENDED CORROSION IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 409) · airframe 30,021 hrs · 24,973 cycles

NUMEROUS AREAS OF CORROSION AROUND FASTENER HOLES ON FLOOR SUPPORT BS 409+64 - 409+128. C-CHECK, BLENDED CORROSION IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 409) · airframe 30,021 hrs · 24,973 cycles

NUMEROUS AREAS OF CORROSION AROUND FASTENER HOLES ON FLOOR SUPPORT BS 409+15 - 409+64. C-CHECK, BLENDED CORROSION IAW REO.

Part: STOP FITTING — GOUGED (DOOR FRAME) · airframe 30,021 hrs · 24,973 cycles

LEFT EMERGENCY EXIT DOOR FRAME FWD CENTER STOP FITTING NICKED AND GOUGED. C-CHECK, REPAIRED STOP FITTING IAW EA.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 30,021 hrs · 24,973 cycles

FLOORBEAM INBD AND OTBD ANGLES CRACKED AT BS 280, RBL 9. C-CHECK, REPLACED INBD AND OTBD ANGLES IAW SRM.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 30,021 hrs · 24,973 cycles

FLOORBEAM INBD AND OTBD ANGLES CRACKED AT BS 280, LBL 9. C-CHECK, REPLACED INBD AND OTBD ANGLES IAW SRM.

Part: STOP FITTING — NICKED (DOOR FRAME) · airframe 30,021 hrs · 24,973 cycles

LEFT EMERGENCY EXIT DOOR FRAME FWD LOWER STOP FITTING NICKED. C-CHECK, REPAIRED LOWER STOP FITTING IAW EA.

Part: FLOOR SUPPORT — CORRODED (BS 360) · airframe 30,021 hrs · 24,973 cycles

CORROSION AROUND FASTENER HOLE ON FLOOR SUPPORT AT BS 360, LBL36. C-CHECK, BLENDED CORROSION IAW REO.

Part: STOP FITTING — GOUGED (DOOR FRAME) · airframe 30,021 hrs · 24,973 cycles

LEFT EMERGENCY EXIT DOOR FRAME FWD TOP STOP FITTING NICKED AND GOUGED. C-CHECK, REPAIRED STOP FITTING IAW EA.

Part: FLOORBEAM — CORRODED (BS 319) · airframe 30,021 hrs · 24,973 cycles

FLOORBEAM TEE CORRODED AT BS 319.0, RBL 36. C-CHECK, REPLACED FLOORBEAM TEE IAW SRM.

Part: STOP FITTING — GOUGED (DOOR FRAME) · airframe 30,021 hrs · 24,973 cycles

LEFT EMERGENCY EXIT AFT CENTER STOP FITTING GOUGED. C-CHECK, REPAIRED STOP FITTING IAW EA.

Part: STIFFENER — CRACKED (BS 409) · airframe 30,021 hrs · 24,973 cycles

BS 409.0 +128 VERTICAL POST AT RBL 18.0 IS CRACKED ON INBD SIDE. C-CHECK, REPLACED FS 409.0 +128 VERT POST AT RBL 18.0 IAW SRM.

Part: ATTACH FITTING — CHAFED (WING TO FUSELAGE) · airframe 30,021 hrs · 24,973 cycles

RT WING TO FUSELAGE ATTACH FITTING AT BS 473.15 CHAFED AT OTBD FWD CORNER. C-CHECK, REPAIRED ATTACH FITTING IAW EA.

Part: LEVER — CHAFED (PAX DOOR) · airframe 30,021 hrs · 24,973 cycles

PASSENGER DOOR FWD PULL-IN LEVER CHAFED. C-CHECK, BLENDED CHAFE IAW REO.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 30,021 hrs · 24,973 cycles

LEFT WING INBD FLAP, INBD SIDE VANE L/E HAS CHAFED MARK. C-CHECK, BLEND CHAFE IAW REO.

Part: BULKHEAD — CRACKED (BS 202) · airframe 30,021 hrs · 24,973 cycles

PRESSURE BULKHEAD BS 202.75 HAS A CRACK AT PARKING BRAKE CABLE HOLE. C-CHECK, REPAIRED BULKHEAD IAW REO.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 30,021 hrs · 24,973 cycles

PASSENGER DOOR INNER CLOSE OUT SKIN PANEL BELOW UPPER FOLDING STEP HAS AFT ANGLE BRACKET CRACKED. C-CHECK, R & R REPAIRED BRACKET IAW SRM.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 30,021 hrs · 24,973 cycles

LEFT WING INBD FLAP, OTBD SIDE VANE L/E CHAFED. C-CHECK, BLEND CHAFE IAW REO.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 30,021 hrs · 24,973 cycles

PAX DOOR AFT DRAG ANGLE IS CRACKED AT PREVIOUS REPAIR SPLICE. C-CHECK, REMOVED AND REPLACED AFT DRAG ANGLE IAW SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 29,959 hrs · 24,931 cycles

EMERGENCY LIGHTING TRIM STRIP BROKEN. RESECURED EMERGENCY LIGHT TRIM STRIP.

Part: FLAP — DEFECTIVE (LT WING) · airframe 29,188 hrs · 24,358 cycles

AFTER SELECTING FLAPS TO 45° AIRCRAFT WANTED TO ROLL LT. REQUIRED A SIGNIFICANT AMOUNT OF RWD AILERON TRIM TO COMPENSATE. FLT 6281 REPLACED LT OTBD FLAP IAW AMM. PN 601R14501-841, SN ON SB/RJ/585, PN OFF 601R14501-1 & SN OFF SB/RJ/071.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,111 hrs · 24,301 cycles

EMERGENCY OVERHEAD LIGHT NR 2 IS BURNED OUT. FLT 5508 RELAMPED.

Part: SELECTOR VALVE — FAILED (MLG) · airframe 29,074 hrs · 24,268 cycles

MAIN GEAR DISAGREE WARNING MESSAGES. C/W QRH PROCEDURES & ALL 3 GEARS CAME DOWN & LOCKED WITH MANUAL GEAR EXTENSION. FLT 6517 REPLACED MLG SELECTOR VLV. PERFORMED GEAR CYCLES WITH NO DEFECTS NOTED AT THIS TIME. NO LEAKS NOTED AT THIS TIME. OPERATIONS CHECKED GOOD AT THIS TIME IAW AMM PN 750005000, SN ON 0195 & SN OFF 0217T.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,068 hrs · 24,262 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS BURNED OUT. FLT 6503 RELAMPED.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 28,634 hrs · 23,918 cycles

LT WING REAR EXTERNAL EMERGENCY EXIT LIGHT IS BURNED OUT. FLT 6523 RELAMPED.

Part: PIN — OUT OF ALIGNMENT (SERVICE DOOR) · airframe 28,523 hrs · 23,840 cycles

COMMISSARY REPORTS THEY ARE UNABLE TO OPEN SERVICE DOOR FROM OUTSIDE. "PUSH" BUTTON DOES NOT CAUSE HANDLE TO PROTRUDE. FLT 5380 RE-ALIGNED OUTER HANDLE PIN. OPERATIONS CHECKED GOOD.

Part: INVERTER — FAILED (CABIN) · airframe 28,523 hrs · 23,840 cycles

FIRST STRIP OF EMERGENCY FLOOR LIGHTS DO NOT ILLUMINATE. FLT 6393 REPLACED NR 1 INVERTER IAW AMM. EMERGENCY LIGHTS OPERATIONS CHECKED GOOD, PN ON OFF 5925-7.

Part: MECHANISM — LACK OF LUBE (SERVICE DOOR) · airframe 28,449 hrs · 23,784 cycles

GALLEY SERVICE DOOR WILL NOT OPEN FROM OUTSIDE AIRCRAFT. FLT 6497 LUBRICATED SERVICE DOOR OUTER HANDLE CATCH ASSEMBLY AS REQUIRED. OPERATED SERVICE DOOR FROM OUTSIDE MULTIPLE TIMES. OPERATIONS CHECKED GOOD.

Part: PISTON — OBSTRUCTED (SERVICE DOOR) · airframe 28,231 hrs · 23,616 cycles

GALLEY SERVICE DOOR WILL NOT OPEN FROM THE OUTSIDE. FLT#5475 LUBRICATED SERVICE DOOR OUTER HANDLE CLEANED DEBRIS FROM PLUNGER PISTON. GALLEY SERVICE DOOR NOW OPENS NORMALLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,069 hrs · 23,491 cycles

NR 3 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. FLT#5262 RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,897 hrs · 23,371 cycles

EMERGENCY POD LIGHT BURNED OUT. FLT#6538 RELAMPED NR 3 POD LIGHT.

Part: SELECTOR VALVE — FAILED (MLG) · airframe 27,479 hrs · 23,053 cycles

GEAR DISAGREE, PERFORMED QRH, LANDED UNEVENTFULLY. FIRST TRY THE NOSE GEAR WOULD NOT COME OUT OF YELLOW HATCHING. GEAR UP, 2ND TRY NOSE EXTENDED BUT MAINS WOULD NOT. FLAPS 20, DUAL PU-S 180 KTS MANUAL RELEASE TO RELEASE MAINS. FLT#6539 REPLACED THE MLG SELECTER VALVE IAW AMM. PERFORMED EXTENSIVE OPERATIONAL CHECK OF THE LANDING GEAR EXTENSION/RETRACTION. PN ON/OFF 750005000, SN ON 0217T & SN OFF 0038T.

Part: SEAL — FAILED (HYD SYSTEM) · airframe 27,395 hrs · 22,983 cycles

NR 3 HYDRAULICS SYS PRESSURE WENT TO 5 PERCENT. REPLACED THE DAMPER SEALS ON THE 3B HYDRAULIC IAW AMM.

Part: FLAP — DIRTY (WING) · airframe 26,650 hrs · 22,433 cycles

A/C ROLLS TO THE LEFT WHEN FLAPS 45 SELECTED. (FLT 5584) CLEANED AND INSPECTED WING AND SPOILER SURFACES AS NEEDED. REMOVED DIRT AND GREASE FROM LEFT AND RIGHT FLAP AREAS. NO MISSING HARDWARE TO FLAP CANOES OR PANELS. ALL ACTUATORS INSTALLED CORRECTLY. PASSED FUNCTIONAL FLIGHT.

Part: SERVO — FAILED (AUTOPILOT SYS) · airframe 26,584 hrs · 22,366 cycles

AUTO PILOT WHEN ENGAGED CAUSED A/C TO PITCH UP EXCESSIVELY ON ITS OWN AND OSCILLATE. (FLT 6379) REPLACED AUTOPILOT AILERON SERVO, FCC NR 2 CARD IN IAPS DUE TO PERSISTANT FAULT CODES. FAULTS CLEARED. BOTH AILERON AND ELEVATOR SERVO SPIN TESTS PASS. OPS CHECK OF AFCS FOR BOTH SYSTEMS GOOD AT THIS TIME. P/N 622-4404-101 S/N ON 56RJ S/N OFF D0LK; P/N 622-9815-904 S/N ON 02GY S/N OFF 393 P/N ON/OFF 622-4404-101 S/N ON 56RJ S/N OFF DOLK / P/N ON/OFF 622-9815-904 S/N ON 02GY S/N OFF 393.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,566 hrs · 22,354 cycles

NR 2 EMERGENCY OVERHEAD LIGHT BURNED OUT. (FLT 5290) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,529 hrs · 22,327 cycles

NR 1 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. (FLT 6494) RELAMPED EMERGENCY LIGHT.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 26,411 hrs · 22,238 cycles

THERE WAS THE SMELL OF BURNING MATCHES, COULD NOT DETERMINE THE CAUSE OF THE SMELL. (FLT 6445) PERFORMED VISUAL INSPECTION THROUGHOUT COCKPIT, GALLEY AND AVIONIC BAY WITH BOTH LEFT AND RIGHT PACKS ON, NO UNUSUAL SMELL NOTED AND NO VISIBLE BURNING FOUND. VERIFIED NO UNUSUAL SMELL COMING THROUGH ANY GASPER VENTS ON GROUND.

Part: HANDLE — CONTAMINATED (SERVICE DOOR) · airframe 26,368 hrs · 22,209 cycles

CREW REPORTS SERVICE DOOR HANDLE HARD TO OPEN FROM OUTSIDE. (FLT 5345) CLEANED EXCESSIVE GREASE FROM SERVICE DOOR OUTER HANDLE.

Part: CONNECTOR — LOOSE (CABIN) · airframe 26,278 hrs · 22,134 cycles

EMERGENCY LIGHT WILL NOT COME ON BY SERVICE DOOR. (FLT 6482) RE-SECURED LOOSE CONNECTION AT LIGHT.

Part: MECHANISM — DIRTY (SERVICE DOOR) · airframe 26,161 hrs · 22,045 cycles

SERVICE DOOR EXTEND FLAP WILL NOT OPEN, CANNOT OPEN DOOR FROM OUTSIDE. (FLT 5574) CLEANED SERVICE DOOR OUTER HANDLE MECHANISM.

Part: CHARGER — FAILED (CABIN) · airframe 26,161 hrs · 22,045 cycles

EXIT LIGHT BESIDE GALLEY DOOR DOES NOT ILLUMINATE. (FLT 6208) INSTALLED SERVICEABLE BATTERY CHARGER IN NR 1 POSITION.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,784 hrs · 21,780 cycles

CRACK ON FS 621 AFT PRESSURE BULKHEAD WEB FORWARD FACE AT WL 131.0 LBL 27.5 ABOVE AFT CARGO DOOR AFT TRACK. (C-CHECK) REPAIRED FS 621 AFT PRESSURE BULKHEAD WEB FACE AT WL 131.0 LBL 27.5 ABOVE AFT CARGO DOOR AFT TRACK, IAW REO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 25,784 hrs · 21,780 cycles

LEFT FS 250 JUST BELOW PILOTS SIDE WINDOW FRAME CRACKED. (C-CHECK) REPAIRED LEFT FS 250 BELOW PILOTS WINDOW IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,972 hrs · 21,136 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6303) RELAMPED EMERGENCY LIGHT.

Part: WEB — DAMAGED (FUSELAGE) · airframe 24,716 hrs · 20,946 cycles

LEFT FORWARD FUSELAGE BETWEEN FS 169.00 TO FS 202.75, INNER WEB IS DAMAGED. (SERVICE) REPAIRED WEB IN REFERENCE TO REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,618 hrs · 20,870 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5316) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — BROKEN (CABIN) · airframe 24,512 hrs · 20,791 cycles

EMERGENCY FLOODLIGHT NEXT TO PASSENGER DOOR SNAPPED OFF. (FLT 6223) REPLACED FLOODLIGHT NEXT TO PAX DOOR IN REFERENCE TO AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,402 hrs · 20,714 cycles

NR 2 AND NR 4 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 5450) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,370 hrs · 20,688 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6201) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,273 hrs · 20,621 cycles

NR 2 AND NR 3 OVERHEAD EMERGENCY LIGHTS ARE OUT. (SERVICE) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,114 hrs · 20,500 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5514) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,100 hrs · 20,492 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6303) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,985 hrs · 20,408 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5499) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,915 hrs · 20,349 cycles

FLT 6281, EMERGENCY FLOOR LIGHTING AT ROW 9-12 INOPERATIVE. REPLACED NR 4 EMERGENCY LIGHT ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,876 hrs · 20,311 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5641) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,840 hrs · 20,281 cycles

NR 3 EMERGENCY LIGHT IN CABIN IS INOPERATIVE. (FLT 5235) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,726 hrs · 20,181 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5364) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,682 hrs · 20,146 cycles

RIGHT WING FORWARD EMERGENCY LIGHT IS OUT. (FLT 6375) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,605 hrs · 20,076 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5592) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,542 hrs · 20,026 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5312) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,310 hrs · 19,844 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6441) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,273 hrs · 19,820 cycles

THE 2ND FROM AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6506) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,221 hrs · 19,780 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5247) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,205 hrs · 19,770 cycles

RIGHT OVERWING FORWARD EXTERIOR EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,794 hrs · 19,413 cycles

OVERHEAD EMERGENCY LIGHT OVER ROW 5 IS OUT. (FLT 6324) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,690 hrs · 19,308 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5430) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,548 hrs · 19,194 cycles

LEFT WING AFT EMERGENCY LIGHT AND MAIN CABIN DOOR EMERGENCY LIGHTS ARE OUT. (FLT 5303) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,500 hrs · 19,158 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5297) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,300 hrs · 19,001 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS BURNED OUT. (FLT 5511) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,119 hrs · 18,829 cycles

AFT CEILING EMERGENCY LIGHT NOT WORKING. (FLT 5812) RELAMPED EMERGENCY LIGHT.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 21,890 hrs · 18,639 cycles

(C-CHECK) AFT INTERCOSTAL AT FS 340 ON PASSENGER DOOR IS CRACKED. REPAIRED PER SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 21,890 hrs · 18,639 cycles

(C-CHECK) FS 280 OUTBOARD CLIPS AT RBL 11, LBL 11 AND INBOARD CLIPS AT RBL 9 AND LBL 9 ARE CRACKED. REPLACED CLIPS PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,702 hrs · 18,493 cycles

LEFT FUSELAGE AFT EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,243 hrs · 18,133 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6380) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,108 hrs · 18,031 cycles

REAR MOST OVERHEAD EMERGENCY LIGHT OUT. (FLT 6593) RELAMPED EMERGENCY LIGHT.

Part: BEARING — CORRODED (ENGINE MOUNT) · airframe 20,998 hrs · 17,935 cycles

LEFT ENGINE LINK ASSEMBLY HAS CORROSION ON THE BEARINGS. (ENGINE CHANGE) INSTALLED NEW LEFT ENGINE LINK ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,631 hrs · 17,608 cycles

AFT EMERGENCY CEILING LIGHT OUT. (FLT 6766) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,497 hrs · 17,492 cycles

FORWARD EMERGENCY LIGHT OVER LEFT WING INOPERATIVE. (FLT 6842) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 20,497 hrs · 17,492 cycles

MAIN CABIN DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. (FLT 6898) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 20,412 hrs · 17,418 cycles

OUTSIDE RIGHT MIDDLE OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. (FLT 6948) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,862 hrs · 16,941 cycles

THE 3RD EMERGENCY DOME LIGHT BURNED OUT. (FLT 6119) RELAMPED EMERGENCY LIGHT.

Part: MOUNT — CORRODED (RT ENGINE) · airframe 19,497 hrs · 16,636 cycles

RIGHT ENGINE MOUNT FORWARD LINK ASSEMBLY PITTED. (ENG CHANGE) REPLACED RIGHT ENGINE FORWARD LINK ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,969 hrs · 16,215 cycles

NR 3 EMERGENCY CEILING LIGHT INOP. (FLT 6562) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,799 hrs · 16,063 cycles

AFT OVERHEAD EMERGENCY LIGHT INOP. (FLT 6561) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,224 hrs · 15,555 cycles

OVERHEAD EMERGENCY LIGHT SECOND FROM MOST AFT INOP. (FLT 5805) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,890 hrs · 15,281 cycles

AFT CEILING EMERGENCY LIGHT INOP. (FLT 5990) RELAMPED CEILING EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,511 hrs · 14,936 cycles

EMERGENCY CEILING LIGHT AT ROW 5 INOP. (FLT 6554) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,023 hrs · 14,553 cycles

EMERGENCY LIGHT SECOND FROM AFT INOP. (FLT 6146) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,966 hrs · 14,513 cycles

OVERHEAD EMERGENCY FLOODLIGHT INOP. (FLT 6625) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,839 hrs · 14,427 cycles

AFT EMERGENCY LIGHT INOP. (FLT 6016) RELAMPED EMERGENCY LIGHT.

Part: FITTING — CRACKED (FUSELAGE) · airframe 16,785 hrs · 14,387 cycles

LINTEL FITTING CRACKED ZONE 200. (C CHECK) REPAIRED PER REO.

Part: FITTING — CRACKED (FUSELAGE) · airframe 16,794 hrs · 14,395 cycles

CRACK ON LINTEL FITTING, ZONE 200. (C CHECK) REPAIRED PER REO.

Part: FITTING — CRACKED (FUSELAGE) · airframe 17,070 hrs · 14,591 cycles

FS 625 CLIPS CRACKED. (C CHECK) CLIPS REPLACED PER SRM.

Part: SILL — CORRODED (E&E BAY) · airframe 17,070 hrs · 14,591 cycles

MAIN AVIONICS COMPARTMENT DOOR SILL CORRODED. (C CHECK) REPAIRED PER REO.

Part: HANDLE — CORRODED (ESCAPE HATCH) · airframe 17,070 hrs · 14,591 cycles

INTERNAL HANDLE HOUSING OF CREW ESCAPE HATCH CORRODED. (C CHECK) REPLACED HANDLE PER AMM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 17,070 hrs · 14,591 cycles

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

Part: FITTING — CRACKED (FUSELAGE) · airframe 16,759 hrs · 14,371 cycles

FS 625 CLIPS CRACKED. (C CHECK)REPAIRED PER REO.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 16,426 hrs · 14,121 cycles

FLT 6522 - EMERGENCY LIGHT OUTSIDE LAV INOP. RELAMPED.

Part: CABLE — TWISTED (PAX DOOR) · airframe 16,230 hrs · 13,970 cycles

FLT 6410 - MAIN CABIN DOOR WOULD NOT OPEN. FREED TWISTED CABLE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,192 hrs · 13,939 cycles

FLT 6622 - AFT EMERGENCY FLOOD LIGHT INOP. RELAMPED.

Part: COVER — DISPLACED (EMERGENCY LIGHT) · airframe 15,838 hrs · 13,650 cycles

FLT 6637 - RED LENS COVER ON OVERHEAD EMERGENCY LIGHT AT CENTER AISLE CAME OFF. REPLACED RED LENS COVER.

Part: WINDOW — CRACKED (COCKPIT) · airframe 15,200 hrs · 13,160 cycles

FLT 6070 - RIGHT WINDSHIELD CRACKED. REPLACED RIGHT WINDSHIELD P/N OFF, NP139321-14, S/N OFF, 05220H8098.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 15,069 hrs · 13,050 cycles

FLT 6351 - OVERHEAD CABIN EMERGENCY LIGHT INOP. RELAMPED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 14,699 hrs · 12,734 cycles

FLT 6103 - EMERGENCY LIGHT IN OVERHEAD ROW 10 INOP. RELAMPED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 14,560 hrs · 12,620 cycles

FLT 5966 - CEILING EMERGENCY LIGHT INOP. RELAMPED.

Part: HEATING ELEMENT — FAILED (COCKPIT WINDOW) · airframe 14,064 hrs · 12,203 cycles

SMOKE COMING FROM LT WINDOW HEAT BLOCK AND RECEIVED A LT WINDOW HEAT CAUTION MESSAGE. TURNED OFF LT WINDSHIELD HEAT. (FLIGHT 6380) REPLACED CAPTAINS SIDE WINDOW IAW CRJ MM 56-12-01. P/N NP-139322-11 S/N OFF 08012H2159.

Part: WINDOW — CRACKED (COCKPIT) · airframe 13,932 hrs · 12,098 cycles

RT WINDOW SHATTERED ON CLIMBOUT. (FLIGHT NR 6394) REPLACED RT SIDE WINDOW IAW 56-12-01. P/N:NP-139332-6, S/N OFF: 03140H4504.

Part: WINDOW — CRACKED (COCKPIT) · airframe 13,922 hrs · 12,089 cycles

FLT 5820 - LEFT SIDE WINDOW CRACKED WHILE IN FLIGHT. REPLACED LEFT SIDE WINDOW IAW MM 56-12-01, P/N OFF: NP139322-001, S/N OFF: 02241H4783.

Part: ADG — MALFUNCTIONED · airframe 13,522 hrs · 11,755 cycles

FLT 6644 - THE ADG DEPLOYED AFTER TAKEOFF. RESET ADG SENSE C/B AND RESTOWED ADG. OPS CHECK GOOD PER MM 24-23-01.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,009 hrs · 11,338 cycles

FLT 6618 - LEFT WING EMERGENCY LIGHT IS INOP. REPLACED EMERGENCY LIGHT BULB IAW AMM 33-51-00.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 12,952 hrs · 11,293 cycles

FLT 5983 - FORWARD EMERGENCY LIGHT STRIP ON FLOOR AND ALSO AT EMERGENCY EXIT DOOR IS INOP. REPLACED INVERTER ON NR 2 ELBP IAW CRJ 200 AMM 33-51-07. OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 12,952 hrs · 11,293 cycles

FORWARD EMERGENCY LIGHT STRIP ON FLOOR AND ALSO AT LEFT EMERGENCY EXIT DOOR IS INOP. REPLACED NR 2 EMERGENCY LIGHT BATTERY. OPS CHECKS GOOD IAW AMM 33-51-04.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 12,893 hrs · 11,245 cycles

FLT 6753 - A SECTION OF EMERGENCY FLOOR LIGHTS ARE INOP. RESECURED CONNECTOR ON FLOOR STRIP. OPS CHECK GOOD.

Part: WIRE — UNSECURE (EMERGENCY LIGHTS) · airframe 12,356 hrs · 10,782 cycles

FLT 5914 - LEFT OVERWING FLOOR EMERGENCY LIGHT IS INOP. SECURED WIRE TERMINAL. OPS CHECK GOOD.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 12,856 hrs · 11,211 cycles

FORWARD FLOOR SUPPORT IS CRACKED AT LBL 9 AND FS 280, FOUND AT C-CHECK. INSTALLED REPAIR PARTS IAW CRJ200 SRM CH 51-42-06, PG 11, PARA 9.

Part: PANEL — GOUGED (LT AILERON) · airframe 12,856 hrs · 11,211 cycles

LEFT AILERON LEADING EDGE PANEL IS GOUGED, FOUND AT C-CHECK. REPLACED AILERON PANEL PER CRJ200 SRM 51-40-11 PG 2 AND PG 4.

Part: SHAFT — GOUGED (RT ENGINE) · airframe 12,856 hrs · 11,211 cycles

RIGHT ENGINE THRUST SHAFT IS GOUGED, FOUND AT C-CHECK. REPLACED ENGINE THRUST SHAFT PER CRJ200 AMM 71-00-00-020-002 PARA K STEPS 8-9.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 12,856 hrs · 11,211 cycles

FS 280 BEAM IS CRACKED AT APPROX RBL10, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER REO 601R-53-11-171 REV D, REPAIR SCHEME 13, DATED 2/13/07.

Part: BEARING — WORN (ENGINE MOUNT) · airframe 12,856 hrs · 11,211 cycles

LEFT ENGINE THRUST FITTING BEARING IS WORN, FOUND AT C-CHECK. REPLACED LEFT ENGINE THRUST FITTING PER CRJ200 AMM 71-22-01-400-801.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 12,856 hrs · 11,211 cycles

RIGHT SIDE OF RBL 10 UPPER FLOOR SUPPORT AND LEFT SIDE OF LBL 10 UPPER FLOOR SUPPORT IS CRACKED, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER CRJ200 SRM 51-42-06 PG 11 PARA 9 AND REO 601R-53-11-1.36 REV A DATED 2007/11/01.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 12,856 hrs · 11,211 cycles

FS 280 BEAM IS CRACKED AT APPROX LBL10, FOUND AT C-CHECK. INSTALLED FS 280 AT LBL9.0 REPAIR PARTS IAW CRJ200 REO 601R-53-11-171.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 12,313 hrs · 10,739 cycles

FLT 6608 - FO WINDSHIELD IS CRACKED. REPLACED FO'S WINDSHIELD IAW CRJ MM 56-11-01, P/N OFF: 601R33033-14, S/N OFF: 02240H4671.

Part: PUMP — LEAKING (NR 2) · airframe 11,775 hrs · 10,258 cycles

FLT 6635 - FOUND FLUID LEAKING FROM NR 2 EDP. INSTALLED NR 2 EDP IAW AMM 29-11-01.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 11,285 hrs · 9,843 cycles

OVERHEAD EMERGENCY EXIT LIGHT IN CABIN INOP, FLIGHT NR 5879. RELAMPED EMERGENCY OVERHEAD LIGHT AS REQUIRED. OPS CHECK GOOD.

Part: STRIKER — DAMAGED · airframe 10,992 hrs · 9,616 cycles

AFT STRIKER SEAL IS DAMAGED. REPAIRED AFT STRIKER IAW BOMBARDIER REO 601R-53-22-003 TYPE III REPAIR.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 9,407 hrs · 8,255 cycles

LEFT AFT EMERGENCY LIGHT OVERWING EXIT IS INOP. REPLACED EMERGENCY BATTERY CHARGER. OPERATIONAL CHECKS GOOD, PN: 1L0049 SN ON: P429665.

Part: LIGHT — FAILED (CABIN) · airframe 9,292 hrs · 8,159 cycles

FORWARD FLOOR EMERGENCY EXIT STRIP LIGHTING AND THE OVERWING LOWER EMERGENCY EXIT LIGHT LEFT SIDE ARE INOP. REPLACED 3RD AFT SECTION FLOORSTRIP. OPERATIONAL CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,884 hrs · 7,786 cycles

CABIN EMERGENCY FLOOD LIGHT ABOVE ROW 10 BURNED OUT. RELAMPED EMERGENCY FLOOD LIGHT ABOVE ROW 10 PER AMM 33-51-16. OPERATIONAL CHECKS GOOD.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 8,495 hrs · 7,452 cycles

FS 484 RIGHT SIDE BL36 CRACKED INTERCOSTAL, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR ANGLE 601R-53-41-059. RII 53-401 COMPLIED WITH.

Part: ANGLE — CRACKED (PAX DOOR) · airframe 8,495 hrs · 7,452 cycles

PAX DOOR AFT TOP ANGLE CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPAIR PARTS INSTALLED AT AFT LOCATION IAW REO 601R-52-11-279 NOTES 5-10 AND SKYWEST RII 52-401.

Part: ANCHOR FITTING — CRACKED (PAX DOOR) · airframe 8,495 hrs · 7,452 cycles

PAX DOOR FORWARD ANCHOR FITTING CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW ANCHOR FITTING P/N 601R-38074-6 PER CRJ 200 SB601R-52-116 ITEM 2-B STEPS 1-10.

Part: ATTACH ANGLE — CRACKED (PAX DOOR) · airframe 8,495 hrs · 7,452 cycles

PAX DOOR AFT ATTACH ANGLE CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS ON AFT SIDE DRAG ANGLE PER REO NR 601R52-11-513, AND PER SKYWEST RII 53-401.

Part: SUPPORT BEAM — CRACKED (FUSELAGE) · airframe 8,495 hrs · 7,452 cycles

RT ENG SUPPORT BEAM CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS TO RT ENG SUPPORT BEAM PER CRJ200 SRM 51-42-06 PG 11 AND 51-42-20 PF 23 AND SKYWEST RII53-401.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 8,495 hrs · 7,452 cycles

FS640 RT ANGLE/RBL45 CRACKED; BETWEEN STR 9/12, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW ANGLE P/N 601R36002-4 S/B TO FS640 FRAME RT BETWEEN PLUNGER 4R + 12R PER CRJ -200 SRM 51-42-06 P11 AND 51-42-21 P17 AND RII 53-401.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 8,495 hrs · 7,452 cycles

AFT EQUIPMENT BAY FS 625 RBL 40 WL 79 ANGLE IS CRACKED DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP PN 60135012-52 PG 17 IAW RII 53-401.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 8,495 hrs · 7,452 cycles

FS 640 LT ANGLE LBL 45 CRACKED BETWEEN STR 9/12, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW ANGLE AT FS 640 LBL 45 BETWEEN STRG 9 AND 12 IAW CRJ-200 SRM 51-42-06 AND 51-42-21 AND SKYWEST RII 53-401 COMPLIED WITH.

Part: SUPPORT BEAM — CRACKED (FUSELAGE) · airframe 8,495 hrs · 7,452 cycles

LT ENG SUPPORT BEAM LOWER WEB CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR DOUBLER, WEB FILLER AND STRAP IAW REO 601R-53-61-358 REV 'A' AND SKYWEST RII53-401.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 8,495 hrs · 7,452 cycles

AFT EQUIPEMNT BAY FS 625 LBL 40 WL 79 ANGLE CRACK, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW ANGLE PN G0135012-51 PG 17 IAW SRM 51-42-21 PG 17/REO 601R 53-61-422 AND RII 53-401.

Part: SUPPORT BEAM — CRACKED (FUSELAGE) · airframe 8,495 hrs · 7,452 cycles

LT ENG SUPPORT BEAM CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS TO LT ENG SUPPORT BEAM PER CRJ200 SRM 51-42-06 PG 11 AND 51-42-20 PF 23 AND SKYWEST RII53-401.

Part: ANGLE — CRACKED (PAX DOOR) · airframe 8,495 hrs · 7,452 cycles

PAX DOOR FORWARD TOP ANGLE CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS IAW REO 601R-52-11-279 NOTES 5-10 AND SKYWEST RII 52-401.

Part: ANCHOR FITTING — CRACKED (PAX DOOR) · airframe 8,495 hrs · 7,452 cycles

PAX DOOR AFT ANCHOR FITTING CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW ANCHOR FITTING P/N 601R38074-5 PER CRJ 200 SB 601R-52-116 ITEM 2B STEPS 1-10.

Part: MOTOR-BRAKE UNIT — MALFUNCTIONED (T/E FLAP) · airframe 7,264 hrs · 6,382 cycles

WHITE STATUS MSG (FLASH HALFSPEED) JUST BEFORE TAKEOFF. REPLACED RT MOTOR BRAKE IAW AMM 27-52-05. OPERATIONAL CHECK GOOD.

Part: ACTUATOR — FAILED (T/E FLAP) · airframe 7,259 hrs · 6,378 cycles

FLAPS FAIL CAUTION. REPLACED LEFT WING FLAP ACTUATORS 1 THRU 4 ALONG WITH FLEX DRIVE SHAFTS NR 1 AND NR 5.

Part: SENSOR — MALFUNCTIONED (BRAKE POSITION) · airframe 7,189 hrs · 6,319 cycles

FLAPS FAIL AT 0 DEGREES IN FLIGHT. REPLACED RIGHT BPSU IAW MM 27-51-10. OPERATIONAL CHECK GOOD.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 7,189 hrs · 6,319 cycles

"STALL FAIL" CAUTION MESSAGE AFTER TAKE OFF. REPLACED STALL PROTECTION COMPUTER IAW CRJ MM 27-35-01, OPERATIONAL CHECK GOOD.

Part: SENSOR — MALFUNCTIONED (TE FLAPS) · airframe 6,929 hrs · 6,097 cycles

FLAPS FAIL ON TAXI WHEN SELECTED FLAPS 20 DEG. REPLACED LEFT BPSU IAW MM 27-51-10. OPERATIONAL CHECK GOOD.

Part: BPSU — MALFUNCTIONED (TE FLAPS) · airframe 6,853 hrs · 6,030 cycles

FLAPS FAIL CAUTION MSG ON FINAL. REPLACED LT BPSU AND FECU IAW CRJ 200 MM 27-51-10. OPERATIONAL CHECK GOOD, PN 860D100-18; SN OFF 1191, PN 855D100-11; SN OFF 1999.

Part: WIRE — FAILED (EMERGENCY LIGHT) · airframe 6,790 hrs · 5,982 cycles

FIRST STRIP OF FLOOR LEVEL EMERGENCY LIGHTING INOP (5 ROWS). REPLACED CABLE ASSY FOR FIRST SECTION OF EMERGENCY LIGHT STRIP IAW CRJ 200 AMM 33-51-01. OPERATIONAL CHECK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 6,812 hrs · 6,000 cycles

RT WING FWD EMERGENCY EXIT LIGHT INOP. RELAMPED RT WING FWD EMERGENCY LIGHT BULB REF 33-40-00. OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 6,664 hrs · 5,877 cycles

CREW REPORTS FLOOR LIGHTING INOP. CLEANED FLOOR TRACK POWER STRIP ROW 2 TO 6 CONNECTION AND REINSTALLED POWER STRIP AND LIGHT STRIPS. OPERATIONAL CHECK GOOD IAW CRJ 200 MM 33-51-00-710-801.

Part: PCU — MALFUNCTIONED (FLT SPOILERSL) · airframe 6,563 hrs · 5,780 cycles

A -FLIGHT SPOILERS FAULT- STATUS MESSAGE. REPLACED NR 1 SECU AND NR 2 PCU-SPOILERON IAW MM 27-61-05 AND 27-61-05, OPERATIONAL CHECK GOOD. P/N 49-164-05, S/N OFF 01607.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 5,850 hrs · 5,174 cycles

LAST EMERGENCY LIGHT PAD ON CEILING INOPERATIVE. RELAMPED LAST CEILING EMERGENCY LIGHT IAW MM CHAPTER 33-50-00, OPERATIONAL CHECK GOOD.

Part: SWITCH — INOPERATIVE (STAB TRIM) · airframe 5,718 hrs · 5,057 cycles

CAPTAIN'S STAB TRIM SWITCH INOPERATIVE. REPLACED CAPTAIN'S STAB TRIM SWITCH. OPERATIONAL CHECK GOOD IAW CRJ MM 27-41-00 & 27-41-05.

Part: SMOKE WARNING — MALFUNCTIONED (COCKPIT) · airframe 5,605 hrs · 4,970 cycles

CARGO SMOKE MESSAGE ON PUSHBACK. INSPECTED CARGO COMPARTMENT. NO DEFECTS NOTED. PERFORMED ENGINE RUNS WITH CREW. NO DEFECTS NOTED. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 5,564 hrs · 4,935 cycles

DURING FLIGHT CONTROL CHECK RIGHT SPOILERON DEPLOYS 1/4 SCALE DURING LEFT FULL AILERON INPUT, THEN A SPOILERON FAULT STATUS MSG ILLUMINATED. REMOVED AND REPLACED NR 1 AND NR 2 SECU IAW 27-61-05. OPERATIONAL CHECK GOOD. P/N 49-164-06; S/N OFF 01717.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 5,531 hrs · 4,899 cycles

CEILING LEVEL EMERGENCY FLOOD ABOVE ROW 2 INOPERATIVE. REPLACED BULB TO EMERGENCY CEILING LIGHTING AT ROW 2 AREA. OPERATIONAL CHECK GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 5,421 hrs · 4,797 cycles

RIGHT REAR EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED RIGHT REAR EXTERIOR EMERGENCY LIGHT. OPERATIONAL CHECK GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 3,909 hrs · 3,469 cycles

FORWARD CEILING EMERGENCY FLOOD LIGHT INOPERATIVE. REPAIRED BROKEN WIRE LY3D22 IN RT SIDEWALL. EMERGENCY LIGHTING OPERATION CHECKED OKAY.

Part: ANGLE — CRACKED (FUSELAGE)

FLOOR SUPPORT ANGLE AT FS 621, WL 73 OUTBOARD OF LBL AND RBL 27 CRACKED. REPAIR IAW BOMBARDIER AEROSPACE EO NR 601R-53-61-117.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 4,343 hrs · 3,826 cycles

RIGHT FS 621 FLOOR SUPPORT ANGLE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW REO 601R-53-61-117.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 4,343 hrs · 3,826 cycles

LEFT FS 621 FLOOR SUPPORT ANGLE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR ITEMS IAW 601R-53-61-117-1, -3, AND -79 COMPLIED WITH REO 601R-53-61-117.

Part: CONTROL UNIT — MALFUNCTIONED (TRIM MOTOR) · airframe 3,727 hrs · 3,310 cycles

STAB CHANNEL 1 INOP MESSAGE DISPLAYED ON STATUS PAGE. REMOVED AND REPLACED HORIZONTAL STAB TRIM ACTUATOR AND MOTOR CONTROL UNIT. OPERATIONAL CHECK GOOD IAW 27-42-05. STAB TRIM ACTUATOR P/N: 8396-2, S/N OFF: 949.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZONTAL STAB) · airframe 3,663 hrs · 3,254 cycles

STAB TRIM NR 1 CAME OFF ON DESCENT AND ON LEVEL OFF. REPLACED HSTCU AS REQUIRED PER CRJ MM 27-41-01. OPERATIONAL CHECK GOOD.

Part: WINDOW — CRACKED (COCKPIT) · airframe 2,920 hrs · 2,577 cycles

RIGHT WINDOW HAS MANY CRACKS ON THE INNER LAYER. REMOVED AND REPLACED RIGHT SIDE WINDOW IAW CRJ MM 56-12-01 AND RII CARD 56-402. OPS CHECKS GOOD. P/N OFF: 601R33033-12, S/N OFF: 02241H4773.

Part: SWITCH — INOPERATIVE (STAB TRIM) · airframe 2,468 hrs · 2,147 cycles

F/O STAB TRIM INOPERATIVE. REMOVED AND REPLACED F/O'S STAB TRIM SWITCH IAW AMM 27-41-05. OPS CHECK GOOD. P/N: 309-4334.

Part: CONTROL PANEL — FAILED (AIL/RUDDER TRIM) · airframe 2,228 hrs · 1,931 cycles

RUDDER TRIM WILL NOT TRIM PROPERLY TO THE LEFT. REMOVED AND REPLACED AILERON/RUDDER TRIM CONTROL PANEL. OPS CHECK GOOD.

Part: LANDING GEAR — MALFUNCTIONED (MLG) · airframe 1,303 hrs · 1,136 cycles

ON FINAL, AFTER PLACING THE LANDING GEAR LEVER DOWN, THE MAIN LANDING GEAR DID NOT UNLOCK. A DISAGREE MESSAGE APPEARED. WHEN EXECUTING THE MISSED APPROACH, THE GEAR DEPLOYED AND LOCKED. PERFORMED GEAR INSPECTION ON ALL GEARS. NO DEFECTS NOTED. PERFORMED NUMEROUS GEAR SWINGS. OPS CHECKS GOOD IAW MM 32-32-00.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 809 hrs · 690 cycles

ON APPROACH TO SBA, THE RIGHT FLIGHT SPOILER MESSAGE ANNUNCIATED WITH A SLIGHT ROLL TO THE LEFT. UPON LANDING, THE RIGHT SPOILER DID NOT DEPLOY WITH GLDS. PERFORMED FUNCTIONAL CHECK OF FLIGHT SPOILERONS AND GROUND SPOILERS SEVERAL TIMES. ALL CHECKS NORMAL WITH NO FURTHER DISCREPANCIES AT THIS TIME.