N469AW

Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · airframe 39,139 hrs · 37,997 cycles

ABORTED TAKE-OFF PRIOR TO 80 KNOTS, EFIS COMP MON HEADING. MESSAGE CLEARED AFTER EXITING RUNWAY. BRAKE TEMPS: 3,3,4,5. UNABLE TO CONFIRM WHICH SIDE OFF PRIOR TO RUNWAY EXIT. CAPTAIN'S SIDE 4 DEGREE DRIFT AFTER ONE MINUTE AFTER EXITING RUNWAY. *********AIRCRAFT REMOVED FROM SERVICE********* REMOVED AHRS 1 AND FOUND TRAY DIRTY. CLEANED CONNECTION AND TRAY AND REINSTALLED AHRS 1. OPS CHECK GOOD, CONFIRMED HEADING IS NOT DRIFTING AS NOTED IN DISCREPANCY. WORK PERFORMED IAW AMM 34-21-01 AND ESPM 20-17-10.

Part: FAIRING — GOUGED (LT WINGLET) · airframe 38,857 hrs · 37,733 cycles

LEFT HAND WINGLET AT WS400 TRAILING EDGE FAIRING PANEL 572KL P/N 600-15109 HAS GOUGE DAMAGE. ***********AIRCRAFT REMOVED FROM SERVICE********** REPAIRED COMPOSITE OF LEFT HAND WINGLET AT WS400 TRAILING EDGE FAIRING PANEL 572KL. DAMAGE MEASUREMENTS L= 2.0Ï¿½ X W= 1.80Ï¿½ AND ONE PLY DEEP. RESTORED SURFACE PROTECTIVE FINISH. ALL WORK WITHIN LIMITS PERFORMED IAW EA #: AWAC-CRJ257 -01219 REV IR, DATED 10/24/2022. WORK PERFORMED UNDER AERSALE WORK ORDER 003768, CARD NO. 50003, TT: 38857:13 TC: 37733.

Part: FLOOR SUPPORT — CORRODED (FS 574- 621) · corrosion level 2 · airframe 38,857 hrs · 37,733 cycles

CABIN AFT FLOOR SUPPORT BEAM FITTING BETWEEN FS 574.0 AND FS 621.0 AND LBL 27 HAS CORROSION. MEASUREMENTS ARE L= 3.0Ï¿½ X W=1.0Ï¿½ X D= 0.043Ï¿½. ************AIRCRAFT REMOVED FROM SERVICE**************************** BLENDED CORROSION ON PREVIOUS REPAIR OF FLOOR SUPPORT BEAM FITTING BETWEEN FS 574.0 AND FS 621.0 AND LBL 27. MEASUREMENTS ARE L= 3.0Ï¿½ X W=1.0Ï¿½ X D= 0.043Ï¿½. PERFORMED REPAIR BY CUTTING OUT DAMAGED SECTION MEASURING L=2.350Ï¿½ X W= 0.900Ï¿½. FABRICATED AND INSTALLED FILLER WITH MATERIAL 7075-T6, THICKNESS 0.100Ï¿½, P/N 601R-53-61-7909-2. REPAIR STRAP INSTALLED P/N 601R-53-61-7909-1, MATERIAL 7075-T6, THICKNESS 0.900Ï¿½. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS PERFORMED IAW MHI RJ REO 601R-53-61-7909 REV (--) DATED 2022-11-01. WORK PERFORMED UNDER AERSALE WORK ORDER 003768, CARD NO. 20295, TT: 38857:13, TC: 37733.

Part: ANGLE — CORRODED (SVC DOOR SILL) · corrosion level 2 · airframe 38,857 hrs · 37,733 cycles

CORROSION ON SERVICE DOOR LOWER SILL ANGLE P/N 601R38303-253 AND 601R38303-239 AT FS 319.0 TO FS349.0 AND RBL 43. ************AIRCRAFT REMOVED FROM SERVICE***************** REMOVED AND REPLACED SERVICE DOOR LOWER SILL ANGLE P/N 601R38303-253 AND 601R38303-239 AT FS 319.0 TO FS349.0 AND RBL 43. RESTORED SURFACE PROTECTIVE FINISH. ALL WORK WITHIN LIMITS PERFORMED IAW CRJ200 SRM 51-42-13 REV 39 AND SRM 51-12-21 REV 39. WORK PERFORMED UNDER AERSALE WORK ORDER 003768, CARD NO. 20138, TT: 38857:13 TC: 37733.

Part: FLOORBEAM — CORRODED (BS 349 RBL 37-42) · corrosion level 2 · airframe 38,857 hrs · 37,733 cycles

CORROSION ON CABIN FLOOR STRUCTURE CROSSBEAM P/N 601R32005-149 AND CLIP P/N 601R38303-175 AT FS349.0 AND RBL 37 TO 42. AIRCRAFT REMOVED FROM SERVICE. REPAIRED CABIN FLOOR STRUCTURE CROSSBEAM AND CLIP AT FS349.0 AND RBL 37 TO 42. FABRICATED NEW CLIP P/N 601R-53-21-3575-4 FROM .063 ALUM SHEET MATERIAL HEAT TREATED TO 7075-T6. CLIP DIMENSIONS L= 3.90Ï¿½ X W= 2.90Ï¿½. RESTORED SURFACE PROTECTIVE FINISH. ALL WORK WITHIN LIMITS PERFORMED IAW MHIRJ REO 601R-53-21-3575 REV (--), WORK PERFORMED UNDER WORK ORDER 003768,

Part: SEAT TRACK — CORRODED (BS 364-394) · corrosion level 2 · airframe 38,857 hrs · 37,733 cycles

CABIN FLOOR SEAT TRACK FS 364.0 TO FS 394.0 AND RBL 9 HAS CORROSION. SEAT TRACK P/N 20276-288-0-0. **********AIRCRAFT REMOVED FROM THE SERVICE*********************** REPLACED WITH A NEW SEAT TRACK PN 20276-288-0-0 AT FS 364.0 TO FS 394.0 AND RBL 9. ALL WORK WITHIN LIMITS WAS PERFORMED IAW CRJ200 SRM 51-11-00 REV 39, CRJ200 SRM 53-21-49 REV 39, CRJ200 AMM 53-01-11 REV 66, CRJ200 51-40-11 REV 39, CRJ200 SRM 51-12-00 REV 39, CRJ200 SRM 51-25-06 REV 39, CRJ200 SRM 51-25-16 REV 39. ALL WORK WITHIN LIMITS PERFORMED UNDER AERSALE WORK ORDER 003768, CARD NO. 20291, TT: 38857:13 TC: 37733.

Part: DOOR SILL — CORRODED (BS 349) · corrosion level 2 · airframe 38,857 hrs · 37,733 cycles

CORROSION ON SERVICE DOOR LOWER SILL P/N 601R31132-69 AT FS349.0 AND RBL 42. AIRCRAFT REMOVED FROM SERVICE. BLENDED CORROSION SERVICE DOOR LOWER SILL AT FS349.0 AND RBL 42. RESTORED SURFACE PROTECTIVE FINISH. ALL WORK WITHIN LIMITS PERFORMED IAW EA AWAC-CRJ253 -01918 REV IR. WORK PERFORMED UNDER WORK ORDER 003768,

Part: FITTING — CORRODED (SVC DOOR SILL) · corrosion level 2 · airframe 38,857 hrs · 37,733 cycles

CORROSION ON SERVICE DOOR LOWER SILL DOUBLER P/N 601R38534 AND FITTING 601R38533-9 AT FS 319.0 TO FS349.0 AND RBL 43. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SERVICE DOOR LOWER SILL DOUBLER P/N 601R38534 AND FITTING P/N 601R38533-9 AT FS 319.0 TO FS349.0 AND RBL 43. RESTORED SURFACE PROTECTIVE FINISH. ALL WORK WITHIN LIMITS PERFORMED IAW CRJ200 SRM 51-11-00 REV 39 AND SRM 51-12-00 REV 39. WORK PERFORMED UNDER AERSALE WORK ORDER 003768, CARD NO. 20138, TT: 38857:13 TC: 37733.

Part: FLOOR SUPPORT — CORRODED (FS449.8) · corrosion level 2 · airframe 36,813 hrs · 35,694 cycles

RIGHT HAND PRESSURE FLOOR SILL CORROSION AROUND FASTENER HOLE AT FS449.85 + 2Ï¿½ RBL 36. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED CORROSION AROUND FASTENER HOLE AT FS449.85 + 2Ï¿½ RBL36. 1.100Ï¿½ L X 1.0Ï¿½W X 0.002Ï¿½ D. HFEC PERFORMED WITH NO INDICATIONS. RESTORED SURFACE FINISH. ALL WORK WITHIN LIMITS AND PERFORMED IAW REO 601R-53-41-666 REV C DATED 2012-11-06.

Part: FLOOR SUPPORT — CORRODED (PRESSURE DECK) · airframe 36,813 hrs · 35,694 cycles

RIGHT HAND PRESSURE FLOOR SILL CORRODED AROUND FASTENER HOLE AT FS449.85+2 AND RBL36 ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED CORROSION AROUND RIGHT HAND PRESSURE FLOOR SILL FASTENER HOLE AT FS449.85+2 AND RBL36, BLENDED AREA 1.1Ï¿½L X 1.0Ï¿½W X 0.002Ï¿½D. ORIGINAL THICKNESS 0.55Ï¿½. PERFORMED HFEC WITH NO INDICATION AND RESTORED SURFACE FINISH. ALL WORK PERFORMED AND WITHIN LIMITS IAW REO 601R-53-41-666 REV C DATED 2012/11/06.

Part: SKIN — CORRODED (BS 409) · corrosion level 2 · airframe 36,813 hrs · 35,694 cycles

CORROSION ON UPPER FUSELAGE SKIN AT ADF ANTENNA FS409.00 + 84 TO FS409.00 + 87.5 LH STR 0 + 1 TO RH STR 0 + 2.5. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED CORROSION ON UPPER SKIN FS409.00 + 84 TO FS409.00 + 87.5 LH STR 0 + 1 TO RH STR 0 + 2.5. ORIGINAL THICKNESS 0.058" REMAINING THICKNESS OF 0.054" AND ORIGINAL THICKNESS OF 0.45" AND REMAINING THICKNESS OF 0.044". PERFORMED HFEC WITH NO INDICATIONS. RESTORED SURFACE FINISH. ALL WORK PERFORMED IAW EA#: AWAC-CRJ253-01632 REV IR DATED 5/11/2021

Part: SKIN — CHAFED (RT AILERON) · airframe 36,813 hrs · 35,694 cycles

RIGHT HAND AILERON LOWER LEFT END BETWEEN HINGE POINTS D1 AND D2, OUTBOARD OF OUTBOARD HINGE POINT SKIN IS WORN. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED DAMAGE AT D1) A/STA 370.031 TO A/STA 375.857 4.50Ï¿½L X 0.80Ï¿½W 0.009Ï¿½D D2) A/STA 323.843 TO A/STA 329.875 6.0Ï¿½L X 0.90Ï¿½W X 0.007Ï¿½D HFEC PERFORMED WITH NO INDICATIONS AND REAPPLIED PROTECTIVE FINISH. BLENDS AT D1 AND D2 WITHIN LIMITS AND ALL WORK DONE IAW ASAP EA# AWAC-CRJ257-01633 REV IR DATED 5/11/2021

Part: SKIN — DENTED (ZONE 100) · airframe 36,813 hrs · 35,694 cycles

FUSELAGE DENTED BETWEEN FS574+11.40Ï¿½ TO FS589+3.5Ï¿½ AND S21L+1.32Ï¿½ TO S21L+3.75Ï¿½ ***AIRCRAFT REMOVED FROM SERVICE*** CUT OUT DAMAGE BETWEEN FS574+11.40Ï¿½ TO FS589+3.5Ï¿½ AND S21L+1.32Ï¿½ TO S21L+3.75Ï¿½ MEASURING 8.2Ï¿½L X 4.1Ï¿½W, HFEC PERFORMED WITH NO INDICATION, INSTALLED REPAIR DOUBLER IAW CRJ200 SRM 53-00-31 REPAIR 1, REV 38. APPLIED PROTECTIVE FINISH IAW CRJ 200 SRM 51-25-01 PG 1 REV 38.

Part: CAP — CORRODED (FS589-606 LBL 27) · corrosion level 2 · airframe 36,813 hrs · 35,694 cycles

FLOOR SUPPORT BEAM CAP CORRODED FS 589.0+7.5 LBL 27. BLENDED CORROSION AT FS 589.0+7.5 LBL 27, OUT OF LIMITS PER CRJ200 SRM 53-00-0 REV 38. REMOVED AND REPLACED FLOOR BEAM CAP AT FS 589.0+7.5 TO FS 606.0 LBL 27 IAW SRM51-42-21 REV 38.

Part: SKIN — DENTED (FS621-640) · airframe 36,813 hrs · 35,694 cycles

FUSELAGE SKIN DENTS BETWEEN FS621-FS640, S 24 + 3L -S 24 + 5L. NOTED AS D3, D4, D5. ***AIRCRAFT REMOVED FROM SERVICE*** HAND FORMED DENT D3) AT FS 621 + 3.5Ï¿½ AND S24 + 5Ï¿½L, 6.500Ï¿½L X 0.900Ï¿½W X 0.002Ï¿½D, D4) FS 625.00 + 1Ï¿½ AND S24 + 5Ï¿½, 2.850Ï¿½L X 0.550Ï¿½ W X 0.007Ï¿½ D DOUBLER REPAIR AT D5) DENT AT FS 625.00 + 3Ï¿½ S24L + 3Ï¿½ MEASURES 0.800Ï¿½ L X 0.700Ï¿½ X 0.038Ï¿½ W WITH CREASE. HFEC PERFORMED WITH NO INDICATIONS. RESTORED SURFACE FINISH. ALL WORK WITHIN LIMITS AND PERFORMED IAW ASAP EA # AWAC-CRJ253-1630 REV IR DATED 5/7/2021.

Part: SKIN — DENTED (BS 654.5 S26L) · airframe 36,813 hrs · 35,694 cycles

FUSELAGE SKIN DENT AT FS 654.50+2.5" S26L+3.4" ***AIRCRAFT REMOVED FROM SERVICE*** HAND DRESSED DENT AT FS 654.50+2.5" S26L+3.4" TO ORIGINAL CONTOUR, HFEC PERFORMED WITH NO INDICATIONS, REF ASAP EA# AWAC-CRJ253-01631 REV IR DATED 5/7/2021.

Part: RELAY — FAILED (DISPLAY COOLING) · airframe 36,723 hrs · 35,600 cycles

WEIGHT OFF WHEELS, FAN CUT OFF, RECEIVED DISPLAY COOL CAUTION MESSAGE, CONTINUED CLIMB TO 7000 MESSAGE PERSISTED MX ADVISED RETURN TO MKE. A FEW MINUTES LATER F/O'S PFD RECEIVED A DISPLAY TEMP MESSAGE, FOLLOWED BY CAPTAINS PFD DISPLAY TEMP MESSAGE, F/O'S MFD DISPLAY TEMP MESSAGE, AIRCRAFT REMOVED FROM SERVICE. REPLACED RELAYS K7HK AND K11HK ALSO THE AVIONICS COOLING PANEL REF AMM 21-24 AND 24-02 SYS CHECKS GOOD.

Part: STRUT — COLLAPSED (NLG) · airframe 36,706 hrs · 35,574 cycles

RECEIVED GEAR DISAGREE MASTER WARNING SHORTLY AFTER TAKE-OFF AT APPROXIMATELY 300 FT AFE ALONG WITH WOW INPUT CAUTION, STEERING INOP CAUTION, WOW OUTPUT FAIL STATUS MESSAGE. COMPLIED WITH QRH. OCCURRED SHORTLY AFTER SELECTING GEAR UP. ON TAXI-IN AT IAD HYD 3 HI TEMP AND STEERING INOP CAUTION MESSAGES. COMPLIED WITH QRH, ONLY HYDRAULIC HI TEMP MESSAGE CLEARED. EMER GEAR EXTENSION LEVER WAS USED, UNABLE TO STOW LEVER AFTER DEPLOYING. LANDING WEIGHT APPROXIMATELY 46,200. NLG WAS SERVICED TO FULL EXTENSION AFTER GEAR DISAGREE UNABLE TO COLLA PSE STRUT. FLUID APPEARS TO BE HYD FLUID REF LOGBOOK PG 318642 BLOCK 1 FOR CAUTION MESSAGES DURING FLIGHT. R&R NLG REF W/O 303594.

Part: STRUT — COLLAPSED (NLG) · airframe 36,689 hrs · 35,558 cycles

AFTER TAKEOFF RECEIVED GEAR DISAGREE WARNING MSG NOSE GEAR WOULD NOT RETRACT CW QRH, WARNING OCCURED WITHIN 10 SECONDS OF HANDLE SELECTION. SMOOTH NORMAL LANDING BTMS MAX 3. LDG WEIGHT 41700. WOW INPUT CAUTION AND STEERING INOP AFTER THE GEAR DISAGREE AND NOSE WARN MSGS. ALL MSGS ASIDE FROM WOW INPUT AND NWS INOP CUTION CLEARED WITH GEAR DOWN. THOSER MSGS CLEARED ON LANDING ***AIRCRAFT REMOVED FROM SERVICE*** NLG WAS SERVICED TO FULL EXTENSION AFTER GEAR DISAGREE UNABLE TO COLLA PSE STRUT. FLUID APPEARS TO BE SKYDROL REF LOGBOOK PG 318642 BLOCK 1 FOR CAUTION MESSAGES DURING FLIGHT R&R NLG REF WO 303594

Part: WARNING MESSAGE — FALSE ACTIVATION (ANTI SKID SYSTEM) · airframe 34,652 hrs · 33,505 cycles

ON APPROACH AND WHILE SELECTING THE GEAR DOWN, THE FLIGHT CREW RECEIVED AN ANTI-SKID CAUTION MESSAGE. THE FLIGHT CREW CONSULTED THE QRH, CONFERRED WITH DISPATCH, CONTACTED ATC AND DECLARED AN EMERGENCY. CONTINUED TO DESTINATION AND LANDED WITHOUT FURTHER INCIDENT. NO ADVERSE PASSENGER REACTIONS WERE NOTED.

Part: BULKHEAD — CRACKED (BS 621) · airframe 34,346 hrs · 33,227 cycles

INDICATION NOTE AT F.S. 621 REAR PRESSURE BULKHEAD AT LBL 9.50, WL 75 100% F.S.H. AND APPOX 1.4 LONG FAILING NDT.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 34,346 hrs · 33,227 cycles

INDICATION NOTED AT F.S. 621 REAR PRESSURE BULKHEAD FWD FACE AT LBL 18.0, WL 106, APPROX 1.9 LONG, 53% F.S.H. FAILING NDT.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 34,346 hrs · 33,227 cycles

F.S. 621 PRESSURE BULKHEAD FWD FACE HAS AN INDICATION NOTED AT BL 0.00, WL 29.9, 3.2 INCHES LONG, AND 52% FULL SCREEN HEIGHT FAILING NDT.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 34,346 hrs · 33,227 cycles

R/H FLAP VANE SKIN LEADING EDGE IS CHAFED AT STOPS.

Part: SEAT TRACK — CORRODED (BS 399-409) · corrosion level 2 · airframe 34,346 hrs · 33,227 cycles

RBL 9 SEAT RAIL IS CORRODED BETWEEN F.S.399.00 TO F.S.409.00+126.

Part: SEAT TRACK — CORRODED (BS 399-409) · corrosion level 2 · airframe 34,346 hrs · 33,227 cycles

LBL 9 SEAT TRACK IS CORRODED BETWEEN F.S.399 TO F.S.409.00+126.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 34,346 hrs · 33,227 cycles

L/H INBD FLAP VANE SKIN LEADING EDGE IS CHAFED AT CENTER AND INBD STOP LOCATIONS.

Part: BEAM — DAMAGED (BS 574-621) · airframe 34,346 hrs · 33,227 cycles

FOUND DAMAGE ON THE CARGO DOOR BEAM IN MULTIPLE AREAS, MARKED WITH RED TAPE.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 34,346 hrs · 33,227 cycles

R/H F.S.280 BEAM IS CRACKED AT RBL9.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 34,346 hrs · 33,227 cycles

WHILE WORKING R/H F.S.280 BEAM FOUND L/H F.S.280 BEAM CRACKED AT LBL9

Part: INTERCOSTAL — CRACKED (BS 654-672) · airframe 34,346 hrs · 33,227 cycles

APU INLET DOOR ACTUATOR AFT MOUNT BRACKET APPEARS TO BE CRACKED AND INTERCOSTAL FWD END APPEARS CRACKED (FS654).

Part: BRACKET — CRACKED (CARGO DOOR) · airframe 34,346 hrs · 33,227 cycles

LOWER BRACKET ON CARGO DOOR SUPPORT FRAME IS CRACKED

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 34,346 hrs · 33,227 cycles

LBL 9 SEAT TRACK IS CORRODED BETWEEN F.S.559.00+96 TO F.S.559.00-80.

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 34,346 hrs · 33,227 cycles

LBL 27 SEAT TRACK IS CORRODED BETWEEN F.S.559.00+96 TO F.S.559.00+80.

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 34,346 hrs · 33,227 cycles

LBL 9 SEAT TRACK IS CORRODED BETWEEN F.S.559.00+64 TO F.S.559.00+32.

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 34,346 hrs · 33,227 cycles

RBL9 SEAT TRACK IS CORRODED BETWEEN F.S.559.00+112 TO F.S.559.00+80.

Part: WARNING MESSAGE — ILLUMINATED · airframe 34,297 hrs · 33,175 cycles

DISPLAY COOL CAUTION MESSAGE RAN QRH, MESSAGE DID NOT CLEAR. RECIEVED MESSAGE AT 34000 FT

Part: WARNING MESSAGE — FALSE ACTIVATION (MASTER)

THRU 8500 FEET MASTER WARNING FOR ANTI ICE DUCT IN THE RH FUSELAGE LI E. RAN QRH NO OTHER ACTION REQUIRED. QRH REQUIRES THAT THE WING, COWL AND 14TH STAGE VLVS TO BE CLOSED. THE MSG REMAINED FOR 10 MINUTES AFT R ALL VLVS WERE CLOSED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,745 hrs · 30,654 cycles

EMERGENCY LIGHTING INOPERATIVE AT ROW 9 TO BACK. INSPECTED THE LIGHT, NO DEFECTS. NOTED THE AFT RIBBON ASSY HAS NO POWER TO LIGHT.

Part: LIGHT — INOPERATIVE (ROWS 6-8) · airframe 31,674 hrs · 30,587 cycles

EMERGENCY LIGHTS ROW 6-8 DID NOT OPERATE WHEN INITIALLY TESTED, LIGHTS TURNED ON WHEN LEFT IN ON POSITION FOR EXTENDED PERIOD, APPROXIMATELY 90 SECONDS. R & R THE NR 3 EMERGENCY BATTERY INVERTER IAW AMM 33-51-07, R & R THE NR 4 EMERGENCY BATTERY INVERTER AMM 33-51-07, R & R THE NR 3 EMERGENCY BATTERY IAW AMM 33-51-04, R & R THE NR 4 EMERGENCY BATTERY IAW AMM 33-51-04, R & R THE NR 3 EMERGENCY LIGHT BATTERY CHARGER IAW AMM 33-51-05, R & R THE NR 4 EMERGENCY LIGHT BATTERY CHARGER IAW AMM 33-51-05 AND R & R THE EMERGENCY LIGHT CABLE ASSEMBLYS IAW AMM 33-51-01.

Part: SIGN — UNRELIABLE (EMERGENCY LIGHTS) · airframe 31,674 hrs · 30,587 cycles

EMERGENCY LIGHT SYSTEM IS UNRELIABLE. REMOVED AND REPLACED THE RT EMERGENCY EXIT FLOOR LEVEL SIGN IAW AMM 33-51-10-04. SYSTEM OPS CHECKED GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 31,659 hrs · 30,572 cycles

WIRE BROKEN FOR EMERGENCY LIGHTS BETWEEN ROW 6 AND ROW 8. REPAIRED THE WIRE LY22822 IAW ESPM 20-16-00.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,659 hrs · 30,572 cycles

EMERGENCY EXIT FLOOR LIGHTING ROW 5-8 AND RT OVERWING EXIT INOPERATIVE. REMOVED AND REPLACED THE NR 3 INVERTER IAW AMM 33-31-07-04, SYSTEM OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,659 hrs · 30,572 cycles

EMER EXIT FLOOR LIGHTING FROM ROW 8-5 INOP. RT EMER EXIT LIGHT ON SIDEWALL IS INOP. INSPECTED FLOOR TRACK LIGHTING. NO DAMAGE NOTED. NO DAMAGE TO SIDEWALL LIGHT. NO OTHER LIGHTS INOP. REF 316335/4 FOR MEL.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 31,652 hrs · 30,566 cycles

EMERGENCY LIGHTS ON FLOOR ROW 6-8 NOT WORKING. RESECURED EMERG FLOOR TRACK LIGHT CONNECTORS AT ROW 6-8. OP CK GOOD IAW AMM 33-51-00.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 31,652 hrs · 30,566 cycles

PER MAINTENANCE CONTROL, REQUEST FLOOR TRACK LIGHT CONNECTOR AT ROW 6 TO 8 NEEDS REPLACED. FOUND BROKEN CONNECTOR PINS BETWEEN SEAT ROW 7-8. R&R ONE SECTION OF FLOOR TRACK LIGHTING IAW SUPP 16-371A. OP CK GOOD.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 31,652 hrs · 30,566 cycles

FLOOR TRACK EMERGENCY LIGHTS INOP BETWEEN ROWS 5 & 8. RESECURED FLOOR TRACK LIGHT CONNECTOR IAW AMM SUP 16-371A, OPS CK GOOD.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 31,652 hrs · 30,566 cycles

EMERG FLOOR TRACK LIGHTS ARE INOP AT ROW 5-9, MC-ALL OTHER SIGNS WORKING. INSPECTED EMERG FLOOR TRACK LIGHTS, COVER IS INTACT WITH NO DAMAGED ASSURED CONNECTION AT ROW 6 AND 8 AND LIGHTS ILLUMINATED. CW OP TEST IAW AMM 33-51-01, OK AT THIS TIME.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 31,652 hrs · 30,566 cycles

EMERGENCY FLOOR TRACK LIGHTS FROM ROW 5-9 INOP. INSPECTED EMERGENCY FLOOR TRACK LIGHT COVERS, COVERS ARE INTACT WITH NO DEFECT. RE-SECURED CONNECTORS AT ROW 6 AND 8, FLOOR TRACK LIGHTS CHECK GOOD IAW AMM 33-51-00.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 31,648 hrs · 30,562 cycles

EMERGENCY FLOOR TRACK LIGHTS BETWEEN ROWS 5 & 8 PLUS RIGHT FLOOR LEVEL EXIT SIGN DID NOT ILLUMINATE. INSPECTED EMERGENCY FLOOR TRACK LIGHTING BOTTOM TRACK COVER FOUND TO BE SECURE TO FLOOR AND COVER ATTACHED AND IN GOOD CONDITION. FOUND WIRING CONNECTIONS SECURE REF SUPP 13-522 & 12-032 NO OTHER DEFECTS NOTED. R&R INVERTER 3 (P83LY) REF AMM 33-51-07. OPS CK GOOD AT THIS TIME.

Part: BRACKET — CRACKED (BS 589) · airframe 31,039 hrs · 29,975 cycles

BRACKET AT BS 589, STRINGER 14L JUST FWD OF THE POTABLE WATER TANK WAS CRACKED. REPLACED THE BRACKET.

Part: REPAIR — UNSECURE (LT WING TE FLAP) · airframe 31,039 hrs · 29,975 cycles

LEFT INBD FLAP REPAIR ON TRAILING EDGE HAS A REPAIR 21 INCHES FROM THE INBD END THAT HAS A SPLICE PLATE AT REAR SPAR THAT GOT PUSHED AWAY AND FASTENERS DID NOT CATCH. REMOVED AND REINSTALLED REPAIR PARTS IAW SRM 57-52-00, REPAIR 3.

Part: RETAINER — CRACKED (PYLON) · airframe 31,039 hrs · 29,957 cycles

SEAL RETAINER ON PYLON PANEL 412DB IS CRACKED. WELDED PERMANENT REPAIR IAW 16-363.

Part: LOUVER — CRACKED (RT ENGINE) · airframe 31,039 hrs · 29,975 cycles

RIGHT ENGINE LOWER COWL 442AB LOUVERS CRACKED AT SEVERAL PLACES

Part: STIFFENER — CRACKED (RT ENG EXHAUST) · airframe 31,039 hrs · 29,975 cycles

RIGHT ENGINE EXHAUST NOZZLE FAIRING STIFFENER IS CRACKED.

Part: CONNECTOR — NOT REPORTED (WHEEL SPEED) · airframe 31,016 hrs · 29,955 cycles

DURING TAKE-OFF ROLL, RECEIVED AN ANTI-SKID OTBD CAUTION MESSAGE. ABORTED THE TAKE-OFF AT 121 KTS. REMOVED AND REPLACED THE NR 4 WHEEL SPEED TRANSDUCER CONNECTOR P412 IAW SUP 09-062H. OPS CHECKED GOOD.

Part: OVERHEAT LOOP — CHAFED (RT MLG WW) · airframe 30,982 hrs · 29,927 cycles

DURING CLIMB FL240, RECEIVED AN MLG BAY OVERHEAT WARNING. COMPLIED WITH THE QRH. BTMS WAS 1-1-1-1 ON ALL BRAKES. WARNING WAS INTERMITTENT AND WENT OUT AFTER LANDING. PERFORMED GENERAL VISUAL INSPECTION OF AIRCRAFT AND MLG BAYS NO DEFECTS NOTED. FOUND RT MLG WHEEL BIN OVERHEAT ELEMENT CHAFING TO GROUND AND OPEN INTERMITTENTLY. REPLACED ELEMENT IAW AMM 26-14-04. OPS CHECKED GOOD.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 30,530 hrs · 29,531 cycles

ALL EMERGENCY LIGHTS WILL TURN ON FOR 3 SECONDS, THEN ALL TURN OFF

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,311 hrs · 29,339 cycles

EMERGENCY EXIT INDICATOR LIGHT WILL NOT ILLUMINATE. ALL EMERGENCY LIGHTS THAT ARE POWERED BY BATTERY 2 AND INVERTER 2.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHT)

LOWER EMERGENCY EXIT SIGN (GREEN) INOPERATIVE SEAT 8A.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,950 hrs · 29,008 cycles

EMERG FLOOR TRACK LIGHTS INOP ROW 2-8.

Part: UNKNOWN — SMOKE (AFT E/E BAY) · airframe 29,877 hrs · 28,947 cycles

AFT EQUIPMENT BAY FILLED WITH SMOKE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 29,831 hrs · 28,908 cycles

LEFT LOWER EMERGENCY EXIT LIGHT DOES NOT ILLUMINATE WITH SWITCH TURNED ON. R & R EMERGENCY LIGHT INVERTER NR 2 IAW AMM 33-51-07, OPS CHECK GOOD.

Part: ROD — DISCONNECTED (THRUST REVERSER) · airframe 28,447 hrs · 27,592 cycles

DURING REMOVAL OF NR 1 ENG OIL TRANSDUCER, FOUND BLOCKER DOOR ROD, THRUST REVERSER AT 1:30 POSITION DISCONNECTED. INSTALLED SERVICEABLE BLOCKER DOOR LINK PIN AT THE 1:30 POSITION IAW AMM 78+33+21. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,107 hrs · 27,266 cycles

FLOOR ESCAPE PATH EMER LIGHTS WILL NOT REMAIN LIT.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 27,511 hrs · 26,710 cycles

AFTER TAKEOFF, RECEIVED NOSE DOOR OPEN WARNING MSG WITH GEAR DISAGREE WARNING MSG, ALSO WOW INPUT CAUTION MSG & STEERING INOPERATIVE CAUTION & WOW OUTPUT FAIL WHITE STATUS MSG. COMPLIED WITH QRH. NOSE DOOR OPENED, MSG CLEARED WITH GEAR DISAGREE MSG, WAS ABLE TO CLEAR STEERING INOPERATIVE MSG, BUT WOW INPUT CAUTION REMAINS ALONG WITH WOW OUTPUT STATUS MSG. RETURN LANDING NORMAL. LANDING WEIGHT APPROX 39000 LBS.

Part: ADC — FAILED (COCKPIT) · airframe 26,411 hrs · 25,611 cycles

ADC FAILURE, FOUND TO BE FIRST OFFICERS SIDE. R & R NR 2 ADC. ALL OPS & FUNCTIONAL CHECKED.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 26,411 hrs · 25,610 cycles

PAX DOOR OUTER HANDLE CRACKED.

Part: SKIN — DENTED (TE FLAP) · airframe 26,411 hrs · 25,610 cycles

RT OTBD FLAP INBD LOWER SKIN DENTED FROM BIRD STRIKE.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 26,411 hrs · 25,610 cycles

FS 574.00 LOWER U BRACKET CRACKED AT RIVET HEAD.

Part: ATTACH BRACKET — CRACKED (RT WING) · airframe 26,411 hrs · 25,610 cycles

RT WING LE ATTACH BRACKET NEAR WS 150.00 IS CRACKED.

Part: ATTACH BRACKET — CRACKED (RT WING) · airframe 26,411 hrs · 25,610 cycles

RIGHT WING LE ATTACH BRACKET NEAR WS150 IS CRACKED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 26,411 hrs · 25,610 cycles

FWD EQUIPMENT BAY DECK CRACKED AT FS 193.00 LT ADJACENT TO FRAME.

Part: SKIN — CHAFED (RT AILERON) · airframe 26,411 hrs · 25,610 cycles

RT AILERON UPPER LE IS CHAFED.

Part: SEAL — CRACKED (LT SPOILER) · airframe 26,411 hrs · 25,610 cycles

55329-5000-0029 - LT FLIGHT SPOILER CTR & OTBD SEALS ARE CRACKED.

Part: FRAME — DENTED (FUSELAGE) · airframe 26,411 hrs · 25,610 cycles

FUSELAGE FRAME DENTED AT FS 672.00 ABOVE STRINGER 25R.

Part: RETAINER — CRACKED (PYLON) · airframe 26,411 hrs · 25,610 cycles

PYLON PANEL 422BT SEAL RETAINER IS CRACKED.

Part: ATTACH BRACKET — CRACKED (LT WING) · airframe 26,411 hrs · 25,610 cycles

LT WING CTR LE PANEL ATTACH BRACKET CRACKED AT FWD SPAR.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,411 hrs · 25,610 cycles

LT FLOOR SILL HAS CORROSION AT FS 574 THROUGH 559+80.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,411 hrs · 25,610 cycles

RT FLOOR SEAT TRACK AT FS 409+128 THROUGH 364 HAS CORROSION.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,411 hrs · 25,610 cycles

280 LBL & RBL 9 INBD & OTBD CLIPS ARE CRACKED.

Part: TIE DOWN — CORRODED (CARGO BAY) · corrosion level 2 · airframe 26,411 hrs · 25,610 cycles

FOUR EACH CARGO TIE DOWNS AT LBL 9 FS 621 THROUGH 559-96 HAS CORROSION.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 26,411 hrs · 25,610 cycles

RT WINDSHIELD POST LOWER ATTACHED FITTING CRACKED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 26,411 hrs · 25,610 cycles

280 JUST OTBD OF LBL 9 UPPER FLANGE CRACKED.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 26,411 hrs · 25,610 cycles

LT WINDSHIELD POST LOWER ATTACH FITTING IS CRACKED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,411 hrs · 25,610 cycles

LT 484 INBD & OTBD CLIPS CRACKED.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 26,411 hrs · 25,610 cycles

LEFT FS 280, STRINGER 3 CLIP CRACKED.

Part: SEAL — CRACKED (RT SPOILER) · airframe 26,411 hrs · 25,610 cycles

RIGHT FLIGHT SPOILER CTR TE METAL SEAL CRACKED.

Part: ANGLE — CRACKED (RT WING) · airframe 26,411 hrs · 25,610 cycles

RIGHT WING ROOT ANGLE ADJACENT TO BATTERY RIB CRACKED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,411 hrs · 25,610 cycles

RIGHT 484, INBD OTBD CLIPS CRACKED.

Part: MOUNT BRACKET — CRACKED (PAX DOOR) · airframe 26,411 hrs · 25,610 cycles

PAX DOOR POWER ASSIST MOTOR MOUNT BRACKET IS CRACKED.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 26,411 hrs · 25,610 cycles

PAX DOOR AFT DRAG ANGLE IS CRACKED.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,411 hrs · 25,610 cycles

LBL 27 AT FS 621 - 574 HAS CORROSION & CHAFED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 26,412 hrs · 25,610 cycles

FUSELAGE SKIN CRACKED AT NLG WW CUT OUT AFT RADIUS FS 235 & RBL 6.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,653 hrs · 24,909 cycles

FLOOR TRACK EMER LIGHTING ROW 9 - 12 INOPERABLE.

Part: LIGHT — INOPERATIVE (ROW 11) · airframe 25,505 hrs · 24,768 cycles

FLOOR LEVEL LIGHTS AT ROW 11 INOPERATIVE. ORANGE ARROWS STRIP MISSING.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 25,418 hrs · 24,685 cycles

WITH BOTH PACKS OPERATING OFF APU BLEED AIR, FUEL SMELL NOTED IN THE FLIGHT DECK.

Part: ACTUATOR — UNSECURE (HYDRAULIC SYS) · airframe 25,418 hrs · 24,685 cycles

FOUND LT ENG EMER HYD SOV ACTUATOR HANGING FROM CONNECTOR.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 24,673 hrs · 23,991 cycles

FUEL SMELL COMING FROM COCKPIT AIR VENTS WITH APU RUNNING.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 24,258 hrs · 23,625 cycles

3798 POTENT, NOXIOUS FUEL LIKE ODOR INTERMITTENT DURING FLT & GND OPERATIONS, EMITTING FROM RUDDER PEDAL AREA NOTICEABLE WHEN PACKS ARE OFF & HYD ACP'S ON. SAME ODOR IN AVIONICS BAY. CARPETS WERE REMOVED, CLEANED & REINSTALLED.

Part: MOUNT — CHAFED (AC BAY) · airframe 21,839 hrs · 21,223 cycles

RIGHT ACM MOUNT STRUCTURE IS CHAFED AT FS 718 BELOW RIGHT ACM. REMOVED AND REPLACED.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,839 hrs · 21,223 cycles

CORROSION ON LEFT FLOOR SILL AROUND FASTENER HOLES TOP AND BOTTOM OF SILL FROM FS 574 TO FS 621. AFTER BLENDING SILL IT WAS FOUND OUT OF LIMITS SILL WAS REMOVED & REPLACED PER REO 601R-53-61-096.

Part: TRUNNION — DAMAGED (WING) · airframe 21,839 hrs · 21,223 cycles

DURING COLDWORKING PROCESS FOUND TWO EACH LT & RT OVERSIZED FASTENERS ON LOWER MLG TRUNNION FLANGE. REMOVED OVERSIDED HOLES 2 EA LEFT & 1 EA RIGHT LOWER MLG TRUNNION FLANGE IAW BOMBARDIER REO 601R-57-21-1920.

Part: HINGE — CRACKED (FUSELAGE) · airframe 21,839 hrs · 21,223 cycles

CARGO DOOR THRESHOLD HINGES IS CRACKED. REMOVE & REPLACE HINGES IAW CRJ 200 SRM 51-40-11 & CRJ 200 SRM 51-42-06.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 21,839 hrs · 21,223 cycles

ACFT GROUND POWER PLUG BRACKET IS CRACKED AT FWD CIRCUIT BREAKER PORT. REMOVED UNSERVICEABLE GROUND POWER BRACKET AND REPLACED WITH SERVICEABLE POWER BRACKET.

Part: MOUNT — CRACKED (COCKPIT) · airframe 21,839 hrs · 21,223 cycles

FLIGHT DECK WINDSHIELD CENTER POST LOWER MOUNTS ARE CRACKED. REMOVED AND REPLACED FLIGHT DECK WINDSHIELD CENTER POST LOWER MOUNTS.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 21,839 hrs · 21,223 cycles

CRACKED ANGLE AT 484 AND LBL 27. REPAIRED ANGLE BY REPLACING WITH NEW SERVICEABLE ANGLE IAW REO 601R-53-41-059.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 21,839 hrs · 21,223 cycles

FORWARD O/B MOUNTING BRACKET IS CRACKED IN NOSE HYD COMPARTMENT ON UPPER ACCUMULATOR. REMOVED AND REPLACED BRACKET WITH NEW P/N 601R75250-55.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,839 hrs · 21,223 cycles

PAX DOOR LOWER SILL FWD CONNECTOR MOUNT ON I/B OF SILL IS CORRODED. REMOVED AND REPLACED UNSERVICEABLE PAX DOOR LOWER SILL FWD CONNECTOR IAW CRJ 200 SRM 51-42-06.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 21,839 hrs · 21,223 cycles

INTERCOSTAL IS CRACKED AT FS 654, LEFT STRINGER 4. REMOVED DAMAGED PART AND INSTALLED SERVICEABLE DUPLICATED PART IAW CRJ 200 SRM 51-21-11, 51-24-16, 51-24-36, 51-25-06, 51-25-16, 51-40-11, 51-42-06, 51-41-02.

Part: BRACKET — CRACKED (RT MLG WW) · airframe 21,839 hrs · 21,223 cycles

RIGHT MLG BRAKE TRANSDUCER BRACKET CRACKED. REPLACED WITH SERVICEABLE BRACKET P/N 601R75262-157.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 21,839 hrs · 21,223 cycles

RIGHT OBLIQUE ANGLE IS CRACKED JUST AFT OF THE 621 BULKHEAD. REMOVED AND REPLACED ANGLE IAW CRJ 200 SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 21,839 hrs · 21,223 cycles

LEFT OBLIQUE ANGLE IS CRACKED JUST AFT OF THE 621 BULKHEAD. REMOVED & REPLACED PER SRM.

Part: CONTACTOR — FAULTY (ELECTRICAL SYS) · airframe 20,186 hrs · 19,609 cycles

APU VOLTAGE OUTPUT BOUNCES BETWEEN 115 AND MID 80'S. REF WO 182603 FOR REPLACEMENT OF CONTACT K1XB BUSBAR 2W5XA & WORE XB2 A2OB OPS CHECK GOOD AT THIS TIME REMOVED PLACARD/MEL.

Part: COALESCER BAG — ODOR · airframe 20,150 hrs · 19,569 cycles

NOXIOUS ODOR IN ACFT WITH BOTH PACKS ON AND APU RUNNING. PILOT REPORTED ODOR LIKE BURNED PLASTIC. R & R LT AND RT WATER SEPARATOR COALESCER BAGS IAW AMM 21-51-13. OPS CHECKED GOOD. NO ODOR AT THIS TIME.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 20,150 hrs · 19,569 cycles

HOT ELECTRICAL ODOR DETECTED BY ALL CREW STRONGEST PRESCENCE HEAD LEVEL AND NEAR CPB1, 3 APU WAS RUNNING WITH GENERATOR ON AND BLEEDS ENG-OFF ODOR IN COCKPIT FIRST THEN GALLEY APU RUN TIME 40 MINS ODOR LINGERED 3-5 MIN AFTER SHUTDOWN. OPERATED APU WITH PACKS & BLEEDS ON FOR APPROX 1 HR. COULD NOT DUP SMELL. OPS CHECK GOOD IAW AMM 49-10-00.

Part: HINGE — CHAFED (PAX DOOR) · airframe 17,313 hrs · 16,621 cycles

PAX DOOR PIANO HINGE DOOR SIDE HAS MINOR CHAFE. REPAIRED PAX DOOR PIANO HINGE IAW REO 601R-52-11-1347.

Part: LEVER — CHAFED (PAX DOOR) · airframe 17,313 hrs · 16,621 cycles

PAX DOOR FWD LATCH LEVER IS CHAFED. REPAIRED PAX DOOR FWD LATCH LEVER IAW REO 601R-52-11-524.

Part: FLOOR SUPPORT — CRACKED (BS 598-605) · airframe 17,313 hrs · 16,621 cycles

LBL 27, FLOOR SUPPORT IS CRACKED AT NUTPLATE HOLE FWD OF 605 ON OTBD FLANGE C/W REO 601R-53-61-4087.

Part: RIB — CRACKED (LT WING) · airframe 17,313 hrs · 16,621 cycles

LEFT BATTERY RIB IS CRACKED. REPAIRED LT CRACKED BAT RIB IAW REO 601R-57-51-046, REV B, REPAIR NR 3.

Part: FITTING — CHAFED (DOOR SURROUND) · airframe 17,313 hrs · 16,621 cycles

AVIONICS BAY FWD RT FITTING CHAFED. REPAIRED DAMAGE IAW REO 601R-53-21-1297.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 17,313 hrs · 16,621 cycles

SERVICE DOOR EXTERNAL SKIN DAMAGE AROUND DOOR HANDLE RECESS FROM CONTACT WITH DOOR HANDLE. BLENDED TO A SMOOTH FINISH (EA) AREAS IAW REO 601R-52-41-180 AND SRM 51-12-00.

Part: SKIN — CHAFED (LT AILERON) · airframe 17,313 hrs · 16,621 cycles

LT AILERON L/E UPPER SIDE IS CHAFFED AT 8 LOCATIONS. REPAIRED DAMAGE IAW REO 601R-57-60-013.

Part: RETAINER — CRACKED (LT PYLON) · airframe 17,313 hrs · 16,621 cycles

LT PYLON PANEL, 412BT SEAL RETAINER CRACKED. REMOVED UNSERVICEABLE SEAL RETAINER INSTALLED SERVICEABLE RETAINER PN 601-37003299.

Part: SUPPORT BRACKET — CRACKED (CARGO DOOR) · airframe 17,313 hrs · 16,621 cycles

CARGO DOOR FWD TRACK LWR SUPPORT BRACKET CRACKED. R & R BRACKET AT CARGO DOOR FWD TRACK IAW SRM 51-42-06.

Part: RETAINER — CRACKED (RT PYLON) · airframe 17,317 hrs · 16,621 cycles

RT LWR PYLON PANEL 422DB SEAL RETAINER CRACKED. REMOVED UNSERVICEABLE SEAL RETAINER INSTALLED SERVICEABLE RETAINER AND SEAL.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 17,313 hrs · 16,621 cycles

LT INBD FLAP VANE CHAFED IN 3 EA LOCATIONS ON L/E BLEND IAW SRM 51-12-00.

Part: STIFFENER — CHAFED (BS 621) · airframe 17,313 hrs · 16,621 cycles

VERTICAL STIFFENER AT BL 0.00 IS CHAFED FROM 10TH STAGE ISOLATION VALVE BLENDED OUT DAMAGE IAW SRM 51-12-00 & REO 601R-53-61-1523.

Part: HINGE — DAMAGED (PAX DOOR) · airframe 17,317 hrs · 16,621 cycles

PAX DOOR PIANO HINGE FUSELAGE SIDE HAS MINOR CHAFE DAMAGE BLENDED DAMAGE IAW REO 601R-53-21-814, MAT LOSS .025.

Part: PRESSURE BLKHD — CHAFED (BS 621) · airframe 17,317 hrs · 16,621 cycles

REAR PRESSURE BULKHEAD (CARGO SIDE) HAS CHAFE DAMAGE FROM SCREW, BLENDED OUT CHAFE DAMAGE IAW SRM 51-12-00 & REO 601R-53-61-2155.

Part: BULKHEAD — CHAFED (BS 621) · airframe 17,313 hrs · 16,621 cycles

GS 621 BETWEEN BL0 AND LBL9 BETWEEN 2ND AND 3RD ISOLATOR ABOVE FLOOR BULKHEAD SKIN HAS MINOR DAMAGES. BLENDED OUT CHAFED DAMAGE IAW SRM 51-12-00 AND REO 601R-53-61-2155.

Part: STRIKER — CHAFED (BS 310) · airframe 17,313 hrs · 16,621 cycles

FWD AND AFT STRIKER PLATES ON PAX DOOR CHAFED. REPAIRED IAW REO 601R-52-11-296.

Part: SKIN — CHAFED (LT MLG DOOR) · airframe 17,313 hrs · 16,621 cycles

LT MLG DOOR FWD EDGE AT CORNER APPROX W.300 X 4.00 X .035 DEEP CHAFED AREA. CUT AWAY DAMAGE, SMOOTHED AND DEBURRED CUT LINE INSTALLED FILLER AND DOUBLER IAW REO 601R-52-82-102, VIEW A-A REPAIR.

Part: ANGLE — CRACKED (BS 621) · airframe 17,313 hrs · 16,621 cycles

RT OBLIQUE ANGLE CRACKED. REMOVED UNSERVICEABLE OBLIQUE ANGLE AND INSTALLED SERVICEABLE ANGLE IAW REO 601R-53-61-422 AND SRM 51-42-21.

Part: FITTING — CHAFED (EMERGENCY EXIT) · airframe 17,313 hrs · 16,621 cycles

RT OVERWING STOP FITTINGS CHAFED. BLENDED OUT CHAFED AREAS IAW SRM 51-12-00 AND REO 601R-52-21-006. FOUND TO BE WITHIN LIMITS, MAT LOSS .003.

Part: HOUSING — CHAFED (CARGO DOOR HANDL) · airframe 17,313 hrs · 16,621 cycles

CARGO DOOR HANDLE RECESS IS CHAFED BY THE HANDLE. BLENDED OUT CHAFED ARES IAW SRM 51-12-00 AND REO 601R-52-31-086 MAT LOSS .008. FOUND TO BE WITHIN LIMITS.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 16,464 hrs · 15,759 cycles

CARGO DOOR CAUTION JUST AFTER T/O. PRESSURIZATION APPEARED NORMAL. RETURNED TO DEPARTURE, DID NOT LAND OVERWEIGHT, ACARS OOOI TIMES APPEARED NORMAL. UPON ARRIVAL AT GATE, AGENTS REPORT DOOR OUTER HANDLE FLUSH, BUT DOOR APPEARED TO BE NOT FULLY CLOSED. INSPECTED AND OPS CHECKED CARGO DOOR NO DEFECTS NOTED, DOOR WARNING OPS NORMAL, IAW AMM 52-70-00.

Part: COMPRESSOR — DAMAGED (LT ENGINE) · airframe 15,754 hrs · 15,044 cycles

AFTER T/O WITH CLIMB POWER SET, LT ENGINE LOUD NOISE & SHOOK, ITT WENT RED FOR APPROX 3 SECONDS, ACCOMPANIED BY BURNED ODOR IN COCKPIT. C/W QRH, PULLED LT THROTTLE BACK AND AT THAT POINT AMBER VIBE ICON ON LT ENG NR 2, RETURNED TO DEPARTURE, DID NOT LAND OVERWEIGHT. BORESCOPE NR 1 ENG, REF 203569/1, FOUND NUMEROUS BLADES AND VANES OF COMPRESSOR DAMAGED. INCLUDING TEARS, DENT, BEND AND CRACKS, BOTH EDGES. ENGINE REASSEMBLED.

Part: CHECK VALVE — LEAKING (LT ENGINE) · airframe 14,682 hrs · 13,938 cycles

LT ENG LOW OIL PRESSURE MASTER 1 INFLT, OIL PRESS FLUX BETWEEN 35-40 PERCENT PSI, FOLLOWED QRH OIL TEMP NORMAL RANGE, ENG KEPT IDLE DURING DIVERSION APPROX 15 MINUTES OPERATION. REMOVED OIL REPLENISHMENT CHECK VALVE IAW AMM 79-12-13, OPS & LEAK CHECK GOOD, RAN ENGINE FOR 30 MINUTES, CHECKED OIL AT ENGINE TANK, NO OIL ADDED.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 14,578 hrs · 13,826 cycles

FLAPS FAILED AT 6 DEGREES AFRER TAKEOFF ON BOTH SIDES DURING G FLAP RETRACTION RETURNED TO DEPARTURE AND LANDED AT 47000 LBS. COMPLIED WITH SUP 98-018C.1 (AMOC) TROUBLESHOT IAW FIM 27-50-00. PLACED SKEW ON MEL.

Part: SEAL — DIRTY (SERVICE DOOR) · airframe 14,285 hrs · 13,516 cycles

AT GATE- SERVICE DOOR WILL NOT OPEN FROM INSIDE OR OUTSIDE. OPENED AND CLEANED SERVICE DOOR SEAL IAW AMM 52-41-07. FUNCTION CHECKED GOOD.

Part: HANDLE — DAMAGED (SERVICE DOOR) · airframe 14,185 hrs · 13,412 cycles

SERVICE DOOR HARD TO OPEN (FROM INSIDE). CK OPS TEST OF SERVICE DOOR LATCH MECHANISM AND CHECKS BAD DOOR CLOSED AND LOCKED REF 180875/2 FOR MEL CMH 2-12-12:20. REMOVED SERVICE DOOR HANDLE, CLEANED AND LUBED RETURN TUBE AND RETURN GUIDE BOLT IAW AMM 52-41-03, OPS CHECK GOOD, REMOVED FROM MEL.

Part: SEAT TRACK — CORRODED (BS 559-567) · airframe 13,494 hrs · 12,714 cycles

CORROSION FOUND ON BAGGAGE RAIL BTW FS 559.00 +95 TO FS 567.00 AT LBL 9. ON BAGGAGE RAIL BTW FS 559.00 +95 TO FS 567.00 AT LBL 9 REPLACED IAW AMM 53-01-11-400-802. (K)

Part: STRIP — CORRODED (LT NACELLE) · airframe 13,494 hrs · 12,714 cycles

LT ENGINE UPPER CORE COWL INNER WEAR STRIP ERRODED. LT ENGINE UPPER CORE COWL STRIP REPLACED IAW SHORTS CMM 71-12-01-300-820-A01.

Part: STRIP — ERODED (LT NACELLE) · airframe 13,494 hrs · 12,714 cycles

LT ENGINE LWR CORE COWL AFT INNER WEAR STRIP ERODED. AFT INNER WEAR STRIP ON LT ENGINE LWR CORE COWL REPLACED IAW CMM 20-42-06. (K)

Part: BRACKET — CRACKED (RT NACELLE) · airframe 13,494 hrs · 12,714 cycles

RT ENG INBD T/R STOW/THROTTLE LOCK OUT SWITCH BRACKET AT 9 O`CLOCK POS FOUND CRACKED. (K)

Part: PRESSURE BLKHD — CRACKED (BS 202.75) · airframe 13,494 hrs · 12,714 cycles

LT LOWER NOSE HYD COMPARTMENT AT FS 202.75, BL 23.71, WL 69.984, PRESSURE BULKHEAD CRACKED AT PARKING BRAKE LOCATION. LT LOWER NOSE HYD COMPARTMENT AT FS 202.75, BL 23.71, AND WL 69.984 CRACK REPAIRED IAW REO 601R-53-11-1789. (K)

Part: ACCESS PANEL — DAMAGED (RT WING) · airframe 13,494 hrs · 12,714 cycles

RT WING L/E ACCESS PANEL ABOVE LANDING LIGHT BTW W/S 50.54 TO W/S 66.20 FOUND DENTED. RT WING L/E ACCESS PANEL ABOVE LANDING LIGHT BTW W/S 50.54 TO W/S 66.20. REPLACED IAW SRM 51-40-1 SRM 51-40-1 AND SRM 51-24-36. (K)

Part: BRACKET — CRACKED (RT NACELLE) · airframe 13,494 hrs · 12,714 cycles

RT T/R PDU HARNESS BRACKET FOUND CRACKED. RT T/R PDU HARNESS BRACKET REPLACED IAW SRM 51-42-06. (K)

Part: SILL — CRACKED (BS 574) · airframe 13,494 hrs · 12,714 cycles

CARGO BAY FLOOR SILL FOUND CRACKED UNDER STOW PLATE (FWD) BRACKET AT F/S 574, WL 73.00. CARGO BAY FLOOR SILL UNDER STOW PLATE (FWD) BRACKET AT FS 574.00, WL 73.00. REPAIRED IAW REO 601R-53-61-1741, REV N/C. (K)

Part: BRACKET — CRACKED (RT NACELLE) · airframe 13,494 hrs · 12,714 cycles

RT ENG INBD T/R STOW/THROTTLE LOCK OUT SWITCH BRACKET AT 9 O`CLOCK POS FOUND CRACKED. RT ENG INBD T/R STOW/THROTTLE LOCK OUT MICRO SWITCH BRACKET AT 9 O`CLOCK POS REPAIRED/ REPLACED IAW SRM 51-42-06. (K)

Part: LENS — CRACKED (WS 407.08) · airframe 13,494 hrs · 12,714 cycles

CRACK ON LT POSITION LIGHT LENSE. ON LT POSITION LIGHT LENSE REPLACED IAW AMM 51-30-01-400-801. (K)

Part: BRACKET — CRACKED · airframe 13,494 hrs · 12,714 cycles

RT MLG BAY (2) HYDRAULIC SUPPORT BRACKETS CRACKED. RT MLG BAY (2) HYD BRACKET REPLACED IAW SRM 51-42-06. (K)

Part: CARGO TRACK — CORRODED (BS 559+95) · corrosion level 1 · airframe 13,494 hrs · 12,714 cycles

CORROSION FOUND ON BAGGAGE RAIL BTW FS 559.00 +95 TO FS 567.00, RBL 9 ON BAGGAGE RAIL BTW FS 559.00 +95 TO FS 567.00, RBL 9 REPLACED IAW AMM 53-01-11. (K)

Part: BRACKET — CRACKED (BS 718) · airframe 13,494 hrs · 12,714 cycles

AFT EQUIPMENT COMPARTMENT, RT HYD MANIFOLD (SYS 2) SUPPORT BRACKET CRACKED (AFT LOWER AREA) CRACK 10 MM LONG. AFT EQUIPMENT COMP RT HYD MANIFOLD (SYS) SUPPORT BRACKET REPAIRED IAW REO 601R-53-62-031, REV A. (K)

Part: SILL — CORRODED (BS 562.72) · corrosion level 1 · airframe 13,494 hrs · 12,714 cycles

CORROSION ON CARGO FLOOR SILL AROUND NUT PLATE BTW FS 562.72 AND FS 621.00. CARGO BAY FLOOR SILL AROUND NUT PLATES BTW FS 562.72 AND FS 621.00 CORROSION REMOVED IAW SRM 51-21-06. (K)

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 13,494 hrs · 12,714 cycles

PASSENGER DOOR STAIR AFT DRAG ANGLE AT F/S 349.00 IS CRACKED. (1.00" LONG) PASSENGER DOOR STAIR AFT DRAG ANGLE AT FS 349.00 REPAIRED IAW REO 601R-52-11-513, REV A. (K)

Part: STRUCTURE — CRACKED (APU BAY) · airframe 13,494 hrs · 12,714 cycles

(2) CRACKS FOUND ON APU ENCLOSURE. FWD UPPER EDGE (.250" X .400" LONG) (2) CRACKS ON APU ENCLOSURE FWD UPPER EDGE REPAIRED IAW REO 601R-44-11-071. (K)

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 13,494 hrs · 12,714 cycles

PASSENGER DOOR EDGE MEMBER FWD AREA CRACKED (1.250 LONG). REPAIR TO PASSENGER DOOR EDGE MEMBER FWD AREA IAW REO 601R-52-11-279, REV NC. (K)

Part: ACCESS PANEL — DAMAGED (RT WING) · airframe 13,494 hrs · 12,714 cycles

RT WING BUTTE DOOR ACCESS PANEL 694 JB STOP ASSY FOUND DAMAGED. RT WING BUTTE DOOR ACCESS PANEL 694 JB STOP ASSY REPLACED IAW SRM 51-42-06. (K)

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 1 · airframe 13,494 hrs · 12,714 cycles

CORROSION FOUND ON BAGGAGE RAIL BTW FS 559.00 +95 TO FS 567.00 AT LBL 9. ON BAGGAGE RAIL BTW FS 559.00 +95 TO FS 567.00 AT LBL 9 REPLACED IAW AMM 53-01-11-400-802. (K)

Part: SUPPORT BRACKET — CRACKED (WS 266.51) · airframe 13,494 hrs · 12,714 cycles

CRACK ON SUPPORT BRACKET OF RT OTBD FLAP CTR HINGE ARM (LENGTH 0.750:). SUPPORT BRACKET ON RT OTBD FLAP CENTER HINGE ARM REPLACED IAW SRM 51-42-13 AND 51-42-06. (K)

Part: BULKHEAD — CRACKED (BS 621) · airframe 13,494 hrs · 12,714 cycles

FS 621.00 AFT PRESSURE BULKHEAD LT CRACKED AT LINTEL/LOCATION W/L 106.117 (.100 LONG). FS 621.00 AFT PRESSURE BULKHEAD LT CRACK AT LINTEL FITTING LOCATION W/L 106.117. REPAIRED IAW REO 601R-53-61-1230, REV D. (K)

Part: BRACKET — BROKEN (THRUST REVERSER) · airframe 13,494 hrs · 12,714 cycles

RT ENG THRUST REVERSER STOWED SWITCH MOUNTING BRACKET BROKEN. RT ENGINE THRUST REVERSER STOWED SWITCH MOUNTING BRACKET REPLACED IAW SHORT CMM 20-42-06. (K)

Part: STOP — WORN (LT MLG DOOR) · airframe 13,494 hrs · 12,714 cycles

LT MLG DOOR L/E WORN AT STOP LOCATION. LT MLG DOOR L/E AT DOOR STOP REPAIRED IAW REO 601R-53-82-016, REV N/C. (K)

Part: DOOR TRACK — CRACKED (BS 621) · airframe 13,494 hrs · 12,714 cycles

CRACK FOUND RT END OF CARGO DOOR TRACK AT FS 621.00, LBL 27.00, W/L 130.00 ON AFT PRESSURE BULKHEAD (.200) AT END OF CARGO DOOR TRACK AT F/S 621.00, LBL 27.00 W/L 130.00 ON AFT PRESSURE BULKHEAD REPAIR PERFORMED IAW REO 601R-53-61-1541, REV B. (K)

Part: SHIM — CORRODED (BS 319) · airframe 13,494 hrs · 12,714 cycles

SERVICE DOOR THRESHOLD PLATE SHIM (LAMINATED) CORRODED. SERVICE DOOR THRESHOLD PLATE SHIM (LAMINATED) CORROSION REMOVED IAW SRM 51-21-06. (K)

Part: STRIP — ERODED (RT ENGINE) · airframe 13,494 hrs · 12,714 cycles

RT ENGINE LOWER FAN COWL AFT EDGE STRIP IS CHAFED/ERRODED. REMOVED AND REPLACED IAW CMM SHORTS TASK 71-14-01-300-814-A01.

Part: COWLING — ERODED (RT NACELLE) · airframe 13,494 hrs · 12,714 cycles

RT UPPER FAN COWL T/E IS CHAFED/ERODED. REPLACED IAW SHORTS CMM 71-14-01-300-814-A01.

Part: SKIN — GOUGED (LT WING) · airframe 13,494 hrs · 12,714 cycles

LT WING LWR PLANK ACCESS HOLE CUT OUT 540DB VERTICAL SURFACE FOUND GOUGED (.100 X .005" W X .008 DEEP APPROX). LT WING LWR PLANK ACCESS HOLE CUTO OUT 540DB VERTICAL SURFACE REPAIR C/O IAW EO NR E06/021/457. (K)

Part: BRACKET — CRACKED (BS 473.15) · airframe 13,494 hrs · 12,714 cycles

LT MLG BAY FS 473.15 HYD SUPPORT CRACKED (1 X .500" LONG). HYD SUPPORT BRACKET ON LT MLG BAY REPLACED IAW SRM 51-42-06. (K)

Part: FLOORBEAM — CRACKED (BS 484) · airframe 13,494 hrs · 12,714 cycles

PRESSURE FLOORBEAM FS 484.00, LBL 27.00 AND 36.00 CRACKED. PRESSURE FLOORBEAM FS 484.00, LBL 27.00 AND 36.00 REPAIR PERFORMED IAW REO 601R-53-41-059, REV A. (K)

Part: FLOORBEAM — CRACKED (BS 484) · airframe 13,494 hrs · 12,714 cycles

PRESSURE FLOOR INTERCOSTAL FS 484.00, RBL 27.00 AND 36.00 CRACKED. PRESSURE FLOOR INTERCOSTAL FS 484.00, RBL 27.00 AND 36.00 DAMAGE CUTOUT, C/C PERFORMED AND REPAIR DONE IAW REO 601R-53-41-050, REV. (K)

Part: PANEL — CRACKED (PAX DOOR) · airframe 13,494 hrs · 12,714 cycles

PASSENGER DOOR STAIR AFT SIDE PANEL AT FS 349.00 FOUND CRACKED IN ZONE 2 AND ZONE 3. STAIR ON AFT SIDE PANEL AT FS 349.00 ON REPAIRED IAW REO 601R-52-11-702 REV A ZONE 2 AND 3. (K)

Part: SKIN — CORRODED (LT WING) · corrosion level 1 · airframe 13,494 hrs · 12,714 cycles

LT WING LOWER PLANK ACCESS HOLE CUT OUT 540BB LOWER SURFACE CORRODED. LT WING LOWER SURFACE PLANK ACCESS HOLE CUT OUT 540BB LOWER SURFACE REPAIR C/O IAW E06/021/457. (K)

Part: SKIN — GOUGED (LT WING) · airframe 13,494 hrs · 12,714 cycles

LT WING LOWER PLANK ACCESS HOLE CUT OUT 540FB VERTICAL SURFACE FOUND GOUGED (.100L X .005" W X .006" DEEP). LT WING LWR PLANK ACCESS HOLE CUT OUT 540FB VERTICAL SURFACE REPAIR C/O IAW EO E06/021/457. (K)

Part: STIFFENER — CRACKED (PAX DOOR) · airframe 13,494 hrs · 12,714 cycles

PASSENGER DOOR, POWER ASSIST MOTOR STIFFNER AT F/S 349.00 C. 150" LONG. POWER ASSIST MOTOR STIFFNER AT FS 349.00 ON PASSENGER DOOR REPLACED IAW SRM 51-42-06. (K)

Part: BULKHEAD — CRACKED (BS 280) · airframe 13,494 hrs · 12,714 cycles

PILOT BULKHEAD AT FS 280.00, RBL 11.00 FOUND (2) GOUGES BTWN STR 13A AND 14A (SIZE 2.75" L X .230" W X .020 DEEP) EACH. REPAIR PERFORMED ON PILOT BULKHEAD AT FS 280.00, RBL 11.00 IAW REO 601R-53-11-1727, REV C. (K)

Part: WHEEL — LOOSE (NLG & MLG) · airframe 11,535 hrs · 10,832 cycles

LOG 193468/1 EXTREME VIBRATION ON TAKEOFF ROLL. ABORTED TAKEOFF AT 85 KNOTS. BRAKE TEMPS WERE 3,3,2,3. INSPECTED AND RETORQUED NR 1 NLG TIRE, NR 1 MLG TIRE AND NR 4 MLG TIRE IAW CRJ AMM 32-42-01, 32-41-01 AND AMM SUP 08056. NO DEFECTS NOTED.

Part: NUT — LOOSE (CONTROL WHEEL) · airframe 9,872 hrs · 9,262 cycles

DURING AILERON CHECK, BONDING OF CONTROLS FROM LEFT TO RIGHT FROM NEUTRAL AND BACK TO NEUTRAL FROM RIGHT ON BOTH YOKES. TORQUED PILOTS AND CO-PILOTS CONTROL WHEEL LATCHING NUT IAW AMM 27-11-01. OPS CHECK GOOD. OK FOR FURTHER SERVICE. (K)

Part: PCU — FAILED (SPOILERS) · airframe 9,483 hrs · 8,870 cycles

SPOILERONS FAULT STATUS MESSAGE ILLUMINATED. NOTE: THIS OCCURRED ON THE GROUND. AFTER MDC INTERROGATION FOUND SECU 2A LABEL 350 CODE: 00402 CODE: LT IB PCU FAIL. SWAPPED SECU UNITS TO PUT 49-164-05 IN THE NR 1 POSITION AND PLACED PCU ON MEL 27-62-03. (K)

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 9,364 hrs · 8,750 cycles

EXTERNAL AIR COUPLING DOOR FRAME CRACKED AND BENT. (K) REPAIRED IAW BSC EO 601R-53-14474A. (M)

Part: FRAME — CHAFED (FUSELAGE) · airframe 9,364 hrs · 8,750 cycles

LT FUSELAGE FRAME AT STR 654.00 HAS CHAFED BETWEEN STR 8L AND STR 9L FROM THE 10TH STAGE BLEED DUCT TIE ROD. (K) REPAIRED FRAME IAW BSC EO 601R-53-14477 BY TRIMMING OUT DAMAGE AND INSTALLING REPAIR ANGLE. (M)

Part: INTERCOSTAL — CRACKED (BS 484)

FOUND INTERCOSTAL AT FS 484 IS CRACKED. MAINTENANCE REMOVED CRACKED UNSERVICEABLE INTERCOSTAL CLIP AT FS 484 RBL 27 AND REPLACED WITH NEW SERVICEABLE CLIP, P/N 601R31171-9, IAW BSC 601R-53-0029B AND CRJ SRM 51-42-21. (M)

Part: SKIN — CORRODED (RT WING)

RIGHT WING LOWER PLANK FUEL ACCESS DOOR CUTOUT 650BB, WS 54.897, HOLE NR 1, HAS PITTING CORROSION ON INBOARD AND OUTBOARD ENDS IN NON-CRITICAL AREA MEASURES APPROX 10.5 INCH LONG BY .25 INCH WIDE BY .009 INCH DEEP AND 5.5 INCH LONG BY .25 INCH WIDED BY .006 INCH DEEP. MAINTENANCE REPAIRED IAW AWAC EO E06/021/457 AND BOMBARDIER REO 601R-57-21-030 REV F. (M)

Part: FLOOR SUPPORT — CRACKED (BS 280)

FOUND FLOOR SUPPORT STRUCTURE CLIP AT FS 280, LBL 9, OUTBOARD IS CRACKED IN RADIUS APPROX .5 INCH LONG. MAINTENANCE REMOVED CRACKED CLIP AT FS 280 LBL 9.0 OUTBOARD. LOCATED, DRILLED, INSTALLED NEW SERVICEABLE CLIP, P/N 601R31113-57, IAW CRJ SRM 51-42-13, 51-42-21 AND BSC SR 601R-53-0057A. (M)

Part: FLOOR SUPPORT — CRACKED (BS 280)

FOUND FLOOR SUPPORT STRUCTURE CLIP AT FS 280, RBL 9, OUTBOARD IS CRACKED IN RADIUS APPROX .6 INCH LONG. MAINTENANCE REMOVED CRACKED CLIP AT FS 280 RBL 9.0 OUTBOARD LOCATED, DRILLED, INSTALLED NEW SERVICEABLE CLIP, P/N 601R31113-58 IAW CRJ SRM 51-42-13, 51-42-21 AND BSC SR 601R-53-0057A. (M)

Part: LINK — DAMAGED (ELEVATOR PCU)

RIGHT ELEVATOR NR 2 PCU ATTACH FITTING LINK, BOTTOM LOCK FASTENER HAS SHEARED. MAINTENANCE REMOVED SHEARED LOCK FASTENER AND INSTALLED NEW SERVICEABLE LOCK FASTENER AND COLLAR IAW CRJ200 SRM 51-42-21. (M)

Part: FLOOR SUPPORT — CRACKED (BS 621)

FOUND LT FS 621 FLOOR SUPPORT ANGLE CRACKED APPROX .75 INCH LONG. MAINTENANCE CUT AWAY DAMAGED SECTION OF ANGLE AND INSTALLED REPAIR ANGLE AND DOUBLER IAW BOMBARDIER REO 601R-53-61-117 REV C. (M)

Part: FLOOR SUPPORT — CRACKED (BS 280)

FOUND FLOOR SUPPORT STRUCTURE CLIP AT FS 280, LBL 9, INBOARD IS CRACKED IN RADIUS APPROX .3 INCHES LONG. MAINTENANCE REMOVED INBOARD 280 CLIP AT LBL 9 AND REINSTALLED NEW SERVICEABLE CLIP P/N 601R31113-57, IAW CRJ SRM 51-42-21 AND BSC STANDARD REPAIR 601R-53-0057A. (M)

Part: SKIN — CORRODED (LT WING)

LT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT 510AB, WS 12.245, HOLE NR 2 HAS PITTING CORROSION AT INBOARD AND OUTBOARD ENDS IN NON-CRITICAL AREA MEASURES APPROX 9.5 INCH LONG BY .25 INCH WIDE BY .005 INCH DEEP AND 3.5 INCH LONG BY .20 INCH WIDE BY .007 INCH DEEP. MAINTENANCE REPAIRED IAW AWAC EO E06/021/457 AND BOMBARDIER REO 601R-57-030 REV F. (M)

Part: FLOOR SUPPORT — CRACKED (BS 280)

FOUND FLOOR SUPPORT STRUCTURE CLIP AT FS 280, RBL 9, INBOARD IS CRACKED IN RADIUS APPROX .5 INCH LONG. MAINTENANCE REMOVED INBOARD FS 280 CLIP AT RBL 9 AND INSTALLED SERVICEABLE CLIP P/N 601R31113-58, IAW CRJ 200 SRM 51-42-21 AND BSC STANDARD REPAIR 601R-53-0057A. (M)

Part: SKIN — CORRODED (LT WING)

LT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT 540BB, WS 54.897, HOLE NR 1, HAS PITTING CORROSION AT INBOARD AND OUTBOARD ENDS IN NON-CRITICAL AREA. MEASURES APPROX .3 INCH LONG BY .20 INCH WIDE BY .005 INCH DEEP EACH. MAINTENANCE REPAIRED IAW AWAC EO E06/02/457 AND REO 601R-57-21-030 REV F. (M)

Part: FLOOR SUPPORT — CRACKED (BS 621)

FOUND RIGHT FS 621 FLOOR SUPPORT ANGLE CRACKED APPROX .75 INCH LONG. MAINTENANCE CUT AWAY DAMAGED SECTION OF ANGLE AND INSTALLED REPAIR ANGLE AND DOUBLE IAW BOMBARDIER REO 601R-53-61-117 REV C. (M)

Part: INTERCOSTAL — CRACKED (BS 621-625)

FOUND RIGHT SIDE FS 621 TO FS 625.30 INTERCOSTAL AT STRINGER 14R IS CRACKED NEAR RADIUS APPROX 1 INCH LONG. MAINTENANCE REMOVED RT INTERCOSTAL FS 621 TO 625.30 IAW CRJ 200 SRM 51-42-06. INSTALLED NEW INTERCOSTAL P/N 601-35012-52 IAW CRJ 200 SRM 51-42-06. (M)

Part: INTERCOSTAL — CRACKED (BS 621-625)

FOUND LT SIDE FS 621 TO FS 625.30 INTERCOSTAL AT STRINGER 14L IS CRACKED NEAR RADIUS APPROX 1.1 INCH LONG. MAINTENANCE REMOVED LT INTERCOSTAL FS 621 TO FS 625.30 IAW CRJ 200 SRM 51-42-06. INSTALLED NEW INTERCOSTAL P/N 601-35012-51 IAW CRJ 200 SRM 51-42-06. (M)

Part: SWITCH — FAULTED (STAB TRIM)

IN FLIGHT STAB CHANNEL 1 DISENGAGED, ABLE TO REENGAGE NO PROBLEM DURING APPROACH BOTH STAB TRIM AND MACH TRIM FAILED, UNABLE TO REENGAGE. AIRCRAFT CONFIGURATION WAS AUTOPILOT OFF, FLAPS 20 AND TRIM 3.8 COMPLIED WITH QRH AND LANDED. FIRST OFFICERS STAB TRIM DISCONNECT SWITCH FOUND AT FAULT. REMOVED AND REPLACED PER AMM 27-41-30-400-802. (M)

Part: POTENTIOMETER — OUT OF ADJUST (T/E FLAP) · airframe 6,974 hrs · 6,430 cycles

FLAPS FAIL CAS MSG AT ZERO DEGREES, LANDING WEIGHT 40,000 LBS, TOUCHDOWN SPEED 160 KNOTS, MAX BRAKE TEMP = 6.0 FLAP LANDING PERFORMED RIG CHECK OF BPSU`S, IAW AMM 27-51-10, FOUND NR 6 AND NR 7 POTENTIOMETERS OUT OF ADJUSTMENT. ADJUSTED POTENTIOMETERS AND PERFORMED CHECK AGAIN. FOUND TEST TO BE COMPLETE. AC GOOD FOR RETURN TO SERVICE. ADDITIONAL: UPON FURTHER INSPECTION OF FLAPS IN HANGAR, FOUND SLUSH AND ICE PACKED INSIDE RT IB FLAP WING TRAILING EDGE APPROX .7500 INCH THICK AND 36 INCHES LONG. ICE MELTED OUT ON RT IB FLAP, DEPOWERED AND REPOWERED AC AND FLAP SYS RESET IAW SUPP 98-018A. (K)

Part: LOOP — FAILED (FUSELAGE) · airframe 4,141 hrs · 3,736 cycles

DURING CLIMB (ANTI-ICE DUCT OVERHEAT) MESSAGE ILLUMINATED ALSO ON OVERHEAD PANEL WING (OVHT) CAPTION (ON) ON SYNOPTIC PAGE (ANTI-ICE) INDICATED FUSELAGE IN RED. REMOVAL AND REPLACED AFT LT LOOP IAW AMM ON W/O 92640 GROUND RAN AIRCRAFT, OPS CHECKED ANTI-ICE DUCT, LT SIDE OK AT THIS TIME. (K)

Part: COALESCER BAG — DIRTY (A/C BAY) · airframe 2,256 hrs · 1,965 cycles

STRONG FUEL SMELL IN COCKPIT AT CRUISE. SMELL INCREASED WITH TEMP SELECTED IN MANUAL MODE. SELECTED LT PACK OFF, SMELL WENT AWAY. INSPECTED APU AREA, PACK NR 1 AND NR 2, NO LEAKS NOTED. NO EVIDENCE OF FUEL AROUND ENGINES OR APU. REAM ENGINE AND BOTH PACKS, NO SMELL OF FUEL ON RUNS. SUSPECT DIRTY LT COALESCER BAG ON LT PACK. PLACED ON MEL. (K)

Part: FLAP — STUCK (WING TE) · airframe 1,488 hrs · 1,294 cycles

FLAPS FAIL CAS AND FLAPS STUCK AT 20 DEGREES ON APPROACH. RESET FLAPS SYSTEM IAW SUPPLEMENT 98-18, NO FURTHER DISCREPANCIES.

Part: FLAP — MALFUNCTIONED (WING) · airframe 1,511 hrs · 1,313 cycles

FLAPS FAIL CAS AND FLAPS STUCK AT 20 DEGREE ON APPROACH. RESET FLAP SYSTEM IAW AWAC SUPPLEMENT 98-18. NO FURTHER DISCREPANCIES.