N444ZW

Part: WARNING MESSAGE — FALSE ACTIVATION (HYD SYSTEM) · airframe 41,104 hrs · 40,085 cycles

6171 - SHORTLY AFTER TAKEOFF HYD 3 LOW PRESSURE CAUTION MESSAGE. C/W QRH MESSAGE CLEARED. AIRCRAFT REMOVED FROM SERVICE. PER OPS CK SYS 3A AND 3B PER AMM 29-12-03 OPS CK GOOD AT THIS TIME

Part: BRACKET — CORRODED (LWS 48.3) · corrosion level 2 · airframe 41,109 hrs · 39,987 cycles

CORROSION ON BRACKET AT WS 48.30 AT LH TE WING. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED BRACKET AT WS 48.30 AT LH TE WING REF. CRJ-200 SRM 51-42-06 AND 51-42-20 REV. 39. RESTORED PROTECTIVE FINISH. ALL WORK PERFORMED UNDER AERSALE WORK ORDER 004235, CARD NO. 50102, TT: 41,109 TC: 39,987.

Part: BRACKET — CORRODED (BS 310-349 LBL40) · corrosion level 2 · airframe 41,109 hrs · 39,987 cycles

POSSIBLE CORROSION ON ENTRY DOOR SILL AT FS310.00 TO FS349.00 LBL 40 TO 44. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FWD & AFT BRACKETS WITH P/N 601R31527-217 & FABRICATED NEW CLEAT WITH P/N 601R31527-176, ON SURROUND STRUCTURE AT PAX DOOR I.A.W. CRJ-200 SRM 51-42-06 REV. 39. ALL WORK PERFORMED UNDER AERSALE WORK ORDER 004309, CARD NO. 20031, TT: 47,227:03 TC: 44,966.

Part: FLOOR SUPPORT — CORRODED (BS 559-621) · airframe 41,109 hrs · 39,987 cycles

CABIN RH FLOOR SILL SUPPORT PN 601R31133-102 AND PLATE PN 601R31133-101 AT FS559.00 + 85 TO FS559.00 + 116 AND RBL42 TO RBL44 HAS EXFOLIATION CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED CABIN RH FLOOR SILL SUPPORT PN 601R31133-102 AND PLATE PN 601R31133-101 AT FS559.00 + 85 TO FS559.00 + 116 AND RBL42 TO RBL44. ALL WORK WITHIN LIMITS WAS PERFORMED IAW AIR WISCONSIN CRJ200 SRM 53-00-00 REV 39, CRJ200 SRM 51-21-06 REV 39, CRJ200 SRM 53-51-43 REV 39, CRJ200 SRM 51-42-06 REV 39, CRJ200 SRM 51-11-00 REV 39, CRJ200 SRM 51-40-11 REV 39, CRJ200 SRM 51-42-15 REV 39, SRM 51-21-11 REV 39. ALL WORK PERFORMED UNDER AERSALE WORK ORDER 003854, CARD NO. 20180, TT: 39,453:29 TC: 38,270.

Part: BRACE — CRACKED (BS 621) · airframe 41,109 hrs · 39,987 cycles

ANGLE BRACKET FOUND CRACKED ON AFT PRESSURE BULKHEAD ***** AIRCRAFT REMOVED FROM SERVICE ***** REMOVED AND REPLACED ANGLE BRACKET ON AFT PRESSURE BULKHEAD FS621, LBL40 REF CRJ200 SRM 51-42-01 REV 39

Part: BRACKET — CRACKED (FS621) · airframe 41,109 hrs · 39,987 cycles

ANGLE BRACKET FOUND CRACKED ON AFT PRESSURE BULKHEAD ***** AIRCRAFT REMOVED FROM SERVICE ***** REMOVED AND REPLACED ANGLE BRACKET ON AFT PRESSURE BULKHEAD FS621, LBL40 REF CRJ200 SRM 51-42-01 REV 39

Part: UNKNOWN — SMOKE (CABIN) · airframe 40,983 hrs · 39,944 cycles

ON ARRIVAL AT GATE, NOTICED SMOKE IN CABIN, SMELLS ELECTRICAL. AIRCRAFT REMOVED FROM SERVICE. PERFORMED PACK BURN OUT FOR CLEARING UNUSUAL ORDERS IAW AWA SUP 09-037E. NO DISCREPANCIES NOTED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,799 hrs · 39,720 cycles

RECEIVED IDG 2 CAUTION MULTIPLE TIMES IN FLIGHT. DID NOT RUN QRH MESSAGE CLEARED BELOW 15KFT. R/R BROKEN PIN ON P22EZ IAW ESPM 20-16 OPS CHECK GOOD IAW AMM 24-11

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,660 hrs · 39,551 cycles

RECEIVED LT AOA HEAT AFTER TAKE-OFF THEN RECEIVED LT PITOT HEAT, LT STATIC HEAT AND PITOT BASE HEAT. PERFORMED QRH AND MESSAGE REMAINED. C/W FIM RESET. SYSTEM OPERATES NORMAL. *******AIRCRAFT REMOVED FROM SERVICE****** NOTED BY MAINTENANCE

Part: OIL SYSTEM — WARNING MESSAGE · airframe 38,790 hrs · 37,499 cycles

AT CRUISE AT FL280, RECEIVED RT ENG OIL PSI WARNING MESSAGE. OIL PSI WAS FLUCTUATING IN THE GREEN BAND. C/W QRH. REDUCED POWER TO IDLE. DIVERTED TO ICT. AROUND 8,000FT, OIL PSI WENT INTO THE RED AND REMAINED THERE FOR THE REST OF THE FLIGHT. SHUT ENGINE DOWN AFTER LANDING. ****AIRCRAFT REMOVED FROM SERVICE**** IN WORK ***SUPPLEMENTAL INFORMATION ****AT CRUISE AT FL280, RECEIVED RT ENG OIL PSI WARNING MESSAGE. OIL PSI WAS FLUCTUATING IN THE GREEN BAND. C/W QRH. REDUCED POWER TO IDLE. DIVERTED TO ICT. AROUND 8,000FT, OIL PSI WENT INTO THE RED AND REMAINED THERE FOR THE REST OF THE FLIGHT. SHUT ENGINE DOWN AFTER LANDING. ****AIRCRAFT REMOVED FROM SERVICE**** R&R RH ENG IAW MTCM SUPP 12-11. ALL RII AND CKS REF TASK CARD 000-71-400-003AW.

Part: SEAT TRACK — CORRODED (FS409+16-409+112) · corrosion level 2 · airframe 38,791 hrs · 37,500 cycles

L/H SIDEWALL SEAT TRACK FROM FS 409+16 TO FS 409+112 HAS SEVERAL AREAS SURFACE CORROSION. EVALUATED CORROSION ON L/H SIDEWALL SEAT TRACK AT FS 409+16 TO FS 409+112 AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-49 REV 38. *********AIRCRAFT REMOVED FROM SERVICE*************************** REMOVED AND REPLACED 1 EACH L/H SIDEWALL SEAT TRACKS FROM FS 409+16 TO FS 409+112 IAW CRJ200 AMM 53-01-11 REV 65. RESTORED PROTECTIVE FINISH TO SEAT TRACKS PRIOR TO INSTALLATION IAW CRJ200 SRM 51-21-11 REV 38, CRJ200 SRM 51-25-06 REV 38, AND CRJ200 SRM 51-25-00 REV 38. WORK COMPLETED ON AERSALE WO #003644 CARD #20199. CRS #4AER685B N444ZWW TT: 38,791:53 TC: 37,500

Part: SEAL — CRACKED (WS 264) · airframe 38,791 hrs · 37,500 cycles

R/H WING FLIGHT SPOILER AT WS 264 HAS A CRACKED SEAL P/N: 601R10226-130 JUST BENEATH FWD EDGE OF SPOILER ON WING. CRACK DIMENSIONS ARE 6.5"L X .050"W. *********AIRCRAFT REMOVED FROM SERVICE*************************** REMOVED AND REPLACED 1 EACH CRACKED SEAL P/N: 601R10226-130 AT R/H FLIGHT SPOILER WS 264 IAW CRJ200 SRM 51-42-06 REV 39. RESTORED PROTECTIVE FINISH TO R/H WING SEAL IAW CRJ200 SRM 51-21-11 REV 39, CRJ200 SRM 51-25-06 REV 39. WORK COMPLETED ON AERSALE WO #003644 CARD #20196. CRS #4AER685B N444ZWW TT: 38,791:53 TC: 37,500

Part: SEAT TRACK — CORRODED (FS559+87 TO FS55) · corrosion level 2 · airframe 38,791 hrs · 37,500 cycles

R/H FLOOR SEAT TRACK FROM FS 559+87 TO FS 559+96 RBL 9 HAS SEVERAL AREAS OF SURFACE CORROSION. EVALUATED CORROSION ON R/H FLOOR SEAT TRACK AT FS 559+87 TO FS 559+96 AND RBL 9 AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-51-49 REV 39. *********AIRCRAFT REMOVED FROM SERVICE*************************** REMOVED AND REPLACED 1 EACH R/H FLOOR SEAT TRACK FROM FS559+87 TO FS559+96 RBL 9 IAW CRJ200 AMM 53-01-11 REV 65. RESTORED PROTECTIVE FINISH TO SEAT TRACK PRIOR TO INSTALLATION IAW CRJ200 SRM 51-21-11 REV 39, CRJ200 SRM 51-25-06 REV 39, AND CRJ200 SRM 51-25-01 REV 39. WORK COMPLETED ON AERSALE WO #003644 CARD #20276. CRS #4AER685B N444ZW TT: 38,791:53 TC: 37,500

Part: SEAT TRACK — CORRODED (FS 364 - FS 409) · corrosion level 2 · airframe 38,791 hrs · 37,500 cycles

R/H FLOOR SEAT TRACK FROM FS 364 TO FS 409 RBL 9 HAS SEVERAL AREAS OF SURFACE CORROSION. EVALUATED CORROSION ON R/H FLOOR SEAT TRACK AT FS 364 TO FS 409 AND RBL 9 AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-21-49 REV 39. *********AIRCRAFT REMOVED FROM SERVICE*************************** REMOVED AND REPLACED 1 EACH R/H FLOOR SEAT TRACK FROM FS 364 TO FS 409 RBL 9 IAW CRJ200 AMM 53-01-11 REV 65. RESTORED PROTECTIVE FINISH TO SEAT TRACK PRIOR TO INSTALLATION IAW CRJ200 SRM 51-21-11 REV 39, CRJ200 SRM 51-25-06 REV 39, AND CRJ200 SRM 51-25-01 REV 39. WORK COMPLETED ON AERSALE WO #003644 CARD #20254. CRS #4AER685B N444ZW TT: 38,791:53 TC: 37,500

Part: SEAT TRACK — CORRODED (FS559+80 TO FS55) · corrosion level 2 · airframe 38,791 hrs · 37,500 cycles

R/H FLOOR SEAT TRACK FROM FS 559+80 TO FS 559+96 RBL 27 HAS SEVERAL AREAS OF SURFACE CORROSION. EVALUATED CORROSION ON R/H FLOOR SEAT TRACK AT FS 559+80 TO FS 559+96 AND RBL 27 AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-51-49 REV 39. *********AIRCRAFT REMOVED FROM SERVICE*************************** REMOVED AND REPLACED 1 EACH R/H FLOOR SEAT TRACK FROM FS559+80 TO FS559+96 RBL 27 IAW CRJ200 AMM 53-01-11 REV 65. RESTORED PROTECTIVE FINISH TO SEAT TRACK PRIOR TO INSTALLATION IAW CRJ200 SRM 51-21-11 REV 39, CRJ200 SRM 51-25-06 REV 39, AND CRJ200 SRM 51-25-01 REV 39. WORK COMPLETED ON AERSALE WO #003644 CARD #20277. CRS #4AER685B N444ZW TT: 38,791:53 TC: 37,500

Part: BRACKET — CRACKED (#1 ENGINE NOSE C) · airframe 38,791 hrs · 37,500 cycles

L/H #1 ENGINE BRACKET P/N:228-50020-805 CRACKED AT 7 O'CLOCK POSITION AND BRACKET P/N: 228-50020-161 CRACKED AT 11-12 O'CLOCK POSITON ON NOSE INLET ATTACH RING. L/H #1 ENGINE NOSE COWL ATTACH RING FLANGE HAS 2 EA ELONGATED HOLES AT 7 O'CLOCK POSITION AND BETWEEN 11 TO 12 O'CLOCK POSITION. ******AIRCRAFT REMOVED FROM SERVICE****** REMOVED L/H #1 ENGINE BRACKET P/N: 228-50020-805 (7 O'CLOCK) POSITION AND BRACKET P/N: 228-50020-161 (11-12 O'CLOCK) POSITION. UPON REMOVAL OF L/H #1 ENGINE NOSE COWL ATTACH RING BRACKETS FOUND 2 EACH DAMAGED HOLES UNDER EACH REMOVED BRACKET. MEASURED HOLE DAMAGE AT EACH LOCATION: 11-12 O'CLOCK (P1) DIMENSION IS 0.245"(L) X 0.125"(W); 7 O'CLOCK (P2) DIMENSION IS 0.308"(L) X 0.286"(W). OPENED HOLE AT (P1) TO 0.2500" DIAMETER AND (P2) TO 0.3080" DIAMETER. HFEC INSPECTION PERFORMED AT AND AROUND BOTH HOLE LOCATIONS WITH NO INDICATIONS FOUND IAW CRJ200 NDT MANUAL PART 1 51-20-06 REV 43. MANUFACTURED (P1) FREEZE PLUG P/N: 601R-71-61-4348-1 (.2509 DIA) AND FREEZE PLUG P/N: 601R-71-61-4348-2 (.3089 DIA) OUT OF 7075-T6 BAR QQ-A-225/9. INSTALLED FREEZE PLUGS AT (P1) AND (P2) HOLE LOCATIONS. DRILLED .128" HOLE THROUGH FREEZE PLUG AT (P1) AND (P2) HOLE LOCATION MAINTAINING 0.050" WALL THICKNESS IN FREEZE PLUG. RESTORED SURFACE FINISH TO (P1) AND (P2) HOLE LOCATIONS.

Part: SKIN — DENTED (FS589-FS605) · airframe 38,791 hrs · 37,500 cycles

R/H AFT LOWER SKIN IS DENTED AND HAS SCRATCHED ON FS 589 - FS 605 AT S-24R TO S-25R. ****AIRCRAFT REMOVED FROM SERVICE ***** INSTALLED REPAIR DOUBLER, TRIPLER, AND FILLER TO REPAIR AREA ON AIRCRAFT SKIN EXTERIOR IAW ASAP EA #AWAC-CRJ253-01860 REV IR DATED 07-15-2022. RESTORED PROTECTIVE/DECORATIVE FINISH TO AIRCRAFT SKIN EXTERIOR REPAIR/REPAIR PARTS IAW ASAP EA #AWAC-CRJ253-01860 REV IR DATED 07-15-2022. IDENTIFIED REPAIR WITH INDELIBLE INK AS ASAP EA #AWAC-CRJ253-01860 IAW ASAP EA #AWAC-CRJ253-01860 REV IR DATED 07-15-2022. ALL WORK PERFORMED WITHIN ALLOWABLE LIMITS IAW ASAP EA #AWAC-CRJ253-01860 REV IR DATED 07-15-2022. WORK COMPLETED ON AERSALE WO #003644 CARD #20050. N444ZW TT:38,791:53 TC:37,500

Part: STRAP — CORRODED (FS 559+32) · corrosion level 2 · airframe 38,791 hrs · 37,500 cycles

CORROSION ON R/H FLOOR STRAP P/N: 601R31025-29 AT FS 559.00+32 AND RBL 27 TO RBL 36. ******************AIRCRAFT REMOVED FROM SERVICE********************** BLENDED 2 EACH AREAS ON R/H FLOOR STRAP P/N: 601R31025-29 AT FS 559.00+32: (P1) = 4.5"L X 2.0"W X .019"D (RBL 30) AND (P2) = 2.0"L X 1.5"W X .015"D (RBL 32) AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-00 REV 39. FABRICATED REPLACEMENT STRAP OUT OF 7075-T6 .050" IAW CRJ200 SRM 53-41-43 REV 39, CRJ200 SRM 53-41-43 REV 39, AND CRJ200 SRM 51-24-21 REV 39. APPLIED PROTECTIVE AND DECORATIVE FINISH ON FABRICATED FLOOR STRAP IAW CRJ200 SRM 51-21-11 REV 39 AND CRJ 200 SRM 51-25-01 REV 39. REMOVED AND REPLACED R/H FLOOR STRAP P/N: 601R31025-29 IAW CRJ200 SRM 51-42-06 REV 39. WORK COMPLETED ON AERSALE WO #003644 CARD #20259 AT AERSALE CRS #4AER685B. N444ZW TT:38,791:53 TC:37,500

Part: SEAT TRACK — CORRODED (FS559+80 TO FS55) · corrosion level 2 · airframe 38,791 hrs · 37,500 cycles

L/H FLOOR SEAT TRACK FROM FS 559+80 TO FS 559+96 LBL 27 HAS SEVERAL AREAS OF SURFACE CORROSION. EVALUATED CORROSION ON L/H FLOOR SEAT TRACK AT FS 559+80 TO FS 559+96 AND LBL 27 AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-51-49 REV 39. *********AIRCRAFT REMOVED FROM SERVICE*************************** REMOVED AND REPLACED 1 EACH L/H FLOOR SEAT TRACK FROM FS559+80 TO FS559+96 LBL 27 IAW CRJ200 AMM 53-01-11 REV 65. RESTORED PROTECTIVE FINISH TO SEAT TRACK PRIOR TO INSTALLATION IAW CRJ200 SRM 51-21-11 REV 39, CRJ200 SRM 51-25-06 REV 39, AND CRJ200 SRM 51-25-01 REV 39. WORK COMPLETED ON AERSALE WO #003644 CARD #20274. CRS #4AER685B N444ZW TT: 38,791:53 TC: 37,500

Part: SEAT TRACK — CORRODED (FS 349 TO FS 409) · corrosion level 2 · airframe 38,791 hrs · 37,500 cycles

R/H SIDEWALL SEAT TRACK FROM FS 349 TO FS 409 HAVE SEVERAL AREAS OF SURFACE CORROSION. EVALUATED CORROSION ON R/H SIDEWALL SEAT TRACK AT FS 349 TO FS 409 AND RBL 46 AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-21-49 REV 39. *********AIRCRAFT REMOVED FROM SERVICE*************************** REMOVED AND REPLACED 1 EACH R/H SIDEWALL SEAT TRACKS FROM FS 349 TO FS 409 IAW CRJ200 AMM 53-01-11 REV 65. RESTORED PROTECTIVE FINISH TO SEAT TRACKS PRIOR TO INSTALLATION IAW CRJ200 SRM 51-21-11 REV 39, CRJ200 SRM 51-25-06 REV 39, AND CRJ200 SRM 51-25-01 REV 39. WORK COMPLETED ON AERSALE WO #003644 CARD #20201. CRS #4AER685B N444ZW TT: 38,791:53 TC: 37,500

Part: SEAT TRACK — CORRODED (FS364 - FS 409+1) · corrosion level 2 · airframe 38,791 hrs · 37,500 cycles

L/H FLOOR SEAT TRACK FROM FS 364 TO FS 409+128 LBL 9 HAVE SEVERAL AREAS OF SURFACE CORROSION. EVALUATED CORROSION ON L/H FLOOR SEAT TRACK AT FS 364 TO FS409+128 AND LBL 9 AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-21-49 REV 39. *********AIRCRAFT REMOVED FROM SERVICE*************************** REMOVED AND REPLACED 1 EACH L/H FLOOR SEAT TRACK FROM FS 364 TO FS 409+128 LBL 9 IAW CRJ200 AMM 53-01-11 REV 65. RESTORED PROTECTIVE FINISH TO SEAT TRACK PRIOR TO INSTALLATION IAW CRJ200 SRM 51-21-11 REV 39, CRJ200 SRM 51-25-06 REV 39, AND CRJ200 SRM 51-25-01 REV 39. WORK COMPLETED ON AERSALE WO #003644 CARD #20255. CRS #4AER685B N444ZW TT: 38,791:53 TC: 37,500

Part: SEAT TRACK — CORRODED (FS559+87 TO FS55) · corrosion level 2 · airframe 38,791 hrs · 37,500 cycles

L/H FLOOR SEAT TRACK FROM FS 559+87 TO FS 559+96 LBL 9 HAS SEVERAL AREAS OF SURFACE CORROSION. EVALUATED CORROSION ON L/H FLOOR SEAT TRACK AT FS 559+87 TO FS 559+96 AND LBL 9 AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-51-49 REV 39. *********AIRCRAFT REMOVED FROM SERVICE*************************** REMOVED AND REPLACED 1 EACH L/H FLOOR SEAT TRACK FROM FS 559+87 TO FS559+96 LBL 9 IAW CRJ200 AMM 53-01-11 REV 65. RESTORED PROTECTIVE FINISH TO SEAT TRACK PRIOR TO INSTALLATION IAW CRJ200 SRM 51-21-11 REV 39, CRJ200 SRM 51-25-06 REV 39, AND CRJ200 SRM 51-25-01 REV 39. WORK COMPLETED ON AERSALE WO #003644 CARD #20275. CRS #4AER685B N444ZW TT: 38,791:53 TC: 37,500

Part: NONE — NONE · airframe 38,505 hrs · 37,214 cycles

L 14TH BLEED AIR WARNING FREQUENTLY CLIMBING THRU 20,000FT ONCE EVERY 3 SECONDS, C/W QRH BROUGHT ENG TO IDLE. MSG CONTINUED 1 EVERY MINUTE. STOPPED WHEN ENG SHUT DOWMN ON GROUND. (BK 4) SNYOPTIC SHOWED RED BETWEEN 14TH SATGE SOC, MSOV AND COWL SOV. ALSO RECEIVED BLEED AIR DUCT AURAL WARNING. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED LH ENGINE 14TH STAGE BLEED AIR LEAK TEST WITH ENGINES BLEED AIR IAW AMM 36-12-00 FOUND LH 14TH SOV AND LH AICE CLAMPS LOOSE. RE TIGHTENED LOOSE CLAMPS IAW AWAC SUP 10-008, NO LEAKS NOTED AT THE TIME. ALSO PERFORMED LH BLEED AIR LEAK OPERATIONAL CHECK IAW AMM 36-21-10, OPS CHECK GOOD.

Part: WARNING MESSAGE — ILLUMINATED (BLEED SYS) · airframe 38,505 hrs · 37,214 cycles

L 14TH BLEED AIR WARNING FREQUENTLY CLIMBING THRU 20,000FT ONCE EVERY 3 SECONDS, C/W QRH BROUGHT ENG TO IDLE. MSG CONTINUED 1 EVERY MINUTE. STOPPED WHEN ENG SHUT DOWMN ON GROUND. (BK 4) SNYOPTIC SHOWED RED BETWEEN 14TH SATGE SOC, MSOV AND COWL SOV. ALSO RECEIVED BLEED AIR DUCT AURAL WARNING. ***AIRCRAFT REMOVED FROM SERVICE*** MX IN PROGRESS

Part: ENGINE — OVERHEATED (RIGHT) · airframe 37,544 hrs · 36,221 cycles

CLIMBING THROUGH 7000 RH ENG ITT 888 FLASH RED AT N1 87% AFTER APPROXIMATELY 10 SEC HEARD BANG AND SHUTTER. A/C YAWED AS RH, ENG POWER REDUCED. ACCOMPLISHED ENG SHUTDOWN. ***AIRCRAFT REMOVED FROM SERVICE*** REPLACED R/H ENGINE S/N 872452 OFF WITH S/N 872307 ON REF WO 300993 FOR ALL MAINT PERTAINING TO R&R OF RH ENGINE. ALL GRND RUNS AND LEAK CHECKS GOOD.

Part: SKIN — DENTED (FUSELAGE) · airframe 37,515 hrs · 36,190 cycles

3 EA PROTRUDING DENTS IN AFT FUSELAGE SKIN AT FS 682.00 BETWEEN STR 23R AND STR 24R. AIRCRAFT REMOVED FROM SERVICE. CUTOUT DAMAGE AREA AT FS 672 TO FS 682 BETWEEN STR 23R AND STR 24R, REF CRJ200 SRM 53-00-31 REV 38. PERFORMED HFEC INSPECTION AROUND CUTOUT AREA AT FS 672 TO FS 682 BETWEEN STR 23R TO STR 24R, REF CRJ 200 NDTM PART 1 EDDY-CURRENT INSPECTION PROCEDURES 51-30-06 REV 41. FABRICATED REPAIR DOUBLER FROM ALUMINUM SHEET 2024-T3, 0.063" AT FS 672 TO FS 682 BETWEEN STR 23R TO STR 24R. REPAIR DOUBLER L=12.200", W=8.500", REF CRJ 200 SRM 53-00-31 REV 38.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 37,515 hrs · 36,190 cycles

FLOOR SILL PANEL AT FS 441 & RBL 42 AROUND NUTPLATE HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION AT RT FLOOR SILL PANEL AT FS 441 & RBL 42, REF CRJ 200 SRM 51-21-06. REWORK AREA MEASURES 1.067" L X 1.414" W X .003" D. PERFORMED HFEC, NO INDICATIONS NOTED, REF NDTM PART 1 51-20-06 REV 41. TREATED, PRIMED, PAINTED, AND APPLIED CPC, REF BOMBARDIER REO 601R-53-41-666 REV C DTD 2012-11-06.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 37,515 hrs · 36,190 cycles

CORROSION ON FLOOR ANGLE AT STATION 517, RBL 39, TO RBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON FLOOR ANGLE AT STATION 517 RBL 39 TO RBL 42, REF CRJ 200 SRM 51-21-06. MEASURE OF REWORK AREA L=2.000" W=1.800" D=0.007" ORIGINAL THICKNESS 0.080" REMAINING THICKNESS IS 0.073", REF CRJ 200 SRM 53-41-45. REWORKED AREA FOUND TO BE WITHIN LIMITS, REF REPAIR ENGINEERING ORDER (REO) 601R-53-41-666 REV C DATED 2012-11-06.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 37,515 hrs · 36,190 cycles

CORROSION ON FLOOR ANGLE AT FS 448 TO FS 451 AND RBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION AT RT FLOOR ANGLE AT FS 448 TO FS 451 RBL 42, REF CRJ 200 SRM 51-21-06. REWORKED AREA MEASURES 1.80" L X 0.95" W X .003" D. ORIGINAL MATERIAL THICKNESS .080" REMAINING THICKNESS .077". HFEC INSPECTION ACCOMPLISHES WITH NO INDICATIONS NOTED, REF NDTM PART 1 51-20-06 REV 41. TREATED, PAINTED, AND APPLIED CPC WITHIN ALLOWABLE LIMITS, REF BOMBARDIER REO 601R-53-41-666 REV C DTD 2012-11-06.

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 37,515 hrs · 36,190 cycles

CORROSION ON FLOOR ANGLE AT STATION 468 & RBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON FLOOR ANGLE AT STATION 461.50, & RBL 42, REF CRJ 200 SRM 51-21-06. MEASURE OF REWORKED AREA L=0.900" W=0.950" D=0.013" ORIGINAL THICKNESS 0.080" REMAINING THICKNESS AFTER REWORK TO BE 0.067", REF CRJ 200 SRM 53-41-45. REWORK AREA FOUND TO BE WITHIN LIMITS, REF REPAIR ENGINEERING ORDER (REO) 601R-53-41-666 REV C DATED 2012-11-06.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 37,515 hrs · 36,190 cycles

FS 541 & RBL 42 HAS CORROSION ON FLOOR SILL PANEL AT NUTPLATE. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION AT RT FLOOR SILL PANEL AT FS 541 & RBL 42, REF CRJ 200 SRM 51-21-06. REWORK AREA MEASURES 1.267" L X 1.006" W X .004" D. PERFORMED HFEC NO INDICATIONS NOTED, REF NDTM PART 1 51-20-06 REV 41. TREATED, PRIMED, PAINTED, AND APPLIED CPC, REF BOMBARDIER REO 601R-53-41-666 REV C DTD 2012-11-06.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 37,515 hrs · 36,190 cycles

CORROSION ON FLOOR ANGEL AT STATION 438 TO STATION 439 RBL 40C. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION AT RT FLOOR ANGLE AT STATION 439, TO 439 & RBL 42, REF CRJ 200 SRM 51-21-06. MEASURE OF REWORKED AREA L=1.377" W=0.390" D=0.003", ORIGINAL THICKNESS 0.080", REMAINING THICKNESS IS 0.077", REF CRJ 200 SRM 53-41-45. REWORKED AREA FOUND TO BE WITHIN LIMITS, REF REPAIR ENGINEERING ORDER (REO) NR 601R-53-41-666 REV C DATED, 2012-11-06.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 37,515 hrs · 36,190 cycles

CORROSION ON FLOOR ANGLE AT FS 484 & RBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION AT RT FLOOR ANGLE AT FS 484 & RBL 42, REF CRJ 200 SRM 51-21-06. REWORKED AREA MEASURES 1.96" L X 1.44" W X .005" D, ORIGINAL MATERIAL THICKNESS .080", REMAINING MATERIAL THICKNESS .075". HFEC ACCOMPLISHED WITH NO INDICATIONS NOTED, REF NDTM PART 1 51-20-06 REV 41. TREATED, PRIMED, PAINTED, AND APPLIED CPC. WITHIN ALLOWABLE LIMIT,S REF BOMBARDIER REO 601R-53-41-41-666 REV C 2012-11-06.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 37,515 hrs · 36,190 cycles

CORROSION ON FLOOR ANGLE AT STATION 469, RBL 36. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON FLOOR ANGLE AT STATION 469, RBL 36, REF CRJ 200 SRM 51-21-06. MEASURE OF REWORKED AREA L=1.373" W=0.961" D=0.011", ORIGINAL THICKNESS IS 0.080". REMAINING THICKNESS IS 0.069" REWORKED AREA FOUND TO BE WITHIN LIMITS, REF REPAIR ENGINEERING ORDER (REO) 601R-53-41-666 REV C DATED 2012-11-06.

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 37,515 hrs · 36,190 cycles

CORROSION ON FLOOR ANGEL AT STATION 517, LBL 36, TO LBL 37. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON FLOOR ANGEL AT STATION 517, LBL 36, LBL 37, REF CRJ 200 SRM 51-21-06. MEASURE OF REWORK AREA L=0.851" W=0.080" D=0.005", ORIGINAL THICKNESS 0.080", REMAINING THICKNESS IS 0.075", REF CRJ 200 SRM 53-41-45. FOUND REWORKED AREA TO BE WITHIN LIMITS, REF REPAIR ENGINEERING ORDER (REO) 601R-53-41-666 REV C DATED 2012-11-06.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 37,515 hrs · 36,190 cycles

CORROSION ON FLOOR ANGLE AT STATION 468, TO STATION 470, LBL 40. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION AT STATION 468 TO STATION 470, REF CRJ 200 SRM 53-41-06. MEASURE OF REWORK AREA L=3.500" W=I.400" D=0.006" ORIGINAL THICKNESS 0.080" REMAINING THICKNESS AFTER REWORK 0.740", REF CRJ 200 SRM 53-41-45. REWORK AREA FOUND TO BE WITHIN LIMITS, REF REPAIR ENGINEERING ORDER (REO) 601R-53-41-666 REV C DATED 2012-11-06.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 37,515 hrs · 36,190 cycles

CORROSION ON FLOOR SILL PANEL STATION 467, AND LBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON FLOOR SILL PANEL AT STATION 467, AND LBL 42, REF CRJ 200 SRM 51-21-06. MEASURE OF REWORK AREA L=0.950" W=0.780" D=0.006", ORIGINAL THICKNESS 0.055", REF CRJ 200, SRM 53-41-45. REMAINING THICKNESS AFTER REWORK IS 0.490", REWORK AREA FOUND TO BE WITHIN LIMITS, REF REPAIR ENGINEERING ORDER (REO) 601R-53-41-666 REV C DATED 2012-11-06.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 37,515 hrs · 36,190 cycles

CORROSION ON FLOOR ANGLE AT STATION 508, LBL 36 TO 38. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION AT STATION 508, TO STATION 510, LBL 36, TO LBL 38, REF CRJ 200 SRM 51-21-06. MEASURE OF REWORK AREA L=1.702" W=1.643" D=0.006", ORIGINAL THICKNESS 0.080", REMAINING THICKNESS AFTER REWORK IS 0.074", REF CRJ 200 SRM 53-41-45. REWORKED AREA FOUND TO BE WITHIN LIMITS, REF REPAIR ENGINEERING ORDER (REO) 601R-53-41-666 REV C DATED 2012-11-06.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 37,515 hrs · 36,190 cycles

CORROSION ON PRESSURE FLOOR SILL AT STATION 447, AND LBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON PRESSURE FLOOR SILL AT STATION 447, AND LBL 42, REF CRJ 200 SRM 51-21-06. MEASURE OF REWORKED AREA L=1.141" W=0.883" D=0.006", ORIGINAL THICKNESS IS 0.055", REF CRJ 200 53-41-45. REMAINING THICKNESS IS 0.049", REWORKED AREA FOUND TO BE WITHIN LIMITS, REF REPAIR ENGINEERING ORDER (REO) 601R-53-41-666 REV C DATED 2012-11-06.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 37,515 hrs · 36,190 cycles

CORROSION AT NUT PLATE ON FLOOR SILL PANEL FS 522 RBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION AT FS 522 & RBL 42 AT NUT PLATE ON FLOOR SILL, REF CRJ 200 SRM 51-21-06. REWORKED ARE MEASURES .925" L X .912" W X .005" D. ORIGINAL MATERIAL THICKNESS .055", REMAINING MATERIAL THICKNESS .050". HFEC ACCOMPLISHED WITH NO INDICATIONS NOTED, REF NDTM 51-20-06, PART 1, REV 41. TREATED, PRIMED, PAINTED AND APPLIED CPC. WITHIN ALLOWED LIMITS, REF BOMBARDIER 601R-53-41-666, REV C, 2012-11-06.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 37,515 hrs · 36,190 cycles

CORROSION ON FLOOR ANGLE AT STATION 461.50 & RBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON FLOOR ANGLE AT STATION 461.50, & RBL 42, REF CRJ 200 SRM 51-21-06. MEASURE OF REWORKED AREA L=0.900" W=0.950" D=0.003", ORIGINAL THICKNESS 0.080", REMAINING THICKNESS AFTER REWORK TO BE 0.077", REF CRJ 200 SRM 53-41-45. REWORK AREA FOUND TO BE WITHIN LIMITS, REF REPAIR ENGINEERING ORDER (REO) 601R-53-41-666 REV C DATED 2012-11-06.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 37,515 hrs · 36,190 cycles

FS 441 & RBL 42 HAS CORROSION ON FLOOR SILL PANEL AT NUTPLATE. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION AT RT FLOOR SILL PANEL AT FS 441 & RBL 42, REF CRJ 200 SRM 51-21-06. REWORK AREA MEASURES 1.067" L X 1.414" W X .003" D. PERFORMED HFEC NO INDICATIONS NOTED, REF NDTM PART 1 51-20-06 REV 41. TREATED, PRIMED, PAINTED, AND APPLIED CPC, REF BOMBARDIER REO 601R-53-41-666 REV C DTD 2012-11-06.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 37,515 hrs · 36,190 cycles

CORROSION ON FLOOR ANGLE AT FS 500 TO FS 513 RBL 47. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION AT RT FLOOR ANGLE AT FS 500 TO FS 503 AND BL 47, REF CRJ 200 SRM 51-21-06. REWORKED AREA MEASURES 1.6" L X 0.9" W X .006 D. ORIGINAL MATERIAL THICKNESS .080", REMAINING MATERIAL THICKNESS .074". HFEC INSPECTION ACCOMPLISHED WITH NO INDICATION NOTED, REF NDTM PART 1 51-20-06 REV 41. TREATED, PRIMED, PAINTED, AND APPLIED CPC WITHIN ALLOWABLE LIMITS, REF BOMBARDIER REO 601R-53-41-666 REV C DTD 2012-11-06.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 37,515 hrs · 36,190 cycles

CORROSION ON FLOOR ANGLE AT STATION 447,AND RBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON FLOOR ANGLE AT STATION 447 AND RBL 42, REF CRJ 200 SRM 51-21-06. MEASURE OF REWORK AREA L=1.920" W=1.400" D=0.007" ORIGINAL THICKNESS 0.080" REMAINING THICKNESS AFTER REWORK IS 0.073', REF CRJ 200 SRM 53-41-45. REWORK AREA FOUND TO BE WITHIN LIMITS, REF REPAIR ENGINEERING ORDER (REO) 601R-53-41-666 REV C DATED 2012-11-06.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 37,515 hrs · 36,190 cycles

CORROSION ON FLOOR ANGLE FS 523 TO FS 530, RBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION AT RT FLOOR ANGLE AT FS 523 TO FS 530 & RBL 42, REF CRJ 200 SRM 51-21-06. REWORKED AREA MEASURES 2.5" L X 1.40" W X .006" D. ORIGINAL MATERIAL THICKNESS .080", REMAINING MATERIAL THICKNESS .074". HFEC ACCOMPLISHED WITH NO INDICATIONS NOTED, REF NDTM 51-20-06, PART 1, REV 41. TREATED, PRIMED, PAINTED AND APPLIED CPC. WITHIN ALLOWED LIMITS, REF BOMBARDIER REO 601R-53-41-666, REV C, 2012-11-06.

Part: BULKHEAD — PUNCTURED (BS 621) · airframe 34,653 hrs · 33,406 cycles

APB FS 621 IS PUNCTURED JUST ABOVE FLOOR AT LBL 24.0 REPAIRED APB FS 621 JUST ABOVE FLOOR LBL 24 IAW BOMBARIDER REO# 601R-53-61-6673 REV --

Part: BULKHEAD — CRACKED (BS 621) · airframe 34,653 hrs · 33,406 cycles

AFT PRESSURE BULKHEAD WAS CRACKED AT THE AFT CARGO DOOR TRACK, LBL 27.5, WL 125. REPAIRED THE AFT PRESSURE BULKHEAD IAW REO 601R-53-61-1541 REV-F.

Part: FRAME — DAMAGED (VERTICAL STAB) · airframe 34,653 hrs · 33,406 cycles

VERTICAL STAB, AFT FRAME UNDER PANEL 326AT HAD A DAMAGED SCREW HOLE. REPAIRED THE VERTICAL STAB AFT FRAME IAW EA CRJ255-01022, REV-IR.

Part: BULKHEAD — CRACKED (BS 621) · airframe 34,653 hrs · 33,406 cycles

AFT PRESSURE BULKHEAD HAD A CRACK AT THE LINTEL FITTING. REPAIRED THE AFT PRESSURE BULKHEAD IAW REO 601R-53-61-1230, REV F, AND REO 601R-53-61-6671 REV -.

Part: FITTING — DAMAGED (DOOR CONNECTOR) · airframe 34,653 hrs · 33,406 cycles

PAX DOOR ELECTRICAL CONNECTOR FITTING FOR P2MB, AT THE LOWER SILL WAS CORRODED AND CRACKED. REPLACED THE FITTING.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 34,653 hrs · 33,406 cycles

BS 280 FLOORBEAM WEB LWR AFT ANGLE AT LBL 12 WAS CRACKED. REPAIRED THE FLOORBEAM.

Part: ANGLE — CRACKED (BS 280 FLOORBEAM) · airframe 34,653 hrs · 33,406 cycles

FLOORBEAM INBD ANGLE AT BS 280, LBL 9 WAS CRACKED. REPLACED THE ANGLE.

Part: ANGLE — CRACKED (BS 280 FLOORBEAM) · airframe 34,653 hrs · 33,406 cycles

FLOORBEAM OTBD ANGLE AT BS 280, LBL 9 WAS CRACKED. REPLACED THE ANGLE.

Part: ANGLE — CRACKED (BS 280 FLOORBEAM) · airframe 34,653 hrs · 33,406 cycles

FLOORBEAM OTBD ANGLE AT BS 280, RBL 9 WAS CRACKED. REPLACED THE FLOORBEAM ANGLE.

Part: FITTING — WORN (RT WING TE FLAP) · airframe 34,653 hrs · 33,406 cycles

RIGHT OTBD FLAP FITTING AT FLAP STATION 280.66 WAS WORN TO LIMITS. REPLACED.

Part: RIB — CRACKED (LT WING) · airframe 34,653 hrs · 33,406 cycles

LH WING TRAILING EDGE RIB AT WS 130.10 WAS CRACKED. REPLACED THE RIB.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 34,653 hrs · 33,406 cycles

RIGHT INBD FLAP, LOWER INBD SKIN HAD NUMEROUS ROCK PITS. REPLACED THE FLAP.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 34,653 hrs · 33,406 cycles

LEFT INBD FLAP VANE LEADING EDGE WAS CHAFED AT WS 104.0. REPLACED THE FLAP VANE.

Part: RETAINER — CRACKED · airframe 34,653 hrs · 33,406 cycles

PANEL 422AT SEAL RETAINER CRACKED. REPLACED SEAL RETAINER IAW SRM 51-42-06.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 34,653 hrs · 33,406 cycles

FLOORBEAM INBD ANGLE CRACKED AT BS 280, RBL 9. REPLACED THE ANGLE IAW SRM 51-21-43, 51-31-59, 51-24-36, AND 51-41-21.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 34,653 hrs · 33,406 cycles

BS 280 FLOORBEAM WAS CRACKED AT RBL 9. REPLACED THE FLOORBEAM IAW SRM 51-42-06.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 34,653 hrs · 33,406 cycles

AFT PRESSURE BULKHEAD FWD FACE AT BL0 HAS 2 CRACKS 38 IN AND 57 IN ABOVE FLOOR.

Part: PLATE — CRACKED (CARGO DOOR) · airframe 34,653 hrs · 33,406 cycles

CARGO DOOR STEP PLATE WAS CRACKED. REPLACED THE STEP PLATE IAW SRM 51-40-11.

Part: STRAP — CORRODED (BS 559 FLOORBEAM) · airframe 34,653 hrs · 33,406 cycles

FLOORBEAM STRAP CORRODED AT BS 559, RBL 27 TO RBL 43. REPLACED THE STRAP IAW SRM 51-42-06, 53-00-00, AND 53-41-43.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 34,653 hrs · 33,406 cycles

BS 484 FLOORBEAM ANGLE WAS CRACKED AT LBL 36. REPLACED THE FLOORBEAM ANGLE IAW REO 601R-53-41-059, REV-B.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 34,653 hrs · 33,406 cycles

BS 484 FLOORBEAM ANGLE WAS CRACKED AT LBL 27. REPLACED THE FLOORBEAM ANGLE IAW SRM 51-42-26.

Part: RUDDER — UNKNOWN · airframe 33,807 hrs · 32,522 cycles

9898 UNCOMMANDED YAW IN CLIMB RUDDER TRIMMED RIGHT MANUALLY CENTERED THEN RUDDER TRIMMED LEFT MANUALLY RE-CENTERED THEN RUDDER WAS UNCONTROLLABLE C/W QRH DISCONNECTED RUDDER A/P OFF ABLE TO CONTROL A/C. NUMEROUS ERRORS ON FCC 1 IN FCC DIAGNOSTICS, R/R FCC 1 IAW AMM 22-22-14 OPS CHECK GOOD, PERFORMED SPIN TEST OF YAW DAMPER PER AMM 22-22-01 OPS CHECK GOOD

Part: STRUT — DISCHARGED (NLG) · airframe 3,936 hrs · 30,724 cycles

FLT. 4007. GEAR DISAGREE AND NOSE GEAR DOOR OPEN WARNING MESSAGES ON DEPARTURE WHEN GEAR LEVER SELECTED UP. LEVER WAS NOT MOVED WITHIN 30 SECONDS OF ORIGINAL SELECTION. NOSE GEAR SHOWED GREEN DOWN AND LOCK MAINS SHOWED YELLOW WITH HASHES THEN SHOWED UP AND LOCKED. MANUAL RELEASE SYSTEN WAS OPERATED. ICING CONDITIONS WERE ENCOUNTERED WITH GEAR EXTENDED. EMERGENCY LANDING DECLARED MAX AIRSPEED WITH GEAR EXTENDED WAS APRROXIMATELY 200 KNOTS, LANDING WEIGHT WAS 41,500 LBS NO HARD LANDING NOTED. JACKED ACFT IAW AMM 07-11-01. NLG STRUT WOULD NOT FULLY EXTEND. STRUT SERVICING REQ. SERVICED NLG STRUT WITH OIL AND NITROGEN IAW 12-12-32-610-803. STRUT FULLY EXTENDS. PERFORMED GEAR SWINGS. OPS CHECKED GOOD.

Part: APU — SMOKE · airframe 31,340 hrs · 30,184 cycles

APU AUTO SHUTDOWN. FOLLOWED BY SMOKE COMING FROM APU INTAKE.

Part: DAMPER — UNKNOWN · airframe 31,233 hrs · 30,086 cycles

UNCOMMANDED YAW AT FL210, INITIAL ROLL TO THE RIGHT THEN PULSED BACK AND FORTH GENTLY. RAN IAC AND QRH, PROBLEM DISCONTINUED WHEN YAW DAMPER DISCONNECTED

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,067 hrs · 29,941 cycles

INTERCOSTAL THAT SITS ON TOP OF STR 20L HAS CORROSION BETWEEN FRAME 333.00 AND 349.00 IN THE FWD ELECTRONIC EQUIPMENT BAY. REPLACED INTERCOSTAL ON STR 20L BETWEEN FRAME 333.00 AND 349.00 IAW SRM 51-42-06, 51-42-21. REPAIRED STR 20L IAW EA AWAC-CRJ253-00442, REV-IR DATED 07/13/2016.

Part: SKIN — DENTED (FUSELAGE) · airframe 31,067 hrs · 29,941 cycles

LEFT LOWER FUSELAGE SKIN HAS DENT AT FS 621.00 AND STR 19L. REPAIRED LT LOWER FUSELAGE SKIN AT FS 621.00 AND STR 19L IAW EA CRJ253-0430, REV IR DATED 07/09/2016.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,067 hrs · 29,941 cycles

STRINGER 26L HAS CORROSION BETWEEN FS 349.00 AND FS 364.00. REPAIRED STRINGER IAW SRM 53-00-03.

Part: STIFFENER — CRACKED (APU BAY) · airframe 31,067 hrs · 29,941 cycles

APU ENCLOSURE BOTH INTERNAL UPPER STIFFENERS WELDS ARE CRACKED AT AFT FLANGE FORWARD SIDE. REPAIRED APU ENCLOSURE INTERNAL UPPER STIFFENERS IAW SUP: 16-168 AND EA CRJ249-00441 AND SUP: 16-206.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,067 hrs · 29,941 cycles

INBD FLOOR LANDING ON LBL27 HAS CORROSION AND BARE METAL SPOTS BETWEEN FS 574.00 AND FS 621.00 IN THE CARGO BAY. REPAIRED INBD FLOOR LANDING ON LBL27 FROM FS 574.00 TO FS 605.00 IAW SRM 53-61-43, 53-00-00, 51-31-59. REPAIRED INBD FLOOR LANDING ON LBL 27 FROM FS 605.00 TO FS 621.00 IAW EA CRJ253-00436, REV-IR DATED 07/04/2016.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 31,067 hrs · 29,941 cycles

AFT EQUIPMENT COMPARTMENT FS 621, BULKHEAD LT SKIN ATTACH ANGLE AT STR 14L CRACKED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 31,067 hrs · 29,941 cycles

AFT EQUIPMENT COMPARTMENT FS 621 BULKHEAD RT OBLIQUE ANGLE AT STR 14R CRACKED.

Part: SKIN — CHAFED (PAX DOOR) · airframe 31,067 hrs · 29,941 cycles

PASSENGER DOOR OUTER SKIN CHAFED UNDER HINGE PIN TRAVEL AREA BOTH FORWARD AND AFT CORNERS. FOUND DURING EVALUATION OF SKIN DAMAGES FS 310 AND FS 349.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 31,067 hrs · 29,941 cycles

AFT EQUIPMENT COMPARTMENT FS 621 BULKHEAD LT OBLIQUE ATTACH ANGLE AT STR 14L IS CRACKED.

Part: WEB — CRACKED (PA XDOOR) · airframe 31,067 hrs · 29,941 cycles

PASSENGER DOOR HAS A CRACK ON THE AFT WEB UNDER THE AFT DRAG ANGLE. REPAIRED CRACK IAW SUP: 15-310.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 31,067 hrs · 29,941 cycles

FUSELAGE SKIN HAS SCRATCHES ON THE OTBD SIDE, AT THE LOWER FORWARD CORNER OF THE PASSENGER DOOR CUTOUT AT FS 310.00. REPAIRED FUSELAGE SKIN IAW SUP 16-201, DATED 07/06/2016.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 31,067 hrs · 29,941 cycles

PASSENGER DOOR AFT DRAG ANGLE IS CRACKED. REPAIRED PASSENGER DOOR AFT DRAG ANGLE IAW GREO 601R-52-11-513, REV B DATED 2015-07-05.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 31,067 hrs · 29,941 cycles

FUSELAGE SKIN HAS A SCRATCH ON THE OTBD SIDE AT THE LOWER AFT PASSENGER DOOR CUTOUT AT FS 349.00. REPAIRED FUSELAGE SKIN IAW SUP: 16-201 DATED 07/06/2016.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 31,067 hrs · 29,941 cycles

AFT EQUIPMENT COMPARTMENT FS 621.00 BULKHEAD LT ANGLE AT STR 16L IS CRACKED. REPLACED ANGLE ON FS 621.00 BULKHEAD AT STR 16L IAW SRM 51-42-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 31,067 hrs · 29,941 cycles

WINDSHIELD CENTER POST LT LOWER CLIP IS CRACKED. REPLACED WINDSHIELD CENTER POST LOWER LT CLIP IAW SRM 51-42-21.

Part: BRACKET — CRACKED (THRUST REVERSER) · airframe 31,067 hrs · 29,941 cycles

RIGHT T/R PDU WIRE HARNESS BRACKET IS CRACKED. REPLACED BRACKET IAW SRM 51-42-06.

Part: PANEL — CRACKED (ZONE 400) · airframe 31,067 hrs · 29,941 cycles

RIGHT LOWER DIVIDER PANEL 422DB HAS A CRACKED FWD DIVIDER. REPLACED LOWER DIVIDER FROM PANEL 422DB IAW SRM 51-42-06.

Part: FITTING — CRACKED (NR 2 EXHAUST) · airframe 31,067 hrs · 22,941 cycles

NR 2 ENGINE EXAHUST FAIRING ATTACHMENT NUT PLATES HAVE CRACKED CLIPS. REPLACED NUT PLATE CLIPS IAW CMM 20-42-06.

Part: DOUBLER — CRACKED (JET PIPE) · airframe 31,067 hrs · 29,941 cycles

LEFT JET PIPE FAIRING HAS CRACKED DOUBLERS AT NUTPLATES FOR ACCESS PANELS. REPLACED THE JET PIPE DOUBLERS IAW CMM 20-42-06.

Part: SUPPORT ANGLE — CRACKED (BS 234) · airframe 31,067 hrs · 29,941 cycles

LEFT WINDSHIELD SIDE POST SUPPORT, LOWER ATTACH ANGLE BELOW WINDOW LINE IS CRACKED. REPLACED THE ANGLE IAW SRM 51-42-06.

Part: STRINGER — CRACKED (BS 379-394) · airframe 31,067 hrs · 29,941 cycles

PAX DOOR FRAME, NDT VERIFIED CRACKS IN STRINGER 3L AT ATTACH POINT TO AFT UPPER FRAME. REPAIRED THE STRINGER IAW SRM 53-00-03 FIG. 202 SHEET 1.

Part: CARGO TRACK — CORRODED (BS 559-574) · corrosion level 2 · airframe 31,067 hrs · 29,941 cycles

CARGO TRACK HAS CORROSION AT LBL9 BETWEEN BS 559+112 AND 574, IN THE CARGO BAY. REPLACED THE CARGO TRACK IAW REO 601R-53-00-485 REV-B & AMM 53-00-49.

Part: FITTING — CRACKED (BS 235) · airframe 31,067 hrs · 29,941 cycles

RIGHT WINDSHIELD SIDE POST SUPPORT, O/B FITTING IS CRACKED. REPLACED RT O/B SIDE POST SUPPORT FITTING IAW SRM 51-42-21.

Part: FLOOR SUPPORT — CRACKED (BS 589) · airframe 31,067 hrs · 29,941 cycles

CARGO DOOR OPENING FLOOR SUPPORT IS CRACKED BETWEEN RIVET AND INNER EDGE AT BS 589. REPAIRED FLOOR SUPPORT IAW REO 601R-53-61-433.

Part: FRAME — CORRODED (BS 409) · corrosion level 2 · airframe 31,067 hrs · 29,941 cycles

FWD FACE AREA OF THE BS 409 FRAME HAS CORROSION BETWEEN STRINGERS 26 - 27L. REPAIRED AREA IAW SRM 51-42-06, 51-42-21, 51-40-11, AND 51-24-21.

Part: DOOR — STUCK (CABIN) · airframe 31,020 hrs · 29,903 cycles

SERVICE DOOR WILL NOT OPEN FROM OUTSIDE.

Part: HANDLE — STUCK (SERVICE DOOR) · airframe 31,007 hrs · 29,890 cycles

UNABLE TO OPEN SERVICE DOOR FROM OUTSIDE, HANDLE WON'T POP OUT. DOOR OPENS NORMALLY FROM INSIDE.

Part: COVER — UNSECURE (CABIN) · airframe 30,606 hrs · 29,528 cycles

COVER FOR FLOOR EMER LIGHTS AT ROW 1 CAME OFF.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 29,982 hrs · 28,922 cycles

AFTER TAKEOFF & GEAR UP, RECEIVED, STEERING INOPERATIVE, CAUTION MSG. COMPLIED WITH QRH, MSG PERSISTS. MSG WENT OUT ON GEAR EXTENSION.

Part: LIGHT — UNSECURE (CABIN) · airframe 28,866 hrs · 27,844 cycles

FLIGHT 4021 REF 274230 1, TAPE APPLIED TO FLOOR TRACK LIGHTING STRIP AT ROW 1 IAW GMM CHPT 23. APPROVED FOR ONE FLIGHT. PLACED ON DIL. INSTALLED NEW EMER LIGHT STRIP END CAP IAW AMM 33-51-01. THIS CLEARS DIL.

Part: WIRE — BROKEN (CABIN) · airframe 28,584 hrs · 27,568 cycles

FLIGHT NR 3746, FLOOR LEVEL EMER LIGHTS INOPERATIVE ROW 7 & AFT. PULLED UP EMER LIGHTING STRIP, INSPECTED WIRING. FOUND WIRE BROKEN AT J 6LY & P7LY. REINSTALLED STRIP FOR FERRY IAW AMM 33-51-01.

Part: WIRE — UNSECURE (CABIN) · airframe 28,583 hrs · 27,567 cycles

FLIGHT 3849. 3845, 3849, & 3983 EMER LIGHT STRIP 1ST SEGMENT AT ROW 1 PULLED UNLIT. SECURED LIGHTING STRIP WIRES & FLOOR TRACK IAW AMM 33-51-01. OPERATIONS CHECKED GOOD.

Part: ECU — FAILED (APU) · airframe 28,539 hrs · 27,521 cycles

FLIGHT NR 4004, ON FIRST ATTEMPT TO START THE APU THE DOOR DID NOT OPEN, ON SECOND ATTEMPT THE DOOR OPENED BUT THE RPM HUNG 28% & A STRONG FUEL ODOR FILLED THE CABIN. COMPLIED WITH CM ACTION PLACARDED & PLACED ON MEL. R & R APU ECU IAW AMM 49-61-01. OPERATIONS CHECKED GOOD. REMOVED PLACARD & REMOVED FROM MEL.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 27,330 hrs · 26,378 cycles

CAPTAIN`S WINDSHIELD SHATTERED AT APPROX 14,000 FT. CREW STOPPED CLIMB & CONTACTED ATC. EMER DECLARED. INSPECTED & FOUND THE OUTER PLY TO BE CRACKED, REF SUPP 14-201A. R & R CAPTAIN'S WINDSHIELD & PERFORMED WINDSHIELD HEAT CHECK & LEAK CHECK IAW AMM 56-11-01. NOTE, CHECKED GOOD. IAW 269609 3 RESET CBS CB P1-G5 G6, F12, A10 & A11. OPERATIONS CHECKED CHECK GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 27,140 hrs · 26,208 cycles

FLIGHT ATTENDANT SMELLED ELEC BURNING SMELL. IN THE GALLEY AREA SMELLED THE STRONGEST COMPARED TO THE REST OF THE CABIN, WHILE LIGHTS WERE ON DIM.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,423 hrs · 25,546 cycles

FS 349 FRAME IN AVIONICS BAY HAS CORROSION.

Part: RETAINER — CRACKED (PYLON) · airframe 25,423 hrs · 25,546 cycles

PYLON PNL 422BT SEAL RETAINER IS CRACKED.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,423 hrs · 25,546 cycles

LBL 27 CORRODED ON TOP SURFACE AT RS 621.00.

Part: SUPPORT — CRACKED (TE FLAP) · airframe 26,423 hrs · 25,546 cycles

RIGHT INBD FLAP INBD HINGE ARM FAIRING GUIDE PLATE SUPPORT STRUCTURE ON FWD SIDE OF HINGE ARM IS CRACKED.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 26,423 hrs · 25,546 cycles

LOWER U BRACKET CRACKED AT RIVET FS 574.00.

Part: HOUSING — CRACKED (CARGO DOOR) · airframe 26,423 hrs · 25,546 cycles

CARGO DOOR HANDLE HOUSING IS CRACKED.

Part: ATTACH FITTING — GOUGED (TE FLAP) · airframe 26,423 hrs · 25,546 cycles

RT WING INBD FLAP, INBD HINGE BOX, AFT ATTACHMENT FITTING IS GOUGED.

Part: TRUNNION — DAMAGED (LT MLG) · airframe 26,423 hrs · 25,546 cycles

MLG TRUNNION LWR FLANGES FOUND TWO EACH OS HOLES 1LT & 1RT.

Part: PLATE — CRACKED (TE FLAP) · airframe 26,423 hrs · 25,546 cycles

LEFT OTBD FLAP CTR HINGE ARM SHROUD PLATE IS CRACKED.

Part: RETAINER — CRACKED (PYLON) · airframe 26,423 hrs · 25,546 cycles

PYLON PNL 412DB SEAL RETAINER IS CRACKED.

Part: BRACKET — CRACKED (RT MLG WW) · airframe 26,423 hrs · 25,546 cycles

RT MLG BRAKE PRESS TRANSDUCER FWD BRACKET CRACKED.

Part: DRAG ANGLE — CRACKED (RT WING) · airframe 26,423 hrs · 25,546 cycles

RT MLG DRAG ANGLE COMMON TO BATTERY RIB IS CRACKED.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 26,423 hrs · 25,546 cycles

CARGO FLOOR TRACK CORRODED AT FS 574 RBL 9.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 26,423 hrs · 25,546 cycles

CARGO DOOR SUPPORT BEAM AFT LOWER CLIP IS CRACKED.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 26,423 hrs · 25,546 cycles

UPPER BRAKE ACCUMULATOR BRACKET IS CRACKED.

Part: MOUNT BRACKET — CRACKED (FUSELAGE) · airframe 26,423 hrs · 25,546 cycles

NR 2 HYD ACCUMULATOR MOUNT BRACKET IN AEB IS CRACKED.

Part: SEAL — CRACKED (RT COWLING) · airframe 26,423 hrs · 25,546 cycles

RT LOWER NOSE COWL TORQUE BOX SPRING SEAL IS CRACKED.

Part: DRAG ANGLE — CRACKED (LT WING) · airframe 26,423 hrs · 25,546 cycles

LT MLG DRAG ANGLE COMMON TO BATTERY RIB CRACKED.

Part: FLOORBEAM — GOUGED (FUSELAGE) · airframe 26,423 hrs · 25,546 cycles

RBL 27 FLOORBEAM CAP OTBD FLANGE GOUGED NEAR RIVET.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,423 hrs · 25,546 cycles

FS 484 CLIP CRACKED AT LBL 27.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,423 hrs · 25,546 cycles

FS 484 CLIPS CRACKED AT RBL 27 & 36.

Part: PLATE — CORRODED (CARGO BAY) · corrosion level 2 · airframe 26,423 hrs · 25,546 cycles

CARGO BAY PRESS DIAPHRAGM SUPPORT PLATE CORRODED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,423 hrs · 25,546 cycles

RT FLOOR SEAT TRACK CORRODED AT FS 559+24.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,423 hrs · 25,546 cycles

LT SIDE SEAT RAIL CORRODED AT FS 417.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,423 hrs · 25,546 cycles

LOWER FRAME SECTOR AT FS 319 IS CORRODED FROM STRINGER 26L TO 26R.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,423 hrs · 25,546 cycles

LOWER FRAME SECTOR CORRODED AT FS 333 FROM STRINGER 26L TO 26R.

Part: TRIM SWITCH — FAULTY (COCKPIT) · airframe 25,647 hrs · 24,801 cycles

STAB TRIM FAULT AT 2.8 BOTH CHANNELS DISENGAGED, COMPLIED WITH NEITHER CHANNEL WOULD RE-ENGAGE. AUTOPILOT WAS ENGAGED. IAW PG 270843 4 FOR CORRECTIVE ACTION, R & R PILOT'S STAB TRIM DISCONNECT SWITCH. CAPTAIN'S DISCONNECT SWITCH FAILED SENSITIVITY TEST. R & R CAPTAIN`S PITCH TRIM, DISCONNECT SWITCH IAW AMM SUPP 10-048A, OPERATIONS CHECKED GOOD.

Part: FLOORBEAM — CRACKED (FS 280) · airframe 21,524 hrs · 20,808 cycles

FLOORBEAM, FS 280.00 IS CRACKED JUST OTBD OF RBL 9. REPAIRED IAW REO 601R-53-11-2338 BY CUTTING AWAY DAMAGE AND INSTALLING REPAIR ANGLE AND FILLERS.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 21,524 hrs · 20,808 cycles

PAX DOOR AFT DRAG ANGLE IS CRACKED. REMOVED UNSERVICEABLE DRAG ANGLE WITH NEW SERVICEABLE DRAG ANGLE IAW REO 601R-52-11-513, REV A.

Part: STEP — CRACKED (PAX DOOR) · airframe 21,524 hrs · 20,808 cycles

PAX DOOR STAIR STRUCTURE CRACKED ON AFT SIDE PANEL @ 3RD STEP. REPAIRED PAX DOOR AFT SIDE PANEL @ 3RD STEP IAW REO 601R-52-11-702, REV C.

Part: STEP — CRACKED (PAX DOOR) · airframe 21,524 hrs · 20,808 cycles

PAX DOOR STAIR STRUCTURE IS CRACKED ON FWD SIDE OF 4TH STEP. REPAIRED FWD SIDE PANEL AT 4TH STEP ON PAX DOOR IAW REO 601R-52-11-702.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 21,524 hrs · 20,808 cycles

CARGO DOOR FLOOR SILL HAS CORROSION AROUND SCREW HOLES UPPER LOWER SIDES. REMOVED UNSERVICEABLE CARGO DOOR FLOOR SILL AND REPLACED WITH SERVICEABLE FLOOR SILL PN 60135011-63 IAW SRM 51-42-06, 51-40-11.

Part: FLOOR SUPPORT — CORRODED (PAX DOOR) · airframe 21,524 hrs · 20,808 cycles

PAX DOOR SILL FLOOR SUPPORT STRUCTURE HAS CORROSION. REMOVED PAX DOOR SILL FLOOR SUPPORT ANGLE AND REPLACED WITH SERVICEABLE ANGLE IAW SRM 51-24-21, 51-42-06, 51-42-21.

Part: STRUCTURE — DAMAGED (PAX DOOR) · airframe 21,524 hrs · 20,808 cycles

PAX DOOR AFT CORNER DAMAGED. REPAIRED PAX DOOR AFT CORNER IAW REO 601R-52-11-2066.

Part: FITTING — CRACKED (BS 235 S12L) · airframe 21,524 hrs · 20,808 cycles

PILOTS SIDE POST LOWER FITTING CRACKED. REMOVED UNSERVICEABLE WINDOW POST LOWER FITTING. REPLACED WITH SERVICEABLE FITTING, PN 601R33235-3S.

Part: FLOOR SUPPORT — CORRODED (CARGO AREA) · airframe 21,524 hrs · 20,808 cycles

FLOOR SUPPORT LBL27 IN CARGO AREA HAS CORROSION. REMOVED UNSERVICEABLE LBL27 FLOOR SUPPORT CAP AND INSTALLED SERVICEABLE LBL 27 FLOOR SUPPORT CAP IAW SRM 51-42-06, 51-42-27, REO 601R-53-61-3778, REV A.

Part: CARGO TRACK — CORRODED (CARGO AREA) · airframe 21,524 hrs · 20,808 cycles

TWO TIE DOWN TRACKS ON LBL 9 IN CARGO AREA HAS CORROSION. R & R TIE DOWN TRACKS ON LBL 9 IAW AMM 53-01-11.

Part: BULKHEAD — GOUGED (FS 202.75) · airframe 21,524 hrs · 20,808 cycles

PRESSURE BULKHEAD FS 202.75 IS GOUGED JUST OTBD OF PARKING BRAKE CONTROL CABLE PASS THRU. REPAIRED BULKHEAD IAW REO 601R-53-11-563, REV B, REPAIR TYPE V.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 21,524 hrs · 20,808 cycles

LT 9G INBD AND OTBD TIE DOWN TRACKS HAS CORROSION. R & R LT 9G CORRODED TIE DOWN TRACKS IAW AMM 53-01-11.

Part: CARGO TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 21,524 hrs · 20,808 cycles

RIGHT 9G INBD CARGO TRACK HAS CORROSION. R & R RT 9G CARGO TRACK IAW AMM 53-01-11.

Part: EXHAUST DUCT — DENTED (LEFT) · airframe 21,524 hrs · 20,808 cycles

LEFT JET PIPE HAS SMALL SHARP DENT ON THE TOP SIDE. PERFORMED REPAIR ON LIGHT JET PIPE TOP SIDE IAW CMM 78-11-00.

Part: SHUTOFF VALVE — INOPERATIVE (ANTI ICE SYS) · airframe 21,134 hrs · 20,438 cycles

DURING FLIGHT IN ICING CONDITIONS, RECEIVED WING OVERHEAT RED WARNING. EICAS INDICATED RT WING L/E RED. C/W QRH, RECEIVED RT-WING OVERHEAT IN STANDBY MODE. R & R RT MODULATING SHUTOFF VALVE IAW AMM 30-12-14 LEAK AND OPS CK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (WING HEAT) · airframe 20,992 hrs · 20,280 cycles

SELECTED WING HEAT TO STANDBY IM ICING CONDITIONS AND RECEIVED WING O/H WARNING, LT ICING CONDITIONS AND C/W QRH (RT WING). R & R TEMP CONTROL UNIT IAW AMM 31-12-19. OPS CHECKED GOOD. REMOVED PLACARD AND MEL.

Part: SHUTOFF VALVE — FAILED (LT WING) · airframe 20,800 hrs · 20,069 cycles

RT WING OVERHEAT MESSAGE IN FLIGHT. SELECTED WING ANTI-ICE OFF. MESSAGE CLEARED WITHIN 5 SEC. DETERMINED RT WING DUCT TO BE AT FAULT SELECTED RT 14TH STAGE ISO OPEN AND WING ANTI-ICE TO STANDBY. R & R LT MODULATING SHUTOFF VALVE.

Part: BULKHEAD — CRACKED (BS 559) · airframe 20,254 hrs · 19,497 cycles

FOUND WEBBING OTBD OF RBL 9 CRACKED AT FS 559, REPAIRED WEB OF FS 559 PRESSURE BULKHEAD, RT SIDE, RBL 9 TO 18 IAW REO 601R-53-41-1495, REV A.

Part: POST — CRACKED (FS 559) · airframe 20,254 hrs · 19,497 cycles

FOUND LBL 900 OTBD POST CRACKED AT FS 559.0. REPAIRED LBL 9.0 OTBD POST BY FULL INCORPORATION OF REO 601R-53-41-057, REV A.

Part: LANDING GEAR — MALFUNCTIONED (NOSE) · airframe 18,525 hrs · 17,638 cycles

ON TAKEOFF, AFTER RETRACTING GEAR, GOT GEAR UNSAFE/ NOSE DOOR OPEN WARNING. PERFORMED QRH. NOSE GEAR DID NOT SHOW UP AND LOCKED. EVERYTHING WORKED NORMALLY AFTER GEAR EXTENDED. OPEN

Part: GCU — MALFUNCTIONED (LEFT) · airframe 17,556 hrs · 16,629 cycles

WHILE IN FLT, AC 1 AUTO TRANSFER AC BUS 1 GEN 1 OFF AND LT WINDOW HEAT CAUTION MSG ILLUMINATED ON ED1 CW QRH FLAP .5 SPEED ON ED2 IN FLAP SELECTION OTHER AS MSG. R & R GEN CONTROL UNIT.

Part: PANEL — CHAFED (LT WING) · airframe 17,156 hrs · 16,216 cycles

LT OTBD FLAP, BUTTE DOOR PANEL NR 594PB HAS MINOR CHAFING. R & R BUTTE DOOR PANEL NR 594PB WITH SERVICEABLE PART PN 601R102279 IAW SRM 51-42-06.

Part: ANGLE — CRACKED (BS 621-625) · airframe 17,156 hrs · 16,216 cycles

RT OBLIQUE ANGLE IS AEB IS CRACKED. R & R RT OBLIQUE ANGLE BETWEEN FS 621 & FS 625, AT RBL 36, STR 14R IAW SRM 51-42-21.

Part: BULKHEAD — CHAFED (BS 280) · airframe 17,156 hrs · 16,216 cycles

AFT SIDE OF 280 BULKHEAD AFT FLIGHT DECK CUT OUT ON RT SIDE IS CHAFED IN 2 SPOTS REPAIR IAW REO 601R-53-11-1727, REV C 2009/09/24. REPAIR 1 (WEB REPAIR AND CHANNEL MINOR BLEND OUT).

Part: UNKNOWN — ODOR (CABIN) · airframe 16,076 hrs · 15,063 cycles

REQUEST INSPECTION FOR SMOKE ODOR IN REAR OF CABIN NEAR ROW 12. INSPECTED DUCTING, CLEANED AND INSPECTED RT PACK COALERSCER SOCK, INSPECTED PSU ROW 12 RT, NO EVIDENCE OF SMOKE OR ARCING. OPS CHECK GOOD, OK FOR SERVICE.

Part: CONTROL PANEL — MALFUNCTIONED (RUDDER SYS) · airframe 14,138 hrs · 13,180 cycles

ON CLIMBOUT, AFTER INITIAL LT TURN, RUDDER (TRIM) RAN FULL LEFT DEFLECTION UNCOMMANDED. ABLE TO OVER POWER WITH USE OF RUDDER PEDAL. AUTO-PILOT WAS NOT ENGAGED. DECLARED EMERGENCY LANDING IN IAD. REMOVED AND REPLACED TRIM CONTROL PANEL AND RUDDER TRIM ACTUATOR. (K)

Part: LIGHT — FAILED (COCKPIT)

F/O YOKE CLIP LIGHT BROKEN, SPARKED AND SMOKED INTERMITTENTLY AND NOW CEASED TO WORK. FOUND C/B CBP2 U6 POPPED, PULLED AND COLLARD. INSPECTED YOKE CHART HOLDER DAMAGE NOTED. REF LP 188421/1 FOR CHART HOLDER MEL. (K)

Part: O-RING — DETERIORATED (APU FUEL SYS) · airframe 12,839 hrs · 11,934 cycles

FUEL LEAK BELOW APU. FOUND APU FUEL SUPPLY LINE O-RING DETERIORATED. REMOVED AND REPLACED APU FUEL LINE O-RING IAW AMM 49-31-01-420-001. NO LEAKS. OK FOR SERVICE. (K)

Part: BRACKET — BROKEN (BROKEN) · airframe 12,300 hrs · 11,425 cycles

BRACKET OF SERVICE DOOR INNER HANDLE MICRO SWITCH BROKEN. BRACKET OF SERVICE DOOR INNER HANDLE REPLACED. (A)

Part: HINGE — CRACKED (FUSELAGE) · airframe 12,300 hrs · 11,425 cycles

CARGO STOW PLATE HINGES (3) CRACKED. CARGO STOW PLATE HINGES (3) REPLACED IAW CRJ 200 STM 51-42-06. (A)

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 12,300 hrs · 11,425 cycles

REPAIR CRACK ON PASSENGER DOOR. PASSENGER DOOR EDGE MEMBER REPAIRED IAW CRJ 200 REO 601R-53-11-279. (A)

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 12,300 hrs · 11,425 cycles

CARGO DOOR SURROUND STRUCTURE, CHANNEL CRACKED AT FS 574 LBL 45 AND WL 79.5. CARGO DOOR SURROUND STRUCTURE CHANNEL AT FS 574 LBL 45 WL 79.5 REPLACED IAW CRJ 200 SRM 51-42-06. (A)

Part: BULKHEAD — PUNCTURED (FUSELAGE) · airframe 12,300 hrs · 11,425 cycles

COCKPIT BULKHEAD FS 280 PUNCTURED AT LBL 34 AND WL 124. COCKPIT BULKHEAD FS 280 AT LBL 34 AND WL 124 REPAIRED IAW REO 601R-53-11-1414. (A)

Part: STIFFENER — CRACKED (PAX DOOR) · airframe 12,300 hrs · 11,425 cycles

PAX DOOR AFT SIDE PANEL STIFFENER (P/N 601R317745-7) CRACKED AT DOOR ASSIST MOTOR ASSY. STIFFENER (P/N 601R317745-7) REPLACED IAW CRJ 200 SRM 51-42-06 AND SRM 51-42-13. (A)

Part: ATTACH ANGLE — CRACKED (BS 484) · airframe 12,300 hrs · 11,425 cycles

INTERCOSTAL CLIP AT FS 484, RBL 27, WL 72 IS CRACKED. INTERCOSTAL CLIP AT FS 484, RBL 27, WL 72 REMOVED IAW CRJ 200 SRM 51-42-06. NEW CLIP FABRICATED WITH S-6144-33 IAW CRJ 200 SRM 51-24-36 AND REPLACED IAW CRJ 200 SRM 51-42-06 AND SRM 51-42-21. (A)

Part: FITTING — CRACKED (FUSELAGE) · airframe 12,300 hrs · 11,425 cycles

BULKHEAD CLIPS CRACKED AT FS 280, LBL 9 AND WL 72. BULKHEAD CLIPS AT FS 280, LBL 9 AND WL 72 REPLACED IAW CRJ 200 SRM 51-42-06 AND SRM 51-42-21. (A)

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 12,300 hrs · 11,425 cycles

PAX DOOR AFT DRAG ANGLE CRACKED. REPLACED ANGLE IAW SRM 51-42-06 AND 51-42-13. (A)

Part: FITTING — CRACKED (FUSELAGE) · airframe 12,300 hrs · 11,425 cycles

BULKHEAD CLIPS CRACKED AT FS 280, RBL 9 AND WL 72. BULKHEAD CLIPS AT FS 280, RBL 9 AND WL 72 REPLACED IAW CRJ 200 SRM 51-42-06 AND SRM 51-42-21. (A)

Part: HANDLE — CORRODED (ESCAPE HATCH) · airframe 12,300 hrs · 11,425 cycles

FUNCTIONAL TEST OF CREW ESCAPE HATCH FAIL CORROSION FOUND ON OUTER HANDLE SHAFT. OUTER HANDLE REPLACED. (A)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 12,300 hrs · 11,425 cycles

INTERCOSTAL AT FS 484 LBL 36, WL 72 IS CRACKED. NTERCOSTAL AT FS 484.0 LBL 36.0 REPAIRED IAW REO 601R-53-41-059. (A)

Part: SUPPORT BRACKET — CRACKED (HYDRAULIC SYS) · airframe 12,300 hrs · 11,425 cycles

NR 1 AND NR 2 HYDRAULIC SUPPORT BRACKETS CRACKED ON THE AFT LOWER EDGE. REPAIR PERFORMED ON NR 1 AND NR 2 HYDRAULIC MANIFOLD SUPPORT BRACKETS IAW CRJ 200 REO 601R-53-61-031 REV A. (A)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 12,300 hrs · 11,425 cycles

INTERCOSTAL CRACK ON LT SIDE AT STR 14 BTWN FRAME 621.00 AND 625.00. INTERCOSTAL REPLACED IAW SRM 51-42-06. (A)

Part: LANDING GEAR — ICED (NOSE) · airframe 10,840 hrs · 10,009 cycles

ON GEAR RETRACTION AFTER TAKEOFF, GEAR DISAGREE WARNING AND NLG DOOR OPEN WARNING, COMPLIED WITH QRH. IN ICING AFTER TAKEOFF FROM CONTAMINATED RUNWAY AT LESS THAN 200 KNOTS. VISUALLY CHECKED MLG AND NLG COMPONENTS, FOUND AND REMOVED ICE AND SNOW FROM NLG COMPONENTS AND SENSORS. PERFORMED LANDING GEAR EXTENSION AND RETRACTION IAW 32-30-00, OPS CHECK GOOD. (M)

Part: FAN — INOPERATIVE (LAVATORY)

BURNING RUBBER SMELL IN LAV. FOUND LAV EXHAUST FAN INOPERATIVE. REMOVED AND REPLACED LAV EXHAUST FAN IAW AMM 21-23-13. OPS CHECK GOOD. (M)

Part: DRIVE SHAFT — DAMAGED (TE FLAPS)

FLAPS FAIL CAUTION, FLAPS CONFIRMED AT ZERO DEGREES, COMPLIED WITH QRH. REMOVED AND REPLACED FLEX DRIVESHAFT NR 1, (PDU TO INBOARD FLAP) AS PER AMM 27-53-10, OPS TEST OF FLAPS GOOD AT THIS TIME. INSPECTED FLEX SHAFT, FOUND NO BARBER PULL. REMOVED MOISTURE AND LUBED REF AMM 27-53-10. (M)

Part: LANDING GEAR — ICED (NOSE)

AFTER TAKEOFF SELECTED GEAR UP, MAINS CAME UP AND STOWED FULLY. NLG REMAINED DOWN AND LOCKED. COMPLIED WITH QRH, NO HELP. INSPECTED NOSE GEAR, FOUND EXCESSIVE ICE ACCUMULATION, REMOVED ICE AS REQUIRED. PERFORMED SEVERAL GEAR SWINGS REF AMM 07-11-01. CLEANED PROXIMITY SWITCHES AS REQUIRED. NO DEFECTS NOTED. (M)

Part: O-RING — LEAKING (FCU LINE)

WITH BLEEDS SUPPLIED BY APU, STRONG FUEL ODOR NOTED. WITH BLEED SON ENGINE, NO ODOR NOTED. FOUND FUEL LEAKING FROM FCU ELBOW/NUT FITTING. REMOVED AND REPLACED O-RING. LEAK CHECK GOOD. NO FUEL SMELL NOTED. RED AMM 49-30-01. (M)

Part: FLOOR SUPPORT — CORRODED (BS 574-621)

LEFT SIDE CARGO FLOOR SUPPORT EDGE MEMBER HAS MINOR SURFACE CORROSION IN AREA OF NUTPLATE FROM FS 574 TO FS 621. REMOVED CORROSION, TREATED, PRIMED AND PAINTED IAW CRJ SRM 51-21-06. (M)

Part: FLOORBEAM — CORRODED (BS 621)

FOUND RIGHT SIDE FS 621 FLOOR SUPPORT ANGLE IS CRACKED APPROX .7 INCH LONG. MAINTENANCE CUT AWAY DAMAGE SECTION OF RIGHT 621 FLOOR SUPPORT ANGLE TRIMMED TO FIT P/N 601R53-61-117-2, 601R53-61-117-4, 601R53-61-117-6, AND DRILLED IAW REO 601R-53-61-117. (M)

Part: FLOOR SUPPORT — CORRODED (BS 621)

FOUND LEFT SIDE FS 621 FLOOR SUPPORT ANGLE CRACKED APPROX .5 INCH LONG. MAINTENANCE CUT AWAY DAMAGED SECTION OF LEFT 621 FLOOR SUPPORT ANGLE, TRIMMED PARTS 601R-53-61-117-1 AND 601R53-61-117-3 TO FIT AND DRILLED IAW REO 601R-53-61-117. (M)

Part: BRACKET — CRACKED (FUSELAGE)

LEFT MLG WHEEL WELL HYDRAULIC SWITCH BRACKET IS CRACKED IN OUTBOARD RADIUS. REMOVED CRACKED BRACKET AND INSTALLED A FABRICATED BRACKET FROM 2024 T3 .050 INCH CLAD ALUMINUM IAW BSC STANDARD REPAIR 601R-53-0044E. (M)

Part: BRACKET — CRACKED (RT MLG WW)

RT MLG WHEEL WELL HYDRAULIC SWITCH BRACKET IS CRACKED ON INBOARD RADIUS. REMOVED CRACKED BRACKET AND INSTALLED A FABRICATED BRACKET FROM 2024 T-3 .050 INCH CLAD ALUMINUM IAW BSC STANDARD REPAIR 601R-53-0044E. (M)

Part: INTERCOSTAL — CRACKED (BS 484)

FOUND LEFT SIDE FS 484 INTERCOSTAL CRACKED AT LBL 36 APPROX .25 INCH LONG. REPAIRS ACCOMPLISHED IAW REO 601R-53-41-059A AND BSC STANDARD REPAIR 601R-53-0030A. (M)

Part: DRAG ANGLE — CRACKED (PAX DOOR)

PAX DOOR AFT DRAG ANGLE CRACKED APPROX .7 INCH LONG IN AREA OF DOOR ASSIST CABLE PULLEY BRACKET. REPAIRED PAX DOOR AFT DRAG ANGLE IAW BOMBARDIER REO 601R-52-11-513. CUT AWAY DAMAGED AREA FABRICATED AND INSTALLED REPAIR ANGLE. (M)

Part: RETAINER — MISSING (NLG)

AFTER TAKEOFF AT 300 FT, 160 KTS, RECEIVED GEAR UP DISAGREE NLG UPON SELECTION OF GEAR MLG UP AND LOCKED CAUTION WOW STATUS MESSAGE WOW OUTPUT FAILED FOLLOWED QRH DECLARED EMERGENCY LANDING UNEVENTFUL LANDING IN ORD. FOUND NOSE LANDING GEAR STRUT RETAIN COLLAR 90 OUT FROM WEAR DISARMED STRUT. INSPECTED FOUND LOWER RET ATN MISSING. REPLACED MINS AND RERACKED STRUT IAW 37-21-00 AND 32-21-15. NO DEFECTS NOTED. (M)

Part: IDG — DAMAGED (NR 2) · airframe 11,132 hrs · 9,378 cycles

IDG NR 2 AMGER CAS MESSAGE AT TAKEOFF. TAKEOFF ABORTED AT 60 KNOTS. FOUND IDG LEAKING OIL FROM DRAIN PLUG FOUND DRAIN PLUG DAMAGED/ REMOVED AND REPLACED DRAIN PLUG IAW AMM 24-31-00. REMOVED AND REPLACED IDG NR 2. OPS AND LEAK CHECK GOOD.

Part: LIGHT — ODOR (OVERHEAD LIGHT)

BURNING ODOR AT APPROXIMATELY ISLE 7 NEAR OVERHEAD FLOURESCENT LIGHTING. IN PROGRESS.

Part: WARNING LIGHT — ILLUMINATED (HYD PRESSURE)

AFTER TAKEOFF, RECEIVED EDP HYD. (M)