N418AW

Part: SENSOR — OUT OF ADJUST (NLG WOW)

NOSE DOOR OPEN GEAR DISAGREEAND CAUTION WOW INPUT STEERING INOP. HAS BEEN ADJUSTED NOSE LANDING GEAR WOW SENSOR PS4GA UAW AMM 323-61-05/501 AND WAS PERFORMED FUNCTIONAL TEST OF THE EXTENSION AND RETRACTION SYSTEM IAW AMM 32-30-00-720-801 OK.

Part: WIRE — DAMAGED (STICK SHAKER)

QRF CBB-CBB- STALL FAIL. REPAIRED WIRE ON P5CG PLUG MOTO SHAKER CAP SIDE IAW AMM 20-10-00/201 AND WDM 27-35-00. ON TEST OK.

Part: NONE — NONE · airframe 42,108 hrs · 4,024 cycles

ANTI-ICE DUCT WARNING MESSAGE ON CLIMB OUT. WE HAD WING AND COWL ANTI-ICING ON, AND GREEN ICE MESSAGE. RAN QRH. MESSAGE CLEARED AFTER CLOSING 14TH STAGE. LH FUSELAGE SIDE INDICATED RED. FLT 3891 DLH-ORD WITH 47 PAX. CA WAS FLYING THE A/C AND ENCOUNTERED ICE AT 15K BUT RECEIVED ANTI ICE DUCT WARNING AT 24K. CREW SHUT OFF THE ANTI ICE BUT MESSAGE PERSISTED UNTIL 14TH STAGE WERE SHUT OFF. CREW DECLARED AN EMERGENCY BUT DID NOT INFORM THE PASSENGERS. NO ICING CONDITIONS INTO ORD, TAXI WAS NORMAL, A/C WAS DEPLANED NORMAL. NO RESCUE VEHICLES RESPONDED TO EVENT AND NO DAMAGE TO A/C OR PASSENGERS WERE NOTED. A/C LANDED ON 27R. ***AIRCRAFT REMOVED FROM SERVICE*** T/S PER FIM 36-20-00 SECTION 2 RED ANTI-ICE DUCT WARNING. PERFORMED OPERATIONAL TEST OF ANTI-ICE CONTROL AND INDICATION SYSTEM NORMAL MODE GOOD AT THIS TIME.

Part: NONE — NONE · airframe 42,026 hrs · 39,942 cycles

A/ICE DUCT WARNING MSG IN FLIGHT. LH FUSELAGE AND WING RED ON A/ICE SYNOPTIC PAGE. C/W QRH. STBY WORKS. LANDING WEIGHT 47,200 LBS, SMOOTH LANDING. ***AIRCRAFT REMOVED FROM SERVICE*** TROUBLESHOT PER FIM AND AMM 36-121-36-21. NO FAULTS FOUND SUSPECT FAILURE OF LEFT FIX SWITCH. R&R LEFT SWITCH IAW AMM 26-21-01 OPS/FUNCTIONAL TEST GOOD. OPS OF BLEED AIR SYSTEM IS GOOD IAW 36-21. REMOVED PLACARD/MEL

Part: NONE — NONE · airframe 41,961 hrs · 39,880 cycles

RECEIVED LT ANTI-ICE DUCT WARNING MESSAGE IN-FLIGHT WITH WING ANTI-ICE SELECTED TO NORM. SYNOPTIC PAGE SHOW LT FUSELAGE RED. C/Q QRH. MESSAGE CLEARED. ON DESCENT, USED WING A/ICE IN STANDBY. MESSAGE DID NOT REAPPEAR. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED OPS CHECK OF A/I DUCT WARNING SYSTEM PER CRJ 200 AMM 36-21-00. OPS CHECK GOOD.

Part: ENGINE — OVERSPEED (RIGHT) · airframe 41,674 hrs · 39,591 cycles

NOTICED MCT ENGINE RH AND OVERSPEED CONDITION. RH THRUST LEVER EXERCISED FROM MINIMUM TO MAXIMUM WITHOUT RESPONSE. C/W IAC AND QRH, EVENTUALLY FOLLOWED ENG FIRE/SEVERE DAMAGE IAC QRH AND ACCOMPLISHED SHUTDOWN. AIRCRAFT REMOVED FROM SERVICE. REF 342527-1 FOR NO ENG EXEDANCES. REF 342527-4 FOR FINDINGS AND CORRECTIVE ACTION. RAN ENGINE AT IDLE AND THEN RAN UP TO MAX POWER SEVERAL TIMES. PARAMETERS WERE NORMAL AND NO DEFECTS NOTED IN REF TO AMM 71-00-00. CHECKED MDC- FOUND NO EXCEDANCE FOR RH ENGINE IN REF TO AMM 45-45-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (ANTI ICE DUCT) · airframe 41,097 hrs · 38,970 cycles

RECEIVED AINTIICE DUCT WARN MSG. CW QRH RH FUSELAGE WAS RED. MSG CLEARED WITHIN 30 SECONDS OF SELECTING 14TH STAGE SOVS CLOSED. FLAP OVERRIDE IS STUCK ON ***AIRCRAFT REMOVED FROM SERVICE**** PERFORMED INSPECTION OF BLEED AIR DUCT INSIDE THE FUSELAGE, FOUND NO DEFECTS. PERFORMED ENGINE RUNS CANNOT DUPLICATE ANTI-ICE DUCT WARNING, REQUIRES FURTHER T/SING. OPS CHECK NORMAL AT THIS TIME NO DEFECTS NOTED WITH FLAP OVERRIDE SWITCH. REF 326528/4 FOR NEW DISCREPANCY. SEE WO 302214 WCS 1-8 FOR C/AS OF REPLACEMENT OF 14TH ST BLEED AIR DUCT LOOP. OPS CHECKS GOOD AT THIS TIME.

Part: SKIN — CRACKED (PAX DOOR) · airframe 41,087 hrs · 38,956 cycles

PASSENGER DOOR INNER SKIN CRACKED AT FWD SIDE UNDER STEP 832AT. AIRCRAFT REMOVED FROM SERVICE. REPAIRED CRACK ON PASSENGER DOOR INNER SKIN AT FWD SIDE UNDER STEP 832AT, IAW EA AWAC-CRJ252-01551 REV A DATED 1/19/2021.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 41,087 hrs · 38,956 cycles

RT SIDEWALL SEAT TRACK FS 559+32 TO FS 559+80 CORRODED BEYOND LIMITS. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED RT SIDEWALL SEAT TRACK FROM FS 559+32 TO FS 559+80.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 41,087 hrs · 38,956 cycles

SEAT TRACK RIGHT HAND SIDE FS 412 CORRODED BEYOND LIMITS. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACE CORRODED SEAT TRACK AT RT SIDE FS 412 WITH NEW SEAT TRACK.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 41,087 hrs · 38,956 cycles

LT SIDE SEAT RAIL SEAT TRACK FROM STA 430 TO STA 574 CORRODED BEYOND LIMITS. AIRCRAFT REMOVED FROM SERVICE. CLEANED AND RESTORED SEGMENT FROM LT SIDE FS 430 TO FS 499. REMOVED AND REPLACED SEAT TRACK SEGMENTS FROM 400 TO 559+80.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 41,087 hrs · 38,956 cycles

SEAT TRACK RT FLOOR FROM STA 559 TO STA 621 CORRODED BEYOND LIMITS. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED CORRODED SEAT TRACK WITH NEW SEAT TRACK AT FS 559 TO FS 621 FLOOR RT SIDE.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 41,087 hrs · 38,955 cycles

RT SIDEWALL SEAT TRACK FROM FS 461 TO FS 559+32 IS CORRODED BEYOND LIMITS. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED RT SIDEWALL SEAT TRACK FROM FS 461 TO FS 559+32 WITH NEW SEAT TRACK.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 41,087 hrs · 38,956 cycles

SIDEWALL LEFT HAND SEAT TRACK FROM STA 409 TO 461 CORRODED BEYOND LIMITS. AIRCRAFT REMOVED FROM SERVICE. LEFT HAND SIDEWALL SEAT TRACK SEGMENT 409 TO 409+80 AND SEGMENT 409+80 TO 461 REPLACED WITH NEW SEAT TRACK.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 41,087 hrs · 38,956 cycles

SEAT TRACK LEFT HAND SIDE FS 409 CORRODED BEYOND LIMITS. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORRODED SEAT TRACK AND REPLACED WITH NEW SEAT TRACK AT FS 409 LEFT HAND SIDE.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 41,087 hrs · 38,956 cycles

SEAT TRACK RT SIDE FROM FS 509+128 TO STA 559 CORRODED BEYOND LIMITS. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK RT SIDE FS 409+128 TO FS 559 WITH NEW SEAT TRACK.

Part: ACTUATOR — BROKEN (THRUST REVERSER) · airframe 40,663 hrs · 38,506 cycles

RECEIVED RT.REV UNLOCK CAUTION MESSAGE DURING CLIMBOUT, C/W'D QRH & SELECTED EMER STOW SWITCH, MESSAGE REMAINED, ALSO HAD AMBER REV ICON IN N1 GAUGE. M/C DID AIR RETURN TO IAD PER QRH, CREW DID NOT DECLARE AN EMERGENCY. "AIRCRAFT REMOVED FROM SERVICE" FOUND ANTI ROTATION TANG OF RH BOTTOM INNER BALLSCRE ACTUATOR BROKEN. R/R BPTTPM INNER BALLSCREW ACTUATOR IAW AMM 78-32-01, OPS CHECK GOOD. RERIGGED RH BOTTOM OUTER TOP OUTTER BALLSCREW ACTUATORS IAW 78-32-01, OPS CHECK GOOD. REMOVED PLACARD REMOVED FROM MEL. S/N OFF 9633 S/N ON

Part: ELEMENT — FALSE ACTIVATION (RT ENG EXHAUST) · airframe 40,382 hrs · 38,228 cycles

A/C RECEIVED MULTIPLE RIGHT JET PIPE OVERHEAT FAIL CAUTION AND RIGHT JET PIPE OVERHEAT WARNING MESSAGES IN FLT. PILOT RETURNED TO IAD FOR A LOGBOOK ENTRY AND IN ORDER TO HAVE MX INVESTIGATE. AIRCRAFT REMOVED FROM SERVICE LOOP B ON RH SIDE HAD AN MEL APPLIED TO IT LAST NIGHT. PILOT INDICATED THAT HE WAS ONLY USING LOOP A ON THE RH SIDE DUE TO THE MEL BEING APPLIED. MX PERFORMED OPS CHECKS AND DISCOVERED THAT LOOP B IS OPERATIONAL SO WE WERE ABLE TO CLEAR THAT MEL. LOOP A WAS THE ACTUAL FAULTY LOOP. LOOP A ON THE RH SIDE HAS BEEN PLACED ON MEL. R+R RH ENGINE JETPIPE A+B SENSING ELEMENT IAW AWAC SUPP 12-071C ANDM AMM26-11-04. PERFORMED ELECTRICAL TEST. TEST PASSED. REF. 264082/1 FOR ENGINE RUN TEST.

Part: APU — MALFUNCTIONED (APU BAY) · airframe 40,323 hrs · 38,167 cycles

SUPPLEMENTAL, SHORTLY AFTER TAKEOFF, RECEIVED A SMOKE TOILET WARNING MESSAGE AND NOTICED AN ODOR OF SMOKE IN THE COCKPIT AND CABIN. CAPTAIN INSTRUCTED THE FLIGHT ATTENDANT TO CHECK THE LAVATORY FOR ANY INDICATION OF SMOKE. THE FLIGHT ATTENDANT FOUND THE SMOKE ALARM IN THE LAVATORY WAS ACTIVATED BUT DID NOT FIND ANY SMOKE ONLY AN ODOR OF SMOKE THAT WAS PRESENT THROUGHOUT THE CABIN. AIRCRAFT REMOVED FROM SERVICE. PERFORMED PROCEDURE OF SUPP 09-037C. FOUND LT PACK TO BE PRODUCING ODOR. RT PACK OPERATES NORMAL. REF 264070/4 FOR MEL. REF W/O 293766 W/C 2 FOR CORRECTIVE ACTION. PERFORMED PARAGRAPH 3 PROCEDURE STEP A CLEAN APPROPRIATE WATER SEPARATOR & COALSCER. REF TASK 21-51-13-140-801. W/C GENERATED TO COMPLETE (PROCEDURE) STEPS B THROUGH G. ALSO PARAGRAPH CLOSE OUT. STEP A AND B AMM SUPP 09-037C. C/W AMM SUPP 09-037C, NO ODORS OR FUMES PRESENT IN COCKPIT, CABIN OR LAV, OPS CHECK GOOD. R/R APU OPS CK AND LK CK GOOD NO DEFECTS NOTED AT THIS TIME REF SUPP 13-005 AND AMM CH 49-40 REF W/O 290036 FOR ADDITIONAL SERVICEABLE. REMARKS REMOVED PLACARD REMOVED FROM MEL. S/N OFF P-946 S/N ON P-1012.

Part: FITTING — LOOSE (APU) · airframe 40,210 hrs · 38,067 cycles

SUPPLEMENTAL INFORMATION, STRONG FUEL ODOR IN CABIN. AIRCRAFT REMOVED FROM SERVICE. OBSERVED FUEL POURING FROM INLET FITTING OF APU FUEL SOV, TIGHTENED FITTING AND CLEANED APU ENCLOSURE OF RESIDUAL FUEL, LEAK CHECK GOOD FER AMM 49-31-05.

Part: SKIN — CRACKED · airframe 38,790 hrs · 36,720 cycles

FUSELAGE SKIN CRACKED AT R/H AFT NLG SPADE DOOR CUT OUT. REPAIRED SKIN IAW REO 601R-53-11-3410.

Part: ANGLE — CORRODED (BS 319-349) · corrosion level 2 · airframe 38,790 hrs · 36,720 cycles

SERVICE DOOR LOWER SILL ANGLE CORRODED. REPLACED SERVICE DOOR LOWER SILL ANGLE IAW CRJ 200 SRM 53-0-00.

Part: DECK PLATE — CRACKED (BS 193) · airframe 38,790 hrs · 36,720 cycles

FS 193 LBL 30 TRU DECK IS CRACKED AT FRAME CUT OUT REPAIR TRU DECK AT FS 193 LBL 30 IAW REO 601R-53-081

Part: WEB — CRACKED (BS 193) · airframe 38,790 hrs · 36,720 cycles

FS 193 LBL 30 TRU DECK IS CRACKED AT FRAME CUTOUT REPAIRED TRU DECK AT FS 193 LBL 30 IAW BOMBARDIER REO 601R-53-081

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 38,790 hrs · 36,720 cycles

CRACK IN PAX DOOR AFT DRAG ANGLE.

Part: MOUNT — GOUGED (LE FLAP FAIRING) · airframe 38,790 hrs · 36,720 cycles

RH OUTBD FLAP INBD HINGE ARM INBD FAIRING MOUNT GOUGED. REPLACED

Part: ANGLE — CORRODED (BS 349) · corrosion level 2 · airframe 38,790 hrs · 36,720 cycles

SERVICE DOOR CUT-OUT AFT LOWER CORNER AT FS 349 CLIP CORRODED. REPLACED

Part: ATTACH ANGLE — CRACKED (CARGO DOOR) · airframe 38,790 hrs · 36,720 cycles

CARGO DOOR BEAM LOWER AFT ATTACH ANGLE AT THE APB CRACKED. REPLACED.

Part: WEB — CRACKED (BS 193) · airframe 38,790 hrs · 36,720 cycles

WEB AT FS 193 RBL 30 OUTBOARD CUTOUT AREA CRACKED. REPAIRED

Part: SKIN — CRACKED (CARGO DOOR) · airframe 38,790 hrs · 36,720 cycles

AFT ACCESS LATCH HANDLE CRACKED LOWER END AT DOOR 211AL. REPAIRED AFT ACCESS LATCH AREA IAW AWAC SUPP. 19-016B.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 38,790 hrs · 36,720 cycles

AEB STR 14L INTERCOSTAL CRACKED. REPLACE INTERCOSTAL IAW SRM 51-42-06, 51-42-21.

Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 38,790 hrs · 36,720 cycles

FS589.00, LBL43 CLIP UNDER CARGO DOOR SILL IS CRACKED. REPLACED CLIP IAW SRM 51-42-06, 51-42-21.

Part: FITTING — CRACKED (NLG WW) · airframe 38,790 hrs · 36,720 cycles

NLG WHEEL WELL FS 202.75, RBL9 VERTICAL POST O/B IS CRACKED. REPLACED POST CLIP IAW SRM 51-42-06.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 38,790 hrs · 36,720 cycles

AEB INTERCOSTAL AT FS625.00& STR 15L IS CRACKED. REPLACED INTERCOSTAL IAW SRM 51-42-06, 51-42-21.

Part: RETAINER — CRACKED (PYLON) · airframe 38,790 hrs · 36,720 cycles

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

Part: RETAINER — CRACKED (PYLON) · airframe 38,790 hrs · 36,720 cycles

PYLON PNL 412AT HAS CRACKED SEAL RETAINER. REPLACED SEAL RETAINER IAW SRM 51-42-06.

Part: FITTING — CRACKED (FUSELAGE) · airframe 38,790 hrs · 36,720 cycles

CO PILOTS AFT LOWER SIDE POST FITTING CRACKED. REPLACED FITTING IAW SRM 51-42-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 38,790 hrs · 36,720 cycles

FS484.00 RBL CLIP CRACKED. REPLACED CLIP IAW REO601R-53-41-059 REV-B.

Part: GUIDE — CHAFED (LT WING) · airframe 38,790 hrs · 36,720 cycles

LEFT WING, OUTBOARD FLAP, HINGE ARM FAIRING GUIDE AT WS220.00 INBOARD SIDE IS DEEP CHAFES. REPLACED HINGE ARM FAIRING GUIDE IAW SRM 51-42-06.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 38,790 hrs · 36,720 cycles

AEB STR 14R OBLIQUE ANGLE IS CRACKED. REPLACED ANGLE IAW SRM 51-42-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 38,790 hrs · 36,720 cycles

FS484.00, LBL36 CLIP CRACKED. REPLACED CLIP IAW REO 601R53-41-059 REV-B.

Part: RETAINER — CRACKED (PYLON) · airframe 38,790 hrs · 36,720 cycles

PYLON PNL 422AT HAS BROKEN SEAL RETAINER. REPLACED SEAL RETAINER IAW SRM 51-42-06.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 38,790 hrs · 36,720 cycles

AFT PRESSURE BULKHEAD FWD FACE HAS 2 CRACKS, ONE IS 3-1/4" BELOW THE SECOND STANDOFF FROM THE BOTTOM AT RBL27.5, 1/2" LONG. SECOND CRACK IS 6-1/2" BELOW THE SECOND STANDOFF FROM THE BOTTOM AT RBL 27.5, 1/2" LONG. AFT PRESSURE BULKHEAD REPAIRS AT RBL27.5 ACCOMPLISHED ON WO 1016868-2000-0020, SN:6956467. THIS SDR FOR TRACKING PURPOSES ONLY.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 38,138 hrs · 36,101 cycles

MOMENTARY SMOKE TOILET CAUTION IN CRUISE. MSG CLEARED BEFORE QRH COULD BE OPENED. FA REPORTS LAV WAS OCCUPIED. AFTER PAX LEFT, NO EVIDENCE OF SMOKE. SMOKE DETECTOR INTERMITTENTLY GOING OFF AT THE GATE WITH NO EVIDENCE OF SMOKE. REF 318051/4 FOR MEL. REMOVED & REPLACED LAV SMOKE DETECTOR IAW AMM 26-16-01 OP CHECKS GOOD REMOVE FROM MEL REMOVED PLACARD.

Part: NONE — NONE · airframe 36,897 hrs · 348,756 cycles

RIGHT SIDE EMERG EXIT ROW 8 BOTTOM EMERG LIGHT INOP. OPERATED EMERGENCY LIGHTS MANY TIMES OP CK OK AT THIS TIME.

Part: SIGN — INOPERATIVE (EMERGENCY LGIHTS) · airframe 35,913 hrs · 33,896 cycles

DURING ACCEPTANCE INSPECTION, CREW REPORTED THAT THE SERVICE DOOR EXIT SIGN WOULD NOT ILLUMINATE. REMOVED AND REPLACED EXIT SIGN IAW AMM 33-51-10, OPS CHECKED GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 35,509 hrs · 33,509 cycles

RED EXIT SIGN FWD OF SERVICE DOOR FAILED TO ILLUMINATE. REPAIRED A BROKEN WIRE INSIDE BULHEAD IAW ESPM 20-16-00. OPS CHECKED GOOD.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 35,438 hrs · 33,457 cycles

LEFT WING TE FLAP OTBD AFT TRAILING EDGED DENTED. REPAIR .

Part: FLOORBEAM — CRACKED (BS 280) · airframe 35,438 hrs · 33,457 cycles

ANGLE IS CRACKED ON THE INBD SIDE OF LBL 9 AND AFT SIDE OF THE FLOORBEAM BS 280.

Part: RETAINER — CRACKED (BS 663-672) · airframe 35,438 hrs · 33,457 cycles

SEAL RETAINER CRACKED ON PANEL 412BT.

Part: ACCESS PANEL — DAMAGED (BS 228) · airframe 35,438 hrs · 33,457 cycles

ACCESS PANEL 131AL SURROUND HAS ONE DAMAGED AND ONE MISSING FREEZE PLUG

Part: FLOORBEAM — CRACKED (BS 280) · airframe 35,438 hrs · 33,457 cycles

ANGLE IS CRACKED ON THE OTBD SIDE OF LBL 9 AND AFT SIDE OF THE FLOORBEAM BS 280.

Part: FLOORBEAM — CORRODED (BS 349) · corrosion level 2 · airframe 35,438 hrs · 33,457 cycles

FLOORBEAM BS 349 OTBD FLANGE HAS CORROSION JUST INBD OF SERVICE DOOR OPENING.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 35,438 hrs · 33,457 cycles

FWD ANGLE ON BS 280 FLOORBEAM BETWEEN RBL 9 AND LBL 9 FOUND TO BE CRACKED IN THE AFT RADIUS

Part: FLOORBEAM — CRACKED (BS 280) · airframe 35,438 hrs · 33,457 cycles

FLOORBEAM BS 280 UPPER AFT ANGLE IS CRACKED JUST OTBD OF RBL 9, IN MAIN CABIN BELOW FLOOR

Part: SUPPORT — CORRODED (BS 601) · corrosion level 2 · airframe 35,438 hrs · 33,457 cycles

AFT CARGO TIE DOWN SUPPORT AT BS 601, LBL 39 CORRODED. REMOVED AND REPLACED TIE DOWN SUPPORT IAW CRJ200 SRM 51-42-06, 51-42-21.

Part: BRACKET — CRACKED (NR 1 NACELLE) · airframe 35,438 hrs · 33,457 cycles

NR 1 ENGINE ORANGE HARNESS BRACKET CRACKED. REMOVED AND REPLACED THE HARNESS BRACKET IAW CMM 20-42-06.

Part: ANGLE — CRACKED (BS 621) · airframe 35,438 hrs · 33,457 cycles

AFT SIDE OF THE BS 621 BULKHEAD, STRINGER 14L, OBLIQUE ANGLE IS CRACKED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-42-21.

Part: ANGLE — CRACKED (BS 473) · airframe 35,438 hrs · 33,457 cycles

ANGLE AT BS 473.15, LBL 27, OTBD IS CRACKED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-24-36, 51-40-11, AND 51-42-21.

Part: CARGO TRACK — CORRODED (BS 618) · corrosion level 2 · airframe 35,438 hrs · 33,457 cycles

AFT CARGO TIE DOWN SUPPORT AT BS 618 AND LBL 39 CORRODED. REMOVED AND REPLACED TIE DOWN SUPPORT IAW SRM 51-42-06, 51-42-21.

Part: CARGO TRACK — CORRODED (BS 583) · corrosion level 2 · airframe 35,438 hrs · 33,457 cycles

AFT CARGO TIE DOWN SUPPORT AT BS 583, LBL 39 IS CORRODED. REMOVED AND REPLACED TIE DOWN SUPPORT IAW SRM 51-42-06, AND 51-42-21.

Part: VERTICAL BEAM — CRACKED (BS 409) · airframe 35,438 hrs · 33,457 cycles

VERTICAL BEAM AT BS 409+128, LBL 18 IS CRACKED IN THE AFT RADIUS. REMOVED AND REPLACED THE VERTICAL BEAM IAW SRM 51-42-06, AND REO 601R-53-41-889.

Part: SEAT TRACK — CORRODED (BS 544-559) · corrosion level 2 · airframe 35,438 hrs · 33,457 cycles

RIGHT SIDEWALL SEAT TRACK CORRODED BS 544 TO 559+112. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: DOOR SILL — CORRODED (BS 321-323) · corrosion level 2 · airframe 35,438 hrs · 33,457 cycles

FITTING ON FWD END LOWER SIDE OF SERVICE DOOR SILL HAS CORROSION.

Part: TEE FITTING — CORRODED (BS 319) · corrosion level 2 · airframe 35,438 hrs · 33,457 cycles

TEE FITTING ON FRAME BS 319.7 HAS CORROSION JUST ABOVE FLOOR AT THE SERVICE DOOR OPENING.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 35,438 hrs · 33,457 cycles

LEFT INBD FLAP VANE INBD LE IS CHAFED.

Part: DOOR SILL — CORRODED (BS 310-349) · corrosion level 2 · airframe 35,438 hrs · 33,457 cycles

PAX DOOR SILL HAS CORROSION ON BOTH SIDES BETWEEN BS 310 AND 349

Part: BRACKET — BENT (CARGO DOOR) · airframe 35,438 hrs · 33,457 cycles

CARGO DOOR FWD TRACK LOWER BRACKET IS BENT

Part: INTERCOSTAL — CORRODED (BS 349-364) · corrosion level 2 · airframe 35,438 hrs · 33,457 cycles

INTERCOSTAL STRINGER 26R BETWEEN BS 349 AND 364 IS CORRODED.

Part: GUSSET — CORRODED (BS 364) · corrosion level 2 · airframe 35,438 hrs · 33,457 cycles

GUSSET THAT SITS ON FRAME BS 364 AND INTERCOSTAL AT STRINGER 26R HAS CORROSION.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,412 hrs · 33,436 cycles

EMERGENCY LIGHTS, RIGHT SIDE ROWS 6--8 FOUND INOPERATIVE, R & R THE INVERTER IAW AMM 33-51-07, OPS CHECKED GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 34,573 hrs · 32,690 cycles

PASSENGER DOOR OUTER HANDLE CASS MESSAGE ILLUMINATED IN FLIGHT, 20,000 FT, DIFF PRESSURE 7.0. F/A STATED WITNESS MARKS NOT ALIGNED, CW QRH. ONCE ON GROUND CAPTAIN VERIFIED WITNESS MARKS WERE ALIGNED, PRESSURE NORMAL. GROUND CREW VERIFIED PASSENGER DOOR HANDLE WAS FLUSH AND CLOSED PROPERLY, PLACARDED AND PLACED ON MEL.

Part: TARGET — DEFECTIVE (SERVICE DOOR) · airframe 33,939 hrs · 32,083 cycles

RAMP REPORTS SERVICE DOOR WILL NOT OPEN FROM OUTSIDE. FOUND DOOR OPERATES NORMAL WITH OUTER HANDLE TARGET REMOVED. REMOVED EXCESS PRIMER FROM TARGET AND RESECURED TARGET. OUTER HAND OPERATES NORMALLY.

Part: HANDLE — DEFECTIVE (SERVICE DOOR) · airframe 33,919 hrs · 32,063 cycles

SERVICE DOOR OUTER HANDLE WILL NOT STOW.

Part: HANDLE — LACK OF LUBE (SERVICE DOOR) · airframe 33,418 hrs · 31,621 cycles

SERVICE DOOR WILL NOT OPEN FROM OUTSIDE. LUBED SERVICE DOOR OUTER HANDLE. PERFORMED OPERATIONS CHECK IAW AMM 52-40-00. OPERATIONS CHECKED GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 32,812 hrs · 31,036 cycles

ON CLIMB OUT FROM TAKEOFF, RECEIVED HYD 3 LOW CAUTION MSG. APPROX 10 SEC LATER RECEIVED GEAR DISAGREE WARNING MSG & AURAL. GEAR INDICATION SHOWED RED DOWN FOR RT & LT MLG & WHITE DASHES FOR NLG. BOTH MSGS CLEARED DURING EXECUTION OF GEAR DISAGREE QRH. HYD 3B & 2B PUMPS TURNED ON, NO MANUAL EXTENSION OF GEAR. HYD 3 QTY SHOWED 100% FOR AT LEAST 2 MINS AFTER QRH COMPLETION. LANDING WEIGHT BELOW 43,000 LBS.

Part: MOUNT BRACKET — CRACKED (FUSELAGE) · airframe 30,794 hrs · 29,051 cycles

SPR MOUNT BRACKET IS CRACKED IN RADIUS.

Part: CROSSMEMBER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,794 hrs · 29,051 cycles

RIGHT FLOORBEAM CROSS MEMBER IS CORRODED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 30,794 hrs · 29,051 cycles

OBLIQUE ANGLE AT AFT FACE OF FS 621 BULKHEAD RT SIDE STRINGER 13R IS CRACKED AT RADIUS.

Part: STRAP — CRACKED (FUSELAGE) · corrosion level 2 · airframe 30,794 hrs · 29,051 cycles

STRAP BETWEEN FLOOR SILL & VERTICAL STIFFENER RBL 27 AT 559 CORRODED.

Part: BRACKET — CRACKED (APU INLET) · airframe 30,794 hrs · 29,051 cycles

APU AIR INTAKE DOOR ACTUATOR BRACKET IS CRACKED AT LOWER RADIUS.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 30,794 hrs · 29,051 cycles

LOWER U BRACKET CRACKED AT RIVET IN CARGO BAY FS 574.00.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 30,785 hrs · 29,051 cycles

PAX DOOR STAIR AFT SUPPORT DRAG ANGLE CRACKED.

Part: BRACKET — CRACKED (LT MLG WW) · airframe 30,794 hrs · 29,051 cycles

BRAKE TRANSDUCER BRACKET IN LT WW IS CRACKED.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 30,794 hrs · 29,051 cycles

FS 283 STRINGER 3L HAS A CRACK.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,794 hrs · 29,051 cycles

FS 349 IN AVIONICS BAY HAS CORROSION.

Part: SKIN — CHAFED (RT AILERON) · airframe 30,785 hrs · 29,051 cycles

RIGHT AILERON UPPER LE SKIN CHAFED.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 30,794 hrs · 29,051 cycles

STIFFENER IN LT MLG WW AT WS 48 IS CRACKED.

Part: DRAG ANGLE — CRACKED (LT WING) · airframe 30,785 hrs · 29,051 cycles

LEFT MLG WW BATTERY RIB DRAG ANGLE CRACKED.

Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 30,794 hrs · 29,051 cycles

LOWER CARGO DOOR SILL CRACKED AT FWD STOP.

Part: FITTING — CRACKED (FUSELAGE) · airframe 30,794 hrs · 29,051 cycles

LEFT FS 484.00 CLIP CRACKED BL 36.00.

Part: SEAT TRACK — CORRODED (BS 409) · corrosion level 2 · airframe 30,794 hrs · 29,051 cycles

SEAT TRACK AT FS 409 - 409+128 HAS CORROSION.

Part: TIE DOWN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,794 hrs · 29,051 cycles

THREE EACH TIE DOWNS ON LBL 9 AT FS 559+96 - 621.00 HAS CORROSION.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,794 hrs · 29,051 cycles

LBL 27 AT FS 621.00 - 574.00 HAS CORRROSION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,794 hrs · 29,051 cycles

LT & RT FLOOR SEAT TRACK AT FS 349.00 - 409.00 HAS CORROSION.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 30,785 hrs · 29,051 cycles

FS 276 FRAME CREW ESCAPE HATCH HINGE CUT OUT CRACKED AT LBL 5.56.

Part: MOUNT BRACKET — CRACKED (FUSELAGE) · airframe 30,785 hrs · 29,051 cycles

GND POWER RECEPTACLE MOUNT BRACKET CRACKED.

Part: ANGLE — GOUGED (FUSELAGE) · airframe 30,785 hrs · 29,051 cycles

LOWER SEAL STRIKER ANGLE AT SERVICE DOOR SILL GOUGED.

Part: HOUSING — GOUGED (SERVICE DOOR) · airframe 30,785 hrs · 29,051 cycles

SERVICE DOOR HANDLE HOUSING IS GOUGED ON THE INNER BORE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,924 hrs · 28,232 cycles

EMERGENCY FLOOR LIGHTS TRACK ROW 11 INOPERATIVE.

Part: GENERATOR — MALFUNCTIONED (NR 2) · airframe 27,836 hrs · 26,260 cycles

3936 ON TAKEOFF ROLL, REC'D YAW DAMP 2 FOLLOWED BY GEN 2 CAUTION MESSAGES, ABORTED. ON TAXI IN, COMPLIED WITH QRH. REC'D YAW DAMP 2, GEN 2, MACH TRIM MESSAGES. BTMS 6, 5, 5, 7. INSPECTED & FOUND NR 2 GEN DROPPING OFF LINE AFTER APPROXIMATELY 2 MIN RUN TIME. IAW 247426 3 FOR MEL. IAW 247426 4 FOR YAW DAMPER & MACH TRIM CHECKS.

Part: UNKNOWN — ODOR (CABIN) · airframe 26,690 hrs · 25,159 cycles

STRONG FUME AND ODOR OF ELECTRICAL OR PLASTIC BURNING REPORTED BY FLT ATTENDANT DURING DESCENT FROM ROW 2 FWD. INSPECTED ACFT AND ALL ASSOCIATED ELECTRICALLY POWERED SYSTEMS OPERATED ELECTRICAL AND PNEUMATIC BLEED AIR SYSTEMS WITH FLT CREW ASSISTANCE. COULD NOT DUPLICATE ODOR.

Part: DUCT — DISCONNECTED (AC BAY) · airframe 26,206 hrs · 24,679 cycles

SMOKE COMING FROM AIR CONDITIONING SYSTEM WITH PACKS ON. PERFORMED PRESSURE CHECK OF BOTH PACKS WITH APU/ENG 1/ENG 2 IAW CRJ200 AMM 21-50-00 NO SMOKE NOTED. FOUND DUCT TO BE DISCONNECTED AT HEAT EXCHANGER. INSTALLED NEW COUPLING AND RE-INSTALLED DUCT ON EXCHANGER. OPS CHECK GOOD.

Part: RIB — CRACKED (RT MLG WW) · airframe 26,129 hrs · 24,608 cycles

RIGHT MLG BAY BATTERY RIB CRACKED. REPAIRED PER REO 601R-57-51-631 AND 601R-57-51-046.

Part: HINGE — CRACKED (ESCAPE HATCH) · airframe 26,129 hrs · 24,608 cycles

CREW ESCAPE HATCH BOTH HINGE ARMS ARE CRACKED. REMOVED AND REPLACED BOTH CRACKED CREW ESCAPE HATCH HINGE ARMS IAW CRJ 200 SRM 51-41-02.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 26,129 hrs · 24,608 cycles

FLOORBEAM ANGLE CRACKED AT 484 RBL 36. REPLACED ANGLE.

Part: PITOT SYSTEM — DIRTY · airframe 22,987 hrs · 21,535 cycles

ON TAKEOFF ROLL STANDBY AIRSPEED INDICATOR READ 30 KNOTS HIGH, ABORTED TAKEOFF AT 114 KNOTS. BTMS READ 5,5,3,4 MAX. PURGED P3 SYS IAW AMM 34-11-00. STANDBY ALTIMETER/AIRSPEED CHECKED GOOD IAW AMM 34-12-01. PITOT STATIC LEAK CHECKED GOOD. OK FOR SERVICE.

Part: SKIN — DAMAGED (BS 220) · airframe 21,633 hrs · 20,134 cycles

FREEZE PLUG FOR 131AL IS MIGRATING OUT. R & R FREEZE PLUG IAW REO 601R-53-11997.

Part: DOOR — CRACKED (APU BAY) · airframe 21,633 hrs · 20,134 cycles

APU COVER 311BZ IS CRACKED AT TOP OF COVER AT FLANGE WELD. REPAIRED APU ENCLOSURE DOOR 311BZ IAW REO 601R-49-11-070, REV A.

Part: HINGE FITTING — GOUGED (ELEVATOR) · airframe 21,633 hrs · 20,134 cycles

LT HORIZONTAL STABILIZER CENTER HINGE FITTING FOR ELEVATOR IS GOUGED. BLENDED OUT GOUGE TO A SMOOTH CONTOUR. FOUND TO BE WITHIN LIMITS NDT INSP NO DEFECTS NOTED. ALODINED, PRIMED AND TOP COATED.

Part: HINGE — CHAFED (BS 333) · airframe 21,633 hrs · 20,134 cycles

PAX DOOR HINGE ON FUSELAGE AFT LUG LANDING CHAFED FROM HINGE PIN ROLL PIN. BLENDED OUT CHAFED AREA AFT LUG LANDING ON FUSELAGE NO LOSS FOUND TO BE WITHIN LIMITS.

Part: PANEL — CHAFED (PAX DOOR) · corrosion level 1 · airframe 21,633 hrs · 20,134 cycles

PAX DOOR PANEL 832DT IS CHAFED BY THE HINGE AND HAS LIGHT CORROSION AT CHAFED AREA. MEASURED CHAFING AND FOUND PANEL 832DT NOT SERVICEABLE, LOCATED, DRILLED, AND COUNTER SUNK HOLES FOR NUTPLATES FOR HINGE AND INSTALLED NEW NUT PLATES REINSTALLED ON FWD STEPS.

Part: SKIN — CHAFED (PAX DOOR) · airframe 21,633 hrs · 20,134 cycles

DEPRESSURIZATION DOOR ON PAX DOOR IS CHAFING ON INSIDE WITH BROKEN CABLE. BLENDED OUT CHAFED AREA ON PRESSURE VENT FLAP DOOR. REMOVED APPROX .030 OF MATERIAL FOUND TO BE WITHIN LIMITS.

Part: SKIN — CHAFED (SERVICE DOOR) · airframe 21,633 hrs · 20,134 cycles

SERVICE DOOR OUTER SKIN CHAFED FROM OUTER HANDLE. REPAIRED SERVICE DOOR OUTER SKIN AROUND OUTER HANDLE IAW REO 601R-52-41-173.

Part: BEAM — CRACKED (BS 409) · airframe 21,633 hrs · 20,134 cycles

RBL 27.00 INBD SIDE OF VERTICAL BEAM BOTTOM END CRACKED AT FS 409+128. REPAIRED RBL 27.00 INBD SIDE OF VERTICAL BEAM BOTTOM END IAW REO 601R-53-41-056.

Part: STEP — CRACKED (PAX DOOR) · airframe 21,633 hrs · 20,134 cycles

PAX DOOR STAIR STRUCTURE HAS A CRACK ON AFT SIDE IN RADIUS OF STEP BETWEEN 4TH AND 5TH STEP. REPAIRED PAX DOOR STAIR STRUCTURE CRACK ON AFT SIDE IN RADIUS BETWEEN STEPS 4 AND 5 IAW SRM 52-00-31.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 21,633 hrs · 20,134 cycles

PAX DOOR OUTER HANDLE CRACKED. REMOVED CRACKED OUTER HANDLE ON PAX DOOR THEN INSTALLED NEW SERVICEABLE HANDLE ASSY IAW AMM 52-11-03.

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 21,633 hrs · 20,134 cycles

CARGO SEAT RAIL CORRODED RBL 27.00, FS 559.0 +80. REMOVED UNSERVICEABLE SEAT RAIL FROM RBL 27.00 TO FS 559.00 +80 AND INSTALLED SERVICEABLE SEAT RAIL IAW AMM 53-01-11 AND SRM 51-41-02 AND SRM 51-41-04.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 21,633 hrs · 20,134 cycles

PAX DOOR OUTER HANDLE FLAPPER IS CRACKED. REMOVED CRACKED PAX DOOR FLAPPER AND INSTALLED NEW SERVICEABLE FLAPPER, IAW SRM 51-40-11, 51-42-06.

Part: CARGO TRACK — CORRODED (BS559+96) · corrosion level 2 · airframe 21,633 hrs · 20,134 cycles

CARGO PANEL RAILS AT LBL 9.00, RBL 9.00, FS 559.00 + 96 HAVE CORRODED FASTENERS. REMOVED UNSERVICEABLE FASTENERS FROM CARGO FLOOR LBL 9.00 AND RBL 9.00 AT FS 559.00 + 96 AND INSTALLED SERVICEABLE FASTENERS IAW AMM 53-01-11.

Part: ANGLE — CRACKED (BS 625) · airframe 21,633 hrs · 20,134 cycles

LT FS 625.00 OBLIQUE ANGLE IS CRACKED. REMOVED UNSERVICEABLE LT FS 625.00 OBLIQUE ANGLE AND INSTALLED SERVICEABLE ANGLE IAW REO 601R-53-61-422 REV NC.

Part: PANEL — CORRODED (PAX DOOR) · corrosion level 2 · airframe 21,633 hrs · 20,134 cycles

PAX DOOR PANEL 932ET HINGE AREA`S HAVE CORROSION. REPLACED HINGES IAW SRM 52-00-00.

Part: RETAINER — CRACKED (PAX DOOR) · airframe 21,633 hrs · 20,134 cycles

REPAIR PAX DOOR SEAL RETAINER 601R-52-10-878 SEAL RETAINER WAS FOUND TO BE CRACKED, THEN REMOVED CRACKED SEAL RETAINER AND INSTALLED NEW SERVICEABLE, PN 601R31-8-722-1 IAW SRM 51-40-11, 51-42-06.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 21,633 hrs · 20,134 cycles

PAX DOOR STAIR STRUCTURE IS CRACKED IN RADIUS BETWEEN STEPS 1 AND 2 FWD AND AFT. CUT OUT CRACKED AREA ON FWD STEP RADIUS AND FABRICATED NEW PARTS IAW B/A REO 601R-52-11-702, REV C ON AFT SIDE DUPLICATED CRACKED ANGLE ON PREVIOUS REPAIR, IAW REO 601R-52-11-702, REV C5.

Part: SKIN — CHAFED (RUDDER) · airframe 21,633 hrs · 20,134 cycles

RUDDER RT SIDE LT HAS MINOR CHAFING ABOVE AND BELOW BOTTOM HINGE PANEL AND ABOVE CTR HINGE PANEL. REPAIRED CHAFED AREA ON RT RUDDER L/E ABOVE AND BELOW BOTTOM HINGE PANEL IAW SRM 55-40-00.

Part: SKIN — CHAFED (RT AILERON) · airframe 21,633 hrs · 20,134 cycles

RT AILERON UPPER L/E HAS 4 EA CHAFING AREAS. BLENDED AREAS ON RT UPPER L/E IAW REO 601R-57-60-013.

Part: BULKHEAD — CHAFED (BS 280) · airframe 21,633 hrs · 20,134 cycles

RT AFT FS 280 BULKHEAD CHAFED BY FWD GALLEY DOOR. REPAIR CHAFED DAMAGE ON RT AFT FS 280 BULKHEAD IAW REO 601R-53-11-1727, REV E.

Part: STRIKER — CHAFED (PAX DOOR FRAME) · airframe 21,633 hrs · 20,134 cycles

FWD AND AFT PAX DOOR STRIKER PLATES ARE CHAFED, MEASURED FWD AND AFT PAX DOOR STRIKER PLATES FOUND TO BE WITHIN LIMITS IAW REO 601R-52-11-296 REV NC NO FURTHER ACTION REQUIRED.

Part: SKIN — CHAFED (RT MLG DOOR) · airframe 21,633 hrs · 20,134 cycles

RT MLG DOOR L/E CHAFED AT (2 EA) LOCATIONS. R & R WITH SERVICEABLE FILLERS (2EA) AT RT MLG L/E IAW REO 601R-52-82-102.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 21,633 hrs · 20,134 cycles

LT INBD FLAP, FLAP VANE L/E CHAFED IN 3 EA PLACES. REPAIRED LT INBD FLAP VANE L/E CHAFED IN 3 EA AREA IAW REO 601R-57-52-004.

Part: SKIN — CHAFED (LT MLG DOOR) · airframe 21,633 hrs · 20,134 cycles

LT MLG DOOR L/E CHAFED AT 3 EA LOCATIONS. REMOVED CHAFED DAMAGE AND R & R WITH SERVCIEABLE FILLERS (2 EA) ON LT MLG DOOR L/E.

Part: SWITCH — LOOSE (TAXI LIGHTS) · airframe 21,446 hrs · 19,957 cycles

THROUGH FLIGHT LEVEL 180 TURNED RECOG, WING INSP AND LOGO LIGHTS ON THERE WAS A STRONG WIRE ODOR, TURNED THEM OFF ODOR WENT AWAY. FOUND RECOG/TAXI LIGHT SWITCH LOOSE IN SWITCH PANEL AND LOOSE SCREW ON THE SWITCH CAUSING ARCING. R & R SWITCH "S1LE" IAW CMM 33-41-07. OPS CKS GOOD.

Part: VALVE — INOPERATIVE (AV1) · airframe 21,015 hrs · 19,500 cycles

OVERBOARD COOL FAIL MSG AFTER T/O, C/W QRH ACFT DID NOT PRESSURIZE. REF MX WO 154772 CARDS 4-14. R & R OVBD EXHAUST VALVE AND REPLACED SERVICE DOOR HARNESS AND 3 SERV PROX SENSORS. PRESSURIZED ACFT ON GROUND IAW AMM 21-31-00. OPS CK GOOD.

Part: WIRE HARNESS — DAMAGED (SERVICE DOOR) · airframe 20,628 hrs · 19,107 cycles

OVERBOARD COOL FAIL MESSAGE AFTER T/O, C/W QRH, ACFT DID NOT PRESSURIZE. R & R OVERBOARD EXHAUST VALVE AND REPLACED SERVICE DOOR HARNESS AND 3 SERV PROX SENSORS. PRESSURIZED ACFT ON GROUND IAW AMM 21-31-00. OPS CHECKS GOOD.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 20,042 hrs · 18,493 cycles

FS 559 RBL 9 ANGLE IS CRACKED CUT OUT DAMAGE AND REPAIR IAW REO 601R-53-41-260 AND 601R-53-41-609.

Part: RELAY — MALFUNCTIONED (PAX DOOR) · airframe 18,319 hrs · 16,668 cycles

PAX DOOR WILL CLOSE WITHOUT ANYONE PUSHING DOOR DONE BUTTON. REMOVED AND REPLACED RELAY K1MB OPS CHECK OK IAW 24-01-12 R & R 52-10.

Part: MOTOR — MALFUNCTIONED (DOOR ASSIST) · airframe 18,222 hrs · 16,603 cycles

DOOR CLOSE ASSIST WILL NOT DISENGAGE. REMOVED AND REPLACED PAX DOOR POWER ASSIST MOTOR, OPS CHECK GOOD IAW AMM 52-11-08.

Part: SKIN — ERODED (LT MLG DOOR) · airframe 17,128 hrs · 15,539 cycles

MWC 135174-60- LT MLG DOOR INNER SKIN FOUND ERRODED AT L/E FWD CORNER AREA. REPAIR PERFORMED ON LT MLG DOOR INNER SKIN AT L/E FWD CORNER IAW REO 601R-52-82-034. (K)

Part: SILL — CORRODED (BS 317-349) · corrosion level 2 · airframe 17,128 hrs · 15,539 cycles

MWC 135174-158, SERVICE DOOR LOWER SILL LONGERON FWN UPPER FLANGE CLIP ANGLE CORRODED. SERVICE DOOR LOWER SILL LONGERON FWD UPPER FLANGE CLIP ANGLE REPLACED IAW SRM 51-42-21 AND SRM 51-42-06. (K)

Part: SKIN — ERODED (LT MLG DOOR) · airframe 17,128 hrs · 15,539 cycles

MWC 135174-62- LT MLG DOOR INNER SKIN FOUND ERODED AT L/E AND T/E AREA. REPAIR PERFORMED ON LT MLG DOOR INNER SKIN AT L/E AND T/E AREA IAW REO 601R*52-82-102 VIEW AA. (K)

Part: FLOORBEAM — CRACKED (BS 280) · airframe 17,128 hrs · 15,539 cycles

MWC 135174-136 - FLOORBEAM LOWER FLANGE AT FS 280.00, LBL 9.00 CRACKED IN 2 LOCATIONS. FLOOR BEAM LOWER FLANGE AT FS 280.00, LBL 9.00. REPAIRED IAW 601R-53-11-171 REV. D REPAIR SCHEME B. (K)

Part: FLOORBEAM — CORRODED (BS 280) · corrosion level 1 · airframe 17,128 hrs · 15,539 cycles

FS 280, LBL 9.0 TO RBL 9.0, CORROSION FOUND ON FWD FLOOR ANGLE UPPER SURFACE. CORROSION REMOVED ON FWD FLOOR ANGLE AT FS 280 BTW LBL 9 AND RBL 9 - OUT OF LIMITS. ANGLE REPLACED. (K)

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 17,128 hrs · 15,539 cycles

MWC 135174-219 - CRACK FOUND ON INTERCOSTAL BRACKET FS 621-625 ADJACENT TO STR 14 RT (CRACK LENGTH IS .500) INTERCOSTAL BRACKET FS 621-625 ADJACENT TO STR 14 RT REPLACED IAW SRM 51-42-06 AND 51-42-21. (K)

Part: SKIN — ERODED (MLG DOOR) · airframe 17,128 hrs · 15,539 cycles

RT MLG DOOR INNER SKIN FOUND ERODED AT L/E FWD CORNER AREA. REPAIR PERFORMED ON RT MLG DOOR INNER SKIN FWD CORNER IAW REO 601R-52-82-034. (K)

Part: DOOR — ERODED (RT MLG) · airframe 17,128 hrs · 15,539 cycles

MWC 135174-54- RT MLG DOOR INNER SKIN FOUND ERODED ON CENTER CORNER AREA OF L/E. REPAIR PERFORMED ON RT MLG DOOR INNER SKIN ON CENTER AREA CORNER IAW REO 601R-52-82-102. (K)

Part: BULKHEAD — CRACKED (BS 202) · airframe 17,128 hrs · 15,539 cycles

MWC 135174-34 FWD PRESSURE BULKHEAD CRACKED AT FS 202.75, PARKING BREAK CABLE AREA. FWD PRESSURE BULKHEAD AT FS 202.75, PARKING BREAK CABLE, REPAIR CARRIED OUT IAW REO 601R-53-11-563. (K)

Part: BULKHEAD — CRACKED (BS 621) · airframe 16,642 hrs · 15,066 cycles

AFT PRESSURE BULKHEAD CRACKED AT FS 621.00 AFT LINTEL FITTINGAREA. AFT PRESSURE BULKHEAD AT FS 621.00 AT LINTEL FITTING AREA REPAIRED IAW REO 601R-53-61-1230, REV D. (K)

Part: TRIM SYSTEM — MALFUNCTIONED (STAB) · airframe 14,570 hrs · 13,132 cycles

STAB TRIM ACTIVATED NOSE UP AFTER TAKEOFF WITHOUT PILOT INPUT TRIMMING NOSE DOWN STOPPED UNCOMMENDED TRIM. CHECKED PILOT AND COPILOTS STAB TRIM SWITCHES FOR BINDING FREE MOVEMENT. FOUND PILOT AND COPILOT TRIM SWITCHES TO OPERATE NORMALLY. NO BINDING NOTED. SWITCHES NOT STICKING AT THIS TIME IAW AMM 27-40-00. CHECKED FOR MOISTURE CONTAMINATION ON HSTCU. FOUND NO MOISTURE CONTAMINATION. FUNCTIONAL CHECK OF THE HSTCU. OPS CHECK GOOD IAW 27-41-00. R&R HSTCU. OPS CHECK GOOD.

Part: OXYGEN BOTTLE — INOPERATIVE · airframe 14,399 hrs · 12,963 cycles

ONE PORTABLE OXYGEN BOTTLE INOPERATIVE, ONE PORTABLE OXYGEN BOTTLE USED BELOW MIN. REMOVED AND REPLACED PORTABLE OXYGEN BOTTLE ASSEMBLY PER AMM 35-32-01. (M)

Part: HANDLE — DISLODGED (E/E BAY DOOR) · airframe 13,614 hrs · 12,216 cycles

AFTER ROTATION AVIONICS BAY CAUTION MESSAGE CAME ON, RAN QRH AND RETURNED TO ORF. CREW FOUND HANDLE OUT, RESTOWED HANDLE. AVIONICS BAY DOOR INDICATION GREEN AS PER AMM 52-40-00. (M)

Part: LINE — LOOSE (HYD SYSTEM)

HYDRAULIC NR 1 LOW PRESSURE CAUTION MESSAGE ILLUMINATED INFLIGHT, COMPLIED WITH QRH, FLUID QUANTITY INDICATED ZERO. FOUND PRESSURE LINE ON LT EDP LOOSE AND TIGHTENED IAW 51-40, OPERATION TEST AND FUNCTION TEST OF EDP PERFORMED IAW AMM 29-11-01, CHECKED GOOD. SERVICED HYD NR 1 SYSTEM. (M)

Part: FILTER — FAILED (HYD SYSTEM) · airframe 12,450 hrs · 11,115 cycles

AIRCRAFT FAILED HYDRAULIC SYSTEM TEST ON THE FIRST FLIGHT OF THE DAY CHECK. (NR2 SYSTEM) REMOVED AND REPLACED HYDRAULIC MANIFOLD NR 2, REF 29-11-05. (K)

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 12,421 hrs · 11,084 cycles

FLAP FAIL CAS CAUTION MESSAGE IN CRUISE FLIGHT. FLAPS FAILED AT ZERO. QRH COMPLIED WITH. BRAKE TEMPS INDICATE 4,4,5,6, COMPLIED WITH RESET PROCEDURE IAW SUPP 98-018B, STEPS 1.3 AND 1.4. FLAP SYSTEM RESET, OK. REMOVED AND REPLACED LT BPSU, OPS CHECK GOOD IAW AMM 27-51-00. (K)

Part: FLOORBEAM — CRACKED (BS 280)

FLOORBEAM ANGLE AT FS 280, LBL 11, CRACKED IN RADIUS APPROX .5 INCH LONG. (M) [07-31-07] MAINTENANCE REPAIRED ANGLE IAW REO 601R-53-11-138. (K)

Part: FLOORBEAM — CRACKED (BS 460)

FS 460 PRESSURE FLOORBEAM SUPPORT ANGLE CRACKED APPROX .2 INCH LONG OUTBOARD SIDE OF RBL. (M) [07-31-07] MAINTENANCE REMOVED CRACKED FITTING, DRILLED AND INSTALLED NEW SERVICEABLE FITTING PN 600-31068-19, IAW SRM. (K)

Part: FLOORBEAM — CRACKED (BS 460)

FS 460 PRESSURE FLOORBEAM SUPPORT ANGLE IS CRACKED APPROX .2 INCH LONG OUTBOARD SIDE OF RBL. (M)

Part: INTERCOSTAL — CRACKED (BS 484)

LT FS 484 INTERCOSTAL ANGLE CRACKED APPROX .2 INCH LONG AT LBL 27 ON PRESSURE FLOORBEAM. (M) [07-31-07] MAINTENANCE REMOVED CRACKED ANGLE AND INSTALLED REPAIR ANGLE IAW BSC STANDARD REPAIR 601R-53-0029B. (K)

Part: INTERCOSTAL — CRACKED (BS 484)

LT FS 484 INTERCOSTAL PREVIOUS REPAIR ANGLE CRACKED APPROX .3 INCH LONG AT LBL 36 ON PRESSURE FLOORBEAM. (M) [07-31-07] MAINTENANCE REMOVED CRACKED ANGLE AND INSTALLED REPAIR ANGLE IAW BSC STANDARD REPAIR 601R-53-0030A AND REO 601R-53-41-059 REV A. (K)

Part: ANGLE — CRACKED (BS 484)

RIGHT FS 484 INTERCOSTAL ANGLE CRACKED APPROX .1 INCH LONG AT RBL 27 ON PRESSURE FLOORBEAM. (M) [07-31-07] MAINTENANCE REMOVED CRACKED ANGLE, MANUFACTURED AND DRILLED NEW ANGLE IAW BAS STANDARD REPAIR 601R53-0029B AND CRJ 200 SRM INSTALLED NEW FABRICATED ANDLE AT RT FS 484, RBL 27 IAW MFG STANDARD REPAIR 601R-53-0029B. (K)

Part: DRAG ANGLE — CRACKED (PAX DOOR)

AFT PAX DOOR DRAG ANGLE IS CRACKED APPROX 1 INCH LONG. (M) [07-31-07] MAINTENANCE FOUND DAMAGE TO BE LOCATED ON PREVIOUS REPAIR. REMOVED PREVIOUS REPAIR ANGLE FABRICATED NEW ANGLE INSTALLED AND SEALED PAINTED IAW REO 601R52-11513. (K)

Part: ANGLE — CRACKED (BS 484)

RT FS 484 INTERCOSTAL PREVIOUS REPAIR ANGLE CRACKED APPROX .3 INCH LONG AT RBL 36 ON PRESSURE FLOORBEAM. (M) [07-31-07] MAINTENANCE REMOVED CRACKED ANGLE AND INSTALLED REPAIR ANGLE IAW BSC SR 601R-53-0030A AND MFG REO 601R53-41-059, REV A. (K)

Part: BRACKET — CRACKED (LT MLG WW)

HYDRAULIC PRESSURE TRANSDUCER BRACKET CRACKED APPROX .1 INCH LONG IN LT WHEEL WELL CEILING. (M)

Part: BRACKET — CRACKED (RT MLG WW)

HYDRAULIC PRESSURE TRANSDUCER BRACKET CRACKED APPROX .1 INCH LONG IN RT WHEEL WELL CEILING. (M) [07-31-07] MAINTENANCE REMOVED RT HYDRAULIC PRESSURE TRANSDUCER BRACKET PICKED UP HOLES ON SERVICEABLE TRANSDUCER BRACKET AND INSTALLED IAW SRM. (K)

Part: BRACKET — CRACKED (LT MLG WW)

HYDRAULIC PRESSURE TRANSDUCER BRACKET CRACKED APPROX .1 INCH LONG IN LT WHEEL WELL CEILING. (M)

Part: BRACKET — CRACKED (RT MLG WW)

HYDRAULIC LINE Z-BRACKET CRACKED APPROX .1 INCH LONG IN RT WHEEL WELL CEILING FORWARD OF PRESSURE TRANSDUCERS. (M)

Part: BRACKET — CRACKED (RT MLG WW)

HYDRAULIC LINE Z-BRACKET CRACKED APPROX .1 INCH LONG IN RT WHEEL WELL CEILING FORWARD OF PRESSURE TRANSDUCERS. (M) [07-31-07] MAINTENANCE REMOVED CRACKED BRACKET AND INSTALLED NEW BRACKET IAW CRJ 200 SRM. (K)

Part: BRACKET — CRACKED (LT MLG WW)

HYDRAULIC PRESSURE TRANSDUCER BRACKET CRACKED APPROX .1 INCH LONG IN LT WHEEL WELL CEILING. (M) [07-31-07] MAINTENANCE REMOVED LT HYDRAULIC PRESSURE TRANSDUCER BRACKET AND PICKED UP HOLES ON SERVICEABLE TRANDUCER BRACKET AND INSTALLED IAW CRJ 300 SRM 51-42-06, 51-40-11 AND 51-41-02. (K)

Part: UNKNOWN — CRACKED (BS 280)

FOUND FS 280 CLIPS INBOARD AND OUTBOARD AT LBL 9 ARE CRACKED. (M) [07-31-07] MAINTENANCE REMOVED AND REPLACED CLIPS AT FS 280, LBL 9 WITH NEW CLIPS PN 601R3111357. (K)

Part: BRACKET — CRACKED (RT MLG WW)

HYDRAULIC PRESSURE TRANSDUCER BRACKET CRACKED APPROX .1 INCH LONG IN RT WHEEL WELL CEILING. (M)

Part: BRACKET — CRACKED (HYD LINE)

HYDRAULIC LINE Z-BRACKET CRACKED APPROX .1 INCH LONG IN RT WHEEL WELL CEILING FORWARD OF PRESSURE TRANSDUCERS. (M)

Part: BRACKET — CRACKED (RT MLG WW)

HYDRAULIC PRESSURE TRANSDUCER BRACKET CRACKED APPROX .1 INCH LONG IN RT WHEEL WELL CEILING. (M)

Part: INTERCOSTAL — CRACKED (BS 621) · airframe 12,342 hrs · 11,007 cycles

LT SIDE FS 621.00 TO 625.30 INTERCOSTAL AT STR 14L IS CRACKED NEAR RADIUS APPROX 1.0 INCH LONG. [07-31-07] MAINTENANCE REMOVED CRACKED INTERCOSTAL AT LT STR 14L AND INSTALLED NEW INTERCOSTAL IAW CRJ200 SRM 51-42-06. (K)

Part: FLAP SYSTEM — FAILED (TE FLAPS)

FLAPS FAILED AT 21,000 FEET QRH COMPLIED WITH. PERFORMED FLAP RESET PROCEDURE IAW AWAC SUPPLEMENT 98-018B STEPS 1.3 THRU 1.4 FLAP RESET. A/C RELEASED FOR SERVICE. NO TWISTING OR SKEWING DETECTED.

Part: ELEMENT — MALFUNCTIONED (ANTI ICE DUCT)

ANTI-ICE DUCT WARNING ON ED1. LT FUSELAGE SHOWS RED WITH WING ANTI-ICE TURNED OFF. ABORTED TAKEOFF, SPEED AT 70 KNTS. BRAKE TEMPS ARE 03, 03, 04, 05. REMOVED AND REPLACED SENSING ELEMENT A15WK IAW AMM 36-21-04, OPS CHECK GOOD. (M)

Part: B-NUT — LOOSE (APU FUEL LINE)

FUEL ODOR AFTER APU START IN FLIGHT. SHUTDOWN APU, ODOR DISIPATED. INSPECTED AND FOUND LOOSE (B) NUT ON FUEL LINE TO APU FUEL PUMP. RESECURED (B) NUT IAW AMM. OPS AND LEAK CHECK GOOD AT THIS TIME. (K)

Part: STRUT — DISCHARGED (NLG)

AFTER GEAR SELECTED DOWN, NOSE GEAR WOULD NOT EXTEND, HAD RED GEAR DISAGREE CAS MESSAGE, USED EMERGENCY GEAR EXTENSION, NOSE DOORS OPENED BUT DIDN`T EXTEND. REMOVED AND REPLACED PRIORITY VALVE IAW 32-33-15. REMOVED AND REPLACED SELECTOR VALVE IAW 32-33-10. SERVICED NLG SHOCK STRUT IAW 12-1232-610-803. ALL OPS CHECK GOOD. REMOVED PRIORITY VALVE P/N 4622, S/N 1467A. REMOVED NLG SELECTOR VALVE ASSEMBLY P/N 750006000, S/N 1835. (M)

Part: PUMP — INOPERATIVE (HYD SYS) · airframe 9,406 hrs · 8,193 cycles

AFTER SELECTING GEAR DOWN RECEIVED NLG DOOR GEAR DISAGREE WARNING MSSG. C/W QRH ALL 3 GEAR SHOWED DOWN AND LOCKED RESET NORMAL. REMOVED AND REPLACED HYDRAULIC 3A PUMP. PERFORMED GEAR SWING IAW OPS CHECK GOOD AT THIS TIME. (K)

Part: ACTUATOR — FAILED (RT WING) · airframe 8,715 hrs · 7,534 cycles

DEPARTING FLAPS FAIL MSG. WHEN FLAPS WENT FROM 8-0 DEGREES PERFORMED QRH RETURNED. WORK ORDER 90809, REMOVED AND REPLACED NR 3 AND NR 4 FLAP ACTUATORS ON RT WING TRIPPED IAW AMM. OPS CHECK GOOD. (K)

Part: WIRE — DAMAGED (EMERGENCY LIGHT)

TRACK LIGHTING IS INOPERATIVE AT FORWARD CABIN. REMOVED AND REPLACED POWER SUPPLY CABLE, FLOOR TRACK LIGHT AND CONNECTOR IAW CRJ AMM 33-51-01-400 AND CRJ200 WM 20-17-10. OPERATIONAL CHECK GOOD AT THIS TIME. (M)

Part: SUPPORT BEAM — CRACKED (ENGINE) · airframe 7,832 hrs · 6,660 cycles

ENGINE SUPPORT BEAM LOWER WEB IS CRACKED AT FWD IB CORNER OF THE RT ACCESS PANEL CUT OUT. ENGINE SUPPORT BEAM LOWER WEB WAS REMOVED AND REPLACED BY MODIFICATION OF BEAM UNDER WO 81584 JOB CARD 4EOMFG08364, SEG NR 14, EO2/081/453. (K)

Part: SKIN — GOUGED (FUSELAGE) · airframe 7,600 hrs · 6,431 cycles

THE RT SIDE FUSELAGE SKIN AT FS 225.20 ON THE SURROUND STRUCTURE FOR THE ACCESS PANEL WAS GOUGED APPROXIMATELY .5 INCH W X .4 INCH L X .012 DEEP. BLENDED DAMAGED AREA, PERFORMED EDDY CURRENT INSPECTION, ADDED PROTECTIVE TREATMENT AND EXTERIOR FINISH IAW SRM. (K)

Part: BUSHING — MIGRATED (LT MLG TRUNNION) · airframe 7,600 hrs · 6,431 cycles

LT MLG AFT TRUNNION BUSHING MIGRATED .025 INCH. REMOVED BUSHING AND INSTALLED 2ND OVERSIZE BUSHING IAW REO. (K)

Part: SKIN — DENTED (RUDDER) · airframe 7,600 hrs · 6,431 cycles

RUDDER RT SKIN DENTED 2.0 INCHES ABOVE RIB STATION 72.75 AND 14.3750 FORWARD OF TRAILING EDGE. DENT IS 2 INCHES LONG X 1.5 INCHES WIDE AND .020 INCH DEEP. REPAIRED RUDDER RT SKIN IAW EO. (K)

Part: INTERCOSTAL — CRACKED (FUSLEAGE) · airframe 7,600 hrs · 6,431 cycles

THE UNDER FLOOR INTERCOSTAL AT FS 484, RBL 36 IS CRACKED 1 INCH LONG. REPAIRED INTERCOSTAL IAW REO. (K)

Part: DRAG ANGLE — CRACKED (PAX DOOR)

PASSENGER DOOR AFT DRAG ANGLE IS CRACKED AT POWER ASSIST PULLEY BRACKET. REPAIRED AFT DRAG ANGLE IAW REO. (K)

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 7,618 hrs · 7,600 cycles

UNDERFLOOR INTERCOSTALS HAVE CRACKED ATTACH FLANGES AT FS 484, LBL 36, AND RBL 36. REPAIRED INTERCOSTAL IAW REO. (K)

Part: FLOORBEAM — CRACKED (FUSELAGE)

THE LT AND RT SIDE UNDERFLOOR SUPPORT ANGLE IS CRACKED 1.0 INCH AT FS 621, LBL 40 AND RBL 40, WL 73. REPAIRED INTERCOSTALS IAW REO. (K)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 7,600 hrs · 6,431 cycles

RT SIDE FS 621- 625.3 INTERCOSTAL AT STR 14R IS CRACKED IN RADIUS APPROXIMATELY 1.2 INCH LONG. REMOVED AND REPLACED RT SIDE FS 621- FS625.3 INTERCOSTAL AT STR 14R IAW SRM. (K)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

LT SIDE FS 621-625.3 INTERCOSTAL AT STR 14L IS CRACKED IN RADIUS APPROXIMATELY 0.9 INCH LONG. REMOVED AND REPLACED LT SIDE FS621-625.3 INTERCOSTAL AT STR 14L IAW SRM. (K)

Part: COMPUTER — MALFUNCTIONED (AUTOFLIGHT)

RUDDER FLUTTER INFLIGHT, ALL CONDITIONS, AUTOPILOT ENGAGES. REMOVED AND REPLACED FCC NR 1 IAW 22-12-14. PERFORMED OPS TEST IAW AMM 22-11-00. OPS CHECK GOOD. AIRCRAFT CERTIFIED FOR RVSM. (M)

Part: CONNECTOR — LOOSE (PAX DOOR) · airframe 6,779 hrs · 5,723 cycles

PASSENGER DOOR OUTER HANDLE MESSAGE ILLUMINATED DURING FLIGHT. DIVERTED, FOUND PAX DOOR HARNESS PLUG (P7MB) LOOSELY CONNECTED. REMOVED, INSPECTED AND CLEANED DOOR HARNESS. REPLACED DOOR HARNESS, OPS CHECK GOOD. (K)

Part: DUCT — FAILED (BLEED AIR)

LEFT 10TH DUCT RED WARNING MESSAGE AFTER TAKEOFF BLEED AIR DUCT AURAL WARNING. COMPLIED WTH QRH MESSAGE WENT OUT AFTER REDUCING LEFT THROTTLE WHEN DUCT PSI FELL BELOW 60 PSI. REMOVED AND REPLACED 14TH STAGE DUCT AND 14TH STAGE SOV. OPS CHECK GOOD. CLEARED ON LOG PAGE 120506/1. THIS BLOWN DUCT CAUSED THE 10TH STAGE WARNING TO ILLUMINATE. (M)

Part: FLAP — INOPERATIVE (WINGS) · airframe 4,146 hrs

FLAP FAIL MESSAGE. FLAPS AT ZERO, COMPLIED WITH QRH-WEIGHT AT TOUCHDOWN 41,800 LBS, APPROXIMATE SPEED 115 KNOTS. BRAKE APPLICATION 55 MAX BRAKE TEMP 2. RESET FLAPS IAW SUPPLEMENT 98-18 FLAPS OPERATE NORMAL AT THIS TIME.

Part: WARNING LIGHT — FALSE ACTIVATION (A/C PACKS)

AFTER TAKEOFF CAS MESSAGE 'LT PACK HI PRESS' MESSAGE. OVERHEAD PANEL INDICATION 'LT PACK FAIL'. SYNOPTIC PAGE INDICATED NEITHER PACK OPERATING. LANDED AT 50,600 LBS - VI 0 LIGHT BRAKING. HOTTEST TEMP 2, SPEED 135 KNOTS. INSPECTED AND OPERATED BOTH AC PACKS IAW AMM 21-51-00. BOTH PACKS OPERATE NORMALLY. NO FAULTS NOTED. OVERWEIGHT LANDING INSPECTION NOT REQUIRED PER AMM 5-51-01. (M)

Part: DUCT — CRACKED (NR 2 PACK)

EXCESSIVE ENGINE EXHAUST ODOR IN COCKPIT AND CABIN WHILE RUNNING APU. INSPECTION AND FOUND NR 2 PACK COMPRESSOR OUTLET TEMP SWITCH DUCT CRACKED. REMOVED AND REPLACED DUCT ASSEMBLY. (M)

Part: LE BOOT — FAILED (RT WING)

LGA/IAD - FLT 6322 - DURING CRUISE AT 910 HOURS ON 2-15-95, RT WING BOOT NR 2 SECTION WILL NOT INFLATE, AND RT TORQUE FLUCTUATED 10 PERCENT. AIRCRAFT DIVERTED TO SWF WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED LEADING EDGE ASSEMBLY AND CLEANED THE RT ENGINE ECU, HMU, AND TSCU CONNECTORS. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. REF: CONTROL NR 95ZZZX1393, NR 95ZZZX1394. AND NR 95ZZZX1395. (X)

Part: ECU — DIRTY (RT ENGINE)

LGA/IAD - FLT 6322 - DURING CRUISE AT 910 HOURS ON 2-15-95, RT WING BOOT NR 2 SECTION WILL NOT INFLATE, AND RT TORQUE FLUCTUATED 10 PERCENT. AIRCRAFT DIVERTED TO SWF WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED LEADING EDGE ASSEMBLY AND CLEANED THE RT ENGINE ECU, HMU, AND TSCU CONNECTORS. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. REF: CONTROL NR VTZA95061, NR 95ZZZX1393. AND NR 95ZZZX1395.

Part: HMU — DIRTY (RT ENGINE)

LGA/IAD - FLT 6322 - DURING CRUISE AT 910 HOURS ON 2-15-95, RT WING BOOT NR 2 SECTION WILL NOT INFLATE, AND RT TORQUE FLUCTUATED 10 PERCENT. AIRCRAFT DIVERTED TO SWF WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED LEADING EDGE ASSEMBLY AND CLEANED THE RT ENGINE ECU, HMU, AND TSCU CONNECTORS. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. REF: CONTROL NR VTZA95061, NR 95ZZZX1394. AND NR 95ZZZX1395.

Part: TORQUE SIGN COND — DIRTY (RT ENGINE)

LGA/IAD - FLT 6322 - DURING CRUISE AT 910 HOURS ON 2-15-95, RT WING BOOT NR 2 SECTION WILL NOT INFLATE, AND RT TORQUE FLUCTUATED 10 PERCENT. AIRCRAFT DIVERTED TO SWF WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED LEADING EDGE ASSEMBLY AND CLEANED THE RT ENGINE ECU, HMU, AND TSCU CONNECTORS. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. REF: CONTROL NR VTZA95061, NR 95ZZZX1393. AND NR 95ZZZX1394.

Part: PROP CNTL UNIT — FAILED (LT ENG)

FLT 6532 - IAD-ORF - AT 1300 THE CREW SHUT THE LEFT ENGINE DOWN IN FLIGHT FOR LOW OIL PRESSURE. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO RIC. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED LEFT PROP CONTROL UNIT. OPS CHECKED GOOD. AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (Z)