N784SK
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
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
145 reports on file, 2012-06-04 – 2024-09-21.
Part: DETECTOR — FALSE INDICATION · airframe 37,084 hrs · 24,027 cycles
R BLEED WARNING MSG IN FLIGHT. (FLIGHT 5726 - FILED CLOSED) CAPTAIN CONFIRMED L BLEED WARNING MESSAGE WAS THE ISSUE, NOT R BLEED WARNING. HAD CAPTAIN CREATE A NEW WRITE-UP WITH THE CORRECT DISCREPANCY. PLEASE REFERENCE AML#1435403 FOR CORRECT DISCREPANCY. VERIFIED ON MDC L BLEEP LOOP A WAS FLAGGED.
Part: SLAT TRACK — CRACKED (ZONE 500) · airframe 37,077 hrs · 24,023 cycles
SUSPECTED CRACK AT LH SLAT TRACK FUEL CANISTER 1-3 (C-CHECK RO 9/19/2024) PERFORMED REPAIR AT LH SLAT TRACK FUEL CANISTER 1-3 CRACKED BRACKET, REF REO 670-57-42-577 REV-- DATE: 2016-12-02. COMPLIED WITH TASK CARD 51-900-1002-SKY. ALL CHECK GOOD, LEAK CHECK GOOD COMPLIED WITH SKYWEST FORM M-337
Part: SLAT TRACK — CRACKED (ZONE 600) · airframe 37,077 hrs · 24,023 cycles
SUSPECTED CRACK AT RH SLAT TRACK FUEL CANISTER 1-3 (C-CHECK RO 9/19/2024) PERFORMED REPAIR AT AT RH SLAT TRACK FUEL CANISTER 1-3 AND PERFORMED REO 670-57-42-577 REV-- DATE: 2016-12-02. COMPLIED WITH TASK CARD 51-900-1002-SKY. ALL CHECK GOOD
Part: STRINGER — CRACKED (ZONE 200) · airframe 37,077 hrs · 24,023 cycles
STRINGER 3L AT FS280 IS CRACKED (C-CHECK RO 9/19/2024) REPAIRED STGR3L FS280.00 IAW REO 670-53-21-493 REV. D DATE 2015-07-10. SEE CONTINUE CARD FOR WORK PERFORMED. PRESSURE CHECK OF REPAIR AREA GOOD IAW CRJ700 AMM 21-31-00-910-801-A01SERVICE BULLETIN 670BA-53-040, REVISION C, FUSELAGE - CENTER FUSELAGE, PRIMARY STRUCTURE FS280.00 TO FS295.00 - INSPECTION AND REINFORCEMENT OF LINTEL STRINGER 3 OF THE MAIN PASSENGER DOOR, PART A & B, INCORPORATED. COMPLIED WITH TASK CARD -51-900-1002. NO NOTED DEFECTS. ALL CHECKS GOOD
Part: WINDOW POST — CRACKED (ZONE 200) · airframe 37,077 hrs · 24,023 cycles
LH WINDSHIELD POST LOWER OUTBD CLIP APPEARS TO BE CRACKED (C-CHECK RO 9/19/2024) REMOVED AND REPLACED LH WINDSHIELD POST LWR OB CLIP WITH NEW, REF CRJ 700 SRM 51-42-21-001-001-A01 AND DWG CC670-33055 REV -F AND DWG GC212-0045 REV -ACOMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR COMPLIED WITH SKYWEST FORM M-337
Part: FRAME — CRACKED (ZONE 200) · airframe 37,077 hrs · 24,023 cycles
FRAME CRACKED AT FS333.00 BETWEEN STGR 1R AND STGR 2R (MARKED) (C-CHECK RO 9/19/2024) COMPLIED WITH REPAIR TO FRAME SECTOR FS333 BETWEEN STR 1R & STR 2R REF REO 670-53-21-2437 REV -- 2024-07-24. COMPLIED WITH TASK CARD 51-900-1002-SKY
Part: STRUT — GOUGED (NLG) · airframe 37,077 hrs · 24,023 cycles
NLG SHOCK STRUT, THE AFT SIDE OF CHROME PISTON HAS A VERTICLE GOUGE (MARKED) (C-CHECK RO 9/19/2024) REPAIRED NLG SHOCK STRUCT AFT SIDE OF CHROME PISTON GOUGE BY COMPLLYING WITH ALL STEPS OF REO # 670-32-21-237, REV. D, DATED: 2020-07-28 AND GOODRICH SCR # 036-17, REV C. PISTON OD = 3.246" BEFORE SANDING. PISTON OD = 3.245" AFTER SANDING, CALIPER # 10026TUC, DUE DATE: 30-NOV-24, NO ADDITIONAL DEFECTS NOTED. SEE CONTINUATION FOR WORK PERFORMED. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY
Part: LATCH — CRACKED (TRU BAY DOOR) · airframe 37,077 hrs · 24,023 cycles
RH TRU BAY DOOR, THE AFT DOOR LATCH CUTOUT POSSIBLE CRACK IN THE ANGLE RADIUS (MARKED) (C-CHECK RO 9/19/2024) REPLACED THE RH TRU BAY DOOR LANDING REF REO 670-53-11-2003 REV -A 2024-08-26, REO 670-53-11-1996 REV -- 2024-08-05, DWG: CC670-33151 REV -D, CRJ-700 SRM 51-42-06-001-001-A01 REV 38 JUL 25/2020, CRJ-700 SRM 51-42-22-001-001-A01 REV 38 JUL 25/2020. COMPLIED WITH TASK CARD 51-900-1002-SKY
Part: BUTTSTRAP — CORRODED (FAIRING) · airframe 37,077 hrs · 24,023 cycles
MLG FAIRING PANEL 194AB R/H TOP BUTTSTRAP FUSELAGE MULTIPLE AREA HAS CORROSION (MARKED) (C-CHECK RO 9/19/2024) COMPLIED WITH REPAIR TO THE M/C BEAM AT RBL48 BETWEEN FS826 - FS836 REF REO 670-53-42-100 REV -- 2024-08-28. COMPLIED WITH TASK CARD 51-900-1002-SKY
Part: DOOR — CRACKED (TRU BAY) · airframe 37,077 hrs · 24,023 cycles
LH TRU BAY DOOR, THE AFT DOOR LATCH CUTOUT POSSIBLE CRACK IN THE RADIUS (MARKED) (C-CHECK RO 9/19/2024) REPAIRED LH TRU BAY DOOR LANDING REF. REO 670-53-11-1996 REV-- DATED: 2024-08-05. REF CRJ-700 SRM 51-42-06-001-001-A01 AND DWG NO: CC670-33040 REV -G. COMPLIED WITH TASK CARD 51-900-1002-SKY
Part: DOOR SILL — CORRODED (ZONE 200) · airframe 37,077 hrs · 24,023 cycles
GALLEY SERVICE DOOR SILL LOWER SEAL STRIKER CORRODED AT SCREW HOLES AS (MARKED) (C-CHECK RO 9/19/2024) INSTALLED NEW SERVICE DOOR SILL LOWER SEAL STRIKER P/N SH670-31412-7 REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG# SH670-31950 REV-Y. ALL CHECKS GOOD. TASK CARD 51-900-1002-SKY COMPLIED WITH
Part: FITTING — CORRODED (PAX DOOR) · airframe 37,077 hrs · 24,023 cycles
PASSENGER DOOR FITTING, CLOSING CORROSION BETWEEN FS319 AND FS333.00 (MARKED) (C-CHECK RO 9/19/2024) REMOVED CORROSION ON PAX DOOR FITTING, CLOSING. BLEND FOUND TO BE OUT OF LIMITS AT 32% MATERIAL LOSS. REMOVED AND REPLACED PAX DOOR FITTING, CLOSING. NO CHANGE IN WEIGHT. RESTORED FINISH. REF: CRJ-700 SRM 51-21-06-001-001-A01, DWG SH670-31840 REV -A, CRJ 700 SRM 51-42-06-001-001-A01, CRJ 700 SRM 51-40-11-001-001-A01, SH670-31810 REV -Y. COMPLIED WITH 51-900-1002-SKY.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 37,077 hrs · 24,023 cycles
CABIN FLOOR RIGHT T CAP RBL9 BETWEEN FS1007.00 AND FS1045.00 CORRODED AS MARKED (C-CHECK RO 9/19/2024) COMPLIED WITH REPAIR TO THE RBL9 FLOOR BEAM AT FS1007 - FS1045 REF CRJ-700 SRM 53-00-41-201-001-A01, REO 670-53-61-2340 REV -- 2024-08-06, AND REO 670-53-61-2341 REV -- 2024-08-06. COMPLIED WITH TASK CARD 51-900-1002-SKY.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 37,077 hrs · 24,023 cycles
CABIN FLOOR LEFT T CAP LBL27 BETWEEN APPROXIMATELY FS1000.00 AND FS1050.00 CORRODED AS MARKED (C-CHECK RO 9/19/2024) COMPLIED WITH REPAIR TO THE CABIN FLOOR BEAM AT LBL27, APPROX FS1000 - FS1050 REF REO 670-53-61-2337 REV -A 2024-08-22 AND CRJ-700 SRM 53-00-41-201-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY
Part: SPAR — GOUGED (ZONE 600) · airframe 37,077 hrs · 24,023 cycles
RH WING AFT FACE OF REAR WING SPAR HAS GOUGES AROUND 2ND LIGHTNING HOLE BETWEEN WS350.25 AND WS370.25 (C-CHECK RO 9/19/2024) COMPLIED WITH REPAIR TO RH WING AFT FACE OF REAR WING SPAR BETWEEN WS350.25 AND WS370.25 REF REO 670-57-21-987 REV-- DATE 2024-08-16., BLEND AND DAMAGE ALLOWANCE REPAIR. COMPLIED WITH TASK CARD 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR COMPLIED WITH SKYWEST FORM M-337
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 37,077 hrs · 24,023 cycles
R/H FLOOR SILL BETWEEN FS280.00 TO FS295.00 HAS CORROSION (MARKED) (C-CHECK RO 9/19/2024) BLENDED REPORTED CORRODED AREAS FROM R/H FLOOR SILL BETWEEN FS 280 AND FS 295, FOUND BLENDED AREAS OUT LIMITS PER REF CRJ 700 SRM 53-00-00-101-001-A01. REMOVED CORRODED R/H FLOOR SILL FROM FS 280 TO FS 319 AND INSTALLED A NEW ONE PER DWG# SH670-32170 REV V, CRJ 700 SRM 51-42-06-001-001-A01, CRJ 700 SRM 51-42-13-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01. PRESSURE TEST GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKY
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 37,077 hrs · 24,023 cycles
R/H FLOOR SILL BETWEEN FS349.00 TO FS364.00 HAS CORROSION (MARKED) (C-CHECK RO 9/19/2024) REPAIRED R/H FLOOR SILL BETWEEN FS349.00 TO FS364 REF REO 670-53-21-1806 REV--2020-08-27 AND DWG SH670-32170 REV V COMPLIED WITH TASK CARD 51-900-1002-SKY LEAK CHECK GOOD.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 37,077 hrs · 24,023 cycles
L/H FLOOR BEAM LBL 9 HAS CORROSION APPROXIMATELY BETWEEN FS549.00 TO FS565.00 (MARKED) (C-CHECK RO 9/19/2024) PERFORMED FLOOR BEAM SPLICE REPAIR APPROX. FS549.00 TO FS565.00 REF REO 670-53-31-916 REV -- 2024-08-12, REO 670-53-31-918 REV -- 2024-08-12 AND CRJ700 SRM 53-00-41-201-001-A01 REV 38 JUL 25/2020. COMPLIED WITH TASK CARD 51-900-1002-SKY. ALL CHECKS GOOD.
Part: HINGE — CHAFED (ZONE 200) · airframe 37,077 hrs · 24,023 cycles
PAX DOOR HINGE DOOR SIDE, ALL LUG LANDS HAVE CHAFFING AND LUGS HAVE VARIOUS CHAFES AND SCRATCHES AT THE HIGH POINT OF THE LUG AND THE LUG BASE NEAR THE SEAL SIDE. HN00173018 (C-CHECK RO 9/19/2024) BLENDED AND EVAL'D PAX DOOR HINGE LUGS ON DOOR SIDE, FOUND TO BE WITHIN LIMITS AND RESTORED FINISH REF CRJ 700 SRM 52-11-01-201-007-A01. BLEND OUT ONLY, NO WEIGHT CHANGE. COMPLIED WITH TASK CARD 51-900-1002-SKY
Part: STAND OFF — CRACKED (TRANSCOWL) · airframe 37,077 hrs · 24,023 cycles
L/H UPPER TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 9/19/2024) INSTALLED 1 EA. NEW A BRACKET P/N CN624-2082-201 ON L/H UPPER TRANS COWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH STEPS 1-3 AND COMPLIED WITH 51-900-1002-SKY.
Part: HINGE — CHAFED (ZONE 200) · airframe 37,077 hrs · 24,023 cycles
PAX DOOR HINGE FUSELAGE SIDE, ALL LUG LANDS HAVE CHAFFING AND ALL LUGS HAVE SOME DEGREE OF CHAFFING AND SCRATCHES. HN00173016 (C-CHECK RO 9/19/2024) REMOVED AND REPLACED PASSENGER DOOR HINGE (FUSELAGE SIDE) REF. CRJ 700 SRM 53-21-23-201-007-A01, AND DWG SH670-31810 REV AE COMPLIED WITH TASK CARD 51-900-1002-SKY .LEAK CHECK GOOD.
Part: STAND OFF — CRACKED (TRANSCOWL) · airframe 37,077 hrs · 24,023 cycles
R/H UPPER TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 9/19/2024) INSTALLED NEW R/H UPPER TRANSCOWL I/B "A" BRACKET (PN CN624-2082-201) REF REO# 670-54-21-971, REV B, DATED 11/28/23. SEE CONTINUATION SHEET FOR DETAILS.
Part: TRANSCOWL — CRACKED (THRUST REVERSER) · airframe 37,077 hrs · 24,023 cycles
L/H LWR TRANSCOWL OTBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 9/19/2024) REPLACED O/B STAND-OFF ANGLE P/N CN624-2082-201 ON L/H LOWER TRANSCOWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH M-337 AND SKY CARD 51-900-1002-SKY. REF. CAMP 28501667.
Part: HINGE FITTING — GOUGED (ZONE 600) · airframe 37,077 hrs · 24,023 cycles
RH AILERON #2 HINGE FITTING OUTBOARD LUG AND LOWER INBOARD SIDE HAS GOUGES (C-CHECK RO 9/19/2024) REPAIRED RH AILERON #2 HINGE FITTING GOUGES THROUGH COMPLIANCE WITHL STEPS OF REO 670-57-51-562 REV --, DATED 2024-08-15, BLEND REPAIR AND DAMAGE ALLOWNACE, STEPS 1-4 FOR BLEND #2 DAMAGE. SEE CONTINUE CARD FOR WORK PEREFORMED COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR COMPLIED WITH SKYWEST FORM M--337
Part: HINGE FITTING — GOUGED (ZONE 600) · airframe 37,077 hrs · 24,023 cycles
RH AILERON #3 HINGE FITTING INBOARD LUG AND LOWER INBOARD SIDE HAS GOUGES (C-CHECK RO 9/19/2024) REPAIRED GOUGES ON RH AILERON HINGE FITTING #3 BY COMPLYING WITH ALL STEPS OF REO 670--57-51-562 REV -- DATED 2024-08-15, BLEND ALLOWANCE REPAIR, STEPS 1-4 SEE CONTINUE CARD FOR DETAILS. COMPLIED WITH SKYWEST TASK CARD 51--900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR COMPLIED WITH SKYWEST FORM M-337
Part: HINGE FITTING — GOUGED (ZONE 600) · airframe 37,077 hrs · 24,023 cycles
RH AILERON #1 HINGE FITTING OUTBOARD LUG GOUGED (C-CHECK RO 9/19/2024) COMPLIED WITH ALL STEPS OF REO 670-57-51-562 REV --, DATED 2024-08-15. BLEND REPAIR WITH EXCEPTANCE OF REPORTED MATERIAL DIMENSIONS RH AILERON #1 HINGE FITTING. SEE CONTINUE CARD FOR WORK PERFORMED. BLEND ONLY NO WEIGHT CHANGECOMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR COMPLIED WITH SKYWEST FORM M-337
Part: HINGE FITTING — GOUGED (ZONE 600) · airframe 37,077 hrs · 24,023 cycles
RH AILERON #4 HINGE FITTING INBOARD AND OUTBOARD LUG HAS GOUGES (C-CHECK RO 9/19/2024) REMOVED DAMAGE FROM R/H AILERON #4 HINGE I/B AND O/B LUG IAW CRJ700 SRM 51-12-00-001-001-A01. COMPLIED WITH ALL STEPS OF REO 670-57-51-562 REV --, DATED 2024-08-15. COMPLIED WITH TASK CARD 51-900-1002-SKY. SEE CONTINUE CARD FOR WORK PERFORMED.
Part: SKIN — DENTED (ZONE 100) · airframe 37,077 hrs · 24,023 cycles
MULTIPLE DENTS,NICKS, GOUGES ,ON AFT FUSELAGE SKIN IN BETWEEN APPROX FS 1000 TO FS 1051 BETWEEN STR 21R AND STR 27 IN AREA OF GROUND A/C SERVICE DOOR. (C-CHECK RO 9/19/2024) REPAIRED MULTIPLE DENTS,NICKS, GOUGES ,ON AFT FUSELAGE SKIN BETWEEN FS 1000 TO FS 1051 BETWEEN STR 21R AND STR 27 WITHIN BLEND ALLOWANCE REPAIR PER REO 670-53-61-2351 REV -- DATED 2024-08-22COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR COMPLIED WITH SKYWEST FORM M-337
Part: SKIN — DENTED (ZONE 100) · airframe 37,077 hrs · 24,023 cycles
FOUND DENT ON RHS OF REAR FUSELAGE, AFT OF GROUND AIR DOOR, APPROXIMATELY 13 INCH, PARALLEL TO AFT LOWER CORNER RADIUS.OF DOOR CUT-OUT. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES. (C-CHECK RO 9/19/2024) COMPLIED WITH REPAIR TO THE FUSELAGE SKIN BETWEEN FS1015 - FS1051 & STR 23R - STR 27 REF REO 670-53-61-2351 REV -- 2024-08-22. ALL CHECKS GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKY
Part: ENGINE — ODOR (LEFT) · airframe 36,987 hrs · 23,942 cycles
STRONG FUEL ODOR OBSERVED IN CABIN DURING DESCENT AND LANDING. GROUND CABIN OBSERVED WHITE/BLUE SMOKE COMING FROM LEFT ENGINE AS AIRCRAFT APPROACHED THE GATE WITH BOTH ENGINES RUNNING. SMOKE DECREASED IN INTENSITY AFTER ENGINE WAS SHUT DOWN, BUT WHITE SMOKE CONTINUED TO COME FROM THE REAR OF THE LEFT ENGINE FOR 10 MINUTES AFTER SHUTDOWN. MAY 30, 2024 STATION: ASE--COMPLIED WITH CRJ700 FIM 21-22-00-810-806. NO ABNORMAL SMOKE OR FUEL SMELL IN COCKPIT OR PASSENGER CABIN. COMPLIED WITH CRJ700 FIM 79-30-00 NO FUEL SMELL NOTED NO LEAK FUEL LEAKS NOTED. PERFORMED HIGH POWERED ENGINE RUNS WITH THE LEFT AND RIGHT ENGINES REF. CRJ700 AMM 71-00-00. FOR 30 MINUTES WITH ENGINE BLEEDS OR APU BLEEDS AND BOTH AIR-CONDITIONING
Part: ENGINE — SMOKE (LT ENGINE) · airframe 36,985 hrs · 23,938 cycles
STRONG FUEL ODOR OBSERVED IN CABIN DURING DESCENT AND LANDING. GROUND CABIN OBSERVED WHITE/BLUE SMOKE COMING FROM LEFT ENGINE AS AIRCRAFT APPROACHED THE GATE WITH BOTH ENGINES RUNNING. SMOKE DECREASED IN INTENSITY AFTER ENGINE WAS SHUT DOWN, BUT WHITE SMOKE CONTINUED TO COME FROM THE REAR OF THE LEFT ENGINE FOR 10 MINUTES AFTER SHUTDOWN. THIS IS CURRENTLY A WORK IN PROGRESS
Part: UNKNOWN — FUMES (CABIN) · airframe 36,876 hrs · 23,855 cycles
2 MINUTES AFTER TAKEOFF RECEIVED A CALL FROM FA THAT THE AFT CABIN HAD FUMES/VERY LIGHT SMOKE EMITTING FROM THE OVERHEAD VENTS. BLEEDS OPEN TAKEOFF. QRH CLEARED FUMES. NO EICAS MSGS. (FLIGHT 5402 FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS.
Part: UNKNOWN — FUMES (CABIN) · airframe 36,886 hrs · 23,864 cycles
2 MINUTES AFTER TAKEOFF RECEIVED A CALL FROM FA THAT THE AFT CABIN HAD FUMES/VERY LIGHT SMOKE EMITTING FROM THE OVERHEAD VENTS. BLEEDS OPEN TAKEOFF. QRH CLEARED FUMES. NO EICAS MSGS. (FLIGHT 5402 FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 28207637 WITH THE FOLLOWING CORRECTIVE ACTION: "SEE THE FOLLOWING CAMPS FOR WORK PERFORMED:CP 28207871- FOR FIM TASK 21-22-00-810-806-A01.CP 28209696- FOR FDR DOWNLOAD.CP 28211502- FOR LH ENGINE BORESCOPE AFT OF THE FAN DISK AND INTO THE COMPRESSOR.CP 28211503- FOR LH ENGINE BORESCOPE AROUND THE A SUMP AND #1 BEARING HOUSING.CP 28211504- FOR RH ENGINE BORESCOPE AROUND THE A SUMP AND #1 BEARING HOUSING.CP 28211507- FOR RH ENGINE BORESCOPE AFT OF THE FAN DISK AND INTO THE COMPRESSOR.CP 28211554- FOR INSPECTION OF CONDESER/REHEATER UNIT FOR SIGNS OF OIL FOULING.CP 28211556- FOR INSPECTION OF THE THREE FWD, PIPE ASSEMBLIES FROM THE LH DUAL HEAT EXCHANGER.CP 28211558- FOR BORESCOPE INSPECTION OF THE DUAL HEAT EXCHANGER BLEED AIR INLET.CP 28211559- FOR INSPECTION OF LH WATER EXTRACTOR,SWIRL VANES, INLET HOUSING, CENTER HOUSING AND ENTRANCE TO THE ANNULAR SLOT FOR ANY SIGNS OF DEFECTS.CP 28211560- FOR INSPECTION OF THE LH ACM WATER DRAIN LINES FOR ANY DEFECTS.
Earlier reports · 2012–2022 · 112 reports
2022
Part: NONE — DAMAGED · airframe 32,691 hrs · 20,370 cycles
LEFT WINDSHIELD OUTER MOST PAIN SHATTERED IN FLIGHT (FLIGHT 5702 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 24366878 WITH THE FOLLOWING CORRECTIVE ACTION: "SEE CP 24369201-1 FOR REMOVAL OF LH WINDSHIELD. INSTALLED SERVICEABLE CA SIDE WINDSHIELD IN REF TO AMM 56-11-01. COMPLIED WITH TASK CARD 56-220-1000-SKY."
2021
Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 31,425 hrs · 19,452 cycles
NOTICEABLE CRACKING IN THE UPPER RIGHT CORNER AND TO A LESSER EXTENT IN THE LOWER LEFT CORNER OF THE RIGHT SIDE WINDSHIELD. PRESSURIZATION WAS NORMAL DURING FLIGHT. (FLIGHT 4743 - FILED CLOSED) REMOVED AND REPLACED FO'S WINDSHIELD, OPS CHECK GOOD OF WINDSHIELD HEAT REF AMM 56-11-01 PLEASE REFERENCE AML 683210 FOR LEAK CHECK. / TORQUE WRENCH S/N 0314802753 CAL DUE 12/2021
Part: WINDSHIELD — CRACKED (LT COCKPIT) · airframe 30,566 hrs · 18,896 cycles
LEFT WINDOW CRACKED FLIGHT 5344 - FILED CLOSED REMOVED AND REPLACED THE CAPTAIN'S SIDE WINDOW WITH A SERVICEABLE UNIT REF AMM 56-12-01 AND TASK CARD 56-220-1000-SKY. NEW CAPTAIN'S SIDE WINDOW OPS AND LEAK CHECK GOOD AT THIS TIME.
2020
Part: STRIP — CORRODED · airframe 29,833 hrs · 18,425 cycles
JOINER STRIP BETWEEN PANELS 195DL AND 195DR CORRODED. C-CHECK RO 9/20/2020. EVALUATED FAIRING JOINT STRAP BETWEEN PANELS 195DL AND 195DR, 100% MATERIAL LOSS, OUT OF LIMITS. FABRICATED NEW JOINT STRAP, REF BOMBARDIER. REMOVED CORRODED STRAP INSD INSTALLED NEWLY FABRICATED STRAP, REF CRJ 700 SRM. SEE CONTINUATION CARD FOR DETAILS.
Part: MOUNT — DAMAGED (SEAT 15AB) · airframe 29,833 hrs · 18,425 cycles
SEAT 15AB HAS A MISSING SEAT TRACK MOUNT ON THE FWD INBOARD SIDE, MARKED. C-CHECK RO 9/20/2020. INSTALLED NEW SEAT TRACK MOUNT (STUD ASSY FRONT) P/N 41581161-501, REF CRJ 700 CMM. SEE CONTINUATION CARD FOR DETAILS.
Part: MOUNT — DAMAGED (SEAT 20AB) · airframe 29,833 hrs · 18,425 cycles
SEAT 20AB HAS A MISSING SEAT TRACK MOUNT ON THE INBOARD AFT SIDE, MARKED. C-CHECK RO 9/20/2020. REMOVED AND INSTALLED NEW SEAT TRACK MOUNT P/N 41581074-505 PO T52686 /31 INBOARD AFT SIDE ON SEAT 20AB, REF ZODIAC AEROSPACE CMM.
Part: PANEL — DAMAGED (BS 364-379) · airframe 29,833 hrs · 18,425 cycles
THE LT FLOOR SILL HAS TWO DECOMPRESSION PANELS WITH TORN OR MISSING DIAPHRAGMS. THE FIRST IS LOCATED BETWEEN FS 364 AND FS379 AND THE SECOND IS LOCATED BETWEEN FS 453 AND FS 469 THAT REQUIRED REBULID TO INSTALL NEW DIAPHRAGMS. C-CHECK RO 9/20/2020. REMOVED AND REPLACED DAMAGED DECOMPRESSION PANELS 2 EA TORN DIAPHRAGMS LOCATED BETWEEN FS 364-FS 379 AND FS 453-FS 469. DRILLED AND INSTALLED NEW DIAPHRAGM AND RIVETS 10 EA AND EACH PANEL, REF CRJ 700 SRM.
Part: ANGLE — CORRODED · airframe 29,833 hrs · 18,425 cycles
FWD CAP ANGLE AT STGR 18L IS CORRODED. C-CHECK RO 9/20/2020. REMOVED AND REPLACED FWD CAP ANGLE AT STGR 18L, IAW CRJ700 SRM.
Part: HINGE FITTING — CORRODED (NLG DOOR) · airframe 29,833 hrs · 18,425 cycles
AFT NLG DOOR RT HINGE MOUNT CORRODED. C-CHECK RO 9/20/2020. REMOVED DAMAGED RT NLG DOOR FITTING, REF CRJ-700 SRM. INSTALLED NEW LT HINGE FITTING P/N CC670-32212-7, REF CRJ-700 SRM AND DRAWING. C/W SKYWEST ST STRUCTURE MAJOR REPAIR. SEE CONTINUE CARD FOR DETAILS.
Part: HINGE FITTING — CORRODED (NLG DOOR) · airframe 29,833 hrs · 18,425 cycles
AFT NLG DOOR LT HINGE MOUNT CORRODED. C-CHECK RO 9/20/2020. REMOVED DAMAGED LT NLG DOOR FITTING, REF: CRJ-700 SRM. INSTALLED NEW LT HINGE FITTING P/N CC670-32212-7, REF CRJ-700 SRM AND DRAWING. C/W SKYWEST ST STRUCTURE MAJOR REPAIR. SEE CONTINUE CARD FOR DETAILS.
Part: ANGLE — CORRODED · airframe 29,833 hrs · 18,425 cycles
LOWER SILL ANGLE PART NUMBER SH670-31986-1 EVIDENCE OF CORROSION. C-CHECK RO 9/20/2020. REPLACED LOWER SILL ANGLE P/N SH670-31986-1, REF DWG AND CRJ-700 SRM. COMPLIED WITH SKYWEST TASK CARD.
Part: ANGLE — CORRODED · airframe 29,833 hrs · 18,425 cycles
AFT CAP ANGLE AT STGR 18L IS CORRODED. C-CHECK RO 9/20/2020. REMOVED AND REPLACED AFT CAP ANGLE AT STGR 18L, IAW CRJ700 SRM.
Part: PANEL — CRACKED (LT MLG WW) · airframe 29,833 hrs · 18,425 cycles
LEFT MAIN GEAR WHEEL WELL PANEL ATTACHED WING TO FUSELAGE FAIRING MOUNTING STRUCTURE ON THE BOTTOM OF THE CENTER WING IS CRACKED FS 693.00-FS 702.00, FLAGGED. C-CHECK RO 9/20/2020. REMOVED AND REPLACED WITH NEW PART FAIRING MOUNTING STRUCTURE. COMPLIED WITH CRJ-700 SRM.
Part: ANCHOR FITTING — CORRODED (PAX DOOR) · airframe 29,833 hrs · 18,425 cycles
PASSENGER DOOR FORWARD ANCHOR FITTING HAS CORRODED HARDWARE, MARKED. C-CHECK RO 9/20/2020. INSTALLED NEW HARDWARE ON FORWARD ANCHOR FITTING ON PAX DOOR, REF CRJ 700 SRM.
Part: ANGLE — CORRODED (BS 319) · airframe 29,833 hrs · 18,425 cycles
PAX DOOR CLIP AT FS 319 DD4 HAS CORROSION. C-CHECK RO 9/20/2020. REMOVED AND REPLACED PAX DOOR CLIP AT FS 319 DD4, REF DWG AND CRJ 700 SRM. COMPLIED WITH SKYWEST TASK CARD.
Part: MOUNT — CORRODED (BS 295) · airframe 29,833 hrs · 18,425 cycles
THE FWD INBOARD FLOOR MOUNT FITTING ATTACHED TO THE FLOOR SUPPORT CROSSBEAM FS 295 LOCATED APPROX LBL 20 HAS CORROSION ON ITS UPPER SURFACE, MARKED WITH ORANGE FLAG TAPE. C-CHECK RO 9/20/2020. REPLACED FLOOR MOUNT FITTING WITH NEW FROM STOCK, REF CRJ 700 SRM AND DWG.
Part: ANGLE — CORRODED (BS 313) · airframe 29,833 hrs · 18,425 cycles
PAX DOOR CLIP AT FS313, DD4 HAS CORROSION. C-CHECK RO 9/20/2020. REMOVED AND REPLACED PAX DOOR CLIP AT FS 313 DD4, REF DWG AND CRJ 700 SRM. COMPLIED WITH SKYWEST TASK CARD.
Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 29,833 hrs · 18,425 cycles
PAX DOOR INTERCOSTAL DD1 P/N 601R31902-318 IS CRACKED. C-CHECK RO 9/20/2020. REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD1 WITH NEW PN 601R31908-318 BETWEEN FS 339-FS 347 REF DRAWING AND CRJ700 SRM. C/W SKYWEST ST STRUCTURAL MAJOR REPAIR. SEE CONTINUATION CARD FOR DETAILS.
Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 29,833 hrs · 18,425 cycles
PAX DOOR INTERCOSTAL DD5 P/N 601R31902-317 IS CORRODED. C-CHECK RO 9/20/2020. REPLACED PAX DOOR INTERCOSTAL WITH NEW FROM STOCK, REF DWG CRJ 700 SRM. COMPLIED WITH SKYWEST TASK CARD. LEAK CHECKS GOOD.
Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 29,833 hrs · 18,425 cycles
PAX DOOR INTERCOSTAL DD6 P/N 601R318057-1 IS CORRODED. C-CHECK RO 9/20/2020. REMOVED AND REPLACED PAX DOOR INTERCOSTAL WITH NEW PN 601R18057-1 AT DD6 BETWEEN FS 320-FS 339, REF DRAWING AND CRJ700 SRM. C/W SKYWEST ST STRUCTURAL MAJOR REPAIR. SEE CONTINUATION CARD FOR DETAILS.
Part: INTERCOSTAL — CORRODED (PAX DOOR FRAME) · airframe 29,833 hrs · 18,425 cycles
PAX DOOR INTERCOSTAL DD4 P/N 601R31902-317 IS CORRODED. C-CHECK RO 9/20/2020. REPLACED PAX DOOR INTERCOSTAL WITH NEW FROM STOCK, REF DWG CRJ 700 SRM. COMPLIED WITH SKYWEST TASK CARD. LEAK CHECKS GOOD.
Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 29,833 hrs · 18,425 cycles
REPAIR CRACK NOTED IN AFT RT VERTICAL STABILIZER DRAG ANGLE. C-CHECK RO 9/20/2020. COMPLIED WITH REPAIR OF RT VERTICAL STAB DRAG ANGLE, REF CRJ-700 SRM. COMPLIED WITH SKYWEST TASK CARD.
Part: STRUCTURE — DAMAGED (BS 1000-1015) · airframe 29,833 hrs · 18,425 cycles
WING TO FUSELAGE 196DR FAIRING ATTACH HOLE ELONGATED LOCATED BETWEEN FS 1000-FS 1015 AT STGR 25R, MARKED. C-CHECK RO 9/20/2020. COMPLIED WITH REPAIR OF ELONGATED HOLE, REF REO.
Part: PROTECTOR — CORRODED (GALLEY FLOOR) · airframe 29,833 hrs · 18,425 cycles
GALLEY DOOR LOWER SILL FWD WEB FLOOR PROTECTOR HAS EVIDENCE OF CORROSION. C-CHECK RO 9/20/2020. REMOVED AND REPLACED SERVICE DOOR FLOOR PROTECRTOR WITH NEW ONE, REF CRJ-700 SRM AND DWG. COMPLIED WITH TASK CARD.
Part: SEAT FRAME — CORRODED (BS 485-581) · airframe 29,833 hrs · 18,425 cycles
EVALUATE CORROSION ON LEFT FLOOR SEAT TRACK FROM FS 485-581, MARKED. C-CHECK RO 9/20/2020. REMOVED CORRODED SEAT TRACK AND INSTALLED NEW SEAT TRACK WITH NEW HARDWARE ON FLOOR BEAM AT LBL 9 BETWEEN FS 485 AND FS 581, REF CRJ700 AMM.
Part: SEAT TRACK — CORRODED (BS 677-863) · airframe 29,833 hrs · 18,425 cycles
EVALUATE CORROSION ON LEFT FLOOR SEAT TRACK FROM FS 677-863, MARKED. C-CHECK RO 9/20/2020. REMOVED CORRODED SEAT TRACK AND INSTALLED NEW SEAT TRACK WITH NEW HARDWARE ON FLOOR BEAM AT LBL 9 BETWEEN FS 677 AND FS 863, REF CRJ700 AMM.
Part: MOUNT — CORRODED (FWD CARGO) · airframe 29,833 hrs · 18,425 cycles
FWD BAGG FS 533 BETWEEN STGRS 22L-23L MOUNT PLATE CORRODED. C-CHECK RO 9/20/2020. REPAIRED FWD BAGG FS 533 BTWN STGRS 22L-23L MOUNT PLATE. COMPLIED WITH ALL STEPS OF REO.
Part: ANGLE — CORRODED (PAX DOOR FRAME) · airframe 29,833 hrs · 18,425 cycles
PASSENGER DOOR SURROUND STRUCTURE-MID CAP ANGLE ATTACHED TO LOWER SILL IS CORRODED. C-CHECK RO 9/20/2020. REMOVED AND REPLACED PASSENGER DOOR MID CAP ANGLE, IAW CRJ700 SRM. C/W CRJ700 SRM DWG. COMPLIED WITH TASK CARD.
Part: FLOOR SUPPORT — CORRODED (BS 349) · airframe 29,833 hrs · 18,425 cycles
THE RT FLOOR SILL AT APPROX FS 349 HAS CORROSION AT MULTIPLE LOCATIONS, MARKED WITH BLACK GREASE PENCIL. C-CHECK RO 9/20/2020. EVALUATED RT FLOOR SILL AT APPROX FS 349 END OF SILL BROKEN OFF AT FWD FASTENER HOLES, OUT OF LIMITS. REMOVED AND REPLACED RT FLOOR SILL AT APPROX FS 349 REFERENCING APPLICABLE STEPS OF REO COMPLETED.
Part: PLATE — CORRODED (BS 549-565) · airframe 29,833 hrs · 18,425 cycles
FWD BAGG MOUNTING PLATE STGR 24R-25R BETWEEN FS 549-565 CORRODED AS MARKED. C-CHECK RO 9/20/2020. REPLACED MOUNTING PLATE WITH NEW P/N SH670-33852-1, REF CRJ 700 SRM AND BOMBARDIER INC DWG.
Part: INTERCOSTAL — CORRODED (BS 394-409) · airframe 29,833 hrs · 18,425 cycles
A BAY DOOR SURROUND INTERCOSTAL CORRODED BETWEEN FS 394-409 INBOARD OF STGR 26L, AS MARKED. C-CHECK RO 9/20/2020. REPLACED INTERCOSTAL WITH NEW INTERCOSTAL PN SH670-32075-4 INBOARD OF STRG 26L FS 394.00 TO FS 409.00, REF CRJ700 SRM AND DRAWING. C/W SKYWEST ST STRUCTURAL MAJOR REPAIR.
Part: MOUNT — CORRODED (FWD CARGO) · airframe 29,833 hrs · 18,425 cycles
FWD BAGG FS 533 MOUNT PLATE BETWEEN STGRS 27-26L CORRODED. C-CHECK RO 9/20/2020. REMOVED CORROSION ON MOUNT PLATE AT FS 533 BETWEEN STGR 27& 26L WHERE MARKED, REF CRJ700 SRM 51-12-00-001-001-A01. OUT OF LIMITS ORIGINAL MATERIAL THICKNESS: 0.240?, REF DWG SH670-33389 REV NC NR 1 L:0.158" W: 0.155" D:0.007"; NR 2 L:0.510" W:0.362" D:0.017"; NR 3 L:0.443" W:0.170" D:0.017"; NR 4 L:0.168" W:0.107" D:0.015"; NR 5 L:0.845" W:0.257" D:0.019" NO DAMAGE ALLOWED ON FITTINGS, REF CRJ700 SRM. MANUALLY MEASURED DIAL DEPTH GAUGE. REPLACED MOUNT PLATE/MACHINED BRACKET PN SH670-33389-1, REF DRAWING CRJ700 SRM. SEE CONTINUE CARD FOR DETAILS.
Part: DOOR SILL — CORRODED · airframe 29,833 hrs · 18,425 cycles
GALLEY DOOR LOWER SILL ANGLE HAS EVIDENCE OF CORROSION. C-CHECK RO 9/20/2020. REMOVED AND REPLACED GALLEY DOOR LOWER SILL ANGLE WITH A NEW ONE, REF CRJ-700 SRM AND DWG. COMPLIED WITH TASK CARD.
Part: DOUBLER — CORRODED (BS 536) · airframe 29,833 hrs · 18,425 cycles
FWD BAGG FS 536 STGR 25L-26L BUTTERFLY DOUBLER CORRODED AS MARKED. C-CHECK RO 9/20/2020. REMOVED CORROSION ON BUTTERFLY DOUBLER AT FS 536 STGR 25L-26L WHERE MARKED, REF CRJ700 SRM. OUT OF LIMITS ORIGINAL MATERIAL THICKENS: 0.063;? MOST MATERIAL REMOVED: 0.018" (MANUALLY MEASURED TUC 8531 DUE 31-OCT-20); LEAST MATERIAL REMAINING: 0.045? ALLOWABLE: 10% (0.006), REF CRJ700 SRM. FABRICATED NEW DOUBLER P/N 2024T-3 .080 P.O T55606 FWD CARGO BAY AT FS 536 STGR 25L-26L AND LOCATED HOLES OUT TO NR 30, REF DWG. INSTALLED NEW BUTTERFLY DOUBLER, REF DRAWING SRM. C/W ST CARD STRUCTURAL MAJOR REPAIR (RII). SEE CONTINUE CARD FOR DETAILS.
Part: PLATE — CORRODED (BS 581) · airframe 29,833 hrs · 18,425 cycles
FWD BAGG FS 581 MOUNT PLATE BETWEEN STGRS 22L-23L CORRODED. C-CHECK RO 9/20/2020. REPLACED MOUNTING PLATE WITH NEW P/N SH670-33390-2 AT FS 581.00 BETWEEN STGR 22L AND STGR 23L, REF CRJ 700 SRM AND BOMBARDIER INC DWG.
Part: SEAT FRAME — CORRODED (BS 349-477) · airframe 29,833 hrs · 18,425 cycles
THE CABIN FLOOR SEAT TRACK ON RBL 9 BETWEEN APPROX FS 349 AND APPROX FS 477 HAS SCRATCHES AND CORROSION. C-CHECK RO 9/20/2020. CABIN FLOOR SEAT TRACK AT RBL 9 BETWEEN FS 349 AND FS 477. REMOVED AND REPLACED WITH NEW PART AND NEW HARDWARE, REF CRJ700 AMM.
Part: FLOOR SUPPORT — CORRODED (BS 280-310) · airframe 29,833 hrs · 18,425 cycles
THE LT FLOOR SILL BETWEEN FS 280 AND FS 310 HAS CORROSION AROUND ITS NUTPLATES, MARKED WITH BLACK GREASE PENCIL. C-CHECK RO 9/20/2020. BLENDED OUT CORROSION ON LT SILL BETWEEN FS 280-FS 310, REF CRJ700 SRM. MATERIAL THICKNESS IS WITHIN LIMITS, REF CRJ700 SRM AND DWG. SEE CONTINUATION CARD FOR DETAILS.
Part: DOOR SILL — CORRODED · airframe 29,833 hrs · 18,425 cycles
PASSENGER DOOR LOWER SILL ANGLE HAS EVIDENCE OF CORROSION. C-CHECK RO 9/20/2020. REMOVED AND REPLACED PASSENGER DOOR LOWER SILL, IAW CRJ700 SRM DWG AND COMPLIED WITH ST.
Part: POST — CORRODED (BS 280) · airframe 29,833 hrs · 18,425 cycles
LT FS 280.00 POST AT LBL 11.0 IS CORRODED ABOVE FS 280.00 CROSSBEAM. C-CHECK RO 9/20/2020. COMPLIED WITH REPAIR OF LT FS 280.00 POST, REF CRJ-700 SRM. COMPLIED WITH SKYWEST TASK CARD.
Part: SEAT SPRING — CORRODED (BS 364-477) · airframe 29,833 hrs · 18,425 cycles
THE CABIN FLOOR SEAT TRACK ON LBL 9 BETWEEN APPROX FS 364 AND APPROX FS 477 HAS SCRATCHES AND CORROSION. C-CHECK RO 9/20/2020. REMOVED CORRODED SEAT TRACK AND INSTALLED NEW SEAT TRACK WITH NEW HARDWARE ON FLOOR BEAM AT LBL 9 BETWEEN FS 364 AND FS 477, REF CRJ700 AMM.
Part: BRACKET — CORRODED (BS 533) · airframe 29,833 hrs · 18,425 cycles
FS 533 NUTPLATE BRACKET EXTENDING AFT AT STGR 27 CORRODED. C-CHECK RO 9/20/2020. REMOVED CORROSION ON NUTPLATE BRACKET EXTENDING AFT OF FS 533 AT STGR 27, REF CRJ 700 SRM 51-12-00-001-001-A01. OUT OF LIMITS ORIGINAL MATERIAL THICKENS: 0.050, REF CRJ700 SRM 53-32-58-001-001-A01. MATERIAL REMOVED: 0.009" (MANUALLY MEASURED TUC8531 DUE 31-OCT-20) REMAINING MATERIAL : 0.049´ NO DAMAGE ALLOWED, REF CRJ700 SRM53-32-58-101-001-A01. FABRICATED NEW NUTPLATE BRACKET P/N:SH670-33376-3 OUT OF 0.050´ 2024-T3 PO NR T000054674, REF DWG & CRJ700 SRM. INSTALLED NEW NUT PLATE BRACKET PN SH670-33376-3 AT FS 533.00 STRG 27, REF CRJ700 SRM AND DRAWING. SEE CONTINUE CARD FOR DETAILS.
Part: PLATE — CORRODED (BS 549-565) · airframe 29,833 hrs · 18,425 cycles
FWD BAGG MOUNTING PLATE AT STGR 26L TO 27 BETWEEN FS 549-565 CORRODED AS MARKED. C-CHECK RO 9/20/2020. FWD BAGG MOUNTING PLATE AT STGR 26L TO 27 BETWEEN FS 549-565 REPLACED WITH NEW, REF REO. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH TASK CARD.
Part: SEAT FRAME — CORRODED (BS 485-581) · airframe 29,833 hrs · 18,425 cycles
EVALUATE CORROSION ON RIGHT FLOOR SEAT TRACK FROM FS 485-581, MARKED. C-CHECK RO 9/20/2020. CABIN FLOOR SEAT TRACK AT RBL 9 BETWEEN FS 485 AND FS 581. REMOVED AND REPLACED WITH NEW PART AND NEW HARDWARE, REF CRJ700 AMM.
Part: STRINGER — CORRODED (BS 333-349) · airframe 29,833 hrs · 18,425 cycles
A BAY DOOR SURROUND STGR 26L CORRODED BETWEEN FS 333-349, AS MARKED. C-CHECK RO 9/20/2020. REMOVE & REPLACED STGR 26L WITH NEW P/N SH670-31372-3S, BETWEEN FS 333-FS 364, REF DWG & CRJ700 SRM. COMPLIED WITH SKYWEST TASK CARD. SEE CONTINUE CARD FOR DETAILS.
Part: STRINGER — CORRODED (BS 333-349) · airframe 29,833 hrs · 18,425 cycles
A BAY DOOR SURROUND STGR 26R CORRODED BETWEEN FS 333-349, AS MARKED. C-CHECK RO 9/20/2020. REPLACED STRINGER WITH NEW FROM STOCK, REF BOMBARDIER DWG CRJ700 SRM. COMPLIED WITH SKYWEST TASK CARD.
Part: MOUNT — CORRODED (BS 581) · airframe 29,833 hrs · 18,425 cycles
FWD BAGG FS 581 MOUNT PLATE EXTENDING AFT BETWEEN STGRS 26L-27 CORRODED. C-CHECK RO 9/20/2020. REPLACED MOUNTING PLATE WITH NEW AT FS 581.00 BETWEEN STGR 26L AND STGR 27, REF CRJ 700 SRM AND BOMBARDIER INC DWG.
Part: NUT PLATE — CORRODED (FWD CARGO BAY) · airframe 29,833 hrs · 18,425 cycles
FWD BAGG NUTPLATE TAB/BRACKET CORRODED STGR25L, JUST FWD OF FS 533, AS MARKED. C-CHECK RO 9/20/2020. REMOVED CORROSION ON FWD BAGGAGE BAY NUT PLATE BRACKET FS 533.00 STRG 25L, REF CRJ700 SRM 51-12-00-001-001-A01. ORIGINAL MATERIAL IS 0.050 2024 T3 0.050, REF CRJ700 SRM 53-32-58-001-001-A01. MATERIAL REMOVED 0.013, REMAINING MATERIAL THICKNESS OF 0.037, NO DAMAGE ALLOWED, REF. CRJ700 SRM. REMOVED PLATE INSTALLED NEW PLATE, PER CRJ700 SRM AND DRAWING. SEE CONTINUATION CARD FOR DETAILS.
Part: NUT PLATE — CORRODED (BSA 581) · airframe 29,833 hrs · 18,425 cycles
FWD BAGG FS 581 NUTPLATE BRACKET EXTENDING FWD AT STGR 27 CORRODED. C-CHECK RO 9/20/2020. REMOVED CORROSION ON THE NUTPLATE BRACKET AT STGR 27 EXTENDING FWD OF FS 581 WHERE MARKED, REF CRJ700 SRM. ORIGINAL MATERIAL THICKENS: 0.050´, REF CRJ700 SRM. MOST MATERIAL REMOVED: 0.013" (MANUALLY MEASURED) NO DAMAGE ALLOWED, REF CRJ700 SRM. INSTALLED NEW NUT PLATE BRACKET, REF CRJ700 SRM AND DRAWING. INSTALLED 1EA MOUNTING CLIP AT FS 579.00 STRG 27, REF CRJ700 SRM AND 3EA NUT PLATES REF CRJ700 SRM DRAWING. SEE CONTINUE CARD FOR DETAILS.
Part: SEAT TRACK — CORRODED (BS 364-477) · airframe 29,833 hrs · 18,425 cycles
THE CABIN FLOOR SEAT TRACK ON LBL 27 BETWEEN APPROX FS 364 AND APPROX FS 477 HAS SCRATCHES AND CORROSION. C-CHECK RO 9/20/2020. REMOVED CORRODED SEAT TRACK AND INSTALLED NEW SEAT TRACK WITH NEW HARDWARE ON FLOOR BEAM AT LBL 27 BETWEEN FS 364 AND FS 477, REF CRJ700 AMM.
Part: FLOOR SUPPORT — CORRODED (BS 349-364) · airframe 29,833 hrs · 18,425 cycles
THE LT FLOOR SILL BETWEEN FS 349 AND FS 364 HAS CORROSION AT MULTIPLE LOCATIONS, MARKED WITH BLACK GREASE PENCIL. C-CHECK RO 9/20/2020. COMPLIED WITH REPAIR OF LT FLOOR SILL, REF BOMBARDIER REO.
Part: DOUBLER — CORRODED (BS 578) · airframe 29,833 hrs · 18,425 cycles
FWD BAGG FS 578 STGR 25L-26L BUTTERFLY DOUBLER CORRODED. C-CHECK RO 9/20/2020. REPLACE BUTTERFLY DOUBLER WITH NEW FROM STOCK, REF CRJ-700 SRM AND DRAWING.
Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 29,833 hrs · 18,425 cycles
LT FS 280.00 LOWER WEB IS CORRODED. C-CHECK RO 9/20/2020. REMOVED AND REPLACED LT FS 280 LOWER WEB AND LT FS 280 BUTTSTRAP, REFERENCE CRJ700 SRM. COMPLIED WITH TASK CARD.
Part: FLOOR SUPPORT — DAMAGED (BS 453-469) · airframe 29,833 hrs · 18,425 cycles
THE LT FLOOR SILL HAS TWO DECOMPRESSION PANELS WITH TORN OR MISSING DIAPHRAGMS. THE FIRST IS LOCATED BETWEEN FS 364 AND FS 379 AND THE SECOND IS LOCATED BETWEEN FS 453 AND FS 469. C-CHECK RO 9/20/2020. REMOVED AND REPLACED 2EA DECOMPRESSION PANELS LOCATED BETWEEN FS 364 AND FS 379 AND FS 453 AND FS 469, REF: CRJ 700 AMM & SRM.
Part: FLOOR SUPPORT — CORRODED (BS 280-319) · airframe 29,833 hrs · 18,425 cycles
THE RT FLOOR SILL BETWEEN FS 280 AND FS 319.7 IS CORRODED IN MULTIPLE LOCATIONS, MARKED WITH BLACK GREASE PENCIL. C-CHECK RO 9/20/2020. REPLACED FLOOR SILL SECTION FROM FS 280.00 TO FS 319.7 WITH NEW PART P/N-SH670-32172-7, REF CRJ-700 SRM & DRAWING. LEAK CHECK GOOD. COMPLIED WITH TASK CARD.
Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 29,833 hrs · 18,425 cycles
RT FS 280.00 LOWER WEB IS CORRODED. C-CHECK RO 9/20/2020. REMOVED AND REPLACED RT FS 280 LOWER WEB AND RT FS 280 BUTTSTRAP, REFERENCE CRJ700 SRM. COMPLIED WITH TASK CARD.
Part: FLOORBEAM — CORRODED (BS 295) · airframe 29,833 hrs · 18,425 cycles
THE FWD INBOARD FLOOR MOUNT FITTING ATTACHED TO THE FLOOR SUPPORT CROSSBEAM FS 295 FOR GALLEY NR 1 HAS CORROSION ON ITS UPPER SURFACE, MARKED WITH ORANGE FLAG TAPE. C-CHECK RO 9/20/2020. REMOVED AND REPLACED FITTING P/N SH670-32149-3 AT FS 280.00-FS 295.00 RBL 16.0, REF CRJ-700 SRM AND DRAWING.
Part: SEAT TRACK — CORRODED (BS 677-863) · airframe 29,833 hrs · 18,425 cycles
EVALUATE CORROSION ON RIGHT FLOOR SEAT TRACK FROM FS 677-863, MARKED. C-CHECK RO 9/20/2020. REMOVED CORRODED SEAT TRACK AND INSTALLED NEW SEAT TRACK WITH NEW HARDWARE ON FLOOR BEAM AT RBL 9 BETWEEN FS 677 AND FS 863, REF CRJ700 AMM.
Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 29,833 hrs · 18,425 cycles
A BAY DOOR SURROUND INTERCOSTAL BETWEEN STGRS 26L-27 CORRODED BETWEEN FS 349-364, AS MARKED. C-CHECK RO 9/20/2020. REPLACED INTERCOSTAL WITH NEW FROM STOCK, REF DWG SRM. SEE CONTINUATION CARD FOR DETAILS.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 29,833 hrs · 18,425 cycles
THE FS 280 LT CROSSBEAM HAS EVIDENCE OF CORROSION SPILLING OUT FROM UNDER ITS CORROSION CAP AROUND LBL 11, WHERE THE SEALANT HAS DISBONDED AND PUSHED OUT. C-CHECK RO 9/20/2020. REMOVED AND REPLACED LT FS 280 CROSSBEAM P/N CC670-34094-1S, REFERENCE CRJ700 SRM AND DWG. COMPLIED WITH SKYWEST TASK CARD.
Part: INTERCOSTAL — CORRODED (DOOR FRAME) · airframe 29,833 hrs · 18,425 cycles
A BAY DOOR SURROUND INTERCOSTAL BETWEEN STGRS 27-26R CORRODED BETWEEN FS 349-364, AS MARKED. C-CHECK RO 9/20/2020. REMOVED AND REPLACED INTERCOSTAL WITH NEW, PN SH670-32075-4, BETWEEN STRG 27 AND 26R FS 349.00 TO FS 364.00, REF CRJ700 SRM AND SKYWEST TASK CARD STRUCTURAL MAJOR REPAIR RII.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 29,833 hrs · 18,425 cycles
THE FS 280 RT CROSSBEAM HAS EVIDENCE OF CORROSION SPILLING OUT FROM UNDER ITS CORROSION CAP AROUND RBL 11, WHERE THE SEALANT HAS DISBONDED AND PUSHED OUT. C-CHECK RO 9/20/2020. REMOVED AND REPLACED RT FS280 CROSSBEAM P/N CC670-34094-2S, REFERENCE CRJ700 SRM AND DWG. COMPLIED WITH SKYWEST TASK CARD.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 29,833 hrs · 18,425 cycles
THE FS 280 COCKPIT FLOOR PANEL SUPPORT ANGLE, MOUNTED TO THE 280 CROSSBEAM, HAS MULTIPLE SPOTS OF CORROSION. C-CHECK RO 9/20/2020. BLENDED OUT CORROSION AND RESTORED FINISH TO FS 280.00 COCKPIT FLOOR SUPPORT ANGLE, REF: CRJ-700 SRM.
Part: DRIP TRAY — CORRODED (BS 280) · airframe 29,833 hrs · 18,425 cycles
THE FS 280 LT CROSSBEAM DRIP TRAY HAS CORROSION IN MULTIPLE LOCATIONS. C-CHECK RO 9/20/2020. REMOVED AND REPLACED FOR NEW FS 280.00 LT CROSSBEAM DRIP TRAY P/N BA670-31150-1SB, REF CRJ 700 SRM.
Part: BUSHING — FAILED (TORQUE LINK) · airframe 29,833 hrs · 18,425 cycles
NLG TORQUE LINK BUSHINGS AT THE CENTER APEX CONNECTON BETWEEN UPPER & LOWER TORQUE LINKS FAILED CLEARANCE CHECK. GAP EXCEEDS MAX ALLOWABLE GAP OF 0.012" MEASURED 0.019" WITH COMMON FEELER GAUGE, FLAGGED. C-CHECK RO 9/20/2020. REMOVED AND REPLACED NLG TORQUE LINK APEX BUSHINGS, PER CRJ700 AMM TASKS. GAP CHECK GOOD, PER CRJ700 AMM TASK.
Part: SKIN — CHAFED (BS 977) · airframe 29,833 hrs · 18,425 cycles
EVALUATE CHAFE ON THE SKIN AT STGR 27 JUST AFT OF FS 977, MARKED. C-CHECK RO 9/20/2020. COMPLIED WITH ALL STEPS A TO C, REF REO. REMOVED AND INSTALLED (3) NEW FASTENERS AND BLENDED OUT CHAFED IN SKIN BLEND DO NOT EXCEED THE MAX DEPTH OF 0.040", WITHIN LIMITS STEP B. SEE NDT REPORT IN ITEM 3, STEP C, RESTORE TO FINISH ON SKIN AT STGR 27 AFT OF FS 977.00 IN REWORKED AREA.
Part: SKIN — CORRODED (PAX DOOR) · airframe 29,833 hrs · 18,425 cycles
PAX DOOR INNER SKIN HAS NUMEROUS AREAS OF CORROSION AROUND ACCESS PANEL OPENINGS AND SEVERAL AREAS BELOW THE STAIR AREA, LOCATIONS MARKED. C-CHECK RO 9/20/2020. REPLACED PAX DOOR INNER SKIN, PER DRAWING 601R318024 REV -G CRJ 700 SRM. SEE CONTINUATION CARD FOR DETAILS.
Part: ATTACH FITTING — CRACKED (WNG-BDY FAIRING) · airframe 29,833 hrs · 18,425 cycles
RT WING-TO-BODY "ATTACH LINK" LOWER SPHERICAL BEAR "CRACKED". C-CHECK RO 9/20/2020. SERVICE BULLETIN, WINGS, CENTER WING PRIMARY STRUCTURE, DETAILED INSPECTION AND REPLACEMENT OF THE LEFT AND RIGHT REAR-SPAR LINK-ASSEMBLIES, PARTS A, B, & C, INCORPORATED.
Part: STRINGER — CHAFED (7 RIGHT) · airframe 29,833 hrs · 18,425 cycles
RT STGR 7R IS CHAFED FROM LOOSE WATER INJECTION TUBE IN AFT EQUIPMEMT COMP, LOCATION FLAGGED. C-CHECK RO 9/20/2020. BLENDED OUT DAMAGE AT STGR 7R AND INSTALLED NEW REPAIR ANGLE, PER REO. ALL STEPS COMPLIED WITH TASK CARD.
Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 29,833 hrs · 18,425 cycles
PAX DOOR INTERCOSTAL AT FWD CTR AREA, BELOW ACCESS PANEL 832DL HAS CORROSION, LOCATION MARKED. C-CHECK RO 9/20/2020. REPLACED INTERCOSTAL WITH NEW FROM STOCK, REF DWG 601R31702 REV-N CRJ 700 SRM. COMPLIED WITH SKYWEST TASK CARD. LEAK CHECKS GOOD.
Part: SKIN — DENTED (BS 1015-1036) · airframe 29,833 hrs · 18,425 cycles
FUSELAGE SKIN HAS NUMEROUS SMALL NICKS AND DENTS BELOW THE GRD AIR CONDITIONING ACCESS DOOR (182BR) FROM APPROX FS 1015 TO FS 1036 BETWEEN STGR 25R TO STGR 27. C-CHECK RO 9/20/2020. COMPLIED WITH REPAIR OF DAMAGED AREA, REF REO.
Part: TORQUE LINK — GOUGED (NLG) · airframe 29,833 hrs · 18,425 cycles
NLG UPPER TORQUE LINK TOP SIDE HAS 2EA "GOUGES" ONE ON LT RISE AND ONE ON RT RISE, MARKED. C-CHECK RO 9/20/2020. REPAIRED NLG UPPER TORQUE LINK, PER REO, SEE CONTINUATION CARD FOR DETAILS.
Part: SKIN — DENTED (BS 1038-1042) · airframe 29,833 hrs · 18,425 cycles
FUSELAGE SKIN HAS SEVERAL SMALL NICKS AFT OF THE GRD AIR CONDITIONING ACCESS DOOR (182BR) FROM APPROX FS 1038 TO FS 1042 BETWEEN STGR 23R TO BELOW STGR 24R. C-CHECK RO 9/20/2020. COMPLIED WITH REPAIR OF DAMAGED AREA, REF REO.
Part: SUPPORT BRACKET — BROKEN (INJECTION TUBE) · airframe 29,833 hrs · 18,425 cycles
RT WATER INJECTION TUBE IN AFT EQUIPMENT COMP HAS 2 EA BROKEN SUPPORT BRACKETS, LOCATIONS FLAGGED. C-CHECK RO 9/20/2020. REMOVED 2 EA DAMAGED BRACKETS. LOCATED AND DRILLED, CRJ-700 SRM. INSTALLED BRACKET P/N MM670-97111-006, REF AND CRJ-700 SRM AND DRAWING.
Part: MOUNT — CRACKED (ASSIST MOTOR) · airframe 29,833 hrs · 18,425 cycles
PAX DOOR ASSIST MOTOR MOUNT ANGLE IS CRACKED (UPPER ANGLE WHEN DOOR IS CLOSED), LOCATION IS MARKED. C-CHECK RO 9/20/2020. REMOVED AND REPLACED PAX DOOR ASSIST MOTOR MOUNT ANGLE P/N 601R317745-7, REF CRJ 700 SRM.
Part: INTERCOSTAL — CHAFED (BS 1144-1154) · airframe 29,833 hrs · 18,425 cycles
INTERCOSTAL IN AFT EQUIPMENT COMPARTMENT IS CHAFED AT STGR 9R, LOCATION FLAGGED. C-CHECK RO 9/20/2020. BLENDED OUT DAMAGE AND RESTORED FINISH TO STGR 9R FS 1144.00-FS 1154.48, PER REO. ALL STEPS COMPLIED WITH.
Part: STRINGER — CHAFED (BS 1144) · airframe 29,833 hrs · 18,425 cycles
LT STGR 7L IS CHAFED FROM LOOSE WATER INJECTION TUBE IN AFT EQUIPMENT COMP, LOCATION FLAGGED. C-CHECK RO 9/20/2020. EVALUATED CHAFE AT LT STGR 7L IN AFT EQUIPMENT COMPARTMENT AT FS 1144.00 TO FS 1162.00 AND FOUND STGR 7L TO BE OUT OF LIMITS, REF CRJ 700 SRM. PERFORMED REPAIR, PER REO. ALL STEPS OF REO HAVE BEEN COMPLETED. COMPLETED, SEE CONTINUATION CARD FOR DETAILS.
Part: CLAMP — DAMAGED (WIRE HARNESS) · airframe 29,833 hrs · 18,425 cycles
RT WING OUTBOARD TRAILING EDGE, FOUND (7) TOTAL DAMAGED/TORN/DETERIORATED, YELLOW ADEL CUSHION CLAMPS ON ELECTRICAL HARNESS. (2EA) BETWEEN WS 163.00 -170.63 JUST INBOARD OF RT OUTBOARD FLAP (INBOARD) ACTUATOR AND (5EA) BETWEEN THE TWO OUTBOARD MULT-FUNCTION SPOILER ACTUATORS (FLAGGED). C-CHECK RO 9/20/2020. REMOVED AND INSTALLED NEW 7 EA YELLOW ADEL CUSHION CLAMPS, REFERENCE CRJ700 AMM.
Part: ROD END — CORRODED (WING) · airframe 29,833 hrs · 18,425 cycles
ALL 4 ROD ENDS FOR FAIRING PANEL 193AB ARE CORRODED, MARKED. C-CHECK RO 9/20/2020. REMOVED & REPLACED ALL HARDWARE INCLUDING ROD ENDS AS REQUIRED, REF CRJ700 AMM, SEE CONTINUE CARD FOR DETAILS.
Part: RETAINER — BUCKLED (FWD CARGO DOOR) · airframe 29,833 hrs · 18,425 cycles
FWD BAG DOOR LOWER BOTTOM SEAL RETAINER BUCKLED IN SEVERAL PLACES. C-CHECK RO 9/20/2020. REMOVED DAMAGED FWD BAGGAGE BAY DOOR LOWER SEAL RETAINER AND INSTALLED NEW RETAINER P/N: LE670-39647-1, REF CRJ700 SRM.
Part: HINGE FITTING — GOUGED (FWD CARGO DOOR) · airframe 29,833 hrs · 18,425 cycles
FWD BAG BAY DOOR ATTACH HINGE ARM FWD ARM IS GOUGED ON SIDE FACE IN SEVERAL AREAS. C-CHECK RO 9/20/2020. BLEND OUTS PERFORMED TO A SMOOTH CONTOUR AT FWD CARGO BAY DOOR FWD HINGE ARM, REF-CRJ-700 MHIRJ REO, SEE CONTINUATION CARD FOR DETAILS.
Part: SPRING — LOOSE (FWD CARGO DOOR) · airframe 29,833 hrs · 18,425 cycles
FWD BAG BAY DOOR 4 EA COUNTERBALANCE SPRINGS LOOSE/CLICKING WHEN OPERATED. C-CHECK RO 9/20/2020. REMOVED 4 EACH FWD BAG BAY DOOR COUNTERBALANCE SPRINGS AND INSTALLED USING NEW HARDWARE, REF CRJ700 AMM. OPERATIONAL CHECKS GOOD.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 29,833 hrs · 18,425 cycles
RT OUTBOARD CLOSING RIB UNDER PANEL 343AR CRACKED. C-CHECK RO 9/20/2020. REPLACED FWD TIP FAIRING STRAP PN: AV670-23227-002 ON RT HORIZONTAL STAB, REF CRJ-700 SRM AND BOMBARDIER DWG.
Part: ROD END — BENT (PAX DOOR STEP) · airframe 29,833 hrs · 18,425 cycles
PAX DOOR BOTTOM STEP ROD END ASSY BENT, MARKED. C-CHECK RO 9/20/2020. REMOVED AND REPLACED PAX DOOR BOTTOM STEP LOWER ROD END WITH NEW HARDWARE, REF CRJ 700 SRM.
Part: FORMER — CORRODED (PAX DOOR) · airframe 29,833 hrs · 18,425 cycles
PASSENGER DOOR, CORROSION ON THE FORWARD FORMER 2 AREAS, MARKED. C-CHECK RO 9/20/2020. REMOVED AND REPLACED PAX DOOR FORMER WITH NEW, PN 601R318031-5 AT DD1 FS 311.75 REF DRAWING AND CRJ700 SRM. C/W SKYWEST ST STRUCTURAL MAJOR REPAIR, SEE CONTINUATION CARD FOR DETAILS.
Part: FLAP — DENTED (PAX DOOR HANDLE) · airframe 29,833 hrs · 18,425 cycles
PASSENGER DOOR OUTER DOOR HANDLE FLAP IS DENTED ON THE LOWER AFT CORNER, MARKED. C-CHECK RO 9/20/2020. COMPLIED WITH REPLACEMENT OF PAX DOOR OUTER HANDLE FLAP WITH NEW FROM STOCK, REF CRJ-700 SRM AND DWG.
Part: DRAG ANGLE — CRACKED (PAX DOOR STEPS) · airframe 29,833 hrs · 18,425 cycles
PASSENGER DOOR AFT STAIR WEB DRAG ANGLE CRACKED, MARKED. C-CHECK RO 9/20/2020. REPAIRED PASSENGER DOOR AFT STAIR WEB DRAG ANGLE. WET INSTALLED ALL REPAIR PARTS, REF CRJ 700 SRM.
Part: LATCH — WORN (RT NACELLE DOOR) · airframe 29,833 hrs · 18,425 cycles
THUMB LATCH TAB ON RIGHT LOWER TRANS COWL WORN, MARKED. C-CHECK RO 9/20/2020. REPLACED RT LOWER TRANSCOWL LATCH DOOR COAMING, PER REO SEE CONTINUATION CARD FOR DETAILS.
Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 29,833 hrs · 18,425 cycles
ON RT WING INBOARD FLAP, FLAP VANE LEADING EDGE PANEL (684ET) HAS GOUGE/CHAFE. C-CHECK RO 9/20/2020. REMOVED CHAFE ON PANEL 684ET, REF CRJ 700 SRM. EVALUATED BLENDED AREA ORGINAL THICKNESS .050" REMOVED .008" REMAINING .042". FOUND TO BE OUT OF LIMITS DUE TO THE FACT BLENDED OVER FASTENERS, REF CRJ 700 SRM. ORDERED AND RECEIVED NEW NEW PANEL. LOCATED AND DRILLED PER CRJ 700 SRM
Part: WEB — CORRODED (PAX DOOR STEP) · airframe 29,833 hrs · 18,425 cycles
PASSENGER DOOR CORROSION ON THE FORWARD STAIR WEB, MARKED. C-CHECK RO 9/20/2020. REMOVED AND REPLACED PASSENGER DOOR FORWARD STAIR WEB, REF CRJ 700 SRM.
Part: DRAG ANGLE — CRACKED (TAIL CONE) · airframe 29,833 hrs · 18,425 cycles
DURING ZONAL INSP OF TAIL CONE, FOUND "SUSPECTED" CRACK, IN LT DRAG ANGLE, AT 67.5% REAR SPAR AND VERTICAL STABILIZER INTERSECTION, TOP SIDE OF TAIL CONE, MARKED. C-CHECK RO 9/20/2020. COMPLIED WITH REPAIR OF LT DRAG ANGLE CRACK, REF CRJ-700 SRM. COMPLIED WITH SKYWEST TASK CARD.
Part: MOUNT — CORRODED (WINDSCREEN) · airframe 29,833 hrs · 18,425 cycles
RT WINDSCREEN INBOARD MOUNT FITTINGS ON FLOOR STRUCTURE IS CORRODED. C-CHECK RO 9/20/2020. REMOVED AND REPLACED RT WINDSCREEN INBOARD MOUNT FITTING, REF CRJ700 SRM.
Part: DRAG ANGLE — CRACKED (TAIL CONE) · airframe 29,833 hrs · 18,425 cycles
DURING ZONAL INSP OF TAIL CONE, FOUND "SUSPECTED" CRACK, IN RT DRAG ANGLE, AT 67.5% REAR SPAR AND VERTICAL STABILIZER INTERSECTION, TOP SIDE OF TAIL CONE, MARKED. C-CHECK RO 9/20/2020. COMPLIED WITH REPAIR OF RT DRAG ANGLE REF CRJ-700 SRM. COMPLIED WITH SKYWEST TASK CARD.
Part: SKIN — CHAFED (RUDDER LE) · airframe 29,833 hrs · 18,425 cycles
BOTH RUDDER LEADING EDGE SKINS "CHAFED", LT SIDE ALMOST THE ENTIRE LENGTH OF RUDDER AND THE RT SIDE FROM MIDDLE HINGE AREA DOWN, MARKED. C-CHECK RO 9/20/2020. RUDDER LEADING EDGE SKINS REPAIRED, PER REO SEE CONTINUATION CARD FOR DETAILS.
Part: MOUNT — CORRODED (WINDSCREEN) · airframe 29,833 hrs · 18,425 cycles
RT WINDSCREEN OUTBOARD MOUNT FITTINGS ON FLOOR STRUCTURE IS CORRODED. C-CHECK RO 9/20/2020. REMOVED AND REPLACED RT WINDSCREEN OUTBOARD MOUNT FITTING, REF CRJ700 SRM.
Part: STRUCTURE — ERODED (RIGHT) · airframe 29,833 hrs · 18,425 cycles
RT HORIZONTAL TIP (343AR) ERODED, LARGE AREAS OF COMPOSITE MATERIAL EXPOSED ON BOTH TOP AND BOTTOM SURFACES. C-CHECK RO 9/20/2020. REPAIRED RT HORIZONTAL TIP (343AR) WHERE HAS ERODED AREAS OF COMPOSITE MATERIAL ON BOTH TOP AND BOTTOM SURFACES USING EPOXY ADHESIVE, PER CRJ700 SRM TASK.
Part: SKIN — DENTED (PAX DOOR) · airframe 29,833 hrs · 18,425 cycles
1 SMOOTH DENT IN PASSENGER DOOR OUTER SKIN APROX 16" AF OF LEADING EDGE AND 12" FORM TOP. IF WITHIN ACCEPTABLE LIMITS OR REWORKED ELIMINATE EVIDENCE USING STANDARD PRACTICES. C-CHECK RO 9/20/2020. REPAIRED PAX DOOR EXTERNAL SKIN DENT PER REO. SEE CONTINUATION CARD FOR DETAILS.
Part: SKIN — DENTED (RT WING TE FLAP) · airframe 29,833 hrs · 18,425 cycles
COMPLY WITH SCHEDULED MAINTENANCE CODE: RA42654-SRM 57-52-01 784SK RT INBOARD FLAP-RI -FOUND DENT ON RT INBOARD FLAP ON UPPER SKIN 4.8" FROM TRAILING EDGE AND 23" FROM INBOARD EDGE OF FLAP. DENT IS WITHIN LIMITS, PER SRM 57-52-01. DENT MEASURES .065" DEEP AND .9" LONG. EVERY SUBSEQUENT 500 FH INSPECT AERODYNAMIC FILLER ON RT INBOARD FLAP UPPER SKIN LOCATED 4.8" FROM TRAILING EDGE AND 23" FROM INBOARD EDGE OF FLAP, PART NUMBER: CC670-14002-8-VANE ASSY, INBD FLAP RT, SERIAL NUMBER: 10284, POSITION: RIGHT. C-CHECK RO 9/20/2020. COMPLETED REPAIR ON RT INBOARD FLAP UPPER SKIN DENT, REF CRJ 700 SRM. COMPLETED, SEE CONTINUATION CARD FOR DETAILS.
2019
Part: SMOKE DETECTOR — FALSE INDICATION (AFT LAVATORY) · airframe 26,719 hrs · 16,224 cycles
SMOKE AFT LAV MASTER WARNING UPON DESCENT. REPOSITION FLIGHT. DECLARED EMERGENCY. (FLT#1360) INSPECTED AFT LAV. AREA FOR ANY DISCREPANCIES, ELECTRICAL BURNING SMELL. NO SIGNS OF SMOKE NOTED NO DEFECTS NOTED ALSO PERFORMED OPERATIONAL CK OF LAV SMOKE DETECTOR, OPS CK GOOD.NO SMOKE NOTED. NO MSGS NOTED. A/C OK TO CONTINUE SERVICE
2017
Part: FLOOR SUPPORT — CORRODED (BS 319) · airframe 22,205 hrs · 13,028 cycles
RIGHT SIDE BS 319.7 FLOOR SUPPORT HAS CORROSION. INSTALLED A NEW FLOOR SUPPORT FROM BS 280 TO 319.7 IAW REO AND SRM.
Part: FRAME — CORRODED (BS 319.7) · airframe 22,205 hrs · 13,028 cycles
CORROSION FOUND ON FRAME AT BS 319.7 BETWEEN STRINGERS 26L AND 26R. REPAIRED IAW REO. LEAK CHECKED GOOD
Part: FRAME — CORRODED (BS 310) · airframe 22,205 hrs · 13,028 cycles
CORROSION FOUND ON FRAME AT BS 310 BETWEEN STRINGERS 26L AND 26R. ACCOMPLISHED A PERMANENT REPAIR IAW REO. PERFORMED PRESSURE LEAK CHECK IAW AMM. CHECKED GOOD AT THIS TIME.
Part: DOOR SILL — CORRODED (AFT CARGO BAY) · airframe 22,205 hrs · 13,028 cycles
AFT CARGO DOOR SILL HAS CORROSION. INSTALLED A NEW CARGO DOOR SILL IAW SRM.
2015
Part: SKIN — DENTED (LT NACELLE) · airframe 17,434 hrs · 10,000 cycles
DENT ON LT ENGINE LOWER COWL JUST AFT OF THE FAN COWL, OUT OF LIMITS. REPAIRED IAW SRM.
Part: NONE — NONE (NONE) · airframe 16,860 hrs · 9,658 cycles
THE ACFT WAS BEING TOWED WHEN IT WENT OVER AN AREA OF ICE AND JACK-KNIFED. THE TUG STRUCK THE FUSELAGE CAUSING DAMAGE. GROUND TRANSFER, FO: 01/27/2015 CLOSED. FOUND PUNCTURE DAMAGE TO THE FWD FUSELAGE SKIN ON RT SIDE OF THE ACFT AT FS 379-FS 437 AND STR 16-STR 21. REPAIRED IAW REO.
2014
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 13,989 hrs · 8,098 cycles
CRACK FOUND AT FS 274 RT BULKHEAD. C CHECK REPAIRED CRACK AT FS 274.0 RT BULKHEAD IAW REO.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 13,989 hrs · 8,098 cycles
CRACK FOUND AT FS 274 LT BULKHEAD. C CHECK REPAIRED CRACK AT FS 274.0 LT BULKHEAD IAW REO.
Part: PANEL — CHAFED (TE FLAP) · airframe 13,989 hrs · 8,098 cycles
INBD FLAP PANEL 684GB IS CHAFED. C CHECK BLENDED CHAFE ON PANEL 684GB IAW SRM.
Part: ANGLE — CRACKED (PAX DOOR) · airframe 13,989 hrs · 8,098 cycles
PAX DOOR CRACK ON AFT SIDE OF DOOR, INNER SKIN ANGLE, ABOVE DOOR POWER ASSIST CABLE PULLEY BRACKET. C CHECK REPAIRED PAX DOOR CRACK ON AFT SIDE INNER SKIN ANGLE IAW REO.
2013
Part: A/C PACK — MALFUNCTIONED (AC BAY) · airframe 11,466 hrs · 6,716 cycles
SMOKE IN CABIN, PACKS WERE ON ENGINE BLEEDS, APU OFF. RIGHT ENGINE WAS RUNNING, LEFT ENGINE WAS OFF. SMOKE AND ODOR CONCENTRATED IN CABIN BUT ALSO NOTICEABLE IN COCKPIT. (FLT 5378) REPLACED RIGHT PACK IAW AMM. P/N ON: GG670-95009-3 P/N OFF: GG670-95009-5 S/N ON: 01090 S/N OFF: 01576
Part: OXYGEN MASK — UNSECURE (CABIN) · airframe 11,052 hrs · 6,475 cycles
OXYGEN MASK ON ROW 9 A/B DROPPED. (FLT 6470) RESTOWED OXYGEN MASK AT SEATS 9 A/B IAW AMM.
2012
Part: LIGHT — BROKEN (CABIN) · airframe 9,378 hrs · 5,483 cycles
EMERGENCY EXIT LIGHT AT GALLEY SERVICE DOOR IS BROKEN. (FLT 5172) REPLACED EMERGENCY EXIT LIGHT.
Part: ACM — MALFUNCTIONED (AC BAY) · airframe 8,796 hrs · 5,168 cycles
LEFT PACK SEIZED AND HAD SMOKE IN CABIN. (FLT 5214) REPLACED LEFT AIR CYCLE MACHINE IN REFERENCE TO MM. P/N OFF: GG670-95009-3 S/N OFF: 00729