N434AW

Part: SPAR — DAMAGED (WGLT STA 6.36-12) · airframe 45,519 hrs · 44,476 cycles

FOUND DRILL START DAMAGE ON RH WINGLET REAR SPAR P/N: 600-15104-6 ON THE IB SIDE OF THE REAR SPAR CHANNEL BETWEEN WGLT STA 6.36 - 12.50 MEASURING 0.180"L X 0.180"W X 0.026"D. AIRCRAFT REMOVED FROM SERVICE. BLENDED OUT DRILL START DAMAGE TO A SMOOTH CONTOUR IAW MHIRJ REO 601R-57-31- 1417 REV (--) DATED 2023-05-26. ACCOMPLISHED HFEC INSPECTION OF BLEND AREA IAW CRJ200 NDT MANUAL PART 1 51-20-06 REV 44. NO INDICATIONS FOUND AT THIS TIME. ROTO PEENED REWORK AREA IAW CRJ200 SRM 51-24-11 REV 39. RESTORED PROTECTIVE FINISH IAW CRJ200 SRM 51-21-16 REV 39. FILLED BLEND AREA WITH SEALANT PRIOR TO SKIN INSTALLATION IAW CRJ200 SRM 51-23-00. ALL WORK PERFORMED WITHIN ALLOWABLE LIMITS IAW MHIRJ REO 601R-57-31-1417 REV (--) DATED 2023-05-26. WORK PERFORMED ON AERSALE WO #003940 CARD #50001 CARD ID #1864526. N434AW TT:45,519:28 TC:44,476

Part: SKIN — DENTED (FS 314 - 349) · airframe 45,519 hrs · 44,476 cycles

FOUND 3 DENTS ON FUSELAGE SKIN AROUND PASSENGER DOOR CUTOUT, FS 310, STR 14L - 15L = 1.2"L X .400"W X .315"D; FS 349 AT STR 14L = 2.8"L X .350"W X .162"D; AND FS 349, STR 15L - 16L = 0.9"L X 0.320"W X 0.145"D. AIRCRAFT REMOVED FROM SERVICE. PERFORMED TRIM OF DAMAGE AT 3 EA LOCATIONS ON PASSENGER DOOR SKIN CUTOUT AT FS 310 BETWEEN STR 14L - 15L = 1.85"L X .360"W AT SKIN AND DOUBLER; FS 349 AND STR 14L = 2.7"L X .295"W AT SKIN AND DOUBLER, & FS 349 BETWEEN STR 15L - STR 16L = 1.3"L X 0.280"W AT SKIN & DOUBLER IAW REO 601R-53-21-3618 REV --. FABRICATED REPAIR DOUBLER FROM 0.100", 8.85"L X 3.10" W & INSTALLED AT PAX DOOR SKIN CUTOUT AT FS 349, STR 13L - STR 15L IAW REO 601R-53-21-3618 REV --. RESTORED PROTECTIVE FINISH AT ALL REPAIR AREAS IAW REO 601R-53-21-3618 REV --.

Part: SKIN — NONE (LH WING LEADING) · airframe 44,092 hrs · 43,093 cycles

LEFT-WING LEADING-EDGE SKIN P/N 601R12074-3 SHOWS EROSION/ROUGHNESS OF 0.005" MULTIPLE SPOTS. ******AIRCRAFT REMOVED FROM SERVICE******* REMOVED AND REPLACED LEADING EDGE SKIN P/N 601R12074-3.

Part: UNKNOWN — UNKNOWN · corrosion level 2 · airframe 44,092 hrs · 43,093 cycles

RIGHT-WING LEADING-EDGE SHOWS SIGNS OF ROUGHNESS ********AIRCRAFT REMOVED FROM SERVICE********* RE-SKIN OTB SECTION OF RH WING OUTB LEADING EDGE AND INSTALLED 1 EA RIB AND 1 EA STRAP

Part: SKIN — NONE (LH OB LEADING ED) · airframe 44,092 hrs · 43,093 cycles

LH OUTBOARD LEADING EDGE SKIN P/N 601R12074-3 FOUND ERODED BEYOND LIMITS. ******AIRCRAFT REMOVED FROM SERVICE****** REMOVED AND REPLACED SKIN P/N 601R12074-3.

Part: ANGLE — CRACKED (FS621) · airframe 44,092 hrs · 43,093 cycles

FLOOR SUPPORT ANGLE ALONG FS621 BULKHEAD OUTBOARD OF FLOOR BEAM LBL27 IS CRACKED (MARKED) *****AIRCRAFT REMOVED FROM SERVICE***** R&R -1 ANGLE, (EXISTING REPAIR), REF BOMBARDIER REO 601R-53-61-117 REV-D DATED 2017-02-26 REF CRJ 200 SRM 51-42-06, CRJ 200 SRM 51-42-21, AND BOMBARDIER DWG 601R35031 REV-AG

Part: NONE — NONE · airframe 44,092 hrs · 43,093 cycles

DENT RH OTBD FLAP UPPER SKIN *****AIRCRAFT REMOVED FROM SERVICE**** REPAIRED

Part: NONE — NONE · airframe 44,061 hrs · 43,060 cycles

UPON FIRST WALK AROUND FO FOUND LH STANG FAIRING MISSING. R&R LH ENG STANG FAIRING IAW AMM 78-34

Part: TRANSCEIVER — FAULTED (WX RADAR SYS) · airframe 42,978 hrs · 41,958 cycles

WEATHER RDR TURNED ITSELF OFF AND WOULD NOT TURN BACK ON . AIRCRAFT REMOVED FROM SERVICE. R&R WEATHER RADAR RECIEVER/TRANSMITTER ASSY IAW AMM 34-41-01. OPS TEST GOOD. SN REMOVED: 1C6WV SN INSTALLED: 58VU

Part: PSEU — FAULT MESSAGE (MLG) · airframe 42,834 hrs · 41,800 cycles

PROX SYS CHAN CAUTION MSG IN FLIGHT. QRH C/W. MANUALLY EXTENDED LANDING GEAR. INSTALLED GEAR PINS. ***AIRCRAFT REMOVED FROM SERVICE*** INTERROGATED PSEU, FOUND CODES A01-A06 AND RED FAIL LIGHT ILLUMINATED. R&R PSEU IAW AMM 32-61-01. OPS CHECK GOOD. GEAR PINS STOWED IN COCKPIT. JESSE SHERMAN A&P 4092495

Part: SEAT TRACK — CORRODED (BS 379) · corrosion level 2 · airframe 42,827 hrs · 41,792 cycles

SEAT TRACK HAS CORROSION AND GOUGES WITH CORROSION COMMON TO CENTER OF SEAT TRACK AT FS 379.00+3 TO FS 379.00+11 LBL 9. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED SEAT TRACK COMMON TO CENTER OF SEAT TRACK AT FS 379.00+3 TO FS 379.00+11 LBL 9 REF CRJ200 AMM 53-01-11 REV 38 TASK 53-01-11-400-802

Part: BEAM — DAMAGED (BS 409) · airframe 42,827 hrs · 41,792 cycles

LIGHTNING HOLE HAS TORN AREAS X2 AT TOP OF HOLE FS 409.00+69+11.5" TO FS409.00+96+13 RBL 8 ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED 2 DAMAGED AREAS ON LIGHTNING HOLES AT FS 409.00+69+11.5 TO 409.00+69+13 RBL 8 FOUND WITHIN LIMITS REF ASAP EA# AWAC-CRJ253-01590 REV IR DATED 3/19/2021

Part: FLOORBEAM — DAMAGED (BS 364) · airframe 42,827 hrs · 41,792 cycles

TOOL MARK COMMON TO FLOOR STRUCTURE WEB AT FS364.00+8 AND LBL28 ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED TOOL MARK ON FLOOR STRUCTURE WEB AT FS364.00+8 AND LBL28 WITH BLEND DIMENSIONS OF 0.600Ï¿½L X 0.500Ï¿½W X 0.027Ï¿½D WITH A REMAINING THICKNESS OR 0.023Ï¿½ FROM THE ORIGINAL THICKNESS OF 0.050Ï¿½. BLEND FOUND OUT OF LIMITS, REF CRJ SRM 53-00-00 REV 38. REMOVED FLOOR BEAM FROM FS364.00 TO FS379.00 LBL28. DISCOVERED 3 ADDITIONAL TOOL MARKS AFTER REMOVAL OF FLOOR BEAM, 1) 0.3Ï¿½L X 0.1Ï¿½W X 0.001Ï¿½D, 2) 0.3 Ï¿½L X 0.2Ï¿½W X 0.001Ï¿½D, 3) 0.7Ï¿½L X 0.4Ï¿½W X 0.004Ï¿½ D. BLENDED ALL TOOL MARKS TO A SMOOTH CONTOUR, HFEC PERFORMED AT ALL BLENDED AREAS WITH NO INDICATIONS. REPAIRED FLOOR STRUCTURE FROM FS364.00 TO FS379.00 AND REINSTALLED REF MHI REO 601R-53-21-3427 REV Ï¿½ DATED 2021-04-03.

Part: SKIN — DAMAGED (RT WING) · airframe 42,827 hrs · 41,792 cycles

RT WING LOWER PLANK ACCESS PANEL CUTOUT AT 650AB HAS CRACK INDICATION AT OUTBOARD ARC APPROX. WS173.00, INDICATION MEASURES APPROX. 0.10. (INITIATES AWAC EO6/021/457) ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED BLEND AT CRACK INDICATION LOCATION ON R/H WING LOWER PLANK ACCESS PANEL 650 AB, HOLE 9, CUTOUT AT OUTBOARD ARC WS 173.00. HFEC INSPECTION ACCOMPLISHED WITH NO INDICATION. REMAINING THICKNESS OF 0.151 IS WITHIN LIMITS. ALL WORK PERFORMED REF BOMBARDIER REO 601R-57-21-030 REV L DATED 2014-02-05 AND AIR WISCONSIN EO6/021/454 REV D DATED 12/20/18.

Part: SKIN — DAMAGED (RT WING) · airframe 42,827 hrs · 41,792 cycles

RT WING LOWER PLANK ACCESS PANEL CUTOUT AT 650BB HAS CRACK INDICATION AT AFT INBOARD ARC APPROX. WS180.00, INDICATION MEASURES APPROX. 0.10. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED BLEND AT CRACK INDICATION LOCATION ON R/H WING LOWER PLANK ACCESS PANEL 650 AB, HOLE 10, CUTOUT AT OUTBOARD ARC WS 180.00. HFEC INSPECTION ACCOMPLISHED WITH NO INDICATION. REMAINING THICKNESS OF 0.171 IS WITHIN LIMITS. ALL WORK PERFORMED REF BOMBARDIER REO 601R-57-21-030 REV L DATED 2014-02-05 AND AIR WISCONSIN EO6/021/454 REV D DATED 12/20/18

Part: BULKHEAD WEB — DAMAGED (BS 621) · airframe 42,827 hrs · 41,792 cycles

REAR PRESSURE BULKHEAD FORWARD FACE HAS SCRATCHES COMMON TO FORWARD SIDE OF 621.00 BULKHEAD LBL 18 AT TOP OF BULKHEAD AROUND CANNON PLUGS. ***AIRCRAFT REMOVED FROM SERVICE*** EVALUATED THREE BLENDED AREAS ON REAR PRESSURE BULKHEAD DOUBLER FORWARD FACE OF UPPER SIDE FS 621.00 LBL 18 WL 142, FOUND TO BE WITHIN LIMITS REF REO # 601R-53-61-7602 REV A DATED 2021/03/18

Part: FAIRING — GOUGED (VERTICAL STAB) · airframe 42,827 hrs · 41,792 cycles

STAB FAIRING 326CR GOUGED FROM STAB MOVEMENT. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED GOUGE ON VERTICAL STABILIZER FAIRING PANEL 326CR. FOUND WITHIN LIMITS REF EA# AWAC-CRJ255-01588 REV A DATED 3/19/2021

Part: DOOR FRAME — CRACKED (FS 310) · airframe 42,827 hrs · 41,792 cycles

PAX DOOR STRUCTURE O/B PANEL UPPER EDGE INTERIOR SUSPECTED 2'' CRACK O/B OF STEP BULKHD BOTTOM STEP LOOKING AFT ***AIRCRAFT REMOVED FROM SERVICE*** PAX DOOR STRUCTURE O/B PANEL UPPER EDGE INTERIOR SUSPECTED 2'' CRACK O/B OF STEP BULKHD BOTTOM STEP LOOKING AFT REPLACED FRAME REF REO 601R-52-11-402 REV H DATED 2007/11/01

Part: SKIN — DENTED (BS 265) · airframe 42,827 hrs · 41,792 cycles

INWARD DENT COMMON TO EXTERIOR SKIN AT FS 265.00+3, STR 23L+1 ***AIRCRAFT REMOVED FROM SERVICE*** HAND DRESSED INWARD DENT AT FS 265.00+3 STR 23L+1 TO ORIGINAL CONTOUR. HFEC INSPECTION PERFORMED WITH NO INDICATIONS NOTED. REF ASAP EA# AWAC - CRJ253-01585 REV A DATED 3/11/2021.

Part: SKIN — DENTED (FS 265) · airframe 42,827 hrs · 41,792 cycles

INWARD DENT COMMON TO EXTERIOR SKIN AT FS 265.00+3.75, STR 23L+4.25. ***AIRCRAFT REMOVED FROM SERVICE*** HAND DRESSED DENT AT FS 265.00+3.75, SR 23L+4.25 TO ORIGINAL CONTOUR, HFEC INSPECTION PERFORMED WITH NO INDICATIONS NOTED, REF ASAP EA# AWAC-CRJ-253-01585 REV A DATED 3/11/2021.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 42,827 hrs · 41,792 cycles

INWARD DENT COMMON TO EXTERIOR SKIN, LOWER SIDE OF INBOARD RIGHT HAND FLAP AT APPROXIMATELY WING STATION 106.40. ***AIRCRAFT REMOVED FROM SERVICE*** EVALUATED DENT COMMON TO EXTERIOR SKIN, LOWER SIDE OF INBOARD RIGHT HAND FLAP AT APPROX. WING STATION 106.40 MEASURING 1.6"L X 1.3"W X 0.031"D. FOUND TO BE WITHIN ALLOWABLE LIMITS REF EA# AWAC-CRJ257-01587 REV IR DATED 3/13/2021. YELLOW DOT APPLIED REF AIR WISCONSIN GMM VOLUME 1 CHAPTER 18 REV 20-07.

Part: SKIN — DENTED (BS 235) · airframe 42,827 hrs · 41,792 cycles

INWARD DENT COMMON TO EXTERIOR SKIN AT FS 235.00-13, STRINGER 24L+4 ***AIRCRAFT REMOVED FROM SERVICE*** HAND DRESSED DENT AT FS 235.00+13, STR 24L+4 TO ORIGINAL CONTOUR, HFEC INSPECTION PERFORMED WITH NO INDICATIONS NOTED. REF ASAP EA# CRJ253-01586 REV IR DTD 3/11/2021

Part: BPSU — FAILED (RT WING TE FLAPS) · airframe 42,472 hrs · 41,413 cycles

WHILE AT CRUISE FL300, FLAP FAIL CAUTION MESSAGE APPEARED WITH NO INPUT ON FLAP HANDLE. RAN QRH. TOUCHDOWN BELOW MAX LANDING WEIGHT. BRAKE TEMP MAX WERE 5 RT OUTBOARD BRAKE. FLAP FAIL REMAINED DISPLAYED ON TAXI TO GATE. PERFORMED FLAP RESET PROCEDURE, IAW AWAC SUPP 98-18I BOX 12. FLAPS REST. PLACARDED AND PLACED ON MEL. AIRCRAFT REMOVED FROM SERVICE. REF W/O 299528 WC NR 2 & 3 FOR CORRECTIVE ACTION REMOVED PLACARD AND REMOVED FROM MEL. WC NR 2 TROUBLESHOOT, IAW FIM SUPP 98-0181, FAULT LOG MOST PROBABLE IS RT BPSU SEE MX WORD CARD NR 3 FOR CORRECTIVE ACTION. RECORD OF FECU FAULT LOG INCLUDED IN PACKAGE. WC NR 3 R & R RT FLAP BPSU, IAW AMM 27. OPERATIONS CHECK GOOD.

Part: CIRCUIT BREAKER — SHORTED (COCKPIT) · airframe 42,373 hrs · 41,320 cycles

ON TAKE-OFF ROLL, PRIOR TO ROTATION, WE SAW AND HEARD ELECTRICAL FLASHES BEHIND CAPTAIN AND SCREENS FLICKERED, ALSO SMELLED ELECTRICAL SMOKE BRIEFLY. "AIRCRAFT REMOVED FROM SERVICE" INSPECTED AND FOUND RAZOR BLADE MAKING CONTACT WITH CBP1-A2 AND A5 (FOR HYD. PUMPS 3B AND 2B) AND EVIDENCE OF ARCING. REMOVED RAZOR BLADE. REMOVED CIRCUIT BREAKERS IAW ESPM 20-23-00 AND CLEANED WIRING, TERMINALS AND INTERIOR OF CIRCUIT BREAKER PANEL 1 IAW AMM 20-10-00. SEE 325730/1 FOR REPLACEMENT OF CIRCUIT BREAKERS AND OPS CHECKS OF HYD SYSTEM 2 AND 3. INSTALLED NEW CB'S ON CBP-1 A2 AND A5 IN REF TO ESPM 20-23-00 AND OPS CHECKED HYD SYSTEMS 2 AND 3 IN REF TO AMM 29-11-03. OPS CHECKS GOOD. AIRCRAFT OK FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (BS 559) · corrosion level 2 · airframe 42,172 hrs · 41,112 cycles

RH FLOOR SILL IN AFT CARGO HAS SPOTS OF CORROSION, FS559.00+80 TO FS559.00+112. AIRCRAFT REMOVED FROM SERVICE BLENDED TO REMOVE CORROSION ORIGINAL MATERIAL - .063 MATERIAL LOSS - .063 REMAINING THICKNESS - .000 ALLOWABLE LIMITS - .015 REMOVED AND REPLACED FLOOR SILL IAW CRJ200 SRM 51-42-06 & 51-42-21.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · corrosion level 2 · airframe 42,172 hrs · 41,112 cycles

FLOOR SUPPORT IS CORRODED IN NUMEROUS LOCATIONS FROM FS409.00+128 TO FS559.00, RBL 9 AIRCRAFT REMOVED FROM SERVICE ORIGINAL MATERIAL .063 MATERIAL REMOVED .026 REMAINING MATERIAL .037 ALLOWABLE LOSS .005 REPAIRED FLOOR SUPPORT IAW EA AWAC-CRJ253-01439

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 42,114 hrs · 39,600 cycles

AFT PRESSURE BULKHEAD WEB IS CRACKED AT BL 0, WL 111.00. AIRCRAFT REMOVED FROM SERVICE WORK TRANSFERRED TO AAR W.O. 1018176/2000/0019, S/N 7601432, C/W AWAC JOB CARD 4EOAWA21045-E17/003/453 MODIFICATION OF THE REAR PRESSURE BULKHEAD WEB FS621.00 USING BOMBARDIER GREO 601R-53-61-1240 REV.D.

Part: FRAME — CORRODED (BS 333) · corrosion level 2 · airframe 42,172 hrs · 41,112 cycles

FRAME 333 HAS CORROSION SPOTS ON THE FWD AND AFT SIDES BETWEEN STRINGERS 25R AND 26L. AIRCRAFT REMOVED FROM SERVICE BLENDED TO REMOVE CORROSION ORIGINAL THICKNESS .050 MATERIAL LOSS .012 REMAINING MATERIAL .038 ALLOWABLE LOSS .005 REMOVED AND REPLACED FRAME SEGMENT.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · corrosion level 2 · airframe 42,172 hrs · 41,112 cycles

FLOOR SUPPORT IS CORRODED IN NUMEROUS LOCATIONS FROM 409+128-559.00, INBD SIDE OF BEAM. AIRCRAFT REMOVED FROM SERVICE BLENDED TO REMOVE CORROSION ORIGINAL THICKNESS .063 MATERIAL LOSS .026 REMAINING MATERIAL .037 REPAIRED FLOOR SUPPORT IAW EA AWAC-CRJ253-01446.

Part: STRAP — CORRODED (BS 559) · corrosion level 2 · airframe 42,172 hrs · 41,112 cycles

FLOOR SUPPORT STRAP IS CORRODED AT FS559.00+112, RBL27-RBL45. AIRCRAFT REMOVED FROM SERVICE BLENDED TO REMOVE CORROSION ORIGINAL MATERIAL .100 MATERIAL LOSS .013 REMAINING MATERIAL .087 ALLOWABLE LOSS .010 REMOVED AND REPLACED STRAP IAW CRJ200 SRM 51-42-06

Part: FLOOR SUPPORT — CORRODED (BS 584) · corrosion level 2 · airframe 42,172 hrs · 41,112 cycles

FLOOR SUPPORT IS CORRODED AT FS584.00, RBL 9. AIRCRAFT REMOVED FROM SERVICE REMOVED CORROSION IAW AWAC SUPPLEMENT 19-206. ORIGINAL THICKNESS .050 MATERIAL LOST .029 ALLOWABLE LOSS LIMITS .013 REMAINING THICKNESS .021 REMOVED AND REPLACED FLOOR BEAM IAW BOMBARDIER REO 601R-53-61-3780 REV. A.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · corrosion level 2 · airframe 42,172 hrs · 41,112 cycles

FLOOR SUPPORT IS CORRODED FROM FS574.00 TO FS621.00, RBL 9. AIRCRAFT REMOVED FROM SERVICE BLENDED TO REMOVE CORROSION IAW CRJ200 SRM 53-61-43 & 51-31-59. ORIGINAL THICKNESS .050 ALLOWABLE LOSS .020 ACTUAL MATERIAL LOSS .050 REMAINING THICKNESS .000 REMOVED AND REPLACED FLOOR BEAM CAP IAW BOMBARDIER REO 601R-53-61-3780.

Part: SPAR — DAMAGED (LT WING) · airframe 42,172 hrs · 41,112 cycles

L/H WING FRONT SPAR HAS DOUBLE DRILLED HOLE AT TOP CENTER OF CENTER LEADING EDGE. AIRCRAFT REMOVED FROM SERVICE REPAIRED L/H WING FRONT SPAR DOUBLE DRILLED HOLE AT TOP CENTER OF CENTER LEADING EDGE IAW BOMB. REO 601R57-00-116.

Part: ANGLE — CRACKED (LT NACELLE) · airframe 42,172 hrs · 41,112 cycles

RIB ON LH PYLON LOWER FLANGE CRACKED FS605. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED IAW AWAC SUPPLEMENT 14-252A.

Part: FLOOR SUPPORT — CORRODED (BS 574-589) · corrosion level 2 · airframe 42,172 hrs · 41,112 cycles

FLOOR SUPPORT IS CORRODED AT FS621.00 TO FS574, LBL 9. AIRCRAFT REMOVED FROM SERVICE REPAIRED FLOOR SUPPORT IAW AWAC SUPPLEMENT 20-024.

Part: STRAP — CORRODED (BS 559) · corrosion level 2 · airframe 42,172 hrs · 41,112 cycles

FLOOR STRAP AT FS559.00, RBL 45 TO RBL 27, IS CORRODED. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED FLOOR STRAP IAW CRJ200 SRM 51-42-06 AND TR 51-42.

Part: ACCESS PANEL — CRACKED · airframe 42,172 hrs · 41,112 cycles

PANEL 630BL HAS CHAFFING ON INNER SURFACE. CRACK INDICATIONS NOTED DURING HFEC INSPECTION OF REPAIRED SURFACE. AIRCRAFT REMOVED FROM SERVICE REPAIRED PANEL 630BL IAW AWAC SUPPLEMENT 19-218A.

Part: BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 42,172 hrs · 41,112 cycles

LEFT WING TRANSITION PICOLLO TUBE BRACKET BETWEEN INBOARD AND CENTER LEADING EDGES IS CORRODED. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED PICOLLO TUBE TRANSITION TUBE BRACKET IAW CRJ200 SRM 51-42-06 % 51-41-06.

Part: SEAT TRACK — CORRODED (BS 449-499) · corrosion level 2 · airframe 42,172 hrs · 41,112 cycles

LEFT SIDE SEAT TRACK BETWEEN FS449.85 & FS499.00 HAS CORROSION AND GOUGED. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED SEAT TRACK IAW CRJ200 AMM 53-01-11.

Part: FRAME — CORRODED (BS 310) · corrosion level 2 · airframe 42,172 hrs · 41,112 cycles

FRAME 310 HAS CORROSION SPOTS ON THE FWD AND AFT SIDES BETWEEN STRINGER 24L AND 24R, IN THE FWD E&E BAY. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED FRAME SEGMENT IAW CRJ200 SRM 51-42-06 AND 51-42-21.

Part: FRAME ANGLE — CORRODED (BS 409) · corrosion level 2 · airframe 42,172 hrs · 41,112 cycles

FRAME 409 AFT ANGLE SPLICE HAS CORROSION SPOTS BETWEEN STRINGER 26L THRU 26R IN THE FWD E&E BAY AIRCRAFT REMOVED FROM SERVICE. REMOVED DAMAGE AT FRAME 409 AFT ANGLE SPLICE BETWEEN STINGER 26L AND 26R AND INSTALLED NEW ANLGE SPLICE IAW CRJ 200 SRM 51-42-06 AND 51-42-21

Part: FLOORBEAM — CORRODED (BS 589) · corrosion level 2 · airframe 42,172 hrs · 41,112 cycles

FLOOR SUPPORT IS CORRODED AT FS589.00, LBL 9 TO LBL 27. AIRCRAFT REMOVED FROM SERVICE INSTALLED NEW FABRICATED CAP STRIP AT FLOOR SUPPORT AT FS589.00, LBL 9 TO LBL 27 IAW CRJ200 SRM 51-42-06, 51-24-36 AND TR 51-42.

Part: SEAT TRACK — CORRODED (BS 559-574) · corrosion level 2 · airframe 42,172 hrs · 41,112 cycles

CARGO SEAT TRACK AT FS559+112 TO FS574.00, LBL 9 IS CORRODED. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED CARGO TRACK IAW CRJ200 AMM 53-00-49.

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 42,172 hrs · 41,112 cycles

CARGO SEAT TRACK AT FS559+86 TO FS559+96, LBL 9 IS CORRODED. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED CARGO SEAT TRACK IAW CRJ200 AMM 53-00-49.

Part: SEAT TRACK — CORRODED (BS 559-574) · corrosion level 2 · airframe 42,172 hrs · 41,112 cycles

CARGO SEAT TRACK AT FS559+112 TO FS574, RBL 9 IS CORRODED. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED SEAT TRACK IAW CRJ200 AMM 53-00-49.

Part: SEAT TRACK — CORRODED (BS 559-574) · corrosion level 2 · airframe 42,172 hrs · 41,112 cycles

CARGO SEAT TRACK AT FS559+112 TO FS574.00, LBL 9 IS CORRODED. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED CARGO SEAT TRACK IAW CRJ200 AMM 53-00-49.

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 42,172 hrs · 41,112 cycles

CARGO SEAT TRACK AT FS559+86 TO FS559+96, RBL 9 IS CORRODED. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED CARGO SEAT TRACK IAW CRJ200 AMM 53-00-49.

Part: BRACKET — CRACKED (RT WING) · airframe 42,172 hrs · 41,112 cycles

RIGHT WING CENTER LEADING EDGE INBD MOUNT BRACKET IS CRACKED. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED INBD LEADING EDGE MOUNT BRACKET. IAW CRJ200 SRM 51-41-02

Part: BRACKET — CRACKED (RT WING LE) · airframe 42,172 hrs · 41,112 cycles

R/H WING INBD LEADING EDGE OUTBD MOUNT BRACKET CRACKED. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED OUTBD MOUNT BRACKET IAW CRJ200 SRM 51-41-02.

Part: STEERING SYS — INOPERATIVE (NLG) · airframe 41,833 hrs · 40,786 cycles

RECEIVED NOSE WHEEL STEERING INOPERATIVE CAUTION AT 1000 FEET AFTER SELECTING GEAR UP, COMPLIED WITH QUICK REFERENCE HANDBOOK, MESSAGE REMAINS. RECEIVED WEIGHT ON WHEELS INPUT CAUTION, AND WEIGHT ON WHEELS OUTPUT CAUTIONS. COMPLIED WITH QUICK REFERENCE HANDBOOK, MESSAGES REMAIN. EMERGENCY LANDING WAS DECLARED.

Part: STEERING SYS — INOPERATIVE (NLG) · airframe 41,523 hrs · 40,491 cycles

STEERING INOP CAUTION MESSAGE ON CLIMBOUT, COMPLIED WITH QRH, MESSAGE RETURNED, STEERING SELECTED OFF FOR LANDING. ATC DECLARED EMERGENCY. LANDED WITH STEERING SELECTED OFF AND PROCEEDED TO GATE USING DIFFERENTIAL THRUST/BRAKING.

Part: FLOOR SKIN — CRACKED (FUSELAGE) · airframe 40,877 hrs · 39,854 cycles

PRESSURE FLOOR SKIN CRACKED AT ACCESS PNL 165DZ CUT OUT. REPAIRED IAW REO 601R-53-41-2339 REV-.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 40,877 hrs · 39,854 cycles

PRESSURE FLOOR SKIN CRACKED AT ACCESS PNL 165DZ CUT OUT. REPAIRED IAW REO 601R-53-41-2339 REV-.

Part: STRINGER — CRACKED (BS 394) · airframe 40,877 hrs · 39,854 cycles

STRINGER 3L CRACKED AT BS 394. REPAIRED THE STRINGER IAW SRM 53-00-03.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 40,877 hrs · 39,854 cycles

RIGHT WING LEADING EDGE SHROUD ATTACH ANGLE WAS CRACKED AT WS 149.58. REPLACED THE ATTACH ANGLE IAW SRM 51-42-15.

Part: FITTING — CRACKED (COCKPIT) · airframe 40,877 hrs · 39,854 cycles

LEFT FLIGHT DECK WINDOW SIDE POST LOWER AFT FITTING CRACKED. REPLACED FITTING IAW SRM 51-42-26.

Part: BRACKET — CRACKED (LT AILERON HINGE) · airframe 40,877 hrs · 39,854 cycles

LEFT AILERON CENTER HINGE BOLT KEEPER BRACKET CRACKED. REPLACED BRACKET IAW CRJ200 SRM 51-42-06.

Part: RETAINER — CRACKED (LT PYLON) · airframe 40,877 hrs · 39,854 cycles

LEFT PYLON PNL 412AT SEAL RETAINER CRACKED. REPLACED SEAL RETAINER IAW SRM 51-42-06.

Part: FITTING — CRACKED (COCKPIT) · airframe 40,877 hrs · 39,854 cycles

RIGHT FLIGHT DECK WINDOW SIDE POST LOWER AFT FITTING CRACKED. REPLACED FITTING IAW SRM 51-42-21, 51-40-11.

Part: BRACKET — CRACKED (LT AILERON) · airframe 40,877 hrs · 39,854 cycles

LEFT AILERON CENTER HINGE BOLT KEEPER BRACKET CRACKED. REPLACED BRACKET IAW SRM 51-42-06.

Part: SKIN PANEL — CRACKED (FUSELAGE) · airframe 40,877 hrs · 39,854 cycles

LEFT HAND TRU DOOR LANDING SKIN PANEL CRACKED BY LATCH CUT OUT. STOPPED DRILLED CRACK IAW REO601R-53-11-2381 REV-.

Part: SKIN — CHAFED (RT AILERON) · airframe 40,877 hrs · 39,854 cycles

RIGHT AILERON LOWER FWD LEADING EDGE SKIN CHAFED 2 PLACES. REPLACED MID SKIN IAW SRM 51-42-06 AND REPAIRED O/B CHAFE IAW SUPP 16-074.

Part: SKIN — DAMAGED (LT AILERON) · airframe 40,877 hrs · 39,854 cycles

LEFT AILERON UPPER LEADING EDGE SKIN DAMAGED AT CENTER HINGE. REPAIRED IAW SRM 57-60-00, 51-24-26, 51-24-21, 51-42-06.

Part: SKIN — CHAFED (RT AILERON) · airframe 40,877 hrs · 39,854 cycles

RIGHT AILERON UPPER LEADING EDGE IS CHAFED. REPLACED LEADING EDGE ON RIGHT AILERON IAW SRM 51-42-06 AND SUPP 13-055B.

Part: SKIN — CHAFED (LT AILERON) · airframe 40,877 hrs · 39,854 cycles

LEFT AILERON FWD LOWER CLOSEOUT SKIN CHAFED. REPLACED SKIN IAW SRM 51-42-06.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 40,877 hrs · 39,854 cycles

AFT PRESSURE BULKHEAD AFT FACE STIFFENER CRACKED O/B OF LBL36.20, JUST ABOVE FLOOR LEVEL. REPLACED STIFFENER IAW SRM 51-42-06.

Part: FITTING — CRACKED (FUSELAGE) · airframe 40,877 hrs · 39,854 cycles

ANGLE CLIP CRACKED AT FS 484, LBL36. REPLACED ANGLE CLIP IAW REO 601R-53-41-059 REV-B.

Part: YAW DAMPER — DISENGAGED (LEFT) · airframe 35,029 hrs · 34,681 cycles

YAW DAMPENER 1 DISENGAGED IN FLIGHT WITH UNCOMMANDED YAW. R&R LT YAW DAMPER PER AMM 22-22-01.

Part: BRACKET — DAMAGED (SENSOR) · airframe 34,784 hrs · 34,433 cycles

3774 FOLLOWING GEAR RETRACTION AFTER TAKE OFF RECEIVED GEAR DISAGREE WARNING MESSAGE. NOSE GEAR DID NOT RETRACT, MESSAGE APPEARED AFTER 6 SECONDS, ALSO RECEIVED NOSE DOOR WARNING. NO LANDING GEAR LEVEL MOVEMENT FOR APPROX. 4-5 MIN, MANUAL RELEASE USED. NO ICING TURBULENCE OR EXCESSIVE MOVEMENTS. HYD TEMPS PRESSURE AND QTY NORMAL. HYD PUMP IN AUTO. EMERGENCY DECLARED. OCCURRED AT 170 KNOTS AND NO HARD LANDING, LANDED AT 46,000 LBS. R&R SENSOR BRACKET PER CMM 32-20-04 READJUST SENSOR GAP PER AMM 32-61-05. PERFORMED GEAR OPS CHECK, OPS CHECK GOOD.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 34,684 hrs · 34,308 cycles

EXTERNAL EMERGENCY LIGHTS DO NOT ILLUMINATE. REPAIRED A WIRE LF20A20N IAW ESPM. OPS CHECKED GOOD.

Part: WIRE — DISCONNECTED (NR 2 IDG) · airframe 34,537 hrs · 34,166 cycles

RECEIVED A NR 2 IDG CAUTION MESSAGE IN FLIGHT AT 10,000 FT, RETURNED TO DEPARTURE. INSPECTED THE NR 2 ENGINE IDG AND SERVICED WITH 5 PUMPS OF OIL. OPS CHECKED GOOD IAW AMM 24-11-00. FOUND A DISCONNECTED WIRE ON CONNECTER P22EZ. REPAIRED IAW ESPM 20-17-10 OPS CHECKED GOOD.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 34,040 hrs · 33,723 cycles

DURING ACCEPTANCE INSPECTION, CREW REPORTED EMERGENCY LIGHTS ON FLOOR TRACK RIGHT SIDE ROWS 2-6 DID NOT WORK. ALSO LEFT OVERWING EXIT LOWER EMERGENCY SIGN NOT ILLUMINATING. INSPECTED CONNECTIONS ON EMERGENCY FLOOR TRACK LIGHTS, NO DEFECTS FOUND. ALLOWED LIGHTS TO CHARGE FOR 15 MINUTES, NO FIX. SUSPECT BATTERY 2 FAILURE.

Part: DOOR SILL — CORRODED (BS 347) · corrosion level 2 · airframe 39,190 hrs · 38,190 cycles

SERVICE DOOR LOWER SILL HAS CORROSION AT BS 347

Part: FLOOR SUPPORT — CORRODED (BS 559) · corrosion level 2 · airframe 39,190 hrs · 38,190 cycles

RT FLOOR SUPPORT HAS CORROSION BETWEEN BS 559+87 TO 559+112

Part: FLOORBEAM — CORRODED (BS 409) · corrosion level 2 · airframe 39,190 hrs · 38,190 cycles

FLOORBEAM CAP BS 409, RBL 9 IS CORRODED AROUND FASTENER HOLES

Part: SEAT TRACK — CORRODED (BS 394-409) · corrosion level 2 · airframe 39,190 hrs · 38,190 cycles

RBL 9 FLOOR SEAT TRACK CORRODED BETWEEN BS 394 AND 409+128

Part: INTERCOSTAL — CRACKED (BS 621) · airframe 31,910 hrs · 38,190 cycles

INTERCOSTAL AFT OF BS 621 BULKHEAD STRINGER 13L CRACKED.

Part: INTERCOSTAL — CRACKED (BS 621) · airframe 39,190 hrs · 38,190 cycles

INTERCOSTAL AFT OF BS 621 BULKHEAD AT STRINGER 15L FOUND CRACKED.

Part: INTERCOSTAL — CORRODED (BS 349-364) · corrosion level 2 · airframe 39,190 hrs · 38,190 cycles

INTERCOSTAL JUST TO THE RIGHT OF STGR 27 HAS CORROSION BETWEEN FRAMES BS 349 AND 364

Part: FLOORBEAM — CRACKED (BS 280) · airframe 39,190 hrs · 38,190 cycles

FS 280 FLOORBEAM OTBD ANGLE AT LBL 9 WAS FOUND TO BE CRACKED.

Part: INTERCOSTAL — CRACKED (BS 621) · airframe 39,190 hrs · 38,190 cycles

INTERCOSTAL AFT OF BS 621 BULKHEAD AT STRINGER 16L FOUND TO BE CRACKED.

Part: MOUNT — CRACKED (DOOR MOTOR) · airframe 39,190 hrs · 38,190 cycles

PAX DOOR LOWER MOTOR MOUNT CRACKED AT THE BOTOM SIDE AT ANGLE.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 39,190 hrs · 38,190 cycles

BS 280 FLOORBEAM OTBD ANGLE AT RBL 9 IS CRACKED.

Part: FLOOR SUPPORT — CORRODED (BS 409) · corrosion level 2 · airframe 39,190 hrs · 38,190 cycles

FLOOR SUPPORT CHANNEL CORRODED. REPLACED CHANNEL

Part: FLOORBEAM — CRACKED (BS 280) · airframe 39,190 hrs · 38,190 cycles

BS 280 FLOORBEAM UPPER AFT ANGLE AT RBL 12 CRACKED. REPAIRED THE FLOORBEAM ANGLE.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 39,190 hrs · 38,190 cycles

BS 280 FLOORBEAM UPPER AFT ANGLE AT LBL 12 FOUND CRACKED. REPAIRED THE FLOORBEAM.

Part: INTERCOSTAL — CRACKED (BS 621) · airframe 39,190 hrs · 38,190 cycles

INTERCOSTAL ON AFT SIDE OF BS 621 BULKHEAD AT STRINGER 14L IS CRACKED. REPLACED THE INTERCOSTAL IAW SRM 51-42-06, AND 51-42-21.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 39,190 hrs · 38,190 cycles

LT IB FLAP VANE CTR LEADING EDGE IS CHAFED.

Part: DOOR SILL — CORRODED (BS 319-349) · corrosion level 2 · airframe 39,190 hrs · 38,190 cycles

SERVICE DOOR SILL CORRODED. REPLACED SERVICE DOOR SILL IAW CRJ 200 SRM 51-40-11.

Part: VANE — GOUGED (TE FLAP) · airframe 39,190 hrs · 38,190 cycles

LT IB FLAP VANE LE I/B SECTION IS GOUGED.

Part: ATTACH BRACKET — CRACKED (BS 280) · airframe 39,190 hrs · 38,190 cycles

ATTACH BRACKET CRACKED AT FS 280.00, STR 3L. REPLACED BRACKET AT FS 280.00, STR3L IAW CRJ 200 SRM 51-42-06.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 39,190 hrs · 38,190 cycles

RBL9 CARGO TRACK FROM FS 559+110 TO FS569 CORRODED. REPLACED.

Part: ANGLE — CORRODED (BS 319-349) · corrosion level 2 · airframe 39,190 hrs · 38,190 cycles

SERVICE DOOR LOWER SILL ANGLE IS CORRODED BETWEEN BS 319 AND 349. REPLACED LOWER SILL ANGLE ON SERVICE DOOR LOWER SILL IAW SRM 51-42-21, AND 51-42-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,190 hrs · 38,190 cycles

RT SEAT TRACK AT RBL 9 FROM FS 409+128 TO FS 559 CORRODED. REPLACED.

Part: FLOOR SUPPORT — CORRODED (BS 349) · corrosion level 2 · airframe 39,190 hrs · 38,190 cycles

RIGHT FWD WINDSCREEN FLOOR SUPPORT CORRODED. REPLACED FLOOR SUPPORT IAW SRM 51-42-06, 51-42-21, 51-40-11, AND 51-24-36.

Part: VANE — WORN (TE FLAP) · airframe 39,190 hrs · 38,190 cycles

RT INBD FLAP VANE LE HAS WEAR IN THREE PLACES JUST BELOW INBD AND OUTBD GROUND SPOILERS. REPLACED.

Part: FLOORBEAM — CORRODED (BS 559) · corrosion level 2 · airframe 39,190 hrs · 38,190 cycles

MAIN CABIN FLOORBEAM CORRODED AT FS 559.00 TO FS559+80, RBL42 TO RBL 47. REPAIRED FLOOR SILL IAW SUPPLEMENT 17-083 AND REO 601R-53-00-526 REV -- .

Part: FLOORBEAM — CORRODED (BS 349) · corrosion level 2 · airframe 39,190 hrs · 38,190 cycles

MAIN CABIN FLOORBEAM CORRODED AT BS 349, RBL27 TO RBL45. REPAIRED FLOORBEAM IAW REO 601R-53-21-2745.

Part: FRAME — CORRODED (BS 589) · corrosion level 2 · airframe 39,190 hrs · 38,190 cycles

FRAME BS 589 CORRODE BETWEEN STRINGERS 24L TO 25R. REPAIRED THE FRAME IAW EA 253-00674, REV-IR.

Part: FRAME — CORRODED (BS 605) · corrosion level 2 · airframe 39,190 hrs · 38,190 cycles

FRAME BS 605 CORRODED BETWEEN STRINGERS 20L AND 20 R. REPLACED THE FRAME IAW SRM 51-42-06, AND 51-42-21.

Part: FRAME — CORRODED (BS 574) · corrosion level 2 · airframe 39,190 hrs · 38,190 cycles

FRAME BS 574 CORRODED BETWEEN STR 26L AND 26R. REPAIRED THE FRAME IAW EA AWAC-CRJ253-00673, REV-IR.

Part: FLOORBEAM — CORRODED (BS 280) · corrosion level 2 · airframe 39,190 hrs · 38,190 cycles

FLOORBEAM UPPER ANGLE AT BS 280 BETWEEN RBL 9 AND LBL 9 IS CORRODED. REPLACED THE FLOORBEAM ANGLE IAW SRM 51-42-06, AND 51-40-11.

Part: FLOOR SUPPORT — CORRODED (BS 559-564) · corrosion level 2 · airframe 39,190 hrs · 38,190 cycles

FLOOR SUPPORT CORRODED AT BS 559+102 TO 564, LBL 27. REPLACED THE FLOOR SUPPORT IAW SRM 53-00-43, REPAIR 2.

Part: STRUCTURE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 39,190 hrs · 38,190 cycles

PAX DOOR EDGE MEMBER CORRODED REMOVED AND REPLACED EDGE MEMBER IAW SRM 51-42-06.

Part: FLOOR SUPPORT — CORRODED (BS 589-621) · corrosion level 2 · airframe 39,190 hrs · 38,190 cycles

MAIN CABIN FLOOR SUPPORT CORRODED AT BS 589 TO 621, RBL 27. REPLACED THE FLOOR SUPPORT IAW 15-279.

Part: FLOOR SUPPORT — CORRODED (BS 569-621) · corrosion level 2 · airframe 39,190 hrs · 38,190 cycles

FLOOR SUPPORT CORRODED BS 569 TO 621, LBL 27. REPLACED THE FLOOR SUPPORT IAW REO 601R-53-00-0005, REV-B.

Part: WARNING MESSAGE — ILLUMINATED (MLG) · airframe 33,313 hrs · 33,048 cycles

AFTER GEAR UP, GOT A GEAR DISAGREE WARNING WITH NOSE GEAR INDICATING NOT UP.

Part: FLAP SYSTEM — FAILED

FLAPS FAILED AT 30 DEGREES ON FINAL APPROACH.

Part: APU — FAILED · airframe 38,252 hrs · 37,357 cycles

DURING FIRST FLIGHT OF THE DAY CHECKS CREW REPORTED AN APU AUTO SHUTDOWN, APU OIL TEMP CAUTION AND APU FAULT CAUTION MESSAGE ON ED1. STRONG OIL ODOR THROUGH PACK AND IN AFT EQUIPMENT BAY.

Part: STEERING SYS — MALFUNCTIONED (NLG) · airframe 32,680 hrs · 32,469 cycles

AFTER T/O, SELECTED GEAR UP, RECEIVED GEAR DISAGREE WARNING, NWS INOPERATIVE CAUTION, WOW INPUT CAUTION, WOW OUTPUT STATUS MESSAGES. ON ED1, MAINS UP/LOCKED AND NOSE WAS DOWN/LOCKED. C/W QRH, MANUALLY EXTENDED THE GEAR, RECEIVED 3 GREEN DOWN. NWS INOPERATIVE, WOW INPUT AND WOW OUTPUT MESSAGES REMAIN ON. LANDED AT 46800 GROSS. WHILE AIRBORNE, C/W NWS INOPERATIVE QRH, MESSAGE REMAINS. ON TAXIWAY, CYCLED NWS SWITCH- REGAINED NWS. TAXI TO GATE WAS NORMAL. NOSE STRUT SHOWS 0" CHROME WITH PASSENGERS ON, 6" WITH PASSENGERS OFF.

Part: ACTUATOR — MALFUNCTIONED (FUEL SYSTEM) · airframe 35,319 hrs · 34,594 cycles

AFTER TAKEOFF REC GRAVITY XFLOW FAIL STATUS MSG. DECLARED PRECAUTIONARY EMER & DIVERTED. AFTER APPROX 20 MIN MSG CLEARED ON ITS OWN. R & R GRAVITY XFLOW ELEC ACT IAW AMM 28-13-16. OPERATIONS CHECKED GOOD.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 34,601 hrs · 33,889 cycles

ACFT POWER RECEPTACLE ATTACH BRACKET IS CRACKED.

Part: MOUNT BRACKET — CRACKED (FUSELAGE) · airframe 34,601 hrs · 33,889 cycles

NR 3 HYD RESERVOIR AFT MOUNT IS MOUNT.

Part: MOUNT BRACKET — CRACKED · airframe 34,601 hrs · 33,889 cycles

LEFT 10TH STAGE BLEED LOOP MOUNT BRACKET IS CRACKED.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 34,601 hrs · 33,889 cycles

LEFT ACM SUPPORT STRUCTURE BRACKET IS CRACKED.

Part: BRACKET — CRACKED (LT ENGINE) · airframe 34,601 hrs · 33,889 cycles

CRACKED BRACKET ON T2 SENSE LINE ON LT ENG.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 34,601 hrs · 33,889 cycles

CRACK IN UPPER CAP OF PAX DOOR INTERCOSTAL UNDER PANEL 832GL.

Part: RIB — CRACKED (PAX DOOR) · airframe 34,601 hrs · 33,889 cycles

CRACK IN PAX DOOR RIB UPPER CAP RADIUS ABOUT 8" BEHIND AFT CAM LATCH.

Part: SCREW — IMPROPER PART (FUSELAGE) · airframe 34,601 hrs · 33,889 cycles

RT SIDE SEAT RAIL HAS THREE EACH INCORRECT SCREWS 1 AT FS 448 & 2 AT APPROX FS 473.00.

Part: DRAG ANGLE — CRACKED (WING) · airframe 34,601 hrs · 33,889 cycles

DRAG ANGLE ADJACENT TO LT BATTERY RIB IS CRACKED.

Part: SKIN — CHAFED (CARGO DOOR) · airframe 34,601 hrs · 33,889 cycles

UPPER CTR OF CARGO COMPARTMENT DOOR SKIN IS CHAFED.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 34,602 hrs · 33,889 cycles

PAX DOOR INTERCOSTAL UNDER PANEL 832BR CRACKED.

Part: DRAG ANGLE — CRACKED (RT WING) · airframe 33,601 hrs · 33,889 cycles

DRAG ANGLE ADJACENT TO RT BATTERY RIB IS CRACKED.

Part: STIFFENER — CRACKED (RT EXHAUST) · airframe 34,602 hrs · 33,889 cycles

RT ENG EXHAUST FAIRING 2ND STIFFENER CRACKED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 33,601 hrs · 33,889 cycles

LEFT OBLIQUE ANGLE AT AFT SIDE OF RPB CRACKED.

Part: MOUNT FITTING — CRACKED (FUSELAGE) · airframe 34,602 hrs · 33,889 cycles

LEFT LOWER HYD COMPARTMENT ACCUMULATOR FWD MOUNT CLIP CRACKED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,602 hrs · 33,889 cycles

CLIP CRACKED AT FS 484 & RBL 36.

Part: CABLE — DAMAGED (CABIN) · airframe 33,224 hrs · 32,570 cycles

EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE ROWS 9 - 12. R & R EMER FLOOR TRACK LIGHTING CABLE STRIP ASSEMBLY FROM ROW 9 - 12. OPERATIONS CHECKED GOOD AT THIS TIME. IAW SUPP 13-022 & AMM 33-51-01.

Part: HYDRAULIC SYSTEM — LOW PRESSURE (NR 2) · airframe 27,322 hrs · 27,377 cycles

HYD 2 LO PRESS CAUTION MSG DURING DESCENT. COMPLIED WITH QRH. HYD 2 QTY WENT TO ZERO. EDP RAN FOR 35 MINUTES WITH HYD 2 PRESS & QTY AT ZERO.

Part: DRAG BRACE — DEFECTIVE (LANDING GEAR) · airframe 25,919 hrs · 26,012 cycles

3980 INFLIGHT RECEIVED GEAR DISAGREE MESSAGE, PERFORMED QRH & LANDED NORMALLY, GEAR HANDLE IN RETRACT POSITION BTMS READING VISIBLE APPROXIMATELY 20 SECONDS BEFORE NLG UNSAFE. R & R DRAG BRACE. FERRIED FOR EMERGENCY HANDLE MOD. SERVICE BULLETIN COMPLIANCE.

Part: DOUBLER — GOUGED (HORIZ STAB) · airframe 30,031 hrs · 24,699 cycles

HORIZONTAL STAB LT LOWER H STA PIN DOUBLER HAS NUMEROUS GOUGES. R & R DOUBLER IAW SRM.

Part: SILL — CORRODED (PAX DOOR) · corrosion level 2 · airframe 30,031 hrs · 24,699 cycles

PAX DOOR LOWER SILL IS CORRODED. REMOVED CORRECTED SILL AND INSTALLED NEW SERVICEABLE LOWER FLOOR SILL.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,031 hrs · 24,699 cycles

CORROSION ON FWD & AFT SIDE OF FS349 FRAME LWR STR 25R-25L. R & R FRAME FS 349 LWR.

Part: SEAT TRACK — WORN (COCKPIT) · airframe 30,031 hrs · 24,699 cycles

PILOT AND COPILOT SEAT TRACK FRONT SECTIONS WORN BEYOND REPAIRABLE LIMITS. C/W CARD NR/0001, SB 601R-53-022 INSTALLATION OF FWD SEAT TRACK SECTIONS.

Part: TRUNNION — NICKED (RT MLG) · airframe 30,031 hrs · 24,699 cycles

AFTFACE OF RT MLG AFT TRUNNION HAS NICKS. REWORKED AFT FACE OF RT MLG AFT TRUNNION IAW REO 601R-57-21-1942, REV.

Part: TRUNNION — DAMAGED (RT MLG) · airframe 30,031 hrs · 24,699 cycles

RIGHT MLG FWD TRUNNION ON INBD SIDE. REWORKED RT MLG FWD TRUNNION AT INBD SIDE IAW REO 601R-57-21-1942, REV.

Part: TRUNNION — GOUGED (RT MLG) · airframe 30,031 hrs · 24,699 cycles

AFT FACE OF RT FWD MLG TRUNNION FOUND GOUGES UNDER BUSHING FLANGE. REWORKED RT MLG FWD TRUNNION AFT FACE IAW REO 601R-57-21-1939, REV.

Part: SILL — CORRODED (FUSELAGE) · airframe 30,031 hrs · 24,699 cycles

DOOR SILL IS CORRODED ON TOP AND BOTTOM SURFACE FROM FS621 TO FS559+112. REMOVED CORROSION BETWEEN FS559+112 AND 589. REMOVED UNSERVICEABLE SECTION OF FLOOR LANDING BETWEEN FS581 TO 621, FABRICATED AND INSTALLED NEW SERVICEABLE SECTION OF CARGO DOOR FLOOR LANDING BETWEEN FS 581 AND 621.

Part: SKIN — DENTED (TE FLAP) · airframe 30,031 hrs · 24,699 cycles

DENT IN LOWER INBD SKIN OF RT INBD FLAP. REPAIRED DENT IAW EA 12-2013-277.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,031 hrs · 24,699 cycles

CORROSION FOUND ON FLOOR SUPPORT STRUCTURE AT FS349 BELOW PAX DOOR AFT ANCHOR FITTING CONTINUES ON STRUCTURE BELOW FLOOR LEVEL 3 LOCATIONS WITHIN LIMITS 1 LOCATION OUT OF LIMITS REQ'S REO. BLENDED SMOOTH IAW REO 601R-53-21-2435.

Part: CLEAT — CORRODED (FUSELAGE) · airframe 30,031 hrs · 24,699 cycles

CORROSION FOUND ON PAX DOOR LOWER SILL CLEATS FWD & AFT. R & R PAX DOOR SILL CLEATS FWD & AFT IAW SRM 51-40-11 & SRM 51-42-06.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,031 hrs · 24,699 cycles

CORROSION FOUND ON RIGHT FLOOR SILL DIRECTLY FWD OF SERVICE DOOR AT FS 305.00 TO FS 310 MEASUREMENTS AFFECTED ARE 0.5" X 0.5" AROUND FASTENER HOLES. REMOVED CORROSION AND FOUND MATERIAL LOSS GREATER THAN ALLOWABLE LIMITS IAW SRM 51-21-06, TR 53-27. R & R PART.

Part: SKIN — DENTED (TE FLAP) · airframe 30,031 hrs · 24,699 cycles

LEFT INBD FLAP DENT ON LOWR SKIN AFT OF OTBD HINGE ARM. REPAIRED LT INBD FLAP LOWER SKIN IAW SRM 57-52-00, REPAIR NR 3.

Part: ACCESS PANEL — CORRODED (WING) · airframe 30,031 hrs · 24,699 cycles

PITTING FOUND ON FUEL ACCESS PANEL 640BB HOLE NR 1 CUT OUT. BLEND & RESTORE FINISH IAW REO 601R-57-21-030, REV K.

Part: FLOOR SUPPORT — CRACKED (BS 280) · airframe 30,031 hrs · 24,699 cycles

PAX CABIN FLOOR SUPPORT FS 280. RBL 9 INBD ANGLE IS CRACKED. REMOVED & REPLACED ANGLE IAW REO 601R-53-41-059.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 30,031 hrs · 24,699 cycles

CLIP ANGLE IS CRACKED AT FS 484 AND LBL9. R & R CRACKED CLIP ANGLE.

Part: FLOOR SUPPORT — CRACKED (BS 280) · airframe 30,031 hrs · 24,699 cycles

PAX CABIN FLOOR SUPPORT FS 280 LBL 9 INBD ANGLE IS CRACKED UPPER. R & R ANGLE .

Part: ANGLE — CRACKED (FUSELAGE) · airframe 30,031 hrs · 24,699 cycles

CLIP ANGLE IS CRACKED AT FS 484 AND LBL 9. R & R CLIP ANGLE.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 30,031 hrs · 24,699 cycles

CLIP ANGLE CRACKED AT FS 484 AND RBL 36. R & R CLIP ANGLE.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 29,893 hrs · 29,338 cycles

AT FLIGHT LEVEL 180 F/O'S WINDSHIELD OUTER PANE SHATTERED. C/W QRH, DETERMINED THE PRESSURE VESSEL HAD NOT BEEN COMPROMISED AND THE FLIGHT COULD SAFELY CONTINUE TO CLT. DECLARED EMERGENCY, RECEIVED PRIORITY HANDLING TO CLT. ATC OFFERED A DESCENT TO 10000 FEET. LANDED AT 46,400 LBS BRAKE TEMPS 3-3-3-3 NORMAL LANDING. REMOVED AND REPLACED F/O'S WINDSHIELD IAW AMM 56-11-01, OPS/LEAK CHECK GOOD.

Part: ECU — MALFUNCTIONED (TE FLAP) · airframe 29,467 hrs · 28,916 cycles

FLAP FAIL AT ZERO DEGREES WHEN FLAPS SELECTED TO 8 DEGREES. PERFORMED FLAP RESET PROCEDURE IAW AWAC SUP 98-018E BOX 12. FLAPS RESET PLACRD AND PLACED ON MEL. REMOVED AND REPLACED FECU IAW AMM 27-51-05. OPS CHECK GOOD. REMOVED PLACARDS, REMOVED FROM MEL.

Part: WARNING SYSTEM — ACTIVATED (TE FLAP) · airframe 23,706 hrs · 23,835 cycles

RECEIVED FLAPS FAIL CAUTION MESSAGE AFTER TAKEOFF AT ZERO DEGREES. COMPLIED WITH QRH, AIR RETURN TO PHL. LANDED AT 46,700 LBS, NORMAL LANDING. DECLARED EMERGENCY.

Part: INDICATOR — MALFUNCTIONED (COCKPIT) · airframe 23,126 hrs · 23,252 cycles

STANDBY HORIZON INDICATED 20 DEGREES RIGHT BANK AND 5 DEGREES PITCH UP WHEN STRAIGHT AND LEVEL. REMOVED AND REPLACED INDICATOR IAW AMM 34-33-01. OPS CHECK GOOD.

Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 22,928 hrs · 23,067 cycles

AT 1000 FT, FELT AND HEARD BANG AND SHUTTER RT EGT SHOT INTO RED HIGH 900'S REDUCED THRUST ON RT ENG EGT RETURNED TO GREEN VIB ICON ON N2 EVEN AT IDLE, PERFORMED PRECAUTIONARY SHUTDOWN IAW GRH. ALL PARAMETERS NORMAL ENGINE WAS NOT WINDMILLING. REMOVED AND REPLACED RIGHT ENGINE ASSY IAW AMM 71-00-00, RUNS AND LEAK AND OPS CHECK AND ALL LRU'S CHECK GOOD. ENGINE RUNS ARE ALL IN PROMITERS IAW AMM 71-00-00. S/N OFF 950364 S/N ON 872453 PC 72 10 40.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 28,063 hrs · 27,533 cycles

AFTER DEPARTURE, SELECTING FLAPS FROM 8 TO 0 DEG. RECEIVED FLAP FAIL CAUTION MESSAGE. FLAP FAILED AT 0 DEG. CIRCUIT BREAKER RESET FAILED.

Part: APU — CONTAMINATED · airframe 21,465 hrs · 21,564 cycles

SMOKE IN COCKPIT AND CABIN AFTER TAKEOFF, PRIOR TO FLAP RETRACTION, SECURED PACKS, SMOKE CLEARED. PACKS OPERATING OFF OF APU. FOUND APU COMPARTMENT FLOODED WITH TYPE 4 GLYCOHOL, CLEANED FLUID. INSPECTED ACFT, NO DAMAGE NOTED. PERFORMED PACK & DUCT CLEARING IAW SUPP 09-037A, PAC OPS GOOD.

Part: APU — SMOKE · airframe 21,344 hrs · 21,452 cycles

ON DEPARTURE, VISABLE SMOKE ENTERED COCKPIT ALONG WITH ACRID ODOR. SMOKE CLEARED WHEN COMPLETED. LANDED OVERWEIGHT, LANDING WEIGHT 50170. INSPECTED AND FOUND GLYCOL IN APU AREA, CLEANED AREA UP AND RAN WITH NO RE-OCCURANCE OF SMOKE REF LP 229736/2 FOR DFDR DOWN LOAD.

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 25,450 hrs · 24,825 cycles

CARGO TRACK AND HARDWARE CORRODED AT FS 559.0+80 TO FS 559+112 LBL 27.0, . REMOVED UNSERVICEABLE FLOOR TRACK AND INSTALLED SERVICEABLE SEAT TRACK ON FS 559.0+80 TO FS 559.0+112 LBL 27.0, IAW AMM 53-01-11.

Part: BRACKET — CRACKED (RT NACELLE) · airframe 25,450 hrs · 24,825 cycles

RT SET PIPE FAIRING, FIRE LOOP SHIELD BRACKET NR 1, NR 2 AND NR3 ARE CRACKED. R & R BRACKETS (3EA) IAW SRM 51-42-06.

Part: SKIN — CHAFED (RT MLG DOOR) · airframe 25,450 hrs · 24,825 cycles

RT MLG DOOR L/E IS CHAFED IN 3 PLACES. REPAIRED IAW REO 601R-52-82-102.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · corrosion level 2 · airframe 25,450 hrs · 24,825 cycles

CARGO FLOOR SUPPORT CORRODED LBL 27.0, FS 621.0 TO FS574.0. R & R IAW SRM 51-40-11 & REO 601R-53-61-3778.

Part: SILL — CRACKED (BS 621) · airframe 25,450 hrs · 24,825 cycles

WHILE PERFORMING LPI OF CARGO DOOR C/O FLOOR SILL, FOUND LT FS 621 FLOOR SUPPORT ANGLE CRACKED. REPAIR IAW REO 601R-53-61-117, REV C.

Part: SKIN — CHAFED (LT NACELLE) · airframe 25,450 hrs · 24,825 cycles

LT ENG LOWER CORE COWL HAS 3 CHAFE MARKS THRU SKIN CUT OUT DAMAGE SECTION IAW REO 601R-71-12-4059 AND APPLY EA934NO ADHESIVE TO AREA.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 25,450 hrs · 24,825 cycles

FUEL PANEL C/O 550EB HAD CORROSION WORKED IAW REO 601R-57-21-030.

Part: PANEL — CHAFED (RT PYLON) · airframe 25,450 hrs · 24,825 cycles

PANEL 422DB HAS KNIFE EDGE (QTY 2). R & R SEPARATOR PANELS IAW SRM 51-42-06.

Part: SKIN — GOUGED (RT MLG DOOR) · airframe 25,450 hrs · 24,825 cycles

RT MLG DOOR HAS GOUGE ON INNER SKIN BLENDED DAMAGE EVEN ON RT MLG DOOR IAW REO 601R-52-82-311. TREATED IAW SRM 51-21-11, 51-25-06, AND 51-25-16.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 25,450 hrs · 24,825 cycles

LT FS 484, CLIP CRACKED AT LBL 27.0. R & R LT FS 484 CLIP IAW SRM 51-42-06 & 51-42-21.

Part: SILL — CORRODED (BS 424) · airframe 25,450 hrs · 24,825 cycles

LIGHT CORROSION APPEARING IN AREAS OF LT FLOOR SILL FS 409.00+128 TO FS 559.00 PREVIOUSLY REPAIRED IAW REO 601R-53-41-666. REPAIRED CORROSION DAMAGE ON FLOOR ANGLE AT LBL 36.0, FS 424.00 AND LBL 36.0, FS 439.0 IAW 601R-53-41-666, REV B.

Part: SEAT TRACK — CORRODED (BS 409-559) · corrosion level 2 · airframe 25,450 hrs · 24,825 cycles

RT SIDE SEAT RAIL HAS SURFACE CORROSION FROM FS 409+128 TO FS 559.0+48 IN VARIOUS PLACES. REMOVED UNSERVICEABLE SEAT RAILS, FABRICATED, NEW SERVICEABLE SEAT RAILS.

Part: BRACKET — CRACKED (RT NACELLE) · airframe 25,450 hrs · 24,825 cycles

RT ENGINE NOSE INLET FAN CASING WIRE HARNESS BRACKET CRACKED 8 O`CLOCK POSITION AFT END. REPAIRED RT HOSE INLET FAN CASING WIRE HARNESS BRACKET CRACKED AT 8 O`CLOCK POSITION BY INCORPORATING REO 601R-71-61-3941.

Part: DOOR FRAME — CRACKED (PAX DOOR) · airframe 25,450 hrs · 24,825 cycles

PAX DOOR FRAME 338.00 IS CRACKED NEAR LWR TORQUE TUBES. REMOVED CRACKED FRAME AT FS 338.00 AT LOWER TORQUE TUBES AND INSTALLED NEW SECTION OF FRAME IAW B/A REO 601R-52-11-402, REV H.

Part: TORQUE BOX — CRACKED (THRUST REVERSER) · airframe 25,450 hrs · 24,825 cycles

RT ENGINE TORQUE BOX AFT FLANGE CRACKED AT FASTENER LOCATION 5 O`CLOCK. REPAIRED IAW REO 601R-78-34-2527, REV B.

Part: FLANGE — CRACKED (THRUST REVERSER) · airframe 25,450 hrs · 24,825 cycles

LT ENGINE TORQUE BOX FLANGE CRACKED AT 7 O`CLOCK POSITION BELOW SKIN PANEL BRACKET. REPAIRED IAW REO 601R-78-34-2527, REV B.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 25,450 hrs · 24,825 cycles

CRACKED CLIP AT FS 484.0, RBL 27.0 PN 601R31171-009 CRACKED FROM RIVET TO INBD CORNER. INSTALLED SERVICEABLE REPLACEMENT PN 601R31171-009.

Part: SKIN — CRACKED (RT MLG DOOR) · airframe 25,450 hrs · 24,825 cycles

RT MLG DOOR HAS CRACK AT HINGE SHIELD. REPAIRED RT MLG DOOR HINGE SHIELD IAW REO 601R-52-82-310.

Part: SEAT TRACK — CORRODED (BS 364-559) · corrosion level 2 · airframe 25,450 hrs · 24,825 cycles

LT SIDE SEAT RAIL HAS SURFACE CORROSION FROM FS 409 & 559.0 + 80 IN VARIOUS PLACES. REMOVED UNSERVICEABLE SIDE SEAT RAILS, FABRICATE NOW REPLACEMENT SIDE REAILS AND INSTALL.

Part: HINGE — GOUGED (RT ELEVATOR) · airframe 25,450 hrs · 24,825 cycles

RT ELEVATOR NR 2 HINGE THAT ATTACHES TO HORIZ STABILIZER GOUGED FROM TOOLING. REPAIR IAW REO 601R-55-11-372.

Part: DOUBLER — BENT (BS 280 BULKHEAD) · airframe 25,450 hrs · 24,825 cycles

DOUBLER ON AFT SIDE OF RT 280 BULKHEAD BENT. R & R DOUBLER ON AFT SIDE OF RT 280 BULKHEAD IAW SRM 51-42-06.

Part: LINK — CHAFED (THRUST REVERSER) · airframe 25,450 hrs · 24,825 cycles

LT ENGINE NR 10 BLOCKER DOOR LINK ARM CHAFING DAMAGE BLENDED CHAFED AREA LT NR 10 BLOCKER DOOR LINK ARM MATERIAL LOSS .007 REMAINING MATERIAL .193. FOUND TO BE WITHIN LIMITS IAW REO 601R-78-30-2940.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 25,450 hrs · 24,825 cycles

PAX DOOR AFT DRAG ANGLE TOP CLIP CRACKED. REMOVED CRACKED CLIP AND INSTALLED NEW SERVICEABLE CLIP PN 601R31907-299 IAW SRM 51-42-06.

Part: HINGE — GOUGED (RT ELEVATOR) · airframe 25,450 hrs · 24,825 cycles

RT ELEVATOR HINGE GOUGED FROM TOOLING. REPAIRED IAW REO 601R-55-21-321.

Part: FITTING — GOUGED (LT INBD FLAP) · airframe 25,450 hrs · 24,825 cycles

PRIOR TO REMOVAL OF HINGE BOX WS 80.50 (LT) FOUND AFT LUG TO HAVE DAMAGE. REPAIRED IAW REO 601R-57-21-1448.

Part: ATTACH FITTING — CORRODED (PAX DOOR) · corrosion level 2 · airframe 25,450 hrs · 24,825 cycles

AFT CLEAT BY PAX DOOR IS CORRODED, REMOVED AND REPLACED.

Part: FITTING — GOUGED (RT INBD FLAP) · airframe 25,450 hrs · 24,825 cycles

UPON REMOVAL OF INBD HINGE BOX (RT) WS 80.50. FOUND AFT LUGS TO HAVE DAMAGE. REPAIRED IAW REO 601R-57-21-1448.

Part: HINGE — GOUGED (HORIZONTAL STAB) · airframe 25,450 hrs

LT ELEVATOR CENTER HINGE THAT ATTACHES TO HORIZ STABILIZER GOUGED FROM TOOLING BLEND. REPAIR IAW REO 601R-55-11-372 AND REO 601R-55-21-320.

Part: HINGE — GOUGED (PAX DOOR) · airframe 25,450 hrs · 24,825 cycles

AFT END OF FUSELAGE HALF OF PAX DOOR HINGE IS GOUGED. REPAIRED AFT END OF FUSELAGE, HALF OF PAX DOOR HINGE BY BLENDING PAX HINGE (FUSELAGE HALF) AFT LEAD TO DEPTH OF .021 FOUND TO BE WITHIN LIMITS IAW REO 601R-53-21-814, TYPE IV DISPOSITION.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 25,450 hrs · 24,825 cycles

PAX DOOR INTERCOSTAL UNDER PAX DOOR PANEL 832GL IS CRACKED. REMOVED CRACKED INTERCOSTAL UNDER PAX DOOR PNL 832GL, THEN FABRICATED AND INSTALLED NEW INTERCOSTAL IAW SRM 52-11-14, 51-42-06, 51-24-21, 51-25-06, 51-25-16.

Part: CARGO TRACK — CORRODED (BS 574-621) · corrosion level 2 · airframe 25,450 hrs · 24,825 cycles

CARGO FLOOR TRACK AND HARDWARE FS 574.0, LBL 9.0 AND FS 621.0, LBL 9.0, 2 EA HAVE CORROSION. REMOVED UNSERVICEABLE FLOOR TRACK AND HARDWARE AND INSTALLED SERVICEABLE SEAT TRACK AT FS 574.0, LBL 9.0 AND FS 621.0, LBL 9.0 AND SCREWS IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 409) · corrosion level 2 · airframe 25,450 hrs · 24,825 cycles

RT SIDE SEAT RAIL HAS LIGHT SURFACE LOWER FROM FS 409-FS 409+128. REPLACED UNSERVICEABLE SEAT RAIL IAW AMM 53-01-11.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 25,450 hrs · 24,825 cycles

INTERCOSTAL INSIDE PAX DOOR PANEL 832AT CRACKED. REMOVED CRACKED INTERCOSTAL INSIDE PAX DOOR AT PANEL 832AR AND INSTALLED NEW SERVICEABLE INTERCOSTAL PN 601R31902-318 AND IAW SRM 51-42-21, 51-42-06, 51-40-11.

Part: STIFFENER — CHAFED (BS 621) · airframe 25,450 hrs · 24,825 cycles

REAR PRESSURE BULKHEAD VERTICAL STIFFENER AT BL 0 IS CHAFED BY THE 10TH STAGE ISOLATION VALVE. REPAIRED DAMAGE AREA AIR PRESSURE BULKHEAD VERTICAL STIFFENER AT BL 00.0 IAW REO 601R-53-61-1523.

Part: SKIN — CHAFED (RT NACELLE) · airframe 25,450 hrs · 24,825 cycles

RT ENGINE UPPER CORE COWL T/E IS CHAFED KNIFE EDGED. REPAIRED CHAFED/KNIFE DAMAGE ON EDGE AFT T/E RT ENGINE UPPER CORE COWL IAW REO 601R-71-12-3276, REV. NC.

Part: SKIN — CHAFED (RT NACELLE) · airframe 25,450 hrs · 24,825 cycles

RT ENG TOWER CORE COWL TIE CHAFED, KNIFE EDGE. REPAIRED CHAFED/KNIFE DAMAGE ON EDGE T/E RT ENG LOWER CORE COWL IAW REO 601R-71-12-3276, REV NC.

Part: BLOCKER DOOR — CHAFED (THRUST REVERSER) · airframe 25,450 hrs · 24,825 cycles

ALL RT THRUST REVERSER BLOCKER DOORS ARE CHAFED ALONG THE BACK SEAL WHERE THEY CONTACT THE STOPS. REPAIRED DOORS NR 1 TO 5 AND 7 TO 10 ON RT T/E BLOCKER DOOR IAW CMM 78-30-00, SRS 100 AND REPLACED DOOR NR 6.

Part: ANGLE — CRACKED (BS 621) · airframe 25,450 hrs · 24,825 cycles

OBLIQUE ANGLE IS CRACKED ON RT SIDE INTERCOSTAL 3RD UP FROM BOTTOM ON REAR PRESSURE BULKHEAD. R & R OBLIQUE ANGLE IAW SRM 51-42-21.

Part: ATTACH FITTING — CORRODED (PAX DOOR) · corrosion level 2 · airframe 25,450 hrs · 24,825 cycles

4 EA CORRODED CLEATS AT LOWER SECTION OF PAX DOOR DRAINAGE RAMP AREA "2 EA" AT FS 320.10 AND FS 338.00 BEYOND LIMITS. REMOVED 4EA CORRODED CLEATS FROM PAX DOOR AT FS320.10 AND 338.00. THEN INSTALLED 4 EA NEW CLEATS PN 600-31902-275, 600-31902-276.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 23,852 hrs · 23,164 cycles

FS559, RBL9 OTBD ANGLE CRACKED AT LOWER EDGE. REPAIRED FS559 PRESSURE BULKHEAD RBL9 OTBD ANGLE BY FULL INCORPORATION OF REO 601R-53-41-260 REV E & REO 601R-53-41-609, REV B AND DEVIATION E ON LT AND RT SIDES, LBL 27 TO RBL 27.

Part: UNKNOWN — ODOR (CABIN) · airframe 22,159 hrs · 21,410 cycles

STRONG ODOR OF ELECTRICAL ODOR IN COCKPIT ON DESCENT. INSPECTED AC FWD CABIN AND COCKPIT LIGHTING, COOLING FAN AND DISPLAY SCREENS. OPERATED AC PACKS FROM BOTH ENGINES AND APU AIR. ALSO INSPECTED GALLEY AND COFFEEMAKERS, NO ELECTRICAL ODOR OBSERVED. AC IS OK FOR SERVICE. (K)

Part: BRACKET — CRACKED (NOSE COWL) · airframe 20,840 hrs · 20,127 cycles

RT ENG NOSE COWL ALIGNMENT STOP BRACKET FOUND CRACKED. RT ENG NOSE COWL ALIGNMENT BRACKET REMOVED FOR NUT PLATE INSTALLATION IAW SRM 51-42-06. (K)

Part: SILL — CRACKED (BS 574) · airframe 20,840 hrs · 20,127 cycles

MID HINGE SUPPORT OF CARGO DOOR LWR SILL PLATE FOUND CRACKED. MID HINGE SUPPORT OF CARGO DOOR LOWER SILL PLATE REPLACED BY A NEW ONE IAW SRM 51-42-06. (K)

Part: STRUCTURE — CORRODED (BS 412) · corrosion level 2 · airframe 20,840 hrs · 20,127 cycles

CORROSION FOUND BTW FS 412.0+128 TO FS 559.0, RBL 46.084. CORROSION BTW FS 412+128 TO 559.0, RBL 46.084 REMOVED IAW REO 601R-53-41-666. (K)

Part: SUPPORT BRACKET — CRACKED (THRUST REVERSER) · airframe 20,840 hrs · 20,127 cycles

MWC 136507-88- RT ENGINE T/R UPPER FWD PYLON TRACK SUPPORT BRACKET CRACKED. RT ENGINE T/R UPPER FWD PYLON TRACK SUPPORT BRACKET REPLACED IAW SRM 51-42-06. (K)

Part: SEAT TRACK — CORRODED (BS 364-394) · corrosion level 2 · airframe 20,840 hrs · 20,127 cycles

MWC 136507-295 - CORRODED SEAT TRACK FOUND AT F/S 364.00 TO F/S 394.00 LBL 9, W/L 74.50. SEAT TRACK REPLACED BTW F/S 364.00, LBL 9.0, W/L 74.50 IAW AMM 53-01-11-000-802 AND AMM 53-01-11-400-802. (K)

Part: SKIN — DENTED (TE FLAP) · airframe 20,840 hrs · 20,127 cycles

MWC 136507-52 - DENT FOUND ON LT INBD FLAP LOWER SKIN W/S 65.0 (9.0 X 8.0 X .160 DEEP). LT INBD FLAP LOWER SKIN W/S 65.0. REPAIRED IAW REO 601R-57-52-1447. (K)

Part: HANDLE — CRACKED (CARGO DOOR) · airframe 20,840 hrs · 20,127 cycles

CRACK FOUND ON CARGO DOOR HANDLE ASSY (CRACK LENGTH IS .250). CARGO DOOR HANDLE ASSY REPLACED IAW SRM 51-40-11 AND SRM 51-42-21. (K)

Part: HANDLE — CRACKED (E/E BAY DOOR) · airframe 20,840 hrs · 20,127 cycles

CRACK FOUND ON MAIN AVIONIC ACCESS DOOR HANDLE ASSY CRACK LENGTH .500. NEW MAIN AVIONIC ACCESS DOOR HANDLE ASSY INSTALLED IAW SRM 51-42-06. (K)

Part: ATTACH FITTING — CRACKED (INTERCOSTAL) · airframe 20,840 hrs · 20,127 cycles

CRACK FOUND ON INTERCOSTAL CLIP FS 625, STR 14L (CRACK LENGTH IS .500) INTERCOSTAL CLIP REPLACED IAW SRM 51-42-06. (K)

Part: ATTACH FITTING — CRACKED (BS 625)

CRACK FOUND ON INTERCOSTAL CLIP F.S. 625, STR 14R (CRACK LENGTH IS .500) INTERCOSTAL CLIP REPLACED AT FS 625 AND STGR 14R IAW SRM 51-42-06. (K)

Part: SILL — CRACKED (BS 605) · airframe 20,840 hrs · 20,127 cycles

MWC 136507-149 - AFT CARGO DOOR LOWER SILL CRACKED AT FS 605.00. AFT CARGO DOOR LOWER SILL REPAIRED AT FS 605.00 IAW REO 601R-53-61-433. (K)

Part: CHANNEL — CRACKED (CARGO DOOR RAIL) · airframe 20,840 hrs · 20,127 cycles

MWC 136507-203 - CRACK FOUND ON CHANNEL OF CARGO DOOR RAIL AND FRAME FS 574 CRACK LENGTH IS .500 CHANNEL OF CARGO DOOR RAIL AND FRAME FS 574 REPLACED IAW SRM 51-42-06. (K)

Part: SILL — CORRODED (BS 319-349) · corrosion level 2 · airframe 20,840 hrs · 20,127 cycles

MWC 136507-228- SERVICE DOOR LOWER SILL PLATE FOUND CORRODED. SERVICE DOOR LOWER SILL PLATE REPLACED IAW SRM 51-45-00 AND 51-21-16. (K)

Part: STRUCTURE — DAMAGED (RT MLG DOOR) · airframe 20,840 hrs · 20,127 cycles

RT MLG DOOR FWD AND AFT EDGE ARE GROOVED. REO 601R-52-82-232 PERFORM FOR FWD EDGE OF RT MLG DOOR AND BLEND OUT DAMAGE (51-12-00) FOR AFT EDGE OF RT MLG DOOR, EDDY CURRENT PERFORMED ON CUTOUT AND BLENDED AREA. (K)

Part: BULKHEAD — CRACKED (BS 621) · airframe 20,840 hrs · 20,127 cycles

CRACK FOUND ON AFT PRESSURE BULKHEAD FWD FACE AT F/S 621.00, BL 0.0, W/L 89.0 (.075 LONG) CRACK AFT PRESSURE BULKHEAD FS 621.00, BL 0.0, REPAIRED IAW REO 601R-53-61-1285. (K)

Part: CARGO TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 20,840 hrs · 20,127 cycles

AFT CARGO TIE DOWN TRACK AT FS 559+112, RBL 9.00 CORRODED. TIE DOWN (RAIL) REPLACED IAW SRM 51-41-00. (K)

Part: HANDLE — CORRODED (ESCAPE HATCH) · airframe 20,961 hrs · 20,241 cycles

CREW ESCAPE HATCH OUTER HANDLE ASSY CORRODED. CREW ESCAPE HATCH OUT HANDLE ASSY REPLACED IAW AMM 52-22-03-400-801. (K)

Part: CARGO TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 20,840 hrs · 20,127 cycles

MWC 136507- 156 - AFT CARGO TIE DOWN TRACK AT FS 559+112, RBL 9.0 CORRODED. TIE DOWN (RAIL) REPLACED IAW SRM 51-41-00. (K)

Part: BULKHEAD — CRACKED (BS 280) · airframe 20,840 hrs · 20,127 cycles

RT PILOTS BULKHEAD FS 280.00, RBL 9.0 FOUND CRACKED. RT PILOTS BULKHEAD FS 280.00, RBL 9.0 CRACKED SECTION CUT OUT AND FILLER ANGLE FABRICATED AND REPAIR PERFORMED IAW REO 601R-53-11-171, REV D. (K)

Part: BULKHEAD — CRACKED (BS 280) · airframe 20,840 hrs · 20,127 cycles

MWC 136507-63- LT PILOTS BULKHEAD FS 280.00, LBL 9.0 FOUND CRACKED. LT PILOTS BULKHEAD FS 280.00, LBL 9.0 CRACKED SECTION CUT OUT AND FILLER ANGLE FABRICATED AND REPAIR PERFORMED IAW REO 601R-53-11-171, REV D. (K)

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 20,840 hrs · 20,127 cycles

CRACK FOUND ON INTERCOSTALS FS 484.00, RBL 27.00 AND RBL 36.00. REPAIR PERFORMED ON INTERCOSTAL FS 484.00, RBL 27.00 AND RBL 36.00 IAW REO 601R-53-41-059, REV A. (K)

Part: BULKHEAD WEB — CRACKED (BS 202) · airframe 20,840 hrs · 20,127 cycles

MWC 136507-49 -CRACK FOUND AT FS 202.75 AT BL 23.71 PRESSURE BULKHEAD AROUND PARKING BRAKE. REPAIR PERFORMED ON FWD PRESS BULKHEAD AT BL 23.71 AROUND PARKING BRAKE IAW REO 53-11-563 AND REO 601R-53-11-166. (K)

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 19,975 hrs · 19,328 cycles

LOG 193688/3 - RE3866 - RECEIVED FLAPS FAIL CAUTION MSG AT FIRST DETENT OF 8. FLAP INDICATOR INDICATES ZERO. C/W QRH LANDED WITH NORMAL BRAKING. CORRECTIVE ACTION IN PROGRESS. (K)

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 19,859 hrs · 19,214 cycles

LOG 193677/1 FLAPS FAIL CAUTION MSG IN FLIGHT. COMPLIED WITH QRH LANDED FLAPS O DEGREES WITH NORMAL BRAKING.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 18,803 hrs · 18,184 cycles

IN DESCENT, AT FL130, 310K IAS, RT WINDSHIELD INNER PANE CRACKED. REMOVED AND REPLACED RT WINDSHIELD. OPS AND LEAK CHECK GOOD. (S)

Part: ENGINE — SHUTDOWN (NR 2) · airframe 18,763 hrs · 18,146 cycles

AIR DIVERT TO IAD, ENGINE NR 2 SHUTDOWN ON TAKEOFF. FELT DISTINCT POP ON THROTTLE CONTROLS. ENGINE SPOOLED UP NORMALLY. UPON LEVEL-OFF, FIRST OFFICER ATTEMPTED TO REDUCE POWER AND RT ENGINE FAILED TO RESPOND. FLEW AROUND ON BOTH ENGINE FOR ABOUT 10 MINUTES BEFORE PERFORMING A PRECAUTIONARY SHUTDOWN. USED RT ENGINE FIRE PUSH TO SHUTDOWN THE ENGINE. DID NOT PUSH THE FIRE BOTTLE BUTTON. CORRECTIVE ACTION IN PROGRESS. (A)

Part: PUMP — INOPERATIVE (HYDRAULIC SYS) · airframe 17,217 hrs · 16,672 cycles

HYD NR 1 LOW PRESS CAUTION MESSAGE IN FLIGH, HYD 1 QUANTITY READ ZERO FOR 35 MINUTES. PERFORMED PRECAUTIONARY SHUTDOWN OF NR 1 ENGINE AFTER LANDING. FOUND NR 1 SUCTION LINE CHAFED THROUGH AND PRESSURE FLEX PERMASWEDGE REPAIR, REMOVED AND REPLACED PRESSURE LINE REF AMM 29-11-52, AND REMOVED AND REPLACED EDP. LINES LEAK CHECK GOOD. (K)

Part: UNKNOWN — ODOR

NOTICED A STRONG FUEL ODOR FROM EWR, CONTINUED TO DETECT A FUEL OR EXHAUST ODOR DURING CLIMB. DIVERTED TO PHL. NO SMOKE, HOWEVER FLIGHT ATTENDANT AND PASSENGER NOTICED ODOR. REMOVED AND REPLACED APU INLET BELLOWS ASSEMBLY IAW AMM 49-10-00, OPS CHECK GOOD. NO EVIDENCE OF FORWARD FUEL ODOR. (M)

Part: UNKNOWN — MALFUNCTIONED (FLT CONTROLS)

ABORTED TAKEOFF PRIOR TO 80 KNOTS DUE TO TAKEOFF WARNING FOR CONFIG TRIM, CONFIG SPOILERS AT WEIGHT OF APPROXIMATELY 46,000 LBS. WHEN MESSAGE CLEARED AILERON AND RUDDER TRIM INDICATIONS FLUTTERED FROM WHITE TO GREEN. PERFORMED NUMEROUS, OPS CHECKS OF FLIGHT CONTROLS, PERFORMED TAXI RUN, NO DEFECTS NOTED AT THIS TIME, ALL INDICATIONS NORMAL. (M)

Part: PCU — MALFUNCTIONED (SPOILERS)

ON CLIMB-OUT, MOMENTARILY UNCOMMANDED ROLL TO RIGHT OCCURRED FOLLOWED BY SPOILERON FAULT STATUS MESSAGE. FLIGHT CONTROL PAGE INDICATES RIGHT SPOILERON WHITE. REMOVED AND REPLACED RT OUTBOARD SPOILERON PCU IAW AMM 27-62-02-943-004. (M)

Part: BULKHEAD — CRACKED (BS 621) · airframe 16,043 hrs · 15,532 cycles

REAR PRESSURE BULKHEAD WEB AT RBL 9.5 NL 85.5 HAS AN INDICATION NOTED APPROX .5 INCHES IN LENGTH IN VERTICAL DIRECTION FAILED NDT INSPECTION. [07-31-07] MAINT REPAIRED REAR PRESSURE BULKHEAD WEB AT RBL 9.5, WL 85..5 BY CUTTING AWAY DAMAGE, FABBIN REPAIR PARTS AND INSTALLING IAW REO 601-53-61-1285. (K)

Part: SKIN — CRACKED (FUSELAGE) · airframe 16,043 hrs · 15,532 cycles

NLG AFT DOOR CUTOUT CRACKED IN LT AND RT RADIUS .5 INCH EACH SIDE. (K)

Part: SKIN — CRACKED (BS 220) · airframe 16,043 hrs · 15,532 cycles

NLG AFT DOOR CUTOUT CRACKED IN LT AND RT RADIUS .5 INCH EACH SIDE. MAINTENANCE REPAIRED CRACKED AREAS IAW REO 601R53-11-010, REV C. (K)

Part: RIB — CRACKED (RT WING) · airframe 16,043 hrs · 15,532 cycles

RT WING STR 53.60 BATT RIB IS CRACKED 1.0 INCH ON UPPER AFT CORNER. MAINTENANCE REPAIRED IAW REO 601R-57-51-046. (K)

Part: RIB — CRACKED (LT WING) · airframe 16,043 hrs · 15,532 cycles

LT WING STR 53.60 BATTERY RIB IS CRACKED 1.0 INCH ON UPPER AFT CORNER. MAINTENANCE REPAIRED IAW REO 601R-57-51-046. (K)

Part: SKIN — CORRODED (LT WING) · airframe 16,043 hrs · 15,532 cycles

LT WING PLANK AT PANEL 540BB HAS CORROSION APPROX .004 DEEP X 4 INCHES LONG X .2500 INCHES WIDE IN NON-CRITICAL AREA. MAINTENANCE PERFORMED MAJOR REPAIR TO WING PLANK ACCESS HOLE AT WS 54.897 (LT) BY REMOVING CORROSION IN NON-CRITICAL AREAS IAW REO 601R-57-21-030, REV F. (K)

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 16,043 hrs · 15,532 cycles

LT FS 484 INTERCOSTAL ANGLE CRACKED APPROX .2 INCH LONG LBL 27 AT FLOORBEAM. MAINTENANCE REPAIRED IAW CRJ 200 SRM 51-42-21 AND BSC STANDARD REPAIR NR 601R-53-0029B. (K)

Part: PANEL — CORRODED (RT WING) · airframe 16,043 hrs · 15,532 cycles

RT WING PLANK AT PANEL 640BB HAS CORROSION APPROX .004 DEEP X 4 INCH LONG X .2500 INCH WIDE IN NON-CRITICAL AREAS. MAINTENANCE PERFORMED MAJOR REPAIR TO WING PLANK ACCESS HOLE AT WS 54.897 (RT) BY REMOVING CORROSION IN NON-CRITICAL AREAS OF HOLE IAW REO 601R-57-21-030, REF F. (K)

Part: BRACKET — CORRODED (SILL) · airframe 16,043 hrs · 15,532 cycles

LOWER SILL JOINT BRACKET (PN 601R38335-1) CORRODED AT FS 318.70, RBL 36, WL 73. MAINTENANCE REMOVED AND REPLACED BRACKET (PN 601R38335-1) IAW CRJ 200 SRM 51-42-21. (K)

Part: ATTACH FITTING — CRACKED (FLOORBEAM) · airframe 16,043 hrs · 15,532 cycles

RT FLOORBEAM ATTACH CLIPS ARE CRACKED AT IB AND OB SIDES FS 280, RBL 9, WL 72. (K) [07-31-07] MAINTENANCE REPAIRED IAW BSC STANDARD REPAIR 601R53-0057A, AND CRJ 200, SRM 51-42-13 AND 51-42-21. (K)

Part: ATTACH FITTING — CRACKED (FLOORBEAM) · airframe 16,043 hrs · 15,532 cycles

LT FLOORBEAM ATTACH CLIPS ARE CRACKED AT IB AND OB SIDES FS 280, LBL 9, WL 72. (K) [07-31-07] MAINTENANCE REPAIRED IAW CRJ 200 SRM 51-42-13 AND 51-42-21 AND BSC STANDARD REPAIR NR 601R-53-0057A. (K)

Part: HANDLE — MALFUNCTIONED (PAX DOOR)

HANDLE WILL NOT STOW ON PASSENGER DOOR. REMOVED AND REPLACED OUTER DOOR INNER COVER AND STOW HANDLE ROLL PIN IAW 52-11-03. OPS CHECK GOOD. (M)

Part: WARNING MESSAGE — ILLUMINATED (THRUST REVERSER)

RECEIVED RIGHT REVERSER UNLOCK MESSAGE IN FLIGHT. COMPLIED WITH QRH NO YAW OR BUFFETING. COMPLIED WITH MAINTENANCE ACTION. REMOVED AND REPLACED RIGHT ENGINE STOW SWITCH AND ADJUSTED PER AMM 78-31-01. REMOVED EQUIPMENT AND RECOVERED ENGINE PERFORMED FUNCTION CHECK WITH SHOP AIR IAW 78-30-00. REMOVE FROM MEL. (M)

Part: RELIEF VALVE — MALFUNCTIONED (ANTI ICE SYS)

AFTER TAKEOFF ENTERED ICING CONDITIONS, TURNED ON LEFT AND RIGHT COWL ANTI-ICE. LEFT ICING CONDITIONS AND TURNED OFF COWL ANTI-ICE, LEFT COWL ANTI-ICE AMBER CAS MESSAGE APPEARED ON EICAS. REMOVED AND REPLACED PRESSURE RELIEF VALVE ON LEFT ENGINE IAW AMM 30-22-04. OPS CHECK GOOD. (M)

Part: STATIC INVERTER — UNSERVICEABLE · airframe 12,763 hrs · 12,340 cycles

WHILE PERFORMING SERVICE CHECK NOTECED SMOKE AND FIRE IN AUXILIARY EQUIPMENT BAY FROM WIRE BUNDLE-R LEANING TO STATIC INVERTER MOUNTED ON PRESSURE BULKHEAD. MAINTENANCE REMOVED AND REPLACED STATIC INVERTER. REWIRED STATIC INVERTER CONNECTOR PLUG AND WIRES KB1A14, KB4A20, KB4B20, KB4D20. REPLACED RELAYS 2K3KB AND 1K3KB IAW WMM 74-00-00. OPS CHECK GOOD. (K)

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 12,738 hrs · 12,317 cycles

FLOORBEAM WEB AFT ANGLE AT FS 559.00 + 48, LBL9, IS CRACKED APPROX .2500 INCH LONG, MAINTENANCE CUTOFF CRACKED FLANGE AND INSTALLED REPAIR ANGLE IAW EO. (K)

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,738 hrs · 12,317 cycles

SERVICE DOOR LOWER SILL ANGLE (PN 601R38303-225), HAS SEVERAL LARGE AREAS OF CORROSION ON SURFACE. (VERTICAL AND HORIZONTAL PLANES AND IN RADIUS.) MAINTENANCE REMOVED LOWER SILL ANGLE AND INSTALLED NEW ANGLE (PN 601R38303-253) IAW SRM. SEALED PAINTED AND APPLIED CORROSION PROTECTIVE COATING IAW SRM. (K)

Part: SKIN — CORRODED (WING) · airframe 12,738 hrs · 12,317 cycles

RT WING PLANK HOLE NR8, WS 136.676 HAS CORROSION AT IB SIDE 4 INCH L X .002-.003 INCH D AND AT AFT IB SIDE 2 INCH L X .001 INCH - .002 D. AFT IB SIDE IN CRITICAL AREA. MAINTENANCE REPAIRED CORROSION DAMAGE IAW REO, BY BLEND AND TREAT. (K)

Part: SKIN — CORRODED (RT WING) · airframe 12,738 hrs · 12,317 cycles

RT WING PLANK HOLE NR 14, WS 274.319 HAS CORROSION AT FWD OB SIDE, NR 3 INCH L X .002 INCH- .005 INCH D. NOT IN CRITICAL AREA. MAINTENANCE REPAIRED CORROSION DAMAGE IAW REO, BLEND AND TREAT. (K)

Part: SKIN — CORRODED (RT WING) · airframe 12,738 hrs · 12,317 cycles

RT WING PLANK HOLE NR12, WS 230.415 HAS CORROSION AT IB SIDE 1 INCH L X .001 INCH-.002 INCH D AND AT OB SIDE 6 INCH L X .002 INCH-.005 INCH D. NOT IN CRITICAL AREA. MAINTENANCE REPAIRED CORROSION DAMAGE IAW REO, BLEND AND TREAT. (K)

Part: SKIN — CORRODED (WING) · airframe 12,738 hrs · 12,317 cycles

RT WING PLANK HOLE NR 10, WS 188.040 HAS CORROSION AT IB FORWARD SIDE 4 INCH L X .002 INCH-.003 INCH D. NOT IN CRITICAL AREA. MAINTENANCE REPAIRED CORROSION DAMAGE IAW REO, BLEND AND TREAT. (K)

Part: SKIN — CORRODED (WING) · airframe 12,738 hrs · 12,317 cycles

RT WING PLANK HOLE NR 3, WS 32.263 HAS CORROSION AT OB SIDE 2 INCH L X .001 INCH-.002 INCH D. NOT IN CRITICAL AREA. MAINTENANCE REPAIRED CORROSION DAMAGE IAW REO, BY BLEND AND TREAT. (K)

Part: SKIN — CORRODED (WING) · airframe 12,738 hrs · 12,317 cycles

RT WING PLANK HOLE NR 1, WS 54.897 HAS CORROSION AT IB SIDE 6 INCHES L X .005 INCH - .010 INCH D AND AT OB SIDE 8 INCH L X .005 INCH - .010 INCH D. NOT IN CRITICAL AREA. MAINTENANCE REPAIRED CORROSION DAMAGE IAW REO, BY BLED AND TREAT. (K)

Part: SKIN — CORRODED (WING) · airframe 12,738 hrs · 12,317 cycles

RT WING PLANK HOLE NR 7, WS 116.366 HAS CORROSION AT IB SIDE 14 INCH L X .002 INCH- .005 INCH D AND AT OB FWD SIDE 4 INCH L X .001 INCH-.002 INCH D AND AT OB AFT SIDE 2 INCH L X .001 INCH - .002 INCH D. OB FWD IS IN CRITICAL AREA. MAINTENANCE REPAIRED CORROSION DAMAGE IAW REO, BY BLEND AND TREAT. (K)

Part: SKIN — CORRODED (WING) · airframe 12,738 hrs · 12,317 cycles

RT WING PLANK HOLE NR 5, WS 76.161 HAS CORROSION AT OB FWD SIDE 6 INCH L X .001-.002 INCH D. LOCATED IN CRITICAL AREA. MAINTENANCE REPAIRED CORROSION DAMAGE IWA REO, BY BLEND AND TREAT. (K)

Part: SKIN — CORRODED (RT WING) · airframe 12,738 hrs · 12,317 cycles

RT WING PLANK HOLE NR 13, WS 253.022 HAS CORROSION AT IB SIDE 12 INCH L X .002 INCH - .003 INCH D AND AT FWD OB SIDE 5 INCH L X .001 INCH - .003 INCH D AND AFT OB SIDE 6 INCH L X .002 INCH - .003 INCH D. FWD OB IS IN CRITICAL AREA. MAINTENANCE REPAIRED CORROSION DAMAGE IAW REO, BLEND AND TREAT. (K)

Part: SKIN — CORRODED (RT WING) · airframe 12,738 hrs · 12,317 cycles

RT WING PLANK HOLE NR 15, WS 294.048 HAS CORROSION AT IB SIDE 2 INCH L X .001 INCH-.002 INCH D AND AT FWD CENTER SIDE 2 INCH L X .002 INCH- .003 INCH D AND AT OB SIDE 1INCH L X .002 INCH-.003 INCH D. FORWARD CENTER SIDE IS IN CRITICAL AREA. MAINTENANCE REPAIRED CORROSION DAMAGE IAW REO, BLEND AND TREAT. (K)

Part: SKIN — CORRODED (LT WING) · airframe 12,738 hrs · 12,317 cycles

LT WING PLANK HOLE NR 6, WS 95.950 HAS CORROSION AT OB SIDE 12 INCH L X .002 INCH-.003 INCH D AND IB 4 INCH L X .001 INCH-.002 INCH D. NOT IN CRITICAL AREA. MAINTENANCE REPAIRED CORROSION DAMAGE IAW REO. BY BLEND AND TREAT. (K)

Part: SKIN — CORRODED (LT WING)

FOUND LEFT WING PLANK HOLE NR 16 WS 303.861 HAS CORROSION AT OUTBOARD SIDE 8 INCHES LONG BY .005 INCH AND INBOARD SIDE 7 INCHES LONG BY .002 INCH DEEP. NOT IN CRITICAL AREA. MAINTENANCE REPAIRED CORROSION DAMAGE IAW BOMBARDIER REO 601R-57-21-030 REV D BY BLEND AND TREAT. (M)

Part: SKIN — CORRODED (LT WING)

FOUND LEFT WING PLANK HOLE NR 11, WS 209.040 HAS CORROSION AT INBOARD SIDE 4 INCHES LONG BY .002 INCH - .003 INCH DEEP. NOT IN CRITICAL. MAINTENANCE REPAIRED CORROSION DAMAGE IAW BOMBARDIER REO 601R-57-21-030 REV D, BY BLEND AND TREAT. (M)

Part: PANEL — CORRODED (LT WING)

FOUND LEFT WING PLANK HOLE NR 9, WS 163 HAS CORROSION AT INBOARD SIDE 5 INCHES LONG BY .002 INCH - .003 INCH DEEP. NOT IN CRITICAL AREA. MAINTENANCE REPAIRED CORROSION DAMAGE IAW BOMBARDIER REO 601R-57-21-030 REV D, BY BLEND AND TREAT. (M)

Part: PANEL — CORRODED (LT WING)

FOUND LEFT WING PLANK HOLE NR 8, WS 136.676 HAS CORROSION AT OUTBOARD SIDE 6 INCH LONG BY .001 INCH - .002 INCH DEEP AND INBOARD SIDE 5 INCH LONG BY .001 - .002 INCH DEEP. NOT IN CRITICAL AREA. MAINTENANCE REPAIRED CORROSION DAMAGE IAW BOMBARDIER REO 601R-57-21-030 REV D, BY BLEND AND TREAT. (M)

Part: SKIN — CORRODED (LT WING)

FOUND LEFT WING PLANK HOLE NR 10, WS 188.040 HAS CORROSION AT OUTBOARD SIDE 12 INCHES LONG BY .002 INCH - .005 INCH DEEP AND INBOARD SIDE 8 INCHES LONG BY .002 INCH - .003 INCH DEEP. NOT IN CRITICAL AREA. MAINTENANCE REPAIRED CORROSION DAMAGE IAW BOMBARDIER REO 601R-57-21-030 REV D, BY BLEND AND TREAT. (M)

Part: SKIN — CORRODED (WING) · airframe 12,738 hrs · 12,317 cycles

LT WING PLANK HOLE NR 2, WS 12.245 HAS CORROSION AT IB SIDE 8 INCH L X .005 INCH D AND FORWARD SIDE 4 INCH L X .002 INCH - .003 INCH D. FORWARD SIDE IS IN CRITICAL AREA. MAINTENANCE REPAIRED CORROSION DAMAGE IAW REO, BY BLEND AND TREAT. (K)

Part: SKIN — CORRODED (WING) · airframe 12,738 hrs · 12,317 cycles

LT WING PLANK HOLE NR 3 WS 32.263 HAS CORROSION AT OB SIDE 4 INCH L X .002 INCH-.003 INCH D AND IB SIDE 1 INCH L X .003 INCH D. NOT IN CRITICAL AREA. MAINTENANCE REPAIRED CORROSION DAMAGE IAW REO, BY BLEND AND TREAT. (K)

Part: SKIN — CORRODED (WING) · airframe 12,738 hrs · 12,317 cycles

LT WING PLANK HOLE NR 5, WS 76.161 HAS CORROSION AT OB SIDE 6 INCH L X .002 INCH D AND IB SIDE 7 INCH L X .001 INCH - .002 INCH D. NOT IN CRITICAL AREA. MAINTENANCE REPAIRED CORROSION DAMAGE IAW REO, BY BLEND AND TREAT. (K)

Part: SKIN — CORRODED (LT WING)

FOUND LEFT WING PLANK HOLE NR 13, WS 253.022 HAS CORROSION AT OUTBOARD SIDE 4 INCHES LONG BY .001 DEEP - .002 INCH DEEP. NOT IN CRITICAL AREA. MAINTENANCE REPAIRED CORROSION DAMAGE IAW BOMBARDIER REO 601R-57-21-030 REV D, BY BLEND AND TREAT. (M)

Part: SKIN — CORRODED (WING) · airframe 12,738 hrs · 12,317 cycles

LT WING PLANK HOLE NR 1, WS 54.897 HAS CORROSION AT OB SIDE 1 INCH L X .005 INCH D AND IB SIDE 8 INCH L X .005 INCH - .010 INCH D. NOT IN CRITICAL AREA. MAINTENANCE REPAIRED CORROSION DAMAGE IAW REO, BY BLEND AND TREAT. (K)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 12,738 hrs · 12,317 cycles

FLOOR SUPPORT OB ANGLE PN 601R3471-9 CRACKED IN RADIUS MAINTENANCE REPAIRED IAW REO. (K)

Part: BRACKET — BENT (NLG) · airframe 12,617 hrs · 12,201 cycles

NOSE DOOR WARNING MESSAGE AND GEAR DISAGREE MESSAGE. INSPECTED AND FOUND NOSE GEAR CENTERING/ EXTENDED PROX SENSOR BRACKET BENT. REMOVED AND REPLACED BRACKET IAW CMM. PERFORMED GEAR SWING IAW AMM. OPS CHECK NORMAL. ALL INDICATIONS ARE NORMAL. (K)

Part: UNKNOWN — MALFUNCTIONED (WING) · airframe 9,848 hrs · 9,637 cycles

AFTER GEAR SELECTED DOWN, AIRCRAFT STARTED UNCONTROLLED ROLL LT (AUTO-PILOT OFF), STOPPED AFTER 5 SECONDS. THEN HAPPENED SECOND AND THIRD TIME 3 MILE END-TO-END TRAILING B737. ALL ROLLS TO LT. M/C (FIRST TIME FLAPS AT 0. SECOND FLAPS AT 20, THIRD FLAPS. PERFORMED VISUAL INSPECTION OF EXTERIOR OF AIRCRAFT INCLUDING FLIGHT CONTROL SURFACES. NO DEFECTS FOUND. PERFORMED SYSTEM SECU BITE CHECK IAW MM AND CHECKED MOVEMENT OF FLAPS AND AILERONS ALL SYSTEMS CHECKS GOOD. (K)

Part: FRAME — CRACKED (FUSELAGE)

FOUND RIGHT FS 718 FRAME FLANGE CRACKED BETWEEN STRINGERS 10R AND 12R. REMOVED DAMAGED FLANGE, PERFORMED NDT, FITTED AND INSTALLED REPAIR DOUBLER IAW BOMBARDIER REO 601R-53-61-193 REV A. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

LT FS 625 OBLIQUE ANGLE ON INTERCOSTAL CRACKED. REMOVED AND REPLACED NEW INTERCOSTAL AT FS 625.

Part: FRAME — CRACKED (FUSELAGE)

FOUND LEFT FS 718 FRAME FLANGE CRACKED BETWEEN STRINGERS 10L AND 12L. REMOVED DAMAGED FLANGE, PERFORMED NDT, FITTED AND INSTALLED DOUBLER BOMBARDIER REO NR 601R-53-61-19. (M)

Part: SUPPORT ANGLE — CRACKED (FUSELAGE)

LEFT AND RIGHT VERICAL SUPPORT ANGLES ARE CRACKED AT FS 280. REMOVED CRACKED ANGLES P/N 601R31113-58 AND P/N 601R31113-57 AND INSTALLED NEW ANGLES P/N 601R31113-58 AND P/N 601R31113-57 IAW CRJ 200 SRM 51-42-06 AND 51-42-21. (M)

Part: TORQUE LINK — DISCONNECTED (NLG) · airframe 8,573 hrs · 8,448 cycles

NOSE LANDING GEAR DOOR OPEN AND CAUTION DISAGREE MESSAGES, ACCOMPANIED BY WOW INPUT AND STEERING INOPERATIVE CAUTION MESSAGE ON DEPARTURE. RAN QRH FOR NLG DOOR OPEN, GEAR DISAGREE REMOVED WITH GEAR DOWN, RAN QRH FOR CAUTIONS. RECONNECTED TORQUE LINKS, REMOVED AND REPLACED LOWER TORQUE LINK, RETRACTION CHECK GOOD.

Part: WARNING LIGHT — ILLUMINATED (MLG)

AFTER TAKEOFF AND GEAR RETRACTION GOT RED DISAGREE ALONG WITH GEAR DOWN, GOT THREE GEAR DOWN INDICATORS AND RETURNED TO DAY. REMOVED AND REPLACED MLG SELECTOR VALVE IAW MM 32-32-10. OPS CHECK GOOD. (M)

Part: SOLENOID — STUCK (APU FUEL)

DURING ENGINE MAINTENANCE, SMOKE WAS NOTED COMING FROM THE APU INLET DOOR. MECHANICS TRIED TO DRY MOTOR THE APU TO EXTINGUISH THE FLAMES, BUT WERE UNSUCCESSFUL. DRY CHEMICAL WAS USED TO EXTINGUISH THE FLAMES. DURING INVESTIGATION AND TEARDOWN OF THE APU AT THE MFG REPAIR STATION, THE APU FUEL SOLENOID FAILED FUNCTIONAL CHECK AND WAS FOUND TO BE STUCK IN THE OPEN POSITION. TESTING OF THE SOLENOID IS ON-GOING WITH THE INVESTIGATION.

Part: APU — FIRE

AFTER APU SHUTDOWN FIRE WAS NOTED IN THE INTAKE. AGENTS USED HALON/DRY CHEMICAL TO EXTINGUISH. REMOVED AND REPLACED THE APU, SUSPECT CAUSE AS EITHER THE LOAD CONTROL VALVE OR THE FUEL SHUTOFF VALVE. (M)

Part: STRIKER — DENTED (DOOR FRAME)

DURING BRIDGING INSPECTION FOUND PAX DOOR SEAL STRIKER AT FS 349, WL 86 IS DENTED APPROXIMATELY .025 INCH DEEP BY .5 INCH LONG.

Part: DEICE BOOT — FAILED (PROPELLER BLADE)

INTERNAL SHORT OF ELECTRIC DEICE BOOT CAUSED AN OVERHEAT CONDITION, MELTING COMPOSITE AND FOAM FILLER OF PROPELLER BLADE. (APPROXIMATELY 1 INCH SQUARE BY 1 INCH DEEP AREA AT MID-POINT OF BLADE.) FOUND DURING PRE-FLIGHT INSPECTION ON THE LEFT PROPELLER, NR 4 BLADE.