N439AW

ATA 5330

RH AFT FUSELAGE HAS DENTS. AIRCRAFT REMOVED FROM SERVICE. PERFORMED REPAIR ON RH FUSELAGE SKIN BETWEEN FS 625.30 TO FS672.20 STR 20-23R IAW MHIRJ REO 601R-53-61-8276 REV -- DATED 2025-02-04.

ATA 2120

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.

ATA 3220

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.

ATA 3222

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.

ATA 3230

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

ATA 3244

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

ATA 3230

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.

ATA 2700

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.

ATA 2797

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.

ATA 2751

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.

ATA 3197

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.

ATA 5344

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

ATA 5344

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

ATA 5200

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

ATA 5532

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.

ATA 5344

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.

ATA 5344

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.

ATA 5300

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.

ATA 5300

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.

ATA 5300

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.

ATA 5300

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.

ATA 5344

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.

ATA 5324

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

ATA 5344

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.

ATA 5300

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

ATA 5300

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.

ATA 5324

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.

ATA 5344

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.

ATA 5200

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.

ATA 5300

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

ATA 3400

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.

ATA 5300

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.

ATA 5521

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.

ATA 5300

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.

ATA 5522

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.

ATA 5300

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.

ATA 5700

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.

ATA 5300

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.

ATA 5270

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.

ATA 5512

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

ATA 5513

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

ATA 3250

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

ATA 5312

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.

ATA 2211

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

ATA 2750

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.

ATA 2750

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,

ATA 2750

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.

ATA 3241

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.

ATA 2220

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

ATA 5330

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

ATA 5320

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

ATA 5311

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

ATA 5320

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

ATA 5210

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

ATA 5315

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

ATA 5320

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

ATA 5320

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

ATA 5320

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

ATA 5320

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

ATA 5320

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

ATA 5320

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

ATA 5410

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

ATA 5410

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

ATA 5230

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.

ATA 3230

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

ATA 2750

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.

ATA 2750

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

ATA 5240

SERVICE DOOR WILL NOT OPEN FROM INSIDE OR OUTSIDE

ATA 5240

SERVICE DOOR WILL NOT OPEN FROM INSIDE OR OUTSIDE.

ATA 5240

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.

ATA 5240

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

ATA 5240

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.

ATA 3350

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

ATA 3350

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

ATA 5313

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

ATA 5311

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

ATA 5347

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

ATA 5210

MAIN ENTRY DOOR HINGE, AFT LAND IS GOUGED.

ATA 7110

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

ATA 5730

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

ATA 5320

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

ATA 5210

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

ATA 5210

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

ATA 5210

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

ATA 5740

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

ATA 5340

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.

ATA 5340

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

ATA 5340

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

ATA 5320

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

ATA 5320

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

ATA 5347

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.

ATA 2611

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.

ATA 2420

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.

ATA 2710

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

ATA 5755

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

ATA 5320

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

ATA 7830

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

ATA 5330

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.

ATA 5320

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.

ATA 5730

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

ATA 5720

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

ATA 5210

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

ATA 5330

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.

ATA 5320

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.

ATA 5347

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.

ATA 5344

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.

ATA 2550

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

ATA 5230

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

ATA 5320

LEFT MLG WW BRAKE PRESS TRANSDUCER BRACKET CRACKED, REPLACED.

ATA 5320

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

ATA 5340

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

ATA 5320

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

ATA 2840

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.

ATA 5751

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.

ATA 5740

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

ATA 5210

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.

ATA 5315

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.

ATA 5240

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.

ATA 5753

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.

ATA 5344

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

ATA 5340

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

ATA 5210

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

ATA 5753

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.

ATA 5315

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

ATA 5315

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

ATA 5210

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

ATA 5320

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

ATA 7160

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.

ATA 5753

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

ATA 5743

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

ATA 5315

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.

ATA 5753

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.

ATA 5420

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.

ATA 5312

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

ATA 5320

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.

ATA 5320

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.

ATA 5410

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.

ATA 5340

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

ATA 2120

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.

ATA 2620

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.

ATA 7830

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.

ATA 7830

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.

ATA 5330

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.

ATA 7830

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.

ATA 7830

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.

ATA 5210

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.

ATA 5712

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

ATA 7830

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.

ATA 5321

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.

ATA 5751

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.

ATA 5311

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.

ATA 7830

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.

ATA 5712

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

ATA 5320

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

ATA 2150

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

ATA 5753

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)

ATA 2740

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

ATA 7930

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)

ATA 2120

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)

ATA 5751

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

ATA 5340

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

ATA 5340

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

ATA 5310

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

ATA 5340

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)

ATA 5320

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)

ATA 5311

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

ATA 5340

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)

ATA 5311

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)

ATA 5320

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

ATA 5340

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

ATA 3150

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)

ATA 2150

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)

ATA 4930

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)

ATA 2140

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)

ATA 4930

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)

ATA 3010

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.

ATA 5320

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

ATA 3350

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)

ATA 5320

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)

ATA 4930

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)

ATA 2611

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)

ATA 4920

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)

ATA 2740

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

ATA 5330

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)

ATA 5300

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)

ATA 5743

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)