N468AW

Part: TIRE — FAULTED (MLG) · airframe 41,434 hrs · 40,648 cycles

RISING BTMS ON #2 TIRE AFTER LANDING. MINIMAL BRAKING. ON TAXI IN BTMS CONTINUED TO RISE. APPROACHING GATE BRAKE OVER HEAT WARNING BTMS VALUE 11 Q/W QRH. AFTER PARKING #2 TIRE OFF RIM WITH OCCASIONAL SMOKE. AIRCRAFT REMOVED FROM SERVICE. INSP #2 BREAK TIRE AND HARNESS IAW AMM 05-51-27 REQ BOTH L/H MAIN LANDING GEAR WHEEL REPLACED ,BTMS SENSORS SENSOR ON #2, BREAK AND #2 WHEEL SPEED SENSOR. R&R #1 MLG TIRE WHEEL ASSEMBLE IAW AWAC SUPP 12-015M COMPLIED WITH THE M061 INSTRUCTIONS, THE SPACER AND WASHER WERE RETAINED FROM THE REMOVED WHEEL ASSEMBLY AND USED ON THE INSTALLED WHEEL ASSEMBLY. R&R#2 MLG TIRE ASSEMBLY IAW AWAC 12-015M COMPLIED WITH THE M061 INSTRUCTIONS, THE SPACER AND WASHER WERE RETAINED FROM THE REMOVED WHEEL ASSEMBLY AND USED ON THE INSTALLED WHEEL ASSEMBLY.

Part: FITTING — GOUGED (W.S.424, RBL45) · airframe 40,356 hrs · 39,404 cycles

UPON REMOVAL OF THE R/H WING TO FSLG FITTING, FOUND DAMAGE ON FITTING. ******AIRCRAFT REMOVED FROM SERVICE******** REPAIRED R/H WING TO FUSELAGE FITTING AND UPPER WING SKIN AT W.S.424, RBL 45 IAW MHIRJ REO 601R-57-11-101.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,193 hrs · 39,222 cycles

WHEN SELECTING GEAR UP ON TAKE-OFF, GOT GEAR DISAGREE WARNING. RAN QRH AND GEAR EXTENDED NORMALLY. NOSE GEAR RED SYMBOL AND NOSE DOOR OPEN RED WARNING. GEAR DISAGREE MESSAGE APPEARED WITHIN 5 SECS. *******AIRCRAFT REMOVED FROM SERVICE*********** VISUALLY INSPECTED NLG. NO OBVIOUS DAMAGE, LEAKS OR DEFECTS NOTED TO GEAR ASSY, RETRACTION COMPONENTS OR PROXI SENSORS. C/W "M" ACTION FOR MEL 32-30-01. GEAR PINS INSTALLED AND FLAGS REMOVED.

Part: FUEL CAP — CORRODED · corrosion level 2 · airframe 40,106 hrs · 39,113 cycles

LH AND RH OVER WING FUEL CAP RING AREAS SHOWN SIGNS OF CORROSION AND DETERMINED OUTSIDE OF SRM LIMITATIONS. ***** AC REMOVED FROM SERVICE ***** BLEND REPAIR IAW MHI TECH DATA AS PROVIDED.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 36,677 hrs · 38,656 cycles

CORROSION ON CARGO FLOOR SILL PN601R31132-58 AT FS605.00+5 AND RBL42. ***** AC REMOVED FROM SERVICE ***** REPLACED FLOOR SILL SUPPORT ANGLE WITH A NEW FABRICATED ANGLE 601R AT FS559 AND LBL28.00. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW CRJ200 SRM 51-26-00, SRM 51-61-43, SRM 53-00-00, SRM 51-11-00, SRM 51-25-06, SRM 51-12-00 REV 39, SRM51-25-06 REV 39, AND SRM 51-25-16 REV 39. WORK PERFORMED UNDER AERSALE WORK ORDER 003870, CARD NO. 20064, TT: 39,677:48 TC: 38,656.

Part: RUDDER — DENTED (RUDDER) · airframe 39,677 hrs · 38,656 cycles

DENT ON LH RUDDER RS 125.44-RS131.17 *******AIRCRAFT REMOVED FROM SERVICE****** REPAIRED DENT ON LH RUDDER AT RS125.44-RS131.17 AND FOUND TO BE ACCEPTABLE PER REO. DENT DIMENSION L = 1.500Ï¿½ X W = 1.150Ï¿½ X D = 0.027Ï¿½. PERFORMED HFEC WITH NO INDICATIONS. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP REO 601R-55-41-278 REV 2021-05 DATED 4/27/2023.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 39,677 hrs · 38,656 cycles

LH WING INBOARD FLAP IB FLAP HAS CHAFFING PN 601R14303-41 LH WING LEADING EDGE SKIN MID IB FLAP PN 601R14303-39 ****AIRCRAFT REMOVED FROM SERVICE********* LH WING INBOARD FLAP IB FLAP HAS CHAFFING PN 601R14303-41 LH WING LEADING EDGE SKIN MID IB FLAP PN 601R14303-39 BLENDED OUT 2 EA P1 AND P2 ON LE FLAP IB VANE SKIN IAW EA# AWAC-CRJ257-01979 AND EA# AWAC-CRJ257-01980. BLENDED CHAFF DAMAGES TO A SMOOTH CONTOUR. RESTORED SURFACE PROTECTIVE FINISH. ALL WORK WITHIN LIMITS PERFORMED IAW EA#: AWAC-CRJ257-01979 REV IR AND EA#: AWAC-CRJ257-01980 REV IR DATED 4/12/2023. WORK PERFORMED UNDER AERSALE WORK ORDER 003870, CARD NO. 20061, TT: 39,677:48 TC:38,656.

Part: STIFFENER — DENTED (APU ENCLOSURE) · airframe 39,677 hrs · 38,656 cycles

DENT ON V STIFFENER ON AFT ACCESS PANEL PN#15A150-1 OF APU ENCLOSURE ASSY PN#15A104-103) *****AIRCRAFT REMOVED FROM SERVICE********* DENT ON V STIFFENER ON AFT ACCESS PANEL PN#15A150-1 OF APU ENCLOSURE ASSY PN#15A104-103) EVALUATED DENTED AREA AT V STIFFENER ON APU ENCLOSURE AFT ACCESS PANEL 311BZ, FOUND TO BE STRUCTURALLY ACCEPTABLE PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW MHIRJ REO#601R-49-11-215 REV--DATED 4/12/2023.WORK PERFORMED UNDER AERSALE WORK ORDER 003813, CARD NO. 70000, TT: 39,454:52 TC: 38,132.

Part: FLOOR SUPPORT — CORRODED (FS559) · corrosion level 2 · airframe 39,677 hrs · 38,656 cycles

CORROSION ON RH FLOOR SILL STRAP PN# 601R31133-1225 AND LIPPED PLATE PN#601R31133-101 AT FS559.00+12-559-80 FS559 .00+112-559.00+80 AND RBL28.00 *******AIRCRAFT REMOVED FROM SERVICE******** REPLACED FLOOR SILL WITH A NEW FABRICATED P/N 601R31133-1225 AT FS559 AND LIPPED PLATE PN#601R31133-101. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW CRJ200 SRM51-11-00 REV 39, SRM 51-12-00 REV 39, SRM 51-40-06 REV 39, SRM 51-42-06 REV 39, SRM 53-00-00 REV 39, SRM 53-51-43 REV 39. WORK PERFORMED UNDER AERSALE WORK ORDER 003870, CARD NO. 20117, TT: 39,677:48 TC: 38,656.

Part: RUDDER — DENTED · airframe 36,677 hrs · 38,656 cycles

DENT ON SKIN RUDDER AT RS121.80 *******AIRCRAFT REMOVED FROM SERVICE****** DENT ON SKIN RUDDER AT RS121.80 EVALUATED DENT ON RUDDER AT RS 121.80 AND FOUND TO BE ACCEPTABLE PER EA. DENT DIMENSION L = 1.90Ï¿½ X W = 0.400 X D = 0.012Ï¿½. PERFORMED HFEC WITH NO INDICATIONS. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA # AWAC-CRJ255-01977 REV IR DATED 4/08/2023. WORK PERFORMED UNDER AERSALE WORK ORDER 003870, CARD NO. 20042, CARD ID 1870963 TT: 39,677:48 TC: 38,656

Part: FLOOR SUPPORT — CORRODED (FS621) · corrosion level 2 · airframe 39,677 hrs · 38,656 cycles

BLENDED CORROSION ON RH FLOOR SUPPORT STRUCTURE BETWEEN FS621.00 AT RBL 9 AND RBL 27 ******AIRCRAFT REMOVED FROM SERVICE******* CORROSION 2 AREAS ON RH FLOOR SUPPORT STRUCTURE BETWEEN FS621 .00 AT RBL 27 BLENDED CORROSION ON RH FLOOR SUPPORT STRUCTURE BETWEEN FS621.00 AT RBL 9 AND RBL 27. REPAIRED FITTING ASSY PN#601R35280-2 ANGLE PN#601R35031-275 P1 - L= 2.10Ï¿½ X W= 0.800Ï¿½ X D= 0.007Ï¿½ RBL 9+10.5 P2 - L= 2.400Ï¿½ X W= 0.850Ï¿½ X D= 0.005Ï¿½ RBL 9+5 FITTING ASSY PN601R35280-2 FS605.0+7 AND RBL9 P1=L=2.5Ï¿½X W=1.1 X D=0.038Ï¿½ CUT DIMENSIONS- L=2.500Ï¿½ X W=1.00Ï¿½ FS605.0+7 BLENDED 2AREAS ON RH FLOOR SILL BETWEEN FS621.00 AND RBL9- 27 AND REPAIRED FITTING ASSY PN#601R35280-2 ANGLE ORIGINAL THICKNESS 0.094 REMAINING STRAP THICKNESS 0.087 AND FITTING ASSY THICKNESS 0.080. PERFORMED HFEC WITH NO INDICATIONS. RESTORED SURFACE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW CRJ200 NDT 51-20-06 REV 44 SRM 51-25-06 REV 39SRM 51-25-16 REV 39, SRM 51-12-00 REV 39, SRM 53-61-43 REV 39, SRM 53-63-43 REV 39, SRM 53-31-59 REV 39, SRM 53-00-00 REV 39, MHIRJ REO 601R53- 61-8014 REV 2021-02 AND. WORK PERFORMED UNDER AERSALE WORK ORDER 003870, CARD NO. 20116, TT: 39,677:48 TC: 38,656.

Part: BRACKET — CORRODED (PAX DOOR) · corrosion level 2 · airframe 39,677 hrs · 38,656 cycles

CORROSION ON PASSENGER DOOR LOWER SILL AT BETWEEN FS310.00 AND FS349.00. ***** AC HAS BEEN REMOVED FROM SERVICE ***** BLENDED CORROSION ON PASSENGER DOOR LOWER SILL AT BETWEEN FS310.00 AND FS349.00. BRACKET P/N 601R31527-217. MEASUREMENTS P1-L=5.900Ï¿½ X W=1.100Ï¿½X D=0.006Ï¿½ FS310.00 +6 P2L=5.900Ï¿½ X W=1.100Ï¿½X D=0.023Ï¿½ FS333.00+11 ORIGINAL THICKNESS 0.063Ï¿½, REMAINING THICKNESS 0.057 MATERIAL REMOVED .006Ï¿½

Part: SEAT TRACK — CORRODED (FS589 TO FS605) · corrosion level 2 · airframe 39,677 hrs · 38,656 cycles

CORROSION ON SEAT RAIL AT FS589.00+8 TO FS605.00 & LBL27. P1-L=1.800Ï¿½X W=0.900Ï¿½X D=.050 AIRCRAFT REMOVED FROM SERVICE. CORROSION ON SEAT RAIL BLENDED CORROSION ON SEAT RAIL FS589.00+8 & RBL27.ORIGINAL MATERIAL THICKNESS 0.050Ï¿½ & REMAINING THICKNESS 0.00Ï¿½. PERFORMED A CUTOUT WITH DIMENSIONS L=2.093Ï¿½X W=0.531 AT APPROX. FS600 LBL 27 INBOARD FLANGE IAW REO 601R-53-61-8008, STANDARD S6144 CMS6144 REV--. PERFORMED HFEC INSP AT CUTOUT AREA ON CARGO FLOOR FRAME AT FS600 LBL 27 INBOARD FLANGE NO INDICATIONS NOTED IAW NDT PART 1 51-50-06 12/2023 NO INDICATIONS. RESTORED SURFACE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW CRJ200 SRM 51-12-00 REV 39, SRM 51-26-00 REV 39, SRM 53-61-43 REV 39, AND SRM 53

Part: CONTROLLER — FAILED (NR 3) · airframe 39,361 hrs · 38,330 cycles

R WINDOW HEAT CAUTION MESSAGE IN FLIGHT. INFLIGHT SMELT ELECTRICAL SMELL. C/W QRH MESSAGE CLEARED. AIRCRAFT REMOVED FROM SERVICE. FOUND RT WINDSHIELD HEAT CONTROLLER HAS BURNED SMELL, R&R RT WINDSHIELD HEAT CONTROLLER IAW AMM 30-41-01 PERFORMED RT WINDOW AND WINDSHIELD ADJUSTMENT TEST IAW AMM 30-41-01 OPS CHECK GOOD.

Part: RELIEF VALVE — FAULTED (LEFT) · airframe 39,244 hrs · 38,224 cycles

LH COWL ANTI ICE CAU IN FLT WITH COWL SWITCH SELECTED OFF. C/W QRH RETURNED TO DAY, AIRCRAFT REMOVED FROM SERVICE. R & R THE RELIEF VALAVE OF LT ENG IAW AMM 30-22-04 , OPS CHECKED GOOD.

Part: SKIN — DENTED · airframe 37,701 hrs · 36,690 cycles

MULTIPLE DENTS AND GOUGES ON AFT FUSELAGE SKIN BTW FS589.00 Ï¿½ FS605.00 AND STR24R Ï¿½ STR26R. DRESSED 4 DENTS AND BLENDED 22 GOUGES ON AFT FUSELAGE SKIN BTW FS589.00 Ï¿½ FS605.00 AND STR24R Ï¿½ STR26R. SKIN PN 601R35005. POST DRESS DENT DIMENSIONS P1 - L= 0.700Ï¿½ X W= 0.500Ï¿½ X D= 0.004Ï¿½, P2 - L= 0.300Ï¿½ X W= 0.300Ï¿½ X D= 0.002Ï¿½, P3 - L= 0.400Ï¿½ X W= 0.400Ï¿½ X D= 0.004Ï¿½ AND P4 - L= 0.200Ï¿½ X W= 0.200Ï¿½ X D= 0.002Ï¿½. GOUGE REMAINING THICKNESS DIMENSIONS RANGE FROM 0.046Ï¿½- 0.058Ï¿½. HFEC PERFORMED WITH NO INDICATIONS. RESTORED SURFACE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW MHIRJ REO 601R-53-61-7732 REV (-) DATED 2021-10-23. WORK PERFORMED UNDER AERSALE WORK ORDER 003471, CARD NO. 20013, TT: 37701:42 TC: 36690.

Part: SKIN — DENTED (FS605Ï¿½FS621) · airframe 37,701 hrs · 36,690 cycles

DENT ON AFT FUSELAGE SKIN AT FS605.00 Ï¿½ FS621.00 AND S21L TO S23L. EVALUATED DENT ON AFT FUSELAGE SKIN AT FS682.00 Ï¿½ FS700.00 AND S23R TO S24R. AND FOUND TO BE ACCEPTABLE PER EA. DENT DIMENSION L = 4.200Ï¿½ X W = 0.800Ï¿½ X D = 0.008Ï¿½. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA # AWAC-CRJ253-01700 REV IR DATED 10/19/2021. WORK PERFORMED UNDER AERSALE WORK ORDER 003471, CARD NO. 20017, TT: 37701:42 TC: 36690.

Part: SKIN — DENTED · airframe 37,701 hrs · 36,690 cycles

DENT ON AFT FUSELAGE SKIN AT FS672.00 Ï¿½ FS682.00 AND S22-L TO S23L. EVALUATED DENT ON AFT FUSELAGE SKIN AT FS672.00 Ï¿½ FS682.00 AND S22-L TO S23L. AND FOUND TO BE ACCEPTABLE PER EA. DENT DIMENSION L = 0.150Ï¿½ X W = 0.100Ï¿½ X D = 0.004Ï¿½. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA # AWAC-CRJ253-01699 REV A DATED 10/21/2021. WORK PERFORMED UNDER AERSALE WORK ORDER 003471, CARD NO. 20021, TT: 37701:42 TC: 36690.

Part: SKIN — DENTED · airframe 37,701 hrs · 36,690 cycles

DENT ON AFT FUSELAGE SKIN AT FS682.00 Ï¿½ FS700.00 AND S23R TO S24R. EVALUATED DENT ON AFT FUSELAGE SKIN AT FS682.00 Ï¿½ FS700.00 AND S23R TO S24R. AND FOUND TO BE ACCEPTABLE PER EA. DENT DIMENSION L = 0.600Ï¿½ X W = 0.250Ï¿½ X D = 0.006Ï¿½. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA # AWAC-CRJ253-01694 REV IR DATED 10/19/2021. WORK PERFORMED UNDER AERSALE WORK ORDER 003471, CARD NO. 20023, TT: 37701:42 TC: 36690.

Part: WARNING MESSAGE — FALSE ACTIVATION (THRUST REVERSER) · airframe 36,762 hrs · 35,708 cycles

LT REVERSER UNLOCKED CAUTION IN FLIGHT. CW WITH IAPS AND QRH. A/C PERFORMANCE NORMAL THROUGHOUT. AIRCRAFT REMOVED FROM SERVICE. PERFORMED OPERATIONAL TEST OF THRUST REVERSER SYSTEM, REFERENCE AMM 71-00-00-710-806. OPERATIONAL TEST NORMAL, AIRCRAFT OK FOR RETURN TO SERVICE.

Part: TRANSDUCER — MALFUNCTIONED (LT HYD SYS) · airframe 35,941 hrs · 34,852 cycles

3926 AT ALTITUDE OBSERVED THAT HYD SYS WAS AT APPROX 2400 PSI AND 60% QTY, DECREASING PRESSURE AND FLUCTUATION. WHEN PRESSURE WAS AT 1800 PSI, RAN APPROPIATE QRH PROCEDURE. DIVERTING TO SDF. DURING DESCENT NOTICED LARGE FLUCTUATIONS IN HYD 1 PRESSURE FROM 1600 PSI-3200PSI. TEMP AND QTY WITHIN LIMITS. AIRCRAFT REMOVED FROM SERVICE PERFORMED OPS CHECK OF ACMP 1B IAW AMM 29-11-03. OPS CHECK GOOD. C/W O ACTION OF MEL 29-31-01. OPS CHECK GOOD. REF 311313/2/3 FOR MELS BRYAN TUTT A&P 3606587 COULD NOT DUPLICAT. REMOVED AND REPLACED #1 SYS PRESSURE TRANSDUCER. OP'S AND LEAK CHECKS GOOD. REF AMM29-11. REMOVED PLACARD, REMOVED FROM MEL S/N OFF: 8257-8-111 S/N ON: 8545-10-50

Part: POST — CRACKED (BS 409) · airframe 35,388 hrs · 34,319 cycles

FS 409+128 RBL 18 POST OUTBOARD IS CRACKED IN THE RADIUS AT THE BOTTOM PASSED ONE RIVET. REPAIRED FS 409+128 RBL 18 OUTBOARD POST IAW REO 601R-53-41-056 REV F

Part: TRACK — GOUGED (BS 574-621) · airframe 35,388 hrs · 34,319 cycles

PERMANENT REPAIR CARGO DOOR BEAM TRACK. REPLACED CARGO DOOR BEAM MEMBER IAW SRM 51-42-06 AND 51-42-21

Part: STEP — CORRODED (PAX DOOR) · corrosion level 2 · airframe 35,388 hrs · 34,319 cycles

PAX DOOR LOWER STEP CORRODED (832AT). REMOVED AND REPLACED PAX DOOR LOWER STEP IAW AMM 52-11-04

Part: SUPPORT ANGLE — CRACKED (PAX DOOR) · airframe 35,388 hrs · 34,319 cycles

PAX DOOR LOWER CLOSING PLATE SUPPORT ANGLE IS CRACKED. REMOVED AND REPLACED LOWER CLOSING PLATE SUPPORT ANGLE IAW SRM 51-41-02.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 35,388 hrs · 34,319 cycles

PAX DOOR LOWER AFT INTERCOSTAL HAS POSSIBLE CRACK INDICATION. REMOVED AND REPLACED PAX DOOR LWR AFT INTERCOSTAL IAW CRJ-200 SRM 51-42-066 AND 51-42-21

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 35,388 hrs · 34,319 cycles

LEFT WING INBOARD FLAP VANE SKIN CHAFFED IN MIDDLE OF VANE. REMOVED AND REPLACED L/H WING INBOARD FLAP VANE SKIN MIDDLE OF VANE IAW SRM 51-42-13

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 35,388 hrs · 34,319 cycles

LEFT WING INBOARD FLAP VANE SKIN CHAFFED ON I/B SIDE. REMOVED AND REPLACED L/H INBOARD FLAP VANE, INBOARD VANE SKIN IAW SRM 51-42-10

Part: ANGLE — CRACKED (BS 621) · airframe 35,388 hrs · 34,319 cycles

FS 621 APB FWD SIDE MACHINED ANGLE AT WL 73 LBL 42 HAS A CRACK. REMOVED AND REPLACED FWD SIDE MACHINED ANGLE FS 621 AT WL 73 LBL 42 IAW BOMB. REO 601R-53-61-117.

Part: BRACKET — CORRODED (BS 349) · corrosion level 2 · airframe 35,388 hrs · 34,319 cycles

PAX DOOR LWR SILL ANGLE BOTH CONNECTOR PLUG BRACKETS HAVE CORROSION. REMOVED AND REPLACED PAX DOOR LWR SILL CONNECTOR PLUG BRACKETS IAW SRM 51-42-06.

Part: BRACKET — CORRODED (BS 310) · corrosion level 2 · airframe 35,388 hrs · 34,319 cycles

PAX DOOR LWR SILL ANGLE BOTH CONNECTOR PLUG BRACKETS HAVE CORROSION. REMOVED AND REPLACED PAX DOOR LWR SILL CONNECTOR PLUG BRACKETS IAW CRJ-200 SRM 51-42-06.

Part: FLOOR SUPPORT — CORRODED (BS 310) · corrosion level 2 · airframe 35,388 hrs · 34,319 cycles

FLOOR SILL AT FS 310 BY PAX DOOR HAS CORROSION. REMOVED AND REPLACED DOUBLER IAW CRJ-200 SRM 51-42-10

Part: RIB — CRACKED (EXHAUST FAIRING) · airframe 35,388 hrs · 34,319 cycles

PANEL 436AL EXHAUST FAIRING #2 RIB CRACKED AT TOOLING HOLE. REPAIRED CRACKED STIFFENER IAW 78-11-11 SRS042

Part: SKIN — CRACKED (NLG DOOR) · airframe 35,388 hrs · 34,319 cycles

NLG DOOR CUT-OUT HAS A CRACK ON R/H AFT SIDE. REPAIRED CRACKED AREA ON NOSE LANDING GEAR DOOR CUT-OUT. R/H AFT SIDE IAW B/A REO 601R-53-11-048 REV. D

Part: POST — CRACKED (BS 409) · airframe 35,388 hrs · 34,319 cycles

FS 409+128 VERTICAL POST AT BL 0 IS CRACKED AT AFT ANGLE, 6TH FASTENER DOWN FROM TOP, IN RADIUS ON BOTH LEFT AND RIGHT SIDES. REMOVED AND REPLACED VERTICAL POST AT BL 0 IAW SRM 51-42-06 AND REO 601R-53-41-889.

Part: ANGLE — CRACKED (BS 280) · airframe 35,388 hrs · 34,319 cycles

ANGLE CLIP AT LBL 9 AND FS 280 IS CRACKED REMOVED AND REPLACED CLIP IAW CRJ-200 SRM 51-42-21.

Part: BRACKET — CRACKED (RT MLG WW) · airframe 35,388 hrs · 34,319 cycles

RIGHT MLG WHEEL WELL VOLUMETRIC FUSE LINE BRACKET IS CRACKED. REPLACED BRACKET IAW SRM 51-41-02, 51-42-06.

Part: BRACKET — CRACKED (RT MLG WW) · airframe 35,388 hrs · 34,319 cycles

RIGHT WHEEL WELL AREA VOLUMETRIC FUSE BRACKET CRACKED. REPLACED BRACKET IAW SRM 51-41-02, 51-42-06.

Part: SKIN — CRACKED (BS 187.72) · airframe 35,388 hrs · 34,319 cycles

LEFT TRU DOOR CUT OUT CRACKED AT AFT LATCH. REPAIRED IAW 19-016B.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 34,989 hrs · 33,939 cycles

WHILE ENROUTE FROM KCAK TO KORD, THE FLIGHT CREW RECEIVED A NOSE WHEEL STEERING INOP CAUTION MESSAGE. THE FLIGHT CREW FOLLOWED THE QRH, COORDINATED WITH ATC AND DISPATCH, BRIEFED THE FLIGHT ATTENDANT AND PASSENGERS AND CONTINUED TO KORD FOR AN OTHERWISE NORMAL LANDING. ALTHOUGH THE FLIGHT CREW DID NOT DECLARE AN EMERGENCY, ARFF RESPONDED. THE AIRCRAFT WAS THEN TOWED TO THE GATE.

Part: WIRE HARNESS — CRUSHED (NLG) · airframe 34,921 hrs · 33,877 cycles

AFTER GEAR RETRACTION (6 TO 10 SECONDS) RECIEVED GEAR DISAGREE WARNING WITH NOSE DOOR WARNING WITH GEAR LEVER IN UP POSITION. RAN QRH,MESSAGE WENT AWAY, GEAR DOWN AND LOCKED. CREW PERFORMED AN AIR RETURN TO ORD. ON POST FLIGHT, FO FOUND HYD FLUID IN NOSE GEAR BAY. INSP AND FOUND NLG WOFFW2 AND OLEO CENTERED/EXTENDED HARNESS CRUSHED AT LOWER PROX SENSOR.

Part: ESCAPE ROPE — SHORT (CABIN) · airframe 34,160 hrs · 33,123 cycles

FLIGHT ATTENDANT REPORTS LT OVER WING ESCAPE ROPE TOO SHORT WHEN USED FOR TRAINING.

Part: WINDSHIELD — FAILED (COCKPIT RT) · airframe 32,505 hrs · 31,520 cycles

DURING CLIMB OUT, AT 15,000 FT, THE RIGHT WINDSHIELD SHATTERED INFLIGHT, APPEARS TO BE INNER OR OUTER PANE. COMPLIED WITH QRH. DECLARED EMERGENCY.

Part: INTERCOSTAL — CRACKED (BS 621-625.3) · airframe 32,037 hrs · 31,014 cycles

BS 621 TO 625.3 INTERCOSTAL CRACKED AT STRINGER 13L.

Part: SUPPORT ANGLE — CRACKED (BS 349) · airframe 32,037 hrs · 31,014 cycles

PAX DOOR POWER ASSIST MOTOR LWR SUPPORT ANGLE IS CRACKED

Part: RIB — CRACKED (LT WING) · airframe 32,037 hrs · 31,014 cycles

LEFT WING BATTERU RIB CRACKED.

Part: STRINGER — CRACKED (BS 379) · airframe 32,037 hrs · 31,014 cycles

STRINGER 3L CRACKED AT BS 379. REPAIRED THE STRINGER IAW SRM 53-00-03.

Part: BRACKET — CRACKED (BS 210) · airframe 32,037 hrs · 31,014 cycles

CENTER POST, RT SIDE LOWER BRACKET CRACKED. REPLACED THE BRACKET IAW SRM 51-42-21.

Part: DRAG ANGLE — CRACKED (BS 310-349) · airframe 32,037 hrs · 31,014 cycles

PAX DOOR AFT RISER DRAG ANGLE IS CRACKED. REPLACED THE AFT DRAG ANGLE IAW REO 601R-52-11-513, REV B.

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 32,037 hrs · 31,014 cycles

INTERCOSTAL CRACKED AT BS 621 TO 625, STRINGER 14L. REPLACED THE INTERCOSTAL IAW SRM 51-42-21, AND 51-42-22.

Part: INTERCOSTAL — CRACKED (BS 621 BULKHEAD) · airframe 32,037 hrs · 31,014 cycles

RIGHT AFT PRESSURE BULKHEAD INTERCOSTAL CRACKED, RBL 36. REPLACED THE INTERCOSTAL IAW SRM 51-42-21.

Part: STRINGER CLIP — DAMAGED (BS 280) · airframe 32,037 hrs · 31,014 cycles

STRINGER CLIP 3L AT BS 280 HAS ELONGATED FASTENER HOLES AND LOOSE RIVETS. REPAIRED THE STRINGER CLIP IAW SRM 51-42-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,037 hrs · 31,014 cycles

LT WALL SEAT TRACK STICK NR 7 IS CORRODED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,037 hrs · 31,014 cycles

LT FLOOR SEAT TRACK STICK NR 1 IS CORRODED.

Part: LOUVER — CRACKED (LT COWLING) · airframe 32,037 hrs · 31,014 cycles

LT LWR NOSE COWL 432AB LOUVERED VENT IS CRACKED.

Part: FLOOR SUPPORT — CORRODED (BS 589-598) · corrosion level 2 · airframe 32,039 hrs · 31,014 cycles

FLOOR SUPPORT LBL 27 CORRODED BETWEEN BS 589 TO 598. REMOVED THE DAMAGE IAW REO 601R-53-00-005, REV-B.

Part: BRACKET — CRACKED (BS 468) · airframe 32,037 hrs · 31,014 cycles

LEFT OVERWING PANEL SUPPORT BRACKET CRACKED AT BS 468. REPLACED THE BRACKET IAW SRM 51-42-20.

Part: BRACKET — CRACKED (BS 449) · airframe 32,037 hrs · 31,014 cycles

RIGHT OVERWING PANEL SUPPORT BRACKET CRACKED AT BS 449.85. REPLACED THE BRACKET IAW SRM 51-42-06, 51-25-06, 51-40-11, AND 51-25-16.

Part: SKIN — CHAFED (LT AILERON) · airframe 32,037 hrs · 31,014 cycles

LEFT AILERON FIXED LOWER LEADING EDGE CHAFED. REPLACED LOWER LEADING EDGE IAW SRM 51-42-06, AND 51-42-21.

Part: NONE — NONE · airframe 31,942 hrs · 30,921 cycles

4214 EMERGENCY TRACK LIGHTS OUT FROM ROW 2 TO 5. INSPECTED FLOOR TRACK LIGHTING IAW AMM 33-51-01, NO DEFECTS NOTED AND OPS CHECK GOOD AT THIS TIME

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 31,719 hrs · 30,705 cycles

AISLE EMERGENCY LIGHTS DO NOT ILLUMINATE FROM ROWS 2-5. FOUND LOOSE CONNECTOR AT ROW 5. CONNECTED AND THE LIGHT OPS CHECKED GOOD IAW AMM 33-51-00.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 31,490 hrs · 30,501 cycles

CRACK FOUND USING ULTRASONIC TESTING OF AFT PRESSURE BULKHEAD BS 621, RBL 28.5, WL 97, MEASURING 0.5 INCHES LONG.

Part: SERVO — MALFUNCTIONED (AUTOPILOT) · airframe 30,956 hrs · 29,991 cycles

AT 1000FEET, FIRST OFFICER DISENGAGED AUTOPILOT, CAVALRY CHARGE SOUNDED, BUT AUTOPILOT DID NOT ACTUALLY DISENGAGE UNTIL CONSIDERABLE FORCE WAS APPLIED TO CONTROL YOKE, HE PUSHED FORWARD AND A LOUD POP SOUND WAS HEARD.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 30,000 hrs · 29,097 cycles

OTBD COOL CAUTION MSG AT 1000 FT AFTER TAKEOFF CW QRH. RETURNED TO DEPARTURE.

Part: ROLLER — OUT OF ADJUST (PAX DOOR) · airframe 29,819 hrs · 28,932 cycles

PASSENGER DOOR WILL NOT OPEN FROM OUTSIDE. ADJUSTED ROLLER ON AFT DOOR FRAME AS REQUIRED. PERFORMED OPS CHECK OF PASSENGER DOOR IAW AMM 52-11-00. NO DEFECTS NOTED.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 29,666 hrs · 28,797 cycles

NR 2 IDG CAUTION MSG, CW QRH NR 1 IDG ALREADY ON MEL. DIVERTED, LANDING WEIGHT APPROXIMATELY 43000 LBS, BRMS 4, 4, 4, 4.

Part: UNKNOWN — MALFUNCTIONED (AUTOPILOT SYS) · airframe 28,051 hrs · 27,213 cycles

UNCOMMANDED YAW MOTION SHORTLY AFTER ENGAGING AUTOPILOT ABOVE 20,000 FT, NOSE SWUNG RIGHT. DISCONNECTED YAW DAMP AUTOPILOT, ACFT SWING BACK TO THE LEFT & IS NO LONGER TRIMMED OUT IN COORDINATED FLIGHT AS IT WAS BEFORE AUTOPILOT WAS ENGAGED. RE-TRIMMED ACFT FOR COORDINATED FLIGHT, STRAIGHT + LEVEL. RE-ENGAGED YAW DAMP & AUTOPILOT, 2 OR 3 MINUTES LATER, ACFT STARTED TO YAW. NO QRH AVAILABLE. DISCONNECTED YAW DAMP AUTOPILOT & DIVERTED. ON DESCENT & APPROACH, SLOWED TO LESS THAN 250 KTS & ACFT STILL HAD A MILD YAW MOTION.

Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 27,888 hrs · 27,051 cycles

FIRST OFFICERS MFD WENT BLANK DURING TAKEOFF. ABORTED TAKEOFF BELOW 60KTS.

Part: BONDING STRAP — OUT OF POSITION (RT WING) · airframe 27,865 hrs · 27,028 cycles

ON TAKEOFF ROLL, RECEIVED ANTI-ICE DUCT WARNING. ABORTED TAKEOFF AT 125 - 130 KNOTS. HIGHEST BRAKE TEMP NOTED WAS 8 UNITS. REPOSITIONED BONDING STRAP ON RT WING PICOLO TUBE BROM TOUCHING TERMINAL EB44WK IAW ESPM 20-20. OPERATIONS CHECKED GOOD IAW AMM 36-21-00.

Part: DOUBLER — CHAFED (FUSELAGE) · airframe 27,862 hrs · 27,026 cycles

FS 280 BULKHEAD AFT FACE HAS PREVIOUS REPAIR THAT IS CHAFED AT APPROX RBL9, 20 INCHES ABOVE FLOOR. REPLACED PREVIOUS REPAIR DOUBLER.

Part: INTERCOSTAL — CHAFED (FUSELAGE) · airframe 27,862 hrs · 27,026 cycles

LEFT SIDE HYD RACK IN AEB. C CHANNEL IS CHAFED AT TOP NEAR HYD NR 1 RETURN MANIFOLD. REMOVED DAMAGED HYD EQUIPMENT RACK ON LT SIDE SYS 1 PRESS & RETURN MANIFOLD INTERCOSTAL. REPLACED WITH NEW SERVICEABLE PART IAW SRM 51-42-06.

Part: SKIN — DENTED (TE FLAP) · airframe 27,862 hrs · 27,026 cycles

LEFT OTBD FLAP LOWER SKIN HAS A LARGE SHALLOW DENT, BETWEEN INBD & CTR HINGE NEAR TE, REPAIRED.

Part: HINGE — DAMAGED (LAV SERVICE DOOR) · airframe 27,862 hrs · 27,026 cycles

AFT LAVATORY SERVICING DOOR 196AR, LOWER HINGE IS CORRODED & BOLT HOLE ELONGATED.

Part: CLEAT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,862 hrs · 27,026 cycles

PAX DOOR OPENING, LOWER FRAME AFT CLEAT HAS CORROSION, REPLACED.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 27,862 hrs · 27,026 cycles

CABIN FLOOR SUPPORT ANGLE AT FS 621 CRACKED AT LBL 36, REPLACED.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 27,862 hrs · 27,026 cycles

CARGO DOOR FWD TRACK SUPPORT ANGLE, CRACKED AT LOWER END, REPLACED.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,862 hrs · 27,026 cycles

CARGO DOOR OPENING, LOWER FLOOR SILL HAS CORROSION SPOTS, BETWEEN FS 574 - 621, REPLACED.

Part: ANGLE — CRACKED (LT WING) · airframe 27,862 hrs · 27,026 cycles

LEFT WING LE MOUNT ANGLE CRACKED AT WS 149.58.

Part: RETAINER — CRACKED (LT PYLON) · airframe 27,862 hrs · 27,026 cycles

PYLON PANEL 412BT SEAL RETAINER IS CRACKED.

Part: ATTACH FITTING — CRACKED (RT WING) · airframe 27,862 hrs · 27,026 cycles

RIGHT WING LE PANEL 630BL INBD ATTACH ON WING CRACKED.

Part: FRAME — CORRODED (BS 333) · corrosion level 2 · airframe 27,862 hrs · 27,026 cycles

FRAME 333.00 CORRODED, BETWEEN STRINGERS 27 & 26R. REPAIRED IAW EA CRJ253-00170.

Part: FITTING — CRACKED (FUSELAGE) · airframe 27,785 hrs · 26,900 cycles

RIGHT FLIGHT DECK WINDOW POST, LOWER OTBD FITTING CRACKED.

Part: HINGE — CRACKED (RT WING) · airframe 27,862 hrs · 27,026 cycles

RT BUTTE DOOR PANEL 694SB, HINGE CRACKED. REPLACED HINGE.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 27,862 hrs · 27,026 cycles

STRINGER 3L ATTACH BRACKETS ARE CRACKED, BOTH INBD & OTBD, JUST AFT OF FS 280. REPLACED BRACKETS.

Part: BEAM — CRACKED (FUSELAGE) · airframe 27,862 hrs · 27,026 cycles

BEAM IS CRACKED AT VERTICAL POST JUST OTBD OF RBL9, REPAIRED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 27,862 hrs · 27,026 cycles

FS 280 UPPER FLOOR ANGLE ON BEAM IS CRACKED AT VERTICAL POST OTBD OF RBL 9, REPAIRED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 27,862 hrs · 27,026 cycles

FS 484 CLIP, CRACKED LBL 36 INBD. R & R CRACKED CLIP AT FS 484, LBL 36 IAW REO 601R-53-41-059 REV B.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 27,862 hrs · 27,026 cycles

FS 484 CLIP ANGLE CRACKED, LBL 27 OTBD. R & R CRACKED CLIP AT FS 484, LBL 27 OTBD SIDE IAW SRM 53-41-43 & 51-42-21.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 27,766 hrs · 26,928 cycles

FLIGHT 3885, EMERGENCY LIGHTS ROW 8 & AFT INOPERATIVE. R & R NR 4 INVERTER. PERFORMED OPS CHECK IAW AMM 33-51-07. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,741 hrs · 26,899 cycles

EMERGENCY FLOOR TRACK LIGHTS ROWS 8 - 13 INOPERATIVE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,640 hrs · 26,805 cycles

EMER FLOOR TRACK LIGHTS AFT OF ROW 8 NOT ILLUMINATING.

Part: LIGHT — MALFUNCTIONED (ROWS 8-12) · airframe 27,473 hrs · 26,640 cycles

FLIGHT 3955, FLOOR EMERGENCY LIGHTS ROW 8 - 12 INOPERATIVE. PERFORMED OPERATIONS CHECK OF THE EMERGENCY LIGHTS. OPS CHECKED GOOD .

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,543 hrs · 26,618 cycles

EMERGENCY FLOOR TRACK STRIP AT ROW 5 INOPERATIVE.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 23,284 hrs · 22,650 cycles

PASSENGER DOOR OUTER HANDLE CRACKED. R & R PAX DOOR OUTER HANDLE WITH NEW SERVICEABLE HANDLE IAW CRJ AMM 52-11-03, BA SB 601R-52-119.

Part: BRACKET — CRACKED · airframe 23,284 hrs · 22,650 cycles

NR 2 RETURN FILTER BRACKET CRACKED. R & R BRACKET.

Part: WHEEL — CHAFED (PAX DOOR) · airframe 23,284 hrs · 22,650 cycles

PASSENGER DOOR SUPPORT WHEEL CHAFED. UPON FURTHER INVESTIGATION FOUND SUPPORT WHEEL TO BE CRACKED. R & R SUPPORT WHEEL WITH NEW SERVICEABLE SUPPORT WHEEL PN 601R317092-1 IAW CRJ 200 AMM 52-11-13.

Part: CLEAT — CORRODED (DOOR SILL) · corrosion level 2 · airframe 23,284 hrs · 22,650 cycles

PAX DOOR SILL AFT CLEAT IS CORRODED. R & R CLEAT.

Part: RETAINER — CORRODED (E&E DOOR) · corrosion level 2 · airframe 23,284 hrs · 22,650 cycles

AVIONICS BAY DOOR SEAL RETAINERS HAS CORROSION, APM REMOVAL OF CORROSION SEAL WERE FOUND TO BE OUT OF SERVICE LIMITS. REMOVED UNSERVICEABLE FOUR EACH SEAL RETAINERS & REPLACED FOUR EACH SERVICEABLE SEAL RETAINERS IAW CRJ 200 SRM 51-42-06.

Part: STRUCTURE — DAMAGED (LT NACELLE INTAK) · airframe 23,284 hrs · 22,650 cycles

LT ENG LOWER CORE COWL ALIGNMENT HOLES ELONGATED. FABRICATED 2 EA DOUBLERS FOR ELONGATED HOLES ON LT ENG LOWER CORE COWL.

Part: FLOOR SUPPORT — CORRODED (BS 597-609) · corrosion level 2 · airframe 23,284 hrs · 22,650 cycles

OTBD FLANGE OF LBL 27.0 FLOOR SUPPORT CAP FROM FS 597 - 609 HAS CORROSION AT FASTENER HOLE LOCATIONS. REMOVED DAMAGED SECTION FABRICATE NEW AND INSTALLED.

Part: BRACKET — CRACKED (RT MLG WW) · airframe 23,284 hrs · 22,650 cycles

RT MLG WW BRAKE PRESSURE TRANSDUCER BRACKET CRACKED. FABRICATED NEW SERVICEABLE BRAKE PRESSURE TRANSDUCER BRACKET.

Part: TRUNNION — DAMAGED (RT MLG) · airframe 23,284 hrs · 22,650 cycles

FOUND TWO EACH OVERSIZED HOLES ONE EACH LT & ONE EACH RT LOWER MLG TRUNNION FLANGES.

Part: SUPPORT — CRACKED (DOOR ASSIST) · airframe 23,284 hrs · 22,650 cycles

PAX DOOR POWER ASSIST SUPPORT IS CRACKED. REPLACED WITH SERVICEABLE IAW SRM 51-42-06.

Part: DRAG BRACE — CRACKED (LT MLG WW) · airframe 23,284 hrs · 22,650 cycles

LT MLG WW DRAG BRACE COMMON TO BATTERY RIB IS CRACKED. REMOVED UNSERVICEABLE LT MLG W/W DRAG BRACE REPLACED WITH SERVICEABLE LT MLG W/W DRAG BRACE, PN 600-10389-1.

Part: DRAG BRACE — CRACKED (RT MLG WW) · airframe 23,284 hrs · 22,650 cycles

RT MLG WW DRAG BRACE COMMON TO BATTERY RIB CRACKED AT FWD SECTOR. REMOVED UNSERVICEABLE RT MLG DRAG BRACE & REPLACED WITH SERVICEABLE RT MLG W/W DRAG BRACE PN 600-10389-2.

Part: SUPPORT ANGLE — CORRODED (THRESHOLD) · corrosion level 2 · airframe 23,284 hrs · 22,650 cycles

PAX DOOR THRESHOLD FLOOR SUPPORT ANGLE HAS CORROSION. REPLACED ANGLE IAW SRM.

Part: FITTING — CORRODED (CARGO NET) · corrosion level 2 · airframe 23,284 hrs · 22,650 cycles

CARGO NET FITTING AT LBL9 & FS 582 HAS CORROSION. R & R CORRODED CARGO NET FITTING.

Part: FITTING — CORRODED (BS 559-564) · corrosion level 2 · airframe 23,284 hrs · 22,650 cycles

CARGO NET FITTING AT LBL27 FS 559+105, FS 559+111 & FS 564 CORRODED. R & R CARGO NET FITTING AT LBL 27 FS 559+105, 559+111, 564.

Part: CARGO TRACK — CORRODED (BS 559-569) · corrosion level 2 · airframe 23,284 hrs · 22,650 cycles

CARGO TRACK AT RBL 9 & FS 559+110 TO 569 HAS NUMEROUS AREAS OF EXFOILATION CORROSION. R & R CARGO TRACK.

Part: CARGO TRACK — CORRODED (BS 559-569) · corrosion level 2 · airframe 23,284 hrs · 22,650 cycles

CARGO TRACK AT RBL 9 & FS 559+110 - 569 HAS NUMEROUS AREAS OF EXFOILATION CORROSION. R & R CARGO TRACK.

Part: COALESCER BAG — DIRTY (AC BAY) · airframe 21,787 hrs · 21,192 cycles

FLT 3622/3591: SMOKE IN CABIN/COCKPIT, SMOKE TOILET CAUTION, NO SIGN OF FIRE IN LAV. SMOKE SMELL NEAR APU EXHAUST AND R PACK EXHAUST AREA. C/W CLEANING OF WATER SEPARATOR COALESCERS, RAN APPROPRIATE A/C SYSTEM IN "HOT" MODE. NO SMOKE PRESENT, NO ODORS NOTICED AT THIS TIME, OK FOR SERVICE IAW AMM 21.51.13.

Part: ENGINE — FAILED (APU) · airframe 18,629 hrs · 18,070 cycles

APU AUTOSHUTDOWN AFTER START, FOLLOWED BY APU FAULT. SMOKE VISIBLE FROM APU EXHAUST AND APU INLET DOOR. CW OPS TEST OF APU POWERPLANT IAW AMM 49-10-00. OPS CK GOOD, NO OIL LEAKS NOTED, ACFT OK FOR SERVICE, NO EVIDENCE OF FIRE NOTED.

Part: RETAINER — CRACKED (NACELLE) · airframe 18,326 hrs · 17,769 cycles

PYLON PANEL 412BT SEAL RETAINER CRACKED. R & R SEAL RETAINER.

Part: DOOR — CHAFED (LT MLG) · airframe 18,326 hrs · 17,769 cycles

LT MLG CHAFED AT FWD AND AFT EDGE. REPAIRED LT MLG DOOR DAMAGED AREAS FWD AND AFT IAW REO 601R-52-82-034, REO 601R-52-82-102 AND REO 601R-52-82-327.

Part: RETAINER — CRACKED (NACELLE) · airframe 18,326 hrs · 17,769 cycles

PYLON PANEL SEAL RETAINER CRACKED 422DB. R & R SEAL RETAINER.

Part: HINGE — GOUGED (SERVICE DOOR) · airframe 18,326 hrs · 17,769 cycles

SERVICE DOOR HINGE GOUGED LOWER AND TOP SIDE BLENDED DAMAGE TO CONTOUR REO 601R-52-41-198.

Part: BRACKET — CRACKED (FS 574) · airframe 17,769 hrs · 17,761 cycles

LOWER BRACKET ON CARGO DOOR SUPPORT FRAME CRACKED. R & R BRACKET WITH NEW PART IAW SRM.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 18,326 hrs · 17,769 cycles

RIGHT INBD FLAP VANE CHAFED IN 3 PLACES. REPAIRED RT INBD FLAP VANE CHAFE DAMAGE IAW REO 601R-57-52-004.

Part: HANDLE — GOUGED (SERVICE DOOR) · airframe 17,769 hrs · 17,761 cycles

SERVICE DOOR INNER HANDLE GOUGED 2 AREAS. BLENDED DAMAGE AND REPAIRED IAW REO 601R-52-41-197.

Part: SKIN — CHAFED (RT NACELLE) · airframe 18,326 hrs · 17,769 cycles

RT UPPER CORE COWL IS CHAFED ON INNER FWD SIDE. BLENDED CHAFED AREA ON RT UPPER CORE COWL FWD SIDE AND REPAIRED IAW CMM 71-12-200-802-A01, MATT LOSS .002 MAT REMAINING .028. REMAINING MAT IS WITHIN SERVICEABLE LIMITS IAW CMM 71-12-200-802-A01.

Part: SKIN — CRACKED (LT JET PIPE)

SKIN AROUND THE UPPER OTBD PANEL ON LT JET PIPE IS CRACKED. REMOVED UNSERVICEABLE DOUBLER AND INSTALLED SERVICEABLE DOUBLER IAW CMM 78-11-00 AND SRM 51-42-06.

Part: STRUCTURE — CHAFED (FUSELAGE) · airframe 18,326 hrs · 17,769 cycles

FUSELAGE AREA BEHIND RT STUB FAIRING CHAFED EDGE. REPAIRED CHAFED AREA BEHIND RT STUB FAIRING IAW REO 601R-53-41-341.

Part: BRACKET — CORRODED (LIGHT) · airframe 18,326 hrs · 17,769 cycles

LAVATORY FILL INDICATOR LIGHT LENS MISSING & LIGHT BRACKET CORRODED. R & R LAV FILL INDICATION LIGHT & BRACKET.

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 18,326 hrs · 17,769 cycles

BS 280 RBL AND LBL 9 ATTACH FITTINGSARE CRACKED. REPLACED ATTACH FITTING IAW REO 601R-53-11-138 & LBL 9 FLOOR SUPPORT. REPAIRED IAW REO 601R-53-11-138.

Part: SKIN — CHAFED (LT AILERON) · corrosion level 1 · airframe 18,326 hrs · 17,769 cycles

LT AILERON L/E CHAFED ON UPPER SIDE, BLEND CHECK LIMITS, ALSO, NDT AND RESTORE.

Part: RETAINER — CRACKED (RT NACELLE) · airframe 18,326 hrs · 17,769 cycles

PYLON PANEL 422BT SEAL RETAINER CRACKED. R & R SEAL RETAINER.

Part: SKIN — CHAFED (RT AILERON) · airframe 18,326 hrs · 17,769 cycles

RT AILERON UPPER AND LOWER L/E`S CHAFED BLEND CHECK LIMITS, ALSO NDT AND RESTORE.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 17,769 hrs · 17,761 cycles

LT INBD FLAP VANE CHAFED 3 EA PLACES. REPAIRED IAW REO 601R-57-52-004 AND SRM 57-42-13.

Part: SKIN — DENTED (RT NACELLE) · airframe 18,326 hrs · 17,769 cycles

RT LOWER CORE COWL IS DENTED IN 2 LOCATIONS OF FWD INNER SIDE. REPAIR AREA IAW CMM 71-12-01-300-805-A01.

Part: FRAME — CORRODED (BS 605) · airframe 18,326 hrs · 17,769 cycles

FRAME BS 605, CORRODED BETWEEN STR 26-27L. REMOVED MINOR CORROSION.

Part: ANGLE — CRACKED (FS 625) · airframe 18,326 hrs · 17,769 cycles

RT OBLIQUE ANGLE CRACKED AT FS 6251. FABRICATED AND INSTALLED NEW OBLIQUE ANGLE IAW REO 601R-53-61-100, REV A.

Part: STIFFENER — CHAFED (BS 621) · airframe 18,326 hrs · 17,769 cycles

MINOR CHAFE DAMAGE ON AEB VERTICAL STIFFENER AT FS 621.00 BL0-MAX DEPTH 0.008" WIDTH 0.250". BLENDED AREA IAW REO 601R-53-61-1523 TO MAX DEPTH OF 0.008".

Part: ANGLE — CRACKED (FS 625) · airframe 18,326 hrs · 17,769 cycles

LT OBLIQUE ANGLE CRACKED AT FS 625. FABRICATED AND INSTALLED NEW OBLIQUE ANGLE IAW REO 601R-53-61-100, REV A.

Part: SKIN — DENTED (LT NACELLE) · airframe 18,326 hrs · 17,769 cycles

LT LOWER CORE COWL DENTED ON INNER FWD SIDE. REPAIR AREA IAW CMM 71-12-01.

Part: DRAG ANGLE — CRACKED (PAX DOOR)

PAX DOOR FIXED STAIRS AFT DRAG ANGLE CRACKED AT PREVIOUS REPAIR. REPAIRED AFT DRAG ANGLE ON PAX DOOR IAW REO 601R-57-11-513, REV A.

Part: STRIKER — WORN (PAX DOOR) · airframe 18,326 hrs · 17,769 cycles

PAX DOOR FWD & AFT STRIKER PLATES ARE WORN. REPAIRD PAX DOOR FWD & AFT STRIKER PLATES BY BLENDING OUT IAW REO 601R-52-11-296 & SRM 51-12-00.

Part: HANDLE — GOUGED (CARGO DOOR) · airframe 13,449 hrs · 12,605 cycles

GOUGE FOUND AROUND CARGO DOOR HANDLE (.500 LONG X .90 WIDE X .060 DEEP) CARGO DOOR HANDLE REPLACED IAW SRM 51-42-21. (K)

Part: STRUCTURE — CRACKED (APU ENCLOSURE) · airframe 13,449 hrs · 12,605 cycles

APU ENCLOSURE, TIP LIPS FOUND CRACKED (.750 LONG) APU ENCLOSURE TOP LIPS REPAIR PERFOMED IAW REO 601R-49-11-071. (K)

Part: SILL — CORRODED (BS 319-349) · corrosion level 2 · airframe 13,449 hrs · 12,605 cycles

SERVICE DOOR FLOOR PLATE CORRODED (SILL). SERVICE DOOR FLOOR PLATE REPLACED IAW SRM 51-42-02. (K)

Part: RIB — BENT (WS 407.08) · airframe 13,449 hrs · 12,605 cycles

WHILE PERFORMING 4DMI13269 REPAIR, WINGTIP FAIRING UNDERLYING STRUCTURE (RIB) FOND BENT AT WS 407.08. WINGTIP FAIRING UNDERLYING STRUCTURE (RIB) AT WS 407.08. REPLACED IAW SRM 51-42-06. (K)

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 13,449 hrs · 12,605 cycles

CLIP OF INTERCOSTAL FS 484, RBL 36, WL 73 FOUND CRACK. CLIP OF INTERCOSTAL FS484, RBL 36, WL 73. REPLACED IAW REO 601R-53-41-059.

Part: FITTING — CRACKED (BS 460) · airframe 13,449 hrs · 12,605 cycles

CRACK FOUND ON MACHINED FITTING AT FS 460.00, RBL 10 W/L 73.00. MACHINED FITTING AT F/S 460.00, RBL 10, W/L 73.00. REPLACED IAW SRM 51-42-06 AND SRM 52-42-21. (K)

Part: LENS — CRACKED (RT WING) · airframe 13,449 hrs · 12,605 cycles

RT WING, POSITION LIGHT LENS FOUND CRACKED. RT WING, POSITION LIGHT LENS REPLACED IAW AMM 57-30-01-400-801 AND SUPLEMENT NR 07-009. (K)

Part: LENS — CRACKED (POSITION LIGHT) · airframe 13,449 hrs · 12,605 cycles

LT WING, POSITION LIGHT LENSES FOUND CRACKED. LT WING, POSITION LIGHT LENS REPLACED IAW AMM 57-30-01 TASK 57-30-01-400-801 AND AWAC SUPPLEMENT NR 07-009. (K)

Part: PRESSURE BLKHD — CRACKED (FS 202.75) · airframe 13,449 hrs · 12,605 cycles

CRACK FOUND AT FS 202.75, LBL 23.71 ON PRESSURE BULKHEAD AT PARKING BRAKE LOCATION. AT FS 202.75, LBL 23.71 ON PRESSURE BULKHEAD AT PARKING BRAKE LOCATION. REPAIR CARRIED OUT IAW REO 601R-53-11-563. (K)

Part: BULKHEAD — CRACKED (BS 621) · airframe 13,449 hrs · 12,605 cycles

CRACK FOUND ON AFT PRESSURE BULKHEAD AT FS 621.00, LBL 27.50, W/L 130.0 (UPPER END OF CARGO TRACK). REPAIR PERFORMED ON AFT PRESSURE BULKHEAD AT FS 621.00, LBL 27.50, W/L 130.00. PERFORMED IAW REO 601R-53-61-1541.

Part: BEAM — CRACKED (CARGO DOORWAY) · airframe 13,449 hrs · 12,605 cycles

CARGO DOOR BEAM ANGLE CRACKED (CRACK LENGTH IS 1.00) CARGO DOOR BEAM ANGLE REPLACED IAW SRM 51-42-21.

Part: BULKHEAD — GOUGED (FS 280) · airframe 13,449 hrs · 12,605 cycles

GOUGES FOUND ON PILOT BULKHEAD AT FS 230.00, WL 94.00, RBL 10, (700" X 2.00", .052 " DEEP AND .300, .200, .020 DEEP). REPAIR PERFORMED ON PILOT BULKHEAD AT FS 280 WL 94.00, RBL 10 IAW REO 601R-53-11-1727 REV C. (K)

Part: DOOR — GOUGED (LT NACELLE) · airframe 13,449 hrs · 12,605 cycles

LT ENGINE NOSE ACCESS COWL 432 AT LIPS FUND GOUGED OUT OF LIMITS (1" X 0.3" X 0.08"). REPLACED IAW CMM 71-14-01-300-814-401. (K)

Part: BULKHEAD — CRACKED (FS 621) · airframe 13,449 hrs · 12,605 cycles

AFT PRESSURE BULKHEAD AT FS 621.00 FOUND CRACKED AT LINTEL FITTING LOCATION (.250 LONG). AFT PRESSURE BULKHEAD FS 621.00 AT LINTEL LOCATION REPAIR PERFORMED IAW REO 601R-53-61-1230. (K)

Part: ACCESS PANEL — WORN (RT PYLON) · airframe 13,449 hrs · 12,605 cycles

SEPARATOR WORN ON RT PYLON ACCESS PANEL 422DB. SEPARATOR ON RT PYLON ACCESS PANEL 422DB REPLACED IAW SRM 51-42-06 AND 51-42-13. (K)

Part: PLATE — CRACKED (BS 589-605) · airframe 21,796 hrs · 19,774 cycles

LT SILL (FLOOR LANDING PLATE PN 601R35011-53) CRACKED AT FS 589.00 AND FS 605.00, BOTH CRACKS LENGTH .500" LT SILL (FLOOR LANDING PLATE) REPAIRED IAW REO 601R-53-61-433. (K)

Part: PANEL — DAMAGED (RT WING TE FLAP) · airframe 13,449 hrs · 12,605 cycles

RT INBD FLAP, PANEL 684AB L/E SCREW HOLES DAMAGED. RT INBD FLAP, PANEL 684AB L/E, RETAINING PLATE REPLACED IAW SRM 51-42-06. (K)

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 13,449 hrs · 12,605 cycles

PASSENGER DOOR AFT DRAG ANGLE FOUND CRACK AT FS 349.00, 1" LONG. PASSENGER DOOR AFT DRAG ANGLE REPAIRED. JOB COMPLETED IAW REO 601R-52-11-513, REV A. (K)

Part: DOOR — STUCK · airframe 9,799 hrs · 9,145 cycles

UNABLE TO OPEN SERVICE DOOR USING OUTSIDE HANDLE. (M)

Part: UNKNOWN — SMOKE (LAVATORY) · airframe 9,479 hrs · 8,844 cycles

SMOKE TOILET CAUTION MESSAGE ON SHORT FINAL. FLIGHT ATTENDANT REPORTS PHYSICAL SMOKE COMING FROM AREA OF LAV CEILING. REMOVED SMOKE DETECTOR AND LAV SPEAKER AND INSPECTED AREA BEHIND BOTH. REINSTALLED AND PERFORMED OPS TEST OF DETECTOR PER AMM 26-16-01. NO DEFECTS NOTED. (M)

Part: SMOKE WARNING — MALFUNCTIONED (LAVATORY) · airframe 9,289 hrs · 8,660 cycles

INFLIGHT DURING BLEED TRANSFER (SMOKE TOILET) CAS MESSAGE APPEARED. COMPLIED WITH QRH. MESSAGE WENT AWAY. FLIGHT ATTENDANT REPORTED ACRID SMELL IN CABIN. (K)

Part: TERMINAL — BURNED (GENERATOR)

GENERATOR NR 1 CAUTION RECEIVED AT CRUISE, COMPLIED WITH QRH. FOUND AC GENEATOR BURNED UP AT TERMINALS. REMOVED AND REPLACED GENERATOR NR 1 ASSY IAW AMM 24. (K)

Part: SKIN — CORRODED (RT WING)

RIGHT LOWER WING PLANK FUEL PANEL CUT OUT FOR PANEL 640BB HOLE NR 1 HAS MINOR CORROSION IN NON-CRITICAL AREA APPROX .003 INCH DEEP. MX REPAIRED RIGHT LOWER WING PLANK FUEL PANEL CUT OUT FOR PANEL 640BB HOLE NR 1 IAW AIR WISCONSIN E06/021/457 AND BOMBARDIER REO 601R-57-21-030 REV F. (M)

Part: SKIN — CORRODED (RT WING)

RIGHT LOWER WING PLANK FOR FUEL PANEL 650AB CUT OUT HOLE NR 9 HAS MINOR CORROSION IN NON-CRITICAL AREA APPROX .003 INCH DEEP. MAINTENANCE REPAIRED RT LOWER WING PLANK FOR FUEL PANEL 650AB CUT OUT HOLE NR 9 IAW AIR WISCONSIN E06/021/457 AND BOMBARDIER REO 601R-57-21-030 REV F. (M)

Part: SKIN — CORRODED (LT WING)

LT LOWER WING PLANK FUEL PANEL CUTOUT FOR PANEL 510AB HOLE NR 2 HAS MINOR CORROSION IN NON-CRITICAL AREA APPROX .003 INCH DEEP. MAINTENANCE REPAIRED LT LOWER WING PLANK FUEL PANEL CUT OUT FOR PANEL 510AB HOLE NR 2 IAW AIR WISCONSIN E06/021/457 AND BOMBARDIER REO 601R-57-21-030 REV F. (M)

Part: ANGLE — CRACKED (BS 621)

FOUND LEFT 621 ANGLE IS CRACKED APPROX 1.5 INCH LONG. 10-25-07 MAINTENANCE REPAIRED ANGLE IAW BOMBARDIER REO 601R5361117. (M)

Part: ANGLE — CRACKED (BS 621)

FOUND RIGHT 621 ANGLE IS CRACKED APPROX 1.5 INCH LONG. 10-25-07 MAINTENANCE REPAIRED ANGLE IAW BOMBARDIER REO 601R-53-61-117. (M)

Part: ANGLE — CRACKED (BS 484)

FOUND LEFT 484 ANGLE IS CRACKED AT LBL 36 APPROX .25 INCH LONG. 10-25-07 MAINTENANCE REPAIRED IAW REO 601R-53-41-059. (M)

Part: ANGLE — CRACKED (BS 484)

FOUND RIGHT 484 ANGLE IS CRACKED AT RBL 36 APPROX .25 INCH LONG. 10-25-07 MAINTENANCE REPAIRED IAW REO 601R-53-41-059. (M)

Part: ANGLE — CRACKED (BS 484)

FOUND RIGHT 484 ANGLE IS CRACKED AT RBL 27 APPROX .25 INCH LONG. 10-25-07 MAINTENANCE REMOVED CRACKED ANGLE AT FS 484 RBL 27. FABRICATED REPAIR ANGLE FROM PERFORMED ANGLE LOCATED, DRILLED AND INSTALLED IAW BSC STANDARD REPAIR 601R-53-0029B. (M)

Part: ANGLE — CRACKED (BS 484)

FOUND LEFT 484 ANGLE IS CRACKED AT LBL 27 APPROX .25 INCH LONG. 10-15-07 MAINTENANCE REMOVED CRACKED ANGLE AT FS 484 LBL 27. FABRICATED REPAIR ANGLE FROM PREFORMED ANGLE LOCATED DRILLED AND INSTALLED IAW BSC STANDARD REPAIR 601R-53-0029B. (M)

Part: ATTACH FITTING — DAMAGED (LT ELEVATOR)

LT ELEVATOR NR 1 HYD SYSTEM PCU ATTACHMENT FITTING ASSY ON ELEVATOR, P/N 601R24056-45, HAS SHEARED LOCK FASTENER AT BOTTOM OF LINE. 10-25-07 MAINTENANCE REPLACED LOCK FASTENER IAW SRM 51-42-21. (M)

Part: ATTACH FITTING — DAMAGED (RT ELEVATOR)

RIGHT ELEVATOR NR 3 HYD SYSTEM PCU ATTACHMENT FITTING ASSY ON ELEVATOR, P/N 601R24056-41, HAS SHEARED LOCK FASTENER AT BOTTOM OF LINK. 10-25-07 MAINTENANCE REPLACED LOCK FASTENER IAW SRM 51-42-21. (M)

Part: ATTACH FITTING — DAMAGED (LT ELEVATOR)

LT ELEVATOR NR 2 HYD SYSTEM PCU ATTACHMENT FITTING ASSY ON ELEVATOR, P/N 601R24056-443, HAS SHEARED LOCK FASTENER AFT BOTTOM OF LINK. IAW SRM 51-42-21. (M)

Part: INTERCOSTAL — CRACKED (BS 621-625)

FOUND RIGHT FS 621 TO FS 625.30 INTERCOSTAL AT STRINGER 14R IS CRACKED NEAR RADIUS APPROX 1 INCH LONG. 10-25-07 MAINTENANCE REPLACED RT INTERCOSTAL AT FS 621 TO 625.30 AT STRINGER 14R IAW CRJ 200 SRM 51-42-06. (M)

Part: INTERCOSTAL — CRACKED (BS 621-625)

FOUND LEFT FS 621 TO 625.30 INTERCOSTAL AT STRINGER 14L IS CRACKED NEAR RADIUS APPROX 1.1 INCH LONG. 10-25-07 MAINTENANCE REMOVED AND REPLACED LT SIDE INTERCOSTAL LOCATED AT FS 621 TO 625.30 STRINGER 14 P/N 601-35012-51 IAW CRJ200 SRM 51-42-06. (M)

Part: UNKNOWN — UNKNOWN (THRUST REVERSER) · airframe 7,226 hrs · 6,691 cycles

UPON LANDING THRUST REVERSERS WOULD NOT DEPLOY UNTIL AFTER 3,000 FT ROLLOUT, NEITHER REVERSER WOULD UNLOCK UNTIL BRAKES TOOK EFFECT. PERFORMED BRAKES OPS TEST IAW 32-43-00, PERFORMED ANTI-SKID COMPUTER BITE TEST IAW 32-44-06. INTERROGATED MDC, NO FAULTS FOUND. COMPLIED WITH FDR DOWNLOAD AND DATA ANALYSIS REVEALS ALL SYSTEMS OPS NORMALLY. (K)

Part: ADG — UNWANTED DEPLOY

AIR DRIVEN GENERATOR AUTO DEPLOYED IN FLIGHT. NO ADVERSE ELECTRICAL MESSAGES. NOTED ADG HANDLE STOWED. FLIGHT LEVEL 370. RESTOWED AIR DRIVEN GENERATOR IAW CRJ AMM 24-23-01 AS REQUIRED. UPLOCK FUNCTIONS NORMALLY. (M)

Part: DOOR — MISSING (LT NACELLE) · airframe 3,933 hrs · 3,492 cycles

ON CLIMB OUT, FELT LURCH. UPON INSPECTION, DISCOVERED LT ENGINE DOOR MISSING. REMOVED AND REPLACED LT LOWER COWL DOOR. (PN 228-50081-141). (K)

Part: WHEEL — DAMAGED (NLG)

UPON LANDING, NOSEWHEEL MADE STRANGE NOISE, STOP ON TAXI WAY AND LEFT NOSEWHEEL MISSING BEARING AND ABOUT TO FALL OFF. REMOVED AND REPLACED NLG SLIDING MEMBER, PER AIRCRAFT AMM 32-21-30. ALL OPS CHECK NORMAL. REMOVED AND REPLACED BOTH NLG WHEEL ASSEMBLIES. (M)