N460SW

Part: FLOORBEAM — CORRODED (BS 280) · airframe 39,894 hrs · 37,080 cycles

F.S. 280 FLOORBOARD SUPPORT ANGLE IS CORRODED BETWEEN LBL9 TO RBL9. REMOVED AND REPLACED CORRODED FS280 FLOORBOARD SUPPORT ANGLE BETWEEN LBL9 TO RBL9 IAW REO 601R-53-11-926 REV B.

Part: FLOORBEAM — MECHANIC ERROR (BS 280) · airframe 39,894 hrs · 37,080 cycles

F.S. 280 TOP OF ANGLE BETWEEN LBL27 TO LBL36 HAS A SNOW MAN HOLE AROUND NUTPLATE. REPAIRED FS280 LBL27 TO LBL36 IAW MHIRJ REO 601R-53-11-3815 REV. -.

Part: FLOORBEAM — CORRODED (BS 409) · airframe 39,894 hrs · 37,080 cycles

RBL9 FLOOR BEAM IS CORRODED BETWEEN F.S. 409+32 TO F.S. 409+48. INSTALLED NEW SERVICEABLE RBL9 FLOOR BEAM CAP FROM F.S 409.00+5 F.S 409.00+118 IAW MHIRJ REO 601R-53-31-1254 DATED: 2022-12-12 REV: -- , CRJ 200 SRM 51-42-21 AND 51-42-06.

Part: FLOORBEAM — CORRODED (BS 409) · airframe 39,894 hrs · 37,080 cycles

LBL9 FLOOR BEAM IS CORRODED BETWEEN F.S. 409+64 TO F.S. 409+80. INSTALLED NEW SERVICEABLE FLOOR BEAM IAW REO 601R-53-31-1256 REV.

Part: HINGE — CHAFED (PAX DOOR) · airframe 39,894 hrs · 37,080 cycles

WHILE INSPECTING REPAIR ON PAX DOOR PIANO HINGE HALF ON DOOR SIDE HAS CHAFES ON THE FOLLOWING LUGS (FROM FWD SIDE TO AFT): 1, 2, 4, 5, 12, 13, 15, 16, 19, 20, 22, 24, 25, 26, AND 27. JOB 9780385 OP 00053, CAMP 25881132 FOUND ALL LUGS ON FUSELAGE SIDE OF HINGE TO BE ELONGATED WITH A GREATER DIAMETER THAN .295" CAUSING ALL FUSELAGE SIDE LUG LANDINGS TO BE CHAFED. REO 601R-53-21-814 RECOMMENDS HINGE REPLACEMENT REPLACED PAX DOOR HINGE FUSELAGE SIDE IAW CRJ-200 SRM 53-21-23 REV. 39 AND REO 601R-53-21-656 REV. -A

Part: POST — CRACKED (BS 409) · airframe 39,894 hrs · 37,080 cycles

FS409+128 LBL18 OUTBD VERTICAL POST HAS AN INDIACTION .2" LONG BY 50% FSH IN THE AFT RADIUS @WL69. FAILED NDT INSPECTION, REMOVED AND REPLACED INBD AND OUTBD VERTICAL POST AT FS 409+128 LBL18 IAW REO 601R53-41-889D AND CRJ-200 SRM 51-42-06,

Part: POST — CRACKED (BS 409) · airframe 39,894 hrs · 37,080 cycles

FS409+128 RBL18 OUTBD VERTICAL POST HAS AN INDIACTION .2" LONG BY 60% FSH IN THE AFT RADIUS @WL69. FAILED NDT INSPECTION, (C-CHECK RO 12/29/2022) INSTALLED NEW SERVICABLE FS409+128 RBL18 OUTBD VERTICAL POST IAW REO 601R-53-41-889 REV-D DATED 2018-10-04.

Part: BRACKET — CRACKED (BS 621 BULKHEAD) · airframe 39,894 hrs · 37,080 cycles

BS 621 REAR PRESSURE BULKHEAD AFT SIDE, AT STGR 15R INTERCOSTAL CENTER ATTACH ANGLE IS CRACKED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-21.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 39,894 hrs · 37,080 cycles

RIGHT INBD. FLAP VANE HAS 3 EA. CHAFS ON L/E AT POSITIONS WHERE BUMPER STOPS MAKE CONTACT. REMOVED AND REPLACED RH I/B FLAP VANE LEADING EDGES IAW SRM 51-42-13.

Part: NONE — FAILED · airframe 39,120 hrs · 36,126 cycles

ON APPROACH LANDING GEAR DISAGREE WHEN LOWERING GEAR, CYCLED GEAR PER QRH AND STILL HAD DISAGREE (NOSE GREEN MAIN WHITE) PROCEEDED WITH QRH AND GOT 3 GREEN WITH MANUAL GEAR EXTENSION (FLIGHT 4234 - FILED CLOSED) TROUBLESHOT LANDING GEAR DISAGREE. PERFORMED EXTENSION AND RETRACTION OF LANDING GEAR. BOTH MLG STAYED UP AND LOCKED DURING EXTENSION. NLG EXTENDED TO DOWN AND LOCKED. REMOVED AND REPLACED MLG SELECTOR VALVE IAW AMM 32-32-10. PERFORMED EMERGENCY EXTENSION AND 8 SUCCESSFUL EXTENSIONS AND RETRACTIONS. OPS AND LEAK CHECK GOOD AT THIS TIME.

Part: NONE — WORN · airframe 38,909 hrs · 35,876 cycles

L/H INBOARD FLAP MOVEABLE VANE IS SHOWING WEAR ALONG LEADING EDGE WHERE VANE MEETS STOPS. (FILED - CLOSED) REPLACED L/H INBD FLAP ASSY AS REQUIRED REFERENCING APPLICABLE STEPS OF AMM 57-21-34 AND AMM 27-54-01 AND COMPLIED WITH 27-900-1006. / TORQUE WRENCH S/N 0719113377, DUE 8/22

Part: CONNECTOR — OUT OF TOLERANCE (SPOILER PSU) · airframe 37,377 hrs · 33,953 cycles

RT INBOARD FLIGHT SPOILER PCU RESISTANCE VALUE MEASURED AT SECU PLUG: 1P1CN-B PINS: 1K/2K WAS FOUND TO BE OUT OF RANGE (1,024 K OHMS). FILED CLOSED. REMOVED AND REPLACED RT FLIGHT SPOILER INBOARD PCU, IN REFERENCE TO CRJ 200 AMM. OPERATIONS CHECK GOOD AT THIS TIME, REF CP 21820703 FOR LEAK CHECK.

Part: CONNECTOR — OUT OF TOLERANCE (SPOILER PCU) · airframe 37,377 hrs · 33,953 cycles

LT INBOARD SPOILERON PCU RESISTANCE VALUE MEASURED AT SECU PLUG: 2P1CN-B PINS: 1A/2A WAS FOUND TO BE OUT OF RANGE (6.2M OHMS). FILED CLOSED. REMOVED AND REPLACED LT SPOILERON INBOARD PCU, IAW AMM. OPERATIONS CHECK GOOD, REF CP 21820650 FOR LEAK CHECK.

Part: CONNECTOR — OUT OF TOLERANCE (SPOILER PCU) · airframe 37,377 hrs · 33,953 cycles

LT OUTBOARD SPOILERON PCU RESISTANCE VALUE MEASURED AT SECU PLUG: 1P1CN-A PINS:11A/12A WAS FOUND TO BE OUT OF RANGE (1,029 K OHMS). FILED CLOSED. REMOVED AND REPLACED LT SPOILERON OUTBOARD PCU, IAW AMM. OPERATIONS CHECK GOOD, REF CP 21826310 FOR LEAK CHECK.

Part: CONNECTOR — OUT OF TOLERANCE (SPOILER PCU) · airframe 37,377 hrs · 33,953 cycles

RT OUTBOARD FLIGHT SPOILER PCU RESISTANCE VALUE MEASURED AT SECU PLUG: 2P1CN-A PINS: 11K/12K WAS FOUND TO BE OUT OF RANGE (1,040 K OHMS). FILED CLOSED. REMOVED AND REPLACED RT FLIGHT SPOILER OUTBOARD PCU, IN REFERENCE TO CRJ 200 AMM. OPERATIONS CHECK GOOD AT THIS TIME, REF CP 21820704 FOR LEAK CHECK.

Part: BOLT — CORRODED (LT WING MOUNT) · airframe 36,367 hrs · 32,668 cycles

* LEFT WING CORRODED MOUNTING HARDWARE LEFT WING , GROUND, FLIGHT AND SPOILERONS. HINGE FITTINGS HAVE CORRODED MOUNT BOLTS, NUTS , WASHERS. (C-CHECK) RO 12/13/2019 REMOVED AND REPLACED HINGE HARDWARE ON LH OUTBOARD GROUND SPOILER, LH FLIGHT SPOILER, AND LH SPOILERON REF AMM. RIGS GOOD. OPS TESTS GOOD

Part: BOLT — CORRODED (ACTUATOR MOUNT) · airframe 36,367 hrs · 32,668 cycles

* LEFT WING OUTBOARD GROUND SPOILER HAS CORRODED ACTUATOR MOUNT HARDWARE. BOLT, NUT, AND WASHER. MARKED WITH ORANGE FLAG. (C-CHECK) RO 12/13/2019 REMOVED OLD AND INSTALLED NEW HARDWARE ON LH OUTBOARD GROUND SPOILER AMM. OPS TEST GOOD. RIG CHECK GOOD

Part: BOLT — CORRODED (ACTUATOR MOUNT) · airframe 36,367 hrs · 32,668 cycles

* RIGHT WING INBOARD GROUND SPOILER HAS CORRODED ACTUATOR MOUNT HARDWARE. BOLT, NUT, AND WASHER. MARKED WITH ORANGE FLAG. (C-CHECK) RO 12/13/2019 REMOVED CORRODED HARDWARE, AND REPLACED WITH NEW HARDWARE REF AMM. OPS CHECK GOOD. RIG CHECK GOOD

Part: RETAINER — CORRODED (RT AILERON BOLT) · airframe 36,367 hrs · 32,668 cycles

* R/H AILERON OBD HINGE BOLT RETAAINERS HAVE CORRODED HARDWARE, (C-CHECK) RO 12/13/2019 REMOVED RIGHT AILERON OUTBOARD HINGE BOLT RETAINERS HARDWARE REF AMM AND INSTALLED (4EA) NEW BOLTS/WASHERS REF AMM.

Part: RETAINER — CORRODED (LT AILERON HINGE) · airframe 36,367 hrs · 32,668 cycles

* L/H AILERON OBD HINGE BOLT OBD RETAINER HARDWARE CORRODED. (C-CHECK) RO 12/13/2019 ORDERED AND RECEIVED NEW L/H OBD HINGE BOLTS OBD RETAINER HARDWARE; BOLTS (2EA) AND WASHERS (2EA). INSTALLED ON JOB 2780375 OP 5174 AND TRANS # 19723205.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 36,367 hrs · 32,668 cycles

*PAX DOOR LOWER FLOOR SILL IS CORRODED. FLAGGED (C-CHECK) RO 12/13/2019 REPLACED WITH NEW PART PAX DOOR LOWER FLOOR SILL REF SRM, SEE CONTINUATION CARD FOR DETAILS.

Part: RETAINER — CORRODED (LT AILERON HINGE) · airframe 36,367 hrs · 32,668 cycles

* L/H AILERON OBD HINGE BOLT OBD RETAINER HARDWARE CORRODED. (C-CHECK) RO 12/13/2019 ORDERED AND RECEIVED NEW L/H OBD HINGE BOLTS OBD RETAINER HARDWARE; BOLTS (2EA) AND WASHERS (2EA). INSTALLED ON JOB 2780375 OP 5174 AND TRANS # 19723205.

Part: HINGE — CORRODED (LAVATORY DOOR) · airframe 36,367 hrs · 32,668 cycles

* LAVATORY SERVICE DOOR ( 196AR ) HAS UPPER AND LOWER HINGES ( BOTH HALFS ) CORRODED. (C-CHECK) RO 12/13/2019 REMOVED AND REPLACED BOTH SIDES OF THE HINGES ON LAV SERVICE DOOR 196AR REF SRM. ALL PARTS PART FOUND TO BE EXFOLIATED. BOND CHECKS GOOD

Part: RETAINER — CORRODED (LT AILERON HINGE) · airframe 36,367 hrs · 32,668 cycles

* L/H AILERON OBD HINGE BOLT OBD RETAINER HARDWARE CORRODED. (C-CHECK) RO 12/13/2019 ORDERED AND RECEIVED NEW L/H OBD HINGE BOLTS OBD RETAINER HARDWARE; BOLTS (2EA) AND WASHERS (2EA). INSTALLED ON JOB 2780375 OP 5174 AND TRANS # 19723205.

Part: BOLT — CORRODED (ACTUATOR MOUNT) · airframe 36,367 hrs · 32,668 cycles

* LEFT WING INBOARD GROUND SPOILER HAS CORRODED ACTUATOR MOUNT HARDWARE. BOLT, NUT AND WASHER. MARKED WITH ORANGE FLAG. (C-CHECK) RO 12/13/2019 REMOVED OLD HARDWARE AND REPLACED WITH NEW HARDWARE AMM. OPS TEST GOOD. RIG GOOD

Part: BOLT — CORRODED (RT WING MOUNT) · airframe 36,367 hrs · 32,668 cycles

* RIGHT WING CORRODED MOUNTING HARDWARE RIGHT WING, GROUND, FLIGHT AND SPOILERONS. HINGE FITTINGS HAVE CORRODED MOUNT BOLTS, NUTS, WASHERS. (C-CHECK) RO 12/13/2019 REPLACED CORRODED MOUNTING HARDWARE AT RIGHT WING GROUND SPOILERS, FLIGHT SPOILER AND SPOILERON HINGE FITTINGS REF AMM. RIG AND OPS CHECK GOOD.

Part: HINGE FITTING — GOUGED (LT AILERON) · airframe 36,367 hrs · 32,668 cycles

* L/H AILERON INB AND OBD CENTER HINGE FITTINGS ATTACHED TO AFT WING SPAR HAVE SMALL GOUGES ON LOWER SIDES OF FITTINGS. (C-CHECK) RO 12/13/2019 BLENDED GOUGES - EVALUATED REPAIRS, FOUND TO BE OUT OF LIMITS. REQUESTED ENGINEERING SUPPORT AND RECIEVED REO, COMPLIED WITH ALL STEPS OF REO. PART IN LIMITS. REF REO.

Part: DOOR SILL — CORRODED (CABIN) · airframe 36,367 hrs · 32,668 cycles

**PAX DOOR LOWER FLOOR SILL CAP ANGLE IS CORRODED. FLAGGED (C-CHECK) RO 12/13/2019 FOUND NO CORROSION ON PAX DOOR LOWER FLOOR SILL CAP ANGLE ( MADE FROM STEEL PER SRM) AFTER CLEANED RUST FROM CORRODED SCREWS REF AMM.

Part: DOOR FRAME — CORRODED (E/E BAY) · airframe 36,367 hrs · 32,668 cycles

*AVIONICS DOOR CUT-OUT AFT SRUCTURE IS CORRODED FRAME "ANGLE. FLAGGED" (C-CHECK) RO 12/13/2019 REMOVED CORROSION FROM AVIONICS CUT-OUT AFT STRUCTURE ANGLE AT FS394.00 REF SRM. FOUND TO BE OUT OF LIMITS REF SRM. MEASURED THICKNESS ..042. ORIGINAL THICKNESS .050 REF SRM. MATERAL LOSS .008 MAX ALLOWED .005. COMPLIED WITH ALL STEPS OF REO. LEAK CHECK GOOD

Part: BOLT — CORRODED (GROUND SPOILER) · airframe 36,367 hrs · 32,668 cycles

RIGHT WING OUTBOARD GROUND SPOILER HAS CORRODED ACTUATOR MOUNT HARDWARE. BOLT, NUT, AND WASHER . MARKED WITH ORANGE FLAG. (C-CHECK) RO 12/13/2019 REMOVED CORRODED HARDWARE AND INSTALLED NEW HARDWARE REF AMM. OPS TEST GOOD. RIG GOOD

Part: DUCT — CRACKED (APU AIR INLET) · airframe 36,367 hrs · 32,668 cycles

* APU LOWER AIR INLET DUCT HAS MULTIPLE CRACKED STIFFENERS. (C-CHECK) RO 12/13/2019 ORDERED AND RECEIVED APU AIR INLET DUCT, INSTALLED ON JOB 2780375, OP/23, MX TRANS #19808669.

Part: ATTACH ANGLE — CRACKED (LT WING LE) · airframe 36,367 hrs · 32,668 cycles

* L/H WING CENTER LEADING EDGE PANEL INB ATTACHMENT ANGLE CRACKED. ( FLAGGED ) (C-CHECK) RO 12/13/2019 LOACATED AND DRILLED A NEW ATTACH ANGLE FOR THE LH WING CENTER LEADING EDGE, IB END REF SRM AND INSTALLED IT REF SRM.

Part: ANGLE — CRACKED (RT WING TE) · airframe 36,367 hrs · 32,668 cycles

RH WING TRAILING EDGE IB CAP ANGLE ( BATT RIB) IS CRACKED, FOUND WHILE ACCESSING TRUNNION REPLACEMENT. (C-CHECK) RO 12/13/2019 REMOVED CRACKED CAP ANGLE( BATT RIB) ON RH WING AND INSTALLED A NEW CAP ANGLE REF SRM.

Part: SHROUD — CRACKED (CAPTAIN'S SEAT) · airframe 36,367 hrs · 32,668 cycles

* FLIGHT COMPARTMENT SEATS, CAPTAINS SEAT STRUCTURE PLASTIC SEAT BACK SHROUDS / INBOARD AND OUTBOARD CRACKED , BROKEN. (C-CHECK) RO 12/13/2019 REMOVED AND REPLACED (2) NEW BACKREST ASSEMBLY SHROUD ON CAPTAIN SEAT REF SRM.

Part: SHROUD — CRACKED (F/O SEAT) · airframe 36,367 hrs · 32,668 cycles

* FLIGHT COMPARTMENT SEATS , CO-PILOTS SEAT STRUCTURE PLASTIC SEAT BACK SHROUDS / BOTH INBD AND OUTBOARD ARE CRACKED. (C-CHECK) RO 12/13/2019 REMOVED AND REPLACED (2) NEW BACKREST ASSEMBLY SHROUD PN #1C3076-1AJT AND PN #1C3076-2AJT ON CO-PILOT SEAT REF SRM.

Part: SEAL — CRACKED (WINDSHIELD) · airframe 36,367 hrs · 32,668 cycles

*SEAL AROUND PILOTS WINDSHIELD IS CRACKED AND WIND CHAFED. FLAGGED (C-CHECK) RO 12/13/2019 REPAIRED SEAL AROUND PILOTS WINDSHIELD REF AMM, SEE CONTINUATION CARD FOR DETAILS.

Part: TRUNNION — CRACKED (LT MLG) · airframe 36,367 hrs · 32,668 cycles

WHILE PERFORMING SB 601R-57-046 FOUND CRACK INDICATIONS IN HOLE #20 LH MLG TRUNNION. (C-CHECK) RO 12/13/2019 REPAIRED HOLE 20 LH MLG TRUNNION REF REO, NO MEASURABLE WIEGHT CHANGES NOTED.

Part: DUCT — CRACKED (APU AIR INLET) · airframe 36,367 hrs · 32,668 cycles

* APU UPPER AIR INLET DUCT HAS CRACKED STIFFENER. (C-CHECK) RO 12/13/2019 CLEANED AND WELDED CRACK ON APU UPPER INLET REF. MEGGITT CMM 49-14-01 REPAIR 8-B

Part: WINDOW FRAME — CRACKED (WINDSHIELD) · airframe 36,367 hrs · 32,668 cycles

* R/H WINDSHIELD SIDE POST SUPPORT CRACKED. (C-CHECK) RO 12/13/2019 REMOVED AND INSTALLED NEW RIGHT SIDE POST SUPPORT PN# 601R34032-22 PER REFERENCE DRAWING AND SRM. SEE CONTINUATION CARD FOR DETAILS. LEAK AND OPS CHECKS GOOD.

Part: STRINGER — CRACKED (BS 379) · airframe 36,367 hrs · 32,668 cycles

*STGR 3 L IS CRACKED WHERE IT ATTACHES TO PAX DOOR UPPER SILL/LONGERON AT FS379. (C-CHECK) RO 12/13/2019 CUT OUT DAMAGE STRINGER SECTION OF 3L AT FS 386 APPRX RREF SRM. FABRICATED REPLACEMENT STRINGER SECTION USING S6807 P.O.#62664. REF:SRM. WEIGHT OF REMOVED PART IS .16 LB. WEIGHT OF NEW ADDED PARTS IS .30 LB. TOTAL ADDED WEIGHT IS .14 LB. FABRICATED REPAIR PARTS. INSTALLED ALL REPAIR PARTS AT STR 3L AT FS 379 PER SRM. RESTORED FINISH. REF. THE CONTINUE CARD FOR DETAILED DESCRIPTION OF WORK PERFORMED.

Part: WINDOW FRAME — CRACKED (WINDSHIELD) · airframe 36,367 hrs · 32,668 cycles

* L/H WINDSHIELD SIDE POST SUPPORT CRACKED. (C-CHECK) RO 12/13/2019 REMOVED AND INSTALLED NEW SIDE POST SUPPORT PN# 601R34032-21 PER REFERENCE DRAWING# 601R34032 REV V AND SRM. SEE CONTINUATION CARD FOR DETAILS. LEAK AND OPS CHECKS GOOD.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 36,367 hrs · 32,668 cycles

*PAX DOOR AFT DRAG ANGLE IS CRACKED. FLAGGED (C-CHECK) RO 12/13/2019 REMOVED AND INSTALLED NEW PAX DOOR AFT DRAG ANGLE REF REO. SEE CONTINUE CARD FOR DETAILS.

Part: FRAME — CRACKED (BS 333) · airframe 36,367 hrs · 32,668 cycles

*FRAME ABOVE THE PAX DOOR AT FS333 BETWEEN STGR O AND STGR 1 L IS CRACKED AT TOOLING HOLE. (C-CHECK) RO 12/13/2019 REMOVED AND INSTALLED REPLACEMENT FRAME AT FS333.00 FROM STR0 TO STR1L REF: SRM. SEE CONTINUATION CARD FOR DETAILS.

Part: SEAL — CRACKED (C/P WINDSHIELD) · airframe 36,367 hrs · 32,668 cycles

*SEAL AROUND CO- PILOTS WINDSHIELD IS CRACKED AND WIND CHAFED. FLAGGED (C-CHECK) RO 12/13/2019 REPAIRED AND APPLIED NEW SEALANT AROUND CO-PILOTS WINDSHIELD REF AMM, SEE CONTINUATION CARD FOR DETAILS.

Part: SENSOR — FAILED (WOW) · airframe 33,753 hrs · 29,691 cycles

AFTER TAKE OFF, RECEIVED A NOSE WHEEL STEERING INOPERATIVE, WOW INPUT CAUTION AND WOW OUTPUT FAIL STATUS MESSAGE. NOSE WHEEL STEERING WOULDN'T RE-ARM. ADJUSTED THE NR 2 NLG WOW SENSOR IAW AMM. PERFORMED NLG SWINGS OPS CHECKED GOOD IAW AMM. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: FLOOR SKIN — CRACKED (BS 460) · airframe 32,744 hrs · 28,569 cycles

PRESSURE FLOOR SKIN IS CRACKED AT BS 460, LBL 9 TO BL 0. REPAIRED THE PRESSURE FLOOR SKIN IAW SRM. MAJOR REPAIR. LEAK CHECKED GOOD.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 31,054 hrs · 26,639 cycles

DECLARED EMERGENCY - LAV SMOKE ALARM ON LANDING. SMOKE TOILET CAUTION MESSAGE ON ARRIVAL. NO SMOKE OR FIRE PRESENT. PERFORMED OPERATIONAL TEST OF LAV SMOKE DETECTION SYSTEM IAW AMM. INSPECTED BOTH ENGINES FOR OIL CONTAMINATION IN BLEEDS. NONE FOUND. INSPECTED THE APU FOR OIL CONTAMINATION, RAN BOTH ENGINES AND APU WITH BLEEDS ON. NO SMOKE NOTED. NO TOILET SMOKE MESSAGE RECEIVED. OPS CHECKED GOOD.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 29,137 hrs · 24,574 cycles

LT INBD FLAP VANE L/E SKIN OTBD SECTION CHAFED. R & R LT INBD FLAP VANE L/E SKIN OTBD SECTION IAW SRM AND STS EA.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 29,137 hrs · 24,574 cycles

RT INBD FLAP VANE L/E SKIN CENTER SECTION CHAFED. R & R RT INBD FLAP VANE L/E SKIN CENTER SECTION IAW SRM AND STS EA.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 29,137 hrs · 24,574 cycles

RT INBD FLAP VANE L/E OTBD SKIN SECTION CHAFED. R & R RT INBD FLAP VANE L/E SKIN OTBD SECTION IAW SRM AND STS EA.

Part: SEAT TRACK — CORRODED (BS 364-396) · airframe 29,137 hrs · 24,574 cycles

SEAT TRACK HAS MULTIPLE LOCATIONS OF CORROSION BS 364 -- 396, RBL 9. REMOVED AND INSTALLED NEW SEAT TRACK IAW AMM.

Part: SEAT TRACK — CORRODED (BS 396-409) · airframe 29,137 hrs · 24,574 cycles

SEAT TRACK HAS MULTIPLE LOCATIONS OF CORROSION BS 396 - 409+128, RBL9. INSTALLED NEW SEAT TRACK IAW AMM.

Part: SWITCH — FAILED (PAX DOOR HANDLE) · airframe 27,635 hrs · 23,031 cycles

DURING TAKEOFF ROLL, INBD COOL FAIL STATUS MESSAGE. AFTER WHEELS UP, OVERBOAD COOL CAUTION MESSAGE. QRH AND RETURNED TO DEPARTURE, AFTER LANDING COOL EXHAUST FAIL STATUS. THE STATUS AND CAUTION MESSAGES ALL CLEARED DURING ROLLOUT. TROUBLESHOT ALL 3 MESSAGES; INBD COOL FAIL, OVBD COOL CAUTION, COOL EXHAUST FAIL IAW FIM AND FOUND PASSENGER DOOR OUTER HANDLE SWITCH S102MB TO BE AT FAULT. R & R PAX DOOR OUTER HANDLE SWITCH, S102MB IAW AMM, OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 27,327 hrs · 22,732 cycles

OVERBOARD COOL CAUTION AND INBD COOL FAIL STATUS MESSAGE. INSPECTED WIRING CONNECTIONS FOR PAX DOOR PROXIMITY SWITCHES AND SERVICE DOOR PROXIMITY SWITCHES. FOUND ACCEPTABLE AT THIS TIME COULD NOT DUPLICATE. OPS CHECKED GOOD.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 26,608 hrs · 22,025 cycles

LIGHT COVER FOR MAIN CABIN DOOR EMERGENCY LIGHT MISSING. REPLACED MAIN CABIN DOOR EMERGENCY LIGHT ASSY IAW AMM, PN: BR9279-232.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,502 hrs · 21,920 cycles

SERVICE DOOR FLOOR LEVEL LIGHTED EXIT SIGN HAS AN INOPERATIVE BULB. REPLACED THE BULB IAW AMM.

Part: LINK — GALLED (ENGINE MOUNT) · airframe 26,486 hrs · 21,906 cycles

LEFT ENGINE FWD MOUNT LINK IS GALLED. SERVICE, R & R LT ENGINE FWD MOUNT LINK IAW AMM.

Part: LIGHT — INOPERATIVE (FWD) · airframe 26,451 hrs · 21,870 cycles

FWD EMERGENCY LIGHT INOPERATIVE. REPLACED INOPERATIVE FWD EMERGENCY LIGHT.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,419 hrs · 21,842 cycles

NR 2 LT EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPED IAW AMM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,419 hrs · 21,842 cycles

LT NR 2 EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R THE LAMP IAW AMM.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 26,335 hrs · 21,758 cycles

GALLEY DOOR EXIT SIGN AND FIRST CEILING EMERGENCY OVERHEAD LIGHT DOES NOT ILLUMINATE. R & R MOST FWD EMERGENCY LIGHT BATTERY IAW AMM.

Part: STRUT — LOW (NLG) · airframe 25,894 hrs · 21,345 cycles

GEAR DISAGREE MESSAGE. NLG WOULD NOT COME UP, RAN QRH PROCEDURE. FLT 4550 PERFORMED FULL STRUT SERVICE ON NLG IAW AMM. PERFORMED FUNCTIONAL TESTS OF THE LG EXTENSION & RETRACTION SYS IAW AMM. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,863 hrs · 21,310 cycles

NR 3 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. FLT 4840 RELAMPED.

Part: POST — CRACKED (BS 409) · airframe 26,071 hrs · 21,511 cycles

FOUND FS 409 +128, VERTICAL POST AT BL 0 LT AND RT SIDES HAVE INDICATIONS NOTED AT AFT FLANGE RADIUS AT WL 69.00 APPROXIMATELY .4" IN LENGTH, 60 PERCENT FSH. C-CHECK, REPLACED LT AND RT VERTICAL POSTS IAW SRM AND REO.

Part: POST — CRACKED (FUSELAGE) · airframe 25,874 hrs · 21,324 cycles

FOUND FS 409.00+128 VERTICAL POST AT BL 0.0, LT & RT SIDES, HAVE INDICATIONS NOTED AT FT FLANGE RADIUS AT WL 69.00. APPROXIMATELY 4 INCHES IN LENGTH 60% FSH. C-CHECK INSTALLED NEW LT & RT VERTICAL POSTS IAW SRM & REO.

Part: SILL — CORRODED (PAX DOORWAY) · airframe 26,082 hrs · 21,522 cycles

MAIN CABIN DOOR LOWER SILL ANGLE IS CORRODED AT BS 310 349. C-CHECK, REPLACED MAIN CABIN DOOR LOWER SILL ANGLE IAW SRM AND AMM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 25,775 hrs · 21,226 cycles

WINDSHIELD CTR POST LOWER LT & RT POST FITTINGS ARE CRACKED. C-CHECK REPLACED LT & RT WINDSHIELD CTR POST LOWER FITTINGS WITH NEW POST FITTINGS IAW SRM.

Part: POST — CRACKED (WINDSHIELD) · airframe 26,071 hrs · 21,511 cycles

WINDSHIELD CENTER POST LOWER LT AND RT POST FITTINGS ARE CRACKED. C-CHECK, REPLACED POST IAW SRM.

Part: BULKHEAD — CRACKED · airframe 26,100 hrs · 21,540 cycles

REAR PRESSURE BULKHEAD WEB AT LBL 27.50, WL130 HAS A CRACK INDICATION NOTED APPROXIMATELY 0.3" IN LENGTH 90 PERCENT FSH. C-CHECK, REPAIRED IAW REO.

Part: BULKHEAD — CRACKED · airframe 26,082 hrs · 21,522 cycles

REAR PRESSURE BULKHEAD WEB SURROUNDING THE LINTEL ATTACHMENT FITTING HAS INDICATION NOTED, APPROXIMATELY 0.4" IN LENGTH 100 PERCENT FSH. C-CHECK, REPAIRED IAW REO.

Part: BATTERY — DISCHARGED (CABIN) · airframe 25,470 hrs · 20,932 cycles

OVERHEAD EMERGENCY EXIT SIGN FWD SECTION AT OVER WING EXIT DOES NOT ILLUMINATE. FLT 7378 REPLACED NR 2 & NR 3 EMERGENCY LIGHT BATTERIES IAW AMM. PN 20013-1A, SN ON 96189, SN OFF 70746, PN 2013-1A, SN ON 67792 & SN OFF 55582.

Part: BRAKE — FAILED (MLG) · airframe 23,549 hrs · 19,054 cycles

AT THE START OF THE TAKEOFF ROLL AIRCRAFT VEERED TO THE RIGHT SHARPLY. (FLT 4743) REPLACED NR 3 BRAKE ASSEMBLY IN REFERENCE TO 200 AMM. P/N OFF 5010520-1 S/N OFF APR02-3357

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,069 hrs · 18,550 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4820) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,958 hrs · 18,444 cycles

CEILING EMERGENCY LIGHT BY LAVATORY IS OUT. (FLT 4711) RELAMPED EMERGENCY LIGHT.

Part: BALLAST — DEFECTIVE (LAVATORY) · airframe 22,820 hrs · 18,306 cycles

AN ELECTRICAL SMELL IN LAVORATORY. (FLT 4688) REPLACED LAVORATORY LIGHT BALLAST IN REFERENCE TO AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,756 hrs · 18,235 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4821) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,496 hrs · 17,965 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 7774) RELAMPED EMERGENCY LIGHT.

Part: SKIN — DAMAGED (RT WING) · airframe 22,254 hrs · 17,724 cycles

LIGHTNING STRIKE DAMAGE ON RIGHT LOWER WING PLANK BETWEEN STRINGER 8 AND 9 AT BL11.218 AND ON LOWER FORWARD WING PLANK BETWEEN STRINGER 23 AND 24 AT BL11.14. (SERVICE) REPAIRED LIGHTNING STRIKE DAMAGE PER BOMBARDIER REO.

Part: STRUCTURE — DAMAGED (LT HORIZ STAB) · airframe 22,254 hrs · 17,724 cycles

LIGHTNING STRIKE DAMAGE ON LEFT HORIZONTAL STAB UNDER THE STAB CAP TO REAR SPAR, UPPER SPLICE, AND UPPER ANGLE OUTBOARD OF CLOSING RIB 9. (SERVICE) REPAIRED LIGHTNING STRIKE DAMAGE IAW REO.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 22,254 hrs · 17,724 cycles

LIGHTNING STRIKE DAMAGE ON FUSELAGE SKIN AT FS 734. (SERVICE) DRILLED OUT DAMAGED AREA AND INSTALLED RIVET IAW REO.

Part: SKIN — DENTED (FUSELAGE) · airframe 22,254 hrs · 17,724 cycles

DENT LOCATED ON FUSELAGE BETWEEN FS 409+32 AND FS 409+48, STRINGER 24L AND 25L. (SERVICE) REPAIRED FUSELAGE SKIN BETWEEN FS 409+32 AND FS 409+48, STR 24L AND STR 25L PER REO.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 22,235 hrs · 17,703 cycles

CRACK FOUND AT FS 280 RBL 9. (C-CHECK) REPAIRED CRACK FOUND AT FS 280 RBL 9 IN ACCORDANCE WITH REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,987 hrs · 17,459 cycles

NR 4 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 4622) RELAMPED EMERGENCY LIGHTS.

Part: HYDRAULIC SYSTEM — CONTAMINATED (NR 3) · airframe 21,763 hrs · 17,231 cycles

NR 3 HYDRAULIC LOW PRESSURE WITH GEAR DISAGREE. (FLT 4534) PURGED AIR FROM NR 3 HYDRAULIC SYSTEM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 21,580 hrs · 17,055 cycles

THE 3RD EXTERIOR LEFT OVERWING EMERGENCY LIGHT IS OUT. (FLT 4676) RELAMPED EMERGENCY LIGHT.

Part: DOOR — OUT OF ADJUST (CABIN) · airframe 21,050 hrs · 16,577 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. (FLT 4518) ADJUSTED MAIN CABIN DOOR FORWARD CABLE FULCRUM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,871 hrs · 16,407 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4548) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,499 hrs · 16,087 cycles

AFT CEILING EMERGENCY LIGHT IS OUT. (FLT 4655) RELAMPED EMERGENCY LIGHT.

Part: INVERTER — FAILED (CABIN) · airframe 20,392 hrs · 15,988 cycles

AFT FLOOR CABIN EMERGENCY LIGHTS ARE OUT. (FLT 4591) REPLACED NR 4 INVERTER ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,064 hrs · 14,835 cycles

LAST CABIN EMERGENCY CEILING FLOOR LIGHT BURNED OUT. (FLT 4563) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,226 hrs · 14,108 cycles

LAST OVERHEAD EMERGENCY CEILING LIGHT INOP. (FLT 4444) RELAMPED EMERGENCY LIGHT.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 18,135 hrs · 14,026 cycles

PASSENGER DOOR AFT DRAG ANGLE CRACKED. (C CHECK) REPAIRED PER SRM AND REO.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 18,135 hrs · 14,026 cycles

FS 625 INTERCOSTALS CRACKED. (C CHECK) REPAIRED PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 18,135 hrs · 14,026 cycles

FS 559 PRESSURE BULKHEAD CRACKED. (C CHECK) REPAIRED PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,154 hrs · 13,243 cycles

AFT LEFT EMERGENCY LIGHT INOP. (FLT 4747) RELAMPED EMERGENCY LIGHT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 16,181 hrs · 12,468 cycles

FLT 4634 - RIGHT EXTERNAL EMERGENCY LIGHT INOP. RELAMPED.

Part: DOOR — STIFF (GALLEY) · airframe 15,793 hrs · 12,168 cycles

FLT 4598 - GALLEY SERVICE DOOR IS DIFFICULT TO OPEN FROM OUTSIDE. OPS CHECKS NORMAL.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 15,434 hrs · 11,889 cycles

FLT 4640 - RIGHT WINDSHIELD CRACKED IN CRUISE. REPLACED RIGHT WINDSHIELD.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 14,769 hrs · 11,371 cycles

STA 280 BEAM RBL 12 AFT FACE CRACKED (C-CHECK). REPAIRED PER REO.

Part: FITTING — CRACKED (FUSELAGE) · airframe 14,769 hrs · 11,371 cycles

STATION 280 BEAM LBL 12 AFT FACE LOWER RADIUS AND CLIPS CRACKED (C-CHECK). REPAIRED PER REO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 14,769 hrs · 11,371 cycles

FLOORBEAM AT STA 286 RBL 9 CRACKED (C-CHECK). REPAIRED PER REO.

Part: STRUT — UNDERSERVICED (NLG) · airframe 13,865 hrs · 10,647 cycles

RECEIVED A "GEAR DISAGREE" WARNING MESSAGE AFTER TAKE-OFF, FLIGHT NR 3917. INSPECTED AND SERVICED NOSE STRUT. OPS CHECK GOOD.

Part: DRAIN LINE — LEAKING (HYD SYSTEM) · airframe 13,665 hrs · 10,497 cycles

FLT 5450 - HYDRAULIC SYSTEM NR 2 QUANTITY SHOWED 0 PERCENT. REPAIRED LEAK IN CASE DRAIN LINE IAW 20-22-00. LEAK CHECK GOOD.

Part: HANDLE — DEFECTIVE (SERVICE DOOR) · airframe 13,503 hrs · 10,367 cycles

FLT 3775 - SERVICE DOOR WON'T OPEN OR CLOSE USING OUTER HANDLE. REPLACED SERVICE DOOR OUTER HANDLE ASSEMBLY IAW AMM 52-41-03. OPS CHECK GOOD.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 13,227 hrs · 10,155 cycles

FLOOR EMERGENCY LIGHT STRIP PLUG IS LOOSE, FLIGHT NR 3901. SECURED LIGHT STRIP CONNECTORS. OPS CHECK GOOD.

Part: O-RING — LEAKING (HYD SYSTEM) · airframe 11,357 hrs · 8,733 cycles

ON TAXI OUT IN SLC, LOST ALL HYDRAULIC FLUID IN SYSTEM NR 2. RETURNED TO GATE. REPLACED O-RING ON PRESSURE SIDE OF MLG EMERGENCY EXTENSION VALVE. OPS AND LEAK CHECK GOOD.

Part: SENSOR — MALFUNCTIONED (TE FLAPS) · airframe 9,530 hrs · 7,381 cycles

FLAPS FAIL CAUTION MESSAGE EN ROUTE TO SLC. REPLACED LEFT BPSU IAW MM 27-51-00. OPERATIONAL CHECKS GOOD.

Part: FCU — OUT OF ADJUST (TE FLAPS) · airframe 9,463 hrs · 7,332 cycles

FLAPS FAIL MESSAGE AT FLAPS 45 DEGREES, RETURNED TO FIELD. RERIGGED BOTH BPSU'S AND FECU POT'S IAW MM 27-51-10-220-005. OPERATIONAL CHECKS GOOD.

Part: FITTING — CRACKED (FUSELAGE) · airframe 9,324 hrs · 7,230 cycles

LEFT SIDE STA 484 CLIP CRACKED (LBL36), DISCOVERED DURING C-CHECK INSPECTION. INSTALLED FABRICATED PART 601R-53-41-059-1 REPAIR ANGLE IAW REO 601R-53-41-059.

Part: FITTING — CRACKED (FUSELAGE) · airframe 9,324 hrs · 7,230 cycles

RT AT STA 621 CLIP CRACKED AT FLOOR LEVEL, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS 601R-53-61-117C -1; -3; -5 PER REO 601R-53-61-117C AND SRM 51-421-06 PGS 1-13 AND SRM 51-42-21 PG 1;13;17.

Part: FITTING — CRACKED (FUSELAGE) · airframe 9,324 hrs · 7,230 cycles

LT STA 621 CLIP CRACKED AT FLOOR LEVEL, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS PER REO 601R 53-61-117.

Part: FITTING — CRACKED (FUSELAGE) · airframe 9,324 hrs · 7,230 cycles

LT 625 CLIP CRACKED RIB 13, DISCOVERED DURING C-CHECK INSPECTION. REPLACED LT STA 625 CLIP; RIB 13 PER SRM 51-42-06 PG 4 AND RII 53-401.

Part: WEB — CRACKED (PAX DOOR) · airframe 9,324 hrs · 7,230 cycles

PAX DOOR AFT WEB CRACKED UNDER HANDRAIL SUPPORT BRACKET, DISCOVERED DURING C-CHECK INSPECTION. REPAIRED PAX DOOR AFT WEB UNDER HANDRAIL SUPPORT BRACKET PER REO 601R 52-11-702, P/N 52-11-702-2 AND -3.

Part: FITTING — CRACKED (FUSELAGE) · airframe 9,324 hrs · 7,230 cycles

RIGHT SIDE STA 484 CLIP CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED CLIP AT STA 484 RBL 27 WITH NEW PER REO 601R-53-41-059.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 9,324 hrs · 7,230 cycles

UPPER FLOOR SUPPORT ANGLE AT FS 280; APROX. LBL 12 CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS AT STA 280 LBL9/LBL12 PER REO 601R 53-11-138 NOTE 1 AND RII 53-401.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 9,324 hrs · 7,230 cycles

PAX DOOR HANDLE CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW PAX DOOR HANDLE 601R 31763-1 PO NR 66207-8 PER CRJ200 AMM 52-11-03-000-802/400-802. OPERATIONAL CHECKS GOOD.

Part: FITTING — CRACKED (FUSELAGE) · airframe 9,324 hrs · 7,230 cycles

LT I/B CLIP CRACKED AT FS 280 LBL 9, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP PER CRJ200 SRM 51-42-21 PG 9/51-42-06 AND RII 53-401 REV 22.

Part: FITTING — CRACKED (FUSELAGE) · airframe 9,324 hrs · 7,230 cycles

RT STA 625 CLIP CRACKED RIB 13, DISCOVERED DURING C-CHECK INSPECTION. REPLACED RT STA 625 CLIP; RIB 13 PER SRM 51-42-06 PG 4 AND RII 53-401.

Part: WEB — CRACKED (PAX DOOR) · airframe 9,324 hrs · 7,230 cycles

FWD PAX DOOR WEB CRACKED UNDER HANDRAIL SUPPORT FITTING, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED FABRICATED PART 601R 52-11-702-2 AND -3 PER REO 601R-52-11-702.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 9,324 hrs · 7,230 cycles

LEFT SIDE STA 484 BRACKET CRACKED (LBL 27), DISCOVERED DURING C-CHECK INSPECTION. REPLACED CLIP P/N NR 601R-31171-9 AT STA 484 LBL 27 IAW REO NR 601R-53-41-059 AND RII 53-401.

Part: TRIM SWITCH — INOPERATIVE · airframe 8,099 hrs · 6,307 cycles

FO TRIM SWTICH INOP. REPLACED FO TRIM SWTICH IAW 27-41-05, OPERATIONAL CHECK GOOD.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 7,272 hrs · 5,693 cycles

CARGO SMOKE AURAL AND MESSAGE AT THE GATE. REPLACED CARGO COMPARTMENT FORWARD DETECTOR IAW MM 26-15-01. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB TRIM) · airframe 5,702 hrs · 4,458 cycles

BOTH STAB TRIMS DISENGAGED EN ROUTE. REPLACED HSTCU IAW MM 27-41-01. OPERATIONAL CHECK GOOD.

Part: CONTROL SYSTEM — MALFUNCTIONED (HORIZ STAB TRIM) · airframe 5,359 hrs · 4,189 cycles

STAB TRIM CH 1 KICKED OFF DURING FLIGHT. REPLACED HSTCU PER CRJ MM 27-41-00. OPERATIONAL CHECK GOOD.

Part: WINDOW — CRACKED (COCKPIT) · airframe 5,359 hrs · 4,189 cycles

DURING DESCENT, FO'S SIDE WINDOW CRACKED. REPLACED FO'S SIDE WINDOW IAW AMM 56-12-01. OPERATIONAL CHECK GOOD, P/N: NP-139322-10 S/N OFF: 03051H6864

Part: CLIP — CRACKED (FUSELAGE) · airframe 4,541 hrs · 3,540 cycles

FUSELAGE FLOORBEAM TO TRANSVERSE BEAM ATTACH CLIP IS CRACKED; FS 280.00, LBL 9.0 OUTBOARD CLIP. ITEM FOUND AT C-CHECK INSPECTION. CLIP REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-25-16, AND 51-21-11.

Part: CLIP — CRACKED (FUSELAGE) · airframe 4,541 hrs · 3,540 cycles

FUSELAGE FLOORBEAM TO TRANSVERSE BEAM ATTACH CLIPS ARE CRACKED; FS 280.00, RBL 9.0 INBOARD AND OUTBOARD CLIPS. ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIPS IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-25-16, 51-21-11.

Part: COMPUTER — FAULTY (AUTOPILOT SYS) · airframe 2,175 hrs · 1,695 cycles

AFTER SELECTING A NEW HEADING WHILE IN HDG MODE, THE A/C CONTINUED TURNING THROUGH THE NEW HEADING (OPPOSITE THE FLIGHT DIRECTOR COMMANDS) AND THEN JERKED SUDDENLY TO THE LEFT TWICE. THE A/P DISCONNECTED ON ITS OWN. REMOVED AND REPLACED FCC NR 1 IAW MM 22-12-1A. OP CHECKS GOOD. P/N 622-9815-704, S/N ON 642, S/N OFF 13N2T.

Part: MANIFOLD — MALFUNCTIONED (GROUND SPOILERS) · airframe 1,386 hrs · 1,100 cycles

INBOARD GROUND SPOILERS WILL NOT RETRACT AFTER LANDING. REMOVED AND REPLACED GROUND SPOILER MANIFOLD IAW MM 27-63-00. OPS AND LEAK CHECK GOOD. P/N: 60175124-, S/N OFF: 1193.

Part: CONTROL PANEL — INOPERATIVE (RUDDER TRIM) · airframe 1,242 hrs · 990 cycles

RUDDER TRIM IS INOPERATIVE, SWITCH WILL TRIM NOSE RT BUT WILL NOT TRIM NOSE LT. REMOVED AND REPLACED RUDDER/AILERON TRIM PANEL WITH SERVICEABLE UNIT IAW MM 27-12-10. OPS CHECK GOOD.

Part: CONNECTOR — DISCONNECTED (NLG DOOR) · airframe 947 hrs · 764 cycles

RETRACTED GEAR AFTER TAKEOFF AND NOSE GEAR DOOR AURAL WARNING SOUNDED. RETURNED TO DFW. FOUND CANNON PLUG FOR NOSE DOOR SELECTOR VALVE DISCONNECTED. RECONNECTED CANNON PLUG. OPS CHECK GOOD IAW MM 33-22-20.

Part: CONTROL HANDLE — MALFUNCTIONED (COCKPIT) · airframe 548 hrs · 456 cycles

AFTER LANDING FLAPS FAILED WITH A 'FLAPS FAIL' CAUTION ON ED1. REMOVED AND REPLACED FLAP CONTROL HANDLE IAW MM 27-51-01 OPS CHECK GOOD.