N460SW
Registered owner: SKYWEST AIRLINES INC, UT (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
ON APPROACH TO RWY 22L, WE SELECTED FLAPS 45. WE RECEIVED FLAPS FAIL. WE EXECUTED A GO-AROUND. WE NEVER UTILIZED GO-AROUND THRUST SINCE IT WAS EXECUTED AT OVER 1000 FT. WE PERFORMED ALL CHECKLISTS TO INCLUDE QRH (FLAPS FAIL CHECKLIST) AND APPLICABLE DOCUMENTATION.WE LANDED AT 38,000 POUNDS AND LESS THAN 350 FPM AT ORD. (FLIGHT 3911 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 82505 WITH THE FOLLOWING CORRECTIVE ACTION: "REFERENCE CP 82511 FOR TROUBLESHOOTING OF FLAPS FAIL CAUTION AND REMOVAL OF THE RH BPSU. REFERENCE CP 82512 FOR INSTALLATION OF THE RH BPSU, OPS CHECKS AND PARTS INFO. REFERENCE CP 82510 FOR COMPLETION OF FLAP FAIL AD 2009-06-12/09. "
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.
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. -.
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.
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.
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,
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
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.
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.
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.
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.
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
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.
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.
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.
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.
* 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
* 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.
* 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
* 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
* 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.
**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.
*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.
*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
* 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.
* 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.
* 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.
* 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.
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
* 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
* 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
* 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.
* 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
* 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.
* 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.
* 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.
* 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.
* 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.
*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.
*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.
*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.
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.
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.
*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.
*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.
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.
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.
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.
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.
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.
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.
SEAT TRACK HAS MULTIPLE LOCATIONS OF CORROSION BS 364 -- 396, RBL 9. REMOVED AND INSTALLED NEW SEAT TRACK IAW AMM.
SEAT TRACK HAS MULTIPLE LOCATIONS OF CORROSION BS 396 - 409+128, RBL9. INSTALLED NEW SEAT TRACK IAW AMM.
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.
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.
LIGHT COVER FOR MAIN CABIN DOOR EMERGENCY LIGHT MISSING. REPLACED MAIN CABIN DOOR EMERGENCY LIGHT ASSY IAW AMM, PN: BR9279-232.
SERVICE DOOR FLOOR LEVEL LIGHTED EXIT SIGN HAS AN INOPERATIVE BULB. REPLACED THE BULB IAW AMM.
LEFT ENGINE FWD MOUNT LINK IS GALLED. SERVICE, R & R LT ENGINE FWD MOUNT LINK IAW AMM.
FWD EMERGENCY LIGHT INOPERATIVE. REPLACED INOPERATIVE FWD EMERGENCY LIGHT.
NR 2 LT EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPED IAW AMM.
LT NR 2 EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R THE LAMP IAW AMM.
GALLEY DOOR EXIT SIGN AND FIRST CEILING EMERGENCY OVERHEAD LIGHT DOES NOT ILLUMINATE. R & R MOST FWD EMERGENCY LIGHT BATTERY IAW AMM.
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.
NR 3 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. FLT 4840 RELAMPED.
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.
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.
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.
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.
WINDSHIELD CENTER POST LOWER LT AND RT POST FITTINGS ARE CRACKED. C-CHECK, REPLACED POST IAW SRM.
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.
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.
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.
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
NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4820) RELAMPED EMERGENCY LIGHT.
CEILING EMERGENCY LIGHT BY LAVATORY IS OUT. (FLT 4711) RELAMPED EMERGENCY LIGHT.
AN ELECTRICAL SMELL IN LAVORATORY. (FLT 4688) REPLACED LAVORATORY LIGHT BALLAST IN REFERENCE TO AMM.
NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4821) RELAMPED EMERGENCY LIGHT.
AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 7774) RELAMPED EMERGENCY LIGHT.
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.
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.
LIGHTNING STRIKE DAMAGE ON FUSELAGE SKIN AT FS 734. (SERVICE) DRILLED OUT DAMAGED AREA AND INSTALLED RIVET IAW REO.
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.
CRACK FOUND AT FS 280 RBL 9. (C-CHECK) REPAIRED CRACK FOUND AT FS 280 RBL 9 IN ACCORDANCE WITH REO.
NR 4 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 4622) RELAMPED EMERGENCY LIGHTS.
NR 3 HYDRAULIC LOW PRESSURE WITH GEAR DISAGREE. (FLT 4534) PURGED AIR FROM NR 3 HYDRAULIC SYSTEM.
THE 3RD EXTERIOR LEFT OVERWING EMERGENCY LIGHT IS OUT. (FLT 4676) RELAMPED EMERGENCY LIGHT.
MAIN CABIN DOOR DIFFICULT TO OPEN. (FLT 4518) ADJUSTED MAIN CABIN DOOR FORWARD CABLE FULCRUM.
AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4548) RELAMPED EMERGENCY LIGHT.
AFT CEILING EMERGENCY LIGHT IS OUT. (FLT 4655) RELAMPED EMERGENCY LIGHT.
AFT FLOOR CABIN EMERGENCY LIGHTS ARE OUT. (FLT 4591) REPLACED NR 4 INVERTER ASSEMBLY.
LAST CABIN EMERGENCY CEILING FLOOR LIGHT BURNED OUT. (FLT 4563) RELAMPED EMERGENCY LIGHT.
LAST OVERHEAD EMERGENCY CEILING LIGHT INOP. (FLT 4444) RELAMPED EMERGENCY LIGHT.
FS 625 INTERCOSTALS CRACKED. (C CHECK) REPAIRED PER SRM.
FS 559 PRESSURE BULKHEAD CRACKED. (C CHECK) REPAIRED PER REO.
PASSENGER DOOR AFT DRAG ANGLE CRACKED. (C CHECK) REPAIRED PER SRM AND REO.
AFT LEFT EMERGENCY LIGHT INOP. (FLT 4747) RELAMPED EMERGENCY LIGHT.
FLT 4634 - RIGHT EXTERNAL EMERGENCY LIGHT INOP. RELAMPED.
FLT 4598 - GALLEY SERVICE DOOR IS DIFFICULT TO OPEN FROM OUTSIDE. OPS CHECKS NORMAL.
FLT 4640 - RIGHT WINDSHIELD CRACKED IN CRUISE. REPLACED RIGHT WINDSHIELD.
STA 280 BEAM RBL 12 AFT FACE CRACKED (C-CHECK). REPAIRED PER REO.
STATION 280 BEAM LBL 12 AFT FACE LOWER RADIUS AND CLIPS CRACKED (C-CHECK). REPAIRED PER REO.
FLOORBEAM AT STA 286 RBL 9 CRACKED (C-CHECK). REPAIRED PER REO.
RECEIVED A "GEAR DISAGREE" WARNING MESSAGE AFTER TAKE-OFF, FLIGHT NR 3917. INSPECTED AND SERVICED NOSE STRUT. OPS CHECK GOOD.
FLT 5450 - HYDRAULIC SYSTEM NR 2 QUANTITY SHOWED 0 PERCENT. REPAIRED LEAK IN CASE DRAIN LINE IAW 20-22-00. LEAK CHECK GOOD.
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.
FLOOR EMERGENCY LIGHT STRIP PLUG IS LOOSE, FLIGHT NR 3901. SECURED LIGHT STRIP CONNECTORS. OPS CHECK GOOD.
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.
FLAPS FAIL CAUTION MESSAGE EN ROUTE TO SLC. REPLACED LEFT BPSU IAW MM 27-51-00. OPERATIONAL CHECKS GOOD.
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.
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.
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.
LT STA 621 CLIP CRACKED AT FLOOR LEVEL, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS PER REO 601R 53-61-117.
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.
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.
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.
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.
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.
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.
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.
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.
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.
FO TRIM SWTICH INOP. REPLACED FO TRIM SWTICH IAW 27-41-05, OPERATIONAL CHECK GOOD.
CARGO SMOKE AURAL AND MESSAGE AT THE GATE. REPLACED CARGO COMPARTMENT FORWARD DETECTOR IAW MM 26-15-01. OPERATIONAL CHECK GOOD.
BOTH STAB TRIMS DISENGAGED EN ROUTE. REPLACED HSTCU IAW MM 27-41-01. OPERATIONAL CHECK GOOD.
STAB TRIM CH 1 KICKED OFF DURING FLIGHT. REPLACED HSTCU PER CRJ MM 27-41-00. OPERATIONAL CHECK GOOD.
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
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.
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.
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.
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.
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.
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.
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.