N402AW

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,058 hrs · 36,635 cycles

EMERGENCY FLOOR LIGHTING ROWS 2 - 6 INOPERATIVE. EMER EXIT SIGN AT ROW 8A INOPERATIVE.

Part: SHOULDER BELT — DEFECTIVE (COCKPIT) · airframe 39,737 hrs · 36,314 cycles

FIRST OFFICER SHOULDER HARNESS WILL NOT LOCK INTO RETAINER.

Part: SHOULDER BELT — DEFECTIVE (COCKPIT) · airframe 39,730 hrs · 36,306 cycles

ON APPROACH FIRST OFFICER WAS NOT ABLE TO LOCK SHOULDER HARNESS.

Part: ENGINE — BIRD INGESTION (RIGHT)

BIRD STRIKE RT ENG AFTER TAKEOFF, ROTATION VIB FELT IN ACFT, N1 FAN BLADES. ENG VIB WENT FROM .3 TO 2.1, LANDED UNDERWEIGHT. VIBE FELT IN FEET & YOKE.

Part: CONNECTOR — DIRTY (APU) · airframe 39,258 hrs · 35,856 cycles

IN FLIGHT RECEIVED APU OIL TEMP CAUTION. RAN QRH, DIVERTED BACK. MSG DID NOT CLEAR. ON GND MANUALLY SHUTDOWN APU. CLEANED APU OIL TEMP CONNECTOR P13 & COMPLIED WITH OPERATIONS CHECK OF APU IAW AMM 49-91-25 & 49-10-01. APU OPERATIONS CHECKED GOOD. GEN 2 WAS ON MEL, CLEARED BY OPERATIONS CHECK.

Part: LIGHT — INOPERATIVE (CABIN)

FLOOR LEVEL EMER LIGHTS ROW 2 - 5 INOPERATIVE.

Part: WARNING LIGHT — FALSE ACTIVATION (BRAKE) · airframe 38,719 hrs · 35,326 cycles

FLIGHT 3812 WHEN EXTENDING GEAR ON APPROACH, RECEIVED ANTI-SKID INBD & OTBD. WHEN GEAR UP, CAUTION GOES AWAY & WHEN PARKING BRAKE SET. PERFORMED ANTI-SKID SYS BITE TEST IAW AMM 32-44-06 & EXTENSION & RETRACTION OF GEAR IAW AMM 32-42-00, NO FAULT FOUND. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,384 hrs · 35,003 cycles

EMERGENCY LIGHTS FROM ROW 5D TO 8F INOPERATIVE WITH SWITCH IN ON POSITION. INSPECTED & FOUND EMERGENCY LIGHTS AT 5F & 8D NOT WORKING. R & R NR 3 INVERTOR IAW AMM 33-51-07. OPS CHECKED GOOD.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,275 hrs · 34,904 cycles

WHITE EMER EXIT SIGN BY SERVICE DOOR INOPERATIVE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,605 hrs · 34,241 cycles

EMERGENCY LIGHT ROWS 6 - 8 & SIDE WALL LIGHT AT ROW 8 RT INOPERATIVE.

Part: UNKNOWN — MALFUNCTIONED (COCKPIT) · airframe 37,410 hrs · 34,051 cycles

AFTER STARTING TAKEOFF ROLL ALL SCREENS, MFD, PFD, RTU, ED 1 & 2 & FMS, WENT BLACK & STARTED TO FLASH ON & OFF. DISPATCH REPORTS 120 KTS AT ABORT. BTMS READS 6456.

Part: ADG — DEPLOYED · airframe 37,409 hrs · 34,051 cycles

IMMEDIATELY AFTER ROTATION ADG AUTO DEPLOYED. FOLLOWED BY ALL CTR PEDESTAL LIGHTS, EICAS & RTU LIGHTS FLASHING ON & OFF. NO MSG'S POSTED ADG SHOWED DEPLOYED ON SYNOPTIC PAGE. LANDED AT 45K LBS.

Part: HINGE FITTING — GOUGED (LT SPOILER) · airframe 36,720 hrs · 33,388 cycles

LT FLT SPOILER CTR INBD HINGE FITTING GOUGED.

Part: COVER — CRACKED (THRUST REVERSER)

LEFT THRUST REVERSER LOWER PYLON COVER IS CRACKED.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,720 hrs · 33,388 cycles

SERVICE DOOR SILL IS CORRODED IN FWD & AFT CORNERS.

Part: SEAL — CRACKED (THRUST REVERSER) · airframe 36,720 hrs · 33,388 cycles

RIGHT THRUST REVERSER TORQUE BOX METAL SEAL CRACKED.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 36,720 hrs · 33,388 cycles

LIGHTNING PROTECTION RETAINING BRACKET IS CRACKED.

Part: SEAL — CRACKED (THRUST REVERSER) · airframe 36,720 hrs · 33,388 cycles

LT THRUST REVERSER LOWER TORQUE BOX METAL SEAL IS CRACKED.

Part: MOUNT BRACKET — CRACKED (RT WING) · airframe 36,720 hrs · 33,388 cycles

RT WING CTR LE MOUNT BRACKET IS CRACKED NEAR WS 150.

Part: SUPPORT — CRACKED (CARGO DOOR) · airframe 36,720 hrs · 33,388 cycles

CARGO BAY DOOR FWD RAIL LOWER SUPPORT HAS A CRACK PN 601R35050-25.

Part: BRACKET — CRACKED (SERVICE PANEL) · airframe 36,720 hrs · 33,388 cycles

EXTERNAL SERVICE PANEL LOWER BRACKET IS CRACKED ON FWD SIDE.

Part: SUPPORT — CRACKED (PAX DOOR) · airframe 36,720 hrs · 33,388 cycles

PAX DOOR SUPPORT STRUCTURE UNDER UPPER STEP CRACKED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 36,719 hrs · 33,388 cycles

FS 280 RBL 9 INBD & OTBD CLIPS CRACKED.

Part: DRAG ANGLE — CRACKED (LT WING) · airframe 36,719 hrs · 33,388 cycles

LEFT MLG WHEEL DRAG ANGLE COMMON TO BATTERY RIB IS CRACKED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,719 hrs · 33,388 cycles

LEFT MID NR 3 SEAT RAIL HAS CORROSION.

Part: DRAG ANGLE — CRACKED (RT WING) · airframe 36,719 hrs · 33,388 cycles

RIGHT MLG WW DRAG ANGLE COMMON TO BATTERY RIB IS CRACKED.

Part: ISOLATOR — CRACKED (FUSELAGE) · airframe 36,719 hrs · 33,388 cycles

621 BULKHEAD AT RBL 27 HAS CRACKED ISOLATOR.

Part: TIE DOWN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,719 hrs · 33,388 cycles

LEFT 9G TIE DOWN HAS CORROSION AT 559 + 96 TO 559 + 80.

Part: TIE DOWN — CORRODED (CARGO BAY) · corrosion level 2 · airframe 36,719 hrs · 33,388 cycles

LBL 9 IN CARGO BAY 2 EACH TIE DOWNS HAS CORROSION.

Part: TIE DOWN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,719 hrs · 33,388 cycles

LBL 27 AT 574 THRU 559+96 TIE DOWNS HAVE CORROSION.

Part: SUPPORT ANGLE — CRACKED (RT MLG WW) · airframe 36,720 hrs · 33,388 cycles

AFT OTBD SIDE OF RT MLG WW HAS A CRACKED SUPPORT ANGLE.

Part: HINGE FITTING — CHAFED (RUDDER) · airframe 36,720 hrs · 33,388 cycles

RUDDER HINGE FITTINGS CHAFED FROM MISSING RUDDER HAT BUSHINGS.

Part: SKIN — CHAFED (WING) · airframe 36,720 hrs · 33,388 cycles

LOWER WING PLANK CHAFED AT RBL 45, .500" X .650" X .048"D. LOWER WING PLANK CHAFED AT LBL 45, 475" X .750" X .044"D.

Part: CLEAT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,719 hrs · 33,388 cycles

FWD & AFT PAX DOOR CLEATS HAVE CORROSION.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,720 hrs · 33,388 cycles

FS 349 FLOOR SUPPORT CROSSBEAM AT PAX DOOR HAS CORROSION BETWEEN LBL 36 - LBL45.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,720 hrs · 33,388 cycles

FRAME AT FS 319 HAS CORROSION ON FWD & AFT SIDES BETWEEN STRINGER 25L & 25R.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 36,720 hrs · 33,388 cycles

PAX DOOR INTERCOSTAL CRACKED UNDER PANEL 832BR.

Part: ACTUATOR — MALFUNCTIONED (LANDING GEAR) · airframe 35,758 hrs · 32,469 cycles

UPON GEAR RETRACTION, RECEIVED THREE MESSAGES, GEAR DISAGREE W, ANTI-SKID INBD C & PARK BRAKE SOV C. COMPLIED WITH QRH, GEAR EXTENDED MANUALLY. LANDED IN PHL AT 41,000 LBS. MC MESSAGE OCCURRED 6 SECONDS AFTER GEAR HANDLE SELECTION, LT GEAR INTEGRATED PSU MEMORY FAULT CODE F34, F14 NEAR. R & R NR 1 SIDE STAY ACTUATOR, FUNCTION & LEAK CHECKED GOOD ALL MESSAGES CLEARED DURING EXT & RET IAW AMM 32-32-01.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 35,757 hrs · 32,467 cycles

UPON GEAR RETRACTION, RECEIVED ANTI-SKID INBD CAUTION, GEAR DISAGREE MESSAGE, LT MLG SHOWED DOWN & GREEN WHILE REST SHOWED UP WHITE, WITH HANDLE UP. STAB TRIM CAUTION & MACH TRIM CAUTION MESSAGES CONTINUED. RESET STAB & MACH TRIM BEFORE WE PERFORM FUNCTION TEST OF LG IAW 32-30-00 NUMEROUS TIMES. FLEXED LT MLG HARNESSES, BASED ON PSEU FAULT CODES S34 DOWN ARROW, NEAR & S19 DOWN, ARROW NEAR. CLEARED FAULT MEMORY IN PSEU IAW FIM 32-60-07 & PERFORMED LG FUNCTION TEST AGAIN. NO FAULT CODES APPEARED ON PSEU.

Part: UNKNOWN — ODOR (CABIN) · airframe 35,318 hrs · 32,037 cycles

F/A REPORTS FUEL ODOR IN ROUTE, FUEL ODOR REMAINS AFTER LANDING, APU OFF, NO LEAKS NOTED ON OUTSIDE OF ACFT. INSPECTED ACFT FOR FUEL LEAKS NO LEAKS NOTED, RAN APU AND LT AND RT PACKS IAW AMM 21-51-00. NO FUEL ODOR NOTED IN CABIN, ACFT OK FOR SERVICE.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 34,249 hrs · 30,984 cycles

FLT LEVEL 250, RECEIVED HYD NR 1 LOW PRESSURE CAUTION. COMPLIED WITH QRH HYD PUMP NR 1 B DIDN'T PROVIDE PRESSURE QTY READS DASHES. REMOVED AND REPLACED EDP 1 HYD PRESSURE LINE IAW AMM 29-11-00, LEAK CHECKS REF LP 234637/2 FOR EDP CHANGE.

Part: FLOORBEAM — CORRODED (FS 589) · airframe 31,971 hrs · 28,749 cycles

FLOORBEAM RBL 27 HAS A CORRODED NUT PLATE HOLE AT FS 589.0. REPAIRED CORRODED RBL 27 FLOORBEAM AT FS 589.0 IAW REO 601R-53-61-4555, REV.

Part: HINGE FITTING — GOUGED (LT WING TE FLAP) · airframe 31,971 hrs · 28,749 cycles

LT OTBD FLAP, OTBD HINGE ARM IS GOUGED. REPAIRED HINGE FITTING ASSY AT WS 264 IAW REO 601R-57-54-222.

Part: SILL — CORRODED (FS 310) · corrosion level 2 · airframe 31,971 hrs · 28,749 cycles

PAX DOOR CUTOUT LOWER SILL CORRODED. FABRICATED SERVICEABLE SILL AND INSTALLED SRM 51-40-11 AND 51-42-21.

Part: BULKHEAD — DENTED (FS 280) · airframe 31,971 hrs · 28,749 cycles

BS 280 BULKHEAD DENTED IN TWO PLACES ON RT AFT INBD SIDE NEAR EDGE FROM CONTACT FROM GALLEY DOOR. CUTOUT DAMAGE ON BULKHEAD AND FABRICATED, INSTALLED REPAIR IAW REO 601R-53-11-1727, REV E.

Part: SILL — CORRODED (FS 310-349) · corrosion level 3 · airframe 31,971 hrs · 28,749 cycles

PAX DOOR CUTOUT FWD AND AFT CLEATS ON LOW SILL CORRODED . R & R IAW SRM 51-4-11 & 51-42-06.

Part: DOOR FRAME — CRACKED (PAX DOORWAY) · airframe 31,971 hrs · 28,749 cycles

PAX DOOR FRAME CRACKED UNDER PANEL 832BR. R & R DOOR FRAME.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 31,971 hrs · 28,749 cycles

LEFT INBD FLAP VANE L/E CHAFED IN 2 PLACES. R & R CENTER FLAP VANE L/E BLENDED INBD CHAFE IAW REO 601R-57-52-004, REV C & SRM 51-42-13.

Part: SILL — CRACKED (FS 605) · airframe 31,971 hrs · 28,749 cycles

CARGO DOOR SILL IS CRACKED AT FS 605. CUTOUT CRACKED AREA AND INSTALLED PLUG RIVET IAW REO 601R-53-61-433 ALODINED, PRIMED AND TOP COATED IAW SRM 51-21-11, 51-25-06 & 51-25-16.

Part: ATTACH FITTING — CRACKED (FS 484) · airframe 31,971 hrs · 28,749 cycles

FS 484 CLIP AT LBL27 CRACKED. R & R CRACKED CLIP AT FS 484.00 IAW SRM 53-41-43, REO 601R-53-41-059.

Part: BULKHEAD — DENTED (FS 621) · airframe 31,971 hrs · 28,749 cycles

REPAIR BULKHEAD AT WL 76.5, LBL 13.80, 601R-53-61-4481. REPAIR BULKHEAD COMPLIED WITH CARD DMI16232 AT WL 76.5, LBL 13.80, 601R-53-61-4481. FABRICATED AND INSTALLED FILLER, SHIM AND DOUBLER IAW REO 601R-53-61-4526.

Part: BULKHEAD — DENTED (FS 621) · airframe 31,971 hrs · 28,749 cycles

BULKHEAD FWD FACE WL 103.43, DENTED. REPAIRED BULKHEAD IAW REO 601R-53-61-1285, REV D.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 31,971 hrs · 28,749 cycles

CARGO COMPARTMENT TIE DOWN TRACKS FS 559.00+96, RBL9 & LBL9 AND LBL27 HAVE CORROSION. R & R RBL9 & LBL9 TIE DOWN TRACKS DUE TO HEAVY CORROSION. PN N126-1075 IAW CRJ 200 51-40-11, AMM 53-01-11. REMOVED CORROSION LBL 27, 559.00+96 IAW SRM 51-21-06, 51-12-00. FOUND TO BE SERVICEABLE LIMITS.

Part: ANGLE — CRACKED (FS 280) · airframe 31,971 hrs · 28,749 cycles

ANGLE AT LBL 9 CRACKED. REMOVED UNSERVICEABLE ANGLE & REPLACED WITH NEW SERVICEABLE ANGLE IAW SRM 51-42-21.

Part: ANGLE — CRACKED (FS 589 S18L) · airframe 31,971 hrs · 28,749 cycles

FRAME ANGLE UNDER CARGO DOOR SILL AT FS 589.0 LT IS CRACKED. R & R ANGLE IAW SRM 51-42-13 & 51-40-11.

Part: HANDLE — DAMAGED (PAX DOOR) · airframe 31,639 hrs · 28,409 cycles

RECEIVED A PAX DOOR OUTER HANDLE MESSAGE IN FLIGHT. COMPLIED WITH QRH, MESSAGE TURNED RED OR CHANGED TO WARNING AFTER F/A PULLED INNER HANDLE, IT REMAINED RED REMAINDER OF FLT. VERIFIED THAT PAX DOOR INNER HANDLE WILL NOT STOW OUTER PAX DOOR HANDLE.

Part: WIRE HARNESS — INOPERATIVE (DOOR WARNING) · airframe 31,605 hrs · 28,377 cycles

PAX DOOR OUTER HANDLE CAUTION MESSAGE IN FLIGHT. R & R OF THE CARGO DOOR WIRING HARNESS.

Part: OVERHEAT LOOP — DAMAGED · airframe 31,557 hrs · 28,329 cycles

LEFT 14TH DUCT WARNING MESSAGE AT 11,000 FT. OPENED UP LT PYLON, PERFORMED LEAK CHECKED GOOD. INSPECTED 14TH STAGE LOOP. R & R LT PYLON LOOP TEST GOOD. COMPLETED FULL POWER RUNS, NO DEFECTS NOTED.

Part: THERMOCOUPLE — FAILED (LT ITT) · airframe 31,536 hrs · 28,304 cycles

AFTER TAKE OFF, LEFT ENGINE ITT SPIKED INTO RED RANGE & HOT ICON SHOWED ON GAGE, THREE TIMES WITHIN 9.5 MI PERIOD. ITT INDICATOR RETURNED TO GREEN BUT WITH HOT ICON DISPLALYED. ALL OTHER ENGINE PARAMETER NORMAL. R & R ITT THERMOCOUPLE ASSY. OPS CHECKED GOOD.

Part: HOUSING — DAMAGED (POWER RECEPTICAL) · airframe 29,268 hrs · 25,931 cycles

DAMAGE TO POWER RECEPTACLE (A/C) HOUSING AND STRUCTURE ASSY. REPAIR IAW REO 601R-53-11-2081.

Part: COALESCER BAG — ODOR · airframe 28,517 hrs · 25,134 cycles

AFTER STARTING ENGINES, CABIN AND COCKPIT WAS ENGULFED WITH THE ODOR OF OIL. R & R LT PACK COALSER BAG, RAN BOTH APU AND ENG AIR NO OIL SMELL NOTED.

Part: SILL — CORRODED (BS 559) · corrosion level 2 · airframe 27,723 hrs · 24,314 cycles

SILL RT 601R31133, REPAIRED DAMAGED AREA OF CORROSION IAW REO 601R-53-51-123.

Part: SKIN — GOUGED (VERTICAL STAB) · airframe 27,723 hrs · 24,314 cycles

PANEL 326CR OUTER SKIN HAS NUMEROUS GOUGES, DEEPEST GOUGE .017". BLENDED GOUGES IAW REO 601R-55-32-267.

Part: SKIN — CHAFED (BS 538.7) · airframe 27,723 hrs · 24,314 cycles

RT FUSELAGE IS CHAFED BETWEEN WING AND FUSELAGE NEAR WING T/E. REPAIRED CHAFED AREA BETWEEN WING AND FUSELAGE NEAR WING T/E IAW REO 601R-53-41-1250.

Part: SILL — CORRODED (BS 310) · airframe 27,723 hrs · 24,314 cycles

CORROSION ON SERVICE DOOR SILL PLATE. R & R SILL PLATE.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 27,723 hrs · 24,314 cycles

FS 280.00 FLOOR SUPPORT CRACKED LBL 11 AND RBL 9 APPROX. R & R FLOOR SUPPORT AT FS 280.00 BETWEEN LBL 11 AND RBL9 IAW REO 601R-53-11-136.

Part: FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 27,723 hrs · 24,314 cycles

RT OTBD FLAP ALIGNMENT FITTING IS CHAFED WITH CORROSION. REPAIR CHAFING DAMAGE ON RT OTBD FLAP ALIGNMENT FITTING IAW REO 601R-57-53-812, DATED 06/26/2010. POST BLENDING INSPECTION SHOW NO EVIDENCE OF CORROSION.

Part: SKIN — GOUGED (PAX DOOR) · airframe 27,723 hrs · 24,314 cycles

PAX DOOR INNER SKIN IS COUGED NEXT TO PANEL 832BR, RIVET NEXT TO SKIN DAMAGE IS ALSO GOUGED INCORPORATED REO 601R-52-11-1829.

Part: STRUCTURE — CRACKED (THRUST REVERSER) · airframe 27,723 hrs · 24,314 cycles

RT ENG THRUST REVERSER 12 O`CLOCK POSITION CASCADE CRACKED AT 3 LOCATIONS. REPLACED 12 O`CLOCK POSITION CASCADE ON RT ENG IAW AMM78-33-01.

Part: DOOR FRAME — CRACKED (BS 338) · airframe 27,723 hrs · 24,314 cycles

PAX DOOR FRAME CRACKED AT FS 338 APPROX 6 INCHES BELOW LATCH CAM TORQUE TUBE. REPAIRED DAMAGE BY INCORPORATING REO 601R-52-11-402, REV G.

Part: STRUCTURE — CORRODED (PAX DOOR) · airframe 27,723 hrs · 24,314 cycles

PAX DOOR AFT LOWER CORNER CORRODED. R & R CORNER IAW SRM 51-42-06 AND 51-42-13.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 27,723 hrs · 24,314 cycles

PAX DOOR FWD LOWER CORNER DENTED AND CRACKED AT DENT. R & R PAX DOOR FWD LOWER CORNER IAW SRM 51-42-06 AND 51-42-13.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 27,723 hrs · 24,614 cycles

NR 2 LT FLOOR SEAT TRACK HAS CORROSION. R & R NR 2 LT SEAT TRACK IAW AMM 53-01-11.

Part: CARGO TRACK — CORRODED (BS 559-574) · corrosion level 2 · airframe 27,723 hrs · 24,314 cycles

RT OTBD 9G FLOOR TRACK CORRODED IN CARGO BAY. R & R RT OTBD 9G FLOOR TRACK IAW AMM 53-01-11.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 27,723 hrs · 24,314 cycles

CARGO BAY FLOOR TRACKS CORRODED NEXT TO FLOOR PANELS 281DLF, 282 FRF, 281 GLF. R & R IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 27,723 hrs · 24,314 cycles

NR 4 LT SEAT TRACK HAS CORROSION. R & R NR 4 LT SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 27,723 hrs · 24,314 cycles

NR 3 LEFT FLOOR SEAT TRACK HAS CORROSION. R & R IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 27,723 hrs · 24,314 cycles

NR 3 RT SEAT TRACK HAS CORROSION, R & R IAW AMM 53-01-11..

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 27,723 hrs · 24,314 cycles

NR 1 LT FLOOR SEAT TRACK CORRODED. R & R SEAT TRACK IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.

Part: PRESSURE BLKHD — CHAFED (BS 621) · airframe 27,723 hrs · 24,314 cycles

MINOR CHAFING IN 4 EA LOCATIONS ON THE FWD FACE OF THE 621 BULKHEAD REPAIR DAMAGE MINOR CHAFING 4 EA LOCATIONS ON FWD FACE FS 621.00 BULKHEAD IAW SRM 53-00-31.

Part: STRUCTURE — CORRODED (PAX DOOR) · corrosion level 1 · airframe 27,723 hrs · 24,314 cycles

CLIP AT FS 329.5 ON LOWER SIDE OF PAX DOOR CORRODED. R & R CLIP IAW SRM 51-42-06 AND 51-42-21.

Part: SUPPORT ANGLE — CRACKED (PAX DOOR) · airframe 27,723 hrs · 24,314 cycles

PAX DOOR LATCH CAM TORQUE TUBE ACCESS PANEL SUPPORT ANGLE FWD AND AFT ARE CRACKED. REMOVED, DUPLICATED AND INSTALLED REPLACEMENT SUPPORT ANGLES IAW SRM 51-40-11, 51-25-16, 51-25-06, 51-21-11, AMM 52-70-07.

Part: FAIRING — CHAFED (RT WING TE FLAP) · airframe 27,723 hrs · 24,314 cycles

RT FLAP STUB FAIRING CHAFE REPLACED UNSERVICEABLE RT FLAP STUB FAIRING FOR SERVICEABLE RT FLAP STUB FAIRING PN 601R31199-92 IAW SRM 51-42-06.

Part: BLOCKER DOOR — CHAFED (THRUST REVERSER) · airframe 27,723 hrs · 24,314 cycles

LT ENG T/R BLOCKER DOOR 1 THRU 5 HAVE CHAFE DAMAGE AT STOPS. REPAIRED LT ENG T/R BLOCKER DOORS 1 THRU 5 AT STOPS IAW CMM 78-30-00-300-8720-A. REPAIR NO SRS.

Part: FLOOR SKIN — GOUGED (BS 495-496) · airframe 27,723 hrs · 24,314 cycles

PRESSURE FLOOR SKIN HAS 3 EA MINOR GOUGES IN SKIN JUST FWD OF FUEL LINE CUT OUT. REPAIRED PRESSURE FLOOR SKIN JUST FWD OF FUEL LINE CUT OUT IAW B/A REO 601R-53-41-1247 REV ORIGINAL.

Part: STRUCTURE — CORRODED (PAX DOOR) · corrosion level 1 · airframe 27,723 hrs · 24,318 cycles

CLIP AT FS 338 AFT SIDE OF THE PAX DOOR IS CORRODED. R & R CLIP IAW SRM 51-42-06 AND 51-42-21.

Part: STRUCTURE — CORRODED (PAX DOOR) · corrosion level 1 · airframe 27,723 hrs · 24,314 cycles

CLIP AT FS 338 FWD SIDE OF PAX DOOR IS CORRODED. R & R CLIP IAW SRM 51-42-06 AND 51-42-21.

Part: SEAT TRACK — CORRODED (BS 364) · corrosion level 2 · airframe 27,723 hrs · 24,314 cycles

RT NR1 FLOOR SEAT TRACK CORRODED. R & R IAW AMM 53-01-11.

Part: STRUCTURE — CORRODED (PAX DOOR) · corrosion level 1 · airframe 27,723 hrs · 24,314 cycles

CLIP ON LOWER FWD SIDE OF FRAME FS 320.10 ON PAX DOOR CORRODED. R & R CLIP IAW SRM 51-42-02 AND 51-42-21.

Part: STRUCTURE — CORRODED (PAX DOOR) · corrosion level 1 · airframe 27,723 hrs · 24,314 cycles

CLIP ON LOWER AFT SIDE OF FRAME FS 320.10 ON PAX DOOR CORRODED. R & R CLIP IAW SRM 51-42-06 AND 51-42-21.

Part: BLOCKER DOOR — CHAFED (THRUST REVERSER) · airframe 27,723 hrs · 24,314 cycles

LT ENGINE T/R BLOCKER DOORS 6 THRU 10 CHAFED AT STOPS. REPAIRED LT ENG T/R BLOCKER DOORS 6 THRU 10 AT STOPS IAW B/A CMM 78-30-300-820-A01, REPAIR NR SRS100.

Part: PRESSURE BLKHD — CRACKED (BS 202.75) · airframe 27,723 hrs · 24,314 cycles

PRESSURE BULKHEAD CRACKE AT PARKING BRAKE CABLE MOUN. REMOVED DAMAGE, INSTALLED DOUBLER IAW REO 601R-53-11-563.

Part: ATTACH BRACKET — CRACKED (LT WING) · airframe 27,723 hrs · 24,314 cycles

L/E ATTACH BRACKET UNDER PNL 520ML IS CRACKED. REMOVED UNSERVICEABLE BRACKET AND REPLACED SERVICEABLE BRACKET PN 600-12045-11 ON L/E UNDER PNL 520MC OTBD IAW SRM 51-42-02.

Part: BRACKET — CRACKED (HYD LINE) · airframe 27,723 hrs · 24,314 cycles

NR 2 HYD MANIFOLD BRACKET CRACKED. R & R IAW SRM 51-42-06, 51-42-13.

Part: RIB — CRACKED (LT WING) · airframe 27,723 hrs · 24,314 cycles

BATT RIB IN LT MLG WW IS CRACKED, 601R107091-REF. REPAIRED CRACKED BATT RIB IAW REO 601R-57-51-046, REV B, REPAIR NR 2.

Part: PDU — MALFUNCTIONED (THRUST REVERSER) · airframe 26,868 hrs · 23,434 cycles

RT REVERSER UNLOCK MESSAGE CAME ON OUT OF 13000 FT. FOLLOWED QRH. RETURNED TO DEPARTURE. MESSAGE EXTINGUISHED AT SHUTDOWN. "MEL. COMPLIED WITH MX ACTION H OF DEACTIVATION OF RT THRUST REVERSER REF AMM 78-30-00-040-802, REF BLK 2 FOR MEL. R & R RT ENGINE PDU RIG CHECK OPS CKD OK WITH SHOP AIR.

Part: POST — CRACKED (BS 409) · airframe 26,416 hrs · 22,962 cycles

CRACK FOUND ON VERTICAL POST FS 409.00 + 128, RBL 18.00 OTBD POST REO 601R-53-41-056 REV E. PERFORM ON VERTICAL POST AT FS 409 + 128, RBL 18. (K)

Part: POST — CRACKED (BS 409) · airframe 26,416 hrs · 22,962 cycles

CRACK FOUND ON VERTICAL POST FS 409.00 + 128, LBL 18.00 OTBD POST REO 601R-53-41-056 REV E. PERFORM ON VERTICAL POST AT FS 409+ 128, LBL 18.00. (K)

Part: BULKHEAD — CRACKED (BS 559) · airframe 26,416 hrs · 22,962 cycles

CRACK ON PRESSURE BULKHEAD LOCATED AROUND CONNECTOR J6CA HOLE BTW RBL 18.00 AND RBL 27.00 (.900" LONG). CRACK ON F/S 559.00 BTW RBL 18.00 AND RBL 27.00 ON CONNECTOR J6CA HOLE REPAIRED IAW REO 601R-53-41-1108.

Part: STRUCTURE — CRACKED (BS 559 BULKHEAD) · airframe 26,416 hrs · 22,962 cycles

PRESSURE BULKHEAD CAP ANGLE CRACK AT FS 559.00, RBL 9.0 AND RBL 18.0. REPAIR PERFORMED ON PRESSURE BULKHEAD CAP ANGLE AND WEB IAW REO 601R-53-41-260 REV D AND CRJ 200 REO 601R-53-41-609, REV A (DEVIATION E). (K)

Part: ANGLE — CRACKED (BS 559 BULKHEAD) · airframe 26,416 hrs · 22,962 cycles

PRESSURE BULKHEAD CAP ANGLE CRACKED AT FS 559.00 AT LBL 18.00. REPAIR PERFORMED ON PRESSURE BULKHEAD CAP ANGLE AT FS 559.00, LBL 18.00 IAW GREO 601R-53-41-260, REV D. (K)

Part: ISOLATION VALVE — MALFUNCTIONED · airframe 26,348 hrs · 22,899 cycles

ISOLATION VALVE WOULD NOT OPERATE IN FLIGHT, RESULTED IN UNPRESSURIZED LANDING. REMOVED AND REPLACED ISOLATION VALVE IAW AMM 36-11-07. OPS CHECK GOOD. (K)

Part: HANDLE — LACK OF LUBE (PAX DOOR) · airframe 26,326 hrs · 22,878 cycles

PAX DOOR OUTER HANDLE DIFFICULT TO STOW FROM INSIDE. LUBED PAX DOOR OUTER HANDLE GREASE FITTING IAW AMM 12-20-52. OPS CK GOOD. (K)

Part: DOOR — UNKNOWN (MAIN PAX) · airframe 26,138 hrs · 22,703 cycles

MAIN PASSENGER DOOR WILL NOT LATCH CLOSED FROM INSIDE AND WILL NOT OPEN FROM OUTSIDE. PERFORMED PAX DOOR OPS CK NUMEROUS TIMES, FOUND TO BE OPERATING NORMAL IAW AMM 52-11-00. (K)

Part: PROXIMITY SWITCH — OUT OF ADJUST (PAX DOOR) · airframe 25,335 hrs · 21,938 cycles

190515/1 PASSENGER DOOR OUTER HANDLE CAUTION MESSAGE ON INFLIGHT. PAX DOOR WILL NOT OPEN FROM OUTSIDE. DOOR CLOSES, LATCHES, AND LOCKS. PLACARDED AND PLACED ON MEL. REF W/O 138471 FOR MX PERFORMED, PAX DOOR OPENS AND CLOSES AND INDICATION OK FROM INSIDE AND OUTSIDE OF ACFT IAW AMM 52-10. 190527/4 ADJUST PAX DOOR HANDLE PROX SWITCH PS2MB FOR AMM 52-70-04. OPS CHECK GOOD INDICATION. REMOVED FROM MEL PLACARD REMOVED. (K)

Part: STRUT — DISCHARGED (NLG) · airframe 24,524 hrs · 21,146 cycles

GEAR DISAGREE WARNING AFTER GEAR SELECTED UP AFTER TAKEOFF FOLLOWED QRH. AIR RETURN DUE TO MKE INDICATED RED X-MARKS 10 SECONDS AFTER GEAR RETRACTION. FOUND NLG OLEO STRUT LOW REF SUPP 08-067 SERVICED NLG SHOCK STRUT WITH OIL AND NITROGEN PER AMM 12-12-32 TR 12-122. OPS TEST LNDG GEAR EXTENSION REF GOOD PER AMM 32-30-00.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 24,311 hrs · 20,946 cycles

LOG 189664/2 ON CLIMBOUT RECEIVED PAX DOOR LATCH CAUTION AND PAX DOOR WARNING MSGS. COMPLIED WITH QRH. DURING DESCENT WARNING MSG CLEARED YET CAUTION REMAINED. AFTER LANDING ALL MSGS CLEARED AND DOOR INDICATES NORMAL. PSI NORMAL. INTERROGATED PSEU AND FOUND S46 AND S47 DOOR CAM 1/2 CODES STORED. OPERATED PAX DOOR AND VERIFIED DOOR CAMS OPERATE NORMAL AND WITNESS MARKS ALIGNED. NO MSG DISPLAYED AT THIS TIME. DOOR INDICATES NORMAL.

Part: HYDRAULIC SYSTEM — LEAKING (NR 2) · airframe 24,032 hrs

SHORTLY AFTER TAKEOFF, EICAS NR 2 HYDRA LOW PRESSURE, NR 2 HYDRAULIC QUANTITY 5 PERCENT. COMPLIED WITH QRH, RETURNED TO LAND. FLUID DRIPPING FROM AFT EQUIPMENT BAY. OPERATED 35 MINUTES AT 5 PERCENT INDICATED. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,261 hrs · 19,941 cycles

CORROSION FOUND ON FLOOR STRUCTURE FS 574 TO 605 LBL 27. FLOORBEAM REPLACED IAW SRM 51-42-06, SRM 51-42-21, SRM 51-42-36. (A)

Part: ANGLE — CRACKED (RT PYLON) · airframe 23,261 hrs · 19,941 cycles

ANGLE CRACKED ON RT PYLON ACCESS PANEL 422 BT. ANGLE REPLACED IAW SRM 51-42-06. (A)

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 23,261 hrs · 19,941 cycles

CRACK ON FLOORBEAM ANGLE FS 621 LBL 40. CRACK ON FLOOR SUPPORT ANGLE AT FS 621 LBL 40 REPAIRED IAW REO 601R-53-61-117 REV C. (A)

Part: WEB — CRACKED (FUSELAGE) · airframe 23,261 hrs · 19,941 cycles

CRACK EXIST ON FLOOR WEB FS 280 LBL 9. REWORK PERFORMED IAW REO 601R-53-11-1402. (A)

Part: PANEL — CRACKED (PAX DOOR) · airframe 232,611 hrs · 19,941 cycles

REPAIR CRACKS IN PASSENGER DOOR PANELS. CRACKS ON PASSENGER DOOR PANELS REPAIRED IAW CRJ 200 REO 601R-52-11-279. (A)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 23,261 hrs · 19,941 cycles

CRACK FOUND ON INTERCOSTAL FS 484 RBL 27 AND RBL 36. DAMAGE REMOVED NEW ANGLE FABRICATED, HFEC PERFORMED AND FABRICATED ANGLE INSTALLED IAW REO 601R53-41-059 REV A AT FS 484 RBL 27 NEW ANGLE INSTALLED IAW REO 601R-53-41-059 REV A. (A)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 23,261 hrs · 19,941 cycles

CRACK FOUND ON INTERCOSTAL FS 484 LBL 27 AND LBL 36. DAMAGE REMOVED, NEW ANGLE FABRICATED, HFEC PERFORMED AND FABRICATED ANGLE INSTALLED IAW REO 601R-53-41-059 REV A. AT FS 484 LBL 27 NEW ANGLE INSTALLED IAW REO 601R-53-41-059 REV A. (A)

Part: PRESSURE PANEL — CORRODED (BS 449-529) · corrosion level 1 · airframe 23,261 hrs · 19,941 cycles

CORROSION ON PRESSURE FLOOR WEB FS 449 TO FS 529 LBL 45. CORROSION BLENDED IAW CRJ 200 SRM 51-21-06. (A)

Part: PRESSURE PANEL — CORRODED (BS 449-529) · corrosion level 1 · airframe 23,261 hrs · 19,941 cycles

CORROSION FOUND ON PRESSURE FLOOR WEB FS 449 TO FS 529 RBL 45. CORROSION ON PRESSURE FLOOR WEB FS 449 TO FS 529 RBL 45 BLENDED IAW CRJ 200 SRM 51-21-06. (A)

Part: SILL — CORRODED (FUSELAGE) · airframe 23,261 hrs · 19,941 cycles

CORROSION FOUND ON PAX DOOR LOWER SILL FS 315 AND FS 344 LBL 43. CORROSION REMOVED IAW SRM 51-21-06. (A)

Part: FLOORBEAM — CRACKED (BS 589) · airframe 23,261 hrs · 19,941 cycles

CRACK FOUND ON FLOOR LANDING PLATES FS 589 LBL 45. FLOOR LANDING PLATES FS 589 LBL 45 REPAIRED IAW CRJ 200 REO 601R-53-61-433. (A)

Part: FLOOR PANEL — CRACKED (BS 280) · airframe 23,261 hrs · 19,941 cycles

CRACK FOUND ON FLOOR WEB FS 280 RBL 9. FLOOR WEB AT FS 280 RBL 0 REPAIRED IAW CRJ 200 REO 601R-53-11-171 REV D SCHEME B. (A)

Part: SKIN — CORRODED (SERVICE DOOR) · airframe 23,261 hrs · 19,941 cycles

CORROSION ON SKIN AROUND SCREW HOLES UNDER PROTECTIVE PLATE OF SERVICE DOOR. CORROSION ON SKIN AROUND SCREW HOLES REMOVED IAW SRM 51-41-06. (A)

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,261 hrs · 19,941 cycles

SERVICE DOOR LOWER SILL PLATE ASSY CORRODED. SERVICE DOOR LOWER SILL PLATE REMOVED AND REPLACED IAW SRM 51-41-02 AND 51-41-04. (A)

Part: SKIN — DENTED (AIRSTAIR DOOR) · airframe 23,261 hrs · 19,941 cycles

REPAIR DENTS IN AIRSTAIR DOOR UPPER FWD CORNER COVER AND UPPER AFT CORNER COVER. REPAIRED IAW REO 601R-52-11-827. FWD UPPER CORNER COVER REPLACED IAW SRM 51-42-13. (A)

Part: WARNING MESSAGE — ILLUMINATED (STAB TRIM) · airframe 22,818 hrs · 19,499 cycles

STAB TRIM CHANNEL 1 STATUS MESSAGE IN FLIGHT, COMPLIED WITH QRH AND MESSAGE DID NOT CLEAR. (M)

Part: CONTROL PANEL — MALFUNCTIONED (RUDDER TRIM) · airframe 22,859 hrs · 19,540 cycles

RUDDER TRIM STICKS IN RIGHT RUDDER. RUDDER TRIM IS CENTERED. REMOVED AND REPLACED RUDDER TRIM PANEL, OPS CHECK OK PER AMM 27-20. (M)

Part: WARNING MESSAGE — ILLUMINATED · airframe 22,047 hrs · 18,774 cycles

FLAP FAIL CAUTION MESSAGE IN FLIGHT AT FLT LEVEL 260 AND FLAPS AT 0. COMPLIED WITH QRH. COMPLIED WITH RESET PROCEDURE IAW AWAC SUPP 98-018B STEPS 1.3 AND 1.4, FLAP SYSTEM RESET OK. (M)

Part: COMPUTER — MALFUNCTIONED (FLT CONTROL)

RUDDER FLUTTER IN FLIGHT AT 290 KNOTS, CAUSING LIGHT AIRFRAME VIBRATION, FLUTTER REDUCED WITH REDUCED AIRSPEED TO 250 KNOTS, FLUTTER REDUCED WITH RUDDER PEDAL PRESSURE. REMOVED AND REPLACED FLIGHT CONTROL COMPUTER (FCC) NR 2 IAW MM 22-12-14, OPS CHECK OK. (M)

Part: FRAME — DAMAGED (FUSELAGE)

WHILE REMOVING TOP CENTER SKIN AT FS 169-202.75 UNDERLYING FRAME WAS DAMAGED BY DRILL BIT. MAINTENANCE PERFORMED MAJOR REPAIR TO FRAME IAW BSC EO 601R-53-10389. (M)

Part: ATTACH ANGLE — CRACKED (RT WING LE)

RIGHT WING LEADING EDGE SPAR ATTACH ANGLE FOR THE INBOARD END OF THE MIDDLE LEADING EDGE SECTION IS CRACKED AT UPPER CORNER .5 INCH LONG, P/N 600-12045-12. MAINTENANCE REMOVED AND REPLACED ATTACH ANGLE FOR THE INBOARD END OF THE MIDDLE LEADING EDGE SECTION IAW CRJ 200 SRM 51-41-02. (M)

Part: ATTACH ANGLE — CRACKED (LT WING)

FOUND LEFT WING LEADING EDGE SPAR ATTACH ANGLE FOR THE INBOARD END OF THE MIDDLE LEADING EDGE SECTION IS CRACKED UPPER CORNER .5 INCH LONG, P/N 600-12045-11. MAINTENANCE REMOVED AND REPLACED ATTACH ANGLE FOR THE INBOARD END OF THE MIDDLE LEADING EDGE SECTION IAW CRJ 200 SRM 51-41-02. (M)

Part: ATTACH FITTING — CRACKED (FUSELAGE)

FOUND RIGHT FS 280.00 AT RBL 9 INBOARD CLIP IS CRACKED AT UPPER RADIUS .25 INCH LONG. MAINTENANCE REPLACED CLIP P/N 601R31113-58 IAW BSC S/R 601R-53-0057A, CRJ 200 SRM 51-42-06 AND SRM 51-42-21. (M)

Part: SPRING — OUT OF ADJUST (PAX DOOR)

REQUEST INSPECTION OF PASSENGERS DOOR OPERATION DUE TO DOOR INTERMITTENT OPERATION OPENING DOOR FROM OUTSIDE. LUBRICATED DOOR SHUT BOLTS AND CAMS, PERFORMED COUNTER BALANCE ADJUSTMENT OF REAR COUNTER SPRING, PERFORMED OPS CHECK OF PASSENGER DOOR, FORCE TEST OF HANDLE IAW CRJ AMM 51-22-00, WITHIN LIMITS. (M)

Part: SKIN — CORRODED (LT WING)

LT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT AT HOLE NR 5, PANEL 540CB HAS MINOR PITTING CORROSION. MAINTENANCE REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV D. (M)

Part: SKIN — CORRODED (RT WING)

FOUND RT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT AT HOLE NR 4, PANEL 640AB HAS MINOR PITTING CORROSION. MAINTENANCE REPAIRED IAW BOMBARDIER REO 601R-57-21-030. (M)

Part: SKIN — CORRODED (LT WING)

FOUND LT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT AT HOLE NR 8, PANEL 540FB HAS MINOR PITTING CORROSION. MAINTENANCE REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV D. (M)

Part: SKIN — CORRODED (LT WING)

FOUND LT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT AT HOLE NR 2, PANEL 510AB HAS MINOR PITTING CORROSION. MAINTENANCE REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV D. (M)

Part: ACCESS DOOR — CORRODED (RT WING)

FOUND RT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT AT HOLE NR 11, PANEL 650CB HAS MINOR PITTING CORROSION. MAINTENANCE REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV D. (M)

Part: SKIN — CORRODED (RT WING)

RIGHT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT AT HOLE NR 1, PANEL 640BB HAS MINOR PITTING CORROSION. MAINTENANCE REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV D. (M)

Part: SKIN — CORRODED (RT WING)

FOUND RT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT AT HOLE NR 9, PANEL 650AB HAS MINOR PITTING CORROSION. MAINTENANCE REPAIRED IAW BOMBARDIER REO 601R-57-21-030. (M)

Part: ACCESS DOOR — CORRODED (LT WING)

FOUND LT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT AT HOLE NR 1, PANEL 510BB HAS MINOR PITTING CORROSION. MAINTENANCE REPAIRED IAW BOMBARDIER, INC REO 601R-57-21-030 REV D. (M)

Part: SKIN — CORRODED (RT WING)

FOUND RT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT AT HOLE NR 8 PANEL 640FB HAS MINOR PITTING CORROSION. MAINTENANCE REPAIRED IAW BOMBARDIER REO 601R-57-21-030. (M)

Part: LINE — LOOSE (AC SYS) · airframe 17,673 hrs · 14,518 cycles

RT PACK HI PRESS MSG ON TAKEOFF- ABORTED TAKEOFF AT 20 KNOTS. AFTER CLEARING RUNWAY COMPLIED WITH QRH. PACK RESET NORMAL BTMS SHOWS 2,1,1,3 ALL IN GREEN. FOUND LOOSE LIINE ON RT ACM, SECURED LINE, RT PACK PRESSURE NORMAL. OPERATIONAL CHECK WITH APU GOOD IAW AMM. (K)

Part: PROXIMITY SENSOR — INOPERATIVE (NOSE WW) · airframe 17,659 hrs · 14,508 cycles

PROX SYS CHANNEL CAUTION MESSAGE INFLIGHT CREW RAN QRH, INCLUDING MANUAL GEAR EXTENSION AND LANDING WITHOUT NOSEWHEEL STEERING. REMOVED AND REPLACED PSEU REF AMM. OPS CHECK GOOD PERFORMED GEAR EXTENSION AND RETRACTION WITH NO DEFECTS NOTED AT THIS TIME. (K)

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY)

SMOKE TOILET MESSAGE ON GROUND WITH AURAL WARNING WHILE WAITING FOR GATE. NO SIGN OF FIRE OR SMOKE. RAN PACK AT FULL HOT, TESTED LAV SMOKE/TOILET DETECTION, OPS CHECK OK. COULD NOT DUPLICATE. OK FOR SERVICE. (M)

Part: CONNECTOR — LOOSE (SMOKE DETECTOR) · airframe 16,671 hrs · 13,516 cycles

(SMOKE TOILET) MESSAGE WITH AUDIBLE ALARM. NO SMOKE NOTED. LASTED FOR 2 MINUTES. COMPLIED WITH QRH. RESECURED CONNECTOR PLUG TO SMOKE DETECTOR (THAT WAS FOUND LOOSE), OPS CHECK GOOD IAW AMM. (K)

Part: IDG — FAILED (NR 1 ENGINE) · airframe 16,404 hrs · 13,252 cycles

IDG NR 1 CAUTION MESSAGE ON TAKEOFF ROLL, ABORTED TAKEOFF, IDG MESSAGE EXTINGUISHED AND REPLACED WITH GEN NR1 OFF CAUTION MESSAGE. FOLLOWED QRH, MESSAGE CLEARED ALL. ABORTED TAKEOFF AT 40 KNOTS. REMOVED AND REPLACED IDG NR 1, OP CHECK AND LEAK CHECK GOOD. (K)

Part: ENGINE — FLAMED OUT (RIGHT)

RIGHT ENGINE FLAMED OUT ON LANDING ROLL, WHILE ATTEMPTING TO USE REVERSE THRUST. CHECKED RIGGING, ADJUSTED TO TOP OF LIMITS, CHECKED ATR, RIGGED, SET IDLE SPEED, PERFORMED POWER ASSURANCE ATR, N1 DISABLE TO ACCEL/DECEL IAW CRJ AMM CHP 71, 76, 78. (M)

Part: STRUT — LACK OF LUBE (NLG) · airframe 15,074 hrs · 12,127 cycles

GEAR DISAGREE UPON GEAR RETRACTION COMPLIED WITH. SERVICED NOSE STRUT WITH OIL AND NITROGEN IAW AMM. IAW AMM GEAR SWING, OPS CHECK GOOD IAW 32-30-00.

Part: APU — LEAKING (APU BAY) · airframe 14,957 hrs · 12,020 cycles

OIL SMELL COMING FROM BOTH PACKS. TROUBLESHOOTING AND FOUND APU LEAKING OIL. REPLACED BOTH COALESCER BAGS. RAN ENGINE. NO SMELL NOTED.

Part: SUPPORT CHANNEL — CRACKED (FUSELAGE) · airframe 14,510 hrs · 11,660 cycles

MWC 189, CARGO DOOR FORWARD TACK SUPPORT CHANNEL IS CRACKED. REMOVED CRACKED SUPPORT CHANNEL AND INSTALLED NEW SUPPORT CHANNEL IAW SRM 51-42-06.

Part: CHANNEL — CRACKED (FUSELAGE)

FOUND CARGO DOOR, FORWARD TRACK SUPPORT CHANNEL IS CRACKED. REMOVED CRACKED SUPPORT CHANNEL AND INSTALLED NEW SUPPORT CHANNEL IAW CRJ SRM 51-42-06. (M)

Part: COAX — FAILED (RADAR ALTIMETER)

RADAR ALT ERRONEOUS INDICATIONS ON CLIMB TOO LOW TERRAIN AND PULL-UP SOUNDED INTERMITTENT. GLD UNSAFE AMBER CASS, COMPLIED WITH QRH. REPLACED RAD ALT TRANSMIT AND RECEIVE COAX CABLES. SYSTEM CHECKED GOOD.

Part: ODOR — DETECTED (CABIN)

FLIGHT ATTENDANT REPORTING GASSY FUMES IN VICINITY OF GALLEY, IRRITATING TO NOSE, THROAT AND EYES. INSPECTED INTERNAL/EXTERNAL OF AIRCRAFT, NO EVIDENCE OF UNUSUAL SMELL. APU AND PASSENGER OPS NORMALLY. REVIEWED AIRCRAFT HISTORY. NO RECORD OF SMOKE. (M)

Part: BRACKET — BENT (NLG)

ON TAKEOFF, GEAR HANDLE UP NOSE GEAR UNSAFE AND GEAR DOOR OPEN WARNING MESSAGE. REMOVED AND REPLACED OLEO CENTER/PROXIMITY CENTER BRACKET. GEAR SWING OPS CHECK GOOD IAW AMM. (M)

Part: CLIP — CRACKED (FUSELAGE)

CLIP IS CRACKED. REPAIRS ACCOMPLISHED BY FABRICATON OF REPLACEMENT ANGLE. WORK ACCOMPLISHED IAW FAA 81103 PER WVAC EO 601R-53-4403. (M)

Part: ANGLE — CRACKED (FUSELAGE)

FOUND FS 621 ANGLE ON LEFT SIDE OF CARGO BAY IS CRACKED .25 INCH, INCORPORATED CANADAIR REO 601R-53-61-004 REV B. (M)

Part: SEAL — DAMAGED (PAX DOOR)

PASSENGER DOOR SEAL STRINGER AT FS 349, 18 INCHES ABOVE STRINGER 18 IS DAMAGED AT FS 349 APPROXIMATELY 18 INCHES UP FROM BOTTOM OF STRINGER 18. COMPLIED WITH REO 601R-52-11-008. (M)

Part: ANGLE — CRACKED (FUSELAGE)

OBLIQUE ANGLES, LEFT AND RIGHT AT FS 625 ARE CRACKED, REMOVED DEFECTIVE 625 OBLIQUE ANGLES, LEFT AND RIGHT SIDES AND INSTALLED NEW ANGLES P/N'S 601-35012-51 AND 601-35012-52 IAW CRJ SRM 51-42-06. (M)

Part: ADC — MALFUNCTIONED (COCKPIT)

MACH TRIM FAIL CAS, F/O ALT AND VERTICAL SPEED INDICATION DISAPEARED. ELT AND VSI RED MESSAGE. MAINTENANCE REMOVED AND REPLACED NR 2 AIR DATA COMPUTER. OPERATIONAL CHECK AND LEAK CHECK GOOD. (M)

Part: WARNING LIGHT — FALSE ACTIVATION (LAVATORY) · airframe 5,691 hrs · 4,225 cycles

INFLIGHT, RECEIVED SMOKE TOILET MESSAGE, C/W CHECKLIST, MESSAGE WENT OUT PRIOR TO COMPLETION OF CHECKLIST. MAINTENANCE INSPECTED LAV DUCTING AND FIRE EXTINGUISHER ALL FOUND TO BE GOOD. PERFORMED PACK BURNOUT PROCEDURE AS A PRECAUTION.