N971SW
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
LEFT FLAP HINGE BOX (WS178.00), AFT INBOARD LOWER FLANGE GOUGED (NEAR LUG HOLE). OPEN
FA REPORTED A BURNING RUBBER ODORL ON CLIMB OUT OF CHA. ODOR WENT AWAY AFTER APPROX 10 MINS. NO SMOKE OR OTHER INDICATIONS. MEL 21-40-1ACAT C. (FLIGHT 5660) TROUBLESHOT SMOKE SMELL IN CABIN IN REF TO FIM 21-21-00. FA REPORTS SMOKE CAME FROM FWD GALLEY. PERFORMED OPS CHK OF GALLEY HEATER IN REF TO AMM 21-23-05. FOUND SMOKE SMELL TO BE COMING FROM GALLEY FAN AND FAN GOES INOP WITHIN 5SEC. PLACED GALLEY HEATER SYSTEM ON DEFERRAL IN REF TO CRJ200 MEL21-40-1A. MX ACTIONS COMPLIED WITH, GALLEY HEATER DEACTIVATED, PLACARDS INSTALLED, R & R GALLEY VENTILATION FAN IAW AMM 21-23-07. OPS CHECK GOOD, NO ODOR. DMI CLEARED PLACARDS REMOVED.
R REV UNLOCKED CAUTION MESSAGE DURING CLIMB. LEVELED AT 17,000?, RAN QRH. QRH RESOLVED MESSAGE WITH EMER STOW.MEL 78-30-1CAT "C" REF AML 1805384: SMOD APPROVED IS REQUIRED DUE TO ODI (RTF)(FLIGHT 5128) RT THRUST REVERSER PER MEL 78-30-1. DUE TO NATURE OF FAULT & RESULTING QRH RESOLVING ISSUE, SUSPECT POSSIBLE PDU MOTOR BRAKE FAILURE. R & R RT T/R PDU IAW AMM 78-32-03. MANUALLY RAN RT T/R ACTUATING SYSTEM THROUGH FULL RANGE OF MOTION, NO DISCREPANCIES NOTED, ALL EICAS INDICATIONS NORMAL IN ALL STAGES OF TRAVEL. REFERENCE CP 31607246 FOR MICROSWITCH REPLACEMENTS & RIGGING. REFERENCE CP 31607247 FOR OPS CHECK OF RT T/R SYSTEM (PER MIP 78-440-1002-SKY) OPS CHECK GOOD.
ATC ADVISED US WE HAD BLOWN A TIRE DEPARTING RUNWAY 8. RETURNED TO DENVER. TIRES REPORTED NORMAL BY EMERGENCY VEHICLES. TIRES NEED INSPECTION PLEASE (FLIGHT 5031 FILED CLOSED)VERIFIED AND CONFIRMED THIS AIRCRAFT IS NOT THE AIRCRAFT WITH THE BLOWN TIRE EVENT. PERFORMED INSPECTION OF MAIN WHEEL AND TIRE ASSEMBLIES PER CRJ-200 AMM 32-41-01. NO DEFECTS NOTED. PERFORMED INSPECTION OF NOSE WHEEL AND TIRE ASSEMBLIES PER CRJ-200 AMM 32-42-01. NO DEFECTS NOTED. VERIFIED ALL TIRE PRESSURES ARE WITHIN LIMITS PER CRJ-200 AMM 12-12-32 AND FORM M-76. A/C IS OK FOR SERVICE.
RH FUSELAGE DRAG ANGLE NEAR DATUM 61.5625% WAS MIS-DRILLED. FABRICATE A NEW RH DRAG ANGLE (C-CHECK RO 7/23/2023) REMOVED & INSTALLED NEWLY FABRICATED RH FUSELAGE DRAG ANGLE REPAIR SECTION NEAR DATUM 61.5625% REF CRJ 200 SRM 51-42-21 ,CRJ 200 SRM 51-42-22 AND DWG# CC600-21117 REV - J AND MHIRJ REO 601R-55-31-445 REV-- DATED 2023-07-04 SEE CONTINUE CARD FOR DETAILED, OPS CHECKS GOOD. COMPLIED WITH 51-900-1003-SKY
FOUND DOUBLE HOLE ON THE LH FUSELAGE DRAG ANGLE NEAR DATUM 61.5625% (C-CHECK RO 7/23/2023) REPLACED AND PERFORMED REPAIR TO LH FUSELAGE DRAG ANGLE NEAR DATUM 61.5625%. PERFORMED AND COMPLIED WITH ALL STEPS OF REO 601R-55-31-445 REV -- DATED 2023-07-04. COMPLIED WITH TASK CARD 51-900-1003-SKY.
EVALUATE GOUGE/SCRATCH INSIDE LH WING FUEL BAY UNDER PANEL 540CB, FWD SIDE, ON LOWER WING PLANK STRINGER BETWEEN WS85.50 - WS65.75, STGR 15 (C-CHECK RO 7/23/2023) BLENDED GOUGE/SCRATCH INSIDE LH WING FUEL BAY UNDER PANEL 540CB FWD SIDE ON LOWER WING PLANK STRINGER BETWEEN WS85.50 - WS65.75 AT STR 15. REF CRJ200 SRM 51-12-00. PERFORMED AND COMPLIED WITH ALL STEPS OF REO 601R-57-21-3769 REV -- DATED 2023-06-28. COMPLIED WITH TASK CARD 51-900-1003-SKY. -NO WEIGHT CHANGE, BLEND ONLY-
VERITCAL STAB REAR SPAR AS A GOUGE WITH RAISED METAL ON THE RH TRAILING EDGE (MARKED). (C-CHECK RO 7/23/2023) REPAIRED VERTICAL STAB REAR SPAR GOUGE TO MHIRJ REO 601R-55-31-448 REV -- DATED 2023-06-20COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY (CL600-2B19) STRUCTURAL MAJOR REPAIR COMPLIED WITH SKYWEST FORM M-337
*R/H PRESSURE FLOOR SILL HAS 2EA AREAS OF CORROSION AT APPROX FS424 AND FS529. (C-CHECK RO 7/23/2023) BLENDED OUT CORROSION AT 2EA LOCATIONS ON RH PRESSURE FLOOR SILL AT F.S. 424.00 AND F.S. 554.00. CORROSION AT F.S. 554.00 WAS FOUND WITHIN LIMITS OF GREO 601R-53-41-666 REV -C DATED 2012-11-06CORROSION AT F.S. 424.00 WAS REPAIRED TO REO 601R-53-41-3176 REV -- DATED 2023-06-14COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY (CL600-2B19) STRUCTURAL MAJOR REPAIRCOMPLIED WITH SKYWEST FORM M-337. LEAK CHECK GOOD.
*FLOOR SUPPORT STRAP AT FS559 BETWEEN FLOOR BEAM AT LBL27 AND PRESSURE FLOOR SILL IS CORRODED. (C-CHECK RO 7/23/2023) REMOVED AND REPLACED THE FLOOR SUPPORT STRAP AT FS 559 BETWEEN LBL 27 AND THE PRESSURE FLOOR SILL REF DRAWING 601R31025 REV: N, CRJ 200 SRM 51-42-06 AND 51-42-15. COMPLIED WITH 51-900-1003-SKY
CARGO COMPARTMENT FS621 BULKHEAD FLOOR SUPPORT ANGLE BETWEEN RH FLOOR SILL AND RBL27.00 HAS CORROSION (MARKED) (C-CHECK RO 7/23/2023) REMOVED AND REPLACED CARGO COMPARTMENT FS621 BULKHEAD FLOOR SUPPORT ANGLE BETWEEN RH FLOOR SILL AND RBL27.00 REF. CRJ200 SRM 51--42-06, CRJ200 SRM 51-42-21 AND REO 601R-53-61-117 REV -D DATE 2017-02-26 STEPS 5 AND 8.SEE CONTINUATION CARD FOR DETAILS
*CLIP ANGLE IN ATF ACCESSORY COMPARTMENT ATTACHING INTERCOSTAL TO FRAME AT FS625, STGR 14L IS CRACKED. (C-CHECK RO 7/23/2023) REMOVED AND REPLACED CRACKED CLIP ANGLE IN AFT ACCESSORY COMPARTMENT ATTACHING INTERCOSTAL TO FRAME AT FS 625 & STGR 14L REF CRJ200 SRM 51-42-21 & DWG 601-35012 REV -D. SEE CONTINUE CARD FOR DETAILS. ALL STEPS OF TASK CARD 51-900-1003-SKY COMPLIED WITH.
*FRAME ABOVE PAX DOOR AT FS333 IS CRACKED. (C-CHECK RO 7/23/2023) REMOVED AND INSTALLED NEW FRAME AND ALL REPAIR PARTS WET WITH SEALANT PER REO 601R-53-21-3636 REV -- DATED 2023/06/17.LEAK CHECK GOOD.SEE CONTINUATION CARD FOR DETAILS.COMPLIED WITH TASK 51-900-1003-SKY
PAX DOOR SILL ANGLE IS CORRODED. FLAGGED (C-CHECK RO 7/23/2023) CORROSION ON PAX DOOR SILL ANGLE FOUND TO BE OUT OF LIMITS DUE TO 100% MATERIAL LOSS. REMOVED DAMAGE SILL ANGLE. LOCATED DRILLED AND INSTALLED NEW PAX DOOR SILL ANGLE. REF CRJ-200 SRM 51-42-06, CRJ-200 SRM 51-42-21 AND DWG 601R31527 REV. AM.
PAX DOOR AFT HAND RAIL CUP CORRODED. FLAGGED (C-CHECK RO 7/23/2023) REMOVED AND REPLACED PAX DOOR AFT HAND RAIL CUP WITH NEW, REF CRJ 200 SRM 51-42-06 AND DWG 601R31527 REV AMCOMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY (CL600-2B19)COMPLIED WITH SKYWEST FORM M-337
PAX DOOR FWD HAND RAIL CUP CORRODED. FLAGGED (C-CHECK RO 7/23/2023) REMOVED AND REPLACED PAX DOOR FWD HAND RAIL CUP WITH NEW, REF CRJ 200 SRM 51-42-06 AND DWG 601R31527 REV AMCOMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY (CL600-2B19)COMPLIED WITH SKYWEST FORM M-337
R/H SIDE INBOARD FLAP CENTER LOWER SKIN HAS DENT (MARKED) (C-CHECK RO 7/23/2023) REPAIRED DENT ON R/H I/B FLAP LOWER SKIN REF CRJ 200 SRM 57-52-00, REPAIR #3, FIGURE 202. COMPLIED FULLY W/SKYCARD 51-900-1003-SKY.
*PILOTS WINDSHEILD SIDE POST LOWER SUPPORT STUCTURE IS CRACKED (MARKED) (C-CHECK RO 7/23/2023) REMOVED AND INSTALLED NEW PILOT'S WINDSHIELD SIDE POST LOWER SUPPORT STRUCTURE ANGLE PER CRJ 200 SRM 51-42-06 AND DRAWING 601R34032 REV -U, LEAK CHECK GOOD.COMPLIED WITH TASK 51-900-1003-SKY
POSSIBLE CRACKED CLIP AT L/H APPROX. FS280 STGR3. FLAGGED (C-CHECK RO 7/23/2023) REMOVED AND INSTALLED 2EA ANGLES AND 1EA CLIP AT APPROX. FS 280 AND STGR 3L REF CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-21 AND DWG# SH600-31057 REV-P. COMPLIED WITH TASK CARD 51-900-1003-SKY AND M-337 FORMPRESSURE CHECK GOOD
*CO-PILOTS WINDSHEILD SIDE POST LOWER SUPPORT STUCTURE IS CRACKED (MARKED) (C-CHECK RO 7/23/2023) REPLACED LOWER SUPPORT ANGLE AT CO-PILOT WINDSHIELD SIDE POST. PER CRJ200 SRM 51-42-06 AND BOMBARDIER DWG 601R34032 REV. V. ALL CHECKS GOOD.
LH ELEVATOR FRONT SPAR CENTER HINGE FITTING OUTBOARD FLUTTER DAMPER LUG RADIUS GOUGED (MARKED) (C-CHECK RO 7/23/2023) REPAIRED THE LH ELEVATOR FRONT SPAR CENTER HINGE FITTING INBOARD FLUTTER DAMPER LUG RADIUS REF REO 601R-55-21-582, REV-A, DATED 2023-06-23. FOUND TO BE WITHIN LIMITS. SEE CONTINUE CARD FOR DETAILS ON WORK PERFORMED. COMPLIED WITH TASK 51-900-1003-SKY
PAX DOOR, INTERCOSTAL INSIDE THE PRESSURE VALVE CUTOUT APPEARS TO BE CORRODED. (MARKED & FLAGGED) (C-CHECK RO 7/23/2023) REMOVED AND INSTALLED NEW PAX DOOR INTERCOSTAL DD4 FS320.00 - FS338.00. REF: CRJ-200 SRM 51-42-06, CRJ-200 SRM 51-42-21, AND DRAWING 601R31702 REV N, LEAK CHECK GOOD.COMPLIED WITH TASK 51-900-1003-SKY
CARGO DOOR FORWARD DOOR TRACK SUPPORT "CHANNEL" IS BENT . FS574.00. (MARKED) (C-CHECK RO 7/23/2023) REMOVED AND REPLACED CARGO DOOR FWD DOOR TRACK SUPPORT [email protected] WITH A NEW ON PER DWG 601R35050 REV AC AND CRJ 200 SRM 51-42-06. SEE CONTINUATION CARD FOR DETAILSCOMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY (CL600-2B19) STRUCTURAL MAJOR REPAIR COMPLIED WITH SKYWEST FORM M-337
LEFT CENTER WING LOWER SKIN IS CHAFED AT THE OUTBOARD AFT END. (MARKED) (C-CHECK RO 7/23/2023) BLENDED LH CENTER WING LOWER SKIN AT OUTBD AFT END. REF CRJ200 SRM 51-12-00. FOUND TO BE OUT OF LIMITS. PERFORMED AND COMPLIED WITH ALL STEPS OF GREO 601R-57-21-880 REV -D DATED 2017-03-06. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. NO WEIGHT CHANGE, BLEND OUT ONLY.
POSSIBLE CRACK ON INTERCOSTAL FOR AC EXTERNAL POWER RECEPTACLE (MARKED) (C-CHECK RO 7/23/2023) REMOVED AND REPLACED THE INTERCOSTAL FOR THE AC EXTERNAL POWER RECEPTACLE, REF CRJ 200 SRM 51-42-06, 51-42-21, AND DRAWING #600-33283 REV -F. ENERGIZED THE EXTERNAL AC SYSTEM IN THE EXTERNAL SERVICE CONFIGURATION, REF CRJ 200 AMM 24-41-00-861-801, NO DEFECTS NOTED.COMPLIED TASK 51-900-1003-SKY
FOUND DOUBLE HOLE ON TAIL CONE 361AL (MARKED) (C-CHECK RO 7/23/2023) REPAIRED DOUBLE HOLES IN TAILCONE PANEL 361AL PER MHIRJ REO 601R-53-84-335 REV -- DATED 07-10-2023, SEE CONTINUE CARD FOR DETAILS OF REO REPAIR.COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY (CL600-2B19) STRUCTURAL MAJOR REPAIRCOMPLIED WITH SKYWEST FORM M-337
AFT BAGGAGE BAY EXTERIOR DOOR HAS A GOUGE ALONG THE TOP, CENTER OF THE DOOR ON A PREVIOUS REPAIR. FLAGGED (C-CHECK RO 7/23/2023) BLENDED AREA ON AFT BAGGAGE BAY EXTERIOR DOOR ALONG THE TOP, CENTER OF THE DOOR ON A PREVIOUS REPAIR. REF CRJ200 SRM 51-12-00 ORIGINAL THICKNESS: 0.100", REMAINING THICKNESS: 0.087", DAMAGE LIMITS NOT AVAILABLE FOR AIRCRAFT SPECIFIC REPAIR DOUBLER INSTALLED, DAMAGE IS OUT OF LIMITS. REF REO 601R-52-31-156 REV: -- DATED: 2011-06-24 INSTALLED THE NEW DOUBLER REF CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-21 WITH REO 601R-52-31-156 REV: -- DATED: 2011-06-24. COMLPIED WITH SKYWEST TASK CARD 51-900-1003-SKY
FLAPS FAIL AT 0 DEGREES DURING CLIMB OUT. RAN QRH. PER THE QRH, OUR MAX LANDING WEIGHT (LIMITED BY MAXIMUM TIRE SPEED) WAS 37,000 LBS. OUR ZFW WAS 42,692, AND WE LANDED AT ABOUT 45,000 LBS. NORMAL LANDING. (FLT 5291, FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 26637396 WITH THE FOLLOWING CORRECTIVE ACTION: "SEE CP26637473 FOR FULL FLAP EVALUATION AD COMPLIANCE. SEE CP 26640016 FOR REPLACMENT OF LH BPSU. SEE CP 26637602 FOR FDR DOWNLOAD TO VERIFY VERTICAL SPEED AT LANDING. FOUND VERTICAL SPEED AT TOUCHDOWN TO BE WITHIN ACCEPTABLE RANGE, NO INSPECTION REQUIRED. AFTER REPLACMENT OF LH BPSU PERFORMED OPS CHECK OF FLAPS WITH REFERENCE TO AMM 27-54-00. OPS CHECK GOOD AT THIS TIME,"
PASSENGER DOOR INNER HANDLE MOUNTING ASSY BRACKET BROKEN ON INBD SIDE. (FILED - CLOSED) REMOVED PASSENGER DOOR INNER HANDLE MOUNTING ASSEMBLY AFT ANGLE IN REFERENCE TO SRM 51-42-06. SEE CP 24257171 FOR INSTALLATION OF PAX DOOR INNER HANDLE AFT ANGLE BRACKET
CRACKED RH WINDSHIELD, DIVERTED TO DEN. DECLARED EMERGENCY. / NO OVERWEIGHT LANDING (FLIGHT 4682 - FILED CLOSED) REMOVED AND REPLACED RH WINDSHIELD IN PER SKYWEST TASK CARD 56-220-1000-SKY.
POP SOUND AT IDLE AT 14000 FEET. RIGHT ENGINE LO PRESS WARNING AND HIGH ITT. ENGINE SHUTDOWN INFLIGHT PERFORMED. FLIGHT 4676 REFERENCE AML 604626 REFERENCE AML 604683 REFERENCE AML 604711, AML 606556, FOR WORK PERFORMED. RIGHT ENGINE FUEL CONTROL REMOVED AND REPLACED, RIGHT FUEL PUMP REMOVED AND REPLACED. THROTTLE CABLE AT GEAR BOX REPLACED WITH CORRECT CABLE. 10TH STAGE BLEED CHECK VALVES AND VG ACTUATORS INSPECTED AND BOROSCOPE PERFORMED. NO DISCREPANCIES FOUND. PERFORMED POWER ASSURANCE, ACCELERATION CHECK, VIBE CHECK PER AMM 71-00-00 AFTER WORK PERFORMED WITH NO FAULTS NOTED
RIGHT ENGINE Ãâ¬ÅN2 VIBÃâ¬? MESSAGE DURING CLIMB. N1 ROLLED BACK BELOW 30%. WE FOLLOWED THE QRH/QRC AND SHUT THE ENGINE DOWN. NO INDICATIONS OF FIRE DISPLAYED AND NO BOTTLES WERE BLOWN. FLIGHT 4710 - FILED CLOSED THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 22484833 WITH THE FOLLOWING CORRECTIVE ACTION: "REMOVED AND REPLACED RH ENGINE ASSY IAW AMM 72-00-00 AND TASK CARD 71-900-1000-SKY. ALL ENGINE RUNS AND OPERATIONAL CHECKS ARE GOOD AT THIS TIME. ALL LEAK CHECKS GOOD AT THIS TIME.
FUSELAGE SKIN GOUGED AT FS 341 BETWEEN STR 24R AND STR 25R. REPAIRED GOUGE IN FUSELAGE SKIN AT FS 341 BETWEEN STR 24R AND STR 25R IAW MHIRJ REO AND SKYWEST TASK CARD.
RBL 9 O/B ATTACH BRACKET @ FS 280 UPPER AFT HOLE HAS NO ED, BREAKS THROUGH EDGE OF INNER L ANGEL (C-CHECK) RO 8/8/2020 REPAIRED BRACKET AT RBL 9 O/B @ F.S. 280 IAW REO FORM 337 FILED AND SKYCARD C/W AND ATTACHED NO WT CHANGE
FLOOR SEAT TRACK CORRODED IN SEVERAL LOCATIONS AT RBL 9 BETWEEN BS 409 TO 409+128. FABRICATED A NEW SEAT TRACK IAW REO.
RBL 9 SEAT TRACK WAS CORRODED BETWEEN BS 559 TO 559+80. FABRICATED A NEW SEAT TRACK IAW REO.
RBL 9 SEAT TRACK, BETWEEN BS 409+128 TO 559 DAMAGED. FABRICATED A NEW SEAT TRACK IAW REO .
F.S.280.00 FLOORBEAM CLIPS ON THE INBOARD SIDE OF LBL 9.00 AND RBL 9.00 ARE CRACKED. REMOVED AND REPLACED LBL9 AND RBL9 IB CLIPS IAW SRM.
BS 280 J ANGLE WAS CORRODED ALONG ENTIRE LENGTH, REMOVED AND REPLACED THE FWD J CHANNEL IAW SRM
CABIN SEAT TRACK CORRODED AND GOUGED. REMOVED & REPLACED THE SEAT TRACK IAW AMM. REPLACED WITH NEW SERVICABLE FABRICATED SEAT TRACK.
GALLEY MOUNT PADS, FWD AND AFT, INBOARD OF RBL 9.00 ARE CORRODED AROUND BOLT HOLES. FWD GALLEY MOUNT PAD WAS FOUND TO HAVE NO CORROSION .AFT PAD WAS REMOVED AND REPLACED IAW SRM.
SEAT TRACK CORRODED AT LBL 9 BETWEEN BS 409 TO 409+128. REPLACED SEAT TRACK IAW AMM.
FLOOR SEAT TRACK CORRODED IN SEVERAL LOCATIONS AT RBL9 BETWEEN FS409 TO FS409+128. (C-CHECK) RO 8/8/2020 REMOVED CORRODED SEAT TRACK AT RBL 9 BETWEEN FS 409 TO FS409+128 AND INSTALL NEWLY FABRICATED SERVICEABLE SEAT TRACK IAW CRJ 200 AMM.
BS 280 CROSSBEAM IS CORRODED BETWEEN LBL 9 AND RBL 9. COMPLIED WITH REPAIR IAW REO.
FRAME AT F.S. 349.00 CORRODED BETWEEN STGR 27 AND STGR 26L. (C-CHECK) RO 8/8/2020 REMOVED AND REPLACED F.S.349 FRAME IAW CRJ 200 SRM AND DWG ( FASTENER CALL OUT). COMPLETED AND ATTACHED TASK CARD AND M- 337. NO WEIGHT CHANGE.
FUSELAGE STRINGER 3L IS CRACKED AT F.S. 379.00. REPAIRED CRACKED FUSELAGE STRINGER 3L AT F.S.379.00 IAW SRM.
RBL 9 CARGO SEAT TRACK IS CORRODED BETWEEN BS 574 TO 621. REMOVED & REPLACED SEAT TRACK IAW CRJ AMM.
LBL 18 FLOOR BEAM IS CORRODED BETWEEN F.S. 574 TO F.S. 621 AROUND NUTPLATES. (C-CHECK) RO 8/8/2020 REMOVED AND REPLACED LBL 18 FLOORBEAM BETWEEN FS 574-621 IAW CRJ 200 SRM AND BOMBARDIER REO. COMPLETED AND ATTACHED TASK CARD AND M-337. NO WEIGHT CHANGE.
F.S. 574 FRAME IS CORRODED BETWEEN STRG 27 TO STRG 26L, AND 27 TO 26R AND 22L TO 21L. REMOVED AND REPLACED F.S. 574 LOWER FRAME SECTOR BETWEEN STRG 21R TO 21L. IAW CRJ 200 SRM AND DWGS.
LBL 9 CARGO TRACK FROM BS 574 TO 621 IS CORRODED. REMOVED AND REPLACED CARGO TRACK IAW AMM.
RBL 9 CARGO SEAT TRACK IS CORRODED BETWEEN BS. 559+96 TO 574. REMOVED & REPLACED CARGO SEAT TRACK IAW AMM
RBL 9 SEAT TRACK WAS CORRODED BETWEEN BS 559 TO 559+80. REMOVED AND REPLACED THE SEAT TRACK WITH NEWLY FABRICATED SEAT TRACK IAW AMM.
LBL 9 CARGO TRACK IS CORRODED BETWEEN F.S. 559+96 TO F.S. 574. REMOVED AND REPLACED THE CARGO TRACK IAW AMM.
L/H PRESSURE FLOOR SILL IS CORRODED BETWEEN F.S. 424 TO F.S. 559. (C-CHECK) RO 8/8/2020 REPAIRED CORROSION DAMAGE ON L/H PRESSURE FLOOR SILL BETWEEN F.S. 424 AND F.S 559 IAW DISPOSITION 1.2 OF BOMBARDIER REO. FORM 337 FILED AND SKYCARD C/W NO WT CHANGE.
F.S. 461 INTERCOSTAL INBOARD SUPPORT CLIP IS CRACKED AT LBL9. REMOVED CRACKED I/B INTERCOSTAL SUPPORT CLIP AND INSTALLED NEW SERVICEABLE SUPPORT CLIP IAW SRM.
RBL 9 SEAT RAIL IS CORRODED BETWEEN F.S. 409+128 TO F.S. 559. INSTALLED NEW FABRICATED SEAT TRACK FROM EXTRUSION P.N. 20276-288-0-0 IAW AMM .
LBL 9 FLOOR SEAT RAIL IS CORRODED. INSTALLED NEW SERVICABLE FABRICATED SEAT TRACK BETWEEN BS 409+128 TO 559 IAW AMM.
R/H PRESSURE FLOOR SILL IS CORRODED. BETWEEN F.S. 409+128 TO F.S. 559. (C-CHECK) RO 8/8/2020 REPAIRED R/H PRESSURE FLOOR SILL CORROSION DAMAGE BETWEEN F.S. 409+128 AND F.S 559 IAW DISPOSITION 1.2 OF BOMBARDIER REO
BATT RIB AT WS53.6 RHS IS CORRODED ON FLANGE AND WEB, AND IS CRACKED ALONG UPPER FLANGE. (C-CHECK) RO 8/8/2020 REMOVED AND REPLACED BATT RIB WEB, BOTH INNER AND OUTER DOUBLERS, AND CLEAT AT R/H W.S. 53.9 IAW CRJ 200 SRM.
RH ELEVATOR HINGE HARDWARE CORRODED, HINGE NR 1 NUT, 24.5 HINGE NUT, HINGE NR 2 NUT. REPLACED RH ELEVATOR HARDWARE IAW AMM.
LH ELEVATOR FLUTTER DAMPER NUTS ARE CORRODED (INBD AND OUTBD). REMOVED AND REPLACED LH ELEVATOR INB AND OBD FLUTTER DAMBER NUTS IAW AMM.
BATT RIB AT WS53.6 LHS IS CORRODED ON FLANGE AND WEB, AND IS CRACKED ALONG UPPER FLANGE. REMOVED AND REPLACED BATT RIB WEB, INNER AND OUTER DOUBLE, AND CLEAT AT L/H W.S. 53.9 IAW CRJ 200 AMM.
RUDDER LOWER HINGE POINT HAS A CORRODED NUT. (C-CHECK) RO 8/8/2020 RECIEVED NEW SERVICEABLE NUT REFERENCE JOB 9794791 OP 156 FOR INSTALLATION
RIGHT ELEVATOR INBD FLUTTER DAMPER HAS A CORRODED NUT. REMOVED AND REPLACED RT INBD ELEVATOR FLUTTER DAMPER NUT IAW AMM.
LOWER SKIN AT FWD AND AFT CARGO DOOR CUTOUT HAVE A FEW SMALL NICKS. COMPLIED WITH REPAIR OF LOWER SKIN AT FWD AND AFT CARGO DOOR CUT OUT IAW REO.
L/H WING INBOARD GROUND SPOILER PCU BOLT IS CORRODED. REMOVED AND INSTALLED NEW HARDWARE ON THE LH WING INBOARD GROUND SPOILER PCU IAW CRJ-200 AMM.
LEFT UPPER STAB FAIRING 326AL WAS CRACKED. INSTALLED NEW PART.
RIGHT WING OUTBOARD GROUND SPOILER PCU HARDWARE IS CORRODED. REMOVED AND REPLACED HARDWARE ON RH WING OUTBOARD GROUND SPOILER PCU IAW CRJ-200 AMM.
L/H WING OUTBOARD GROUND SPOILER PCU HARD WARE IS CORRODED. REMOVED AND REPLACED LH WING OUTBOARD GROUND SPOILER PCU HARDWARE, 2EA NUTS, 2EA COTTER PINS AND 2 EA WASHERS, IAW AMM
AVIONICS DOOR LT SIDE AFT FITTING ON THE FUSELAGE IS CRACKED. REMOVED AND REPLACED FITTING AT AVIONIC DOOR LT SIDE AFT FUSELAGE IAW SRM.
GEAR WOULD NOT COME DOWN. RAN QRH AND MANUALLY DEPLOYED GEAR WITH EMERGENCY EXT. HANDLE. GEAR CAME DOWN 3 GREEN AND LOCKED. FLIGHT 5648 - FILED CLOSED STOWED LANDING GEAR MANUAL RELEASE HANDLE AND PERFORMED OPERATIONAL TEST OF LANDING GEAR IAW AMM. OPS CHECK GOOD AT THIS TIME.
STARTING AT FL260, FOÃâ¬â¢S VSI BECAME ERRATIC AND FLUCTUATED CONSTANTLY BETWEEN 300 FPM AND 1000 FPM WHILE CAPTAINS REMAINED CONSTANT AT 500 FPM. FOÃâ¬â¢S ALTITUDE TAPE FLUCTUATED BETWEEN LEVELING OFF AND CLIMBING RAPIDLY, CORRESPONDING WITH VSI READINGS. IN CRUISE, FOÃâ¬â¢S VSI FLUCTUATED +/-200 FPM. VSI AND ALTIMETER APPEARED TO OPERATE NORMALLY DURING DESCENT. PERFORMED UNRELIABLE AIR DATA CHECK, FOUND WATER IN ADC-2 STATIC DRAIN TUBE, EMPTIED DRAIN TUBE; CHECKED ADC-2 COMPUTER FOR TIGHTNESS IN THE RACK, RE-SECURED COMPUTER; ALL HEATERS CHECK GOOD. OPS CHECK GOOD AT THIS TIME. WORK DONE IAW AMM.
RT FLOOR SILL IN AFT CARGO COMPARTMENT HAS CORROSION AROUND SCREW HOLES BETWEEN FS559+80 TO 559+96. (C-CHECK) RO: 10/01/2018 REMOVED AND INSTALLED NEW RT FLOOR SILL P/N: 601R31133-86 IN AFT CARGO BETWEEN FS559+80 TO FS559+112 IAW SRM.
FLOOR ANGLE AT CARGO DOOR CUTOUT IS CORRODED IN SEVERAL LOCATIONS. (C-CHECK) RO: 10/01/2018 BLENDED OUT CORROSION ON FLOOR ANGLE AT CARGO DOOR SILL IAW REO.
IN MLG TRUNNION, FOUND 1 EACH OVERSIZED HOLE, LOCATED AT MOST AFT HOLE OF THE STEEL STRAP, AND 1 EACH HOLE WITH CRACK INDICATION, MARKED ON AC, ON THE RT MLG TRUNNION. (C-CHECK) RO: 10/01/2018 COMPLIED WITH REO FOR REPAIR OF 1EA CRACKED HOLE AND 1EA OVERSIZED HOLE ON RT TRUNNION.
IN MLG TRUNNION, FOUND 1 EACH OVERSIZED HOLE LOCATED AT THE MOST AFT HOLE ON THE STEEL STRAP OF LT MLG TRUNNION. (C-CHECK) RO: 10/01/2018 REPAIRED OF 1 EA OVERSIZED HOLE ON LT TRUNNION IAW REO.
LT FLOOR SILL AT CARGO DOOR OPENING HAS SEVERAL AREAS OF CORROSION FROM FS574.00 TO FS621. (C-CHECK) RO: 10/01/2010 BLENDED OUT CORROSION ON LT FLOOR SILL AT CARGO DOOR IAW SRM AND REO.
RT FLOOR SUPPORT STRAP AT FS559 FROM RBL27 TO RBL40 HAS AREAS OF CORROSION. (C-CHECK) RO: 10/01/2018 REPLACED DAMAGED RT FLOOR SUPPORT STRAP AT FS559 FROM RBL27 TO RBL40 IAW SRM.
LT FLOOR SUPPORT STRAP AT FS559 FROM LBL27 TO LBL40 HAS AREAS OF CORROSION. (C-CHECK) RO: 10/01/2018 REMOVED CORROSION ON THE LEFT-HAND SUPPORT STRAP AT FS559 FROM LBL27 TO LBL40. IAW SRM. NO LEAKS DETECTED.
LEFT AILERON O/B L/E LOWER RUB STRIP HAS CHAFING. (C-CHECK) RO: 10/01/2010 BLENDED LEFT AILERON O/B LEAD EDGE RUB STRIP(AILERON FIXED PANEL) IAW SRM AND REO.
RT FUSELAGE BETWEEN STRINGERS 6&7, BETWEEN FS621.00 & FS 736.00. 0.7" LONG X 0.4" WIDE X 0.017". (C-CHECK) RO: 10/01/2010 COMPLIED WITH PERMANENT REPAIR DENT IAW REO.
RIGHT SIDE OF NOSE NEAR F.S. 235.00 AFT OF PITOT TUBE. TWO SMALL DENTS WITH SCRATCHES, EACH 0.5 " LONG WITH DEPTHS OF 0.023" AND 0.010". (C-CHECK) RO: 10/01/2010 REPAIRED RIGHT SIDE OF NOSE NEAR F.S. 235.00 AFT OF PITOT TUBE. TWO SMALL DENTS WITH SCRATCHES. CUT AWAY DAMAGED AREA, FABRICATED AND INSTALLED ALL REPAIR PARTS IAW REO. PRESSURIZATION CHECK GOOD.
LT ENG LOW OIL PRESS MSG DURING FLIGHT. COMPLIED WITH QRH. (FLT#5504) FO: 07/24/2018 CLOSED REMOVED AND REPLACED HYDRAULIC PUMP, IDG, AND STARTER CARBON SEALS IAW ENGINE MANUAL. ALSO REMOVED AND REPLACED C-SUMP COMPONENTS . EXHAUST FRAME AND NR 7 CARBON SEAL IAW ENGINE MANUAL. OPS AND LEAK CHECKS GOOD.
EVIDENCE OF AN ELECTRICAL BURN ON FRAME AT FS 409.00+65 BETWEEN STR 4R AND STR 5R. COMPLIED WITH STS EA ALL STEPS COMPLETED OF PERMANENT REPAIR.
LEFT INBD FLAP OTBD VANE L/E IS CHAFED. REMOVED AND INSTALLED LT INBD FLAP OTBD L/E VANE CAP, PN 601R14303-43 IAW SRM.
LEFT INBD FLAP, CENTER VANE L/E IS CHAFED. REMOVED AND INSTALLED NEW LT INBD FLAP, VANE CENTER L/E CAP, PN 601R14303-51 IAW SRM AND STS EA.
RIGHT INBD FLAP, INBD VANE L/E IS CHAFED. R & R RT INBD FLAP, INBD VANE L/E IAW SRM.
LEFT OTBD FLAP, OTBD FLAP HINGE ARM CHAFED FORWARD EDGE OF BEARING. REPAIRED LT OTBD FLAP, OTBD FLAP HINGE ARM IAW REO.
RIGHT OTBD FLAP, OTBD HINGE ARM CHAFED AT FORWARD SIDE OF BEARING. REPAIRED LT OTBD FLAP, OTBD FLAP HINGE ARM IAW REO.
LEFT WING ACCESS PANEL 599BB IS CHAFED. REPLACED LT WING ACCESS PANEL 599BB IAW SRM.
DURING CLIMBOUT, GOT A "CABIN ALT" CAUTION MESSAGE WHICH OCCURED AT FL230. CABIN PRESSURE WAS RISING RAPIDLY. DONNED MASKS AND "CABIN ALT" WARNING MESSAGE APPEARED. EXECUTED EMERGENCY DESCENT, RAN QRH. RETURNED TO FIELD. INSULATION BLANKET WAS FOUND STUCK IN THE SECONDARY OUTFLOW VALVE. REMOVED BLANKET AND OPS CHECKED IAW AMM. OPS CHECKED GOOD.
CABIN ALT WARNING AT FL220. CABIN ALT STARTED CLIMBING. CREW DECLARED EMERGENCY. FO: 01/04/2016 TROUBLESHOT CABIN ALT CAUTION AND WARNING MESSAGE IAW FIM. FOUND PSEU SUPPLYING GROUND TO WOW RELAY, K1GA WHILE IN WOW CONDITION CAUSING CPC TO GO THROUGH WOW PROCEDURES. R & R PSEU IAW AMM. PERFORMED OPS TEST OF THE PSEU IAW AMM. PERFORMED FUNCTIONAL TEST OF THE CPC IAW AMM. NO DEFECTS NOTED. R & R WOW RELAYS K1GA AND K2GA. PASSED FUNCTIONAL FLIGHT NO DEFECTS NOTED.
FLAPS FAILED, RTF, AND LANDED WITHOUT INCIDENT. R & R RT BPSU AND FECU IAW AMM. OPS CHECKED GOOD IAW AMM.
F/A FLASHLIGHT DISCHARGED. R & R BATTERY IAW AMM.
CALL INDICATOR LIGHT ON EXIT SIGN DOES NOT ILLUMINATE. REPLACED ALL PINS IN CONNECTOR P56MD AND CLEANED AND TREATED CONNECTOR P56MD IAW AMM.
OVERHEAD FWD EMERGENCY LIGHT IS BURNED OUT. FLT 6495 RELAMPED.
EXTERNAL LT SIDE FWD EMERGENCY LIGHT IS BURNED OUT. FLT 4968 RELAMPED.
IN APPROACH MODE AUTOPILOT DID NOT CAPTURE LOCALIZER & FLIGHT DIRECTOR STARTED PITCHING UP AGGRESSIVELY. FLT 6377 COULD NOT DUPLICATE ISSUE. FLIGHT DIRECTOR & AUTOPILOT OPERATIONS CHECKED GOOD IAW AMM.
MAIN CABIN DOOR HARD TO OPEN FROM GROUND. SERVICE ADJUSTED MAIN CABIN DOOR IAW AMM.
FLT 6257, RT PACK HIGH PRESSURE CAUTION DURING BLEED TRANSFER, & INTERMITTENT HIGH PRESSURE CAUTIONS ON ED2. REPLACED RT PACK PRSOV IAW AMM.
LEFT MLG LOWER LONGERON FRAME AND INTERCOSTAL CRACKED AT FS 529.00 DUE TO LEFT MLG BELLCRANK PUNCTURE. (C-CHECK) REPAIRED LEFT MLG BAY LOWER LONGERON AND INTERCOSTAL IAW REO.
GALLEY SERVICE DOOR DIFFICULT TO OPEN. (FLT 5558) CLEANED AND LUBED GALLEY SERVICE DOOR SEAL AND CAMS.
GEAR DISAGREE WARNING MESSAGE (RIGHT LANDING GEAR) AFTER TAKEOFF. (FLT 6190) ADJUSTED RIGHT MAIN LANDING GEAR PROX SENSOR PS7GA IN REFERENCE TO AMM.
AFT RIGHT WING EXTERIOR EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.
VERTICAL GALLEY EMERGENCY LIGHT BROKEN. (SERVICE) REPLACED VERTICAL GALLEY EMERGENCY LIGHT.
LOWER RIGHT OVERWING INTERIOR EMERGENCY EXIT SIGN IS OUT. (FLT 5582) RELAMPED EMERGENCY EXIT SIGN.
AFT OVERWING EMERGENCY EXIT LIGHT ON LEFT SIDE IS OUT. (FLT 5230) RELAMPED EMERGENCY LIGHT.
LEFT AND RIGHT OVERWING MIDDLE EXTERIOR EMERGENCY LIGHTS ARE OUT. (FLT 6424) RELAMPED EMERGENCY LIGHTS.
RIGHT OVERWING AFT AND ROW 10 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 5463) RELAMPED EMERGENCY LIGHTS.
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6297) RELAMPED EMERGENCY LIGHT.
AILERON UPPER CONTROL CABLE CORRODED. (SERVICE) INSTALLED SERVICEABLE AILERON UPPER CONTROL CABLE.
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6259) RELAMPED EMERGENCY LIGHT.
RIGHT SIDE MIDDLE AND AFT EXTERNAL EMERGENCY LIGHTS ARE OUT. (FLT 6220) RELAMPED EMERGENCY LIGHTS.
FS 621 FORWARD FACE CRACKED AT LINTEL FITTIING. (C-CHECK) REPAIRED PER REO.
FORWARD INTERCOSTAL FS 319 AT DATUM 7 IS CRACKED ON PAX DOOR. (C-CHECK) REPLACED INTERCOSTAL AT FS 319.00 DATUM 7 ON PAX DOOR.
RIGHT MIDDLE EMERGENCY EXTERIOR LIGHT IS OUT. (FLT 6350) RELAMPED EMERGENCY LIGHT.
LEFT AFT AND RIGHT FORWARD EXTERIOR EMERGENCY LIGHTS ARE OUT. (FLT 6626) RELAMPED EMERGENCY LIGHT.
NR 4 CEILING EMERGENCY LIGHT INOPERATIVE. (FLT 6727) RELAMPED EMERGENCY LIGHT.
ONE BULB IN FLOOR LEVEL EMERGENCY FLOODLIGHT CLUSTER IS BURNED OUT. (FLT 6718) REMOVED AND REPLACED THE LIGHT ASSEMBLY.
FS 280 FLOOR SUPPORT ANGLE CRACKED. (C CHECK) REPLACED ANGLE PER SRM.
SUPPORT BEAM ANGLE AT FS 621 CRACKED. (C-CHECK) REPLACED PER SRM.
CARGO DOOR FORWARD SUPPORT CHANNEL CRACKED. (C-CHECK) REPLACED PER SRM.
COFFEEMAKER SPARKING. (FLT 6741) DEACTIVATED AND REPLACED COFFEEMAKER.
GEAR DISAGREE DISPLAYED. (FLT 5854) REPLACED RUPTURED HYDRAULIC LINE.
FLT 6143 - EXTERNAL EMERGENCY LIGHT BY MAIN CABIN DOOR IS INOP. RELAMPED.
FLT 5849 - "CABIN ALT" WARNING MESSAGE APPEARED. INSPECTED AND SECURED DUCT TO PRIMARY HEAT EXCHANGER ASSEMBLY. OPS CHECK GOOD.
RBL9 LOWER FLOOR SUPPORT IS CRACKED, FOUND AT C-CHECK. INSTALLED REPAIR PARTS FOR RBL 9 LOWER FLOOR SUPPORT PER CRJ200 REO 601R-53-11-171 REV D DATED 02/13/07.
FOUND AT C-CHECK, HORIZONTAL STABILIZER HINGE BUSHINGS AND INNER PIN SHOWS SIGNS OF WEAR. REPLACED STABILIZER HINGE PIN AND BUSHINGS IAW CRJ200 AMM SUBTASK 12-20-27-640-008.
FS 484 AT LBL 36 INTERCOSTAL IS CRACKED, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER REO601R-53-059 REV A.
LEFT SIDE OF STA 621 MOST OUTBOARD FLOOR FRAME IS CRACKED, FOUND AT C-CHECK. COMPLIED WITH REPAIRS PER CRJ200 REO 601R 53-61-117 REV C DATED 2004-AUG-25.
LBL9 AND RBL9 AT FS 280 UPPER FLOOR SUPPORT IS CRACKED, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER CR200 REO 601R-53-11-136 DATED 02/13/99.
LBL 9 LOWER FLOOR SUPPORT CRACKED, FOUND AT C-CHECK. INSTALLED REPAIR PARTS FOR LBL 9 LOWER FLOOR SUPPORT PER CRJ200 REO 601R-53-11-171 REV D DATED 02/13/07.
BIRD STRIKE TO LEFT INBOARD FLAP ON APPROACH INTO YWG. REPLACED LEFT INBOARD FLAP INBOARD LEADING EDGE PER 57-52-01.
BURNING ODOR IN FLIGHT DECK WHILE AT THE GATE IN PHOENIX. NO EVIDENCE OF ODOR SMELL IN COCKPIT AT THIS TIME. UNABLE TO DUPLICATE DISCREPANCY.
AFT EQUIPMENT COMPARTMENT FS625.00 LBL36 STR 13 CLIP CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP AT FS 625.00 LBL 36 STRINGER 13 REFERENCE CRJ200 SRM 51-42-06 PG 11 AND SRM 51-42-21 PG 17 STEP 9 REO 601R-53-61-088.
PAX DOOR CRACKED BEHIND AFT HANDRAIL SUPPORT, DISCOVERED DURING C-CHECK INSPECTION. REPAIR PIECES INSTALLED AT AFT HANDRAIL SUPPORT STEP C/W CRJ 200 REO 601R-52-11-702.
PAX DOOR CRACKED BEHIND THE FWD HANDRAIL SUPPORT, DISCOVERED DURING C-CHECK INSPECTION. REPAIR PIECES INSTALLED AT FWD HANDRAIL SUPPORT STEP COMPLIED WITH CRJ200 REO 601E 52-11-702.
FS 621 RT FLOOR SUPPORT STRUCTURE IS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS PER REO 601R 53-61-117 AND CRJ200 SRM 51-42-06 PG 1-20/51-42-21 PG 1-21.
FOUND "FLAPS FAIL" CAUTION MESSAGE. REPLACED SENSOR PER CRJ 200 MM 27-51-15, OPERATIONAL CHECK GOOD, PN 80-044-03, SN OFF 2618.
FLAP FAIL CAUTION AFTER ATTEMPTED FLAP RETRACTION ON CLIMB-OUT. ADJUSTED LT BPSU IAW MM 27-51-10. REPLACED FLAP SKEW DETECT PANEL IAW MM 27-51-15, OPERATIONAL CHECK GOOD.
YD2 INOP, IAPS DEGRADED, FD 2 FAIL STATUS MESSAGES DISPLAYED. REPLACED IOC CARD 2A IAW MM 22-16-06. REPLACED NR 2 FCC CARD IAW MM 22-12-14. OPERATIONAL CHECK GOOD, PN OFF: 622-9815-904 SN OFF: 10BMP PN: 622-9814-008 SN OFF: IGM7N.
AIRCRAFT REQUIRES EXCESSIVE AMOUNT OF RT WING DOWN TRIM. RETENSIONED LT AND RT AILERON CABLES IAW AMM 27-00-00.
RIGHT EMERGENCY DOOR CAUTION MESSAGE IN FLIGHT. CLEANED DEBRIS FROM RIGHT EMERGENCY DOOR PROXIMITY SWITCH. OPERATIONAL CHECKS GOOD.