N869AS

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 42,019 hrs · 36,876 cycles

RECEIVED A GEAR DISAGREE WARNING AND NOSE DOOR WARNING DURING GEAR EXTENSION ON APPROACH. BOTH WARNINGS DISAPPEARED AND GEAR DISPLAYED DOWN AND 3 GREEN WHEN GEAR WAS DOWN AND LOCKED. (FLT#5361) FO: 03/08/2019 WORK IN PROGRESS

Part: SKIN — CHAFED (FUSELAGE) · airframe 41,039 hrs · 36,006 cycles

RT EXTERNAL FUSELAGE SKIN FOUND CHAFED FROM APPROX FS 700.00 TO FS 736.00 AND FROM STR 11R TO STR 10R. (C-CHECK) RO: 09/12/2018. REPAIRED CHAFED SKIN AT AFT END OF RT ENGINE PYLON FROM STR 9R TO 12R AND APPROX FS700 TO FS755 IAW REO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,039 hrs · 36,006 cycles

MULTIPLE CRACKS IN THE ATTACHMENT FLANGE OF FS718 BTWN STR 11R-12R. (C-CHECK) RO: 09/12/2018. REPLACED FRAME SECTION AT FS718 WITH ATTACHMENT FLANGE BTWN STR 11R-12R IAW REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 41,039 hrs · 36,006 cycles

FS 280 BLKHD WEB REQUIRES DUE TO CRACKS FOUND AT LBL9 AND RBL9. (C-CHECK) RO: 09/12/2018. COMPLIED WITH REPAIR OF THE FS280 BLKHD IAW REO.

Part: FRAME — CORRODED (FUSELAGE) · airframe 41,039 hrs · 36,006 cycles

FS 605.00 FRAME HAS CORROSION (BOTH SIDES) BETWEEN APPROX STR 21L TO STR 27. (C-CHECK) RO: 09/12/2018. REMOVED AND REPLACED FS605.00 FRAME IAW SRM. ALL CHECKS GOOD.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 41,039 hrs · 36,006 cycles

THE RT INTERCOSTAL FWD OF THE AVIONICS BAY DOOR CUTOUT, BETWEEN FS 349 AND FS 364 ADJACENT TO STRINGER 27, HAS MULTIPLE SPOTS OF CORROSION. (C-CHECK) RO: 09/12/2018. REPAIRED CORROSION RT INTERCOSTAL ADJACENT TO STR 27 BETWEEN FS 349 AND 364 IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 41,039 hrs · 36,006 cycles

FS 349 FRAME HAS MULTIPLE SPOTS OF CORROSION ALONG ITS FWD VERTICAL WEB FACE AND AFT WEB FACE AND LOWER FLANGE BETWEEN STRINGER 26L AND STRINGER 26R. (C-CHECK) RO: 09/12/2018. REMOVED AND INSTALLED NEW FRAME SECTION P/N 601R32005-69 IAW REO.

Part: FRAME — CORRODED (FUSELAGE) · airframe 41,039 hrs · 36,006 cycles

FS 364 FRAME HAS MULTIPLE SPOTS OF CORROSION ALONG ITS FWD FACE LOWER FLANGE FROM THE OUTBOARD SIDE OF STRINGER 26L TO STRINGER 26R. (C-CHECK) RO: 09/12/2018. REMOVED AND INSTALLED NEW FRAME P/N 601R32007-11 AT AVIONICS DOOR OPENING (FS364) IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 41,039 hrs · 36,006 cycles

THE LT INTERCOSTAL FWD OF THE AVIONICS BAY DOOR CUTOUT, BETWEEN FS 349 AND FS 364 ADJACENT TO STRINGER 27, HAS MULTIPLE SPOTS OF CORROSION. (C-CHECK) RO: 09/12/2018. REMOVED CORROSION, LT INTERCOSTAL ADJACENT TO STGR27 BETWEEN FS349 AND FS364, IAW SRM AND REO.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 41,039 hrs · 36,006 cycles

SEVERAL DENTS ON RIGHT SIDE OF FUSELAGE BELOW WL 73.50 FS542.00 TO FS581.00. (C-CHECK) RO: 09/12/2018. C/W REPAIR OF SEVERAL DENTS ON RIGHT SIDE OF FUSELAGE BELOW WL 73.50, FS542.0 TO FS581.0 IAW REO.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 41,039 hrs · 36,006 cycles

PROTRUDING DENT ON RIGHT SIDE OF FUSELAGE BELOW WL 73.50 FS658.00. (C-CHECK) RO: 09/12/2018. REWORKED DENT LOCATED ON FUSELAGE BELOW WL 73.50 AT FS658.00, IAW REO.

Part: SKIN — DENTED (LT WING) · airframe 41,039 hrs · 36,006 cycles

MULTIPLE DENTS ON THE LT WING LEADING EDGE AT APPROX WS 137.00. (C-CHECK) RO: 09/12/2018. REPAIRED 4 EA DENTS ON LT WING CENTER L/E SKIN IAW REO.

Part: BRACKET — DAMAGED (PROXIMITY SENSOR) · airframe 38,695 hrs · 33,694 cycles

STEERING INOPERATIVE CAUTION INFLIGHT. COMPLIED WITH QRH AND RETURN TO FIELD. DECLARED EMERGENCY. REMOVED AND REPLACED THE PROXIMITY SENSOR BRACKET IAW AMM. OPS CHECKED GOOD. PERFORMED GEAR SWINGS. OPS CHECKED GOOD.

Part: BRACKET — CRACKED (NLG) · airframe 37,198 hrs · 32,158 cycles

AIRCRAFT RETURNED TO THE FIELD WITH A NOSE DOOR OPEN, GEAR DISAGREE MESSAGE. DID NOT DECLARE AN EMERGENCY. R & R THE BENT AND CRACKED PROXIMITY SWITCH SENSOR BRACKET. ADJUSTED AND SWUNG GEAR, OPS GOOD.

Part: CONNECTOR — UNSECURE (NLG) · airframe 35,763 hrs · 30,842 cycles

IN FLIGHT GEAR DISAGREE. SECURED CONNECTOR FOR NOSE GEAR DOORS SEQUENCING VALVE AND ADJUSTED WOW SENSOR, SYSTEMS OPERATE NORMAL.

Part: UNKNOWN — ODOR (CABIN) · airframe 33,765 hrs · 28,849 cycles

BURN SMELL INFLIGHT. INSPECTED AND OPERATED BOTH PACKS USING APU AND ENGINE BLEED FOR SEVERAL MINUTES. DID NOT NOTICE A BURN SMELL. ALSO INSPECTED ALL CABIN LIGHTS FOR ANY SIGNS OF BURN MARKS OR FALSE CONTACT. COULD NOT FIND ANY DISCREPANCY. R & R UNITS AT 10 A/B & 11 C/D FOR TEST. OPS CHECK GOOD AT THIS TIME, PN: BR9500-5.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 32,234 hrs · 27,360 cycles

FLOOR EXIT SIGN HAS A BROKEN WIRE. REPAIRED THE WIRES IAW ESPM.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 32,234 hrs · 27,360 cycles

GALLEY EMERGENCY EXIT SIGN HAS TWO BROKEN WIRES. REPAIRED WIRES IAW ESPM.

Part: WIRE — LOOSE (EMERGENCY LIGHT) · airframe 32,234 hrs · 27,360 cycles

EXIT SIGN ON LOWER CORNER OF WARDROBE HAS A LOOSE WIRE. REPAIRED WIRE IAW ESPM AND AMM.

Part: FRAME — CORRODED (BS 333) · airframe 32,234 hrs · 27,360 cycles

BS 333 FRAME CORRODED BETWEEN STRINGERS 26L-26R ON FWD AND AFT SIDES. REPLACED FRAME IAW SRM.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 32,234 hrs · 27,360 cycles

RT SIDE, BS 484 OUTSIDE FUSELAGE INTERCOSTAL HAS SUSPECT CRACK AT UPPER RADIUS. C-CHECK, REPLACED INTERCOSTAL IAW SRM.

Part: ATTACH FITTING — CHAFED (LT MLG DOOR) · airframe 32,234 hrs · 27,360 cycles

LEFT MLG DOOR STRUT ATTACH FITTING CHAFED, REPAIRED LT MLG DOOR STRUT ATTACH FITTING IAW REO.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 32,234 hrs · 27,360 cycles

LEFT INBD FLAP VANE, INBD L/E CHAFED. BLENDED CHAFE IAW REO & SRM.

Part: BELLCRANK — CHAFED (RT MLG DOOR) · airframe 32,234 hrs · 27,360 cycles

RIGHT MLG DOOR BELLCRANK CHAFED, C-CHECK, REPAIRED RT MLG DOOR BELLCRANK.

Part: STRUT — CHAFED (RT MLG DOOR) · airframe 32,234 hrs · 27,360 cycles

RIGHT MLG DOOR STRUT CHAFED, C-CHECK. REPAIRED RT MLG DOOR STRUT IAW REO.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 32,234 hrs · 27,360 cycles

RT INBD FLAP VANE INBD L/E CHAFED. BLENDED CHAFE IAW REO & SRM.

Part: ATTACH FITTING — CHAFED (RT MLG DOOR) · airframe 32,234 hrs · 27,360 cycles

RIGHT MLG DOOR STRUT ATTACH FITTING CHAFED, C-CHECK, REPLACED RT MLG ATTACH FITTING REF SRM.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 32,234 hrs · 27,360 cycles

LEFT INBD FLAP VANE OTBD L/E CHAFED. BLENDED CHAFE IAW REO & SRM.

Part: STRUCTURE — CHAFED (LT MLG DOOR) · airframe 32,234 hrs · 27,360 cycles

LEFT MLG DOOR INTERIOR L/E CHAFED, C-CHECK. REMOVED DAMAGE, FABBED REPAIRED PARTS, AND INSTALLED REPAIR PARTS ON LT MLG DOOR REF REO.

Part: STRUCTURE — DAMAGED (CARGO DOOR) · airframe 32,234 hrs · 27,360 cycles

CARGO DOOR IS GOUGED & CHAFED IN REPAIR DOUBLER TOP SIDE. BLENDED OUT DAMAGED AREA ON TOP OF REPAIR DOUBLER ON CARGO DOOR IAW SRM. REPLACED DOUBLER IAW REO.

Part: UNKNOWN — SMOKE (COCKPIT & CABIN) · airframe 31,852 hrs · 26,973 cycles

OIL ODOR AND SMOKE IN COCKPIT AND CABIN, STARTED WHEN SELECTED PACKS ON. RAN LT AND RT ENGINES THRU HIGH POWER SETTINGS SELECTED AC PACKS IN MANUAL AND AUTO. NO SMOKE NOTED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 31,529 hrs · 26,660 cycles

OVERHEAD EMERGENCY LIGHT IS BURNED OUT, REPLACED LAMP.

Part: CONNECTOR — DIRTY (CABIN) · airframe 31,386 hrs · 26,520 cycles

EMERGENCY LIGHT DOES NOT ILLUMINATE ON LT, EXIT ROW, FWD OF EXIT DOOR. FLT 2622 CLEANED & RECONNECTED LT OVERWING EXIT SIGN CONNECTOR, OPERATIONS CHECKED GOOD.

Part: CONTROL UNIT — FAILED (ELEVATOR) · airframe 31,301 hrs · 26,441 cycles

THE ELEVATORS FEEL AS THOUGH SOMETHING IS BINDING & OR RESTRICTING THEIR MOVEMENT & A DELAY IN PITCH MOVEMENT. FLT 2643 REPLACED PITCH FEEL CONTROL UNIT, PN ON OFF 30000-09, SN ON 02-743 & SN OFF 00-536.

Part: CONNECTOR — LOOSE (CABIN) · airframe 31,265 hrs · 26,399 cycles

FWD SECTION OF FLOOR EMERGENCY LIGHTS WILL NOT ILLUMINATE. SERVICE SECURED LOOSE CONNECTOR ON FLOOR STRIP.

Part: SIGN — INOPERATIVE (CABIN) · airframe 31,265 hrs · 26,399 cycles

EMERGENCY EXIT SIGN AT OVERWING EXIT IS BURNED OUT. FLT 2602 REPLACED EMERGENCY EXIT SIGN ON LT OVERWING EXIT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,216 hrs · 26,344 cycles

LOWER LT EMERGENCY EXIT DOOR LIGHT NEAR FLOOR DOES NOT ILLUMINATE. FLT 2612 RESET.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 31,156 hrs · 26,285 cycles

EMERGENCY LIGHTS INOPERATIVE. FLT 2592 CHARGED EMERGENCY LIGHT BATTERY PACKS EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,156 hrs · 26,285 cycles

EXIT DOOR LIGHT, LOWER ON A/C LT OVERWING DOOR BURNED OUT. FLT 2606 CHARGED EXIT DOOR LIGHT ON A/C LT OVERWING DOOR WITH GND POWER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,978 hrs · 26,090 cycles

LT OVERWING EMERGENCY EXIT LIGHT AT ROW 8 AB IS BURNED OUT. FLT 2620RELAMPED.

Part: O-RING — DAMAGED (APU) · airframe 30,873 hrs · 25,988 cycles

STRONG JET FUEL ODOR THROUGHOUT THE COCKPIT & SERVICE GALLEY. FLT NR 2858 REPLACED O-RING TO APU FUEL CONTROL.

Part: LENS — UNKNOWN (CABIN) · airframe 29,359 hrs · 24,366 cycles

EMERGENCY FLOOR FLOODLIGHT LENS COVER BY MAIN CABIN DOOR. (FLT 2680) REPLACED EMERGENCY FLOOR FLOODLIGHT ASSEMBLY.

Part: COOLING FAN — FAILED (NR 1) · airframe 28,806 hrs · 23,784 cycles

DISPLAY COOL CAUTION MESSAGE IN FLIGHT. MESSAGE EXTINGUISHED, BUT A STRONG ELECTRICAL SMELL IS PRESENT. (FLT 2600) REPLACED DISPLAY COOL FAN NR 1 IAW AMM. P/N ON AE0804C01 S/N ON L1147 P/N OFF AE0804AA2 S/N OFF 2033.

Part: SIGN — DETACHED (CABIN) · airframe 28,284 hrs · 23,176 cycles

EMERGENCY EXIT SIGN OVER THE GALLEY SERVICE DOOR FELL OFF. (FLT 4531) REPLACED LIGHT ASSEMBLY. P/N: BF1-0044-004

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 28,106 hrs · 23,014 cycles

CRACK ON FS 621 BULKHEAD WEB, FORWARD FACE, ABOVE UPPER CARGO DOOR TRACK FITTING. (C-CHECK) REPAIRED CRACK ON FS 621 BULKHEAD WEB IN REFERENCE TO REO.

Part: POST — CRACKED (FUSELAGE) · airframe 28,106 hrs · 23,014 cycles

CRACK AT LEFT FS 409+128 VERTICAL POST AT LBL 18, OUTBOARD C-CHANNEL, AFT RADIUS. (C-CHECK) REPLACED OUTBOARD C-CHANNEL VERTICAL POST AT FS 409+128 LBL 18 PER CRJ 200 REO.

Part: POST — CRACKED (FUSELAGE) · airframe 28,106 hrs · 23,014 cycles

CRACK AT RIGHT FS 409+128 VERTICAL POST AT RBL 18, OUTBOARD AND INBOARD C-CHANNELS, AFT RADIUS. (C-CHECK) REPLACED OUTBOARD AND INBOARD C-CHANNELS AT FS 409+128 RBL 18 PER CRJ 200 REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 28,106 hrs · 23,014 cycles

CRACK ON FS 621 BULKHEAD WEB, FORWARD FACE AT BL 0.0 ON WL 100. (C-CHECK) REPAIRED PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,959 hrs · 22,874 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4597) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,659 hrs · 22,586 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4835) RELAMPED EMERGENCY LIGHT.

Part: TIRE — BURST (MLG) · airframe 27,659 hrs · 22,586 cycles

NR 2 MLG TIRE BURST ON LANDING. (FLT 4846) REPLACED NR 1 AND NR 2 MLG WHEEL ASSEMBLY'S. P/N 5010571 S/N'S OFF DEC01-4581 AUG01-4289.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,617 hrs · 22,547 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4517) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,218 hrs · 22,127 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4475) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,176 hrs · 22,087 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4735) RELAMPED EMERGENCY LIGHT.

Part: BEARING — CORRODED (ENGINE MOUNT) · airframe 27,060 hrs · 21,985 cycles

THE LEFT ENGINE FORWARD YOKE MOUNT UPPER LINK HAS PITTING ON THE BEARINGS. (SERVICE) INSTALLED A SERVICABLE LINK TO THE LEFT ENGINE FORWARD YOKE MOUNT.

Part: BEARING — CORRODED (ENGINE MOUNT) · airframe 27,060 hrs · 21,985 cycles

THE LEFT ENGINE FORWARD YOKE MOUNT HAS PITTING ON THE BEARINGS. (SERVICE) INSTALLED A SERVICABLE FORWARD YOKE MOUNT ON THE LEFT ENGINE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,938 hrs · 21,864 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 13 IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 26,415 hrs · 21,358 cycles

NR 7 EXTERIOR EMERGENCY LIGHT INOPERATIVE. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,208 hrs · 21,162 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4600) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,073 hrs · 21,041 cycles

FORWARD AND AFT LEFT OVERWING EMERGENCY LIGHTS ARE OUT. (FLT 4491) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,645 hrs · 20,656 cycles

EMERGENCY LIGHT OVER ROW 5 IS OUT. (FLT 4655) RELAMPED EMERGENCY LIGHT.

Part: CONNECTOR — LOOSE (CABIN) · airframe 25,425 hrs · 20,458 cycles

FLOOR EMERGENCY LIGHTS FROM EMERGENCY EXIT ROW TO THE AFT OF THE CABIN ARE OUT. (FLT 4759) TIGHTENED EMERGENCY FLOOR LIGHTING CONNECTOR.

Part: SIGN — BROKEN (CABIN) · airframe 25,284 hrs · 20,347 cycles

EMERGENCY EXIT SIGN ABOVE SERVICE DOOR IS BROKEN. (FLT 4565) REMOVED EMERGENCY LIGHT ASSEMBLY.

Part: SELECTOR VALVE — FAILED (LANDING GEAR) · airframe 24,769 hrs · 19,932 cycles

GEAR WAS SELECTED DOWN, NOSE GEAR CAME DOWN AND BOTH MAIN GEARS REMAINED UP. USED EMERGENCY RELEASE AND ALL GEAR MOVED DOWN AND LOCKED. (FLT 4585) REPLACED MAIN LANDING GEAR SELECTOR VALVE PER AMM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 24,734 hrs · 19,900 cycles

FS 202.75 CRACKED AT PARKING BRAKE CABLE HOLE. (C-CHECK) REPAIR PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,665 hrs · 18,981 cycles

NR 1 CEILING EMERGENCY LIGHT INOP. (FLT 4780) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,160 hrs · 18,549 cycles

EMERGENCY EXIT OVERHEAD CEILING LIGHT NR 2 INOP. (FLT 4604) RELAMPED EMERGENCY LIGHT.

Part: FLAP — OUT OF RIG (WING) · airframe 22,758 hrs · 18,213 cycles

WITH FLAPS SELECTED TO 45° AIRCRAFT DEVELOPS A LEFT ROLL. (FLT 4601) RE-RIGGED RIGHT FLAPS AND LEFT OUTBOARD FLAP SPRING BACK.

Part: FLAP — OUT OF RIG (WING) · airframe 22,758 hrs · 18,213 cycles

WHEN FLAPS SELECTED TO 45 DEGREES AIRCRAFT ROLLED LEFT UNCOMMANDED. (FLT 4779) RIGGED LEFT AND RIGHT FLAPS.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 21,307 hrs · 17,063 cycles

GEAR DISAGREE WARNING MESSAGE DISPLAYED. (FLT 4869) INSPECTIONS AND OPERATION CHECKS NORMAL.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 20,367 hrs · 16,354 cycles

C-CHECK, 4 CLIPS AT RBL9 AND LBL9 FS280 CRACKED. REPAIRED PER REO.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 20,367 hrs · 16,354 cycles

C-CHECK, RIGHT FLOOR SUPPORT INTERCOSTAL AT FS484, INBOARD BRACKET TO FLOOR BEAM RBL27 CRACKED. REPLACED PER SRM.

Part: WINDOW POST — CRACKED (FUSELAGE) · airframe 20,367 hrs · 16,354 cycles

DURING C-CHECK, LEFT WINDSHIELD SIDE POST OUTBOARD CLIP CRACKED. REPLACED PER SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 20,367 hrs · 16,354 cycles

C-CHECK, CRACK ON AFT PRESSURE BULKHEAD AT LOWER BOTTOM LINTEL FITTING. REPAIRED PER REO.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 20,367 hrs · 16,354 cycles

DURING C-CHECK, LEFT FLOOR SUPPORT INTERCOSTAL AT FS 473 ATTACH BRACKET CRACKED. REPAIRED PER REO.

Part: WINDOW POST — CRACKED (FUSELAGE) · airframe 20,367 hrs · 16,354 cycles

C-CHECK, RIGHT WINDSHIELD SIDE POST OUTBOARD CLIP CRACKED. REPLACED PER SRM.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 20,172 hrs · 16,208 cycles

FLT 4489 - EMERGENCY LIGHT NR 2 INOP. RELAMPED.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 17,131 hrs · 13,876 cycles

FLT 3836 - ON TAKEOFF, CAPTAIN'S FORWARD WINDSHIELD CRACKED. REPLACED LEFT WINDSHIELD IAW AMM 56-11-01, PN NPN-139321-13, SN OFF 00301H2214.

Part: WEB — CRACKED (PAX DOOR) · airframe 15,613 hrs · 12,755 cycles

PAX DOOR, THE AFT WEB IS CRACKED UNDER THE HANDRAIL STOW BRACKET AND IN THE RADIUS BETWEEN THE 3RD AND 4TH FIXED STEPS, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED 3RD STEP AND REPAIR STOW BRACKET PER CRJ200 SRM 51-42-20 PG 23.

Part: BRACKET — CRACKED (RT MLG WW) · airframe 15,613 hrs · 12,755 cycles

RT WHEEL WELL HAS THE BRAKE TRANSDUCER BRACKET CRACKED/BROKEN AT TOP MID OF THE WHEEL WELL, DISCOVERED DURING C-CHECK INSPECTION. REPLACED BRAKE TRANSDUCER BRACKET AT RT SIDE WHEEL WELL IAW CRJ200 SRM 51-77-00 PG 1 PARA 3.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 15,613 hrs · 12,755 cycles

FOUND PASSENGER DOOR OUTER HANDLE IS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED PAX DOOR OUTER HANDLE PER CRJ200 SRM 51-42-20 PG 24 .

Part: WEB — CRACKED (PAX DOOR) · airframe 15,613 hrs · 12,755 cycles

PAX DOOR,THE FWD WEB IS CRACKED UNDER THE HANDRAIL STOW BRACKET, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED FABRICATED REPAIR PARTS ON PAX DOOR FWD SIDE PANEL WEB IAW IAW CRJ200 REO 601R-52-11-702, REV NC & C/W SKYWEST RII 52-900-1001 CABIN DOOR REPAIR.

Part: STRINGER CLIP — CRACKED (BS 621) · airframe 15,613 hrs · 12,755 cycles

FOUND CLIP CRACKED AFT SIDE OF 621 BULKHEAD LT, DISCOVERED DURING C-CHECK INSPECTION. REPLACED CLIP 601-35012-51 P/O 71471 AT STA621 STR 14 IAW CRJ200 SRM 51-42-21 PG 17-21 51-40-11 PG 4,15.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 15,613 hrs · 12,755 cycles

PAX DOOR AFT DRAG ANGLE IS CRACKED ADJACENT TO DOOR ASSIST CABLE PULLEY BRACKET, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED ANGLE SECTION PER CRJ200 REO 601R 52-11-513 REV 'A' SHEET 2.

Part: SUPPORT ANGLE — CRACKED (NACELLE) · airframe 15,613 hrs · 12,755 cycles

ENG BEAM RBL8.0 UPPER WEB SUPPORT ANGLE CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW SUPPORT ANGLE AT RBL8.0 UPPER WEB PER CRJ200 SRM 51-42-06 PG 13.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 15,613 hrs · 12,755 cycles

FS 280 LBL9-13 CRACKS BOTH FLOORBEAM SUPPORT ATTACH CLIPS AND 280 BEAM UPPER AND LOWER, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS AT FS280 LBL9-13 UPPER/LOWER BEAM REPAIR PER REO 601R 53-11-138 AND REO 601R 53-11-171.

Part: BRACKET — CRACKED (DOOR ASSIST MOTR) · airframe 15,613 hrs · 12,755 cycles

FOUND PAX DOOR-DOOR ASSIST MOTOR MOUNTING BRACKET CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED PAX DOOR ASSIST MOTOR MOUNTING BRACKET PER CRJ200 SRM 51-42-06 PG 4/SRM 51-41-02 PG 5.

Part: BRACKET — CRACKED (LT MLG WW) · airframe 15,613 hrs · 12,755 cycles

LT WHEEL WELL HAS THE BRAKE TRANSDUCER BRACKET CRACKED/BROKEN AT TOP MID OF THE WHEEL WELL, DISCOVERED DURING C-CHECK INSPECTION. REPLACED BRAKE TRANSDUCER BRACKET AT LT SIDE WHEEL WELL IAW CRJ200 SRM 51-77-00 PG 1 PARA 3.

Part: HANDLE — STUCK (SERVICE DOOR) · airframe 13,417 hrs · 11,122 cycles

SERVICE DOOR WON'T OPEN. REPLACED SERVICE DOOR HANDLE ASSY IAW SRM 51-42-21.

Part: LATCH — LACK OF LUBE (SERVICE DOOR) · airframe 13,196 hrs · 10,966 cycles

SERVICE DOOR OUTER HANDLE WONT COME OUT WHEN PUSH BUTTON IS PRESSED. CLEANED AND LUBED OUTER SERVICE DOOR HANDLE LATCH, OPERATIONAL CHECK GOOD.

Part: PCU — MALFUNCTIONED (FLT SPOILERS) · airframe 13,107 hrs · 10,896 cycles

SPOILERON FAULT MESSAGE INFLIGHT. REPLACED HYD NR 3 OB PCU IAW 27-62-01, OPERATIONAL CHECK GOOD.

Part: INTERCOSTAL — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE INTERCOSTALS AT FS 484, BL 27.00-36.00 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE INTERCOSTALS AT FS 484, BL 27.00-36.00 IAW ASA EO 600-53-0111. (M)

Part: FLOORBEAM — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE FLOORBEAM SUPPORT ANGLE AT FS 280, LBL 9 INBOARD WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM SUPPORT ANGLE AT FS 280, LBL 9 INBOARD IAW SRM 51-00. (M)

Part: SILL — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CARGO BAY FLOOR SILL AT FS 562.72 - FS 589.00 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO BAY FLOOR SILL AT FS 562.72 - FS 589.00 IAW ASA EO 600-53-0095. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE FLOOR SUPPORT AT FS 280 LBL 9.0 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FLOOR SUPPORT AT FS 280.0, LBL 9.0 IAW ASA EO 600-53-0123. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCH, THE FLOOR SUPPORT ANGLE AT FS 621 ON THE LEFT AND RIGHT SIDES WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FLOOR SUPPORT ANGLE AT FS 621 ON THE LEFT AND RIGHT SIDES IAW ASA EO 600-53-0105. (M)

Part: ANCHOR — CRACKED (PAX DOOR)

DURING A C-CHECK IN MCN, THE AFT ANCHOR ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFT ANCHOR ON THE PASSENGER DOOR. (M)

Part: LIGHT — INOPERATIVE (CABIN)

FLT 4512 - DURING A HANGAR INSPECTION IN BTR, THE AFT EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY CEILING LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CONNECTOR — CONTAMINATED (EMERGENCY LIGHT)

DURING A GROUND IN ATL, THE EMERGENCY FLOOR LIGHTS BETWEEN ROWS TWO AND FOUR WERE FOUND TO BE INOPERATIVE. MAINTENANCE CLEANED WATER AND DIRT FROM THE EMERGENCY FLOOR LIGHT CONNECTORS BETWEEN ROWS TWO AND FOUR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DURING A GROUND INSPECTION IN ATL, THE FORWARD SECTION EMERGENCY FLOOR LIGHT STRIPS WERE FOUND TO BE BURNED OUT. MAINTENANCE REMOVED AND REPLACED THE FORWARD SECTION EMERGENCY FLOOR LIGHT STRIPS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

FLT 4585 - DURING A GROUND INSPECTION IN ATL, THE FORWARD SECTIN OF THE EMERGENCY FLOOR LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD SECTION EMERGENCY FLOOR LIGHT STRIPS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DURING A GROUND INSPECTION IN DFW, A FLOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE CLEANED WATER FROM THE FLOOR EMERGENCY LIGHT TRACKS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT)

FLT 4761 - DURING A GROUND INSPECTION IN ATL, THE FORWARD EMERGENCY FLOOR LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE FOUND THE POWER STRIP CONNECTORS TO THE FORWARD EMERGENCY FLOOR LIGHTS WET. MAINTENANCE DRIED, CLEANED AND RECONNECTED THE EMERGENCY FLOOR LIGHT STRIP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

FLT 4418 - DURING A GROUND INSPECTION IN ATL, THE FLOOR EMERGENCY LIGHTS FROM ROWS 1-5 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FLOOR EMERGENCY FLEX LAMP STRIP FROM ROWS 2-5. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — BURNED OUT (CABIN)

DURING A HANGER INSPECTION, THE CEILING EMERGENCY LIGHTING AT ROW 5 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A BURNED OUT EMERGENCY LIGHT BULB AT ROW 5. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.