N435AW

Part: PUMP — FAULTED (AFT E/E BAY) · airframe 41,848 hrs · 40,607 cycles

ON CLIMB AT FL290, RECV'D "HYD 2 LO PSI" CAUTION. SYS PAGE SHOWED HYD 2 QUANTITY @ 5%. EDP2 WAS IN YELLOW WITH NO FLOW LINE. C/W QRH. EDP2 OPERATED FOR 57 MINS WITHOUT FLUID. AIRCRAFT REMOVED FROM SERVICE. R&R ACMP #2B IAW AMM TASK 29-11-03-100-801 P/N:848847, S/N OFF:MX670652, S/N ON:MX664373. R/R #2 HYD RESERVOIR IAW AMM 29-11-30

Part: RELIEF VALVE — UNKNOWN (RH HYD EQUIP RAC)

HYD 2 LOW PRESS CAUTION MSG SHORTLY AFTER LANDING, OUTBD BRAKE PRESS CAUTION MSG. BRAKING ACTION LIMITED. QTY IS 5 PERCENT. FLUID IS DRIPPING FROM ECS BAY. AIRCRAFT REMOVED FROM SERVICE. INSPECTED AND FOUND HYD #2 RESERVOIR PRESSURE RELIEF VALVE LEAKING. R&R PRESSURE RELIEF/BLEED VALVE IAW AMM 29-11-34. OPS CHECK, LEAK CHECK GOOD. CLEANED RESIDUAL FLUID.

Part: BPSU — FAILED (RT TE FLAPS) · airframe 41,072 hrs · 39,770 cycles

ON APPROACH WHEN EXTENDING FLAPS FROM 0 TO 8 DEGREES, RECEIVED FLAPS FAIL. FLAPS FAILED AT 6 DEGREES. DECLARED EMERGENCY. NORMAL LANDING AND BRAKING. MAX BTMS WAS 5. AIRCRAFT REMOVED FROM SERVICE. R & R RT FLAPS BPSU IAW AMM 27-51-10 OPS TESTED GOOD.

Part: NONE — GOUGED (FS574-605) · airframe 40,472 hrs · 39,170 cycles

CARGO DOOR OUTER SKIN GOUGE DAMAGE FROM INCORRECT SCREWS INSTALLED IN CARGO BAY LINERS ABOVE THE DOOR OPENING. MX DISCOVERED ON RON WALKAROUND. A****AIRCRAFT REMOVED FROM SERVICE ***** CARGO DOOR OUTER SKIN WAS REPAIRED PER REO 601R-52-31-370. CORRECT SCREWS WERE INSTALLED IN THE CARGO LINER ABOVE THE DOOR OPENING.

Part: HARNESS — INOPERATIVE (NLG ASSEMBLY) · airframe 40,351 hrs · 39,050 cycles

AFTER TAKE OFF APROX 13 SECONDS RECIEVED GEAR DISAGREE WARNING MSG AND NOSE GEAR DOOR MSG. MANUAL RELEASE USED TO EXTEND GEAR.ALL HYD SYSTEMS IN AUTO POSITION. NO ICEING CONDITIONS DURING EVENT. EMERGENCY WAS DECLARED. ***AIRCRAFT REMOVED FROM SERVICE*** C/W M ACTION FOR MEL 32-30-01. REF 344971/1 FOR MEL R&R NLG ELECTRICAL HARNESS PER AWA SUP 12-029E. OPS CHECK GOOD REMOVED PLACARD AND REMOVED FROM MEL.

Part: WARNING MESSAGE — ILLUMINATED (NLG) · airframe 40,252 hrs · 38,957 cycles

GEAR DISAGREE - NOSE LANDING GEAR DID NOT RETRACT DURING TAKEOFF *** AIRCRAFT REMOVED FROM SERVICE *** C/W LANDING GEAR EXTENSION AND RETRACTION SEVERAL TIMES WITH NO FAULTS FOUND IAW AMM 32-30-00. REMOVED PLACARD AND FROM MEL

Part: NONE — NONE · airframe 40,089 hrs · 38,797 cycles

ON TAKE OFF,RECEIVED GEAR DISAGREE NOSE WHEEL DID NOT RETRACT. C/W QRH MANUALLY LOWERED GEAR, GEAR WAS DOWN AND LOCKED AND LANDED WITHOUT ANY FURTHER INCIDENTS. USED MANUAL HANDLE AND STOWED WHEN GEAR WAS LOWERED. NO ABNORMAL HYD MESSAGES. 3A WAS ON AND 3B SELECTED AUTO. ***AIRCRAFT REMOVED FROM SERVICE*** T/S GEAR DISAGREE EICAS MESSAGE IAW AWA SUPP 08-067. FOUND PROX SENSOR TARGET JAMMED INTO PROX SENSOR PS14GA, BOTH TARGET BRACKET AND PROX SENSOR BRACKET DAMAGED. ALSO PROX SENSOR DAMAGED, REMOVED PS14GA AND PS4GA AND REMOVED PROX SENSOR TARGET BRACKET IAW AMM 32-61-05. REMOVED AND REPLACED PROXI SENSOR BRACKET PN 16215-105 IAW AMM TASK 32-21-01-00-804 SUB TASK 32-21-01- 020-008. STEP 4. REF 218840-3 FOR INSTALL OF PS14GA, PS4GA AND PROX SENSOR TARGET BRACKET.

Part: NONE — NONE · airframe 39,996 hrs · 38,708 cycles

ON CLIMBOUT RECIEVED R COWL ANTI ICE MESSAGE. C/W QRH AND MESSAGE CLEARED. ***AIRCRAFT REMOVED FROM SERVICE*** C/W OPERATIONAL CHECK OF RH COWL ANTI ICE SYSTEM IAW 32-20-00 AC OK FOR SERVICE. FOUND RH TURKEY POPPER OUT. REF 218827/2 FOR MEL R&R RT ENGINE TURKEY POPPER IAW AMM 30-22. REMOVED PLACARD AND REMOVED FROM MEL. OPS CHECK GOOD.

Part: SKIN — DENTED (FS 193+7) · airframe 39,961 hrs · 38,675 cycles

AIRCRAFT SKIN R/H EXTERIOR HAS 1 EACH DENT AT FS 193.00+7 AND S13R+3. DENT DIMENSIONS ARE: (P1) 2.100L X 1.500W X .016D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE*********************** HAND DRESSED DENTED AREA BACK TO ORIGINAL CONTOUR. NO OIL CANNING NOTED AT THIS TIME. VERIFIED NO LOOSE/PULLED FASTENERS AND NO DAMAGE TO UNDERLYING STRUCTURE COMMON TO REPAIR AREA. HFEC PERFORMED WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. RE-EVALUATED SKIN AND FOUND WITHIN LIMITS IAW ASAP EA #AWAC-CRJ253-01745 REV IR DATED 11/18/2021. ALL WORK PERFORMED IAW ASAP EA # AWAC-CRJ253-01745 REV IR DATED 11/18/2021. WORK COMPLETED AT AERSALE CRS4AER685B ON W/O #003486 CARD #20034. N435AW TT:39,961 TC: 38,675

Part: NONE — GOUGED (RH HORIZONTAL ST) · airframe 39,961 hrs · 38,675 cycles

MAINTENANCE FOUND SCRATCH DAMAGE ON R/H HORIZONTAL STABILIZER ATTACHMENT VISOR SUPPORT ANGLE AT RBL 6. DIMENSIONS OF SCRATCH ARE: 4.20"L X 0.70"W X 0.005"D. ************AIRCRAFT REMOVED FROM SERVICE************************* BLENDED DAMAGED AREA TO A SMOOTH CONTOUR. DIMENSIONS AFTER BLEND ARE: 4.20"L X .700"W X .005"D. REMAINING MATERIAL THICKNESS OF .058". ORIGINAL THICKNESS OF .063". HFEC INSPECTION PERFORMED WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK PERFORMED WITHIN ALLOWABLE LIMITS IAW ASAP EA #AWAC-CRJ253-01764 REV IR DATED 12/02/2021. WORK COMPLETED ON AERSALE WO #003486 CARD #20450 AT AERSALE CRS #4AER685B. N435AW TT:39,961 TC:38,675.

Part: BULKHEAD — DENTED (FS 621) · airframe 39,961 hrs · 38,675 cycles

AFT PRESSURE BULKHEAD AT FS 621 LBL 30.00 TO LBL 32.80 HAS A DENT 2.80"L X 2.20"W .045"D AND A GOUGE AT DENTED AREA MEASURING 1.40"L X 1.00"W X .029"D ON FWD SIDE OF BULKHEAD AT WL 111.63 TO WL 114.43. ************AIRCRAFT REMOVED FROM SERVICE************************** HAND DRESSED DENTED AREA BACK TO ORIGINAL CONTOUR. NO OIL-CANNING NOTED AT REWORKED AREA AT THIS TIME. BLENDED DAMAGED AREA TO A SMOOTH CONTOUR WITH MAX REMAINING THICKNESS = .046". MINIMUM REMAINING THICKNESS = .034". HFEC INSPECTION WAS PERFORMED AT REPAIR AREA WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK PERFORMED WITHIN ALLOWABLE LIMITS IAW MHIRJ REO 601R-53-61-7759 REV (--) DATED 2021-12-10. WORK COMPLETED ON AERSALE WO #003486 CARD #20111 CRS #4AER685B. TT: 39,961 TC:38,675

Part: BULKHEAD — GOUGED (FS 621) · airframe 39,961 hrs · 38,675 cycles

AFT PRESSURE BULKHEAD AT FS 621 LBL 9.50 TO LBL 18 AT WL 77.4 HAS A PREVIOUSLY BLENDED AREA ON FWD SIDE. DIMENSIONS ARE: 1.40"L X 1.00"W X .029"D. ************AIRCRAFT REMOVED FROM SERVICE************************** BLENDED DAMAGED AREA TO A SMOOTH CONTOUR WITH DIMENSIONS OF: 1.40"L X 1.00"W X .029"D. ORIGINAL THICKNESS = .063". REMAINING THICKNESS = .034". HFEC INSPECTION WAS PERFORMED AT REPAIR AREA WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK PERFORMED WITHIN ALLOWABLE LIMITS IAW MHIRJ REO 601R-53-61-7759 REV (--) DATED 2021-12-10. WORK COMPLETED ON AERSALE WO #003486 CARD #20112 CRS #4AER685B. TT: 39,961 TC:38,675.

Part: SKIN — DENTED (FS 409+64+4) · airframe 39,961 hrs · 38,675 cycles

AIRCRAFT SKIN R/H EXTERIOR HAS 1 EACH DENT AT FS 409.00+64+4 AND S23R+3. DENT DIMENSIONS ARE: (P1) .375L X .340W X .004D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE*********************** VERIFIED NO LOOSE/PULLED FASTENERS AND NO DAMAGE TO UNDERLYING STRUCTURE COMMON TO REPAIR AREA. HFEC PERFORMED WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. RE-EVALUATED SKIN AND FOUND WITHIN LIMITS IAW ASAP EA #AWAC-CRJ253-01744 REV IR DATED 11/17/2021. ALL WORK PERFORMED IAW ASAP EA # AWAC-CRJ253-01744 REV IR DATED 11/17/2021. WORK COMPLETED AT AERSALE CRS4AER685B ON W/O #003486 CARD #20086. N435AW TT:39,961 TC: 38,675

Part: BULKHEAD — GOUGED (FS621) · airframe 39,961 hrs · 38,675 cycles

AFT PRESSURE BULKHEAD AT FS 621 RBL 14.75 HAS SETMARK IN DOUBLER COMMON TO FWD SIDE OF BULKHEAD. DIMENSIONS ARE: .300"L X .040"W X .007"D. ************AIRCRAFT REMOVED FROM SERVICE************************** BLENDED DAMAGED AREA TO A SMOOTH CONTOUR WITH DIMENSIONS OF: .750"L X .750"W X .008"D. ORIGINAL THICKNESS = .040". REMAINING THICKNESS = .032". HFEC INSPECTION WAS PERFORMED AT REPAIR AREA WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK PERFORMED WITHIN ALLOWABLE LIMITS IAW MHIRJ REO 601R-53-61-7759 REV (--) DATED 2021-12-10. WORK COMPLETED ON AERSALE WO #003486 CARD #20107 CRS #4AER685B. TT: 39,961 TC:38,675.

Part: NONE — CORRODED (FS349-349+12.5) · corrosion level 2 · airframe 39,961 hrs · 38,675 cycles

CORROSION DAMAGE LOCATED ON R/H FLOOR SILL WEB AT FS 349 TO FS 349+12.5" AND RBL 42 TO RBL 44. DIMENSIONS ARE: (P1) = FS 349+1" - FS 349+6" & RBL 42 = 5.40"L X 2.80"W X .019"D (P2) = FS 349+9 - FS 349+12.5" & RBL 42 = 3.60"L X 1.80"W X .003"D ***************AIRCRAFT REMOVED FROM SERVICE*********************** BLENDED BOTH AREAS OF DAMAGE TO A SMOOTH CONTOUR IAW CRJ200 SRM 51-21-06 REV 38. FLOOR SILL IS 7075-T6 .063". (P2) IS WITHIN ALLOWABLE LIMITS AND (P1) IS NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-00 REV 38. HFEC PERFORMED AT BOTH AREAS WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH AT (P2) IAW CRJ200 SRM 51-25-06 REV 38. APPLIED CIC TO AREA (P2) IAW CRJ200 SRM 51-21-11 REV 38. FABRICATED REPAIR DOUBLER OUT OF 7075-T6 .050" 5.40"L X 2.80"W IAW ASAP EA #01770 REV B DATED 12- 09-2021. INSTALLED REPAIR DOUBLER AT FS 349 TO FS 349+6 AND RBL 41 TO RBL 44. RESTORED PROTECTIVE FINISH AT (P1). RESTORED CIC AT (P1). ALL WORK PERFORMED AT (P1) WITHIN ALLOWABLE LIMITS IAW ASAP EA #01770 REV B DATED 12/09/2021. WORK COMPLETED ON AERSALE WO #003486 CARD #50040 CRS #4AER685B. N435AW TT: 39,961 TC:38,675

Part: BULKHEAD — GOUGED (FS 621) · airframe 39,961 hrs · 38,675 cycles

AFT PRESSURE BULKHEAD AT FS 621 LBL 25 HAS A DENT ON PREVIOUSLY INSTALLED DOUBLER 3.400"L X .800"W X .028"D AND A SETMARK AT DENT MEASURING .250"L ON FORWARD SIDE OF BULKHEAD AT LBL 24.75 TO LBL 25.75 AND WL 130 TO WL 133.400. ************AIRCRAFT REMOVED FROM SERVICE************************** PERFORMED CUT ON PREVIOUSLY INSTALLED DOUBLERS AT FS621 LBL 27.5 AT WL 128.23-133.3. DOUBLER CUT DIMENSION: 5.100"L X 2.100"W. FABRICATED REPAIR DOUBLER FROM 2024-T3 .040", REPAIR TRIPLER FROM 2024-T3 .063", ORIGINAL REPAIR SPLICE FROM 2024-T3 .063", AND REPAIR FILLER FROM 2024-T3 .063". REPAIR PART DIMENSIONS ARE: 20"L X 6.3"W (DOUBLER); 22"L X 4.6"W (TRIPLER); 4.1"L X 3.5"W (SPLICE); AND 5.0"L X 2.0"W (FILLER). PERFORMED HAND DRESS OF DENTED AREA BACK TO ORIGINAL CONTOUR. NO OIL-CANNING NOTED AT REWORKED AREA AT THIS TIME. INSTALLED ALL REPAIR PARTS AT REPAIR AREA ON AFT PRESSURE BULKHEAD IAW MHIRJ REO 601R-53-61-7757 REV (--) DATED 2021-12-22. HFEC INSPECTION WAS PERFORMED AT REPAIR AREA WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK PERFORMED WITHIN ALLOWABLE LIMITS IAW MHIRJ REO 601R-53-61-7757 REV (--) DATED 2021-12-22. WORK COMPLETED ON AERSALE WO #003486 CARD #20108 CRS #4AER685B. TT: 39,961 TC:38,675

Part: NONE — GOUGED (RH HORIZONTAL ST) · airframe 39,961 hrs · 38,675 cycles

MAINTENANCE FOUND SCRATCH DAMAGE ON R/H HORIZONTAL STABILIZER ATTACHMENT VISOR SUPPORT ANGLE AT RBL 6. DIMENSIONS OF SCRATCH ARE: .900"L X 0.600"W X 0.002"D. ************AIRCRAFT REMOVED FROM SERVICE************************* BLENDED DAMAGED AREA TO A SMOOTH CONTOUR. DIMENSIONS AFTER BLEND ARE: .900"L X .600"W X .002"D. REMAINING MATERIAL THICKNESS OF .061". ORIGINAL THICKNESS OF .063". HFEC INSPECTION PERFORMED WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK PERFORMED WITHIN ALLOWABLE LIMITS IAW ASAP EA #AWAC-CRJ253-01765 REV IR DATED 12/03/2021. WORK COMPLETED ON AERSALE WO #003486 CARD #20450 AT AERSALE CRS #4AER685B. N435AW TT:39,961 TC:38,675.

Part: SKIN — GOUGED (VERTICAL STABILI) · airframe 39,961 hrs · 38,675 cycles

MAINTENANCE FOUND 2 EACH SCRATCHES ON VERTICAL STABILIZER R/H SIDE COMMON TO ACCESS PANEL 325DR. DIMENSIONS OF SCRATCHES ARE: (P1) = 3.00"L X 0.500"W X 0.004"D AND (P2) = 4.00"L X 0.300"W X .004"D ************AIRCRAFT REMOVED FROM SERVICE************************* BLENDED DAMAGED AREAS TO A SMOOTH CONTOUR. (P1) AND (P2) BLENDS DID NOT SURPASS ORIGINAL DIMENSION. REMAINING MATERIAL THICKNESS OF .096". ORIGINAL THICKNESS OF .100". HFEC INSPECTION PERFORMED WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK PERFORMED WITHIN ALLOWABLE LIMITS IAW ASAP EA #AWAC-CRJ253-01766 REV A DATED 12/04/2021. WORK COMPLETED ON AERSALE WO #003486 CARD #20473 AT AERSALE CRS #4AER685B. N435AW TT:39,961 TC:38,675.

Part: NONE — GOUGED (VERTICAL STABILI) · airframe 39,961 hrs · 38,675 cycles

MAINTENANCE FOUND 4 EACH SCRATCHES ON VERTICAL STABILIZER R/H SIDE COMMON TO ACCESS PANEL 325CR. DIMENSIONS OF SCRATCHES ARE: (P1) = 2.500"L X 0.800"W X 0.006"D AND (P2) = 3.00"L X 1.400"W X .007"D (P3) = 1.500"L X 1.300"W X .004"D (P4) = 1.500"L X .500"W X .005"D (P5) = 1.500"L X 1.00"W X .003"D. (P3) WAS FOUND TO BE WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 55-31-31 REVISION 38. (P1,P2,P4, AND P5) ARE NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 55-31-31 REVISION 38. ************AIRCRAFT REMOVED FROM SERVICE************************* BLENDED DAMAGED AREAS TO A SMOOTH CONTOUR. (P1) AND (P2) BLENDS DID NOT SURPASS REMAINING MATERIAL THICKNESS OF .093". ORIGINAL THICKNESS OF .100". (P4) AND (P5) BLENDS DID NOT SURPASS REMAINING MATERIAL THICKNESS OF .035" ORIGINAL THICKNESS OF .040." HFEC INSPECTION PERFORMED WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK PERFORMED WITHIN ALLOWABLE LIMITS IAW ASAP EA #AWAC-CRJ253-01769 REV A DATED 12/04/2021. WORK COMPLETED ON AERSALE WO #003486 CARD #20474 AT AERSALE CRS #4AER685B. N435AW TT:39,961 TC:38,675.

Part: BULKHEAD — DENTED (FS 621) · airframe 39,961 hrs · 38,675 cycles

AFT PRESSURE BULKHEAD AT FS 621 LBL 21.00 TO LBL 23.30 HAS A DENT 1.250"L X 1.00"W .020"D AND A PREVIOUS BLEND AT DENT MEASURING 1.10"L X .850"W X .028"D ON FWD SIDE OF BULKHEAD AT WL 75.95 TO WL 78.60. ************AIRCRAFT REMOVED FROM SERVICE************************** HAND DRESSED DENTED AREA BACK TO ORIGINAL CONTOUR. NO OIL-CANNING NOTED AT REWORKED AREA AT THIS TIME. BLENDED DAMAGED AREA TO A SMOOTH CONTOUR WITH MAX REMAINING THICKNESS = .049". MINIMUM REMAINING THICKNESS = .035". HFEC INSPECTION WAS PERFORMED AT REPAIR AREA WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK PERFORMED WITHIN ALLOWABLE LIMITS IAW MHIRJ REO 601R-53-61-7759 REV (--) DATED 2021-12-10. WORK COMPLETED ON AERSALE WO #003486 CARD #20113 CRS #4AER685B. TT: 39,961 TC:38,675

Part: NONE — GOUGED (FS621) · airframe 39,961 hrs · 38,675 cycles

AFT PRESSURE BULKHEAD AT FS 621 LBL 21.00 TO LBL 23.30 HAS A PREVIOUS BLENDED AREA MEASURING 0.075"L X 0.550"W X 0.031"D ON FWD SIDE OF BULKHEAD AT WL 76.1 TO WL 76.9. ************AIRCRAFT REMOVED FROM SERVICE************************** BLENDED DAMAGED AREA TO A SMOOTH CONTOUR WITH MAX REMAINING THICKNESS OF 0.049." MINIMUM REMAINING THICKNESS = .035". NO CRACKS NOTED AT BLEND. HFEC INSPECTION WAS PERFORMED AT REPAIR AREA WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK PERFORMED WITHIN ALLOWABLE LIMITS IAW MHIRJ REO 601R-53-61-7759 REV (--) DATED 2021-12-10. WORK COMPLETED ON AERSALE WO #003486 CARD #20114 CRS #4AER685B. TT: 39,961 TC:38,675

Part: NONE — GOUGED (RH HORIZONTAL ST) · airframe 39,961 hrs · 38,675 cycles

MAINTENANCE FOUND SCRATCH DAMAGE ON R/H HORIZONTAL STABILIZER ATTACHMENT VISOR AT RBL 6. DIMENSIONS OF SCRATCH ARE: 38.00"L X 0.70"W X 0.005"D. ************AIRCRAFT REMOVED FROM SERVICE************************* BLENDED DAMAGED AREA TO A SMOOTH CONTOUR. DIMENSIONS AFTER BLEND ARE: 38"L X .700"W X .005"D. REMAINING MATERIAL THICKNESS OF .070". ORIGINAL THICKNESS OF .075". HFEC INSPECTION PERFORMED WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK PERFORMED WITHIN ALLOWABLE LIMITS IAW ASAP EA #AWAC-CRJ253-01763 REV IR DATED 12/02/2021. WORK COMPLETED ON AERSALE WO #003486 CARD #20450 AT AERSALE CRS #4AER685B. N435AW TT:39,961 TC:38,675.

Part: NONE — CORRODED (FS 439.00+8 - 44) · corrosion level 2 · airframe 39,961 hrs · 38,675 cycles

FUSELAGE PRESSURE FLOOR SILL HAS CORROSION AT FS 439.00+8 AND RBL 40 COMMON TO PRESSURE FLOOR SILL P/N: 601R31145-140 AND PRESSURE FLOOR ANGLE P/N: 601R31145-218. ****************AIRCRAFT REMOVED FROM SERVICE************************ BLENDED 5 EACH AREAS: PRESSURE FLOOR SILL P/N: 601R31145-140 AT FS 449.00+1 AND RBL 40 (P1) = 1.00"L X .900"W X .005"D AND FS 439.00+8 AT RBL 40 (P2) = 1.300"L X 1.200"W X .002"D; AND PRESSURE FLOOR ANGLE P/N: 601R31145-218 AT FS 449.00 AND RBL 41 (P3) = 1.150"L X .700"W X .004"D, FS 449.00+1 AT RBL 41 (P4) = 1.800"L X 1.100"W X .005"D, AND FS 449.00 AT RBL 39 (P5) = .700"L X .250"W X .002"D. ALL BLENDS WITHIN ALLOWABLE LIMITS IAW BOMBARDIER GREO 601R 53-41-666 REV C DATED 2012 -11-06. HFEC PERFORMED AT EACH BLEND AREA WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. RESTORED CIC PROTECTION. ALL WORK PERFORMED IS WITHIN ALLOWABLE LIMITS IAW BOMBARDIER GREO 601R-53-41-666 REV C DATED 2012-11-06. WORK COMPLETED ON AERSALE W/O #003486 CARD #20159 AT AERSALE CRS4AER685B.

Part: NONE — CORRODED (FS 439.00+2) · corrosion level 2 · airframe 39,961 hrs · 38,675 cycles

FUSELAGE PRESSURE FLOOR SILL HAS CORROSION AT FS 439.00+2 AND RBL 40 COMMON TO PRESSURE FLOOR SILL P/N: 601R31145-140. ***************AIRCRAFT REMOVED FROM SERVICE**************************** BLENDED 1 EACH AREA ON PRESSURE FLOOR SILL P/N: 601R31145-140 AT FS 439.00+2 AND RBL 40 (P1) = 1.400"L X 1.050"W X .003"D. BLEND IS WITHIN ALLOWABLE LIMITS IAW BOMBARDIER GREO 601R 53-41-666 REV C DATED 2012-11-06. HFEC PERFORMED AT BLEND AREA WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. RESTORED CIC PROTECTION. ALL WORK PERFORMED IS WITHIN ALLOWABLE LIMITS IAW BOMBARDIER GREO 601R-53-41-666 REV C DATED 2012-11-06 WORK COMPLETED ON AERSALE W/O #003486 CARD #20158 AT AERSALE CRS4AER685B.

Part: NONE — CORRODED (FS449.85+9) · corrosion level 2 · airframe 39,961 hrs · 38,675 cycles

FUSELAGE PRESSURE FLOOR SILL HAS CORROSION AT FS 449.85+9 AND RBL 40 COMMON TO PRESSURE FLOOR SILL P/N: 601R31145-140. ***************AIRCRAFT REMOVED FROM SERVICE**************************** BLENDED 1 EACH AREA ON PRESSURE FLOOR SILL P/N: 601R31145-140 AT FS 449.85+8 AND RBL 40 (P1) = .800"L X .900"W X .004"D. BLEND IS WITHIN ALLOWABLE LIMITS IAW BOMBARDIER GREO 601R 53-41-666 REV C DATED 2012-11-06. HFEC PERFORMED AT BLEND AREA WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. RESTORED CIC PROTECTION. ALL WORK PERFORMED IS WITHIN ALLOWABLE LIMITS IAW BOMBARDIER GREO 601R-53-41-666 REV C DATED 2012-11-06 WORK COMPLETED ON AERSALE W/O #003486 CARD #20160 AT AERSALE CRS4AER685B.

Part: ANGLE — CORRODED (FS549+13-FS559) · corrosion level 2 · airframe 39,961 hrs · 38,675 cycles

FUSELAGE PRESSURE FLOOR SILL HAS CORROSION AT FS 549.00+13 TO FS 559.00 AND RBL 30 TO RBL 40 COMMON TO PRESSURE FLOOR SILL P/N: 601R31145-140, PRESSURE FLOOR ANGLE P/N: 601R31145-222, AND PRESSURE FLOOR CROSS MEMBER STRAP. ***************AIRCRAFT REMOVED FROM SERVICE**************************** BLENDED 3 EACH AREAS: PRESSURE FLOOR SILL P/N: 601R31145-140 AT FS 544.00+12 AND RBL 40 (P1) = 1.70"L X 1.60"W X .003"D; PRESSURE FLOOR ANGLE P/N: 601R31145-222 AT FS 544.00+13 AND RBL 40 (P2) = 3.20"L X 1.60"W X .004"D; AND PRESSURE FLOOR CROSS MEMBER STRAP AT FS 544.00+13 TO FS 559.00 AND RBL 30 TO RBL 40 (P3) = 2.00"L X 9.60"W X .004"D. (P1) AND (P2) WITHIN ALLOWABLE LIMITS IAW BOMBARDIER GREO 601R- 53-41-666 REV C DATED 2012-11-06. (P3) WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-00 REV 38. HFEC PERFORMED AT EACH BLEND AREA WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. RESTORED CIC PROTECTION. ALL WORK PERFORMED IS WITHIN ALLOWABLE LIMITS IAW BOMBARDIER GREO 601R-53-41-666 REV C DATED 2012-11-06 AND CRJ200 SRM 53-00-00 REV 38. WORK COMPLETED ON AERSALE W/O #003486 CARD #20167 AT AERSALE CRS4AER685B.

Part: ANGLE — CORRODED (FS513.00-FS513.0) · corrosion level 2 · airframe 39,961 hrs · 38,675 cycles

CORROSION COMMON TO PRESSURE FLOOR ANGLE AT FS 513.00 TO FS 513.00+4 AND LBL 40 TO LBL 43. ****************AIRCRAFT REMOVED FROM SERVICE************************** BLENDED 2 EACH AREAS: FS 513.00 AT LBL 41 (P1) 1.20"L X .800"W X .004"D; FS 513.00+4 AT LBL 43 (P2) 1.30"L X 1.00"W X .003"D. ORIGINAL MATERIAL THICKNESS IS .080". HFEC PERFORMED AT BOTH BLEND AREAS WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. RESTORED CIC PROTECTION. ALL WORK WITHIN ALLOWABLE LIMITS IAW BOMBARDIER GREO 601R-53-41-666 REV C DATED 2012-11-06. WORK COMPLETED ON AERSALE W/O #003486 CARD #20154 AT AERSALE CRS4AER685B.

Part: NONE — CORRODED (FS 484.00+8) · corrosion level 2 · airframe 39,961 hrs · 38,675 cycles

FUSELAGE PRESSURE FLOOR SILL HAS CORROSION AT FS 484.00 +8 AND RBL 40 COMMON TO PRESSURE FLOOR SILL P/N: 601R31145-140. ***************AIRCRAFT REMOVED FROM SERVICE**************************** BLENDED 1 EACH AREA ON PRESSURE FLOOR SILL P/N: 601R31145-140 AT FS 484.00+8 AND RBL 40 (P1) = 1.00"L X 1.00"W X .004"D. BLEND IS WITHIN ALLOWABLE LIMITS IAW BOMBARDIER GREO 601R 53-41-666 REV C DATED 2012-11-06. HFEC PERFORMED AT BLEND AREA WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. RESTORED CIC PROTECTION. ALL WORK WITHIN ALLOWABLE LIMITS IAW BOMBARDIER GREO 601R-53-41-666 REV C DATED 2012-11-06 WORK COMPLETED ON AERSALE W/O #003486 CARD #20163 AT AERSALE CRS4AER685B.

Part: NONE — CORRODED (FS513+5-FS513+8) · corrosion level 2 · airframe 39,961 hrs · 38,675 cycles

FUSELAGE PRESSURE FLOOR SILL HAS CORROSION AT FS 513.00+5 TO FS 513.00+8 AND RBL 40 COMMON TO PRESSURE FLOOR SILL P/N: 601R31145-140. ***************AIRCRAFT REMOVED FROM SERVICE**************************** BLENDED 2 EACH AREAS ON PRESSURE FLOOR SILL P/N: 601R31145-140 AT FS 513.00+3 AND RBL 40 (P1) = .700"L X .700"W X .002"D AND FS 513.00+7 AND RBL 40 (P2) = .800"L X .800"W X .003"D. (P1) AND (P2) WITHIN ALLOWABLE LIMITS IAW BOMBARDIER GREO 601R- 53-41-666 REV C DATED 2012-11-06. HFEC PERFORMED AT EACH BLEND AREA WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. RESTORED CIC PROTECTION. ALL WORK PERFORMED IS WITHIN ALLOWABLE LIMITS IAW BOMBARDIER GREO 601R-53-41-666 REV C DATED 2012-11-06 WORK COMPLETED ON AERSALE W/O #003486 CARD #20166 AT AERSALE CRS4AER685B.

Part: NONE — CORRODED (FS473.15+6-484.0) · corrosion level 2 · airframe 39,961 hrs · 38,675 cycles

FUSELAGE PRESSURE FLOOR SILL HAS CORROSION AT FS 473.15+6 TO FS 484.00+2 AND RBL 39 TO RBL 42 COMMON TO PRESSURE FLOOR SILL P/N: 601R31145-140 AND PRESSURE FLOOR ANGLE P/N: 601R31145-220. ***************AIRCRAFT REMOVED FROM SERVICE**************************** BLENDED 3 EACH AREAS: PRESSURE FLOOR SILL P/N: 601R31145-140 AT FS 484+1 AND RBL 40 (P1) = 1.30"L X 1.25"W X .002"D; PRESSURE FLOOR ANGLE P/N: 601R31145-220 AT FS 473.15+8 AND RBL 41 (P2) = 1.30"L X 1.40"W X .002"D AND FS 484 AT RBL 39 (P3) = 1.00"L X .600"W X .003"D. BLENDS ARE WITHIN ALLOWABLE LIMITS IAW BOMBARDIER GREO 601R 53-41-666 REV C DATED 2012-11-06. HFEC PERFORMED AT EACH BLEND AREA WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. RESTORED CIC PROTECTION. ALL WORK PERFORMED IS IAW BOMBARDIER GREO 601R-53-41-666 REV C DATED 2012-11. WORK COMPLETED ON AERSALE W/O #003486 CARD #20162 AT AERSALE CRS4AER685B.

Part: SKIN — DENTED (FS 625.30+11) · airframe 39,961 hrs · 38,675 cycles

AIRCRAFT L/H SKIN EXTERIOR HAS 1 EACH DENT AT FS 625.30+11 AND S24L+2. DENT DIMENSIONS ARE: (P1) .700L X .600W X .015D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE*********************** PERFORMED CUTOUT (.700" DIA) AT FS 625.30 & S24L+2. HFEC INSPECTION PERFORMED AT CUTOUT WITH NO INDICATIONS. FABRICATED REPAIR DOUBLER OUT OF 2024-T3 .063" DOUBLER IS 6.00"L X 5.70"W. INSTALLED REPAIR DOUBLER AT REPAIR AREA. IDENTIFIED REPAIR DOUBLER AS EA AWAC-CRJ253-01734. ALL WORK PERFORMED IAW ASAP EA # AWAC-CRJ253-01734 REV A DATED 11/20/2021. WORK COMPLETED AT AERSALE CRS4AER685B ON W/O #003486 CARD #20024. N435AW TT:39,961 TC: 38,675

Part: SKIN — GOUGED (FS255 - FS267) · airframe 39,961 hrs · 38,675 cycles

DURING INSPECTION, MAINTENANCE FOUND 8 EACH AREAS OF DAMAGE TO THE FUSELAGE SKIN BETWEEN FS 255.00 AND FS 267.00 AND S25R - S27R. DIMENSIONS ARE: (P1) = 0.800"L X 0.700"W X 0.007"D (P2) = 0.650"L X 0.600"W X 0.008"D (P3) = 0.650"L X 0.600"W X 0.007"D (P4) = 0.850"L X 0.700"W X 0.011"D (P5) = 0.850"L X 0.650"W X 0.009"D (P6) = 0.800"L X 0.650"W X 0.009"D (P7) = 0.600"L X 0.500"W X 0.008"D (P8) = 0.800"L X 0.350"W X 0.002"D AREAS (P1) - (P8) ARE NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV 38. *****************AIRCRAFT REMOVED FROM SERVICE********************* BLENDED AREAS (P1) TO (P8) TO A SMOOTH CONTOUR AND RE-EVALUATED WITHIN ALLOWABLE LIMITS IAW ASAP EA #AWAC-CRJ253-01758 REV IR DATED 11/23/2021. HFEC INSPECTION PERFORMED AT ALL AREAS WITH NO INDICATIONS. VERIFIED MINIMUM REMAINING THICKNESS OF 0.032" AT AREAS (P1) - (P5). VERIFIED MINIMUM REMAINING THICKNESS OF 0.049" AT AREAS (P6) - (P8). VERIFIED NO UNDERLYING DAMAGE AT ALL AREAS. RESTORED PROTECTIVE FINISH AT ALL AREAS. ALL WORK PERFORMED WITHIN LIMITS IAW ASAP EA #AWAC-CRJ253-01758 REV IR DATED 11/23/2021. WORK COMPLETED ON AERSALE W/O #003486 CARD #20016 AT AERSALE CRS#4AER685B. TT: 39,961 TC: 38,675

Part: SKIN — GOUGED (FS 409+48 - 409+) · airframe 39,961 hrs · 38,675 cycles

MAINTENANCE FOUND 3 EACH PREVIOUS BLENDS AT FS 409+48 TO FS 409+48+6 AND S27L ON L/H SKIN EXTERIOR. DIMENSIONS ARE: (P1) FS 409+48 AT S27L .600"L X .500"W X .003"D (P2) FS 409+48+1.6 AT S27L .500"L X .400"W X .002"D (P3) FS 409+48+6 AT S27L .500"L X .450"W X .003"D (P1)(P2)AND (P3) FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV 38. ***************AIRCRAFT REMOVED FROM SERVICE************************* RE-EVALUATED DAMAGE (P1),(P2), AND (P3) AND FOUND WITHIN LIMITS IAW ASAP EA #AWAC-CRJ253-01749 REV IR DATED 11/18/2021. HFEC INSPECTION PERFORMED AT ALL BLENDS WITH NO INDICATIONS. VERIFIED MINIMUM REMAINING THICKNESS OF 0.054" USING UT INSPECTION. VERIFIED NO UNDERLYING DAMAGE AT ALL BLENDS. RESTORED PROTECTIVE FINISH AT ALL BLEND AREAS. ALL WORK PERFORMED AT ALL BLEND AREAS WITHIN ALLOWABLE LIMITS IAW ASAP EA #AWAC-CRJ253-01749 REV IR DATED 11/18/2021. WORK COMPLETED ON AERSALE W/O #003486 CARD #20089 AT AERSALE CRS4AER685B. TT: 39,961 TC: 38,675

Part: SKIN — DENTED (FS 319.70+11) · airframe 39,961 hrs · 38,675 cycles

AIRCRAFT L/H SKIN EXTERIOR HAS 1 EACH DENT AT FS 319.70+11 AND S24L+3. DENT DIMENSIONS ARE: (P1) .600L X .600W X .013D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE*********************** HAND DRESSED DAMAGED AREA TO ORIGINAL CONTOUR OF SKIN. VERIFIED NO CRACKS. VERIFIED NO LOOSE/PULLED FASTENERS AND NO DAMAGE TO UNDERLYING STRUCTURE COMMON TO REPAIR AREA. HFEC PERFORMED WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. RE-EVALUATED SKIN AND FOUND WITHIN LIMITS IAW ASAP EA #AWAC-CRJ253-01746 REV IR DATED 11/18/2021. ALL WORK PERFORMED IAW ASAP EA # AWAC-CRJ253-01746 REV IR DATED 11/18/2021. WORK COMPLETED AT AERSALE CRS4AER685B ON W/O #003486 CARD #20015. N435AW TT:39,961 TC: 38,675

Part: SKIN — DENTED (FS 319.70+3) · airframe 39,961 hrs · 38,675 cycles

AIRCRAFT SKIN EXTERIOR HAS 1 EACH DENT AT FS 319.70+3 AND S27. DENT DIMENSIONS ARE: (P1) .500L X .468W X .006D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE*********************** HAND DRESSED DAMAGED TO .500"L X .450"W X .003"D. VERIFIED NO CRACKS. VERIFIED NO LOOSE/PULLED FASTENERS AND NO DAMAGE TO UNDERLYING STRUCTURE COMMON TO REPAIR AREA. HFEC PERFORMED WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. RE-EVALUATED SKIN AND FOUND WITHIN LIMITS IAW ASAP EA #AWAC-CRJ253-01739 REV A DATED 11/23/2021. ALL WORK PERFORMED IAW ASAP EA # AWAC-CRJ253-01739 REV A DATED 11/23/2021. WORK COMPLETED AT AERSALE CRS4AER685B ON W/O #003486 CARD #20031. N435AW TT:39,961 TC: 38,675

Part: NONE — DENTED (FS 621) · airframe 39,961 hrs · 38,675 cycles

MAINTENANCE FOUND DENT COMMON TO FWD SIDE OF AFT PRESSURE BULKHEAD AT FS621 AND RBL 41. DAMAGE MEASURES .600"L X .500"W X .012"D. DAMAGE IS NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-61-19 REV 38. ***********AIRCRAFT REMOVED FROM SERVICE*************************** HAND-DRESSED AREA TO ORIGINAL CONTOUR AND RE-EVALUATED WITHIN ALLOWABLE LIMITS IAW ASAP EA #AWAC-CRJ253-01754 REV IR DATED 11/20/2021. VERIFIED NO LOOSE OR DAMAGED FASTENER COMMON TO REPAIR AREA. HFEC INSPECTION PERFORMED AT REPAIR AREA WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH TO REPAIR AREA. ALL WORK PERFORMED WITHIN ALLOWABLE LIMITS IAW ASAP EA #AWAC-CRJ253-01754 REV IR DATED 11/20/2021. WORK COMPLETED ON AERSALE W/O #003486 CARD #20101 AT AERSALE #CRS4AER685B. N435AW TT: 39,961 TC: 36,875

Part: SKIN — GOUGED (FS 409+48) · airframe 39,961 hrs · 38,675 cycles

MAINTENANCE FOUND 1 EACH SCRATCH AT FS 409+48 AND S25L+4 ON L/H SKIN EXTERIOR. DIMENSIONS ARE: (P1) .600"L X .500"W X .005"D. SCRATCH WAS FOUND NOT TO BE WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV 38. ***************AIRCRAFT REMOVED FROM SERVICE************************* BLENDED AREA AND RE-EVALUATED DAMAGE (P1) AND FOUND WITHIN LIMITS IAW ASAP EA #AWAC-CRJ253-01750 REV A DATED 12/02/2021. HFEC INSPECTION PERFORMED AT (P1) BLEND WITH NO INDICATIONS. VERIFIED MINIMUM REMAINING THICKNESS OF 0.039" USING UT INSPECTION. VERIFIED NO UNDERLYING DAMAGE AT (P1) BLEND. RESTORED PROTECTIVE FINISH ATL BLEND AREAS. ALL WORK PERFORMED AT BLEND AREA WITHIN ALLOWABLE LIMITS IAW ASAP EA #AWAC-CRJ253-01750 REV A DATED 12/02/2021. WORK COMPLETED ON AERSALE W/O #003486 CARD #20090 AT AERSALE CRS4AER685B. TT: 39,961 TC: 38,675

Part: NONE — GOUGED (FS 621) · airframe 39,961 hrs · 38,675 cycles

MAINTENANCE FOUND 2 EACH SCRATCHES COMMON TO FWD SIDE OF AFT PRESSURE BULKHEAD AT FS 621 AND RBL 29.75 AT WL 137.18-137.95 . DAMAGE MEASURES: (P1) = .350"L X .010"X .005" AND (P2) = .500"L X .010"W X .005"D. DAMAGE IS NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-61-19 REV 38. ***********AIRCRAFT REMOVED FROM SERVICE*************************** HAND-DRESSED (P1) AND (P2) AND RE-EVALUATED WITHIN ALLOWABLE LIMITS IAW ASAP EA #AWAC-CRJ253-01753 REV IR DATED 11/20/2021. VERIFIED NO LOOSE OR DAMAGED FASTENER COMMON TO REPAIR AREAS. HFEC INSPECTION PERFORMED AT REPAIR AREAS WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH TO REPAIR AREAS. ALL WORK PERFORMED WITHIN ALLOWABLE LIMITS IAW ASAP EA #AWAC-CRJ253-01753 REV IR DATED 11/20/2021. WORK COMPLETED ON AERSALE W/O #003486 CARD #20106 AT AERSALE #CRS4AER685B. N435AW TT: 39,961 TC: 36,875

Part: ANGLE — GOUGED (FS863 - FS891) · airframe 39,961 hrs · 38,675 cycles

MAINTENANCE FOUND SCRATCH DAMAGE ON L/H HORIZONTAL STABILIZER FAIRING ATTACHMENT VISOR ANGLE P/N: 600-23072 AT LBL 6 FROM FWD TO AFT END MEASURING: 38.00"L X .700"W X .005"D. VISOR IS FORMED FROM PA21068 .075" 2024-T3511. ***************AIRCRAFT REMOVED FROM SERVICE********************** BLENDED DAMAGED AREA TO A SMOOTH CONTOUR ON VISOR ANGLE P/N: 600-23072. BLEND DIMENSIONS ARE: 38.00"L X .700"W X .005"D. HFEC INSPECTION PERFORMED AT REPAIR AREA WITH NO INDICATIONS. VERIFIED MINIMUM REMAINING THICKNESS OF .070". RESTORED PROTECTIVE FINISH TO REPAIR AREA. ALL WORK PERFORMED WITHIN LIMITS IAW ASAP EA #AWAC- CRJ255-01768 REV IR DATED 12/02/2021. WORK PERFORMED ON AERSALE W/O #003486 CARD #20452 AT AERSALE CRS #4AER685B. N435AW TT: 39,961 TC: 38,675

Part: SKIN — DENTED (FS 672.20+5.4) · airframe 39,961 hrs · 38,675 cycles

AIRCRAFT SKIN UPPER CROWN EXTERIOR HAS 1 EACH DENT AT FS 672.20+5.2" AND S3R+4". DENT DIMENSIONS ARE: (P1) 1.900L X .900W X .008D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE*********************** VERIFIED NO LOOSE/PULLED FASTENERS AND NO DAMAGE TO UNDERLYING STRUCTURE COMMON TO REPAIR AREA. HFEC PERFORMED WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. RE-EVALUATED SKIN AND FOUND WITHIN LIMITS IAW ASAP EA #AWAC-CRJ253-01767 REV IR DATED 12/03/2021. ALL WORK PERFORMED IAW ASAP EA # AWAC-CRJ253-01767 REV IR DATED 12/03/2021. WORK COMPLETED AT AERSALE CRS4AER685B ON W/O #003486 CARD #20495. N435AW TT:39,961 TC: 38,675

Part: DOOR — GOUGED (FS295-FS364) · airframe 39,961 hrs · 38,675 cycles

PASSENGER DOOR UPPER SILL P/N: 601R31522 HAS SEVERAL GOUGES/ABRASIONS BETWEEN FS 295.00 - FS 364.00 AT S3L. DAMAGE LOCATIONS AND MEASUREMENTS ARE: (P1) FS 310+2 & S3L = .450"L X .250"W X .002"D (P2) FS 319.70+1 & S3L = .850"L X .500"W X .003"D (P3) FS 319.70+6 & S3L = .900"L X .550"W X .002"D (P4) FS 333.00+2 & S3L = 1.350"L X .800"W X .011"D (P5) FS 333.00+10 & S3L = .800"L X .700"W X .006"D FOUND DAMAGE NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-00 REV 38. ****************AIRCRAFT REMOVED FROM SERVICE*********************** BLENDED DAMAGE TO A SMOOTH CONTOUR AT AREAS (P1) - (P5). VERIFIED BLEND DIMENSIONS. VERIFIED NO LOOSE/PULLED FASTENERS AND NO DAMAGE TO UNDERLYING STRUCTURE COMMON TO REPAIR AREAS. HFEC PERFORMED WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. RE-EVALUATED REPAIRS AND FOUND WITHIN LIMITS IAW ASAP EA #AWAC-CRJ253-01760 REV IR DATED 11/29/2021. ALL WORK PERFORMED IAW ASAP EA # AWAC-CRJ253-01760 REV IR DATED 11/29/2021. WORK COMPLETED AT AERSALE CRS4AER685B ON W/O #003486 CARD #20339. N435AW TT:39,961 TC: 38,675

Part: SKIN — DENTED (FS 409+15) · airframe 39,961 hrs · 38,675 cycles

AIRCRAFT SKIN L/H EXTERIOR HAS 1 EACH DENT AT FS 409.00+15" AND S18L+3.80". DENT DIMENSIONS ARE: (P1) .500L X .450W X .002D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE*********************** VERIFIED NO LOOSE/PULLED FASTENERS AND NO DAMAGE TO UNDERLYING STRUCTURE COMMON TO REPAIR AREA. HFEC PERFORMED WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. RE-EVALUATED SKIN AND FOUND WITHIN LIMITS IAW ASAP EA #AWAC-CRJ253-01752 REV IR DATED 11/19/2021. ALL WORK PERFORMED IAW ASAP EA # AWAC-CRJ253-01752 REV IR DATED 11/19/2021. WORK COMPLETED AT AERSALE CRS4AER685B ON W/O #003486 CARD #20091. N435AW TT:39,961 TC: 38,675

Part: NONE — GOUGED (FS 250) · airframe 39,961 hrs · 38,675 cycles

TOOL MARKS COMMON TO AFT SIDE OF PILOT'S WINDSHIELD SIDE WINDOW POST AT FS 250. DIMENSIONS ARE: (P1) = .900"L X .600"W X .015"D. *************AIRCRAFT REMOVED FROM SERVICE************************ BLENDED DAMAGE TO A SMOOTH CONTOUR AT AREA (P1). VERIFIED REPORTED DIMENSIONS ARE NOT EXCEEDED. HFEC PERFORMED WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. RE-EVALUATED BLEND AND FOUND WITHIN LIMITS IAW MHIRJ REO 601R-53-11-3744 REV (--) DATED 12/06/2021. ALL WORK PERFORMED IAW MHIRJ REO 601R-53-11-3744 REV (--) DATED 12/06/2021. WORK COMPLETED AT AERSALE CRS4AER685B ON W/O #003486 CARD #20441. N435AW TT:39,961 TC: 38,675

Part: NONE — NONE (HOR STAB) · airframe 39,961 hrs · 38,675 cycles

PRIOR TO INSTALLATION OF HSTA PINS & TRUNNION INSTALLATION OF THE UPPER PIN FOUND ATTACH HOLES IN AIRCRAFT STRUCTURE BELOW SERVICE BULLETIN NOMINAL SIZE (.189" - .195"). PRIOR TO INSTALLATION OF HSTA PINS & TRUNNION INSTALLATION OF THE LOWER PIN FOUND ATTACH HOLES IN AIRCRAFT STRUCTURE BELOW SERVICE BULLETIN NOMINAL SIZE (.200" - .210"). *************AIRCRAFT REMOVED FROM SERVICE*********************** OPENED HOLES IN THE AIRCRAFT STRUCTURE, COMMON TO UPPER PIN, L/H (.182" UPPER/.182" LOWER) AND R/H (.182" UPPER/.182" LOWER) UP TO .190" IAW MHIRJ SNIEO DWG # K601R92308 S59. REFERENCE EO #E16/007/427 STEP #53 AND STEP #62. OPENED HOLES IN THE AIRCRAFT STRUCTURE, COMMON TO LOWER PIN, L/H (.193" FWD/.191" AFT) AND R/H (.190" FWD/.193" AFT) UP TO .200" IAW MHIRJ SNIEO DWG # K601R92308 S58. REFERENCE EO #E16/007/427 STEP #76 AND STEP #85. WORK ACCOMPLISHED ON AERSALE WO #003486 CARDS #20574 AND #00007. CRS #4AER685B. N435AW TT:39,961 TC: 38,675

Part: SKIN — DENTED (654.50+10-654.50) · airframe 39,861 hrs · 38,675 cycles

AIRCRAFT LOWER BELLY SKIN EXTERIOR HAS 3 EACH DENTS AT FS 654.50+10-FS 654.50+16 AND S25R+1 S26L+4. DENT DIMENSIONS ARE AS FOLLOW: (P1) = FS654.50+12 & S26L+4 = .500"L X .455"W X .016"D (P2) = FS654.50+10 & S26R+4 = .550"L X .450"W X .007"D (P3) = FS654.50+16 & S25R+1 = .500"L X .400"W X .017"D ALL (3 EACH) DENTS ARE NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. MAINTENANCE FOUND GOUGE ON INTERIOR SIDE OF DENT (P2) WITH DIMENSIONS OF: (P4) = FS654.50+10 & S26R+4 = 1.00"L X .700"W X .004"D. GOUGE (P4) IS NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV 38. ****************AIRCRAFT REMOVED FROM SERVICE*********************** HAND DRESSED DAMAGED AREAS (P1)-(P3) TO ORIGINAL CONTOUR OF SKIN. BLENDED GOUGE (P4) TO A SMOOTH CONTOUR AT FS654.50+10 & S26R+4 AT SKIN INTERIOR. VERIFIED NO CRACKS. VERIFIED NO LOOSE/PULLED FASTENERS AND NO DAMAGE TO UNDERLYING STRUCTURE COMMON TO REPAIR AREAS. HFEC PERFORMED WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH AT P1 TO P4 RE-EVALUATED SKIN AND FOUND WITHIN LIMITS IAW ASAP EA #AWAC-CRJ253-01747 REV B DATED 12/13/2021. ALL WORK PERFORMED IAW ASAP EA # AWAC-CRJ253-01747 REV B DATED 12/13/2021. WORK COMPLETED AT AERSALE CRS# 4AER685B ON W/O #003486 CARD #20028. N435AW TT:39,961 TC: 38,675

Part: SKIN — GOUGED (FS 640+2) · airframe 39,961 hrs · 38,675 cycles

MAINTENANCE FOUND 1 EACH GOUGE AT FS 640+2 AND S19L ON L/H SKIN EXTERIOR. DIMENSIONS ARE: (P1) 1.6"L X 1.2"W X .014"D. GOUGE WAS FOUND NOT TO BE WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV 38. ***************AIRCRAFT REMOVED FROM SERVICE************************* BLENDED AREA AND RE-EVALUATED DAMAGE (P1) AND FOUND WITHIN LIMITS IAW ASAP EA #AWAC-CRJ253-01751 REV IR DATED 11/18/2021. HFEC INSPECTION PERFORMED AT (P1) BLEND WITH NO INDICATIONS. VERIFIED MINIMUM REMAINING THICKNESS OF 0.049" USING UT INSPECTION. VERIFIED NO UNDERLYING DAMAGE AT (P1) BLEND. RESTORED PROTECTIVE FINISH ATL BLEND AREAS. ALL WORK PERFORMED AT BLEND AREA WITHIN ALLOWABLE LIMITS IAW ASAP EA #AWAC-CRJ253-01751 REV IR DATED 11/18/2021. WORK COMPLETED ON AERSALE W/O #003486 CARD #20025 AT AERSALE CRS4AER685B. TT: 39,961 TC: 38,675

Part: SKIN — DENTED (FS 310+7) · airframe 39,961 hrs · 38,675 cycles

AIRCRAFT L/H SKIN EXTERIOR HAS 1 EACH DENT AT FS 310.00+7 AND S22L+2. DENT DIMENSIONS ARE: (P1) .900L X .900W X .003D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE*********************** VERIFIED NO LOOSE/PULLED FASTENERS AND NO DAMAGE TO UNDERLYING STRUCTURE COMMON TO DAMAGED AREA. HFEC PERFORMED WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. RE-EVALUATED DENT AND FOUND WITHIN LIMITS IAW ASAP EA #AWAC-CRJ253-01757 REV IR DATED 11/21/2021. ALL WORK PERFORMED IAW ASAP EA # AWAC-CRJ253-01757 REV IR DATED 11/21/2021. WORK COMPLETED AT AERSALE CRS4AER685B ON W/O #003486 CARD #20014. N435AW TT:39,961 TC: 38,675

Part: SKIN — DENTED (FS 559+80) · airframe 39,961 hrs · 38,675 cycles

AIRCRAFT R/H SKIN EXTERIOR HAS 1 EACH DENT AT FS 559+80 AND S7R+3. DENT DIMENSIONS ARE: (P1) .600L X .350W X .005D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE*********************** VERIFIED NO LOOSE/PULLED FASTENERS AND NO DAMAGE TO UNDERLYING STRUCTURE COMMON TO DAMAGED AREA. HFEC PERFORMED WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. RE-EVALUATED DENT AND FOUND WITHIN LIMITS IAW ASAP EA #AWAC-CRJ253-01740 REV A DATED 11/19/2021. ALL WORK PERFORMED IAW ASAP EA # AWAC-CRJ253-01740 REV A DATED 11/19/2021. WORK COMPLETED AT AERSALE CRS4AER685B ON W/O #003486 CARD #20036. N435AW TT:39,961 TC: 38,675

Part: SKIN — DENTED (FS 409+12) · airframe 39,961 hrs · 38,675 cycles

AIRCRAFT L/H SKIN EXTERIOR HAS 1 EACH DENT AT FS 319.70+11 AND S24L+3. DENT DIMENSIONS ARE: (P1) .600L X .600W X .013D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE*********************** HAND DRESSED DAMAGED AREA TO ORIGINAL CONTOUR OF SKIN. VERIFIED NO CRACKS. VERIFIED NO LOOSE/PULLED FASTENERS AND NO DAMAGE TO UNDERLYING STRUCTURE COMMON TO REPAIR AREA. HFEC PERFORMED WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. RE-EVALUATED SKIN AND FOUND WITHIN LIMITS IAW ASAP EA #AWAC-CRJ253-01746 REV IR DATED 11/18/2021. ALL WORK PERFORMED IAW ASAP EA # AWAC-CRJ253-01746 REV IR DATED 11/18/2021. WORK COMPLETED AT AERSALE CRS4AER685B ON W/O #003486 CARD #20015. N435AW TT:39,961 TC: 38,675

Part: SKIN — GOUGED (FS 409+72 - 409+) · airframe 39,961 hrs · 38,675 cycles

MAINTENANCE FOUND A PREVIOUS BLEND (P1) AT FS 409.00+80 AT S26R+1 MEASURING .500"L X 007"D AND A SCRATCH (P2) AT FS 409.00+72 AT S26R MEASURING .450"L X .005"D. BOTH AREAS FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31. ***************AIRCRAFT REMOVED FROM SERVICE************************* RE-EVALUATED DAMAGE (P1) AT FS 409+80 AND S26R+1 AND FOUND WITHIN LIMITS IAW ASAP EA #AWAC-CRJ253-01737 REV B DATED 11/17/2021. HFEC INSPECTION PERFORMED AT (P1) BLEND WITH NO INDICATIONS. VERIFIED MINIMUM REMAINING THICKNESS OF 0.051" USING UT INSPECTION. VERIFIED NO UNDERLYING DAMAGE AT (P1) BLEND. RESTORED PROTECTIVE FINISH AT (P1) BLEND AREA. ALL WORK PERFORMED AT (P1) BLEND AREA WITHIN ALLOWABLE LIMITS IAW ASAP EA #AWAC-CRJ253-01737 REV B DATED 11/17/2021. BLENDED AREA AT (P2) SMOOTH TO REPORTED MEASUREMENT OF .450"L X .500"D IAW ASAP EA # AWAC-CRJ253- 01736 REV A DATED 11/17/2021. RE-EVALUATED (P2) BLEND AREA AND FOUND WITHIN ALLOWABLE LIMITS IAW ASAP EA # AWAC-CRJ253-01736 REV A DATED 11/17/2021. HFEC INSPECTION PERFORMED AT (P2) BLEND WITH NO INDICATIONS. VERIFIED MINIMUM REMAINING THICKNESS OF 0.053" AT (P2) BLEND USING UT INSPECTION. VERIFIED NO UNDERLYING DAMAGE AT (P2) BLEND AREA. RESTORED PROTECTIVE FINISH AT (P2) BLEND AREA. ALL WORK PERFORMED AT (P2) BLEND AREA WITHIN ALLOWABLE LIMITS IAW ASAP EA # AWAC-CRJ253-01736 REV A DATED 11/17/2021. WORK COMPLETED ON AERSALE W/O #003486 CARD #20087 AT AERSALE CRS4AER685B. TT: 39,961 TC: 38,675

Part: NONE — GOUGED (FS 621) · airframe 39,961 hrs · 38,675 cycles

MAINTENANCE FOUND SETMARK DAMAGE AROUND RIVET ON AFT PRESSURE BULKHEAD AT FS621 AND RBL 38. DAMAGE MEASURES 1.00"L X .750"W X .040"D. DAMAGE IS NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-61-19 REV 38. ***********AIRCRAFT REMOVED FROM SERVICE*************************** HAND-DRESSED AREA TO ORIGINAL CONTOUR AND RE-EVALUATED WITHIN ALLOWABLE LIMITS IAW ASAP EA #AWAC-CRJ253-01755 REV IR DATED 11/20/2021. VERIFIED NO LOOSE OR DAMAGED FASTENER COMMON TO REPAIR AREA. HFEC INSPECTION PERFORMED AT REPAIR AREA WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH TO REPAIR AREA. ALL WORK PERFORMED WITHIN ALLOWABLE LIMITS IAW ASAP EA #AWAC-CRJ253-01755 REV IR DATED 11/20/2021. WORK COMPLETED ON AERSALE W/O #003486 CARD #20105 AT AERSALE #CRS4AER685B. N435AW TT: 39,961 TC: 36,875

Part: SKIN — DENTED (FS 559.00+7) · airframe 39,961 hrs · 38,675 cycles

AIRCRAFT SKIN EXTERIOR HAS 1 EACH DENT AT FS 559.00+7 AND S8L. DENT DIMENSIONS ARE: (P1) .800L X .650W X .004D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE*********************** VERIFIED DAMAGE DIMENSION: .800"L X .650"W X .004"D. VERIFIED NO CRACKS. VERIFIED NO LOOSE/PULLED FASTENERS AND NO DAMAGE TO UNDERLYING STRUCTURE COMMON TO REPAIR AREA. HFEC PERFORMED WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. RE-EVALUATED SKIN AND FOUND WITHIN LIMITS IAW ASAP EA #AWAC-CRJ253-01742 REV A DATED 11/19/2021. ALL WORK PERFORMED IAW ASAP EA # AWAC-CRJ253-01742 REV A DATED 11/19/2021. WORK COMPLETED AT AERSALE CRS4AER685B ON W/O #003486 CARD #20037. N435AW TT:39,961 TC: 38,675

Part: SKIN — DENTED (FS 700.00+13) · airframe 39,961 hrs · 38,675 cycles

AIRCRAFT L/H SKIN EXTERIOR HAS 1 EACH DENT AT FS 700.00+13 AND S21L+4. DENT DIMENSIONS ARE: (P1) .600L X .600W X .008D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE*********************** VERIFIED NO LOOSE/PULLED FASTENERS AND NO DAMAGE TO UNDERLYING STRUCTURE COMMON TO DAMAGED AREA. HFEC PERFORMED WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. RE-EVALUATED DENT AND FOUND WITHIN LIMITS IAW ASAP EA #AWAC-CRJ253-01738 REV IR DATED 11/16/2021. ALL WORK PERFORMED IAW ASAP EA # AWAC-CRJ253-01738 REV IR DATED 11/16/2021. WORK COMPLETED AT AERSALE CRS4AER685B ON W/O #003486 CARD #20026. N435AW TT:39,961 TC: 38,675

Part: SKIN — DENTED (FS 319.70+8) · airframe 39,961 hrs · 38,675 cycles

AIRCRAFT R/H SKIN EXTERIOR HAS 1 EACH DENT AT FS 319.70+8 AND S22R+4. DENT DIMENSIONS ARE: (P1) 1.00L X 1.00W X .001D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE*********************** HAND DRESSED DAMAGED AREA TO ORIGINAL CONTOUR OF SKIN. VERIFIED NO CRACKS. VERIFIED NO LOOSE/PULLED FASTENERS AND NO DAMAGE TO UNDERLYING STRUCTURE COMMON TO REPAIR AREA. HFEC PERFORMED WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. RE-EVALUATED SKIN AND FOUND WITHIN LIMITS IAW ASAP EA #AWAC-CRJ253-01743 REV A DATED 12/06/2021. ALL WORK PERFORMED IAW ASAP EA # AWAC-CRJ253-01743 REV A DATED 12/06/2021. WORK COMPLETED AT AERSALE CRS4AER685B ON W/O #003486 CARD #20022. N435AW TT:39,961 TC: 38,675

Part: ANGLE — CORRODED (FS 319.70-FS349) · corrosion level 2 · airframe 39,961 hrs · 38,675 cycles

MAINTENANCE FOUND CORROSION ON SERVICE DOOR LOWER SILL ANGLE P/N: 601R38303-253 AT FS 319.70 TO FS 349 AND RBL 38 TO RBL 39. **************AIRCRAFT REMOVED FROM SERVICE************************ BLENDED 3 EACH AREAS ON SERVICE DOOR LOWER SILL ANGLE AS FOLLOW: FS 319+6 & RBL 39 (P1) = 4.0"L X 1.9"W X .015"D FS 333+3 & RBL 39 (P2) = 2.0"L X 1.0"W X .005"D FS 333+7 & RBL 39 (P3) = 3.6"L X 1.7"W X .014"D VERIFIED COMPLETE REMOVAL OF CORROSION AT BLEND AREAS. HFEC INSPECTION PERFORMED AT REPAIR AREAS WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. RESTORED CIC PROTECTION. ALL WORK PERFORMED WITHIN ALLOWABLE LIMITS IAW MHIRJ REO 601R-53-21-3512 REV (--) DATED 2021-12-04. WORK COMPLETED ON AERSALE W/O #003486 CARD #20377 AT AERSALE CRS #4AER685B. N435AW TT: 39,961 TC: 38,675

Part: SKIN — DENTED (FS 280+1) · airframe 39,961 hrs · 38,675 cycles

AIRCRAFT SKIN L/H EXTERIOR HAS 1 EACH DENT AT FS 280.00+1 AND S14L. DENT DIMENSIONS ARE: (P1) 1.200L X 1.00W X .008D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE*********************** VERIFIED NO LOOSE/PULLED FASTENERS AND NO DAMAGE TO UNDERLYING STRUCTURE COMMON TO REPAIR AREA. HFEC PERFORMED WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. RE-EVALUATED SKIN AND FOUND WITHIN LIMITS IAW ASAP EA #AWAC-CRJ253-01741 REV A DATED 11/19/2021. ALL WORK PERFORMED IAW ASAP EA # AWAC-CRJ253-01741 REV A DATED 11/19/2021. WORK COMPLETED AT AERSALE CRS4AER685B ON W/O #003486 CARD #20147. N435AW TT:39,961 TC: 38,675

Part: BRAKE ASSY — FAULTED (MLG) · airframe 39,654 hrs · 38,367 cycles

TIRE #1 BLOWN. BTMS READS 14. PILOT REPORTED SMOKE FROM TIRE, CALLED FIRE DEPARTMENT THEY CHECKED TEMP IT READ 200. DEPLANED PAX ON TAXIWAY. PERFORMED INSPECTION IAW AMM 05-51-27, VERIFIED NO DAMAGE TO MLG AND NLG. PERFORMED VISUAL INSPECTION OF TIRES, NO DEFECTS NOTED. #1 BRAKE ASSY REQUIRES REPLACEMENT, REF 342816/3 FOR R&R**FLIGHT NO 3902*** REF 342816/2 #1 BTMS SHOWING 14. #1 BRAKE ASSY REQUIRES REPLACEMENT ***AIRCRAFT REMOVED FROM SERVICE*** R&R #1 BRAKE ASSEMBLY IN REFRENCE TO AWAC SUPP 12-039G. P/N: 5010520-1, S/N OFF: MAY02-3397, S/N ON: DEC00-2449 ARW

Part: SKIN — DAMAGED (BS 226.75) · airframe 39,108 hrs · 37,801 cycles

L/H ACCESS PANEL 131AL HAS A LOOSE FREEZE PLUG AT FS226.75 AND STR 19L-1.05. ***AIRCRAFT REMOVED FROM SERVICE*** REPAIRED FUSELAGE SKIN AT STATION 226.75 AND STR19L-1.05 REF ASAP EA# AWAC CRJ253-01593 REV IR DATED 3/31/2021.

Part: SKIN — DAMAGED (FS383) · airframe 39,108 hrs · 37,801 cycles

LIGHTNING STRIKE DAMAGE TO OF FUSELAGE AT FS383 LEFT OF STRINGER 0 TO EDGE OF ANTENNA ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED DAMAGE AT FS383 LEFT OF STR0, PERFORMED UT THICKNESS CHECK, REMAINING MATERIAL 0.052", PERFORMED HFEC NO DEFECTS NOTED, AREA IS WITHIN LIMITS, APPLIED ALODINE REF REO 601R-53-00-115 REV E DATED 2013/09/18

Part: SKIN — DAMAGED (FS391.75) · airframe 39,108 hrs · 37,801 cycles

LIGHTNING STRIKE DAMAGE TOP OF FUSELAGE AT FS391.75 JUST RIGHT OF STR0 ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED DAMAGE AT FS391.75 JUST RIGHT OF STR0, PERFORMED UT THICKNESS CHECK, REMAINING MATERIAL 0.051", PERFORMED HFEC NO DEFECTS NOTED, AREA IS WITHIN LIMITS, REMOVED AND REPLACED FASTENERS, APPLIED ALODINE REF REO 601R-53-00-115 REV E DATED 2013/09/18

Part: SKIN — DAMAGED (FS389.25) · airframe 39,108 hrs · 37,801 cycles

LIGHTNING STRIKE DAMAGE TOP OF FUSELAGE AT FS389.25 JUST RIGHT OF STR0 ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED DAMAGE AT FS389.25 JUST RIGHT OF STR0, PERFORMED UT THICKNESS CHECK, REMAINING MATERIAL 0.052", PERFORMED HFEC NO DEFECTS NOTED, AREA IS WITHIN LIMITS, APPLIED ALODINE REF REO 601R-53-00-115 REV E DATED 2013/09/18

Part: SKIN — DAMAGED (BS 381) · airframe 39,108 hrs · 37,801 cycles

LIGHTNING STRIKE DAMAGE TOP OF FUSELAGE AT FS 381.00 L/H AND R/H OF STRINGER 0 ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED DAMAGE AT FS 381.00 L/H AND R/H OF STRINGER 0. PERFORMED UT THICKNESS CHECK. REMAINING MATERIAL, 0.050". PERFORMED HFEC WITH NO DEFECTS NOTED. PERFORMED CONDUCTIVITY TEST PER NDT 53-00-099 REV 42 WITH NO CHANGE NOTED. REWORKED AREA IS WITHIN LIMITS, REF EA# AWAC CRJ253-01591 REV A DATED 03/25/2021.

Part: CONTROL PANEL — MALFUNCTIONED (MLG) · airframe 39,003 hrs · 37,690 cycles

AFTER TAKE-OFF, CWA, LANDING GEAR WOULD NOT RETRACT, STAYED THREE GREEN. RECEIVED INBOARD A/SKID CAUTION AND PARKING BRAKE SOV CAUTION MESSAGES. PUT GEAR HANDLE DOWN, MESSAGES CLEARED. AIRCRAFT REMOVED FROM SERVICE. CODE ON PROX SYSTEM BOX. DI-11-DOWN. OFF PER FIMM 32-60-20 FIG 101. SHEET 3 ITEM 6. R & R LANDING GEAR CONTROL PANEL, REF 32-31-01. C/W FUNC TEST LANDING GEAR EXTENSION RETRACTION MINIMUM 8 TIMES. CHECKS GOOD NO CODES.

Part: BYPASS VALVE — DAMAGED (LT A/C PACK) · airframe 38,785 hrs · 37,463 cycles

RECEIVED LAV SMOKE DET CAUTION AT 600 FT, CW QRH NO SMOKE OR HAZE EVIDENT. HOWEVER, THERE WAS AN ODER OF "ROTTEN EGGS" RETURN TO LNK LANDING WEIGHT 42870, NORMAL LANDING. NO INDICATIONS OF FAILURE IN PACKS. AIRCRAFT REMOVED FROM SERVICE. FOUND LT CONDITIONING PACK STUCK IN FULL HOT POSITION, UNCONTROLLABLE IN MANUAL OR AUTO MODE. REPLACED LT DUAL BYPASS VALVE, PER AMM 21-61-31. BOTH LT AND RT CONDITIONING PACKS OPERATE NORMALLY, NO FURTHER SMELL IN CABIN. C/W SUP 09-037C.

Part: RELAY — FAILED (JUNCTION BOX 3) · airframe 38,594 hrs · 37,254 cycles

AFTER TAKEOFF WE RECEIVED A GEAR DISAGREE WITH NOSE GEAR DOWN AND MAINS UP. RAN QRH LANDED WITHOUT INCIDENT. A/C WAS CARRYING 5 PASSENGERS, NO JUMPSEATER, WITH CA FLYING. FA AND PAX WERE NOTIFIED AND NO ADVERSE REACTIONS NOTED. FIRE/EMS RESPONDED DUE TO EMERGENCY DECLARED. "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED RELAY K1RH FROM JCT BOX #3. IAW W/W 23-51-00. A/C REQUIRES GEAR SWING. PERFORMED FUNCTIONAL CHECK THE LANDING GEAR. EXTENSION AND RETRACTION SYSTEM. IAW AMM 32-30-00. OPS CHECK GOOD.

Part: SKIN PANEL — DENTED (FUSELAGE) · airframe 38,590 hrs · 37,249 cycles

DENT ON AFT FUSE AT FS 662.70 BET S22L & S23L. "AIRCRAFT REMOVED FROM SERVICE" CUT OUT DAMAGED AREA AND HFEC WITH NO INDICATIONS NOTED AT THIS TIME. FABRICATED REPAIR DOUBLER FROM 2024-T3 .063" 9.5"L X 7.5"W AND INSTALLED REF CRJ-200 SRM 53 00-31.

Part: SKIN — DENTED (FUSELAGE) · airframe 38,590 hrs · 37,249 cycles

DENT ON FUSELAGE SKIN AT FS 630.00 BETWEEN S23R & S24R. "AIRCRAFT REMOVED FROM SERVICE" CUTOUT THE DAMAGE AREA DIMENSION IS 3.1" X 2.3" WITH 0.35" RADIUS ON CORNERS. HFEC PERFUMED WITH NO CRACK INDICATIONS NOTED. FABRICATED REPAIR DOUBLER FROM 2024-T3 .063" 8.3"L X 7.9"W AND INSTALLED REF ASAP EA # AWAC-CRJ253-01484 REV IR DTD 4/3/2020

Part: SKIN PANEL — DENTED (FUSELAGE) · airframe 38,590 hrs · 37,249 cycles

DENT AT FS 692.5 & S24L-3". "AIRCRAFT REMOVED FROM SERVICE" COLD FORMED DENT TO ORIGINAL CONTOUR WITH HFEC PERFORMED WITH A.5" INDICATION. CUT OUT DAMAGE AND HFEC WITH NO INDICATIONS NOTED AT THIS TIME. FABRICATED DOUBLER FROM 2024 T-3 .063" 7" X 6.5" AND INSTALLED REPAIR DOUBLER REF ASAP EA# CRJ253-01472REV IR DTD 3/10/2020

Part: CABLE — DAMAGED (AILERON) · airframe 38,590 hrs · 37,249 cycles

R/H O/B AILERON FUSELAGE CABLE IS FRAYED AT QUADRANT IN WHEEL WELL. "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED R/H O/B AILERON FUSELAGE CABLE P/N 601R-90020-133 CRJ-200 AMM 27-00 & 27-11-00 REV 60.

Part: SKIN — DENTED (FUSELAGE) · airframe 38,590 hrs · 37,249 cycles

2 FUSELAGE DENTS AT FS 703.875 & S21L AND FS 705 BETWEEN S19L & S20L. DENT @ FS 703.875 &S21L MEASURES .550"L X .4"W X .006"D DENT @ FS 705 BETWEEN S 19L & S20L MEASURES 1.0"L X 1.0"W X .022"D "AIRCRAFT REMOVED FROM SERVICE" BOTH DENTS HAVE BEEN HFEC WITH NO INDICATIONS AND NO FURTHER ACTION IS REQUIRED. REF ASAP EA# AWAC-CRJ253-01475 REV B DTD 3/17/2020

Part: STRUCTURE — CRACKED (APU BAY) · airframe 38,590 hrs · 37,249 cycles

MULTIPLE CRACKS ON BACK OF APU ENCLOSURE. "AIRCRAFT REMOVED FROM SERVICE" CRACK #1 IS 1.62" IN LENGTH AND LOCATED 9" AFT OF FWD EDGE AND 8" I/B OF LWR O/B EDGE. CRACK #2 IS 1.60" IN LENGTH AND LOCATED 9" AFT OF LWR FWD EDGE AND 5" O/B OF LWR I/B EDGE. BOTH CRACKS ARE STOP DRILLED AND HFEC WITH NO FURTHER INDICATIONS. FABRICATED REPAIR DOUBLERS FROM 0.032" CRES 301 1/2 HARD STAINLESS STEEL. CRACK #1 DOUBLER DIMENSIONS ARE 6.7"L X 3.6"W AND CRACK #2 DOUBLER DIMENSIONS ARE 6.5"L X 3.5"W. BOTH CRACK DOUBLER REPAIR LOCATIONS WERE DRILLED AND INSTALLED REF AWAC SUPPLEMENT NO 15-200 DATE OF ISSUE 8/21/2015.

Part: SKIN — DENTED (FUSELAGE) · airframe 38,590 hrs · 37,249 cycles

DENT @ FS 656 & S20L+1.5" THAT MEASURES .650"L X .3" X .0140"D WITH A W/D 21.43 DENT IS NOT WITHIN ALLOWABLE SRM LIMITS REF CRJ 200 53-00-31 FIG 103 SHEET 104 W/D <25. "AIRCRAFT REMOVED FROM SERVICE" ASAP ENGINEERING EA AWAC-CRJ253-01467 REV IR DTD 3/9/2020 WITH A MINOR REPAIR CLASSIFICATION AND PERMANENT REPAIR STATUS, WITH NO UNDERLYING DAMAGE, AND HFEC NDT OR LDI TO THE SKIN AND UNDERLYING STRUCTURE TO ENSURE NO CRACKS EXIST. AWAC SUPPLEMENT NO: 20-049 ISSUE 3/10/2020 WAS CREATED FROM ASAP EA AWAC-CRJ253-01467 REV IR DTD 3/9/2020

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 38,590 hrs · 37,249 cycles

CRACK INDICATION L/H AFT PRESSURE BULKHEAD APPROX LBL 27.5 BELOW WL 138.8. "AIRCRAFT REMOVED FROM SERVICE" MAPPED AFT PRESSURE BULKHEAD WITH A TOTAL OF 10 INDICATIONS FOUND MEASURING AT THE FOLLOWING LOCATIONS: 1. WL 109.5-110.5 & RBL 27.5 L=1.0" 2. WL 106-106.5 & RBL 27.5 L=.5" 3. WL 92.9-93.5 & RBL 27.5 L=.6" 4. WL 128.5-134.5 & RBL 18.00 L=6.0" 5. WL 126.5-134.5 & BL 0.0 L=8.0" 6. WL 108.5-115 & BL 0.0 L=6.5" 7. WL 109-111.5 & LBL 18.0 L=2.5" 8. WL 96.5-100.5 & LBL 18.0 L=4.0" 9. WL 131.4-133 & LBL 27.5 L=2.6" 10. WL 94.2-101.2 & LBL 27.5 L=7.0" OLYMPUS/NORTEC 600D S/N 60007150515 CAL DUE 03 SEP 2020 PROBE EC/NDT PAB90602FX (50-500KZ) STANDARD ECRS-0824/AZ2024T3 S/N 1214003 MODIFICATION TO FS 621.00 PRESSURE BULKHEAD WEB REF AWAC EO # E17/003/453 REV B DTD JULY 3, 2019, AND BOMBARDIER REO 601R-53-61=1240 REV D DTD 10-31-2016 TO BE ACCOMPLISHED ON CARD NO 4EOAWA21045.

Part: CONTROL CABLE — FRAYED (VERTICAL STAB) · airframe 38,590 hrs · 37,249 cycles

L/H VERTICAL STABILIZER AUTO PILOT HAS RUST AND & FRAYED CABLE. "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED FRAYED CABLES P/N 601R90020-131 & 601R90020-79, ELEVATOR SERVO MOTOR P/N 622-5027-101, AND CLUTCH ASSY 822-0260-001. OPS CHECKS OK AT THIS TIME REF CRJ 200 AMM 22-11-24 REV 60.

Part: DOOR — DELAMINATED (NLG) · airframe 38,590 hrs · 37,249 cycles

R/H NLG DOOR LWR FWD CORNER HAS DELAMINATION THAT MEASURES .669"L X .299"W X .210"D. "AIRCRAFT REMOVED FROM SERVICE" TRIMMED OUT DELAMINATED AREA AND PERFORMED PERMANENT REPAIR REF ASAP EA # AWAC-CRJ252-01466 REV. A DTD 3/3/2020 AND AIR WISCONSIN SUPPLEMENT NO 20-046.

Part: A/C PACK — MALFUNCTIONED (RIGHT) · airframe 38,517 hrs · 37,178 cycles

EN ROUTE FROM ATW TO DEN OVER NEBRASKA WITH THE LH PACK ON MEL RECEIVED RH PACK OVERPRESSURE MULTIPLE TIMES. FLIGHT DECLARED AN EMERGENCY, DESCENDED TO 10,000 FT AND CONTINUED TO DEN. AIRCRAFT REMOVED FROM SERVICE CW OPS CHECK OF RH PACK IAW AMM 21-51-00. OPS CHECK GOOD .

Part: CONTACTOR — DAMAGED (AC BUSS) · airframe 38,115 hrs · 36,801 cycles

AC SERVICE BUSS CAUTION. RELAY K4XA WAS FOUND OVERHEATED AND ELECTRICALLY CHARRED. RELAY IS LOCATED UNDER THE COCKPIT FLOOR ON THE RH RELAY TRAY. THIS WAS REPORTED TO ME BY AVIONICS TECH DURING MAINTENANCE. AIRCRAFT REMOVED FROM SERVICE FOUND RING TERMINALS LOOSE ON CONTACTOR K4XA NAD BLACK SOOT SURROUNDING SAME CONTACTOR REPLACED K4XA AND CHECKED AC SERVICE BUS DC SERIVCE BUS AND SERVICE TRU ALL GOOD S/N OFF CM-44617 S/N ON CU-04076 JLC

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 37,609 hrs · 36,345 cycles

ON DEPARTURE THE FLIGHT CREW EXPERIENCED A LT PACK HIGH PRESSURE CAUTION MESSAGE WITH RT PACK ALREADY ON MEL. THEY ACCOMPLISHED THE QRH, COMMUNICATED WITH DISPATCH, ADVISED ATC OF THE PROBLEM, REQUESTED DELAY VECTORS TO BURN OFF FUEL AND DECLARED AN EMERGENCY. THE CREW ADVISED THE FLIGHT ATTENDANT AND PASSENGERS OF THE SITUATION. THE FLIGHT RETURNED TO KHPN FOR A NORMAL APPROACH, LANDING, AND TAXI. NO ADVERSE PASSENGER REACTION TO THE EVENT WAS OBSERVED BY CREW MEMBERS DURING DEPLANING. AFTER TRANSFERING BLEED PER APPX B MEL HANDBOOK, UPON COMPLETING AND INCREASING POWER RECEIVED LT PACK OVER PRESS CAUTION MSG. C/W QRH MSG REMAINED, CONTINUE FROM 317082/4 A/C LANDED UNEVENTFULLY AT NORMAL LANDING WT OVER PRESS CONDICTION OCCURED AT APPROX 70%-76% N1.

Part: DOOR SILL — CORRODED (BS 349) · corrosion level 2 · airframe 35,018 hrs · 33,877 cycles

FWD SERVICE DOOR AFT LOWER SILL CORRODED AT FS 349.00, RBL36. REPAIRED FLOOR SILL AT FS 349.00, RBL36 AFT OF SERVICE DOOR LOWER SILL IAW AWAC EA# AWAC-CRJ253-00925 REV-IR.

Part: SKIN — CRACKED (BS 169-202) · airframe 35,018 hrs · 33,877 cycles

LEFT LOWER NOSE HYDRAULIC COMPARTMENT SKIN PANEL CRACKED AT AFT LATCH CUT-OUT.

Part: SKIN — CRACKED (RT WING) · airframe 35,018 hrs · 33,877 cycles

RIGHT WING DRAIN HOLE AT WS 85.50 CRACKED.

Part: FRAME — CRACKED (BS 605) · airframe 35,018 hrs · 33,877 cycles

FRAME BS 605 IS CRACKED IN 2 SPOTS ON THE FWD SIDE JUST ABOVE AND BELOW STRINGER 9L. REPAIRED THE FRAME.

Part: SKIN — CHAFED (RT WING AILERON) · airframe 35,018 hrs · 33,877 cycles

RIGHT WING AILERON IS CHAFING ON LEADING EDGE LOWER SKIN BETWEEN INBD HINGE AND INBD PCU LINK.

Part: BRACKET — CRACKED (RT MLG) · airframe 35,018 hrs · 33,877 cycles

RIGHT MLG PRESSURE TRANSDUCER BRACKET IS CRACKED. REPLACED THE BRACKET IAW SRM 51-42-06, 51-40-11, AND 51-25-16.

Part: FITTING — CRACKED (BS 461) · airframe 35,018 hrs · 33,877 cycles

BATHTUB FITTING CRACKED AT BS 461.00 OTBD SIDE OF LBL 9. REPLACED THE FITTING IAW SRM 51-40-11, 51-42-06, AND 51-42-21.

Part: ANGLE — CRACKED (BS 625) · airframe 35,018 hrs · 33,877 cycles

REAR PRESSURE BULKHEAD, STRINGER 14L OBLIQUE ANGLE IS CRACKED. REPLACED THE ANGLE IAW SRM 51-42-21, AND REO 601R-53-61-422.

Part: ANGLE — CRACKED (BS 625) · airframe 35,018 hrs · 33,877 cycles

REAR PRESSURE BULKHEAD, STRINGER 15L OBLIQUE ANGLE IS CRACKED. REPLACED THE OBLIQUE ANGLE IAW SRM 51-42-21, AND 51-42-06.

Part: ANGLE — CORRODED (BS 319) · corrosion level 2 · airframe 35,018 hrs · 33,877 cycles

LOWER SERVICE DOOR SILL ANGLE AT BS 319 FOUND CORRODED. REPLACED THE DOOR SILL ANGLE.

Part: ANGLE — CRACKED (PYLON) · airframe 35,018 hrs · 33,877 cycles

PANEL 412BT DIVERTER ANGLES CRACKED. REPLACED THE DIVERTER ANGLES IAW SRM 51-42-06.

Part: ANGLE — CRACKED (PYLON) · airframe 35,018 hrs · 33,877 cycles

PANEL 442BT DIVERTER ANGLES CRACKED. REPLACED THE DIVERTER ANGLES IAW SRM 51-42-06.

Part: FLOORBEAM — DAMAGED (BS 280) · airframe 35,018 hrs · 33,877 cycles

DURING REPAIR OF FS 280 FLOORBEAM, A DAMAGED LIGHTING HOLE BELOW FLOOR WAS FOUND. REPAIRED IAW ROE 601R-53-11-3243 REV --.

Part: CHANNEL — CRACKED (CRGO DOOR TRACK) · airframe 35,018 hrs · 33,877 cycles

CARGO DOOR FWD TRACK LOWER CHANNEL CRACKED. REPLACED THE CHANNEL IAW SRM 51-42-06.

Part: RETAINER — CRACKED (BS 654-672) · airframe 35,018 hrs · 33,877 cycles

PANEL 412BT SEAL RETAINER IS CRACKED.

Part: RETAINER — CRACKED (BS 654-672) · airframe 35,018 hrs · 33,877 cycles

PANEL 422DB SEAL RETAINER CRACKED.

Part: ANGLE — CRACKED (BS 280) · airframe 35,018 hrs · 33,877 cycles

ANGLE CLIP CRACKED, INBD OF RBL 9 , AFT OF FRAME BS 280. REPLACED THE ANGLE IAW REO 601R-53-11-136, REV-A.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 35,018 hrs · 33,877 cycles

FLOORBEAM ANGLE CRACKED OTBD OF LBL 9 BS 280. REPLACED THE ANGLE IAW REO 601R-53-11-136, REV A.

Part: ANGLE — CRACKED (BS 280) · airframe 35,018 hrs · 33,877 cycles

ANGLE CRACKED BS 280, INBD OF LBL 9 AFT SIDE OF BEAM. REPLACED THE ANGLE IAW REO 601R-53-11-136, REV A.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 35,018 hrs · 33,877 cycles

FLOORBEAM ANGLE BS 280 CRACKED, RBL9. REPAIRED THE FLOORBEAM ANGLE IAW REO 601R-53-11-136, REV A.

Part: ANGLE — CRACKED (BS 484) · airframe 35,018 hrs · 33,877 cycles

ANGLE CRACKED ON THE OTBD OF LBL 27, BS 484. REPLACED THE ANGLE IAW REO 601R-53-41-059, REV-B.

Part: LANDING — CRACKED (ACCESS PANEL) · airframe 35,018 hrs · 33,877 cycles

RIGHT ENGINE TAIL PIPE FAIRING PANEL 446AL HAS A DAMAGED LANDING FOR PANEL 446BL. REPLACED THE PANEL LANDING IAW CMM 20-42-06.

Part: PANEL — CRACKED (EXHAUST PIPE) · airframe 35,018 hrs · 33,877 cycles

RIGHT ENGINE, TAIL PIPE FAIRING PANEL 446AL , THIRD FLANGE FROM FWD END IS CRACKED. REPAIRED THE FLANGE IAW CMM 78-11-00-300-810-A01.

Part: WARNING MESSAGE — ILLUMINATED (DISPLAY COOLING) · airframe 34,972 hrs · 33,626 cycles

DISPLAY COOL CAUTION MESSAGE, CLIMBING THROUGH FL200. COMPLIE WITH QRH, MSG PERSISTED. SWITCHED TO FLIGHT ALTERNATE & STANDBY DURING DIVERSION IAW QRH CAUTION MESSAGE EXTINGUISHED, DESCENDING THROUGH 15,000 FT. REMOVED AND REPLACED THE DISPLAY COOL LOW FLOW DETECTOR. R & R THE DISPLAY COOLING FLEX DUCT UNDER CAPTAIN`S PLENUM. R & R AVIONICS COOLING PANEL ASSY. MX CHECK FLIGHT WAS SATISFACTORY.

Part: FAN — DAMAGED · airframe 34,791 hrs · 33,624 cycles

AT FL 300 RECEIVED DISPLAY COOL CAUTION. C/W QRH UNABLE TO CLEAR MSG. FAN SET TO STANDBY, MSG BECAME INTERMITTENT OUT OF APPROX FL 180 AND ALL THE WAY TO THE GROUND. INSPECTED COOLING FANS & DUCTS. OPENED FWD KIDNEY PANEL & INSP DUCTS & FOUND NO DEBRIS. R&R LOW FLOW SENSOR. INSPECTED AVIONICS COOLING DUCTING AND FAN ASSYS. OBSERVED FLT FAN CHECK VLV BINDING TO OPEN POSITION AND DEBRIS IN STANDBY FAN. REMOVED AND REPLACED FLT FAN AND CLEARED DEBRIS FROM STANDBY FAN.

Part: FUEL SYS — LEAKING (APU) · airframe 33,023 hrs · 31,916 cycles

FUEL LEAKING FROM DRAIN TUBES UNDER APU.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 31,423 hrs · 30,433 cycles

ON TAKEOFF AT 80 KNOTS, RECEIVED MASTER WARNING & CONFIG TRIM AURAL MSG. NOTICED AILERON TRIM FULL LT WING DOWN & RUDDER TRIM FULL NOSE RT. FLAPS INDICATE DASHES. RUDDER & AILERON TRIM WILL NOT MOVE. NO OTHER MSGS NOTED. RECEIVED FLAPS DEGRADED MSG AFTER SELECTING 0 DEGREES. FLAP POSITION AND SELECTION MATCH BUT NOT INDICATION.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 31,151 hrs · 30,177 cycles

LEFT FWD AVIONICS ACCESS PANEL 131AL, FASTENER HOLES IN SKIN HAVE 6 FREEZE PLUGS PULLING THROUGH. REPAIRED LT FWD AVIONICS PANEL HOLES IN FUSELAGE OUTER SKIN IAE REO 601R-53-11-2879, REV A DATED 2016 03 23 & REO 601R-53-11-162 REV C.

Part: RISER — CRACKED (PAX DOOR) · airframe 31,151 hrs · 30,177 cycles

PASSENGER DOOR AFT STEP RISER AT THIRD FIXED STEP IS CRACKED. REPAIRED.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,151 hrs · 30,177 cycles

FS 589.00 FLOOR STRAP RBL 27 TO RT SILL CORRODED, REPLACED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 31,151 hrs · 30,177 cycles

FS 605.00 CLIP UNDER CARGO DOOR SILL CRACKED, REPLACED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 31,151 hrs · 30,177 cycles

AFT SIDE OF FS 280 AT STRINGER 3L, INBD ANGLE CRACKED, REPLACED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,151 hrs · 30,177 cycles

RBL 27 SEAT RAIL BEAM OTBD FLANGE, FROM FS 589.00 - 621.00, CORRODED. REPAIRED.

Part: BRACKET — CRACKED · airframe 31,151 hrs · 30,177 cycles

FORWARD ATTACH BRACKET FOR LT LOWER VISOR PANEL 326BL IS CRACKED. REPLACED.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 31,151 hrs · 30,177 cycles

E & E COMPARTMENT, FWD SIDE OF FS 280 FLOORBEAM SUPPORT ANGLE AT LBL 9 CRACKED, REPLACED.

Part: SUPPORT ANGLE — CRACKED (PAX DOOR) · airframe 31,151 hrs · 30,177 cycles

PASSENGER DOOR AFT RISER SUPPORT ANGLE BY ASSIST MOTOR IS CRACKED, REPAIRED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 31,151 hrs · 30,177 cycles

AFT ACCESSORY COMPARTMENT FS 621 BULKHEAD AFT SIDE, RT INTERCOSTAL OBLIQUE ANGLE TO STRINGER 14R CRACKED, REPAIRED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,151 hrs · 30,177 cycles

LBL 27 SEAT RAIL BEAM INBD & OTBD FLANGES HAVE CORRODED FASTENERS HOLES, FS 559+112 - 621, 7 PLACES MARKED.

Part: POST — CRACKED (FUSELAGE) · airframe 31,151 hrs · 30,177 cycles

FS 409.00+128 VERTICAL POST, LBL 27, INBD FLANGE IS CRACKED, REPAIRED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,151 hrs · 30,177 cycles

LBL 9 SEAT RAIL BEAM, OTBD FLANGE, BETWEEN FS 605.00 & 621.00 HAS 2 CORRODED FASTENER HOLES, REPAIRED.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,151 hrs · 30,177 cycles

DRAIN MAST REINFORCEMENT CHANNEL HAS CORROSION, JUST OTBD OF STRINGER 25R, BETWEEN FRAME 349.00 & 333.00, IN THE FWD E & E BAY. REPLACED DRAIN MAST REINFORCEMENT CHANNEL IAW SRM 51-21-06, 51-24-21,51-40-11 & 51-42-06.

Part: FITTING — CRACKED (COCKPIT) · airframe 31,151 hrs · 30,177 cycles

FLIGHT DECK LT LOWER FITTING ON CENTER WINDSHIELD POST CRACKED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 31,151 hrs · 30,177 cycles

FLOOR SUPPORT STRUCTURE OTBD AT FS 484, RBL 27 IS CRACKED. R & R RT FLOOR SUPPORT CLIP AT FS 484, RBL 27 IAW REO 601R-53-41-059.

Part: ATTACH ANGLE — CRACKED (COCKPIT) · airframe 31,151 hrs · 30,177 cycles

RIGHT WINDSHIELD SIDE POST SUPPORT, OTBD LOWER ATTACH ANGLE CRACKED. R & R RT WINDSHIELD SIDE POST SUPPORT, OTBD LOWER ATTACH ANGLE IAW SRM 51-42-21.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 31,030 hrs · 30,062 cycles

SMOKE TOILET CAUTION MSG DURING DESCENT. COMPLIED WITH QRH & PULLED CB`S 2C5, 2D14, 2D15, 2S2 & 2U2. MSG CLEARED ON SHORT FINAL, NO INDICATIONS OF FIRE. INSPECTED LAVATORY FOR EVIDENCE OF SMOKE & FIRE, NO EVIDENCE FOUND. R & R LAVATORY SMOKE DETECTOR IAW AMM 26-16-01. OPERATIONS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 30,264 hrs · 29,338 cycles

WOW INPUT, CAUTION MSG MOMENTARILY CAME ON AFTER GEAR RETRACTION ON TAKEOFF. CAME ON AGAIN AFTER GEAR EXTENSION ON APPROACH. AFTER NOSE WHEEL TOUCH DOWN, WOW INPUT CAUTION CAME ON STEADY, BELOW 80 KTS, STEERING INOPERATIVE CAUTION & WOW OUTPUT FAIL STATUS MSG. UNABLE TO ENGAGE NWS. COMPLIED WITH QRH, NWS STILL INOPERATIVE. ACFT WAS TOWED TO PARKING.

Part: BUSS BAR — DAMAGED (ELECTRICAL) · airframe 28,255 hrs · 27,407 cycles

AC ESS BUSS MESSAGE DISPLAYED INTERMITTENTLY. REPLACED AC ESS CIRCUIT BREAKER C2 & BUSS BAR A2B2C2 & B2. OPS CHECKED GOOD IAW AMM 24-51-00.

Part: BALLAST — MALFUNCTIONED (CABIN) · airframe 26,261 hrs · 25,526 cycles

ON A REPO FLIGHT, NO SMOKE OR FLAMES WERE SEEN, NO ODOR WAS DETECTED. THERE WAS NO FLIGHT ATTENDANT AVAILABLE TO GO CHECK THE LAVATORY, SO AN EMERGENCY WAS DECLARED. ON APPROACH AT 5000' RECEIVED SMOKE TOILET MASTER CAUTION, IAW QRH DECLARED EMERGENCY. MSG EXTINGUISHED, LANDED WITHOUT INCIDENT. AFTER THE INSPECTION, FOUND BALLAST B129 ABOVE ROW 11 BURNED OUT. R &R CEILING LIGHT BALLAST IAW AMM 33-20. OPERATIONS CHECKED GOOD.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 26,242 hrs · 25,514 cycles

AIRCRAFT GRD POWER PLUG MOUNT STRUCTURE CRACKED AT SCREW HOLE. REMOVED SERVICEABLE BRACKET & INSTALLED NEW SERVICEABLE PN 600-33283-33 IAW CRJ 200 SRM 51-42-21 & SRM 51-42-13.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 26,242 hrs · 25,514 cycles

COMPLIED WITH AWCA CARD 4DMI14642 INSP FS 621 INTERCOSTAL CRACK 601R-53-61-105A. REMOVED CRACKED INTERCOSTAL AT FS 621 - 625 AT STRINGER 13L IAW BA 601R-53-048REV C, CRJ200 SRM 51-42-21, 51-25-16.

Part: SEAT TRACK — CHAFED (FUSELAGE) · airframe 26,242 hrs · 25,514 cycles

LEFT SIDE SEAT TRACK IS CHAFED AT FS 551.00. R & R LT SIDE SEAT TRACK & INSTALLED NEW SERVICEABLE SEAT TRACK IAW BA REO 601R-53-00-0485, CRJ200 SRM 51-42-02, 53-41-49, 53-21-49, 51-25-06, 51-25-16, 51-40-11 & 51-21-11.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 26,242 hrs · 25,514 cycles

LEFT 131AL CUTOUT HAS 1 LOOSE & 1 MIGRATED FREEZE PLUG. REPAIRED TWO EACH FASTENER HOLES ON LT FWD FUSELAGE SKIN AT PANEL 131AL CUTOUT IAW AWAC SUPPLEMENT 14-039.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 26,242 hrs · 25,514 cycles

LEFT SIDE SEAT RAIL IS WORN AT FS 492.0. REMOVED WORN LT SEAT RAIL & INSTALLED SERVICEABLE SEAT RAIL IAW BA REO 601R-53-00-485,CRJ200 SRM 51-42-02, 53-41-49, 53-21-49, 51-25-06 & 51-25-16.

Part: PANEL — CRACKED (VERTICAL STAB) · airframe 26,242 hrs · 25,514 cycles

VISOR PANEL 326AL IS CRACKED. REPLACED WITH NEW SERVICEABLE PART.

Part: NOSE COWL — CHAFED (RT ENGINE) · airframe 26,242 hrs · 25,515 cycles

RIGHT UPPER NOSE COWL TE GOUGED & CHAFED. REMOVED UNSERVICEABLE TE & INSTALLED NEW SERVICEABLE TE IAW BA CMM 71-14-01.

Part: NOSE COWL — CHAFED (LT ENGINE) · airframe 26,242 hrs · 25,514 cycles

LEFT UPPER NOSE COWL CHAFED ENTIRE LENGTH TE. REMOVED UNSERVICEABLE TE & INSTALLED NEW SERVICEABLE TE IAW BA CMM 71-14-01.

Part: TRUNNION — DAMAGED (RT MLG) · airframe 26,242 hrs · 25,514 cycles

DURING COLD WORKING OF THE RT MLG TRUNNION LOWER FLANGE, FOUND 3 OVERSIZE HOLES. REPAIRED HOLES IAW REO 601R-57-21-2129

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 26,242 hrs · 25,514 cycles

LEFT INBD FLAP VANE IS CHAFFED AT INBD END. REMOVED CHAFFED LE SKIN & INSTALLED NEW SERVICEABLE SKIN IAW REO 601R-57-52-004 & SRM 51-42-13.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 26,242 hrs · 25,514 cycles

AIRCRAFT GND POWER PLUG MOUNT STRUCTURE CRACKED. REMOVED CRACKED BRACKET & INSTALLED NEW SERVICEABLE BRACKET IAW SRM 51-42-21 & 51-42-13.

Part: INTERCOSTAL — CRACKED (APU BAY) · airframe 26,242 hrs · 25,514 cycles

COMPLIED WITH CARD NR 0001 DIL 270864 122 REPAIR APU INLET DOOR STRUCTURE. R & R APU INLET DOOR STRUCTURE INTERCOSTAL IAW SRM 51-42-06 & 51-40-11.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,242 hrs · 25,514 cycles

CARGO BAY FWD DOOR TRACK LOWER CLIP CRACKED. R & R WITH NEW SERVICEABLE CLIP IAW SRM 51-42-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,242 hrs · 25,514 cycles

RIGHT SEAT TRACK FS 374 TO 409+128 HAS CORROSION. R & R SEAT TRACK RBL FS 409+128 IAW SRM 53-01-11.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,242 hrs · 25,514 cycles

CLIP CRACKED AT FS 484 & RBL 36. REMOVED CRACKED CLIP ,THEN FABRICATED SERVICEABLE CLIP & INSTALLED IAW REO 601R-53-41-059 REV B.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 26,242 hrs · 25,514 cycles

RIGHT OBLIQUE ANGLE CRACKED IN AEB. REMOVED CRACKED RT OBLIQUE ANGLE, THEN FABRICATED SERVICEABLE ANGLE & INSTALLED IAW 51-21-11, 53-61-17 & 51-21-11.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 26,242 hrs · 25,514 cycles

PASSENGER DOOR PRESS VENT AFT DRAG ANGLE CRACKED. REMOVED UNSERVICEABLE DRAG ANGLE & FABRICATED SERVICEABLE ANGLE IAW SRM 51-40-11, 51-24-21, 52-10-14 & 51-21-11.

Part: TIE DOWN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,242 hrs · 25,514 cycles

THREE EACH TIE DOWN ON LBL 27 FS 574 THROUGH 559+80 HAVE CORROSION. R & R THREE EACH TIE DOWNS ON LBL 27 FS 574 THROUGH 559+80 IAW CRJ 200 SRM 51-41-02 & 53-61-49.

Part: RETAINER — CORRODED (E&E DOOR) · corrosion level 2 · airframe 26,242 hrs · 25,514 cycles

AVIONICS DOOR SEAL RETAINERS AT RT FWD & AFT IS CORRODED. REMOVED FOUR EACH SEAL RETAINERS & INSTALLED FOUR EACH NEW SERVICEABLE RETAINERS IAW SRM 51-42-06 & 51-42-13.

Part: FITTING — CRACKED (LEFT) · airframe 26,242 hrs · 25,514 cycles

LEFT JET PIPE LOWER MOUNT FITTING OTBD SUPPORT RIB CRACKED. REMOVED CRACKED FITTING & INSTALLED NEW FITTING IAW CMM20-42-06,20-42-21.

Part: MOUNT BRACKET — CRACKED (HYDRAULIC BAY) · airframe 26,242 hrs · 25,514 cycles

FORWARD MOUNT BRACKET CRACKED FOR HYD NR 3 ACCUMULATOR. REMOVED CRACKED BRACKET & INSTALLED NEW SERVICEABLE BRACKET IAW SRM51-40-11 & 51-42-06.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,642 hrs · 25,514 cycles

LEFT BUTT LINE 280 & RBL 9 OTBD CLIPS CRACKED. REMOVED CRACKED CLIPS & REPLACED WITH SERVICEABLE CLIPS IAW SRM 51-42-21, 51-25-06, 51-25-16 & 51-21-11.

Part: TIE DOWN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,242 hrs · 25,514 cycles

THREE EACH TIE DOWNS ON LBL 27, FS 574 TO 559+80 HAVE CORROSION. R & R TIE DOWNS ON LBL 27, FS 574 TO 559+80 IAW 51-41-02,53-61-49.

Part: RETAINING CLIP — CRACKED (FUSELAGE) · airframe 26,242 hrs · 25,514 cycles

LEFT & RT 280 BULKHEAD LOWER INBD RETAINING CLIP CRACKED. REMOVED CRACKED CLIP & INSTALLED NEW SERVICEABLE CLIP IAW SRM 51-42-21, 51-40-11, 51-21-11, 51-25-06 & 51-25-16.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,242 hrs · 25,514 cycles

CLIP AT FS 280 AFT SIDE AT STRINGER 3L CRACKED. REMOVED CRACKED CLIP & INSTALLED NEW SERVICEABLE CLIP AT FS 280 AT STRINGER L3 IAW SRM 51-40-11, 51-25-06-, 501-25-16 & 51-21-11.

Part: TIE DOWN — CORRODED (CARGO BAY) · corrosion level 2 · airframe 26,242 hrs · 25,214 cycles

FIVE EACH CARGO TIE DOWNS ON LBL 9, FS 621 TO 559+80 CORRODED. REMOVED TWO EACH TIE DOWNS & REPLACED WITH NEW SERVICEABLE PART, THEN BLENDED THREE EACH TIE DOWNS IAW SRM 51-41-02,53-61-49.

Part: MOUNT BRACKET — CRACKED (PAX DOOR) · airframe 26,242 hrs · 25,514 cycles

PASSENGER DOOR ASSIST MOTOR LOWER MOUNT BRACKET CRACKED. R & R WITH SERVICEABLE PN 601R3117745-7 IAW CRJ200 SRM 51-40-11 & 51-42-06.

Part: TIE DOWN — CORRODED (CARGO BAY) · corrosion level 2 · airframe 26,242 hrs · 25,514 cycles

TWO EACH CARGO TIE DOWNS AT RBL 9 FS 574 TO 559+80 HAVE CORROSION. R & R CARGO TIE DOWN PLATES TWO EACH & NEW SEAT TRACK IAW SRM 53-11-49, 51-40-11 & 53-01-11.

Part: APU — FIRE · airframe 26,118 hrs · 25,405 cycles

GROUND CREW REPORTED FLAMES FROM APU EXHAUST. OPS CHECKED APU IAW AMM 49-10-00. OPS CHECKED GOOD.

Part: PSEU — FAILED (LANDING GEAR) · airframe 24,316 hrs · 23,641 cycles

AT ROTATION, DURING T/O, RECEIVED WOW INPUT CAUTION FOLLOWED BY WOW OUTPUT CAUTION + WOW OUTPUT FAIL STATUS + PROX SYS FAULT STATUS MSG'S. UPON LANDING RECEIVED NUMEROUS OTHER CAUTION + STATUS FAULT MSG'S. QRH C/W AND NWS INOP CAUTION MSG. INSPECTED MLG AND DOOR HARNESSES FOUND PSEU FAILED "NO COM". REMOVED AND REPLACED PSEU PER AMM 32-62-01 OPS CHECK GOOD. MC SEE LP 242378/4 ALSO REPLACED CARGO DOOR HARNESS AS A PRECAUTIONARY MEASURE.

Part: LIGHT — ODOR (LAVATORY) · airframe 23,019 hrs · 22,391 cycles

DEFECT DESCRIPTION - LAV LIGHT INOP, BURNING SMELL NOTED IN LAV NEAR LIGHT. REMOVED AND REPLACED THE LAV LIGHT ASSEMBLY IAW CRJ AMM 33-25-07 OPS CHECK GOOD. NOTE: THE WHOLE ASSEMBLY WAS CHANGED DUE TO HARDWARE ISSUES - THE SMELL WAS THE BALLAST.

Part: WIRE — SHORTED (MLG) · airframe 22,064 hrs · 21,440 cycles

CLIMBING OUT OF DEPARTURE AT 9000 FT, INTERMITTENT GEAR DISAGREE WARNING. SHOWED NLG RED. COMPLIED WITH QRH, PROBLEM STOPPED. RETURN TO DEPARTURE WT AT 46400 LBS. C/W M ACTION FOR MEL 32-30-01 NOTE, GEAR PIN FLAGS STOWED IN PILOTS WARDROBE. INTEROGATED PSEU, FOUND S35 SHORT. FRE LB 215918, BLK 3 & 4.

Part: PROXIMITY SENSOR — OUT OF ADJUST (NLG) · airframe 21,997 hrs · 21,374 cycles

GEAR DISAGREE WARNING MESSAGE CLIMBING THRU 10,000 FT. NOSE GEAR SHOWED AMBER THEN RED HASH MARKS AFTER 1 MINUTE. WHITE NOSE GEAR UP MSG RETURNED. COMPLIED WITH QRH, AIR RETURN TO DEPARTURE. ADJUSTED BOTH NLG DOWNLOCK PROXIMITY SENSORS CLEARANCE IAW AMM 32-61-05, OPS CK GOOD.

Part: THRESHOLD — CORRODED (SERVICE DOOR) · airframe 21,580 hrs · 20,948 cycles

SERVICE DOOR THRESHOLD CORRODED OUT OF LIMITS. R & R THRESHOLD IAW SRM 51-40-11, 51-42-06.

Part: FLOOR SUPPORT — CORRODED (FS 574-621) · airframe 21,580 hrs · 20,948 cycles

LEFT FLOOR SUPPORT FS 574 TO 621 HAS CORRODED ON UPPER AND LOWER SURFACES. R & R LT FLOOR SUPPORT IAW SRM 51-42-06.

Part: FLOOR SUPPORT — CORRODED (FS 570-615) · corrosion level 2 · airframe 21,580 hrs · 20,948 cycles

CARGO FLOOR SUPPORT LBL 27, FS 570 TO 615 CORRODED. R & R FLOOR SUPPORT IAW SRM 51-40-11, 51-42-21, 51-42-22.

Part: SILL — CORRODED (FUSELAGE) · airframe 21,580 hrs · 20,948 cycles

SERVICE DOOR CUTOUT LOWER SILL IS CORRODED ALONG THE ENTIRE LENGTH OF SILL. REMOVED CORRODED SILL AND INSTALLED NEW SERVICEABLE LOWER SILL IAW SRM 51-42-21.

Part: SILL — CORRODED (FUSELAGE) · airframe 21,580 hrs · 20,948 cycles

PAX DOOR CUT OUT LOWER SILL IS CORRODED ALONG THE ENTIRE LENGTH OF THE SILL. R & R SILL IAW SRM 51-40-00, 51-41-06, 51-40-11, 51-21-06.

Part: CARGO TRACK — CORRODED (FS 614-619) · airframe 21,580 hrs · 20,948 cycles

CARGO TIE DOWN TRACK CORRODED LBL9, FS 614.00 TO 619.00. R & R TIE DOWN CARGO TRACK IAW AMM 53-01-11.

Part: CARGO TRACK — CORRODED (FS 569) · airframe 21,580 hrs · 20,948 cycles

CARGO TIE DOWN TRACK CORRODED LBL9, FS 560.00 TO F69.00. R & R CARGO TRACK IAW AMM 53-01-11, PN 601R38779-5.

Part: FLOOR SUPPORT — CRACKED (FS 589) · airframe 21,580 hrs · 20,948 cycles

LT FLOOR SUPPORT ANGLE UNDER CARGO DOOR STOP AT FS 589 IS CRACKED. R & R IAW SRM 51-42-21, 51-61-43.

Part: ANGLE — CRACKED (FS 625) · airframe 21,580 hrs · 20,948 cycles

LT OBLIQUE ANGLE AT FS 625 CRACKED. REMOVED CRACKED LT OBLIQUE ANGLE AT FS 625, DISCARD, LOCATED, & INSTALLED NEW ANGLE PN 601-35012-51 IAW SRM 51-40-11, 51-42-21.

Part: ATTACH ANGLE — CRACKED (FS 484) · airframe 21,580 hrs · 20,948 cycles

ATTACH ANGLE CRACKED OTBD SIDE LBL 36, . R & R IAW REO 601R-53-41-059.

Part: ATTACH ANGLE — CRACKED (FS 484) · airframe 21,580 hrs · 20,948 cycles

LEFT ATTACH ANGLE CRACKED AT FS 484, LBL27. R & R ATTACH ANGLE IAW REO 601R-53-41-059, REV B.

Part: CARGO TRACK — CORRODED (FS 560-569) · airframe 21,580 hrs · 20,948 cycles

CARGO TRACK RBL 9 FS 560-569 CORRODED. R & R CARGO TRACK IAW AMM 53-01-11.

Part: ATTACH ANGLE — CRACKED (FS 484) · airframe 21,580 hrs · 20,948 cycles

ATTACH ANGLE CRACKED INBD SIDE RT RBL 27. R & R DAMAGED ATTACH ANGLE IAW REO 601R-53-41-059, REV.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 21,580 hrs · 20,948 cycles

LEFT INBD FLAP VANE CHAFED ON UPPER INBD T/E. REPAIR LT INBD FLAP VANE ON UPPER INBD T/E IAW SRM 51-12-00 AND SRM 57-52-00.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 20,148 hrs · 19,423 cycles

"FLAP FAIL" WHEN FLAPS REACHED 20 DEGREES ON APPROACH RESET IAW AWAC SUPPLEMENT, PLACED ON MEL. INTERROGATED FWD FECU FAULTED SEVERAL TIMES CW FIM PROCEDURE FOR FECU LU BPSU AND LT BPSU WING NO DISCREPANCIES NOTED FOR LT PBSU R & R FECU IAW 27-51-05. OPS CK GOOD.

Part: BRACKET — CRACKED (CARGO DOOR) · airframe 19,594 hrs · 18,810 cycles

CARGO BAY DOOR LOWER TRACK OTBD BRACKET TOWARD BOTTOM OF DOOR HAS CRACK AT LOWER ROW OF RIVETS. REMOVED CRACKED BRACKET AT CARGO BAY DOOR LOWER TRACK OTBD END, AND INSTALLED NEW BRACKET IAW SRM 51-41-00 AND 51-42-06.

Part: FIRE BOTTLE — LOW PRESSURE (CARGO BAY) · airframe 17,871 hrs · 17,023 cycles

CARGO BOTTLE LO MSG IN FLT. C/W QRH- DIVERTED. LANDED AT 37500 WEIGHT. CFR REPORTS NO FIRE/SMOKE- PLACARD AND PLACED ON MEL. R & R LT FIRE BOTTLE IAW AMM 26-25-01. OPS CK GOOD REMOVED PLACARD. REMOVED FROM MEL.

Part: PROXIMITY SWITCH — SHORTED (MLG) · airframe 17,381 hrs · 16,481 cycles

SHORTLY AFTER TAKEOFF, RECEIVED "GEAR UP DISAGREE" WITH NOSE ICON AMBER, IT WENT OUT AND THEN REAPPEARED WITHIN A COUPLE OF MINUTES, THIS TIME RED. QRH AND LANDED WITH NORMAL INDICATIONS. INSTALLED NLG AND MLG DOWNLOCK PINS AND PLACED ON MEL REF 213702/2 FOR MEL. INTERROGATED PSEU. FOUND S21 SHORTED. R & R NR 1 NLG DOWNLOCK PROX SWITCH HARNESS. REF AMM32-61-05. OPS CHECK GOOD. REMOVED PLACARD, REMOVED MEL.

Part: RUDDER — MALFUNCTIONED (RUDDER SYSTEM) · airframe 17,072 hrs · 16,125 cycles

AT T/O, 20 KNOTS RECEIVED HARD RT RUDDER DEFLECTION RESPONDED WITH FULL RT RUDDER PEDAL INPUT WITH LITTLE RESPONSE. ABORTED T/O BTMS READ 3-3-3-4. ALSO RECEIVED CONFIG SPOILER MSG. FDR DOWNLOADED AND ANALYZED IAW AMM 31-30. NO ABNORMALITIES NOTED. PERFORMED TAXI TEST AND NOSE WHEEL STEERING TEST IAW 32-50-00. UNABLE TO DUPLICATE FAULT. FLIGHT SPOILER FAULT MSG WAS NORMAL OPERATION.

Part: VANE — CRACKED (RT ENGINE) · airframe 16,755 hrs · 15,794 cycles

CRACK ON RT ENG UPPER CASCADE. REPAIR IAW AW-78-30-0711-04.

Part: STRUCTURE — CHAFED (LT WING TE FLAP) · airframe 16,755 hrs · 15,794 cycles

LT WING T/E INBD SIDE OF OTBD FLAP HAS CHAFING DAMAGE. REO 601R-57-51-447.

Part: RIB — CRACKED (LT WING) · airframe 16,755 hrs · 15,794 cycles

RIB AT W/S 350 IN LT OTBD L/E CRACKED. R & R RIB IAW SRM.

Part: SEAL — CRACKED (LT WING SPOILER) · airframe 16,755 hrs · 15,794 cycles

LT WING FLIGHT SPOILER, METAL SEAL BETWEEN CTR HINGES ON WING IS CRACKED. R & R UNSERVICEABLE SEAL IAW SRM 51-42-06 & 51-42-21.

Part: STIFFENER — CHAFED (BS 621) · airframe 16,755 hrs · 15,794 cycles

REAR PRESSURE BULKHEAD VERTICAL STIFFENER AT BL0.0 CHAFED ON UPPER END FROM 10TH STAGE BLEED AIR ISOLATION VALVE. REPAIRED IAW REO 601R-53-61-1523.

Part: SUPPORT ANGLE — CRACKED (BS 280) · airframe 16,755 hrs · 15,794 cycles

WEB SUPPORT ANGLE UNDER FS280 IS CRACKED ON FWD SIDE OF BULKHEAD. REO REPAIR.

Part: BRACKET — CRACKED (BS 718) · airframe 16,755 hrs · 15,794 cycles

NR 1 PRESS/RETURN FILTER MOUNT BRACKET IN AEB CRACKED (AFT RADIUS). REO REPAIR 601R-53-62-031.

Part: INTERCOSTAL — CRACKED (BS 621) · airframe 16,755 hrs · 15,794 cycles

INTERCOSTAL CRACKED ON AFT SIDE OF REAR PRESSURE BULKHEAD. REPAIR IAW REO 601R-53-61-105, DISPOSITION FOR FS 621 BULKHEAD INTERCOSTAL CRACKS WHICH REFERS TO SB 601R-53-048 DATED AUGUST 25, 2000, PARA 2.B(B).2.A.

Part: ANGLE — CRACKED (BS 625) · airframe 16,755 hrs · 15,794 cycles

LT OBLIQUE ANGLE CRACKED IN AEB. REPLACED IAW SRM 51-40-11, 51-25-16, 51-42-21.

Part: ANGLE — CRACKED (BS 625) · airframe 16,755 hrs · 15,794 cycles

RT OBLIQUE ANGLE CRACKED IN AEB REPAIR IAW SRM.

Part: BRACKET — CRACKED (VERTICAL STAB) · airframe 16,755 hrs · 15,794 cycles

LT LOWER VISOR ATTACH BRACKET IS CRACKED. R & R UNSERVICEABLE BRACKET ON LT LOWER VISOR ATTACH.

Part: SKIN — CRACKED (PAX DOOR) · airframe 16,755 hrs · 15,794 cycles

CRACK ON PAX DOOR FWD SKIN UNDER STEP 832AT. REPAIR IAW REO 601R-52-11-1779.

Part: RIB — CRACKED (LT WING) · airframe 16,755 hrs · 15,794 cycles

BATT RIB CRACKED (LT) REPAIR IAW REO. REPAIRED IAW REO 601R-57-51-046.

Part: SKIN — CRACKED (PAX DOOR) · airframe 16,755 hrs · 15,794 cycles

CRACK ON PAX DOOR FWD SKIN UNDER STEP 832CT. REPAIRED IAW REO 601R-52-11-702.

Part: RIB — CRACKED (RT WING) · airframe 16,755 hrs · 15,794 cycles

BATT RIB CRACKED. REPAIRED IAW REO 601R-57-51-046 DEVIATION DATED 2010-03-01.

Part: PRESSURE BLKHD — CRACKED (BS 202.75) · airframe 16,603 hrs · 15,632 cycles

EVAL AND REPAIR 202 BULKHEAD CRACK REPAIRED CRACK IN FS 202.75 BULKHEAD IAW REO 601R-53-11-1827.

Part: LIGHT — SMOKE (COCKPIT) · airframe 15,306 hrs · 14,358 cycles

CAPTS YOKE MAP LIGHT SMOKING, PULLED C/B U6 ON CBP2 AND SMOKE STOPPED. REMOVED AND REPLACED CAPTAINS LAMPLIGHT ASSY IAW AMM33-13-00. (K)

Part: APU — FIRE (APU BAY) · airframe 14,587 hrs · 13,666 cycles

DURING ACCEPTANCE CHECK WITH APU RUNNING, HEARD LOUD BANG FROM REAR OF ACFT. ON WALKAROUND, F/O NOTICED FIRE COMING FROM APU COMPARTMENT. APU FIRE PUSH LIGHTS SELECTED AND FIRE EXTINGUISHED. NO APU FIRE LIGHTS ILLUMINATED. C/W IMMEDIATE ACTION CHECKLIST. REMOVED AND REPLACED APU AND APU GENERATOR IAW AMM, OPS CHECK GOOD, REMOVED FROM MEL. (K)

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 12,530 hrs · 11,686 cycles

GEN NR 1 CAS MESSAGE AROUND 18,000 FT ON CLIMBOUT. COMPLIED WITH QRH AND STARTED APU. APU OIL CAS MASSAGE AT FL 29.0. APU OIL CHECK AND TEST COMPLIED WITH. C/W FIM 49-60-00 AND AMM 49-10-00 OPS TEST OF APU CHECKS NORMAL. VERIFIED NO ECU FAULT. CODES AND OIL SERVICE FOUND FULL APU OPS NORMAL.

Part: A/C PACK — OVERHEATED (NR 2) · airframe 12,104 hrs · 11,278 cycles

PACK NR 2 OVERHEATED ON GROUND CAUSING SMOKE IN THE CABIN. UNCONTROLLABLE IN AUTO OR MANUAL. (M)

Part: PANEL — UNKNOWN (AIRSTAIR)

REPAIR PAX DOOR AFT STAIR SIDE PANEL. REPLACED SIDE PANEL IAW SRM 51-42-06, 51-42-21 AND 51-23-00. (M)

Part: HOUSING — GOUGED (CARGO DOOR) · airframe 12,093 hrs · 11,266 cycles

GOUGE ON CARGO DOOR HANDLE HOUSING OF .300 LONG BY .140 WIDE AND .100 DEEP. REPLACED WITH NEW PART IAW SRM 51-42-21. (M)

Part: FLOORBEAM — CRACKED (BS 280) · airframe 12,093 hrs · 11,266 cycles

BULKHEAD WEB FLOORBEAM CRACK AT FS 280 RBL 9.0. REPAIR PERFORMED IAW REO 601R53-11-171 REV D SCHEM B. (M)

Part: BRACKET — CRACKED (BS 280) · airframe 12,093 hrs · 11,266 cycles

RIGHT AND LEFT BRACKET CRACK AT FS 280 LBL 9. REPLACED IAW SRM 51-42-06 PG 11 AND SRM 51-42-21 PAGE 18. (M)

Part: BULKHEAD — CRACKED (BS 621) · airframe 12,093 hrs · 11,266 cycles

CRACK FOUND ON AFT PRESSURE BULKHEAD WEB AT FS 621 BTW 113.33 AND WL 106.17 LBL 36. REPAIR TO PRESSURE BULKHEAD WEB CARRIED OUT IAW REO 601R-53-61-1230 REV D. (M)

Part: INTERCOSTAL — CRACKED (BS 484)

CRACK FOUND ON RT INTERCOSTAL FS 484 RBL 36 AND RBL 27, CRACK LENGTH .100. INTERCOSTAL CLIPS AT FS 484 RBL 36 AND 27 REPAIRED IAW REO 601R53-41-059 EDDY CURRENT PERFORM ON INTERCOSTAL CUT LINE AND FABRICATED PARTS. (M)

Part: STOP — CRACKED (DOOR)

ON RT WING BUTEDOOR, STOP ASSY CRACKED. REPLACED IAW SRM 51-42-06, 51-42-113. REPLACED IAW SRM 51-42-06, 51-42-13. (M)

Part: PANEL — DAMAGED (RT NACELLE) · airframe 12,093 hrs · 11,266 cycles

RIGHT PYLON PANEL 422DB, SEPARATORS ABRADED. RIGHT PYLON PANEL 422DB, SEPARATORS REPLACED IAW CRJ200 SRM 51-42-06. (M)

Part: STOP — BROKEN (DOOR) · airframe 12,093 hrs · 11 cycles

LT WING DOOR STOP ASSY BROKEN W/S 163.00. REPLACED IAW SRM 51-42-06, 51-42-13. (M)

Part: LENS — CRACKED (RT WING)

RIGHT WING TIP POSITION LIGHT LENSES FOUND CRACKED. REPLACED IAW AMM 57-30-61-400-801. (M)

Part: BULKHEAD — CRACKED (BS 280)

BULKHEAD WEB CRACK AT FS 280 LBL 9. REMOVED IAW REO 53-11-171 REV D SHEET 2 EDDY CURRENT PERFORMED ON CUTOUT FPI PERFORMED ON FABRICATED PARTS. REPAIR PERFORMED IAW REO 601R-53-11-171 REV D SCHEM B. (M)

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 12,093 hrs · 11,266 cycles

PAX DOOR STAIR AFT DRAG ANGLE CRACK. (M)

Part: DOOR — DAMAGED (LT MLG)

LT MLG FIXED DOOR FOUND WORN ON LT END SECTION. REPAIRED IAW REO 601R-52-82-034 SHEET 1 THROUGH 4. (M)

Part: DOOR — WORN (RT MLG) · airframe 12,093 hrs · 11,266 cycles

RIGHT MLG FIXED DOOR FOUND WORN ON L/E END SECTION. RIGHT MLG FIXED DOOR REPAIRED IAW REO 601R-52-82-016 SHEET 1 THROUGH 4. (M)

Part: SILL — CRACKED (FUSELAGE) · airframe 12,093 hrs · 11,266 cycles

CRACK FOUND ON CARGO BAY FLOOR SILL FS 574 LBL 45 UNDER BRACKET RETAINER. NEW UNDER BRACKET RETAINER INSTALLED IAW CRJ REO 601R-53-61-690 REV D. (M)

Part: FITTING — CRACKED (BS 460) · airframe 12,093 hrs · 11,266 cycles

CRACK FOUND ON MACHINE FITTING FS 460 RBL. NEW MACHINED FITTING, REPLACED IAW SRM 51-42-21 AND 51-23-00. (M)

Part: SILL — CRACKED (BS 605)

FOUND LOWER SILL CRACK ON FS 605 LBL 45 OF CARGO DOOR. REPAIRED IAW REO 601R-53-61-433. (M)

Part: BRACKET — CRACKED (BS 529-523)

CRACK FOUND ON HYDRAULIC BRACKET ON MLG BAY FS 529 AND 523 RBL 27. REPLACED IAW CRJ 200 SRM 51-42-06. (M)

Part: PLATE — CRACKED (CARGO DOOR)

FOUND CARGO DOOR SCUFF PLATE IS CRACKED. REPLACED IAW SRM 51-41-02 AND AMM 53-60-31. (M)

Part: SUPPORT BRACKET — CRACKED (BS 718)

AT FS 718, RBL 27 APPROX, HYDRAULIC MANIFOLD SUPPORT BRACKET FOUND CRACKED. REPAIRED IAW REO 601R-53-62-031. (M)

Part: ATTACH FITTING — CRACKED (BS 621-625 S14L) · airframe 12,093 hrs · 11,266 cycles

BTW - FS 621 AND 625.3 AT STRINGER 14 LEFT AND RIGHT SIDE, INTERCOSTAL FITTING FOUND CRACKED. REPLACED INTERCOSTAL FITTING IAW SRM 51-42-20. (M)

Part: BRACKET — CRACKED (BS 529) · airframe 12,093 hrs · 11,266 cycles

CRACK FOUND ON HYDRO BRACKET IS MLG BAY FS 529 LBL 27. REMOVED AND REPLACED IAW SRM 51-42-06. (M)

Part: ADC — FAILED (NR 1) · airframe 12,046 hrs · 11,222 cycles

AIR DATA COMPUTER NR 1 FAILED IN FLIGHT. COMPLIED WITH QRH , SWITCHED TO AIR DATA COMPUTER NR 2, ALL INDICATING NORMAL AIR DIVERSION AND LANDING UNEVENTFUL. (K)

Part: SWITCH — OUT OF ADJUST (BRAKES)

ANTI-SKID IB CAUTION MESSAGE AFTER TAKEOFF FOLLOWED BY PARKING BRAKE SHUTOFF VALVE CAUTION MESSAGE. LANDING GEAR HESITATED TO RETRACT THEN RETRACTED SLOWLY, CAUTION MESSAGES WENT AWAY. HYD SYS NR3 QUANTITY AND PRESS NORMAL, ON GROUND SYSTEM 3 HYD QTY 60 PERCENT. ADJUSTED PARKING BRAKE SWITCH IAW AMM 32-45-16. OPS CHECK GOOD. PERFORMED GEAR SWING AND TIMED GEAR SWINGS W/ 3A AND3B ALONE 7 TOGETHER . NO DEFECTS NOTED DUE TO DISCREPANCY INSPECTED HARNESSES PROX SWITCHES INTERGRATED PSCU NO FAULTS IN MEMORY. (K)

Part: SELECTOR VALVE — MALFUNCTIONED (NLG)

NOSE GEAR DOOR FLAPPING NOISE HEARD AFTER GEAR EXTENSION, TOOK LANDING GEAR CYCLE LONGER THAN NORMAL TO EXTEND. GEAR INDICATOR SHOWED 3 GREEN SIMULTANEOUSLY. EMERGENCY LANDING DECLARED WITH UNEVENTFUL LANDING. (K) R&R NOSE LANDING GEAR SELECT VALVE PER AMM 32-33-10. (A)

Part: GUST LOCK — INOPERATIVE (SERVICE DOOR)

GUST LOCK ON SERVICE DOOR INOPERATIVE. INSPECTED AND FOUND HANDLE ROLL PIN BROKEN. REMOVED AND REPLACED PIN, PERFORMED OPS CHECK IAW AMM 52-41-00, OPS CHECK GOOD. (M)

Part: WARNING MESSAGE — ILLUMINATED (SPOILERONS) · airframe 10,056 hrs · 9,278 cycles

HIGH SPEED ABORTED TAKEOFF DUE TO (SPOILERON) CAUTION MESSAGE. SPEED WAS 110 KNOTS. BRAKE TEMPS WERE 7-8-8-8. FAULT CLEARED USING FIM RESET PROCEDURE IAW AMM 05-51-27-210-801. NO FURTHER INSPECTION REQUIRED FOR REJECTED TAKEOFF. AC OK FOR SERVICE. (K)

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 7,127 hrs · 6,440 cycles

PASSENGER DOOR AFT DRAG ANGLE IS CRACKED .500 INCH LONG. MAINTENANCE REPAIRED DRAG ANGLE IAW REO REV`D BY INSTALLING REPAIR ANGLE. (K)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 7,127 hrs · 6,440 cycles

INTERCOSTAL CRACKED AT FS 484, RBL 27. MAINTENANCE REMOVED AND INSTALLED NEW SERVICEABLE ANGLE IAW REO. (K)

Part: STRUCTURE — CORRODED (RT WING) · corrosion level 1 · airframe 7,127 hrs · 6,440 cycles

RT WING FUEL PANEL 640BB ACCESS HOLE HAS CORROSION, NON-CRITICAL AREA .002D X 2.0 INCH L. MAINTENANCE BLENDED AREA IAW REO. (K)

Part: ANGLE — CORRODED (LT WING) · corrosion level 1 · airframe 7,127 hrs · 6,440 cycles

LT WING FUEL ANGLE 540BB HAS MINOR CORROSION ON LIP, NON CRITICAL AREA .002D X 2.0L. MAINTENANCE BLENDED MINOR CORROSION IWA REO. (K)

Part: PANEL — CORRODED (RT WING) · corrosion level 1 · airframe 7,127 hrs · 6,440 cycles

RT WING FUEL PANEL 6500B ACCESS HOLE CORROSION, NON-CRITICAL AREA .002D X 2.75 INCHES L. MAINTENANCE BLENDED OUT CORROSION IAW REO. (K)

Part: STRUCTURE — CORRODED (LT WING) · airframe 7,127 hrs · 6,440 cycles

LT WING FUEL PANEL 510AB, ACCESS HOLE HAS MINOR CORROSION ON LIP, NON-CRITICAL AREA .003D X 2.5L. MAINTENANCE BLENDED MINOR CORROSION IAW REO. (K)

Part: STRUCTURE — CORRODED (RT WING) · corrosion level 1

RT WING FUEL 650VV ACCESS HOLE LIP HAS MINOR CORROSION, NON-CRITICAL AREA .002 D X 1.5 INCHES L. MAINTENANCE BLENDED MINOR CORROSION IAW REO. (K)

Part: STRUCTURE — CORRODED (RT WING) · corrosion level 1 · airframe 7,127 hrs · 6,440 cycles

RT WING FUEL PANEL 640BB ACCESS HOLE HAS CORROSION ON LIP, NON-CRITICAL AREA .002 INCH DEEP. MAINTENANCE BLENDED DAMAGED AREA AS REQUIRED IAW REO. (K)

Part: PANEL — CORRODED (RT WING) · corrosion level 1 · airframe 7,127 hrs · 6,440 cycles

RT WING FUEL PANEL 640 CB ACCESS HOLE LIP HAS CORROSION NON-CRITICAL AREA .002D X 1.0 INCH L. MAINTENANCE BLENDED OUT DAMAGED AREA AS REQUIRED IAW REO. (K)

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 7,127 hrs · 6,440 cycles

RT FS 621.00 FLOOR SUPPORT ANGLE IS CRACKED .5 INCH LONG ON OB RADIUS. MAINTENANCE REMOVED AND REPLACED IAW REO. (K)

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 7,127 hrs · 6,440 cycles

LT FS 621.00 FLOOR SUPPORT ANGLE IS CRACKED .5 INCH LONG ON OB RADIUS. MAINTENANCE REPAIRED LT FS 621.00 FLOOR SUPPORT ANGLE IAW REO. (K)

Part: HANDLE — DEFECTIVE (ESCAPE HATCH)

CREW ESCAPE HATCH, OUTER HANDLE WILL NOT DEPLOY. REMOVED AND REPLACED HANDLE ASSEMBLY. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 7,127 hrs · 6,440 cycles

RT SIDE FS 621.0 TO FS 625.3 INTERCOSTAL AT STRINGER 14R IS CRACKED NEAR RADIUS APPROX 1.1 INCH LONG. MAINTENANCE REMOVED AND REPLACED ANGLE IAW SRM. (K)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 7,127 hrs · 6,440 cycles

LT SIDE FS 621.0 TO FS 625.3 INTERCOSTAL AT STRINGER 14L IS CRACKED NEAR RADIUS APPROX 1.0 INCH LONG. MAINTENANCE AND REPLACED ANGLE IAW SRM. (K)

Part: WARNING LIGHT — ILLUMINATED (ANTI- ICE SYSTEM) · airframe 3,980 hrs · 3,567 cycles

LT COWL ANTI-ICE AMBER CASS ILLUMINATED WHEN COWL ANTI-ICE SWITCH TURNED OFF. COMPLIED WITH QRH MESSAGE EXTINGUISHED 14TH STAGE BLEED CLOSED.

Part: FLOOR PANEL — CORRODED (FUSELAGE)

FOUND CARGO FLOOR LANDING PLATE HAS MINOR CLASS 1 CORROSION AT FLOOR PANEL ANCHORING NUTS IN AREA OF CARGO DOOR OPENING. (M)

Part: FLOOR PANEL — DAMAGED (CARGO BAY)

FOUND CARGO FLOOR LANDING PLATE HAS MINOR CLASS 1 CORROSION AT FLOOR PANEL ANCHOR NUTS IN AREA OF CARGO DOOR OPENING. REMOVED MINOR CLASS 1 CORROSION IN AREA OF AFT CARGO ANCHOR NUTS BY HAND BURNISHING WITH SCOTCHBRIGHT IAW CRJ 200 SRM 51-21-11 PAGE 31. TREATED, PRIMED AND PAINTED AREAS IAW CRJ 200 SRM 51-21-06 PAGE 1. (M)

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 3,895 hrs · 3,491 cycles

CARGO FLOOR LANDING PLATE HAS MINOR CLASS 1 CORROSION AT FLOOR PANEL ANCHOR NUTS IN AREA OF CARGO DOOR OPENING. REMOVED MINOR CLASS 1 CORROSION IN AREA OF AFT CARGO ANCHOR NUTS BY HAND. BURNISHING WITH SCOTCHBRITE IAW SRM 51-21-11 PG 31. TREATED, PRIMED AND PAINTED AREAS IAW SRM 51-21-06, PG 1.

Part: SKIN — DENTED (CARGO DOOR)

FOUND SCRATCH AND DENT ON LOWER SECTION OF CARGO DOOR 10 INCHES LONG VERTICALLY AND 2 INCHES FROM FORWARD EDGE. REPAIRED DAMAGE TO CARGO DOOR BY INSTALLING REPAIR PER BOMBARDIER REO 601R-52-31-050. (M)

Part: BOLTS — LOOSE (ELEVATOR CONTL)

DURING COMPLIANCE OF FCD 95-32, THE LEFT ELEVATOR OUTPUT LEVER BOLTS THAT ATTACH THE OUTPUT LEVER, P/N 82710093105, TO THE TORQUE TUBE WERE ALL LOOSE. TORQUED ALL LOOSE BOLTS IAW DASH 8 MM 27-32-41. NO DISCREPANCIES ON THE RIGHT SIDE. NO OTHER DAMAGE IS NOTED. (M)