N455AW

Part: SENSOR — MALFUNCTIONED (NLG) · airframe 41,639 hrs · 40,915 cycles

NOSE GEAR WOULD NOT RETRACT, ASSOCIATED GEAR DISAGREE AND DOOR WARNING MSGS. HAPPENED ON CLIMB OUT WHEN SELECTING GEAR TO RETRACT AFTER 6 SECONDS. HYD PUMPS IN AUTO. UNDER 150 KNOTS. LANDING WEIGHTS 46,800 IBS. AIRCRAFT REMOVED FROM SERVICE, INSTALLED DOWN LOCK PINS IAW AMM 10-11-00 AND REMOVED THE FLAGS. REF 374446-3 FOR MEL. ACOSTA III, RAYMOND A&P 3745031 NLG OLEO CENTERED/EXTENDED PROX SENSOR (PS14GA) JAM NUTS FOUND LOOSE AND MISSING SAFETY WIRE, SENSOR IS LOOSE IN BRACKET. ADJUSTED AND RESECURRED NLG SENSOR PS14GA PER AMM 32-61-05, OPS CHECK GOOD. NLG RETRACT/EXTENSION CHECKS GOOD PER AMM 32-30-00. REMOVED PLACARD AND MEL.

Part: ESCAPE ROPE — BOUND (ZONE 200) · airframe 41,481 hrs · 40,729 cycles

6041 - EMER ESCAPE ROPE IMPROPERLY ZIP TIED. UNABLE FOR USE. EMER EGRESS ROPE WAS ZIPTIED TO IT'S SELF. THE ROPE WOULD NOT BE ABLE TO DEPLOY IN AN EMERG. AIRCRAFT REMOVED FROM SERVICE. CUT ZIP TIED AND RE-STOWED LH AND RH EMERGENCY STOW LINE IAW AWA SUPP 12-058A

Part: PCU — FAULTED (ELEVATORS) · airframe 41,425 hrs · 40,658 cycles

AIRCRAFT FLUTTERS AT AIRSPEED ABOVE 280KIAS. EXPERIENCED FLUTTER IN AIRFRAME ON CLIMB THROUGH 10000FT. FLUTTER DISAPPEARED AFTER LEVELING OFF AND SLOWING BELOW 250KIAS AT 14,000FT. NO FLUTTER ON DECENT OR APPROACH. AIRCRAFT REMOVED FROM SERVICE. R & R ELEVATOR TO PCU ATTACHMENT HARDWARE FOR LH AND RH SIDE PCU #1#2 AND #3 IAM AMM 27-33-01 AND SUPP 09-020C

Part: PRIORITY VALVE — FAULTED (ZONE 700) · airframe 41,109 hrs · 40,281 cycles

455 ORD-AZO EXPERIENCED A GEAR DISAGREE WHILE DEPARTING ORD. THE CREW RAN THE QRH AND ELECTED TO RETURN TO ORD. AN EMERGENCY WAS DECLARED. AIRCRAFT REMOVED FROM SERVICE. PERFORMED OPS CHECK OF NOSE DOOR IAW AMM 32-22-01 OPS CHECK GOOD. RETRIEVED PSUE CODES FOUND C/W M ACTION FOR MEL 32-30-01 REF BLK 2 FOR MEL.

Part: CONTROL UNIT — MALFUNCTIONED (ADG) · airframe 41,081 hrs · 40,242 cycles

AFTER ROTATION, LOUD BUZZING NOISE. ADG DEPLOYED ON ITS OWN. LANDING NOT OVERWEIGHT, , AIR-RETURN TO MKE. AIRCRAFT REMOVED FROM SERVICE. R/R ADG AUTO DEPLOY CONTROL PANEL IAW AMM 24-23-15. OPS CHECK GOOD AT THIS TIME.

Part: OIL SYSTEM — LEAKING (LT ENGINE) · airframe 40,883 hrs · 39,988 cycles

IN CLIMB, NOTICED L ENG OIL PRESSURE FLUCTUATING. RECEIVED L OIL PRESS WARN MSG. C/W QRH. DID NOT REQ ENG SHUT DOWN. MSG CLEARED AT IDLE. OIL PRESSURE WAS FLUCTUATING BETWEEN 27-32 AT IDLE AND WARNING CLEARED. OIL TEMP NORMAL ENTIRE TIME. DURING WALK AROUND FO FOUND OIL LEAKING OUT OF LH ENG. AIRCRAFT REMOVED FROM SERVICE. R & R LT ENGINE OPS AND LEAK CHECK GOOD.

Part: YOKE — UNKNOWN (COCKPIT) · airframe 40,554 hrs · 39,602 cycles

YOKE HAS SLACK IN THE NEUTRAL POSITION WHEN BANKING IN FLT, USING BOTH YOKES, MORE PRONOUNCED IN LEFT BANK, HAPPENS WITH FLAPS IN ANY POSITION. FEELS NORMAL ON THE GRD. NO BINDING FELT. AIRCRAFT REMOVED FROM SERVICE. OPEN

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 39,382 hrs · 38,275 cycles

AFTER SELECTING GEAR UP, RECEIVED NOSE DOOR OPEN WARNING AND GEAR DISAG WARNING. CW QRH MESSAGES CLEARED. NLG SHOWED GREEN DURING EVENT. MANUAL RELEASE NOT USED. *******AIRCRAFT REMOVED FROM SERVICE********* REMOVED AND REPLACED NOSEWHEEL CENTERING PROX SENSOR BRACKET IAW AMM 32-61, OPS CHECK GOOD. REMOVED PLACARD AND REMOVED FROM MEL.

Part: SKIN — GOUGED (CARGO DOOR) · airframe 38,924 hrs · 37,740 cycles

DURING OVERNIGHT RON MX, INSPECTION DISCOVERED DAMAGE TO THE CARGO DOOR OUTER SKIN UPPER EDGE FROM INCORRECT SCREWS INSTALLED IN THE CARGO BAY LINERS. AIRCRAFT REMOVED FROM SERVICE. PERMANENT REPAIR PERFORMED PER REO 601R-52-31-396. INCORRECT SCREWS REMOVED AND CORRECT ONES INSTALLED.

Part: STRINGER — CRACKED (BS 379 S4L) · airframe 38,770 hrs · 37,584 cycles

STRINGER 4L AT FS379.00 CRACKED. AIRCRAFT REMOVED FROM SERVICE, REPAIRED PER EA AWACCRJ253-10905

Part: FLOORBEAM — CORRODED (BS 559 RBL 27) · corrosion level 2 · airframe 38,770 hrs · 37,584 cycles

FLOOR BEAM IS CORRODED AT FS559.0, RBL 27. AIRCRAFT REMOVED FROM SERVICE, BLENDED AND REMOVED CORROSION. REPAIRED PER EA AWAC253-01907

Part: TIP CAP — DAMAGED (HORIZONTAL STAB) · airframe 38,770 hrs · 37,584 cycles

LH HORIZONTAL STAB TIP STRUCTURE HAS (5 TOTAL) ELONGATED SCREW HOLES. AIRCRAFT REMOVED FROM SERVICE, REPAIRED PER EA 105-2022-010

Part: ANGLE — CRACKED (RT MLG WW) · airframe 38,770 hrs · 37,584 cycles

ANGLE STRUCTURE CRACKED AT RH MLG BAY WEB, FORWARD, OUTBOARD SIDE. ***AIRCRAFT REMOVED FROM SERVICE*** REPLACED ANGLE

Part: ACCESS PANEL — CORRODED (TRUNNION ACCESS) · corrosion level 2 · airframe 38,770 hrs · 37,584 cycles

PITTING CORROSION ON LH FORWARD TRUNNION ACCESS PANEL. AIRCRAFT REMOVED FROM SERVICE. REPLACED

Part: FRAME — CORRODED (PAX DOOR) · corrosion level 2 · airframe 38,770 hrs · 37,584 cycles

PAX DOOR INTERNAL FRAME STRUCTURE AT FS 327.763 IS CORRODED. AIRCRAFT REMOVED FROM SERVICE, REPLACED PAX DOOR INTERNAL FRAME.

Part: NONE — NONE · airframe 37,859 hrs · 36,697 cycles

DURING CRUISE @ 15000', NOTICED APU SOV OPEN AND ECU FAIL STATUS MESSAGES ON ED 2. AIR RETURN TO IAD. ***AIRCRAFT REMOVED FROM SERVICE*** INTEROGATED APU ECU FOUND NO LRU FALURES AND PREV CODES INDICATE DOOR ISSUES ONLY. CLEARED CODES AND CW OPERATIONAL CHECK OF APU IAW AMM 49-10-00. OPS CHECK GOOD.

Part: NONE — NONE · airframe 37,770 hrs · 36,604 cycles

DISPLAY COOL MESSAGE IN FLIGHT. C/W QRH MESSAGE REMAINS. ***AIRCRAFT REMOVED FROM SERVICE*** FOUND DISPLAY COOLING DUCT DETACHED FROM PLENUM UNDER PILOTS DISPLAYS. RE SECURED DUCT IAW AMM 21-24-22 OPERATIONAL TEST IS GOOD.

Part: NONE — NONE · airframe 37,755 hrs · 36,588 cycles

DURING DECENT RIGHT ENGINE BECAME UNRESPONSIVE AT LOW TO MID POWER SETTING. WAS ABLE TO SHUT DOWN ENGINE WITH THROTTLE QUADRENT. NO EICAS MSGS PRESENT. ***AIRCRAFT REMOVED FROM SERVICE*** R/R #2 ENGINE IAW MAINTENANCE TASK CARD 000-71-400-002AW TASK CARD 000-71-400-003AW AND AMM 71-00 OPS CHECK GOOD LEAK CHECK GOOD. RII QC013

Part: WARNING MESSAGE — ILLUMINATED (TE FLAPS) · airframe 37,019 hrs · 35,832 cycles

RECEIVED FLAP FAIL CAUTION ON CLIMB OUT OF ORD WITH FLAPS AT ZERO RETURNED TO ORD FOR UNEVENTFUL LANDING AFTER C/W QRH. NOTE FLAPS WERE ON MEL AT THE TIME. AIRCRAFT REMOVED FROM SERVICE. REPLACED RH BPSU REF AMM 27-51-10 FECU ABORTS BPSU TEST.

Part: WARNING MESSAGE — ILLUMINATED (TE FLAPS) · airframe 37,017 hrs · 35,829 cycles

RECEVED FLAP FAIL CAUTION AT ZERO DEGREES. DECLARED EMERG. SMOOTH UNEVENTFUL LANDING MAX BTMS 7. PERFORMED FLAP RESET PROCEEDURE IAW AWAC SUP 98-018I BOX 12. FLAPS RESET. AIRCRAFT REMOVED FROM SERVICE. REPLACED RH BPSU REF AMM 27-51-10 FECU ABORTS BPSU TEST.

Part: BPSU — FAULTED (TE FLAP SYSTEM) · airframe 36,744 hrs · 35,548 cycles

FLAPS FAIL MESSAGE AT 30 THOUSAND FT.CREW REPORTED AFTER ENCOUNTERING MODERATE TURBULENCE OVER MUSCLE SHOALS VOR WHILE IN CRUISE FLIGHT, A FLAPS FAILURE OCCURRED AT 0 DEGREES. CAPTAIN STATED HE WILL DECLARE AN EMERGENCY WHILE ON ARRIVAL TO ORD. FLIGHT IS CONTINUING ON TO ORD. PERFORMED FLAP RESET PROCEDURE IAW AWAC SUP 98-18I BOX 12.FLAPS RESET. PLACARDED AND PLACED ON MEL ***AIRCRAFT REMOVED FROM SERVICE*** T/S TO FAULTY RH BPSU. REMOVE AND REPLACED RH BPSU. OPS CHECKS GOOD. REF AMM 27-51-10. REMOVE PLACARD. REMOVE MEL. RII-YES. INSP#I-285

Part: FLAP SYSTEM — FAILED · airframe 36,744 hrs · 35,548 cycles

FLAPS FAIL MESSAGE AT 30 THOUSAND FT.CREW REPORTED AFTER ENCOUNTERING MODERATE TURBULENCE OVER MUSCLE SHOALS VOR WHILE IN CRUISE FLIGHT, A FLAPS FAILURE OCCURRED AT 0 DEGREES. CAPTAIN STATED HE WILL DECLARE AN EMERGENCY WHILE ON ARRIVAL TO ORD. FLIGHT IS CONTINUING ON TO ORD. PERFORMED FLAP RESET PROCEDURE IAW AWAC SUP 98-18I BOX 12.FLAPS RESET. PLACARDED AND PLACED ON MEL ***AIRCRAFT REMOVED FROM SERVICE*** MX IN PROGRESS

Part: FLAP SYSTEM — OUT OF TOLERANCE · airframe 36,476 hrs · 35,272 cycles

FLAPS FAIL CAUTION AT 0 DEG DURING CRUISE AT FL340. AFTER NORMAL LANDING, BTMS TEMP NR 3 BRAKE - 2. PERFORMED FLAP RESET PROCEDURE, IAW AWAC SUPP 98-18I BOX 12. FLAPS RESET. PLACARDED AND PLACED ON MEL. AIRCRAFT REMOVED FROM SERVICE. FOUND FLAP BPSU LEFT/RIGHT DIFFERENTIAL TOO GREAT. RERIGGED LEFT AND RIGHT FLAP BPSU'S, REFERENCE AMM 27-51-10. OPERATIONS CHECK GOOD. REMOVED PLACARD+ REMOVED FROM MEL.

Part: ECU — MALFUNCTIONED (TE FLAPS) · airframe 36,451 hrs · 35,242 cycles

DURING CLIMB OUT AT FLAP RETRACTION ALTITUDE FLAP FAILED AT 6 DEGREES. LAST GOOD POSITION 8 DEGREES, RETRACTING FROM 8 TO ZERO AND NO OTHER INDICATIONS. AIRCRAFT REMOVED FROM SERVICE. TROUBLESHOT, IAW FIM 27-50-00. DURING TSING FECU FAILED SELF TEST. REMOVED AND RPELACED FECU, IAW AMM 27-50. OPERATIONS CHECK GOOD.

Part: PDU — FAULT MESSAGE (TE FLAPS) · airframe 36,440 hrs · 35,231 cycles

ON FINAL FLAPS FAILED AT 8 DEGREES. WE WENT AROUND, CLIMBED TO 10,000' COMPLIED WITH QRH AND RETURNED FOR LANDING. NO BRACE OR EMERGENCY DECLARED. AIRCRAFT REMOVED FROM SERVICE. INTERRROGATED THE FECU, IAW FIM 27-50. FOUND NUMEROUS FAULT CODES FOR THE PDU. R & R FLAP PDU, IAW AMM 27-52-01. OPERATIONS CHECK GOOD, REMOVED FROM PLACARD AND REMOVED FROM MEL.

Part: BPSU — FAILED (TE FLAPS) · airframe 36,415 hrs · 35,202 cycles

CREW RECEIVED FLAP FAIL ON APPROACH INTO ORD AT 0. CREW BROKE OFF APPROACH AND ARE NOW GETTING READY GET BACK ON FINAL. FLAPS FAIL CAUTION MESSAGE WHEN FLAPS WERE SELECTED ZERO TO 8 DEG IN FLIGHT. FLAPS FAILED AT ZERO DEGREES PEAK BTMS 6,4,9,7. QRH WAS C/W FLAPS FAIL LANDING PERFORMED. FLAPS WERE ALREADY ON MEL FROM TWO FLIGHTS PREVIOUSLY. AFTER EMERGENCY DEBRIEF, MX PULLED CODES AND A/C IS FERRYING TO MKE FOR REPAIR. EMERGENCY WAS DECLARED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED RT BPSU, IAW AMM 27-51 00 FLAP OPERATION CHECKS GOOD. REMOVE PLACARD AND REMOVE FROM MEL.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 36,382 hrs · 35,164 cycles

FLAP FAIL CAUTION MESSAGE WITH FLAPS ZERO AT FINAL APPROACH. PERFORMED FLAP RESET PROCEDURE, IAW AWAC SUPPLEMENT 98-18I BOX 11, FLAPS RESET. PLACARDED AND PLACED FLAPS ON MEL. AIRCRAFT REMOVED FROM SERVICE. INTERROGATED FECU, TROUBLESHOOT PER FIM 27-50-00, BPSU, WIRING INTEGRITY CHECK GOOD, PER ESPM 20-12-01. FLAP FUNCTIONAL TEST GOOD, PER AMM 27-51-05. BPSU TEST GOOD, PER AMM 27-51-10. COULD NOT DUPLICATE, REMOVED FROM MEL OK FOR SERVICE. PLACARD REMOVED.

Part: FLOORBEAM — CORRODED (BS 572) · corrosion level 2 · airframe 36,338 hrs · 35,112 cycles

REMOVED NUTPLATE AND FOUND AREA HAD CORROSION OUT OF LIMITS ON FLOOR BEAM AT RBL 9 STA FS 572, IAW SRM53-61-13. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FLOOR BEAM, IAW DRAWING 601R35031.

Part: SEAT TRACK — CORRODED (BS 424-559) · corrosion level 2 · airframe 36,338 hrs · 35,112 cycles

CLEANED LT & RT SEAT TRACKS FS 424 & FS 559. RT HAND SEAT TRACK RBL 9 CORRODED AND FOUND TO BE OUT OF LIMITS. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK, IAW REO 601R-53-00-764.

Part: PROXIMITY SENSOR — OUT OF ADJUST (RIGHT MLG) · airframe 36,333 hrs · 35,108 cycles

GEAR RETRACTION RECEIVED GEAR DISAGREE WARNING RT MAIN DID NOT RETRACT SELECTING 3B AND 2B ON. RECEIVED 3 GREEN AFTER SELECTING MANUAL RELEASE. MSG APPEARED WITH IN 6 SECOND OF SELECTING GEAR UP WITH LT MAIN AND NOSE AMBER AND RT MAIN RED. AIRCRAFT REMOVED FROM SERVICE ADJUSTED RT MLG UPLOCK PROX SENSOR AND SECURED TARGET. CHECKS GOOD, PER AMM CH 32. PLACARD REMOVED. CLEARS MEL 32-30-01.

Part: PUMP — MALFUNCTIONED (HYDRAULIC SYS) · airframe 36,257 hrs · 35,025 cycles

RH MLG DISAGREE ON CLIMB AFTER GEAR SELECTED UP. "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED #3A HYD PUMP PER AMM 29-12-03 OPS/LEAK CHECK GOOD PERFORMED FUNCTIONAL TEST OF LANDING GEAR EXTENSION AND RETRACTION PER AMM 32-30-00 OPS CHECK GOOD. NO DEFECTS NOTED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 34,072 hrs · 32,893 cycles

LEFT THRUST REVERSER UNLOCK MESSAGE INFLIGHT. THRUST REVERSER DID NOT DEPLOY. CW QRH.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 33,801 hrs · 32,627 cycles

INDICATION NOTED AT FS 621.00 REAR PRESSURE BULKHEAD FWD FACE AT LBL36.0, WL 79.30 - 80.30 1" LONG AND 100% FULL SCREEN HEIGHT, FAILING NDT. REPAIRED FS 621.00 REAR PREASURE BULKHEAD IAW REO 601R-53-61-1240 REV D AND 601R-53-61-6775 REV-.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 33,801 hrs · 32,627 cycles

L/H INBOARD FLAP HAS APPROX. 1" X 1" DENT BETWEEN W.S.47.61 AND W.S.56.30 (LOWER SIDE). REPAIRED L/H INBD FLAP LOWER SKIN IAW EA# AWAC-CRJ257-01096.

Part: CHANNEL — CRACKED (BS 621- 625) · airframe 33,801 hrs · 32,627 cycles

CHANNEL BETWEEN F.S.621.00 AND F.S.625.30 AT STGR 13L OUTBD OF LBL36.2 IS CRACKED.

Part: SEAT TRACK — CORRODED (BS 559+64-80) · corrosion level 2 · airframe 33,801 hrs · 32,627 cycles

L/H SIDE SEAT RAIL IS CORRODED BETWEEN F.S.559+64 TO F.S.559+80. REMOVED SIDE SEAT RAIL, FABRICATED NEW SERVICABLE SIDE SEAT RAIL AND INSTALLED IAW BOMBARDIER REO 601R-53-00-055 REV C DATED 2017-03-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,801 hrs · 32,627 cycles

LT SIDE SEAT RAIL IS CORRODED BETWEEN FS 559+64 TO FS 559+80. REMOVED SIDE SEAT RAIL, FABRICATED NEW SERVICEABLE SIDE SEAT RAIL AND INSTALLED IAW REO 601R-53-00-055 REV C DATED 2017-03-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,801 hrs · 32,627 cycles

LBL9 SEAT RAIL IS CORRODED BETWEEN FS 364 TO FS 379. REMOVED CORRODED SEAT RAIL AND INSTALLED NEW SERVICEABLE SEAT RAIL IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 364-400) · corrosion level 2 · airframe 33,801 hrs · 32,627 cycles

LBL9 SEAT RAIL IS CORRODED BETWEEN F.S.364 TO F.S.379. REMOVED CORRODED SEAT RAIL AND INSTALLED NEW SERVICABLE SEAT RAIL IAW CRJ 200 AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,801 hrs · 32,627 cycles

RBL 9 SEAT RAIL IS CORRODED BETWEEN FS 364 TO FS 409. REMOVED CORRODED SEAT RAIL FROM RBL9 BETWEEN FS 364 TO FS 409 AND INSTALLED NEW SERVICEABLE SEAT RAIL IAW REO 601R-53-00-485 REV C DATED 2017-12-18 AND AMM 53-01-11-400-802.

Part: INVERTER — INOPERATIVE (EMERGENC LIGHTS) · airframe 32,135 hrs · 30,912 cycles

DURING AN ACCEPTANCE CHECK, CREW REPORTED THE RIGHT OVERWING EXIT EMERGENCY SIGN WAS INOPERATIVE. REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHTS INVERTER IAW AMM 33-51-07, OPS CHECKED GOOD.

Part: INVERTER — FAILED (EMERGENCY LIGHTS) · airframe 32,103 hrs · 30,880 cycles

FLOOR EMERGENCY EXIT SIGN AT SEAT 8D INOPERATIVE. R & R THE INVERTER IAW AMM 33-51-07. OPS CHECKED GOOD.

Part: O-RING — LEAKING (HYD PUMP) · airframe 31,874 hrs · 30,663 cycles

IN CRUISE FLIGHT RECEIVED HYD 3 LOW PRESS CTN MESSAGE, HYD 3 QUANTITY 5 % , HYD 3 PRESS 2000. COMPLIED WITH QRH, HYD 3 B ACMP TURNED ON. UPON LANDING HYD 3 QUANTITY 5% AND PRESSURE 0. INSPECTED AND FOUND HYD PUMP 3A BALL ATTENUATOR LEAKING. REMOVED AND REPLACED HYD PUMP 3A BALL ATTENUATOR O-RINGS IAW AMM 29-12 INSPECTED SYSTEM 3 PRESSURE, RETURN, AND CASE FILTERS NO DEFECTS NOTED. OPS AND LEAK CHECKED GOOD.

Part: FLAP — MALFUNCTIONED (WING) · airframe 31,799 hrs · 30,595 cycles

FLAP FAIL CAUTION MESSAGE INFLIGHT FAILED AT ZERO DEGREES. PERFORMED FLAP REST PROCEDURES IAW SUP 98-018G. FLAPS RESET.

Part: ANGLE — CORRODED (BS 349) · corrosion level 2 · airframe 31,182 hrs · 30,032 cycles

RIGHT WINDSCREEN SUPPORT ANGLE AT BS 349, LBL 27-36 IS CORRODED

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,182 hrs · 30,032 cycles

CARGO FLOORBEAM AT FS 559+80 BETWEEN RBL9 AND LBL9 CORRODED. REPAIRED.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,182 hrs · 30,032 cycles

FRAME 333 HAS CORROSION ON THE FWD SIDE BETWEEN STR 23R AND 22R.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,182 hrs · 30,032 cycles

FRAME FS 333 CRACKED JUST I/B OF STR 1L.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 31,182 hrs · 30,032 cycles

INTERCOSTAL THAT ATTACHES TO STR 20R BTW FS 333-349 FRAMES HAS ELONGATED HOLES.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,182 hrs · 30,032 cycles

FLOOR LANDING ANGLE ON THE FWD SIDE OF THE 280 BEAM HAS CORROSION AROUND NUTPLATES ON BOTTOM SIDE.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 31,182 hrs · 30,032 cycles

AFT CARGO STA 559+112 RBL 9 CARGO TRACK IS CORRODED AND GOUGED.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 31,182 hrs · 30,032 cycles

PAX DOOR AFT RISER DRAG ANGLE CRACKED BY ASSIST PULLEY BRACKET.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,182 hrs · 30,032 cycles

FLOOR SUPPORT FS349 AT RT FLOOR SILL IS CORRODED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 31,182 hrs · 30,032 cycles

FLOOR LANDING ANGLE AT AFT SIDE OF FS280 HAS CORROSION BETWEEN LBL9 AND RBL13.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 31,182 hrs · 30,032 cycles

RT WING TO FUSELAGE FAIRING ATTACH STRUCTURE AT FS 439.00 IS CRACKED. REPLACED RT WING TO FUSELAGE FAIRING ATTACH ANGLE IAW SRM 51-42-06.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 31,182 hrs · 30,032 cycles

LT WING TO FUSELAGE FAIRING ATTACH STRUCTURE AT FS 449.85 IS CRACKED. REPLACED LT WING TO FUSELAGE FAIRING ATTACH STRUCTURE ANGLE IAW SRM 51-42-06.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 31,182 hrs · 30,032 cycles

RT WING TO FUSELAGE FAIRING ATTACH STRUCTURE AT FS 449.85 IS CRACKED. REPLACED ANGLE STRUCTURE AT RT WING STATION FS 449.85 IAW SRM 51-42-06.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 31,182 hrs · 30,032 cycles

LT WING TO FUSELAGE FAIRING ATTACH STRUCTURE AT FS 476.00 IS CRACKED. REPLACED LT WING TO FUSELAGE ATTACH STRUCTURE ANGLE AT FS 476.00 IAW SRM 51-42-06.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 31,182 hrs · 30,032 cycles

RT WING TO FUSELAGE FAIRING ATTACH STRUCTURE AT FS 470.00 IS CRACKED. REPLACED RT WING TO BODY FAIRING ATTACH ANGLE IAW SRM 51-42-06.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 31,182 hrs · 30,032 cycles

RT WING TO FUSELAGE FAIRING ATTACH STRUCTURE AT FS 461.00 IS CRACKED. REPLACED ANGLE AT FS 461.00 RT SIDE WING TO FUSELAGE FAIRING SUPPORT IAW SRM 51-42-06.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,182 hrs · 30,032 cycles

RT FLOOR SILL 319.70 HAS CORROSION.

Part: FITTING — CRACKED (FUSELAGE) · airframe 31,182 hrs · 30,032 cycles

FS 484 CLIP AT RBL 27 CRACKED. REPLACED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 31,182 hrs · 30,032 cycles

FS 484 CLIP AT RBL 36 CRACKED. REPLACED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 31,182 hrs · 30,032 cycles

FS 484 CLIP AT LBL 27 CRACKED. REPLACED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 31,182 hrs · 30,032 cycles

CLIP AT FS 484 AND LBL 36 CRACKED. REPLACED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 31,182 hrs · 30,032 cycles

FLIGHT DECK CENTER WINDSHIELD POST LT LOWER FITTING IS CRACKED. REPLACED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 31,182 hrs · 30,032 cycles

LT WINDSHIELD SIDE POST LOWER OUTBD CLIP CRACKED. REPLACED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 31,182 hrs · 30,032 cycles

FLIGHT DECK CENTER WINDSHIELD POST RT LOWER FITTING IS CRACKED. REPLACED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 31,182 hrs · 30,032 cycles

I/B CLIP AT STR 3L FS 280 IS CRACKED.

Part: WIRE HARNESS — DEFECTIVE (CABIN) · airframe 30,990 hrs · 29,859 cycles

1ST ROW AMBER EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE. R & R ROW 1 EMERGENCY TRACK LIGHT HARNESS. OPS CHECK GOOD IAW AMM 33-51-01.

Part: ATTENUATOR — LOOSE (HYDRAULIC SYS) · airframe 30,967 hrs · 29,835 cycles

DURING CLIMBOUT OBSERVED NR 1 HYD SYS QUANTITY DECREASES FROM 55 PERCENT TO 45 PERCENT. INSPECTED AND FOUND HYDRAULIC FLUID SEEPING OUT OF NR 1 HYDRAULIC ACMP VALVE ATTENUATOR ASSEMBLY, RETIGHTENED NR 1 HYD ACMP VALVE ATTENUATOR REF AMM 29-11-03. BLED NR 1 HYD SYSTEM IAW AMM 29-10-00. RESERVICED NR 1 HYD SYSTEM IAW AMM 12-00-06, LEAK CHECK GOOD AND QTY LEVEL GOOD.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 30,939 hrs · 29,886 cycles

INOPERATIVE CAUTION MSG IN FLT. CW QRH AND MESSAGE REMAINED. OCCURRED AT FLT LEVEL 200. NR 3 HYDRAULIC PRESSURE NORMAL AND STEERING TILLER CENTERED. CW FIM FAULT RESET MESSAGE DOES NOT CLEAR.

Part: DOOR — BINDING (MAIN PAX) · airframe 30,658 hrs · 29,538 cycles

ON ARRIVAL AT THE GATE, FA INFORMED THE PILOT THAT THE MAIN PASSENGER DOOR AS DIFFICULT TO OPEN. DOOR DID OPEN.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,981 hrs · 27,981 cycles

EMERGENCY FLOOR TRACK LIGHTS AFT OF ROW 11 INOPERATIVE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,822 hrs · 27,818 cycles

EMERGENCY LIGHTS WOULD NOT ILLUMINATE AFT OF ROW 8.

Part: UNKNOWN — NOISE (CABIN)

AFTER TAKEOFF AT APPROX 6000 FT, FLIGHT CREW NOTICED AN INTERMITTENT THUMP OCCURRING, FELT MOSTLY IN THE FLOORBOARDS. FLIGHT ATTENDANT REPORTS THE NOISE WAS PRESENT SOONER THAN FLIGHT CREW NOTICED IT. MOST NOTICEABLE IN FWD CABIN AREA. NO ABNORMAL INDICATIONS OR FEEL IN FLIGHT CONTROLS, ENGS, APU OR PRESSURIZATION. RETURNED & NOISE CONTINUED UNTIL LANDING.

Part: UNKNOWN — ODOR (LAVATORY) · airframe 27,710 hrs · 26,733 cycles

FL 3762 CLEANERS REPORT POSSIBLE BURNING ODOR IN LAVATORY. INSPECTED LAVATORY AREA FOR POSSIBLE ODOR. NO BURNING ODOR NOTED. ALSO CHECKED CABIN AREA, NO ODOR DETECTED.

Part: PRESSURE SWITCH — MALFUNCTIONED (LT ENGINE OIL) · airframe 27,594 hrs · 26,611 cycles

AFTER TAKEOFF, RECEIVED NUMEROUS LT ENGINE OIL WARNING MESSAGES ALONG WITH A FLUCTUATION OF LT LOW OIL PRESSURE INDICATIONS. OIL PRESSURE NEVER DROPPED BELOW 5 PSI. DECLARED AN EMERGENCY. COMPLIED WITH QRH & RETURNED TO DEPARTURE. R & R OIL PRESSURE TRANSDUCER IAW 79-31-05. R & R LOW OIL PRESSURE SWITCH AMM 71-31-03. OPS CHECKED GOOD IAW AMM 80-10-00.

Part: FITTING — CRACKED (COCKPIT) · airframe 26,495 hrs · 25,565 cycles

RT WINDSHIELD POST LOWER CLIP CRACKED.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 26,495 hrs · 25,565 cycles

LT INTERCOSTAL MEMBER ON THE AFT FACE OF THE FS 621 BULKHEAD AT STRINGER 14L IS CRACKED.

Part: DRAG ANGLE — CRACKED (RT WING) · airframe 26,495 hrs · 25,565 cycles

RT WW DRAG ANGLE COMMON TO BATTERY RIB IS CRACKED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 26,495 hrs · 25,565 cycles

AFT 621 BULKHEAD LT & RT UPPER OBLIQUE ANGLE IS CRACKED.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 26,495 hrs · 25,565 cycles

DURING INSTALL OF AFT BRAKE PRESS TRANSDUCER BRACKET FOUND FWD BRACKET CRACKED.

Part: STRUCTURE — CRACKED (LT WING) · airframe 26,496 hrs · 25,565 cycles

LT WING INBD LE IS CRACKED AT LOWER SCREW HOLE.

Part: MOUNT BRACKET — CRACKED (PAX DOOR) · airframe 26,496 hrs · 25,565 cycles

PAX DOOR POWER ASSIST MOTOR MOUNT BRACKET CRACKED.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 26,496 hrs · 25,565 cycles

LT INTERCOSTAL AFT OF FS 621 AT STRINGER 16L IS CRACKED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,495 hrs · 25,565 cycles

LT & RT FLOOR SEAT TRACKS AT FS 364 TO 394 HAS CORROSION.

Part: HINGE BRACKET — DEFORMED (VERTICAL STAB) · airframe 26,496 hrs · 25,565 cycles

ON VERTICAL STAB AFT SPAR, UPPER CTR RUDDER HINGE BRACKET LOWER HALF BORE MALFORMED.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 26,496 hrs · 25,565 cycles

INBD & OTBD FLOORBEAM ATTACH CLIPS AT LBL 9 & RBL 9 AT FS 280 ARE CRACKED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,496 hrs · 25,565 cycles

FLOORBEAM CAP AT LBL 27 FROM FS 559 + 112 TO 621 HAS CORROSION.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,496 hrs · 25,565 cycles

PAX DOOR SILL LOWER SUPPORT ANGLE CORRODED.

Part: BRACKET — CRACKED (RT MLG WW) · airframe 26,496 hrs · 25,565 cycles

RT MLG WW BRAKE TRANSDUCER BRACKET CRACKED.

Part: BRACKET — CRACKED (LT MLG WW) · airframe 26,496 hrs · 25,565 cycles

LT MLG WW BRAKE TRANSDUCER BRACKET CRACKED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 25,678 hrs · 24,802 cycles

CARGO BOTTLE LOW CAUTION MSG IN FLT. COMPLIED WITH QRH. ACFT LANDED OVERWEIGHT, 48123 LANDING WT. MSG CLEARED AFTER LANDING WITH BLEEDS SWITCHED TO APU CARGO BOTTLE PRESS SWITCH SUSPECTED INTERMITTENTLY INOPERATIVE. COMPLIED WITH VISUAL INSPECTION OF CARGO BOTTLE PRESS GAUGES IAW AMM 26-25-01, NO DISCREPANCIES NOTED. ALSO COMPLIED WITH OVERWEIGHT LANDING ANALYSIS IAW AMM 05-51-01 HARD & OVERWEIGHT LANDING DID NOT TAKE PLACE. R & R CARGO BOTTLE A4HL IAW AMM 26-52-01 OPERATIONS CHECKED GOOD BOTTLE LO MSG DISPLAYED SN OFF 21659F1 & SN ON 24292F1.

Part: ENGINE — CONTAMINATED · airframe 24,907 hrs · 24,059 cycles

CABIN & COCKPIT FILLED WITH SMOKE & FUMES ONCE BLEEDS WERE TRANSFERRED TO ENGINES. SWAPPED BLEEDS BACK TO APU & SMOKE & FUMES STOPPED. CONTACTED MX & CONFIRMED THIS WAS 1ST FLIGHT AFTER COMPRESSOR CLEANING. SUSPECT RESIDUAL CHEMICALS FROM COMPRESSOR WASH. RETURNED TO PHL, NO EMERGENCY DECLARED, UNEVENTFUL LANDING. PERFORMED ENG RUN IAW AMM 71-00-00 FOR 20 MINUTES. NOTED NO ODOR OR SMOKE AT THIS TIME.

Part: CONTROL UNIT — MALFUNCTIONED (STAB TRIM) · airframe 23,535 hrs · 22,732 cycles

STAB & MACH TRIM DISENGAGED IN FLT C/W QRH UNABLE TO RE-ENGAGE EITHER STAB TRIM CHANNEL( WOULD RE-ENGAGE BUT WOULD DIS-ENGAGE WHEN TRIM WAS MOVED) BTMS 8,7,6,6. HSTCU WAS SIEZED R&R HSTCU PER AMM 27-41-01-04.

Part: SERVO — DEFECTIVE (AILERON) · airframe 21,773 hrs · 21,021 cycles

IN CLIMB & CRUISE EXPIERINCED SLIGHT DUTCH ROLL MOVEMENT WITH ASSOCIATED LEFT WING DOWN AILIERON INDICATION. REF WO 193452 FOR ALL WORK PERFORMED REPLACED AILERON SERVO AND FCC # 2 AND ACCOMPLISHED FLIGHT CONTROL RIG AND OP CHECKS.

Part: GUARD — CRACKED (FUSELAGE) · airframe 21,668 hrs · 20,915 cycles

RAIN / DRIP GUARD ABOVE PAX DOOR CUTOUT IS CRACKED IN HALF AND DISBONDING. COMPLIED WITH REO 601R-53-22-015 DATED AUGUST 14, 2003 BY REMOVING LOOSE SECTION OF RAIN GUARD & RESTORING FINISH.

Part: BRACKET — GOUGED (ESCAPE HATCH) · airframe 21,668 hrs · 20,915 cycles

STOP BRACKET ON THE SIDE OF THE CREW ESCAPE HATCH IS GOUGED. REPAIRED IAW REO 601R-52-22-028.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,668 hrs · 20,915 cycles

CARGO BAY FLOOR LEVEL FS 574 & FS 621 LBL 29 FLOORBEAM TOP CAP HAS LIGHT TO MODERATE CORROSION AT NUT PLATE. REPAIRED CARGO BAY FLOOR LEVELS FS 574 TO 621 LBL 29 FLOORBEAM TOP CAP IAW B/A REO 601R-53-00-493 REV - AND CRJ 200 SRM 53-00-43, FIG 203 SHT 2.

Part: SKIN — DENTED (TRANS COWL) · airframe 21,668 hrs · 20,915 cycles

RIGHT UPPER TRANS COWL OUTER SKIN DENTED, 4 SPOTS. DRILLED & FILLED DENTS IAW CMM 78-30-00 & REO 601R-78-33-4006 REV NC.

Part: FITTING — DAMAGED (LT MLG TRUNNION) · airframe 21,668 hrs · 20,915 cycles

DURING COLD WORKING OF THE MLG TRUNNION FITTING LOWER FLANGES FOUND 1 OVER SIZED HOLE IN LEFT SIDE. REPAIRED HOLE IN LEFT MLG TRUNNION FITTING LOWER FLANGE IAW REO 601R-57-21-1775 REV-.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 21,668 hrs · 20,915 cycles

PAX DOOR AFT DRAG ANGLE CRACKED. REMOVED & REPLACED PAX DOOR AFT DRAG ANGLE PREVIOUS REPAIR ANGLE, UPPER SPLICE & LOWER SPLICE ANGLE IAW REO 601R-52-11-563 REV A.

Part: FITTING — CRACKED (FUSELAGE) · airframe 21,668 hrs · 20,915 cycles

CRACKED LOWER CLIP ON FS 621 ON CARGO BAY DOOR SUPPORT STRUCTURE AT LBL 36. REMOVED & REPLACED LOWER CLIP IAW CRJ 200 53-61-23 & CRJ 200 SRM 51-42-21.

Part: SKIN — CHAFED (CARGO DOOR) · airframe 21,668 hrs · 20,915 cycles

CARGO DOOR OUTER SKIN CHAFED AT TOP CENTER OF DOOR. BLENDED OUT CHAFE DAMAGE AND FOUND TO BE WITHIN LIMIT IAW CRJ 200 SRM 52-00-31.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 21,668 hrs · 20,915 cycles

CARGO BAY LEFT FLOOR EDGE MEMBER HAS CRACKS AT FS 589 AND FS 605 BOTH CRACKS ARE JUST I/B OF CARGO DOOR STOPS. CUT OUT DAMAGE AREA OF FLOOR LANDING PLATE AT FS 589 & FS 605 IAW REO 601R-53-61-433 REV B.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 21,668 hrs · 20,915 cycles

CARGO BAY LEFT FLOOR EDGE MEMBER, FS 574 TO FS 621 HAS MODERATE CORROSION ON TOP SURFACE AT NUT PLATE, SOME CORROSION UNDER NUT PLATES. BLENDED CORROSION LEFT CARGO DOOR FLOOR EDGE MEMBER FS 574 TO FS 621 FOUND TO BE WITHIN LIMITS IAW CRJ SRM 53-00-00, FIG 102.

Part: VANE — CHAFED (TE FLAP) · airframe 21,668 hrs · 20,915 cycles

LEFT AND RIGHT FLAP VANE VENT L/E CHAFED. BLENDED 5 EA AREAS ON RIGHT & LEFT FLAP VANE L/E FOUND 5 AREAS TO BE WITHIN ALLOWABLE DAMAGE LIMITS. LEFT INBOARD FLAP VANE L/E OUT OF ALLOWABLE LIMITS, REMOVED UNSERVICEABLE L/E AND INSTALLED SERVICEABLE L/E IAW REO 601R-57-52 REV C CRJ 200 SRM 51-42-11, 51-42-13.

Part: DOOR — CHAFED (LT MLG) · airframe 21,668 hrs · 20,915 cycles

LEFT MLG DOOR IS CHAFED THREE PLACES ON THE LEADING EDGE. REPAIRED O/B CORNER ON LEFT MLG DOOR L/E IAW BOMBARDIER REO 601R-52-82-034 REV NC, REPAIRED TWO CHAFED AREAS IAW CRJ SRM 52-82-00, 51-12-00, 51-21-11, 51-25-06, 51-25-16.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 21,668 hrs · 20,915 cycles

CARGO TIE DOWN TRACKS AT FS 559+110 -559+121 LBL & RBL 9 HAVE MODERATE CORROSION ENTIRE LENGTH OF TRACK. REMOVED & REPLACED 4EA CARGO TIE DOWN TRACKS IAW CRJ 200 SRM 51-41-02.

Part: GUIDE — DAMAGED (TE FLAP) · airframe 21,668 hrs · 20,915 cycles

RIGHT O/B FLAP CENTER HINGE ARM GUIDE DAMAGED. FAB SERVICEABLE BRACKET P/N 601R14629 IAW CRJ 200 SRM 51-54-00 AND 51-42-06.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 21,668 hrs · 20,915 cycles

CARGO TIE DOWN TRACK AT FS 612 TO FS 617 LBL 9 HAS MODERATE CORROSION ENTIRE LENGTH OF TRACK. REMOVED CORRODED SEAT TRACKS AND INSTALLED NEW SEAT TRACK IAW CRJ 200 SRM 51-41-02.

Part: SKIN — CHAFED (LT MLG DOOR) · airframe 21,668 hrs · 20,915 cycles

LEFT MLG DOOR INNER SKIN IS CHAFED IN 4 PLACES. REPAIRED CHAFES ON LEFT MLG DOOR INNER SKIN IAW 51-12-00, 52-82-00, 51-24-21, 51-42-13.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 21,668 hrs · 20,915 cycles

CARGO TIE DOWN TRACKS AT FS 559+78 TO FS 559+95 LBL 27 AND RBL 27 HAVE LIGHT TO MODERATE CORROSION. REMOVED CORRODED SEAT TRACKS AND INSTALLED NEW SEAT TRACKS IAW CRJ 200 SRM 51-41-02.

Part: MONITOR — MALFUNCTIONED (EFIS) · airframe 21,144 hrs · 20,423 cycles

REJECTED TAKE OFF AT 58 KTS FOR EFIS COMP MON HEADING, BTMS READS 4, 4, 3, 3. PERFORMED OPS TEST OF AHRS IAW AMM 34-21-01. OPS CHECKED GOOD.

Part: STRUCTURE — CHAFED (MLG DOOR) · airframe 21,763 hrs · 21,706 cycles

LEFT AND RIGHT MLG DOORS L/E CHAFED. CUTTING AWAY DAMAGED INNER SKIN ON LT MLG DOOR. BLENDED AND SMOOTHED MINOR CHAFING IAW REO 601R-52-82-034 & 601R-52-82-102

Part: APU — CONTAMINATED · airframe 19,727 hrs · 18,963 cycles

ABORTED TAKE OFF AT AROUND 40 KTS FOR APU OVERTEMP, FOLLOWED BY APU SHUTDOWN AND APU FAULT CAUTION MESSAGE. FOUND GYLCOL INGESTED IN APU INTAKE. R & R APU ASSY REF AMM 49-10-00. OPS AND LEAK CHECKED GOOD AT THIS TIME.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 19,203 hrs · 18,406 cycles

LT WINDSHIELD DELAMINATION. M/C WINDSHIELD IS CRACKED. R & R LT WINDSHIELD IAW AMM 56-11-01. OPS CK WINDSHIELD TEMP CONTROLLER IAW AMM 30-41-01. OPS CHECKS GOOD, REF AMM 229617/4 ROR PRESSURIZATION AND LEAK CK OF ACFT.

Part: WARNING LIGHT — FALSE ACTIVATION · airframe 18,804 hrs · 17,989 cycles

ABORTED T/O FOR T/O CONFIG WARNING AT 106 KNOTS BRAKE TEMPS 7, 6, 6, 5. INSPECTED ALL TIRES AND FOUND TO BE OK FOR SERVICE. HAD CREW C/W CONFIG TEST. OPS CHECKED GOOD IAW AMM 31-41-00.

Part: UNKNOWN — UNKNOWN · airframe 18,804 hrs · 17,989 cycles

ABORTED TAKE OFF FOR T/O CONFIGURATION WARNING AT 106 KNOTS BRAKE TEMPS 7, 6, 6, 5. INSPECTED ALL TIRES AND FOUND TO BE OK FOR SERVICE. HAD CREW C/W CONFIGURATION TEST. OPS CHECKED GOOD IAW AMM 31-41-00.

Part: TRANSMITTER — INOPERATIVE (LT WING TE FLAPS) · airframe 18,792 hrs · 17,972 cycles

IN CLIMB, FLAPS RETRACTED TO ZERO NORMALLY AND LT FLAP INDICATION MOVED TO 7 DEGREES, THEN BACK TO ZERO. FLAPS OPERATED EXTENDED NORMALLY FOR LANDING AND RETRACTED AFTER LANDING. R & R LT FLAP POSITION TRANSMITTER UNIT.

Part: RIB — CRACKED (RT WING) · airframe 17,715 hrs · 16,835 cycles

RT BATT RIB CRACKED. REPAIRED RT BATT RIB IAW REO 601R-57-046, REV B AND REO 601R-57-51-507.

Part: SKIN — DAMAGED (LT WING) · airframe 17,715 hrs · 16,835 cycles

LT WING OTBD L/E HAS ELONGATED FASTENER HOLES WS 386..48 (4 EA). REPAIRE (4EA) DAMAGED HOLES IAW REO 601R-57-41-751.

Part: SKIN — CHAFED (LT WING AILERON) · airframe 17,715 hrs · 16,835 cycles

LT AILERON UPPER AND LWR L/E SKIN CHAFED. REPAIRED LT AILERON UPPER AND LWR L/E SKIN IAW REO 601R-57-60-013 AND REO 601R-57-60-020.

Part: MOUNT — CHAFED (LT ENGINE) · airframe 17,715 hrs · 16,835 cycles

UPON INSTALLATION OF ANTI-ICE DUCT, FOUND CHAFING ON LT ENG FWD MOUNTS ATTACH STRUCTURE. REPAIR LT FWD ENG MOUNTS ATTACH STRUCTURE IAW REO 601R-54-51-102.

Part: SKIN — CHAFED (RT WING AILERON) · airframe 17,715 hrs · 16,835 cycles

RT AILERON UPPER AND LOWER L/E SKIN CHAFE. REPAIR AILERON UPPER AND LOWER L/E SKINS AND REO 601R-57-60-013 REV NC AND REO 601R-57-60-020, REV NC.

Part: FLOORBEAM — DAMAGED (BS 559) · airframe 17,715 hrs · 16,835 cycles

FS559, LBL9 INBD AND OTBD POSTS MISDRILLED INTO FLOORBEAM. REPAIRED MISDRILLED HOLES IAW REO 601R-53-41-1374, REV A SEATING B & C.

Part: PLATE — CHAFED (RT WING TE FLAP) · airframe 17,715 hrs · 16,835 cycles

RT INBD FLAP INBD HINGE LOT PLATE CHAFED. BLENDED IAW REO 601R-57-52-1536, TYPE 1 ZONE A.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 17,715 hrs · 16,835 cycles

PAX DOOR STAIR STRUCTURE AFT SIDE CRACKED UNDER STEP. CUT OUT CRACKED SECTION ON AFT SIDE OF STAIR STRUCTURE THEN FABRICATED NEW SECTION AND INSTALLED IAW REO 601R-52-11-702, REV C.

Part: FITTING — CRACKED (BS 461) · airframe 17,715 hrs · 16,835 cycles

BATHTUB FITTING AT RBL 9 AND FS 461 IS CRACKED. R & R BATHTUB FITTING AT FS 461, RBL 9 IAW SRM 51-42-21, 51-42-06.

Part: SKIN — CHAFED (CARGO DOOR) · airframe 17,715 hrs · 16,835 cycles

CARGO DOOR HANDLE CUTOUT CHAFED IN 4 LOCATIONS. REPAIRED IAW REO 601R-52-31-086.

Part: SKIN — CHAFED (LT NACELLE) · airframe 17,715 hrs · 16,835 cycles

LT LOWER COWL CHAFED BY FWD LATCHES DAMAGED WITHIN BLENDABLE LIMITS AND REPAIRED IAW REO 601R-71-12-2326.

Part: ANGLE — CRACKED (LT PYLON) · airframe 17,715 hrs · 16,835 cycles

LT PYLON PANEL 410BT ANGLE CRACKED. R & R LT PYLON PANEL 410BT ANGLE IAW SRM 51-42-06.

Part: FAIRING — CHAFED (LT EXHAUST) · airframe 17,715 hrs · 16,835 cycles

LT JETPIPE FAIRING CHAFED FROM PYLON. REPAIRED LT JETPIPE IAW REO 601R-78-11-3960.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 17,715 hrs · 16,835 cycles

RT INBD FLAP VANE L/E SKIN CHAFED IN 3 PLACES. REPAIRED IAW REO 601R-57-52-004, REV C.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 17,715 hrs · 16,835 cycles

PAX DOOR STAIR STRUCTURE AFT SIDE CRACKED UNDER STEP CUT OUT CRACKED SECTION ON AFT SIDE OF STAIR STRUCTURE THEN FABRICATED NEW SECTION AND INSTALLED IAW B/A REO 601R-52-11-702, REV C.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 17,715 hrs · 16,835 cycles

OTBD RT 484.00, CLIP IS CRACKED. R & R -2 ANGLE (OTBD RT 484.00 CLIP) IAW REO 601R-53-41-509, REV B.

Part: INTERCOSTAL — CRACKED (BS 718) · airframe 17,715 hrs · 16,835 cycles

NR 2 HYD MANIFOLD INTERCOSTAL IS CRACKED AFT LOWER CORNER FWD SIDE INSTALLED CORNER BRACKET IAW REO 601R-53-62-031, REV A.

Part: HEAT SHIELD — CRACKED (APU ENCLOSURE) · airframe 17,715 hrs · 16,835 cycles

APU FWD HEAT SHIELD CRACKED. REPAIRED APU EXHAUST HEAT SHIELD IAW REO 601R-49-81-003.

Part: RIB — CRACKED (LT WING) · airframe 17,715 hrs · 16,835 cycles

LT MLG WHEEL WELL BATT RIB IS CRACKED. REPAIRED IAW REO 601R-57-51-046, REV B, REPAIR NR 2.

Part: STRUCTURE — CRACKED (APU ENCLOSURE) · airframe 17,715 hrs · 16,835 cycles

BACK OF APU ENCLOSURE IS CRACKED 4 SPOT AROUND TACK WELDS. REPAIRED CRACKS ON APU ENCLOSURE IAW REO 601R-49-11-070.

Part: SKIN — DENTED (BS 349) · airframe 17,715 hrs · 16,835 cycles

FUSELAGE SKIN AROUND PAX DOOR CUT OUT DENTED. COMPLIED WITH REO 601R-53-21-1251, DENT ACCEPTABLE AS FS.

Part: STRUCTURE — CRACKED (APU ENCLOSURE) · airframe 17,715 hrs · 16,835 cycles

APU ENCLOSURE LID HAS CRACK IN WELD AT TOP CENTER. REPAIRED CRACKS IN APU ENCLOSURE LID IAW REO 601R-49-11-070, REV A.

Part: FRAME — CORRODED (BS 333) · airframe 17,715 hrs · 16,835 cycles

FS 333.00, FRAME CORRODED IN FWD AVIONICS BAY. REMOVED DAMAGED AREA FROM FRAME IAW REO 601R-53-21-1253, REV C. INSTALLED SERVICEABLE PARTS, IAW REO 601R-53-21-1253, REV C.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 17,715 hrs · 16,835 cycles

CRACK AT STA 280 IN FLOORBOARD SUPPORT AT APPROX 12 LBL CUT AWAY DAMAGE SECTION AT STA 280 IN FLOORBOARD SUPPORT ANGLE AND INSTALLED NEW REPAIR ANGLE AND SPLICE ANGLES IAW REO 601R-53-11-138, REV A.

Part: PANEL — CORRODED (LT WING) · corrosion level 1 · airframe 17,715 hrs · 16,835 cycles

FUEL PANEL 510AB HAS FRETTING, CORROSION. REPAIRED FWD PANEL CUT OUT 510AB IAW REO 601R-57-21-030, REV H.

Part: STRUCTURE — DAMAGED (THRUST REVERSER) · airframe 17,715 hrs · 16,835 cycles

LT THRUST REVERSER HAS DRILL START 10TH HOLE FROM LT SIDE OF OPENING FOUND UNDER GRAY SEAL. REPAIRED DRILL START IN LT THRUST REVERSER 10TH HOLE FROM LT SIDE OF OPENING UNDER GRAY SEAL IAW REO 601R-78-30-4051, REV NC.

Part: STRUCTURE — DAMAGED (THRUST REVERSER) · airframe 17,715 hrs · 16,835 cycles

LT THRUST REVERSER HAS DOUBLE DRILLED HOLE 4TH HOLE FROM LEFT SIDE OF OPENING FOUND UNDER GRAY SEAL. REPAIRED DOUBLE DRILLED HOLES IN LT THRUST REVERSER 4TH HOLE FROM LT SIDE OF OPENING UNDER GRAY SEAL IAW REO 601R-78-30-4051, REV NCNB.

Part: PANEL — CORRODED (RT WING) · corrosion level 1 · airframe 17,715 hrs · 16,835 cycles

SUSPECTED PITTING ON INBD SIDE OF FUEL TANK OPENING 640BB. REPAIRED FUEL CUT OUT 640BB IAW REO 601R-57-21-030, REV H.

Part: STRUCTURE — GOUGED (THRUST REVERSER) · airframe 17,715 hrs · 16,835 cycles

LT THRUST REVERSER HAS 2 GOUGES UNDER GRAY SEAL. REPAIRED 2 GOUGES IN LT THRUST REVERSER UNDER GRAY SEAL IAW REO 601R-78-30-4051, REV NC.

Part: SEAL — DAMAGED (THRUST REVERSER) · airframe 17,715 hrs · 16,835 cycles

LT THRUST REVERSER FWD GRAY SEAL DAMAGED. REMOVED UNDERSERVICEABLE GRAY SEAL AND REPLACED WITH SERVICEABLE GRAY SEAL. LT THRUST REVERSER FWD IAW REO 601R-78-30-4057, REV NC.

Part: SKIN — ERODED (LT NACELLE) · airframe 17,715 hrs · 16,835 cycles

LT ENGINE NOSE COWL LIP SKIN PITTED & ERODED. REPAIRED LT ENGINE NOSE INLET COWL LIP SKIN IAW REO 601R-71-61-2532, REV C.

Part: PANEL — CHAFED (LT WING AILERON) · airframe 17,715 hrs · 16,835 cycles

LT AILERON PANEL 599BB CHAFED. REPAIRED LT AILERON LWR L/E PANEL 599BB IAW REO 601R-57-60-020.

Part: PANEL — CHAFED (LT WING AILERON) · airframe 17,715 hrs · 16,835 cycles

LT AILERON PANEL 599AB CHAFED. REPAIRED LT AILERON LWR L/E PANEL 599AB IAW REO 601R-57-60-020.

Part: PLATE — CHAFED (LT WING TE FLAP) · airframe 17,715 hrs · 16,835 cycles

LT INBD FLAP INBD HINGE LUG PLATE CHAFED. REPAIRED IAW REO 601R-57-15-3, TYPE 1, ZONE A.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 17,715 hrs · 16,835 cycles

LT INBD FLAP VANE L/E CHAFED AT 3 LOCATIONS. REPAIRED 3EA LOCATIONS ON LT INBD FLAP VANE L/E IAW REO 601R-57-52-0004, REV C.

Part: ACTUATOR — MALFUNCTIONED (THRUST REVERSER) · airframe 17,467 hrs · 16,586 cycles

LT THRUST REVERSER UNLOCK MSG IN FLIGHT, C/W`D QRH DIVERTED TO PIT. RESET ALL 4 BALLSCREW ACTUATORS TO PROPER POSITIONS AND REZEROED ON DOG STOPS. RECONNECTED TO TRACKS AND INSTALLED FLEX DRIVES IAW AMM 78-32-01. OPS CHECKED GOOD.

Part: CHANNEL — DAMAGED (TE FLAP) · airframe 17,206 hrs · 16,925 cycles

LT OTBD FLAP DAMAGED AT INBD T/E. REMOVED UNSERVICEABLE T/E CHANNEL AND REPLACED FOR NEW SERVICEABLE CHANNEL.

Part: BULKHEAD WEB — CHAFED (RT NACELLE) · airframe 17,206 hrs · 16,925 cycles

RT PAX INLET 12 O`CLOCK INSP DOOR HOLES ELONGATED AND AREA AROUND IS CHAFED/ GOUGED. REMOVED DAMAGED WEB SECTION AND REPAIRED IAW SHORTS CMM 71-61-101.

Part: ANGLE — CRACKED (BS 621) · airframe 17,206 hrs · 16,925 cycles

LT OBLIQUE ANGLE CRACKED. R & R LT OBLIQUE ANGLE IAW SRM 51-42-06, SRM 51-42-21, AND REO 601R-53-61-422.

Part: ENGINE — FAILED (RIGHT) · airframe 15,749 hrs · 14,767 cycles

WHILE IN CRUISE AT 30,000 FT HEARD BOOM WITH RT ENG ITT CLIMBING ABOVE 900C AT SAME TIME FELT ACFT YAW AND RECEIVED "FUEL LOW PRESS" MSG. EMERGENCY DECLARED PERFORMED ENGINE SHUTDOWN OF RT ENGINE AIR DIVERSION W/NORMAL LANDING RT ENG SHUTDOWN FOR 36 MINUTES IN FLIGHT. R & R RT ENG IAW 71-00-00. ALL WORK PERFORMED ON WO 154476.

Part: COALESCER BAG — CONTAMINATED · airframe 14,141 hrs · 13,139 cycles

AFTER BLEED TRANSFERE RECEIVED A STRONG BURNING RUBBER ODOR, APPEARED TO BE MORE IN COCKPIT THAN CABIN. REF WO 142295 W/C 1-5 FOR WORK COMPLETED. ODOR CAUSED BY COMP WASH FLUID THAT WAS NOT PROPERLY BURNED OFF. ALSO CHANGED COALESCER SOCKS. OPS CHECK GOOD. (K)

Part: PUMP — INOPERATIVE (HYD SYSTEM) · airframe 131,489 hrs · 12,514 cycles

HYD SYS NR1 QUANTITY DROPPED TO 25 PERCENT IN FLIGHT. REMOVED AND REPLACED ENG DRIVEN HYD PUMP NR 1 IAW AMM 29-11-01. OPS AND LEAK CHECKS GOOD. (K)

Part: FLOORBEAM — CRACKED (BS 280) · airframe 13,269 hrs · 12,294 cycles

LT PILOT - BULKHEAD FLOOR SUPPORT AT FS 280, LBL 9.0 FOUND CRACKED. REPAIR TO LT PILOT BULKHEAD FLOOR SUPPORT AT FS 280.00 LBL 9.0 CARRIED OUT IAW REO 601R-53-11-171. (K)

Part: STRUCTURE — CRACKED (BS 280) · airframe 13,269 hrs · 12,294 cycles

CLIP OF FS 280.00, LBL 9.0 INBD AND OTBD FOUND CRACKED IAW SRM 51-42-21. NEW CLIP OF FS 280.00 LBL 9.0 INBD AND OTBD INSTALLED. (K)

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 13,269 hrs · 12,294 cycles

CARGO DOOR FWD RAIL LOWER CHANNEL SUPPORT FOUND CRACKED 2 PLACES. CARGO DOOR FWD RAIL LWR SUPPORT REPLACED IAW SRM 51-42-06. (K)

Part: BRACKET — CRACKED (PAX DOOR) · airframe 13,269 hrs · 12,294 cycles

MWC 132379-184- PASSENGER DOOR FWD SIDE PANEL, RETAINING BRACKET (REF: PN 601R317727-1) FOUND CRACKED. PASSENGER DOOR FWD SIDE PANEL, RETAINING BRACKET (REF:PN 601R31727-1) REPLACED IAW SRM 51-42-21. (K)

Part: PANEL — CRACKED (PAX DOOR) · airframe 13,269 hrs · 12,294 cycles

MWC 132379-33 - PASSENGER DOOR AFT SIDE PANEL FOUND CRACK (REO 601R-52-11-702, ZONE2) CRACK LENGTH .150. REPAIR TO PASSENGER DOOR AFT SIDE PANEL CARRIED OUT IAW REO 601R -52-11-702, REV A.

Part: SILL — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 13,269 hrs · 12,294 cycles

SERVICE DOOR LOWER SILL, SCUFF PLATE FOUND CORRODED. SERVICE DOOR LOWER SILL PLATE REPLACED IAW SRM 51-42-02. (K)

Part: PRESSURE BLKHD — CRACKED (BS 202) · airframe 13,269 hrs · 12,294 cycles

PRESSURE BULKHEAD CRACK AT FS 202.75 (PARKING BRAKE CUTOUT AND LBL 23.71) FWD PRESSURE BULKHEAD AT FS 202.75, LBL 23.71. REPAIR PERFORMED IAW REO 601R-53-11-563. (K)

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 13,269 hrs · 12,294 cycles

HYD SUPPORT BRACKET IN RT WHEEL WELL FOUND CRACKED. HYD SUPPORT BRACKET IN RT WHEEL WELL REPLACED IAW SRM 51-42-06. (K)

Part: PANEL — CRACKED (PAX DOOR) · airframe 13,269 hrs · 12,294 cycles

MWC 132379-34 - PASSENGER DOOR FWD SIDE PANEL FOUND CRACKED (REF: REO601R-52-11-702, ZONE 2) CRACK LENGTH .180. REPAIR ON PASSENGER DOOR FWD SIDE PANEL PERFORMED IAW REO 601R-52-11-702, REV A. (K)

Part: SUPPORT — CRACKED (BS 280) · airframe 13,269 hrs · 12,294 cycles

MWC 132380-46 - RT PILOT BULK SUPPORT AT FS 280.00, RBL 9.0 FOUND CRACKED (.800 LONG). TR PILOT BULK SUPPORT AT FS 280.00, RBL 9.0, REPAIR PERFORMED IAW REO 601R-53-11-171 SCHEME B REV D. (K)

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 13,269 hrs · 12,294 cycles

HYD SUPPORT BRACKET IN LT MLG WHEEL WELL FOUND CRACKED. HYD SUPPORT BRACKET IN LT MLG WHEEL WELL REPLACED IAW SRM 51-42-06. (K)

Part: LATCH — DIRTY (JUMPSEAT) · airframe 12,834 hrs · 11,882 cycles

FLIGHT ATTENDANT JUMPSEAT LATCH HARD TO RELEASE. CLEANED AND ADJUSTED FAA JUMPSEAT LATCH AS PER AMM 25-22. OPS CHECK GOOD AT THIS TIME. REMOVED PLACARD AND REMOVED FROM MEL.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 12,800 hrs · 11,858 cycles

FLAPS FAILED AT ZERO DEGREES ON ARRIVAL INTO YOW. PERFORMED ZERO FLAP LANDING. BRAKE TEMP NOT OVER 4. COMPLIED WITH RESET PROCEDURE IAW AWAC SUPPLEMENT 98-018B, STEPS 1.3 AND 1.4. FLAP SYSTEM RESET OK.

Part: FIRE LOOP — MALFUNCTIONED (LT FUSELAGE) · airframe 12,531 hrs · 11,611 cycles

ANTI ICE DUCT WARNING MSG ON TAKEOFF. TAKEOFF ABORTED AT 80 KNOTS, BRAKE TEMPS WERE 5,6,3,3 SYNOPTIC PAGE SHOWS LT FUSELAGE RED. R&R LT FUSELAGE FIRE DETECTION LOOP AS PER AMM 36-21-04, OPS CHECK GOOD AT THIS TIME.

Part: CONTROL UNIT — FAILED (TE FLAP) · airframe 12,279 hrs · 11,377 cycles

AT FL280 LANDING CONFIGURATION INDICATION APPEARED AND ACFT NOSED OVER AND BACKUP. FLAP DEGRADE STATUS MSG APPEARED. PERFORMED FLAP FAULT ISOLATION PER AMM 27-50-00 WHICH INDICATED A FAULT WITH SKEW DETECTION SYS. PERFORMED TEST OF SDS SYS PER FIM. NO FAULTS INDICATED. PERFORMED FECU TEST PER AMM 27-51-05 AND CONTROL UNIT FAILED. PER MX CNTRL, DEACTIVATE SDS SYS PER MEL 27-51-03 AND RETEST FECU. DEACTIVATION OF SDS, THE FECU TEST OK PER AMM 27-51-05. FLAPS OPS TEST GOOD PER AMM 27-54-00-710-801. HORIZ STAB CONTROL SYS ALSO TEST OK PER AMM 27-41-00. REPLACED SDU PER AMM 27-51-15. REACTIVATED SKEW DETECTION SYSTEM PER AWAC SUPP 06-076A. SYSTEM TESTS GOOD. OK FOR SERVICE.

Part: SENSOR — FAILED (RT BRAKE)

FLAPS FAIL CAUTION MESSAGE ON APPROACH AT ZERO DEGREES, COMPLIED WITH QRH AND NORMAL LANDING. FOUND REPEAT RT BRAKE AND POSITION SENSOR UNIT FAILURES. REMOVED AND REPLACED RT BPSU PER AMM 27. OPS CHECK GOOD. (M)

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 10,768 hrs · 9,939 cycles

FLAPS FAIL CAUTION MESSAGE FLAPS FAILED AT 0 DURING EXTENSION. COMPLIED WITH RESET PROCEDURE IAW AWAC SUPP 98-018B STEPS 1.3 AND 1.4 FLAP SYSTEM RESET, OK. (M)

Part: FLAP — FAILED (WING) · airframe 10,516 hrs · 9,685 cycles

FLAP FAIL CAS MESSAGE IN FLIGHT, FLAP FAILED AT ZERO DEGREES. LDNG WT= 44,300. APPROX 150 KNTS. MAT BTMS = 5,4,2,2 AND VERTICAL DESCENT RATE LESS THAN 10 FT PM. COMPLIED WITH RESET PROCEDURE IAW AWAC SUPP 98-018B. STEPS 13 AND 1.4, FLAP SYS OK. (K)

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 8,574 hrs · 7,803 cycles

PAX DOOR AFT DRAG ANGLE CRACKED. (K) [07-17-07] MAINTENANCE REMOVED DAMAGED SECTION OF DRAG ANGLE AND INSTALLED SERVICEABLE SECTION IAW BOMBARDIER REO 601R-52-11-513. (M)

Part: ANGLE — CRACKED (BS 484) · airframe 8,574 hrs · 7,803 cycles

FS 484.0 ANGLE AT LBL 27 IS CRACKED APPROX 1.0 INCH. (K) [07-17-07] MAINTENANCE REMOVED AND REPLACED ANGLE IAW BOMBARDIER SRM 601R-53-0029B AND CRJ 200 SRM 51-42-06. (M)

Part: ANGLE — CRACKED (BS 484) · airframe 8,574 hrs · 7,803 cycles

FS 484.0 ANGLE AT RBL 27 IS CRACKED APPROX 1.0 INCH. (K) [07-17-07] MAINTENANCE REMOVED AND REPLACED ANGLE IAW BOMBARDIER SR 601R-53-0029B AND CRJ 200 SRM 51-42-06. (M)

Part: ANGLE — CRACKED (BS 484) · airframe 8,574 hrs · 7,803 cycles

FS 484.0 ANGLE AT LBL36 IS CRACKED APPROX 1.0. CORRECTIVE ACTION IN PROGRESS. (K) [07-17-07] MAINTENANCE REMOVED AND REPLACED ANGLE IAW BOMBARDIER REO 601R-53-41-059. (M)

Part: ANGLE — CRACKED (BS 484) · airframe 8,574 hrs · 7,803 cycles

FS484.0 ANGLE AT RBL 36 IS CRACKED APPROX 1.0 INCH. (K) [07-17-07] MAINTENANCE REMOVED AND REPLACED ANGLE IAW BOMBARDIER REO 601R-53-41-059 AND BSC SR 601R-53-0030A. (M)

Part: FLOORBEAM — CRACKED (BS 621) · airframe 8,574 hrs · 7,803 cycles

RT FS 621..00 FLOOR SUPPORT ANGLE IS CRACKED 1.2500 INCH LONG IN OB RADIUS. (K) [07-17-07] MAINTENANCE CUT AWAY DAMAGED AREA AND INSTALLED SERVICEABLE REPAIR IAW BOMBARDIER REO 601R-53-61-117. (M)

Part: FLOORBEAM — CRACKED (FUSELAGE)

FOUND LEFT FS 621 FLOOR SUPPORT ANGLE IS CRACKED 1.25 INCH LONG IN OUTBOARD RADIUS. MAINTENANCE CUT OUT DAMAGED AREA AND INSTALLED REPAIR IAW BOMBARDIER REO 601R-53-61-117. (M)

Part: FLOORBEAM — CRACKED (BS 621) · airframe 8,574 hrs · 7,803 cycles

LT FS 621.00 FLOOR SUPPORT ANGLE IS CRACKED 1.2500 INCH LONG IN OB RADIUS. (K)

Part: ANGLE — CRACKED (FUSELAGE) · airframe 8,574 hrs · 7,803 cycles

LT FS 621.00 AND 625.00 OBLIQUE ANGLE HAS A 1.5 INCH LONG CRACK IN AFT RADIUS. (K) [07-17-07] MAINTENANCE REMOVED CRACKED ANGLE AND INSTALLED NEW ANGLE IAW CRJ200 SRM 51-42-06. (M)

Part: ANGLE — CRACKED (FUSELAGE) · airframe 8,574 hrs · 7,803 cycles

RT FS 621.00 TO 625.00 OBLIQUE ANGLE HAS A 1.2500 INCH LONG CRACK IN AFT RADIUS. (K) [07-17-07] MAINTENANCE REMOVED CRACKED ANGLE AND INSTALL NEW ANGLE IAW CRJ200 SRM 51-42-06. (M)

Part: ACTUATOR — UNKNOWN (ELEVATOR)

AFTER DISCONNECTION AUTOPILOT ON APPROACH UNABLE TO MOVE CONTROL COLUMN FORWARD AND AFT, EVENTUALLY FIXED ITSELF. REMOVED AND REPLACED ELEVATOR SERVO SERV N/R OFF 13VYD. (M)

Part: SHUTOFF VALVE — MALFUNCTIONED (A/C PACK)

IN THE AIR AND ON THE GROUND WITH THRUST LEVERS AT IDLE, BOTH PACKS OFF LINE AND UNABLE TO MAINTAIN PRESSURIZATION. REMOVED AND REPLACED LEFT AND RIGHT PRESSURE REGULATING SHUTOFF VALVE FILTERS IAW AMM SUP 0639, OPS CHECK GOOD. (M)

Part: BULB — INOPERATIVE (IDG TEMP)

GENERATOR NR 1 OFF MESSAGE IN FLIGHT. COMPLIED WITH QRH, COULD NOT RESET. REMOVED AND REPLACED IDG TEMP BULB IAW CRJ AMM 24-13-05, OPS AND LEAK CHECK GOOD AT THIS TIME. (M)

Part: CONTROL PANEL — INOPERATIVE (COCKPIT) · airframe 4,677 hrs · 4,109 cycles

ADG INADVERDENTLY DEPLOYED DURING CLIMBOUT, PERFORMED QRH AMBER CAS MESSAGE FOR L WINDOW HEAT, L AOA HEAT, PITOT BASE HEAT ILLUMINATED. ADG POWERED AC ESS BUS. EMERGENCY LIGHTS ILLUMINATED BEFORE ADG DEPLOYMENT. REMOVED AND REPLACED AUTO DEPLOY CONTROL PANEL IAW MM 24-23-15 STOWED ADG IAW MM 24-23-01. PERFORMED INSPECTION OF ADG IAW 05-51-19. OPS CHECK GOOD. (K)

Part: SKIN — DENTED (T/E FLAP) · airframe 3,795 hrs · 3,276 cycles

LT IB FLAP HAS A DENT 22 INCHES FROM IB EDGE AND 14 INCHES FROM THE DENT IS 2 INCH X 2 INCH X 0.55 INCH. LOWER SKIN. PERFORMED A MAJOR REPAIR B4 INSTALLING A 8 INCH X 16 INCH NON-FLUSH REPAIR. (K)

Part: BUSHING — MIGRATED (RT TRUNNION) · airframe 3,795 hrs · 3,276 cycles

RT AFT MAIN LANDING GEAR TRUNNION BUSHING MIGRATED .058 INCH. REMOVED RT AFT MLG TRUNNION BUSHING AND INSTALLED NEW SERVICEABLE BUSHING IAW MFG REO. (K)

Part: BUSHING — MIGRATED (LT MLG TRUNNION) · airframe 3,795 hrs · 3,276 cycles

LT AFT MLG TRUNNION BUSHING MIGRATED .053 INCH. REMOVED LT AFT MLG TRUNNION BUSHING AND INSTALLED NEW SERVICEABLE BUSHING IAW MFG REO. (K)

Part: WINDSHIELD — CRACKED (COCKPIT)

FIRST OFFICER FORWARD WINDSHIELD OUTER PANEL ONLY SHATTERED FAILURE OCCURRED AT 31,000 FT ON CLIMB-OUT. COMPLIED WITH QRH UNEVENTFUL LANDING SYRACUSE. REMOVED AND REPLACED FIRST OFFICERS WINDSHIELD REF MM 56-11-01. PRESSURIZED AIRCRAFT, OPS CHECK GOOD. (M)

Part: COALESCER BAG — DIRTY (A/C BAY) · airframe 3,002 hrs · 2,599 cycles

SUSPECT LT PACK. PERFORMED OPS CHECK OF BOTH LT AND RT PACKS. RT OPS NORMAL, LT PACK EMITS ODOR DURING OPERATION. REMOVED AND REPLACED COALESCER SOCK ON LT PACK. OPS CHECK NORMAL. (K)