N406AW

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,879 hrs · 32,346 cycles

EMERGENCY FLOOR TRACK LIGHTS ROW 8 - 12 INOPERATIVE.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 34,762 hrs · 32,243 cycles

DESCENDING THROUGH 20,000' ALL CRTS EXCEPT ED1 & 2 WENT BLANK. FMS WENT BLANK. FMS, FD MAP CAUTION, FMS NOT AVAILABLE. G/S WARNING APPEARED. THROUGH 10,000' APU BATTERY CHARGER STATUS MSG APPEARED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,682 hrs · 32,164 cycles

FLOOR TRACK EMER LIGHTS 2 - 5 WILL NOT ILLUMINATE.

Part: TRIM SYSTEM — OUT OF ADJUST (RUDDER) · airframe 34,429 hrs · 31,941 cycles

ON DEPARTURE LEVELING OFF AT 8,000 FT UNCOMMANDED FULL RT RUDDER TRIM. AUTO PILOT HAD BEEN ENGAGED FOR 2 MINUTES. COMPLIED WITH QRH DISCONNECTED AUTO PILOT & YAW DAMP. DISCOVERED RUDDER TRIM WAS AT FULL RT WITH NO INPUT FROM THE KNOB. KNOB WAS CENTERED. AT THIS TIME THE ACFT IS STILL PULLING HARD RT. ADJUSTED RUDDER TRIM TO CTR, ACFT CORRECTED & WAS HAND FLOWN BACK. LANDING & BRAKING WERE NORMAL. LANDED UNDERWEIGHT.

Part: MOUNT BRACKET — CRACKED (NLG WW) · airframe 33,822 hrs · 31,350 cycles

FWD LT NOSE HYD COMPARTMENT BRAKE ACCUMULATOR FWD OTBD MOUNT BRACKET CRACKED. R & R WITH SERVICEABLE PART, PN 601R75250-55 IAW SRM 51-40-11 & 51-42-21.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,822 hrs · 31,350 cycles

LBL 27 FLOORBEAM CAP CORRODED AROUND NUTPLATE HOLES, FS 574 TO 621. R & R FLOORBEAM CAP WITH SERVICEABLE SECTION IAW SRM 51-40-11 & 51-42-21.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 33,822 hrs · 31,350 cycles

LEFT INBD FLAP VANE LE SKIN IS CHAFED AT 3 LOCATIONS. REMOVED & REPLACED INBD & CTR FLAP VANE LE SKIN IAW SRM 51-42-13 & 51-40-11.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,822 hrs · 31,350 cycles

PAX DOOR LWR SILL IS CORRODED BETWEEN FS 315 TO FS 344. R & R WITH NEW SERVICEABLE SILL ANGLE IAW SRM 51-41-02, 51-42-06 & 51-42-13.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 33,822 hrs · 31,350 cycles

PAX DOOR AFT FRAME AT FS 338 IS CRACKED UNDER PREVIOUS REPAIR. REMOVED CRACKED FRAME & REPLACED WITH NEW SERVICEABLE FRAME IAW REO 601R-52-11-402 REV H.

Part: MOUNT BRACKET — CRACKED (FUSELAGE) · airframe 33,822 hrs · 31,350 cycles

EXTERNAL SERVICES PANEL ASSEMBLY UPPER MOUNT BRACKET CRACKED. R & R EXTERNAL SERVICES PANEL UPPER MOUNT BRACKET WITH SERVICEABLE PART, PN 601R51590-13 IAW SRM 51-40-11 & 51-42-06.

Part: FITTING — CORRODED (CABIN) · corrosion level 2 · airframe 33,822 hrs · 31,350 cycles

RIGHT WINDSCREEN LWR FITTINGS HAVE CORROSION ON LWR SIDE. R & R UNSERVICEABLE FITTINGS & INSTALLED NEW SERVICEABLE FITTINGS IAW SRM 51-41-02.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 33,822 hrs · 31,350 cycles

COMPLIED WITH CARD 4DMI16358 REPAIR LT ELEVATOR DAMAGE NR 12 & 13 601R-51-00-293. PERFORMED PERMANENT REPAIR IAW SRM 55-20-00 FIG 204.

Part: CLEAT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,822 hrs · 31,350 cycles

PAX DOOR LWR SILL FWD & AFT CLEATS ARE CORRODED. REMOVED FWD & AFT CLEATS ON LWR PAX DOOR SILL & INSTALLED NEW SERVICEABLE CLEATS IAW SRM 51-42-06.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,822 hrs · 31,350 cycles

LOWER SECTION OF FS 605 FRAME HAS CORROSION. REPAIRED FRAME FS 605 IAW EA 15-2014-122 REV C DATED 5/24/2014.

Part: CLEAT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,822 hrs · 31,350 cycles

SERVICE DOOR CUT OUT THRESHOLD CLEATS HAVE CORROSION ATTACHED FASTENERS. REMOVED CORRODED FASTENERS & INSTALLED NEW SERVICEABLE FASTENERS IAW AMM 20-24-00.

Part: SKIN — GOUGED (RT WING) · airframe 33,822 hrs · 31,350 cycles

UPPER SURFACE OF LWR WING PLANK IS GOUGED AT WS 88.5. REPAIRED GOUGED UPPER SURFACE OF LWR WING PLANK IAW REO 601R--57-21-2192 DATED 5-21-14.

Part: RIB — CRACKED (LT WING) · airframe 33,822 hrs · 31,350 cycles

LEFT BATTERY RIB CRACKED ON FWD END. REMOVED CRACKED RIB & INSTALLED SERVICEABLE BATTERY RIB IAW REO 601R-57-51-046 REV B.

Part: HOUSING — CHAFED (SERVICE DOOR) · airframe 33,822 hrs · 31,350 cycles

SERVICE DOOR HANDLE HOUSING CHAFED. R & R HANDLE HOUSING WITH SERVICEABLE PART, PN 119935-1 IAW SRM 51-40-11 & 51-42-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 33,822 hrs · 31,350 cycles

CLIPS AT FS 280 & STRINGER 3L CRACKED. REMOVED UNSERVICEABLE CLIP & INSTALLED SERVICEABLE CLIP IAW SRM 51-42-06, 51-41-02, 51-42-06 & 51-42-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 33,822 hrs · 31,350 cycles

CLIP AT FS 280 & STRINGER 3L CRACKED. REMOVED CRACKED CLIP & INSTALLED SERVICEABLE CLIP IAW SRM51-41-11 & 51-41-02.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 33,822 hrs · 31,350 cycles

LEFT & RIGHT OBLIQUE ANGLES IN AEB ARE CRACKED. R & R CRACKED RT OBLIQUE ANGLE WITH NEW SERVICEABLE ANGLE IAW SRM 51-40-11 & 51-42-21. SEE W C 54596-3000-0004 FOR REMOVAL & REPLACEMENT OF LT OBLIQUE ANGLE.

Part: DRAG ANGLE — CRACKED (FUSELAGE) · airframe 33,822 hrs · 31,350 cycles

LEFT DRAG ANGLE COMMON TO BATTERY RIB CRACKED AT AFT END. R & R CRACKED LT DRAG ANGLE WITH NEW SERVICEABLE DRAG ANGLE IAW SRM 51-42-21, 51-40-11 & 51-25-16.

Part: SKIN — CRACKED (FUSELAGE) · airframe 33,822 hrs · 31,350 cycles

EXTERNAL LWR FUSELAGE SKIN AT AFT NLG CUT OUT ON BOTH LT & RT CORNERS ARE CRACKED. REPAIRED NLG WW CUT OUT IAW REO 601R-53-11-048 REV C 10-1-08.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 33,822 hrs · 31,350 cycles

PAX DOOR DRAG ANGLE FWD OF POWER ASSIST PULLEY BRACKET IS CRACKED. REPAIRED PAX DOOR DRAG ANGLE IAW REO 601R-52-11-513 REV A.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 33,822 hrs · 31,350 cycles

LEFT LWR OBLIQUE ANGLE CRACKED ON AFT SIDE OF 621 BULKHEAD. R & R LWR OBLIQUE ANGLE WITH NEW SERVICEABLE ANGLE IAW SRM 51-42-21.

Part: DRAG ANGLE — CRACKED (FUSELAGE) · airframe 33,822 hrs · 31,350 cycles

RIGHT DRAG ANGLE COMMON TO BATTERY RIB IS CRACKED. R & R RT DRAG ANGLE IAW SRM 51-42-21.

Part: MOUNT BRACKET — CRACKED (FUSELAGE) · airframe 33,822 hrs · 31,350 cycles

EXTERNAL SERVICE PANEL 122CR CUT OUT LWR MOUNT BRACKET FOR SERVICE BOX CRACKED. REMOVED CRACKED MOUNT BRACKET & INSTALLED NEW BRACKET IAW SRM 51-42-13 & 51-40-11.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,822 hrs · 31,350 cycles

SERVICE DOOR FWD SILL ATTACH AT FRAME IS CORRODED. R & R WITH NEW SERVICEABLE PART IAW SRM 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,822 hrs · 31,350 cycles

CABIN NR 1 FLOOR SEAT TRACK CORRODED AT FWD END OF LBL 9 FS 364.00. REMOVED CORRODED SEAT TRACK & REPLACED WITH NEW SERVICEABLE SEAT TRACK IAW AMM 53-01-11.

Part: SKIN — DENTED (LT ELEVATOR) · airframe 33,822 hrs · 31,350 cycles

LEFT ELEVATOR HAS 4 DENTS ON LOWER SURFACE. REPAIRED 2 DENTS IAW SRM 55-20-00 FIG 204 & FOUND 2 DENTS TO BE IN LIMITS IAW SRM 55-20-00 FIG 101.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,822 hrs · 31,350 cycles

CABIN NR 1 FLOOR SEAT TRACK CORRODED AT FWD END RBL 9 AT FS 364.00. REMOVED CORRODED FLOOR SEAT TRACK & REPLACED WITH NEW SERVICEABLE FLOOR SEAT TRACK IAW SRM 53-01-11.

Part: POST — CRACKED (FUSELAGE) · airframe 33,822 hrs · 31,350 cycles

VERTICAL POST AT RBL 18 ON FS 409+128 BULKHEAD IS CRACKED AT LOWER END, OTBD AFT FLANGE. REPAIRED RBL 18 OTBD POST AT FS 409+128 IAW REO 601R-53-41-056 REV F DATED 2011/09/02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,822 hrs · 31,350 cycles

SEAT TRACK AFT OF 9G TIE DOWN AT FS 559+112 HAS CORROSION AROUND FASTENERS HOLES. REMOVED UNSERVICEABLE SEAT TRACK & INSTALLED A NEW SERVICEABLE TRACK IAW SRM 53-01-11.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 33,822 hrs · 31,350 cycles

FS 280.00 FLOOR ANGLES CORRODED & RBL 9 OTBD CLIP CRACKED. REPAIRED FWD 7 AFT FLOOR ANGLES AT FS 280 RBL 9 - LBL9. R & R OTBD CLIP AT FS 280 & RBL 9 IAW SRM 51-21-06, 53-00-00 & REO 601R-53-11-171 REV D.

Part: APU — SHUTDOWN (APU BAY) · airframe 33,246 hrs · 30,819 cycles

TURNED APU GENERATOR ON, APU AUTO SHUTDOWN. HEAVY SMELL OF JET FUEL & SMOKE FROM EXHAUST. ACTION TAKEN IN PROGRESS.

Part: FUEL SYS — LEAKING (APU) · airframe 32,896 hrs · 30,477 cycles

3847 WITH PACKS ON THERE IS A STRONG FUEL SMELL IN THE AIRPLANE WITH APU ON. FOUND FUEL LEAK BY FUEL CONTROL. R, OPERATIONS & LEAK CHECKED GOOD AT THIS TIME NO FUEL SMELL NOTED IN CABIN.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 30,953 hrs · 28,613 cycles

FLAPS FAIL CAUTION MSG DURING RETRACTION AFTER LANDING. PERFORMED FLAP RESET PROCEDURE IAW AWAC SUP 98-18E BOX 12. FLAPS RESET. PLACARD AND PLACED ON MEL.

Part: WINDSHIELD — DAMAGED (COCKPIT) · airframe 30,722 hrs · 28,387 cycles

IN FLIGHT SAW SPARKING AND MELTING ON LEFT WINDSHIELD. COMPLIED WITH QRH. TURNED WINDSHIELD HEAT OFF, SPARKS STOPPED. COORDINATED WITH DISPATCH AND ATC, RETURNED TO LAND AT DCA. LANDING WEIGHT 39,000. NO FURTHER INCIDENT. REPLACED LEFT WINDSHIELD.

Part: BPSU — FAILED (TE FLAPS) · airframe 29,659 hrs · 27,362 cycles

FLAPS FAILED WHEN SELECTED 20-30. FLAPS STAYED AT 20 DEGREES. REPLACED RT BPSU PER 27 51 OPS CK GOOD.

Part: BPSU — FAILED (LT TE FLAPS) · airframe 29,657 hrs · 27,360 cycles

FLAPS FAILED IN FLT AT 20 DEGREES WHEN 30 DEGREES WAS SELECTED. PERFORMED FLAP RESET PROCEDURE IAW SUPPLEMENT 98-18E BOX 12, FLAPS RESET. FOUND REPEAT BPSU FAULT CODES IN FECU, REPLACED LT BPSU IAW AMM 27-51. OPS CK GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION

CARGO BOTTLE LOW CAUTION MESSAGE IN FLIGHT, NO INDICATION OF FIRE/SMOKE. INSPECTED CARGO BAY, NO EVIDENCE OF FIRE/SMOKE. NO BOTTLE DISCHARGE.

Part: PANEL — CRACKED (RT PYLON) · airframe 29,051 hrs · 26,771 cycles

RT ENGINE PYLON PANEL 422AB HAS CRACKED SEAL RETAINER. REMOVED UNSERVICEABLE RT ENG PYLON PANEL 422AB SEAL RETAINER AND INSTALLED SERVICEABLE SEAT RETAINER IAW SRM 51-42-06.

Part: BRACKET — BROKEN (SENSE LINE) · airframe 29,051 hrs · 26,771 cycles

T2 SENSE LINE BRACKET BROKEN, SUPPORT BRACKET FOR THE T2 SENSE LINE ON TOP OF THE ENGINE. REMOVED ENG INLET AND INSTALLED A NEW SERVICEABLE BRACKET.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 29,051 hrs · 26,771 cycles

DURING REPAIR OF AFT END FLANGE OF NR 2 HYD MANIFOLD BRACKET, FOUND CRACKS IN FWD AREAS REQUIRING BRACKET REPLACEMENT. REMOVED UNSERVICEABLE MANIFOLD BRACKET, FABRICATED AND INSTALLED SERVICEABLE MANIFOLD BRACKET.

Part: BRACKET — CRACKED (FS 718) · airframe 29,051 hrs · 26,771 cycles

HYD SYS NR 2 MANIFOLD BRACKET CRACKED. REPAIR CRACK IN NR 2 HYD MANIFOLD SUPPORT BRACKET IAW REO 601R-53-62-211 ON RT SIDE.

Part: HANDLE — GOUGED (CARGO DOOR) · airframe 29,051 hrs · 26,771 cycles

OUTER HANDLE RECESS GOUGED ON CARGO DOOR. REMOVED UNSERVICEABLE CARGO DOOR HANDLE AND INSTALLED SERVICEABLE CARGO DOOR HANDLE IAW CRJ 200 51-42-21.

Part: DOOR — CHAFED (LT MLG) · airframe 29,051 hrs · 26,771 cycles

LT MLG DOOR L/E AND T/E CHAFED. BLENDED CHAFE ON LT MLG DOOR T/E FOUND TO BE WITHIN LIMITS ORIGINAL .050. REMOVED .012 REMAINING .038 IAW SRM 51-12-00 AND 52-82-00 USING THICKNESS GAUGE ALODINED, PRIMED AND TOP COATED IAW SRM 51-21-11, 51-25-06, 51-25-16. BLENDED CHAFE ON LT MLG DOOR L/E. CONT. FOUND TO BE OUT OF LIMITS ORIGINAL .050 REMOVED, .028 REMAINING, .022 IAW SRM 52-82-00, 51-12-00.

Part: SKIN — GOUGED (FS 672) · airframe 29,051 hrs · 26,771 cycles

SKIN AT TOP OF FUSELAGE AT FS 672 IS GOUGED. FOUND TO BE BEYOND SERVICEABLE LIMITS, COMPLIED FULLY WITH REPAIR NR 3 EXTERNAL NON-FLUSH PERMANENT REPAIRS NON-PRESSURIZED AREA IAW SRM 53-00-31.

Part: SUPPORT BRACKET — CRACKED (CASE DRAIN) · airframe 29,051 hrs · 26,771 cycles

SYS 2 CASE DRAIN BRACKET SUPPORT CRACKED. REMOVED UNSERVICEABLE BRACKET AND INSTALLED SERVICEABLE BRACKET IAW SRM 51-42-06.

Part: BRACKET — CRACKED (STOW SWITCH) · airframe 29,051 hrs · 26,771 cycles

LT ENGINE THRUST REVERSER STOW SWITCH BRACKET CRACKED. R & R LT ENGINE T/R STOW SWITCH BRACKET WITH NEW SERVICEABLE PN 228-55410-835 IAW SRM 51-42-06.

Part: LUG — WORN (RT MLG DOOR) · airframe 29,051 hrs · 26,771 cycles

RT MLG DOOR PUSH LUG, WORN BEYOND LIMITS IN REO 601R-52-82-143 INSTALLED SERVICEABLE REPLACEMENT LUG IAW SRM 51-41-011, 51-42-21.

Part: SEAT TRACK — WORN (COCKPIT) · airframe 29,051 hrs · 26,771 cycles

COPILOT SEAT TRACK AND SEAT STOP ARE WORN. REMOVED UNSERVICEABLE COPILOT SEAT TRACK AND SEAT STOP AND REPLACED WITH SERVICEABLE SEAT TRACK IAW AMM53-01-05 AND SRM 51-42-21.

Part: SEAT TRACK — CORRODED (FS 559) · airframe 29,051 hrs · 26,777 cycles

CENTER ATTACH SEAT TRACK ARE CORRODED. R & R SEAT TRACK IAW AMM 53-01-11.

Part: TRUNNION — DAMAGED (RT MLG) · airframe 29,051 hrs · 26,771 cycles

DURING OILED WORKING OF RT MLG TRUNNION LOWER FLANGE FOUND 1 EA OVER SIZE HOLE IN TRUNNION PLANK AND PLATE.

Part: CARGO TRACK — CORRODED (FS 559) · airframe 29,051 hrs · 26,771 cycles

CORROSION FOUND ON CARGO TRACK RBL 27 AFT OF FS 559+80. R & R CARGO TRACK WITH SERVICEABLE IAW AMM 52-01-11.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 24,672 hrs · 22,208 cycles

(AT GATE) SIDEWALL LIGHTS AT ROW 9DF ARE FLICKERING WITH A SLIGHT BURNING SMELL. R & R 8/9F SIDEWALL LIGHT FIXTURE REF AMM 33 21 07. OPS CK GOOD. NO EVIDENCE OF BURNING SMELL FROM THIS LIGHT FIXTURE.

Part: FITTING — BENT (VERT STABILIZER) · airframe 24,647 hrs · 22,179 cycles

LT VISOR FITTING ON HORIZONTAL STUB IS BENT ON LOWER SIDE. R & R IAW REO 601R-55-11-016, REV A.

Part: PRESSURE BLKHD — CRACKED (BS 202.75) · airframe 24,647 hrs · 22,179 cycles

CRACK IN FWD PRESSURE BULKHEAD AT BRAKE CABLE FEED THROUGH IN LT HYD BAY FS202.75. REPAIRED CRACKED IN FWD PRESSURE BULKHEAD FS 202.75 IAW REO 601R-53-11-563.

Part: SUPPORT ANGLE — GOUGED (VERTICAL STAB) · airframe 24,647 hrs · 22,179 cycles

LOWER VISOR SUPPORT ANGLE ON LT SIDE OF VERTICAL STAB GOUGED BLENDED OUT GOUGED AREAS ON SUPPORT ANGLE IN AREAS B, C.

Part: FITTING — CHAFED (VERTICAL STAB) · airframe 24,647 hrs · 22,179 cycles

VERT STAB FITTING CHAFED UNDER HORIZ STAB ON T AFT CORNER BLENDED CHAFE AREA AFT LT CORNER OF FITTING UNDER HORIZ STAB IAW SRM 51-12-00 AND REO 601R-55-31-192.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 24,647 hrs · 22,179 cycles

FS 280 FWD FLOOR SUPPORT ANGLE BENEATH CTR FLIGHT COMPARTMENT FLOORBOARD CRACKED. R & R FS 280 FWD ANGLE IAW SRM 51-42-06 & 51-42-21.

Part: ATTACH FITTING — CORRODED (BS 319 S17R) · corrosion level 2 · airframe 24,647 hrs · 22,179 cycles

SERVICE DOOR LOWER SILL FWD CLIP IS CORRODED. SERVICE DOOR LOWER SILL FWD CLIP R & R IAW SRM 51-42-21.

Part: FLOORBEAM — CORRODED (BS 349) · corrosion level 2 · airframe 24,647 hrs · 22,179 cycles

FLOORBEAM AT FS 349 IS CORRODED, REO 601R-53-21-1143 CARRIED OUT.

Part: FLOORBEAM — CORRODED (BS 280) · corrosion level 2 · airframe 24,647 hrs · 22,179 cycles

FS 280 FLOOR STRUCTURE BENEATH FLIGHT COMPARTMENT CTR FLOOR PANEL HAS CORROSION. REPAIRED DAMAGE TO FS 280 BULKHEAD WEB IAW REO 601R-53-11-926.

Part: ATTACH FITTING — CORRODED (BS 349) · airframe 24,647 hrs · 22,179 cycles

SERVICE DOOR AFT CLIP IS CORRODED SERVICE DOOR AFT CLIP R & R IAW SRM 51-42-21.

Part: PRESSURE BLKHD — CRACKED (BS 621) · airframe 24,647 hrs · 22,179 cycles

FOUND CRACK AT RBL 36 ON FS 621.00 PRESSURE BULKHEAD APPROX 2 INCHES ABOVE FIRST ISOLATOR ABOVE FLOOR LINE. REPAIRED DAMAGED AREA BY INCORPORATION OF REO 601R-53-61-1285, REV B DATED 04/19/10.

Part: BRACKET — CRACKED (BS 674) · airframe 24,647 hrs · 22,179 cycles

CARGO BAY DOOR FWD LOWER 4 CHANNEL TRACK BRACKET CRACKED FROM RIVET HOLE, REPLACED TRACT BRACKET IAW SRM 51-42-06, 51-40-11, 51-41-02 AND AMM 51-23-00, 51-21-11.

Part: ATTACH FITTING — CHAFED (LT WING TE FLAP) · airframe 24,647 hrs · 22,179 cycles

LT INBD FLAP INBD AFT HINGE BOX ATTACH LUG (ON THE WING) IS CHAFED BLEND, LPI OR EDDY CURRENT AND SHOT PEEN IAW REO 601R-57-21-1299.

Part: PANEL — GOUGED (RT NACELLE) · airframe 24,647 hrs · 22,179 cycles

T/E OF UPPER TRANSLATING COWL PANEL 444AT GOUGED. BLEND, NDT, TREAT AREA (PROTECT UNFINISH) AND RECORD REO NR ON COMPONENT SERIAL PLATE IAW REO 601R-78-33-3935.

Part: STRUCTURE — CRACKED (THRUST REVERSER)

T/E RT THRUST REVERSER IS CRACKED AT THE 5:30 AND 6:30 POSITIONS. REMOVED DAMAGE AND INSTALLED DOUBLERS IAW REO 601R-78-30-3999.

Part: FITTING — CHAFED (HORIZONTAL STAB) · airframe 24,647 hrs · 22,179 cycles

DAMAGE TO LT STAB ON INBD LUG OF HINGE FITTING NR2, PN 600-23046 REF AT BL 55.8865. THE CHAFE DAMAGE IS LOCATED ON THE BOTTOM FACE OF THE FITTING, INBD LUG (0790"L X 0.100" X 0.200D MAX). NICK DAMAGE IS LOCATED ON THE EDGE PLATE. BLEND OUT EACH DAMAGE TO SMOOTH CONTOUR (5:1 TRANSITION) IAW SRM 51-12-00. DO NOT EXCEED MAX REPORTED DAMAGE DEPTH 10.020 & 0.015 REF) LPI ON EDDY CURRENT INSPECT SHOT PEEN OR ROTO PEEN, REWORKED AREA TOUCH UP. REWORKED AREA TO FINISH.

Part: RIB — CRACKED (RT WING) · airframe 24,647 hrs · 22,179 cycles

BATT RIB CRACKED IN RT WW CUTOUT DAMAGE & INSTALL DOUBLER IAW REO 601R-57-51-046.

Part: FRAME — CRACKED (BS 559) · airframe 24,647 hrs · 22,179 cycles

FOUND LBL 18, FS 559, CRACKED FROM LOWER RIVET TO EDGE OF ANGLE. REPAIR IAW REO 601R-53-41-260, REV D.

Part: BRACKET — CHAFED (BS 574) · airframe 24,647 hrs · 22,179 cycles

CARGO DOOR STEP PLATE FWD AND AFT BRACKETS ARE CHAFED. R & R CARGO DOOR STEP PLATE FWD AND AFT BRACKETS IAW SRM 51-40-11, 51-42-21, AMM 51-23-00.

Part: THRESHOLD — CRACKED (BS 574) · airframe 24,647 hrs · 22,179 cycles

CARGO DOOR THRESHOLD IS CRACKED LOCATED FWD SIDE AROUND HI LOCK COMPLIED WITH REO 601R-53-61-1741 IAW SRM 51-25-06, 51-25-16, 51-21-16, 51-42-06 AND AMM 51-21-11.

Part: FITTING — CRACKED (BS 461) · airframe 24,647 hrs · 22,179 cycles

RT BATH TUB FITTING AT RBL9 AND FS 461 IS CRACKED. REMOVED CRACKED FITTING, INSTALLED NEW FITTING.

Part: SKIN — DENTED (LT WING) · airframe 24,647 hrs · 22,179 cycles

C/W AWAC CARD 4DMI13898, REPAIR LT WING L/E DENT ( C-CHECK) SRM 57-41-31. REMOVED DAMAGED LT CTR L/E SKIN BETWEEN WS 149.58 & WS 247.95, & INSTALLED SERVICEABLE LT CTR L/E SKIN (PN 601R12057-3) IAW SRM 51-42-06, 51-40-11, 51-42-13.

Part: ANGLE — CRACKED (BS 621) · airframe 24,647 hrs · 22,179 cycles

RT OBLIQUE ANGLE ON AFT PRESSURE BULKHEAD CRACKED. R & R ANGLE IAW SRM 51-42-00.

Part: DOOR FRAME — CRACKED (BS 338.9) · airframe 24,647 hrs · 22,179 cycles

PAX DOOR FRAME 338.90 CRACKED AT UPPER TORQUE TUBE CUT OUT DAMAGED FRAME AND SPLICED IN NEW FRAME PN 601R-31902-5 IAW REO 601R-52-11-402.

Part: STRIP — CHAFED (LT NOSE COWL) · airframe 24,647 hrs · 22,179 cycles

LT UPPER NOSE COWL T/E CHAFED. REPLACED AFT EDGE STRIP PN 228-50080-107 IAW CMM 71-14-01-300-814-A01 REPAIR NR SRS091.

Part: PANEL — CHAFED (RT NACELLE) · airframe 24,647 hrs · 22,179 cycles

PANEL 422DB DIVIDERS ARE KNIFE EDGED. INSTALLED NEW SEPARATORS ON PANEL 422DB.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 24,647 hrs · 22,179 cycles

OTBD CLIP ON LBL 9 AT FS 280 IS CRACKED. R & R CLIP AT FS 280, OTBD SIDE OF LBL 9.0 IAW SRM 51-42-21.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 24,647 hrs · 22,179 cycles

INBD CLIP ON RBL 9 AT FS 280 IS CRACKED. R & R CLIP AT FS 280, INBD SIDE OF RBL 9.0 IAW SRM 51-42-21.

Part: LIGHT — ODOR (CABIN) · airframe 24,599 hrs · 22,131 cycles

WITH CABIN CEILING LIGHTS ON, ACRID OZONE SMELL IN CABIN. SMELLS SEEM WORSE WITH CEILING AND SIDEWALL LIGHTS ON, SMELL DISIPATES WITH LIGHTS OFF. R & R CEILING LIGHT ASSY IAW AMM 33-21-01. OPS CHECK GOOD.

Part: DETECTION SYS — MALFUNCTIONED (APU BAY) · airframe 23,738 hrs · 21,232 cycles

ON APPROACH WHEN TRANSFERRING BLEEDS TO APU RECEIVED APU OVERTEMP WARNING FOLLOWED BY APU FIRE WARNING. SHUT APU DOWN MESSAGES WENT AWAY APU DOOR INHIBIT STATUS MESSAGE DISPLAYED. INSP APU, APU COMPARTMENT FOUND NO EVIDENCE OF FIRE BUT NOTED SLIGHT ODOR. UNINHIBITED DOOR AND RECORDED FAULT CODES 109, 226, 227, AND 230. INSPECTED APU INLET APU FIRE LOOP FOUND NO DEFECTS OPERATED APU FOR 25 MINUTES NO FAULTS NOTED EGT NORMAL IAW AMM 49-10-00. REMOVED FROM MEL.

Part: WIRE — BROKEN (WHEEL XDUCER) · airframe 23,042 hrs · 20,535 cycles

AT ROTATION SPEED, OTBD ANTISKID CAUTION MSG ILLUMINATED. CLIMBED OUT, C/W QRH AND RETURNED TO DEPARTURE FOR LANDING. FOUND BROKEN WIRE ON LT OTBD WHEEL SPEED TRANSDUCER, REINSTALLED CONNECTOR IAW ESPM 20 17 00 ANTISKID CONTROL UNIT BITE TEST GOOD AT THIS TIME, CAUTION MESSAGE EXTINGUISHED. (K)

Part: LATCH — INOPERATIVE (PAX DOOR) · airframe 22,739 hrs · 20,227 cycles

REQUEST INSP OF MAIN PASSENGER DOOR. WILL NOT LATCH CLOSED FROM INSIDE OR OUTSIDE. (K)

Part: CONTROL PANEL — MALFUNCTIONED (RUDDER TRIM) · airframe 22,717 hrs · 20,209 cycles

ON DEPARTURE, RUDDER TRIM CONTROL STUCK IN FULL NOSE LEFT WHEN USED. REMOVED AND REPLACED RUDDER TRIM PANEL REF AMM 27-12-10. OPS CHECK GOOD AT THIS TIME. (K)

Part: LINE — LEAKING (HYD SYSTEM) · airframe 22,160 hrs · 19,656 cycles

HYD NR 2 LOW PRESSURE, FOLLOWED QRH, QTY 5 PERCENT. REMOVED AND REPLACED NR 2 HYD PRESSURE LINE FROM FILTER TO AIRFRAME. AMM 29-10-00. LEAK CHECK GOOD. (K)

Part: SENSOR — MALFUNCTIONED (TE FLAPS) · airframe 21,036 hrs · 18,617 cycles

FLAP FAIL AT ZERO DEGREES IB. PERFORMED ZERO FLAP LANDING. BRAKE TEMPS 3,2,1,2. R&R BPSU. BPSU OPS AND RIG CHECK GOOD AT THIS TIME.

Part: SCAVENGE PUMP — MALFUNCTIONED (LT ENGINE) · airframe 21,013 hrs · 18,592 cycles

LOG 192858/1&2 LOSS OF LT OIL PRESSURE INFLIGHT AT FLIGHT LEVEL 340. COMPLIED QRH SHUTDOWN LT ENGINE. R&R LT ENG SCAVANGE PUMP IAW AWAC 70-21-01. PERFORMED OIL CONSUMPTION CHECK AND OK LEAK CHECK. ALL CHECKS GOOD AT THIS TIME.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 1 · airframe 14,844 hrs · 12,616 cycles

CORROSION ON FLOOR ANGLE BETWEEN FS 409+128 TO FS 559 TO LBL 46. CORROSION ON FLOOR ANGLE FS 409+128 TO FS 559 AT LBL 46, REMOVED IAW CRJ 200 SRM 53-41-45 FIG 101. (A)

Part: PLATE — GOUGED (T/E FLAP) · airframe 14,844 hrs · 12,616 cycles

GOUGE FOUND ON AFT HINGE LOG PLATE OF LT INBOARD FLAP. GOUGE REMOVED IAW REO 601R-57-1343. (A)

Part: STRUCTURE — CRACKED (APU BAY) · airframe 14,844 hrs · 12,616 cycles

APU ENCLOSURE CRACKED. APU ENCLOSURE REPAIR DONE IAW REO 601R-49-11-071. (A)

Part: ATTACH FITTING — GOUGED (T/E FLAP) · airframe 14,844 hrs · 12,616 cycles

LEFT OUTBOARD FLAP, OUTBOARD FLAP HINGE ARM FOUND GOUGED ON BEARING ATTACHMENT PLATE, FWD FACE. GOUGE ON BEARING ATTACHMENT PLATE FWD FACE REMOVED IAW REO 601R-57-54-112. (A)

Part: PLATE — GOUGED (T/E FLAP) · airframe 14,844 hrs · 12,616 cycles

GOUGE FOUND ON AFT HINGE LOG PLATE OF RT INBOARD FLAP. GOUGE ON AFT HINGE LUG PLATE OF RT INDB FLAP REMOVED IAW REO 601R-57-52-1341. (A)

Part: FITTING — CORRODED (CARGO BAY) · airframe 14,844 hrs · 12,616 cycles

CORROSION ON THREE TIE DOWN CARGO DOOR NET AROUND FLOOR SCREW. CORROSION ON THREE TIE DOWNS OF CARGO DOOR NET REMOVED AND TREATED IAW SRM 51-21-06. (A)

Part: SKIN — DENTED (PAX DOOR) · airframe 14,844 hrs · 12,616 cycles

DENTS ON PASSENGER DOOR FWD AND AFT UPPER CORNER COVERS. ON FURTHER INVESTIGATION, CRACKS FOUND ON PARTS (CORNERS) ON PAX DOOR FWD AND AFT REMOVED AND REPLACED IAW SRM 51-42-06 AND SRM 51-42-13. (A)

Part: SILL — CORRODED (FUSELAGE) · airframe 14,844 hrs · 12,616 cycles

CORROSION ON FLOOR SILL LEFT SIDE BETWEEN FS 574 AND FS 621. CORROSION ON FLOOR SILL LT SIDE BETWEEN FS 574 AND FS 621. REMOVED AND TREATED IAW SRM 51-21-06. (A)

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 14,844 hrs · 12,616 cycles

CORROSION FOUND ON CARGO TRACK RBL 9 BETWEEN FS 559 + 110 AND FS 568. CARGO TRACK REPLACED IAW AMM 53-01-11-400-802. (A)

Part: PLATE — CORRODED (SERVICE DOOR) · airframe 14,844 hrs · 12,616 cycles

SERVICE DOOR LOWER PROTECTIVE PLATE P/N 601R38957-19, FOUND CORRODED OVER LIMITS. SERVICE DOOR LOWER PROTECTIVE PLATE REPLACED IAW SRM 51-41-04. (A)

Part: SILL — CORRODED (BS 319-349) · airframe 14,844 hrs · 12,616 cycles

CORROSION ON ANGLE OF PAX DOOR LOWER SILL BETWEEN FS 319 TO FS 349, WL 72. CORROSION ON ANGLE REMOVED IAW SRM 51-21-06. (A)

Part: PLATE — CORRODED (LT PYLON) · corrosion level 2 · airframe 14,844 hrs · 12,616 cycles

LEFT PYLON TRAINING EDGE, INBOARD UPPER BONDING PLATE CORRODED. REMOVED CORROSION ON UPPER BONDING PLATE LT PYLON TRAILING EDGE INBOARD SIDE IAW CRJ 200 SRM 51-21-06 AND WITHIN LIMITS IAW SRM 54-00-00. (A)

Part: PLATE — CORRODED (LT PYLON) · corrosion level 2 · airframe 14,844 hrs · 12,616 cycles

LEFT PYLON TRAILING EDGE, OUTBOARD UPPER BONDING PLATE CORRODED. REPLACED BECAUSE OF MATERIAL OUT OF LIMITS TOLERANCE IAW ARM 54-00-00. FORMED AND INSTALLED NEW BONDING PLATE IAW SRM 51-24-21 AND SRM 51-42-10. (A)

Part: PLATE — CORRODED (RT NACELLE) · corrosion level 2 · airframe 14,844 hrs · 12,616 cycles

RIGHT PYLON TRAILING EDGE, OUTBOARD UPPER BONDING CORRODED. CORROSION REMOVED IAW 51-21-06 AND WITHIN LIMITS IAW SRM 54-00-00. (A)

Part: CARGO TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,844 hrs · 12,616 cycles

CORROSION ON CARGO TRACK AT LBL 9 BTW FS 559 + 110 AND FS 570. CARGO TRACK REPLACED IAW AMM 53-01-11-400-802. (A)

Part: PLATE — CORRODED (RT PYLON) · corrosion level 2 · airframe 14,844 hrs · 12,616 cycles

RT PYLON TRAILING EDGE, INBOARD UPPER BONDING PLATE CORRODED. CORROSION REMOVED IAW CRJ 200 SRM 51-21-06 AND WITHIN LIMITS IAW SRM 54-00-00. (A)

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 14,844 hrs · 12,616 cycles

CORROSION ON BOTH CLEATS OF PAX DOOR SURROUND STRUCTURE LOWER SILL BETWEEN FS 310 TO FS 349. CORROSION REMOVED IAW SRM 51-21-06. (A)

Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 14,844 hrs · 12,616 cycles

PILOT`S BULKHEAD, CROSSBEAM CRACKED AT FS 280, LBL 9. BULKHEAD CROSSBEAM REPAIRED IAW REO 601R-53-11-171 REV D SCHEME B. (A)

Part: CROSSBEAM — CRACKED (BULKHEAD) · airframe 14,844 hrs · 12,616 cycles

PILOT`S BULKHEAD, CROSSBEAM CRACKED AT FS 280, RBL 9. BULKHEAD REPAIRED IAW REO 601R-53-11-171 REV D SCHEME B. (A)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 14,844 hrs · 12,616 cycles

CRACK EXIST ON BRACKET INTERCOSTAL FS 621 TO 625 ADJACENT TO STR 14 LEFT. BRACKET OF INTERCOSTAL FS 621 TO 625 ADJACENT TO STR 14 LT REPLACED IAW SRM 51-42-21. (A)

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 14,844 hrs · 12,616 cycles

PAX DOOR EDGE MEMBER CRACKED AT FS 338. REPAIRED IAW REO 601R-52-11-279. (A)

Part: WHEEL — BENT (NLG) · airframe 18,695 hrs · 16,356 cycles

RIGHT NOSE WHEEL RIM BENT. REMOVED AND REPLACED RIGHT AND LEFT NOSE LANDING GEAR TIRE ASSEMBLIES IAW AMM 32-40. NLG WHEEL ASSY LT P/N 5010598 S/N AUG99-2288 TSN 6672 CSN 6269, AND NLG WHEEL ASSY RT P/N 5010598 S/N APR03-4829 TSN 4436 CSN 4228. (M)

Part: CONNECTOR — DIRTY (SELECTOR VALVE)

GEAR DISAGREE AND DOOR WARNING MESSAGE INFLIGHT, COMPLIED WITH QRH AND RETURNED TO PHL. FOUND ERROR CODE D046/SELECTOR VALVE IN PSEU. CLEANED CONNECTOR AND FILTER AT NLG SELECTOR VALVE. PERFORMED NLG EXTENSION AND RETRACTION TEST IAW AMM 32-33-00. OPS CHECK GOOD. (M)

Part: HANDLE — LACK OF LUBE (PAX DOOR) · airframe 17,083 hrs · 14,773 cycles

AT ROTATION GOT PAX DOOR CAUTION MESSAGE ILLUMINATED COMPLIED WITH QRH GREEN WITNESS MARKS NOT ALIGNED AT GATE DOOR STILL WOULD NOT CLOSE PROPERLY. INSPECTED DOOR AND FOUND EXTERNAL HANDLE WOULD NOT STOW WITHOUT USE OF EXCESSIVE FORCE FROM INTERNAL STOW HANDLE. HANDLE STOWS NORMALLY FROM OUTSIDE AIRCRAFT. CAX FLT 3952, 3969, 3596 REF 168980/1. LUBRICATED PAX DOOR LATCH PINS AND OUTER HANDLE. STOWS NORMAL WITH LOCKED GREEN INDICATORS ALIGNED IAW EO E98/023/452. FOR PHASE 4 DOOR. REMOVED FROM MEL. (K)

Part: WIRE HARNESS — DEFECTIVE (MLG WOW) · airframe 16,664 hrs · 14,369 cycles

APPROXIMATELY 17,000 AGL (STEERING INOP) CAS MESSAGE ILLUMINATED MOMENTS LATER (WOW INPUT) MESSAGE ILLUMINATED. COMPLIED WITH QRH. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED MLG WOW NR 1 ELECTRICAL HARNESS. OPS CHECK GOOD AT THIS TIME, IAW AMM 32-61-05.

Part: CLAMP — LOOSE (FIRE LOOP)

APU FIRE WARNING MESSAGE WITH ASSOCIATED AURAL AND VISUAL WARNING, APU FAULT MESSAGE ALSO APPEARED. COMPLIED WITH IMMEDIATE ACTION CHECKLIST AND QRH. EMERGENCY LANDING IN CLT. BOTTLES NOT DISCHARGED. INSPECTED APU INTAKE AND APU COMPARTMENT, NO EVIDENCE OF FIRE, SUSPECT FAULTY APU FIRE DETECTION LOOP. FOUND TWO LOOSE CLAMPS, ADJUSTED ROUTING OF SENSOR ELEMENT AND RECONNECTED TWO EACH CLAMPS. OPS CHECK GOOD. (M)

Part: WINDSHIELD — DELAMINATED (COCKPIT) · airframe 15,964 hrs · 13,691 cycles

RT WINDSHIELD HEAT MESSAGE, FOLLOWED BY RT WINDSHIELD DELAMINATION. REMOVED AND REPLACED RT WINDSHIELD ASSY IAW AMM. (K)

Part: FRAME — DAMAGED (BS 640)

OVERSIZED HOLE ON THE LEFT SIDE FUSELAGE AT STRINGER 10L FRAME STATION 640. MAINTENANCE REPAIRED OVERSIZE HOLE BY TRIMMING OUT SKIN AND FABRICATING AND INSTALLING FILLER IAW BOMBARDIER SERVICES EO 601R-53-9303. (M)

Part: FLOOR SUPPORT — CRACKED (BS 621)

FOUND LEFT FS 621 FLOOR SUPPORT ANGLE HAS A 1 INCH LONG CRACK IN OUTBOARD RADIUS. (M)

Part: CLIP — CRACKED (BS 280)

FOUND LEFT FS 280 CLIP AT LBL 9 INBOARD HAS A .5 INCH LONG CRACK. MAINTENANCE REPLACED CLIP, P/N 601R31113-57, AT FS 280 LBL 9 IAW CRJ SRM 51-42-06 AND SRM 51-42-21. (M)

Part: CLIP — CRACKED (BS 280)

FOUND LEFT FS 280 CLIP AT LBL 9 OUTBOARD HAS A .5 INCH LONG CRACK. MAINTENANCE REPLACED CLIP, P/N 601R31113-57 AT FS 280 LBL 9 OUTBOARD IAW BSC STANDARD REPAIR 601R-53-0057A AND CRJ SRM 51-42-21. (M)

Part: CLIP — CRACKED (BS 280)

FOUND RT FS 280 CLIP AT RBL 9 OUTBOARD HAS A .5 INCH LONG CRACK. MAINTENANCE REPLACED CLIP, P/N 601R31113-58 AT FS 280 RBL 9 OUTBOARD IAW BSC STANDARD REPAIR 601R-53-0057A AND CRJ SRM 51-42-21. (M)

Part: CLIP — CRACKED (BS 280)

FOUND RT FS 280 CLIP AT RBL 9 INBOARD HAS A .5 INCH LONG CRACK. MAINTENANCE REPLACED CLIP, P/N 601R31113-58 AT FS 280 RBL 9 IAW CRJ SRM 51-42-06 AND SRM 51-42-21. (M)

Part: FLOOR SUPPORT — CRACKED (BS 621)

LEFT FS 621 FLOOR SUPPORT ANGLE HAS A 1 INCH LONG CRACK IN OUTBOARD RADIUS. MAINTENANCE REPAIRED LT FS 621 FLOOR SUPPORT ANGLE IAW BOMBARDIER REO 601R-53-61-117 REV C. (M)

Part: SKIN PANEL — CORRODED (WING)

THE WING PLANK ACCESS HOLE CUT OUT FOR PANEL 510AB AT WS 12.245 HAS CORROSION PITTING AT THE OUTBOARD RADIUS .004 INCH DEEP AND AT THE INBOARD RADIUS .003 INCH DEEP. MAINTENANCE BLENDED MINOR CORROSION IAW BOMBARDIER REO 601R-57-21-030 REV D. (M)

Part: SKIN PANEL — CORRODED (WING)

THE WING PLANK CUTOUT FOR PANEL 640BB AT WS 54.897 HAS 3 SPOTS OF MINOR CORROSION PITTING ONE .003 INCH DEEP AT THE OUTBOARD RADIUS AND TWO ON THE INBOARD RADIUS .004 INCH AND .007 INCH DEEP. MAINTENANCE BLENDED MINOR CORROSION IAW BOMBARDIER REO 601R-57-21-030 REV D. (M)

Part: INTERCOSTAL — CRACKED (BS 484)

THE INTERCOSTAL AT FS 484 LBL 27 LBL 36 HAS A .60 INCH CRACK AT THE FLANGE AT LBL 36. MAINTENANCE REPAIRED INTERCOSTAL IAW BOMBARDIER REO 601R-53-41-059 AND STANDARD REPAIR 601R-53-003A. (M)

Part: INTERCOSTAL — CRACKED (BS 484)

THE ANGLE ON THE INTERCOSTAL AT FS 484 LBL 27 HAS A .50 INCH CRACK. (M)

Part: INTERCOSTAL — CRACKED (BS 484)

THE INTERCOSTAL AT FS 484 RBL 27-RBL 36 HAS A CRACKED FLANGE .80 INCH LONG. MAINTENANCE REPAIRED INTERCOSTAL IAW BOMBARDIER REO 601R-53-41-059 AND STANDARD REPAIR 601R-53-0030A. (M)

Part: INTERCOSTAL — CRACKED (BS 484)

THE ANGLE ON THE INTERCOSTAL AT FS 484 RBL 27 HAS A .70 INCH CRACK IN IT. MAINTENANCE REPLACED ANGLE IAW STANDARD REPAIR 601R-53-0029B. (M)

Part: INTERCOSTAL — CRACKED (BS 484)

THE ANGLE ON THE INTERCOSTAL AT FS 484 LBL 27 HAS A .50 INCH CRACK. MAINTENANCE REPLACED ANGLE IAW STANDARD REPAIR 601R-53-0029B. (M)

Part: INTERCOSTAL — CRACKED (BS 484)

THE INTERCOSTAL AT FS 484 LBL 27 - LBL 36 HAS A .60 INCH CRACK AT THE FLANGE AT LBL 36. (M)

Part: ACCESS PANEL — DAMAGED (LT WING)

WHILE ACCOMPLISHING SB 601R-57-037, THE NR 18 HOLE AT WS 148 LT WAS FOUND TO BE ELONGATED TO .280 INCH. REPAIRED ELONGATED HOLE AT LT WS 148 BY INSTALLING FREEZE PLUG IAW BRAS REO 601R-57-5757. (M)

Part: SKIN PANEL — DAMAGED (LT WING)

FOUND SCREW HOLE NEAR NACA SCOOP AT LT WS 148 ELONGATED TO .300 INCH. REPAIRED BY INSTALLING COUNTERSUNK FREEZE PLUG IN SKIN PANEL AND INNER STRINGER EO NR 601R-57-5753 REV A. (M)

Part: BUSHING — MIGRATED (LT MLG)

LEFT MAIN LANDING GEAR AFT TRUNNION BUSHING IS MIGRATED .025 INCH. (M)

Part: CONTROL SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 11,132 hrs · 9,378 cycles

ON APPROACH TO LANDING FLAPS FAILED AT 0 DEGREES UPON FLAP SELECTION TO 8 DEGREES. PLACED ON 72 FLAP WATCH C/W AWAC SUPPLEMENT 01-05. RESET FLAPS. NO DAMAGE NOTED.

Part: BUSHING — MIGRATED (LT MLG) · airframe 11,277 hrs · 9,495 cycles

LT MAIN LANDING GEAR AFT TRUNNION BUSHING IS MIGRATED .025 INCH. REMOVED MIGRATED BUSHING AND INSTALLED 2ND OVERSIZED BUSHING IAW REO.

Part: LANDING GEAR — MALFUNCTIONED (MAINS) · airframe 10,952 hrs · 9,223 cycles

WHEN C/W QRH FOR GEAR DISAGREE, MLG DID NOT EXTEND WHEN LANDING. MANUAL RELEASE HANDLE WAS PULLED PERFORMED OPS TEST OF MANUAL RELEASE SYSTEM FOR LANDING GEAR. NO FAULTS FOUND, ALL CHECKED IAW AMM32-34-00.

Part: WARNING LIGHT — ILLUMINATED (PAX DOOR)

PASSENGER DOOR OUTER HANDLE CAS MESSAGE IN FLIGHT. COMPLIED WITH QRH. CABIN PRESSURE NORMAL ALL SIX CAMS INDICATE LOCKED, MEL'D. (M)

Part: STRINGER — DAMAGED (FUSELAGE)

FOUND STRINGER 17L DAMAGED BETWEEN FS 687 AND FS 710. REMOVED DAMAGED SECTION OF STRINGER 17L FROM FS 686 TO FS 707. INSTALLED SECTION OF STRINGER P/N 601R35004-51 WITH SPLICE PIECES FROM 7075-T6 .050 INCH IAW WVAC EO 601R-53-4653A. (M)

Part: FRAME — DAMAGED (FUSELAGE)

FOUND FRAME 700 DAMAGED BETWEEN STRINGERS 16L AND 18L. REMOVED DAMAGED SECTION OF FRAME 700 FROM STRINGER 14L TO EXISTING SPLICE AT STRINGER 20L. FABRICATED SPLICE DOUBLER FROM 2024-T3 .040 INCH. INSTALLED SECTION OF FRAME P/N 600-360290-35 AND SPLICE DOUBLER IAW WVAC EO 601R-53-4653A. (M)

Part: SKIN — DAMAGED (FUSELAGE)

FOUND SKIN DAMAGED, LEFT SIDE OF AIRCRAFT AT FS 682 TO FS 718 BETWEEN STRINGERS 16L AND 18L. (M)

Part: WARNING LIGHT — FALSE ACTIVATION (NLG STEERING)

STEERING INOPERATIVE MESSAGE SHORTLY AFTER GEAR RETRACTION, GEAR DISAGREE MESSAGE AND NOSE DOOR OPEN MESSAGE. CYCLED GEAR SEVERAL TIMES. COULD NOT DUPLICATE. OPS CHECK GOOD IAW AMM 32-30-00. (M)

Part: PUMP — INOPERATIVE (HYD SYSTEM)

AFTER TAKEOFF GOT (GEAR DISAGREE) WARNING LIGHT, COMPLIED WITH QRH ALSO HAD STEERING INOP CAUTION MESSAGE. MESSAGE RESET. REPLACED HYDRAULIC PUMP 3A, GEAR SWINGS CHECKED GOOD. (M)

Part: STRUCTURE — DENTED (SPOILER)

FOUND LEFT FLIGHT SPOILER HAS A DENT THAT IS 1 INCH IN DIAMETER AND .038 INCH DEEP. PERFORMED INSPECTION AND EDDY CURRENT OF AREA IAW WVAC EO 601R-57-3945. (M)

Part: SKIN — CHAFED (RT TE FLAPS)

RT INBOARD FLAP, FLAP VANE HAS CHAFE DEEPER THAN PRESCRIBED LIMITS PER REO 601R-57-52-004, .014 DEEP. REMOVED AND REPLACED DEFECTIVE SECTION OF RIGHT FLAP VANE IAW WVAC EO 601R-57-3940. (M)

Part: PANEL — DAMAGED (DOOR)

RIGHT BUTE DOOR PANEL 694PB, HAS ELONGATED HOLE REAMED HOLE, FABRICATED FREEZE PLUG, INSTALLED FREEZE PLUG. ALL WORK ACCOMPLISHED IAW WVAC EO 601R-57-3931. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

THE RIGHT CARGO FLOOR SUPPORT ANGLE IS CRACKED AT FS 621, ABL36, WL 73. REMOVED SECTION OF RIGHT CARGO FLOOR SUPPORT ANGLE FS 621. REPAIRED RIGHT FLOOR SUPPORT ANGLE IAW BOMBARDIER INC REO 601R-53-61-117 REV B. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

THE LEFT CARGO FLOOR SUPPORT ANGLE IS CRACKED AT FS 621, LBL 36, WL 73. REMOVED CRACKED SECTION OF ANGLE AND INSTALLED REPAIR ANGLES IAW BOMBARDIER INC REO 601R-53-61-117 REV B. (M)

Part: BLOCKER DOOR — CRACKED (THRUST REVERSER)

RT ENGINE THRUST REVERSER BLOCKER DOOR NR 2 IS CRACKED AT DOOR HINGE MOUNTING POINT. REMOVED AND INSTALLED NEW SERVICEABLE DOOR IAW CRJ AMM 78-33-21-400-801. 9M)

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT)

14TH DUCT WARNING MESSAGE IN FLIGHT, COMPLIED WITH QRH MESSAGE CAME BACK TWICE MOMENTARILY. AFTER LANDING P/L IDLE MESSAGE CAME BACK STAYED ON GROUND RAN A/C AT VARIOUS POWER SETTINGS. RAN ALL SYSTEMS ASSOCIATED WITH 14TH STAGE BLEED, NO FAULTS NOTED. PER MAINTENANCE CONTROL SWAPPED LOOP CONTROL UNITS. OPS CHECK GOOD. (M)

Part: GCU — INOPERATIVE (ADG)

COMPLY WITH ADG INFLIGHT DEPLOYMENT IAW TASK 024/24/220/701. ADG FUNCTIONAL CHECK FAILED. REMOVED AND REPLACED GCU, S/N 0290. FLIGHT OPERATIONAL TEST OF ADG AUTO DEPLOYMENT SUCCESSFUL. GCU COMPONENT REPAIR SHOP TEAR-DOWN FINDINGS, NO FAULT FOUND (NFF).

Part: A/C PACK — SHUTDOWN (A/C BAY) · airframe 1,542 hrs · 1,336 cycles

LEFT AND RIGHT AIR CONDITIONING PACKS OVERHEATED AND SHUTDOWN. COULD NOT RESET IN FLIGHT. MAINTENANCE COMPLIED WITH OPERATIONAL CHECK OF AIR CONDITION SYSTEM I.A.W. THE AIRCRAFT MAINTENANCE MANUAL OPERATIONAL CHECK GOOD AT THIS TIME.