N218PS

Part: COUPLING — LEAKING (ZONE 400) · airframe 41,436 hrs · 41,215 cycles

RIGHT 14TH DUCT WARNING MESSAGE WHEN CLIMBING THROUGH ABOUT 8000FT. RAN QRH. MESSAGE CLEARED. RETURNED TO ORD. (FLIGHT 5610) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 30875407, SEE THE FOLLOWING CPS FOR MX PERFORMED:CP 30882896 FOR REPLACEMENT OF THE RT PYLON 14TH DUCT SENSING ELEMENT A58WKCP 30883007 FOR LEAK FOUND AND REPLACEMENT FOR A COUPLING ON THE RH 14TH STAGE DUCTCP 30886551 FOR LEAK CHECKS AND REPLACEMENT OF THE RH 14TH BLEED AIR SOV & COUPLINGCP 30886735 FOR COMPLETION OF BLOCKAGE TEST FOR THE RH 14TH STAGE DUCTINGCP 30889306 FOR LEAK CHK OF RT 14TH BLEED AIR SOVCP 30889331 FOR REPLACEMENT OF 2 BOOTS ALONG THE RT 14TH STAGE DUCTING. OPS CHECKS GOOD. NO MESSAGES NOTED. ACFT OK FOR SERVICE.

Part: WARNING MESSAGE — ILLUMINATED · airframe 41,378 hrs · 41,149 cycles

RIGHT 14TH DUCT WARNING MESSAGE WHEN CLIMBING THROUGH ABOUT 8000FT. RAN QRH. MESSAGE CLEARED. RETURNED TO ORD. (FLIGHT 5610) OPEN.

Part: DUCT — WARNING MESSAGE (ZONE 400) · airframe 41,377 hrs · 41,148 cycles

R 10TH DUCT WARNING MSG DURING CLIMB AT 3500FT, APPLIED THE QRH MSG DISAPPEARED, RETURNED TO KORD WITH NO FURTHER ISSUE. (FLIGHT 5215 - FILED OPEN)

Part: CLAMP — DAMAGED (ZONE 100) · airframe 41,378 hrs · 41,149 cycles

RIGHT 10TH DUCT WARNING MSG DURING CLIMB AT 3500FT. APPLIED QRH, MSG DISAPPEARED, RETURNED TO KORD WITH NO FURTHER ISSUE. (FLIGHT 5215) SEE CP 30863533 FOR 10TH STAGE LEAK CHECK. SEE CP 30863951 FOR ACM COMPRESSOR INLET DUCT CLAMP REPLACEMENT SEE CP 30863548 FOR 14TH STAGE LEAK CHECK AROUND 10TH STAGE SENSING COMPONENTS SEE CP 30863994 FOR RT 14TH STAGE MODULATING AND SHUTOFF VALVE SEE CP 30863908 FOR SENSING LOOPS WIRING CHECKS SEE CP 30863918 FOR REPLACEMENT OF LOOP A57WK SEE CP 30864432 FOR HIGH POWER ENGINE RUNS AFTER MX IS COMPLETE TO ENSURE NO WARNING MESSAGES.SEE CP 30865706 FOR LEAK CHECK OF R 10TH AND R 14TH STAGE DUCTING IN AREA OF SENSING LOOPS WITH ENGINES AT HIGH POWER.

Part: BLEED VALVE — WARNING MESSAGE · airframe 41,377 hrs · 41,147 cycles

R 14TH STAGE BLED AIR DUCT MASTER WARNING N CLIMB OUT (FLIGHT 5038) PERFORMED VISUAL INSPECTION OF THE RH 14TH STAGE BLEED DUCTS REFERENCING APPLICABLE STEPS OF AMM 36-12-00. NO DEFECTS NOTED AT THIS TIME. PERFORMED LEAK TEST OF THE 10TH STAGE BLEED AIR SYSTEM USING GROUND AIR SUPPLY REF APPLICABLE STEPS OF AMM 36-11-00. FOUND RT 10TH STAGE BLEAD AIR SHUT OFF VALVE LEAKING AIR TOWARDS RT 14TH STAGE BLEED LEAK SENSING ELEMENTS IN THE AFT EQUIPMENT BAY. R & R RT 10TH STAGE BLEAD AIR SHUT OFF VALVE REF 36-11-04. OPS CHECK GOOD AT THIS TIME. LEAK CHECK GOOD AT THIS TIME. PERFORMED OPS TEST OF BLEED-AIR LEAK DETECTION & WARNING SYSTEM REFERENCING APPLICABLE STEPS OF AMM 36-21-00. OPS CHECK GOOD AT THIS TIME.

Part: LANDING GEAR — WARNING MESSAGE · airframe 40,205 hrs · 39,885 cycles

ON DEPARTURE OUT OF RIW WE BROUGHT THE GEAR UP AT 230 KTS AND GOT GEAR DISAGREE. SLOWED THE AIRPLANE DOWN AND THE MESSAGE EXTINGUISHED. RAN QRH. NO ISSUES BRINGING GEAR DOWN ON LANDING. (FLIGHT 5130 FILED CLOSED) UPON ARRIVAL TROUBLESHOT REF CRJ FIM 32-60-07. INTERROGATED THE PSEU MEMORY AND FOUND CODES S30, S31, S32, DI14, DI15, INDICATING THE NOSE DOOR WAS OPEN AND DID NOT CLOSE AND LOCK WITHIN 30 SECONDS. SUSPECTED TO BE CAUSED BY RETRACTION ABOVE ESTABLISHED RETRACTION SPEED. PERFORMED RIGGING CHECK AND AND INSPECTION OF THE FORWARD NLG DOOR REF CRJ AMM 32-22-01. OPS CHECK GOOD WITH NO DISCREPANCIES NOTED AT THIS TIME. PERFORMED OVERSPEED CONDITION INSPECTION PLEASE REFERENCE AML 1355934 FOR CORRECTIVE ACTION. NO 30 DAY HISTORY NOTED, AIRCRAFT OKAY FOR CONTINUED SERVICE AT THIS TIME.

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 39,326 hrs · 38,958 cycles

TRANSFER FROM EAML 1226325 : HAD ARCING ON THE CAPTAIN€™S SIDE WINDSHIELD DURING CRUISE. DURING THE DESCENT THE WINDSHIELD STARTED CRACKING ON THE OUTSIDE. ALL APPLICABLE QRHS WERE COMPLIED WITH. (FLIGHT 5060 - FILED CLOSED) SEE CP 27284480 FOR REMOVAL OF CAPTAIN SIDE WINDSHIELD. INSTALLED CA SIDE WINDSHIELD IN REFERENCE TO TASK CARD 56-220-1000-SKY AND AMM 56-11-01. OPS CHECK AND LEAK CHECK GOOD. OK FOR SERVICE

Part: UNKNOWN — WARNING MESSAGE (UNKNOWN) · airframe 39,102 hrs · 38,722 cycles

GEAR DISAGREE WARNING MSG POSTED SHORTLY AFTER TAKEOFF AND DURING INITIAL TURNOUT. AIRSPEED APPROX 160 KIAS AND ALTITUDE AROUND 600 AGL. LEFT MAIN GEAR SHOWED A RED INDICATION. GEAR MANUAL RELEASE HANDLE WAS PULLED PER QRH AND ALL GEAR RETURNED TO GREEN INDICATIONS. MAX 195 KIAS MAINTAINED DURING MANEUVERING AND RETURN TO FIELD. (FLT 2934 FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 26992613 WITH THE FOLLOWING CORRECTIVE ACTION: "REFERENCE CP 26992699 FOR CORRECTIVE ACTION. AND CP 26995386 FOR GEAR SWINGS "

Part: UNKNOWN — GOUGED (UNKNOWN) · airframe 38,715 hrs · 38,351 cycles

COMPLY WITH PERMANENT REPAIR OF GOUGE DAMAGE TO CARGO DOOR OUTER SKIN UPPER EDGE BETWEEN FS589.00 - FS605.00 PER REO 601R-52-31-404. THIS IS CLASSIFIED AS A MAJOR REPAIR. FORM M-337 INITIATED. (FILED CLOSED)COMPLIED WITH PERMANENT REPAIR OF CARGO DOOR OUTER SKIN UPPER EDGE BETWEEN FS589.00 - FS605.00 PER REO 601R-52-31-404 REV -A DATED 2023-04-25.

Part: UNKNOWN — GOUGED (UNKNOWN) · airframe 38,715 hrs · 38,351 cycles

COMPLY WITH PERMANENT REPAIR OF GOUGE DAMAGE TO CARGO DOOR OUTER SKIN UPPER EDGE BETWEEN FS589.00 - FS605.00 PER REO 601R-52-31-404. THIS IS CLASSIFIED AS A MAJOR REPAIR. FORM M-337 INITIATED. (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS

Part: WINDSHIELD — CRACKED (L1) · airframe 38,377 hrs · 38,036 cycles

L WSHLD CRACKED ACROSS HALF THE WINDOW. (FILED CLOSED)REMOVED, AND REPLACED LEFT WINDSHIELD AS REQUIRED REF AMM AMM 56-11-01, SEE CARD 56-220-1000-SKY OPS AND LEAK CHECKS GOOD.

Part: NONE — CORRODED · airframe 37,283 hrs · 36,894 cycles

L/H FLIGHT SPOILER I/B PCU FAILS BACKLASH CHECK. TROUBLESHOOT & REPAIR AS REQUIRED PER MM & COMPLETE BACKLASH CHECK OF FLIGHT SPOILER I/B PCU (C CHECK RO 1/20/22) REMOVED AND REPLACED LOWER MOUNTING HARDWARE AT LH FLIGHT SPOILER INBOARD PCU IAW CRJ 200 AMM 27-62-01. COMPLETED BACKLASH CHECK OF LH FLIGHT SPOILER INBOARD PCU. CHECK IS GOOD IAW CRJ 200 AMM 27-64-05. / CALIBRATED TOOLS USED: / DIAL INDICATOR AV7157C CAL DUE: DEC 22 / FORCE GAUGE AG1380 CAL DUE: SEP 22 / TORQUE WRENCH AV3067 CAL DUE: SEP 22 / DIGITAL SCALE AV5118 CAL DUE: JUL 22

Part: NONE — CORRODED · airframe 37,283 hrs · 36,894 cycles

CARGO DOOR KICKPLATE AFT HINGE SECTION HAS CORROSION (C CHECK RO 1/20/22) REMOVED AND REPLACED HINGE ON CARGO DOOR KICKPLATE AFT HINGE SECTION IAW CRJ 200 SRM 51-40-11 AND SRM 51-42-06

Part: NONE — DAMAGED · airframe 37,283 hrs · 36,894 cycles

INSTALL SERVICEABLE FLAP L/H I/B (C CHECK RO 1/20/22) REMOVED L/H I/B UNSERVICEABLE FLAP AND REPLACED WITH SERVICEABLE FLAP IAW CRJ 200 AMM 27-54-01-000-801 AND CRJ 200 AMM 27-54-01-400-801. REMOVED AND REPLACED L/H I/B FLAP #1 AND #2 ACTUATORS IAW CRJ 200 AMM 27-53-01-000-801 AND CRJ 200 AMM 27-53-01-400-801. RIGGED FLAPS IAW CRJ 200 AMM 27-54-00-830-801.PERFORMED OPERATIONAL TEST OF THE FLAPS IAW CRJ 200 AMM 27-54-00-710-801. OPERATIONAL TEST GOOD NO DEFECTS NOTED. / CALIBRATED TOOLS: / TORQUE WRENCH AV7334 CAL DUE: DEC21 / TORQUE WRENCH AV7325 CAL DUE: AUG22 / VERNIER CALIPERS AG1167 CAL DUE: FEB22 / TORQUE WRENCH AV7328 CAL DUE: JUL22 / TORQUE WRENCH AV7139 CAL DUE: SEP22 / TORQUE WRENCH AV7624 CAL DUE: AUG22

Part: NONE — WORN · airframe 37,283 hrs · 36,894 cycles

REPLACE I/B BUSHINGS ON I/B R/H GROUND SPOILER (C CHECK RO 1/20/22) REPLACED INBOARD BUSHING ON INBOARD RH GROUND SPOILER IAW CRJ 200 AMM 20-26-00 AND REO 601R-57-51-982 REV -A DATED 2022-01-19 ANALASIS TO DETERMIN ADDITIONAL REQUIREMENTS WILL BE COMPLETED WITHIN 12 MONTHS OF THE ISSUE DATE OF THIS REPAIR (AIRCRAFT MUST NOT BE OPERATED BAYOND 12 MONTHS FROM THE ISSUE DATE OF THIS REPAIR)

Part: NONE — DAMAGED · airframe 37,283 hrs · 36,894 cycles

2 DAMAGED HOLES ON R/H CHECK PANEL (C CHECK RO 1/20/22) OPENED UP (2) HOLES AND INSTALLED FREEZE PLUG BUSHINGS IAW CRJ200 BOMBARDIER REO 601R-53-11-162. REV. D. DATE: 2019-02-05. / BUSHINGS FABRICATED BY OUTSIDE VENDOR SEE ATTACHED INVOUIC # 12684CURRENT TAT 27,282. TAC 36,894. REPEAT DETAILED VISUAL INSPECTION. (IAW: BOMBADIER CRJ200 NDTM 51-53-11-097 PART #9) EVERY 4695 FC. NEXT INSPECTION DUE 41,589 FC. PRESSURE CHECK GOOD IAW CRJ200 AMM21-31-00. / CALIBRATED TOOLS USED: / MICROMETER AG1308 CAL DUE JUL2022 / OLYMPUS 600 NORTEC AV8958 CAL DUE OCT2022

Part: NONE — CORRODED · airframe 37,283 hrs · 36,894 cycles

RIGHT SIDE SEAT RAILS FROM FS 349.00 TO FS 559+80 HAVE AREAS OF CORROSION & SURFACE WEAR IN VARIOUS SPOTS (C CHECK RO 1/20/22) REMOVED RIGHT HAND SEAT RAILS FROM 349.00 TO 559.00+80. EVALUATED CONDITION OF EACH RAIL. CLEANED CORROSION AS REQUIRED IAW CRJ200 AMM 53-21-49. INSTALLED NEW SEAT TRACK AS REQUIRED, INSTALLED REPAIRED TRACK AS REQUIRED IAW CRJ 200 AMM 53-01-11. / CALIBRATED TOOLS USED: TORQUE WRENCH AV6522 CAL DUE-AUG22, DIGITAL CALIPER AV7110 CAL DUE-AUG22.

Part: NONE — DAMAGED · airframe 37,283 hrs · 36,894 cycles

REPLACE DOUBLE GROMMET ON LOWER L/H NOSE COWLING (C CHECK RO 1/20/22) REMOVED & REPLACED DOUBLE GROMMET ON LOWER L/H NOSE COWLING. .INSTALLATION COMPLETE, IAW CRJ 200 CMM 71-14-01

Part: NONE — MISLOCATED · airframe 37,283 hrs · 36,894 cycles

UPPER FORWARD ROLLER ON CARGO DOOR IS MISSING THE ROLLING PART (C CHECK RO 1/20/22) / REPLACED UPPER FORWARD ROLLER ASSEMBLY ON CARGO DOOR IAW CRJ 200 AMM 52-31-00 / TORQUE WRENCH-AG1132-5AUG2022

Part: NONE — GOUGED · airframe 37,283 hrs · 36,894 cycles

SEAT TRACK LBL9 FROM FS559 TO FS559+80 MULTIPLE GOUGES AND CORROSION MARKED IN RED GREASE PENCIL (C CHECK RO 1/20/22) REMOVED UNSERVICEABLE SEAT TRACKS AND INSTALLED SERVICEABLE TRACKS FROM F/S 559 TO F/S 559+80 LBL9 IAW CRJ 200 AMM 53-01-11-400-802

Part: NONE — GOUGED · airframe 37,283 hrs · 36,894 cycles

SEAT TRACK RBL9 FROM FS559 TO FS559+80 MULTIPLE GOUGES AND CORROSION MARKED IN RED GREASE PENCIL (C CHECK RO 1/20/22) REMOVED UNSERVICEABLE SEAT TRACKS AND INSTALLED SERVICEABLE TRACKS FROM F/S 559 TO F/S 559+80 RBL9 IAW CRJ 200 AMM 53-01-11-400-802

Part: NONE — CORRODED · airframe 37,283 hrs · 36,894 cycles

L/H LONGERON PRESSURE FLOOR ANGLE FS409+128 TO FS559 CORROSION AS MARKED (C CHECK RO 1/20/22) CORROSION DAMAGE ON L/H LONGERON PRESSURE FLOOR ANGLE FS409+128 TO FS559 REMOVED, ORIGINAL THICKNESS 0.080", DAMAGE REMOVED WAS 0.008", REMAINING THICKNESS 0.072". DAMAGE FOUND TO BE WITHIN LIMITS IAW REO 601R-53-41-666 REV -C DATE: 2012-11-06. RESTORED SURFACE FINISH IAW CRJ 200 SRM 51-21-16. TRESHOLD REPEAT INSPECTION AT 8260 FLIGHT CYCLES. CURRENT FLIGHT CYCLES 36,894 NEXT INSPECTION DUE 45,154 FLIGHT CYCLES. IAW: REO 601R-53-41-666 REV-C- 2012-11-06, SHEET #2. PRESSURE CHECK GOOD IAW AMM21-31-00. / CALIBRATED TOOLS USED: / OLYMPUS 650 EPOC AV8959 CAL DUE OCT2021 / OLUMPUS 600 NORTEC AV8958 CAL DUE OCT2021

Part: NONE — CORRODED · airframe 37,283 hrs · 36,894 cycles

R/H LONERON PRESSURE FLOOR ANGLE FS409+128 TO FS559 CORROSION AS MARKED (C CHECK RO 1/20/22) CORROSION DAMAGE ON R/H LONGERON PRESSURE FLOOR ANGLE FS409+128 TO FS559 REMOVED, ORIGNAL THICKNESS 0.080", DAMAGE REMOVED WAS 0.003", REMAINING THICKNESS 0.077". DAMAGE FOUND TO BE WITHIN LIMITS IAW REO 601R-53-41-666 REV-C DATE: 2012-11-06. RESTORED SURFACE FINISH IAW CRJ200 SRM 51-21-16 TRESHOLD REPEAT INSPECTION AT 8260 FLIGHT CYCLES. CURRENT FLIGHT CYCLES 36,894 NEXT INSPECTION DUE AT 45,154 FLIGHTT CYCLES. IAW: REO601R-53-41-666 REV-C- 2021-11-06, SHEET #2. PERFORMED PRESSURE CHECK IAW CRJ200 AMM 21-31-00 REV 64 SEPT10/2021. / CALIBRATED TOOLS USED: / OLYMPUS 650 EPOC AV8959 CAL DUE OCT2021 / OLUMPUS 600 NORTEC AV8958 CAL DUE OCT2021

Part: NONE — CORRODED · airframe 37,283 hrs · 36,894 cycles

R/H LONGERON PRESSURE FLOOR SILL PANEL FS409+128 TO FS559 CORROSION AS MARKED (C CHECK RO 1/20/22) CORROSION DAMAGE ON R/H LONGERON PRESSURE FLOOR SILL PANEL FS409+128 TO FS559 REMOVED, ORIGINAL THICKNESS 0.055", DAMAGE REMOVED WAS 0.004", REMAINING THICKNESS 0.051". DAMAGE FOUND TO BE WITHIN LIMTS IAW REO 601R-53-41-666 REV-C DATE: 2012-11-06. REINSTALLED FASTNERS IAW REO ANDCRJ200 SRM 51-45-00 AND 51-42-21. RESTORED SURFACE FINISH IAW CRJ200 SRM 51-21-16. THRESHOLD REPEAT INSPECTION AT 8260 FLIGHT CYCLES. CURRENT FLIGHT CYCLES 36,894 NEXT INSPECTION DUE AT 45,154 FLIGHT CYCLES.IAW REO 601R-53-41-666 REV-C-- 2012-11-06, SHEET 2. PERFOMED PRESSSURE CHECK IAW CRJ 200 AMM 21-31-00. PRESSURE CHECK GOOD.IAW CRJ200 AMM 21-31-00 REV64 10 SEPT/2021. / CALIBRATED TOOLS USED: / OLYMPUS 650 EPOC AV8959 CAL DUE OCT2021 / OLUMPUS 600 NORTEC AV8958 CAL DUE OCT2021

Part: NONE — CORRODED · airframe 37,283 hrs · 36,894 cycles

L/H LONGERON PRESSURE FLOOR SILL PANEL FS409+128 TO FS559 CORROSION AS MARKED (C CHECK RO 1/20/22) CORROSION DAMAGE ON L/H PRESSURE FLOOR SILL PANEL FS409+128 TO FS 559 REMOVED, ORIGINAL THICKNESS 0.055", DAMAGE REMOVED WAS 0.011", REMAINING THICKNESS 0.044". DAMAGE FOUND TO BE WITHIN LIMITS IAW REO 601R-53-41-666 REV-C DATE: 2012-11-06. REINSTALLED FASTNERS PER CRJ200 SRM 51-42-21, SRM 51-45-00. RESTORED SURFACE FINISH IAW CRJ200 SRM 51-21-16. TRESHOLD REPEAT INSPECTION AT 8260 FLIGHT CYCLES.CURRENT FLIGHT CYCLES 36,894 NEXT INSPECTION DUE AT 45,154 FLIGHT CYCLES. IAW: REO601R-53-41-666 REV-C- DATED 2012-11-06, SHEET #2. PRESSURE CHECK GOOD. IAW CRJ 200 AMM 21-31-00 / CALIBRATED TOOLS USED: / OLYMPUS 650 EPOC AV8959 CAL DUE OCT2021 / OLUMPUS 600 NORTEC AV8958 CAL DUE OCT2021

Part: NONE — GOUGED · airframe 37,283 hrs · 36,894 cycles

F/S 409+ 128 TO F/S 559 RBL 9 SEAT TRACK MULTIPLE AREAS OF GOUGES & CORROSION MARKED IN RED GREASE PENCIL- EVAL (C CHECK RO 1/20/22) REMOVED UNSERVICEABLE SEAT TRACKS AND INSTALLED SERVICEABLE TRACKS FROM F/S 409+128 TO F/S 559 RBL9 IAW CRJ 200 AMM 53-01-11-400-802

Part: NONE — GOUGED · airframe 37,283 hrs · 36,894 cycles

F/S 409+ 128 TO F/S 559 LBL 9 SEAT TRACK MULTIPLE AREAS OF GOUGES & CORROSION MARKED IN RED GREASE PENCIL- EVAL (C CHECK RO 1/20/22) REMOVED UNSERVICEABLE SEAT TRACKS AND INSTALLED SERVICEABLE TRACKS FROM F/S 409+128 TO F/S 559 LBL9 IAW CRJ 200 AMM 53-01-11-400-802 CALIBRATED TOOL USED: TORQUE WRENCH AV7330 CAL DUE DEC 21

Part: NONE — GOUGED · airframe 37,283 hrs · 36,894 cycles

F/S 370 TO F/S 409+ 116 RBL 9 SEAT TRACK MULTIPLE AREAS OF GOUGES & COROSION MARKED IN RED GREASE PENCIL- EVAL (C CHECK RO 1/20/22) REMOVED USERVICEABLE SEAT TRACKS AND INSTALLED SERVICEABLE TRACKS FORM F/S 370 TO 409+116 RBL 9 IAW CRJ 200 AMM 53-01-11 / CALIBRATED TOOLS: / TORQUE WRENCH: AV7327 CAL DUE: DEC 21

Part: NONE — CRACKED · airframe 37,283 hrs · 36,894 cycles

FS 628 STR 15 & 16L CRACKED FOUND DURING NDT INSPECTION OF FS 625 SPLICE SPAR & WEB INSPECTION (C CHECK RO 1/20/22) REMOVED AND REPLACED FS 628 STR 15L AND 16L ANGLES IAW CRJ200 SRM 51-24-38, SRM 51-42-21 FABRICATED REPLACEMENT PARTS, PARTS IDENTIFIED AS AVMAX PN WO 51264 WC 2569 IAW AVMAX QUALITY BULLETIN NO. 2012-08-002 REV 5

Part: NONE — CORRODED · airframe 37,283 hrs · 36,894 cycles

R/H HORIZONTAL REAR SPAR RBL 16 & RBL 95 GROUND STUDS CORRODED 2 EACH FLAGGED (C CHECK RO 1/20/22) REMOVED & REPLACED RH HORIZONTAL REAR SPAR RBL 16 AND RBL 95 GROUND STUDS IAW CRJ200 AMM 51-80-00. / CALIBRATED TOOL USE . TORQUE WRENCH AV7326, CAL DUE DATE MAR 2022

Part: NONE — DENTED · airframe 37,283 hrs · 36,894 cycles

THERE'S DENT ON LOWER SKIN AT FS 589 BETWEEN STGR 26, 25 AND STGER 24 (C CHECK RO 1/20/22) REPAIRED FUSELAGE SKIN BETWEEN FS574.00 - FS621.00 STR24R- 24L. IAW REO601R-53-61-7719 REV-- DATED 2021-10-16 AND CRJ200 SRM 53-00-31. AIRCRAFT NOT TO BE OPERATED BEYOND 12 MONTHS FROM ISSUE DATE OF REPAIR. ANALYSIS TO DETERMINE ADDITIONAL REQUIREMENTS WILL BE ACCOMPLISHED WITHIN 12 MONTHS. IAW: REO 601R-53-61-7719 REV -- DATED 2021-10-16, SHEET #2. / ACCOMPLSHED PRESSURE CHECK IAW CRJ200 SRM 51-23-01. PRESSSURE CHECK GOOD. IAW CRJ 200 AMM 21-31-00 / CALIBRATED TOOLS USED: / DEPTH GAUAGE AG1186 CAL DUE JAN2022 / OLYMPUS 600 NORTEC AV8958 CAL DUE SEP2021

Part: NONE — BROKEN · airframe 37,283 hrs · 36,894 cycles

SERVICE DOOR FORWARD FROM TOP STOP BROKEN (C CHECK RO 1/20/22) REMOVED AND REPLACED SERVICE DOOR STOP AND ADJUSTED THE SCREW IAW CRJ 200 AMM 52-41-00

Part: NONE — CORRODED · airframe 37,283 hrs · 36,894 cycles

L/H FLIGHT SPOILER I/B HINGE BOLT KEEPER BOLTS CORRODED (C CHECK RO 1/20/22) REPLACED L/H FLIGHT SPOILER I/B HINGE BOLT KEEPER BOLTS IAW CRJ 200 AMM 27-64-05 USING TORQUE WRENCH AG1132 CAL DUE AUG 22, SAFETY CABLE GUN AV6061 CAL DUE JUN 22

Part: NONE — CORRODED · airframe 37,283 hrs · 36,894 cycles

L/H FLIGHT SPOILER I/B & O/B ACTUATOR HINGE BOLTS NUTS CORROSION (C CHECK RO 1/20/22) REMOVED AND REPLACED CORRODED FASTENERS ON L/H FLIGHT SPOILER I/B & O/B ACTUATOR HINGE IAW CRJ 200 AMM 27-64-05 / TORQUE WRENCH-AV5920-OCT21

Part: NONE — CORRODED · airframe 37,283 hrs · 36,894 cycles

I/B GROUND SPOILER O/B HINGE BOLT NUT CORRODED (C CHECK RO 1/20/22) REMOVED AND REPLACED O/B HINGE BOLT NUT ON THE I/B GROUND SPOILER IAW CRJ200 AMM 27-65-01. / TORQUE WRENCH AG1132 CAL DUE: AUG 2022

Part: NONE — CORRODED · airframe 37,283 hrs · 36,894 cycles

L/H AILERON FLUTTER DAMPNER ATTACH CLEVIS CORROSION LOWER EDGES OF LEGS (C CHECK RO 1/20/22) REMOVED AND INSTALLED NEW CLEVIS TO L/H AILERON FLUTTER DAMPENER IAW CRJ 200 AMM 27-15-05 / CALIBRATED TOOLING: TORQUE WRENCH AV 7334 CAL. DUE DEC. 21, TORQUE WRENCH AV 1655 CAL. DUE DEC 21

Part: NONE — CORRODED · airframe 37,283 hrs · 36,894 cycles

R/H FLIGHT SPOILER AT CENTER HINGE FITTING WS 191.44 WS 183.00 & I/B SPAR WS 162.49 LOCK BOLTS PLATES SCREWS ARE CORRODED TOTAL 8 SCREWS FLAGGED (C CHECK RO 1/20/22) R/H FLIGHT SPOILER AT CENTER HINGE FITTING WS 191.44 WS 183.00 & I/B SPAR WS 162.49 LOCK BOLTS PLATE SCREWS REPLACED AS NECESSARY IAW CRJ200 AMM 20-21-00 / CALIBRATED TOOL USED: TORQUE WRENCH AV 5920 CAL DUE OCT 2021

Part: NONE — CORRODED · airframe 37,283 hrs · 36,894 cycles

R/H WING SPOILERON, GROUNDING STRAPS ON CENTER AND I/B HINGE FITTINGS HAVE CORRODED HARDWARE (C CHECK RO 1/20/22) REMOVED CORROSION FROM ATTACHING HARD WEAR IAW CRJ 200 SRM 51-21-06

Part: NONE — DAMAGED · airframe 37,283 hrs · 36,894 cycles

REMOVE AND REINSTALL RH IB FLAP ASSY (C CHECK RO 1/20/22) REMOVED AND INSTALLED SERVICEABLE R/H I/B FLAP ASSY IAW CRJ 200 AMM 27-54-01 AND TASK 27-900-1006-SKY. PERFORMED OPS CKECK IAW CRJ 200 AMM 27-54-00-710-801. OPS CHECK GOOD. / TORQUE WRENCH AG1132 CAL DUE: AUG 2022

Part: NONE — DAMAGED · airframe 37,283 hrs · 36,894 cycles

REMOVE AND REINSTALL LH IB FLAP ASSY (C CHECK RO 1/20/22) REMOVED AND REPLACED L/H I/B FLAP ASSY IAW CRJ 200 AMM 27-54-01-000-801 AND 27-54-01-400-801 / CALIBRATED TOOLS: / TORQUE WRENCH AV1655 CAL DATE: DEC21 / TORQUE WRENCH AV2050 CAL DATE: JUN22 / TORQUE WRENCH AG1132 CAL DATE AUG22

Part: NONE — DAMAGED · airframe 37,283 hrs · 36,894 cycles

REMOVE AND REINSTALL LH OB FLAP ASSY (C CHECK RO 1/20/22) REMOVED AND INSTALLED NEW SERVICEABLE L/H O/B FLAP ASSY IAW CRJ 200 AMM 27-54-05-400-801. OPS CHECK GOOD NO DEFECTS NOTED. CALIBRATED TOOLS USED: TORQUE WRENCH AV7335 CAL DUE: MAR 22.

Part: NONE — WORN · airframe 37,283 hrs · 36,894 cycles

REMOVE AND REPLACE BUSHINGS AND HARDWARE ON RH AILERON WING AFT SPAR REF CRJ 200 AMM 20-26-00-910-804 (C CHECK RO 1/20/22) REMOVED RH AILERON HINGE FITTING BUSHINGS LOCATED AT RH WING AFT SPAR. / REPLACEMENT BUSHINGS INSTALLED AND REAMING TO SIZE COMPLETED AT INBOARD AND CENTER HINGE FITTINGS. / OUTBOARD HINGE FITTING REPLACEMENT BUSHINGS INSTALLED AND REAMING TO SIZE COMPLETED ON W/C 6200, CP 23971412. / REPLACEMENT HARDWARE FOR INSTALLATION OF RH AILERON ORDERED AND INSTALLED ON W/C 6119 CP22892654. / WORK ACCOMPLISHED IAW CRJ 200 AMM 20-26-00-910-803, AMM 20-26-00-910-804, SRM 51-40-11.

Part: NONE — WORN · airframe 37,283 hrs · 36,894 cycles

REMOVE AND REPLACE BUSHINGS AND HARDWARE ON LH AILERON WING AFT SPAR REF CRJ 200 AMM 20-26-00-910-804 (C CHECK RO 1/20/22) REMOVED LH AILERON HINGE FITTING BUSHINGS LOCATED AT LH WING AFT SPAR. REPLACEMENT BUSHINGS INSTALLED AND REAMING TO SIZE COMPLETE AT INBOARD AND CENTER HINGE FITTINGS. OUTBOARD HINGE FITTING REPLACEMENT BUSHINGS AND REAMING TO SIZE COMPLETED ON W/C 5315. 23832660 / REPLACEMENT HARDWARE FOR INSTALLATION OF LH AILERON OREDERED AND INSTALLED ON W/C 5174. 22892653 / WORK ACCOMPLISHED IAW CRJ 200 AMM 20-26-00--910-803, AMM 20-26-00-910-804, SRM 51-40-11

Part: UNKNOWN — PRESSURE LOSS (CABIN) · airframe 37,067 hrs · 36,707 cycles

ON CLIMBOUT THRU FL160 CREW RECEIVED A CABIN ALT PRESSURE MESSAGE. CREW OBSERVED CABIN ALT CLIMBING RAPIDLY. LEVELED OFF AND REQUEST DECENT TO ATC. EMERGENCY DECLARED AND DECENT MADE. ONCE BELOW 8000 FT THE CABIN RETURNED TO NORMAL PRESSURIZATION. CHECKED CPCP CANNON PLUGS AND OPS CHECKED IAW CRJ200 AMM. OPS CHECK GOOD. CHECKED CANNON PLUGS FOR CPC IAW AMM. OPS CHECK GOOD. CHECKED CPAM CANNON PLUGS IAW CRJ200 AMM. OPS CHECKED GOOD. PRESSURE TEST OPS. CHECK IAW AMM. NO DEFECTS NOTED.

Part: WARNING MESSAGE — FALSE ACTIVATION (PITOT HEAT) · airframe 36,673 hrs · 36,363 cycles

CREW RECEIVED PITOT HEAT BASE AMBER MSG. THEY RAN THEIR QRH AND DECIDED TO RETURN TO DCA WHERE THEY LANDED WITHOUT INCIDENT. PERFORMED OPERATIONAL CHECK OF THE AIR DATA SENOR HEATER CONTROLLER IAW CRJ200 AMM 30-31-15-710-801 AND OPS CHECKS FOUND GOOD AT THIS TIME.

Part: SKIN — CRACKED (RT WING) · airframe 34,451 hrs · 36,161 cycles

CRACK FOUND AT RH WING LOWER PLANK BETWEEN FUEL PANELS 640CB AND 640DB. C/A: REPAIRED THE RH WING LOWER PLANK AROUND DRAIN HOLE AT W.S. 85.5 BETWEEN STRINGER 14R-15R IAW BBD REO 610R-57-21-3206 REV --, DATED 2019-11-28.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 34,432 hrs · 34,271 cycles

AS GEAR WAS SELECTED UP, THE CREW RECEIVED A STAB AND MACH TRIM AMBER CAUTION MESSAGE. THE CREW DECLARED AN EMERGENCY. THE AIRCRAFT LANDED WITHOUT FURTHUR INCIDENTS. THE AIRCRAFT IS CURRENTLY IN MAINTENANCE.

Part: CONTROL UNIT — UNKNOWN · airframe 34,432 hrs · 34,271 cycles

SUPPLEMENTAL INFORMATION: MX C/W FUNCTIONAL CHECK OF HSTCU IAW CRJ200 AMM. FUNCTIONAL CHECK GOOD. OPS CHECK GOOD. OCF CHECK GOOD.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 34,354 hrs · 34,206 cycles

DISCREPANCY: LBL9 AND RBL9 FS 559 TO FS 559+80 FLOOR SEAT TRACK SEGMENTS ARE CORRODED. C/A: REMOVED AND REPLACED SEAT TRACK BY FABBING AND ISTALLING IAW REO 601R-53-00-485 AND AMM 53-01-11-400-802.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 34,354 hrs · 34,206 cycles

FS621 RPB WEB HAS AN AREA OF CRACK INDICATIONS NOTED IN THE "HEEL LINE" AREA OF VERTICAL POST AT LBL36 WL112.5-WL114 100%FSH. FAILED NDT UT INSP. C/A: COMPLIED WITH REO 601R-53-61-6815.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 34,354 hrs · 34,206 cycles

RBL 9 FLOORBEAM IS CORRODED FROM FS 559+48 TO FS 559+80. C/A: REPAIRED IAW REO 601R-53-00-27.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,354 hrs · 34,206 cycles

LBL 9 AND RBL 9 FS 399 TO FS 409+128 FLOOR SEAT TRACK SEGMENTS ARE CORRODED. C/A: INSTALLED LBL9 & RBL9 FS399 TO FS409+128 FLOOR SEAT TRACK SEGMENTS IAW AMM 53-01-11-400-802 P/N:N126-2075.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,354 hrs · 34,206 cycles

LB 9 AND RBL 9 FS 364 TO FS 399 FLOOR SEAT TRACK SEGMENTS ARE CORRODED. C/A: INSTALLED LBL9 AND RBL FS364 TO FS399 FLOOR SEAT TRACK SEGMENTS IAW AMM 53-01-11-400-802 P/N: N126-2075

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 34,354 hrs · 34,206 cycles

DISCREPANCY: LBL9 AND RBL9 FS 409+128 TO FS 559 FLOOR SEAT TRACK SEGMENTS ARE CORRODED. C/A: REMOVED AND REPLACED SEAT TRACK BY FABBING AND ISTALLING IAW REO 601R-53-00-485 AND AMM 53-01-11-400-802.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 34,354 hrs · 34,206 cycles

FS621 RPB WEB HAS 7EA AREAS OF CRACK INDICATIONS NOTED IN THE "HEEL LINE" AREA OF VERTICAL POSTS. AREA NR 1 - RBL27 WL128-WL132.5 70% FSH ET, NR 2 - RBL27 WL84-WL102 70% FSH ET, NR 3 - RBL9 WL105-WL114 50% FSH ET, NR 4 - LBL9 WL106-WL107.5 50% FSH ET, NR 5 - LBL18 WL126-WL134 60% FSH ET, NR 6 - LBL18 WL109-WL114 60% FSH ET AND NR 7 - RBL36 WL93.5-WL95 100% FSH UT. ALL 7 AREAS FAILED NDT INSP AND ARE MARKED ON THE A/C. C/A: REPAIRED IAW GREO 601R-53-61-1240 REV D

Part: WARNING MESSAGE — ILLUMINATED (A/C PACKS) · airframe 31,600 hrs · 31,597 cycles

CREW REPORTED THAT SHORTLY AFTER TAKEOFF WHEN TRANSFERRING BLEED AIR FROM THE APU TO THE ENGINE BLEEDS RECEIVING A RT AND LT PACK HIGH PRESSURE MESSAGE. THE CREW DECLARED AN EMERGENCY. RAN THE QRH AND THE MESSAGE DID NOT DISAPPEAR. TRANSFERRED THE BLEEDS BACK TO THE APU THE MESSAGE WENT AWAY. CANCELED THE EMERGENCY AND RETURNED TO DEPARTURE AS A PRECAUTION. PERFORMED ENGINE RUNS, OPS CHECKED GOOD.

Part: PRESSURE BLKHD — CRACKED (FUSELAGE) · airframe 30,506 hrs · 30,520 cycles

PERFORMED A MAJOR REPAIR TO THE FS 621.0 REAR PRESSURE BULKHEAD WEB AT LBL 27.50 WL 112.

Part: PRESSURE BLKHD — CRACKED (FUSELAGE) · airframe 30,506 hrs · 30,520 cycles

PERFORMED A MAJOR REPAIR TO THE FS 621.0 REAR PRESSURE BULKHEAD WEB AT BL 0.00 WL 113 AND WL 135, RBL 27.5 WL 114 AND RBL 18.00 WL 112 AND WL 134.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 30,506 hrs · 30,520 cycles

PASSENGER DOOR CUTOUT LOWER SILL ANGLE HAS SURFACE CORROSION BETWEEN FS 310.00 AND FS 349.00. REMOVED AND REPLACED PASSENGER DOOR LOWER SILL ANGLE BETWEEN FS 310.00 AND FS 349.00.

Part: POSITION SENSOR — WARNING MESSAGE (FLIGHT CONTROLS) · airframe 29,991 hrs · 30,048 cycles

FLAPS FAIL CAUTION MESSAGE AT ZERO DEGREES ON APPROACH. THE CREW DECLARED AN EMERGENCY, CONTINUE TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACE THE LEFT HAND BRAKE AND POSITION SENSOR UNIT, AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: UNKNOWN — SMOKE (CABIN) · airframe 29,897 hrs · 29,957 cycles

SLIGHT BURNING ODOR APPEARS TO BE COMING FROM AIR VENTS. MAINTENANCE DEFERRED LT PACK THEN OPS CHECK LT PACK AND CLEARED THE MEL. THE ACFT WAS RELEASED FOR SERVICE.

Part: TRIM SWITCH — FAILED (STAB) · airframe 29,125 hrs · 29,193 cycles

CREW REPORTED RECEIVING STABILIZER TRIM CAUTION MESSAGED AND A STABILIZER TRIM RUNAWAY WARNING DURING CLIMBOUT AT FL010. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R THE PITCH TRIM DISCONNECT SWITCH, AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.

Part: CONTROL UNIT — FAILED (TE FLAPS) · airframe 28,946 hrs · 29,021 cycles

CREW REPORTED FLAPS FAIL CAUTION MESSAGE ON FLAPS EXTENSION AT 45 DEGREES. CREW LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT IAW FIM, R & R FLAP ELECTRONIC CONTROL UNIT AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: SENSOR — FAILED (FLAP CONTROL SYS) · airframe 28,942 hrs · 29,017 cycles

CREW REPORTED FLAPS FAIL MESSAGE AT 4000 FT AFTER SELECTING FLAPS 8 DEGREES. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R THE RT BRAKE AND POSITION SENSOR UNIT AND PERFORMED CHECKS IAW THE AMM. ACFT RELEASED FOR SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 28,730 hrs · 28,813 cycles

CREW REPORTED EMERGENCY EXIT SIGN BY PASSENGER DOOR INOPERATIVE. MAINTENANCE INSPECTED, REPAIRED BROKEN WIRE ON EMERGENCY LIGHT AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: FRAME — CORRODED (FS 605) · corrosion level 2 · airframe 27,685 hrs · 27,766 cycles

FRAME AT FS 605 HAS CORROSION BETWEEN STR 27 AND STR 26L. REMOVED CORRODED FRAME AND INSTALLED A SERVICABLE FRAME.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,685 hrs · 27,766 cycles

BS 319 - 349 SERVICE DOOR LOWER SILL ANGLE HAS CORROSION. R & R SERVICE DOOR SILL ANGLE IAW SRM.

Part: RETAINER — CORRODED (E/E DOOR SEAL) · corrosion level 2 · airframe 27,685 hrs · 27,766 cycles

MAIN AVIONICS BAY DOOR IS CORRODED UNDER DOOR SEAL, ENTIRE CIRCUMFERENCE HAS FILIFORM CORROSION. R & R SEAL RETAINER IAW SRM.

Part: FRAME SPLICE — CORRODED (BS 621) · airframe 27,685 hrs · 27,766 cycles

FORWARD SIDE OF BS 621 FRAME SPLICE AT STR 27 HAS PITTING CORROSION AND PROTECTIVE COATINGS ARE DETERIORATED BETWEEN STR 25L AND STR 26R AT FS 621. REMOVED MINOR CORROSION ON FORWARD SIDE OF FS 621 FRAME SPLICE AT STRINGER 27 AND APPLIED PROTECTIVE COATING BETWEEN STR 25L AND STR 26R, FS 621 IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 559-621) · airframe 27,685 hrs · 27,766 cycles

RIGHT FLOOR SUPPORT BETWEEN BS 559+96 AND 621 HAS CORROSION. REPAIRED THE FLOOR SUPPORT IAW REO.

Part: SWITCH — FAILED (THRUST REVERSER) · airframe 27,051 hrs · 27,126 cycles

CREW REPORTED RECEIVING REV ICON ON RT ENGINE IN FLIGHT. ALL OTHER ENGINE INDICATIONS WERE NORMAL. AN INTERMITTENT RT REVERSER UNLOCKED CAUTION MESSAGE ALSO RECEIVED DURING CLIMB. CREW RETUNED TO FIELD AND LANDED WITHOUT INCIDENT. INSPECTED THRUST REVERSER SYS & FOUND STOW SWITCH TO BE INTERMITTENT. R & R STOW SWITCH IAW AMM 78-37-01-00000-801. OPS CHECK GOOD.

Part: SHUTOFF VALVE — OUT OF POSITION (AVIONICS COOLING) · airframe 26,872 hrs · 26,953 cycles

CREW REPORTED CABIN NOT PRESSURIZING DURING CLIMBOUT. LEVELED AT 10,000 FT AND CABIN WAS AT 8,000 FT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND OVERBOARD EXHAUST SHUTOFF VALVE, SOV, IN OPEN POSITION. MAINTENANCE SELECTED OVERBOARD EXHAUST SOV TO CLOSED POSITION IAW AMM. ACFT RELEASED FOR SERVICE.

Part: ANTI-ICE VALVE — FAILED (INTAKE) · airframe 26,305 hrs · 26,377 cycles

CREW REPORTED LT COWL ANTI-ICE MESSAGE IN FLIGHT WITH SWITCH OFF. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R LT COWL ANTI-ICE VALVE AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: CARBON SEAL — LEAKING (LT ENGINE) · airframe 22,380 hrs · 22,619 cycles

CREW REPORTED SMOKE TOILET CAUTION MESSAGE DURING CRUISE. FLIGHT ATTENDANT CONFIRMED LAVATORY SMOKE ALARM SOUNDED. SMOKE WAS VISIBLE FROM ROW SIX (6) THROUGH 11. SMOKE TOILET QRH (QUICK REFERENCE HANDBOOK) WAS PERFORMED AND SMOKE DISSIPATED SHORTLY THEREAFTER. CREW DIVERTED AND MADE A SAFE LANDING. AIRCRAFT EVACUATED ON RUNWAY AND PASSENGERS BUSSED TO TERMINAL. MAINTENANCE INSPECTED, REMOVED AND REPLACED NUMBER THREE (3) CARBON SEAL ON LEFT ENGINE DUE TO EVIDENCE OF LEAKING AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: CARBON SEAL — LEAKING (RT ENGINE) · airframe 22,377 hrs · 22,616 cycles

CREW REPORTED SMOKE TOILET CAS MESSAGE CAME ON DURING DESCENT. PASSENGER NEAR LAV REPORTED ELECTRIC BURNING SMELL. CREW RAN QRH (QUICK REFERENCE HANDBOOK) AND LANDED SAFELY. MAINTENANCE INSPECTED LAV AND CABIN AREA, GROUND RAN AIRCRAFT WITH CREW AND RAN AIR CONDITIONING SYSTEM. NO DEFECTS AND NO INDICATIONS OR EVIDENCE OF LAV SMOKE NOTED. MAINTENANCE REMOVED AND REPLACED RIGHT ENGINE NUMBER ONE CARBON SEAL DUE TO EVIDENCE OF LEAKING OIL AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: HEAT EXCHANGER — FAILED (AC BAY) · airframe 22,336 hrs · 22,583 cycles

CREW REPORTED RUNAWAY PACK HIGH TEMP FOLLOWED BY SMOKE TOILET CAUTION MESSAGE DURING TAXI OUT. CREW RETURNED TO GATE. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED RIGHT HEAT EXCHANGER AND RIGHT COALESCER AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,319 hrs · 22,568 cycles

CREW REPORTED EMERGENCY CEILING FLOODLIGHT AT ROW TWO (2) INOPERATIVE. MAINTENANCE INSPECTED, RELAMPED EMERGENCY CEILING FLOODLIGHT AT ROW TWO (2) AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: UNKNOWN — MALFUNCTIONED (CABIN) · airframe 22,196 hrs · 24,465 cycles

CREW RECEIVED SMOKE TOILET MESSAGE WITH VISIBLE SMOKE IN CABIN AT FL210 IN DESCENT. CREW LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REMOVED AND REPLACED THE FOLLOWING: PSU PCB (PASSENGER SERVICE UNIT PRINTED CIRCUIT BOARD) ON ROW 11 D/F (BURNT), SIDEWALL BALLAST ABOVE ROW 12 (BURN MARK), ROW 10 SIDEWALL LAMP (DAMAGED) AND LAV SMOKE DETECTOR (PRECAUTIONARY PURPOSES). CHECKS WERE PERFORMED AND AIRCRAFT RELEASED FOR SERVICE. ALL WORK ACCOMPLISHED BY MAINTENANCE USING AIRCRAFT AND COMPONENT MAINTENANCE MANUALS.

Part: LIGHT — SMOKE (LAVATORY) · airframe 22,016 hrs · 22,306 cycles

CREW REPORTED A SMOKE TOILET MESSAGE WITH SMOKE IN CABIN. MAINTENANCE TROUBLESHOT, DETERMINED THE LIGHT UNIT CAUSED SMOKE, SECURED, AND DEFERED THE LAVATORY LIGHT UNIT. PARTS ARE ON ORDER. SUPPLEMENTAL SDR WILL BE SUBMITTED WHEN REPAIRED. AIRCRAFT WAS RELEASED FOR SERVICE. R & R LAV RETURN TO SEAT SIGN IAW AMM 33-24-04-400-801.

Part: CARBON SEAL — DAMAGED (LT ENGINE) · airframe 21,976 hrs · 22,272 cycles

CREW REPORTED LEFT ENGINE OIL PRESSURE CAS MESSAGE IN FLIGHT. LEFT ENGINE AT IDLE FOR REMAINDER OF FLIGHT AND OIL PRESSURE FLUCTUATING. CREW DECLARED EMERGENCY AND LANDED AT DESTINATION WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT LEFT ENGINE, REMOVED AND REPLACED IDG (INTEGRATED DRIVE GENERATOR) CARBON SEAL AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: UNKNOWN — HAZE (CABIN) · airframe 21,804 hrs · 22,123 cycles

CREW REPORTED TOILET SMOKE CAUTION MESSAGE AND HAZE IN CABIN IN FLIGHT. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED LAV WASTE COMPARTMENT AND PERFORMED CHECKS ON LAV SMOKE DETECTOR, AIR CONDITIONING SYSTEM AND CABIN LIGHTS USING AIRCRAFT MAINTENANCE MANUALS. NO DEFECT NOTED. UNABLE TO DUPLICATE FAULT. AIRCRAFT RELEASED FOR SERVICE.

Part: CARBON SEAL — LEAKING (RT ENGINE) · airframe 21,362 hrs · 21,747 cycles

CREW REPORTED SMOKE TOILET AMBER MESSAGE IN FLIGHT. CREW FOLLOWED QRH. MESSAGE EXTINGUISHED PRIOR TO LANDING. CREW LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED RIGHT ENGINE NUMBER ONE CARBON SEAL AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: CARBON SEAL — LEAKING (RT ENGINE) · airframe 20,746 hrs · 21,202 cycles

CREW REPORTED SMOKE / TOILET CAS MESSAGE IN FLIGHT. CREW DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED, REMOVED AND REPLACED NUMBER 1 AND NUMBER 3 CARBON SEALS FOR RIGHT ENGINE (DUE TO LEAKING) AND PERFORMED CHECKS USING AIRCRAFT AND ENGINE MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: MOTOR — MALFUNCTIONED (LAVATORY) · airframe 20,686 hrs · 21,151 cycles

CREW REPORTED LAVATORY SMOKE DETECTOR MESSAGE WITH SMOKE VISABLE. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE LAVATORY WASTE MOTOR ASSEMBLY USING THE AIRCRAFT MANUALS. OPERATIONAL CHECKS WERE PERFORMED USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PROBE — FAILED (FUEL QTY IND) · airframe 19,607 hrs · 20,167 cycles

CREW REPORTED LEFT AND TOTAL FUEL QUANTITY INDICATION WENT TO AMBER DASHES IN CRUISE AND RETURNED ON APPROACH. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT FUEL QUANTITY INDICATING SYSTEM, REMOVED AND REPLACED NUMBER SIX (6) LEFT PROBE AND PERFORMED CHECKS USING MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: COWLING — DAMAGED (LEFT) · airframe 19,330 hrs · 19,902 cycles

CREW REPORTED HEARING LOUD BANG AND AIRCRAFT YAWED TO LEFT DURING FLIGHT. CREW RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND DAMAGE TO LEFT ENGINE LOWER TRANSCOWL AND DENTS IN FUSELAGE. PAINTED LT LOWER TRANSITION COWL IAW SRM 51-25-01. THIS CLEARS DAIMETER INSTALLED SERVICABLE LOWER TRANSCOWL IAW AMM 71-11-01-400-802. REPLACING TRANSCOWL CLEARS THIS ITEM. REPLACEMENT HINGE PINS CAME ON TRANSCOWL ASSY. REINSTALLED LT ENGINE UPPER AND LOWER NOSE ACCESS COWLS IAW AMM 71-14-01-400-801 AND 71-14-01-400-802. PERFORMED OPS TEST OF LT T/R IAW AMM 71-00-00-710-806. OPS CHECK GOOD.

Part: SKIN — DENTED (FUSELAGE) · airframe 18,104 hrs · 18,704 cycles

DURING SCHEDULED MAINTENANCE THE FORWARD FUSELAGE SKIN AT FS 202.75 WAS FOUND DENTED. THE FUSELAGE AT FS 202.75 WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BEAM — CRACKED (FUSELAGE) · airframe 18,104 hrs · 18,704 cycles

DURING SCHEDULED MAINTENANCE THE TRAVERSE BEAM AT FS 280.0 WAS FOUND CRACKED. THE TRAVERSE BEAM WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 18,104 hrs · 18,704 cycles

DURING SCHEDULED MAINTENANCE DAMAGE WAS FOUND ON PRESSURE BULKHEAD AT FS 621.0. THE PRESSURE BULKHEAD WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 18,104 hrs · 18,704 cycles

DURING SCHEDULED MAINTENANCE THE FORWARD FUSELAGE SKIN AT FS 589.0 WAS FOUND DENTED. THE FUSELAGE AT FS 589.0 WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLAP — DENTED (LT WING) · airframe 18,104 hrs · 18,704 cycles

DURING SCHEDULED MAINTENANCE THE LEFT INBOARD FLAP WAS FOUND DENTED. THE LEFT INBOARD FLAP WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 18,104 hrs · 18,704 cycles

DURING SCHEDULED MAINTENANCE A CRACK WAS FOUND AT FASTENER HOLE AT FS 349. THE FASTENER HOLE WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 18,104 hrs · 18,704 cycles

DURING SCHEDULED MAINTENANCE THE FLOORBEAM AT FS 568.0 WAS FOUND CORRODED. THE FLOORBEAM WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 18,104 hrs · 18,704 cycles

DURING SCHEDULED MAINTENANCE THE FORWARD FUSELAGE SKIN AT FS 250.0 WAS FOUND DENTED. THE FUSELAGE AT FS 250.0 WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PRESSURE SWITCH — MALFUNCTIONED (HYDRAULIC SYS) · airframe 17,739 hrs · 18,380 cycles

CREW REPORTED RECEIVING AMBER 3A HYD CAS MESSAGE UPON LIFT-OFF BEFORE GEAR RETRACTION ON DEPARTURE FROM CLT. CREW CYCLED SWITCH, RECOVERED PRESSURE AND CAS MESSAGE WENT AWAY. AFTER CREW CYCLED GEAR UP, GOT RED NOSE GEAR DOOR CAS MESSAGE. CREW RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED HYDRAULIC SYSTEM 3 PRESSURE SWITCH AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: ADC — MALFUNCTIONED (NR 1) · airframe 16,979 hrs · 17,643 cycles

CREW REPORTED CAPTAIN’S PRIMARY FLIGHT DISPLAY (PFD) LOST ALL AIR DATA UPON GEAR RETRACTION DURING TAKEOFF FROM CLT. CREW RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED NR 1 AIR DATA COMPUTER (ADC) AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 16,958 hrs · 17,622 cycles

CREW REPORTED MODERATE TO SEVERE TURBULENCE ON APPROACH TO HPN. DURING CLIMB TO DIVERT TO PHL, CAPTAIN’S PRIMARY FLIGHT DISPLAYS BRIEFLY WENT BLANK. CREW LANDED IN PHL WITHOUT INCIDENT. MAINTENANCE PERFORMED OPERATIONAL TEST OF DISPLAY CONTROL PANEL (DCP )USING AIRCRAFT MAINTENANCE MANUAL. COULD NOT DUPLICATE DISCREPANCY. AIRCRAFT RELEASED FOR SERVICE.

Part: PUMP — LOW PRESSURE (HYDRAULIC SYS) · airframe 16,674 hrs · 17,323 cycles

ON TAKEOFF FROM HSV, CREW REPORTED LANDING GEAR DISAGREE AND NOSE DOOR OPEN MESSAGES WHEN THE LANDING GEAR HANDLE WAS SELECTED UP. CREW RETURNED TO HSV AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE AIRCRAFT, REMOVED AND REPLACED THE 3A HYDRAULIC PUMP AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING SYSTEM — MALFUNCTIONED (ANTI-ICE SYSTEM) · airframe 15,868 hrs · 16,535 cycles

CREW REPORTED PITOT BASE HEAT, LEFT AOA HEAT, LEFT STATIC HEAT AND LEFT PITOT HEAT CAS MESSAGES AT LOW ALTITUDE AFTER TAKEOFF FROM PHL. CREW ELECTED TO RETURN TO PHL AND LANDED WITHOUT INCIDENT. MAINTENANCE CYCLED SYSTEM CIRCUIT BREAKERS IN ACCORDANCE WITH BOMBARDIER SERVICE LETTER. MESSAGES CLEARED AND DID NOT RE-APPEAR. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WHEEL — WORN (LT MLG) · airframe 15,519 hrs · 16,196 cycles

CREW REPORTED A STRONG VIBRATION PRIOR TO AND AFTER ROTATION ON TAKEOFF FROM CLT. AIRCRAFT CONTINUED FLIGHT TO IND AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, REMOVED AND REPLACED THE LEFT OUTBOARD MAIN LANDING GEAR WHEEL / TIRE ASSEMBLY AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 14,756 hrs · 15,411 cycles

DURING SCHEDULED MAINTENANCE A CRACK WAS FOUND ON THE PRESSURE BULKHEAD STRUCTURE AT FS 559.00 STRINGER 23 LEFT AND 23 RIGHT. REPAIRS WERE DONE PER MAINTENANCE MANUALS AND AIRCRAFT RELEASED FOR SERVICE.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 14,313 hrs · 14,906 cycles

FLOOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE DURING TEST AT CAK. MAINTENANCE TROUBLESHOT, RECONNECTED THE FLOOR EMERGENCY LIGHT STRIP AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CARBON SEAL — DEFECTIVE (RT ENGINE) · airframe 12,911 hrs · 13,418 cycles

CREW REPORTED RT ENGINE HAD LOW OIL PRESSURE. AIRCRAFT DIVERTED TO ATL LANDING WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND REMOVED AND REPLACED IDG CARBON SEALS ON RT ENGINE. CHECKS AND LEAK CHECKS WERE ACCOMPLISHED PER THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PUMP — FAILED (RT ENGINE) · airframe 12,171 hrs · 12,631 cycles

CREW REPORTED IN CRUISE THE RT ENGINE OIL PRESSURE AND OIL TEMPERATURE HIGH. AIRCRAFT DIVERTED TO CAK AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND CARBON PIECES IN SCREEN LUBE AND SCAVENGE OIL PUMP. MAINTENANCE REMOVED AND REPLACED THE RT ENGINE OIL PUMP. OPERATIONAL CHECKS WERE DONE PER THE AIRCRAFT MAINTENANCE MANUAL AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING SYSTEM — FALSE INDICATION · airframe 10,727 hrs · 11,103 cycles

AFTER TAKEOFF CREW RECEIVED A STALL FAIL CAS MESSAGE. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED SYSTEM AND FOUND NO DEFECTS. ACFT WAS RELEASED FOR SERVICE. (S)

Part: IDG — FAILED (NR 2) · airframe 9,471 hrs · 9,777 cycles

CREW ABORTED THE TAKEOFF DUE TO A GEN 2 OFF CAS MESSAGE. CREW RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE PERFORMED A REJECTED TAKEOFF INSPECTION AND DEFERRED THE NR 2 IDG PER MEL 24-11-01-3. MAINTENANCE REMOVED AND REPLACED THE NR 2 IDG. MEL WAS CLEARED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: INLET — DAMAGED (LT ENGINE) · airframe 9,092 hrs · 9,371 cycles

CREW REPORTED MULTIPLE BIRD STRIKES TO THE FUSELAGE, WING AND BOTH ENGINES. MAINTENANCE INSPECTED FOUND DAMAGE TO THE LEFT ENGINE INLET, FORWARD EQUIPMENT BAY DOOR AND BULKHEAD, AND THE RIGHT WING LEADING EDGE. MAINTENANCE REMOVED AND REPLACED THE DAMAGED LEFT ENGINE INLET. MAINTENANCE PERFORMED TEMPORARY REPAIRS. AIRCRAFT WAS FERRIED FOR PERMANENT REPAIRS TO BE ACCOMPLISHED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PUMP — FAILED (RT ENGINE) · airframe 8,369 hrs · 8,563 cycles

CREW REPORTED RECEIVING A LOW OIL PRESSURE WARNING MESSAGE FOR THE RIGHT HAND ENGINE. CREW DECLARED AN EMERGENCY AND SHUT DOWN THE ENGINE. CREW LANDED IN PIT WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE SCAVENGE OIL PUMP IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: UNKNOWN — UNKNOWN (SPOILERONS) · airframe 7,975 hrs · 8,142 cycles

CREW REPORTED AN AMBER SPOILERON CAS MESSAGE ON APPROACH. CREW FOLLOWED THE QRH AND NOTIFIED ATC REQUESTING A GO-AROUND. AFTER THE GO-AROUND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND RESET THE SYSTEM IN ACCORDANCE WITH THE SERVICE LETTER SL-00-001. OPERATIONAL CHECKS WERE PERFORMED, MESSAGE DID NOT RE-APPEAR. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: TRIM SWITCH — DIRTY (COCKPIT) · airframe 7,614 hrs · 7,746 cycles

CREW REPORTED THE STAB AND MACH TRIM FAILED ON TAKEOFF. CREW ELECTED TO RETURN TO CHO AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE F/O'S CONTROL WHEEL. MAINTENANCE CLEANED THE HORIZONTAL STAB TRIM SWITCHES ON F/O'S CONTROL WHEEL. MAINTENANCE PERFORMED OPERATIONAL TESTS OF THE HORIZONTAL STAB TRIM SYSTEM IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL 27-40-00-710-801. OPS TESTS GOOD. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: DAMPER — DAMAGED (LT ELEVATOR) · airframe 5,715 hrs · 5,735 cycles

CREW REPORTED LT ELEVATOR -FLUTTER DAMPER FAIL- STATUS MESSAGE. FLUTTER DAMPER WAS FOUND TO HAVE NO FLUID (SYNOPTIC) AND STATUS MESSAGE DISPLAYED. LT ELEVATOR FLUTTER DAMPER WAS REMOVED AND REPLACED. OPERATIONAL CHECKS WERE PERFORMED. NO FAULTS WERE FOUND. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CARBON SEAL — LEAKING (RT ENGINE) · airframe 5,342 hrs · 5,355 cycles

ON CLIMBOUT THE -R ENG OIL PRESS- WARNING MESSAGE ILLUMINATED AND THE OIL PRESSURE INDICATION WAS FLUCTUATING. THE CREW FOLLOWED THE QRH, DIVERTED TO IAD, AND LANDED WITHOUT INCIDENT. OIL QUANTITY WAS FOUND TO BE LOW. MAINTENANCE REPLACED THE ACCESSORY GEARBOX EDP CARBON SEAL. OIL PRESSURE, LEAK, AND CONSUMPTION CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BPSU — FAILED (RT TE FLAPS) · airframe 3,531 hrs · 3,526 cycles

DURING FINAL APPROACH THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED. THE CREW FOLLOWED THE QRH AND LANDED SAFELY. MAINTENANCE REMOVED & REPLACED THE RT FLAP BRAKE AND POSITION SENSOR UNIT IAW CRJ200 AMM 27-51-10-400-801. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FCU — MALFUNCTIONED (TE FLAPS) · airframe 3,527 hrs · 3,522 cycles

DURING CRUISE FLIGHT WITH FLAPS AT 0 DEGREE THE FLAPS FAIL MESSAGE ILLUMINATED. THE CREW FOLLOWED THE QRH AND PERFORMED A NO FLAP LANDING AT DESTINATION. MAINTENANCE INTERROGATED THE MDC, FECU, AND SDU. NO FAULTS WERE DISPLAYED. THE FLAP SYSTEM WAS RESET AND OPERATIONALLY CHECKED GOOD IAW CRJ200 SL 27-084. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 3,515 hrs · 3,513 cycles

ON DOWNWIND THE FLAPS FAIL MESSAGE ILLUMINATED WITH FLAPS AT 8 DEGREES. THE CREW FOLLOWED THE QRH AND LANDED. MAINTENANCE RESET THE FECU IAW CRJ200 SL:00-001. FLAP SYSTEM OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 3,450 hrs · 3,452 cycles

THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED ON APPROACH. THE CREW FOLLOWED THE QRH AND LANDED WITHOUT INCIDENT. MAINTENANCE CYCLED AIRCRAFT POWER. THE FLAP SYSTEM OPERATIONALLY CHECKED GOOD IAW CRJ200 AMM 27-54-00-710-801. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: DOOR — OPEN (CABIN) · airframe 3,266 hrs · 3,270 cycles

DURING CLIMB PASSING 10,500 FT THE FLIGHT ATTENDANT NOTICED AN INCREASE IN NOISE LEVEL AROUND THE SERVICE DOOR. THE F/A REPORTED THAT THE GREEN INDEX MARKS ON THE INDICATOR WINDOW WERE NOT ALIGNED. COCKPIT INDICATIONS WERE NORMAL. THE FLIGHT RETURNED TO PHL WHERE MAINTENANCE OPERATIONALLY CHECKED THE SERVICE DOOR IAW CRJ200 AMM 52-41-00-710-801. OPS CHECKS WERE GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: ODOR — DETECTED (CABIN) · airframe 260 hrs · 241 cycles

THE CREW REPORTED A CARGO OVERHEAT MESSAGE AND A STRONG ELECTRICAL ODOR IN THE CABIN. OUSTATION MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND NO DISCREPENCIES. THE AIRCRAFT WAS THEN FERRIED TO DAY. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS IN ACCORDANCE WITH BOMBARDIER MAINTENANCE MANUAL 21-50-00-863-801 AND NO DEFECTS WERE NOTED. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: STRUT — FAILED (NLG) · airframe 142 hrs · 134 cycles

IN FLIGHT,GEAR WOULD NOT RETRACT. DURING PUSHBACK FROM GATE, NOSE GEAR WAS TURNED PAST ITS LIMIT. NOSE WHEEL STEERING WAS THEN REPORTED INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED ELECTRO HYDRAULIC STEERING VALVE IAW MFG MM. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. AFTER TAKE OFF THE NOSE GEAR WOULD NOT RETRACT AND FLIGHT RETURNED. THE AIRCRAFT WAS THEN FERRIED WITH THE GEAR PINNED. MAINTENANCE INSPECTED AND REPLACE THE NOSE GEAR SHOCK STRUT ASSEMBLY IAW MFG MM. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.