N442AW

Part: SKIN — CORRODED (ZOEN 600) · corrosion level 2 · airframe 43,575 hrs · 42,453 cycles

FOUND EROSION DAMAGE TO THE RIGHT WING LEDAING EDGE SKIN BETWEEN WS350.348 AND WS386.348. THE DAMAGE IS REMOVED MEASURING A MATERIAL LOSS OF UP TO 0.018". THE SKIN IS FORMED FROM 0.080" 6013-T6 AL ALLOY LOCALLY CHEM-MILLED TO 0.042". MAINTENANCE CONTACTED ENGINEERING FOR EVALUATION AND DISPOSITION. AIRCRAFT REMOVED FROM SERVICE PITTING DAMAGE INSPECTED AND REPAIRED REF. EA# AWAC-CRJ257-02085.

Part: SEALANT — FAILED (FAIRING) · airframe 43,532 hrs · 42,411 cycles

DURING CLIMB ABOVE 10K AND SPEED 268KTS A/C BUFFETS. WAS NOT FELT IN YOKE, AP WAS DISENGAGED. BUFFETING NOT PRESENT ABOVE 270KTS AND BELOW 265KTS. FLIGHT CONTROLS OPERATE NORMALLY WHEN BUFFETING OCCURS. BUFFETING OCCURS AT APPROX 2* NOSE UP AND 2* NOSE DOWN. AIRCRAFT REMOVED FROM SERVICE. FOUND IMPROPER CURED SEALANT ON FAIRING 193AB, RESEALED PNL 193AB IAW AMM 51-23 AS REQUIRED

Part: WATER SEPARATOR — ODOR · airframe 43,101 hrs · 41,918 cycles

AFTER LOW PRESSURE AIR WAS DISCONNECTED, ONCE APU LCV AND L PACK WAS TURNED ON, LIGHT HAZE SEEN AND SMELT IN COCKPIT. HAZE REPORTED FA IN CABIN AS WELL. INITIAL THOUGHT SMELT ELECTRICAL. AIRCRAFT REMOVED FROM SERVICE. CLEANED L AND R WATER SEPARATOR COALESCENT IAW AWAC SUPP 14-192A CYC PACKS, OPS CK AND RECHEDCK GOOD AT THIS TIME.

Part: COALESCER BAG — ODOR · airframe 42,955 hrs · 41,760 cycles

DURING FLIGHT AFTER SWITCHING TO APU BLEED AIR, GOT SMOKE IN CABIN AND COCKPIT. SMOKE WAS BLUE WITH OILY SMELL. SMOKE CLEARED AFTER SWITCHING BLEEDS BACK TO ENGINES. AIRCRAFT REMOVED FROM SERVICE REMOVED AND CLEANED WATER SEPARATOR COALESCER THEN PUT IT IN PLACE OPS CHECK GOOD AT THIS TIME IAW AWAC SUP 14-193. C/W AWAC SUP 09-037E NO ODERS OR SMOKE NOTED.

Part: COALESCER BAG — ODOR (WATER SEPARATOR) · airframe 42,955 hrs · 41,760 cycles

DURING FLIGHT AFTER SWITCHING TO APU BLEED AIR, GOT SMOKE IN CABIN AND COCKPIT. SMOKE WAS BLUE WITH OILY SMELL. SMOKE CLEARED AFTER SWITCHING BLEEDS BACK TO ENGINES. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND CLEANED WATER SEPARATOR COALESCER THEN PUT IT IN PLACE OPS CHECK GOOD AT THIS TIME IAW AWAC SUP 14-193. C/W AWAC SUP 09-037E NO ODERS OR SMOKE NOTED.

Part: INDICATOR — MALFUNCTIONED (STNDBY ATTITUDE) · airframe 42,979 hrs · 41,781 cycles

STANDBY ATTITUDE INDICATOR TUMBLED AFTER TAKE-OFF, INACCURATE DURING FLIGHT. STBY AI SHOWED LEVEL BEFORE TAKE-OFF AND AFTER LANDING. ***** AIRCRAFT REMOVED FROM SERVICE ***** R&R STANDBY ATTITUDE IAW AMM 34-23-01. OPS CHECK GOOD AT THIS TIME. P/N 501-1567-10, S/N OFF 3031, S/N ON 2048 SMK

Part: SENSOR — FAULTED (AILERON) · airframe 42,182 hrs · 40,854 cycles

ON APPROACH INTO MHK, THE FLAPS FAILED AT 8 DEGREES. AN EMERGENCY HAS BEEN DECLARED AND THE FLIGHT WILL CONTINUE INTO MHK. R&R OF R/H BPSU IAW AMM 27-51-10

Part: SKIN — DENTED (FS265) · airframe 41,395 hrs · 39,944 cycles

EXTERNAL FUSELAGE SKIN IS DENTED AT FS 265 BETWEEN STGR 24L AND 25L. AIRCRAFT REMOVED FROM SERVICE. COMPLIED WITH MHIRJ REO 601R-53-11-3834 REV-- DATED 2023-03-12 REPAIRED FUSELAGE SKIN BETWEEN FS250-FS265 AND STR23L -24L

Part: FLAP — DENTED (LH IB FLAP) · airframe 41,395 hrs · 39,944 cycles

LH INBD FLAP IS DENTED/PUNCTURED ON LOWER SKIN TRAILING EDGE AT APPROX. FLS 63.0. *******AIRCRAFT REMOVED FROM SERVICE********** REPAIRED LH IB FLAP LOWER SKIN IAW CRJ 200 AIRWIS SUPPLEMENT NO:15-230 AND MHIRJ ENGINEERING ORDER NO. : 600-2B19-57-L07424, DATE: 3/7/2023

Part: ANGLE — CRACKED (FS621 LBL36 WL79) · airframe 41,395 hrs · 39,944 cycles

STIFFENER ANGLE P/N 601R36008-51 LOCATED ON AFT SIDE OF FS621 PRESSURE BULKHEAD BETWEEN LBL36 AND STR 16B AT WL 79 IS CRACKED ON INBOARD END. *********AIRCRAFT REMOVED FROM SERVICE********** REPLACED STIFFENER ANGLE P/N 601R36008-51 AT AFT SIDE OF F.S. 621 BULKHEAD AT LBL 36 WL 79 IAW CRJ-200 SRM 51-42-06.

Part: PLATE — CORRODED (LH NACELLE) · corrosion level 2 · airframe 41,395 hrs · 39,944 cycles

L/H LOWER PYLON TRAILING EDGE BONDING PLATES HAVE CORRODED FASTENERS. ******AIRCRAFT REMOVED FROM SERVICE********** REMOVED AND REPLACED LH LOWER BONDING PLATE IAW AWAC SUPPLEMENT NO: 15-335.

Part: RETAINER — CORRODED (AVIONICS BAY DOO) · corrosion level 2 · airframe 41,395 hrs · 39,944 cycles

CORROSION FOUND ON ALL FOUR SEAL RETAINERS ON MAIN AVIONICS DOOR. ********AIRCRAFT REMOVED FROM SERVICE********* REMOVED AND REPLACED 4 EA. SEAL RETAINERS FOR MAIN AVIONICS DOOR IAW CRJ200 SRM 51-42-06

Part: BONDING PLATE — CORRODED (LH UPPER PYLON) · corrosion level 2 · airframe 41,395 hrs · 39,944 cycles

L/H UPPER PYLON TRAILING EDGE BONDING PLATES HAVE CORRODED FASTENERS. ******AIRCRAFT REMOVED FROM SERVICE********** REMOVED 12 RIVETS FROM LH UPPER PYLON BONDING PLATES IAW CRJ-200 SRM 51-42-13 INSTALLED 12 RIVETS IAW CRJ-200 SRM 51-42-13 REPLACED LH UPPER BONDING PLATE PN

Part: ANGLE — CORRODED (FS424 TO FS513) · corrosion level 2 · airframe 41,395 hrs · 39,944 cycles

LH FLOOR SILL ANGLE IS CORRODED IN MULTIPLE LOCATIONS BETWEEN FS 424 AND FS 513 *******AIRCRAFT REMOVED FROM SERVICE********** REMOVED CORROSION IN MULTIPLE SPOTS ON LH FLOOR SILL ANGLE BETWEEN FS 424 AND FS 513 IAW CRJ 200 SRM 51-21-06-00,REO 60

Part: PANEL — CORRODED (FS461-473 RBL45) · corrosion level 2 · airframe 41,395 hrs · 39,944 cycles

RH FLOOR SILL IS CORRODED BETWEEN FS 461 AND FS 473. *******AIRCRAFT REMOVED FROM SERVICE*********** REPAIRED RH PRESSURE FLOOR SILL PANEL BETWEEN FS461 AND FS 473 IAW MHIRJ REO 601R-53-41-3126 REV -- DATED 2023-03-14 AND BOMBARDIER REO NO. 601R-53-41-666, REV -C

Part: INTERCOSTAL — CRACKED (FS 621) · airframe 41,395 hrs · 39,944 cycles

ATTACHING CLIP CRACKED ON 3RD INTERCOSTAL ON R/H AFT SIDE OF AFT PRESSURE BULKHEAD. *********AIRCRAFT REMOVED FROM SERVICE********* INSTALLED NEW ATTACH CLIP (PN: 601-35012-54) IAW CRJ200 SRM 51-42-21

Part: HINGE ARM — GOUGED (RH IB FLAP WS80.) · airframe 41,395 hrs · 39,944 cycles

RH INBD FLAP HINGE ARM ASSY. AT WS 80.50 IS GOUGED ON LOWER MOUNT LUGS. *****AIRCRAFT REMOVED FROM SERVICE*********** REPAIRED RH IB FLAP HINGE ARM ASSY IAW MHIRJ REO 601R-57-54-358 REV -- DATED 2023-03-08

Part: BRACKET — CRACKED (RH FLAP STUB FAI) · airframe 41,395 hrs · 39,944 cycles

R/H FLAP STUB FAIRING HAS A BROKEN BRACKET THAT REQUIRES REPLACEMENT. ****AIRCRAFT REMOVED FROM SERVICE********** INSTALLED NEW R/H FLAP STUB FAIRING BRACKET AND RESTORED SURFACE FINISH IAW MHIRJ CRJ200 SRM 51-42-06-00 AND 51-21-16-00

Part: SENSOR — FAILED (TE FLAP SYSTEM) · airframe 41,223 hrs · 39,775 cycles

FLAPS FAILED AT 20 DEGREES WHEN TRYING TO SET FLAP TO 30 DEGREES. GEAR WAS DOWN AND WERE IN ICING CONDITIONS. RAN QRH FLAP FAIL PROCEDURE. CW FIM RESET, FLAPS FAILED AT ZERO. AIRCRAFT REMOVED FROM SERVICE. R & R SKEW DETECTION UNIT IRW AMM 27-51-15-04. OPS CHECKED GOOD.

Part: TRANSMITTER — FAULT MESSAGE · airframe 41,009 hrs · 39,586 cycles

FAULTY FLAP IND AND FLAPS DEGRADED MSG, FLUX BETWEEN 8-20 DEGREES @ 30,000' DOWN TO 3000' AND SET FLAPS 8 FOR LANDING- NORMAL IND AFTER THAT, BUT FLAPS DEGRADED MSG PERSISTED. WHEN INDICATION WAS FLUX AUTO PILOT PITCHED UP/DOWN. FLAPS SET 8 THRU 45 OPERATED NORMALLY WHEN SET FOR LANDING. ***AIRCRAFT REMOVED FROM SERVICE **** REF 351368-3 FOR R&R OF LH FLAP POSITION TRANSMITTER, OPS CHECK GOOD R&R LH FLAP POSITION TRANSMITTER IAW AMM 27-55-01 OPS CHECK GOOD P/N: 601R93030-3, S/N OFF: MULT7518604-001, S/N ON: 50796 ARW

Part: VISOR — GOUGED (H STAB LBL6) · airframe 39,682 hrs · 38,340 cycles

MAINTENANCE FOUND SCRATCH DAMAGE ON L/H HORIZONTAL STABILIZER ATTACHMENT VISOR AT LBL6. DIMENSIONS OF SCRATCH ARE: 19.00"L X 0.800"W X 0.007"D. ************AIRCRAFT REMOVED FROM SERVICE************************* BLENDED DAMAGED AREA TO A SMOOTH CONTOUR. DIMENSIONS AFTER BLEND ARE: 19.00"L X .800"W X .007"D. REMAINING MATERIAL THICKNESS OF .068". ORIGINAL THICKNESS OF .075". HFEC INSPECTION PERFORMED WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK PERFORMED WITHIN ALLOWABLE LIMITS IAW ASAP EA #AWAC-CRJ253-01786 REV IR DATED 12/29/2021. WORK COMPLETED ON AERSALE WO #003500 CARD #20463 AT AERSALE CRS #4AER685B. N442AW TT: 39,682:59 TC:38,340.

Part: SKIN — DENTED (FS 736+15) · airframe 39,682 hrs · 38,340 cycles

AIRCRAFT R/H SKIN EXTERIOR HAS 1 EACH DENT AT FS 736+15 AND S20R+2. S21R HAS EDGE DAMAGE AT SAME AREA ON SKIN INTERIOR MEASURING: .450"L X .050"W X .050"D. DENT DIMENSIONS ARE: (P1) .600L X .300W X .008D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE*********************** BLENDED EDGE OF S21R SMOOTH, REMOVING EDGE DAMAGE IAW CRJ200 SRM 53-00-00 REV 38. 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-CRJ253-01783 REV IR DATED 12/28/2021. ALL WORK PERFORMED IAW ASAP EA # AWAC-CRJ253-01783 REV IR DATED 12/28/2021. WORK COMPLETED AT AERSALE CRS4AER685B ON W/O #003500 CARD #20156. N442AW TT:39,682:59 TC: 38,340

Part: VISOR — GOUGED (H STAB RBL6) · airframe 39,682 hrs · 38,340 cycles

MAINTENANCE FOUND SCRATCH DAMAGE ON R/H HORIZONTAL STABILIZER ATTACHMENT VISOR AT RBL 6. DIMENSIONS OF SCRATCH ARE: (P1) = 4.300"L X .700"W X .006"D AND (P2) = 7.00"L X .200"W X .002"D. ************AIRCRAFT REMOVED FROM SERVICE************************* BLENDED DAMAGED AREAS TO A SMOOTH CONTOUR IAW ASAP EA #AWAC-CRJ255-01782 REV IR DATED 12/24/2021. REMAINING MATERIAL THICKNESS OF .069". ORIGINAL THICKNESS OF .075". HFEC INSPECTION PERFORMED WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK PERFORMED WITHIN ALLOWABLE LIMITS IAW ASAP EA #AWAC-CRJ253-01782 REV IR DATED12/24/2021. WORK COMPLETED ON AERSALE WO #003500 CARD #20462 AT AERSALE CRS#4AER685B. N442AW TT:39,682:59 TC:38,340.

Part: SKIN — DENTED (FS 654.50+15") · airframe 39,682 hrs · 38,340 cycles

AIRCRAFT L/H SKIN EXTERIOR HAS 1 EACH DENT AT FS 654.50+15" AND S26L TO S27. DENT DIMENSIONS ARE: (P1) .400"L X .350"W X .020"D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE*********************** CUTOUT DAMAGED AREA .400" DIAMETER AT FS 654.50 AND STR 26R TO STR 27. FABRICATED REPAIR DOUBLER 5.35"L X 4.90"W OUT OF 2024-T3 .063" MATERIAL. HFEC INSPECTION PERFORMED AT REPAIR AREA AND PARTS WITH NO INDICATIONS. INSTALLED FABRICATED REPAIR DOUBLER AT REPAIR AREA AT FS 654.50 TO FS 672.20 AND STR 26R TO STR 27. ALL WORK PERFORMED IAW ASAP EA # AWAC-CRJ253-01784 REV IR DATED 01/05/2022. WORK COMPLETED AT AERSALE CRS4AER685B ON W/O #003500 CARD #20148. N442AW TT:39,682:59 TC: 38,340

Part: SKIN — DENTED (FS 233.276) · airframe 39,682 hrs · 38,340 cycles

AIRCRAFT R/H SKIN EXTERIOR HAS 1 EACH DENT AT FS 233.27+3" AND S1R+2. DENT DIMENSIONS ARE: (P1) 1.700L X 1.700W X .016D. 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-CRJ253-01772 REV A DATED 01/10/2022. ALL WORK PERFORMED IAW ASAP EA # AWAC-CRJ253-01772 REV A DATED 01/10/2022. WORK COMPLETED AT AERSALE CRS4AER685B ON W/O #003500 CARD #20110. N442AW TT:39,682:59 TC: 38,340

Part: ANGLE — GOUGED (H STAB LBL6) · airframe 39,682 hrs · 38,340 cycles

MAINTENANCE FOUND SCRATCH DAMAGE ON L/H HORIZONTAL STABILIZER ATTACHMENT VISOR SUPPORT ANGLE AT LBL 6. DIMENSIONS OF SCRATCH ARE: 4.100"L X 0.900"W X 0.004"D. ************AIRCRAFT REMOVED FROM SERVICE************************* BLENDED DAMAGED AREA TO A SMOOTH CONTOUR. DIMENSIONS AFTER BLEND ARE: 4.100"L X .900"W X .004"D. REMAINING MATERIAL THICKNESS OF .059". ORIGINAL THICKNESS OF .063". HFEC INSPECTION PERFORMED WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK PERFORMED WITHIN ALLOWABLE LIMITS IAW ASAP EA #AWAC-CRJ253-01787 REV IR DATED 12/29/2021. WORK COMPLETED ON AERSALE WO #003500 CARD #20470 AT AERSALE CRS #4AER685B. N442AW TT: 39,682:59 TC:38,340.

Part: SKIN — DENTED (FS605-621) · airframe 39,682 hrs · 38,340 cycles

AIRCRAFT L/H SKIN EXTERIOR HAS 1 EACH DENT AT FS 605.00 TO FS 621.00 AND S17L-19L. DENT DIMENSIONS ARE: (P1) 3.500"L X .800"W X .017"D. 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-CRJ253-01775 REV IR DATED 12/23/2021. ALL WORK PERFORMED IAW ASAP EA # AWAC-CRJ253-01775 REV IR DATED 12/23/2021. WORK COMPLETED AT AERSALE CRS4AER685B ON W/O #003500 CARD #20144. N442AW TT:39,682:59 TC: 38,340

Part: SKIN — DENTED (FS 654.40+18") · airframe 39,682 hrs · 38,340 cycles

AIRCRAFT R/H SKIN EXTERIOR HAS 1 EACH DENT AT FS 654.00 TO FS 672.00 AND S25R-26R. DENT DIMENSIONS ARE: (P1) .600L X .300W X .008D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE*********************** VERIFIED NO LOOSE/PULLED FASTENERS AND NO DAMAGE TO UNDERLYING STRUCTURE COMMON TO REPAIR AREA. HFEC PERFORMED WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. RE-EVALUATED SKIN AND FOUND WITHIN LIMITS IAW ASAP EA #AWAC-CRJ253-01778 REV IR DATED 12/24/2021. ALL WORK PERFORMED IAW ASAP EA # AWAC-CRJ253-01778 REV IR DATED 12/24/2021. WORK COMPLETED AT AERSALE CRS4AER685B ON W/O #003500 CARD #20149. N442AW TT:39,682:59 TC: 38,340

Part: SKIN — DENTED (FS 654.50) · airframe 39,682 hrs · 38,340 cycles

AIRCRAFT R/H SKIN EXTERIOR HAS 1 EACH DENT AT FS 654.00 AND S21R+3. DENT DIMENSIONS ARE: (P1) 1.00L X .800W X .008D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE*********************** VERIFIED NO LOOSE/PULLED FASTENERS AND NO DAMAGE TO UNDERLYING STRUCTURE COMMON TO REPAIR AREA. HFEC PERFORMED WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. RE-EVALUATED SKIN AND FOUND WITHIN LIMITS IAW ASAP EA #AWAC-CRJ253-01779 REV IR DATED 12/24/2021. ALL WORK PERFORMED IAW ASAP EA # AWAC-CRJ253-01779 REV IR DATED 12/24/2021. WORK COMPLETED AT AERSALE CRS4AER685B ON W/O #003500 CARD #20153. N442AW TT:39,682:59 TC: 38,340

Part: SKIN — DENTED (FS394+10") · airframe 39,682 hrs · 38,340 cycles

AIRCRAFT R/H SKIN EXTERIOR HAS 1 EACH DENT AT FS 394.00+10" AND S19R TO S20R. DENT DIMENSIONS ARE: (P1) .500L X .500W X .007D. 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-CRJ253-01780 REV IR DATED 12/24/2021. ALL WORK PERFORMED IAW ASAP EA # AWAC-CRJ253-01780 REV IR DATED 12/24/2021. WORK COMPLETED AT AERSALE CRS4AER685B ON W/O #003500 CARD #20042. N442AW TT:39,682:59 TC: 38,340

Part: VISOR — GOUGED (H STAB LBL6) · airframe 39,682 hrs · 38,340 cycles

MAINTENANCE FOUND SCRATCH DAMAGE ON L/H HORIZONTAL STABILIZER ATTACHMENT VISOR AT LBL6. DIMENSIONS OF SCRATCH ARE: 35.00"L X 0.900"W X 0.004"D. ************AIRCRAFT REMOVED FROM SERVICE************************* BLENDED DAMAGED AREA TO A SMOOTH CONTOUR. DIMENSIONS AFTER BLEND ARE: 35.00"L X .900"W X .004"D. REMAINING MATERIAL THICKNESS OF .071". ORIGINAL THICKNESS OF .075". HFEC INSPECTION PERFORMED WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK PERFORMED WITHIN ALLOWABLE LIMITS IAW ASAP EA #AWAC-CRJ253-01785 REV IR DATED 12/29/2021. WORK COMPLETED ON AERSALE WO #003500 CARD #20470 AT AERSALE CRS #4AER685B. N442AW TT: 39,682:59 TC:38,340.

Part: SKIN — DENTED (FS 310.00) · airframe 39,682 hrs · 38,340 cycles

AIRCRAFT L/H SKIN EXTERIOR HAS 1 EACH DENT AT FS 310.00 AND S13L+5". DENT DIMENSIONS ARE: (P1) .350L X .200W X .004D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE*********************** VERIFIED NO LOOSE/PULLED FASTENERS AND NO DAMAGE TO UNDERLYING STRUCTURE COMMON TO REPAIR AREA. HFEC PERFORMED WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. RE-EVALUATED SKIN AND FOUND WITHIN LIMITS IAW ASAP EA #AWAC-CRJ253-01777 REV IR DATED 12/24/2021. ALL WORK PERFORMED IAW ASAP EA # AWAC-CRJ253-01777 REV IR DATED 12/24/2021. WORK COMPLETED AT AERSALE CRS4AER685B ON W/O #003500 CARD #20138. N442AW TT:39,682:59 TC: 38,340

Part: RIB — CORRODED (LH TIP HORIZ STA) · corrosion level 2 · airframe 39,682 hrs · 38,340 cycles

LH HORIZONTAL STABILIZER TIP CLOSING RIB #9 P/N 600-23037-22 HAS TWO ELONGATED FASTENER HOLES CAUSED BY CORROSION. HORIZONTAL REAR SPAR AND LBL112.0. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED DAMAGED SECTIONS OF CLOSING RIB AT TWO LOCATIONS. MEASUREMENTS P1= L=.700Ï¿½ X W= 0.400Ï¿½ AND P2= L=0.350Ï¿½ X W= 0.300Ï¿½. FABRICATED A REPAIR STRAP, REPAIR ANGLE AND FILLERS. PERFORMED HFEC TO CUTOUT EDGES WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA #AWAC-CRJ255-01789 REV IR DATED 1/15/2022. WORK PERFORMED UNDER AERSALE WORK ORDER 003500, CARD NO. 20510, TT: 39682:59 TC: 38340.

Part: NONE — NONE (DOOR HINGE) · airframe 39,682 hrs · 38,340 cycles

REMOVE AND REPLACE PAX DOOR HINGE PINHOLES WORN BEYOND LIMITS ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED PAX DOOR HINGE ON DOOR HALF REF MHI RJ REO 601R-52-11-2912 REV -- DTD 2022-01-04 FOR DISPOSITION FOR FASTENER SUBSTITUTION DURING REPLACEMENT OF PAX DOOR SIDE.

Part: SKIN — DAMAGED (FS 349) · airframe 39,682 hrs · 38,340 cycles

OUTER SKIN FS349.00 AT PAX DOOR CUTOUT P/N 601R31018-9 IS DAMAGED. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED DAMAGE BY EDGE BLENDING OUTER SKIN AT FS349.00. MEASUREMENT L= 1.180Ï¿½ X W= 0.113Ï¿½ X D= 0.060Ï¿½. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA #AWAC-CRJ253-01776 REV IR DATED 12/23/2021. WORK PERFORMED UNDER AERSALE WORK ORDER 003500, CARD NO. 20137, TT: 39682:59 TC: 38340.

Part: DOOR — CRACKED (FS 320) · airframe 39,682 hrs · 38,340 cycles

MAIN ENTRY DOOR HAS A CRACK ON THE FORWARD SIDE PANEL OF UPPER STEP FS320.10. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED DAMAGE OF MAIN ENTRY DOOR FORWARD SIDE PANEL OF UPPER STEP FS320.10, DIMENSIONS L= 12.00Ï¿½ X W= 6.00Ï¿½. FABRICATED 1 WEB REPLACEMENT L=13.00Ï¿½ X W= 3.50Ï¿½ AND 3 DOUBLERS DIMENSIONS, L=12.00Ï¿½ X W=8.50Ï¿½, L= 6.00Ï¿½ X W=3.50Ï¿½ AND L= 6.00Ï¿½ X W=3.50Ï¿½. PERFORMED HFEC TO CUTOUT EDGES AND FABRICATED PARTS WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED AWA SUPPLEMENTAL NO. 13-134 DATE OF ISSUE 12/9/2013. WORK PERFORMED UNDER AERSALE WORK ORDER 003500, CARD NO. 20478, TT: 39682:59 TC: 38340.

Part: PLATE — CORRODED · corrosion level 2 · airframe 39,682 hrs · 38,340 cycles

REMOVED AND REPLACED 4 EACH BONDING PLATES P/N 601-37012-33. ***AIRCRAFT REMOVED FROM SERVICE*** RESTORED SURFACE FINISH. BOND CHECKED GOOD. ALL WORK WITHIN LIMITS WAS PERFORMED IAW AWA SUPPLEMENT NO. 15-335 DATE OF ISSUE 12/22/2015. WORK PERFORMED UNDER AERSALE WORK ORDER 003500, CARD NO. 20101, TT: 39682:59 TC: 38340.

Part: BRACKET — CORRODED · corrosion level 2 · airframe 39,682 hrs · 38,340 cycles

CORROSION ON CONNECTOR BRACKET P/N 601R31771-1 LOCATED AT FS310.00+12 AND AND LBL42 UNDER FLOOR STRUCTURE AT PASSENGER ENTRY DOOR. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED CONNECTOR BRACKET P/N 601R31771-1 LOCATED AT FS310.00+12 AND LBL42. RESTORED SURFACE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED CRJ200 SRM 51-11-000 REV 38. WORK PERFORMED UNDER AERSALE WORK ORDER 003500, CARD NO. 20398, TT: 39682:59 TC: 38340.

Part: NONE — CORRODED (LWR) · corrosion level 2 · airframe 39,682 hrs · 38,340 cycles

FS 574.00+10 TO FS 589.00+8 & LBL 46 FRETTING CORROSION COMMON TO ANGLE AT LWR SIDE OF CARGO DOOR OPENING AT FLOOR LEVEL ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED 5 OFF AREAS P1 THROUGH P5 OF BLENDED CORROSION DAMAGE AS: P1 1.60"L X 0.80"W X .068" MIN REMAIN THICKNESS P2 3.40"L X 0.80"W X .078" MIN REMAIN THICKNESS P3 3.00"L X 0.60"W X .078" MIN REMAIN THICKNESS P4 2.60"L X 0.60"W X .073" MIN REMAIN THICKNESS P5 1.30"L X 1.30"W X .086" MIN REMAIN THICKNESS THE SUBJECT CONDITION IS CONSIDERED STRUCTURALLY ACCEPTABLE WITH ALL THE CONDITIONS ON SHEET 5 ARE MET. THERE ARE NO ADDITIONAL LIMITATIONS REQUIRED AS PER BLOCK 6, REF MHIRJ 601R-53-61-7783 REV -- DTD 2021-12-30

Part: STRAP — CORRODED (FS 559) · corrosion level 2 · airframe 39,682 hrs · 38,340 cycles

CORROSION ON PRESSURE FLOOR STRAP PN 601R31025-29 LOCATED AT FS559.00 AND RBL30 TO RBL44 PRESSURE FLOOR STRUCTURE. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED PRESSURE FLOOR STRAP PN 601R31025-29 LOCATED AT FS559.00 AND RBL30 TO RBL44 WITH A NEW FABRICATED FLOOR STRAP. MATERIAL ALUMINUM SHT 7075-T6 CLAD 0.050Ï¿½. STRAP DIMENSIONS L=14.700Ï¿½ W=2.100Ï¿½. RESTORED SURFACE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED CRJ200 SRM 51-42-06, SRM 51-40-11, SRM 53-41-43, REV 38. WORK PERFORMED UNDER AERSALE WORK ORDER 003500, CARD NO. 20217, TT: 39682:59 TC: 38340.

Part: SKIN — DENTED (FS 310) · airframe 36,682 hrs · 38,340 cycles

DENT IN EXTERIOR SKIN C/T PAX DOOR OPENING AT F.S. 310.00 & S 14L+3" THAT MEASURES .750 "L X .300"W X .015"D. EVALUATED AND DETERMINED TO BE OUT OF LIMITS REF CRJ 200 SRM 53-00-00 REV 38. VERIFIED LOOSE OR PULLED FASTENERS IN THE SURROUNDING AREA REF ASAP EA# AWAC-CRJ253-01781 REV IR DTD 12/24/21 HFEC PERFORMED NO INDICATIONS NOTED AT THIS TIME REF CRJ 200 NDTM PART 1 51-20-060 REV 43. ***AIRCRAFT REMOVED FROM SERVICE*** DENT DETERMINED TO BE WITHIN ALLOWABLE LIMITS REF ASAP EA# AWAC-CRJ253-01781 REV IR DTD 12/24/21

Part: SKIN — DENTED (FS 625) · airframe 39,682 hrs · 38,340 cycles

STRINGER HAS 4 OUTWARD DENTS COMMON TO EXTERIOR SKIN PN 601R35004-145 AT FS625.30 TO FS640.00 AND STR16R TO STR17R. ****AIRCRAFT REMOVED FROM SERVICE**** VERIFIED NO LOOSE OR PULLED FASTENERS IN THE SURROUNDING AREA AT STRINGER COMMON TO EXTERIOR SKIN AT FS625.30 TO FS640.00 AND STR16R TO STR17R. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA # AWAC-CRJ253-01773 REV IR DATED 12/22/2021.WORK PERFORMED UNDER AERSALE WORK ORDER 003500, CARD NO. 20098, TT: 39682:59 TC: 38340.

Part: SKIN — CRACKED (CORE COWL) · airframe 39,682 hrs · 38,340 cycles

R/H UPPER MAIN CORE COWL UPPER FWD I/B CORNER IS BENT AND DEBONDING.FOUND CRACK IN DEBONDING FWD I/B CORNER LENGTH IS 1.437" & .010"W. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED CUTOUT ON DAMAGE ON OUTER SKIN P/N 228-50142-607 THAT MEASURES 2.5"L X .775"W REF ASAP EA# AWAC CRJ272-01774 REV A DTD 12/29/2021. HFEC ACCOMPLISHED WITH NO INDICATIONS NOTED REF CRJ 200 NDTM PART 1 51-20-06 REV 43. INSTALLED SPIGOT PLATE AND DOUBLER REPAIR WITH REPAIR IDENTIFIED AS NUMBER SRS118 FER ASAP EA# AWAC-CRJ272-01774 REV A DTD 12/29/ 2021.

Part: SEAL — DIRTY (PAX DOOR) · airframe 39,160 hrs · 37,815 cycles

RECEIVED CABIN ALT CAUTION MESSAGE ON CLIMB-OUT; COULD NOT PRESSURIZE AIRCRAFT IN AUTO OR MANUAL PRESSURIZATION MODES. AIRCRAFT REMOVED FROM SERVICE. INSPECTED PAX DOOR SEAL AND CLEANED DEBRIS, NO OTHER DEFECTS NOTED, REF. AMM 52-11-00 PRESSURIZED A/C WITH APU, REF AMM 21-31-00, PRESSURIZATION OKAY.

Part: GCU — MALFUNCTIONED (NR 2 IDG) · airframe 38,492 hrs · 37,094 cycles

WHILE OPERATING WITH AN IDG 2 INOPERABLE MEL APPLIED, APU GCU DISABLED AND APU GEN WAS NO LONGER TO POWER AC BUS 2. SINGLE GEN OPERATIONS. ELECTED TO AIR RETRUN. APU GCU RE-ENABLED ITSELF PRIOR TO LANDING. AIRCRAFT REMOVED FROM SERVICE. R & R APU GCU, IAW AMM 24-11-07. OPERATIONS CHECK GOOD. P/N: 720846D, S/N OFF: 4268, S/N ON: 4216.

Part: ADG — UNWANTED DEPLOY · airframe 38,342 hrs · 36,928 cycles

INADVERTENTLY DEPLOYED ADG DURING GEN 1 CAUTION. AROUND 220 KNOTS ADG RAN FOR APPROXIMATELY 20 MIN IN FLIGHT. APU GEN WAS ON MEL, PILOT CYCLED WRONG GEN SW. RETURNED DUE TO ADG DEPLOYED. IDG 1 CAUTION MSG ON T/O AND THEN MSG CLEARED, THEN RECEIVED GEN 1 CAUTION AFTER APPROXIMATELY 5 MIN, C/Q QRH. AIRCRAFT REMOVED FROM SERVICE. RESTOWED ADG, PER AWAC SUPP 16-015A. OK FOR SERVICE, REF 306638/4 FOR NDT DIL. C/W AMM 05-51-19-06 INSPECTION OF ADG, REF 306639/3 INSPECTED AND FOUND NR 1 IDG OIL LOW, FOUND LEAKING AT FILTER ASSEMBLY, OIL OUT PORT. R & R "O" RING FOR FILTERS OUT PORT IN REF TO AMM 24-12-05. SERVICED NR 1 IDG OIL REF AMM SUPP 16-364, LEAK AND OPERATIONS CHECKED NR 1 IDG, IAW AMM SUPP 19-165. OPERATIONS AND LEAK CHECK GOOD. A/C OK FOR RETURN TO SERVICE.

Part: CAP — CORRODED (BS 513-610) · corrosion level 2 · airframe 38,339 hrs · 36,926 cycles

AFT CARGO BAY LBL 27 FS 610 HAS CORROSION AND PITTING ON T-CAP. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED AFT CARGO T-CAP LBL 27 FS 610 TO FS 513, IAW BOMBARDIER DRAWING 601R35031AND CRJ200 SRM 51-40-11.

Part: RETAINER — CORRODED (LAVATORY) · corrosion level 2 · airframe 38,339 hrs · 36,926 cycles

LAV RETAINER FITTING AT RBL 9 FS 559+80 CORRODED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED RETAINER FITTING AT RBL 9 FS 558, IAW CRJ200 SRM 51-41-02.

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 38,339 hrs · 36,926 cycles

FLOOR SEAT TRACK AT LAVATORY ENTRY FS 559+64 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK SEGMENT FS 559 TO FS 559+80, IAW REO 601R-53-00-764 AND CRJ200 SRM 51-40-11.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 38,339 hrs · 36,926 cycles

AFT CARGO BAY SEAT TRACK SEGMENT FS 559-FS 559+80 RBL 9 HAS SURFACE CORROSION AND PITTING. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED AFT CARGO BAY SEAT TRACK SEGMENT FS 559-559+80, IAW REO 601R-53-00-764 AND CRJ200 SRM 51-40-11.

Part: WIRE HARNESS — FAULTY (NLG) · airframe 37,562 hrs · 36,184 cycles

SUPPLIMENTAL INFORMATION, WHILE ENROUTE THE CREW REPORTED RECEIVING A NOSE WHEEL STEERING FAULT. THEY ARE CONTINUING TO IAD AND THE TOWER HAS DECLARED AN EMERGENCY FOR THE FLIGHT. DURING CRUISE RCVED STEERING INOP CAUTION MSG C/W. QRH MSG DID NOT CLEAR W/SWITCH CYCLE. NO ADDITIONAL ASSOCIATED MSG'S NO HYD SYS NR 3 FAULT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NOSE LANDING GEAR HARNESS PN 17300-233 IAW AMM 32-61-25 REF 316728/3 FOR RVDT REPLACEMENT.

Part: A/C PACK — MALFUNCTIONED (LEFT) · airframe 37,137 hrs · 35,781 cycles

ON INTIAL CLIMB LEFT PACK OVER PRESS (C)_ MSG WHEN TRANSFERING BLEEDS C/W QRH MSG REMAINED DURING INITIAL CLIMB OUT OF IAD, WITH THE RH CONDITIONING PACK ALREADY ON MEL, THE AIRCRAFT LOST THE CAPABILITIES OF THE LH PACK. THE CREW DECIDED TO AIR RETURN TO IAD.

Part: RETAINER — CRACKED (LT PYLON) · airframe 35,027 hrs · 33,745 cycles

LT UPPER PYLON PNL 412AT HAS SMALL CRACK NEAR SEAL RETAINER. REPLACED SEAL RETAINER IAW SRM 51-42-06, 51-26-27, 51-24-36.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 35,027 hrs · 33,745 cycles

AFT PRESSURE BULKHEAD SKIN CRACKED AT LINTEL FITTING. REPAIRED SKIN IAW REO 601R-53-61-1230 REV-F AND REO 601R-53-61-6593 REV-.

Part: RETAINER — CRACKED (RT PYLON) · airframe 35,028 hrs · 33,745 cycles

RIGHT PYLON PANEL 422AT HAS SMALL CRACK AT CENTER EDGE NEAR SEAL RECEPTACLE. REPLACED RECEPTACLE (SEAL RETAINER) IAW SRM 51-42-06, 51-40-11.

Part: RIB — GOUGED (LT WING TE FLAP) · airframe 35,027 hrs · 33,745 cycles

LEFT INBD FLAP, INBD CLOSEOUT RIB WAS GOUGED ON THE FWD END. REPLACED THE RIB IAW SRM 51-42-22, AND 51-42-15.

Part: ANGLE — CRACKED (BS 280) · airframe 35,027 hrs · 33,745 cycles

UPPER REPAIR ANGLE AT FS 280, RBL 9 WAS CRACKED. REPLACED THE REPAIR ANGLE IAW REO 601R-53-11-136, REV-A.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 35,027 hrs · 33,745 cycles

LOWER ANGLE CRACKED AT FS 280.00, LBL9. REPLACED ANGLE IAW REO601R-53-11-171 REV-D.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,027 hrs · 33,745 cycles

UPPER TCAS ANTENNA DOUBLER HAS CORROSION AROUND SCREW MOUNT HOLES. REPLACED DOUBLER EA 15-2014-128 REV-A DATED 5/23/2014.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 35,027 hrs · 33,745 cycles

AFT PRESSURE BULKHEAD WEB WAS CRACKED AT THE CARGO DOOR TRACK, LBL 27.5 WL 130. REPAIRED THE AFT PRESSURE BULKHEAD WEB IAW REO 601R-53-61-1541, REV-F.

Part: FRAME — CRACKED (BS 605) · airframe 35,027 hrs · 33,745 cycles

FRAME BS 605 WAS CRACKED ABOVE AND BELOW STRINGER 9L. REPAIRED THE FRAME IAW REO 601R-53-61-5214, REV-A.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 35,027 hrs · 33,745 cycles

AFT PRESSURE BULKHEAD WEB WAS CRACKED AT BL 0 AND WL-130. REPAIRED AFT PRESSURE BULKHEAD SKIN IAW REO 601R-53-61-1285 REV-E DATED 2016-10-31.

Part: ANGLE — CRACKED (BS 280) · airframe 35,027 hrs · 33,745 cycles

UPPER ANGLE ON THE FWD SIDE OF FRAME BS 280, LBL 9 WAS CRACKED. REPLACED THE ANGLE IAW SRM 51-42-06, AND REO 601R-53-11-136, REV A.

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 35,027 hrs · 33,745 cycles

INTERCOSTAL CRACKED BETWEEN BS 621 AND 625, STRINGER 14R. REPLACED THE INTERCOSTAL IAW SRM 51-42-21.

Part: CHANNEL — BENT (DOOR TRACK) · airframe 35,028 hrs · 33,745 cycles

CARGO DOOR FWD TRACK LOWER C-CHANNEL WAS BENT. REPLACED THE CHANNEL IAW SRM 51-42-06, AND 51-41-02.

Part: RETAINER — CRACKED (RT PYLON) · airframe 35,027 hrs · 33,745 cycles

R/H UPPER PYLON PNL 422BT HAS CRACKED SEAL RETAINER. REPLACED SEAL RETAINER IAW CRJ200 SRM 51-42-06.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 35,027 hrs · 33,745 cycles

AFT PRESSURE BULKHEAD WEB CRACKED AT BL 0 AND WL 120. REPAIRED IAW REO 601R-53-61-1285, REV-E.

Part: UNKNOWN — ODOR (CABIN) · airframe 33,173 hrs · 31,918 cycles

CREW REPORTED STRONG ELECTRICAL ODOR COMING FROM MIDDLE RIGHT OF CABIN, AND CEILING LIGHT AT 7DF WAS FLICKERING.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,953 hrs · 30,789 cycles

FLOOR LEVEL EMERGENCY LIGHTS INOPERATIVE ROW 2-5. LEFT LOWER EMERGENCY EXIT SIGN, ROW 8 INOPERATIVE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,512 hrs · 30,393 cycles

FLIGHT 3985, RT EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED THE NR 3 INVERTER IAW AMM 33-51-07. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,512 hrs · 30,393 cycles

RIGHT EMERGENCY EXIT LIGHT INOPERATIVE.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,235 hrs · 30,129 cycles

STRINGER 26R CORRODED AT FS 231.00 UNDER THE AFT NLG DOOR HINGE FITTING.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,235 hrs · 30,129 cycles

RBL 9 FLOORBEAM CAP CORRODED AT FS 559+80.

Part: FITTING — CRACKED (FUSELAGE) · airframe 31,235 hrs · 30,129 cycles

LBL 27 AFT FITTING IS CRACKED ON INBD FLANGE AT FS 608.

Part: CLEAT — CORRODED (PAX DOOR) · corrosion level 2 · airframe 31,235 hrs · 30,129 cycles

PASSENGER DOOR AFT CLEAT HAS CORROSION, REPLACED.

Part: SKIN — CHAFED (RT AILERON) · airframe 31,235 hrs · 30,129 cycles

COMPLY WITH JC 4DMI17958, PERFORM PERMANENT REPAIR OF RT AILERON UPPER LE. PERFORMED PERMANENT REPAIR OF RT AILERON UPPER LE IAW SRM 51-42-06, 51-42-21 & 51-42-22.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 31,235 hrs · 30,129 cycles

CARGO DOOR UPPER LINTEL MACHINED FITTING SUPPORT ANGLE CRACKED, FS 621 - FS 625.

Part: ATTACH ANGLE — CRACKED (BS 621-625) · airframe 31,235 hrs · 30,129 cycles

FS 621 BULKHEAD AFT SIDE ZEE AT STRINGER 12L, OTBD ATTACH ANGLE CRACKED.

Part: INTERCOSTAL — CRACKED (BS 621) · airframe 31,235 hrs · 30,129 cycles

AFT EQUIPMENT COMPARTMENT FS 621 BULKHEAD AFT SIDE INTERCOSTAL IS CRACKED AT STRINGER 14L.

Part: SKIN — CHAFED (TE FLAP) · airframe 31,235 hrs · 30,129 cycles

RIGHT OTBD FLAP, FLAP VANE OTBD LE CHAFED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 31,235 hrs · 30,129 cycles

FS 379 INTERCOSTAL CLIP AT STRINGER 3L IS CRACKED.

Part: SKIN — CHAFED (RT AILERON) · airframe 31,235 hrs · 30,129 cycles

RIGHT AILERON LOWER INBD FIXED LE CHAFED.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,235 hrs · 30,129 cycles

LOWER FLOOR SUPPORT ANGLE CORRODED AROUND THE SERVICE DOOR LOWER SPIGOT FITTINGS.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 31,235 hrs · 30,129 cycles

PASSENGER CABIN STRINGER 3L ATTACH CLIP IS CRACKED AT AFT SIDE OF 280.00 BULKHEAD. REPLACED CLIP & ANGLE AT FS 280.00 & STRINGER 3L IAW SRM 51-42-06 & 51-42-21.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 31,235 hrs · 30,129 cycles

PASSENGER DOOR AFT DRAG ANGLE HAS POSSIBLE CRACK AT MOTOR CABLE PULLEY. REPLACED AFT DRAG ANGLE IAW REO 601R-52-11-513.

Part: FITTING — CRACKED (FUSELAGE) · airframe 31,235 hrs · 30,129 cycles

BATH TUB FITTING LBL 9, FS 461.00 IS CRACKED. REPLACED BATHTUB FITTING AT LBL 9, FS 461.00 IAW SRM 51-42-21.

Part: BRACKET — CRACKED (RT MLG) · airframe 31,235 hrs · 30,129 cycles

RIGHT MLG BRAKE PRESS TRANSDUCER BRACKET IS CRACKED, REPLACED.

Part: BRACKET — CRACKED (RT WING) · airframe 31,235 hrs · 30,129 cycles

SPOILER BRACKET JUST FWD OF THE RT FWD WING SPAR IS CRACKED, REPLACED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,235 hrs · 30,129 cycles

LEFT SIDE WALL SEAT TRACK STICK 5, BETWEEN FS 449.85 & 499 HAS CORROSION, REPLACED.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 31,235 hrs · 30,129 cycles

RIGHT INBD FLAP VANE LE IS CHAFED AT THE IN BUMPER STOP, REPLACED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,235 hrs · 30,129 cycles

PASSENGER CABIN FRAME AT FS 333.00, STRINGER 2L IS CRACKED AT TOOLING HOLE. REPLACED FRAME SECTION AT FS 333.00 & STRINGER 2L IAW SRM 51-42-06 & 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,235 hrs · 30,129 cycles

LEFT SIDEWALL SEAT TRACK STICK 7, BETWEEN FS 544 & 559+80 HAS CORROSION, REPLACED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 31,235 hrs · 30,129 cycles

FS 484.00, LBL 27 CLIP IS CRACKED. REPLACED CLIP.

Part: FITTING — CRACKED (FUSELAGE) · airframe 31,235 hrs · 30,129 cycles

FS 484.00 CLIP AT RBL 36 IS CRACKED. REPLACED FS 484.00 CLIP AT RBL 36 IAW REO 601R-53-11-059 REV B DATED 09 16 2009.

Part: FITTING — CRACKED (FUSELAGE) · airframe 31,235 hrs · 30,129 cycles

BATH TUB FITTING RBL 9, FS 461.00 IS CRACKED. REPLACED FITTING IAW SRM 51-42-21.

Part: DOUBLER — SCRATCHED (FUSELAGE) · airframe 31,235 hrs · 30,129 cycles

FOUND MULTIPLE SCRATCHES ON THE ACFT UNDER TCAS ANTENNA. REPLACED SKIN DOUBLER UNDER TCAS ANTENNA IAW EA15-2014-128 REV A DATED 03 10 2015.

Part: FITTING — CRACKED (FUSELAGE) · airframe 31,235 hrs · 30,129 cycles

FS 484.00 CLIP AT RBL 27 IS CRACKED. REPLACED CRACKED CLIP WITH NEW CLIP IAW REO 601R-53-41-059 REV B DATED 09 16 2009.

Part: FITTING — CRACKED (COCKPIT) · airframe 31,235 hrs · 30,129 cycles

PILOTS WINDOW SIDE POST LOWER AFT FITTING IS CRACKED. REPLACED PILOTS WINDOW SIDE POST LOWER AFT FITTING IAW SRM 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,235 hrs · 30,129 cycles

RIGHT SIDE WALL SEAT TRACK STICK NR 6 HAS CORROSION, BETWEEN FS 499.00 & 544.00 IN THE CABIN. REPLACED RT SIDE WALL SEAT TRACK NR 6 IAW REO 601R-53-00-485 & AMM 53-01-11.

Part: SKIN — CRACKED (FUSELAGE) · airframe 30,841 hrs · 29,618 cycles

NOSE LANDING GEAR AFT DOOR SKIN CUT OUT IS CRACKED ON RT AFT CORNER.

Part: FITTING — CRACKED (COCKPIT) · airframe 31,235 hrs · 30,129 cycles

CO-PILOTS WINDOW SIDE POST LOWER AFT FITTING IS CRACKED. REPLACE CO-PILOTS WINDOW SIDE POST LOWER AFT FITTING IAW SRM 51-42-21.

Part: STRAP — CRACKED (COCKPIT) · airframe 31,235 hrs · 30,129 cycles

WINDSHIELD CTR POST BL 0.00 AT WL 110.00 STRAP IS CRACKED BELOW WINDSHIELD ATTACH CLIPS. REPLACED CTR POST STRAP IAW SRM 51-42-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 31,235 hrs · 30,129 cycles

FS 484.00 CLIP LBL 36 IS CRACKED.

Part: FITTING — CRACKED (COCKPIT) · airframe 31,235 hrs · 30,129 cycles

LEFT LOWER CTR POST WINDSHIELD CLIP IS CRACKED.

Part: CABLE — BROKEN (PAX DOOR) · airframe 31,224 hrs · 30,124 cycles

AFTER TAKEOFF LOUD BUZZING SOUND FROM PAX DOOR. VIBRATIONS FELT IN DOOR & GALLEY FLOOR. APPEARED TO GET WORSE AS ACFT WAS PRESSURIZED. LANDING WT 46,500, MAX BTMS 4344. INSPECTED PAX DOOR SEAL IAW AMM 52-11-10. CLEANED PAX DOOR SEAL. DURING INSPECTION FOUND ICE BREAK CABLE BROKEN. R & R IAW AMM 52-11-15. PERFORMED PRESSURIZATION CHECK OF ACFT IAW AMM 21-30-00. NO DEFECTS NOTED. ACFT PRESSURIZATION IS NORMAL.

Part: FAIRING — SEPARATED (TE FLAP) · airframe 30,666 hrs · 29,606 cycles

RIGHT INBD FLAP AFT FAIRING MISSING, CAME OFF IN FLIGHT, AFT HINGE AFT BRACKET DAMAGED.

Part: PROXIMITY SENSOR — FAULTY (PAX DOOR) · airframe 30,068 hrs · 29,055 cycles

PASSENGER DOOR WARNING MSG PRESENT WITH PAX DOOR CLOSED. OPENED & CLOSED DOOR MULTIPLE TIMES, MSG REMAINS. R & R PSEU IAW AMM 32-61-01. OPERATIONS CHECKED GOOD. CYCLED PAX DOOR MULTIPLE TIMES WITH NO ISSUES.

Part: CAP — UNSECURE (EMERGENCY LIGHT) · airframe 29,481 hrs · 28,471 cycles

FLIGHT 3993, FWD SECTION OF FLOOR TRACK LIGHTS, END CAP MISSING & METAL STICKING UP. SECURED END CAP & TRACK LIGHTING. .

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 29,309 hrs · 28,295 cycles

ROW 1 EMERGENCY LIGHTS INOPERATIVE. SECURED THE CONNECTOR IAW AMM 33-51-01. OPS CHECKED GOOD.

Part: SEAL — DIRTY (EMERGENCY EXIT) · airframe 29,309 hrs · 28,295 cycles

FLIGHT 3749, 3740. CREW ESCAPE HATCH LEAKING WATER FROM LOWER LT CORNER ONTO LOWER PEDESTAL. CLEANED HATCH SEAL IAW AMM 52-22-07. NO FURTHER LEAKS NOTED.

Part: UNKNOWN — ODOR · airframe 27,045 hrs · 26,172 cycles

ACRID OIL ODOR FROM BOTH PACKS DURING USE OF APU BLEED AIR. HAD TO SHUT DOWN BOTH PACKS & RETURN TO GATE ASAP. ALL 3 CREW MEMBERS WENT TO THE EMER ROOM.

Part: RIB — CRACKED (FUSELAGE) · airframe 26,561 hrs · 25,704 cycles

VERTICAL SKIN UNDER PANEL 412AB CRACKED. REMOVED CRACKED VERTICAL RIB & INSTALLED SERVICEABLE RIB IAW SRM 51-42-21, 54-61-14 & 51-42-20.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 26,561 hrs · 25,704 cycles

PAX DOOR TORQUE LINK BRACKET CRACKED AFT OF ICE BRAKE DOOR. R & R PAX DOOR TORQUE BOX AFT BRACKET IAW SRM 51-42-06, 51-24-21, 51-25-06 & 51-25-16.

Part: BRACKET — CRACKED (SERVICE DOOR) · airframe 26,561 hrs · 25,704 cycles

SERVICE DOOR MICRO SWITCH BRACKET CRACKED. R & R SWITCH BRACKET WITH NEW SERVICEABLE BRACKET IAW SRM 51-21-21, 51-40-11 & 51-25-16.

Part: THRUST REVERSER — CRACKED (RIGHT) · airframe 26,561 hrs · 25,704 cycles

54600-4000-0077 - TOP CASCADE ON RT THRUST REVERSER IS CRACKED. REPAIRED CRACK BY WELDING IAW PROCESS SPECIFICATION 1, DWG AW-78-30-0711-04.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 26,561 hrs · 25,704 cycles

54600-3000-0001 - COMPLIED WITH AWAC CARD 4DMI17244 REPAIR APU INLET DOOR ACT13-085B. REPAIR OF APU INLET DOOR IAW SRM 51-42-06, 51-40-11 & 51-25-16.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 26,561 hrs · 25,704 cycles

CARGO DOOR FWD TRACK LOWER SUPPORT BRACKET CRACKED. R & R BRACKET IAW SRM 51-40-11 & 51-42-06.

Part: RETAINER — CORRODED (E&E DOOR) · corrosion level 2 · airframe 26,561 hrs · 25,704 cycles

AVIONICS DOOR FWD LT & RT SEAL RETAINERS ARE CORRODED. REMOVED FWD AVIONICS DOOR LT & RT SEAL RETAINERS & REPLACED WITH NEW SERVICEABLE RETAINERS IAW SRM 51-42-06.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 26,561 hrs · 25,704 cycles

54600-8000-0040 - PAX DOOR AFT DRAG ANGLE CRACKED AT PULLEY BRACKET. REPAIRED AFT DRAG ANGLE ON PAX DOOR IAW REO 601R-53-11-513 REV A.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,561 hrs · 25,704 cycles

54600-2000-0059 - PAX DOOR LOWER SILL CORRODED. R & R WITH NEW SERVICEABLE SILL IAW SRM 51-42-06, 51-25-06, 51-25-16 & 51-42-21.

Part: VANE — CHAFED (TE FLAP) · airframe 26,561 hrs · 25,704 cycles

RT OTBD FLAP VANE LE CHAFED AT OTBD HINGE JACK SCREW. REPAIRED RT OTBD FLAP VANE LE IAW SRM 57-53-00 REPAIR NR 1.

Part: SKIN — DENTED (FUSELAGE) · airframe 26,561 hrs · 25,704 cycles

COMPLIED WITH AWAC CARD 4DMI16838 REPAIR FWD FUSELAGE SKIN PNL 601R-53-11-2490A. REMOVED FWD FUSELAGE SKIN & INSTALLED NEW SERVICEABLE SKIN IAW SRM 51-42-06, 51-25-06 & 51-25-16.

Part: TIE DOWN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 265,691 hrs · 25,704 cycles

2 TIE DOWNS ON LBL 9 AT APPROX FS 580 & FS 600 HAVE CORROSION. REMOVED NON-SERVICEABLE TIE DOWNS & REPLACED WITH NEW SERVICEABLE TIE DOWNS IAW SRM 51-41-02.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 26,561 hrs · 25,704 cycles

EXTERNAL SERVICES ACFT POWER RECEPTACLE BRACKET IS CRACKED AT CONNECTOR MOUNTING HOLES. R & R WITH NEW SERVICEABLE BRACKET IAW SRM 51-41-02, 51-42-06 & 51-42-13.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,561 hrs · 25,704 cycles

FS 280 LBL & RBL 9 INBD & OTBD CLIPS ARE CRACKED. R & R INBD & OTBD CLIPS AT LBL 9 & RBL 9 & FS 280 IAW SRM 51-40-11, 51-42-13 & REO 601R-53-11-171 REV D DATED 2-7-13.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 26,561 hrs · 25,704 cycles

FWD FACE OF 621 PRESS BULKHEAD HAS 2 EACH SCREW DIVETS AT APPROX RBL 32 & RBL 43 BOTH 3 INCHES FROM FLOOR. REPAIRED 621 PRESS BULKHEAD AT RBL 32 & 43 IAW REO 601-53-61-5282 DATED 5-24-2014.

Part: STAND OFF — BROKEN (FUSELAGE) · airframe 26,561 hrs · 25,704 cycles

LT WIRING HARNESS ATTACHED AT FS 621 MIDDLE HAS BROKEN STANDOFF. REMOVED CRACKED WIRING HARNESS ATTACHED CLIP & REPLACED WITH A SERVICEABLE FABRICATED WIRING HARNESS ATTACHED CLIP IAW SRM 51-42-21.

Part: STIFFENER — CRACKED (RT EXHAUST) · airframe 26,561 hrs · 25,704 cycles

RT EXHAUST FAIRING INNER STIFFENER AT XN214 IS CRACKED. REPAIRED STIFFENER IAW CMM 78-11-00 REPAIR NR SRS042.

Part: DOUBLER — CRACKED (RT EXHAUST) · airframe 26,561 hrs · 25,704 cycles

54600-4000-0030 RT EXHAUST FAIRING INBD MOUNT BOLT ACCESS PANEL CUT OUT LANDING DOUBLER IS CRACKED. R & R PANEL LANDING DOUBLER WITH SERVICEABLE PART IAW CMM 20-40-11 & 20-42-06.

Part: DRAG ANGLE — CRACKED (RT MLG WW) · airframe 26,561 hrs · 25,704 cycles

54600-7000-0004 - RT MLG WW DRAG ANGLE COMMON TO THE BATTERY RIB IS CRACKED. R & R DRAG ANGLE WITH SERVICEABLE PART PN 600-10389-2 IAW SRM 51-40-11 & 51-42-21.

Part: RIB — CRACKED (LT WING) · airframe 26,561 hrs · 25,704 cycles

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

Part: RIB — CRACKED (LT WING) · airframe 26,561 hrs · 25,704 cycles

54600-7000-0022 - LT MLG WW AFT BATTERY RIB CRACKED AT UPPER FWD CORNER. REPAIRED AFT BATTERY RIB, LT MLG WW, IAW STS EA 15-2014-123 DATED 5/20/2014.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 26,561 hrs · 25,704 cycles

LOWER FLANGE OF FS 280 BULKHEAD IS CRACKED OTBD OF RBL 9. REPAIRED FS 280 LOWER FLANGE OTBD OF RBL 9 IAW STS EA15-2014-124 DATED 5/20/2014.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,561 hrs · 25,704 cycles

FLOOR SUPPORT BEAM AT RBL 27 & AT FS 615 HAS CORROSION. REPAIRED FLOOR SUPPORT BEAM AT RBL 27 AT FS 615 IAW SRM 51-21-06, 51-21-16, 51-21-11, 51-25-06 & 51-25-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,561 hrs · 25,704 cycles

LEFT & RIGHT SIDEWALL SEAT TRACKS AT FS 364 TO 409+128 HAS CORROSION. R & R SEAT TRACK WITH SERVICEABLE TRACK IAW REO 601R-53-00-055 REV A.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 26,561 hrs · 25,704 cycles

RIGHT INTERCOSTAL BETWEEN FS 621 TO FS 625 IS CRACKED. R & R INTERCOSTAL WITH NEW SERVICEABLE INTERCOSTAL IAW SRM 51-25-16 & 51-42-21.

Part: BRACKET — CRACKED (RT MLG) · airframe 26,561 hrs · 25,704 cycles

RIGHT MLG PRESS TRANSDUCER HYD LINE BRACKET IS CRACKED. R & R WITH NEW SERVICEABLE BRACKET IAW SRM 51-42-06, 51-41-02, 51-41-04 & 51-40-11.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 26,561 hrs · 25,704 cycles

ACFT SKIN UNDER TCAS ANTENNA HAS MULTIPLE SURFACE SCRATCHES. REPAIRED IAW STS EA 15-2014-128 DATED 5/23/2014.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,561 hrs · 25,704 cycles

FLOOR SUPPORT AT FS 559 BETWEEN LBL 27 & LT FLOOR SILL IS CORRODED. R & R CORRODED FLOOR SUPPORT PLATE WITH SERVICEABLE PLATE IAW SRM TR 52-27 & 51-42-06.

Part: PLATE — CORRODED (CARGO BAY) · corrosion level 2 · airframe 26,561 hrs · 25,704 cycles

CTR CARGO NET TIE DOWN SUPPORT PLATE HAS CORROSION. R & R CARGO NET TIE DOWN SUPPORT PLATE PN 601R35031-173 IAW SRM 51-40-11 & 51-42-06.

Part: BLADES — DAMAGED (ENGINE) · airframe 25,369 hrs · 24,533 cycles

REQ BIRD STRIKE INSP LH ENG GEAR AND FLAPS WERE UP. LT ENG VIBE AT 1.5. N1 REDUCED 10 PERCENT COMPARED TO RT ENG APPROX 2 MINUTES ENG INDICATIONS RETURNED TO NORMAL. KEEP LT ENG AT REDUCED POWER SETTING AUDIBLE CHANGE WHEN TRYING TO INCREASE POWER. CW BS INSPECTION 05-51-25. C/W BIRD STRIKE INSP LT ENG BOROSCOPE INSP. C/W INSP OF LT ENG INLET COWL LIP DAMAGE BEYOND SRM DENT LIMITS IAW SRM 71-61-01, NO CRACKS OR CREASES AND ALL FASTENERS SECURE. R & R NOSE INLET COWL. DURING BS INSP FOUND DAMAGE TO NR 14 BLADE LT ENG. R & R NR 14 AND 28 BLADES LT ENG IAW 72-20-00. DURING BS INSP FOUND DAMAGE TO FAN BLADE NR 20 LT ENG. R & R NR 20 AND NR 6 FAN BLADES LT ENG IAW 72-20-00. DURING BS INSP FOUND DAMAGE TO FAN BLADE NR 10 LT ENG. R & R NR 10 AND NR 24 FAN BLADES LT ENG IAW 72-20-00. DURING BS INSP FOUND DAMAGE TO FAN BLADE NR 21 LT ENG. R & R NR 21 AND NR 7 FAN BLADES LT ENG IAW 72-20-00. C/W LT ENG VIBE AND POWER ASSURANCE CHECKS IAW AMM 71-00-00 VIBES 0.9 POWER ASSURANCE OK C/W LT ENG ANTI-ICE OP CK IAW AMM 30-22-01, NO DEFECTS NOTED.

Part: APU — FIRE · airframe 24,993 hrs · 24,152 cycles

ARRIVED AT GATE WITH APU RUNNING, TRANSFER BLEED NOTICED APU DOOR INHIBIT CLOSED AND RPM AT 76 PERCENT, SHUTDOWN APU AND RECEIVED APU FIRE FAIL CAUTION MESSAGE AFTER OBSERVING SMOKE AND FLAMES FROM APU EXHAUST AREA. PUSHED APU FIRE PUSH BUTTON AND APU BOTTLE BUTTON, FIRE DISSIPATED. CHANGED APU AND APU FIRE BOTTLE. APU OPS AND LEAK CHECKED GOOD.

Part: SLIDE — DEFECTIVE (GALLEY) · airframe 22,303 hrs · 21,538 cycles

GALLEY ICE DRAWER HAS FALLEN OFF TRACK AND IS BLOCKING THE SERVICE DOOR. REPLACED GALLEY ICE DRAWER AND BOTH SLIDES IAW AMM, OP CHECK GOOD R/P/MEL.

Part: FLOORBEAM — CORRODED (FS 589 TO 621) · airframe 21,806 hrs · 21,052 cycles

LBL 27 IN CARGO AREA AT BS 621 FLOORBEAM HAS CORROSION AROUND SCREW HOLES. REMOVED & INSTALLED FLOORBEAM IAW SRM 51-40-11, 51-42-06, 51-42-21. REO 601R-53-61-3778 REV A CORRODED AREA IAW REO 601R-53-61-4514.

Part: CAP — GOUGED (LT WING TE FLAP) · airframe 21,806 hrs · 21,052 cycles

LEFT INBD FLAP END CAP GOUGED ON TOP L/E. R & R END CAP LT INBD FLAP IAW SRM 51-41-11, 51-42-06, 51-42-13, 51-23-00.

Part: BRACKET — CRACKED (BS 540) · airframe 21,726 hrs · 20,976 cycles

PAX DOOR POWER ASSIST MOTOR MOUNT BRACKET CRACKED. R & R ASSIST MOTOR MOUNT BRACKET PN 601R317745-7 IAW AMM 52-11-08-000-802 & SRM 51-42-06.

Part: PANEL — CRACKED (PAX DOOR) · airframe 21,806 hrs · 21,052 cycles

PAX DOOR AFT SIDE PANEL CRACKED SKIN BETWEEN STEPS 2, 3, 4. REPAIRED PAX DOOR AFT SIDE PANEL SKIN IAW REO 601R-52-702, REV C.

Part: PANEL — CRACKED (PAX DOOR) · airframe 21,726 hrs · 20,976 cycles

PAX DOOR AFT SIDE PANEL CRACKED SKIN BETWEEN STEPS 2, 3, 4. REPAIRED PAX DOOR AFT SIDE PANEL SKIN IAW REO 601R-52-11-702.

Part: BRACKET — CRACKED (FS 540) · airframe 21,806 hrs · 2,105 cycles

PAX DOOR POWER ASSIST MOTOR MOUNT BRACKET CRACKED. R & R ASSIST MOTOR MOUNT BRACKET, IAW SRM 52-11-08-000-802 & 51-42-06.

Part: SKIN — GOUGED (CARGO DOOR) · airframe 21,806 hrs · 21,052 cycles

CARGO DOOR EXTERIOR SKIN AT DOOR HANDLE CUTOUT HAS GOUGE AT FWD UPPER EDGE. R & R CARGO DOOR HANDLE OUTER HANDLE IAW SRM 51-42-21.

Part: TRUNNION — DAMAGED (RT MLG) · airframe 21,806 hrs · 21,052 cycles

DURING COLD WORKING, FOUND ONE OVERSIZED HOLE IN RT MLG TRUNNION LOWER FLANGE. REPAIRED OVERSIZED HOLE IN RT LOWER MLG TRUNNION FLANGE IAW REO 601R-57-21-1674, REV.

Part: ISOLATOR — DAMAGED (BULKHEAD 621) · airframe 21,726 hrs · 20,976 cycles

UPON REMOVAL OF ISOLATOR ON 621 BULKHEAD RBL 9, 18" ABOVE FLOOR FOUND PRE-EXISTING DRILL START DAMAGE TO WEB BEHIND ISOLATOR. REPAIR PRE-EXISTING DRILL START IAW REO 601R-53-61-2155, REV.

Part: CARGO TRACK — CORRODED (BS 559-615) · corrosion level 2 · airframe 21,806 hrs · 21,052 cycles

LBL 9 IN CARGO AREA HAS TWO CARGO TRACKS AT FS 559+112 AND FS 615AS CORROSION DAMAGE. REPLACED BOTH TRACKS WITH NEW SERVICEABLE TRACK.

Part: BULKHEAD — DENTED (FS 280) · airframe 21,806 hrs · 21,052 cycles

AFT RT BS 280 BUKLHEAD HAS TWO DENTS NEAR INBD EDGE FROM CONTACT FROM GALLEY STORAGE COMPARTMENT DOOR CUT AWAY DAMAGE ON AFT RT SIDE OF BS 280 BULKHEAD AND INSTALLED REPAIR DOUBLER AND FILLER IAW REO 601R-53-11-1727, REV E.

Part: SILL — CORRODED (CARGO DOOR) · airframe 21,806 hrs · 21,052 cycles

CARGO DOOR LOWER SILL HAS CORROSION AROUND SCREW HOLES. REMOVED UNSERVICEABLE CARGO DOOR SILL SECTION AND INSTALLED SERVICEABLE CARGO DOOR SILL SECTION IAW SRM 51-42-06, 51-42-21, 51-40-11, REO 601R-53-61-690, REV D.

Part: LIGHT — ODOR (CABIN) · airframe 20,373 hrs · 19,529 cycles

STRONG ELECTRICAL SMELL IN CABIN, APPROX AT ROWS 5-8 ON GROUND. R & R PAX SIDEWALL LIGHT AT SEATS 7DF IAW AMM 33-21-07. R & R PAX CEILING LIGHT AT SEATS 7DF IAW AMM 33-21-01. R & R SIDEWALL LIGHT AND CEILING POWER UNITS IAW 33-21-04. OPS CHECK GOOD.

Part: THRUST REVERSER — MALFUNCTIONED · airframe 19,301 hrs · 19,280 cycles

RT T/R UNLOCKED CAUTION MSG 1000 FT AGL. PRESSED EMERGENCY STOW AND SHUTOFF RT T/R MSG REMAINED. RETURNED TO DEPARTURE. LANDING WEIGHT 47000 LBS. C/A IN PROGRESS: PLACED ON MEL.

Part: CONNECTOR — DAMAGED (RT NACELLE) · airframe 17,968 hrs · 16,976 cycles

ON DESCENT RECEIVED R JET OVHT FAIL-CAUTION, FOLLOWED BY R JET OVHT RED WARNING. C/W QRH, PERFORMED RT ENGINE SHUTDOWN, DECLARED EMERGENCY LANDING. LANDING UNEVENTFUL. R & R PIN NR 5 ON CONNECTOR P592 IAW ESPM 20-17-10. PERFORMED OPS CK ON FIRE DETECTION ON NR 2 ENG OPS CK GOOD.

Part: STRIP — CHAFED (RT ENGINE)

RT ENGINE UPPER NOSE COWL AFT EDGE STRIP IS CHAFED. R & R WITH SERVICEABLE AFT EDGE STRIP PN 228-50080-108 IAW CMM 71-14-01.

Part: GUIDE — GOUGED (FLAP ROLLER) · airframe 17,039 hrs · 15,980 cycles

RT OTBD FLAP ROLLER GUIDE IS WORN AND GOUGED. REPAIRED RT OTBD FLAP ROLLER IAW REO 601R-57-51-143.

Part: FITTING — CHAFED (LT WING) · airframe 17,039 hrs · 15,980 cycles

LT OTBD FLAP GUIDE (WING SIDE) CHAFED. BLENDED OUT CHAFED AREA ON LT OTBD FLAP GUIDE IAW SRM 51-12-00 AND REO 601R-57-51-143, REV NC.

Part: SKIN — ERODED (LT ENGINE) · airframe 17,039 hrs · 15,980 cycles

LT ENGINE INLET L/E OUTER SKIN HAS EROSION DAMAGE. REPAIRED THE LT ENGINE INLET L/E OUTER SKIN EROSION DAMAGE.

Part: SKIN — ERODED (RT ENGINE INLET) · airframe 17,039 hrs · 15,980 cycles

RT ENGINE NOSE INLET COWL L/E OUTER SKIN HAS EROSION DAMAGE. REPAIRED THE RT ENGINE NOSE INLET COWL L/E OUTER SKIN EROSION DAMAGE.

Part: STIFFENER — CHAFED (BS 620) · airframe 17,039 hrs · 15,980 cycles

CENTER VERTICAL STIFFENER ON AFT SIDE OF THE AFT PRESSURE BULKHEAD IS CHAFED NEAR TOP BEHIND BLEED AIR SOV. REPAIRED IAW REO 601R-53-61-1573 AND 601R-53-61-3670.

Part: RETAINER — CRACKED (RT PYLON SEAL) · airframe 17,039 hrs · 15,980 cycles

PANEL 422BT CRACKED SEAL RETAINER. REMOVED DAMAGED SEAL AND SEAL RETAINER AND INSTALLED NEW SERVICEABLE SEAL AND SEAL RETAINER IAW AMM 54-63-01 AND 51-41-02.

Part: RETAINER — CRACKED (LT PYLON SEAL) · airframe 17,039 hrs · 15,980 cycles

PANEL 412DB HAS CRACKED SEAL RETAINER. REMOVED DAMAGED SEAL RETAINER AND INSTALLED NEW SERVICEABLE SEAL RETAINER AND SEAL IAW AMM 54-63-01.

Part: STRUCTURE — CRACKED (APU BAY) · airframe 17,039 hrs · 15,980 cycles

APU ENCLOSURE COVER CRACKED IN 3 PLACES TOP CENTER. REPAIRED APU ENCLOSURE DOOR IAW REO 601R-49-11-070, REV A.

Part: STRUCTURE — CRACKED (APU BAY) · airframe 17,039 hrs · 15,980 cycles

APU ENCLOSURE CRACKED UNDER ACCESS DOOR HINGE. REPAIRED APU ENCLOSURE DOOR IAW REO 601R-49-11-070, REV A.

Part: LUG — GOUGED (LT WING TE FLAP) · airframe 17,039 hrs · 15,980 cycles

LT INBD FLAP AFT LUG FOR INBD HINGE ARM HAS DEEP GOUGE SCRATCH ON INBD SIDE. REPAIRED LT INBD FLAP AFT INBD LUG IAW REO 601R-57-52-1536.

Part: SEAT TRACK — CORRODED (BS 364) · corrosion level 2 · airframe 17,039 hrs · 15,980 cycles

LT FLOOR SEAT TRACK NR 1 CORRODED. REPLACED TRACK.

Part: SEAT TRACK — CORRODED (BS 364) · corrosion level 2 · airframe 17,039 hrs · 15,980 cycles

RT NR 1 SEAT TRACK (FLOOR CORRODED) REPLACED SEAT TRACK SECTION IAW AMM 53-01-11.

Part: SKIN — CHAFED (RT WING AILERON) · airframe 17,039 hrs · 15,980 cycles

RT AILERON LOWER L/E PANEL 699AB IS CHAFED. REPAIRED RT AILERON LOWER L/E PANEL 699AB IAW SRM 57-60-00, FIG 101, SHEET 1, VIEW B.

Part: SKIN — CHAFED (RT WING AILERON) · airframe 17,039 hrs · 15,980 cycles

RT AILERON LOWER L/E PANEL 699CB IS CHAFED. REPAIRED CHAFED RT AILERON LOWER L/E PANEL 699CB.

Part: INTERCOSTAL — CRACKED (BS 338-347) · airframe 17,039 hrs · 15,980 cycles

INTERCOSTAL ON PAX DOOR CRACKED AFT UPPER END. R & R INTERCOSTAL IN UPPER PAX DOOR IAW SRM 51-42-06.

Part: BRACKET — CRACKED (EXHAUST) · airframe 17,039 hrs · 15,980 cycles

LT ENGINE JETPIPE PANEL 436BL NUTPLATE BRACKET CRACKED. REMOVED DAMAGED N/P BRACKET PN 228-50181-833 AND INSTALLED SERVICEABLE PN 228-50181-833.

Part: ANGLE — CRACKED (BS 625) · airframe 17,039 hrs · 15,980 cycles

RT 625 OBLIQUE ANGLE CRACKED. R & R CRACKED ANGLE IAW SRM 51-40-11, 51-42-20.

Part: BRACKET — CRACKED (LT ENG EXHAUST) · airframe 17,039 hrs · 15,980 cycles

LT ENGINE JET PIPE PANEL, 436BR, BUTTPLATE BRACKET CRACKED. REMOVED DAMAGED NUTPLATE BRACKET PN 228-50181-883 AND INSTALL NEW SERVICEABLE N/P 228-50181-883.

Part: ANGLE — CRACKED (BS 625) · airframe 17,039 hrs · 15,980 cycles

LT 625, OBLIQUE ANGLE CRACKED. R & R ANGLE IAW SRM 51-42-21.

Part: FLAP — CRACKED (PAX DOOR HANDLE) · airframe 17,039 hrs · 15,980 cycles

PAX DOOR OUTER HANDLE FLAP IS CRACKED. R & R PAX DOOR OUTER FLAP IAW SRM 51-42-06.

Part: ANGLE — CRACKED (BS 484) · airframe 17,039 hrs · 15,980 cycles

CLIP CUP ATTACHING PULLEY GUIDE TO INTERCOSTAL CRACKED AT FS 484, RBL 36 (UNDER FLOORBOARD PANEL 262 DRF) R & R IAW REO 601R-53-41-059.

Part: ANGLE — CRACKED (PAX DOOR) · airframe 17,039 hrs · 15,980 cycles

PAX DOOR INNER HANDLE MOUNTING ANGLE ON AFT SIDE OF INNER HANDLE ASSY IS CRACKED. R & R ATTACH ANGLE ON PAX DOOR INNER MOUNTING ASSY IAW SRM 51-42-06 AND 52-10-14.

Part: ANGLE — CRACKED (PAX DOOR) · airframe 17,039 hrs · 15,980 cycles

PAX DOOR AFT DRAG ANGLE CRACKED 1 INCH BELOW PWR ASSIST PULLEY ATTACH BRACKET. REPAIRED INNER SKIN OF PAX DOOR AND R & R AFT DRAG ANGLE IAW REO 601R-52-11-513 AND PAX STAIR WEB IAW REO 601R-52-11-1810 AND SRM 51-42-00.

Part: SENSE LINE — BROKEN (P3) · airframe 16,753 hrs · 15,668 cycles

RT ENGINE OIL PRESSURE MESSAGE INFLIGHT, ENG SHUTDOWN BY CREW AND COMPLIED WITH QRH. FOUND P3 SENSE LINE BROKEN, R & R P3 LINE IAW AMM 75-30, PERFORMED POWER ASSURANCE RUNS, NO DEFECTS NOTED, THROTTLE RESPONSE NORMAL.

Part: SELECTOR VALVE — MALFUNCTIONED (NLG STEERING) · airframe 14,700 hrs · 13,640 cycles

STEERING INOP MASTER CAUTION ON TAKEOFF. ABORTED TAKEOFF, BTMS 5, 4, 3, 3. REMOVED AND REPLACED NLG SOLENOID SELECTOR VALVE IAW 32-51-25, OPS CK GOOD. (K)

Part: UNKNOWN — ODOR (CABIN) · airframe 13,939 hrs · 12,919 cycles

LOG 192974 - WHEN TURNING BATTERY ON ELECTRICAL ODOR NOTICED. APU ON LINE FLAPS .5 SPEED ADVISORY AND DC TIE 1 CLOSED ADVISORY MSG`S. ON OVER-HEAD DC TIE 1 CLOSED ILLUMINTED. UTILITY BUSS 1 OFF LINE. APPLIED POWER TO ACFT. NO ELECTRICAL ODOR NOTED. ALL MESSAGES NOTED ABOVE WERE ABSENT. ALL BUSSES ON LINE IN NORMAL CONFIGURATION IAW AMM 24-30-00. ACFT OK FOR SERVICE. (K)

Part: SWITCH — MALFUNCTIONED (STAB TRIM) · airframe 13,915 hrs · 12,897 cycles

STAB TRIM AND MACH TRIM CAUTION CAS MSG`S IN FLIGHT WITH FLAPS 45 ON SHORT FINAL. STAB TRIM AND MACH TRIM WILL NOT RE-ENGAGE. C/W QRH AND STAB TRIM AND MACH TRIM RE-ENGAGED ON GROUND. REMOVED AND REPLACED CAPT STAB TRIM DISCONNECT SWITCH IAW AMM 27-40. OPS CHECK GOOD. (K)

Part: HANDLE — CORRODED (ESCAPE HATCH) · airframe 12,271 hrs · 11,318 cycles

OUTER HANDLE CREW ESCAPE HATCH IS CORRODED, DOESN`T OPEN FREELY. OUTER HANDLE CREW ESCAPE HATCH REPLACED IAW AMM 52-22-03-400-801. OPS TEST COMPLIED WITH IAW AMM 52-22-710-081. (A)

Part: CHANNEL — CRACKED (BS 574) · airframe 12,272 hrs · 11,318 cycles

CHANNEL ON CARGO DOOR SUPPORT STRUCTURE CRACKED AT FS 574. CHANNEL ON CARGO DOOR SUPPORT STRUCTURE AT FS 574 REPLACED IAW SRM 51-42-06.

Part: SILL — CORRODED (BS 324-349) · corrosion level 2 · airframe 12,272 hrs · 11,318 cycles

SERVICE DOOR LOWER SILL PLATE CORRODED. SILL PLATE ON SERVICE DOOR LOWER REPLACED IAW SRM 51-41-02.

Part: BRACKET — CRACKED (RT NACELLE) · airframe 12,272 hrs · 11,318 cycles

CRACKED BRACKET ON RT NOSE INLET COWL APPROX 4 O`CLOCK POSITION. BRACKET FABRICATED IAW SRM 51-24-16 AND REPLACED IAW SRM 51-42-13.

Part: STEP — CRACKED (PAX DOOR) · airframe 12,272 hrs · 11,318 cycles

PAX DOOR TOP STEP FWD LOWER CORNER IS CRACKED. PAX DOOR TOP STEP FWD LOWER CORNER REPAIRED IAW REO 601R-52-11-702 REV A.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 12,272 hrs · 11,318 cycles

PAX DOOR AFT DRAG ANGLE CRACK. PAX DOOR DRAG ANGLE REPAIRED IAW REO 601R-53-11-513 REV A.

Part: STEP — CRACKED (PAX DOOR) · airframe 12,272 hrs · 11,318 cycles

PAX DOOR TOP STEP AFT LOWER CORNER IS CRACKED. PAX DOOR TOP STEP AFT LOWER CORNER REPAIRED IAW REO 601R-52-11-702 REV A.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 12,272 hrs · 11,318 cycles

CRACK EXISTS ON INTERCOSTAL FS 484 LBL 36. DAMAGED ATTACHMENT FLANGE CUTOUT, EDDY CURRENT PERFORMED AND NEW SERVICEABLE ANGLE INSTALLED IAW REO 601R-53-41-059 REV A.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 12,272 hrs · 11,318 cycles

CRACK EXISTS ON INTERCOSTAL FS 484 RBL 36 AND RBL 27. DAMAGED ATTACHMENT FLANGE CUTOUT, EDDY CURRENT PERFORMED AND NEW SERVICEABLE ANGLE INSTALLED IAW REO 601R-53-41-059 REV A.

Part: STEP — CRACKED (PAX DOOR) · airframe 12,272 hrs · 11,318 cycles

PAX DOOR MID STEP, AFT CORNER EDGE IS CRACKED. OPEN. (S)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 12,272 hrs · 11,318 cycles

CORROSION EXISTS UNDER FLOOR FS 576, FS 605, FS 618 LBL 40. CORROSION REMOVED UNDER FLOOR FS 576, FS 605, FS 618 LBL 40 IAW SRM 51-21-06.

Part: SILL — CORRODED (FUSELAGE) · airframe 12,272 hrs · 11,318 cycles

CORROSION EXISTS ON LOWER SILL OF CARGO DOOR FS 574 TO FS 621 LBL 45. CORROSION REMOVED IAW SRM 51-21-06.

Part: BRACKET — CRACKED (LT NACELLE) · airframe 12,272 hrs · 11,318 cycles

LEFT TAIL PIPE STANDOFF BRACKET FOR FIRE DETECTION LOOP CRACKED. REPLACED IAW SRM 51-42-06. (S)

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 12,272 hrs · 11,318 cycles

RT FS 280 RBL 8 & 10 ANGLE ON BEAM FOUND CRACKED. RT FS 280 RBL 8 & 10 ANGLE ON BEAM REPLACED IAW SRM 51-42-21.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 12,272 hrs · 11,318 cycles

LEFT FS 280, LBL 8 & 10, ANGLE ON BEAM FOUND CRACKED. LT FS 280, LBL 8 & 10, ANGLE ON BEAM REPLACED IAW SRM 51-42-21.

Part: SEPARATOR — WORN (ACCESS PANEL) · airframe 12,272 hrs · 11,318 cycles

FIREWALL SEPARATOR WORN ON ACCESS PANEL 412DB. (K) FIREWALL SEPARATOR REPLACED IAW SRM 51-42-06.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 12,272 hrs · 11,318 cycles

NR 2 HYDRAULIC SUPPORT MANIFOLD BRACKET CRACKED. HYDRAULIC SUPPORT BRACKET REPAIRED IAW REO 601R-53-62-031 REV A.

Part: FIRE BOTTLE — DISCHARGED (CARGO BAY)

CARGO BOTTLE LOW LIGHT ILLUMINATED, LEFT FIRE BOTTLE BLOWN. RT FIRE BOTTLE BLOWN. REMOVED AND REPLACED LEFT CARGO FIRE BOTTLE PER CRJ AMM 26-25-01, OPS CHECK GOOD. REMOVED AND REPLACED RIGHT FIRE BOTTLE PER AMM 26-25-01, OPS CHECK GOOD, P/N 34600037-1, AND 36500018-3, S/N 22599F1 AND 48048D1.

Part: SPRING — LACK OF LUBE (SERVICE DOOR)

SERVICE DOOR MECHANISM HAS NO TENSION, WILL NOT LATCH OPEN. CLEANED AND LUBED RETURN SPRING ON SERVICE DOOR HOLD OPEN LOCK, ALL IAW CRJ AMM 52-11-00. (M)

Part: LINE — LEAKING (RT BRAKE) · airframe 7,353 hrs · 6,548 cycles

RT BRAKE LINE LEAKING, SMOKING. REMOVED AND REPLACED BRAKE DISCONNECT O-RING IAW AMM. OPS AND LEAK CHECK GOOD AT THIS TIME. (K)

Part: SKIN — DENTED (BS 605 S19-20L)

ONE DENT FORWARD OF FS 605 BETWEEN STRINGER 19L AND 20L. MAINTENANCE PERFORMED REPAIR TO FUSELAGE SKIN FS 605.00 BETWEEN STRINGER 19L AND 20L IAW BSC EO 601R-53-9198B. REQUIRES COMPLIANCE WITH FAR 25.571 (DTA) WITHIN 12 MONTHS OF RETURN TO SERVICE. (M)

Part: SKIN — DENTED (BS 605)

TWO DENTS AFT OF FUSELAGE STATION 605 BETWEEN STRINGER 23L AND 24L. MAINTENANCE PERFORMED REPAIR TO FUSELAGE SKIN AFT OF FS 605 BETWEEN STRINGER 23L AND 24L IAW BSC EO 601R-53-9221. REQUIRES COMPLIANCE WITH FAR 25.571 (DTA) WITHIN 12 MONTHS FROM RETURN TO SERVICE. (M)

Part: SUPPORT ANGLE — CRACKED (ENGINE SUPPORT)

RIGHT REINFORCEMENT ANGLE AT FS 640 BETWEEN STRINGER 9 AND 12 IS CRACKED IN RADIUS APPROX 3 INCHES DOWN FROM TOP OF ANGLE AND APPROX .75 INCH LONG. REF WO 95968 JOB CARD 4EOMFG10776 FOR INCORPORATION OF ENGINE SUPPORT BEAM MODIFICATION. (M)

Part: SUPPORT ANGLE — CRACKED (ENGINE SUPPORT)

LEFT RE-ENFORCEMENT ANGLE AT FS 640 BETWEEN STRINGER 9 AND 12 IS CRACKED IN RADIUS APPROX 3 INCHED DOWN FROM TOP Y-ANGLE AND APPROX .75 INCH LONG. REF WO 95968 JOB CARD 4EOMFG10776 FOR INCORPORATION OF ENGINE BEAM MODIFICATION. (M)

Part: SUPPORT BEAM — UNKNOWN (RT ENGINE)

RIGHT ENGINE SUPPORT BEAM LOWER.

Part: SKIN — CORRODED (LT WING)

THE LOWER WING PLANK ACCESS HOLE FOR PANEL 410AB HAS SOME MINOR CORROSION AND PITTING AROUND OUTER PANEL SURFACE. BLENDED MINOR PITTING AND CORROSION ON LOWER LEFT WING PLANK ACCESS HOLE FOR PANEL 510AB IAW BOMBARDIER REO 601R-57-21-030. (M)

Part: FLOORBEAM — CRACKED (BS 621)

FOUND LEFT FS 621 FLOORBEAM ANGLE HAS 1 INCH CRACK IN OUTBOARD RADIUS. REPAIRED ANGLE AT LT FS 621 IAW BOMBARDIER REO 601R-53-61-117 REV C. (M)

Part: RIB — CRACKED (MLG WW)

FOUND RIGHT MLG WHEEL WELL BATTERY RIB HAS A .5 INCH LONG CRACK IN TOP RADIUS. REPAIRED RT MLG WHEEL WELL BATTERY RIB BY TRIMMING OUT DAMAGED AREA, CUT DOUBLER, FABRICATED REPAIR PARTS AND WET INSTALLED IAW BOMBARDIER REO 601R-57-51-046 REV B REPAIR NR 1. (M)

Part: INTERCOSTAL — CRACKED (BS 484)

LT INTERCOSTAL AT FS 484 LBL 36 HAS A .25 INCH CRACK IN UPPER RADIUS. REPAIRED LEFT INTERCOSTAL AT FS 484 LBL 36 IAW BOMBARDIER REO 601R-53-41-059 AND BSC SR 601R-53-0030A. (M)

Part: FLOORBEAM — CRACKED (BS 621)

RIGHT FS 621 FLOORBEAM ANGLE HAS A 1 INCH CRACK ON OUTBOARD RADIUS. REPAIRED FLOORBEAM ANGLE AT RT FS 621 IAW BOMBARDIER REO 601R-53-61-117 REV C. (M)

Part: INTERCOSTAL — CRACKED (BS 625)

FOUND RIGHT FS 625 OBLIQUE ANGLE IS CRACKED. REMOVED AND REPLACED RT 625 OBLIQUE INTERCOSTAL P/N 601-35012-52 IAW CRJ 200 SRM 51-42-06. (M)

Part: ANGLE — CRACKED (FS 625)

FOUND LEFT FS 625 OBLIQUE ANGLE IS CRACKED. REMOVED AND REPLACED LEFT OBLIQUE INTERCOSTAL P/N 601-35012-51 IAW CRJ 200 SRM 51-42-06. (M)

Part: SUPPORT BEAM — CRACKED (LT ENGINE)

LT ENGINE SUPPORT BEAM LOWER WEB IS CRACKED 1 INCH LONG IN FORWARD INBOARD CORNER OF ACCESS DOOR CUTOUT, REF WO 95968 JOB CARD 4EOMFG10776 FOR INCORPORATION OF ENGINE SUPPORT BEAM MODIFICATION. (M)

Part: IDG — UNKNOWN (ELECT PWR SYS) · airframe 6,625 hrs · 5,872 cycles

IDG NR 2 CAUTION MESSAGE ILLUMINATED ON TAKEOFF ROLL. AC WEIGHT=43000, MAX BTMS= 5. 344. ALL IN GREEN SPEED AT ABORTED TAKEOFF = 45 KNOTS INITIAL LEAK CHECK NO LEAKS NOTED. SERVICED IDG NR 2 GROUND RAN ENGINE IDG/GEN OPERATES NORMAL, POST RUN NO LEAKS NOTED. (K)

Part: LANDING GEAR — MALFUNCTIONED (NOSE) · airframe 6,302 hrs · 5,572 cycles

AFTER GEAR RETRACTION, NOSE GEAR WOULD NOT RETRACT, GEAR RETRACTION HORN SOUNDED. C/W QRH LANDED IN MSP AT 42000. MEL`D GEAR RET SYS FUNCTION TESTED GEAR SYS. PERFORMED GEAR DISAGREE TEST, FULLY SERVICED NLG STRUT.. PERFORMED LANDING GEAR EXT/RETRACT FUNCTION TEST NUMEROUS TIMES, NO FAULTS NOTED. REMOVED FROM MEL. (K)

Part: DOUBLER — DAMAGED (FUSELAGE)

AFTER REMOVING ACCESS PANEL 132AL, FOUND 4 HOLES IN FORWARD FUSELAGE ACCESS PANEL DOOR SURROUND DOUBLER FS 228, STR19R-20R. PERFORMED A MAJOR REPAIR BY OPENING UP HOLES TO REMOVE DAMAGE, FABRICATED AND INSTALLING FREEZE PLUGS. OPENED HOLES IN FREEZE PLUGS USING NR 10 DRILL BIT. ALL WORK DONE IAW REO 601R-53-11-162.