N446AW

Part: NONE — NONE · airframe 39,101 hrs · 37,579 cycles

ON TAKE OFF RECEIVED STEERING INOP AND WOW INPUT CAUTION MESSAGES CYCLED NOSE WHEEL STEERING MESSAGE REMAINS. AFTER GEAR DEPLOY WOW INPUT MESSAGE CLEARED. ***AIRCRAFT REMOVED FROM SERVICE*** MX IN PROGRESS AFTER GEAR RETRACTION RECIEVED NWS INOP CAUTION MSG C/W QRH MSG REMAINED. MSG WAS NOT PRESENT ON GRND. C/W FIM RESET MSG CLEAR. ***AIRCRAFT REMOVED FROM SERVICE*** NOTED BY MAINTENANCE

Part: WIRE — BROKEN (FAUCET SWITCH) · airframe 38,505 hrs · 36,959 cycles

20 MINUTES INTO FLT, AT FL 250. NOTED RT PACK AT MINUS 31 DEG C. A MINUTE LATER GOT A SMOKE TOILET CAUTION MSG. CW QRH, SMOKE MSG WENT OUT. CONTINUED WITH THE FLT. FA REPORTED THAT THE HAZE SEEMED CENTERED IN LAV. HAZE CLEARED AFTER QRH, BREAKERS PULLED. LANDING NORMAL, & PACKS WERE BOTH OPERATING NORMAL. HAZE HAD AN OILY ODOR. HYD QTY NORMAL & AIR WAS OPERATING FROM 10TH STAGE ENG BLEEDS. APU LCV CLOSED. AIRCRAFT REMOVED FROM SERVICE. TROUBLESHOOTING FOUND LAV FAUCET SWITCH WIRE BROKEN & BURNING ON THE WIRE. INSPECTED LAV FOR SIGNS OF BURNS. NO DEFECTS. REPLACED LAV FAUCET SWITCH IAW CMM 25-40-43 AND SUPP 16-385. ACFT OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (DISPLAY COOL) · airframe 38,095 hrs · 36,517 cycles

WHILE AT CRUISE AT 10,000 FT, RECEIVED DISPLAY COOL CAUTION MESSAGE, COMPLIED WITH QRH, MESSAGE DID NOT CLEAR. ON DESCENT, CLEARED AT 8,000 FT. AIRCRAFT REMOVED FROM SERVICE. PERFORMED OPS CHECK OF PILOT DISPLAY REVISION SWITCH PANEL AND CO-PILOT IAW CRJ200 AMM 34-25-11, OPS CHECK GOOD AT THIS TIME. AND PERFROMED OPERATIONAL CHECK OF DISPLAY SWITCH PANELS, OPS CHECK GOOD AT THIS TIME NO FURTHER DISCREPANCIES NOTED.

Part: SEAT TRACK — CORRODED (FS 474-551) · corrosion level 2 · airframe 37,844 hrs · 36,246 cycles

RIGHT INBOARD SEAT TRACK CORRODED AT FS 474 AND FS 551, RBL 9. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORRODED SEAT TRACK AND REPLACED WITH NEW SEAT TRACK AT FS 474 AND 551, IAW REO 601R-53-00-764.

Part: TEE FITTING — CORRODED (BS 600-615) · corrosion level 2 · airframe 37,844 hrs · 36,246 cycles

LBL 27 T-CAP EXTRUSION HAS CORROSION ON THE NUT PLATES AND SURROUNDING AREA. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED T-CAP LBL 27.

Part: SEAT TRACK — CORRODED (BS 484-559) · corrosion level 2 · airframe 37,844 hrs · 36,246 cycles

RBL 9, FS 484 TO FS 559 HAS CORROSION ON SEAT TRACK. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK RBL 9, FS 484 TO FS 559 +80.

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 37,844 hrs · 36,246 cycles

RBL 9, FS 559+80 TO FS 559+88 HAS CORROSION ON SEAT TRACK. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK AT RBL 9 FS 559+80 TO FS 559+88.

Part: BULKHEAD WEB — DENTED (FS 621) · airframe 37,844 hrs · 36,246 cycles

MULTIPLE SCRIBE AND DENTS FOUND OF AFT PRESSURE BULKHEAD LBL 27.5+25 TO OUTBOARD OF CARGO DOOR ENTRANCE WL 93.5 TO WL 132.43 BEHIND CARGO DOOR TRACK. AIRCRAFT REMOVED FROM SERVICE. ACCOMPLISHED REPAIR AT BULKHEAD LBL 27.5+25 OUTBOARD CARGO DOOR ENTRANCE WL 93.5 TO WL 132.43, IAW REO 601R-53-61-7467.

Part: BULKHEAD WEB — CRACKED (FS 621) · airframe 37,844 hrs · 36,246 cycles

CRACK DETECTED ON AFT PRESSURE BULKHEAD WEB FWD FACE AT LBL 27.50 DIRECTLY ABOVE THE UPPER DOOR TRACK, L SHAPED CRACK 0.5"X0.5". AIRCRAFT REMOVED FROM SERVICE. ACCOMPLISHED REPAIR AT BULKHEAD LBL 27.50 ABOVE UPPER DOOR TRACK, IAW REO 601R-53-61-7467 601R-53-61-7468, AND REO 601R-53-61-7469.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 37,844 hrs · 36,246 cycles

CRACK DETECTED ON AFT PRESSURE BULKHEAD WEB FWD FACE AT BL 0.0, 36" ABOVE FLOOR. CRACK IS 2". AIRCRAFT REMOVED FROM SERVICE. REMOVED DAMAGE AND INSTALLED REPAIR AT BL 0.0, IAW REO 601R-53-61-1285.

Part: AMPLIFIER — MALFUNCTIONED (NR 2 ENGINE) · airframe 37,340 hrs · 35,767 cycles

AFTER DEPARTING IAD THE CREW ADVISED DISPATCH THEY WERE RETURNING TO IAD WITH AN ENGINE ISSUE. NO OTHER INFORMATION AVAILABLE AT THIS TIME. LOSS OF POWER UP TO 3% ON TAKE OFF ROLL AND INITIAL CLIMB- AT 10K POWER LOS(N1) EXCEEDED 10% RIGHT ENGINE. AIRCRAFT REMOVED FROM SERVICE R/R R/H ENGINE AMP CONTROL. PER AMM 73-21-03 ACCEL/ DECEELL, APR AND N1 SPEED CONTROL.AMP DISABLE CHECK. ALL OPS CHECK GOOD. NO DEFECTS NOTED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 36,217 hrs · 34,700 cycles

AFTER LANDING GEAR SELECTED UP, RECEIVED A/SKID I/B CAUTION, GEAR DISAGREE WARNING LMLG/NLG & PARK BRAKE SOV CAUTION. R MLG GREEN INDICATION ONLY. SELECTED GEAR DOWN, RECEIVED ALL GREEN LIGHTS. ALL MESSAGES CLEARED ON GEAR DOWN SELECTION. PERFORMED AIR RETURN TO DAY.

Part: STEP — BENT (PAX DOOR) · airframe 35,938 hrs · 34,421 cycles

PAX DOOR LOWER MID STEP IS BENT/BUCKLED.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 35,938 hrs · 34,421 cycles

PASSENGER DOOR AFT DRAG ANGLE IS CRACKED AT POWER ASSIST MOTOR PULLEY BRACKET.

Part: WEB — CRACKED (PAX DOOR) · airframe 35,938 hrs · 34,421 cycles

PASSENGER DOOR AFT WEB IS BUCKLED AND CRACKED.

Part: FLAP SYSTEM — MALFUNCTIONED · airframe 35,789 hrs · 34,288 cycles

AT FLIGHT LEVEL 27,000 RECEIVE FLAP FAIL CAUTION WITH FLAPS AT ZERO DEGREES. NO FLAP SELECTIONS WERE MADE. CREW DECLARED AN EMERGENCY LANDING WITH IAD TOWER. ONCE AT THE GATE THE CREW CALLED MAINTENANCE CONTROL. THE FLAPS WERE SUCCESSFULLY RESET PER FIM SUPPLEMENT 98-018G, AND MEL 27-50-01 WAS APPLIED.

Part: SENSING ELEMENT — SHORTED (BLEED AIR SYS) · airframe 34,853 hrs · 33,388 cycles

IN CLIMB RECEIVED LT 10TH STAGE DUCT WARNING. COMPLIED WITH QRH MSG REMAINS WITH POWER SETTING AT IDLE MSG WAS INTERMITTENT THE REMAINING FLIGHT 10TH STAGE DUCT BETWEEN LT 10TH SOV, LT PACK AND ISOL VALVE IND RED. TROUBLESHOT AND FOUND LEFT 10TH STAGE B LOOP SENSING ELEMENT A40WK SHORTING TO GROUND. REMOVED AND REPLACED ELEMENT A40WK IAW AMM 36-21. OPS CHECK GOOD, NO LEAKS NOTED AT THIS TIME.

Part: CARGO TRACK — CORRODED (BS 614-620) · corrosion level 2 · airframe 34,626 hrs · 33,175 cycles

CARGO TRACK CORRODED, BS 614 TO 620, LBL 35. REPLACED THE CARGO TRACK IAE SRM 51-42-06.

Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 34,626 hrs · 33,175 cycles

CARGO DOOR SILL CRACKED AT FS 589.00, LBL45. REPAIRED CARGO DOOR SILL AT FS 589.00, LBL45 IAW REO 601R-53-61-433 REV-C.

Part: FITTING — CRACKED (BS 461) · airframe 34,626 hrs · 33,175 cycles

BS 461 FLOOR SUPPORT FITTING WAS CRACKED. REPLACED FITTING IAW SRM 51-41-06, AND 51-42-21.

Part: RETAINER — CRACKED (PYLON) · airframe 34,626 hrs · 33,175 cycles

PYLON PNL 422BT SEAL RETAINER CRACKED. REPLACED SEAL RETAINER IAW SRM 51-42-06.

Part: FRAME — CORRODED (BS 589) · corrosion level 2 · airframe 34,626 hrs · 33,175 cycles

FRAME BS 589 CORRODED BETWEEN STRINGERS 23L AND 23R. REPLACED THE FRAME IAW SRM 53-61-15, 51-42-06, 51-42-21, AND 51-21-11.

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,626 hrs · 33,175 cycles

FLOOR SUPPORT BATHTUB FITTING AT FS 461.00, LBL9 CRACKED. REPLACED FITTING IAW SRM 51-42-06, 51-42-21, 51-40-11.

Part: CAP — DAMAGED (RT WING TE FLAP) · airframe 34,626 hrs · 33,175 cycles

RIGHT INBD FLAP VANE INBD END CAP HAD ELONGATED FASTENER HOLES. REPLACED THE END CAP IAW SRM 51-42-13.

Part: SKIN — CRACKED (BS 169-202) · airframe 34,626 hrs · 33,175 cycles

LEFT TRU DOOR AFT LATCH CUTOUT ON PANEL LANDING WAS CRACKED. REPLACED THE SKIN IAW SRM 51-42-06.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 34,626 hrs · 33,175 cycles

RIGHT INBD FLAP LOWER INBD SKIN DENTED AND PITTED. REPLACED THE SKIN IAW SRM 51-42-13.

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 34,626 hrs · 33,175 cycles

LEFT INBD FLAP, LOWER INBD SKIN DENTED AND PITTED. REPLACED THE SKIN IAW SRM 51-42-13.

Part: DOUBLER — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 34,626 hrs · 33,175 cycles

BS 310, LBL 18 DOUBLER CORRODED. REPLACED THE DOUBLER IAW SRM 51-42-13.

Part: SKIN — GOUGED (LT WING TE FLAP) · airframe 34,626 hrs · 33,175 cycles

LEFT OTBD FLAP VANE OTBD LE SKIN WAS GOUGED. REPLACED THE VANE SKIN IAW SRM 51-42-13.

Part: DOUBLER — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 34,626 hrs · 33,175 cycles

BS 280 TO 310, LBL 36 AND RBL 36 TWO DOUBLERS WERE CORRODED. REPLACED DOUBLERS IAW SRM 51-42-13.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 34,626 hrs · 33,175 cycles

RIGHT INBD FLAP VANE SKIN CHAFED. REPLACED THE SKIN IAW SRM 51-42-13.

Part: FRAME — CORRODED (BS 605) · corrosion level 2 · airframe 34,626 hrs · 33,175 cycles

FRAME BS 605 WAS CORRODED FROM STRINGERS 23L TO 23R. REPLACED THE FRAME IAW SRM 53-61-15, 51-42-06, AND 51-42-21.

Part: CONNECTOR — LOOSE (CABIN) · airframe 31,457 hrs · 30,165 cycles

EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE ROW 9-12. INSPECTED EMERGENCY LIGHTS AND FOUND LOOSE CONNECTOR. RESECURED CONNECTOR BY THE LAV AND ADDED SECURITY TAPE TO THAT CONNECTOR REF SUP 13-022. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,440 hrs · 30,149 cycles

EMERGENCY FLOOR TRACK LIGHTING ROWS 9-12 WILL NOT ILLUMINATE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,414 hrs · 30,125 cycles

EMERGENCY LIGHTS INOPERATIVE IN CABIN ROW 9-12.

Part: DOOR — BINDING (MAIN PAX) · airframe 31,183 hrs · 29,911 cycles

PASSENGER DOOR WILL NOT OPEN FROM INSIDE OR OUTSIDE.

Part: SEAL — LACK OF LUBE (PAX DOOR) · airframe 31,183 hrs · 29,911 cycles

PASSENGER DOOR WILL NOT OPEN FROM INSIDE OR OUTSIDE. LUBRICATED PAX DOOR SEAL AS REQUIRED IAW AMM 15-053, OPS CHECKED GOOD.

Part: PANEL — CHAFED (RT PYLON) · airframe 30,841 hrs · 29,618 cycles

PANEL 422DB HAS THREE EACH CHAFES ON OUTER SURFACE. REPAIRED PANEL 422DB IAW SUPPLEMENT 16-155.

Part: COTTER PIN — OUT OF POSITION (LT AIELRON) · airframe 30,841 hrs · 29,618 cycles

LEFT AILERON NR 2 HINGE BOLT COTTER PIN HEAD IS CHAFING ON LE SKIN OF AILERON. REPLACED LE SKIN IAW SRM 51-42-06, 51-42-21. RE-POSITIONED HINGE BOLT COTTER PIN TO PREVENT CONTACT IAW AMM 27-15-01.

Part: SKIN — CRACKED (FUSELAGE) · airframe 30,841 hrs · 29,618 cycles

NLG WW CUT OUT AFT LT CORNER IS CRACKED. REPAIRED NLG WW CUT OUT AFT LT CORNER IAW REO 601R-53-11-048 REV D DATED 2015 06 10 & REO 601R-53-11-2906 REV DATED 2016 05 16.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 30,841 hrs · 29,618 cycles

FLOOR SUPPORT ANGLE AT FS 621 CRACKED AT LBL 36.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,841 hrs · 29,618 cycles

LBL 9 INBD FLOORBOARD SUPPORT HAS CORROSION FROM FS 589.0 - 608.0.

Part: BRACKET — CHAFED (LT WING) · airframe 30,841 hrs · 29,618 cycles

LEFT WING LE BRACKET BEHIND LE ACCESS PANEL 530BL IS CHAFED ON INBD & OTBD FLANGES.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 30,841 hrs · 29,618 cycles

LEFT SIDE INTERCOSTAL MEMBER AT FS 621.00 - 625.00, STRINGER 13L IS CRACKED. REPLACED INTERCOSTAL IAW SRM 51-42-06 & 51-42-21.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 30,841 hrs · 29,618 cycles

LEFT SIDE INTERCOSTAL MEMBER AT FS 621.00 - 625.00, STRINGER 14L IS CRACKED. REPLACED INTERCOSTAL IAW SRM 51-42-21, 51-40-11, 53-61-17, 51-42-06 & 51-42-21.

Part: SKIN — DENTED (FUSELAGE) · airframe 30,841 hrs · 29,618 cycles

PERFORM PERMANENT REPAIR TO FUSELAGE SKIN, 2 OFF DENTS BETWEEN LT FS 409+64 - 409+80, STRINGER 18L - 19L. REPAIRED SKIN IAW SRM 53-00-31 REPAIR NR 1 & SRM 53-00-15.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,841 hrs · 29,618 cycles

PASSENGER CABIN FRAME FS 333.000 CRACKED AT TOOLING HOLE, BETWEEN STRINGER 0 & 1L. REPLACED FRAME IAW SRM 51-42-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 30,841 hrs · 29,618 cycles

INTERCOSTAL AT FS 621.00 - 625.00, ADJACENT TO STRINGER 14L IS CRACKED. REPLACED INTERCOSTAL IAW SRM 51-42-21.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 30,841 hrs · 29,618 cycles

RIGHT LOWER CTR WINDSHIELD POST BRACKET CRACKED. REPLACED BRACKET IAW SRM 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,841 hrs · 29,618 cycles

RIGHT SIDE WALL SEAT TRACK STICK NR 4 HAS CORROSION, BETWEEN FS 409+112 & 449.85 IN CABIN. REPLACED SEAT TRACK IAW REO 601R-53-00-485, SRM 51-42-02 & SUPPLEMENT 13-074.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,841 hrs · 29,618 cycles

LBL 27 FLOOR SUPPORT HAS CORROSION ON INBD & OTBD SIDES, BETWEEN FS 574.00 - 621.00. REPAIRED FLOOR SUPPORT ON INBD & OTBD SIDES, BETWEEN FS 574.00 & SF 621.00 IAW EA CRJ253-00377 DATED 5 9 2016 & REO 601R-53-00-005 REV B DATED 2011 01 06.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 30,841 hrs · 29,618 cycles

PASSENGER CABIN STRINGER 3L CLIP ANGLE IS CRACKED AT FS 280.00. REPLACED CLIP ANGLE AT FS 280.00, STRINGER 3L IAW SRM 51-42-06 & 51-42-21.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 30,841 hrs · 29,618 cycles

STATION 280.00, STRINGER 3L CLIP IS CRACKED. REPLACED CLIP AT FS 280.00 & STRINGER 3L IAW SRM 51-42-06 & 51-42-21.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 30,841 hrs · 29,618 cycles

INTERCOSTAL AT FS 621.00 - 625.00 ADJACENT TO STRINGER 14R IS CRACKED. REPLACED INTERCOSTAL IAW SRM 51-42-06.

Part: BULKHEAD — GOUGED (FUSELAGE) · airframe 30,841 hrs · 29,618 cycles

BULKHEAD FS 755.00, RBL 14 CHANNEL MEMBER IS GOUGED 7" UP FROM LOWER END. REPAIRED BULKHEAD FS 755.00, RBL 14 IAW EA CRJ253-00378 REV IR DATED 5 9 2016.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 30,841 hrs · 29,618 cycles

PASSENGER DOOR AFT DRAG ANGLE IS CRACKED, REPLACED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,841 hrs · 29,618 cycles

RBL 9 SEAT TRACK, BETWEEN FS 559+110 - 568.00 CORRODED, REPLACED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 30,841 hrs · 29,618 cycles

FLIGHT DECK FLOOR, AFT FLOOR ANGLE AT THE FWD SIDE OF THE 280 BEAM JUST INBD OF RBL 9 CRACKED, REPLACED.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 30,841 hrs · 29,618 cycles

RIGHT OVERWING TO FUSELAGE PANEL ATTACH STRUCTURE AT 461.00 IS CRACKED, REPLACED.

Part: ANGLE — CRACKED (COCKPIT) · airframe 30,841 hrs · 29,618 cycles

RIGHT WINDSHIELD SIDE POST LOWER OTBD ANGLE IS CRACKED, REPLACED.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 30,841 hrs · 29,618 cycles

RIGHT OVERWING TO FUSELAGE PANE ATTACH STRUCTURE AT FS 449.85 IS CRACKED, REPLACED.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 30,841 hrs · 29,618 cycles

LEFT OVERWING TO FUSELAGE PANEL ATTACH STRUCTURE AT FS 461.00 CRACKED, REPLACED.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 30,841 hrs · 29,618 cycles

LEFT OVERWING TO FUSELAGE PANEL ATTACH STRUCTURE AT FS 467 IS CRACKED, REPLACED.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 30,841 hrs · 29,618 cycles

SPR CONNECTION STRUCTURE LOWER OTBD CORNER CRACKED, REPLACED.

Part: BRACKET — CRACKED (COCKPIT) · airframe 30,841 hrs · 29,618 cycles

LEFT LOWER WINDSHIELD CENTER POST BRACKET CRACKED, REPLACED.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 30,841 hrs · 29,618 cycles

RIGHT OVERWING TO FUSELAGE PANEL ATTACH STRUCTURE AT FS 467 IS CRACKED, REPLACED.

Part: HANDLE — DIRTY (SERVICE DOOR) · airframe 30,702 hrs · 29,458 cycles

SERVICE DOOR OUTER HANDLE WILL NOT DEPLOY. CLEANED & LUBED SERVICE DOOR HANDLE IAW AMM 52-41-00. OPERATIONS CHECKED GOOD.

Part: HANDLE — OUT OF ADJUST (SERVICE DOOR) · airframe 30,636 hrs · 29,426 cycles

CREW REPORTS SERVICE DOOR CANNOT BE OPENED FROM THE OUTSIDE, OPENS NORMALLY USING THE INSIDE HANDLE. ADJUSTED SERVICE DOOR HANDLE IAW AMM 52-41-03. OPERATIONS CHECKED GOOD.

Part: FLAP — FAILED (WING) · airframe 30,502 hrs · 29,297 cycles

FLIGHT 3844 FLAP FAIL AT 5 DEGREES, AT FLAPS FIRST MOVEMENT ON APPROACH. COMPLIED WITH QRH, FLAP FAIL MESSAGE RETURNED DURING CIRCUIT BREAKER RESET, SUP 98-018G.

Part: LIGHT — BROKEN (CABIN) · airframe 28,446 hrs · 27,312 cycles

EMERGENCY FLOOR FLOODLIGHT MOUNTED ON THE WARDROBES BROKEN. R & R THE FLOODLIGHT IAW AMM 33-51. OPS CHECKED GOOD.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 28,391 hrs · 27,253 cycles

MAIN BATTERY & APU BATTERY CHARGER STATUS MSGS FIM RESET FAILED.

Part: FMS — MALFUNCTIONED (COCKPIT) · airframe 27,811 hrs · 26,697 cycles

ABORTED TAKEOFF AT APPROX 80 KTS, BTMS 5, 5, 3 & 5. FMS FAILED ON TAKEOFF. COMPLIED WITH FIM FAULT RESET OF FMS. OPERATIONS OKAY. IAW MX HIGH ENERGY STOP INSPECTION NOT REQUIRED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,316 hrs · 26,242 cycles

EMERGENCY LIGHTS ROW 2 - 5 INOPERATIVE.

Part: ANGLE — CRACKED (PAX DOOR) · airframe 25,984 hrs · 24,992 cycles

PAX DOOR FWD POWER ASSIST MOTOR MOUNT ANGLE CRACKED. R & R POWER ASSIST ANGLE WITH NEW SERVICEABLE ANGLE IAW SRM 51-42-06.

Part: SUPPORT — CRACKED (PAX DOOR) · airframe 25,984 hrs · 24,992 cycles

PAX DOOR STAIR FWD SUPPORT PANEL CRACKED AT HAND RAIL STOW SUPPORT BRACKET. REMOVED EXISTING REPAIR ANGLE IAW REO 601R-52-11-702 REV C ITEM 19 & REPLACED WITH SERVICEABLE ANGLE IAW SRM 51-40-11, 51-42-06 & 51-42-21.

Part: DRAG ANGLE — CRACKED (RT MLG WW) · airframe 25,984 hrs · 24,992 cycles

DURING BATTERY RIB REPAIR FOUND RT MLG WW BATTERY RIB DRAG ANGLE CRACKED. REMOVED CRACKED RT DRAG ANGLE & REPLACED WITH NEW SERVICEABLE ANGLE IAW SRM 51-42-21.

Part: SKIN — GOUGED (FUSELAGE) · airframe 25,984 hrs · 24,992 cycles

FUSELAGE SKIN UNDER UPPER TCAS HAS GOUGE. REPAIRED FUSELAGE SKIN UNDER TCAS ANTENNA IAW EA 15-2014-110.

Part: SKIN — CRACKED (LT COWLING) · airframe 25,984 hrs · 24,992 cycles

LEFT LOWER CORE COWL CRACKED ON INNER SKIN, FWD OF DRAIN HOLE. REPAIRED INNER SKIN IAW CMM 71-12-01 REPAIR NR SRS046.

Part: SEAL — CRACKED (RT SPOILER) · airframe 25,984 hrs · 24,992 cycles

RIGHT FLIGHT SPOILER CTR RAZOR SEAL IS CRACKED. REMOVED CRACKED RAZOR SEAL & REPLACED WITH NEW SERVICEABLE RT SEAL IAW SRM 51-42-06 & 51-42-21.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 25,984 hrs · 24,992 cycles

HYD SYS 2 FILTER MANIFOLD BRACKET IN AEB, RHS, CRACKED. R & R WITH SERVICEABLE BRACKET IAW SRM 51-24-16, 51-40-11 & 51-42-06.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 25,984 hrs · 24,992 cycles

COMPLIED WITH CARD 4DMI17491 REPAIR APU INLET DOOR (DOOR ACTUATOR MOUNTING INTERCOSTAL CRACKED & PREVIOUS TEMP REPAIR. R & R INTERCOSTAL PN 601R35210-17 IAW SRM 51-40-11 & 51-42-06.

Part: RETAINER — CRACKED (LT PYLON) · airframe 25,984 hrs · 24,992 cycles

LEFT PYLON PANEL 412BT SEAL RETAINER IS CRACKED. REMOVED CRACKED SEAL RETAINER & INSTALLED A NEW SERVICEABLE SEAL RETAINER IAW SRM 51-42-06, 20-40-11 & 51-23-00.

Part: RIB — CRACKED (RT WING) · airframe 25,984 hrs · 24,992 cycles

RIGHT MLG WW BATTERY RIB CRACKED. REPAIRED RT BATTERY RIB REO 601R-57-51-046 REV B 2002-02-28.

Part: STIFFENER — CRACKED (GALLEY) · airframe 25,984 hrs · 24,992 cycles

GALLEY FWD INBD LWR COMPARTMENT DOOR HINGE ATTACH STIFFENER CRACKED. REPAIR OF GALLEY FWD INBD LWR COMPARTMENT DOOR HINGE ATTACH STIFFENER SEE WORK CARD 54587-2000-0020 FOR REPLACEMENT OF DOOR ASSEMBLY.

Part: BRACKET — CRACKED (NLG WW) · airframe 25,984 hrs · 24,992 cycles

NR 2 BRAKE ACCUMULATOR IN NOSE BAY, BRACKET CRACKED. R & R BRAKE ACCUMULATOR BRACKET WITH NEW SERVICEABLE BRACKET IAW 51-42-06.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 25,984 hrs · 24,992 cycles

LEFT FWD EQUIP COMPARTMENT CRACKED AT RIVETS AT FS 193.00. REPAIRED LT FWD ELEC BAY FLOOR AT FS 193.00 IAW REO 601R-53-11-11198-MAR-18.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 25,984 hrs · 24,992 cycles

COMPLIED WITH CARD 4DMI17552 REPAIR PRESS BULKHEAD FS 601R-53-61-5162B. REPAIRED DAMAGED PRESS BULKHEAD FS 621 IAW REO 601R-53-61-52 2014-04-09.

Part: MOUNT BRACKET — CRACKED (LT MLG WW) · airframe 25,984 hrs · 24,992 cycles

LEFT MLG WW BRAKE TRANSDUCER MOUNT BRACKET IS CRACKED. R & R LT TRANSDUCER BRAKE MOUNT BRACKET WITH NEW SERVICEABLE BRACKET IAW SRM 51-42-06, 51-40-11 & 51-41-02.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 25,984 hrs · 24,992 cycles

REAR PRESS BULKHEAD FACE HAS 1 EA CRACKED ISOLATOR. R & R ISOLATOR BRACKET WITH NEW SERVICEABLE BRACKET IAW SRM 51-40-11 & 51-42-06.

Part: CLEAT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,984 hrs · 24,992 cycles

SERVICE DOOR LWR FWD FLOOR SUPPORT CLEAT ON CUT OUT AT FS 320.00 & RBL43 IS CORRODED. R & R LWR FWD FLOOR SUPPORT CLEAT WITH NEW SERVICEABLE PART IAW SRM 51-42-21 & 51-40-11.

Part: BEAM — CRACKED (FUSELAGE) · airframe 25,984 hrs · 24,992 cycles

VERTICAL BEAM AT FS 409+128 HAS CRACK ON LOWER AFT CORNER. REPAIRED VERTICAL BEAM FS 409+128 AT RBL 27 IAW REO 601R-53-41-056 REV F 2011-09-02.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,984 hrs · 24,992 cycles

PAX DOOR LWR SILL HAS CORROSION AT PROX SWITCH PS9MB CUT OUT. REMOVED CORRODED PAX DOOR LWR SILL & REPLACED WITH NEW SERVICEABLE ANGLE IAW SRM 51-40-11, 51-42-21, 51-42-13 & 51-42-06.

Part: RETAINER — CORRODED (E&E DOOR) · corrosion level 2 · airframe 25,984 hrs · 24,992 cycles

AVIONICS DOOR SEAL RETAINER CORRODED. R & R 4 EA SEAL RETAINERS PN'S CC670-38663-5, CC670-38662-5, CC670-38675-3 & CC670-38674-3 IAW SRM 51-40-11 & 51-42-06.

Part: BEAM — CRACKED (FUSELAGE) · airframe 25,984 hrs · 24,992 cycles

LBL 27 HAS SEVERAL CRACKS BETWEEN FS 610 & FS 589. REMOVED, FABRICATED & INSTALLED SERVICEABLE PART IAW CRJ200 SRM 51-40-11 & 51-42-21.

Part: FITTING — CRACKED (COCKPIT) · airframe 25,984 hrs · 24,992 cycles

PILOT WINDSHIELD OTBD WINDOW POST CLIP CRACKED. R & R PILOT WINDSHIELD OTBD AFT CLIP ON WINDOW POST IAW CRJ200 SRM 51-42-21.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 25,984 hrs · 24,992 cycles

AIRCRAFT GND POWER PLUG BRACKET CRACKED AT SCREW HOLE. R & R ACFT GND BRACKET WITH NEW SERVICEABLE BRACKET IAW SRM 51-40-11, 51-42-06 & 51-42-13.

Part: BEAM — CRACKED (FUSELAGE) · airframe 25,984 hrs · 24,992 cycles

VERTICAL BEAM RBL 18 A TFS 409+128 IS CRACKED ON OTBD LOWER CORNER. REPAIRED IAW REO 601R-53-41-056 REV F DATED 2011/09/02.

Part: FITTING — CRACKED (FUSELAGE) · airframe 25,984 hrs · 24,992 cycles

INBD & OTBD CLIPS ARE CRACKED AT FS 280 & LBL 9 FLOOR SUPPORT BEAM. REMOVED, FABRICATED & INSTALLED INBD & OTBD CLIPS FS 280 LBL 9 FLOOR SUPPORT BEAM IAW REO 601R-53-11-171 REV D 13-02-10 & 601R-53-11-138 REV A 2010-11-10.

Part: FITTING — CRACKED (FUSELAGE) · airframe 25,984 hrs · 24,992 cycles

INBD & OTBD CLIPS ARE CRACKED AT FS 280 & RBL 9 FLOOR SUPPORT BEAM. REMOVED, FABRICATED & INSTALLED INBD & OTBD CLIPS AT FS 280 & RBL 9 FLOOR SUPPORT BEAM IAW REO 601R-53-11-171 REV A 2010-11-10.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,984 hrs · 24,992 cycles

RIGHT FLOOR SILL HAS CORROSION AT FS 319 RBL 43. R & R FLOOR SILL WITH SERVICEABLE SILL IAW SRM 51-42-06.

Part: MOUNT BRACKET — CRACKED (RT MLG WW) · airframe 25,984 hrs · 24,992 cycles

RIGHT MLG WW BRAKE TRANSDUCER MOUNT BRACKET & LINE MOUNT BRACKET IS CRACKED. R & R WITH NEW SERVICEABLE BRACKET 1 EA TRANSDUCER MOUNT & LINE MOUNT BRACKET IAW SRM 51-42-06.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 25,984 hrs · 24,992 cycles

CARGO TIE DOWN TRACK ON LBL 9 CORRODED AT FS 559+96. R & R CARGO TIE DOWN TRACK ON LBL 9 AT FS 559+96 IAW SRM 51-41-02 & AMM 20-21-00.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 25,984 hrs · 24,992 cycles

CARGO TIE DOWN TRACK ON RBL 9 CORRODED AT FS 559+96. R & R CARGO TIE DOWN ON TRACK AT RBL 9 FS 559+96 IAW SRM 51-41-02 & AMM 20-21-00.

Part: FITTING — CRACKED (FUSELAGE) · airframe 25,984 hrs · 24,992 cycles

FS 484 CLIP CRACKED ON LBL 36 & LBL27. R & R TWO EACH CRACKED CLIPS WITH SERVICEABLE CLIPS AT LBL 27 & 36 IAW REO 601R-53-41-059 REV B DATED 2009-09-16.

Part: FITTING — CRACKED (FUSELAGE) · airframe 25,984 hrs · 24,992 cycles

FS 484 CLIP CRACKED AT RBL 27. REMOVED CRACKED CLIP FROM FS 484 AT RBL 27 & REPLACED IT WITH A SERVICEABLE FABRICATED CLIP IAW REO 601R-53-41-059 REV B. CORRECTIVE ACTION REJECTED DUE TO IMPROPER MATERIAL USED TO FABRICATE NEW CLIP. PN USED WAS S6144-A14 2024T3 063. CORRECTION OF NEW FS 484 CLIP OF CORRECT MATERIAL IS ON NON-ROUTINE.

Part: TRUNNION — DAMAGED (MLG) · airframe 25,984 hrs · 24,992 cycles

DURING COLD WORKING OF MLG TRUNNION, LOWER FLANGE FASTENER HOLES, FOUND 1 EA O/S HOLE ON THE LT SIDE. REPAIRED FASTENER HOLE & INSTALLED FASTENERS IAW REO 601R-57-21-2182.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 22,720 hrs · 21,847 cycles

AFTER ADVANCING FLAPS FROM 0 TO 8 DEG RECEIVED THE FOLLOWING WOW INPUT AND WOW OUTPUT, WOW OUTPUT FAIL AND PROX SYSTEM FAULT. COMPLIED WITH QRH. COMPLIED WITH PSEU TEST AND BIT TEST IAW FIM 32 60 00 MSG CLEARED, OP CHECK GOOD.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 22,573 hrs · 22,507 cycles

AFTER TAKEOFF RECEIVED APPROX 3 STICK SHAKERS WITH AN ASSOCIATED WIND SHEER FAIL STATUS MSG. MESSAGE CLEARED AT FLAPS 45, AND APPROX 1000' AGL. NO SHAKER DURING APPROACH. INITIAL SPEED 170, FLAPS 8, NO OVERWEIGHT LANDING. REMOVED AND REPLACED STALL PROTECTION COMPUTER IAW AWAC SUPP 08-053. OPS CHECK GOOD IAW AMM 27-35-01.

Part: LEVER — LOOSE (FUEL SHUTOFF) · airframe 21,928 hrs · 21,090 cycles

FUEL SHUTOFF LEVER ON LT THRUST LEVER IS VERY LOOSE. R & R THROTTLE QUADRANT IAW 76-11-01.

Part: CARGO TRACK — CORRODED (FS 574) · corrosion level 1 · airframe 21,208 hrs · 20,378 cycles

TIE DOWN TRACK OF FS 574 AND LBL27 AS CORROSION. R & R TRACK IAW SRM 53-61-49.

Part: SKIN — DAMAGED (LT AILERON) · airframe 21,208 hrs · 20,378 cycles

LIGHTNING DAMAGE TO LT AILERON T/E. REPAIRED IAW REO 601R-57-61-413.

Part: CARGO TRACK — CORRODED (FS 574) · airframe 21,208 hrs · 20,378 cycles

TIE DOWN TRACK AT FS 574 & RBL 9 HAS CORROSION. R & R TIE DOWN TRACK IAW SRM 53-21-49.

Part: CONNECTOR — BROKEN (RT ENGINE) · airframe 21,208 hrs · 20,378 cycles

RT ENGINE INBD SWITCH CONNECTOR PLUG BRACKET IS BROKEN. REMOVED BROKEN BRACKET AND REPLACED WITH NEW SERVICEABLE BRACKET PN 228-55410-835 IAW ECC 20-17-10, SRM 51-42-20, 51-41-00 IN RT ENGINE INBD T/R MICRO SWITCH CONNECTOR PLUG.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 21,208 hrs · 20,378 cycles

LEFT INBD FLAP VANE L/E IS CHAFED IN 3 PLACES. R & REINSTALLED 1 EA SERVICEABLE SKIN PN 601R14303-535 ALSO REPAIRED CENTER AND OTBD AREAS IAW REO 601R-57-52-004, REV C.

Part: BRACKET — CRACKED · airframe 21,208 hrs · 20,378 cycles

EPC UNIT MOUNTING BRACKET CRACKED IN RADIUS. REPLACE BRACKET.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 21,208 hrs · 20,378 cycles

RT INBD FLAP VANE IS CHAFING IN 3 EA PLACES. REPAIR IAW REO 601R-57-52-004, REV C.

Part: BULKHEAD — DENTED (FS 280) · airframe 21,208 hrs · 20,378 cycles

RT AFT SIDE OF 280 BULKHEAD DENTED FROM GALLEY DOOR COMPLIED WITH REO 601R-53-11-1727, REV F.

Part: ANCHOR FITTING — CRACKED (PAX DOOR) · airframe 21,208 hrs · 20,378 cycles

PAX DOOR CUT OUT FWD AND AFT ANCHOR FITTING CRACKED. REMOVED UNSERVICEABLE FWD AND AFT PAX DOOR ANCHOR FITTINGS AND INSTALLED SERVICEABLE FWD AND AFT PAX DOOR ANCHOR FITTINGS.

Part: ANCHOR FITTING — CRACKED (PAX DOOR) · airframe 21,208 hrs · 20,378 cycles

PAX DOOR CUT OUT FWD AND AFT ANCHOR FITTING CRACKED. REMOVED UNSERVICEABLE FWD AND AFT PAX DOOR ANCHOR FITTINGS AND INSTALLED SERVICEABLE FWD AND AFT PAX DOOR ANCHOR FITTINGS.

Part: BRACKET — CRACKED (FS 574) · airframe 21,208 hrs · 20,378 cycles

FWD LOWER CARGO DOOR TRACK MOUNT BRACKET CRACKED AND DENTED. R & R BRACKET IAW SRM 51-40-11 AND SRM 51-42-06, SERVICEABLE PN.

Part: WARNING LIGHT — ILLUMINATED (THRUST REVERSER) · airframe 20,499 hrs · 19,618 cycles

RT THRUST REVERSER UNLOCK MESSAGE DURING TAKE OFF ROLL, ABORTED TAKE OFF AT 102 KTS BTMS MAX READS 7744. OPEN

Part: PDU — FAILED (THRUST REVERSERS) · airframe 20,493 hrs · 19,608 cycles

RIGHT THRUST REVERSER UNLOCK MESSAGE DURING TAKE OFF ROLL, ABORTED TAKE OFF AT 102 KTS BTMS MAX READS 7744. R & R RT PDU IAW 78-32-03. OPS CHECKED GOOD.

Part: RUDDER — BINDING · airframe 20,403 hrs · 19,509 cycles

DURING FLIGHT CONTROL CHECK OF RUDDER, LOUD CLICKING NOISE HEARD LT AND RT, SLIGHT BINDING FELT. RETORQUED PIVIOT BOLTS, NO FIX, ITEM PLACED ON DIL FOR 500 FLT HOURS IAW SUP 06-037, REF DIL 203798/13.

Part: DOOR — LACK OF LUBE (SERVICE) · airframe 20,343 hrs · 19,450 cycles

SERVICE DOOR WILL NOT OPEN FROM OUTSIDE. LUBED AND CHECKED OPERATION. OPS CHECKED GOOD.

Part: BALLAST — FAILED (CABIN LIGHTS) · airframe 19,879 hrs · 18,980 cycles

CABIN SMELLS OF ELECTRICAL SMOKE. ODOR IS STRONGER NEAR LAV. R & R LAV LIGHT BALLAST.

Part: STRUT — DISCHARGED (NLG) · airframe 19,531 hrs · 18,612 cycles

AFTER TAKEOFF, NOSE GEAR W/N RETRACT RECEIVED GEAR DISAGREE WARNING ALONG WITH WOW OUTPUT STATUS AND WOW INPUT CAUTION MSG. C/W QRH. PERFORMED AIR RETURN. LANDED AT 46,500 LBS, NORMAL LANDING. CORRECTLY SERVICED NLG SHOCK STRUT IAW AMM 12-12-32. PERFORMED GEAR SWING AND FOUND ALL INDICATIONS NORMAL. REF AMM 32-21.

Part: CONTROLLER — INOPERATIVE (WINDSHIELD HEAT) · airframe 18,056 hrs · 17,093 cycles

LT WINDSHIELD HEAT CAUTION MSG IN FLIGHT. COMPLIED WITH QRH AND MESSAGE PERSISTS. R & R LT WINDSHIELD CONTROLLER AND ANTI-ICE CONTROL PANEL IAW AMM 30-41-01 AND OPS TEST IAW AMM 30-12-21. M/C WINDSHIELD HEAT CONTROL SWITCH WAS BAD.

Part: RING — DAMAGED (ENGINE) · airframe 17,585 hrs · 16,602 cycles

CONTAINMENT RING AT 5 O`CLOCK POSITION APPROX 1 IN LONG BY .2500 IN DEEP. REPLACED CONTAINMENT CASE IAW AMM 72-20-00. ALL CKS GOOD AT THIS TIME.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 17,232 hrs · 16,235 cycles

RT OTBD FLAP DENTS (2) REPAIRED RT OTBD FLAP DENTS (2EA) IAW SRM 57-53-00, FIG 202, SHT 2, PG 208.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 17,232 hrs · 16,235 cycles

PAX DOOR EXTERNAL HANDLE IS CRACKED. R & R HANDLE.

Part: FITTING — CHAFED (LT WING TE FLAP) · airframe 17,232 hrs · 16,235 cycles

FLAP ROLLER FITTING ON LT WING IS CHAFED. REPAIRED FLAP ROLLER ON LT WING IAW 601R-57-51-143, REV NC DATED 2003-05-26.

Part: FAIRING — GOUGED (LT WING TE FLAP) · airframe 17,232 hrs · 16,235 cycles

LT FLAP STUB FAIRING IS GOUGED. R & R LT FLAP STUB FAIRING IAW AMM 53-82-01.

Part: SKIN — CRACKED (PAX DOOR) · airframe 17,232 hrs · 16,235 cycles

INTERNAL SKIN AT THE BOTTOM OF PAX DOOR IS CRACKED. LOCATED NEXT TO BONDING JUMPER STAND. REPAIRED INTERAL SKIN AT THE BOTTOM AX DOOR IAW B/A 601R-52-11-279, REV NC DATED 2001-10-18.

Part: DOUBLER — CRACKED (PAX DOOR) · airframe 17,232 hrs · 16,235 cycles

PAX DOOR AFT PULL IN CAM DOUBLER IS CRACKED. R & R PAX DOOR AFT PULL IN CAM DOUBLER AND INSTALLED DUPLICATED DOUBLER IAW SRM 51-24-16, 51-25-16, 51-40-11, 51-42-21, AAR FORM 412 FOR PART DETAILS.

Part: SUPPORT ANGLE — CHAFED (BS 700) · airframe 17,232 hrs · 16,235 cycles

LEFT ACM FWD SUPPORT ANGLE CHAFED FROM BLEED DUCT, BLEED DUCT IS ALSO CHAFED. R & R FWD SUPPORT ANGLE IAW SRM 51-24-00 & 51-42-06.

Part: SUPPORT — CRACKED (PAX DOOR) · airframe 17,232 hrs · 16,235 cycles

PAX DOOR STEP G (2ND FROM TOP) STEP SUPPORT IS CRACKED AT LOWER CORNER ON STEP FACE REPAIRED STEP SUPPORT IAW 601R-52-11-702, REV C, DATED 2010-03-09.

Part: SHIELD — GOUGED (LT JET PIPE) · airframe 17,232 hrs · 16,235 cycles

LT ENGINE JET PIPE FAIRING (436AL) FIRE LOOP SHIELD IS GOUGED. R & R IAW CMM 78-11-00.

Part: SHIELD — GOUGED (RT ENGINE) · airframe 17,232 hrs · 16,235 cycles

RT ENGINE JET PIPE FAIRING FIRE LOOP SHIELD IS COUGED. R & R IAW SRM 51-42-02.

Part: PANEL — CHAFED (LT PYLON) · airframe 17,232 hrs · 16,235 cycles

PYLON PANEL 412DB HAS KNIFE EDGES REPLACED (2 EA) SEPARATORS ON PYLON PANEL 412DB IAW CRJ 200 51-77-00, 51-42-06, 51-42-13.

Part: FLOOR SUPPORT — CRACKED (BS 280) · airframe 17,232 hrs · 16,235 cycles

FLOOR SUPPORT CRACKED AT APPROX LBL 10 AT FS 280.00 BY MLG ALT RELEASE CABLE ACCOMPLISHED REO 601R-53-11-138.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 17,232 hrs · 16,235 cycles

PAX DOOR AFT DRAG ANGLE IS CRACKED 601R-52-11-513 REV A DATED 09 MAR 05. REPAIRED AFTER DRAG ANGLE IAW REO.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 17,232 hrs · 16,235 cycles

PAX DOOR INTERCOSTAL 601R31902-9 FWD SIDE UNDER TOP STEP IS CRACKED AND BUCKLED. R & R INTERCOSTAL IAW SRM 51-42-06 AND 51-42-21.

Part: BLOCKER DOOR — CHAFED (THRUST REVERSER) · airframe 17,232 hrs · 16,235 cycles

RT THRUST REVERSER BLOCKER DOORS 1-10 ARE CHAFED ON BACKSIDE FROM STOPS, BLENDED IAW CMM 78-30-00, REPAIR NR SRS 100.

Part: BLOCKER DOOR — CHAFED (THRUST REVERSER) · airframe 17,232 hrs · 16,235 cycles

LEFT THRUST REVERSER BLOCKER DOORS 1-10 CHAFED ON BACKSIDE FROM STOPS. REPAIRED IAW CMM 78-30-00. REPAIR NR SRS100.

Part: BRACKET — CRACKED (LT NACELLE) · airframe 17,232 hrs · 16,235 cycles

LT NOSE INLET MOUNTING FLANGE WIRE HARNESS BRACKET IS CRACKED AT 8 O`CLOCK POSITION. REPLACE BRACKET IAW SRM. REO`S REMOVAL OF INLET TO ACCOMPLISH REPLACEMENT.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 17,232 hrs · 16,235 cycles

NR2 SEAT TRACK LT SIDE WALL FLAKING. REPLACED SEAT TRACK.

Part: RIB — CRACKED (LT WING) · airframe 17,232 hrs · 16,235 cycles

LT MLG BATT RIB APPEARS TO BE CRACKED. REPAIRED IAW REO 601R-57-51-046.

Part: SILL — CORRODED (BS 574) · corrosion level 1 · airframe 17,232 hrs · 16,235 cycles

BAGGAGE LOWER SILL IS CORRODED AROUND NUT PLATE HOLES. BLENDED OUT CORROSION, TREATED MATERIAL, PRIMED AND PAINTED.

Part: BRACKET — CRACKED (BS 424) · airframe 17,232 hrs · 16,235 cycles

BRAKE PRESS TRANSDUCER BRACKETS IN LT AND RT MLG WW`S ARE CRACKED. REMOVED INSERVICEABLE BRACKETS AND REPLACED WITH SERVICEABLE BRACKETS IN THE LT AND RT FRO BRAKE TRANSDUCER IN MLG WW IAW SRM 51-42-06.

Part: SILL — CORRODED (BS 559) · airframe 17,232 hrs · 16,235 cycles

RT FLOOR SILL AT FS 559.00+80 TO FS 559.00+1412 HAS PAINT BLISTERING AROUND NUT PLATE HOLES. REMOVED CORROSION WITH 0.060 MATERIAL REMAINING, FOUND TO BE WITHIN LIMITS IAW SRM 53-00-00.

Part: ANGLE — CRACKED (BS 621) · airframe 17,232 hrs · 16,235 cycles

FS621/625 LT OBLIQUE ANGLE CRACKED. PN 601-35012-51. REMOVED CRACKED ANGLE AND INSTALLED SERVICEABLE OBLIQUE ANGLE IAW SRM 51-42-21 AND REO 601R-53-61-422.

Part: ANGLE — CRACKED (PAX DOOR) · airframe 17,232 hrs · 16,235 cycles

PAX DOOR INNER HANDLE TORQUE TUBE MOUNT LOWER AFT ANGLE IS CRACKED. R & R ANGLE.

Part: WINDOW — FAILED (COCKPIT) · airframe 16,245 hrs · 15,188 cycles

CAPT SIDE WINDOW SHATTERED. R & R PILOT`S SIDE WINDOW IAW AMM 56-12-01 INSTALLED SPEED TAPE OVER I-BEAM SEALANT.

Part: SWITCH — MALFUNCTIONED (STAB TRIM) · airframe 16,108 hrs · 15,056 cycles

STAB TRIM CAS MESSAGE ON EDI AT 300FT AFTER TAKEOFF WITH NOSE PITCH UP. COMPLIED WITH QRH. R & R PITCH DISCONNECT SWITCH IAW AMM 27-41-30. OPS CHECK GOOD.

Part: SWITCH — FAILED (FIRE BUTTON) · airframe 15,717 hrs · 14,671 cycles

OPS TEST OF LT ENGINE FIRE PUSH BUTTON FAILED TO OPERATE LT HYD AND FUEL SHUTOFF VALVES (FAIL TO MOVE OR OPERATE). REPLACED SWITCH SPS1WF LT FIRE PUSH AND OPS CHECK GOOD. (K)

Part: HANDLE — DIRTY (SERVICE DOOR) · airframe 15,323 hrs · 14,293 cycles

SERVICE DOOR IS DIFFICULT TO OPEN FROM OUTSIDE. CLEANED DIRT ON SERVICE DOOR OUTER HANDLE AND OPS CHECK NORMAL IAW AMM 52-41. (K)

Part: SILL — CRACKED (BS 574-589) · airframe 13,549 hrs · 12,639 cycles

CARGO DOOR FLOOR SILL CRACKED UNDER BRACKET AT FS 574.00. AT CARGO DOOR FLOOR SILL (FS 574.00) CUTOUT PERFORMED IAW REO 601R-53-61-1741. AT CARGO DOOR FLOOR SILL (FS 574.00) REPAIR PERFORMED IAW REO 601R-53-61-1741. (K)

Part: OIL FILTER — ODOR · airframe 14,844 hrs · 13,821 cycles

FA REPORTS FUEL ODOR THROUGH GASPERS ON LANDING. INSPECTED AND RAN A/C SYS VIA APU AND ENG AIR SOURCES. REMOVED AND REPLACED ENG OIL FILTER IAW AMM 49-19-10 AND SUP 08-011. OK FOR SERVICE. (K)

Part: CABLE ASSY — UNKNOWN (PAX DOOR) · airframe 14,631 hrs · 13,608 cycles

PASSENGER DOOR VERY DIFFICULT TO OPEN FROM THE INSIDE. CLOSED DOOR AND VERIFIED CLOSED, LATCHED AND LOCKED. REMOVED AND REPLACED ICE BREAKER CABLE ASSY IAW AMM. REMOVED FROM MEL. OPS CK GOOD. (K)

Part: DOOR — STUCK (EMERGENCY EXIT) · airframe 14,605 hrs · 13,586 cycles

AT THE GATE - DURING EMERG DOOR DRILL LT OVERWING EXIT WOULD NOT OPEN. REPLACED LT EMERGENCY EXIT DOOR SEAL IAW AMM 52-21-07. OPS CK GOOD PRESS CHECKS GOOD. (K)

Part: ANGLE — CRACKED (BS 621) · airframe 12,242 hrs · 11,306 cycles

ANGLE CRACKED ON BULKHEAD AT FS 621 AND CARGO DOOR BEAM. ANGLE REPLACED ON BULKHEAD FS 621 AND CARGO DOOR BEAM IAW CRJ 200 SRM 51-42-21. (A)

Part: FLANGE — CRACKED (RT NACELLE) · airframe 12,242 hrs · 11,306 cycles

ON RT ENG AT FLANGE FOUND CRACKED AT 9 O’CLOCK. CRACK REPAIRED ON RT ENG AT FLANGE AT 9 O’CLOCK IAW REO 601R-71-00-3859. (A)

Part: SILL — CORRODED (FUSELAGE) · airframe 12,242 hrs · 11,306 cycles

CORROSION FOUND ON SERVICE DOOR LOWER SILL PLATE. LOWER SILL PLATE OF SERVICE DOOR REPLACED IAW CRJ 200 SRM 51-41-04. (A)

Part: SILL — CORRODED (BS 574-621) · corrosion level 1 · airframe 12,242 hrs · 11,306 cycles

CARGO DOOR SURROUND FLOOR LANDING PLATE (SILL) CORRODED AROUND NUT PLATE HOLES BETWEEN FS 574 TO FS 621. CORROSION REMOVED ON CARGO DOOR SURROUND FLOOR LANDING PLATE. AROUND NUT PLATE HOLE BETWEEN FS 574 AND FS 621 IAW CRJ 200 SRM 51-21-06. (A)

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 12,242 hrs · 11,306 cycles

INTERCOSTAL AT FS 484 LT LBL 36 CRACKED. PERFORM REO 601R-53-41-057. (A)

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 12,242 hrs · 11,306 cycles

INTERCOSTAL AT FS 484 RBL 36 IS CRACKED. PERFORM REO 601R-53-41-059 REV A. (A)

Part: FLOORBEAM — CRACKED (BS 280) · airframe 12,242 hrs · 11,306 cycles

CRACK FOUND ON CROSS BEAM AT FS 280.00 RBL 9.0. CROSS BEAM AT FS 280.00 RBL 9 REPAIRED IAW CRJ 200 REO 601R-53-11-171 REV D SCHEME A. (A)

Part: FLOORBEAM — CRACKED (BS 280) · airframe 12,242 hrs · 11,306 cycles

CRACK FOUND ON CROSS BEAM AT FS 280.00 LBL 9.0. CROSS BEAM AT FS 280.00 LBL 9 REPAIRED IAW CRJ 200 REO 601R-53-11-171 REV D SCHEME A. (A)

Part: BULKHEAD — CRACKED (BS 202) · airframe 12,242 hrs · 11,306 cycles

CRACK EXIST OF FWD PRESSURE BULKHEAD AT FS 202.0, LBL 23.71, PARKING BRAKE AREA. FWD PRESSURE BULKHEAD AT FS 202 AND LBL 23.71 REPAIRED IAW CRJ 200 REO 601R-53-11-563. (A)

Part: FAIRING — CRACKED (LT WING) · airframe 13,169 hrs · 12,196 cycles

LOG 196188/1 REQUEST INSPECTION OF LT WINGLET TRAILING EDGE FOR CRACK. REMOVED LT WINGLET T/E ASSY PER AMM 57-30092 REF LOG PAGE 196188/4 FOR INSTALLATION. INSTALLED NEW LT WINGLET T/E FAIRING ASSY PER AMM 57-30-02.

Part: WARNING MESSAGE — ILLUMINATED · airframe 11,476 hrs · 10,578 cycles

AIR DIVERSION: RED 14TH STAGE RT DUCT CAS MESSAGE DISPLAYED IN FLIGHT. COMPLIED WITH QRH, WARNING MESSAGE CLEARED. (K)

Part: ELEMENT — MALFUNCTIONED (DETECTION SYS) · airframe 11,458 hrs · 10,563 cycles

RT 14TH DUCT FAIL MESSAGE ILLUMINATED AT 15,000 FT AFTER DEPARTURE. PERFORMED QRH, MESSAGE DID NOT EXTINGUISH FOR APPROX 12 MINUTES. AIR DIVERSION DECLARED EMERGENCY LANDING. (K) REMOVED AND REPLACED FUSELAGE SENSING ELEMENT A46WK (RT SIDE) IAW AMM 36-21-04. OPS CHECK OK. (S)

Part: CHECK VALVE — FLUCTUATES (RT ENGINE)

AT FLIGHT LEVEL 28 NOTED OIL FLUCTUATION ON RIGHT ENGINE. RAN QRH. FLUCTUATION MAINTAINED ABOVE 28-40 PSI INDICATED. DECLARED AN EMERGENCY. LANDED WITHOUT ANY PROBLEMS. FOUND LEAK ON ENGINE SERVICING LINE TO RT ENGINE, ALONG WITH AN OPEN OIL SERVICE CHECK VALVE. REMOVED AND REPLACED OIL SERVICE LINE P/N 600-63100-15, IAW AMM 20-21-20 AND 20-22-00. REMOVED AND REPLACED OIL SERVICE CHECK VALVE ON RIGHT ENGINE IAW 79-12-13. (M)

Part: COMPUTER — FAULTED (RT FUEL TANK)

IN FLIGHT RECEIVED FUEL IMBALANCE MESSAGE. RIGHT TANK QUANTITY AND TOTAL FUEL QUANTITY SHOW DASHED LINES. PERFORMED AIR DIVERSION TO ALB. REMOVED AND REPLACED FUEL SYSTEM COMPUTER, IAW AMM 28-41-16. OPS CHECK GOOD. PERFORMED OPS TEST OF TRANSFER SYSTEM, IAW AMM 28-13-00, OPS CHECK GOOD. (M)

Part: CHECK VALVE — LEAKING (AIR STARTER)

RAMP AGENTS REPORTED ELECTRICAL ODOR IN CARGO BIN. CREW INSPECTED AND FOUND HOT SPOT ADJACENT TO GROUND SUPPLY AIR CONNECTION. FOUND GROUND AIR START CHECK VALVE IS LEAKING. REMOVED AND REPLACED GROUND AIR START CHECK VALVE IAW AMM 36-11-27. NO ELECTRICAL ODOR PRESENT. OPS CHECK AND LEAK CHECK GOOD. (M)

Part: HANDLE — LACK OF LUBE (ESCAPE HATCH)

CREW ESCAPE HATCH HANDLE WILL NOT RELEASE. LUBRICATED HANDLE HOUSING PARTS. (M)

Part: SKIN — CORRODED (LT WING)

FOUND LEFT WING PLANK ACCESS HOLE 510AB HAS PITTED AREA. MAINTENANCE REPAIRED FUEL PLANK ACCESS HOLE IAW BSC EO 601R-57-9582B. (M)

Part: INTERCOSTAL — CRACKED (BS 625)

FOUND LT 625 OBLIQUE ANGLE CRACKED, INTERCOSTAL. MAINTENANCE REMOVED AND REPLACED CRACKED OBLIQUE ANGLE WITH NEW ANGLE P/N 601-35012-51 IAW CRJ SRM 51-42-06. (M)

Part: BLOCKER DOOR — MISSING (THRUST REVERSER)

ENGINE NR 1 LOWER OUTBOARD THRUST REVERSER BLOCKER DOOR MISSING. REMOVED AND REPLACED ENGINE NR 1 THRUST REVERSER ASSY IAW AMM 78-30-00. ALSO, REMOVED AND REPLACED BLOCKER DOOR ARM AND DIVERTER STRIP IAW AMM 78, OPS CHECK GOOD. (M)

Part: COALESCER BAG — INOPERATIVE (AFT FUSELAGE) · airframe 5,951 hrs · 5,257 cycles

EXHAUST FUMES IN COCKPIT AND CABIN. WORSE WITH APU ON. INSPECTED APU, FOUND NO LEAKS. REPLACED AC PACKS COALESCER BAGS. OBSERVED CREW RUN UP ENGINES. NO FURTHER FUMES IN COCKPIT OR CABIN. IAW AMM. (K)

Part: VALVE — INOPERATIVE (LT A/C PACK)

LT PACK OVERHEATED AND EMITTED BURNING ODOR. SLIGHT SMOKE NOTICED IN COCKPIT. PACK SHUTOFF BEFORE ANY AMBER CAS MESSAGE ILLUMINATED. PLACED ON MEL. VERIFIED DUAL BYPASS VALVE INOPERATIVE. CAUSING LT PACK TO RUN FULL HOT CREATING PACK SMELL. NO SIGNS OF SMOKE. (M)

Part: BUSHING — MIGRATED (LT MLG TRUNNION) · airframe 1,286 hrs · 1,182 cycles

THE LT MLG AFT TRUNNION BUSHING IS MIGRATED .045 INCH. REMOVED AND REPLACED LT MLG AFT TRUNNION BUSHING IAW REO. (K)

Part: BUSHING — MIGRATED (RT MLG TRUNNION) · airframe 1,286 hrs · 1,182 cycles

THE RT MLG AFT TRUNION BUSHING IS MIGRATED .059 INCH. REMOVED AND REPLACED RT MLG AFT TRUNNION BUSHING IAW REO. (K)

Part: TORQUE LINK — DISCONNECTED (NLG) · airframe 1,694 hrs · 1,499 cycles

AFTER TAKEOFF SELECTED GEAR UP, GOT GEAR UP DISAGREE. RAN THROUGH CHECKLIST AND RETURNED. ALSO, GOT NWS INOPERATIVE, WOW INPUT CAS MESSAGE. INSPECTED AND FOUND NLG TORQUE LINKS DISCONNECTED. RECONNECTED TORQUE LINKS (PN 16144-101UPPER, 16154-101 LOWER).

Part: WARNING LIGHT — ILLUMINATED (FUEL SHUTOFF)

LEFT TRANSFER SHUTOFF VALVE CAUTION AMBER FUEL FAILED OPEN, CHECKED FUEL COMPUTER FOR FAULT CODES, NO CODES NOTED. NO EVIDENCE OF LEFT TRANSFER SHUTOFF VALVE CAUTION. OK FOR SERVICE. (M)