N970SW

Part: SKIN — SCRATCHED (ZONE 800) · airframe 49,523 hrs · 43,291 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: RA106889-601R-52-31-439 REV. -A 2025-11-20 MXCODEID118398-PR - COMPLY WITH PERMANENT REPAIR ON RA ID: 106889DUE TO SCRATCH ON THE OUTSIDE TOP OF THE CARGO DOOR, PER REO 601R-52-31-439 REV. -A 2025-11-20, PERMANENT REPAIR DUE WITHIN 1720FH FR, COMPLIED REO # 601R-52-31-448 - COMPLIED WITH PERMANENT REPAIR SCRATCH ON THE OUTSIDE TOP OF THE CARGO DOOR, IAW REO 601R-52-31-448 JOB COMPLETED

Part: SKIN — DENTED (ZONE 100) · airframe 49,523 hrs · 43,291 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: RA84579-REO 601R-53-11-3871. COMPLY WITH PERMANENT REPAIR ON RA ID: 845792+ CM DENT RIGHT SIDE NOSE, ADJACENT TO N/W DOOR. PERMANENT REPAIR IS DUE WITHIN 5650 FLIGHT HOURS FOR THE DENT DAMAGE TO FUSELAGE SKIN BETWEEN FS177.00-FS185.00 IN REF TO REO 601-53-11-3871 REV A. DUE BY TAT 51254.58 TAT, COMPLIED WITH REO# 601R-53-11-4056 FOR REPAIR ON R/H SIDE NOSE FUSELAGE SKIN BETWEEN FS 177.00-FS 185.00 JOB COMPLETED.

Part: HYDRAULIC LINE — DAMAGED (ZONE 100) · airframe 49,465 hrs · 43,231 cycles

HYDRAULIC 3 LO PRESS WHEN SELECTING GEAR DOWN. IMMEDIATELY FOLLOWED BY A GEAR DISAGREE. WE CHECKED THE HYDRAULICS AND NOTICED SYSTEM 3 AT 0%. WE RAN THE QRH FOR THE GEAR DISAGREE. WE HAD TO PULL THE EMERGENCY GEAR EXTENSION HANDLE. GEAR CAME DOWN AND LOCKED. LOST NOSE WHEEL STEERING ON ROLLOUT AS PER THE QRH. (FLIGHT 5224) FOUND DAMAGED FLEXIBLE PRESSURE LINE ON 3A ACMP, CUT O-RING ON THE NR 3 PRESSURE MANIFOLD PRESSURE OUT FITTING, AND REPLACED BOTH 3A AND 3B ACMP'S. SEE EAML'S 1750113, 1750116, 1750115, AND 1750109 FOR REPLACEMENT OF DAMAGED PARTS AND SEE EAML1750270 FOR OPS CHECK OF MAIN LANDING GEAR EXTENSION AND RETRACTION INCLUDING EMERGENCY EXTENSION.

Part: WARNING MESSAGE — ACTIVATED · airframe 49,208 hrs · 42,928 cycles

FLAPS FAIL. ON CLIMB SEQUENCE (FLIGHT 5754 - FILED CLOSED)RESET AND OPERATED FLAPS 5 FUL CYCLES AND COMPETED AD 2009-16-12/10 COMPLIANCE FORM OK TO CONTINUE IN SERVICE FOR 10 FLIGHT CYCLES COMPLIED WITH IN ACCORDANCE WITH FIM FMRP CHAPTER 27 RESET PROCEDURE AND AD 2009-06-12 TRACKING CREATED FOR FULL AD COMPLIANCE

Part: WARNING MESSAGE — ILLUMINATED (TE FLAP) · airframe 48,994 hrs · 42,715 cycles

FLAP FAIL CAUTION MSG (RESET AND OP FLAPS 5 FULL CYCLES & COMPLETED AD 2009-06-12/10 COMPLIANCE FORM. OK TO CONTINUE IN SERVICE FOR 10 FLT CYCLES. COMPLIED WITH IAW FIM FMRP 27 RESET PROCEDURES & AD 2009-06-12 MCI CREATED FOR FULL AD COMPLIANCE BY MCC. CURRENT TAC 42714, FLAP FAIL CAUTION ONCE FLAPS WERE RETRACTED TO 0 AFTER TAKEOFF. RESET & OPS FLAPS 5 FULL CYCLES AND COMPLETED AD 2009-06-12/10, OK TO CONTINUE FOR 10 FLT CYCLES COMPLIED WITH IAW FIM FMRP 27 RESET PROCEDURE & AD 2009-06-12. COMPLIED WITH STEPS IN FIM 27-50-00 FLAP FAIL CAUTION MSG AND DETERMINED THAT THE FLAP PDU WAS AT FAULT. R & R FLAP PDU, OPS CHECK GOOD IAW AMM 27-52-01.

Part: WARNING MESSAGE — FALSE ACTIVATION (ZONE 700) · airframe 48,312 hrs · 41,935 cycles

MOMENTARY GEAR DISAGREE WARNING MESSAGE ON GO AROUND. GEAR HANDLE WAS UP. (FLIGHT 5232 - FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS

Part: PACKING — FAILED (NLG STRUT) · airframe 47,214 hrs · 40,761 cycles

ON TAKEOFF OUT OF CHICAGO O€™HARE WHEN COMMANDED GEAR UP. GOT GEAR DISAGREE WARNING MESSAGE. NOSE DOOR OPEN WARNING.PERFORMED QRH AND TRRIED TWICE TO BING GEAR UP AND TO NO EVALUATION. THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 28485614 WITH THE FOLLOWING CORRECTIVE ACTION: "SEE CP 28485743 FOR REPACK OF NLG SHOCK STRUT. NO FURTHER FAULTS FOUND AT THIS TIME. OPS CHECK GOOD AT THIS TIME."

Part: UNKNOWN — FUMES (CABIN) · airframe 46,690 hrs · 40,208 cycles

FUEL SMELL IN THE FLT DECK AND IN THE CABIN ON GROUND. IN AIR THE SMELL WAS STRONGER AFTER THE TEMPERATURE WAS INCREASED IN THE FLT DECK NOT IN THE CABIN . WENT AWAY AFTER THE TEMPERATURE WAS DECREASED (FLIGHT 5590 FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 27957581 WITH THE FOLLOWING CORRECTIVE ACTION: "DETERMINED THE FUEL SMELL WAS DUE TO A CHAFFED FUEL LINE INSIDE THE APU ENCLOSURE ALLOWING FUEL TO GET INTO THE AIRSTREAM AND INTO THE PACK'S AIR SUPPLY. REPLACED THE CHAFFED APU FUEL LINE BY INLET BELLOW CLAMPS SEE CP 27957793 FOR WORK PERFORMED. RAN PACKS WITH APU AS THE BLEED SOURCE UNTIL NO FUEL SMELL COULD BE DETECTED FROM THE CONDITIONED AIR."

Part: ANTI-ICE VALVE — FAULTED (WING) · airframe 46,577 hrs · 40,082 cycles

D:WING OVHT WARNING MESSAGE ON TAXI OUT. COMPLIED WITH EMER 9-2. MESSAGE CLEARED.C:DEFERRED WING ANTI-ICE MODULATING AND SOV RH SIDE PER MEL 30-12-1B. MX ACTION CW. PLACARD INSTALLED.CAT C DUE 2-12-24WING OVHT WARNING MESSAGE ON TAXI OUT. COMPLIED WITH EMER 9-2. MESSAGE CLEARED. (FILED CLOSED)REMOVED AND REPLACED THE RIGHT WING ANTI ICE VALVE WITH REFERENCE TO AMM 30-12-04. OPS CHECK AND LEAK CHECK GOOD AT THIS TIME. MEL CLEARED, PLACARDS REMOVED.

Part: UNKNOWN — ODOR (CABIN) · airframe 46,577 hrs · 40,082 cycles

WITH THE APU AND PACKS ON, A STRONG SMELL OF GAS BEGAN FILLING THE CABIN BEFORE BOARDING. FUEL VAPOR CAN VISIBLY BE SEEN IN THE CABIN. TURNED OFF AIRCRAFT. (FLIGHT 5278 FILED CLOSED)FEB 01, 2024 STATION: CID--VERIFIED WITH CREW NO ASSOCIATED EICAS MSG PRESENT AND THAT THEY WERE RUNNING ON APU POWER AND BOTH PACKS. AIRED OUT CABIN WITH FORCED CABIN AIR, NO SMELL OR FUMES REMAIN. INSP ENGINES, APU, AND CABIN FOR LEAKS IN REF TO CRJ 200 FIM 21-21-00 FOR ABNORMAL SMELLS. NONE FOUND. RAN ENGINES ONE AT A TIME ISOLATING PACK AND BLEED SOURCES, NO SMELL OR FUMES PRESENT. SUSPECT EXCEESSIVE FUEL IN APU BEFORE STARTING. MCI CREATED FOR MORE TROUBLESHOOTING. REF EAML 1289715 FOR APU DEFERRAL FEB 02, 2024 STATION: ORD -- REFERENCE CP 27764032 & 27765719 FOR TROUBLESHOOTING AND WORK ACCOMPLISHED. AIRCRAFT OK FOR SERVICE AT THIS TIMERTS APPROVED BY SMOD VIA EMAIL

Part: UNKNOWN — ODOR (CABIN) · airframe 46,566 hrs · 40,069 cycles

WITH THE APU AND PACKS ON, A STRONG SMELL OF GAS BEGAN FILLING THE CABIN BEFORE BOARDING. FUEL VAPOR CAN VISIBLY BE SEEN IN THE CABIN. TURNED OFF AIRCRAFT. (FLIGHT 5278 FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS.

Part: UNKNOWN — WARNING MESSAGE (UNKNOWN) · airframe 46,492 hrs · 39,981 cycles

D:AFTER ROTATION ON TAKEOFF RECEIVED WING OVRHT WARNING MESSAGE. RAN QRH AND MESSAGE CLEARED. MESSAGE NEVER RETURNED USINGWING ANTI ICE STDBY.C:MEL 30-12-3BCAT C DUE 23/JAN/24AFTER ROTATION ON TAKEOFF RECEIVED WING OVRHT WARNING MESSAGE. RAN QRH AND MESSAGE CLEARED. MESSAGE NEVER RETURNED USINGWING ANTI ICE STDBY. (FLIGHT 5348 FILED CLOSED)JAN 13, 2024 STATION: ORD--DEFERRED WING ANTI-ICE NORMAL MODE IAW MEL 30-12-3B. MAINTENANCE ACTIONS C/W. PLACARDS PLACED

Part: UNKNOWN — WARNING MESSAGE (UNKNOWN) · airframe 46,348 hrs · 39,832 cycles

WING OVHT WARNING MESSAGE RECEIVED AFTER TAKEOFF AROUND 2,000 FEET WITH WING AND COWL ANTI ICE SELECTED ON. COMPLETED QRH AND PLACED WING ANTI ICE IN STBY MODE. MESSAGE DID NOT RETURN FOR THE REMAINDER OF FLIGHT WITH STANDBY MODE USED. (FLIGHT 5449 FILED CLOSED) TROUBLESHOT IN REFERENCE TO FIM 30-10-00 PERFORMED OPERATION OF WING ANTI-ICE SYSTEM COULD NOT DUPLICATED DISCREPANCY, NO DISCREPANCIES NOTED OPS CHECK GOOD AT THIS TIME

Part: UNKNOWN — ASYMETRIC (UNKNOWN) · airframe 46,169 hrs · 39,625 cycles

IN CRUISE, AT FL330, AIRSPEED APPROX 270 KIAS, LEFT FLAP INTERMITTENTLY DEPLOYED TO 2. RIGHT FLAP STAYED AT 0. WE COULD FEEL PITCH AND ROLL IN CONTROLS WHEN IT WOULD MOVE TO 2. WOULD CONTINUE INTERMITTENTLY THROUGH DESCENT. WHEN FLAPS SELECTED FOR LANDING, BOTH MOVED SYMMETRICALLY AS COMMANDED. (FLIGHT 4686 FILED CLOSED)TROUBLESHOT LEFT FLAP INTERMITTENTLY DEPLOYING TO POSITION 2 REF CRJ200 FIM 27-50-00. FLAP POSITION SIGNAL WAS DRIFTING CAUSING THE AUTO-PILOT TO OSCILLATE PITCH. FDR DOWNLOADED ON 10/20/23 AND THEN UPLOADED THE SAME DAY FOR ANALYZATION. FDR SHOWED THAT THE FLAP POSITION TRANSMITTER WAS MOVING FROM 0 TO 2.REMOVED AND REPLACED LEFT FLAP POSITION TRANSMITTER REF CRJ200 AMM 27-55-01. PERFORMED OPS CHECK OF LEFT FLAP POSITION TRANSMITTER REF CRJ200 AMM 27-55-01. OPS CHECK GOOD. RIGGING PIN - A4P/N: G601R100001-1

Part: UNKNOWN — WARNING MESSAGE · airframe 45,547 hrs · 38,941 cycles

UPON TAKEOFF, GEAR DISAGREE AND NOSEDOOR UNSAFE WARNING MESSAGES OCCURRED. NOSE GEAR DID NOT COME UP. FOLLOWED QRH PROCEDURES AND SUCCESSFULLY LOWERED ALL THREE GEAR. NO OVERWEIGHT LANDING. NO OVERSPEED OR SOPM LIMITATIONS WERE EXCEEDED. (FLT 5256 FILED OPEN) PLEASE REFERENCE AML 1141483

Part: LANDING GEAR — WARNING MESSAGE · airframe 45,548 hrs · 38,942 cycles

UPON TAKEOFF, GEAR DISAGREE AND NOSEDOOR UNSAFE WARNING MESSAGES OCCURRED. NOSE GEAR DID NOT COME UP. FOLLOWED QRH PROCEDURES AND SUCCESSFULLY LOWERED ALL THREE GEAR. NO OVERWEIGHT LANDING. NO OVERSPEED OR SOPM LIMITATIONS WERE EXCEEDED. (FLT 5256 FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 26642521 WITH THE FOLLOWING CORRECTIVE ACTION: "REFERENCE CP 26642829 FOR GEAR DISAGREE TROUBLESHOOTING HELP SHEET AND INITIAL TROUBLESHOOTING OF GEAR DISAGREE AND NOSEDOOR UNSAFE.REFERENCE ML 26642522 FOR REPLACEMENT OF THE NLG OLEO/CENTERING BRACKET AND OPS CHECKS.REFERENCE CP 26642529 FOR ODI RETURN TO SERVICE APPROVAL."

Part: NONE — BROKEN · airframe 45,195 hrs · 38,598 cycles

REMOVE AND REINSTALL CARGO DOOR TO FOM (C-CHECK RO 2/14/2023) REMOVED AND REINSTALLED CARGO COMPARTMENT DOOR. REF. CRJ 200 AMM 52-31-00-400-801. OPERATIONAL TEST GOOD AT THIS TIME.

Part: NONE — CRACKED · airframe 45,195 hrs · 38,598 cycles

SUPPORT ANGLE FOR RH FLOOR SILL AT FS319 IS CRACKED. (C-CHECK RO 2/14/2023) REPLACED SUPPORT ANGLE AT RH FLOOR SILL FS.319 WITH NEW SUPPORT ANGLE PN 601R31148-73 REF. CRJ 200 SRM 51-42-06 AND DWG #601R31148 REV. AC. CW SKYWEST TASK CARD 51-900-1003-SKY.

Part: NONE — DAMAGED · airframe 45,195 hrs · 38,598 cycles

EVALUATE KNICK ON LEFT HASTA SUPPORT DOUBLER. (MARKED) (C-CHECK RO 2/14/2023) BLENDED OUT DAMAGE AND RESTORED FINISH REF REO 601R-55-31-421 REV -- DATED 2023-01-14 C/W TASK CARD 51-900-1003-SKY.

Part: HINGE — CORRODED · airframe 45,195 hrs · 38,598 cycles

UPON REMOVAL ON JOB 27881105 OP 107 CAMP 26030843, FOUND L/H ELEVATOR L/E HINGE FITTING ASSY P/N 600-24043-1 @ ES16.52 TO HAVE PITTING CORROSION IN BEARING BORES OF BOTH HINGE HALVES. REPLACE HINGE FITTING ASSY. (C-CHECK RO 2/14/2023) REMOVED AND REPLACED L/H ELEVATOR #1 HINGE FITTING ASSY P/N 600-24043-1 LOCATED ON ELEVATOR L/E @ ES16.52 REF. BOMBARDIER DWG 601R24025 REV. G, AND CRJ 200 SRM 51-42-06 AND SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: NONE — BLEW OUT · airframe 45,195 hrs · 38,598 cycles

R/H WING - TIP FAIRING - LOWER SIDE - BOTTOM FASTENER HOLE FOR WINGTIP PANEL 671BB BLOWN OUT AND NUTPLATE IS MISSING (C-CHECK RO 2/14/2023) PERFORMED CUT OUT REPAIR ON R/H WING - TIP FAIRING - LOWER SIDE FOR WINGTOP PANEL 671BB. REF REO 601R-57-31-1412 REV -- DATED 2023-01-30. COMPLIED WITH SKYWEST TASKCARD 51-900-1003-SKY. SEE CONTINUATION CARD FOR DETAILS.

Part: NONE — ELONGATED · airframe 45,195 hrs · 38,598 cycles

PAX DOOR HINGE - DOOR SIDE - HOLE FOR HINGE PIN RETAINING SPRING ELONGATED (C-CHECK RO 2/14/2023) REMOVED AND INSTALLED NEW PAX DOOR HINGE - DOOR SIDE. REF CRJ-200 SRM 51-42-06 AND SRM 51-42-21. LEAK CHECK GOOD. COMPLIED WITH SKYWEST TASKCARD 51-900-1003-SKY. SEE CONTINUATION CARD FOR DETAILS.

Part: NONE — CORRODED · airframe 45,195 hrs · 38,598 cycles

PAX DOOR INTERCOSTAL DD5 AFT CORRODED (C-CHECK RO 2/14/2023) REMOVED AND INSTALLED NEW PAX DOOR INTERCOSTAL DD5 AFT. REF CRJ-200 SRM 51-42-06 AND DWG 601R31702 REV N. LEAK CHECK GOOD. COMPLIED WITH SKYWEST TASKCARD 51-900-1003-SKY. SEE CONTINUATION CARD FOR DETAILS.

Part: NONE — DENTED · airframe 45,195 hrs · 38,598 cycles

EVALUATE DENT ON RH PRESSURE FLOOR SILL PANEL BETWEEN FS 499.00 - 513.00 (C-CHECK RO 2/14/2023) EVALUATED AND REPAIRED DENT ON RH PRESSURE FLOOR SILL PANEL BETWEEN FS 499.00 - 513.00. INSTALLED REPAIR DOUBLE ON RH PRESSURE FLOOR SILL PANEL. REF MHIRJ REO 601R-53-41-3115 REV -- DATE 2023-01-16. LEAK CHECK GOOD. COMPLIED WITH SKYWEST TASKCARD 51-900-1003-SKY. SEE CONTINUATION CARD FOR DETAILS.

Part: NONE — CORRODED · airframe 45,195 hrs · 38,598 cycles

RH SILL CORRODED APPROX FS319.70 / WL73.50. MARKED WITH GREASE PENCIL (C-CHECK RO 2/14/2023) REMOVED AND REPLACED RH FLOOR SILL AND DOUBLER AT APPROX. FS310 - FS319.70 CRJ200 SRM 51-42-06, REV 39, DATED MAR 10/21. AND DWG# 601R31148, REV AC SEE CONTINUATION CARD FOR MAINTENANCE PREFORMED. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY

Part: NONE — CORRODED · airframe 45,195 hrs · 38,598 cycles

CORROSION ON FLOOR SUPPORT STRAP AT FS 559.00 BETWEEN RBL 27 - RBL 45 (C-CHECK RO 2/14/2023) REPAIRED FLOOR SUPPORT STRAP AT FS. 559.00 BETWEEN RBL 27 - RBL 45 REF. CRJ200 SRM 51-42-06 & CRJ20 SRM 51-40-11. AND DWG 601R31145 REV M. COMPLIED WITH SKYWEST TASKCARD 51-900-1003-SKY. SEE CONTINUATION CARD FOR DETAILS.

Part: NONE — CORRODED · airframe 45,195 hrs · 38,598 cycles

AREAS OF CORROSION ON FLOOR SEAT TRACK AT RBL9 BETWEEN FS 473.00 - 589.00 (C-CHECK RO 2/14/2023) REMOVED AND REPLACED FLOOR SEAT TRACK AT RBL9 BETWEEN FS 473.00 - 589.00 WITH NEW, PER CRJ200 AMM 53-01-11-400-802. SEE CONTINUE CARD FOR DETAILS.

Part: NONE — DENTED · airframe 45,195 hrs · 38,598 cycles

EXTERNAL FUSELAGE AT FS283 BETWEEN STR 24R & 25R HAS TWO EACH DENTS (MARKED WITH TAPE) (C-CHECK RO 2/14/2023) REPAIRED DENT BY COMPLYING WITH REO 601R-51-00-309 REV-A DATED 2017-08-23 AND REO 601R-53-21-3595 REV -- DATE 2023-01-23..SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED. COMPLIED WITH 51-900-1003-SKY

Part: NONE — CRACKED · airframe 45,195 hrs · 38,598 cycles

FS 484 AT LBL 36.0 AND LBL 27( CLIPS ARE CRACKED.UNDER FLOOR). (C-CHECK RO 2/14/2023) REMOVED 2EA. CLIPS, LOCATED, DRILLED AND INSTALLED 2EA.CLIPS P/N 601R31171-17 AND FABRICATED PART -1 LH ANGLE OUT OF S6144-14 ANGLE. REF REO 601R-53-41-059 REV-C DATED 2020-03-11 STEPS 5 TO 14 AND STEPS 1 TO 4 PREVIOUSLY COMPLIED WITH.COMPLIED WITH 51-900-1003-SKY.

Part: NONE — CORRODED · airframe 45,195 hrs · 38,598 cycles

PAX DOOR INTERCOSTAL DD4 MID CORRODED (C-CHECK RO 2/14/2023) REMOVED AND INSTALLED NEW DD4 INTERCOSTAL P/N 601R318081-1 ON PASSENGER DOOR. REF. DWG 601R31702, REV: N, AND CRJ 200 SRM 51-42-06. COMPLIED WITH 51-900-1003-SKY. FOUND TO BE OUT OF LIMITS REF CRJ 200 SRM 52-00-00. LR\EAK CHECKS GOOD

Part: NONE — GOUGED · airframe 45,195 hrs · 38,598 cycles

PAX DOOR CUT-OUT FRAME FS349.00, REPAIR STRIIP BENT AND GOUGED ST APPROXIMATE STRINGER 12. (C-CHECK RO 2/14/2023) INSTALLED NEW REPAIR STRAP AT FRAME FS349.00 REF GREO 601R-53-22-033 REV C 2007/07/18 REPAIR TYPE 1. AND CRJ 200 SRM 51-42-06. LEAK CHECK AND OPERATIONAL CHECK GOOD. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED CW 51-900-1003-SKY

Part: NONE — CORRODED · airframe 45,195 hrs · 38,598 cycles

*PAX DOOR INTERCOSTAL DD3 MID CORRODED (C-CHECK RO 2/14/2023) AREMOVED AND INSTALLED NEW PAX DOOR INTERCOSTAL DD3 MID. REMOVED AND REINSTALLED FS329.50 FORMER. REF CRJ-200 SRM 51-42-06 AND DWG 601R31702, REV N.LEAK CHECK GOOD. COMPLIED WITH SKYWEST TASKCARD 51-900-1003-SKY. SEE CONTINUATION CARD FOR DETAILS.

Part: WINDSHIELD — DAMAGED · airframe 45,195 hrs · 38,598 cycles

FO WINDSHIELD FAILS SENSOR RESISTANCE CHECK. (C-CHECK RO 2/14/2023) REMOVED AND INSTALLED COPILOT WINDSHIELD REF. CRJ200 AMM 56-11-01-400-801. COMPLIED WITH 56-220-1000-SKY .OPS CHECK LEAK CHECKS GOOD

Part: NONE — DAMAGED · airframe 45,195 hrs · 38,598 cycles

AFTER REMOVAL OF THE ADF ANTENNA FOUND TOOLING DAMAGE ON THE AIRCRAFT MOUNTING SURFACE (C-CHECK RO 2/14/2023) PERFORMED CUT OUT REPAIR OF ADF ANTENNA MOUNTING SURFACE. REF MHIRJ REO 601R-53-31-1257 REV -- DATED 2023-01-20. COMPLIED WITH SKYWEST TASKCARD 51-900-1003-SKY. SEE CONTINUATION CARD FOR DETAILS.

Part: NONE — CHAFED (NONE) · airframe 45,195 hrs · 38,598 cycles

*RH AILERON LOWER OUTBD RUB SEAL CHAFFED (C-CHECK RO 2/14/2023) REPLACED RH AILERON LOWER OUTBD RUB SEAL (PANEL) WITH NEW DUE TO BLEND OUT OF LIMITS SEE CONTINUATION CARD FOR WORK DETAILS REF. CRJ 200 SRM 51-42-21 AND DWG #CC670-13000 REV. D. CW 51-900-1003-SKY AND SKYWEST M-337 FORM.

Part: NONE — DAMAGED · airframe 45,195 hrs · 38,598 cycles

THERE ARE SIGNS OF DAMAGE ON THE RH NOSE OF THE AIRCRAFT BETWEEN THE ADG DOOR AND THE NLG DOOR. PLEASE PLOT, MAP AND EVALUATE DAMAGE. IF DAMAGE IS FOUND IN LIMITS, ELIMINATE ALL EVIDENCE OF DAMAGE USING AIRCRAFT STANDARD PRACTICES AND PROCEDURES. (C-CHECK RO 2/14/2023) REMOVED AND INSTALLED ON NEW SKIN PANEL P/N: 601R33010-55 BETWEEN ADG DOOR AND NLG DOOR REF. CRJ-200 SRM 51-42-06 AND BOMBARDIER DWG# 601R33010 REV-J AND REO 601R-53-11-3821 REV-- DATED 2023-01-24 . COMPLIED WITH 51-900-1003-SKY. SKIN FOUND TO BE OUT OF LIMITS REF CRJ 200 SRM 53-00-31

Part: NONE — CHAFED · airframe 45,195 hrs · 38,598 cycles

INSTALL LH INBD FLAP TO FACILITATE OTHER MAINTENANCE PER AMM TO FOM. (C-CHECK RO 2/14/2023) INSTALLED LH I/B FLAP REF. CRJ 200 AMM 27-54-01-400-801

Part: WIRE HARNESS — FAILED (NLG) · airframe 45,064 hrs · 38,478 cycles

GEAR DISAGREE AFTER TAKEOFF. NOSE INDICATED DWN . MAIN GEAR HAD WHITE INDICATORS. RAN QRH, MANUAL DEPLOY HANDLE PULLED. SUCCESSFUL GEAR EXTENSION. RETURN TO FIELD (FLIGHT 4737) REF CP 25745965 FOR TROUBLESHOOTING GEAR DISAGREE. REF CP 25750887 FOR DAMAGED NLG HARNESS REPLACEMENT. REF CP 25745944 FOR REPLACEMENT OF THE NLG SENSOR BRACKET. REF CP 25750899 FOR OPS CHECK OF PROXIMITY SYSTEM. REF CP 25750895 FOR OPS CHECK OF NLG EXTENTION AND RETRACTION.

Part: WINDSHIELD — FAILED (COCKPIT LT) · airframe 41,665 hrs · 35,434 cycles

LEFT WINDSHIELD SHATTERED AT FL 320. LT WINDSHIELD HEAT CAUTION MESSAGE AT SAME TIME. FILED CLOSED RO 10/3/2020. REMOVED AND REPLACED LT WINDSHIELD WITH SERVICEABLE UNIT, REF AMM. OPERATIONAL CHECK OF WINDSHIELD HEAT WAS FOUND TO BE GOOD, WITH NO DISCREPANCIES AT THIS TIME.

Part: SKIN — DENTED (LT WING SPOILER) · airframe 40,237 hrs · 34,141 cycles

L/H WING FLIGHT SPOILER SMALL DENT IN THE CENTER OF THE SPOILER APPROXIMATELY 6 INCHES AFT OF THE SPOILER LEADING EDGE. IT IS AN APPROXIMATELY 1-1/8 INCH DIAMETER CIRCULAR DENT. (C-CHECK) RO: 11/9/2019 DENT WAS FOUND OUT OF LIMITS. REMOVED AND REPLACED THE L/H FLIGHT SPOILER IAW AMM. RIGGING CHECK GOOD. OPERATIONAL TEST GOOD.

Part: FRAME — CORRODED (BS 333) · airframe 40,237 hrs · 34,141 cycles

FS 333 BETWEEN STR 25R - 25L CORRODED ON AFT SIDE. (C-CHECK) RO: 11/9/2019 --REMOVED CORROSION FROM THE FS333 FRAME BETWEEN STR25R - STR25L "OUT OF LIMITS"--REMOVED AND REPLACED FS333 FRAME SECTION STR25R - STR25L RESTORED ACCESS AND FINISH. LEAK CHECKS GOOD.

Part: SKIN — DENTED (LT WING SPOILER) · airframe 40,237 hrs · 34,141 cycles

LEFT WING OUTBD GROUND SPOILER HAS DENTS ON TOP SKIN MARKED. (C-CHECK) RO: 11/9/2019 LH OTBD GROUND SPOILER DAMAGE FOUND OUT OF LIMITS. REMOVED AND INSTALLED NEW GROUND SPOILER IAW AMM. CLEARANCE CHECK GOOD. OPERATIONAL TEST GOOD.

Part: THRUST REVERSER — DENTED · airframe 40,237 hrs · 34,141 cycles

UPPER TRANSLATING COWL 434AT HAS MULTIPLE EXTERIOR DENTS. (C-CHECK) RO: 11/9/2019 UPPER TRANSLATING COWL 434AT FOUND TO BE OUT OF REPAIABLE LIMITS. ORDERED AND RECEIVED SERVICABLE COWL

Part: FRAME — CORRODED (BS 574) · airframe 40,237 hrs · 34,141 cycles

FS 574 LBL38 BETWEEN STR 20L-19LCORROSION ON FRAME. (C-CHECK) RO: 11/9/2019 --REMOVED CORROSION ON FS574 FRAME BETWEEN STR20L - 19L "OUT OF LIMITS" --REPAIRED FRAME SECTOR FS574 LBL36 BETWEEN STR20L - STR19L BY FABRICATING AND INSTALLING NEW FRAME AND SPLICE. RESTORED AIR DUCT AND TIE DOWNS. LEAK CHECKS GOOD.

Part: SENSOR — OUT OF LIMITS (GROUND SPOILERS) · airframe 40,237 hrs · 34,141 cycles

LH OTBD GRD SPOILER ALWAYS INDICATES DEPLOYED WITH ASSOCIATED GRD SPOILER FAULT CAS MSG, RESET AND ENGAGED GLD, MESSAGE AND FAULT PERSISTS. (C-CHECK) RO: 11/9/2019 TROUBLESHOT LH OTBD GRD SPOILER ALWAYS INDICATES DEPLOYED WITH ASSOCIATED GRD SPOILER FAULT CAS MSG. PERFORMED PSEU INPUT TEST FOR L/H OUTBOARD GROUND SPOILER. INPUT S05 (SENSOR PS22GA) SHOWED FAR WITH L/H OUTBOARD GROUND SPOILER CLOSED. SHOULD SHOW NEAR. OPENED L/H OUTBOARD GROUND SPOILER AND INPUT S05 SHOWED FAR. CHECKED THE MDC DIAGNOSTIC WORD SECU LABEL 351 BIT 18. BIT 18 SET 1 WHICH IS AN INVALID POSITION SIGNAL. PERFORMED CLEARANCE CHECK OF THE L/H OUTBOARD PROXIMITY SENSOR (PS22GA). SENSOR IS OUT OF LIMITS. READJUSTED SENSOR TO .045 IAW AMM. PERFORMED PSEU IMPUT TEST FOR L/H OUTBOARD GROUND SPOILER. IMPUT S05 (SENSOR PS22GA ) SHOWS NEAR WITH L/H OUTBOARD GROUND SPOILER CLOSED AND OPENED L/H OUTBOARD GROUND SPOILER AND INPUT S05 SHOWS FAR. INPUT TEST GOOD AT THIS TIME. CHECKED THE MDC DIAGNOSTIC WORD SECU LABEL 351 BIT 18 IS SET TO 0 WHICH IS A VALID POSITION SIGNAL. PERFORMED OPS TEST OF THE GROUND SPOILER CONTROL SYSTEM. OPS TEST GOOD AT THIS TIME.

Part: DOWNLOCK — SHORTED (NLG) · airframe 37,493 hrs · 31,654 cycles

AFTER TAKEOFF IN PUB HAD A GEAR DISAGREE WARNING MESSAGE COME ON. (FLT 5065) CLOSED PSEU NOTED S35 NOSE GEAR DOWN LOCK NR 2 SHORTED. REPLACED AND ADJUSTED NOSE GEAR DOWN LOCK IAW AMM. GEAR SWING OPS CHECK GOOD.

Part: TRUNNION — DAMAGED (MLG) · airframe 35,869 hrs · 30,244 cycles

FOUND TWO HOLES ON THE RT SIDE & ON HOLE ON THE LT SIDE TO BE OUT LIMITS. REPAIRED THE HOLES ON THE MLG TRUNNION FITTING IAW REO.

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 35,869 hrs · 30,244 cycles

INTERCOSTAL BETWEEN BS 621 AND 625, STRINGER 14L IS CRACKED. INSTALLED A NEW INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 35,869 hrs · 30,244 cycles

INTERCOSTAL BETWEEN BS 621 AND 625, STRINGER 13L IS CRACKED. REPLACED THE INTERCOSTAL IAW SRM.

Part: POST — DAMAGED (BS 409) · airframe 35,869 hrs · 30,244 cycles

CRACK INDICATION NOTED AT BS 409+128 VERTICAL POST AT WL 69, RBL18 INBD. CHANNEL 60% FULL SCREEN HEIGHT APPROX. .375" IN LENGTH. REMOVED AND REPLACED THE VERTICAL POST IAW REO AND SRM.

Part: FLOOR SUPPORT — CORRODED (BS 439) · airframe 35,869 hrs · 30,244 cycles

RT PRESSURE FLOOR SUPPORT ANGLE IS CORRODED AT BS 439. REPAIRED IAW REO.

Part: DOOR SILL — CRACKED (CARGO BAY) · airframe 35,869 hrs · 30,244 cycles

CARGO DOOR SILL IS CORRODED AND CRACKED IN TWO LOCATIONS AT BS 589 AND 605. REPAIRED CARGO DOOR SILL IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 484) · airframe 35,869 hrs · 30,244 cycles

RT PRESSURE FLOOR SUPPORT ANGLE IS CORRODED AT BS 484. REPAIRED IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 484) · airframe 35,869 hrs · 30,244 cycles

LEFT PRESSURE FLOOR SUPPORT ANGLE IS CORRODED AT BS 484. REPAIRED IAW REO.

Part: FRAME — CORRODED (BS 589) · airframe 35,869 hrs · 30,244 cycles

FRAME CORRODED AT BS 589 BETWEEN STRINGERS 26L AND 27L.. REMOVED AND REPLACED THE FRAME IAW SRM.

Part: FRAME — CORRODED (BS 605) · airframe 35,869 hrs · 30,244 cycles

FRAME CORRODED AT BS 605 BETWEEN STRINGERS 26L AND 26R. REPLACED THE FRAME IAW SRM.

Part: STIFFENER — CHAFED (BS 621) · airframe 35,869 hrs · 30,244 cycles

AFT EQUIPMENT COMPARTMENT BS 621 VERTICAL STIFFENER AT TOP OF BL 0 CHAFED. REPAIR COMPLETED IAW REO.

Part: SKIN — DENTED (BS 574-589) · airframe 35,869 hrs · 30,244 cycles

DENT IN FUSELAGE SKIN BETWEEN BS 574 AND 589, STRINGERS 14R AND 15R. REPAIRED THE SKIN IAW SRM.

Part: PRIORITY VALVE — MALFUNCTIONED (LANDING GEAR) · airframe 33,118 hrs · 27,688 cycles

GEAR DISAGREE WARNING AFTER TAKE OFF. NOSE GEAR WOULD GO UP. RAN QRH BROUGHT MAIN GEAR DOWN. R & R LANDING GEAR PRIORITY VALVE IAW AMM. NO LEAKS NOTED. COMPLIED WITH SEVERAL GEAR OPS CHECKS IAW AMM. OPS CHECKED GOOD.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 28,910 hrs · 23,914 cycles

SET OF EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE CHANGED THE NR 3 BATTERY PACK.

Part: SELECTOR VALVE — FAILED (NLG) · airframe 27,364 hrs · 22,673 cycles

RECEIVED GEAR DISAGREE WARNING ACCOMPANIED WITH NLG UNSAFE INDICATION. COMPLIED WITH QRH PROCEDURE & RETURNED TO FIELD. FLT 5256 REPLACED NLG DOOR SELECTOR VLV & REPLACED LG CONTROL HANDLE IAW AMM. PERFORMED SEVERAL GEAR SWINGS, PN 601R50967-11, SN ON 1602, SN OFF 1352, PN 750006000, SN ON 0293T & SN OFF 1257.

Part: SELECTOR VALVE — FAILED (NLG) · airframe 27,323 hrs · 22,640 cycles

GEAR DISAGREE MESSAGE INDICATED NOSE GEAR UNSAFE. COMPLIED WITH QRH, RETURNED TO FIELD. FLT 5576 REPLACED NLG SELECTOR VLV & NLG PRIORITY VLV IAW AMM. PERFORMED MULTI GEAR SWINGS INCLUDING EMERGENCY FREE FALL. NO DEFECTS NOTED, PN 750006000, SN ON 0547T, SN OFF 0113T, PN 4622, SN ON1953A & SN OFF 2234A.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,941 hrs · 22,328 cycles

RT FS 280 INBD OTBD CLIPS CRACKED. C-CHECK REMOVED TWO EACH CRACKED CLIPS AT FS 280 RBL 9 INBD & OTBD & INSTALLED TWO EACH NEW CLIPS IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 26,941 hrs · 22,328 cycles

FS 280 LT SIDE LOWER WEB ANGLE CRACKED. C-CHECK PERFORMED REPAIR TO FS 280 LT SIDE LOWER WEB ANGLE IAW REO.

Part: DOOR — CHAFED (RT MLG) · airframe 26,941 hrs · 22,328 cycles

FWD EDGE OF THE RT MLG DOOR HAS CHAFING. C-CHECK REPAIRED CHAFING ON RT MLG DOOR IAW REO.

Part: DOOR — CHAFED (RT MLG) · airframe 26,941 hrs · 22,328 cycles

AFT EDGE OF RT MLG DOOR HAS CHAFING. C-CHECK REPAIRED AFT EDGE OF RT MLG DOOR IAW REO.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 26,941 hrs · 22,328 cycles

FLIGHT COMPARTMENT FLOOR BOARD 221ALF AFT CENTER SUPPORT ATTACH ANGLE CRACKED. C-CHECK REMOVED DAMAGED FLOOR SUPPORT ANGLE 600-34017-351 & INSTALLED NEW IAW REO.

Part: DOOR — CHAFED (LT MLG) · airframe 26,941 hrs · 22,328 cycles

FWD EDGE OF LT MLG DOOR HAS CHAFING. C-CHECK CORRECTED CHAFFING ON LT MLG DOOR IAW REO.

Part: DOOR — CHAFED (LT MLG) · airframe 26,941 hrs · 22,328 cycles

AFT EDGE OF LT MLG DOOR HAS CHAFING. C-CHECK REPAIRED CHAFING ON LT MLG DOOR, AFT EDGE IAW REO.

Part: VANE — CHAFED (TE FLAP) · airframe 26,941 hrs · 22,328 cycles

LT INBD FLAP VANE, LE IS CHAFED, OTBD SIDE. C-CHECK REPAIRED CHAFE ON LT INBD FLAP VANE LE IAW REO.

Part: VANE — CHAFED (TE FLAP) · airframe 26,941 hrs · 22,328 cycles

LT INBD FLAP VANE, LE IS CHAFED, INBD SIDE. C-CHECK REPAIRED CHAFE ON INBD SIDE OF LT INBD FLAP VANE LE IAW REO.

Part: SKIN — CHAFED (TE FLAP) · airframe 26,941 hrs · 22,328 cycles

LT INBD FLAP, OTBD VANE ACTUATOR, FLAP UPPER SKIN IS CHAFED ON INTERNAL SURFACE. C-CHECK REPAIRED LT INBD FLAP, AT OTBD VANE ACTUATOR INNER SURFACE IAW REO.

Part: VANE — CHAFED (TE FLAP) · airframe 26,941 hrs · 22,328 cycles

LT INBD FLAP VANE, LE IS CHAFED, CENTER. C-CHECK REPAIRED CHAFE ON LT INBD FLAP VANE LE CENTER IAW REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 26,941 hrs · 22,328 cycles

CRACK NOTED ON FS 621 BULKHEAD WEB, FWD FACE, AT LINTEL FITTING TO BULKHEAD WEB INTERFACE. C-CHECK REPAIRED CRACKED LINTEL ASSEMBLY AT FS 621 BULKHEAD IAW REO.

Part: POST — CRACKED (FUSELAGE) · airframe 26,941 hrs · 22,328 cycles

CRACK NOTED IN FS 409+128 VERTICAL POST AT BL0.0 IN THE RT C CHANNEL, AFT CAP RADIUS. C-CHECK INSTALLED RT VERTICAL POST FS 409+128 AT BL.0 IAW REO.

Part: POST — CRACKED (FUSELAGE) · airframe 26,941 hrs · 22,328 cycles

VERTICAL POST AT FS 409+128 LBL 27 IS CRACKED ON INBD SIDE LOWER RADIUS. C-CHECK INSTALLED NEW VERTICAL POST AT FS 409+128, LBL 27 IAW REO.

Part: POST — CRACKED (FUSELAGE) · airframe 26,941 hrs · 22,328 cycles

VERTICAL POST AT 409+128 RBL 27 IS CRACKED ON LOWER RADIUS ON INBD SIDE. C-CHECK INSTALLED NEW VERTICAL POST AT FS 409+128 RBL 27 IAW REO & SRM.

Part: POST — CRACKED (FUSELAGE) · airframe 26,941 hrs · 22,328 cycles

CRACK NOTED IN FS 409+128 VERTICAL POST AT BL0.0 IN THE LT C CHANNEL, AFT CAP RADIUS. C-CHECK INSTALLED RT VERTICAL POST FS 409+128 AT BL. 0 IN LT C CHANNEL IAW REO.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 26,941 hrs · 22,328 cycles

RT & LT AFT UPPER FLOOR SUPPORT CRACKED OTBD OR RBL 9 & LBL 9. C-CHECK REPAIRED AFT UPPER FLOOR SUPPORT IAW REO.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 26,941 hrs · 22,328 cycles

FS 484 INTERCOSTAL IS CRACKED RBL 27 TO RBL 36 ON OTBD SIDE. C-CHECK REMOVED, FABRICATED & REPLACED CRACKED CLIP CONNECTED TO INTERCOSTAL AT FS 484 RBL 36. IAW REO.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 26,941 hrs · 22,328 cycles

FS 484 INTERCOSTAL IS CRACKED AT LBL 27-LBL 36 ON INBD & OTBD SIDES. C-CHECK REMOVED, FABRICATED & REPLACED CRACKED CLIPS CONNECTED TO INTERCOSTAL AT FS 484 LBL 27 & LBL 36, IAW REO.

Part: SILL — CORRODED (FUSELAGE) · airframe 26,941 hrs · 22,328 cycles

FS 621-605 RT FLOOR EDGE MEMBER HAS SURFACE CORROSION AROUND FOUR NUTPLATE HOLES, FS 559+80 THROUGH FS 559+112 RT FLOOR EDGE MEMBER HAS SURFACE CORROSION AROUND THREE NUTPLATE HOLES. FS 559+80 THROUGH FS 559 +96 RT FLOOR EDGE MEMBER HAS SURFACE CORROSION AROUND FOUR NUTPLATE HOLES & AROUND 5 FASTENERS HEADS. C-CHECK REPAIRED DAMAGE TO RT FLOOR SILL FS 559.00+80 TO FS 621.00 IAW REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,864 hrs · 22,263 cycles

NR 1 CEILING EMERGENCY LIGHT IS BURNED OUT. FLT 5269 RELAMPED.

Part: INVERTER — FAILED (CABIN) · airframe 26,735 hrs · 22,161 cycles

LT SIDE EMERGENCY LIGHT ON INTERIOR DOES NOT ILLUMINATE. FLT#5544 REPLACED NR 2 EMERGENCY LIGHT INVERTER AS REQUIRED.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 26,676 hrs · 22,113 cycles

EMERGENCY FLOOR LIGHT NOT ILLUMINATING FROM ROWS 2-5. FLT#6408 RECONNECTED EMERGENCY LIGHT FLOOR STRIP AT SEAT 2-5.

Part: CONNECTOR — LOOSE (CABIN) · airframe 26,658 hrs · 22,099 cycles

EMERGENCY LIGHT STRIP FROM ROW 2 TO 5 DOES NOT ILLUMINATE. FLT#6215 CLEANED & RECONNECTED FLOOR LEVEL EMERGENCY LIGHT STRIP CONNECTION LOOSE AT ROW 5 & 6.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 26,615 hrs · 22,065 cycles

EMERGENCY LIGHTS STRIP FROM ROW 2-5 & FLOOR LEVEL EXIT SIGN ON THE LT SIDE EXIT OPERATE INTERMITTENTLY. REPLACED NR 1 EMERGENCY BATTERY PACK & EMERGENCY BATTERY PACK CHARGER. PN ON AD-2013-1A, SN ON 83453, SN ON 2013-1A, SN OFF 76576.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 26,615 hrs · 22,065 cycles

LOWER EMERGENCY EXIT LIGHT AT 8A DOES NOT ILLUMINATE. FLT#6351 RESECURED CONNECTOR ON FLOOR.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 26,615 hrs · 22,065 cycles

EMERGENCY LIGHTS ON FLOOR FROM ROW 2-5 NOT ILLUMINATING. FLT#6351 RESECURED CONNECTOR ON FLOOR EMERGENCY LIGHT STRIP.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 26,502 hrs · 21,974 cycles

FIRST FIVE ROWS OF FLOOR EMERGENCY LIGHTING DO NOT ILLUMINATE. FLT#6362 RESECURED CONNECTOR AT SEAT 5C ON EMERGENCY LIGHTS FLOOR TRACK.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 26,484 hrs · 21,962 cycles

FLOOR STRIP LIGHTING INOPERATIVE FROM ROW 2 TO ROW 7 & LT OVERWING EXIT LIGHT DOES NOT ILLUMINATE. FLT#6486 RESECURED CONNECTION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,012 hrs · 21,630 cycles

NR 4 EMERGENCY EXIT LIGHT IS BURNED OUT. FLT#6400 RELAMPED.

Part: WIRE HARNESS — FAULTY (NLG STEERING) · airframe 26,012 hrs · 21,630 cycles

DURING INITIAL TAKEOFF, THRUST LEVERS WERE PUSHED FWD, BOTH N1`S SPOOLED UP TOGETHER, AIRCRAFT STARTED VEERING RT. TAKEOFF WAS ABORTED & RETURNED TO GATE. EXPERIENCED RT CROSSWIND, HAD RT AILERON & FULL LT RUDDER. NOSE WHEEL STEERING WAS ARMED. FLT#5659 REPLACED NOSE GEAR STEERING HARNESS, LT & RT RVDT`S & RIGGED NOSE WHEEL STEERING IAW AMM.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 25,951 hrs · 21,584 cycles

FLT 6284, LAST EMERGENCY LIGHT POD IS BURNED OUT. REPLACED LAMP.

Part: LANDING GEAR — MALFUNCTIONED (NOSE) · airframe 25,716 hrs · 21,420 cycles

NOSE GEAR REMAINED DOWN AND LOCKED AFTER SELECTING GEAR UP AFTER TAKEOFF, RECEIVED GEAR DISAGREE WARNING MESSAGE. AFTER RUNNING QRH PROCEDURE NOSE GEAR RETRACTED. INTERROGATED PSEU, NO FAULTS LOGGED IN MEMORY, NO CURRENT FAULTS. PERFORMED OPERATIONAL TEST OF LANDING GEAR EXTENSION AND RETRACTION SYS IAW AMM. COULD NOT DUPLICATE PROBLEM. SYSTEM OPERATES NORMALLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,654 hrs · 21,371 cycles

LAST EMERGENCY OVERHEAD LIGHT IS BURNED OUT. RELAMPED.

Part: PUMP — WEAK (HYDRAULIC SYS) · airframe 25,578 hrs · 21,315 cycles

RECEIVED NOSE GEAR DOOR WARNING AND GEAR DISAGREE WARNING MESSAGES, NOSE GEAR WOULD NOT RETRACT. DEBRIEFED CREW FOUND THAT PUMP 3B RETRACTED GEAR NORMALLY. FOUND PUMP 3A TO BE WEAK AND REPLACED ACMP 3A IAW AMM. PUMP OPS AND LEAK CHECK GOOD. PERFORMED TEST OF LANDING GEAR EXTENSION AND RETRACTION IAW AMM. OPS CHECK GOOD, NO GEAR DISAGREE OR NOSE GEAR DOOR WARNING MESSAGES. PN ON/OFF 848847, SN ON MX634695, SN OFF MX555513.

Part: WIRE HARNESS — FAILED (NLG STEERING) · airframe 25,158 hrs · 20,992 cycles

ON INITIATION OF TAKEOFF ROLL NOSE WHEEL STEERING WENT HARD OVER TO THE LEFT. (FLT 5538) REPLACED NLG STEERING WIRE HARNESS. FUNCTIONAL FLIGHT AND TAXI CHECK GOOD. P/N 17300-233.

Part: AUTOPILOT SYS — MALFUNCTIONED (COCKPIT) · airframe 24,930 hrs · 20,805 cycles

AUTOPILOT DISENGAGED MULTIPLE TIMES AND PITCHED DOWN AGGRESSIVELY. (FLT 5594) PERFORMED OPERATIONAL CHECK OF AUTOPILOT, OPS CHECK GOOD AT THIS TIME. AIRCRAFT UPGRADED TO CAT II AND RVSM STATUS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,168 hrs · 19,395 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 5 IS OUT. (FLT 6298) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,053 hrs · 19,299 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6306) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,770 hrs · 19,063 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5238) RELAMPED EMERGENCY LIGHT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 22,770 hrs · 19,063 cycles

FLOOR LEVEL EMERGENCY LIGHTS FROM ROWS 2-6 ARE OUT. (FLT 5235) REPLACED THE NR 2 ELBP IN REFERENCE TO THE AMM. PN: 2013-1A, SN OFF: 106493

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,770 hrs · 19,063 cycles

FORWARD OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: SELECTOR VALVE — FAILED (NLG DOOR) · airframe 22,748 hrs · 19,049 cycles

RECEIVED NOSE DOOR OPEN AND GEAR DISAGREE WARNING MESSAGES. (FLT 6453) REPLACED NOSE GEAR DOOR SELECTOR VALVE. PN: 750006000 SN OFF 0388T

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,657 hrs · 18,980 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5299) RELAMPED EMERGENCY LIGHT.

Part: TORQUE LINK — DISCONNECTED (NLG) · airframe 22,657 hrs · 18,980 cycles

GEAR DISAGREE MESSAGES. (FLT 5326) FOUND TORQUE LINKS DISCONNECTED. REPLACED NR 1 AND NR 2 NOSE TIRES AND RECONNECTED TORQUE LINKS. P/N: 5010598 S/N OFF: JAN01-0084 P/N: 5010598 S/N OFF: JAN02-3883

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,534 hrs · 18,863 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: PRIORITY VALVE — FAILED (NLG) · airframe 22,390 hrs · 18,736 cycles

NOSE GEAR WILL NOT GO UP AFTER SELECTING GEAR HANDLE TO THE UP POSITION. (FLT 5603) REPLACED NLG PRIORITY VALVE AND THE NLG SELECTOR VALVE IN REF TO AMM. PART OFF: 4622 S/N OFF: 1690A PART OFF: 750006000 S/N OFF: 1827.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 22,325 hrs · 18,686 cycles

FS 202.75 BULKHEAD FORWARD LEFT SIDE IS CRACKED. (C-CHECK) REPAIRED CRACK AT FS 202.75 BULKHEAD FORWARD LEFT SIDE.

Part: SKIN — CHAFED (LT AILERON) · airframe 22,325 hrs · 18,686 cycles

LEFT AILERON ASSEMBLY UPPER LEADING EDGE IS CHAFED. (C-CHECK) REPAIRED LEFT AILERON ASSEMBLY UPPER LEADING EDGE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,249 hrs · 18,632 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6384) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,160 hrs · 18,570 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5356) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,160 hrs · 18,570 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6196) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 22,144 hrs · 18,558 cycles

AFT EXTERNAL EMERGENCY LIGHTS ON RIGHT ARE OUT. (FLT 6215) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 22,124 hrs · 18,542 cycles

EXTERIOR SERVICE DOOR EMERGENCY EXIT LIGHT IS OUT. (FLT 5329) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 22,124 hrs · 18,542 cycles

LEFT WING EXTERIOR CENTER EMERGENCY EXIT LIGHT IS OUT. (FLT 5329) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,044 hrs · 18,481 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5630) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,934 hrs · 18,392 cycles

NR 3 CEILING EMERGENCY LIGHT IS OUT. (FLT 5342) RELAMPED EMERGENCY LIGHT.

Part: INVERTER — FAILED (CABIN) · airframe 21,862 hrs · 18,336 cycles

SEVERAL FLOOR EMERGENCY LIGHT STRIPS AND EMERGENCY EXIT SIGN BY LEFT EXIT DOOR ARE INOPERATIVE. (SERVICE) REPLACED NR 2 INVERTER FOR EMERGENCY LIGHTS.

Part: STRUT — LOW (NLG) · airframe 21,831 hrs · 18,316 cycles

NOSE GEAR WOULD NOT RETRACT. (FLT 6250) PERFORMED FULL SERVICE OF NOSE STRUT PER AMM.

Part: STRUT — INOPERATIVE (EXTERIOR) · airframe 21,831 hrs · 18,316 cycles

LEFT REAR EXTERIOR EMERGENCY LIGHT IS OUT. (FLT 6369) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 21,750 hrs · 18,254 cycles

FORWARD EMERGENCY LIGHT FLOOR STRIP IS OUT. (FLT 5508) RE-CONNECTED FORWARD EMERGENCY LIGHT FLOOR STRIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,717 hrs · 18,225 cycles

FIRST OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5552) RELAMPED EMERGENCY LIGHT.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 21,717 hrs · 18,225 cycles

SOME EMERGENCY FLOOR LIGHTS DO NOT LIGHT UP WHEN TESTED. (FLT 5294) RE-SECURED CONNECTOR AT FORWARD EMERGENCY LIGHT BATTERY PACK.

Part: CONNECTOR — DIRTY (CABIN) · airframe 21,633 hrs · 18,142 cycles

1ST FOUR GREEN FLOOR EMERGENCY LIGHT STRIP SEGMENTS ARE OUT. (FLT 5229) CLEANED CONNECTOR TO FORWARD EMERGENCY LIGHT BATTERY PACK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,475 hrs · 18,002 cycles

NR 2 AND 2ND TO LAST OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 5557) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,475 hrs · 18,002 cycles

RIGHT SIDE OVERWING AFT EMERGENCY LIGHT IS OUT. (FLT 6217) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,342 hrs · 17,879 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6406) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,270 hrs · 17,821 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6324) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,195 hrs · 17,763 cycles

NR 2 AND NR 3 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 6209) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,145 hrs · 17,711 cycles

NR 1 AND NR 3 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 5824) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,133 hrs · 17,697 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS BURNED OUT. (FLT 5297) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,019 hrs · 17,611 cycles

CABIN EMERGENCY LIGHT ABOVE ROW TWO IS NOT WORKING. (FLT 5441) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,019 hrs · 17,611 cycles

RIGHT WING AFT EMERGENCY EXIT LIGHT IS OUT. (FLT 5458) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 21,019 hrs · 17,611 cycles

LEFT OVERWING EXTERIOR FORWARD EMERGENCY LIGHT IS OUT. (FLT 5458) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,019 hrs · 17,611 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5562) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,019 hrs · 17,611 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6471) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,859 hrs · 17,482 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5364) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,820 hrs · 17,458 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6194) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,703 hrs · 17,372 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5588) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 20,601 hrs · 17,289 cycles

LEFT MIDDLE EXTERIOR EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,394 hrs · 17,137 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6222) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,202 hrs · 16,975 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6769) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 20,099 hrs · 16,890 cycles

NR 2 LEFT MIDDLE EXTERIOR EMERGENCY LIGHT IS OUT. (FLT 6511) RELAMPED EMERGENCY LIGHT.

Part: HOUSING — CORRODED (ENGINE MOUNT) · airframe 19,600 hrs · 16,461 cycles

RIGHT ENGINE AFT MOUNT SPHERICAL BUSHING HOUSING HAS SOME PITTING. (ENGINE CHANGE) REPLACED RIGHT ENGINE SPHERICAL BUSHING HOUSING.

Part: SIGN — DISLODGED (CABIN) · airframe 19,088 hrs · 16,010 cycles

EXIT SIGN OVER GALLEY SERVICE DOOR DISLODGED. (FLT 6565) REPLACED SERVICE DOOR EXIT SIGN ASSEMBLY.

Part: OVERHEAT LOOP — BROKEN (LT ENGINE) · airframe 18,650 hrs · 15,650 cycles

L JETPIPE OVERHEATT WARNING MESSAGE IN FLIGHT. LED TO LT ENGINE SHUTDOWN IN FLIGHT. (FLT 6611) REPAIRED LOOP A AND B TERMINAL ENDS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,376 hrs · 15,425 cycles

AFT CEILING EMERGENCY LIGHT IS INOPERATIVE. (SERVICE CHECK) RELAMPED EMERGENCY LIGHT.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 17,988 hrs · 15,072 cycles

FS 559 PRESSURE BULKHEAD WEB CRACKED ON CAP ANGLE BELOW VERTICAL POST. (C CHECK) REPAIRED PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 18,273 hrs · 15,335 cycles

A .5 INCH CRACK NOTED ON FS 559.0 PRESSURE BULKHEAD WEB AT RBL 18.0 WL 59.10 & .5 INCH CRACK ON CAP ANGLE BELOW VERT POST AT RBL 18.0. (C-CHECK) REPAIRED PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,988 hrs · 15,072 cycles

NR 2 EMERGENCY FLOODLIGHT INOP. (FLT 6220) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,252 hrs · 14,473 cycles

EMERGENCY LIGHTS OVER ROW 10 INOP. (FLT 5989) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,998 hrs · 14,280 cycles

EMERGENCY CEILING LIGHTS NR 1 & NR 3 INOP. (FLT 5881) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,942 hrs · 14,234 cycles

FURTHEST AFT CEILING EMERGENCY LIGHT INOP. (FLT 6306) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,620 hrs · 13,965 cycles

FLT 5983 - AFT EMERGENCY CEILING LIGHT INOP. RELAMPED.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 16,124 hrs · 13,552 cycles

EMERGENCY LIGHTS BETWEEN ROW 6 & 8 INOP. (FLT 6608)REPLACED NR 3 INVERTER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,086 hrs · 13,520 cycles

FLOOR EMERGENCY LIGHT SEGMENT INOP. (FLT 6692) REPOWERED AIRCRAFT, OPERATION NORMAL.

Part: SIGN — INOPERATIVE (CABIN) · airframe 16,073 hrs · 13,506 cycles

LOWER EMERGENCY EXIT SIGN AT RIGHT OVERWING EXIT INOP. (FLT 6595) OPERATIONAL CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,962 hrs · 13,416 cycles

RIGHT WING LOWER EMERGENCY LIGHT INOP. (FLT 6657) REPLACED LIGHT ASSEMBLY.

Part: CONNECTOR — LOOSE (CABIN) · airframe 15,962 hrs · 13,416 cycles

EMERGENCY FLOOR LIGHTS INOP. (FLT 6701) RE-SEATED BATTERY CHARGER CONNECTION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,946 hrs · 13,402 cycles

EMERGENCY LIGHT IN CEILING AT ROW 2 INOP. (FLT 6529) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,343 hrs · 12,916 cycles

FIRST EMERGENCY CEILING FLOOD LIGHT INOP. (FLT 6000) RELAMPED EMERGENCY LIGHT.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 15,276 hrs · 12,864 cycles

PHOTO ILLUMINESCENT STRIP MISSING FROM THE RIGHT SIDE OF GALLEY DOOR. (FLT 6688) REPLACED STRIP.

Part: CONNECTOR — LOOSE (CABIN) · airframe 15,121 hrs · 12,754 cycles

AFT EMERGENCY LIGHT STRIPS INOP. (FLT 6407) RESECURED CONNECTOR.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 14,670 hrs · 12,405 cycles

FLT 5964 - LAST EMERGENCY CEILING LIGHT INOP. RELAMPED.

Part: TIRE — FLAT (MLG) · airframe 14,556 hrs · 12,307 cycles

FLT 6562 - NR 4 TIRE FLAT ON TAXI. RESEATED BRAKE QUICK DISCONNECT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 14,182 hrs · 12,015 cycles

FLT 6719 - OVERHEAD CEILING EMERGENCY LIGHT (3RD BACK) INOP. RELAMPED.

Part: COALESCER BAG — DIRTY (AC BAY) · airframe 13,799 hrs · 11,733 cycles

FLT 5862 - BURNING ODOR FROM GASPERS WITH SMOKE TOILET CAUTION MESSAGE DISPLAYED. REPLACED LEFT AND RIGHT COALESCER BAGS AND PERFORMED COMPRESSOR WASH.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,653 hrs · 11,616 cycles

FLT 6014 - OVERHEAD EMERGENCY DOME LIGHT INOP. RELAMPED.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 13,247 hrs · 11,302 cycles

FLT 5891 - FIRST OVERHEAD EMERGENCY LIGHT INOP. REPLACED BATTERY CHARGER.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 13,247 hrs · 11,302 cycles

FLT 6517 - FORWARD EMERGENCY LIGHTS DIM. REPLACED BATTERY PACK, PN AD-2013-1A, SN ON 79469, SN OFF 69315.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 13,453 hrs · 11,467 cycles

C-CHECK, FS 280 RBL 9 FLOOR SUPPORT ANGLE CLIPS CRACKED. REPLACED PER SRM.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 13,453 hrs · 11,467 cycles

C-CHECK, FS 280 RBL 12 FLOOR SUPPORT ANGLE CLIP CRACKED. REPLACED PER SRM.

Part: UNKNOWN — SMOKE (CABIN) · airframe 11,751 hrs · 10,050 cycles

FLT 6676 - CREW SMELLED SMOKE IN THE COCKPIT FOLLOWED BY A "SMOKE TOILET" MESSAGE. INSPECTED AND PERFORMED HIGH POWER RUNS ON AIRCRAFT WITH NO DISCREPANCIES NOTED. REPLACED LAVATORY SMOKE DETECTOR IAW RJ 200 MM REF 26-16-01. OPS CHECK GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 11,118 hrs · 9,499 cycles

FLT 6331 - CREW REPORTED BURNING ODOR NEAR ROW 7. INSPECTED LIGHT FIXTURES AND OVERHEAD PANELS AS WELL AS AVIONICS BAY. NO DISCREPANCY NOTED. NO ODOR NOTED.

Part: A/C PACK — CONTAMINATED · airframe 11,029 hrs · 9,423 cycles

FLT 5865 - RECEIVED A SMOKE TOILET INDICATION AFTER TAKEOFF. FOUND LEFT AND RIGHT PACKS SATURATED WITH DE ICING FLUID. CLEANED DUCTS AND REPLACED SOCKS, PER AMM 21-51-13.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 10,230 hrs · 8,754 cycles

FLT 6028 - AFT CEILING LEVEL EMERGENCY FLOODLIGHT IS INOP. RELAMPED AFT CEILING EMERGENCY LIGHT. OPS CHECK GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 9,025 hrs · 7,691 cycles

FIRST EMERGENCY CEILING FLOOD LIGHT IS INOP. REPLACED BULB ON FIRST CEILING EMERGENCY LIGHT.

Part: UNKNOWN — ODOR (CABIN) · airframe 8,177 hrs · 6,969 cycles

AT APPROXIMATELY 2000 AGL, COULD HEAR A BUZZING/CLICKING NOISE FROM CBP NR 2 AND AT TIMES COULD SMELL AN 'OVERHEATING' TYPE ODOR. INSPECTED CB PANEL NR 2. NO DEFECTS/ODOR. UNABLE TO DUPLICATE DISCREPANCY.

Part: NUT CLIP — CRACKED (FLOOR SUPPORT) · airframe 8,400 hrs · 7,157 cycles

FOUND STA 280 RBL 9.0 INBD AND OTBD CLIPS ON FLOOR SUPPORT ARE CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED RT OTBD CLIP AT STA 280 RBL 9.0 PER CRJ200 SRM 51-42-21.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 8,400 hrs · 7,157 cycles

FOUND FS 484 LBL 28 INTERCOSTAL, BRACKET CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP P/N 601R31171-17 TO FS 484 INTERCOSTAL LBL 28 PER CRJ200 SRM 51-42-06 PG 11 AND 51-42-21 PG 17.

Part: WEB — CRACKED (PAX DOOR) · airframe 8,400 hrs · 7,157 cycles

FOUND PAX DOOR FWD WEB IS CRACKED AT HANDRAIL DOWN STOP BRACKET, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED 2 ANGLES AND 1 DOUBLER ON PAX DOOR FWD WEB IAW REO 601R-52-11-702A PAGE 4 ITEM 8.

Part: NUT CLIP — CRACKED (FLOOR SUPPORT) · airframe 8,400 hrs · 7,157 cycles

FOUND STA 280 LBL 9.0 OTBD CLIP ON FLOOR SUPPORT IS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED OTBD CLIP AT FS 280 AS PER CRJ200 SRM 51-42-06.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 8,400 hrs · 7,157 cycles

FOUND PAX DOOR OUTER HANDLE CRACKED AT RADIUS, DISCOVERED DURING C-CHECK INSPECTION. REPLACED OUTER PAX DOOR HANDLE PER CRJ200 AMM 52-11-03-000-802/400-802.

Part: WEB — CRACKED (BS 5280) · airframe 8,400 hrs · 7,157 cycles

FOUND CRACK ON FS 5280 WEB AT RBL10 LOWER PART OF BEAM AT INTERSECTION POINT WITH FLOOR POST AND WEB, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED ANGLE PER CRJ200 SRM 51-42-21.

Part: WEB — CRACKED (PAX DOOR) · airframe 8,400 hrs · 7,157 cycles

FOUND PAX DOOR AFT WEB CRACKED AT STAIR 832DT AND 832CT RADIUS, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR ANGLES AND DOUBLER IAW REO 601R-52-11-702.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 8,400 hrs · 7,157 cycles

FOUND FS 484 LBL 36 INTERCOSTAL BRACKET CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED ANGLE AT FS 484 PER REO 601R-53-41-059 REV A.

Part: SILL — CORRODED (FUSELAGE) · airframe 8,400 hrs · 7,157 cycles

FOUND PAX DOOR OPENING LOWER AFT SILL AREA AFT STEP PLATE HAS 4 EA CORRODED RUSTED BOLTS BOLTS ATTACH ANCHOR FITTING TO STEP PLATE, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW BOLTS AND SCREWS ON PASSENGER DOOR COUNTER BALANCE ANCHOR FITTING PER CRJ200 AMM 52-11-17-400-804.

Part: ATTACH ANGLE — CRACKED (BS 621) · airframe 8,400 hrs · 7,157 cycles

FOUND STA 621 BULKHEAD TO FLOOR ATTACH ANGLE CRACKED LT OTBD SIDE, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED SPLICE, REPAIR ANGLES AND STRAP AS PER REO 601R-53-61-117.

Part: BRACKET — CRACKED (LT MLG WW) · airframe 8,400 hrs · 7,157 cycles

FOUND LT WHEEL WELL TRANSDUCER BRACKET CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED LEFT WHEEL WELL TRANSDUCER BRACKET PER CRJ200 SRM 51-42-06 AND 51-80-00.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 8,400 hrs · 7,157 cycles

FOUND PAX DOOR AFT DRAG ANGLE CRACKED AT CABLE EXIT FOR PULL IN MOTOR, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED ANGLE SECTION AND SPLICE ANGLE IAW REO 601R-52-11-513.

Part: LIGHT — FAILED (CABIN) · airframe 7,683 hrs · 6,557 cycles

LEFT EMERGENCY EXIT FLOURESCENT STRIP FLOOR LIGHT INOP. REPLACED NR 2 BATTERY PACK INVERTER REF AMM 33-55-00. OPERATIONAL CHECKS GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 7,353 hrs · 6,244 cycles

NR 1 EMERGENCY END LIGHT IN CEILING IS INOP. REPLACED NR 1 EMERGENCY FLOODLIGHT BULB ON CEILING IAW 33-51-16. OPERATIONAL CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 6,823 hrs · 5,789 cycles

FORWARD EMERGENCY LIGHT POD IS BURNED OUT. RELAMPED FORWARD EMERGENCY FLOODLIGHT. OPERATIONAL CHECKS GOOD.

Part: TRIM PANEL — INOPERATIVE (RUDDER CONTROL) · airframe 3,887 hrs · 3,278 cycles

RUDDER TRIM KNOB INOP. REPLACED RUDDER/AILERON TRIM CONTROL PANEL. OPERATIONAL CHECK GOOD IAW CRJ MM 27-22-00 AND 27-12-10.

Part: ACTUATOR — MALFUNCTIONED (HORIZONTAL STAB) · airframe 4,129 hrs · 3,480 cycles

UPON T/O RECEIVED A STAB CH 1 INOP STATUS MSG. INSTALLED A SERVICEABLE HSTCA & MCU IAW MM 27-40-00. MCU P/N: 7062-3 S/N OFF: 1212.

Part: CLIP — CRACKED (BS 280) · airframe 4,783 hrs · 4,000 cycles

FWD AVIONICS COMPARTMENT STA 280 RBL 9 INBD FRAME CLIP CRACKED, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW FRAME CLIP AT STA280 RBL 9 INBD IAW CRJ200 SRM 51-42-06 AND 51-42-16.

Part: CLIP — CRACKED (BS 280) · airframe 4,783 hrs · 4,000 cycles

FWD AVIONICS COMPARTMENT STA 280 LBL 9 INBD FRAME CLIP CRACKED, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW FRAME CLIP IAW CRJ200 SRM 51-42-06 AND 51-42-21.

Part: CLIP — CRACKED (BS 280) · airframe 4,783 hrs · 4,000 cycles

FWD AVIONICS COMPARTMENT STA 280 LBL 9 OTBD FRAME CLIP CRACKED ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW FRAME CLIP IAW CRJ200 SRM 51-40-11.

Part: CLIP — CRACKED (BS 280) · airframe 4,783 hrs · 4,000 cycles

FWD AVIONICS COMPARTMENT STA 280 RT BL 9 OTBD FRAME CLIP CRACKED, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW FRAME CLIP AT STA 280 RBL 9 OTBD IAW CRJ200 SRM 51-42-06 AND 51-42-16.