N466AW

Part: RIB — CHAFED (LE FLAP) · airframe 40,896 hrs · 39,941 cycles

CHAFING DAMAGE NOTED TO LEFT INBOARD FLAP NOSE RIB. MATERIAL LOSS RECORDED UP TO 0.015". INITIAL FLANGE THICKNESS WAS 0.06". ENGINEERING SUPPORT WAS SOUGHT FOR REPAIR PROCESS. AIRCRAFT REMOVED FROM SERVICE REPAIRED IN ACCORDANCE WITH EA AWAC-CRJ257-02062.

Part: STIFFENER — CORRODED (ZONE 200) · corrosion level 2 · airframe 40,896 hrs · 39,941 cycles

FRETTING CORROSION NOTED ON STIFFENER P/N: 601R32026-131 AT FS 559 BETWEEN LBL 7 AND LBL 38. CORROSION WAS REMOVED THROUGH BLENDING WITH RESULTING MATERIAL THICKNESS BEING LESS THAN PERMITTED PER SRM 53-00-00. ENGINEERING RESOLUTION WAS SOUGHT AND THE AREA REPAIRED PER ENGINEERING AUTHORIZATION AWAC-CRJ253-02050 REV. IR, DATED JUNE 15, 2024. ***** AIRCRAFT REMOVED FROM SERVICE ***** CORROSION REMOVED AND AREA REPAIRED IN ACCORDANCE WITH EA AWAC-CRJ253-02050 REV. IR, DATED JUNE 15, 2024.

Part: RIB — CHAFED (ZONE 300) · airframe 40,896 hrs · 39,941 cycles

THREE (3) AREAS OF CHAFING DAMAGE NOTED ON RIB 9 OF VERTICAL STABILIZER UPPER SECTION. AREAS WERE BLENDED PER SUPPLEMENT 18-325 AND MEASURED OUTSIDE OF PERMISSIBLE LIMITS. AIRCRAFT REMOVED FROM SERVICE. AREAS WERE BLENDED AND REPAIRED PER EA AWAC-CRJ-255-02048 REV. IR, DATED JUNE 13, 2024.

Part: SENSING ELEMENT — FAULTED (ANTI-ICE DUCT) · airframe 40,859 hrs · 39,906 cycles

ON TAKE-OFF ROLL AT APPROX. 80KNOTS; RECEIVED ANTI-ICE DUCT WARNING MESSAGE. TAKE-OFF ABORTED. ON A/ICE EICAS PAGE RT FUSELAGE STILL ILLUMINATED RED. MESSAGE REMAINS WITH NO BLEEDS ON. ALL BTMS INDICATIONS IN THE GREEN. AIRCRAFT REMOVED FROM SERVICE. R&R SENSING ELEMENT A18WK IAW AMM 36-21-04. OPS CHECK REQUIRED. PERFOMED OPS CHECK OF SENSING ELEMENT A18WK IAW AMM 36-21-00. OPS CHECK GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,512 hrs · 39,512 cycles

AFTER TAKE-OFF WHEN PUTTING GEAR UP RECEIVED GEAR DISAGREE CAUTION AND NOSE DOOR CAUTION MESSAGES. MAIN GEAR INDICATED UP AND LOCKED. NOSE GEAR NOT RETRACTED. C/W QRH. RECEIVED THREE DOWN AND GREEN INDICATIONS. GEAR DISAGREE CAUTION OCCURS 150 KNOTS. HIGHEST SPEED WITH GEAR EXTENDED WAS 240 KNOTS WITHIN 10 SECS. LANDING WEIGHT WAS 46700 LBS AND SMOOTH. R & R #2 WOW AND CENTERED HARNESS IAW AMM 32-61-25. RIGGED CENTERED AND WOW #2 PROX SENSORS. IAW AMM 32-61-00. C/W EXTENSION/RETRACTION IAW AMM 32-32-00. OPS TEST GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 39,553 hrs · 38,402 cycles

GEAR DISAGREE AND NOSE DOOR OPEN WARNING MESSAGE AFTER SELECTING GEAR UP. NOSE GEAR SHOWED DOWN/LOCKED WITH MAINS UP/LOCKED. UPON LANDING RECEIVED NWS INOP CAUTION. AFTER TURNING OFF RUNWAY RECEIVED HYD 3 HI TEMP CAUTION WITH 3A, AND 3B PUMPS ON. PRESSURE INDICATED 1900 PSI AT 70% AIRCRAFT REMOVED FROM SERVICE. INSPECTED AND FOUND NLG HARNESS DAMAGED R/R NLG HARNESS (LWOFWN GEAR NLG OBXT PROX HRANESS) IAW AWAC SUP 12-029E. PERFORMED OPS TEST OF HYD SYSTEM 3A IN REF TO AMM 29-12-03, RAN FOR 30 MIN. NO OVERHEATING.

Part: UNKNOWN — DENTED (RH LEADING EDGE) · airframe 39,453 hrs · 38,270 cycles

RH WING LEADING EDGE PANEL P/N 601R12016-6 HAS DENTS MEASURES P1 L= 2.100 X W= 1.300Ï¿½ P2 L= 2.500 X W= 1.500Ï¿½ P3 L= 2.400 X W= 1.650Ï¿½ P4 L= 2.100 X W= 0.500Ï¿½ ON LE INBOARD SECTION BETWEEN WS96.134-WS131.800 . *******AIRCRAFT REMOVED FROM SERVICE********** PREFORMED HAND DRESS ON FOUR DENTED AREAS P1-P4 TO REFORM PANEL TO ORIGINAL CONTOUR AT RH WING LE. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA #AWAC- CRJ257-01969 REV IR DATED 3/13/2023. WORK PERFORMED UNDER AERSALE WORK ORDER 003854, CARD NO. 20158, TT: 39453:29 TC: 38,270.

Part: BRACKET — CORRODED (FS319.70) · corrosion level 2 · airframe 39,453 hrs · 38,270 cycles

CORROSION ON FLOOR SUPPORT STRUCTURE BRACKET PN 601R31527-217 AT FS319.70 AND LBL44. DIMENSIONS P1 - L= 3.900Ï¿½ X W= 3.100Ï¿½ X D= 0.003Ï¿½, ORIGINAL THICKNESS 0.063Ï¿½ REMAINING THICKNESS 0.060Ï¿½. CORROSION ON FLOOR SUPPORT STRUCTURE BRACKET PN 601R31527-217 AT FS341.00 AND LBL44. DIMENSIONS P1 - L= 3.900Ï¿½ X W= 3.100Ï¿½ X D= 0.023Ï¿½, ORIGINAL THICKNESS 0.063Ï¿½, REMAINING THICKNESS 0.040Ï¿½. *****AIRCRAFT REMOVED FROM SERVICE************ BLENDED FLOOR SUPPORT STRUCTURE BRACKET PN 601R31527-217 AT FS319.70 AND LBL44 AND FOUND TO BE WITHIN LIMITS. BRACKET PN 601R31527-217 AT FS341.00 AND LBL44 FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED BRACKET PN 601R31527-217 AT FS341.00 AND LBL44. PERFORMED HFEC WITH NO INDICATIONS IAW CRJ200 NDTM 51-20-06 PART 1 REV 44. ALL WORK WITHIN LIMITS WAS PERFORMED IAW AIR WISCONSIN CRJ200 SRM 53-00-00 REV 39, CRJ200 SRM 51-26-00 REV 39, CRJ200 SRM 51-21-06 REV 39, CRJ200 SRM51-21-11 REV 39, CRJ200 SRM 51-42-06 REV39, CRJ200 SRM 51-25-06 REV 39, CRJ200 SRM 51-40-11 REV 39, CRJ200 SRM 51-42-20 REV 39, CRJ200 SRM 51-25-16 REV 39. ALL WORK PERFORMED UNDER AERSALE WORK ORDER 003854, CARD NO. 20175, TT: 39,453:29 TC: 38,270.

Part: VANE — CHAFED (LH IB FLAP) · airframe 39,453 hrs · 38,270 cycles

CHAFE DAMAGE TO THE LH INBOARD FLAP VANE LEADING EDGE SKIN PN 601R14303-53. WEAR DIMENSIONS FOR P1 ARE - L = 1.600Ï¿½ X W = 0.700Ï¿½ X D = 0.014Ï¿½, WS50.498+7. *****AIRCRAFT REMOVED FROM SERVICE******** BLENDED DAMAGE OF LH INBOARD FLAP VANE CHAFE DAMAGE AT LEADING EDGE SKIN PN 601R14303-53. ORIGINAL THICKNESS .050 AND REMAIN THICKNESS .036. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA # AWAC-CRJ257-01966 REV IR DATED 3/07/2023. WORK PERFORMED UNDER AERSALE WORK ORDER 003854, CARD NO. 20131, CARD ID # 1844363. N466AW TT: 39,453:29 TC: 38,270.

Part: VANE — CHAFED (LH IB FLAP) · airframe 39,453 hrs · 38,270 cycles

CHAFE DAMAGE TO THE LH INBOARD FLAP VANE LEADING EDGE SKIN PN 601R14303-43. WEAR DIMENSIONS FOR P3 ARE - L = 1.600Ï¿½ X W = 0.600Ï¿½ X D = 0.015Ï¿½, WS137.012+4. ********AIRCRAFT REMOVED FROM SERVICE************ BLENDED DAMAGE OF LH INBOARD FLAP VANE CHAFE DAMAGE AT LEADING EDGE SKIN PN 601R14303-43. ORIGINAL THICKNESS .050 AND REMAIN THICKNESS .035. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA # AWAC-CRJ257-01968 REV IR DATED 3/07/2023. WORK PERFORMED UNDER AERSALE WORK ORDER 003854, CARD NO. 20131, CARD ID # 1844363. N466AW TT: 39,453:29 TC: 38,270.

Part: SUPPORT — CORRODED (FS559+85 TOFS559) · corrosion level 2 · airframe 39,453 hrs · 38,270 cycles

CABIN RH FLOOR SILL SUPPORT PN 601R31133-102 AND PLATE PN 601R31133-101 AT FS559.00 + 85 TO FS559.00 + 116 AND RBL42 TO RBL44 HAS EXFOLIATION CORROSION. ********AIRCRAFT REMOVED FROM SERVICE******** REMOVED AND REPLACED CABIN RH FLOOR SILL SUPPORT PN 601R31133-102 AND PLATE PN 601R31133-101 AT FS559.00 + 85 TO FS559.00 + 116 AND RBL42 TO RBL44. ALL WORK WITHIN LIMITS WAS PERFORMED IAW AIR WISCONSIN CRJ200 SRM 53-00-00 REV 39, CRJ200 SRM 51-21-06 REV 39, CRJ200 SRM 53-51-43 REV 39, CRJ200 SRM 51-42-06 REV 39, CRJ200 SRM 51-11-00 REV 39, CRJ200 SRM 51-40-11 REV 39, CRJ200 SRM 51-42-15 REV 39, SRM 51-21-11 REV 39. ALL WORK PERFORMED UNDER AERSALE WORK ORDER 003854, CARD NO. 20180, TT: 39,453:29 TC: 38,270.

Part: VANE — CHAFED (LH IB FLAP) · airframe 39,453 hrs · 38,270 cycles

CHAFE DAMAGE TO THE LH INBOARD FLAP VANE LEADING EDGE SKIN PN 601R14303-51. WEAR DIMENSIONS FOR P2 ARE - L = 1.400Ï¿½ X W = 0.700Ï¿½ X D = 0.007Ï¿½, WS98.509+7. *****AIRCRAFT REMOVED FROM SERVICE******** BLENDED DAMAGE OF LH INBOARD FLAP VANE CHAFE DAMAGE AT LEADING EDGE SKIN PN 601R14303-51. ORIGINAL THICKNESS .050 AND REMAIN THICKNESS .043. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA # AWAC-CRJ257-01967 REV A DATED 3/13/2023. WORK PERFORMED UNDER AERSALE WORK ORDER 003854, CARD NO. 20131, CARD ID # 1844363. N466AW TT: 39,453:29 TC: 38,270

Part: FITTING — CORRODED (FLOOR FS349 LBL4) · corrosion level 2 · airframe 39,453 hrs · 38,270 cycles

CORROSION ON FLOOR SUPPORT PN 601R38673-43 AT FS349.00 AND LBL38 TO LBL44. **********AIRCRAFT REMOVED FROM SERVICE****** REPLACED FLOOR SUPPORT PN 601R38673-43 AT FS349.00 AND LBL38 TO LBL44. ALL WORK WITHIN LIMITS WAS PERFORMED IAW AIR WISCONSIN CRJ200 SRM 53-00-00 REV 39, CRJ200 SRM 51-26-00 REV 39, CRJ200 SRM 51-25-16 REV 39, CRJ200 SRM 51-42-20 REV 39, CRJ200 SRM 51-25-16 REV 39, CRJ200 SRM 51-40-11 REV 39, CRJ200 SRM 51-42-11 REV 39. ALL WORK PERFORMED UNDER AERSALE WORK ORDER 003854, CARD NO. 20192, TT: 39,453:29 TC: 38,270.

Part: SPLICE — DENTED (HORIZ STAB LE) · airframe 39,453 hrs · 38,270 cycles

HORIZONTAL STABILIZER LEADING EDGE SHROUD DENTED BETWEEN FSS 31.999 AND FSS 59.221, RHS. ******AIRCRAFT REMOVED FROM SERVICE******** REPAIRED HORIZONTAL STABILIZER LEADING EDGE SHROUD DENT BETWEEN FSS 31.999 AND FSS 59.221, RHS. REMOVED DAMAGED SECTION OF SHROUD. FABRICATED REPAIR ITEMS 601R-55-11-741-1/-2/-3/-4/-5/-6 AND -7 FROM ALUMINUM SHEET 2024-T3. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WERE PERFORMED IAW MHIRJ REO 601R-55-11-741 REV (--) DATED 2023-03-22. WORK PERFORMED UNDER AERSALE WORK ORDER 003854, CARD NO. 70000, TT: 39,453:29 TC: 38,270.

Part: NONE — NONE · airframe 39,177 hrs · 38,008 cycles

A-SKID INOP CAUTION MSG OBSERVED AT 120KIAS, T/O ABORTED, BTMS 5,5,7,3 MAX ***AIRCRAFT REMOVED FROM SERVICE ***** REMOVED AND REPLACED A-SKID CONTROL UNIT IAW AMM 32-42-06 PERFORMED A-SKID ADJUSTMENT TEST. OPS CHECK GOOD P/N: 42-885-3, S/N OFF 653, S/N ON 925 ARW

Part: NONE — NONE · airframe 38,457 hrs · 37,321 cycles

ON TAKEOFF RECEIVED NOSE DOOR OPEN AND GEAR DISAGREE WARNING MSG C/W QRH RETURNED TO LAND WITH GEAR DOWN AND THREE GREEN. CW M ACTION IN PREPARATION FOR MEL 32-30-01 REF 347921-2 FOR MEL PER FIM PER FIM32-60-08 NOSE DOOR OPEN INDICATION IS NORMAL CODE S23 FAR PRESENT. RIGGED THE NLG OLEO CENTERED/EXTENDED (PS14GA) PROX SENSOR IAW AMM 32-61-05, OPS CHECK GOOD. REMOVED PLACARD AND MEL.

Part: SKIN — CORRODED (BS 295-310) · corrosion level 2 · airframe 37,591 hrs · 36,458 cycles

FUSELAGE SKIN CORROSION AND SCRIBE MARKS AT VHF #1 ANTENNA LOCATION FS295.00 Ï¿½ FS310.00 S1L Ï¿½ S1R. AIRCRAFT REMOVED FROM SERVICE. BLENDED FUSELAGE SKIN CORROSION AND SCRIBE MARKS AT VHF #1 ANTENNA LOCATION FS295.00 Ï¿½ FS310.00 S1L Ï¿½ S1R. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA # AWAC- CRJ253-01661 REV IR DATED 7/30/2021.

Part: ANGLE — CRACKED (FS 280 FLOORBEAM) · airframe 37,591 hrs · 36,458 cycles

FLOOR SUPPORT STRUCTURE 1.500Ï¿½ CRACK AT FS280 LBL9.0 Ï¿½ RBL9.0 AND WL73.0. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED REPAIR ON THE FLOOR STRUCTURE AT FS280 LBL9.0 - RBL9.0 AND WL73.0. FABRICATED FILLER ANGLE P/N 601R-53-11-3720-1 DIM. L= 28.40Ï¿½ X W=1.850Ï¿½, SPLICE ANGLE P/N 601R-53-11-3720-4 DIM. L=6.40Ï¿½ X W=1.70Ï¿½ AND STIFFENER P/N 601R53-11-136-3 DIM. L=6.50Ï¿½ X W= 1.70Ï¿½. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW REO 601R-53-11-136 REV A DATED 2007/11/01, REO 601R53-11-137 REV A DATED 12-FEB-07 AND REO 601R-53-11-3720 REV A DATED 2021-08-09 WHICH IS A DEVIATION TO GREO 601R-53-11-136.

Part: FITTING — CORRODED (FS 310) · corrosion level 2 · airframe 37,591 hrs · 36,458 cycles

FORWARD GALLEY INBOARD AFT MOUNT FITTING IS CORRODED AT FS310.00 RBL10 AND WL73.5. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED FORWARD GALLEY INBOARD AFT MOUNT FITTING P/N 4602319-5 AT FS310.00 RBL10 AND WL73.5. RESTORED SURFACE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW CRJ200 SRM 51-26-00 REV 38, SRM 51-41-02 REV 38 AND C&D ZODIAC CMM 25-33-39-300-001 A01 REV 2.

Part: SKIN — CORRODED (FS 409 S1L-R) · airframe 37,591 hrs · 36,458 cycles

SKIN SURFACE CORROSION AT ADF ANTENNA SKIN SURFACE FS409.00 + 63 TO FS409.00 + 73 AND AROUND 3 BOLT HOLES AT FS409.00 + 73 AND FS409.00 + 82. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED CORROSION AT ADF SKIN SURFACE FS409.00 + 63 TO FS409.00 + 73 AND AROUND 3 BOLT HOLES AT FS409.00 + 73 AND FS409.00 + 82. ORIGINAL SKIN THICKNESS IS 0.063Ï¿½. SKIN PART NUMBER 601R38320. MEASUREMENTS ARE AS FOLLOWS: P1= L=10.700Ï¿½ X W=1.700Ï¿½ X D=0.052Ï¿½ P2= L=3.800Ï¿½ X W=1.800Ï¿½ X D=0.058Ï¿½ P3= L=7.00Ï¿½ X W=2.700Ï¿½ X D=0.046Ï¿½ P4= L=7.00Ï¿½ X W=2.900Ï¿½ X D=0.048Ï¿½ P5= L=15.00Ï¿½ X W=1.800Ï¿½ X D=0.052Ï¿½ HFEC PERFORMED WITH NO INDICATIONS. RESTORED SURFACE FINISH. ALL WORK WITHIN LIMITS AND PERFORMED IAW ASAP EA # AWAC-CRJ253-01660 REV IR DATED 7/30/2021.

Part: SKIN — DENTED (BS 636) · airframe 37,591 hrs · 36,458 cycles

AFT FUSELAGE SKIN DENT AT FS636.5, S27R-3.5Ï¿½. *AIRCRAFT REMOVED FROM SERVICE*** BLENDED SKIN DENT AT FS636.5 S27R-3.5Ï¿½ TO ORIGINAL SKIN CONTOUR. DIMENSIONS L = 1.700Ï¿½ X W = 1.00Ï¿½ D = 0.023Ï¿½. PART NUMBER 601R35005 AND SKIN THICKNESS 0.063Ï¿½. HFEC PERFORMED WITH NO INDICATIONS. RESTORED SURFACE FINISH. ALL WORK WITHIN LIMITS AND PERFORMED IAW ASAP EA # AWAC-CRJ253-01657 REV IR DATED 7/26/2021.

Part: WINDOW FRAME — GOUGED (COCKPIT) · airframe 37,591 hrs · 36,458 cycles

CO- PILOTS SIDE WINDOW POST SPLICE STRAP PN 601R33224-4 HAS NUMEROUS SCRATCHES AND GOUGES ON UPPER AND LOWER AREAS. AIRCRAFT REMOVED FROM SERVICE, BLENDED 11 TOOLING MARKS ON RH WINDSHIELD SIDE POST SPLICE STRAP. MEASUREMENTS: P1=L=3.00Ï¿½XW=1.500Ï¿½XD=0.008Ï¿½, ORIGINAL THICKNESS 0.190Ï¿½, REMAINING THICKNESS 0.177Ï¿½ P2=L=1.00Ï¿½XW=0.700Ï¿½XD=0.001Ï¿½,ORIGINAL THICKNESS 0.190Ï¿½,REMAINING THICKNESS 0.179Ï¿½ P3=L=1.700Ï¿½XW=1.200Ï¿½XD=0.004Ï¿½, ORIGINAL THICKNESS 0.190Ï¿½, REMAINING THICKNESS 0.181Ï¿½ P4=L=2.500Ï¿½ X W=1.00Ï¿½XD=0.004Ï¿½, ORIGINAL THICKNESS 0.290Ï¿½,REMAINING THICKNESS 0.283Ï¿½P5=L=1.500Ï¿½XW=1.00Ï¿½XD=0.004Ï¿½,ORIGINAL THICKNESS 0.250Ï¿½, REMAINING THICKNESS 0.241Ï¿½ P6=L=1.800Ï¿½XW=0.500Ï¿½XD=0.003Ï¿½, ORIGINAL THICKNESS 0.290Ï¿½, REMAINING THICKNESS 0.285Ï¿½ P7=L=1.00Ï¿½XW=0.800Ï¿½XD=0.001Ï¿½,ORIGINAL THICKNESS 0.250Ï¿½,REMAINING THICKNESS 0.244Ï¿½ P8=L=1.500Ï¿½XW=1.00Ï¿½XD=0.005Ï¿½,ORIGINAL THICKNESS 0.290Ï¿½,REMAINING THICKNESS 0.277Ï¿½ P9=L=3.00Ï¿½X W=1.00Ï¿½X D=0.003Ï¿½, ORIGINAL THICKNESS 0.190Ï¿½, REMAINING THICKNESS 0.175Ï¿½ P10= L=1.500Ï¿½XW=0.800Ï¿½XD=0.005Ï¿½, ORIGINAL THICKNESS 0.190Ï¿½, REMAINING THICKNESS 0.174Ï¿½ P11= L=1.200Ï¿½XW=0.800"XD=0.006Ï¿½, ORIGINAL THICKNESS 0.190Ï¿½,REMAINING THICKNESS 0.174Ï¿½ BLENDED DAMAGES IAW REO 601R-53-11-3719 REV (--) DATED 2021-07-28. HFEC PERFORMED WITH NO INDICATIONS. RESTORED SURFACE FINISH. ALL WORK WITHIN LIMITS AND PERFORMED IAW REO 601R-53-11-3719 REV (--) DATED 2021-07-28.

Part: SKIN — DENTED (BS 590 S22-23L) · airframe 37,591 hrs · 36,458 cycles

AFT FUSELAGE DENT AT FS590.00 + 3Ï¿½ STR23L + 1Ï¿½ AND FS590.00 + 2Ï¿½ STR22L + 5Ï¿½. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED SKIN DENTS AT FS590.00 + 3Ï¿½ STR23L + 1Ï¿½ AND FS590.00 + 2Ï¿½ STR22L + 5Ï¿½. PART NUMBER 601R35005 SKIN THICKNESS 0.063Ï¿½. DIMENSIONS DENT #1 - L = 1.00Ï¿½ X W = 0.800Ï¿½ D= 0.003Ï¿½ AND DENT #2 - L = 1.200Ï¿½ X W = 1.00Ï¿½ D = 0.004Ï¿½. HFEC PERFORMED WITH NO INDICATIONS. RESTORED SURFACE FINISH. ALL WORK WITHIN LIMITS AND PERFORMED IAW ASAP EA # AWAC-CRJ253-01659 REV A DATED 8/01/2021.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 37,591 hrs · 36,458 cycles

PASSENGER DOOR AFT DRAG ANGLE CRACKED, LOCATED ON AFT SIDE OF DOOR AT MOTOR ASSIST PULLEY AT FS344.00. ***AIRCRAFT REMOVED FROM SERVICE*** REPAIRED PASSENGER DOOR STAIRS AFT DRAG ANGLE AT FS344.00. MEASUREMENT OF CRACK 0.300Ï¿½ IN LENGTH. INSTALLED REPAIR DOUBLER, DOUBLER FILLER, DRAG ANGLE FILLER AND CUTOUT FILLER ON DOOR PART NUMBER 601R31907. HFEC PERFORMED WITH NO INDICATIONS. RESTORED SURFACE FINISH. ALL WORK WITHIN LIMITS AND PERFORMED IAW ASAP EA # AWAC-CRJ252-01656 REV A DATED 7/26/2021.

Part: SKIN — DENTED (BS 654-672) · airframe 37,591 hrs · 36,458 cycles

AFT FUSELAGE HAS 3 SKIN DENTS AT FS654.50 THROUGH FS672.00 AND S21R Ï¿½ S23R. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED AFT FUSELAGE SKIN AT FS654.50 THROUGH FS672.00 AND S21R Ï¿½ S23R TO ORIGINAL CONTOUR. DIMENSIONS DENT #1 - L = 1.600Ï¿½ X W = 0.600Ï¿½ D = 0.009Ï¿½, DENT #2 - L = 0.400Ï¿½ X W = 0.300Ï¿½ D = 0.004Ï¿½ AND DENT #3 - DIA X 0.350Ï¿½ X D = 0.005Ï¿½. PART NUMBER 601R35005 AND SKIN THICKNESS 0.063Ï¿½. HFEC PERFORMED WITH NO INDICATIONS. RESTORED SURFACE FINISH. ALL WORK WITHIN LIMITS AND PERFORMED IAW ASAP EA # AWAC-CRJ253-01658 REV IR DATED 7/26/2021.

Part: ACCESS PANEL — DAMAGED (RT WING) · airframe 37,591 hrs · 36,458 cycles

RIGHT HAND WING PCU ACCESS PANEL 650KB HAS DAMAGE ON LOWER SURFACE NEXT TO SCREW HOLE. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED DRILL MARKS DAMAGED AREA OF PANEL 650KB. MEASUREMENTS L = 1.500Ï¿½ X W = 1.200Ï¿½ D = 0.008Ï¿½. PART NUMBER 601R10049 AND PANEL THICKNESS OF 0.125Ï¿½, MATERIAL 7075-T76. PANEL THICKNESS REMAINING 0.117Ï¿½. MATERIAL LOSS 0.008Ï¿½. HFEC PERFORMED WITH NO INDICATIONS. RESTORED SURFACE FINISH. ALL WORK WITHIN LIMITS AND PERFORMED IAW ASAP EA # AWAC-CRJ257-01655 REV IR DATED 7/24/2021.

Part: UNKNOWN — MALFUNCTIONED (A/C SYSTEM) · airframe 36,312 hrs · 35,084 cycles

UPON INITIAL CLIMB OUT OF KMCO THE CREW WAS NOT ABLE TO TRANSFER TO THE LEFT PACK, THE RIGHT PACK WAS ON MEL. THE CREW RETURNED TO KMCO FOR MAINTENANCE "AIRCRAFT REMOVED FROM SERVICE" ACCOMPLISHED VISUAL INSPECTION OF AIR CONDITIONING COOLING DUCTS, FOUND NORMAL. PERFORMED OPS TEST OF AIR CONDITIONING SYSTEM IAW AMM 21-51-00 LH PACK HI PRESS ON TAKEOFF WITH RH PACK ON MEL. MX EXAMINED DUCTS FOR DAMAGE/LEAKS AND OPS CHECKED LH PACK GOOD. SUSPECT CREW ERROR, NOT FOLLOWING APPENDIX B FOR THE MEL.

Part: WIRE HARNESS — FAULTY (ANTI-SKID SYS) · airframe 35,949 hrs · 34,728 cycles

SUPPLIMENTAL INFORMATION, THE CREW REPORTED THAT THE ANTISKID FAILED AND WERE DIVERTING TO MLI DUE TO THE AVAILABLE RUNWAY LENGTH FOR CID. ANTI SKID OB CAUTION MESSAGE OCCURED 3 TIMES AFTER SELECTING GEAR DOWN FOR LANDING. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED OB ANTI SKID TRANSDUCER HARNESS IAW AMM SUPP 09-062H. OPS CHECKED GOOD REMOVED PLACARD AND REMOVED FROM MEL.

Part: FRAME — CORRODED (BS 605) · corrosion level 2 · airframe 35,427 hrs · 34,250 cycles

AFT FUSELAGE FS 605 FRANE HAS SEVERAL AREAS OF CORROSION FROM STGR 25R TO 23L.

Part: BEAM — GOUGED (CARGO DOOR) · airframe 35,427 hrs · 34,250 cycles

CARGO DOOR BEAM MEMBER CHAFFED AT FWD AND AFT COUNTER BALANCE CABLE PULLEY LOCATIONS.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 35,427 hrs · 34,250 cycles

RT SEAT SIDE TRACK AT THE #2 LOCATION FROM FWD SIDE OF A/C IS GOUGED APPROX 0.375 LONG, 0.250 WIDE AND 0.025 DEEP. FS 409+16 - 409+112.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,427 hrs · 34,250 cycles

LT #3 SIDE SEAT TRACK FROM FWD SIDE OF A/C IS CORRODED, MARKED WITH TAPE. FS 409+112 - 449.85.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,427 hrs · 34,250 cycles

RT SIDE #4 SEAT RAIL IS CORRODED, MARKED WITH TAPE. FS 449+85 - 529.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,427 hrs · 34,250 cycles

RT SIDE SEAT TRACK #3 IS CORRODED, MARKED WITH TAPE. 409+112 - 449.85.

Part: BRACKET — CRACKED (RT MLG WW) · airframe 35,427 hrs · 34,250 cycles

RIGHT MAIN LANDING GEAR WHEEL WELL HYDRAULIC TRANSDUCER BRACKET CRACKED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,427 hrs · 34,250 cycles

FLOOR SEAT TRACK CORRODED FS 364 - F.S.400 RBL9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,427 hrs · 34,250 cycles

LT SIDE SEAT TRACK AT THE #5 LOCATION FROM FWD OF A/C IS CORRODED, MARKED WITH TAPE. FS 499.00 - 529.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,427 hrs · 34,250 cycles

LT SIDE SEAT TRACK AT THE #4 LOCATION IS CORRODED, MARKED WITH TAPE. FS 449.85 - 499.00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,427 hrs · 34,250 cycles

LT #2 SIDE SEAT TRACK IS CORRODED MARKED WITH TAPE. FS 409+112 - 409+116.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,427 hrs · 34,250 cycles

RT SEAT TRACK #6 IS CORRODED, MARKED WITH TAPE. FS 529.00 - 559+16.

Part: FITTING — CRACKED (FUSELAGE) · airframe 35,427 hrs · 34,250 cycles

PRESSURE FLOOR SUPPORT BEAM CLIP AT FS 484, LBL36 IS CRACKED.

Part: POST — CRACKED (FUSELAGE) · airframe 35,427 hrs · 34,250 cycles

FOUND INDICATIONS BL0 409+128 VERTICAL POSTS L AND R AFT FLANGE RADIUS APPROX .25" LONG 55% FSH BOTH FAILS NDT.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,427 hrs · 34,250 cycles

FLOOR SEAT TRACK CORRODED FS 364 - FS 400 LBL9.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,427 hrs · 34,250 cycles

FLOORBOARD SUPPORT STRAP AT FS 559 BETWEEN LBL27 AND LBL36 IS CORRODED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 35,427 hrs · 34,250 cycles

PRESSURE FLOOR SUPPORT BEAM CLIP AT FS 484, LBL27 IS CRACKED.

Part: BRACKET — CRACKED (LT MLG WW) · airframe 35,427 hrs · 34,250 cycles

LEFT MAIN LANDING GEAR WHEEL WELL HYD. TRANSDUCER BRACKET CRACKED.

Part: ANGLE — CRACKED (BS 484) · airframe 35,427 hrs · 34,250 cycles

PRESSURE FLOOR SUPPORT BEAM CLIP AT F.S.484, RBL27 IS CRACKED.

Part: SEAT TRACK — CORRODED (BS 529-559) · corrosion level 2 · airframe 35,427 hrs · 34,250 cycles

R/H SEAT TRACK #6 IS CORRODED, MARKED WITH TAPE, F.S.529.00 - 559+16.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 35,427 hrs · 34,250 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS 2 AREAS THAT HAVE MULTIPLE INDICATIONS NOTED. 1) BL0.0 WL112-106 6 INCHES LONG 90% FSH, 2) RBL 18.00 . 2 INCHES LONG 50% FSH. BOTH FAILED NDT INSPECTION.

Part: WARNING MESSAGE — ILLUMINATED (NLG STEERING) · airframe 35,298 hrs · 34,130 cycles

MULTIPLE STEERING INOP CAUTION MESSAGES IN FLIGHT WITH GEAR UP. C/W'D QRH & MESSAGES PERSISTED. CYCLED STEERING AFTER LANDING, MESSAGE RETURNED AND PERSISTED. (CREW DECLARED EMERGENCY)

Part: UNKNOWN — MALFUNCTIONED (LANDING GEAR) · airframe 35,186 hrs · 34,027 cycles

REF 315380/3,4 & 314381/1 ON APPROACH AFTER SELECTING GEAR HANDLE DOWN, RECEIVED NOSE DOOR OPEN, & GEAR DISAGREE WARNING MESSAGES AFTER APPROXIMATELY 15 SECONDS AFTER SELECTING GEAR HANDLE DOWN. LEFT & RIGHT GEAR SHOWED DOWN, NOSE GEAR SHOWED UP. RAN QRH & USED MANUAL EXTENSION RELEASE HANDLE. GEAR DISAGREE MESSAGE CLEARED AND ALL 3 GEAR SHOWED DOWN & LOCKED. RECEIVED HYD 3 HI-TEMP MSG ON GROUND. LANDING GEAR MANUAL RELEASE HANDLE IS STILL PULLED.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 35,030 hrs · 33,885 cycles

RECEIVED WARNING GEAR DISAGREE TWICE AND MESSAGE DISAPPEARED WITH GEAR UP. MESSAGE APPEARED 3RD TIME AND WAS PERMANENT. DECLARED EMERGENCY AND PERFORMED MANUAL LANDING GEAR RELEASE PER QRH.

Part: WARNING MESSAGE — FALSE ACTIVATION (MLG) · airframe 34,674 hrs · 33,535 cycles

UPON GEAR EXTENSION THE CREW RECEIVED A GEAR DISAGREE ALONG WITH A NOSE DOOR CAUTION. THEY PERFORMED A GO-AROUND, DECLARED AN EMERGENCY AND RAN THE QRH. THE MESSAGE CLEARED AND THE EMERGENCY LANDING WAS CANCELED. THE FLIGHT LANDED WITHOUT INCIDENT. ARFF DID NOT RESPOND.

Part: WIRE HARNESS — DAMAGED (NLG) · airframe 33,231 hrs · 32,080 cycles

AFTER TAKEOFF, RECEIVED A GEAR DISAGREE AND NOSE DOOR WARNING, AFTER SELECTING THE GEAR UP. COMPLIED WITH QRH, PULLED THE EMERGENCY GEAR EXTENSION HANDLE, GEAR INDICATED DOWN, 3-GREEN AND MESSAGES CLEARED. LANDING WAS NORMAL. INSPECTED AND FOUND NLG CENTER PROXIMITY SWITCH BRACKET CRUSHED AND HARNESS DAMAGED,

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,178 hrs · 31,066 cycles

FRAME 333 HAS CORROSION ON THE FWD SIDE BETWEEN STRINGER 23R AND 22R IN THE FWD E&E BAY.

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 32,278 hrs · 31,066 cycles

LEFT INBD FLAP HAD AN OVERSIZED HOLE COMMON TO THE INBD SEAL AT AFT END.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 32,278 hrs · 31,066 cycles

STRINGER 20R CRACKED BETWEEN FS 333.00 AND 349.00. REPLACED STRINGER 20R IAW SRM 51-42-06, 51-42-21.

Part: TRANSITION PANEL — CRACKED (RT WING) · airframe 32,278 hrs · 31,066 cycles

TRANSITION PANEL 620ML IS CRACKED AT SCREW HOLE. REPAIRED PANEL 620ML IAW SUPP 13-141 DATED 12-16-2013.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 32,278 hrs · 31,066 cycles

CORRODED INTERCOSTAL AT FS 333.00 TO 349.00, STR 20R IS CRACKED BETWEEN FASTENER HOLES. REPLACED INTERCOSTAL IAW SRM 51-42-06.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 32,278 hrs · 31,066 cycles

CRACKED REPAIR ON THE AFT PRESSURE BULKHEAD WEB, BS 621.00, LT SIDE. REPAIRED IAW REO 601R-53-61-1230, REV-F.

Part: FRAME — CORRODED (BS 295) · corrosion level 2 · airframe 32,278 hrs · 31,066 cycles

FRAME BS 295 CORRODED BETWEEN STRINGERS 23R AND 25R. REPLACED THE FRAME IAW SRM 51-42-06, AND 51-42-21.

Part: PLATE — CORRODED (BS 280) · corrosion level 2 · airframe 32,278 hrs · 31,066 cycles

SPLICE ANGLE PLATE CORRODED JUST AFT OF FRAME 280, STRINGERS 22R TO 23R. REPLACED THE SPLICE ANGLE PLATE IAW IAW SRM 51-42-06.

Part: FRAME — CORRODED · corrosion level 2 · airframe 32,278 hrs · 31,066 cycles

FRAME BS 310 CORRODED BETWEEN STRINGERS 23L AND 26R. REPLACED THE FRAME IAW SRM 51-42-06, AND 51-42-21.

Part: STRINGER — CORRODED (BS 280-319) · corrosion level 2 · airframe 32,278 hrs · 31,066 cycles

STRINGER 24R CORRODED BETWEEN BS 280 AND 319.7. REPAIRED THE STRINGER IAW SRM 53-00-03.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 32,278 hrs · 31,066 cycles

LEFT INBD FLAP VANE IS CHAFED ON LE AT MULTIPLE AREAS. REPLACED THE INBD AND MID LEADING EDGES IAW SRM 51-42-13, OTBD LEADING EDGE IN LIMITS IAW REO 601R-57-52-004.

Part: CARGO TRACK — CORRODED (BS 559-574) · corrosion level 2 · airframe 32,278 hrs · 31,066 cycles

CARGO TRACK CORRODED FROM BS 559+112 TO 574, RBL 9. REPLACED THE CARGO TRACK IAW REO 601R-53-00-485, REV B, AND SRM 51-42-02.

Part: SKIN — CHAFED (LT AILERON) · airframe 32,278 hrs · 31,066 cycles

LEFT AILERON LOWER SURFACE IS CHAFED ON L/E. REPLACED THE SKIN IAW SRM 51-42-21, AND 51-42-06.

Part: BRACKET — CORRODED (BS 310) · corrosion level 2 · airframe 32,278 hrs · 31,066 cycles

PAX DOOR LOWER SILL FWD AND AFT CONNECTOR PLUG BRACKETS CORRODED.

Part: STRAP — MISSING (ESCAPE ROPE) · airframe 29,838 hrs · 28,803 cycles

EMERGENCY ROPE RETAINING STRAP MISSING.

Part: AILERON — STIFF (WING) · airframe 29,726 hrs · 28,704 cycles

ABNORMAL RESISTANCE WITH AILERON CONTROLS. FELT ON BOTH SIDES. GREATER STIFFNESS WHEN TURNING RT.

Part: LATCH — DIRTY (SERVICE DOOR) · airframe 29,225 hrs · 28,259 cycles

PILOT REPORTED SERVICE DOOR DIFFICULT TO OPEN. HANDLE WAS DIFFICULT TO MOVE. DOOR TRAVELED FREELY ONCE HANDLE RELEASED. CLEANED, LUBRICATED & ADJUSTED INNER HANDLE LATCH ASSEMBLY IAW AMM 52-41-00. OPERATIONS CHECKED GOOD.

Part: LINK — WORN (AILERON) · airframe 28,163 hrs · 27,232 cycles

FLIGHT 9368, AFTER TAKEOFF, ACCELERATED TO 200 KTS, AIRPLANE HAD A TENDENCY TO BANK RIGHT. ACCELERATED TO 250 KTS, ACFT TRIM PAST THE FIRST TRIM MARK ON AILERON TRIM INDICATOR WITH ZERO AILERON TRIM & NO PILOT INPUT, THE ACFT STARTED A CONTINUOUS ROLL TO THE RIGHT. FUEL WAS BALANCED, N1'S WERE MATCHED & NO VIBRATION WAS FELT IN FLIGHT CONTROLS. IP FOUND NR 1 PCU LINK WORN & FAILED BACKLASH CHECK. R & R NR 1 PCU LINK. PASSED RECHECK OF CHECK IAW AMM 27-14-00.

Part: SKIN — CHAFED (CARGO DOOR) · airframe 27,895 hrs · 26,974 cycles

CARGO DOOR OUTER SKIN IS GOUGED AT TOP CENTER.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 27,895 hrs · 26,974 cycles

FORWARD FACE OF FS 621 BULKHEAD HAS MULTIPLE SCREW SHANK MARKS.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 27,895 hrs · 26,974 cycles

PASSENGER DOOR OUTER HANDLE CRACKED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 27,895 hrs · 26,974 cycles

BATHTUB FITTING CRACKED AT LBL 9 & FS 461.

Part: MOUNT BRACKET — CRACKED (FUSELAGE) · airframe 27,895 hrs · 26,974 cycles

NUMBER 1 HYDRAULIC SYSTEM PRESSURE FILTER MOUNT BRACKET HAS CRACK IN LOWER AFT CORNER.

Part: FITTING — CRACKED (FUSELAGE) · airframe 27,895 hrs · 26,974 cycles

BATHTUB FITTING CRACKED RBL 9 AT FS 461.

Part: BULKHEAD — DENTED (FUSELAGE) · airframe 27,895 hrs · 26,974 cycles

FS 621 BULKHEAD WEB HAS SHARP DENT AT LBL 23, 2.5" ABOVE FLOOR.

Part: FITTING — CRACKED (FUSELAGE) · airframe 27,895 hrs · 26,974 cycles

RIGHT SIDE WINDOW POST LOWER OUTBOARD CLIP CRACKED.

Part: HOUSING — CRACKED (CARGO DOOR) · airframe 27,895 hrs · 26,974 cycles

CARGO DOOR HANDLE HOUSING CRACKED.

Part: FITTING — CORRODED (FUSELAGE) · airframe 27,895 hrs · 26,974 cycles

FS 280.00, RBL 9 & LBL 9, INBOARD & OUTBOARD CLIPS CRACKED.

Part: DRAG ANGLE — CRACKED (RT WING) · airframe 27,895 hrs · 26,974 cycles

RIGHT MAIN LANDING GEAR WHEEL WELL BATTERY RIB DRAG ANGLE CRACKED.

Part: ANGLE — CRACKED (PAX DOOR) · airframe 27,895 hrs · 26,974 cycles

PASSENGER DOOR ASSIST MOTOR MOUNT ANGLE CRACKED.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 27,895 hrs · 26,974 cycles

RIGHT INBOARD FLAP VANE LEADING EDGE SKIN CHAFED THREE SPOTS. MID & INBOARD LOCATIONS BEYOND LIMITS.

Part: STRUCTURE — CRACKED (LT WING) · airframe 27,895 hrs · 26,974 cycles

WING LEADING EDGE TRANSITION BETWEEN INBOARD & CENTER LEADING EDGES UNDER PANEL 620ML UPPER AFT CORNER CRACKED.

Part: UNKNOWN — ODOR (CABIN) · airframe 26,952 hrs · 26,042 cycles

AFTER APU START, PACKS TURNED ON, BAD FUEL SMELL THROUGHOUT ACFT.

Part: LIGHT — MISSING (CABIN) · airframe 25,877 hrs · 25,047 cycles

FIRST ORANGE FLOOR TRACK LIGHT STRIP MISSING. PLACARDED & PLACED ON MEL.

Part: SILL — CORRODED (PAX DOORWAY) · corrosion level 2 · airframe 23,447 hrs · 22,692 cycles

PAX DOOR LOWER SILL HAS CORROSION DAMAGE. R & R SILL.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 23,447 hrs · 22,692 cycles

EXTERNAL GROUND POST SUPPORT BRACKET IS CRACKED. R & R BRACKET.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 23,447 hrs · 22,692 cycles

CARGO TRACK IS CORRODED. REPLACE TRACK.

Part: CARGO TRACK — CORRODED (BS 559-566) · airframe 23,447 hrs · 22,692 cycles

CARGO TRACK CORRODED AROUND FASTENERS AT FS 559+110 - 566 RBL9. R & R WITH SERVICEABLE CARGO TRACK IAW AMM 53-01-11.

Part: TIE DOWN — CORRODED (BS 559-568) · airframe 23,447 hrs · 22,692 cycles

CARGO TRACK CORRODED ON LBL 27 AT FS 559+110, 559+112, 568. R & R CARGO TRACK IAW SRM 51-41-02.

Part: FAIRING — GOUGED (JET PIPE) · airframe 23,447 hrs · 22,692 cycles

LT JET PIPE FAIRING HAS GOUGE PUNCTURE HOLE ON L/E STIFFENER. REMOVED DAMAGED STIFFENER AND INSTALLED NEW, IAW CMM 20-23-00,20-42-06, 20-40-11, 20-42-20.

Part: INTERCOSTAL — CRACKED (APU DOOR) · airframe 23,447 hrs · 22,692 cycles

APU INLET DOOR INTERCOSTAL IS CRACKED. REMOVED DAMAGED INTERCOSTAL AND INSTALL NEW IAW SRM 51-42-06.

Part: SHIELD — CRACKED (JET PIPE) · airframe 23,447 hrs · 22,692 cycles

RT ENGINE JET PIPE FIRE DETECTOR LOOP SHIELD IS CRACKED. REPLACED WITH SERVICEABLE FIRE DETECTOR LOOP SHIELD.

Part: FLOOR SUPPORT — CRACKED (BS 589) · airframe 23,447 hrs · 22,692 cycles

CARGO FLOOR LANDING PLATE ATTACH ANGLE IS CRACKED. R & R ANGLE.

Part: BRACKET — CRACKED (RT ENGINE) · airframe 23,447 hrs · 22,692 cycles

RT ENGINE JET PIPE FIRE LOOP SHIELD FWD SUPPORT MOUNT BRACKET IS CRACKED. REPLACED WITH NEW SERVICEABLE BRACKET.

Part: BRACKET — CRACKED (BS 718) · airframe 23,447 hrs · 22,692 cycles

NR 2 HYD FILTER ASSY BRACKET IS CRACKED AT AFT LOWER CORNER. CUT OUT DAMAGE AND INSTALL ANGLE IAW REO 601R-53-62-031, REV A.

Part: THRESHOLD — CORRODED (SERVICE DOORWAY) · corrosion level 2 · airframe 23,447 hrs · 22,692 cycles

SERVICE DOOR THRESHOLD IS CORRODED. REMOVED CORROSION ON SERVICE DOOR THRESHOLD DAMAGE FOUND TO BE OUT OF LIMITS AND LOCATED AND DRILLED SERVICEABLE SERVICE DOOR THRESHOLD IAW SRM 51-21-06, TR 53-27, 51-40-11, 51-42-06 AND 51-25-16.

Part: ANGLE — CRACKED (BS 484) · airframe 23,447 hrs · 22,692 cycles

RT OTBD FS 484 ANGLE CRACKED. REMOVED CRACKED ANGLE AND REPLACED WITH SERVICEABLE.

Part: ANGLE — CRACKED (BS 484) · airframe 23,447 hrs · 22,692 cycles

LEFT INBD FS 484 ANGLE HAD .2500" CRACK. REPLACED LEFT INBD FS 484 ANGLE.

Part: TRUNNION — DAMAGED (RT MLG) · airframe 23,447 hrs · 22,692 cycles

DURING COLD WORKING PROCESS, FOUND FOUR OVERSIZED HOLES, TWO ON LT & TWO ON RT LOWER MLG TRUNNION FLANGES. REPAIRED OVERSIZED HOLES IAW REO 601R-57-21-1993, REV.

Part: SKIN — CRACKED (BS 574-589) · airframe 23,447 hrs · 22,692 cycles

LOW PRESSURE ACFT DOOR CUT OUT STRUCTURE IS SEPARATED AND CRACKED ON FWD AND AFT EDGES. RETURNED FWD LAND TO ORIGINAL CONTOUR IAW SRM 51-24-16 AND R & R AFT LAND IAW SRM 51-42-06, 51-42-16.

Part: BALLAST — FAILED (CABIN LIGHTS) · airframe 23,108 hrs · 22,365 cycles

STRONG BURNING ODOR IN CABIN NEAR ROW 3. R & R LIGHT BALLAST ABOVE BIN 5/6 FD IAW AMM 33-10. RESEALED ALL BIN ACCESS DOORS PER AMM SUP 13-018A.

Part: HEATER — INOPERATIVE (GALLEY) · airframe 22,339 hrs · 21,619 cycles

STRONG ELECTRICAL ODOR DURING FLIGHT NO SMOKE OR OTHER ABNORMALITIES NOTED WITHIN COCKPIT-SMELL ISOLATED TO COCKPIT. T/S AND FOUND GALLEY HTR SYS CAUSING BURNING SMELL. REMOVED AND REPLACED NR 1 GALLEY HEATER BLOWER IAW AMM 21-23-05, OPS CHECK GOOD.

Part: LUG — CRACKED (RT WING TE FLAPS) · airframe 18,520 hrs · 17,775 cycles

RT OTBD FLAP HINGE ARM (WS220) AFT LUG IS GOUGED AND MARRED. REPAIRED RT OTBD FLAP HINGE ARM IAW REO 601R-57-53-896 WORKED PERFORMED.

Part: RETAINER — CORRODED (E/E BAY DOOR) · corrosion level 2 · airframe 18,520 hrs · 17,775 cycles

CORRODED MAIN AVIONICS BAY DOOR SEAL RETAINERS. R & R 4EC DOOR SEAL RETAINERS PN CC670-38662-5, CC670-38675-3, CC670-38663-5, CC670-38674-3.

Part: ANGLE — DAMAGED (BS 559) · airframe 18,520 hrs · 17,775 cycles

FS 559 LOWER CAP ANGLE LEFT HAS SEVERAL DOUBLE AND ELONGATED HOLES THRU SKIN AND ANGLE. REPAIRED IAW REO 601R-53-41-1475.

Part: SKIN — BENT (TAIL PIPE) · airframe 18,520 hrs · 17,775 cycles

RIGHT ENGINE TAIL PIPE FAIRING CUT OUT FOR ACCESS PANEL 446BB IS BENT AND GOUGED. REPAIRED RT ENGINE TAIL PIPE IAW CMM 78-11-00, REPAIR SRS 062.

Part: FITTING — CRACKED (BS 236) · airframe 18,520 hrs · 17,775 cycles

PILOT SIDE WINDOW POST AFT LOWER FITTING CRACKED IN RADIUS. R & R WITH SERVICEABLE FITTING.

Part: LUG — CHAFED (THRUST REVERSER) · airframe 18,520 hrs · 17,775 cycles

LEFT THRUST REVERSER OTBD LOWER TRACK LUG CHAFED, BLENDED DISCREPANT AREA IAW SRM 51-21-06 AND COMPLIED WITH REO 601R-78-34-2435.

Part: SHROUD — CRACKED (RT WING) · airframe 18,520 hrs · 17,775 cycles

RIGHT OTBD L/E INNER SHROUD IS CRACKED. REMOVED DAMAGED AREA AND REPAIRED IAW REO 601R-57-41-773 AND SRM 51-24-36.

Part: PLATE — WORN (PAX DOOR) · airframe 18,520 hrs · 17,775 cycles

PAX DOOR FWD AND AFT CENTERING PLATES ARE WORN. REPAIRED PAX DOOR FWD AND AFT CENTERING PLATES IAW REO 601R-52-11-296.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 18,520 hrs · 17,775 cycles

FS280, RBL 9, OTBD CLIP CRACKED. REMOVED UNSERVICEABLE CLIP AT FS 280, LBL 9 OTBD IAW SRM 51-42-21. FABRICATED CLIP IAW SRM.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 18,520 hrs · 17,775 cycles

PAX DOOR FIXED STAIRS AFT DRAG ANGLE IS CRACKED. REPAIRED PAX DOOR FIXED STAIRS AFT DRAG ANGLE IAW REO 601R-52-11-513.

Part: FLOOR SUPPORT — CRACKED (BS 484) · airframe 18,520 hrs · 17,775 cycles

FS484 FLOOR SUPPORT CLIP CRACKED AT RBL36. REMOVED DAMAGED 484 CLIP AND INSTALLED SERVICEABLE 484 FLOOR SUPPORT CLIP IAW REO 601R-53-11-059.

Part: BRACKET — CHAFED (BS 559) · airframe 18,520 hrs · 17,775 cycles

LEFT STUB FAIRING BRACKET CHAFED/ PN 601R10371-1. REMOVED UNSERVICEABLE LT STUB FAIRING BRACKET AND INSTALLED SERVICEABLE STUB FAIRING BRACKET IAW SRM 51-47-21.

Part: BRACKET — CRACKED (BS 544-549) · airframe 18,520 hrs · 17,775 cycles

BRACKET FOR HYD LINES (PRESSURE NR 2) CRACKED IN LT WHEEL WELL. REMOVED UNSERVICEABLE BRACKET 601R75262-159 IAW SRM 51-42-06. REPLACED 601R75262-159 SERVICEABLE BRACKET IAW 51-41-11 SRM.

Part: ANGLE — CRACKED (BS 621-625) · airframe 18,520 hrs · 17,775 cycles

OBLIQUE ANGLES CRACKED ON APB AFT SIDE. COMPLIED WITH REO 601R-53-61-100 AND REO 601R-53-61-422 TO REMOVE UNSERVICEABLE LT AND RT OBLIQUE ANGLES AND REPLACE WITH SERVICEABLE LT AND RT OBLIQUE ANGLES PN 601-35012-51/52.

Part: BRACKET — CRACKED (BS 574) · airframe 18,520 hrs · 17,775 cycles

CARGO DOOR FWD TRACK LOWER MOUNT BRACKET CRACKED. REMOVED CHANNEL IAW SRM 51-42-06. FAB CHANNEL IAW SRM 53-61-23, INSTALLED IAW SRM 51-42-06, 51-41-04.

Part: BRACKET — CRACKED (RT WHEEL WELL) · airframe 18,520 hrs · 17,775 cycles

BRACKET FOR HYDRAULIC LINES CRACKED IN RT WHEEL WELL, REMOVED AND REPLACED.

Part: GCU — MALFUNCTIONED (NR 3) · airframe 17,059 hrs · 16,269 cycles

AC1 AUTOTRANSFER AND AC2 AUTOTRANSFER CAUTION MSG`S ON GROUND. WILL NOT ACCEPT EXT AC PWR. WILL NOT ACCEPT GEN PWR. MAIN GEN`S WON`T SUPPLY OPPOSITE SIDE. R & R GCU NR 3 IAW AMM 24-11-07. PERFORMED OPS CHECK IAW 24-22-01. OPS CK GOOD AT THIS TIME.

Part: TRIM PANEL — MALFUNCTIONED (COCKPIT) · airframe 15,187 hrs · 14,289 cycles

ACFT ROLLED TO RT ON APPROACH AND FELT SPRING LIKE, FLAPS AT 45 DEGREES, GOT AILERON TRIM WITH AUTOPILOT ON. DURING OPS CK OF AILERON TRIM, CAN`T TRIM ACFT LEFT WING DOWN. R & R AILERON TRIM PANEL IAW 21-12-10, OPS CK GOOD. C/W OPS CK OF AUTO PILOT AILERON SERVO GOOD. SN OFF AW0128.

Part: RUDDER PEDAL — STIFF (COCKPIT) · airframe 15,179 hrs · 14,282 cycles

RUDDER PEDALS WERE STIFF AND EXTRA SENSITIVE ON TAKEOFF ROLL ON F/O`S SIDE. C/W VISUAL INSP OF VISIBLE CABLES AND PULLEYS C/W OP CK OF RUDDER CONTROL SYS REF AMM 27-21-00, OPS CK GOOD AT THIS TIME. C/W HI SPEED TAXI CHECK, NO FAULTS DEFECTS NOTED.

Part: BULKHEAD — CRACKED (BS 621) · airframe 13,549 hrs · 12,639 cycles

AFT PRESSURE BULKHEAD WEB IS CRACKED ABOVE THE CARGO DOOR TRACK AT FS 621.00, LBL 27.50, WL 130.00, CRACK LENGTH IS .250 INCH REO 601R-53-61-1541 PERFORMED. (K)

Part: BUSHING — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 13,549 hrs · 12,639 cycles

ON LT WING, FLAP HINGE BOX LOCATED AT WS 220.00 FOUND CORRODED INBD OA FLAP ATTACHMENT FITTING, ON THE SIDE OF THE STAINLESS BUSHING. REO 601R-57-21-1144 PERFORMED. (K)

Part: FLOORBEAM — CRACKED (484) · airframe 13,549 hrs · 12,639 cycles

UNDER FLOOR AT FS 484.00, LBL 36 CLIP CRACKED. CLIP UNDER FLOOR AT FS 484.00, LBL 36 REPLACED IAW SRM 51-42-21. (K)

Part: SKIN — DENTED (TE FLAP) · airframe 13,549 hrs · 12,639 cycles

SKIN DENTED ON LT INNER FLAP AS REQUIRED. UNDERSIDE SKIN OF LT INNER FLAP REPAIRED IAW REO 601R-57-52-1483. (K)

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 13,549 hrs · 12,639 cycles

UNDER FLOOR AT FS 484.00, RBL 27 CLIP CRACKED. UNDER FLOOR AT FS 484.00, RBL 27 CLIP REPLACED IAW SRM 51-42-06 AND SRM 51-42-20, ALODINED, PRIMED AND PAINTED IAW SRM 51-21-16. (K)

Part: BULKHEAD — CRACKED (BS 621) · airframe 13,549 hrs · 12,639 cycles

AFT PRESSURE BULKHEAD (FS 621) CRACK AT LINTEL FITTING LOCATION, CRACK LENGTH .500 INCH. AFT PRESSURE BULKHEAD AT FS 621 REPAIRED IAW REO 601R-53-61-1230, REV D.

Part: BRACKET — CRACKED (BS 621) · airframe 13,549 hrs · 12,639 cycles

LINTEL BRACKET (AFT FS 621 BULKHEAD), UPPER BRACKET CRACKED. LINTEL BRACKET REPLACED IAW SRM 51-42-06. (K)

Part: SUPPORT BRACKET — CRACKED (THRUST REVERSER) · airframe 13,549 hrs · 12,639 cycles

LT ENGINE UPPER PYLON TRACK SUPPORT BRACKET IS CRACKED. LT ENG T/R UPPER PYLON TRACK SUPPORT BRACKET REPLACED IAW SRM 51-42-06. (K)

Part: ANGLE — CRACKED (BS 280) · airframe 13,549 hrs · 12,639 cycles

UPPER AFT ANGLE AT FS 280. LBL 11.00, WL 72.00 IS CRACKED. CRACK LENGTH IS .500 INCH. UPPER AFT ANGLE AT FS 280, LBL 11, WL 72.00 REPAIRED IAW REO 601R-53-11-138-NC.

Part: PRESSURE BLKHD — CRACKED (BS 202) · airframe 13,549 hrs · 12,639 cycles

CRACK FOUND ON PRESSURE BULKHEAD AT FS 202.75, LBL 23.71 AT PARKING BRAKE LOCATION. CRACK LENGTH .50 INCH CRACK ON PRESSURE BULKHEAD AT FS 202.75, LBL 23.71 AT PARKING BRAKE LOCATION, REPAIRED IAW REO 601R-53-11-563. (K)

Part: SILL — CORRODED (BS 574-621) · corrosion level 1 · airframe 13,549 hrs · 12,639 cycles

CARGO DOOR FLOOR SILL CORRODED AROUND NUTPLATES. CORROSION REMOVED ON CARGO FLOOR SILL AROUND NUTPLATES IAW SRM 51-21-00. PROTECTION RESTORED ON CARGO DOOR FLOOR SILL AROUND NUTPLATES IAW SRM 51-21-16.

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 13,549 hrs · 12,639 cycles

CLIPS AT FS 280.00, LBL 9.0, WL 72.00 IS CRACKED. CRACKED LENGTH IS .500 INCHES. CLIP REPLACED AT FS 280, LBL 9, WL 72, IAW SRM 51-42-06 AND 51-42-21. (K)

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 13,549 hrs · 12,639 cycles

CLIP AT FS 280.00, RBL 9.0, WL 72.00 IS CRACKED. CRACK LENGTH IS .200 INCH. CLIP AT FS 280, RBL 9.0 REPLACED IAW SRM 57-42-06 AND 57-42-21 AT FS 280, WL 72.0, RBL 9.0. (K)

Part: SILL — CRACKED (BS 589-605) · airframe 13,549 hrs · 12,639 cycles

CARGO DOOR FLOOR SILL CRACKED AT FS 589.00. AT CARGO DOOR FLOOR SILL (FS 589.00) CUTOUT PERFORMED IAW REO 601R-61-433. (K)

Part: FLOORBEAM — CRACKED (BS 280) · airframe 13,549 hrs · 12,639 cycles

LOWER RADIUS OF CROSSBEAM AT FS 280, LBL 9.00, WL 72.00 CRACKED LOWER RADIUS OF CROSSBEAM AT FS 280.00, LBL 9.00, WL 72.00 REPAIRED IAW REO 601R-53-11-171, REV D. (K)

Part: FLOORBEAM — CRACKED (BS 280) · airframe 13,549 hrs · 12,639 cycles

LOWER ANGLE RADIUS OF CROSSBEAM AT FS 280.00, RBL 9.00, WL 72.00 FOUND CRACKED. REPAIRED IAW REO 601R-11-171, REV D. (K)

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 13,549 hrs · 12,639 cycles

UNDER FLOOR AT FS 484 AND LBL 27 CLIP CRACKED. CLIP AT FS 484, LBL 27. REPLACED IAW SRM 51-42-21. (K)

Part: CARBON SEAL — LEAKING (LT ENGINE) · airframe 12,454 hrs · 11,568 cycles

LT OIL PRESS FLUX BETWEEN 28 AND 53 PSI. LT OIL TEMP RUNNING 15 DEG WARMER THAT RT ENG. THEN LT OIL PRESS WARNING MESSAGE ON SHORT FINAL. FOUND LT IDG CARBON SEAL LEAKING. REPLACED LT ENG IDG CARBON SEAL AND MOUNTING RING IAW AMM 72-60-00 AND 05-018A. PERFORMED OIL CONSUMPTION RUNS IAW AMM 71-00-00 LEAK CHECK GOOD. (K)

Part: A/C PACK — SMOKE (LEFT) · airframe 12,395 hrs · 11,510 cycles

AFTER BLEEDS TRANSFERRED TO APU, SMELLED SMOKE IN COCKPIT, TURNED PACKS OFF, SMOKE CLEARED. T/S TO LT PACK PRODUCING SMOKE REF LP 187703/3 FOR MEL. (K)

Part: DOOR — STIFF (SERVICE) · airframe 10,039 hrs · 9,231 cycles

SERVICE DOOR HARD TO OPEN. LUBED AND OPS CHECKED IAW 52-40-00, OPS CHECK GOOD. (K)

Part: COOLER — VIBRATION (HYD SYSTEM) · airframe 9,661 hrs · 8,859 cycles

AIRFRAME VIBRATION FELT AF VIBES FELT FROM T/O, TO DESCENT , WENT AWAY ON FINAL APPROACH. FELT IN REAR ON LT SIDE OF THE AC EVIDENT AT ROW 13 BUT NOT EVIDENT IN LAV. REMOVE AND REPLACED HYDRAULIC COOLER REF AMM 29-11-42, OPS CHECK GOOD. (K)

Part: ENGINE — LEAKING (RIGHT) · airframe 9,549 hrs · 8,738 cycles

SMOKE TOILET CAS MESSAGE INFLIGHT, SMOKE VISIBLE COMPLIED WITH QRH. SMOKE SOURCE APPEARED TO BE FROM ACROSS LAV ROW 13, AREA LOWER AREA. (K) AIRCRAFT WAS TROUBLESHOT TO RT ENGINE INTERNAL LEAK. REMOVED AND REPLACED. (VENDOR FINDINGS: CARBON SEAL PRESSURIZATION VALVE BODY CRACKED, LRU). (A)

Part: UNKNOWN — SMOKE · airframe 9,548 hrs · 8,736 cycles

TOILET SMOKE CAS MESSAGE IN FLIGHT, COMPIED WITH QRH SMOKE VISIBLE IN COCKPIT, ELECTRICAL SMOKE ODOR IN LAV, SMOKE SUBSIDED WHEN QRH COMPLIED WITH. CORRECTIVE ACTION IN PROGRESS. (K)

Part: O-RING — FAILED (HYD PUMP)

DURING CLIMB AT 25,000 FT, LT ENGINE LOW OIL PRESSURE WARNING ILLUMINATED 23 PSI 2-3 SECONDS AS PER QRH REDUCED THRUST LEVER, OIL PRESSURE STAYED BETWEEN 30-40 PSI LOW OIL PRESSURE ILLUMINATED. REMOVED AND REPLACED ENGINE NR 1 HYD ENGINE DRIVEN PUMP O-RINGS AT ENGINE NR 1 HYD EDP AXIS F CARBON SEAL AND MATING RING, OPS AND LEAK CHECK GOOD, IAW AMM 72-60-00, SUPP 05-018A. (M)

Part: SKIN — CORRODED (LT WING)

LEFT FUEL TANK ACCESS CUTOUT 540BB AT WS 54.897 HAS CORROSION IN NON-CRITICAL AREA MEASURING 3.5 INCH BY .35 NCH BY .004 INCH DEEP ALONG INBOARD LIP LANDING. MAINTENANCE BLENDED CORROSION ON LEFT FUEL TANK ACCESS CUTOUT 540BB AT WS 54.897 IAW BOMBARDIER REO 601R-57-21-030 REV F. (M)

Part: FLOORBEAM — CRACKED (BS 621)

FOUND RIGHT 621 FLOOR SUPPORT ANGLE IS CRACKED. (M)

Part: FLOORBEAM — CRACKED (BS 621)

FOUND LEFT 621 FLOOR SUPPORT ANGLE IS CRACKED. (M)

Part: DRAG ANGLE — CRACKED (PAX DOOR)

FOUND PASSENGER DOOR AFT DRAG ANGLE IS CRACKED. (M)

Part: SKIN — CORRODED (BS 586)

FUSELAGE EXTERIOR LOWER SKIN HAS 2 AREAS OF CORROSION LOCATED AT FS 586 FUSELAGE DRAIN HOLES .1 AREA MEASURES APPROX 1 INCH BY .75 INCH OTHER AREA MEASURES APPROX .50 INCH BY .50 INCH. BOTH AREAS ARE APPROX .005 INCH DEEP. (M)

Part: INTERCOSTAL — CRACKED (BS 621-625)

FOUND RT SIDE FS 621 TO FS 625.30 INTERCOSTAL AT STRINGER 14R IS CRACKED NEAR RADIUS APPROX 1 INCH LONG. (M)

Part: INTERCOSTAL — CRACKED (BS 621-625)

LT SIDE FS 621 TO FS 625.30 INTERCOSTAL AT STRINGER 14L IS CRACKED NEAR RADIUS APPROX .8 INCH LONG. (M)

Part: DOOR — OUT OF RIG (SERVICE) · airframe 8,460 hrs · 7,697 cycles

(DURING WALKAROUND) SERVICE DOOR OUTER HANDLE IS DIFFICULT TO OPEN. RIGGED SERVICE DOOR UPPER STABILIZER BAR AND CLEANED SERVICE DOOR SEAL AND OUTER HANDLE. OPS CHECK GOOD IAW AMM 52-41-00. (K)

Part: UNKNOWN — UNKNOWN

AT TAKEOFF UNDER 80 KNOTS, RED WARNING IDG MESSAGE FOLLOWED BY GEN 2 CAUTION MESSAGE BRAKE TEMPS NR 1 AND 2 AT 4, NR 3 AT 6, AND NR 4 AT 4. SERVICED OIL ON IDG NR 2 IAW AMM 12-13-24. OPS CHECK GOOD. ALL PARAMETER DO NOT REQUIRE REJECTED TAKEOFF INSPECTION IAW AMM 05-51-27-601. (M)

Part: FLAP — MALFUNCTIONED (WING)

FLAPS FAIL ON APPROACH AT 20 DEGREES. (M)

Part: FAIRING — LOOSE (FUSELAGE)

UNUSUAL VIBRATION IN AIRFRAME AND YOKE WHEN FLAPS EXTENDED AND RETRACTED. FOUND FORWARD AND AFT MOUNTS OF RIGHT AND LEFT BELLY FAIRING TO HAVE EXCESS MOVEMENT. SEALANT BROKEN AND BELLY FAIRING LOOSE. (M)

Part: SKIN — DAMAGED (FUSELAGE)

FUSELAGE SKIN DAMAGED BETWEEN FS 605 AND 621 BETWEEN STRINGERS 18L AND 20L. (K) MAINTENANCE REPAIRED BY REMOVING DAMAGE, RE-CONTOURED SKIN, FABRICATING FILLER AND DOUBLER, INSTALLING FILLER AND EXTERNAL NON-FLUSH DOUBLER IAW BSC EO 601R-53-8866. (M)

Part: STRINGER — BENT (FUSELAGE) · airframe 5,181 hrs · 4,543 cycles

FS 605 STRINGER 20L IS BENT. (K) MAINTENANCE REPAIRED BY REMOVING DAMAGE SECTION OF STRINGER FS 600 TO 620, FABRICATED REPLACEMENT STRINGER AND SPLICES, INSTALLED REPAIR PARTS IAW CRJ 200 SRM 53-00-03 PAGE 204. (M)

Part: SKIN — DAMAGED (BS 605-621)

FOUND FUSELAGE SKIN PANEL DAMAGED BETWEEN FS 605 AND 621 BETWEEN STRINGERS 20L AND 21L. REPAIRED BY REMOVING DAMAGE, FABRICATING FILLER AND DOUBLER, INSTALLING EXTERNAL NON-FLUSH DOUBLER IAW BSC EO 601R-53-8866. (M)

Part: SOLENOID VALVE — LEAKING (APU) · airframe 4,920 hrs · 4,280 cycles

DURING APU START UP IN FLIGHT, SIGNIFICANT FUEL SMELL DETECTED BY FLIGHT CREW. REMOVED AND REPLACED APU FUEL SHUT-OFF SOLENOID VALVE IAW SRM. LEAK AND OPS CHECK GOOD. (K)

Part: ANGLE — CRACKED (FS 625) · airframe 3,657 hrs · 3,149 cycles

LT FS 625 OBLIQUE ANGLE CRACKED NEAR RADIUS APPROX 1.0 INCH LONG. REPLACED ANGLE IAW SRM. (K)

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 3,657 hrs · 3,179 cycles

PASSENGER DOOR AFT DRAG ANGLE CRAKED APPROX 1 INCH LONG ADJECENT TO DOOR ASSIST CABLE PULLEY BRACKET. CUT OUT DAMAGED AREA, PERFORMED EDDY CURRENT, FABED REPAIR ANGLE, SPLICES AND INSTALLED IAW EO. (K)

Part: STRUT — DISCHARGED (MLG) · airframe 1,762 hrs · 1,498 cycles

GEAR DISAGREE AFTER TAKEOFF, COMPLIED WITH QRH LANDING WEIGHT 47,000 LBS. JACKED AIRCRAFT AND OBSERVED NLG NOT SELF-CENTERING SERVICED HYDRAULIC FLUID IN STRUT AND NITROGEN CHARGE IAW MM 12-1232. JACKED AIRCRAFT AGAIN, NLG CENTERS ON ITS OWN. SWUNG ALL 3 GEARS. OPS CHECKED GOOD.