N438AW

Part: PDU — FAILED (TE FLAPS) · airframe 43,261 hrs · 43,228 cycles

RECEIVED FLAP FAIL CAUTION MSG ON APPROACH TO LAND WHEN SELECTING FLAPS 30 FROM 20. FLAPS FAILED AT 20. FLAPS WER ON MEL. AIRCRAFT REMOVED FROM SERVICE. R & R FLAP PDU IAW AMM 27-52-01 FLAP PDU OPS TEST GOOD.

Part: WHEEL — UNKNOWN (NLG) · airframe 43,160 hrs · 43,120 cycles

UPON APPLYING TAKE-OFF POWER, AIRCRAFT YAWED HARD TO THE RIGHT, FULL LEFT RUDDER WOULD NOT COUNTERACT YAW. REJECTED TO PERFORMED. ON TAXI BACK TO HANGAR AC YAWED RIGHT WITH NO RUDDER / TILLER INPUT. BTMS SHOWED 2,1,1,1. AIRCRAFT REMOVED FROM SERVICE. REF LP 373747 BLOCKS 2 & 3 FOR NLG TIRE CHENGE. PERFORMED TAXI CHECK PER AMM 09-20. GOOD FOR CONTINUED SERVICE. R & R NR 1 & 2 NLG TIRE IAW AWA SUPP 12-016M COMPLIED WITH THE M061 INSTRUCTIONS, THE SPACER &WASHER WERE RETAINED FROM THE REMOVED WHEEL ASSEMBLY AND USED ON THE INSTALLED WHEEL. R&R #2 NLG TIRE IAW AWA SUPP 12-016M COMPLIED WITH THE M061INSTRUCTIONS,

Part: IDG — FAULTED (RT ENGINE) · airframe 42,629 hrs · 42,467 cycles

ABORTED TAKE OFF DUE TO IDG 2 CAUTION MSG. CAUTION MSG CLEARED WHEN POWER BROUGHT BACK TO IDLE. QRH NOT PERFORMED. AIRCRAFT REMOVED FROM SERVICE. C/W M ACTION FOR MEL 24-11-01-01. REF 365898-3 FOR MEL IN WORK. REFERENCE WORK ORDER 337826 MAINTENANCE WORKCARD # 9-10. REMOVED AND REPLACED RIGHTHAND IDG. OPS CHECK GOOD AT THIS TIME. REMOVED PLACARD & FROM MEL.

Part: SKIN — DENTED (BS 574-621) · airframe 42,008 hrs · 41,722 cycles

DENTS ON RH FUSELAGE LOW PRESSURE GROUND AIR CONDITIONING CONNECTION. AIRCRAFT REMOVED FROM SERVICE. ACCOMPLISHED REPAIR OF AFT LOWER FUSELAGE SKIN AT FS 574.0 TO FS621 BETWEEN STR 20R TO 24L IAW REO 601R-53-61-8143. REV DATED 2024-03-06. HFEC ACCOMPLISHED, AND ALL FINISHES RESTORED IAW REO 601R-53-61-8143. AERSALE WORK ORDER 004164, CARD NO 50027, CID2099709. TT: 42008:52, TC: 41722.

Part: SKIN — DENTED (RT WING LE) · airframe 42,008 hrs · 41,722 cycles

DENTS ON R/H WING OUTBOARD LEADING EDGE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED R/H WING OUTBOARD LEADING EDGE ASSY REF AMM 57-41-01 REV 66. REMOVED AND REPLACED LEADING EDGE SKIN REF CRJ200 SRM 51-40-11 REV 39.

Part: DOUBLER — CRACKED (PAX DOOR) · airframe 42,008 hrs · 41,722 cycles

50033 334403 452-830-606 - 70HRS PAX DOOR AFT ANGLE IS CRACKED AT PULL IN CAN AREA. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED DOUBLER PULL IN CAN WITH PN 601R318094-2. IAW CRJ200 SRM 51-42-00, AND 51-42-13 REV 39 WORK PERFORMED UNDER AERSALE WORK ORDER 004164, CARD NO. 50033, TT: 42,008:52 TC: 41,722.

Part: STRUT — DISCHARGED (NLG) · airframe 39,801 hrs · 39,386 cycles

INFLIGHT RECV'D GEAR DISAGREE AND NOSE DOOR WARNING MESSAGES. ALSO RECV'D WOW INPUT AND NOSE WHEEL STEERING CAUTION MESSAGES. ALONG WITH WOW OUTPUT STATUS MESSAGE. NOSE GEAR DID NOT RETRACT. C/W QRH. LANDING GEAR EXTENDED AND ALL MESSAGES EXTINGUISHED. *** AIRCRAFT REMOVED FROM SERVICE *** SERVICED NLG SHOCK STRUTS IAW AMM 12-12-32 OPS CHECK GOOD

Part: BRACKET — NONE (ENGINE MOUNT) · airframe 39,745 hrs · 39,335 cycles

NUMBER 1 ENGINE (ESN801422) NOSE COWL SUPPORT BRACKET IS LOOSE INBOARD SIDE OF ENGINE. ***AIRCRAFT REMOVED FROM SERVICE*** INTERIM REPAIR - VERIFIED NUMBER 1 ENGINE NOSE COWL SUPPORT BRACKET P/N 228-50082-145 HAS NOT CAUSED DAMAGE TO SURROUNDING STRUCTURE. INTERIM INSPECTIONS EVERY 500FC TO ENSURE NO DAMAGE PROPAGATION AND NO DAMAGE TO SURROUNDING STRUCTURE. PERMANENT REPAIR WITHIN 10,100FC TO REPAIR OR REPLACE THE DAMAGED SUPPORT. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA #AWAC-CRJ254-0182 REV A DATED 2/2/2022. WORK PERFORMED UNDER AERSALE WORK ORDER 003526, CARD NO. 20404, TT: 39,745:56 TC: 39,335.

Part: AILERON — CORRODED (LH AILERON) · corrosion level 2 · airframe 39,745 hrs · 39,335 cycles

LH WING AILERON PN CC670-13000-1 HAS INTERNAL STRUCTURE CORROSION. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED LH WING AILERON PN CC670-13000-1, SN 7693. PERFORMED RIGGING CHECK AND OPERATIONAL TESTS OF THE FLIGHT CONTROL SYSTEM. ALL WORK WITHIN LIMITS WAS PERFORMED IAW AIR WISCONSIN SUPPLEMENT NO. 19-047 DATE OF ISSUE 3/22/2019, CRJ200 AMM 27-11-00-710-803 REV 64 AND CRJ200 AMM 27-11-00- 220-801 REV 64. WORK PERFORMED UNDER AERSALE WORK ORDER 003526, CARD NO. 20368, TT: 39,745:56 TC: 39,335.

Part: BEAM — DAMAGED (BEAM) · airframe 39,745 hrs · 39,335 cycles

CABIN FLOOR BEAM SUPPORT P/N 601R31118-127 AT FS559.00 AND BL0.0 HAS TOOL SET MARKS ON UPPER HORIZONTAL SURFACE. ***AIRCRAFT REMOVED FROM SERVICE*** CUT AWAY DAMAGED SECTION OF BEAM AT FS559.00 AND BL0.0 AND REPLACED WITH FLOOR BEAM SUPPORT P/N 601R31118-127. FABRICATED TWO CHANNEL REPAIR ANGLES MATERIAL 0.080Ï¿½ 7075-T0 CLAD AL ALLOY AND HEAT TREATED TO 7075-T6 CONDITION. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA #AWAC- CRJ253-01800 REV IR DATED 2/4/2022. WORK PERFORMED UNDER AERSALE WORK ORDER 003526, CARD NO. 20369, TT: 39,745:56 TC: 39,335.

Part: FITTING — GOUGED (ELEVATOR) · airframe 39,745 hrs · 39,335 cycles

LH ELEVATOR HINGE FITTING HAVE DAMAGE ON INBOARD AND OUTBOARD HALVES AT LBL55.88 ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED GOUGE DAMAGE DIMENSION L=1.500Ï¿½ X W= 0.300Ï¿½ X W D= 0.010Ï¿½. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW MHIRJ REO 601R-55-21-560 REV (-) DATED 2022-01-18. WORK PERFORMED UNDER AERSALE WORK ORDER 003526, CARD NO. 20339, TT: 39,745:56 TC: 39,335.

Part: NONE — CORRODED (WING SKIN) · corrosion level 2 · airframe 39,745 hrs · 39,335 cycles

PITTING CORROSION ON LH WING UPPER SKIN LANDING FOR PANEL 540AT. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED DAMAGE ON LH WING UPPER SKIN LANDING P/N 601R10042-7 FOR PANEL 540AT. PERFORMED HFEC WITH NO INDICATIONS. PERFORMED ROTO PEEN TO REWORKED AREAS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA #AWAC-CRJ257-01793 REV IR DATED 1/16/2022. WORK PERFORMED UNDER AERSALE WORK ORDER 003526, CARD NO. 20297, TT: 39,745:56 TC: 39,335.

Part: FITTING — GOUGED (ELEVATOR) · airframe 39,745 hrs · 39,335 cycles

LH HORIZONTAL STABILIZER HINGE FITTING HAS DAMAGE IN TWO PLACES AT LBL55.8865. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED GOUGE DAMAGE ON LH STABILIZER HINGE FITTING DIMENSION P1- L= 0.700Ï¿½ X W= 0.200Ï¿½ X D= 0.012Ï¿½, P2- L= 1.100Ï¿½ X W= 0.200Ï¿½ X D= 0.008Ï¿½. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW MHIRJ REO 601R-55-11-710 REV (A) DATED 2022-02-03. WORK PERFORMED UNDER AERSALE WORK ORDER 003526, CARD NO. 20339, TT: 39,745:56 TC: 39,335.

Part: NONE — DAMAGED (PAX DOOR) · airframe 39,745 hrs · 39,335 cycles

PAX DOOR LOWER SILL SEAL STRIKER AT FS349.00 IS DAMAGED. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED PAX DOOR LOWER SILL SEAL STRIKER AT FS349.00 PN 600-31535. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA #AWAC-CRJ253-01804 REV A DATED 2/16/2022. WORK PERFORMED UNDER AERSALE WORK ORDER 003526, CARD NO. 20361, TT: 39,745:56 TC: 39,335.

Part: DOUBLER — CORRODED (FS 319) · corrosion level 2 · airframe 39,745 hrs · 39,335 cycles

SERVICE DOOR LOWER SURROUND STRUCTURE DOUBLER AND BRACKETS AT FS319.00 AND FS349.00 HAVE CORROSION. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED SERVICE DOOR LOWER SURROUND STRUCTURE DOUBLER P/N 601R38669-49 AT FS309.00 Ï¿½ FS319.00 AND BRACKET P/N 601R38335-1S AT FS319.00 AND BRACKET P/N 601R38224-3 AT FS349.00. DURING REPAIR FOUND TWO ELONGATED HOLES FOR BRACKET AT FS319.00. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA #AWAC-CRJ253-01797 REV IR DATED 1/20/2022. WORK PERFORMED UNDER AERSALE WORK ORDER 003526, CARD NO. 20241, TT: 39,745:56 TC: 39,335.

Part: SHROUD — CRACKED (LEADING EDGE) · airframe 39,745 hrs · 39,335 cycles

LH WING LEADING EDGE PANEL P/N 601R12076 HAS A CRACK MEASURES L= 0.700 X W= 0.010Ï¿½ THE LOWER FLANGE OF INNER SHROUD AT INBOARD END AT WS149.58. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED DAMAGE ON LOWER FLANGE AND FABRICATED AND INSTALLED A REPAIR ANGLE FROM 0.020Ï¿½ 301 Ï¿½ SS AND FILLER FROM 0.040Ï¿½ 2024-T3 AL ALLOY. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA #AWAC- CRJ257-01796 REV IR DATED 1/19/2022. WORK PERFORMED UNDER AERSALE WORK ORDER 003500, CARD NO. 20284, TT: 39745:56 TC: 39,335.

Part: ANGLE — CORRODED (SILL) · corrosion level 2 · airframe 39,745 hrs · 39,335 cycles

CORROSION ON CABIN FLOOR SILL RHS AT FS349.00 AND RBL41, WL73.5. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED DAMAGED FLOOR SILL SECTION AND REPLACED WITH REPAIR ANGLE P/N 601R31148-1355 TO MATCH ORIGINAL FLOOR SILL CUTOUT AT FS349.00 Ï¿½ FS375.00 AND RBL 41. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW MHIRJ REO 601R-53-21-3522 REV (--) DATED 2022-02-04. WORK PERFORMED UNDER AERSALE WORK ORDER 003526, CARD NO. 20255, TT: 39,745:56 TC: 39,335.

Part: WEB — NONE (AFT BULKEAD) · airframe 39,745 hrs · 39,335 cycles

REAR SKIN PANEL OF AFT PRESSURE BULKHEAD IS MISSING ALL REINFORCEMENT ANGLES (7 EA) -59, -61, -62, -65, -66, -69, & -70 REF BOMBARDIER REO 601R-53-61-1240 REV D DTD 2016-10- 13 ***AIRCRAFT REMOVED FROM SERVICE*** GENERAL AND DETAILED INSPECTION C/W, WITH NO DEFECTS NOTED REF CRJ 200 NDTM 51-20-09 (PART 1) REV 43ON 01/11/22 WITH NO ADDITIONAL STRUCTURAL INSPECTION STEPS AND/OR REQUIREMENTS AT THIS TIME REF MHI RJ ENGINEERING MEMO ISE-STR- 001 REV -- DTD 2022-01-06. INSTALLED REINFORCEMENT ANGLES 7EA. P/N 601R-53-61-1240-59; -61; -62; -65; -66; 69; & -70; POCKET SHIMS AT AFT PRESSURE BULKHEAD FS 621.00; COMMON TO BULKHEAD WEB AND 2 STIFFNERS AT BL 0.0; RBL AND LBL 9.5; LBL & RBL 18.0; & LBL & RBL 27.5. REF BOMBARDIER REO 601R-53-61-1240REV D DTD 2016-10-31.

Part: DOUBLER — DENTED (PRESSURE BULKHEA) · airframe 39,745 hrs · 39,335 cycles

AFT PRESSURE BULKHEAD HAS A DENT LOCATED AT FS621.00 AND RBL6.0, WL80.0. ***AIRCRAFT REMOVED FROM SERVICE*** CUT AWAY EXISTING UPPER DOUBLERS P/N 601R-53-61-1240-3 AND -4 AND EXISTING LOWER DOUBLERS P/N 601R-53-61-1240-1 AND -2. REMOVED DENT DAMAGE. FABRICATED AND INSTALLED WEB DOUBLER REPAIR P/N 601R53-61-7796-1 MATERIAL ALUMINUM CLAD 2024-T3, 0.040Ï¿½ THICKNESS, DIMENSIONS L= 13.750Ï¿½ X W= 10.250Ï¿½. FABRICATED AND INSTALLED TWO DOUBLERS P/N 601R53-61-7796-2 AND -3, MATERIAL ALUMINUM CLAD 2024-T3, THICKNESS 0.063Ï¿½, DIMENSIONS L= 13.150Ï¿½ X W= 3.500Ï¿½. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW MHIRJ REO 601R-53-61-7796 REV (--) DATED 2022-02-03. WORK PERFORMED UNDER AERSALE WORK ORDER 003526, CARD NO. 20192, TT: 39,745:56 TC: 39,335.

Part: SEAT TRACK — CORRODED (LH SEAT TRACK) · corrosion level 2 · airframe 39,745 hrs · 39,335 cycles

LH SIDEWALL SEAT TRACK FROM FS409.00 TO FS559.00 +112 HAS SURFACE CORROSION. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED LH SIDEWALL SEAT TRACK PN 20276-144-0-0 FROM FS409.00 TO FS559.00 +112. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW CRJ200 SRM 51-40-11 REV 38 AND AMM 53-01-11 REV 64. WORK PERFORMED UNDER AERSALE WORK ORDER 003526, CARD NO. 20146, TT: 39,745:56 TC: 39,335.

Part: SKIN — DENTED (FS 310+1) · airframe 39,745 hrs · 39,335 cycles

AIRCRAFT L/H SKIN AT PAX DOOR CUTOUT HAS 1 EACH DENT AT FS 310.00+1" AND S13L+1.5". DENT DIMENSIONS ARE: (P1) .400L X .300W X .032D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE*********************** HAND DRESSED DAMAGED AREA TO ORIGINAL CONTOUR OF SKIN. VERIFIED NO CRACKS. VERIFIED NO LOOSE/PULLED FASTENERS AND NO DAMAGE TO UNDERLYING STRUCTURE COMMON TO REPAIR AREA. HFEC PERFORMED WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. RE-EVALUATED SKIN AND FOUND WITHIN LIMITS IAW MHIRJ REO 601R-53-21-3523 REV (--) DATED 2022-01-14. ALL WORK PERFORMED IAW MHIRJ REO 601R-53-21-3523 REV (--) DATED 2022-01-14. WORK COMPLETED AT AERSALE CRS4AER685B ON W/O #003526 CARD #20038. N438AW TT:39,745:56 TC: 39,335

Part: BULKHEAD — NONE (FS 621) · airframe 39,745 hrs · 39,335 cycles

AFT PRESSURE BULKHEAD REAR WEB HAS 2 EACH RIVETS INSTALLED AT THE EDGE OF CHEM MILL I/B OF Z STIFFENER AT LBL 17 WL 140.5 AND 141.5. ******************AIRCRAFT REMOVED FROM SERVICE********************** REMOVED 2 EACH RIVETS AT THE EDGE OF CHEM MILL ON AFT PRESSURE BULKHEAD AT FS 621 LBL 17 WL 140.5 AND 141.5 AT REAR WEB. PERFORMED SPOT FACE WITH A 0.250" RADIUS FLAT AROUND DISCREPANT HOLES. ENSURED TRANSITION RADIUS OF 0.300" MIN WITH CHEM MILL EDGES. HFEC INSPECTION PERFORMED AT BOTH DISCREPANT HOLES WITH NO INDICATIONS. HFEC ROTARY PROBE INSPECTION PERFORMED AT BOTH DISCREPANT HOLES WITH NO INDICATIONS. INSTALLED 2 EACH FASTENERS AT REWORKED AREA. RESTORED PROTECTIVE FINISH AT REWORKED AREA. ALL WORK PERFORMED IAW MHIRJ REO 601R-53-61-7792 REV (--) DATED 2022-01-14. WORK COMPLETED ON AERSALE WO #003526 CARD #20260. N438AW TT: 39,745:56 TC: 39,335

Part: CHANNEL — GOUGED (FS574-FS589) · airframe 39,745 hrs · 39,335 cycles

CARGO DOOR UPPER FWD SUPPORT CHANNEL P/N: 601R35050-129 HAS A GOUGE ON FLANGE. DIMENSIONS ARE: (P1) 1.900L X .063W X .190D. EVALUATED GOUGE AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-00 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE*********************** BLENDED DAMAGED AREA ON EDGE OF FLANGE TO A SMOOTH CONTOUR. VERIFIED NO CRACKS. VERIFIED NO LOOSE/PULLED FASTENERS AND NO DAMAGE TO UNDERLYING STRUCTURE COMMON TO REPAIR AREA. HFEC PERFORMED WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. RE-EVALUATED SKIN AND FOUND WITHIN LIMITS IAW MHIRJ REO 601R-53-61-7797 REV (--) DATED 01/25/2022. ALL WORK PERFORMED IAW MHIRJ REO 601R-53-61-7797 REV (--) DATED 01/25/2022. WORK COMPLETED AT AERSALE CRS4AER685B ON W/O #003526 CARD #20323. N438AW TT:39,745:56 TC: 39,335

Part: NONE — DAMAGED (FS 937.13) · airframe 39,745 hrs · 39,335 cycles

L/H HORIZONTAL STABILIZER SPLICE AT CLOSING RIB #9 HAS DAMAGE FROM LIGHTNING STRIKE. PREVIOUS TEMPORARY REPAIR COMPLIED WITH IAW MHIRJ REO 601R-55-11-677 REV A. PERMANENT REPAIR REQUIRED. *************AIRCRAFT REMOVED FROM SERVICE************************ CUTOUT DAMAGED AREA AT SPLICE 1.00"L X 0.500"W. HFEC INSPECTION PERFORMED AT CUTOUT WITH NO INDICATIONS. FABRICATED REPAIR PLATE OUT OF 2024-T3 .050" (7.5"L X ,950"W), FILLER FROM 2024-T3 .032" (1.6"L X .600"W), REPAIR ANGLE FROM 2024-T3 .040" (4.2"L X 1.6"W), AND FILLER FROM 2024-T3 .032" (1.6"L X .800"W). ALODINED AND PRIMED REPAIR PARTS. INSTALLED REPAIR PARTS TO REPAIR AREA . ALL WORK PERFORMED WITHIN ALLOWABLE LIMITS IAW MHIRJ REO 601R-55-11-708 REV (--) DATED 2022-01-20. WORK COMPLETED ON AERSALE WO #003526 CARD #50011. N438AW TT: 39,745:56 TC: 39,335.

Part: BRACKET — GOUGED (L/H HSTAB BRACKE) · airframe 39,745 hrs · 39,335 cycles

L/H HORIZONTAL STABILIZER JACKSCREW FITTING HAS GOUGE ON I/B FASTENER BRACKET. DIMENSIONS ARE: (P1) 2.150L X 1.650W X .010D. EVALUATED GOUGE AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 55-11-27 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE*********************** BLENDED DAMAGED AREA ON BRACKET TO A SMOOTH CONTOUR. SHOT-PEENED REPAIR AREA. VERIFIED NO LOOSE/PULLED FASTENERS AND NO DAMAGE TO UNDERLYING STRUCTURE COMMON TO REPAIR AREA. HFEC PERFORMED WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. RE-EVALUATED AREA AND FOUND WITHIN LIMITS IAW MHIRJ REO 601R-55-11-709 REV (--) DATED 2022-01-15. ALL WORK PERFORMED IAW MHIRJ REO 601R-55-11-709 REV (--) DATED 2022-01-15. WORK COMPLETED AT AERSALE CRS4AER685B ON W/O #003526 CARD #20149. N438AW TT:39,745:56 TC: 39,335

Part: NONE — GOUGED (L/H HSTABPANEL 3) · airframe 39,745 hrs · 39,335 cycles

L/H LEADING EDGE PANEL 331AL HAS TOOL MARKS ON I/B FASTENER HOLES. DIMENSIONS ARE: (P1) 7.100L X 1.00W X .018D. EVALUATED GOUGE AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 55-00-00 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE*********************** BLENDED DAMAGED AREA ON PANEL 331AL TO A SMOOTH CONTOUR. VERIFIED NO CRACKS. VERIFIED NO LOOSE/PULLED FASTENERS AND NO DAMAGE TO UNDERLYING STRUCTURE COMMON TO REPAIR AREA. HFEC PERFORMED WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. RE-EVALUATED SKIN AND FOUND WITHIN LIMITS IAW ASAP EA #AWAC-CRJ255-01795 REV IR DATED 01/18/2022. ALL WORK PERFORMED IAW ASAP EA #AWAC-CRJ255-01759 REV IR DATED 01/18/2022. WORK COMPLETED AT AERSALE CRS4AER685B ON W/O #003526 CARD #20114. N438AW TT:39,745:56 TC: 39,335

Part: SKIN — DENTED (FS 235+5") · airframe 39,745 hrs · 39,335 cycles

AIRCRAFT R/H SKIN EXTERIOR HAS 1 EACH DENT AT FS 235+5" AND S19R. DENT DIMENSIONS ARE: (P1) 1.950L X 1.50W X .011D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE*********************** VERIFIED NO LOOSE/PULLED FASTENERS AND NO DAMAGE TO UNDERLYING STRUCTURE COMMON TO REPAIR AREA. HFEC PERFORMED WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. RE-EVALUATED SKIN AND FOUND WITHIN LIMITS IAW ASAP EA #AWAC-CRJ253-01794 REV IR DATED 01/17/2022. ALL WORK PERFORMED IAW ASAP EA # AWAC-CRJ253-01794 REV IR DATED 01/17/2022. WORK COMPLETED AT AERSALE CRS4AER685B ON W/O #003526 CARD #20095. N438AW TT:39,745:56 TC: 38,335

Part: SEAT TRACK — CORRODED (FS364-FS559.79) · corrosion level 2 · airframe 39,745 hrs · 39,335 cycles

R/H SIDEWALL SEAT TRACKS FROM FS 364.00 TO FS 559.79 HAVE SEVERAL AREAS OF SURFACE CORROSION. EVALUATED CORROSION ON R/H SIDEWALL SEAT TRACKS AT FS 364.00 TO FS 559.00+80 AT RBL 42 AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-49 REV 38. *********AIRCRAFT REMOVED FROM SERVICE*************************** REMOVED AND REPLACED SIDEWALL SEAT TRACK FROM FS 364.00 TO FS 510.10 AT RBL 42 IAW CRJ200 AMM 53-01-11 REV 64. REMOVED AND REPLACED SIDEWALL SEAT TRACK FROM FS 510.10 TO FS 559.79 RBL42 IAW CRJ200 AMM 53-01-11 REV 64. RESTORED PROTECTIVE FINISH TO BOTH SEAT TRACK INSTALLATIONS PRIOR TO INSTALLATION IAW CRJ200 SRM 51-21-11 REV 38, CRJ200 SRM 51-25-06 REV 38, AND CRJ200 SRM 51-25-00 REV 38. WORK COMPLETED ON AERSALE WO #003526 CARD #20147. CRS #4AER685B N438AW TT:39,745:56 TC:39,335

Part: NONE — GOUGED (R/H ELEVATOR) · airframe 39,745 hrs · 39,335 cycles

R/H ELEVATOR I/B AND O/B FITTING HAS GOUGE ON FITTING ASSY AT ES60.525 (RBL55.8865). DIMENSIONS ARE: (P1) 2.100L X 0.300W X .005D. EVALUATED GOUGE AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 55-11-27 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE*********************** BLENDED DAMAGED AREA ON FITTING TO A SMOOTH CONTOUR. SHOT-PEENED REPAIR AREA. VERIFIED NO LOOSE/PULLED FASTENERS AND NO DAMAGE TO UNDERLYING STRUCTURE COMMON TO REPAIR AREA. HFEC PERFORMED WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. RE-EVALUATED AREA AND FOUND WITHIN LIMITS IAW MHIRJ REO 601R-55-21-561 REV (--) DATED 2022-01-17. ALL WORK PERFORMED IAW MHIRJ REO 601R-55-21-561 REV (--) DATED 2022-01-17. WORK COMPLETED AT AERSALE CRS4AER685B ON W/O #003526 CARD #20331. N438AW TT:39,745:56 TC: 39,335

Part: FITTING — GOUGED (R/H HSTAB) · airframe 39,745 hrs · 39,335 cycles

R/H H STAB FITTING #2 HAS 2 EACH GOUGES AT ES60.525 (RBL55.8865). DIMENSIONS ARE: (P1) 1.00L X 0.200W X .006D (P2) 1.100L X 0.200W X .015D. BOTH GOUGES ARE NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 55-11-27 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE*********************** BLENDED DAMAGED AREAS ON FITTING TO A SMOOTH CONTOUR. SHOT-PEENED REPAIR AREA. VERIFIED NO LOOSE/PULLED FASTENERS AND NO DAMAGE TO UNDERLYING STRUCTURE COMMON TO REPAIR AREA. HFEC PERFORMED WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. RE-EVALUATED AREA AND FOUND WITHIN LIMITS IAW MHIRJ REO 601R-55-21-711 REV A DATED 2022-01-17. ALL WORK PERFORMED IAW MHIRJ REO 601R-55-21-711 REV A DATED 2022-01-17. WORK COMPLETED AT AERSALE CRS4AER685B ON W/O #003526 CARD #20331. N438AW TT:39,745:56 TC: 39,335

Part: ANGLE — GOUGED (FS 139.54) · airframe 39,745 hrs · 39,335 cycles

L/H WING I/B LE PANEL UPPER MOUNT LANDING HAS A GOUGE ON ANGLE DWG #600-12031. GOUGE IS NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 57-00-00 REV 38. *************AIRCRAFT REMOVED FROM SERVICE************************ EDGE TRIMMED THE CHAFED AREA DIMENSIONS: 1.1"L X .040"W X .100"D. HFEC INSPECTION PERFORMED AT CUTOUT WITH NO INDICATIONS. VERIFIED MINIMUM 2D EDGE DISTANCE BETWEEN TRIMMED AREA AND ADJACENT FASTENERS. RESTORED PROTECTIVE FINISH. ALL WORK PERFORMED IAW ASAP EA #AWAC-CRJ257-01792 REV IR DATED 2022-01-19. WORK COMPLETED ON AERSALE WO #003526 CARD #50011. N438AW TT: 39,745:56 TC: 39,335.

Part: NONE — NONE · airframe 39,645 hrs · 39,231 cycles

CAPTS WS CRACKED SPIDERWEB ACROSS ENTIRE PANEL ***AIRCRAFT REMOVED FROM SERVICE*** REF WO 309800 WC 6,7,8,9, & 11 FOR R&R OF CAPT WINDSHIELD IAW CRJ AMM 56-11-01.

Part: CONTROL UNIT — FAULTED (TE FLAPS) · airframe 38,538 hrs · 38,087 cycles

ON APPROACH, WHILE SELECTING FLAPS TO 8 DEGREES, RECEIVED FLAP FAIL MESSAGE. C/W QRH. PERFORMED ZERO FLAP LANDING. LANDED AT 41,000LBS. MAX BRAKE TEMP DURING TAXI WAS "4". PERFORMED FLAP RESET PROCEDURE, IAW AWAC SUPP 98-18I BOX 12. FLAPS RESET. PLACARDED AND PLACED ON MEL. AIRCRAFT REMOVED FROM SERVICE. R & R FECU, IAW AMM 27-51-05. OPERATIONS CHECK GOOD. REMOVED PLACARDS AND MEL.

Part: BULKHEAD WEB — CRACKED (AFT) · airframe 38,355 hrs · 37,882 cycles

SDI OF THE AFT PRESSURE BULKHEAD FWD FACE, IAW NDTM AWAC SUPPLEMENT 09-008 REV 41. ACCOMPLISHED UT INSPECTION ON AFT PRESSURE BULKHEAD FWD FACE, IAW NDTM PART 4, 53-61-153 REV 41 NO INDICATIONS NOTED. ACCOMPLISHED HFEC INSPECTION ON AFT PRESSURE BULKHEAD FWD FACE, IAW NDTM PART 1, 51-20-06 REV 41. 9. EACH CRACKS FOUND IN THE FOLLOWING LOCATIONS: 1) LBL 18.00 WL 127.18-127.805 THAT MEASURES 6.625'' IN LENGTH; 2) LBL 18.00 WL 113.43-98.43 THAT MEASURES 15.00'' IN LENGTH; 3) LBL 9.50 WL 113.43-101.93 THAT MEASURES 11.50'' IN LENGTH; 4) BL 0.00 WL 125.93-136.81 THAT MEASURES 10.25'' IN LENGTH; 5) BL 0.00 WL 115.18-100.43 THAT MEASURES 14.75'' IN LENGTH; 6) RBL 9.50 WL 115.18-81.93 THAT MEASURES 33.25'' IN LENGTH; 7) RBL 18.00 WL 102.68-101.93 THAT MEASURES 0.75'' IN LENGTH; 8) RBL 27.50 WL 113.18-101.68 THAT MEASURES 11.50'' IN LENGTH; 9) RBL 27.50 WL 97.43-87.68 THAT MEASURES 9.75'' IN LENGTH. AIRCRAFT REMOVED FROM SERVICE. REPAIR/MODIFICATION OF AFT PRESSURE BULKHEAD WEB ACCOMPLISHED ON WORK ORDER NO: 002867, AERSALE WORK CARD NR 4EOAWA21045, IAW EO NR E17/003/453.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 38,355 hrs · 37,882 cycles

NDT-3 INDICATION FOUND COMING FROM UNDER MACHINED FITTING OF THE BAGGAGE BAY DOOR (LINTEL AREA) FOUND 3 EACH CRACKS AT FS 621.00. NR 1 VERTICAL CRACK THAT MEASURES 1.7'' UPPER HORIZONTAL CRACK THAT MEASURES .5'' AND LOWER HORIZONTAL CRACK THAT MEASURES .5'' RESPECTIVELY. AIRCRAFT REMOVED FROM SERVICE. CUT OUT CRACKED AREA CUT OUT MEASURES 3.5'' X 3.8'', PERFORMED HFEC OF CUT OUT NO INDICATIONS NOTED, REF CRJ NDTM PART 1 REV 41 51-20-06 PER BOMBARDIER REO NR 601R-53-61-1230 REV-F. FOUND 3 EACH CRACKS AROUND FITTING. VERTICAL CRACK MEASURES 1.7'' UPPER HORIZONTAL CRACK THAT MEASURES .5'' AND LOWER HORIZONTAL CRACK THAT MEASURES .5''. FABRICATED FILLER FROM 2024-T3 .063. FABRICATED DOUBLER FROM 2024-T3 .071INSTALLED REPAIR. COMPLIED WITH REPAIR TO PRESSURE BULKHEAD WEB AT FS 621.00 LINTEL INSTALLATION, REF REO 601R-53-61-1230 REF-F DATED 2011/10/31

Part: PRESSURE DECK — CORRODED (BS 452) · corrosion level 2 · airframe 38,355 hrs · 37,882 cycles

LT PRESS FLOOR SILL PANEL HAS CORROSION AROUND FASTENER HOLE AT FS 452.35 & BL 43. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION AT FLOOR SILL PANEL AT FS 452.35 & BL 43 WITH A REWORK AREA THAT MEASURES L=1.88 X W=1.134 X D=.003" ORIGINAL THICKNESS .080" MATERIAL REMAINING .077" FOUND TO BE WITHIN ALLOWABLE LIMITS REF BOBBARDIER REO 601R53-41-666 REV C DTD 2012-11-06.

Part: SKIN — DAMAGED (BS 409) · airframe 38,355 hrs · 37,882 cycles

RT DME ANTENNA CUTOUT HAS SCRATCHES ON ANTENNA PAD AREA OF FUSELAGE SKIN. AIRCRAFT REMOVED FROM SERVICE. LOCATED AND BLENDED OUT DAMAGE WITH .001" MATERIAL REMOVED WITHIN REMAINING .054" MINIMUM SKIN THICKNESS CHECK. WITHIN ALLOWABLE LIMITS, REF AIR WISCONSIN SUPP NO 20-110 DATE OF ISSUE 09/14/2020.

Part: SKIN — DAMAGED (BS 409) · airframe 38,355 hrs · 37,882 cycles

LT DME ANTENNA CUTOUT HAS SCRATCHES ON ANTENNA PAD AREA OF FUSELAGE SKIN. AIRCRAFT REMOVED FROM SERVICE. LOCATED AND BLENDED OUT DAMAGE WITH .002" MATERIAL LOSS AND A MINIMUM REMAINING MATERIAL THICKNESS OF .054" WITHIN ALLOWABLE LIMITS, REF AIR WISCONSIN SUPP NO 20-120.

Part: DOUBLER — CRACKED (PAX DOOR) · airframe 34,936 hrs · 34,560 cycles

PAX DOOR EXISTING REPAIR DOUBLER ON AFT RISER UNDER COUNTER BALANCE CRACKED.

Part: ANGLE — CRACKED (BS 280) · airframe 34,936 hrs · 34,560 cycles

ANGLE IS CRACKED ON THE OTBD SIDE OF RBL 9 AND JUST AFT OF THE FLOORBEAM BS 280.

Part: FITTING — CRACKED (BS 460) · airframe 34,936 hrs · 34,560 cycles

BS 460 RBL BATH TUB FITTING CRACKED.

Part: STIFFENER — CRACKED (ASSIST MOTOR) · airframe 34,936 hrs · 34,560 cycles

PAX DOOR ASSIST MOTOR LOWER STIFFNER CRACKED

Part: ANGLE — CRACKED (BS 280) · airframe 34,936 hrs · 34,560 cycles

FS 280 AFT SIDE RBL 9 CLIP CRACKED. REPLACED

Part: SEAT TRACK — DAMAGED (BS 250-280) · airframe 34,936 hrs · 34,560 cycles

PILOT SEAT TRACKS HAVE GROVES WORN INTO TRACKS. REPAIRED THE SEAT TRACK IAW SRM 53-11-49, AND 51-12-00.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 34,598 hrs · 34,202 cycles

WHILE PERFORMING NDT ON THE AFT PRESSURE BULKHEAD, BS 621. FOUND DISCONTINUITY INDICATION AT LBL 36.2. 5 INCHES ABOVE WL 73.50. INDICATION IS APPROX. 3/4 INCHES IN LENGTH.

Part: CROSSBEAM — CHAFED (CARGO DOOR) · airframe 34,031 hrs · 33,583 cycles

CARGO DOOR CROSS BEAM LOWER OUTBOARD CHANNEL CHAFED BY THE CABLES.

Part: DOOR SEAL — LACK OF LUBE (SERVICE DOOR) · airframe 31,900 hrs · 31,569 cycles

UNABLE TO OPEN SERVICE DOOR FROM EXTERIOR. LUBRICATED SERVICE DOOR SEAL, HANDLE, AS REQUIRED. OPS CHECK NORMAL. DOOR OPENS FROM OUTSIDE, ACFT OK FOR SERVICE.

Part: CIRCUIT BREAKER — POPPED (HYDRAULIC SYS) · airframe 31,158 hrs · 30,888 cycles

FOLLOWING AIRFRAME VIBRATION HYD SYNOPTIC PAGE SYS 3 MANIFOLD OUTPUT BOX INDICATED ZERO PSI. LOW LINE BELOW BOX SHOWED YELLOW LG, NOSE STEERING & NOSE DOOR SHOWED YELLOW. SYS 3 QTY NORMAL AT 55%. ON GND FOUND HYD SYS 3 INDICATIONS CB N12 ON CBP2 POPPED. GEAR EXTENSION NORMAL, BRAKING & STEERING NORMAL.

Part: SKIN PANEL — CHAFED (FUSELAGE) · airframe 31,071 hrs · 30,811 cycles

LEFT APRON SKIN PANEL HAS WEAR DAMAGE AT FS 554.00 & WL 51.58. REPAIRED LT APRON SKIN PANEL IAW REO 601R-53-41-610 REV C.

Part: LANDING — BENT (SERVICE DOOR) · airframe 31,071 hrs · 30,811 cycles

GROUND ACFT SERVICE DOOR FWD & AFT LANDINGS ARE BENT. REPAIRED ACFT SERVICE DOOR FWD & AFT LANDINGS IAW SUPPLEMENT 16-008.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 31,071 hrs · 30,811 cycles

LEFT SIDE FLOOR SUPPORT INTERCOSTAL MEMBER IS CRACKED AT LBL 36 & FS 484.00. REPAIRED LT SIDE FLOOR SUPPORT INTERCOSTAL MEMBER AT LBL 36 & FS 484.00 IAW EA 253-00334 REV IR DATED 03 30 2016.

Part: FRAME — CHAFED (FUSELAGE) · airframe 31,071 hrs · 30,811 cycles

FRAME 559+48 IS CHAFED BELOW STRINGER 5R, AT THE BOTTOM SIDE. REPAIRED FRAME IAW EA 00333 REV IR DATE 03 29 2016.

Part: SUPPORT FRAME — CRACKED (FUSELAGE) · airframe 31,071 hrs · 30,811 cycles

FLIGHT DECK LT SIDE POST LOWER SUPPORT FRAME IS CRACKED. R & R FRAME SECTION IAW SRM 51-42-06, REPAIRED DRILL START DAMAGE ON LT SIDE OF POST LOWER SUPPORT CHANNEL IAW SUPPLEMENT 16-113 & EA 00346.

Part: STOP FITTING — CHAFED (TE FLAP VANE) · airframe 31,071 hrs · 30,811 cycles

RIGHT INBD FLAP VANE, INBD STOP PAD CONTACT POINT CHAFED, REPLACED.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 31,071 hrs · 30,811 cycles

NUMBER 2 HYD FILTER MOUNT CHANNEL IS CRACKED ON AFT LOWER CORNER, REPLACED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,071 hrs · 30,811 cycles

280 FRAME CRACKED OTBD OF LBL 9 BY ALT RELEASE CABLE PULLEY BRACKET, REPAIRED.

Part: SKATE ANGLE — CRACKED (PAX DOOR) · airframe 31,071 hrs · 30,811 cycles

PASSENGER ENTRY DOOR AFT SKATE ANGLE IS CRACKED, REPAIRED.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 31,071 hrs · 30,811 cycles

C CHANNEL IS CRACKED ON STRINGER 14L, INTERCOSTAL ON AFT SIDE OF AFT PRESS BULKHEAD.

Part: CLEAT — CORRODED (PAX DOOR) · corrosion level 2 · airframe 31,071 hrs · 30,811 cycles

PASSENGER DOOR AFT CLEAT IS CORRODED. R & R PAX DOOR AFT CLEAT IAW SRM 51-40-11, 51-42-06 & 51-42-10.

Part: SEAT TRACK — CHAFED (COCKPIT) · airframe 31,071 hrs · 30,811 cycles

CO-PILOT OTBD SEAT TRACK HAS CHAFE MARKS ON THE TOP SIDE. REPAIRED CO-PILOT OTBD SEAT TRACK TOP SIDE IAW REO 601R-53-11-953 & SRM 53-11-49.

Part: PLATE — CRACKED (FUSELAGE) · airframe 31,071 hrs · 30,811 cycles

CARGO DOOR STEP PLATE & HINGE CRACKED. REPLACED CARGO DOOR STEP PLATE & HINGE ASSEMBLY IAW SRM 51-40-11, 51-42-06 & 51-25-01.

Part: MOUNT BRACKET — CRACKED (FUSELAGE) · airframe 31,071 hrs · 30,811 cycles

SYSTEM 3 ACCUMULATOR FWD OTBD MOUNT BRACKET IS CRACKED. REPLACED SYS 3 OTBD MOUNT BRACKET WITH NEW PART IAW SRM 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,071 hrs · 30,811 cycles

LEFT AISLE SEAT TRACK STICK NR 1 HAS CORROSION, BETWEEN FS 364.00 & 409.00 IN THE CABIN. R & R LT AISLE SEAT TRACK NR 1 IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,071 hrs · 30,811 cycles

LEFT SIDEWALL SEAT TRACK NR 3 HAS CORROSION, BETWEEN FS 409+16 TO 409+112. R & R LT SIDEWALL SEAT TRACK NR 3 IAW AMM 53-01-11.

Part: SUPPORT — CRACKED (RT WING) · airframe 31,071 hrs · 30,811 cycles

RIGHT WING FUEL RECEPTACLE SUPPORT IS CRACKED AT LE. R & R RT WING FUEL RECEPTACLE SUPPORT IAW SRM 51-41-02 & 51-42-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,071 hrs · 30,811 cycles

SEAT RAIL BEAM LBL 27, FS 574.00 - 609.00 HAS CORROSION INBD & OTBD FLANGES. R & R LBL 27 FLOORBEAM IAW SRM 51-24-36, 51-40-11 & REO 601R-53-61-3778.

Part: RIB — CRACKED (NR 2 EXHAUST) · airframe 31,071 hrs · 30,811 cycles

NUMBER 2 ENG EXHAUST FAIRING NR 1 RIB IS CRACKED. REPAIRED NR 2 ENG EXHAUST FAIRING NR 1 RIB IAW CMM 78-11-00 REPAIR SR5042.

Part: FRAME — CHAFED (FUSELAGE) · airframe 31,071 hrs · 30,811 cycles

FRAME 559+48 IS CHAFED BELOW STRINGER 3R AT THE AFT SIDE. REPAIRED FRAME IAW SRM 51-12-00.

Part: FITTING — CRACKED (FUSELAGE) · airframe 31,071 hrs · 30,811 cycles

FLIGHT DECK RT WINDOW POST, LOWER FITTING IS CRACKED. REPLACED CRACKED FITTING WITH NEW FITTING IAW SRM 51-42-21.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,335 hrs · 30,113 cycles

ROW 8 - 12 EMER FLOOR TRACK LIGHTING INOPERATIVE.

Part: CONNECTOR — CONTAMINATED (EMERGENCY LIGHTS) · airframe 29,867 hrs · 29,666 cycles

FLIGHT 4027, EMERGENCY LIGHTS ROWS 1- 5 ARE DIM. INSPECTED & CLEANED CONDENSATION FROM LIGHTING CONNECTORS. REINSTALLED THE EMERGENCY LIGHT IAW AMM 33-51-01, SUP 12-032 & 13-022. PERFORMED OPS CHECK. OPS CHECKED GOOD.

Part: ACTUATOR — FAILED (YAW DAMPER) · airframe 29,602 hrs · 29,393 cycles

FLIGHT 3926, WITH AUTOPILOT OFF, RECEIVED UNCOMMANED YAW. COMPLIED WITH IAC & QRH, ISSUE CLEARED WITH YAW DAMPER OFF. INTERROGATED FCC & FOUND NR 2 YAW DAMPER FAILED. R & R NR 2 LINEAR YAW DAMPER ACTUATOR IAW AMM 22-22-01. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (ROWS 2-6) · airframe 27,662 hrs · 27,516 cycles

EMERGENCY LIGHTS INOPERATIVE ROW 2 - 6.

Part: UNKNOWN — ODOR · airframe 27,224 hrs · 27,129 cycles

AIRCRAFT WAS LEFT POWERED ON BATTERY FOR UNKNOWN AMOUNT OF TIME. ELEC ODOR SMELL. APU WAS RUNNING WITH APU GEN SELECTED OFF. SHUTDOWN ACFT.

Part: TAB — CRACKED (NAV LIGHT) · airframe 26,404 hrs · 26,333 cycles

SAFETY WIRE TAB FOR AFT NAV LIGHTS BROKEN. REMOVED CRACKED TAB & INSTALLED SERVICEABLE TAB IAW SRM 51-41-02, 51-21-11 & 51-25-06.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,404 hrs · 26,333 cycles

FS 349.00 IS CORRODED IN FWD AVIONICS BAY. REMOVED CORRODED FRAME AT FS 349.00 & INSTALLED NEW SERVICEABLE FRAME IAW SRM 51-42-21, 51-42-06, 51-21-06, TR53-27, 51-40-11, 51-25-16 & 51-25-06 EA 15-2014-098 REV A.

Part: HINGE BRACKET — CRACKED (LAV SERVICE) · corrosion level 2 · airframe 26,404 hrs · 26,333 cycles

LAVATORY SERVICING DOOR LOWER ATTACH HINGE CORRODED. R & R WITH NEW LOWER ATTACH HINGE IAW SRM 51-41-02.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 26,404 hrs · 26,333 cycles

LINTEL FITTING AT 621 BULKHEAD IS CRACKED ON UPPER AFT ANGLE. R & R CRACKED ANGLE WITH NEW SERVICEABLE ANGLE IAW REO 601R-53-61-1230REV C DATED 4-10-12.

Part: DRAG ANGLE — CRACKED (LT WING) · airframe 26,404 hrs · 26,333 cycles

LEFT MLG DRAG BRACE ANGLE COMMON TO BATTERY RIB CRACKED. REMOVED CRACKED DRAG ANGLE & REPLACED WITH NEW SERVICEABLE DRAG ANGLE IAW SRM 51-42-21, 51-40-11 & 51-25-16.

Part: INTERCOSTAL — CRACKED (APU DOOR) · airframe 26,404 hrs · 26,333 cycles

REPAIR APU DOOR STRUCTURE INTERCOSTAL. REMOVED CRACKED INTERCOSTAL & INSTALLED NEW SERVICEABLE INTERCOSTAL IAW SRM 51-42-06, 51-41-02 & 51-40-11.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,404 hrs · 26,333 cycles

SERVICE DOOR LOWER SILL CORRODED. REMOVED CORRODED LOWER SILL & INSTALLED SERVICEABLE LOWER SILL IAW SRM 51-42-21, 51-42-13 & 51-42-06.

Part: SKIN — DAMAGED (LT WING) · airframe 26,404 hrs · 26,333 cycles

LEFT INBD LOWER EXTERIOR SKIN AT WS 75.00 & INBD OF HINGE BOX HAS SEVERAL GOUGES & POSSIBLE PUNCTURE. REPAIRED DAMAGED SKIN IAW EA15-2014-092.

Part: RIB — CRACKED (LT WING) · airframe 26,404 hrs · 26,333 cycles

LEFT MLG BATTERY RIB CRACKED. REPAIRED LT MLG BATTERY RIB IAW REO 601R-57-51-046 REV B.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 26,404 hrs · 26,333 cycles

CARGO SURROUND SILL AT FS 589 & LBL 44 INBD END OF SUPPORT ANGLE CRACKED UNDER SILL. REMOVED CRACKED ANGLE & INSTALLED SERVICEABLE ANGLE IAW SRM 51-42-06 & 51-42-21.

Part: REPAIR — CRACKED (FUSELAGE) · airframe 26,404 hrs · 26,333 cycles

CRACK IN PREVIOUS REPAIR OF FLOORBEAM CAP AT FS 280 LBL 9. R & R CRACKED ANGLE ON FS 280 IAW REO 601R-53-11-137 REV A.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 26,404 hrs · 26,333 cycles

RIGHT AFT FS 280 BULKHEAD SKIN IS CHAFED AT PREVIOUS REPAIR. R & R REPAIR DOUBLER ON RT AFT SIDE OF FS 280 IAW SRM 51-42-06 & REO 601R-53-11-1127 REV E.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,404 hrs · 26,333 cycles

CABIN FLOOR SEAT TRACK AT 559+112 & RBL 9 IS CORRODED. REMOVED CORRODED SEAT TRACK & INSTALLED NEW SEAT TRACK IAW SRM 51-21-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,404 hrs · 26,333 cycles

CABIN FLOOR SEAT TRACK AT FS 614 LBL 9 IS CORRODED. REMOVED CORRODED SEAT TRACK & REPLACED WITH SERVICEABLE SEAT TRACK IAW 53-21-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,404 hrs · 26,333 cycles

CABIN FLOOR SEAT TRACK AT FS 559+90 AT RBL 9 CORRODED. REMOVED CORRODED SEAT TRACK & INSTALLED SERVICEABLE SEAT TRACK IAW REO-53-00-485.

Part: SKIN — DENTED (TE FLAP) · airframe 26,404 hrs · 26,333 cycles

LEFT OTBD FLAP LOWER SKIN DENTED CTR. REPAIRED LT OTBD FLAP LOWER SKIN IAW SRM 57-53-00 REPAIR NO-03 PG 201-207 FIG 201 & 202, SHEET 1, REV 32.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,404 hrs · 26,333 cycles

FLOOR CROSSBEAM CORRODED AT 349.00. REPAIRED CROSSBEAM DAMAGE ON FLOOR CROSS MEMBER IAW EA 15-2014-090.

Part: TIE DOWN — CORRODED (CARGO BAY) · corrosion level 2 · airframe 26,404 hrs · 26,333 cycles

CABIN FLOOR THREE EACH CARGO TIE DOWN FITTINGS AT LBL 27 & FS 559+102, 559+112 & 566 HAVE CORROSION. REMOVED CORRODED CARGO FLOOR TIE DOWNS FITTINGS & INSTALLED NEW SERVICEABLE TIE DOWN FITTINGS AT LBL 27 & 559+102, 559+112 & 566.00 IAW SRM 53-61-49 & 51-41-02.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 26,404 hrs · 26,333 cycles

CABIN FLOOR SUPPORT AT FS 484 AT RBL 27 IS CRACKED. REMOVED CRACKED ANGLE & INSTALLED SERVICEABLE ANGLE IAW REO 601R-53-41-059 REV B.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 26,404 hrs · 26,333 cycles

CABIN FLOOR ANGLE AT FS 484 IS CRACKED. REMOVED CRACKED ANGLE & INSTALLED SERVICEABLE ANGLE IAW REO 601R-53-41-059 REV B.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,404 hrs · 26,333 cycles

CABIN FLOOR SEAT TRACK FROM 559+50 TO FS 559+80 & RBL 9 HAS CORROSION. R & R SEAT TRACK FROM FS 559+04 TO FS 559+86 AT RBL 9.0 IAW AMM 53-01-11.

Part: SEAL — CRACKED (LT SPOILER) · airframe 26,404 hrs · 26,333 cycles

LEFT FS RAZOR SEAL IS CRACKED. REMOVED CRACKED SPRING SEAL & REPLACED WITH NEW SERVICEABLE SEAL IAW SRM 51-42-06.

Part: BRACKET — CRACKED (RT MLG WW) · airframe 26,404 hrs · 26,333 cycles

RIGHT WW BRAKE TRANSDUCER BRACKET CRACKED. REMOVED CRACKED BRACKET & INSTALLED NEW SERVICEABLE BRACKET IAW SRM 51-40-11 & 51-42-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,404 hrs · 26,333 cycles

CABIN FLOOR SEAT TRACK AT FS 559+91 & LBL 9 IS CORRODED. REMOVED CORRODED SEAT TRACK & REPLACED WITH NEW SERVICEABLE SECTION IAW AMM 53-01-11 & SRM 51-50-11.

Part: BRACKET — CRACKED (RT MLG WW) · airframe 26,404 hrs · 26,333 cycles

RIGHT WW HAS BRAKE TRANSDUCER LINE BRACKET CRACKED. R & R CRACKED BRACKET WITH NEW SERVICEABLE BRACKET IAW SRM 51-42-06 & 51-40-11.

Part: CHANNEL — CRACKED (LT TAIL PIPE) · airframe 26,404 hrs · 26,333 cycles

LEFT TAIL PIPE FAIRING FIRE LOOP CHANNEL IS CRACKED. R & R CRACKED CHANNEL WITH NEW SERVICEABLE CHANNEL IAW CMM 78-11-00-440-001-A01.

Part: APU — FIRE (APU BAY) · airframe 26,013 hrs · 25,966 cycles

APU FIRE, PILOTS NOTICED HIGH EGT BUT NO RPM. EMERGENCY CREWS WERE ALERTED. COMPLIED WITH QRH, BOTTLE NEVER DISCHARGED. FIRE WENT OUT ON ITS OWN AFTER SHUTTING DOWN APU. INSPECTED APU & SURROUNDING AREA, NO FIRE DAMAGE NOTED. IAW 25643 4 FOR MEL. VERIFIED NO FIRE DAMAGE INSIDE APU ENCLOSURE.

Part: WARNING MESSAGE — ILLUMINATED (ANTI SKID SYS) · airframe 22,998 hrs · 23,083 cycles

ON TAKEOFF ROLL, RECEIVED ANTI-SKID OTBD CAUTION MESSAGE. ABORTED TAKEOFF BELOW 60 KTS.

Part: FLOORBEAM — CORRODED (FS 605) · corrosion level 2 · airframe 21,466 hrs · 21,601 cycles

FLOORBEAM AT FS 605 AND LBL 27 HAS CORROSION AROUND NUTPLATE. REMOVED CORROSION ON LBL 27 FLOORBEAM CAP AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. REMOVED AND REPLACED FLOORBEAM IAW REO 601R-53-21-3778.

Part: VANE — DENTED (RT WING TE FLAP) · airframe 21,519 hrs · 21,657 cycles

RT OTBD FLAP VANE HAS A DENT INBD ON VANE AT WS 162.49. REPAIRED RT OTBD FLAP VANE IAW REO 601R-57-53-041, REV B.

Part: ANGLE — CRACKED (FS 621) · airframe 21,519 hrs · 21,651 cycles

FS 621, FWD FACE LBL JUST BELOW W/L 120 ANGLE CRACKED. R & R ANGLE FS 621, LBL 36, W/L 120, SRM 51-40-11, 51-42-21.

Part: STRIKER — DAMAGED (FS 310) · airframe 21,466 hrs · 21,601 cycles

PAX DOOR CUT OUT FWD SEAL STRIKER DAMAGED FS 310.00. REPAIRED DAMAGE IAW REO 601R-53-22-033, REV C.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 21,519 hrs · 21,651 cycles

PAX DOOR AFT DRAG ANGLE CRACKED. REPAIRED PAX DOOR AFT DRAG ANGLE IAW REO 601R-52-11-513, REV A.

Part: BULKHEAD — CHAFED (FS 280) · airframe 21,466 hrs · 21,601 cycles

RT AFT FS 280 BULKHEAD CHAFED FROM GALLEY DOOR. REPAIRED DAMAGE IAW REO 601R-53-11-1727, REV E.

Part: WARNING LIGHT — FALSE ACTIVATION (SPOILERONS) · airframe 21,275 hrs · 21,368 cycles

SPOILERONS CAUTION MESSAGE TEMP DISPLAYED IN FLT ( 5 SEC`S) EXTINGUISHED ON ITS OWN. LATER ON APPROACH GEAR DOWN FLAPS 30 RECEIVED (GLD). INTEROGATED SECU NR 1, NR 2 FOR FAULTS ON FLT LEGS NO FAULTS NOTED PERFORM FIM RESET PROCEDURE, NO FURTHER DEFECTS NOTED IAW 27-61-05 FOR SECU INTEROGATION.

Part: THROTTLE — MALFUNCTIONED · airframe 21,119 hrs · 21,194 cycles

CONFIGUATION SPOILER WARNING MESSAGE AT 20 KTS ON TO ROLL. R & R THROTTLE QUADRANT IAW AMM 76-11-01, OPS AND RIGGING CHECKED GOOD.

Part: COMPUTER — FAILED (AHRS) · airframe 20,222 hrs · 20,276 cycles

AHRS NR 1 FAILED IN FLIGHT. COMPLIED WITH QRH SWITCHED TO AHRS NR 2. R & R NR1 AHRS IAW AMM 34-21-01. OPS CHECK GOOD.

Part: TRANSFER VALVE — MALFUNCTIONED (FUEL SYSTEM) · airframe 20,002 hrs · 20,045 cycles

IN FLT, RECEIVED FUEL IMBALANCE CAS MESSAGE. FUEL WAS IMBALANCED UP TO 1100 LBS. ESTIMATED T/O FUEL WAS 4500 LBS EACH WING AND 2500 LBS IN CENTER TANK. DURING QRH, IMBALANCE WAS 3570 LBS LT WING, 1370 LBS CENTER TANK, AND 4390 RT WING. IMBALANCED INCREASED AND LANDED WITH 1000 LBS IMBALANCE. REPLACED RT POWER CROSSFLOW VALVE.

Part: UNKNOWN — ODOR (CABIN) · airframe 19,806 hrs · 19,822 cycles

APU AUTOSHUTDOWN AT GATE WITH STRONG FUEL ODOR. INSPECTED APU FOUND NO EVIDENCE OF FUEL LEAKS.

Part: STRUT — BINDING (NLG) · airframe 19,683 hrs · 19,685 cycles

"WOW INPUT" CAUTION, "STEERING INOP" CAUTION, AND "WOW OUTPUT FAIL "STATUS, NORMALLY EXTENDED GEAR. RECEIVED 3 GREEN GEAR DISAGREE MESSAGE EXTINGUISHED. REARMED NWS. STEERING RE-ENGAGED. "WOW INPUT" AND "WOW OUTPUT FAIL" MESSAGE CLEARED DURING TAXI. FOUND NOSE STRUT INTERNAL PARTS BINDING JAMMED, R2 NLG STRUT ASSY IAW AMM 32-22-01, REF L/P 221069-2 FOR RIGGING OF NOSE WHEEL STEERING.

Part: RELAY — MALFUNCTIONED (CABIN ALTITUDE) · airframe 18,844 hrs · 18,809 cycles

WHILE HOLDING AT 16,000 FT RECEIVED CABIN ALTITUDE MESSAGE IMMEDIATELY FOLLOWED BY CABIN ALTITUDE WARNING MESSAGE COMPLIED WITH IAL AND QRH. R & R RELAYS K1GA & K2GA IAW ESPM REF W/C NR 2 FOR OPS CK OF JB11.

Part: CAM — WORN (FLAP VANE) · airframe 17,469 hrs · 17,373 cycles

RT OTBD FLAP, FLAP VANES CAMS WORN MEASURED RT OTBD FLAP VANE CAMS AND FOUND CAMS TO BE IN SERVICEABLE LIMITS IAW REO 601R-57-53-195.

Part: CAM — WORN (LT WING TE FLAP) · airframe 17,469 hrs · 17,373 cycles

LT OTBD FLAP CAMS ARE WORN. MEASURED LT OOTBD FLAP CAMS AND FOUND CAMS TO BE IN SERVICEABLE LIMITS IAW REO 601R-57-53-195.

Part: MOUNT — CRACKED (PAX DOOR) · airframe 17,469 hrs · 17,373 cycles

AFT PAX DOOR COUNTER BALANCE SPRING MOUNT CRACKED. R & R AFT PAX DOOR COUNTER BALANCE SPRING MOUNT WITH NEW IAW SRM 51-42-06, 51-42-43.

Part: PANEL — CRACKED (THRUST REVERSER) · airframe 17,469 hrs · 17,373 cycles

RT T/R CRACKED AT 6 O`CLOCK POSITION BELOW SAM PANEL. REPAIRED RT T/R IAW REO 601R-78-30-3998.

Part: SKIN — CHAFED (LT WING AILERON) · airframe 17,469 hrs · 17,373 cycles

LT AILERON L/E SKIN CHAFED FROM OTBD CTR HINGE BUT COTTER KEY. REPAIRED LT AILERON L/E SKIN FROM OTBD CTR HINGE NUT COTTER KEY IAW B/A REO 601R-57-60-078, REV A.

Part: SKID — CHAFED (APU) · airframe 17,469 hrs · 17,373 cycles

APU SKID ASSY CHAFED BY DRAIN LINE, REPOSITIONED DRAIN LINE. REPAIRED SKID IAW REO 601R-49-12-008.

Part: STEP — CRACKED (PAX DOOR) · airframe 17,469 hrs · 17,373 cycles

PAX DOOR AFT UPPER CORNER ON STAIR STEPS CRACKED. REPAIRED IAW REO 601R-52-11-279.

Part: FITTING — CHAFED (LT WING) · airframe 17,469 hrs · 17,373 cycles

LT OTBD FLAP GUIDE ROLLER FITTING CHAFED. REPAIRED IAW REO 601R-57-53-809.

Part: FITTING — CHAFED (RT WING TE FLAP) · airframe 17,469 hrs · 17,373 cycles

RT OTBD FLAP, GUIDE ROLLER FITTING CHAFED. REPAIRED IAW REO 601R-57-53-809.

Part: SEAL — CRACKED (LT WING) · airframe 17,469 hrs · 17,373 cycles

SEAL ON OTBD SIDE OF LT FLIGHT SPOILER ATTACHED TO WING HAS A 5" CRACK. R & R WITH NEW SERVICEABLE SEAL IAW SRM 51-42-06 AND SRM 51-41-02.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 17,469 hrs · 17,373 cycles

INTERCOSTAL CRACKED BETWEEN FS 338.0 AND 347.25 WL 147 INTERNAL PAX DOOR STRUCTURE. REPLACED IAW SRM.

Part: FRAME — CORRODED (BS 333 S26L/R) · corrosion level 2 · airframe 17,469 hrs · 17,373 cycles

CORROSION ON FRAME FS 333.00 BETWEEN STR 26L AND STR 26R. REMOVED CORROSION (LEVEL 1) BETWEEN STR 27 AND STR 26L IAW SRM 51-21-06 AND REPAIR FRAME AS 333.00 BETWEEN STR 27 AND 26R IAW REO 601R-53-21-149, REV ORIGINAL.

Part: STRIP — CHAFED (LT NACELLE) · airframe 17,469 hrs · 17,373 cycles

LT ENGINE LOWER NOSE COWL AFT EDGE STRIP IS CHAFED. R & R UNSERVICEABLE LT ENGINE LOWER NOSE COWL AFT EDGE STRIP AND INSTALLED SERVICEABLE AFT EDGE STRIP IAW CMM 71-14-10.

Part: FAIRING — CHAFED (LT FUSELAGE) · airframe 17,469 hrs · 17,373 cycles

LT FUSELAGE UNDER LT INBD FLAP STUB FAIRING AND FWD OF FAIRING CHAFED. REPAIRED CHAFE DAMAGE ON LT FUSELAGE UNDER INBD FLAP STUB FAIRING FWD IAW MFG REV ORIG REO 601R-53-41-1233.

Part: FAIRING — CHAFED (FUSELAGE) · airframe 17,469 hrs · 17,373 cycles

RT FUSELAGE UNDER FLAP STUB FAIRING HAS CHAFING DAMAGE AND FWD OF FAIRING. REPAIRED CHAFE DAMAGE ON RT FUSELAGE UNDER FLAP STUB FAIRING FWD, IAW REV ORIG REO 601R-53-41-1233.

Part: SKIN — UNSERVICEABLE (RT WING AILERON) · airframe 17,469 hrs · 17,373 cycles

RT AILERON BOTTOM L/E INBD SKIN PN CC670-13052-2. R & R NEW SERVICEABLE SKIN.

Part: STIFFENER — CHAFED (BS 621) · airframe 17,469 hrs · 17,373 cycles

VERTICAL STIFFENER ON REAR FACE OF 621 BULKHEAD CHAFED APPROX 6" DOWN FROM TOP. REPAIRED VERTICAL STIFFENER ON REAR FACE OF 621 BULKHEAD APPROX 6" DOWN FROM TOP IAW B/A REP NR 601R-53-61-1523, REV ORIGINAL.

Part: FLOORBEAM — CORRODED (BS 280) · corrosion level 2 · airframe 17,469 hrs · 17,373 cycles

FWD FLOOR ANGLE FS 280.00, WL 73.10 HAS CORROSION. R & R FWD FLOOR ANGLE IAW SRM 51-42-06.

Part: PANEL — CHAFED (LT WING TE FLAP) · airframe 17,469 hrs · 17,373 cycles

LT INBD FLAP STUB PANEL HAS CHAFING. REMOVED UNSERVICEABLE FLAP STUB FROM LT INBD FLAP AND INSTALLED SERVICEABLE FLAP STUB.

Part: PLATE — DAMAGED (BS 574) · airframe 17,469 hrs · 17,373 cycles

CARGO STEP PLATE DAMAGED (2EA) GOUGES (1) FWD AND (1) AFT REMOVED STEP PLATE UNSERVICEABLE AND REPLACED SERVICEABLE CARGO STEP PLATE PN 601R35205-65 IAW SRM 51-42-06.

Part: HINGE — DAMAGED (BS 574) · airframe 17,469 hrs · 17,373 cycles

DAMAGED SCREW HOLES IN CARGO STEP PLATE HINGE ASSY. REMOVED UNSERVICEABLE HINGES (3 EA) AND REPLACED W/NEW HINGES (3 EA) PN 601R35205-06, 601R35205-71, AND 601R3520567 IAW SRM 51-42-06.

Part: STRUCTURE — CHAFED (RT NACELLE) · airframe 17,469 hrs · 17,373 cycles

RT UPPER NOSE COWL AFT EDGE STRIP IS CHAFED. REPAIR CHAFED DAMAGE ON RT UPPER NOSE COWL AFT AND EDGES STRIP IAW CMM 71-14-01.

Part: ATTACH FITTING — CORRODED (BS 338.0) · corrosion level 2 · airframe 17,469 hrs · 17,373 cycles

AFT ATTACH CLIP IS CORRODED ON PAX DOOR INNER FRAME UPPER END AT FS 338.00. R & R WITH NEW IAW SRM 51-42-06.

Part: PANEL — CHAFED (RT WING AILERON) · airframe 17,469 hrs · 17,373 cycles

RT AILERON L/E PANEL 699BB HAS MINOR CHAFE DAMAGE BLENDED IAW SRM 57-60-00 WITH .002" MATERIAL LOSS.

Part: PANEL — CHAFED (RT WING AILERON) · airframe 17,469 hrs · 17,373 cycles

RT AILERON L/E 699CB HAS MINOR CHAFE DAMAGE. REPAIRED IAW 200-57-60-06 WITH 0.0003 MATERIAL LOSS.

Part: PANEL — CHAFED (RT WING AILERON) · airframe 17,469 hrs · 17,373 cycles

RT AILERON PANEL 699AB HAS MINOR CHAFE DAMAGE. REAPIRE IAW REO 601R-57-60-020 WITHIN .013 MATERIAL LOSS.

Part: ATTACH FITTING — CORRODED (PAX DOOR) · corrosion level 2 · airframe 17,469 hrs · 17,373 cycles

FWD ATTACH CLIP IS CORRODED ON PAX DOOR INNER FRAME UPPER EOP AT FS 320.10. R & R WITH NEW SRM 51-42-06.

Part: ATTACH FITTING — CORRODED (BS 320) · corrosion level 2 · airframe 17,469 hrs · 17,373 cycles

AFT ATTACH CLIP IS CORRODED ON PAX DOOR INNER FRAME UPPER EOP AT FS 320. R & R SRM 51-42-06.

Part: RIB — CRACKED (RT WING) · airframe 17,469 hrs · 17,373 cycles

RT MLG BATT RIB IS CRACKED, REO 601R-57-51-046.

Part: SKIN — CHAFED (BS 559) · airframe 17,469 hrs · 17,373 cycles

SKIN BELOW LAV CHARGE PORT IS CHAFED. REPAIRED CHAFE ON SKIN BELOW LAV CHARGE PORT IAW SRM 53-00-31 AND SRM 53-51-31.

Part: INTERCOSTAL — CRACKED (BS 625) · airframe 17,469 hrs · 17,373 cycles

RT INTERCOSTAL LOCATED BETWEEN FS 621 AND FS 625.30 IS CRACKED. REMOVED AND FABRICATED NEW INTERCOSTAL AND INSTALLED IAW REO 601R-53-61-100, REV A AND REO 601R-53-61-422.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 17,469 hrs · 17,373 cycles

FLOOR SUPPORT AT FS 280 CRACKED OTBD OF RBL 9.0 AND LBL 9.0 REO REPAIR 601R-53-11-136, REV A.

Part: INTERCOSTAL — CRACKED (BS 621-625.3) · airframe 17,469 hrs · 17,373 cycles

LT INTERCOSTAL LOCATED BETWEEN FS 621 AND 625.30 IS CRACKED. R & R WITH NEW FABRICATED INTERCOSTAL IAW REO 601R-53-61-100 REV A AND REO 601R-53-61-422.

Part: CHANNEL — CRACKED (BS 574) · airframe 17,469 hrs · 17,373 cycles

CARGO DOOR FWD ROLLER GUIDE "C" CHANNEL CRACKED. GOING FROM UNDER RIVET HEAD. REPLACE IAW SRM 51-42-06 AND 51-31-06.

Part: VANE — CHAFED (LT WING TE FLAP) · corrosion level 1 · airframe 17,469 hrs · 17,373 cycles

LT INBD FLAP VANE CHAFING DAMAGE TO L/E IN 3 PLACES DAMAGE MINOR IN PAINT ONLY. HAND BLENDED IAW SRM 57-52-00 AND 57-00-31. REAPPLIED PRIMER AND TOP COAT IAW SRM 51-25-06 AND 51-25-26. DELETED DAMAGE MINOR IN PAINT ONLY.

Part: BRACKET — CRACKED (LT ENGINE) · airframe 17,469 hrs · 17,373 cycles

LT JET PIPE PANEL 436BR NUT PLATE BRACKET IS CRACKED IN HALF XN 221.0. R & R BRACKET IAW SRM 51-42-06, 51-40-11.

Part: BRACKET — CRACKED (LT EXHAUST) · airframe 17,469 hrs · 17,373 cycles

LT JET PIPE PANEL 436BL NUTPLATE BRACKET IS CRACKED IN HALF XN 221.0. R & R BRACKET IAW SRM 51-42-06, 51-40-11.

Part: RETAINER — CRACKED (PYLON) · airframe 17,469 hrs · 17,373 cycles

SEAT RETAINER CRACKED ON PANEL 412AT. RETAINER REPAIRED IAW SRM 54-00-00, CRACK APPROX .030" IN LENGTH.

Part: PANEL — CORRODED (PAX DOOR) · corrosion level 2 · airframe 17,469 hrs · 17,373 cycles

PAX DOOR TOP STEP PANEL 832 ET HINGE IS CORRODED. REMOVED UNSERVICEABLE HINGE AND REPLACED SERVICEABLE HINGE P/N 601R31980-41 IAW ARM 52-11-04-400-801.

Part: RETAINER — CRACKED (RT PYLON) · airframe 17,469 hrs · 17,373 cycles

RT PYLON 422BT SEAL RETAINER IS CRACKED. R & R SEAL RETAINER IAW AMM 54-63-01 IAW SRM 51-42-06. R & R.

Part: GUIDE — CRACKED (PYLON) · airframe 17,469 hrs · 17,373 cycles

RT PYLON PANEL DIVERTER GUIDE HAS CRACK. R & R DIVERTER GUIDE.

Part: RETAINER SEAL — CRACKED (PYLON) · airframe 17,469 hrs · 17,373 cycles

LT PYLON SEPARATOR PANEL NR 412DB SEAL RETAINER CRACKED AND SEAL WORN. R & R LT PYLON PANEL NR 412DB SEAL AND SEAL RETAINER PN 601-37003-65 AND PN 601-337003-303 IAW SRM 51-42-06, 51-40-11 AND AMM 54-63-01.

Part: SKIN — CHAFED (RUDDER) · airframe 17,469 hrs · 17,373 cycles

MINOR CHAFING FULL LENGTH OF RUDDER RT SIDE TOWARDS L/T REPAIR CHAFING DAMAGE ON RUDDER RT L/E IAW SRM 55-40-00.

Part: ACCESS PANEL — CRACKED (TAILCONE) · airframe 17,469 hrs · 17,373 cycles

TAILCONE ACCESS DOOR 361AB HAS A CRACKED LOUVER REPAIRED TAILCONE ACCESS DOOR CRACKED LOUVERS IN (2) LOCATIONS IAW REO 601R-53-84-012.

Part: ANGLE — CRACKED (BS 559) · airframe 16,336 hrs · 16,177 cycles

CRACK FOUND IN CAP ANGLE AT FS 559.00, LBL 18.00, LENGTH IS 0.500". REPAIR PERFORMED AT FS 559.00, LBL 18.00 ON CAP ANGLE IAW REO 601R-53-61-260, REV D AND REO 601R-53-61-609, REV A DEVIATION E. (K)

Part: BULKHEAD — CRACKED (BS 621) · airframe 16,336 hrs · 16,177 cycles

CRACK FOUND ON AFT PRESSURE BULKHEAD AT END OF CARGO TRACK FS 621.00, LBL 27.50, WL 130.00. REPAIR PERFORMED ON AFT PRESSURE BULKHEAD AT END OF CARGO TRACK FS 621.00, LBL 27.50, WL 130.00 IAW REO 601R-53-61-1541, REV B. (K)

Part: ANGLE — CRACKED (BS 559) · airframe 16,336 hrs · 16,177 cycles

CRACK FOUND IN CAP ANGLE AT FS 559.00, RBL 18.00, CRACK LENGTH IS .500". REPAIR PERFORMED ON CAP ANGLE AT FS 559.00, RBL 18.00 IAW REO 601R-53-41-260, REV D AND REO 601R-53-41-609, REV A. (K)

Part: A/C PACK — OVERHEATED (RIGHT) · airframe 14,857 hrs · 14,752 cycles

(AT GATE) RT PACK HIGH TEMP IND FOLLOWED BY REPORT FROM F/A OF WARM CABIN TEMP AND HAZE IN CABIN. OPERATED RT PACK FOR 30 MINUTES, ZERO DEFECTS NOTED. OPERATED LT PACK, LIGHT, FANS, LAV FLUSH ETC IN CABIN AND LAV. NO DEFECTS NOTED. ACFT RELEASED FOR SERVICE. (K)

Part: FLAP — MALFUNCTIONED (WING) · airframe 14,071 hrs · 14,001 cycles

LOG 193206/3 FLAPS FAILED AT ZERO. COMPLIED WITH QRH. DIVERTED TO ALB. BRAKE TEMP 4,2,1,3. COMPLIED WITH RESET PROCEDURE IAW AWAC SUPPLEMENT 98-018B STEPS 1.3 AND 1.4. FLAP SYSTEM RESET OK. NOTED BY MX.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 13,959 hrs · 13,886 cycles

PRE FLIGHT SMELL OF SMOKE IN COCKPIT WITH LT PACK ON. UPON BOARDING ACFT FOUND APU RUNNING WITH BOTH LT AND RT PACKS ON AND OPERATING NORMALLY. INSPECTED ALL WINDOW HEAT CONNECTIONS, TERMINALS, COCKPIT CB`S AND LIGHTS. ALL APPEAR NORMAL. NO ODOR OR SMOKE NOTED AT THIS TIME. ACFT OK FOR SERVICE.

Part: DUCT — SEPARATED (COOL AIR) · airframe 12,804 hrs · 12,777 cycles

DISPLAY COOL CAUTION MESSAGE IN FLIGHT. RAN QRH AND MESSAGE PERSISTED. MESSAGE EXTINGUISHED BELOW 8000 FT. FOUND COOLING AIR SUPPLY DUCT PARTED AT CLAMP. RE-INSTALLED CLAMP IAW 21-20-00. NO FURTHER DEFECTS FOUND AT THIS TIME. (A)

Part: LANDING GEAR — LACK OF LUBE (NOSE) · airframe 12,792 hrs · 12,767 cycles

WHEN LANDING GEAR WAS SELECTED DOWN, A CLICKING OR BINDING SOUND WAS HEARD FROM NOSE GEAR AREA UNTIL NOSE GEAR WAS LOCKED DOWN. SWUNG NLG ON GROUND, LUBED NLG PER AMM 12-32-00. OK FOR SERVICE.

Part: HOLDER — SPARKS (COCKPIT) · airframe 12,755 hrs · 12,726 cycles

FIRST OFFICERS CHART HOLDER SPARKED WHEN MOVED-POPPED CIRCUIT BREAKER ON CBP2 UG. SUFFICIENT LIGHTING EXISTS FOR DUTIES. PLACARDED AND PLACED ON MEL. OPEN (A)

Part: PLATE — CRACKED (FUSELAGE) · airframe 12,711 hrs · 12,688 cycles

FWD BRACKET OF CARGO STEP PLATE AT FS 575.00, WL 73.50. LBL 40 IS CRACKED. FWD BRACKET OF CARGO STEP PLATE AT FS 575, WL 73.5, LBL 40 REPLACED IAW SRM 51-42-21. (A)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 12,711 hrs · 12,688 cycles

FLOOR SUPPORT ANGLE AT FS 621.00, WL 73.50, LBL 40 IS CRACKED, DIMESNSIONS OF CRACK IS .400" LONG. DAMAGED PORTION OF ASSY ANGLE 601R35031-239 CUT AWAY, IAW REO 601R53-60-117 REV A, AT FS 621.00, WL 73.50, LBL 40, REPAIRED IAW REO 601R53-61-117 REV C. (A)

Part: BRACKET — CRACKED (FUSELAGE) · airframe 12,711 hrs · 12,688 cycles

AFT BRACKET OF HYDRAULIC RESERVOIR (SYSTEM 3) CRACK IN MLG BAY BL 0. AFT BRACKET OF HYDRAULIC RESERVOIR (SYSTEM 3) IN MLG BAY BL 0 REPLACED IAW SRM 51-42-13. (A)

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 12,711 hrs · 12,688 cycles

CRACK ON PAX DOOR EDGE MEMBER AT FS 316. CRACK ON PAX DOOR EDGE MEMBER AT FS 316 REPAIRED IAW REO 601R-52-11-279. (A)

Part: SILL — CRACKED (FUSELAGE) · airframe 12,711 hrs · 12,688 cycles

CARGO BAY FLOOR SILL AT FS 574.00, WL 73.5, LBL 39 IS CRACKED. CARGO BAY FLOOR SILL AT FS 574, WL 73.5, LBL 39 REPAIRED IAW REO 601R-53-61-1741. (A)

Part: SUPPORT — BROKEN (RT NACELLE) · airframe 12,711 hrs · 12,688 cycles

RT ENGINE NOSE INLET HAS A SUPPORT ASSY BROKEN FOR THE T2 LINE AT 12 O`CLOCK POSTIOIN. RT ENGINE NOSE INLET SUPPORT ASSY FOR T2 LINE AT 12 O`CLOCK POSITION REPLACES IAW SRM 51-42-06. (A)

Part: GUARD — TORN (PAX DOOR) · airframe 12,711 hrs · 12,688 cycles

PAX DOOR WEATHER GUARD IS TORN AND RETAINER IS CRACKED. REPLACED PAX DOOR WEATHER GUARD RETAINER IAW SRM 51-42-13 AND SRM 51-41-02. (A)

Part: PLATE — CRACKED (FUSELAGE) · airframe 12,711 hrs · 12,688 cycles

CARGO FLOOR LANDING PLATE AT FS 605, WL 73.5, LBL 39 IS CRACKED. CARGO FLOOR LANDING PLATE AT FS 605, WL 73.5, LBL 39 REPAIRED IAW REO 601R-53-61-433. (A)

Part: FITTING — CRACKED (FUSELAGE) · airframe 12,711 hrs · 12,688 cycles

CLIP CRACKED AT FS 484 RBL 27 UNDER FLOOR. CLIP AT FS 484, RBL 27 UNDER FLOOR REPLACED IAW SRM 51-42-06 AND SRM 51-42-21. (A)

Part: SILL — CORRODED (FUSELAGE) · corrosion level 1 · airframe 12,711 hrs · 12,688 cycles

LT LOWER SILL CORRODED AROUND NUT PLATE HOLES BTWN FS 574 TO FS 621 AT LBL 43 AND WL 73. CORROSION REMOVED AROUND NUT PLATE HOLES ON SILL IAW SRM 51-21-06. (A)

Part: FITTING — CRACKED (FUSELAGE) · airframe 12,711 hrs · 12,688 cycles

BOTH CLIPS CRACKED AT FS 280 AND LBL 9 ON CROSSBEAM. BOTH CLIPS REPLACED AT FS 280 AND LBL 9 ON CROSSBEAM IAW CRJ 200 SRM 51-42-06 AND SRM 51-42-21. (A)

Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 12,711 hrs · 12,688 cycles

CROSSBEAM CRACKED AT FS 280 AND RBL 9.0. CROSSBEAM AT FS 280 RBL 9.0 REPAIRED IAW REO 601R-53-11-171 REV D. (A)

Part: LONGERON — CORRODED (BS 319) · corrosion level 1 · airframe 12,711 hrs · 12,688 cycles

CORROSION AT PASSENGER DOOR LOWER LONGERON ON FUSELAGE AT FS319. CORROSION AT PAX DOOR LOWER LONGERON AT FS 319 REMOVED IAW CRJ 200 SRM 51-21-06. (A)

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 12,193 hrs · 12,189 cycles

FLAP FAIL AT ZERO ON APPROACH, COMPLIED WITH REST PROCEDURE IAW AWAC SUPPLEMENT 98-018B STEPS 1.3 AND 1.4 FLAP SYSTEM RESET OK. RESET NOTED BY MAINTENANCE. (M)

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 12,193 hrs · 12,189 cycles

FLAPS FAIL AT ZERO ON APPROACH. C/W RESET PROCEDURE IAW AWAC SUPP 98-018B STEPS 1.3 AND 1.4, FLAP SYSTEM RESET OK. RESET NOTED BY MAINTENANCE. (M)

Part: FLAP SYSTEM — FAILED (WING) · airframe 12,136 hrs · 12,133 cycles

FLAPS FAILED AT ZERO IN FLIGHT. RESET PROCEDURE IAW AWAC SUPP 98-018B STEPS 1.3 AND 1.4. FLAP SYSTEM RESET OK. (K)

Part: FLAP — FAILED (WING) · airframe 111,995 hrs · 12,005 cycles

FLAPS FAILED AT ZERO DEGREES, COMPLIED WITH QRH. FAILED ON APPROACH, OAT -1C. (K)

Part: FLAP — FAILED (WING)

ON APPROACH, WHEN FLAPS SELECTED, THE FLAPS FAILED TO MOVE AND (FLAPS FAIL) EICAS MESSAGE APPEARED, DIVERTED TO PIT, LANDED WITHOUT INCIDENT. (K)

Part: FLAP — FAILED (WING)

FLAPS FAILED AT 0 DEGREES ON APPROACH. (K)

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS)

FLAPS FAILED AT 0 DEGREES ON APPROACH. REMOVED AND REPLACED FECU REF AMM 27-51-05. OP CHECKS GOOD REF BLOCK 3 DURING TROUBLESHOOTING FOUND FAULT CODES TO SHOW LOGIC PROBLEM IN THE FECU. (K)

Part: FLAP SYSTEM — FAILED (TE FLAPS)

FLAPS FAIL AT ZERO ON APPROACH, DURING FLAP EXTENSION. (K)

Part: FLAP — MALFUNCTIONED (WING) · airframe 11,894 hrs · 11,904 cycles

FLAPS FAIL CAUTION MESSAGE AT ZERO ON APPROACH. COMPLIED WITH RESET PROCEDURE IAW AWAC SUPPLEMENT 98-018B STEPS 1.3 AND 1.4. FLAP SYSTEM RESET, OK. (K)

Part: WARNING MESSAGE — ILLUMINATED

ABORTED TAKEOFF AT 80 KNOTS FOR YELLOW "ICE" CAS MESSAGE, BRAKE TEMPS 7-5-4-7. OPS CHECK OF ICE DETECTION IAW 30-81-01. OPS CHECK GOOD AT THIS TIME.

Part: IDG — UNDERSERVICED (NR 2)

TAKEOFF ABORTED DUE TO RIGHT IDG CAUTION AND THEN RIGHT GENERATOR DROPPING OFF LINE. TAKEOFF ABORTED AT 70 KNOTS, MINIMAL BRAKING. BTMS BRAKE TEMPS READ 2-1-1-2. SERVICED IDG NR 2 IAW CRJ AMM 12-13-24. RAN ENGINE WITH OPS CHECK OF IDG NR 2. OPS CHECK GOOD. (M)

Part: IDG — UNDERSERVICED (NR 2) · airframe 11,724 hrs · 11,748 cycles

TAKEOFF ABORTED DUE TO RIGHT IDG CAUTION AND THEN RIGHT GENERATOR DROPPING OFF LINE. TAKEOFF ABORTED AT 70 KNOTS, MINIMAL BRAKING. BTMS BRAKE TEMPS READ 2-1-1-2. SERVICED IDG NR 2 IAW CRJ AMM 12-13-24. RAN ENGINE WITH OPS CHECK OF IDG NR 2. OPS CHECK GOOD. (M)

Part: PRIORITY VALVE — INOPERATIVE (MLG) · airframe 10,544 hrs · 10,584 cycles

GOT GEAR DISAGREE WHEN LOWERING GEAR FOR LANDING. CYCLED GEAR UP AND DISAGREE WITH GEAR UP ALSO. COMPLIED WITH DISAGREE CHECKLIST AND HAD NORMAL INDICATION. REMOVED AND REPLACED MLG PRIORITY VALVE IAW AMM 32-32-15. OPS CHECK GOOD. (K)

Part: MOTOR — MALFUNCTIONED (PAX DOOR)

PAX DOOR VERY DIFFICULT TO OPEN. COMPLY WITH `M` ACTION FOR MEL. PAX DOOR ASSIST DEACTIVATED. PLACARDED AND PLACED ON MEL. REMOVED AND REPLACED PAX DOOR ASSIST MOTOR. REMOVED AND REPLACED DOOR STRUTS PER CRJ AMM 52-11-17. OPERATIONAL CHECK GOOD. REMOVED PLACARD, REMOVED OFF MEL. (M)

Part: SKIN — CRACKED (PAX DOOR)

AFT PAX DOOR SKIN AT RADIUS OF STEP 2 AND 3 CRACKED IN 2 PLACES. MAINTENANCE PAX DOOR SKIN IAW BOMBARDIER REO 601R-52-11-702. (M)

Part: DRAG ANGLE — BUCKLED (PAX DOOR)

PASSENGER DOOR AFT DRAG ANGLE IS BUCKLED IN AREA OF ASSIST MOTOR CABLE PULLEY. MAINTENANCE REPAIRED AFT DRAG ANGLE IAW BOMBARDIER REO 601R-52-11-513. (M)

Part: CASE — CRACKED (LT ENGINE)

LT ENGINE LOW PRESSURE TURBINE CASE IS CRACKED 1.5 INCHES LONG AT 9 O`CLOCK POSTION .75 INCH AFT OF FORWARD FLANGE. CLEANED SUSPECT AREA AND PERFORMED LPI IAW CRJ NDTM 51-20-08. FOUND 1 CRACK LIKE INDICATION APPROXIMATELY 1.5 INCH LONG AT 9 O`CLOCK POSITION. ENGINE IS OK FOR CONTINUED SERVICE IAW GE CDR CF34-3-06-140R WITH CONTINUING INSPECTION REQUIREMENTS. (M)

Part: SUPPORT BRACKET — CRACKED (RT MLG WW)

HYDRAULIC PRESSURE TRANSDUCER LINE SUPPORT BRACKET, P/N 601R75262-153 IN RT WHEEL WELL CEILING CRACKED. REMOVED AND REPLACED HYDRAULIC PRESSURE TRANSDUCER LINE SUPPORT BRACKET P/N 601R75262-153 IN RT WHEEL WELL IAW CRJ 200 SRM 51-42-06. (M)

Part: BRACKET — CRACKED (LT MLG WW)

HYDRAULIC PRESSURE TRANSDUCER BRACKET P/N 601R75262-159 CRACKED IN LEFT WHEEL WELL CEILING. REMOVED AND REPLACED BRACKET, P/N 601R75262-159, IAW CRJ SRM 51-40-11. (M)

Part: BRACKET — CRACKED (RT MLG WW)

HYDRAULIC PRESSURE TRANSDUCER BRACKET P/N 601R75262-157 IN RT WHEEL WELL CEILING CRACKED. REMOVED AND REPLACED BRACKET P/N 601R75262-157 IAW CRJ SRM 51-40-11. (M)

Part: INTERCOSTAL — CRACKED (BS 484)

FOUND RIGHT FS 484 INTERCOSTAL HAS A .25 INCH CRACK AT RBL 36 ANGLE. REPAIRED ANGLE IAW REO 601R-53-41-059 REV A AND BSC STANDARD REPAIR 601R-53-0030A. (M)

Part: FLOOR SUPPORT — CRACKED (BS 621)

FOUND RT FS 621 FLOOR SUPPORT ANGLE CRACKED .5 INCH LONG IN OUTBOARD RADIUS. REPAIRED FLOOR SUPPORT ANGLE IAW REO 601R-53-61-117 REV C. (M)

Part: INTERCOSTAL — CRACKED (BS 484)

FOUND LEFT FS 484 INTERCOSTAL HAS A .25 INCH CRACK AT LBL 36 ANGLE. REPAIRED INTERCOSTAL IAW REO 601R-53-41-059 REV A AND BSC STANDARD REPAIR 601R-53-0030A. (M)

Part: SUPPORT CHANNEL — CRACKED (DOOR CAM TRACK)

FOUND FS 574 BAGGAGE DOOR CAM TRACK LOWER SUPPORT CHANNEL P/N 601R-35050-25 IS CRACKED .75 INCH LONG. REMOVED AND REPLACED CHANNEL, P/N 601R35050-25 IAW CRJ SRM 51-42-06. (M)

Part: INTERCOSTAL — CRACKED (BS 621-625)

FOUND LEFT UPPER FS 621 TO FS 625 INTERCOSTAL/OBLIQUE ANGLE IS CRACKED 1.5 INCHES LONG IN THE AFT RADIUS P/N 601-35012-51. REMOVED LEFT UPPER FS 621 TO 625 OBLIQUE ANGLE CRJ 200 SRM 51-42-06. INSTALLED NEW INTERCOSTAL/OBLIQUE ANGLE AT LBL 45 AT STRINGER 14L IAW CRJ 200 SRM 51-42-06. (M)

Part: INTERCOSTAL — CRACKED (FS 625)

RT UPPER FS 621 TO FS 625 INTERCOSTAL/OBLIQUE ANGLE P/N 601-35012-52 IS CRACKED 1.5 INCHES LONG IN AFT RADIUS. REMOVED RT UPPER 621 TO 625 OBLIQUE ANGLE IAW CRJ 200 SRM 51-42-06. (M)

Part: WARNING LIGHT — ILLUMINATED (CAS SYS) · airframe 5,085 hrs · 5,358 cycles

AT 32,000 FT, A FUEL IMBALANCE CAS MESSAGE APPEARED ON EICAS. THE PROBLEM WAS NOT CORRECTABLE USING AUTO, MANUAL OR GRAVITY CROSSFLOW. LT WING HEAVY AT LANDING AN IMBALANCE 1700 LBS C/W QRH. SHUTDOWN ENG NR 2, LANDING WEIGHT WAS NOT EXCEEDED. PERFORMED SYSTEM OPS CHECK OF FUEL CROSS FLOW, NO FAULTS FOUND, ALSO PERFORMED GRAVITY CROSSFLOW, NO FAULTS FOUND. REMOVED AND REPLACED FUEL COMPUTER SYSTEM, OPS CHECK GOOD. (K)

Part: RELIEF VALVE — FAILED (A/C PACK)

DURING DESCENT WITH POWER AT IDLE BOTH PACKS DROP OFF LINE. REMOVED AND REPLACED RT AND LT PRESSURE RELIEF VALVES IAW 21-51-43. (M)

Part: SKIN — LIGHTNING STRIKE (FUSELAGE)

WHILE PERFORMING LIGHTNING STRIKE DAMAGE INSPECTION FOUND RIGHT FUSELAGE AREA BETWEEN STRINGER 24R-25R AT FS 220-235 TO BE PREVIOUSLY BLENDED BEYOND LIMITS OF SRM 53-00-31. BLEND DEPTH .010 INCH. CUTOUT DAMAGED SECTION AND INSTALLED LOCALLY FABRICATED DOUBLER AND FILLER IAW BRAS EO 601R-53-5343. (M)

Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 3,782 hrs · 4,215 cycles

MWC 121, LIGHTNING STRIKE DAMAGE AT FS 202.75, STR 22R. BLEND DAMAGED AND ENSURED AREA IS CRACK FREE IAW REO 601R-53-11-814.

Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 3,782 hrs

MWC 122, LIGHTNING STRIKE DAMAGE AT FS 235.00, STR 15R. BLENDED DAMAGE AND ENSURED ARE IS CRACK FREE IAW REO 601R-53-11-814.

Part: SKIN — LIGHTNING STRIKE (FUSLEAGE)

WHILE PERFORMING LIGHTNING STRIKE DAMAGE INSPECTION FOUND RIGHT FUSELAGE AREA BETWEEN STRINGER 27R-26R AT FS 257 TO BE PREVIOUSLY BLENDED BEYOND LIMITS OF SRM 53-00-31. BLEND DEPTH .010 INCH. CUTOUT DAMAGED SECTION AND INSTALLED LOCALLY FABRICATED DOUBLER AND FILLER IAW BRAS EO 601R-53-5344. (M)

Part: SKIN — LIGHTNING STRIKE (FUSELAGE)

DURING LIGHTNING STRIKE DAMAGE INSPECTION OF RIGHT FUSELAGE FOUND AREA BETWEEN STRINGER 26R-27R AT FS 243 TO BE PREVIOUSLY BLENDED BEYOND LIMITS OF SRM 53-00-31. BLEND DEPTH .007 INCH. CUT OUT DAMAGED SECTION AND INSTALLED LOCALLY FABRICATED DOUBLER AND FILLER IAW BRAS EO 601R-53-5342. (M)