N920SW

Part: RETAINER — CORRODED (E/E DOOR SEAL) · airframe 45,858 hrs · 39,106 cycles

MAIN AVIONICS DOOR SEAL RETAINER TRACK HAS MULTIPLE AREAS OF CORROSION. (FILED CLOSED) REMOVED AND REPLACED ALL FOUR MAIN AVIONICS DOOR SEAL RETAINER SEGMENTS IN REF TO SRM 51-42-06.

Part: SUPPORT ANGLE — CRACKED (CARGO DOORWAY) · airframe 45,858 hrs · 39,106 cycles

CARGO DOOR CUTOUT, UPPER BEAM AFT SUPPORT ANGLE IS CRACKED. FS 621.00 AT WL 115.08. (FILED CLOSED) REMOVED AND REPLACED CARGO DOOR CUTOUT, UPPER BEAM AFT SUPPORT ANGLE IN REF TO SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLETED M-337.

Part: TRACK — CRACKED (CARGO DOOR) · airframe 45,858 hrs · 39,106 cycles

CARGO DOOR FORWARD TRACK, LOWER SUPPORT BRACKET AT FS 574.00, WL 77.61 IS CRACKED. (FILED CLOSED) REMOVED AND REPLACED CARGO DOOR FORWARD TRACK, LOWER SUPPORT BRACKET AT FS 574.00, WL 77.61 IN REF TO SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLETED M-337.

Part: SKIN — CORRODED (SERVICE DOOR) · airframe 45,858 hrs · 39,106 cycles

SERVICE DOOR HAS CORRODED FASTENERS ON THE LOWER AFT CORNER AND UPPER FORWARD CORNERS OF THE INNER SKIN. (FILED CLOSED) REMOVED AND REPLACED CORRODED FASTENERS ON THE LOWER AFT CORNER AND UPPER FORWARD CORNERS OF THE SERVICE DOOR INNER SKIN IN REF TO SRM 51-42-22. PIMED AND PAINTED IN REF TO SRM 51-25-16.

Part: NUT — LOOSE (STOW SWITCH) · airframe 45,571 hrs · 38,850 cycles

RIGHT REV UNLOCKED IN FLIGHT, FLIGHT 5038 - FILED CLOSED. PLEASE REFERENCE AML 581409. THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 22323893 WITH THE FOLLOWING CORRECTIVE ACTION: BEFORE RIGGING THE RT ENGINE STOW MICRO SWITCH, FOUND THE JAM NUTS LOOSE CAUSING THE STOW SWITCH TO HAVE A SMALL AMOUNT OF FWD AND AFT PLAY. RIGGED THE RT ENGINE STOW MICRO SWITCH AND THE THROTTLE LOCKOUT MICRO SWITCH IN REF TO CRJ 200 AMM 78-37-01. OPS CHECK GOOD AT THIS TIME.

Part: BPSU — FAILED (TE FLAPS) · airframe 44,758 hrs · 38,077 cycles

WHEN CONFIGURING FOR APPROACH AND LAND INTO DENVER FLAPS FAIL CAUTION MESSAGE WHEN SELECTING FLAP 8. FLAPS WERE AT 0 FOR APPROACH, LANDED AT 42700 LBS AND AT 100 PFM VSI. FLIGHT 5791. INSTALLED NEW RH BPSU IN REF WITH AMM. OPS CHECK GOOD AT THIS TIME. FLAP FAIL MESSAGE NO LONGER PRESENT AND FLAPS ABLE TO DEPLOY TO ALL POSITIONS.

Part: ENGINE — FAILED (NR 1) · airframe 43,939 hrs · 37,332 cycles

DURING CLIMB-OUT, LOSS OF NR 1 ENGINE AND LOUD BANG. ENGINE ITT WAS IN THE RED FOR ABOUT 15-20 SECONDS WITH NEEDLE FLUTTERING AT THE BOTTOM OF THE GAUGE. N1 AND N2 SPOOLED DOWN DURING THE FAILURE. CREW WAS NOT ABLE TO IDENTIFY ANY MESSAGES. AFTER ENGINE RESTARTED, ALL INDICATIONS NORMAL UNTIL LANDING. EMERGENCY TRUCKS REPORTED FLAMES FROM THE NR 1 ENGINE ON SHORT FINAL. FLIGHT 5669. REMOVED AND REPLACED LEFT ENGINE ASSEMBLY IN REF TO THE AMM AND TASK CARD. OPS AND LEAK CHECK GOOD AT THIS TIME.

Part: GUSSET — CORRODED (BS 364) · airframe 43,070 hrs · 36,578 cycles

CORROSION ON GUSSET ATTACHED TO FRAME 364 AT STR 26R. (C-CHECK) RO: 08/07/2019 REPLACED GUSSET ATTACHED TO FRAME 364 AT STR 26R IAW SRM.

Part: GUSSET — CORRODED (BS 364) · airframe 43,070 hrs · 36,578 cycles

CORROSION ON GUSSET ATTACHED TO FRAME 364 AT STR 26L. (C-CHECK) RO: 08/07/2019 REMOVED AND REPLACED GUSSET ATTACHED TO FRAME 364 AT STR 26L IAW SRM.

Part: FLOORBEAM — CORRODED (BS 574) · airframe 43,070 hrs · 36,578 cycles

FLOOR BEAM AT FS 574 IS CORRODED AT THE L/H FLOOR SILL. (C-CHECK) REMOVED CORROSION ON FLOOR BEAM LOCATED AT FS574.00. C/W ALL STEPS OF REO.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 43,070 hrs · 36,578 cycles

BOTH INBOARD AND OUTBOARD CLIPS ON THE BL9L FLOOR BEAM, AT THE FS280.00 BULKHEAD, ARE CRACKED. (C-CHECK) REPLACED INBOARD AND OUTBOARD CLIPS ON THE BL9L FLOOR BEAM, AT THE FS280.00 IAW REO.

Part: ANGLE — CORRODED (BS 364) · airframe 43,070 hrs · 36,578 cycles

CORROSION ON ANGLE ATTACHED TO AFT SIDE OF FRAME 364. (C-CHECK) RO: REMOVED AND REPLACED ATTACH ANGLE TO FRAME AT FS364 STGR 25L - STGR 25R IAW SRM.

Part: FAIRING — CHAFED (LT WING TE FLAP) · airframe 43,070 hrs · 36,578 cycles

L/H FLAP STUB FAIRING IS CHAFED. (C-CHECK) REMOVED AND REPLACED L/H FLAP STUB FAIRING IAW SRM.

Part: NOT REPORTED — MALFUNCTIONED (NLG) · airframe 41,629 hrs · 35,269 cycles

ON TAKEOFF NOSE GEAR DID NOT COME UP. LANDED WITHOUT INCIDENT. (FLT 5517) FO: 10/18/2018 WORK IN PROGRESS.

Part: SENSOR — OUT OF ADJUST (NLG) · airframe 41,754 hrs · 35,388 cycles

ON TAKEOFF NOSE GEAR DID NOT COME UP. LANDED WITHOUT INCIDENT. (FLT#5517) FO: 10/18/2018 CLOSED ADJUSTED NLG OLEO EXTENDED/CENTERED SENSOR IAW AMM. PERFORMED FULL STRUT SERVICE OF NLG IAW AMM.

Part: SENSOR — OUT OF ADJUST (NLG) · airframe 41,658 hrs · 35,300 cycles

GEAR DISAGREE WARNING SHORTLY AFTER GEAR SELECTED UP FOLLOWED BY NOSE DOOR WARNING MESSAGE. THE NOSE GEAR WAS STILL SHOWING DOWN AND LOCKED. COMPLIED WITH QRH FOR GEAR DISAGREE UNTIL MANUAL RELEASE HANDLE STEP. BOTH HYDRAULIC 3B AND 2B PUMPS SELECTED ON. MESSAGES DID NOT CLEAR. THEN COMPLIED WITH QRH FOR NOSE DOOR BY SELECTING GEAR DOWN. THE MAIN GEAR CAME DOWN AND BOTH MESSAGES CLEARED. ALL THREE GEAR SHOWED DOWN AND LOCKED. DIVERTED TO RAP. (FLT 5101) CLOSED ICE BUILDUP ON NLG OLEO CENTERED/EXTENDED SENSOR CAUSED A FAR CONDITION IAW FIM. ADJUSTED SENSOR PS14GA IAW AMM. PERFORMED MULTIPLE GEAR SWINGS IAW AMM, NO FAULTS FOUND.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 38,656 hrs · 32,529 cycles

FLOORBEAM ANGLE CORRODED OUT OF LIMITS FWD AT BS 280 BETWEEN LBL 9 AND RBL 9. REMOVED AND REPLACED THE FWD FLOORBEAM ANGLE IAW SRM.

Part: BRACKET — CORRODED (DOOR SILL) · airframe 38,656 hrs · 32,529 cycles

PASSENGER DOOR SILL ANGLE. BOTH MOUNT BRACKETS FOR THE DOOR HARNESS BLOW OUT. INBD SIDE OF THE ANGLE. REMOVED AND REPLACED THE BRACKETRS IAW SRM.

Part: DOOR SILL — CORRODED (BS 310-349) · airframe 38,656 hrs · 32,529 cycles

LEFT DOOR SILL BS 310 - 349 HAS CORROSION. REMOVED AND INSTALLED A NEW DOOR SILL ANGLE IAW AMM.

Part: DOOR SILL — CORRODED (BS 319-349) · airframe 38,656 hrs · 32,529 cycles

RIGHT DOOR SILL BS 319.7 - 349 HAS CORROSION. REMOVED DOOR SILL LOWER ANGLE AND INSTALLED A NEW ANGLE IAW SRM.

Part: SKIN — CHAFED (RT AILERON) · airframe 38,656 hrs · 32,529 cycles

RIGHT AILERON LOWER INBOARD FIXED LEADING EDGE SKIN CHAFED. REPAIRED IAW REO.

Part: SKIN — CHAFED (RT AILERON) · airframe 38,656 hrs · 32,529 cycles

RH AILERON LOWER OUTBOARD FIXED LEADING EDGE CHAFED. REPAIRED IAW REO.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 38,656 hrs · 32,529 cycles

PASSENGER DOOR INTERCOSTAL (HINGE SIDE OF DOOR) UNDER PANEL 832ER HAS CORROSION. INSTALLED A NEW INTERCOSTAL IAW SRM.

Part: FLOOR PANEL — CRACKED (COCKPIT) · airframe 33,969 hrs · 28,236 cycles

FLOOR PANEL 222FLW CRACKED AT SCREW HOLE. REPAIRED THE COCKPIT FLOOR PANEL IAW EA.

Part: SKIN — GOUGED (SERVICE DOOR) · airframe 33,969 hrs · 28,236 cycles

SERVICE DOOR OUTER SKIN GOUGED AT EXTERNAL HANDLE CUT OUT. REPAIRED SERVICE DOOR OUTER SKIN GOUGES AT EXTENAL HANDLE CUT OUT IAW EA.

Part: DOOR SILL — CRACKED (BS 589) · airframe 33,969 hrs · 28,236 cycles

FOUND CRACK ON CARGO DOOR SILL AT FS 589. REPAIRED THE DOOR SILL IAW REO.

Part: BULKHEAD WEB — DAMAGED (BS 621) · airframe 33,969 hrs · 28,236 cycles

BS 621 AFT PRESSURE BULKHEAD FWD SIDE, DEFECTS NOTED AT RBL 27.50, RBL 18.00, RBL 9.50, LBL 18.00, LBL 27.50, LBL 36.20 BETWEEN WL 120.43 AND WL 73.50. REPAIRED THE PRESSURE BULKHEAD IAW REO.

Part: DOOR FRAME — DENTED (BS 349) · airframe 33,969 hrs · 28,236 cycles

PAX DOOR FRAME DENTED AT FS 349, BY THE CAM FITTING. REPAIRED THE DOOR FRAME IAW REO.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 33,969 hrs · 28,236 cycles

LIGHTNING STRIKE FOUND ON RT ELEVATOR T/E INBD SIDE. REPAIRED THE RT ELEVATOR T/E SKIN IAW REO.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 33,969 hrs · 28,236 cycles

LEFT INBD FLAP LOWER SKIN HAS A DENT INBD SIDE. DAMAGE WAS REMOVED, REPAIR DOUBLER AND FILLER WERE INSTALLED IAW SRM.

Part: PCU — CORRODED (RT SPOILER) · airframe 33,969 hrs · 28,236 cycles

RT FLIGHT SPOILER OTBD PCU HAS CORRODED HARDWARE. REMOVED CORROSION FROM THE RT FLIGHT SPOILER OTBD PCU ATTACH HARDWARE IAW SRM.

Part: BOLT — CORRODED (RT SPOILERON) · airframe 33,969 hrs · 28,236 cycles

RT SPOILERON PCU'S HAVE CORRODED HARDWARE. REMOVED CORROSION FROM THE RT SPOILERON PCU CONNECTING HARDWARE IAW SRM.

Part: HANDLE — GOUGED (SERVICE DOOR) · airframe 33,969 hrs · 28,236 cycles

SERVICE DOOR INNER DOOR HANDLE HAS SEVERAL AREAS THAT CONTAIN CHAFED AND GOUGED. REPAIRED THE SERVICE DOOR INNER HANDLE IAW STS EA.

Part: RIB — CORRODED (LT SPOILERON) · airframe 33,969 hrs · 28,236 cycles

LT SPOILERON INBD RIB HAS CORRODED HARDWARE. R & R CORRODED HARDWARE IAW SRM.

Part: FITTING — CORRODED (RT WING) · airframe 33,969 hrs · 28,236 cycles

RT WING T/E FITTING, OTBD OF SPOILERON, HAS CORRODED HARDWARE. REMOVED CORROSION FROM THE CONNECTING HARDWARE ON THE RT WING T/E FITTING OTBD OF THE SPOILERON IAW SRM.

Part: ATTACH FITTING — CORRODED (RT SPOILERON) · airframe 33,969 hrs · 28,236 cycles

RT SPOILERON OTBD FITTING ATTACH RIB HAS CORRODED HARDWARE. REMOVED CORROSION FROM THE RT SPOILERON OTBD FITTING ATTACH RIB IAW SRM.

Part: ATTACH FITTING — CORRODED (RT AILERON) · airframe 33,969 hrs · 28,236 cycles

RT AILERON INBD AND OTBD ATTACH FITTING BOLT RETAINERS HAVE CORRODED HARDWARE. REMOVED CORROSION FROM THE RT AILERON INBD AND OTBD ATTACH FITTING BOLT RETAINERS HARDWARE IAW SRM.

Part: FLOOR PANEL — CRACKED (COCKPIT) · airframe 33,969 hrs · 28,236 cycles

FLOOR PANEL 222WZ CRACKED. REPAIRED THE FLOOR PANEL IAW EA.

Part: WIRE — CHAFED (OVERHEAT SYS) · airframe 32,781 hrs · 27,266 cycles

LEFT JET OVERHEAT FAIL. REPAIRED CHAFED WIRES TO LT ENGINE LOOP A & LOOP B IAW ESPM. OPS CHECKED FIRE DETECTION SYSTEM - GOOD IAW AMM.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 31,725 hrs · 26,443 cycles

F/A FLASHLIGHT INOPERATIVE. INSTALLED NEW BATTERIES.

Part: LINE — FAILED (NR 1 HYD SYS) · airframe 31,679 hrs · 26,415 cycles

ACFT LOST ALL FLUID IN NR 1 HYDRAULIC SYSTEM. REPLACED HYDRAULIC LINE AND NR 1 EDP IAW AMM.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 31,114 hrs · 25,965 cycles

NR 2 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. REPLACED LAMP.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 30,879 hrs · 25,773 cycles

EMERGENCY LIGHT EXIT SIGN FORWARD OF GALLEY SERVICE DOOR HAS 1 LIGHT BULB BURNED OUT. REPLACED BULB.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 30,865 hrs · 25,763 cycles

TWO EMERGENCY EXIT LIGHTS BURNED OUT IN GALLEY, REPLACED LAMPS.

Part: DOOR — BINDING (GALLEY) · airframe 30,797 hrs · 25,706 cycles

THE GALLEY SERVICE DOOR IS DIFFICULT TO OPEN AND CLOSE. REPLACED THE GALLEY SERVICE DOOR LIFT DEVICE IAW AMM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 30,498 hrs · 25,485 cycles

ONE OF THE LIGHT BULBS ON THE EMERGENCY EXIT SIGN NEXT TO SERVICE DOOR IS BURNED OUT. FLT 6415 RELAMPED.

Part: RELAY — FAULTY (ELECTRICAL SYS) · airframe 30,048 hrs · 25,160 cycles

AC ESS BUS CAUTION MESSAGE ON & EMERGENCY LIGHT ON STATUS MESSAGE. FLT 5549 REPLACED THE AC ESS TRANSFER RELAY K1X10.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 29,904 hrs · 25,037 cycles

202 PRESSURE BULKHEAD CRACKED AT PARKING BRAKE CABLE PASS THROUGH. C-CHECK REPAIRED FS 202 BULKHEAD IAW REO.

Part: VANE — CHAFED (TE FLAP) · airframe 29,904 hrs · 25,037 cycles

LT INBD FLAP VANE HAS A CHAFE ON THE CTR LE. C-CHECK CHAFE IN LT INBD FLAP VANE CTR LE WAS FOUND TO BE OUT OF LIMITS, REPLACED LT INBD FLAP VANE CTR LE IAW SRM.

Part: POST — CRACKED (FUSELAGE) · airframe 29,904 hrs · 25,037 cycles

CRACK ON FS 409+128 VERTICAL POST OTBD AFT RADIUS AT RBL18.00 WL71.00. C-CHECK REPLACED CRACKED POST AT 409+128 RBL 18 IAW REO.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 29,904 hrs · 25,037 cycles

PAX DOOR AFT DRAG ANGLE CRACKED. C-CHECK REPAIRED PAX DOOR AFT DRAG ANGLE IAW REO.

Part: VANE — CHAFED (TE FLAP) · airframe 29,904 hrs · 25,037 cycles

LT INBD FLAP VANE HAS A CHAFE ON THE INBD LE. C-CHECK REPAIRED CHAFE ON LT INBD FLAP VANE ON INBD LE IAW REO.

Part: VANE — CHAFED (TE FLAP) · airframe 29,904 hrs · 25,037 cycles

LT INBD FLAP VANE HAS A CHAFE ON THE OTBD LE. C-CHECK REPAIRED CHAFE ON LT INBD FLAP VANE ON OTBD LE IAW REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 29,904 hrs · 25,037 cycles

CRACK ON FS 621 BULKHEAD WEB, FWD FACE, ALONG BL0.0 AT APPROXIMATE WL108. C-CHECK REPAIRED DAMAGE ON FS 621 BULKHEAD WEB, FWD FACE, ALONG BL0.0 AT APPROXIMATE WL108 IAW REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 29,904 hrs · 25,037 cycles

CRACK ON FS 621 BULKHEAD WEB, FWD FACE, ALONG BL0.0 AT APPROXIMATE WL127. C-CHECK REPAIRED DAMAGE ON FS 621 BULKHEAD WEB, FWD FACE, ALONG BL0.0 AT APPROXIMATE WL127 IAW REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,259 hrs · 24,503 cycles

EMERGENCY LIGHTS AT GALLEY DOOR ARE BURNED OUT. FLT#5547 RELAMPED.

Part: INVERTER — FAILED (CABIN) · airframe 29,100 hrs · 24,378 cycles

EMERGENCY LIGHTS ON FLOOR AT ROWS 2-4 & LOWER WALL LIGHT AT ROW 8 DO NOT ILLUMINATE. FLT#5232 REPLACED NR 2 INVERTER FOR EMERGENCY LIGHTS.

Part: INVERTER — FAILED (CABIN) · airframe 28,005 hrs · 23,511 cycles

ROW 3 TO7 EMERGENCY FLOOR LIGHTING DOES NOT ILLUMINATE. (FLT 6386) REPLACED INVERTER ON NR 2 ELBP.

Part: TIRE — FAILED (NLG) · airframe 27,976 hrs · 23,486 cycles

FLT 6297, NOSE TIRE BLEW AND DAMAGED AFT NOSE GEAR DOOR AND BELLY AREA AFT OF NOSE GEAR ASSEMBLY. REPLACED BOTH NOSE LANDING GEAR WHEEL ASSEMBLIES IAW AMM AND INSTALLED DOUBLER REPAIR FLOOR DENT DAMAGE TO FUSE SKIN FS 235 - 265 S25-27R IAW REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,986 hrs · 23,497 cycles

NR 4 EMERGENCY OVERHEAD LIGHT BURNED OUT. (FLT 5337) RELAMPED EMERGENCY LIGHT.

Part: CONNECTOR — DIRTY (EXIT SIGN) · airframe 27,986 hrs · 23,497 cycles

LOWER LEFT WING EMERGENCY EXIT SIGN DOES NOT ILLUMINATE. (FLT 6242) CLEANED CONNECTOR ON LOWER LEFT WING EMERGENCY EXIT SIGN.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,943 hrs · 21,889 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5545) RELAMPED EMERGENCY LIGHT.

Part: ADC — FAILED (NR 1) · airframe 25,860 hrs · 21,823 cycles

AT FL 330, FIRST OFFICER'S ALTIMETER READS 33,000. CAPTAIN'S ALTIMETER READS 33,110, AND STANDBY ALTIMETER READS 33,260 WITH AUTOPILOT SELECTED TO FIRST OFFICER'S SIDE. (FLT 5297) REPLACED ADC NR 1. PN: 822-0372-445 SN OFF: 2695

Part: ADC — FAILED (NR 1) · airframe 25,829 hrs · 21,797 cycles

FIRST OFFICER'S ALTIMETER INDICATES 150 FEET LOWER THAN CAPTAIN'S SIDE AT FL 340. STAND-BY ALTIMETER INDICATES 300 FEET HIGHER THAN CAPTAIN SIDE AT FL 340. (FLT 6456) PURGED NR 1 AND NR 2 STANDBY PITOT SYSTEMS AND REPLACED NR 1 AIR DATA COMPUTER.

Part: PROBE — FAILED (PITOT/STATIC SYS) · airframe 25,815 hrs · 21,787 cycles

CAPTAIN ALTIMETER READS 250 FEET LOWER THAN FIRST OFFICER'S ALTIMETER AT ALL CRUISE ALTITUDES ABOVE FL 250. (FLT 5415) REPLACED THE NR 1 PITOT STATIC PROBE. P/N: 0856KV9 S/N OFF: 242809

Part: COUNTERBALANCE — OUT OF ADJUST (CABIN DOOR) · airframe 25,732 hrs · 21,732 cycles

MAIN CABIN DOOR LATCH IS STICKY. (FLT 6294) ADJUSTED PASSENGER DOOR FORWARD AND AFT COUNTER BALANCE AND RE-SHIMMED THE FORWARD STRIKER PLATE ROLLER IN REFERENCE TO AMM.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 25,630 hrs · 21,650 cycles

FLT 5373, NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,566 hrs · 21,598 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6350) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,297 hrs · 21,378 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5486) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,253 hrs · 21,336 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6494) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,066 hrs · 21,177 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5410) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,918 hrs · 21,045 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5475) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,852 hrs · 20,995 cycles

RIGHT AFT EMERGENCY LIGHT OUT. (FLT 6227) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,852 hrs · 20,995 cycles

NR 2 EMERGENCY LIGHT INOPERATIVE. (FLT 5549) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,745 hrs · 20,905 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5533) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,692 hrs · 20,861 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6479) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,636 hrs · 20,821 cycles

NR 2 OVERHEAD EMERGENCY LIGHT OUT OF SERVICE. (FLT 5303) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,611 hrs · 20,803 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5553) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,412 hrs · 20,628 cycles

NR 3 CEILING EMERGENCY LIGHT IS OUT. (FLT 5441) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,107 hrs · 20,357 cycles

OVERWING EXTERIOR EMERGENCY LIGHT IS OUT ON LEFT SIDE OF AIRCRAFT. (FLT 5615) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 24,009 hrs · 20,274 cycles

RIGHT FORWARD EXTERIOR EMERGENCY LIGHT IS OUT. (FLT 5363) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,009 hrs · 20,274 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6394) RELAMPED EMERGENCY LIGHT.

Part: CABLE — OUT OF ADJUST (PAX DOOR) · airframe 23,970 hrs · 20,237 cycles

PAX DOOR HARD TO OPEN. (SERVICE) ADJUSTED PAX DOOR COUNTERBALANCE CABLES.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,970 hrs · 20,237 cycles

LAST OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6199) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,912 hrs · 20,194 cycles

RIGHT WING AFT EXTERIOR EMERGENCY LIGHT IS OUT. (FLT 5455) RELAMPED EMERGENCY LIGHT.

Part: SIGN — INOPERATIVE (CABIN) · airframe 23,718 hrs · 20,036 cycles

EMERGENCY EXIT SIGN BY GALLEY SERVICE DOOR IS OUT. (FLT 5606) RELAMPED EMERGENCY EXIT SIGN.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,180 hrs · 19,628 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6398) RELAMPED EMERGENCY LIGHT.

Part: TIRE — BLOWN (NLG) · airframe 22,851 hrs · 19,390 cycles

NLG TIRE BLOWN OUT ON TAKEOFF. (FLT 6627) COMPLIED WITH TIRE BURST INSPECTION. REPLACED BOTH NLG WHEEL ASSEMBLIES AND AFT NOSE GEAR DOOR. P/N: 5010598, S/N'S OFF: NR 1 AUG02-4337; NR 2 AUG07-6641.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,574 hrs · 19,160 cycles

NR 3 CABIN OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6394) RELAMPED EMERGENCY LIGHT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 22,352 hrs · 18,979 cycles

NR 3 EMERGENCY CEILING FLOODLIGHT INOPERATIVE. (FLT 6324) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,006 hrs · 18,696 cycles

FORWARD MOST OVERHEAD EMERGENCY LIGHT IS NOT ILLUMINATING. (FLT 6676) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,840 hrs · 18,562 cycles

OVERHEAD EMERGENCY LIGHT INOPERATIVE. (FLT 6760) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,573 hrs · 18,348 cycles

NR 1 CEILING EMERGENCY LIGHT IS INOPERATIVE. (FLT 6698) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 21,348 hrs · 18,163 cycles

RIGHT OVERWING FORWARD EXTERIOR EMERGENCY FLOODLIGHT INOPERATIVE. (SERVICE CHECK) RELAMPED EMERGENCY LIGHT.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 20,904 hrs · 17,772 cycles

FS 621 AFT PRESSURE BULKHEAD CRACKED AT CARGO DOOR ROLLER GUIDE TRACK. (C CHECK) REPAIRED PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,258 hrs · 18,087 cycles

FS 621 AFT PRESSURE BULKHEAD WEB AT CARGO AFT ROLLER GUIDE TRACK AT TOP CRACK INDICATION NOTED. (C-CHECK) REPAIRED PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,541 hrs · 17,479 cycles

NR 4 CABIN CEILING LEVEL EMERGENCY FLOOD LIGHT INOP. (FLT 5859) RELAMPED EMERGENCY LIGHT.

Part: SHUTOFF VALVE — DEFECTIVE (AC BAY) · airframe 20,395 hrs · 17,345 cycles

LEFT PACK (IN AUTO) WENT TO 100°, PRODUCED SMOKE IN COCKPIT. (FLT 5808) REPLACED LEFT PRSOV. P/N OFF: 3215622-2, S/N OFF: 1254.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,297 hrs · 17,259 cycles

LAST OVERHEAD EMERGENCY CEILING LIGHT INOP. (FLT 5918) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,988 hrs · 16,997 cycles

EMERGENCY LIGHT ON CEILING NEAR LAVATORY INOP. (FLT 6062) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,830 hrs · 16,877 cycles

EMERGENCY LIGHT IN FRONT OF RIGHT EMERGENCY EXIT INOP. (FLT 6739) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,601 hrs · 16,689 cycles

FLT 6374 - EMERGENCY EXIT LIGHT BESIDE MAIN CABIN DOOR INOP. RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,333 hrs · 16,477 cycles

NR 3 EMERGENCY CEILING LIGHT INOP. (FLT 6671)RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,024 hrs · 16,203 cycles

SECOND TO LAST CEILING EMERGENCY LIGHT INOP. (FLT 5897) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,024 hrs · 16,203 cycles

RIGHT WING CENTER EMERGENCY EXIT LIGHTS INOP. (FLT 5835) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,826 hrs · 16,043 cycles

NR 2 AND NR 3 CABIN POD LIGHTS OUT. (FLT 6689) RELAMPED NR 2&3 CABIN EMERGENCY POD LIGHTS IAW AMM 33-51-16.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,826 hrs · 16,043 cycles

NR 3 EMERGENCY LIGHT POD IN CEILING INOP. (FLT 6736) INSTALLED SERVICEABLE LAMP.

Part: SIGN — INOPERATIVE (CABIN) · airframe 18,753 hrs · 15,977 cycles

GREEN EMERGENCY SIGN FORWARD OF SERVICE DOOR INOP. (FLT 6686) REPLACED EMERGENCY SIGN.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 18,699 hrs · 15,929 cycles

FORWARD MOST EXTERNAL EMERGENCY LIGHT ON RIGHT SIDE INOP. (FLT 5879) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,699 hrs · 15,929 cycles

ROW 10 CEILING EMERGENCY FLOOD LIGHT INOP. (FLT 6735) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,536 hrs · 15,799 cycles

EMERGENCY EXIT LIGHT ABOVE GALLEY SERVICE DOOR INOP. (FLT 6547) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,430 hrs · 15,709 cycles

EMERGENCY LIGHT ON OVERHEAD AT ROW 4 INOP. (FLT 6491) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,135 hrs · 15,466 cycles

NR 2 CEILING LEVEL EMERGENCY FLOODLIGHT INOP. (FLT 6330) RELAMPED EMERGENCY LIGHT.

Part: WINDOW — CRACKED (COCKPIT) · airframe 17,956 hrs · 15,331 cycles

F/O'S SIDE WINDOW CRACKED. (FLT 6737) REPLACED WINDOW.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 17,521 hrs · 14,964 cycles

FLT 6541 - SECOND TO LAST EMERGENCY FLOOD LIGHT INOP. RELAMPED.

Part: MOTOR — JAMMED (PAX DOOR) · airframe 17,036 hrs · 14,581 cycles

FLT 5951 - PAX DOOR WOULD NOT OPEN. REPLACED DOOR ASSIST MOTOR PN 2R5206B SN OFF A0468.

Part: UPLOCK HOOK — OUT OF ADJUST (LT MLG) · airframe 16,968 hrs · 14,516 cycles

FLT 5969 - LEFT GEAR DISAGREE WARNING MESSAGE. LEFT AND RIGHT UPLOCK HOOK PROXIMITY SWITCHES ADJUSTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,472 hrs · 14,132 cycles

FLT 5937 - CEILING EMERGENCY FLOOD LIGHT NEXT TO LAV INOP. REPLACED LIGHT ASSEMBLY.

Part: FITTING — CORRODED (TE FLAP) · airframe 16,632 hrs · 14,258 cycles

RIGHT INBOARD FLAP INBOARD HINGE/FLAP ACTUATOR FITTING INBOARD BEARING CORRODED (C-CHECK). REPLACED PER AMM.

Part: COVER — LEAKING (ENGINE) · airframe 14,342 hrs · 12,307 cycles

RECEIVED A RIGHT ENGINE OIL PRESS WARNING MESSAGE ON DESCENT. PERFORMED PRECAUTIONARY SHUT DOWN, FLIGHT NR 5873. SECURED CRANK PAD COVER AND VERIFIED INSTALLATION IAW CRJ 200 AMM 72-00-00. OPS CHECK GOOD.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 13,680 hrs · 11,772 cycles

OVERHEAD, RIGHT SIDE AND FORWARD GALLEY EMERGENCY LIGHTS ARE INOP. REPLACED NR 2 EMERGENCY LIGHT CHARGER ASSEMBLY IAW AMM 33-52-04.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 13,599 hrs · 11,702 cycles

EMERGENCY FLOOR LIGHTING AFT OF OVERWING EXIT IS INOP. REPLACED NR 4 EMERGENCY LIGHT POWER INVERTER. OPS CHECK GOOD IAW CRJ 200 MM 33-51-00.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 12,051 hrs · 10,343 cycles

TWO OVERHEAD EMERGENCY LIGHTS IN CABIN WILL NOT TEST. RELAMPED BOTH OVERHEAD EMERGENCY EXIT LIGHTS.

Part: STEP — CRACKED (PAX DOOR) · airframe 11,617 hrs · 9,956 cycles

PAX DOOR BOTTOM FOLDING STEP CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW PAX DOOR BOTTOM FOLDING STEP PER CRJ200 AMM 52-11-04-400-802.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 11,617 hrs · 9,956 cycles

AFT EQUIPMENT COMPARTMENT DIRECTLY UNDER RT ACM, ANGLE BRACKET IS CRACKED IN 2 PLACES, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED ANGLE BRACKET UNDER RT AC IN AFT EQUIPMENT COMPARTMENT PER CRJ200 SRM 51-42-06 PG 18 AND CRJ200 SRM 51-42-20 PG 12 FIG-7.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 11,617 hrs · 9,956 cycles

FS 280 FLOOR SUPPORT BEAM CRACKS FOUND AT RBL12 AND LBL12, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED PARTS PER CRJ200 REO 601R-53-11-171 REV C AND COMPLIED WITH SKYWEST RII 53-900-1001.

Part: SUPPORT BEAM — CRACKED (LT ENGINE) · airframe 11,617 hrs · 9,956 cycles

ENGINE SUPPORT BEAM LOWER WEB FOUND TO BE CRACKED AT FWD INBD CORNER OF LT ACCESS PANEL, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR AT LT LOWER WEB OF ENG SUPPORT BEAM FWD INBD CORNER OF ACCESS PN CUTOUT PER REO 601R 53-61-358.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 11,617 hrs · 9,956 cycles

PAX DOOR AFT DRAG ANGLE CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR ANGLE AND SPLICE ANGLES PER CRJ200 REO 601-R52-11-513 STEP 6-10.

Part: ANGLE — CRACKED (PAX DOOR) · airframe 11,617 hrs · 9,956 cycles

PAX DOOR NR 5 STEP AFT ANGLE CRACKED AT DOOR RAIL FITTING AND AT BOTTOM OF NR 4 STEP AFT WEB, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PART AND AFT GAS SPRING MOUNT BRACKET PER CRJ200 REO 601R-53-11-702 ZONES 2,2 AND 4 REPAIR STEPS 8, 10, 13, 16 AND 17.

Part: SUPPORT BEAM — CRACKED · airframe 11,617 hrs · 9,956 cycles

ENGINE SUPPORT BEAM LOWER WEB FOUND TO BE CRACKED AT FWD INBD WEB CORNER OF RT ACCESS PANEL CUTOUT, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS TO LOWER WEB RT ENG SUPPORT BEAM PER CRJ200 SRM 51-42-06 PG 11 SRM 51-42-20 PG 23.

Part: DOUBLER — CRACKED (BS 640) · airframe 11,617 hrs · 9,956 cycles

RT STA 640 REINFORCEMENT DOUBLER BETWEEN STR 9 AND STR 12 FOUND TO BE CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED FS 640 RHS DOUBLER IAW CRJ200 SRM 51-42-06 PG 11 FIG 8 SRM 51-42-21 PG 17 AND REO 601R-53-61-2056 A.

Part: BULKHEAD — CRACKED (BS 280) · airframe 11,617 hrs · 9,956 cycles

CABIN 280 BULKHEAD BELOW THE FLOOR AT STRINGER 9L AND 9R EACH HAVE A CRACK, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED CLIPS AT RBL9 AND LBL9.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 11,617 hrs · 9,956 cycles

PAX DOOR OTBD HANDLE CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED PAX DOOR OUTER HANDLE AS PER CRJ200 AMM 52-11-03-000-802 AND 52-11-03-400-802.

Part: ANGLE — CRACKED (PAX DOOR) · airframe 11,617 hrs · 9,956 cycles

PAX DOOR NR 5 STEP FWD STEP ANGLE CRACKED AT DOOR RAIL FITTING, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED DOUBLER AND REPAIR ANGLES PER CRJ200 REO 601-R52-11-702 (REV-) RII 52-900-1001 AND REO 601R-52-11-702.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 11,266 hrs · 9,654 cycles

EMERGENCY LIGHT OVERHEAD ROW 5 INOP. REPLACED LAMP. OPERATIONAL TEST GOOD, REF MM CH 33-51-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,879 hrs · 8,501 cycles

NUMBER THREE POD EMERGENCY LIGHT IN CEILING INOP. REPLACED LAMP IAW CRJ AMM 33-00-00. OPERATIONAL CHECKS GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 9,225 hrs · 7,894 cycles

MOST FORWARD EMERGENCY LIGHT IN CABIN CEILING IS INOP. RELAMPED FWD EMERGENCY LIGHT. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB TRIM) · airframe 8,893 hrs · 7,593 cycles

"STAB CH 2" STATUS MSG IN FLIGHT WOULD NOT TAKE RESET ON GROUND. REPLACED THE HSTCU AND REPLACED HSTCA MOTOR CONTROL UNIT IAW CRJ 200 MM 27-41-01. OPERATIONAL CHECK SATISFACTORY.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB TRIM) · airframe 8,893 hrs · 7,593 cycles

"STAB TRIM CH 1" STATUS MSG ILLUMINATED IN FLIGHT. REPALCED HSTCU. OPERATIONAL CHECK GOOD REF 27-41-01.

Part: CONTROL UNIT — MALFUNCTIONED (TRIM SYSTEM) · airframe 8,879 hrs · 7,575 cycles

A/P PITCH TRIM CAUTION IN INITIAL DESCENT. REPLACED HSTCU IAW MM 27-41-01 AND REPLACED FCC IAW MM 22-12-14. OPERATIONAL CHECK NORMAL, P/N: 7060-9 S/N OFF: 1203 P/N: 622-9815-704 S/N OFF: YXRL.

Part: ACTUATOR — MALFUNCTIONED (HORIZ STAB) · airframe 8,835 hrs · 7,527 cycles

STAB CH1 INOP STATUS MESSAGE. REPLACED MCU AND TRIM ACTUATOR WITH SERVICEABLE UNITS PER CRJ MM 27-42-01. OPERATIONAL CHECK GOOD. PN 1 ON/OFF 8396-3 SN 1 OFF 796, PN 2 ON/OFF 7062-3 SN 2 OFF 1009.

Part: CONTROL UNIT — MALFUNCTIONED (STAB TRIM) · airframe 8,801 hrs · 7,495 cycles

"STAB CH1 INOP" STATUS MESSAGE ILLUMINATED INFLIGHT. REPLACED STAB TRIM/PITCH DISCONNECT SWITCH IAW MM 27-41-30, HSTCU IAW 27-41-00 AND STAB TRIM PANEL IAW AMM 27-41-15. OPERATIONAL CHECK GOOD.

Part: TRIM SWITCH — INOPERATIVE (COCKPIT) · airframe 8,354 hrs · 7,087 cycles

CAPTAIN SIDE TRIM SWITCH INOP, WILL NOT TRIM NOSE UP OR DOWN. REPLACED CAPTAIN'S TRIM SWITCH ON YOKE. OPERATIONAL TEST GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 7,723 hrs · 6,551 cycles

EMERGENCY CEILING LIGHT AT ROW 10 INOP. RE-LAMPED CEILING LIGHT AT ROW 10 AS REQUIRED. OPERATIONAL CHECK GOOD.

Part: POSITION SENSOR — MALFUNCTIONED (TE FLAPS) · airframe 7,537 hrs · 6,404 cycles

FLAPS FAIL MESSAGE IN FLIGHT. REPLACED BRAKE POSITION SENSOR UNIT ON LEFT SIDE REF 27-52-05. OPERATIONAL CHECK GOOD.

Part: BPSU — MALFUNCTIONED (TE FLAPS) · airframe 7,510 hrs · 6,382 cycles

FLAPS FAIL MESSAGE WILL NOT RESET. REPLACED LEFT BPSU AND RIGGED PER MM 27-51-10. OPERATIONAL CHECK GOOD.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 8,199 hrs · 6,957 cycles

AT FS 484 AND RBL 36 JUST UNDER FLOOR LEVEL INTERCOSTAL CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW REO 601R-53-41-059 AND SRM 51-42-06.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 8,199 hrs · 6,957 cycles

FLOOR SUPPORT AT FS 621 REAR CARGO BAY LEFT FOUND TO BE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW REO 601R-53-61-114.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 8,199 hrs · 6,957 cycles

FS 280 AT LBL 9 I/B ANGLE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. ANGLE REPAIRED IAW REO 601R-53-11-136 AND SRM 51-42-06 AND 51-42-21.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 8,199 hrs · 6,957 cycles

FS 280 AT RBL 9 I/B AND O/B ANGLE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. ANGLES REPAIRED IAW REO 601R-53-11-136 AND SRM 51-42-06 AND 51-42-21.

Part: HANDLE — LACK OF LUBE (SERVICE DOOR) · airframe 6,536 hrs · 5,570 cycles

SERVICE DOOR WILL NOT OPEN FROM THE OUTSIDE. LUBED SERVICE DOOR INNER AND OUTER HANDLE, OPERATIONAL & FUNCTIONAL CHECK GOOD IAW CRJ 200 MM 52-41-00.

Part: ROD END — OUT OF ADJUST (SERVICE DOOR) · airframe 6,378 hrs · 5,434 cycles

SERVICE DOOR REQUIRES EXCESSIVE FORCE TO OPEN. REPLACED ROD ENDS AND ADJUSTED SERVICE DOOR UPPER ATTACHMENT ARM AND CLEANED DOOR SEAL. OPERATIONAL CHECK GOOD.

Part: BEARING — ROUGH (SERVICE DOOR) · airframe 5,030 hrs · 4,300 cycles

GALLEY SERVICE DOOR DIFFICULT TO CLOSE. LUBRICATED/SERVICED SERVICE DOOR CORNER SLIDE BEARINGS. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (MOTOR) · airframe 4,785 hrs · 4,125 cycles

AUTO-PILOT PITCH TRIM CAUTION MESSAGE WHEN FLAPS EXTENDED TO 30 DEGREES. REMOVED AND REPLACED MOTOR CONTROL UNIT AND HSTA IAW CRJ MM 27-42-05 AND 27-42-01. OPERATIONAL CHECK GOOD IAW CRJ MM 27-40-00. P/N (HSTA): 8396-3, S/N OFF: 908.

Part: CONTROL PANEL — MALFUNCTIONED (RUDDER TRIM) · airframe 4,460 hrs · 3,821 cycles

DURING ORIGINATING CHECK, RUDDER TRIM WOULD ONLY MOVE RIGHT, NOT LT. REMOVED AND REPLACED TRIM CONTROL PANEL IAW CRJ 200 MM CHAPTER 27-12-10. OPS CHECK GOOD.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 3,957 hrs · 3,363 cycles

FS 484 LEFT INTERCOSTAL OUTBOARD FLANGE LBL 36 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. INTERCOSTAL REPAIRED IAW CRJ REO 601R-53-41-059 REV A & RII 53-401.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 3,957 hrs · 3,363 cycles

FS 625 RIGHT INTERCOSTAL ANGLE STR 14R CRACKED. DISCOVERED DURING C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40-11, 51-42-06. P/N: 601-35012-52.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 3,957 hrs · 3,363 cycles

FS 280 LEFT FLOORBEAM LBL 9.0 O/B ATTACH ANGLE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00, RII 53-401. P/N: 601R31113-57.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 3,965 hrs · 3,377 cycles

FS 621 RIGHT FLOOR SUPPORT ANGLE RBL 42 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. ANGLE AT FS 261 RIGHT REPAIRED IAW CRJ REO 601R-53-61-117 REV A AND RII 53-401. P/N: 601R53-61-117-4, 601R53-61-117-2.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 3,957 hrs · 3,363 cycles

FS 280 RIGHT FLOORBEAM RBL 9.0 INBOARD AND OUTBOARD ATTACH ANGLES CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLES IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00, RII 53-401. P/N: 601R31113-58.

Part: ODOR — DETECTED (CABIN) · airframe 2,266 hrs · 1,882 cycles

DETECTED SMOKE IN THE CABIN AT 500 FT AFTER T/O. SMOKE WAS NOT THICK BUT SMELLED LIKE PLASTIC. SMOKE DISSIPATED UPON RETURN TO FIELD. INSPECTED AFT EQUIPMENT BAY, GEAR BAY, AVIONIC BAY, ALL INTERIOR LIGHTS AND BALLAST. NO MESSAGES ON ECAS. EVERYTHING WORKS, ALL CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 2,111 hrs · 1,743 cycles

EMERGENCY LIGHT, FORWARD - CENTER - CEILING, IS INOP. REMOVED AND REPLACED FORWARD - CENTER - CEILING EMERGENCY LAMP IAW CRJ MM 33-51-16. OPS CHECK GOOD.

Part: WINDOW — CRACKED (COCKPIT) · airframe 1,207 hrs · 1,024 cycles

RT COCKPIT SIDE WINDOW CRACKED. REPLACED RIGHT COCKPIT SIDE WINDOW. OPS CHECK GOOD. NO LEAKS NOTED IAW MM 56-11-01 AND 56-12-01. P/N: NP-139322-6 S/N OFF: 02052H9140.

Part: CONTROL PANEL — MALFUNCTIONED (COCKPIT) · airframe 705 hrs · 629 cycles

AIRCRAFT HAD SEVERAL OCCASIONS WHERE WE RECEIVED `AP TRIM` MESSAGES BOTH PITCH TRIM AND TRIM LEFTWARD. AIRCRAFT ALSO WENT INTO AN UNCOMMANDED LEFT ROLL. REMOVED AND REPLACED FLIGHT CONTROL PANEL AS REQUIRED. SYSTEM OPS CHECKS GOOD IAW 22-11-00.

Part: BPSU — FAILED (T/E FLAP) · airframe 99 hrs · 89 cycles

FLAP FAIL MESSAGE APPEARED DURING TAXI IN. REMOVED AND REPLACED RIGHT FLAP BPSU IAW CRJ MM 27-51-10. OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 2,320 hrs · 1,949 cycles

FOUND ON PREFLIGHT INSPECTION SECOND EMERGENCY LIGHT AFT OF FORWARD DOOR (LEFT SIDE) BURNED OUT. RE-LAMPED SECOND EMERGENCY LIGHT ON LEFT OVERWING WITH SERVICEABLE BULB. OPS CHECK GOOD AT THIS TIME.