N432AW

Part: DOUBLER — DAMAGED (WINGLET) · airframe 46,934 hrs · 45,528 cycles

LH WINGLET DOUBLER PN 600-10380-63 HAS SEVERAL TOOL MARKS. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED DAMAGE TO A SMOOTH CONTOUR TO LH WINGLET DOUBLER PN 600-10380-63, REF CRJ200 SRM 57-31-31 REV 38, PG6, FIGURE 1, SHT 2, ITEM 34, MATERIAL 0.071Ï¿½ CLAD 2024-T3. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA # AWAC-CRJ257-01728 REV A DATED 11/11/2021. WORK PERFORMED UNDER AERSALE WORK ORDER 003472, CARD NO. 20227, TT: 46934 TC: 45528.

Part: STRAP — DAMAGED (WINGLET) · airframe 46,934 hrs · 45,528 cycles

LH WINGLET LOWER STRAP PN 600-15108 HAS SEVERAL TOOL MARKS. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED DAMAGE TO A SMOOTH CONTOUR TO LH WINGLET LOWER STRAP PN 600-15108, REF CRJ200 SRM 57-31-31 REV 38, PG5, FIGURE 1, SHT 1, ITEM 3, MATERIAL 0.040Ï¿½ CLAD 2024-T3. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA # AWAC-CRJ257-01726 REV IR DATED 11/10/2021. WORK PERFORMED UNDER AERSALE WORK ORDER 003472, CARD NO. 20227, TT: 46934 TC: 45528.

Part: STRAP — DAMAGED (WINGLET) · airframe 46,934 hrs · 45,528 cycles

LH WINGLET LOWER STRAP PN 600-15108 HAS SEVERAL TOOL MARKS. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED DAMAGE TO A SMOOTH CONTOUR TO LH WINGLET LOWER STRAP PN 600-15108, REF CRJ200 SRM 57-31-31 REV 38, PG5, FIGURE 1, SHT 1, ITEM 8, MATERIAL 0.040Ï¿½ CLAD 2024-T3. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA # AWAC-CRJ257-01727 REV IR DATED 11/10/2021. WORK PERFORMED UNDER AERSALE WORK ORDER 003472, CARD NO. 20227, TT: 46934 TC: 45528.

Part: STRAP — DAMAGED (WINGLET) · airframe 46,934 hrs · 45,528 cycles

LH WINGLET LOWER STRAP PN 600-15108 HAS SEVERAL TOOL MARKS. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED DAMAGE TO A SMOOTH CONTOUR TO LH WINGLET LOWER STRAP PN 600-15108, REF CRJ200 SRM 57-31-31 REV 38, PG5, FIGURE 1, SHT 1, ITEM 6, MATERIAL 0.071Ï¿½ CLAD 2024-T3. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA # AWAC-CRJ257-01725 REV IR DATED 11/10/2021. WORK PERFORMED UNDER AERSALE WORK ORDER 003472, CARD NO. 20227, TT: 46934 TC: 45528.

Part: DOUBLER — DAMAGED (WINGLET) · airframe 46,934 hrs · 45,528 cycles

LH WINGLET DOUBLER PN 600-10380-59 HAS SEVERAL TOOL MARKS. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED DAMAGE TO A SMOOTH CONTOUR TO LH WINGLET DOUBLER PN 600-10380-59, REF CRJ200 SRM 57-31-31 REV 38, PG6, FIGURE 1, SHT 2, ITEM 33, MATERIAL 0.071Ï¿½ CLAD 2024-T3. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA # AWAC-CRJ257-01724 REV IR DATED 11/10/2021. WORK PERFORMED UNDER AERSALE WORK ORDER 003472, CARD NO. 20227, TT: 46934 TC: 45528.

Part: NONE — CORRODED (PAX DOOR FS 333.) · corrosion level 2 · airframe 46,934 hrs · 45,528 cycles

CORROSION FOUND ON BRACKET ASSEMBLY COMMON TO PASSENGER DOOR SURROUND STRUCTURE FS 318.00 LBL 40. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED CORROSION ON BRACKET ASSY 601R31527-149 AT FS 318.00 AT 4 EACH LOCATIONS. (P1) 2.100L X 1.200W X .008D (P2) 2.5L X 1.100W X .008D (P3) 1.400L X .800W X .005D (P4) 1.400L X .400W X .004D. (P1) AND (P2) FOUND TO BE OUT OF LIMITS AND (P3) AND (P4) WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-00 REV 38. REMOVED BRACKET ASSEMBLY P/N: 601R31527-149 COMMON TO FS 318.00 AND PASSENGER DOOR LOWER SURROUND STRUCTURE. INSTALLED BRACKET ASSEMBLY 601R31527-217 (PART NUMBER INTERCHANGEABLE WITH P/N: 601R31527-149) AT FS 318.00 AND PASSENGER DOOR LOWER SURROUND STRUCTURE IAW CRJ200 SRM 51-42-06 REV 38. RESTORED PROTECTIVE FINISH. ALL WORK PERFORMED AT AERSALE CRS4AER685B ON W/O #003472 AND CARD #20189.

Part: NONE — CORRODED (PAX DOOR FS 333.) · corrosion level 2 · airframe 46,934 hrs · 45,528 cycles

CORROSION FOUND ON FLOOR STRUCTURE COMMON TO PASSENGER DOOR SURROUND STRUCTURE AT FS 333.00 TO FS 349.00 LBL 36 TO LBL 40. ***AIRCRAFTY REMOVED FROM SERVICE*** BLENDED CORROSION ON BRACKET ASSY 601R31527-149 AT FS 333.00 AT 4 EACH LOCATIONS. (P1) 2.100L X 1.200W X .008D (P2) 2.5L X 1.100W X .008D (P3) 1.400L X .800W X .005D (P4) 1.400L X .400W X .004D. (P1) AND (P2) FOUND TO BE OUT OF LIMITS AND (P3) AND (P4) WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-00 REV 38. REMOVED BRACKET ASSEMBLY P/N: 601R31527-149 COMMON TO FS 333.00 AND PASSENGER DOOR LOWER SURROUND STRUCTURE. INSTALLED BRACKET ASSEMBLY 601R31527-217 (PART NUMBER INTERCHANGEABLE WITH P/N: 601R31527-149) AT FS 333.00 AND PASSENGER DOOR LOWER SURROUND STRUCTURE IAW CRJ200 SRM 51-42-06 REV 38. CLEANED FLOOR STRUCTURE COMMON TO PASSENGER DOOR SURROUND AND FS 333.00 TO FS 349.00 AND LBL 36 TO LBL 40 IAW CRJ200 SRM 51-26-00 REV 38. NO FURTHER CORROSION FOUND. RESTORED PROTECTIVE FINISH. ALL WORK PERFORMED AT AERSALE CRS4AER685B ON W/O #003472 AND CARD #20184.

Part: NONE — DENTED (FS 621) · airframe 46,934 hrs · 45,528 cycles

AFT PRESSURE BULKHEAD HAS DENT WITH A GOUGE .500"L X .300"W X .015"D AT FS 621, LBL 9.5 TO LBL 18.00, AND 2.0" ABOVE WL 73.50. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED GOUGE FROM DENTED AREA. GOUGE MEASURES: .250"L X .050"W X .013"D. CUTOUT DAMAGED AREA (.350" DIAMETER). FABRICATED, LOCATED AND DRILLED REPAIR DOUBLER (3.0" DIA) OUT OF 2024-T3 .050" MATERIAL. INSTALLED REPAIR DOUBLER (3.0" DIA) TO REPAIR AREA ON AFT PRESSURE BULKHEAD AT FS 621, LBL 9.5 TO LBL 18.00, AND 2" ABOVE WL 73.50. HFEC PERFORMED AT REPAIR AREA WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. APPLIED CIC PROTECTION TO REPAIR AREA. ALL WORK PERFORMED WITHIN ALLOWABLE LIMITS IAW MHIRJ REO 601R- 53-61-7748 REV (--) DTD 2021-11-15 AT AERSALE CRS4AER685B ON W/O #003472 CARD #20152. N432AW TT: 46,934 TC: 45,528

Part: STRAP — DAMAGED (WINGLET) · airframe 46,934 hrs · 45,528 cycles

RH WINGLET LOWER OUTBOARD FAIRING STRAP PN 600-10388 HAS SEVERAL TOOL MARKS. ***AIRCRAFT REMOVED FROM SERVICE*** RH WINGLET LOWER OUTBOARD FAIRING STRAP PN 600-10388 HAS SEVERAL TOOL MARKS. BLENDED DAMAGE TO A SMOOTH CONTOUR TO RH WINGLET LOWER OUTBOARD FAIRING STRAP PN 600-10388. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA # AWAC-CRJ257-01721 REV IR DATED 11/09/2021. WORK PERFORMED UNDER AERSALE WORK ORDER 003472, CARD NO. 20159, TT: 46934 TC: 45528.

Part: NONE — DENTED (FS 621) · airframe 46,934 hrs · 45,528 cycles

AFT PRESSURE BULKHEAD HAS DENT WITH A GOUGE .600"L X .500"W X .025"D AT FS 621, 3.7" O/B OF RBL 36.20, AND 2.0" ABOVE WL 73.50. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED GOUGE FROM DENTED AREA. GOUGE MEASURES: .250"L X .050"W X .011"D. CUTOUT DAMAGED AREA (1.0" DIAMETER). FABRICATED, LOCATED AND DRILLED REPAIR DOUBLER (3.8" DIA) OUT OF 2024-T3 .050" MATERIAL. INSTALLED REPAIR DOUBLER (3.8" DIA) TO REPAIR AREA ON AFT PRESSURE BULKHEAD AT FS 621, 3.7" O/B OF RBL 36.20, AND 2" ABOVE WL 73.50. HFEC PERFORMED AT REPAIR AREA WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. APPLIED CIC PROTECTION TO REPAIR AREA. ALL WORK PERFORMED WITHIN ALLOWABLE LIMITS IAW MHIRJ REO 601R- 53-61-7751 REV (--) DTD 2021-11-15 AT AERSALE CRS4AER685B ON W/O #003472 CARD #20150. N432AW TT: 46,934 TC: 45,528

Part: NONE — CORRODED (L/H WING LOWER P) · corrosion level 2 · airframe 46,934 hrs · 45,528 cycles

CORROSION DAMAGE COMMON TO L/H WING ACCESS PANEL #540AT AT LOWER WING PLANK LAND AROUND ENTIRE AREA OF LAND. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION ON LOWER WING PLANK LAND COMMON TO L/H WING ACCESS PANEL #540AT. BLEND DIMENSIONS ARE 19.50"L X .340"W X .O13"D. REMAINING THICKNESS IS .187" WITH A NOMINAL THICKNESS OF .200". HFEC PERFORMED AT REPAIR AREA WITH NO INDICATIONS. FLAP PEENED ENTIRE REPAIR AREA. RESTORED PROTECTIVE FINISH. VERIFIED GAPS BETWEEN ACCESS DOOR PANEL AND WING LAND ARE WITHIN LIMITS IAW CRJ200 SRM 51-14-06 REV 38. ALL WORK PERFORMED WITHIN ALLOWABLE LIMITS IAW MHIRJ REO 601R-57-21-3544 REV (--) DATED 2021- 11-12 AT AERSALE CRS4AER685B ON W/O #003472 CARD #20175. N432AW TT: 46,934 TC: 45,528.

Part: DOUBLER — DAMAGED (WINGLET) · airframe 46,934 hrs · 45,528 cycles

RH WINGLET INNER SKIN LOWER STRAP PN 600-15108 HAS SEVERAL TOOL MARKS. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED DAMAGE TO A SMOOTH CONTOUR TO RH WINGLET INNER SKIN LOWER STRAP PN 600-15108. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA # AWAC-CRJ257-01723 REV IR DATED 11/10/2021. WORK PERFORMED UNDER AERSALE WORK ORDER 003472, CARD NO. 20159, TT: 46934 TC: 45528.

Part: NONE — DENTED (FS 621) · airframe 46,934 hrs · 45,528 cycles

AFT PRESSURE BULKHEAD HAS DENT .400"L X .300"W X .010"D AT FS 621 IN BETWEEN LBL 27.50 AND LBL 36.20 AND 1.70" ABOVE WL 73.50. ***AIRCRAFT REMOVED FROM SERVICE*** DRESSED BACK DENT ON AFT PRESSURE BULKHEAD TO ORIGINAL CONTOUR. HFEC WAS PERFORMED AT REWORK AREA WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. RESTORED CIC PROTECTION. ALL WORK PERFORMED WITHIN ALLOWABLE LIMITS IAW MHIRJ REO 601R-53-61-7750 REV (--) DTD 2021-11-15 AND MHIRJ REO 601R-51-00-309 REV(A) DTD 2017-08-23 AT AERSALE CRS4AER685B ON MNT W/O #003472 CARD #20153.

Part: DOUBLER — DAMAGED (WINGLET) · airframe 46,934 hrs · 45,528 cycles

RH WINGLET DOUBLER PN 600-10388-60 HAS SEVERAL TOOL MARKS. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED DAMAGE TO A SMOOTH CONTOUR TO RH WINGLET DOUBLER PN 600-10388-60. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA # AWAC-CRJ257-01722 REV IR DATED 11/09/2021. WORK PERFORMED UNDER AERSALE WORK ORDER 003472, CARD NO. 20159, TT: 46934 TC: 45528.

Part: SKIN — DENTED (FS589) · airframe 46,934 hrs · 45,528 cycles

AIRCRAFT R/H SKIN EXTERIOR HAS 5 EACH DENTS AT FS 589.00 TO FS 605.00 AND S24R - S25R. DENT DIMENSIONS ARE: (P1) .500L X .400W X .006D; (P2) .450L X .400W X .004D; (P3) .200L X .200W X .001D; (P4) .350L X .200W X .001D; (P5) .350L X .300W X .003D. EVALUATED DENTS P1 - P5 AND FOUND ALL NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV 38. ****************AIRCRAFT REMOVED FROM SERVICE*********************** VERIFIED NO LOOSE/PULLED FASTENERS AND NO DAMAGE TO UNDERLYING STRUCTURE COMMON TO DAMAGED AREA. HFEC PERFORMED WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. RE-EVALUATED ALL 5 DENTS AND FOUND WITHIN LIMITS IAW ASAP EA #AWAC-CRJ253-01714 REV A DATED 11/18/2021. ALL WORK PERFORMED IAW ASAP EA # AWAC-CRJ253-01714 REV A DATED 11/18/2021. WORK COMPLETED AT AERSALE CRS4AER685B ON W/O #003472 CARD #20017. N432AW TT:46,934 TC:45,528

Part: SKIN — DENTED (FS 640) · airframe 46,934 hrs · 45,528 cycles

DENT ON AFT FUSELAGE SKIN AT FS625.30+13 - FS640.00 AND S22R - S23R. ***AIRCRAFT REMOVED FROM SERVICE*** EVALUATED DENT ON AFT FUSELAGE SKIN AT FS625.30+13 - FS640.00 AND S22R - S23R AND FOUND TO BE ACCEPTABLE PER EA. DENT DIMENSIONS P1- L = 0.900Ï¿½ X W = 0.800Ï¿½ X D = 0.002Ï¿½. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA # AWAC -CRJ253-01705 REV IR DATED 11/4/2021. WORK PERFORMED UNDER AERSALE WORK ORDER 003472, CARD NO. 20019, TT: 46934 TC: 45528.

Part: SKIN — DENTED (FS 379+3) · airframe 46,934 hrs · 45,528 cycles

AIRCRAFT HAS OUTWARD DENT ON R/H FUSELAGE SKIN EXTERIOR AT FS 379.00 +3 AT S18R+4. DIMENSIONS = .200"L X .100"W X .003"D. DENT NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV 38. ********AIRCRAFT REMOVED FROM SERVICE*********** PERFORMED CUTOUT (.400" DIA.) AT FS 379.00+3 AND S18R+4. FABRICATED, LOCATED, AND DRILLED REPAIR DOUBLER FROM 2024-T3 .063". INSTALLED REPAIR DOUBLER (7.0"L X 6.7"W) AT REPAIR LOCATION. HFEC PERFORMED AT CUTOUT AND ALL REPAIR PARTS WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. IDENTIFIED REPAIR WITH INDELIBLE INK AS EA#AWAC-CRJ253-01712. ALL WORK PERFORMED WITHIN ALLOWABLE LIMITS IAW ASAP EA #AWAC-CRJ253-01712 REV IR DATED 11/16/2021. WORK PERFORMED AT AERSALE CRS4AER685B ON W/O #003472 CARD #20006.

Part: SKIN — DENTED (R/H SKIN)

AIRCRAFT HAS 2EA DENTS LOCATED ON R/H FUSELAGE SKIN EXTERIOR BETWEEN FS 589+5 TO FS 589+8 JUST BELOW S25R. DENT DIMENSIONS (D1) 1.100L X .900W X .003D (D2) 1.100L X .900W X .009D. (P1) AND (P2) ARE NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV 38. ***AIRCRAFT REMOVED FROM SERVICE*** VERIFIED NO LOOSE/PULLED FASTENERS OR DAMAGE TO THE UNDERLYING STRUCTURE IN PROXIMITY TO BOTH DENTS. HFEC PERFORMED WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK PERFORMED AND BOTH DENTS WITHIN ALLOWABLE LIMITS IAW ASAP EA#AWAC-CRJ253-01713 REV A DATED 11/18/2021. WORK COMPLETED AT AERSALE CRS4AER685B ON W/O #003472 CARD #20016 N432AW TT:46,934 TC:45,528

Part: SKIN — DENTED (FS 625) · airframe 46,934 hrs · 45,528 cycles

DENT ON AFT FUSELAGE SKIN AT FS625.3 - FS640.00 AND S25R - S26R. ***AIRCRAFT REMOVED FROM SERVICE*** HAND DRESSED DENT ON AFT FUSELAGE SKIN AT FS625.3 - FS640.00 AND S25R - S26R DENT DIMENSIONS P1- L = 1.200Ï¿½ X W = 0.900Ï¿½X D = 0.006Ï¿½. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA # AWAC -CRJ253-01706 REV IR DATED 11/4/2021. WORK PERFORMED UNDER AERSALE WORK ORDER 003472, CARD NO. 20018, TT: 46934 TC: 45528.

Part: SKIN — DENTED (FS 654.5) · airframe 46,934 hrs · 45,528 cycles

DENTS (11 TOTAL) ON AFT FUSELAGE SKIN AT FS654.5 - FS672.20 AND S22R - S24R. ***AIRCRAFT REMOVED FROM SERVICE*** EVALUATED 11 DENTS ON AFT FUSELAGE SKIN AT FS654.5 - FS672.20 AND S22R - S24R. DENTS DIMENSION: FS654.50 Ï¿½ FS672.2 AND S22R Ï¿½ S23R: P1= L = 0.200Ï¿½ X W = 0.180Ï¿½X D = 0.002Ï¿½. P2= L = 0.150Ï¿½ X W = 0.125Ï¿½X D = 0.002Ï¿½. P3= L = 0.175Ï¿½ X W = 0.150Ï¿½X D = 0.002Ï¿½. P4= L = 0.100Ï¿½ X W = 0.100Ï¿½X D = 0.002Ï¿½. P5= L = 0.175Ï¿½ X W = 0.175Ï¿½X D = 0.002Ï¿½. P6= L = 0.150Ï¿½ X W = 0.150Ï¿½X D = 0.003Ï¿½. FS654.50 Ï¿½ FS672.2 AND S23R Ï¿½ S24R: P7= L = 0.150Ï¿½ X W = 0.150Ï¿½X D = 0.002Ï¿½. P8= L = 0.150Ï¿½ X W = 0.150Ï¿½X D = 0.002Ï¿½. P9= L = 0.200Ï¿½ X W = 0.150Ï¿½X D = 0.005Ï¿½. P10= L = 0.175Ï¿½ X W = 0.150Ï¿½X D = 0.002Ï¿½. P11= L = 0.150Ï¿½ X W = 0.150Ï¿½X D = 0.002Ï¿½. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA # AWAC - CRJ2 53-01715 REV IR DATED 11/6/2021.WORK PERFORMED UNDER AERSALE WORK ORDER 003472, CARD NO. 20022, TT: 46934 TC: 45528.

Part: SKIN — DENTED (FS 682+4) · airframe 46,934 hrs · 45,528 cycles

DENT ON AFT FUSELAGE SKIN AT FS682.00+4Ï¿½ AND S19R - S20R. ***AIRCRAFT REMOVED FROM SERVICE*** HAND DRESSED DENT TO RE-FORM ORIGINAL CONTOUR ON AFT FUSELAGE SKIN AT FS682.00+4Ï¿½ AND S19R - S20R. DENT DIMENSION L = 0.500Ï¿½ X W = 0.400Ï¿½ X D = 0.008Ï¿½. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA # AWAC-CRJ253-01703 REV IR DATED 11/3/2021. WORK PERFORMED UNDER AERSALE WORK ORDER 003472, CARD NO. 20027, TT: 46934 TC: 45528.

Part: WEB — CRACKED (FS311.75 TO FS34) · airframe 46,934 hrs · 45,528 cycles

PASSENGER DOOR HAS A CRACK .375"L ON INNER WEB P/N:601R31902-537 AT FS 320 AT UPPER FORWARD CORNER. **************AIRCRAFT REMOVED FROM SERVICE********************** DURING INCORPORATION OF GENERIC REO 601R-52-11-402 REV H, HFEC INSPECTION FOUND CRACK ON INNER WEB FWD OF INNER SKIN CUTOUT AT FS 320 AND SEVERAL CRACKS ON FORMER P/N:601R31902-455. PERFORMED CUTOUT 13.4"L X 6.7"W ON INNER WEB AT FS 320. CUTOUT 1"L X .600"W ON INNER WEB AT FS 320. PERFORMED CUTOUT TO INNER FORMER AT FS 320 12"L X 4.3"W. HFEC WAS PERFORMED AT ALL CUTOUTS WITH NO INDICATIONS. REPAIRED INNER FORMER P/N:601R31902-455 WITH REPAIR SPLICES IAW GENERIC REO 601R-52-11- 402 REV H. REPAIRED INNER WEB P/N:601R31902-537 WITH REPAIR DOUBLER 17.8"L X 10.5"W 2024-T3 .050" IAW GREO 601R-52-11-402 REV H AND MHIRJ REO 601R- 52- 11-2905 REV (--) RESTORED PROTECTIVE FINISH. ALL WORK PERFORMED WITHIN ALLOWABLE LIMITS IAW GREO 601R-52-11-402 REV (H) AND MHIRJ 601R-52-11-2905 REV (--). WORK COMPLETED ON AERSALE W/O #003472 CARD #20106 CRS4AER685B. PASSENGER DOOR P/N:601R31901-69 S/N:7257

Part: WEB — CRACKED (FS 338) · airframe 46,934 hrs · 45,528 cycles

PASSENGER DOOR HAS CRACK ON INNER WEB AT FS 338.9 DOOR HAS EXISTING REPAIR IAW GREO 601R-52-11-402 REV H. ********************AIRCRAFT REMOVED FROM SERVICE*********************** EXTENDED CUTOUT ON INNER WEB PN:601R31902-537 AT FS 338.9 TO 13.300"L X 6.800"W. PERFORMED CUTOUT ON INNER FORMER PN: 601R31902-5 ( 12.5"L X 4.5"W). COMPLETED FRAME REPAIR AND REPAIR ON INNER WEB WITH DOUBLER 17.8"L X 9.6"W 2024-T3 .050" IAW GREO 601R-52-11-402 REV H. HFEC PERFORMED AT CUTOUTS WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. WORK PERFORMED ON AERSALE W/O #003472 CARD #20105 AT AERSALE CRS4AER685B. ALL WORK WITHIN LIMITS IAW GREO 601R-52-11-402 REV H.

Part: NONE — GOUGED (PAX DOOR) · airframe 46,934 hrs · 45,528 cycles

PASSENGER DOOR ROLLER BRACKET PN: 600-31471-9 HAS A GOUGE 0.400"L X 0.165"W X 0.020"D ON OUTSIDE EDGE OF BRACKET. ***************AIRCRAFT REMOVED FROM SERVICE******************* BLENDED THE DAMAGE TO A SMOOTH CONTOUR. HFEC PERFORMED WITH NO INDICATIONS. ROTO- PEENED REPAIR AREA. RESTORED PROTECTIVE FINISH. ALL WORK PERFORMED WITHIN ALLOWABLE LIMITS IAW ASAP EA # AWAC-CRJ252-01759 REV IR DATED 11/24/2021. WORK COMPLETED ON AERSALE W/O #003472 CARD #20256 AT AERSALE CRS4AER685B.

Part: ANGLE — CORRODED (FS 621) · corrosion level 2 · airframe 45,892 hrs · 44,416 cycles

T CAP CORRODED BEYOND LIMITS AT FS 621 TO FS 559+112 LBL 27. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED TCAP AT FS 559+112 TO FS 621, IAW CRJ SRM 51-42-21 AND BOMBARDIER DWG 601R35031.

Part: WIRE HARNESS — DEFECTIVE (NLG) · airframe 45,200 hrs · 43,698 cycles

DURING TAKE OFF CLIMB, WHEN SELECTING GEAR UP, RECEIVED NOSE GEAR DISAGREE WITHIN 6 SECONDS OF SELECTION. LH+RH GEAR INDICATED GEAR UP AND LACKED. NOSE GEAR WHITE IN TRANSIT. DECLARED EMERGENCY. LANDING WAS BELOW MAX LANDING WEIGHT @ 146 KNOTS. AIRCRAFT REMOVED FROM SERVICE RESET MANUAL GEAR EXTENTION. C/W M ACTION FOR MEL 32-30-01. REF. 319366/3 FOR MEL. R&R NLG WOW HARNESS PER AMM 32-61-25. OPS CHECK GOOD AT THIS TIME. REMOVED PLACARD/ MEL.

Part: TRANSDUCER — MALFUNCTIONED (HYD SYSTEM) · airframe 44,791 hrs · 43,207 cycles

PRESSURE INDICATOR ON HYD 1 FROM 200-1800 PSI. C/W QRH. QTY AND TEMPS NORMAL AT 15-20 DEG AND 60% QTY. NEVER RECEIVED LOW PRESS CAUTION. AIRCRAFT REMOVED FROM SERVICE R&R HYD SYS #1 PRESSURE TRANSDUCER. OPS CHECK GOOD.

Part: SELECTOR VALVE — ABNORMAL (MLG) · airframe 44,723 hrs · 43,232 cycles

SUPPLIMENTAL INFORMATION, AT 170 KTS APROX 2200 FT AGL RECEIVED GEAR DISSAGREE WARNING ON GEAR EXTENSION. NLG SHOWS DOWN AND LOCKED. MLG SHOW UP AND LOCKED. PER QRH CYCLED GEAR HANDLE CONDITION PERSISTS. PER QRH PULLED MANUAL GEAR EXTENSION. ALL SHOW DOWN AND LOCKED. MANUAL GEAR HANDLE NEEDS TO BE STOWED. NORMAL GEAR HANDLE IS SELECTED DOWN. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED MLG SELECTOR VALVE IAW AMM 32-32 OPS CHECK GOOD S/N OFF: 286 S/N ON: 0236.

Part: SEALANT — LOOSE (WINDSHIELD) · airframe 44,713 hrs · 43,226 cycles

SUPPLEMENTAL INFORMATION, AFTER TAKE-OFF, FIRST OFFICER'S WINDSHIELD SEALANT CAME LOOSE. STARTED MAKING LOUD SOUNDS AGAINST FIRST OFFICER'S WINDSHIELD THEN DEPARTED AIRCRAFT. MX INSPECTED AND FOUND FIRST OFFICER'S WINDSHIELD MISSING APPROXIMATELY 18" OF MOISTURE SEAL. AIRCRAFT REMOVED FROM SERVICE. REPAIRED FIRST OFFICER'S WINDSHEILD OUTBOARD MOISTURE SEAL, REFERENCE AMM 56-11-00-300-801.

Part: SUPPORT BEAM — CRACKED (BS 621) · airframe 44,681 hrs · 43,191 cycles

ANGLE AT FS 621 BAGGAGE DOOR UPPER SUPPORT BEAM IS CRACKED AIRCRAFT REMOVED FROM SERVICE FABRICATED REPLACEMENT ANGLE FROM 2024 T-3 .040" AND INSTALLED REFERENCE CRJ 200 SRM 51-42-20, 51-24-21, AND 53-61-23 REV 37.

Part: BRACKET — CRACKED (BS 574) · airframe 44,681 hrs · 43,191 cycles

BRACKET ASSY AT FS 574.00 & S6L HAS A CRACK AIRCRAFT REMOVED FROM SERVICE FABRICATED REPLACEMENT BRACKET FROM 2024 T-3 .050" REF CRJ 200 SRM 51-24-21 AND 53-61-15 REV 37. AND INSTALLED REF CRJ 200 SRM 51-42-21 AND 51-23-00 REV 37.

Part: BRACKET — CRACKED (BS 621) · airframe 44,681 hrs · 43,191 cycles

BRACKET ASSY AT FS 621.00 & S6L IS CRACKED. AIRCRAFT REMOVED FROM SERVICE FABRICATED REPLACEMENT BRACKET FROM 2014 T-3 .050" REF CRJ 200 SRM -51-24-21 AND 53-61-15 REV 37 AND INSTALLED REF CRJ 200 SRM 51-42-21 AND 51-23-00 REV 37.

Part: STRUCTURE — DAMAGED (RT WING TE FLAP) · airframe 44,681 hrs · 43,191 cycles

R/H O/B FLAP T/E DAMAGED 14" O/B FROM I/B CORNER. DAMAGE WAS INDUCED DURING MAINTENANCE. AIRCRAFT REMOVED FROM SERVICE REPAIRED DAMAGE ON R/H O/B FLAP T/E AT APPROX 14" O/B FROM I/B CORNER WITH A REPAIR DOUBLER THAT MEASURES 5.6" X 3.1" REF CRJ 200 SRM 57-53-00 REV 37.

Part: FITTING — CRACKED (SERVICE DOOR) · airframe 44,681 hrs · 43,191 cycles

FOUND CRACK ON MICRO SWITCH MOUNTING BRACKET INSTALLED ON THE SERVICE DOOR. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED MOUNTING BRACKET ON R1 SERVICE DOOR REF CRJ 200 SRM 51-42-20 REV 37.

Part: FITTING — CHAFED (RT WING TE FLAP) · airframe 44,681 hrs · 43,191 cycles

R/H WING O/B FOREFLAP / AFT FLAP FITTING WORN DUE TO SEIZED ROLLER.AT FZ 189.57. AIRCRAFT REMOVED FROM SERVICE BLENDED CHAFE DAMAGE AREA ON R/H WING O/B FLAP O/B FOREFLAP FITTING AND AFT FLAP FITTING IN AN AREA OF 4.2"L X .20"W X .005"D WITHIN LIMITS REF ASAP EA#AWAC CRJ257-01385 REV B AND AWAC SUPPLEMENT NO: 19-320.FITTING PART NUMBERS 601R14932-2 AND 601R14908-2

Part: PANEL — CRACKED (NACELLE) · airframe 44,681 hrs · 43,191 cycles

PANEL 433AB HAS A CRACK AIRCRAFT REMOVED FROM SERVICE REPLACED WITH SERVICEABLE PANEL 433AB REF CRJ200 SRM 52-41-02 REV 37.

Part: HINGE FITTING — CHAFED (RT WING TE FLAP) · airframe 44,681 hrs · 43,191 cycles

R/H WING O/B FLAP HINGE BOX AT WS 264.00 HAS 2 AREAS OF CHAFING DAMAGE. DAMAGE AREA 1 IS TO THE I/B FLAP HINE ARM FITTING DWG 601R10910 WITH DAMAGE DIMENSIONS OF .20"L X .15"W X .032"D. DAMAGE 2 IS TO THE AFT SIDE PLATE DWG 601R10180 WITH DAMAGE DIMENSIONS OF .20"L X .10" X .35"D. AIRCRAFT REMOVED FROM SERVICE BLENDED DAMAGED AREA #1 TO A SMOOTH CONTOUR ON R/H FLAP HINGE ARM FITTING AT WS 264.00 BLEND DIMENSIONS ARE .20"L X .15"W X .028"D BLENDED DAMAGE AREA #2 ON R/H FLAP HINGE BOX AT WS 264.00 I/B AFT PLATE STRUCTURAL PLATE LOWER EDGE WITH BLEND DIMENSIONS OF .20"L X .10"W X .020"D. HFEC PERFORMED NO DEFECTS NOTED. REF BOMBARDIER REO 601R-57-21-3193.

Part: SPOILER SYS — MALFUNCTIONED · airframe 44,297 hrs · 42,823 cycles

GROUND LIFT DUMP SYSTEM DID NOT DEPLOY ON INITIAL TOUCHDOWN CAUSING BOUNCE. DEPLOYED ON 2ND TOUCHDOWN. NO ASSOCIATED MSGS.

Part: CABIN PRESSURE — MALFUNCTIONED · airframe 43,966 hrs · 42,504 cycles

DURING CLIMB, THE CABIN WOULD NOT PRESSURIZE. THE FLIGHT LEVELED OFF AND THE CREW RAN THE QRH. THE FLIGHT RETURNED TO ORD AND LANDED WITHOUT FURTHER ISSUES.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 43,379 hrs · 41,928 cycles

ON CLIMBOUT, RECIEVED NOSE DOOR WARNING MESSAGE AND GEAR DISAGREE WARNING MESSAGES, C/W QRH, MESSAGE CLEARED, THEN DIVERTED.

Part: CONNECTOR — UNSECURE (PSU) · airframe 42,147 hrs · 40,739 cycles

DURING OPERATIONAL TEST OF PAX O2, PSU AT ROW 6CD FAILED TO DEPLOY. RESECURED CONNECTOR TO DEPLOY SOLENOID. SUBSEQUENT OPS TEST OF PAX O2 SYSTEM, AMM 35-20-00 PROVES GOOD.

Part: SKIN — CHAFED (BS 529-554) · airframe 41,252 hrs · 39,748 cycles

LEFT WING UPPER INBD AFT TE TO BODY (APRON SKIN) HAS LARGE CHAFE AREA. REPAIRED

Part: FRAME — CRACKED (BS 333) · airframe 41,252 hrs · 39,748 cycles

FRAME BS 333, OTBD OF STRINGER 0, FOUND CRACKED. REPLACED THE FRAME.

Part: ANGLE — CORRODED (BS 409-559) · airframe 41,252 hrs · 39,748 cycles

PRESSURE FLOOR SUPPORT ANGLES AT BS 409+128 TO 559, LBL 36 - 47 CORRODED. REPAIRED.

Part: FRAME — CRACKED (BS 333) · corrosion level 2 · airframe 41,252 hrs · 39,748 cycles

FRAME BS 333 HAS CORROSION ON THE FWD AND AFT SIDE BETWEEN STRINGERS 26L AND 26R. A .14 INCH CRACK WAS DISCOVERED DURING CORROSION REMOVAL. REPLACED.

Part: FLOOR SUPPORT — CORRODED (BS 310-349) · corrosion level 2 · airframe 41,252 hrs · 39,748 cycles

MAIN CABIN L1 DOOR CUT OUT LOWER SILL VERTICAL FLOOR SUPPORT IS CORRODED BS 310 - 349, LBL 42

Part: STIFFENER — CRACKED (BS 731) · airframe 41,252 hrs · 39,748 cycles

STIFFENER CRACKED BEHIND PANEL 326ER.

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 41,252 hrs · 39,748 cycles

LEFT WING INBD FLAP LOWER SKIN HAS DAMAGE IN LINE WITH MLG TIRES.

Part: SUPPORT ANGLE — CRACKED (BS 621-625) · airframe 41,252 hrs · 39,748 cycles

INTERCOSTAL SUPPORT ANGLE COMMON WITH SKIN CRACKED AT BS 621 TO 625.3, STRINGER 15L.

Part: FLOOR SUPPORT — CORRODED (BS 559) · corrosion level 2 · airframe 41,252 hrs · 39,748 cycles

RIGHT FLOOR SUPPORT CORRODED BETWEEN BS 559+84 AND 559+112

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 41,252 hrs · 39,748 cycles

INTERCOSTAL SUPPORT ANGLE COMMON TO SKIN CRACKED AT BS 621.00 TO 625.3, STRINGER 14L. REPLACED INTERCOSTAL ANGLE IAW SRM 51-42-21, AND 51-42-06.

Part: SUPPORT — CRACKED (BS 625) · airframe 41,252 hrs · 39,748 cycles

CRACK INDICATED DURING HFEC INSPECTION OF ENGINE SUPPORT BEAM AT FWD VERTICAL STIFFENER LOWER FASTENER HOLE. RBL 36.2, WL 111.09, BS 625.3.

Part: STRINGER — CRACKED (BS 379) · airframe 41,252 hrs · 39,748 cycles

STRINGER 3L FOUND CRACKED AT BS 379.

Part: ANGLE — CRACKED (BS 625) · airframe 41,252 hrs · 39,748 cycles

OBLIQUE ANGLE CRACKED AT BS 625, STRINGER 15L. REPLACED THE ANGLE IAW SRM 51-42-21.

Part: VANE — GOUGED (LT WING TE FLAP) · airframe 41,252 hrs · 39,748 cycles

LEFT INBD FLAP VANE CTR LEADING EDGE IS GOUGED.

Part: ANGLE — CRACKED (BS 700) · airframe 41,252 hrs · 39,748 cycles

AFT EQUIPMENT COMPARTMENT DOOR SURROUND ANGLE CRACKED AT BS 700, STRINGER 24L. REPLACED THE ANGLE IAW SRM 51-42-06, 53-61-23, 51-24-16, 51-24-21, 51-40-11, 51-21-11, 51-23-06, AND 51-25-16.

Part: ANGLE — CRACKED (BS 700) · airframe 41,252 hrs · 39,748 cycles

AFT EQUIPMENT DOOR CUTOUT SURROUND ANGLE CRACKED AT BS 700, STRINGER 24R. REPLACED THE ANGLE IAW SRM 51-42-06, 53-61-23, 51-24-16, 51-24-21, 51-40-11, 51-21-11, 51-23-06, AND 51-25-16.

Part: ANGLE — GOUGED (BS 621 BULKHEAD) · airframe 41,252 hrs · 39,748 cycles

AFT PRESSURE BULKHEAD HORIZONTAL ANGLE GOUGED OTBD OF AFT CARGO DOOR TRACK

Part: SUPPORT BRACKET — CRACKED (BS 469.63) · airframe 41,252 hrs · 39,748 cycles

LEFT OVERWING PANEL SUPPORT BRACKET CRACKED AT BS 469.63. REPLACED THE SUPPORT BRACKET IAW SRM 51-42-06.

Part: STRINGER CLIP — CRACKED (BS 280) · airframe 41,252 hrs · 39,748 cycles

BS 280, STRINGER CLIP 3L CRACKED.

Part: SUPPORT BRACKET — CRACKED (BS 449) · airframe 41,252 hrs · 39,748 cycles

LEFT OVERWING PANEL SUPPORT BRACKET CRACKED AT BS 449.85. REPLACED THE SUPPORT BRACKET IAW SRM 51-42-06.

Part: ANGLE — CRACKED (BS 280) · airframe 41,252 hrs · 39,748 cycles

BS 280, STRINGER 3L FWD ANGLE IS CRACKED.

Part: FLOOR SUPPORT — CORRODED (BS 559) · corrosion level 2 · airframe 41,252 hrs · 39,748 cycles

RIGHT FLOOR SUPPORT CORRODED AT BS 559+80 TO 559+114. REPLACED THE FLOOR SUPPORTL IAW SRM 51-42-06, 51-21-06, 51-25-06, AND 51-25-16.

Part: SUPPORT BRACKET — CRACKED (BS 476) · airframe 41,252 hrs · 39,748 cycles

LEFT OVERWING PANEL SUPPORT BRACKET CRACKED AT BS 476.67. REPLACED THE SUPPORT BRACKET IAW SRM 51-42-06.

Part: SUPPORT BRACKET — CRACKED (BS 461) · airframe 41,252 hrs · 39,748 cycles

RIGHT OVERWING PANEL SUPPORT BRACKET CRACKED AT BS 461. REPLACED THE SUPPORT BRACKET IAW SRM 51-42-06.

Part: SUPPORT BRACKET — CRACKED (BS 449.85) · airframe 41,252 hrs · 39,748 cycles

RIGHT OVERWING PANEL SUPPORT BRACKET CRACKED AT BS 449.85. REPLACED THE SUPPORT BRACKET IAW SRM 51-42-06.

Part: MOUNT — CORRODED (GALLEY) · corrosion level 2 · airframe 41,252 hrs · 39,748 cycles

GALLEY MOUNT PLATE AT BS 310 - 319, RBL 42 CORRODED. REPLACED THE GALLEY MOUNT.

Part: FITTING — CORRODED (BS 325) · corrosion level 2 · airframe 41,252 hrs · 39,748 cycles

MAIN CABIN DOOR SILL FITTING AT BS 325, LBL 42 CORRODED. REPLACED THE FITTING IAW SRM 51-42-06.

Part: DOOR SILL — CORRODED (BS 343) · corrosion level 2 · airframe 41,252 hrs · 39,748 cycles

PAX DOOR SILL CUTOUT CORRODED AT BS 343, LBL 42. REPLACED DOOR SILL IAW SRM 51-42-06.

Part: ANGLE — CORRODED (BS 319-349) · corrosion level 2 · airframe 41,252 hrs · 39,748 cycles

SERVICE DOOR LOWER SILL ANGLE CORRODED. REPLACED DOOR SILL ANGLE IAW SRM 51-42-06, AND 51-42-21.

Part: BRACKET — CORRODED (BS 315) · corrosion level 2 · airframe 41,252 hrs · 39,748 cycles

PAX DOOR SILL CUTOUT BRACKET CORRODED AT BS 315, LBL 42. REPLACED THE BRACKET IAW SRM 51-42-06.

Part: FORMER — CRACKED (L1 DOOR) · airframe 37,874 hrs · 36,641 cycles

INNER FORMER AT FS 338.9 ON L1 DOOR IS CRACKED NEAR TOP. REPAIRED INNER FORMER AT FS 338.9 ON L1 DOOR IAW REO 601R-52-11-402.

Part: INTERCOSTAL — CRACKED (L1 DOOR) · airframe 37,874 hrs · 36,641 cycles

LOWER FWD INTERCOSTAL ON L1 DOOR IS CRACKED. R & R LOWER FWD INTERCOSTAL ON PAX DOOR IAW SRM 51-42-06 & 51-42-21.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 37,874 hrs · 36,641 cycles

LEFT LANDING FOR THE CTR FLOOR PANEL IN THE FLIGHT DECK IS CRACKED AT THE VERY AFT FASTENER HOLE, FWD OF FS 280.00. REMOVED CRACKED ANGLE & INSTALLED NEW ANGLE FOR FLIGHT DECK CTR FLOOR LT SIDE IAW SRM 51-42-06, 51-42-21, 51-40-11 & 51-25-16.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 37,874 hrs · 36,641 cycles

AIRCRAFT SKIN AT ADF ANTENNA MOUNTING SURFACE HAS SCRIBE DAMAGE AROUND PERIMETER. REPAIRED ACFT SKIN AT ADF ANTENNA MOUNTING AREA IAW SUPPLEMENT 16-013A.

Part: FLOOR SKIN — CRACKED (FUSELAGE) · airframe 37,874 hrs · 36,641 cycles

RIGHT FWD UPPER AVIONICS BAY FLOOR CRACKED, OTBD OF THE ADG PUMP. REPAIRED UPPER AVIONICS BAY FLOOR IAW REO 601R-53-11-245 REV B DATED 2005 08 01.

Part: STRUCTURE — CRACKED (CARGO DOOR) · airframe 37,874 hrs · 36,641 cycles

CARGO DOOR VERTICAL MEMBER AT AFT LOWER CORNER OF DOOR APPROX 13 INCHES FROM AFT EDGE IS CRACKED. REMOVED CRACKED VERTICAL MEMBER & INSTALLED NEW MEMBER AT AFT LOWER CORNER OF CARGO DOOR IAW SRM 51-42-06, 51-42-13, 51-42-21, 51-40-11 & 51-25-16.

Part: ATTACH BRACKET — CRACKED (RT WING) · airframe 37,874 hrs · 36,641 cycles

OUTBOARD ATTACH BRACKET ON RT WING FOR OTBD LE IS CRACKED. REPLACED OTBD ATTACH BRACKET ON RT WING FOR OTBD LE IAW SRM 51-41-02.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,874 hrs · 36,641 cycles

FUSELAGE SKIN UNDER TCAS ANTENNA HAS CORROSION AROUND FASTENER HOLES & SCRIBE MARKS ON MATING SURFACE, INCLUDING UNDER SEALANT AROUND ANTENNA. REMOVED CORROSION & SCRIBE MARKS IAW SRM 51-21-06, 51-12-00 & REPAIRED REWORKED AREA IAW 253-00236 REV A.

Part: SKIN — DENTED (RUDDER) · airframe 37,874 hrs · 36,641 cycles

RUDDER LT SKIN HAS A DENT APPROX 12 INCHES UP FROM BOTTOM & 6 INCHES FWD OF THE AFT EDGE. REPAIRED LT RUDDER SKIN IAW SRM 55-40-00.

Part: UNKNOWN — MALFUNCTIONED (HORIZ STAB) · airframe 30,336 hrs · 29,954 cycles

ON APPROACH MULTIPLE STAB CHANNEL 1 STATUS MSGS. ACFT REQUIRES EXCESSIVE TRIM NOSE UP TO MAINTAIN STABLE DESCENT. 8.8 NEEDED FOR 2.5 DEGREE NOSE DOWN, 750 FEET PER MINUTE, AUTOPILOT OFF.

Part: WARNING MESSAGE — ILLUMINATED (MLG) · airframe 36,221 hrs · 35,052 cycles

GEAR UP DISAGREE WARNING MESSAGE AFTER TAKEOFF. LT MAIN GEAR SHOWING RED. COMPLIED WITH QRH GEAR EXTENDED NORMAL LANDING. THE MESSAGE CAME ON ABOUT 30 SECONDS AFTER GEAR WAS SELECTED UP.

Part: STRUT — UNKNOWN (NLG) · airframe 28,779 hrs · 28,461 cycles

GEAR DISAGREE AFTER TAKEOFF. RECEIVED NOSE DOOR OPEN WARNING & DOOR AURAL WARNING, NLG REMAINED GREEN. COMPLIED WITH QRH, NORMAL GEAR INDICATION AFTER SELECTING EMER GEAR DOWN, NWS INOPERATIVE APPEARED. AFTER LANDING NWS RESET WITH NO FAILURES AFTERWARD. REMOVED & REPLACES THE NLG SHOCK STRUT ASSEMBLY.

Part: LIGHT — INOPERATIVE (ROWS 9-12) · airframe 35,537 hrs · 34,401 cycles

EMERGENCY LIGHT ROW 9 - 12 INOPERATIVE.

Part: LANDING GEAR — MALFUNCTIONED (MAINS) · airframe 28,278 hrs · 27,982 cycles

AFTER DEPARTURE, SELECTED GEAR UP & AIRFRAME SHUTTERED. MLG INDICATION CHANGED FROM WHITE TO DASHES & NEVER INDICATED UP & GREEN, WITH NO ASSOCIATED MESSAGES, HYDRAULIC PRESSURE WAS NORMAL. ON GEAR EXTENSION NO GEAR ABNORMALITIES NOTED, DOWN & LOCKED INDICATED.

Part: LANDING GEAR — MALFUNCTIONED (NOSE) · airframe 28,269 hrs · 27,973 cycles

AFTER TAKEOFF AND GEAR UP, HEARD BANGING & VIBRATION FROM NOSE GEAR AREA. NO EICAS MESSAGE, SELECTED GEAR DOWN & NOISE STOPPED. EMERGENCY DECLARED, RETURNED TO DEPARTURE AND LANDED.

Part: ATTACH BRACKET — CRACKED (VERTICAL STAB) · airframe 33,028 hrs · 25,790 cycles

ATTACH BRACKET FOR THE 326CR PANEL IS CRACKED. RT FWD SIDE OF V STAB. R & R WITH NEW SERVICEABLE PART IAW CRJ 200 SRM 51-24-21, 51-40-11 & 51-42-21.

Part: SILL — CRACKED (FUSELAGE) · airframe 33,028 hrs · 25,790 cycles

CARGO DOOR SILL CRACKED FWD LATCH BRACKET AT FS 524. REPAIRED IAW REO 601R-53-61-1741.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 33,028 hrs · 25,790 cycles

PASSENGER DOOR AFT GUIDE ARM CUP AT FS 343 HAS CORROSION AROUND 1/13 SCREW HOLE. R & R CORRODED BRACKETS.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 33,028 hrs · 25,790 cycles

PASSENGER DOOR INNER HANDLE CRACKED. R & R PAX DOOR INNER HANDLE.

Part: STRUCTURE — CORRODED (PAX DOOR) · airframe 33,028 hrs · 25,790 cycles

PASSENGER DOOR HAS CORROSION ON FWD LOWER CORNER WITH THE DOOR CLOSED. BLENDED OUT CORROSION ALODINED, PRIMED & TOP COATED.

Part: HINGE — CRACKED (BUTE DOOR) · airframe 33,028 hrs · 25,790 cycles

LEFT INBD BUTE DOOR 594IB HAS CRACKED HINGE. R & R HINGE ON BUTE DOOR 594IB.

Part: BRACKET — CRACKED (TE FLAP) · airframe 33,028 hrs · 25,790 cycles

LEFT OTBD FLAP OTBD HINGE FLAP SIDE HINGE FAIRINGS BRACKET ON INBD SIDE CRACKED. REMOVED, FABRICATED & INSTALLED NEW BRACKET.

Part: FITTING — CRACKED (FUSELAGE) · airframe 33,028 hrs · 25,790 cycles

CLIPS CRACKED AT FS 280 ON LBL & RBL 9 FLOOR BEAMS. REMOVED CRACKED CLIPS, REPLACED WITH NEW SERVICEABLE ONES.

Part: SUPPORT BRACKET — CRACKED (CARGO DOOR) · airframe 33,028 hrs · 25,790 cycles

CARGO DOOR LOWER FWD TRACK SUPPORT BRACKET. R & R SUPPORT BRACKET.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,028 hrs · 25,790 cycles

SERVICE DOOR THRESHOLD CORRODED. REPLACED CORRODED THRESHOLD WITH NEW SERVICEABLE THRESHOLD IAW CRJ 200 SRM 51-40-11.

Part: MOUNT BRACKET — CRACKED (CARGO BAY) · airframe 33,028 hrs · 25,790 cycles

CARGO DOOR FWD UPPER MOUNT BRACKET CRACKED. REMOVED UNSERVICEABLE BRACKET & REPLACED WITH SERVICEABLE BRACKET.

Part: BULKHEAD — DENTED (FUSELAGE) · airframe 33,028 hrs · 25,790 cycles

BULKHEAD THREE DENTS IN SKIN JUST ABOVE FLOOR. 9 SALVATION DETERMINED MINOR DENTS, MEASURED WERE WITHIN SERVICEABLE LIMITS.

Part: SWITCH — OUT OF RIG (THRUST REVERSER) · airframe 24,329 hrs · 24,217 cycles

RIGHT THRUST REVERSER UNLOCK CAS MESSAGE AT FL 270, CRUISE POWER, YELLOW N1 ICON, DEPLOY / STOW POSITIONS NORMAL, COMPLIED WITH QRH, MESSAGE REMAINED TO GATE. FOUND RIGHT THRUST REVERER STOW SWITCH EXCESSIVELY OUT OF RIG IAW SUP 11-014. OPS CHECKED GOOD IAW AMM 78-37-01.

Part: FLEX HOSE — DAMAGED (HYDRAULIC SYS) · airframe 24,187 hrs · 24,084 cycles

HYD 1 LOW PRESS CAUTION-QTY READS DASHES.PSI FOR HYD 1 READS "00" ENGINE DRIVEN PUMP RAN DRY FOR 33 MIN IN FLIGHT. C/W QRH PER MX CONTROL DOCUMENTATION EDP WAS CHANGED AND IT APPEARS A FLEX HOSE WAS CHANGED AS WELL. LEAK CHECK WAS GOOD.

Part: CLAMP — LOOSE (ANTI-ICE VALVE) · airframe 23,094 hrs · 23,051 cycles

RIGHT 14TH STAGE DUCT RED WARNING DURING CLIMB AT 1000 FT. COMPLIED WITH QRH REDUCED THROTTLE WARNING EXTINGUISHED. SHOWED RED ON DUCT BETWEEN COWL ANTI-ICE VALVE AND WING ANTI-ICE VALVE. LANDING WT 46,800 NOT OVERWEIGHT. FOUND CLAMPS LOOSE ON RIGHT COWL ANTI-ICE VALVE TIGHTENED CLAMPS IAW 30-22-01 LEAK CHECK OPS CHECK GOOD. RAN RIGHT ENGINE AT HIGH POWER WITH DIFFERENT CONFIGS AT ANTI-ICE VALVES, NO WARNING MESSAGE NOTED.

Part: ENGINE — INOPERATIVE (APU) · airframe 28,532 hrs · 27,669 cycles

APU FAILED TO START, SMOKE COMING FROM INTAKE. OPEN

Part: FITTING — CHAFED (FLAP ROLLER) · airframe 28,288 hrs · 27,410 cycles

RT OTBD FLAP ROLLER FITTING CHAFED. REPAIRED IAW REO 601R-57-53-909.

Part: SEAT TRACK — WORN (COCKPIT) · airframe 28,249 hrs · 27,371 cycles

SEAT TRCK WORN . INSTALLED SERVICEABLE COCKPIT SEAT TRACK, IAW SRM 51-40-11.

Part: TRANSCOWL — CRACKED (RT LOWER) · airframe 28,288 hrs · 27,410 cycles

RT LOWER TRANS COWL UPPER FWD INTERLOCK FITTING IS CRACKED. R & R FITTING PN 228-50242-122 IAW SRM 51-42-14.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · corrosion level 2 · airframe 28,249 hrs · 27,371 cycles

LBL 27 FROM FS 574.00 TO FS 621.00 HAS CORROSION ON TOP CAP AND AROUND NUT PLATES INSTALLED SERVICEABLE TOP FLOORBEAM CAP ON LBL 27.0 FROM FS 574.00 TO FS 621.00 IAW SRM 51-42-06, 51-42-21, 51-41-02 & 51-21-16.

Part: SKIN — CRACKED (RT NOSE WW) · airframe 28,249 hrs · 27,371 cycles

RIGHT LOWER SKIN NOSE WHEEL CUTOUT AT CORNER IS CRACKED. C/W REO 601R-53-11-048, REV B.

Part: DOOR — CHAFED (LT MLG) · airframe 28,249 hrs · 27,371 cycles

LEFT MLG DOOR CHAFED AT L/E & T/E. REPAIRED IAW REO 601R-52-82-033 & SRM 52-82-00, 51-12-00.

Part: SILL — CORRODED (PAX DOORWAY) · airframe 28,249 hrs · 27,371 cycles

PAX DOOR SILL HAS FWD AND AFT CORRODED HANDRAIL BRACKETS REPAIRED IAW REO 601R-53-21-2242, REV A.

Part: LONGERON — CORRODED (BS 310-349) · airframe 28,288 hrs · 27,410 cycles

PAX DOOR LOWER SILL LONGERON CORRODED UNDER NUT PLATES FS 310 TO 349. R & R PAX DOOR LOWER SILL LONGERON.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 28,288 hrs · 27,410 cycles

RBL9 SEAT TRACK 5 & 6 CORRODED IN CARGO AREA. REMOVED UNSERVICEABLE SEAT TRACKS 5 & 6 RBL 9 IAW AMM 53-00-49 AND REPLACED WITH SERVICEABLE SEAT TRACKS 5 & 6, RBL 9 IAW AMM 53-00-49.

Part: SEAT TRACK — CORRODED (BS559.0) · airframe 28,288 hrs · 27,410 cycles

RBL 9 CARGO TRACK CORRODED. REMOVED UNSERVICEABLE CARGO TRACK IAW AMM 53-00-49 AND REPLACED IAW AMM 53-00-49.

Part: FASTENER — MISSING (ELEVATOR HINGE) · airframe 28,288 hrs · 27,410 cycles

LEFT CENTER PCU ATTACHING HINGE ON ELEVATOR HAS A MISSING RIVET. INSTALLED FASTENER IAW REO 601R-55-21-346.

Part: CHANNEL — CHAFED (TE FLAPS) · airframe 28,249 hrs · 27,371 cycles

RIGHT AND LEFT OTBD FLAP ROLLER CHANNELS ARE CHAFED. BLENDED RT AND LT OTBD FLAP ROLLER CHANNELS IAW SRM 51-12-06. RT CHANNEL OPENING GAUGE AT .800 AFTER BLEND .838, LT CHANNEL OPENING GAUGED .800 AFTER BLEND .838 REMAINING MATERIAL IS WITHIN SERVICEABLE LIMITS IAW REO 601R-57-51-143.

Part: SUPPORT BRACKET — CRACKED (LT OTBD FLAP) · airframe 28,288 hrs · 27,410 cycles

LT OTBD FLAP AT CENTER AFT FAIRING SUPPORT. FAIRING BRACKET IS CRACKED. R & R CRACKED FAIRING BRACKET IAW SRM 51-40-11 & 51-45-00.

Part: ACCESS PANEL — CHAFED (LT WING) · airframe 28,288 hrs · 27,410 cycles

LOWER WING CHAFED WHERE LT OTBD T/E, OF PANEL 193AB MEETS WING SURFACE, BLENDED IAW REO 601R-57-21-880.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 28,288 hrs · 27,410 cycles

RT INBD FLAP L/E CHAFED IN 3 PLACES. REPAIRED IAW REO 601R-57-52-004.

Part: CARGO TRACK — CORRODED (FS 559-605) · corrosion level 2 · airframe 28,288 hrs · 27,410 cycles

LBL 9 CARGO TRACK CORRODED. REMOVED CARGO TRACK AND INSTALLED NEW.

Part: SEAT TRACK — CORRODED (BS 559-605) · corrosion level 2 · airframe 28,288 hrs · 27,410 cycles

LBL9, SEAT TRACK CORRODED (CARGO AREA). REMOVED UNSERVICEABLE SEAT TRACK AND INSTALL SERVICEABLE SEAT TRACK.

Part: VANE — CHAFED (TE FLAP)

INBD FLAP VANE L/E SKIN CHAFED OUT OF ALLOWABLE LIMITS IAW REO 61R-57-52-004. REPLACED L/E SKIN WITH NEW PN 601R14303-53S.

Part: BEARING — LOOSE (ELEVATOR HINGE) · airframe 28,288 hrs · 27,410 cycles

LT ELEVATOR NR1 HINGE SPHERICAL BEARING LOOSE. REMOVED UNSERVICEABLE HINGE FITTING AND INSTALLED SERVICEABLE HING FITTING ON LT ELEVATOR IAW SRM 51-42-06/ 51-42-21.

Part: STRIKER — CHAFED (PAX DOOR) · airframe 28,249 hrs · 27,371 cycles

PAX DOOR FWD AND AFT STRIKER PLATES CHAFED. BLENDED FWD AND AFT STRIKER PLATES IAW REO 601R-52-11-196, FWD STRIKER PLATE REMOVED .013, REMOVED .011 OF MAT ON AFT STRIKER PLATE MAX ALLOWED 040 REMAINING MAT IS WITHIN SERVICEABLE LIMITS IAW REO 601R-52-11-296.

Part: BRACKET — CORRODED (DOOR SILL) · airframe 28,288 hrs · 27,410 cycles

PAX DOOR LOWER SILL CONNECTOR PLUG BRACKETS CORRODED AT PLUGS JIMB AND J2M8. REMOVED AND REPLACED BRACKET.

Part: SILL — CORRODED (SERVICE DOORWAY) · airframe 28,249 hrs · 27,371 cycles

SERVICE DOOR LOWER SILL HAS CORROSION AT FWD END BLENDED MINOR SERVICE CORROSION IAW SRM 51-21-06. REMOVED .003, ORIGINAL THICKNESS .063 REMAINING MATERIAL .060 REMAINING MAT IS WITHIN SERVICEABLE LIMITS IAW SRM 51-21-06.

Part: SKIN — DENTED (THRUST REVERSER) · airframe 28,249 hrs · 27,371 cycles

LT LOWER TRANS COWL 434AB HAS APPPROX 1" DENT ON OUTER SURFACE. REPAIRED LT LOWER TRANS COWL OUTER SKIN IAW CMM 78-30-00.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 28,249 hrs · 27,371 cycles

RBL 9 OTBD 280 FLOORBEAM TEE CRACKED. R & R FLOORBEAM TEE

Part: HINGE FITTING — GOUGED (HORIZONTAL STAB) · airframe 28,249 hrs · 27,371 cycles

RT HORIZONTAL STAB NR 2 HINGE FITTING GOUGED. BLENDED IAW REO 601R-55-21-080.

Part: ANGLE — CRACKED (FS 625) · airframe 28,249 hrs · 27,371 cycles

LEFT FS 625.00 OBLIQUE ANGLE CRACKED. REMOVED UNSERVICEABLE OBLIQUE ANGLE AT LT FS 625.00 AND INSTALLED SERVICEABLE OBLIQUE ANGLE PN 601-35012-51 IAW AWAC SRM 51-42-21, SRM 51-40-11, SRM 51-21-11, SRM 51-25-16 AND REO 601R-53-61-422.

Part: HINGE FITTING — GOUGED (HORIZONTAL STAB) · airframe 28,249 hrs · 27,371 cycles

LEFT HORIZONTAL STAB NR 2 HINGE FITTING GOUGED. BLENDED IAW REO 601R-55-21-080.

Part: STRUCTURE — CHAFED (RT NACELLE) · airframe 28,249 hrs · 27,371 cycles

RT UPPER NOSE COWL AFT EDGE STRIP IS CHAFED. R & R RT UPPOER NOSE COWL AFT EDGE STRIP IAW CMM 71-14-01-300-814-A01.

Part: CONTROL WHEEL — BINDING (AILERONS) · airframe 25,599 hrs · 24,597 cycles

ON LANDING FELT AILERONS BINDING (HARD TO MOVE) AND DURING POST FLIGHT AILERON CHECK A MECHANICAL RATCHETING CAN BE FELT IN BOTH CONTROL WHEELS. R & R CAPTS CONTROL WHEEL SHAFT FWD AND AFT BEARINGS IAW AMM CH 27-11-01.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 25,599 hrs · 24,597 cycles

ON TAKEOFF, GOT STRONG ODOR IN FLT DECK AND CABIN. THEN GOT STAB TRIM AND MACH TRIM CAUTION MESSAGES. C/W QRH, MESSAGES AND ODOR WENT AWAY. ODOR WAS ELECTRICAL IN NATURE. REPLACED CAPT YOKE HORIZ STAB PITCH TRIM SWITCH AND COFFEE MAKER, HORIZ STAB TRIM SYS OPS CHECK GOOD IAW AMM 27-40-.

Part: SEAT — DISLODGED (CABIN) · airframe 25,000 hrs · 23,979 cycles

SEAT 9D AND 9F CAME OUT OF THE SIDE WALL TRACK. RESECURED SEAT ASSY AT 9DF FOUND WALL BOLT NUT IN PLACE.

Part: ACTUATOR — BINDING (AILERONS) · airframe 24,636 hrs · 23,596 cycles

DURING APPR F/O FELT BINDING IN AILERONS (BOTH LT AND RT) UPON LANDING, PERFORMED AILERON CHECK AND FELT BINDIING IN BOTH DIRECTIONS ON BOTH SIDES. R & R AILERON TRIM ACTUATOR IAW AMM 27-12-01. OPS TEST GOOD.

Part: WARNING MESSAGE — ILLUMINATED (ANTI ICE DUCT) · airframe 24,235 hrs · 23,172 cycles

ANTI-ICE DUCT WARN MSG IN FLIGHT, COMPLIED WITH QRH, MESSAGE CLEARED. R & R DUCT ASSY.

Part: UNKNOWN — ODOR (CABIN) · airframe 24,214 hrs · 23,146 cycles

FUEL SMELL AFTER DEPARTURE. INSPECTED APU FUEL SYS FOR POSSIBLE LEAKS, ALSO EXTERNAL FUEL DRAINS NO LEAKS NOTED. STARTED APU AND BOTH ENGINES NO EVIDENCE OF FUEL SMELL THROUGH THE PACKS, OK TO CONTINUE SERVICE IAW AMM 49-10-00 AND AMM 21-50-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,916 hrs · 22,850 cycles

RT NR 3 SEAT TRACK CORRODED BS 409+128. REMOVED AND REPLACED SEAT TRACK.

Part: ATTACH ANGLE — CRACKED (FUSELAGE)

CARGO DOOR FWD ROLLER TRACK LWR ATTACH ANGLE CRACKED. REMOVED DAMAGED CHANNEL, DUPLICATED SERVICABLE CHANNEL, AND INSTALLED SERVICE CHANNEL IAW SRM 51-42-06.

Part: BULKHEAD — DAMAGED (BS 559) · airframe 23,916 hrs · 22,850 cycles

BULKHEAD REPAIRED FS 559 LT & RT IAW REO 601R-53-41-609 AND REO 601R-53-41-260.

Part: ARM — GOUGED (LT WING) · airframe 23,916 hrs · 22,850 cycles

LT INBD FLAP OTBD HINGE ARM HAS DAMAGE ON L/E FWD LOWEST ATTACH POINT. REPAIRED GOUGE IAW REO 601R-57-54-158.

Part: FITTING — GOUGED (RT WING) · airframe 23,916 hrs · 22,850 cycles

RT WING OTBD FLAP OTBD AFT HINGE BOX FILLING ON A/C GOUGED. REPAIRED GOUGE IAW REO 601R-57-54-157.

Part: SEAT TRACK — CORRODED (BS 409) · corrosion level 2 · airframe 23,916 hrs · 22,850 cycles

RT NR 2 FLOOR SEAT TRACK CORRODED BEYOND LIMITS REQUIRES REPLACEMENT. REPLACED RT NR 2 FLOOR SEAT TRACK.

Part: LINK — INTERFERENCE (BS 513) · airframe 23,916 hrs · 22,850 cycles

LT AND RT 513 DOGBONE LINKS TOUCHING. INSP AND DEFERRED IAW REO 601R-53-41-1148 5000 HR PERM REPAIR 1000 HR REINSPECT.

Part: TUBE — CHAFED (RT WING TE FLAP) · airframe 23,916 hrs · 22,850 cycles

RT INBD FLAP MIDDLE VANE ACTUATOR INNER TUBE WORN UNDER BOTTOM ROLLER. REPAIRED IAW REO 601R-57-52-1552.

Part: TUBE — CHAFED (FLAP VANE) · airframe 23,916 hrs · 22,850 cycles

RT INBD FLAP INBD VANE ACTUATOR INNER TUBE WORN UNDER BOTTOM ROLLER. REPAIRED IAW REO 601R-57-52-1557.

Part: ANGLE — CRACKED (RT WING LE) · airframe 23,976 hrs · 22,850 cycles

RT MIDDLE WING L/E. INBD ATTACH ANGLE IS CRACKED. REPLACED ANGLE PN 600-12025-8 IAW SRM 51-41-02, 51-40-11.

Part: FRAME — CRACKED (PAX DOOR) · airframe 23,916 hrs · 22,850 cycles

PAX DOOR FRAME UPPER FLANGE AT FS 338 CRACKED. REPAIRED IAW REO 601R-52-11-402.

Part: BRACKET — BROKEN (LT FIRE LOOP) · airframe 23,916 hrs · 22,850 cycles

LT JET PIPE FIRE LOOP MOUNT COVER FWD MOUNT STANDOFF BRACKET BROKEN. REMOVED BROKEN BRACKET AND REPALCED WITH FABRICATED BRACKET.

Part: DOOR — CRACKED (APU) · airframe 23,916 hrs · 22,850 cycles

APU ENCLOSURE DOOR CRACKED TOP CENTER AS MARKED. REPAIRED 3 EA CRACKS IAW REO 601R-49-11-070.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 23,916 hrs · 22,850 cycles

RT INBD WING L/E, OTBD ATTACH ANGLE IS CRACKED. REMOVED DAMAGED RT INBD WING L/E OTBD ATTACH ANGLE PN 600-12045-12.

Part: ANGLE — CRACKED (LT WING) · airframe 23,916 hrs · 22,850 cycles

LT WING CTR L/E INBD ATTACH ANGLE CRACKED. REMOVED DAMAGED ANGLE, LOCATED FASTENER HOLES IN SERVICEABLE ANGLE AND INSTALLED SERVICEABLE ANGLE IAW SRM 51-41-02.

Part: ANGLE — CRACKED (BS 621) · airframe 23,916 hrs · 22,850 cycles

INTERCOSTAL ATTACH ANGLE ABOVE LINTEL FITTING ON AFT SIDE OF F/S 621 IS CRACKED. R & R IAW SRM 51-40-00, 53-61-19.

Part: PRESSURE BLKHD — CHAFED (BS 621) · airframe 23,916 hrs · 22,850 cycles

10TH STAGE BLEED AIR SHUTOFF VALVE ABOVE APU ENCLOSURE CHAFING CTR BEAM. REO 601R-53-61-1523 BLEND EDDY CURRENT INSPECT TREAT PRIME AND TOP COAT.

Part: SEAT TRACK — CORRODED (BS 364) · airframe 23,916 hrs · 22,850 cycles

LT NR 1 FLOOR SEAT TRACK CORRODED. R & R SEAT TRACK.

Part: SEAT TRACK — CORRODED (BS 364) · corrosion level 2 · airframe 23,916 hrs · 22,850 cycles

RT FLOOR SEAT TRACK CORRODED, R & R TRACK.

Part: ANGLE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 23,916 hrs · 22,850 cycles

PAX DOOR AFT CORNER HAS CORROSION. R & R UPPER AND LOWER ANGLES.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 23,916 hrs · 22,850 cycles

PAX DOOR FWD LOWER CORNER HAS A CRQCKED INTERCOSTAL. DUPLICATED ORIGINAL PART IAW SRM 51-24-21.

Part: ATTACH FITTING — CORRODED (PAX DOOR) · corrosion level 2 · airframe 23,916 hrs · 22,850 cycles

PAX DOOR LOWER AFT SIDE AT F/S 329.50 HAS CORROSION ON CLIP. REMOVED OLD CLIP AND FABRICATED NEW CLIP IAW SRM 51-31-59.

Part: ATTACH FITTING — CORRODED (PAX DOOR) · corrosion level 2 · airframe 23,916 hrs · 22,850 cycles

PAX DOOR LOWER AFT SIDE AT F/S 320.10 HAS CORROSION ON CLIP. REMOVED OLD CLIP AND FABRICATED NEW CLIP IAW SRM 51-31-59.

Part: ATTACH FITTING — CORRODED (PAX DOOR) · corrosion level 2 · airframe 23,916 hrs · 22,850 cycles

PAX DOOR LOWER FWD SIDE AT F/S 320.10 HAS CORROSION CLIP. REMOVED CORRODED CLIP, FABRICATED NEW CLIP IAW SRM 51-31-59.

Part: ATTACH FITTING — CORRODED (PAX DOOR) · corrosion level 2 · airframe 23,916 hrs · 22,850 cycles

PAX DOOR LOWER AFT AT F/S 338.0 JAS CORROSION ON CLIP. REMOVED OLD CLIP, FABRICATED NEW CLIP IAW SRM 51-31-59.

Part: ATTACH FITTING — CORRODED (PAX DOOR) · corrosion level 2 · airframe 23,916 hrs · 22,850 cycles

PAX DOOR LOWER FWD AT FS 338.00 HAS CORROSION ON CLIP. REMOVED OLD CLIP AND FABRICATED NEW CLIP IAW SRM 51-31-54.

Part: BRACKET — CRACKED (EXHAUST) · airframe 23,916 hrs · 22,850 cycles

LT JETPIPE UPPER INBD ATTACH POINT NUTPLATE BRACKET CRACKED. REMOVED DAMAGED BRACKET, DUPLICATED SERVICEABLE BRACKET IAW CMM 78-11-00, AND INSTALLED SERVICEABLE BRACKET IAW CMM 20-42-06.

Part: BRACKET — CRACKED (VERTICAL STAB) · airframe 23,916 hrs · 22,850 cycles

NUT BRACKET UNDER PANEL 326CL, LT SIDE OF VERTICAL STAB, CRACKED. REMOVED DAMAGED BRACKET AND INSTALLED SERVICEABLE PN 600-21137-5 BRACKET.

Part: DRAG ANGLE — DAMAGED (TAILCONE) · airframe 22,614 hrs · 21,544 cycles

MWC 137953-7 - FOUR FWD MISALIGNED BOLT HOLES ON LT AND RT TAILCONE DRAG ANGLES. TRIMMED DRAG ANGLES, FABRICATED AND INSTALLED FILLERS AND REPAIR ANGLES IAW EO 601R-53-16986. (K)

Part: WHEEL — CRACKED (MLG) · airframe 22,468 hrs · 21,400 cycles

191210/3 - MAIN TIRE NR 1 FLAT, TIRE WAS NORMAL ON POST FLIGHT WALKAROUND, AGENT FOUND TIRE FLAT PRIOR TO PUSHBACK. WHEEL RIM NR 1 FOUND CRACKED. REMOVED AND REPLACED MAIN TIRE ASSEMBLIES NR 1 AND NR 2. MLG WHEEL ASSY, NR 1 PN 5010571-1, SN DEC03-6173, TSN=8732, CSN=8243 - MLG WHEEL ASSY NR 2 PN 5010571-1, SN OCT01-4370, TSN=233, CSN 220.

Part: DUCT — LEAKING (RT A/C PACK) · airframe 21,824 hrs · 20,791 cycles

LOG 188027/2- AFTER CLIMBOUT RT PACK OVERPRESSURE. COMPLIED WITH QRH. PERFORMED AIR RETURN TO DEPARTURE. REMOVED AND REPLACED LT DUCT ASSY IAW AMM 21-51-15. OPS AND LEAK CHECK GOOD AT THIS TIME. REMOVED PLACARD, REMOVED FROM MEL. (K)

Part: UNKNOWN — ODOR (CABIN) · airframe 21,686 hrs · 20,658 cycles

LOG 188020/1 STRONG ODOR IN CABIN AND COCKPIT WITH APU AND ENGINE AIR SELECTED ON. DOES NOT DISSIPATE.

Part: SCREEN — COKED (SCAVE PUMP) · airframe 21,636 hrs · 20,615 cycles

RT ENGINE OIL PRESSURE WARNING MSG AT CRUISE. WARNING PERSISTED AT POWER SETTINGS ABOVE IDLE. CW QRH DIVERTED TO PHL. ENGINE REMAINED AT IDLE DURING THE 40 MINUTE FLIGHT TO PHL. LOWEST OIL PRESSURE SHOWN WAS 24 PSI. REMOVED RT LUBE SCAVENGE PUMP AND FOUND SCREENS COKED UP CAUSING RESTRICTING. CLEANED SCREEN IAW EO8/016/479 AND REINSTALLED PUMP IAW AMM 79-21-01 OPS AND LEAK CHECK GOOD.

Part: CARBON SEAL — LEAKING (RT ENGINE) · airframe 20,770 hrs · 19,788 cycles

IN FLIGHT RT ENG OIL PRESSURE FLUCTUATED BETWEEN 30-45 PSI. ON SHORT FINAL RECEIVED "RT ENG OIL PRESSURE" WARNING MESSAGE, PRESSURE FLUCTUATED BETWEEN 23-33 PSI. ALSO, RECEIVED AURAL "ENG OIL" WARNING. REMOVED AND REPLACED RT ENG INTEGRATED DRIVE GENERATOR CARBON SEAL. (S)

Part: PLATE — CORRODED (SERVICE DOOR) · corrosion level 1 · airframe 19,120 hrs · 18,245 cycles

SERVICE DOOR PLATE FIND CORRODED, OUT OF LIMITS IAW SRM 53-00-00, FIG 101. SERVICE DOOR PLATE REPLACED IAW SRM 51-42-00, 51-41-02, 51-41-04. (K)

Part: BRACKET — CRACKED (CARGO DOOR) · airframe 19,120 hrs · 18,245 cycles

CARGO DOOR CONNECTOR BRACKET CRACKED. (K) CARGO DOOR CONNECTOR BRACKET FABRICATED AND INSTALLED IAW SRM 51-24-15 AND 51-42-06.

Part: NUT CLIP — CRACKED (BS 484) · airframe 19,120 hrs · 18,245 cycles

FS 484.0 RT SIDE, CLIP FOUND CRACKED ON FLOOR SUPPORT STRUCTURE AT RBL 27.0, FS 484.00, RBL 27.00, FLOOR SUPPORT CLIP REPLACED IAW SRM 51-42-16, 51-21-16 AND SRM 51-42-06. (K)

Part: BULKHEAD — CRACKED (BS 202) · airframe 19,120 hrs · 18,245 cycles

CRACK ON FWD PRESSURE BULKHEAD AROUND PARKING BRAKE AT FS 202.00 LT LBL 23.00. CRACK ON FWD PRESSURE BULKHEAD AROUND PARKING BRAKE REPAIRED IAW REO 601R53-11-563. (K)

Part: DIAPHRAGM — CRACKED (PAX DOOR) · airframe 19,120 hrs · 18,245 cycles

DIAPHRAGM CRACK UNDER FWD UPPER PAX DOOR CORNER COVER. (K) BRACKET CRACKED UNDER FWD UPPER PAX DOOR CORNER COVER REPLACED IAW SRM 51-42-06.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 19,120 hrs · 18,245 cycles

BRACKET CRACK ON LOWER PAX DOOR EDGE (LOCK MECHANISM AREA) AFT STA 334.00. CRACKED BRACKET ON PAX DOOR BTW FS 329.5 TO FS 338.0 IS REPLACED IAW SRM 51-41-04. (K)

Part: FLOOR PANEL — CORRODED (BS 280) · corrosion level 1 · airframe 19,120 hrs · 18,245 cycles

CORROSION EXIST ON FLOOR STRUCTURE FS 280, LBL 9 TO RBL 9. PERFORMED ON FLOOR STRUCTURE FS 280, LBL 9 TO RBL 9 IAW REO 601R-53-11-926. (K)

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 19,120 hrs · 18,245 cycles

CRACK FOUND ON INTERCOSTAL FS 484, LBL 27 AND LBL 36, WL 72.00. INTERCOSTAL AT FS 484, LBL 27 AND LBL 36 AT WL 72.00. REPAIRED IAW REO 601R-53-41-059 REV A AND SRM 51-24-16, 51-21-16 AND SRM 51-42-06. (K)

Part: COVER — CRACKED (PAX DOOR) · airframe 19,120 hrs · 18,245 cycles

AFT UPPER CORNER COVER CRACK ON PAX DOOR. (K) AFT UPPER CORNER COVER REPLACED IAW SRM 51-42-13. (K)

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 19,120 hrs · 18,245 cycles

EDGE MEMBER CRACK ON PAX DOOR AT FOLDING STEP HINGE. (K) PAX DOOR EDGE MEMBER FABRICATED IAW SRM 51-24-26 AND INSTALL IAW SRM 51-42-13.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 19,120 hrs · 18,245 cycles

CRACK SUSPECTED ON AC CONNECTOR BOX. CRACK CONFIRMED BY EDDY CURRENT INSPECTION. INTERCOSTAL AND RECEPTACLE SUPPORT REPLACED IAW SRM 51-42-06. (K)

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 19,120 hrs · 18,245 cycles

CRACK FOUND ON AFT ATTACH ANGLE OF PAX DOOR (DRAG ANGLE). AFT ATTACH ANGLE OF PAX DOOR REPAIRED IAW REO 61R-52-11-513 REV A. (K)

Part: SUPPORT BRACKET — CRACKED (BS 718) · airframe 19,120 hrs · 18,245 cycles

RT HYDRAULIC SUPPORT BRACKET AT FS 718 IS CRACKED. RT HYDRAULIC SUPPORT BRACKET AF FS 718 IS CRACKED. (K)

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 19,120 hrs · 18,245 cycles

FWD UPPER CORNER COVER CRACK ON PAX DOOR. (K) FWD UPPER CORNER COVER OF PAX DOOR REPLACED IAW SRM 51-42-13.

Part: SKIN — DAMAGED (MLG DOOR)

ON MLG DOOR RIGHT INNER SKIN, ABRASION EXIST ON FORWARD SIDE OF DOOR, LOWER AND UPPER. (M) REPAIRED IAW REO 601R-52-82-016 AND REO 601R-52-82-102. (K)

Part: SKIN — DAMAGED (LT MLG DOOR) · airframe 19,120 hrs · 18,245 cycles

ON LT MLG DOOR INNER SKIN, FOUND ABRASION ON FORWARD SIDE OF DOOR, LOWER AND UPPER. (M) REPAIRED IAW REO 601R-52-82-016 AND REO 601R-52-82-102. (K)

Part: STRUCTURE — GOUGED (PAX DOOR) · airframe 19,120 hrs · 18,245 cycles

FWD PAX DOOR PULL IN LEVEL GOUGED PULL IN LEVEL GOUGED .070 INCH AND ALLOWABLE MAXIMUM .050 INCH IAW REO 601R-52-11-524. (K) FWD PAX DOOR PULL IN LEVER REPAIRED IAW REO 601R-52-11-524.

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 19,120 hrs · 18,245 cycles

LT INTERCOSTAL CLIP AT FS 621.0 TO FS 625.0 IS CRACKED. INTERCOSTAL CLIP AT FS 621.0 TO FS 625.0 LT REPLACED IAW SRM 51-42-20. (K)

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 8,681 hrs · 7,865 cycles

RT FS 625 OBLIQUE ANGLE IS CRACKED APPROX 1 INCH L. MAINTENANCE REMOVED AND REPLACED ANGLE IAW SRM 51-42-21 AND REO 601R-53-61-422. (K)

Part: SKIN — GROUND DAMAGE (BS 615) · airframe 17,366 hrs · 16,533 cycles

LAV TRUCK HIT AC - 4 INCH HOLE IN FUSELAGE FS 615, WL 73. MAINTENANCE PERFORMED A MAJOR REPAIR BY CUTTING AWAY DAMAGED SKIN AND INSTALLING A 14 INCH X 8 INCH EXTERNAL REPAIR DOUBLER IAW EO 601R-11202. (K)

Part: SKIN — CORRODED (KT WING) · corrosion level 1 · airframe 14,440 hrs · 13,718 cycles

LT LOWER WING PLANK HOLE NR 7, WS 166.366 HAS CORROSION ON IB SIDE 4 INCH L X .002 INCH D. NOT IN CRITICAL AREA. MAINTENANCE REPAIRED LT WING PLANK ACCESS HOLE NR 7 IAW REO. (K)

Part: SKIN — CORRODED (LT WING) · corrosion level 1 · airframe 14,440 hrs · 13,718 cycles

LT LWR WING PLANK HOLE NR 2, WS 12.245 HAS CORROSION AT OB SIDE AFT 2 INCH L X .005 INCH D AND AT IB SIDE 8 INCHES L X .005 INCH D. NOT IN CRITICAL AREA. MAINTENANCE REPAIRED LT WING LOWER PLANK ACCESS HOLE NR 2 IAW REO. (K)

Part: SKIN — CORRODED (RT WING) · corrosion level 1 · airframe 14,440 hrs · 13,718 cycles

RT WING LOWER PLANK HOLE NR 16, WS 303.861 HAS CORROSION AT IB SIDE 1 INCH L X .005 INCH D. NOT CRITICAL. MAINTENANCE REPAIRED RT LWR WING PLANK ACCESS HOLE NR 16 IAW REO. (K)

Part: CLIP — CRACKED (FUSELAGE) · airframe 14,440 hrs · 13,718 cycles

FS280 FRAME CLIP AT RBL 9 ON OB SIDE IS CRACKED. MAINTENANCE REPLACED CLIP (PN 601R3111358) IAW SRM. (K)

Part: SKIN — CORRODED (LT WING) · corrosion level 1 · airframe 14,440 hrs · 13,718 cycles

LT WING LOWER PLANK HOLE NR4, WS 54.681 HAS CORROSION AT OB SIDE 5 INCH L X .002 INCH D AND AT IB SIDE 5 INCH L X .002 INCH D. NOT IN CRITICAL AREA. MAINTENANCE REPAIRED LT WING LOWER PLANK ACCESS HOLE NR 4 AT WS 54.681 IAW REO. (K)

Part: SKIN — CORRODED (RT WING) · airframe 14,440 hrs · 13,718 cycles

RT WING LOWER PLANK HOLE NR 5 WS 76.161 HAS CORROSION AT IB FORWARD SIDE 4 INCHES L X .002 INCH D. NOT IN CRITICAL AREA. MAINTENANCE REPAIRED RT WING LOWER WING PLANK ACCESS HOLE NR 5 IAW REO. (K)

Part: COVER — CRACKED (PAX DOOR) · airframe 14,440 hrs · 13,718 cycles

PASSENGER DOOR UPPER FORWARD CORNER CAP IS CRACKED. MAINTENANCE REPAIRED PASSENGER DOOR UPPER FWD CORNER CAP IAW REPAIR BY INSTALLING NEW COVER PN 6003190278. (K)

Part: SKIN — CORRODED (RT WING) · corrosion level 1 · airframe 14,440 hrs · 13,718 cycles

RT WING LWR PLANK HOLE NR 7, WS 116.366 HAS CORROSION AT IB SIDE 2 INCHES L X .005 INCH DEEP AND FWD SIDE .5 INCH L X .005 INCH D, NOT IN CRITICAL AREA. MAINTENANCE REPAIRED RT LWR WING PLANK ACCESS HOLE NR 7 IAW REO. (K)

Part: SKIN — CORRODED (LT WING) · corrosion level 1 · airframe 14,440 hrs · 13,718 cycles

LT LOWER WING PLANK HOLE NR 1, WS 54.897 HAS CORROSION AT IB SIDE FORWARD EDGE 2 INCH L .005 INCH D AND AT OB SIDE AFT 4 INCH L X .005 INCH D. NOT IN CRITICAL AREA. MAINT REPAIRED LT LOWER WING PLANK ACCESS HOLE NR 1 IAW REO. (K)

Part: CLIP — CRACKED (FUSELAGE) · airframe 14,440 hrs · 13,718 cycles

FS 280 FRAME CLIP AT LBL 9 IB IS CRACKED. MAINTENANCE REPLACED CLIP PN 601R3111357 IAW SRM. (K)

Part: CLIP — CRACKED (FUSELAGE) · airframe 14,440 hrs · 13,718 cycles

FS 280 FRAME CLIP AT LBL 9 OB IS CRACKED. MAINTENANCE REPLACED CLIP (PN 601R3111357) IAW SRM. (K)

Part: HANDLE — OUT OF POSITION (ESCAPE HATCH) · airframe 7,202 hrs · 7,321 cycles

CREW ESCAPE HATCH OUTER HANDLE STICKS IN THE CLOSED POSITION. CLEANED AND LUBRICATED OUTER HANDLE MECHANISM IAW AMM. (K)

Part: ANGLE — CRACKED (BS 625) · airframe 14,440 hrs · 13,718 cycles

LT FS 625 OBLIQUE ANGLE IS CRACKED. MAINTENANCE REMOVED AND REPLACED OBLIQUE ANGLE LT SIDE PH 601R-35012-51 IAW CRJ 200 SRM 51-42-06. (K)

Part: RIB — CRACKED (LT WING) · airframe 14,440 hrs · 13,718 cycles

LT BATT RIB ASSY AT WS 53.60, FS 523.8 CRACKED 1 INCH RADIUS MAINTENANCE REPAIRED BATT RIB ASSY IAW REO. (K)

Part: RIB — CRACKED (RT WING) · airframe 14,440 hrs · 13,718 cycles

RT BAH RIB ASSY WS 53.60, FS 523.8 CRACKED 1 INCH IN RADIUS. MAINTENANCE REPAIRED RT BAH RIB ASSY IAW REO. (K)

Part: WINDSHIELD — CRACKED (COCKPIT)

CAPTAINS WINDSCREEN CRACKED AT 32 FL FOLLOWED QUICK REFERENCE HANDBOOK AND DECLARED EMERGENCY. DIVERTED TO BUFFALO, NO SIGNS OF CRACKING ON INSIDE OR OUTSIDE OF WINDSCREEN. REMOVED AND REPLACED CAPTAINS WINDSCREEN. OPS AND LEAK CHECK GOOD REFERENCE CHAPTER 56-11-01. (M)

Part: COMPRESSOR — VIBRATION (ENGINE) · airframe 12,279 hrs · 11,755 cycles

RETURNED TO DEPARTURE, DUE TO HIGH N1 FAN VIBRATION 2.8 IN CLIMB POWER SET ITT AND N1 NORMAL. INSPECTED NR 2 ENGINE INLET FAN BLADES, EXHAUST AND CHIP DETECTORS. NO DEFECTS FOUND. GROUND RAN ENGINE VIBRATION .8 MILS WITHIN LIMITS REF CF34 ENG MANUAL 72-00-00, TESTING 01 PAGE 1325 AND 1326. (M)

Part: FUEL BOWL — CONTAMINATED (RT ENGINE)

ON APPROACH, RT ENG RED OIL PRESSURE WARNING MESSAGE. ENGINE FLAMED OUT C/W QRH, ENG WINDMILLED FOR 3 MINUTES. FOUND WATER IN RT ENG FUEL BOWL. ALL INSPECTION AND CHECKS GOOD EXCEPT FOR WATER IN BOWL IAW 769-10-00 AND 73-11-03.

Part: BUSHING — WORN (MLG TRUNNION) · airframe 10,717 hrs · 10,401 cycles

MUC 44 LT MAIN LANDING GEAR AFT TRUNNION BUSHING IS MIGRATED .020. REMOVED AND REPLACED LT MAIN LANDING GEAR AFT TRUNNION BUSHING IAW MFG REO 601R5721003 REV B.

Part: FRAME — CRACKED (FUSELAGE)

RT 718 FRAME FLANGE BETWEEN STRINGERS 11 AND 12 IS CRACKED. REPAIRED RT 718 LOWER FRAME FLANGE AT STRINGERS 11 AND 12 IAW MFG REO 601R-53-61-193 REV A.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 10,717 hrs · 10,401 cycles

CLIP ANGLE AT FS 280.0 IB SIDE OF RBL 9 IS CRACKED. REMOVED CRACKED ANGLE AND INSTALLED NEW ANGLE PN 601R31113-58 IAW CRJ SRM 51-42-06 AND 51-42-21.

Part: WINDOW — FAILED (COCKPIT)

AT 33,000 FEET, LEFT SIDE WINDOW SHATTERED 'PRESSURIZATION SPIKED DOWN 500 FEET THEN STABILIZED. AIRCRAFT EN ROUTE FROM ICT TO ATL. REMOVED AND REPLACED LEFT SIDE WINDOW PER AMM 56-12-01. (M)

Part: WARNING LIGHT — FALSE ACTIVATION (A/C PACK)

RIGHT PACK HI PRESSURE CAUTION MESSAGE. PERFORMED PACK OPS CHECK WITH ENGINES IAW AMM 21-50-863-805 AND PERFORMED OPS CHECK IAW AMM 21-50-863-801. OPS CHECK GOOD. OK FOR SERVICE. (M)

Part: WARNING LIGHT — FALSE INDICATION (APU)

ABORTED TAKEOFF AT 100 KNOTS DUE TO APU WARNING (HI-TEMP) TEMP 999 DEGREES FOLLOWED BY AMBER CAS MESSAGE APU OIL PRESSURE. NORMAL BRAKING APPLIED. INSPECTED APU, NO VISUAL SIGNS ON APU FIRE. INSPECTED TAILPIPE, NO EVIDENCE OF APU DAMAGE, COMPLIED WITH RTO INSPECTION IAW 05-51-27, NO DEFECTS MEL'D APU. (M)

Part: ODOR — DETECTED (CABIN)

STRONG BURNING SULFUR ODOR IN FLIGHT. COMPLIED WITH PACK BURN OUT PROCEDURE. NO SMELLS OR DEFECTS NOTED AT THIS TIME. INSPECTED AVIONICS AND APU BAY, NO DEFECTS NOTED. AIRCRAFT OK FOR CONTINUED SERVICE. (M)

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY)

CARGO SMOKE MESSAGE INTERMITTENT DURING FLIGHT AT 20,000 FT COMPLIED WITH EMERGENCY ACTION CHECKLIST. REMOVED AND REPLACED NR 2 FIRE BOTTLE (REF BLK 2) SEE 116092/2 FOR MEL. FIRE DEPARTMENT FOUND NO EVIDENCE OF SMOKE OR FUMES. SMOKE DETECTION SYSTEM, OPS TEST GOOD AT THIS TIME. (M)

Part: STRUT — LOW (NLG)

RECEIVED NOSE GEAR OPEN WARNING IN FLIGHT AND GEAR DISAGREE MESSAGE IN FLIGHT. SERVICED STRUT. (M)

Part: UPLOCK SENSOR — MALFUNCTIONED (NLG)

AFTER TAKEOFF WITH GEAR HANDLE UP, GEAR UP DISAGREE AND NOSE DOOR OPEN MESSAGES ILLUMINATED. REMOVED AND REPLACED NOSE LANDING GEAR UPLOCK SENSOR. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

DURING BRIDGING INSPECTION, FOUND RIGHT HAND SIDE CARGO FLOOR SUPPORT ANGLE IS CRACKED AT FS 621.00.

Part: ANGLE — CRACKED (FUSELAGE)

DURING BRIDGING INSPECTION DISCOVERED RIGHT UPPER OBLIQUE ANGLE CRACKED IN RADIUS 1.0 INCH AT FS 621-625.3.

Part: FRAME — CRACKED (FUSELAGE)

LEFT FS 718.0 FRAME IS CRACKED AT STRINGER 11L, CRACK IS .5 INCH LONG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

DURING BRIDGING INSPECTION DISCOVERED FLOOR SUPPORT ANGLE AT FS 484, LBL27, WL73.1 CRACKED.

Part: FRAME — CRACKED (FUSELAGE)

DURING BRIDGING INSPECTION DISCOVERED LEFT FS 718 FRAME CRACKED AT STRINGER 11L, .5 INCHES LONG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

DURING BRIDGING INSPECTION FOUND LEFT HAND SIDE CARGO FLOOR SUPPORT ANGLE IS CRACKED AT FS621.00.

Part: SKIN — NICKED (FUSELAGE)

DURING BRIDGING INSPECTION, FOUND NICK IN SKIN BELOW CARGO DOOR, FS 605.00 WL 89.00.

Part: SKIN — DENTED (FUSELAGE)

DURING BRIDGING INSPECTION, FOUND DENT IN FUSELAGE AT FS 605.00, WL 86, .010 DEEP BY 1 INCH LONG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

DURING BRIDGING INSPECTION DISCOVERED FLOOR SUPPORT ANGLE AT FS484, LBL34, WL73.1 CRACKED.

Part: ENGINE — MALFUNCTIONED (RIGHT)

AIRCRAFT DEPARTED GJT. WHEN THE ENGINE BLEEDS WERE SELECTED ON, THE CABIN AND COCKPIT BEGAN TO FILL WITH SMOKE. THE AIRCRAFT RETURNED TO GJT. AFTER TROUBLESHOOTING AND A TEST FLIGHT, IT WAS DETERMINED THE NR 2 ENGINE WAS LEAKING OIL INTERNALLY INTO THE BLEED AIR SYSTEM. THE TURBOMACHINE WAS REPLACED. GROUND RUNS AND ANOTHER TEST FLIGHT WERE PERFORMED WITH NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: WINDOW — CRACKED (LT COCKPIT)

DEN - AIRCRAFT WAS IN-FLIGHT EN ROUTE TO DEN WHEN THE PILOT NOTICED HIS SIDE (LEFT) WINDOW HAD CRACKED, AIRCRAFT PROCEEDED TO DEN WHERE THE WINDOW WAS REMOVED AND REPLACED. AIRCRAFT WAS RETURNED TO SERVICE. (X)

Part: BOLTS — LOOSE (ELEVATOR CONTL)

DURING MAINTENANCE, THE LEFT YOKE WAS FOUND TO HAVE PLAY IN THE PITCH CONTROL. AFTER INSPECTION, IT WAS FOUND THAT THE SIX BOLTS ON THE ELEVATOR OUTPUT LEVER WERE ALL LOOSE, NO APPARENT VISUAL DAMAGE WAS FOUND TO THE OUTPUT LEVER ASSY. THE BOLTS REQUIRED RETORQUING ON THE LEFT AND THE RIGHT OUTPUT LEVER, P/N 82710093103. THESE BOLTS WERE RETORQUED IAW DASH 8-300 MAINTENANCE MANUAL 27-32-41 PAGE 201. A TEST FLIGHT WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: ELEV OUTPUT LVR — LOOSE BOLTS (CONTROL COLUMN)

DURING MAINTENANCE, THE LT YOKE WAS FOUND TO HAVE PLAY IN THE PITCH CONTROL. AFTER INSPECTION, FOUND THE 6 BOLTS ON THE ELEVATOR OUTPUT LEVER WERE ALL LOOSE, NO APPARENT VISUAL DAMAGE FOUND TO THE OUTPUT LEVER ASSY. THE BOLTS REQUIRED RE-TORQUING ON THE LT AND RT OUTPUT LEVER. THESE BOLTS WERE RE-TORQUED IAW DASH 8-300 MM 27-32-41, PAGE 201. A TEST FLIGHT WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SPOILER CABLE — WORN (WS 90)

DURING INSPECTION, THE LEFT WING ROLL SPOILER CABLE WAS FOUND TO BE WORN 50 PERCENT AT YW 90 BY A FAIRLEAD. THE CABLE WAS REPLACED ON FIELD AVIATION COMPANY WORKORDER NR 21978 AT C-CHECK. (M)

Part: CONTROL CABLE — WORN (RT AILERON)

DURING INSPECTION, THE RIGHT WING AILERON CABLE WAS FOUND TO BE WORN BY A PULLEY AT YW 170 RT. THE CABLE WAS REPLACED ON FIELD AVIATION COMPANY WORKORDER NR 21978 AT C-CHECK. (M)

Part: CONTROL CABLE — WORN (RT AILERON)

DURING INSPECTION, THE LEFT AND RIGHT WING AILERON CABLES WERE FOUND TO BE WORN 40 TO 50 PERCENT BY A PULLEY AT YW 404. THE CABLES WERE REPLACED ON FIELD AVIATION COMPANY WO NR 21978 AT C-CHECK.

Part: CONTROL CABLE — WORN (LT AILERON)

DURING INSPECTION, THE LEFT WING AILERON CABLE WAS FOUND TO BE WORN 50 PERCENT BY A FAIRLEAD AT YW 155 LEFT. THE CABLE WAS REPLACED ON FIELD AVIATION COMPANY WORKORDER NR 21978 AT C-CHECK.

Part: CONTROL CABLE — DAMAGED (RT AILERON)

INSPECTION OF AILERON CABLE REVEALED NUMEROUS BROKEN STRANDS ON RIGHT LOWER AILERON CABLE AT STA YW177, RENDERING CABLE UNSERVICEABLE. THE CABLE WAS REPLACED AND RIGGED, A TEST FLIGHT WAS PERFORMED, AND THEN THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BOLT — FAILED (LT MLG DOOR)

GJT - ATER DEPARTURE, PILOTS NOTICED LDG GEAR DOORS CYCLING OPEN AND CLOSED. AIRCRAFT RETURNED TO GJT. UPON INSPECTION, MECHANICS FOUND BOLT ATTACHING THE REAR OF THE AFT OUTBOARD LDG GEAR DOOR ON THE LT MAIN GEAR HAD BACKED OUT AND DEPARTED THE AIRCRAFT. THIS RESULTED IN THE DOOR PIVOTING ON THE REMAINING ATTACH POINT WHICH THEN PULLED TWO INSERTS OUT OF THE COMPOSITE DOOR. A REPAIR WAS DONE TO THE DOOR IAW DHC-8 SRM 51-20-71. A NEW BOLT INSTALLED AS WELL AS A NEW LDG GEAR UPLOCK HOOK. RETRACTIONS WERE PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE.

Part: UPLOCK HOOK — DIRTY (LT MLG)

DEN - ON APPROACH, LEFT MAIN GEAR DID NOT EXTEND WHEN SELECTED DOWN, CREW PUMPED GEAR DOWN AND LANDED WITHOUT INCIDENT. GEAR WAS THEN PINNED IN THE DOWN AND LOCKED POSITION AND GEAR PINS SECURED AND FERRIED DIRECT FROM DEN TO GJT FOR MAINTENANCE INSPECTION. MAINTENANCE PERFORMED INSPECTION OF LT MLG UPLOCK, CLEANED AND LUBRICATED, PERFORMED RETRACT AND EXTENSION OPERATIONAL CHECK IAW DHC-8-300 MM SYSTEM OPS CHECKED NORMAL. AIRCRAFT WAS RETURNED TO SERVICE. (X)