N439AW

Part: SHUTOFF VALVE — MALFUNCTIONED (LT A/C PACK) · airframe 44,059 hrs · 43,788 cycles

WHILE PERFORMING APPENDIX D PROCEDURE AFTER T/O, RT 10TH STAGE SOV WOULD NOT OPEN. LH PACK ON MEL AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED BLEED AIR SOV IAW AWAC SUPP 19-036 AND AMM AMM 36-11-04, PERFORMED OPS CHECK, BLEED LEAK CHECK IAW AWAC SUPP 99-015, OPS CK GOOD.

Part: BRACKET — DAMAGED (NLG PROX SENSOR) · airframe 43,433 hrs · 43,075 cycles

6060 - AFTER TO GEAR UP NLG WOULD NOT RETRACT RAN QRH GEAR DOWN IN GREEN . NO ASSOC MSG, NO MAN RELEASE. HYDS ON. ATC DECLARED EMER, NO HARD. AIRCRAFT REMOVED FROM SERVICE. INSPECTED AND FOUND NLG TOW GUARD COLLAR MIGRATED UP AND DAMAGED NLG PROX SENSOR AND BRACKET. INSTALLED GEAR PINS AND REMOVED FLAGS IAW AWA SUP 11-054A. R+R NLG WOW PROX SNESOR BRACKET. REF AMM 32-61-25 NO DAMAGE NOTED TO PROX SENSOR OR HARNESS. PEROFMRED GEAR SWING TO VERIFY OPERATION. ALL FUNCTIONS CORRECT.

Part: STRUT — LOW PRESSURE (NLG) · airframe 43,171 hrs · 42,765 cycles

GEAR DISAGREE AFTER TAKEOFF, AIRCRAFT REMOVED FROM SERVICE. PERFORMED SERVICING OF NOSE LANDING GEAR SHOCK STRUT IAW AMM 12-12-32 AND AWAC SUP 16-250A. OPSERATIONAL AND FUNCTIONAL TEST ARE GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 42,454 hrs · 41,910 cycles

GEAR DISAGREE ON TAKEOFF ******AIRCRAFT REMOVED FROM SERVICE******** C/W M ACTION FOR MEL 32-30-01 REF 362977/3 FOR MEL. R&R NLG S/A BRACKET IAW CMM 32-20-04 AND AMM 32-61-00-05. OPS CHECK GOOD, REMOVED PLACARD AND REMOVED FROM MEL

Part: WHEEL — DAMAGED (MLG) · airframe 42,256 hrs · 41,679 cycles

ON TAXI INTO GATE, HIT POTHOLE RESULTING TO BOTH RIGHT TIRES BLOWN ON. TAXI WAY A ABEAM A14. BTMS INDICATIONS 4,3,3,3. AIRCRAFT REMOVED FROM SERVICE. CW TIRE BURST INSPECTION OF #3 AND #4 TIRE AIW AMM 05-51-29 NO DEFECTS NOTED. REF 362958-4 AND 362599-1 FOR PERMANENT INSTALL OF #3 AND #4 MLG TIRES. R&R #3 MLG TIRE IAW AMM 32-41-01 AND AWAC SUP 12-015J C/W THE MO16 INSTRUCTIONS THE SPACER AND WASHER WERE RETAINED FROM THE REMOVED WHEEL ASSY AND USED ON THE INSTALLED WHEEL ASSY P/N 5010571-1, S/N OFF JUL02-4998, S/N ON S-SEP11-08

Part: UNKNOWN — UNKNOWN (UNKNOWN)

ON CLIMB OUT GEAR UP GEAR DISAGREE WARNING. MESSAGE CLEARED CONTINUED CLIMB RECEIVED GEAR DISAGREE AGAIN. RAN QRH MESSAGE CLEARED WITH B PUMPS ON. NO ISSUES LOWERING GEAR FOR LANDING. NOSE GEAR DISPLAYED WHITE. MANUAL RELEASE NOT USED, NO OTHER ASSOCIATED MESSAGES. AIRCRAFT REMOVED FROM SERVICE. CW M ACTION FOR MEL 32-30-01 REF 358288/2 FOR MEL. REMOVED, REPLACED, AND ADJUSTED #1 NLG DOWNLOCK LANDING GEAR PROXIMITY SENSOR, IAW AMM 32-61-00. OPS CHECKS NORMAL. REMOVED PLACARD AND REMOVED FROM MEL.

Part: SENSOR — UNKNOWN (UNKNOWN) · airframe 42,029 hrs · 41,422 cycles

FLAPS FAILED AT 30' ON APPROACH, WHEN SELECTING FLAPS 45', LANDED WITH 1400 LBS FUEL. AIRCRAFT REMOVED FROM SERVICE. R&R RH BPSU OPS CHECK GOOD AT THIS TIME. REF AMM 27-51-10.

Part: CONNECTOR — BROKEN (FLAP SKEW DETECT) · airframe 41,345 hrs · 40,739 cycles

WHILE ON APPROACH WITH FLAPS 20 FLAP FAIL CAUTION WITH FLAPS 14 DEG. RAN QRH. AIRCRAFT REMOVED FROM SERVICE. WHEN RECONNECTING SKEW DETECTION SYSTEM FOUND BACK SHELL ON P11CE BROKE. R & R BACK SHELL. OPS CHECK GOOD.

Part: DETECTOR — FAULTED (TE FLAP SKEW) · airframe 41,344 hrs · 40,738 cycles

LAP FAIL CAUTION AT 15 DEG. AIRCRAFT REMOVED FROM SERVICE. REF 351843/4, 351844/1,2,3,4 AND 351845/1 FOR CORRECTIVE ACTIONS AND MEL. SDU WAS DETERMINED TO BE THE CAUSE OF THE FLAP FAIL.

Part: WIRE — FAILED (CIRCUIT BREAKER) · airframe 39,929 hrs · 39,321 cycles

DURING CLIMB, AT ABOUT 10,000 FEET THE CREW RECEIVED MULTIPLE CAUTION MESSAGES. CREW RAN THE QRH BASED ON THE MESSAGES AND WERE LEAD TO BELIEVE IT WAS A POSSIBLE ELECTRICAL ISSUE. THE FLIGHT ATTENDANT KNOCKED ON COCKPIT DOOR TO NOTIFY CREW THAT THE CHIMES AND PA SYSTEM WAS NOT OPERATIVE. CREW WAS UNSURE IF FLAPS WOULD BE AVAILABLE FOR LANDING AND DECIDED TO DECLARE AN EMERGENCY WITH ATC AND PREPARED FOR A FLAPS ZERO LANDING IN KORD. AIRCRAFT REMOVED FROM SERVICE. SPLICED WIRE CB1 WIRE # PA238B8 IAW ESPM 20-16-00 OPS CHECKS GOOD.

Part: NONE — CORRODED (FLIGHT DECK DOOR) · corrosion level 2 · airframe 39,871 hrs · 39,263 cycles

FLIGHT DECK DOOR LOWER TRIM SURFACE HAS CORROSION AND IS DELAMINATED REMOVED AND REPAIRED FLIGHT DECK DOOR LOWER TRIM IAW C&D ZODIAC RPM 25-6000-1 REV 1 DATE 2-18-06 AND SRM 51-26-00 REV 38. ACCOMPLISHED REINSTALL OF FLIGHT DECK DOOR. ALL WORK PERFORMED AT AERSALE CRS 4AER685B UNDER WORK ORDER 003442

Part: NONE — CORRODED (FS438 TO FS443) · corrosion level 2 · airframe 39,871 hrs · 39,263 cycles

2 SPOTS OF CORROSION ON R/H FLOOR SILL PANEL WITHIN 2.50IN OF EACH OTHER FROM FS438.0 TO FS443.0. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED BOTH SPOTS IAW REO 601R-53-41-666 REV C. DATE 2012-11-06. DIMENSIONS #1 L=1.025IN X W=.900IN X D=.005IN #2 L=1.0IN X W=.800IN X D=.005IN. BLENDED AREAS FOUND TO BE OUT OF LIMITS DUE TO CLOSE PROXIMITY. RE-EVALUATED BLENDED AREAS IAW EA#: CJ253-01697 AND FOUND TO BE ACCEPTABLE. RESTORED PROTECTIVE FINISH, ALL WORK PERFORMED AT AERSALE CRS 4AER685B UNDER WORK ORDER 003442

Part: NONE — CORRODED (FS450 TO FS559) · corrosion level 2 · airframe 39,871 hrs · 39,263 cycles

16 AREAS ON THE L/H FLOOR SILL AND FLOOR ANGLE FROM FS450 TO FS559 FOUND TO HAVE CORROSION. ALL 16 AREAS WERE BLENDED IAW REO# 601R-53-41-666 AND THE MEASUREMENT ARE LISTED BELOW. 1. FS 424 + 3Ï¿½ L= 1.3Ï¿½ X W= 1Ï¿½ X D= .005Ï¿½ FLOOR SILL 2. FS 424 + 9Ï¿½ L= 1.3Ï¿½ X W= 1Ï¿½ X D= .004Ï¿½ FLOOR SILL 3. FS 439 + 8Ï¿½ L= 1.4Ï¿½ X W= 1Ï¿½ X D= .005Ï¿½ FLOOR SILL 4. FS 449 L= 3.8Ï¿½ X W= 2Ï¿½X D= .005Ï¿½ FLOOR ANGLE 5. FS 449 + 10Ï¿½ L= 1.8Ï¿½ X W= .9Ï¿½ X D = .001Ï¿½ FLOOR ANGLE 6. FS 473.15Ï¿½ L= 1Ï¿½ X W= .8Ï¿½ X D= .004Ï¿½ FLOOR ANGLE 7. FS 473.15Ï¿½ L= 2.2Ï¿½ X W= 1.3Ï¿½ X D= .002Ï¿½ FLOOR ANGLE 8. FS 473.15 + 9Ï¿½ L= 1.5Ï¿½ X W= 1.1Ï¿½ X D= .003Ï¿½ FLOOR SILL 9. FS 499 L= 9.3 X W= 1.2Ï¿½ X D= .009Ï¿½ FLOOR ANGLE 10. FS 513 L= 2.1 X W= 1Ï¿½ X D= .009Ï¿½ FLOOR ANGLE 11. FS 513 + 2Ï¿½ L= 1.9Ï¿½ X W= .7Ï¿½ X D= .005Ï¿½ FLOOR ANGLE 12. FS 513 + 3Ï¿½ L= 1.6 X W = .9Ï¿½ X D= .004Ï¿½ FLOOR SILL 13. FS 513+6Ï¿½ L= 1.3Ï¿½ X W= .8Ï¿½ X D= .003Ï¿½ FLOOR SILL 14. FS 529+6Ï¿½ L= 1.3Ï¿½ X W= 1Ï¿½ .004Ï¿½ FLOOR SILL 15. FS 529+12Ï¿½ L= 1.4Ï¿½ X W= 1.2Ï¿½ X D= .002Ï¿½ FLOOR SILL 16. FS 544+4Ï¿½ L= 1.1Ï¿½ W= 1Ï¿½ X D= .002Ï¿½ FLOOR SILL BLEND 12 AND 13 WERE FOUND TO BE OUT OF LIMITS, RE-EVALUATED AND FOUND 12 AND 13 TO BE WITHIN LIMITS IAW EA #: AWAC-CRJ253-01689, REV C AND ACCOMPLISHED HFEQ INSPECTION IAW NDTM PART 1 51-20-06. ACCOMPLISHED REPLACEMENT OF THE PROTECTIVE COAT ON ALL 16 AREAS IAW REO 601R-53-41-666 REV C DATE 2012-11-06. ALL WORK PERFORMED AT AERSALE CRS 4AER685B UNDER WORK ORDER #:003442

Part: NONE — DENTED (STAB) · airframe 39,871 hrs · 39,263 cycles

DENT WITH SCRATCH ON SKIN OF RH HORIZONTAL STABILIZER LE PANEL 341AR ON UPPER OUTBOARD END BETWEEN STABILIZER BL96.26 AND BL112.00. ***AIRCRAFT REMOVED FROM SERVICE*** HAND FORMED DENT AND REMOVED SCRATCH BY BLENDING ON SKIN OF RH HORIZONTAL STABILIZER LE PANEL 341AR ON UPPER OUTBOARD END BETWEEN STABILIZER BL96.26 AND BL112.00. PN 600-23060. DENT DIMENSION L= 0.600Ï¿½ X W= 0.450Ï¿½ X D= 0.019Ï¿½ AND SCRATCH DIMENSION L= 0.200Ï¿½ X W= 0.200Ï¿½ X D= 0.007Ï¿½. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA # AWAC-CRJ255-01696 REV A DATED 10/14/2021. WORK PERFORMED UNDER AERSALE WORK ORDER 003442, CARD NO. 20281, TT: 39871:10 TC: 39263.

Part: NONE — CORRODED (FS441.00 TO) · corrosion level 2 · airframe 39,871 hrs · 39,263 cycles

CORROSION AT 3 AREAS ON RH FLOOR SILL PANEL AROUND FASTENER HOLES BETWEEN FS441.00 TO FS459.00 AND RBL41. BLENDED CORROSION AT 3 AREAS ON RH FLOOR SILL PANEL AROUND FASTENER HOLES BETWEEN FS441.00 TO FS459.00 AND RBL41. DIMENSIONS P1 - L= 1.025Ï¿½ X W= 0.900Ï¿½ X D= 0.010Ï¿½, P2 - L= 0.900Ï¿½ X W= 0.750Ï¿½ X D= 0.012Ï¿½, P3 - L= 0.500Ï¿½ X W= 0.420Ï¿½ X D= 0.008Ï¿½. PERFORMED HFEC WITH NO INDICATIONS. RESTORED SURFACE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA #AWAC-CRJ253-01697 REV IR DATED 10/13/2021. WORK PERFORMED UNDER AERSALE WORK ORDER 003442, CARD NO. 20276, TT: 39871:10 TC: 39263.

Part: SEAT TRACK — CORRODED (FS546 TO FS559+8) · corrosion level 2 · airframe 39,871 hrs · 39,263 cycles

SEAT TRACK P/N: 20276-144-0-0 AT FS 546 TO FS 559+80 L/H SIDE HAS NUMEROUS SPOTS OF CORROSION AND WEAR. ***AIRCRAFT REMOVED FROM SERVICE*** REPLACED WITH A NEW SEAT TRACK P/N: 20276-144-0-0 AT FS 546 TO FS 559+80 L/H SIDE. ALL WORK WITHIN LIMITS IAW CRJ200 AMM 53-01-11 REV 38. WORK PERFORMED UNDER AERSALE W/O #03442 CARD #20244. TT:39,871 TC:39,263.

Part: SEAT TRACK — CORRODED (FS 409+16) · corrosion level 2 · airframe 39,871 hrs · 39,263 cycles

SEAT TRACK PN 20276-144-0-0 AT FS409.00 + 16Ï¿½ Ï¿½ FS409.00 + 112Ï¿½ HAS CORROSION AT NUMEROUS LOCATIONS. ***AIRCRAFT REMOVED FROM SERVICE*** REPLACED WITH A NEW SEAT TRACK PN 20276-144-0-0 AT FS364.00 Ï¿½ FS409.00 + 18Ï¿½. ALL WORK WITHIN LIMITS WAS PERFORMED IAW CRJ200 AMM 53-01-11 REV 38. WORK PERFORMED UNDER AERSALE WORK ORDER 003442, CARD NO. 20246, TT: 39871:10 TC: 39263.

Part: SEAT TRACK — CORRODED (FS 409+18) · corrosion level 2 · airframe 39,871 hrs · 39,263 cycles

SEAT TRACK PN 20276-144-0-0 AT FS409.00 + 18 - FS409.00 + 110 LHS HAS CORROSION AT NUMEROUS LOCATIONS. ***AIRCRAFT REMOVED FROM SERVICE*** REPLACED WITH A NEW SEAT TRACK PN 20276-144-0-0 AT FS409.00 + 18 - FS409.00 + 110 LHS. ALL WORK WITHIN LIMITS WAS PERFORMED IAW CRJ200 AMM 51-01-11 REV 38. WORK PERFORMED UNDER AERSALE WORK ORDER 003442, CARD NO. 20241, TT: 39871:10 TC: 39263.

Part: SEAT TRACK — CORRODED (FS449.83 TO FS54) · corrosion level 2 · airframe 39,871 hrs · 39,263 cycles

SEAT TRACK P/N: 20276-144-0-0 AT FS 449.83 TO FS 546 L/H SIDE HAS NUMEROUS SPOTS OF CORROSION AND WEAR. ***AIRCRAFT REMOVED FROM SERVICE*** REPLACED WITH A NEW SEAT TRACK P/N: 20276-144-0-0 AT FS 449.83 TO FS 546 L/H SIDE. ALL WORK WITHIN LIMITS IAW CRJ200 AMM 53-01-11 REV 38. WORK PERFORMED UNDER AERSALE W/O #03442 CARD #20248. TT:39,871 TC:39,263

Part: SEAT TRACK — CORRODED (FS 409+110) · corrosion level 2 · airframe 39,871 hrs · 39,263 cycles

SEAT TRACK PN 20276-144-0-0 AT FS409.00 + 110 - FS449.83 LHS HAS CORROSION AT NUMEROUS LOCATIONS. ***AIRCRAFT REMOVED FROM SERVICE*** REPLACED WITH A NEW SEAT TRACK PN 20276-144-0-0 AT FS409.00 + 110 - FS449.83 LHS. ALL WORK WITHIN LIMITS WAS PERFORMED IAW CRJ200 AMM 51-01-11 REV 38. WORK PERFORMED UNDER AERSALE WORK ORDER 003442, CARD NO. 20242, TT: 39871:10 TC: 39263.

Part: NONE — CORRODED (FS449) · corrosion level 2 · airframe 39,871 hrs · 39,263 cycles

SEAT TRACK PN 20276-144-0-0 AT FS449.83 Ï¿½ FS546.00 HAS CORROSION AT NUMEROUS LOCATIONS. ***AIRCRAFT REMOVED FROM SERVICE*** REPLACED WITH A NEW SEAT TRACK PN 20276-144-0-0 AT FS449.83 Ï¿½ FS546.00. ALL WORK WITHIN LIMITS WAS PERFORMED IAW CRJ200 AMM 53-01-11 REV 38. WORK PERFORMED UNDER AERSALE WORK ORDER 003442, CARD NO. 20243, TT: 39871:10 TC: 39263.

Part: SEAT TRACK — CORRODED (FS 546) · corrosion level 2 · airframe 39,871 hrs · 39,263 cycles

SEAT TRACK PN 20276-144-0-0 AT FS546.00 Ï¿½ FS599.00 + 80 RHS HAS CORROSION AT NUMEROUS LOCATIONS. ***AIRCRAFT REMOVED FROM SERVICE*** REPLACED WITH A NEW SEAT TRACK PN 20276-144-0-0 AT FS546.00 Ï¿½ FS599.00 + 80 RHS. ALL WORK WITHIN LIMITS WAS PERFORMED IAW CRJ200 AMM 51-01-11 REV 38. WORK PERFORMED UNDER AERSALE WORK ORDER 003442, CARD NO. 20249, TT: 39871:10 TC: 39263.

Part: SEAT TRACK — CORRODED (FS364 TO FS409+1) · corrosion level 2 · airframe 39,871 hrs · 39,263 cycles

SEAT TRACK P/N: 20276-144-0-0 AT FS 364.00 TO FS 409+18 L/H SIDE HAS NUMEROUS SPOTS OF CORROSION AND WEAR. ***AIRCRAFT REMOVED FROM SERVICE*** REPLACED WITH A NEW SEAT TRACK P/N 20276-144-0-0 FS 364.00 TO FS 409+18 L/H SIDE. ALL WORK WITHIN LIMITS WAS PERFORMED IAW CRJ200 AMM 53-01-11 REV 38. WORK PERFORMED UNDER AERSALE W/O #003442 CARD #20240. TT:39,871 TC:39,263

Part: SEAT TRACK — CORRODED (FS 364) · corrosion level 2 · airframe 39,871 hrs · 39,263 cycles

SEAT TRACK PN 20276-144-0-0 AT FS364.00 Ï¿½ FS409.00 + 18Ï¿½ HAS CORROSION AT NUMEROUS LOCATIONS. ***AIRCRAFT REMOVED FROM SERVICE*** REPLACED WITH A NEW SEAT TRACK PN 20276-144-0-0 AT FS364.00 Ï¿½ FS409.00 + 18Ï¿½. ALL WORK WITHIN LIMITS WAS PERFORMED IAW CRJ200 AMM 53-01-11 REV 38. WORK PERFORMED UNDER AERSALE WORK ORDER 003442, CARD NO. 20245, TT: 39871:10 TC: 39263.

Part: SEAT TRACK — CORRODED (FS 409+10) · corrosion level 2 · airframe 39,871 hrs · 39,263 cycles

SEAT TRACK PN 20276-144-0-0 AT FS409.00 + 10Ï¿½ Ï¿½ FS449.83 HAS CORROSION AT NUMEROUS LOCATIONS. ***AIRCRAFT REMOVED FROM SERVICE*** REPLACED WITH A NEW SEAT TRACK PN 20276-144-0-0 AT FS364.00 Ï¿½ FS409.00 + 18Ï¿½. ALL WORK WITHIN LIMITS WAS PERFORMED IAW CRJ200 AMM 51-01-11 REV 38. WORK PERFORMED UNDER AERSALE WORK ORDER 003442, CARD NO. 20247, TT: 39871:10 TC: 39263.

Part: NONE — NONE · airframe 39,871 hrs · 39,263 cycles

CRACK INDICATIONS (2 TOTAL) AT FS 621 AFT PRESSURE BULKHEAD. CRACKS AT THE FOLLOWING LOCATIONS: FS 621 WL 107-WL 110 AT BL 0 CRACK IS 3"LENGTH; FS 621 WL 112.5-WL 115.5 AT LBL 27.5 CRACK IS 3" LENGTH. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED CUTOUT ON SKIN WEB AT AFT PRESSURE BULKHEAD AT FS 621 BL 0.0 WL 106.5 TO WL 111.5 DIMENSIONS: 5.15" LENGTH X 1.7" WIDTH. PERFORMED CUTOUT AT FS 621 LBL 27.5 WL 111.5 TO WL 116.65. DIMENSIONS: 5.15" LENGTH X 2.975" WIDTH. REPAIRED FS 621 BL 0 IAW REO 601R-53-61-1240 REV D DATED 2016-10-31. REPAIRED FS 621 LBL 27.5 IAW MHIRJ REO 601R-53-61-7722 REV (--) DATED 2021-10-13. HFEC PERFORMED WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK PERFORMED AT AERSALE CRS #4AER685B ON WO #003442 CARD #00015.

Part: FITTING — GOUGED (FS 345) · airframe 39,871 hrs · 39,263 cycles

PAX DOOR SUPPORT WHEEL FITTING PN 601R317092-3 HAS A GOUGE BELOW SPRING FS345.00. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED PAX DOOR SUPPORT WHEEL FITTING GOUGE BELOW SPRING FS345.00. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA # AWAC-CRJ252-01691 REV IR DATED 10/04/2021.

Part: NONE — CORRODED (FLOOR SILL) · corrosion level 2 · airframe 39,871 hrs · 39,263 cycles

CORROSION ON FLOOR SILL STRAP P/N 601R31025-29 AT FS559 AND LBL28.00". ***AIRCRAFT REMOVED FROM SERVICE*** REPLACED FLOOR SILL STRAP WITH A NEW FABRICATED STRAP P/N 601R31025-29 AT FS559 AND LBL28.00. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW CRJ200 SRM 51-24-16, SRM 51-42-06, SRM 51-45-00, SRM 51-21-11, SRM 51-25-06, SRM 5151-25-01, ALL AT REV 38.

Part: NONE — GOUGED (FS 559+80) · airframe 39,871 hrs · 39,263 cycles

GOUGE FOUND ON FWD SIDE OF I/B FLANGE OF FRAME SPLICE ANGLE AT FS 559.00 + 80 AT STR 6R. GOUGE DIMENSIONS ARE: .200"L X .200" W X .032"D. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED BLEND OUT ON FRAME SPLICE ANGLE AT FS 559.00 + 80 AT STR 6R. BLEND DIMENSIONS ARE: 1.0"L X .124"W WITH ORIGINAL FLANGE WIDTH OF .970" AND REMAINING FLANGE WIDTH OF .846" PERFORMED HFEC WITH NO INDICATIONS RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS REF MHIRJ REO 601R-53-51-604 REV (--) DATED 2021-10-13. WORK PERFORMED UNDER AERSALE W/O # 003442 CARD #20203. THIS IS TEMPORARY REPAIR STRUCTURALLY ACCEPTABLE FOR 5000 FLIGHT HOURS WITH INSPECTION INTERVALS NOT TO EXCEED 1000 FLIGHT HOURS. TT:39,871 TC:39,263

Part: ANTENNA — CORRODED (FS409.00+32) · corrosion level 2 · airframe 39,871 hrs · 39,263 cycles

GPS ANTENNA RH HAS CORROSION ON MATING SURFACE, FS409.00+32, STR 0.0. REMOVED AND REPLACED WITH A NEW GPS ANTENNA AT FS409.00+32, STR 0.0. PN S67-1575-52 / SN 512-32090. ALL WORK WITHIN LIMITS WAS PERFORMED IAW CRJ200 AMM 34-58-400-801, REV 64. WORK PERFORMED UNDER AERSALE WORK ORDER 003442, CARD NO. 20007 / 20193, TT: 39871:10 TC: 39263.

Part: FITTING — GOUGED (ELEVATOR) · airframe 39,871 hrs · 39,263 cycles

GOUGE ON RH ELEVATOR MID HINGE NO. 2 BL55.88 LOWER SIDE. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED DAMAGE ON RH ELEVATOR MID HINGE NO. 2 BL55.88 LOWER SIDE. PN 600-23046. FITTING DIMENSION L= 0.500Ï¿½ X W= 0.100Ï¿½ X D= 0.010Ï¿½, PLATE DIMENSION L= 0.700Ï¿½ X W= 0.100Ï¿½ X D= 0.017Ï¿½. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA # AWAC-CRJ255-01687 REV IR DATED 9/27/2021. WORK PERFORMED UNDER AERSALE WORK ORDER 003442, CARD NO. 20067, TT: 39871:10 TC: 39263.

Part: NONE — GOUGED (ELEVATOR) · airframe 39,871 hrs · 39,263 cycles

RH ELEVATOR HAS A GOUGE AT INBOARD PCU FORWARD ATTACHMENT FITTING LOWER SIDE BETWEEN 1 AND RIB 2 RHS. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED GOUGE AT INBOARD PCU, FORWARD ATTACHMENT FITTING LOWER SIDE BETWEEN 1 AND RIB 2 RHS. GOUGE DIMENSION L = 0.400Ï¿½ X W = 0.250Ï¿½ X D = 0.017Ï¿½. ROTO PEENED REWORKED AREA. HFEC PERFORMED WITH NO INDICATIONS. RESTORED SURFACE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW MHIRJ REO 601R-55-11-697 REV (-) DATED 2021-09-30. WORK PERFORMED UNDER AERSALE WORK ORDER 003442, CARD NO. 20068, TT: 39871:10 TC: 39263.

Part: SKIN — DENTED (FS 640) · airframe 39,871 hrs · 39,263 cycles

AFT FUSELAGE SKIN HAS 3 DENTS AT FS640.00 + 8Ï¿½ RH STR24 + 1.75Ï¿½, FS640.00 + 9Ï¿½ RH STR24 + 1.25Ï¿½ AND FS640.00 + 10Ï¿½ RH STR24 + 2.70Ï¿½. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED DOUBLER REPAIR TO THE AFT FUSELAGE SKIN HAS 3 DENTS AT FS640.00 + 8Ï¿½ RH STR24 + 1.75Ï¿½, FS640.00 + 9Ï¿½ RH STR24 + 1.25Ï¿½ AND FS640.00 + 10Ï¿½ RH STR24 + 2.70Ï¿½. DENT DIMENSION P1- L = 0.450Ï¿½ X W = 0.300Ï¿½ X D = 0.001Ï¿½, P2- L = 0.300Ï¿½ X W = 0.250Ï¿½ X D = 0.001Ï¿½, P3- L = 0.300Ï¿½ X W = 0.250Ï¿½ X D = 0.001Ï¿½. NO CUTOUT FOR P1. CUTOUT DIMENSIONS FOR P2 Ï¿½ L= 0.500Ï¿½ X W= 0.500Ï¿½ AND P3 L= 0.500Ï¿½ X W = 0.500Ï¿½. FABRICATED DOUBLER DIMENSIONS L = 9.250Ï¿½ X W = 7.700Ï¿½ FROM 0.063Ï¿½ CLAD ALUMINUM. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA # AWAC-CRJ253-01693 REV IR DATED 10/3/2021. WORK PERFORMED UNDER AERSALE WORK ORDER 003442, CARD NO. 20130, TT: 39871:10 TC: 39263.

Part: SKIN — DENTED (FS 589) · airframe 39,871 hrs · 39,263 cycles

DENT ON AFT FUSELAGE SKIN AT FS589.00 AND LH STR20+3Ï¿½. ***AIRCRAFT REMOVED FROM SERVICE*** EVALUATED DENT ON AFT FUSELAGE SKIN AT FS589.00 AND LH STR20+3Ï¿½. AND FOUND TO BE ACCEPTABLE PER EA. DENT DIMENSION L = 9.00Ï¿½ X W = 0.600Ï¿½ X D = 0.016Ï¿½. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA # AWAC-CRJ253-01685 REV IR DATED 9/27/2021. WORK PERFORMED UNDER AERSALE WORK ORDER 003442, CARD NO. 20126, TT: 39871:10 TC: 39263.

Part: SKIN — DENTED (FS 605) · airframe 39,871 hrs · 39,263 cycles

DENT ON AFT FUSELAGE SKIN AT FS605.00 +2Ï¿½ AND LH STR23+2.5Ï¿½. ***AIRCRAFT REMOVED FROM SERVICE*** EVALUATED DENT ON AFT FUSELAGE SKIN AT FS605.00 +2Ï¿½ AND LH STR23+2.5Ï¿½. AND FOUND TO BE ACCEPTABLE PER EA. DENT DIMENSION L = 1.200Ï¿½ X W = 1.100Ï¿½ X D = 0.008Ï¿½. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA # AWAC-CRJ253-01686 REV IR DATED 9/27/2021. WORK PERFORMED UNDER AERSALE WORK ORDER 003442, CARD NO. 20128, TT: 39871:10 TC: 39263.

Part: SKIN — CORRODED (WS 65) · corrosion level 2 · airframe 39,871 hrs · 39,263 cycles

CORROSION AND PITTING ON LH WING UPPER ACCESS FOR PANEL 540AT AT WS65.75. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED CORROSION DAMAGE AT TWO PLACES ON LH WING UPPER ACCESS FOR PANEL 540AT AT WS65.75. DIMENSION P1- L = 3.800Ï¿½ X W = 0.4.0Ï¿½ X D = 0.194Ï¿½, P2 - L = 15.00Ï¿½ X W = 0.400Ï¿½ X D = 0.191Ï¿½. HFEC PERFORMED WITH NO INDICATIONS. ROTO PEENED REWORKED AREA. RESTORED SURFACE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW HIRJ REO 601R-57-21-3522 REV (-) DATED 2021-09-28. WORK PERFORMED UNDER AERSALE WORK ORDER 003442, CARD NO. 20061, TT: 39871:10 TC: 39263.

Part: SKIN — DENTED (FS 755) · airframe 39,871 hrs · 39,263 cycles

TWO DENTS ON AFT FUSELAGE SKIN FS755.00 - 67.50 DATUM AND STR26L AND STR26R. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED TWO DOUBLER REPAIRS TO THE AFT FUSELAGE SKIN AT FS755.00 - 67.50 DATUM AND STR26L AND STR26R. DENT DIMENSION LH S26 L= 2.300Ï¿½ X W = 1.200Ï¿½ X D = 0.008Ï¿½ AND RH S26 L= 2.850Ï¿½ X W = 1.300Ï¿½ X D= 0.035Ï¿½. CUTOUT DIMENSIONS LH S26 ARE L= 3.100Ï¿½ X W = 1.00Ï¿½, AND RH 26 ARE L= 3.100Ï¿½ X W = 1.100Ï¿½. FABRICATED TWO DOUBLER WITH SAME DIMENSIONS L = 8.600Ï¿½ X W = 5.750Ï¿½ FROM 0.063Ï¿½ CLAD ALUMINUM. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA # AWAC-CRJ253-01663 REV IR DATED 8/19/2021. WORK PERFORMED UNDER AERSALE WORK ORDER 003442, CARD NO. 20040, TT: 39871:10 TC: 39263.

Part: WARNING MESSAGE — FALSE ACTIVATION (PAX DOOR) · airframe 39,813 hrs · 39,200 cycles

RECEIVED PAX DR WARNING CLIMBING THRU FL 330 PRESSURIZATION REMAINED NORMAL THROUGH FLIGHC/Q QRH DESCENDED TO 11,000 FT MSG CLEARED ON ITS OWN. AIRCRAFT REMOVED FROM SERVICE. INSPECTED PAX DOOR WIRING, CONNECTORS AND SPLICES FOUND ALL TO BE TIGHT AND NO DEFECTS NOTED. PERFORMED OPS CHECK IAW AMM 52-70-04-710-803 OPS CHECK GOOD, ALL GREEN WITNESS MARKS ALIGN. OK FOR SERVICE.

Part: NONE — NONE (HOR STAB) · airframe 39,871 hrs · 39,263 cycles

H/STAB PCU ACCESS PANEL #332AB (P/N: 601R23052-11) HAS 3EACH DAMAGED HOLES. DIMENSIONS: HOLE #1: .195" X .258"; HOLE #2: .310" X .220"; HOLE #3: .195" DIA ***AIRCRAFT REMOVED FROM SERVICE*** REAMED HOLES TO FOLLOWING DIMENSIONS: HOLE #1: .3685"; HOLE #2: .3750"; HOLE#3: .3685". PERFORMED HFEC WITH NO INDICATIONS. INSTALLED FREEZE PLUG AT EACH HOLE LOCATION. OPENED HOLES AT 3 EACH LOCATIONS TO 0.190" - 0.192." RESTORED PROTECTIVE FINISH. ALL WORK PERFORMED IAW MHIRJ REO 601R-55-11-691 REV (--) DATED 2021-07-09. WORK PERFORMED UNDER AERSALE WORK ORDER #003442 CARD #00012, TT: 39,871 TC: 39,263

Part: NONE — NONE (HOR STAB) · airframe 39,871 hrs · 39,263 cycles

ELONGATED HOLE COMMON TO H/STAB LHS LOWER DOUBLER (DWG 600-23044) AND RIB (DWG 601R23030) AT PCU ACCESS DOOR. HOLE DIMENSIONS AT DOUBLER ARE (P2) = .370" X .250. HOLE DIMENSIONS AT RIB ARE (P1) = .370" X .370. ***AIRCRAFT REMOVED FROM SERVICE*** REAMED HOLES TO FOLLOWING DIMENSIONS: (P1) = .3750" AND (P2) = 0.3750". PERFORMED HFEC WITH NO INDICATIONS. FABRICATED 2 EACH FREEZE PLUGS OUT OF 7075-T6 ALUMINUM ALLOY. INSTALLED FREEZE PLUG AT EACH HOLE LOCATION. OPENED HOLES AT (P1) AND (P2) TO 0.190" - 0.192" DIA. RESTORED PROTECTIVE FINISH. ALL WORK PERFORMED IAW MHIRJ REO 601R-55-11-698 REV (--) DATED 2021-10-27. WORK PERFORMED UNDER AERSALE WORK #003442 CARD #00011 TT: 39,871 TC: 39,263

Part: RVDT — FAULTED (NLG STEERING) · airframe 39,271 hrs · 38,635 cycles

RECIEVED STEERING INOP CAUTION MSG IN FLIGHT C/W QRH AND MSG PERSISTS. ***AIRCRAFT REMOVED FROM SERVICE*** R&R LFT NLG RVDT IAW AWAC SUP 15-177A OPS TEST OF NWS GOOD P/N OFF:16735-109,S/N OFF:NSN/447/1,P/N ON:3A1252D,S/N ON:D0796. MPM

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 38,681 hrs · 37,991 cycles

AFT PRESSURE BULKHEAD AT FS 621.00 & LBL 27.5 WL 133-135 HAS A FAILED INDICATION APPROXIMATELY 2" LONG IAW CRJ 200 NDT MANUAL PART 1 57-20-06 REV 41. "AIRCRAFT REMOVED FROM SERVICE" REPAIRED DAMAGED AREA ON APB REF CRJ 200 REO 601-53-61-1541 REV F.

Part: CABLE — DAMAGED (A/P ELEV SERVO) · airframe 38,681 hrs · 37,991 cycles

L/H VERTICAL AUTO PILOT SERVO CABLE IS RUSTED AROUND SERVO BOTTOM. "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED ELEVATOR SERVO P/N 822-0260-001 REF CRJ 200 AMM. REMOVED AND REPLACE L/H ELEVATOR FUSELAGE CABLE P/N 601R90020-79 FOR BROKEN STRANDS REF CRJ 200 AMM 27-31-00 REV 60

Part: WARNING MESSAGE — ILLUMINATED (TE FLAPS) · airframe 37,980 hrs · 37,341 cycles

DURING CRUISE FLIGHT, THE FLIGHT CREW RECEIVED A FLAP FAIL MESSAGE. THE CREW NOTIFIED DISPATCH, DECLARED AN EMERGENCY AND DIVERTED. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO INJURIES OR ADVERSE PASSENGER REACTION.

Part: WARNING MESSAGE — ILLUMINATED (TE FLAPS) · airframe 37,956 hrs · 37,317 cycles

CLIMBING OUT OF 17,000 FLAP FAIL CAUTION MESSAGE, C/W QRH, MESSAGE REMAINED, LANDED FLAPS 0, NORMAL T/D, NORMAL LANDING, PERFORED FLAP RESET PROCEDURE IAW 98-18G BOX 12,

Part: WARNING MESSAGE — ILLUMINATED (TE FLAPS) · airframe 37,838 hrs · 37,198 cycles

FLAP FAIL CAUTION MESSAGE IN FLIGHT FLAPS INDICATED 0 DEGREES PERFORMED FLAP REST PROCEDURE IAW AWAC SUP 98-18G BOX 12 ABOUT 20 MINS AFTER DEPARTURE, ABOUT 17000 FEET, THE PLANE SHOWED A FLAPS FAIL CAUTION MESSAGE. THE FO WAS FLYING AT THE TIME. WE PERFORMED THE QRH AND NOTIFIED ATC AND DECLARED AN EMERGENCY AND DECIDED TO CONTINUE TO DESTINATION.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 37,805 hrs · 37,166 cycles

ON APPROACH TO GSO THE FLIGHT RECEIVED AN ANTI-SKID OUTBOARD CAUTION MESSAGE. THE CREW DID A GO-A-ROUND AND HAD THE EQUIPMENT STANDING BY BUT DID NOT DECLARE AN EMERGENCY. FLIGHT LANDED AND TAXIED TO THE GATE WITH OUT INCIDENT. 3869 - RECEIVED ANTI-SKID OUTBOARD CAUTION ON APPROACH. COMPLIED WITH QRH, LANDED UN-EVENTFULLY. MESSAGE INTERMITTENT ON TAXI INTO GATE. MESSAGE APPEARED BOTH TIMES SELECTING GEAR DOWN.

Part: UNKNOWN — MALFUNCTIONED (COCKPIT) · airframe 37,527 hrs · 36,910 cycles

3884 STAB AND MACH TRIM WOULD NOT STAY ENGAGED. FAILED 8 TIMES. RAN QRH EACH TIME. WOULD STAY ENGAGED ABOUT 25 SECONDS.

Part: SKIN — DENTED (FUSELAGE) · airframe 35,265 hrs · 34,669 cycles

DENT ON LOWER FUSELAGE SKIN AT FS605.00, STGR24L.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,265 hrs · 34,669 cycles

FRAME AT FS 605 HAS CORROSION BETWEEN STR 24L AND 25R. REPLACED.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,265 hrs · 34,669 cycles

UPON REMOVAL OF REINFORCEMENT ANGLE AT FS 605 ANGLE FOUND TO HAVE CORROSION.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 35,265 hrs · 34,669 cycles

FLOOR SUPPORT ANGLE CRACKED AT FS 280.00, RBL9. REPLACED ANGLE IAW SRM 51-42-21.

Part: RISER — CRACKED (PAX DOOR) · airframe 35,265 hrs · 34,669 cycles

PAX DOOR AFT STAIR RISER CRACKED. REPAIRED AFT STEP RISER IAW REO601R-52-11-702 REV E.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 35,265 hrs · 34,669 cycles

CRACKED FLOOR BEAM ANGLE AT FS 280.00, LBL9. REPLACED ANGLE IAW SRM 51-42-21.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 35,265 hrs · 34,669 cycles

RIGHT OVER WING BRACKET CRACKED AT FS 449.85. REPLACED BRACKET IAW SRM 51-42-06.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 35,265 hrs · 34,669 cycles

RIGHT OVERWING BRACKET CRACKED AT FS 473.15. REPLACED BRACKET IAW SRM 51-42-06.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 35,265 hrs · 34,669 cycles

RIGHT OVER WING BRACKET CRACKED AT FS 461.00. REPLACED BRACKET IAW SRM 51-42-06.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 35,265 hrs · 34,669 cycles

LEFT OVER WING BRACKET CRACKED AT FS 473.15. REPLACED BRACKET IAW SRM 51-42-06.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 35,265 hrs · 34,669 cycles

LEFT OVER WING BRACKET CRACKED AT FS 461.00. REPLACED BRACKET IAW SRM 51-42-06.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 35,265 hrs · 34,669 cycles

LEFT OVER WING BRACKET CRACKED AT FS 449.85. REPLACED BRACKET IAW SRM 51-42-06.

Part: RETAINER — CRACKED (PYLON SEAL) · airframe 35,265 hrs · 34,669 cycles

PYLON PANEL 412DB HAS A CRACKED SEAL RETAINER. REPAIRED THE SEAL RETAINER IAW 16-363.

Part: RETAINER — CRACKED (PYLON SEAL) · airframe 35,265 hrs · 34,669 cycles

CRACKED SEAL RETAINER ON PANEL 412BT. REPAIRED THE SEAL RETAINER IAW 16-363.

Part: CROSSBEAM — DAMAGED (CARGO DOOR) · airframe 34,607 hrs · 34,003 cycles

DURING ROUTINE INSPECTION OF THE AFT PRESSURE BULKHEAD MAINTENANCE FOUND THE CARGO DOOR CROSSBEAM DAMAGED. DAMAGE WAS CAUSED FROM THE FORWARD CARGO DOOR CABLE COMING OFF THE PULLEY AND CHAFFING AGAINST THE BEAM.

Part: SELECTOR VALVE — INOPERATIVE (NLG) · airframe 34,499 hrs · 33,895 cycles

ON GEAR DOWN SELECTED, RECEIVED NOSE DOOR OPEN WARNING MESSAGE. MESSAGE DID NOT EXTINGUISH. AND GEAR DOORS FOUND OPEN AFTER LANDING. REMOVED AND REPLACED NLG DOOR SELECTOR VALVE IAW AMM 32-22-20. NLG OPS CHECKED GOOD AND LEAK CHECKED GOOD

Part: FLAP SYSTEM — FAILED · airframe 33,797 hrs · 33,239 cycles

FLAPS FAILED AT 5 DEGREES AFTER TAKEOFF DURING RETRACTION. DECLARED EMERGENCY, AND LANDED. RATE OF DESCENT WAS 200 FEET PER MINUTE. LANDING WAS SMOOTH AND UNEVENTFUL. ATTEMPTED RESET PROCEDURE IAW SUPPLEMENT 98-018G, FLAP FAIL MESSAGE RETURNED IMMEDIATELY AFTER BREAKERS WERE RESET.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 33,584 hrs · 33,048 cycles

ENROUTE, FL290, FLAP FAIL CAUTION AT FLAPS ZERO. AFTER LANDING BTMS READ 7,5,5,5.

Part: DOOR — BINDING (SERVICE) · airframe 33,193 hrs · 32,698 cycles

SERVICE DOOR WILL NOT OPEN FROM INSIDE OR OUTSIDE

Part: SERVICE DOOR — STUCK (CABIN) · airframe 32,903 hrs · 32,427 cycles

SERVICE DOOR WILL NOT OPEN FROM INSIDE OR OUTSIDE.

Part: HANDLE — OBSTRUCTED (SERVICE DOOR) · airframe 32,625 hrs · 32,165 cycles

SERVICE DOOR OUTER HANDLE IS DIFFICULT TO POP OUT. DOOR OPENS NORMAL WHEN HANDLE IS OUT. FOUND EXCESSIVE PRIMER ON OUTER DOOR HANDLE TARGET. REMOVED EXCESS PRIMER AND DOOR HANDLE OPERATES SMOOTHLY, REF AMM 52-40-00.

Part: HANDLE — DIRTY (SERVICE DOOR) · airframe 32,612 hrs · 32,151 cycles

SERVICE DOOR HANDLE WILL NOT OPEN FROM OUTSIDE. CLEANED AND LUBRICATED SERVICE DOOR OUTER HANDLE AS REQUIRED. OPS CHECK GOOD AT THIS TIME.

Part: LOCK — OBSTRUCTED (SERVICE DOOR) · airframe 32,473 hrs · 32,016 cycles

SERVICE DOOR HANDLE WILL NOT POP OUT FROM OUTSIDE. INSPECTED SERVICE DOOR OUTER HANDLE FOUND LATCH LOCK STICKING DUE TO PAINT OUR SPRAY BUILD UP AND DIRT. CLEANED OUTER HANDLE LOCK SWITCH AS REQUIRED. OPS CHECK GOOD IAW AMM 52-41-03.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,117 hrs · 31,686 cycles

EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROW 2 - 5. LT LOWER EMER EXIT SIGN SEAT 8A WILL NOT ILLUMINATE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,088 hrs · 31,660 cycles

FLOOR LEVEL EMER TRACK LIGHTING IS INOPERATIVE FROM ROW 2 - 5.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 31,460 hrs · 31,092 cycles

STRINGER 14R AT FRAME 625.30, HORIZONTAL STIFFENER TO FRAME, ATTACH ANGLE CRACKED, REPLACED.

Part: LANDING — GOUGED (ENTRY DOOR) · airframe 31,460 hrs · 31,092 cycles

MAIN ENTRY DOOR HINGE, AFT LAND IS GOUGED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,460 hrs · 31,092 cycles

FRAME 235 IS CRACKED, JUST BELOW THE RT WINDSHIELD POST SUPPORT FITTING, IN THE FLIGHT DECK.

Part: SKIN — CRACKED (LT WING) · airframe 31,460 hrs · 31,092 cycles

LEFT WING LOWER PLANK DRAIN HOLE AT WS 85.0, BETWEEN 14 & 15, IS CRACKED IN TWO PLACES.

Part: SKIN — DENTED (LT COWLING) · airframe 31,460 hrs · 31,092 cycles

LEFT ENG LOWER CORE COWL, EXTERNAL SKIN HAS DENT AT THE 11 O CLOCK POSITION, ADJACENT TO NACA VENT. REPAIRED IAW EA CRJ271-00262.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,460 hrs · 31,092 cycles

SEAT RAIL BEAM LBL 27, OTBD FLANGE HAS CORROSION, FS 574.00 - 620.00, INBD & OTBD FLANGE.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,460 hrs · 31,092 cycles

PASSENGER DOOR OPENING LOWER FRAME HAS CORROSION IN SPOTS, AT LONGERON LOWER ANGLE, BETWEEN FS 310 & 349, REPLACED.

Part: SUPPORT RIB — CRACKED (ENTRY DOOR) · airframe 31,460 hrs · 31,092 cycles

MAIN ENTRY DOOR AFT WEB SUPPORT RIB, IS CRACKED ON LOWER END AT DOOR ASSIST MECHANISM, REPLACED.

Part: ANGLE — CRACKED (ENTRY DOOR) · airframe 31,460 hrs · 31,092 cycles

MAIN ENTRY DOOR STAIR PANEL EDGE MEMBER HAS A CRACKED PREVIOUS REPAIR, REPLACED.

Part: DRAG ANGLE — CRACKED (ENTRY DOOR) · airframe 31,460 hrs · 31,092 cycles

MAIN ENTRY DOOR AFT DRAG ANGLE CRACKED. R & R AFT DRAG ANGLE IAW REO 601R-52-11-513 REV-B DATED 2015 07 05.

Part: SHROUD — CRACKED (RT WING) · airframe 31,460 hrs · 31,092 cycles

SHROUD FOR FUEL INLET ADAPTER IS CRACKED. R & R SHROUD FOR FUEL INLET ADAPTER IAW SRM 51-42-06 & 51-41-02.

Part: FITTING — CRACKED (FUSELAGE) · airframe 31,460 hrs · 31,092 cycles

RIGHT WINDSHIELD SIDE POST LOWER, OTBD AFT ANGLE FITTING IS CRACKED. REPAIRED RT WINDSHIELD SIDE POST LOWER OTBD AFT ANGLE FITTING IAW SRM 51-42-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 31,460 hrs · 31,092 cycles

FS 484.0 CLIP AT RBL 36 IS CRACKED. R & R CLIP AT FS 484.00 & RBL 36 IAW REO 601R-53-41-059.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 31,460 hrs · 31,092 cycles

CENTER WINDOW POST, LT LOWER LUG ATTACH FITTING CRACKED IN RADIUS, REPLACED.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 31,460 hrs · 31,092 cycles

PERFORM PERM REPAIR OF THE DENT ON THE LT FUSELAGE, BETWEEN FS 589 & 605, STRINGER 21L & 22, REPAIRED.

Part: FITTING — CRACKED (COCKPIT) · airframe 31,460 hrs · 31,092 cycles

LEFT WINDSHIELD SIDE POST, LOWER OTBD AFT ANGLE FITTING IS CRACKED, REPLACED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,460 hrs · 31,092 cycles

RIGHT AISLE SEAT TRACK STICK 3 HAS CORROSION, BETWEEN FS 409+128 - 559.00 IN CABIN. R & R SEAT TRACK FS 409+128 - FS 559.00 IAW AMM 53-01-11.

Part: SMOKE DETECTOR — FAULTY (CARGO BAY) · airframe 31,295 hrs · 30,942 cycles

SMOKE CARGO RED WARNING ON THE GND, NO FIRE DETECTED, CARGO BOTTLES NOT DEPLOYED. PERFORMED VISUAL INSPECTION OF CARGO COMPARTMENT & SMOKE DETECTORS, NO DEFECTS NOTED AT THIS TIME. NO PRESENCE OF SMOKE OR FLAME IN THE CARGO COMPARTMENT. CONFIRMED CARGO COMPARTMENT IS EMPTY, DEACTIVATED SMOKE DETECTORS IAW AMM 26-15-00, M ACTION COMPLIED WITH. REPLACED FWD CARGO SMOKE DETECTOR IAW AMM 26-15-01. OPERATIONS CHECKED OK. REMOVED PLACARD & MEL.

Part: CONTROL PANEL — FAULTY (ADG) · airframe 31,295 hrs · 30,942 cycles

ADG DEPLOYED INFLIGHT ON TAKEOFF AT 2,000 FEET. ENG & APU GENERATORS OPERATED NORMALLY. PILOT REPORTED LANDING UNEVENTFUL, UNDER MAX LANDING WEIGHT & DID NOT DECLARE EMER. PERFORMED VISUAL INSPECTION OF ADG STRUT & HOUSING. REF LP 259734 1 FOR ADG MEL & LP 259734 2 FOR NDT REQUIREMENT. LP 259734 1 TROUBLE SHOT IAW FIM 24-23-00, ADG AUTO DEPLOY CONTROL PANEL FAILS IN UNIT POSITION. R & R ADG AUTO DEPLOY CONTROL PANEL, OPERATIONS CHECKED GOOD. REMOVED PLACARD, RESET BREAKERS, REMOVED MEL. LP 259734 2 COMPLIED WITH LPI IAW EO E10 026 424, NO DEFECTS NOTED. REMOVED FROM MEL & REMOVED PLACARD.

Part: AILERON — BINDING (WING) · airframe 29,194 hrs · 28,890 cycles

AUTOPILOT ENGAGED, AILERON TRIM INDICATOR A, MANUALLY DISCONNECTED, AUTOPILOT HAD LT WING DOWN TENDENCY, BINDING AILERON & CLUNKING SOUND WHEN ACTUATED

Part: SEAL — CRACKED (SPOILER) · airframe 26,652 hrs · 26,509 cycles

CRACK FOUND UPON FLIGHT SPOILER INBD SPRING SEAL. R & R IAW SRM 51-40-11 & SRM 51-42-06.

Part: SUPPORT BRACKET — CRACKED (HYDRAULIC BAY) · airframe 26,652 hrs · 26,509 cycles

1000, 0024 HYD COMPARTMENT UPPER FWD HYD ACCUMULATOR SUPPORT BRACKET CRACKED.

Part: PANEL — CRACKED (THRUST REVERSER) · airframe 26,652 hrs · 26,509 cycles

SAM PANEL AT BLOCKER DOORS 9 & 10 ON RT ENG TORQUE BOX IS CRACKED. REPLACED SAM PANEL IAW CMM 78-30-00.

Part: SKIN — DENTED (FUSELAGE) · airframe 26,652 hrs · 26,509 cycles

DENT IN SKIN AT FS 625.3 TO 640 FROM STRINGER 21R TO 22R. REMOVED DAMAGED SKIN IAW NOTE 1 REO 601R-53-61-5150 REV A. INSTALL A DOUBLER IAW REO 601R-53-61-5150.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 26,652 hrs · 26,509 cycles

PASSENGER DOOR INTERCOSTAL UNDER PANEL 832BR IS CRACKED. R & R INTERCOSTAL PN 601R-31902-318 IAW CRJ 200 SRM 51-42-06, 51-42-21 & 51-40-11.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 26,652 hrs · 26,509 cycles

LT WING CTR PANEL LE RB ATTACH ANGLE CRACKED AT BOTTOM FASTENER HOLE. REMOVED DAMAGE PART & REINSTALLED NEW PN 600-12025-7.

Part: SKIN — CRACKED (LT WING) · airframe 26,652 hrs · 26,509 cycles

LEFT WING INBD LE OTBD ATTACH FLANGE CRACKED IN RADIUS. REMOVED DAMAGED FLANGE & INSTALLED NEW FW 600-12045-11.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 26,652 hrs · 26,509 cycles

INSTALLATION OF FWD LATCH ANGLE AT CARGO FLOOR SILL CRACK NOTED AT FWD OTBD FASTENING HOLE. CRACK DAMAGE CUT OUT & CHANNEL & FILLER INSTALLED IAW REO 601R-53-61-1741.

Part: SKIN — GOUGED (FUSELAGE) · airframe 26,652 hrs · 26,509 cycles

LEFT FUSELAGE 3 INCH GOUGE DAMAGE AT FS 409+16 & WK 73.50. CUT OUT DAMAGE, FABRICATED REPAIR DOUBLER & FILLER, NDT CUTOUT, APPLIED CORROSION PREVENTION TREATMENT, PRIMER SURFACE TREATMENT, FAY & FILLET SEALED, INSTALLED REPAIR DOUBLER & FILLER, RESTORED TOP COAT.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 26,652 hrs · 26,509 cycles

CARGO TIE DOWN TRACK AT RBL 9 & FS 559.112 CORRODED ENTIRE LENGTH. R & R TIE DOWN TRACK IAW CAJ 200 SRM 51-40-11 & 51-41-02.

Part: DOUBLER — CRACKED (PAX DOOR) · airframe 26,652 hrs · 26,509 cycles

PASSENGER DOOR FRAME INNER DOUBLER, PN 601R-318094-2, IS CRACKED. R & R DOUBLER.

Part: HINGE — GOUGED (FUSELAGE) · airframe 26,652 hrs · 26,509 cycles

PASSENGER DOOR HINGE HALF ON FUSELAGE HAS GOUGE & CHAFE ON AFT LUG LANDING. BLENDED OUT GOUGE & CHAFE & FOUND TO BE WITHIN LIMIT. REMAINING THICKNESS DOES NOT EXCEED LESS THAN .070 IAW REO 601R-53-21-2494.

Part: TIE DOWN — CORRODED (CARGO BAY) · corrosion level 2 · airframe 26,652 hrs · 26,509 cycles

FITTING CORROSION FOUND ON 2 CARGO TIE DOWN FITTINGS AT LBL 9 & FS 583 & 599.

Part: HANDLE — CRACKED (CARGO DOOR) · airframe 26,652 hrs · 26,509 cycles

CARGO DOOR HANDLE ASSEMBLY IS CRACKED & HAS GOUGE AROUND CUT OUT. R & R WITH SERVICEABLE CARGO DOOR HANDLE ASSEMBLY.

Part: BRACKET — CRACKED (LT MLG WW) · airframe 26,652 hrs · 26,509 cycles

LEFT MLG WW BRAKE PRESS TRANSDUCER BRACKET CRACKED, REPLACED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 26,652 hrs · 26,509 cycles

LEFT UPPER & RT LOWER OBLIQUE ANGLES CRACKED. R & R UNSERVICEABLE OBLIQUE ANGLES.

Part: MOUNT BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,653 hrs · 26,509 cycles

POINT TEST SWITCH MOUNTING BRACKET HAS CORROSION AT PUSH BUTTON. REMOVED & MANUFACTURED NEW MOUNTING BRACKET DUE TO SEVERE PITTING.

Part: DRAG ANGLE — CRACKED (LT MLG WW) · airframe 26,652 hrs · 26,509 cycles

LEFT MLG DING ANGLE COMMON TO BATT CRACKED. R & R DING ANGLE IAW CRJ 200 SRM 51-40-11.

Part: COMPUTER — INOPERATIVE (FUEL SYSTEM) · airframe 23,058 hrs · 22,998 cycles

FUEL CHANNEL 1 FAILED IN FLIGHT. CW FIM FAULT RESET MESSAGE DID NOT CLEAR. R & R FUEL SYS COMPUTER. OPS CHECKED GOOD IAW AMM 28-41.

Part: SKIN — CHAFED (LT AILERON) · airframe 22,001 hrs · 21,952 cycles

LEFT AILERON UPPER SKIN CHAFED AND GOUGED. INSTALLED SERVICEABLE LT AILERON L/E SKIN IAW REO 601R-57-61-023 & SRM 51-42-06, 51-42-21.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 22,001 hrs · 21,952 cycles

PAX DOOR EXTERNAL HANDLE PUSH IN DOOR CRACKED. REMOVED UNSERVICEWABLE PAX DOOR EXTERNAL PUSH IN DOOR WITH NEW SERVICEABLE PAX DOOR EXTERNAL PUSH IN DOOR ASSY.

Part: NUT PLATE — BROKEN (WING) · airframe 22,001 hrs · 21,952 cycles

BROKEN NUT PLATE TAB UNDER PANEL 326CR. REPLACED UNSERVICEABLE NUT PLATE TAB WITH NEW SERVICEABLE NUT PLATE TAB.

Part: BRACKET — DAMAGED (SERVICE DOOR) · airframe 22,001 hrs · 21,952 cycles

BRACKET AT FS 310 AT SVC DOOR SURROUND STRUCTURE IS DAMAGED ( FWD SIDE OF DOOR) ALSO WRONG HARDWARE ON BRACKET FABRICATED NEW BRACKET IAW SRM 51-42-16, INSTALLED NEW BRACKET IAW SRM 51-42-21.

Part: FLOORBEAM — CORRODED (FS 524-321) · corrosion level 2 · airframe 22,001 hrs · 21,952 cycles

LBL 27, FLOORBEAM CAP HAS CORROSION AROUND NUTPLATE HOLES FROM FS 574.00 TO FS 621.00. COMPLIED WITH REO 601R-53-00-005 BY INSTALLING SERVICEABLE FLOORBEAM CAP FROM FS 574.00 TO FS 615.00. C/W REO 601R-53-61-4336 BY INSTALLING A STRAP DOUBLER & 2 TAPERED SHIMS AT FS 618.00.

Part: MOUNT BRACKET — CRACKED (PAX DOOR) · airframe 22,001 hrs · 21,952 cycles

PAX DOOR ASSIST MOTOR MOUNTING BRACKET. R & R PAX DOOR ASSIST MOUNTING BRACKET WITH NEW SERVICEABLE BRACKET IAW SRM 51-42-06.

Part: GUIDE — WORN (PAX DOOR) · airframe 22,001 hrs · 21,952 cycles

FWD ROLLER GUIDE ON PAX DOOR IS WORN. REPAIRED GUIDE PLATE IAW REO 601R-52-11-296.

Part: HINGE — DAMAGED (PAX DOOR) · airframe 22,001 hrs · 21,952 cycles

PAX DOOR PIANO HINGE LUGS HAVE SCRATCHES AND GROVES ON HINGE HALF. BLENDED OUT GOUGES IAW REO 601R-52-11-1347.

Part: ROD — CHAFED (INBD FLAP VANE) · airframe 22,001 hrs · 21,952 cycles

INBD FLAP VANE ACTUATOR ROD ON INBD FLAP IS CHAFED/WORN FROM ROLLERS BLENDED & SMOOTHES MINOR CHAFING IAW SRM 51-12-00 IAW REO 601R-57-52-1843. POLISHED BLENDING AREA TO 125, R & R SMOOTHERS.

Part: FLOORBEAM — CRACKED (BS 489) · airframe 22,001 hrs · 21,952 cycles

CLIPS AT FS 484 ARE CRACKED LBL 27 AND LBL 37. R & R CLIP IAW REO 601R-53-41-059, REV.

Part: SKIN — CRACKED (PAX DOOR) · airframe 22,001 hrs · 21,952 cycles

SKIN AT FWD PULL IN LEVER CRACKED. REPAIRED SKIN IAW REO 601R-52-11-2041.

Part: ARM — CRACKED (RT WING TE FLAP) · airframe 22,001 hrs · 21,952 cycles

RIGHT OTBD FLAP CENTER HINGE ARM OTBD SUPPORT CRACKED. DUPLICATED & INSTALLED SERVICEABLE CENTER HINGE ARM OTBD SUPPORT IAW SRMS 51-40-11, 51-42-15, 51-42-06, 51-21-11, 51-25-06, 51-25-16.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 22,001 hrs · 21,952 cycles

FLOORBEAM CRACKED AT FS 484, RBL 37. R & R IAW REO 601R-53-41-059, REV B.

Part: FLOORBEAM — CRACKED (FS 280) · airframe 22,001 hrs · 21,952 cycles

RBL 9 AND LBL 9 ANGLE CRACKED ON FS 280 CROSSBEAM. R & R RBL9 & LBL9 ANGLE AT FS 280 IAW SRM 51-24-16 & SRM 51-42-21.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 22,001 hrs · 21,952 cycles

LEFT INBD FLAP VANE CHAFED ON L/E AND ALOS ON UPPER SKIN. C/W REO 601R-57-52-004.

Part: SKIN — SCRATCHED (L/E NOSE INLET) · airframe 22,001 hrs · 21,952 cycles

RT ENGINE NOSE INLET L/E HAS A SCRATCH & SEVERAL PITTS ON INBD UPPER & LOWER. BLENDED PITTING AND SCRATCH ON RT ENG NOSE INLET WITHIN LIMITS IAW REO 601R-71-61-2532.

Part: TRUNNION — DAMAGED (LEFT) · airframe 22,001 hrs · 21,952 cycles

LEFT MLG LOWER TRUNNION HAS OVERSIZE HOLE (FWD HOLE). REPAIRED IAW REO 601R-57-21-1594, REV.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 22,001 hrs · 21,952 cycles

RT INBD FLAP VANE L/E CHAFED ON UPPER SKIN AT 1/B SIDE C/W REO 601R-57-52-004, REV C BY BLENDING IAW SRM 51-12-00. FOUND TO BE IN SERVICEABLE LIMITS IAW REO 601R-57-52-004, REV C.

Part: STOP FITTING — CRACKED (FS 589) · airframe 22,001 hrs · 21,952 cycles

FWD CARGO DOOR STOP FITTING CLIP CRACKED. R & R CLIP IAW SRM 53-61-23.

Part: STAND OFF — CRACKED (FIRE LOOP) · airframe 21,885 hrs · 21,834 cycles

RT JETPIPE FAIRING FIRE LOOP FWD SHIELD FWD STANDOFF HAS A CRACKED ATTACHMENT ANGLE. R & R ATTACHMENT ANGLE PN 228-50181-285 AND STANDOFF PN WSI4A12-5 IAW SRM 51-24-06.

Part: BULKHEAD — CRACKED (BS 202.95) · airframe 22,001 hrs · 21,952 cycles

FRAME STATION 202 FWD PRESSURE BULKHEAD CRACKED WHERE BRAKE ROD RUNS THROUGH BULKHEAD IN FWD HYD COMPARTMENT COMPLIED WITH REO 601R-53-11-563.

Part: ANGLE — CRACKED (FS 625) · airframe 22,001 hrs · 21,952 cycles

LEFT FS 625 OBLIQUE ANGLE CRACKED. R & R ANGLE PN 601-35012-51 IAW SRM 51-42-21 & 51-40-11 AND REO 601R-53-61-422.

Part: ANGLE — CRACKED (FS 625) · airframe 22,001 hrs · 21,952 cycles

RT FS 625 OBLIQUE ANGLE CRACKED. R & R ANGLE IAW SRM 51-42-21 & 51-40-11 AND REO 601R-53-61-422, REV NC.

Part: RETAINER — DEBONDED (NAC HEAT SHIELD) · airframe 22,001 hrs · 21,952 cycles

LT LOWER CORE COWL HEAT SHIELD HAS AREAS AND DEBONDED. FABRICATED AND INSTALLED RETAINER STRIP ON LT LOWER CORE COWL HEAT SHIELD IAW CMM 71-12-01.

Part: BRACKET — CRACKED (RT MLG WW) · airframe 22,001 hrs · 21,952 cycles

RT MLG WHEEL WELL BRAKE PRESSURE TRANSDUCER BRACKET CRACKED. R & R RT MLG WHEEL WELL TRANSDUCER BRACKET IAW SRM 51-42-06.

Part: UNKNOWN — ODOR (CABIN) · airframe 21,736 hrs · 21,682 cycles

F/A REPORTS BURNED POPCORN ODOR IN FLIGHT FROM ROW 8 AFT. PERFORMED OPS CHECK OF PACK 1 & 2 WITH ENGINE AND APU BLEEDS, IAW AMM 21-50-00. NO ODOR NOTED AT ANY SECTION OF CABIN.

Part: FIRE BOTTLE — DISCHARGED (CARGO BAY) · airframe 18,119 hrs · 17,862 cycles

CARGO BOTTLE LOW CAUTION MSG ON TAXI OUT, C/W`D QRH SMELLED ODOR IN COCKPIT, PERFORMED EMERGENCY EVACUATION ONTO RAMP. R & R LT CARGO BOTTLE IAW AMM 26-25-04. OPS CK GOOD. NO LKS NOTED AT THIS TIME.

Part: THRUST REVERSER — MALFUNCTIONED (RT ENGINE) · airframe 17,502 hrs · 17,210 cycles

RT REV UNLOCK CAUTION MSG IN FLT. AFTER T/R`S HAD BEEN SELECTED OFF. RT THRUST REVERSER REMOVED ALONG WITH RT ENGINE CHANGE NEW THRUST REVERSER OP CHECKS GOOD AT THIS TIME.

Part: SWITCH — MALFUNCTIONED (THRUST REVERSER) · airframe 17,502 hrs · 17,210 cycles

R & R REV UNLOCK MESSAGE CLIMBING THROUGH 15,000 FT, COMPLIED WITH QRH. REF LOG: 202457/2 - REPLACED RT T/R STOW SWITCH IAW AMM 78-37-01. OPS CHECKS AT THIS TIME. REMOVED PLACARD, REMOVED FROM MEL.

Part: SKIN — DAMAGED (BS 295) · airframe 17,439 hrs · 17,143 cycles

SKIN UNDER UPPER TCAS ANTENNA HAS A MISDRILLED START ON BOTTOM SIDE OF SKIN UNDER AFT LT NUTPLATE DOUBLE REPAIRED DAMAGE IAW REO 601R-53-21-1156.

Part: BRACKET — CRACKED (THRUST REVERSER) · airframe 17,439 hrs · 17,143 cycles

R/G ENG THRUST REVERSER TORQUE BOX SAM PANEL ATTACH BRACKET RIVET HAS EVIDENCE OF A CRACK FROM UNDER RIVET HEAD AT 7:00 POSITION. REPAIRED IAW REO 601R-78-30-3981.

Part: BRACKET — CRACKED (THRUST REVERSER) · airframe 17,439 hrs · 17,143 cycles

RT ENG THRUST REVERSER TORQUE BOX ATTACH BRACKET RIVET HAS EVIDENCE OF CRACK FROM UNDER RIVET HEAD AT 5:00 POSITION. REPAIRED IAW REO 601R-78-30-3981.

Part: PANEL — CRACKED (PAX DOOR) · airframe 17,439 hrs · 17,143 cycles

PAX DOOR STAIR FWD PANEL AT 3RD STEP FROM BOTTOM CORNER RADIUS IS CRACKED. PAX DOOR AT FS 320.0 AND BETWEEN DATUM NR 1 AND NR 4. CUT OUT DAMAGE AND INSTALL FILLERS AND DOUBLER IAW REO 601R-52-11-702.

Part: SKIN — CHAFED (LT AILERON) · airframe 17,439 hrs · 17,143 cycles

LT AILERON UPPER AND LOWER L/E`S ARE CHAFED. BLENDED LOWER SKIN IN LIMITS (REO 601R-57-60-020) UPPER SKIN OUT OF LIMITS - REPLACE SKIN.

Part: RIB — CRACKED (LT WING) · airframe 17,439 hrs · 17,143 cycles

LT BATT RIB IS CRACKED IN LT WHEEL WELL. REPAIR LT BATT RIB IAW REO 601R-57-51-046.

Part: FRAME — CRACKED (BS 559) · airframe 17,439 hrs · 17,143 cycles

FS 559 LBL 9 OTBD HAS CRACK FROM BOTTOM RIVET TO EDGE. VERTICAL POST AT LBL9. REPAIRED BY INCORPORATION OF REO`S 601R-53-41-260 AND 601R-53-41-609.

Part: TRACK — GOUGED (THRUST REVERSER) · airframe 17,439 hrs · 17,143 cycles

RT THRUST REVERSER LOWER INBD SLIDE TRACK IS GOUGED ON AFT ATTACH LUG, R&R RT THRUST REVERSER LOWER INBD SLIDER TRACK IAW SHORTS CMM 78-34-11.

Part: LUG — GOUGED (THRUST REVERSER) · airframe 17,439 hrs · 17,143 cycles

RT T/R LOWER INBD ATTACH LUGS FOR SLIDER TRACK ARE GOUGED 0.055" DEEP. R & R RT TR LOWER INBD ATTACH LUG FOR SLIDER TRACK.

Part: FLOOR SKIN — GOUGED (BS 540) · airframe 17,439 hrs · 17,143 cycles

GOUGE TO FLOOR SKIN UNDER FUEL PRESSURE BOX. (CAUSED BY A SCREW TRAPPED BETWEEN THE SKIN AND THE FUEL PRESSURE BOX). CUT OUT DAMAGE AND INSTALL SHIMS AT A DOUBLER IAW 601R-53-41-1185.

Part: RIB — CRACKED (RT WING) · airframe 17,439 hrs · 17,143 cycles

RT BATTERY RIB IS CRACKED IN RT WW. REPAIRED DAMAGE IAW REO 601R-57-51-046.

Part: STRUCTURE — CRACKED (BS 484) · airframe 17,439 hrs · 17,143 cycles

FS 484 AND RBL 18 HAS CRACK ON INBD CLIP R & R CLIP WITH NEW AIW SRM 51-42-06, 51-42-21.

Part: ACM — ODOR (RT) · airframe 16,314 hrs · 16,007 cycles

SMOKE IN REAR OF CABIN WITH ELECTRICAL ODOR. REMOVED AND REPLACED AIR CYCLE MACHINE IAW 21-51-10. OPS CHECK GOOD.

Part: ABRASION STRIP — CONTAMINATED (TE FLAPS) · airframe 16,003 hrs · 15,693 cycles

ACFT ROLLS TO RIGHT WHEN FLAPS ARE EXTENDED TO 45 DEG. REQ`D JUST UNDER 50 PERCENT STRAIGHT/LEVEL FLT ON APPROACH. REMOVED PAINT AND PAINTED FLAPS LEADING EDGE TEFLON ABRASION STRIP IAW SRM 51-25-26 AND REO 601R-51-25-002. OPS CK OF FLAPS GOOD. (K)

Part: TRIM SWITCH — INTERMITTENT (COCKPIT) · airframe 14,276 hrs · 14,035 cycles

FIRST OFFICERS STAB TRIM SWITCH INTERMITTENT IN FLIGHT. R&R FIRST OFFICERS STAB TRIM SWITCH IAW AMM 27-41-05. OPS CHECK GOOD.

Part: OIL SYSTEM — LOW PRESSURE (LT ENGINE) · airframe 13,801 hrs · 13,586 cycles

LT ENGINE OIL PRESSURE MESSAGE IN CRUISE, COMPLIED WITH QRH AND SHUTDOWN ENGINE, DIVERTED. OIL PRESSURE INDICATING BETWEEN 10 AND 20 PSI REGARDLESS OF THROTTLE POSITION. RED WARNING EXTINGUISHED AFTER THROTTLE IDLE BUT FLICKERED ON AND OFF. CORRECTIVE ACTION IN PROGRESS. (K)

Part: UNKNOWN — ODOR (COCKPIT) · airframe 13,061 hrs · 12,881 cycles

ELECTRICAL ODOR WHILE AT GATE. PACKS ON APU BLEEDS. NOTED SCENT FROM LEFT SIDE FIRST. INSPECTED LIGHTS IN FLIGHT DECK, NO ODOR DETECTED, PERFORMED ENGINE FIRE TEST, NO ODOR OR DEFECTS DETECTED. INSPECTED AVIONICS BAY, NO SMOKE OR ODOR DETECTED. NO ELECTRICAL ODOR COMING FROM EITHER PACK WITH APU AIR OR ENGINE AIR. NO ODOR DETECTED WHEN WINDOW HEAT OR PITOT HEAT SELECTED ON, NO ODOR DETECTED WHEN SELECTING THRU FANS, DISPLAY OR ARINC. AIRCRAFT OK FOR SERVICE. (A)

Part: SKIN — DAMAGED (LT AILERON) · airframe 12,735 hrs · 12,561 cycles

LT AILERON LEADING EDGE UPPER SKIN FOUND ABRADED. LT AILERON LEADING EDGE UPPER SKIN SHROUD REPLACED IAW CRJ 200 SRM 51-42-21. (M)

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 12,735 hrs · 12,561 cycles

CRACK FOUND ON HYDRAULIC SUPPORT BRACKET ON MLG BAY LEFT. NEW SUPPORT BRACKET ON MLG BAY INSTALLED IAW SRM 51-42-06. (M)

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 12,735 hrs · 12,561 cycles

CRACK FOUND ON PAX DOOR STAIR AFT DRAG ANGLE. AFT DRAG ANGLE REPAIRED IAW REO 601R-52-11-513 REV A. (M)

Part: BRACKET — CRACKED (BS 625 S14R) · airframe 12,735 hrs · 12,561 cycles

CRACK FOUND ON BRACKET OF INTERCOSTAL FS 625 STRINGER 14RT. BRACKET ON INTERCOSTAL FS 625 STRINGER 14 RT REMOVED AND REPLACED IAW CRJ 200 SRM 51-42-21. (M)

Part: SUPPORT BRACKET — CRACKED (BS 718) · airframe 12,735 hrs · 12,561 cycles

CRACK FOUND ON HYDRAULIC MANIFOLD SUPPORT BRACKET FS 718. REPAIRED IAW REO 601R-53-02-031 REV A. (M)

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 12,735 hrs · 12,561 cycles

CRACK EXISTS ON INTERCOSTAL FS 484 LBL 27. ATTACH FITTING ON INTERCOSTAL AT FS 484 LBL 27 REMOVED AND REPLACED IAW CRJ 200 SRM 51-42-06 AND 51-42-21. (M)

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 12,735 hrs · 12,561 cycles

CRACK FOUND ON HYDRAULIC SUPPORT BRACKET ON MLG BAY RT FORWARD. NEW SUPPORT BRACKET ON MLG BAY INSTALLED IAW SRM 51-42-06. (M)

Part: FRAME — CRACKED (BS 280) · airframe 12,735 hrs · 12,561 cycles

CRACK FOUND ON FRAME FS 280 RBL 9 AND BRACKET INBOARD. FLOOR STRUCTURE REPAIRED IAW REO 601R-53-11-171 REV D. (M)

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 12,735 hrs · 12,561 cycles

CRACK EXIST ON INTERCOSTAL FS 484 RBL 36. REPAIRED IAW REO 601R-53-41-059 REV A. (M)

Part: FRAME — CRACKED (BS 280) · airframe 12,735 hrs · 12,561 cycles

CRACKS EXISTS ON FRAME FS 280 LBL 9. REPAIR ON FLOORBEAM AT FS 280 LBL 9. PERFORMED IAW REO 601R-53-11-171 REV D. (M)

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 12,735 hrs · 12,561 cycles

CRACK FOUND ON HYDRAULIC SUPPORT BRACKET ON MLG BAY RT. SUPPORT BRACKET ON RT MLG BAY FABRICATED AND INSTALLED IAW REO 601R-83-42-007 REV A. (M)

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT)

DURING TAKEOFF ROLL, GOT CONFIG SPOILERS AND CONFIG TRIM WARNINGS. ABORTED TAKEOFF BELOW 60 KNOTS, ALL TRIM SHOWING IN GREEN. NO SPOILERS SHOWED DEPLOYED. COMPLIED WITH FIM PROCEDURE IAW 27-60, OPS CHECK GOOD. VISUALLY INSPECTED ALL SPOILER AND AILERON PCU`S AND POSITION TRANSMITTERS FOR SECURITY IAW CHAP 27, NO FAULTS FOUND. COMPLIED WITH OPS CHECK AND TAKEOFF CONFIG CHECK IAW CHAPTER 27, OPS CHECK GOOD. (M)

Part: ACM — LEAKING (A/C BAY)

FUEL SMELL NOTICED IN ENVIRONMENTAL SYSTEM WITH BLEEDS ON APU OR ENGINE. INSPECTED ECS SYSTEM AND FOUND LEFT AIR CYCLE MACHINE TO BE LEAKING OIL SEVERELY. NO OIL IS LEFT IN ACM. REPLACED ACM PER AMM 21-51-10. OPS CHECKS GOOD. SMELL IS GONE. (M)

Part: SOLENOID — UNKNOWN (APU)

EN ROUTE AT CRUISE WHEN COCKPIT A/C WAS SELECTED WARMER A STRONG SMELL OF WHAT APPEARED TO BE FUEL WAS OBSERVED THROUGH THE COCKPIT ECS SYSTEM WHEN TEMP CONTROLLER WAS MOVED BACK TO COLD THE ODOR WENT AWAY AND WAS NOT OBSERVED ANYMORE. REMOVED AND REPLACED FUEL VALVE SOLENOID ON APU. RAN PACKS FROM ENGINE AND APU. FUEL SMELL NOT PRESENT, WATER SEPARATOR IS CLEANED. (M)

Part: PRESSURE VALVE — ODOR (A/C SYSTEM) · airframe 8,511 hrs · 8,476 cycles

DURING FLIGHT, HAD FUEL SMELL COMING FROM AIR CONDITIONING. APU NOT RUNNING. TROUBLESHOT FUEL SMELL DOWN TO ENGINE NR 1 EXCEPT SMELL IS NOT FUEL, BUT OIL. ISOLATED OIL SMELL COMING ONLY FROM ENGINE NR 1 WITH EITHER PACK RUNNING. WITH ENGINE NR 2 OR APU RUNNING PACKS THERE IS NO APPARENT SMELL BUT WITH PATH NR 1 OR NR 2 RUNNING FROM ENGINE NR 1 THERE IS A STRONG BURNED OIL SMELL COMING OUT OF THE PACK VENT. (K)

Part: SOLENOID VALVE — LEAKING (APU)

SMELL OF RAW FUEL COMING FROM ECS SYSTEM EN ROUTE WITH APU NOT OPERATING. SEEMS STRONGEST WITH LT PACK TEMP IS INCREASED. FUEL SMELL AFTER ENGINE START BUT ONLY LASTED FOR SECONDS. REMOVED AND REPLACED APU FUEL SHUTOFF SOLENOID VALVE IAW 49-31-05. OPS CHECK GOOD. NO SMELL NOTED. (M)

Part: THERMAL SWITCH — INOPERATIVE (WING) · airframe 7,751 hrs · 7,749 cycles

DEPARTED, WING ANTI-ICE SELECTED ON, (ANTI-ICE DUCT) CAS MESSAGE AND AURALWARNING CAME ON, RETURNED. LT WING L/E SHOWED RED ON SYNOPTIC PAGE. REMOVED AND REPLACED THERMAL SWITCHES ON LT WING. C/W POWER RUNS. NO DEFECTS NOTED AT THIS TIME.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 7,748 hrs · 7,745 cycles

LT FLOOR SUPPORT ANGLE AT FS 621 CRACKED. MAINTENANCE INSTALLED STRAP AND REPAIRED ANGLE IAW REO. (K)

Part: BATTERY PACK — DEFECTIVE (CABIN) · airframe 7,806 hrs · 7,799 cycles

WARDROBE FLOOR LEVEL FLOODLIGHT AND BOTH LT AND RT FWD OVERWING EXT EMERGENCY LIGHTS DO NOT ILLUMINATE. FOUND NR 2 EMERGENCY BATTERY TO BE DEFECTIVE. REMOVED NR 2 BATTERY PACK AND INSTALLED SERVICEABLE BATTERY PACK IAW AMM. OPERATIONAL CHECK GOOD. (K)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

LT FS484.00 INTERCOSTAL AT LBL36.0 HAS A .2500 INCH CRACK AT TOP OF ANGLE. MAINTENANCE REMOVED CRACKED FLANGE IAW REO. COMPLIED WITH STEP 3 OF REO, PERFORMED EDDY CURRENT OF LT FS 484 INTERCOSTAL REPAIR. NO INDICATIONS NOTED AT THIS TIME. (K)

Part: B-NUT — LOOSE (APU FUEL SYS) · airframe 6,724 hrs · 6,757 cycles

WHILE APU RUNNING HEARD LOUD BANG NOISE FROM REAR OF AIRCRAFT. APU RPM DROPPED BY 10 PERCENT. FLIGHT ATTENDANT NOTICED SMELL OF FUEL IN REAR OF AIRCRAFT. NO INDICATION OF FIRE. SHUTDOWN APU. INSPECTED APU, FOUND LOOSE B-NUT ON FUEL SOLENOID. RETORQUED B-NUT. NO FURTHER FUEL LEAKS NOTED. ATTEMPTED TO START APU. HAGS AT 49 PERCENT, PLACED ON MEL. (K)

Part: SMOKE DETECTOR — MALFUNCTIONED (AFT CARGO BAY)

UPON CARGO SMOKE DETECTOR TEST, SMOKE DETECTOR MESSAGE WOULD NOT GO OUT. REMOVED AND REPLACED CARGO FIRE SMOKE DETECTOR IAW AMM 26-15-01, OPS CHECK GOOD AT THIS TIME. (M)

Part: APU — FAILED (APU BAY) · airframe 4,933 hrs · 5,154 cycles

APU FAILED AND SHUTDOWN ON TAKEOFF ROLL AND ROTATION. TRIED TO RELIGHT ON DESCENT, RAN APPROXIMATELY 3 MINUTES AND SHUTDOWN. STRONG FUEL SMELL PRESENT IN CABIN. PERFORMED APU OPS CHECK IAW AMM. INSPECTED AND FOUND NO EVIDENCE OF FUEL LEAK. NO FAULTS ON ECU. OK FOR CONTINUED SERVICE. (K)

Part: CONTROL UNIT — MALFUNCTIONED (E/E BAY) · airframe 4,661 hrs · 4,910 cycles

MACH TRIM CAUTION MESSAGE IN FLIGHT. COMPLIED WITH QRH, MESSAGE RE-OCCURRED. REMOVED AND REPLACED HORIZONTAL STAB TRIM CONTROL UNIT. OPS CHECK GOOD.

Part: PANEL — DAMAGED (FUSLEAGE)

ONE FASTENER HOLE ELONGATED FOR ATTACHING PANEL 131AL. REAMED HOLE FABRICATED FREEZE PLUG FROM 2025-T6 .3332 DIAMETER AND INSTALLED IAW BOMBARDIER, INC REO 601R-53-11-162. (M)

Part: SKIN — DAMAGED (FUSELAGE)

FOUND DENT AND CREASE IN FUSELAGE SKIN AT FS 760 BETWEEN STRINGERS 8R AND 9R. REMOVED DAMAGE, FABRICATED EXTERNAL DOUBLER FROM 2024-T3 .050 INCH, AND INSTALLED EXTERNAL DOUBLER IAW BRAS EO 601R-53-5200B. (M)

Part: BUSHING — MIGRATED (LT MLG TRUNNION)

FOUND LEFT MLG AFT TRUNNION BUSHING MIGRATED .006 NCH. REMOVED MIGRATED BUSHING. REAMED TRUNNION LUG BORE TO 1ST OVERSIZE AND INSTALLED 1ST OVERSIZE BUSHING IAW REO 601R-57-21-003 REV B. (M)