N740SK
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.
194 reports on file, 2005-03-05 – 2023-12-19.
Part: TRACK — DAMAGED (UNKNOWN) · airframe 48,075 hrs · 31,541 cycles
DRILL STOP NOTED ON RHS FIXED LEADING EDGE TRACK 2-3 ON OUTBD RIB COMPLY WITH MHIRJ REO 670-57-41-519 (C-CHECK RO 1/19/2024) REPAIRED NOTED DAMAGE ON RHS FIXED LEADING EDGE TRACK 2-3 ON OUTBD RIB, CUT OUT DAMAGED AREA, NDT INSPECTED NO DEFECTS NOTED, INSTALLED REPAIR, APPLIED FINISH, COMPLIED WITH MHIRJ REO 670-57-41-519 REV -A DATED 2024-01-05 COMPLIED WITH SKYWEST M-337 FORM AND SKYWEST CARD # 51-900-1002-SKY, FOR COMPLETE DETAILS OF WORK PERFORMED SEE ATTACHED CONTINUATION CARD.
Part: SKIN — CORRODED (BS 801-847) · airframe 48,075 hrs · 31,541 cycles
FS801 - FS847 RH APRON SKIN TOP ROW SMOKING FASTENERS SHOWING SIGNS OF FRETTING CORROSION. (C-CHECK RO 1/19/2024) REMOVED 47EA SMOKING SOLID RIVETS & 2EA HI-LITE FASTENERS LOCATED ON THE RH APRON SKIN, TOP ROW BTWN FS.801-FS.847. REF. CRJ700 SRM 51-42-06-001-001-A01 & CRJ700 SRM 51-42-21-001-001-A01. PERFORMED REPAIR TO FS801 - FS847 RH APRON SKIN IAW ALL STEPS OF REO 670-53-42-071 REV--, DATED 2023-12-08. COMPLIED WITH TASK CARD 51-900-1002-SKY.
Part: SKIN — CORRODED (BS 801-847) · airframe 48,075 hrs · 31,541 cycles
FS801 - FS847 LH APRON SKIN TOP ROW SMOKING FASTENERS SHOWING SIGNS OF FRETTING CORROSION. (C-CHECK RO 1/19/2024) REMOVED 45EA SMOKING RIVETS LOCATED ON THE LH APRON SKIN, TOP ROW BTWN FS.801-FS.847. REF. CRJ700 SRM 51-42-06-001-001-A01. PERFORMED REPAIR TO FS801 - FS847 LH APRON SKIN IAW ALL STEPS OF REO 670-53-42-070 REV--, DATED 2023-12-08. COMPLIED WITH TASK CARD 51-900-1002-SKY.
Part: SKIN — GOUGED (CARGO DOOR) · airframe 48,075 hrs · 31,541 cycles
GOUGE ON FWD CARGO DOOR AREA, FUSELAGE SKIN AFT TOP CORNER. (C-CHECK RO 1/19/2024) REMOVED GOUGING FROM FWD CARGO DOOR AREA, FUSELAGE SKIN AFT TOP CORNER AND REPAIRED REF. REO 670-53-31-838 REV.-A DATED 2023-12-29 STEPS 1-7. COMPLIED WITH SKYWEST M-337 FORM AND SKYWEST TASK CARD 51-900-1002-SKY. SEE CONTINUATION CARD FOR WORK DETAILS.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 48,075 hrs · 31,541 cycles
FLOOR POST AT FS.280.00 AND RBL12 WL.72. CORRODED (FLAGGED). (C-CHECK RO 1/19/2024) REMOVED CORROSION ON FLOOR POST AT FS 280.00 RBL 12 REF CRJ 700 SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS. REF: CRJ-700 SRM 53-11-10-001-003-A01. REPAIRED REF CRJ700 SRM 53-11-10-201-006-A01.COMPLIED WITH 51-900-1002-SKY
Part: FLOORBEAM — CRACKED (BS 280) · airframe 48,075 hrs · 31,541 cycles
POSSIBLE CRACK ON COCKPIT FLOOR BEAM AT FS.280.00 AND RBL12.(FLAGGED). (C-CHECK RO 1/19/2024) REPAIRED COCKPIT FLOOR BEAM SECTION AT FS.280.00 AND RBL12 REF CRJ 700 SRM 53-11-43-201-003-A01. COMPLIED WITH 51-900-1002-SKY. SEE CONTINUATION CARD FOR WORK PERFORMED.
Part: FLOORBEAM — CRACKED (BS 280 LBL 12) · airframe 48,075 hrs · 31,541 cycles
COCKPIT FLOOR PANEL LANDING CRACKED AT FS.280.00 AND LBL12.(FLAGGED). (C-CHECK RO 1/19/2024) INSTALLED NEW COCKPIT FLOOR PANEL LANDING AT FS280 LBL 12 REF CRJ 700 SRM 51-42-06-001-001-A01 AND DWG.NO. CC670-33052 REV-G. COMPLIED WITH TASK CARD 51-900-1002-SKY
Part: FLOORBEAM — CRACKED (BS 280) · airframe 48,075 hrs · 31,541 cycles
COCKPIT FLOOR PANEL LANDING CRACKED AT FS.280.00 AND RBL12.(FLAGGED). (C-CHECK RO 1/19/2024) REMOVED AND INSTALLED NEW COCKPIT FLOOR PANEL LANDING AT FS.280.00 AND RBL12 REF CRJ 700 SRM 51-42-06-001-001-A01 / BOMBARDIER DWG CC670-33199 REV B. COMPLIED WITH TASK CARD 51-900-1002-SKY.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 48,075 hrs · 31,541 cycles
POSSIBLE CRACK ON COCKPIT FLOOR BEAM AT FS.280.00 AND LBL12.(FLAGGED). (C-CHECK RO 1/19/2024) REPAIRED COCKPIT FLOOR BEAM AT FS.280.00 AND LBL12. REF: CRJ-700 SRM 53-11-43-201-003-A01
Part: FLOORBEAM — CORRODED (BS 1031) · airframe 48,075 hrs · 31,541 cycles
L/H OTBD FLOOR BEAM @ FS1031.0 HAS CORROSION (TOP SIDE) (C-CHECK RO 1/19/2024) REPAIRED FLOOR BEAM WITH NEW SECTION AT (LH IB) LBL 27.0 BETWEEN FS1026.00 TO FS1038.00 REF: CRJ700 SRM 53-00-41-201-001-A01 AND REO 670-53-61-2218 REV-- DATED 2023-12-18 . COMPLIED WITH SKYWEST M-337 FORM AND SKYWEST STRUCTURAL REPAIR CARD 51-900-1002-SKY.
Part: FLOORBEAM — CORRODED (BS 1031) · airframe 48,075 hrs · 31,541 cycles
L/H INBD FLOOR BEAM @ FS1031.0 HAS CORROSION (TOP SIDE) (C-CHECK RO 1/19/2024) REPAIRED FLOOR BEAM WITH NEW SECTION AT (LH IB) LBL 9.0 BETWEEN FS1026.00 TO FS1038.00 REF: CRJ700 SRM 53-00-41-201-001-A01 AND REO 670-53-61-2218 REV-- DATED 2023-12-18 . COMPLIED WITH SKYWEST M-337 FORM AND SKYWEST STRUCTURAL REPAIR CARD 51-900-1002-SKY.
Part: BRACKET — CRACKED (RT NACELLE) · airframe 48,075 hrs · 31,541 cycles
R/H LWR TRANSCOWL OTBD "A" BRACKET IS CRACKED. (C-CHECK RO 1/19/2024) INSTALLED 1EA. NEW A-BRACKET P/N CN624-2082-201 ON R/H LOWER TRANS COWL, REF. REO 670-54-21-971, REV. B, DATED 2023-11-28. COMPLIED WITH SKYCARD 51-900-1002-SKY
Part: FLOORBEAM — CORRODED (BS 280) · airframe 48,075 hrs · 31,541 cycles
FLOOR PANEL LANDING COMMON TO THE FS,280.00 BEAM BETWEEN RBL12 AND LBL12 CORRODED (MARKED). (C-CHECK RO 1/19/2024) INSTALLED NEW FLOOR SUPPORT ANGLE ASSY. P/N CC670-34095 AT FS 280.00 BEAM BETWEEN LBL12 AND RBL 12 REF CRJ 700 SRM 51-42-06-001-001-A01, CRJ 700 SRM 51-42-21-001-001-A01 AND DWG. NO. CC670-34010 REV. K. COMPLIED WITH SKY WEST TASK CARD 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR
Part: FLOOR SUPPORT — CRACKED (BS 280) · airframe 48,075 hrs · 31,541 cycles
POSSIBLE CRACK ON FLOOR PANEL LANDING GUSSET COMMON TO THE FS,280.00 FLOOR BEAM AT RBL12 (MARKED) (C-CHECK RO 1/19/2024) REMOVED AND INSTALLED NEW COCKPIT FLOOR PANEL LANDING GUSSET AT FS.280.00 RBL12 REF CRJ 700 SRM 51-42-06-001-001-A01 / BOMBARDIER DWG CC670-33467 REV-NC COMPLIED WITH 51-900-1002-SKY
Part: FLOORBEAM — CRACKED (BS 280) · airframe 48,075 hrs · 31,541 cycles
POSSIBLE CRACK ON FLOOR PANEL LANDING GUSSET COMMON TO THE FS,280.00 FLOOR BEAM AT LBL12 (MARKED) (C-CHECK RO 1/19/2024) INSTALLED NEW COCKPIT FLOOR PANEL LANDING GUSSET AT FS280 LBL 12 REF CRJ 700 SRM 51-42-06-001-001-A01 AND DWG.NO. CC670-33052 REV-G COMPLIED WITHD TASKCARD 51-900-1002-SKY
Part: WINDSHIELD — CRACKED (COCKPIT LEFT) · airframe 48,075 hrs · 31,541 cycles
FLIGHT DECK L/H SIDE WINDSHIELD SIDE POST HAS CRACK BOTH INBOARD AND OUT BOARD SIDE OF UPPER MOST BARREL NUT LOCATION.VISIBLE. (C-CHECK RO 1/19/2024) REMOVED AND REPLACED FLIGHT DECK L/H SIDE WINDSHIELD SIDE POST WITH NEW REF. CRJ 700 SRM 51-42-21-001-001-A01, CRJ 700 SRM 51-45-00-001-001-A01 AND DWG CC670-33055 REV F. COMPLIED WITH SKYWEST M-337 FORM AND SKYWEST TASK CARD 51-900-1002-SKY. SEE CONTINUATION CARD FOR WORK DETAILS.
Part: SKIN — DENTED (BS 1000-1051) · airframe 48,075 hrs · 31,541 cycles
MULTIPLE DENTS, NICKS AND GOUGES ON AFT FUSELAGE FROM FS1000 TO FS1051, BETWEEN STRINGERS 21R-27 (C-CHECK RO 1/19/2024) REMOVED DAMAGED AREAS ON FUSELAGE SKIN BETWEEN FS1000 - FS1051, STGR21R - STGR27 REF CRJ700 SRM 51-12-00-001-001-A01. FOUND TO BE OUT OF LIMITS. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 670-53-61-2215 REV--, DATED 12/8/2023. COMPLIED WITH TASK CARD 51-900-1002-SKY.
Part: PLATE — CORRODED (BS 533) · airframe 48,075 hrs · 31,541 cycles
FORWARD BAGGAGE BAY DOOR SURROUND STRUCTURE FORWARD JOINT PLATE, FS533.00, HAS CORROSION AROUND FASTENERS. (MARKED) (C-CHECK RO 1/19/2024) REMOVED & REPLACED FORWARD BAGGAGE BAY DOOR SURROUND STRUCTURE FORWARD JOINT PLATE, AT FS533.00 REF CRJ700 SRM 51-42-21-001-001-A01, CRJ700 SRM 51-42-13-001-001-A01 REV 38 DATED: JUL 25/2020 AND DWG# SH670-33600 REV -AD. SEE CONTINUATION CARD FOR WORK ACCOMPLISHED. COMPLIED WITH TASK CARD 51-900-1002-SKY.
Part: REPAIR — CORRODED (BS 969-989) · airframe 48,075 hrs · 31,541 cycles
BOTH REPAIR PLATES UNDER SS PLATE ARE CORRODED. FS969.00 - FS989.00 STGR27. (MARKED) (C-CHECK RO 1/19/2024) EVALUATED. NO ALLOWABLE LIMITS FOR DAMAGE ON PREVIOUS REPAIR. REF CRJ700 SRM 51-13-02-001-001-A01. REMOVED AND INSTALLED NEW 1EA BOTTOM DOUBLER, 1 EA NEW TOP DOUBLER, 2 EA FILLER, 2 EA NEW TAPERED SHIMS AND 1EA NEW PROTECTIVE PLATE IN REF REO 670-53-00-290 REV -F DATED 2019-04-26 SOLUTION 1 (CRJ 700) STEP 24 TO 29. COMPLIED WITH TASK CARD 51-900-1002-SKY
Part: UNKNOWN — LEAKING (UNKNOWN) · airframe 48,054 hrs · 31,522 cycles
LOCATION AMARILLO TX. DIVERTED.LOSS OF HYD2. ALL FLUID GONE. (FLIGHT 4957 FILED OPEN)
Part: UNKNOWN — DENTED (UNKNOWN) · airframe 48,003 hrs · 31,477 cycles
TRANSFER FROM EAML 1225301 : REF EAML 1225150 FOR DENT FOUND AT FS1015.00 - FS1031.00AND BETWEEN STRINGER 24L-25L MEASURING 0.016D" X 4.00L" X 3.50W" WITH SMOOTH CREASE. DENT IS IS 0.075" FROM STRG 24L RIVET CENTER LINE. (FILED CLOSED)REPAIRED FUSELAGE SKIN BETWEEN FS1015.00 - FS 1031.00 AND STR 23L - 25L: COMPLIED WITH REO 670-53-61-2180 REV "--" DATED 2023-10-18 & 670-51-00-085 REV "-A" DATED 2017-08-23. COMPLIED WITH TASK CARD 51-900-1002-SKY AND FORM M-337.
Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 47,772 hrs · 31,273 cycles
L/H FWD DRAG ANGLE IS CRACKED ON AFT END AT APPROXIMATELY 67.5% REAR SPAR DATUM, WL 102.5. (FILED CLOSED)COMPLIED WITH REPAIRS TO LH FWD VERTICAL STABILIZER TO FUSELAGE ATTACHMENT DRAG ANGLE PER SRM TASK 55-31-00-201-001-A01, AND REO 670-55-31-165 REV --, DATED 08-10-2023. COMPLETED STRUCTURAL MAJOR REPAIR RII FORM 51-900-1002-SKY. MAJOR REPAIR FORM M-337 ALSO COMPLETED.
Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 47,743 hrs · 31,253 cycles
L/H FWD DRAG ANGLE IS CRACKED ON AFT END AT APPROXIMATELY 67.5% REAR SPAR DATUM, WL 102.5. (FILED OPEN)COMPLIED WITH REPAIRS TO LH FWD VERTICAL STABILIZER TO FUSELAGE ATTACHMENT DRAG ANGLE PER SRM TASK 55-31-00-201-001-A01, AND REO 670-55-31-165 REV --, DATED 08-10-2023. COMPLETED STRUCTURAL MAJOR REPAIR RII FORM 51-900-1002-SKY. MAJOR REPAIR FORM M-337 ALSO COMPLETED.
Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 47,772 hrs · 31,273 cycles
R/H FWD DRAG ANGLE IS CRACKED ON AFT END AT APPROXIMATELY 67.5% REAR SPAR DATUM, WL 102.5. (FILED CLOSED)COMPLIED WITH REPAIRS TO RH FWD VERTICAL STABILIZER TO FUSELAGE ATTACHMENT DRAG ANGLE PER SRM TASK 55-31-00-201-001-A01, AND REO 670-55-31-165 REV --, DATED 08-10-2023. COMPLETED STRUCTURAL MAJOR REPAIR RII FORM 51-900-1002-SKY. MAJOR REPAIR FORM M-337 ALSO COMPLETED.
Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 47,743 hrs · 31,253 cycles
R/H FWD DRAG ANGLE IS CRACKED ON AFT END AT APPROXIMATELY 67.5% REAR SPAR DATUM, WL 102.5. (FILED OPEN)COMPLIED WITH REPAIRS TO RH FWD VERTICAL STABILIZER TO FUSELAGE ATTACHMENT DRAG ANGLE PER SRM TASK 55-31-00-201-001-A01, AND REO 670-55-31-165 REV --, DATED 08-10-2023. COMPLETED STRUCTURAL MAJOR REPAIR RII FORM 51-900-1002-SKY. MAJOR REPAIR FORM M-337 ALSO COMPLETED.
Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 47,743 hrs · 31,253 cycles
R/H AFT DRAG ANGLE IS CRACKED ON FWD END AT APPROXIMATELY 67.5% REAR SPAR DATUM, WL 102.5. (FILED OPEN)COMPLIED WITH REPAIRS TO RH AFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT DRAG ANGLE PER SRM TASK 55-31-00-201-001-A01, AND REO 670-55-31-165 REV --, DATED 08-10-2023. COMPLETED STRUCTURAL MAJOR REPAIR RII FORM 51-900-1002-SKY. MAJOR REPAIR FORM M-337 ALSO COMPLETED.
Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 47,743 hrs · 31,253 cycles
L/H AFT DRAG ANGLE IS CRACKED ON FWD END AT APPROXIMATELY 67.5% REAR SPAR DATUM, WL 102.5. (FILED OPEN)COMPLIED WITH REPAIRS TO LH AFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT DRAG ANGLE PER SRM TASK 55-31-00-201-001-A01, AND REO 670-55-31-165 REV --, DATED 08-10-2023. COMPLETED STRUCTURAL MAJOR REPAIR RII FORM 51-900-1002-SKY. MAJOR REPAIR FORM M-337 ALSO COMPLETED.
Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 47,772 hrs · 31,273 cycles
R/H AFT DRAG ANGLE IS CRACKED ON FWD END AT APPROXIMATELY 67.5% REAR SPAR DATUM, WL 102.5. (FILED CLOSED)COMPLIED WITH REPAIRS TO RH AFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT DRAG ANGLE PER SRM TASK 55-31-00-201-001-A01, AND REO 670-55-31-165 REV --, DATED 08-10-2023. COMPLETED STRUCTURAL MAJOR REPAIR RII FORM 51-900-1002-SKY. MAJOR REPAIR FORM M-337 ALSO COMPLETED.
Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 47,772 hrs · 31,273 cycles
L/H AFT DRAG ANGLE IS CRACKED ON FWD END AT APPROXIMATELY 67.5% REAR SPAR DATUM, WL 102.5. (FILED CLOSED)COMPLIED WITH REPAIRS TO LH AFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT DRAG ANGLE PER SRM TASK 55-31-00-201-001-A01, AND REO 670-55-31-165 REV --, DATED 08-10-2023. COMPLETED STRUCTURAL MAJOR REPAIR RII FORM 51-900-1002-SKY. MAJOR REPAIR FORM M-337 ALSO COMPLETED.
Part: UNKNOWN — CHAFED (UNKNOWN) · airframe 47,466 hrs · 31,024 cycles
RH AILERON OUTBOARD PCU LUGS HAVE CHAFING DAMAGE. (FILED CLOSED) REPLACED RH AILERON WITH NEW SERVICABLE UNIT IN REFERENCE TO MIP TASK CARD 27-900-1001-SKY CAL TOOLS USED TORQUE WRENCH S/N: 0917103017CAL DUE: 6-30-2023SAFETY CABLE GUN CERT # 22362-0708CAL DUE: 12-31-2023
Part: UNKNOWN — DAMAGED (UNKNOWN) · airframe 47,393 hrs · 30,964 cycles
TRANSFER FROM EAML 1110834 : DESCENDING THROUGH FL200 LH SIDE WINDSCREEN OUTSIDE PLY SHATTERED. RAN QRH. (FILED CLOSED)REMOVED, AND REPLACED LH WINDSHIELD AS REQUIRED REF AMM AMM 56-11-01 SEE CARD 56-220-1000-SKY NO LEAKS NOTED OPS CHECKS GOOD.
Part: CABIN PRESSURE — MALFUNCTIONED · airframe 46,959 hrs · 30,598 cycles
RECEIVED CABIN ALT WARNING MESSAGE DURING CLIMB OUT. CAB ALTITUDE REACHED 10,000FT. PERFORMED QRH PROCEDURES AND RETURNED TO LAX. PERFORMED CPC TEST IN THE MDC TEST PASSED PRESSURIZED AIRCRAFT PER AMM 21-31-00-910-801 PRESSURIZATION CHECKS GOOD ON THE GROUND AT THIS TIME.
Earlier reports · 2005–2022 · 162 reports
2022
Part: NONE — CORRODED · airframe 46,555 hrs · 30,243 cycles
DURING REMOVAL OF WASTE TANK LOWER DRAIN TUBE, FOUND CORROSION DAMAGE TO LAV WASTE SERVICING SURROUND STRUCTURE (FOR REFERENCE SEE SRM 53-51-23), DAMAGE IS BETWEEN FS953.00 AND 969.00 AND BETWEEN STR23R AND STR24R. (FILED CLOSED) STRUCTURAL REPAIR - COMPLIED WITH REPAIRS TO LAV WASTE SERVICING SURROUND STRUCTURE REFERENCE SRM 53-51-23, BY REPLACEMENT OF ITEMS 1, 2, 3, 4 (NUTPLATE SUPPORT ANGLES) PER APPLICABLE SRM STANDARD PRACTICES 51-24-00, 51-25-00, 51-42-00. COMPLIED WITH REPLACEMENT OF STRINGER SECTIONS STR22R BETWEEN FS939.00 AND 923.00, AND FOR STR23R BETWEEN FS953.00 AND 939.00 PER SRM TASK 53-00-03-201-001-A01 AND APPLICABLE SRM STANDARD PRACTICES. FOR REPLACEMENT OF STRINGER SECTIONS, FRAME SECTIONS AT LOWER RH FS953.00 AND FS969.00 HAD TO BE REMOVED. THESE FRAME SECTIONS WERE REMOVED AND REPLACED PER REO 670-53-51-253 REV --, DATED 09-29-2022. M-337, RII TASK CARDS 51-900-1002-SKY AND CORROSION FINDINGS REPORT COMPLETED AND ATTACHED.
2020
Part: ANGLE — CORRODED (FAIRING) · airframe 41,889 hrs · 26,872 cycles
EXTERNAL SUPPORT STRUCTURE AFT WING TO FUSELAGE FAIRING FS939.00 ANGLE IS CORRORED (AS MARKED) (C-CHECK) RO 3/25/2020 REMOVED AND REPLACED NEW ANGLE P/N SH670-39189-1 AT EXTERNAL SUPPORT STRUCTURE AFT WING TO FUSELAGE FAIRING FS932.00 REF CRJ700 SRM.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 41,889 hrs · 26,872 cycles
ANGLE CRACKED INSIDE OF RBL 12 FLOOR BEAM AFT INSIDE ANGLE AT FS280 (C-CHECK) RO 3/25/2020 REMOVED AND INSTALLED NEW ANGLE INSIDE RBL12 FLOORBEAM AFT INSIDE ANGLE AT FS280 REF-CRJ-700 SRM & DWG.
Part: STRINGER — DAMAGED (FUSELAGE) · airframe 41,889 hrs · 26,872 cycles
PERFORM REPAIR OF FS469.00 @ STGR16R FOR REMOVAL OF STGR19R (C-CHECK) RO 3/25/2020 PERFORMED REPAIR OF FS469.00 @ STGR16R REF-CRJ-700 BOMBARDIER REO, LEAK CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS.
Part: STRINGER — DAMAGED (FUSELAGE) · airframe 41,889 hrs · 26,872 cycles
PERFORM REPAIR OF FS453.00 @ STGR16R FOR REMOVAL OF STGR19R (C-CHECK) RO 3/25/2020 PERFORMED REPAIR OF FS453 AT STGR16R FOR REMOVAL OF STGR19R REF CRJ-700 SRM AND REO. COMPLIED WITH TASK CARD STRUCTURAL MAJOR REPAIR (**RII**). LEAK CHECK GOOD
Part: STRINGER — CORRODED (FUSELAGE) · airframe 41,889 hrs · 26,872 cycles
CORROSION ON STRINGER 19R BETWEEN FS 364 - 379 AS MARKED (C-CHECK) RO 3/25/2020 REPLACED STRINGER AT STGR19R BETWEEN FS349 - FS3477 REF CRJ-700 SRM, DWG. COMPLIED WITH TASK CARD STRUCTURAL MAJOR REPAIR (**RII**). LEAK CHECK GOOD
Part: STRINGER — CORRODED (FUSELAGE) · airframe 41,889 hrs · 26,872 cycles
STGR26R JOINT PIECE IS CORRODED AFT OF FS333.00 (C-CHECK) RO 3/25/2020 STGR 26R JOINT PIECE HAS INTERGRANULAR CORROSION NEAR FASTENER HOLES OUT OF LIMITS REF CRJ 700 SRM. REMOVED AND INSTALLED NEW STRINGER JOINT PIECE STGR 26R FS333 REF CRJ 700 SRM AND DWG. PERFORMED LEAK CHECK OF OUTER SKIN IN REPAIR AREA LEAK CHECK GOOD NO DEFECTS NOTED REF CRJ 700 AMM.
Part: ANGLE — CORRODED (PAX DOOR) · airframe 41,889 hrs · 26,872 cycles
PASSENGER DOOR AFT CAP ANGLE HAS EVIDENCE OF CORROSION (C-CHECK) RO 3/25/2020 PASSENGER DOOR AFT CAP ANGLE WAS REMOVED AND NEW ONE INSTALLED, PER REF CRJ-700 SRM, BOMBARDIER DRAWING.
Part: ANGLE — CORRODED (PAX DOOR) · airframe 41,889 hrs · 26,872 cycles
PASSENGER DOOR MID CAP ANGLE HAS EVIDENCE OF CORROSION (C-CHECK) RO 3/25/2020 PASSENGER DOOR MID CAP ANGLE WAS REMOVED AND NEW ONE INSTALLED, PER REF CRJ-700 SRM, DRAWING.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 41,889 hrs · 26,872 cycles
4EA ANGLES ON SERVICE DOOR LOWER SILL ATTACHED TO FLOOR WEB PROTECTOR CORRODED FROM FS310 TO FS349 (C-CHECK) RO 3/25/2020 4EA ANGLES ON SERVICE DOOR LOWER SILL ATTACHED TO FLOOR WEB PROTECTOR OUT OF LIMITS FROM FS310 TO FS349 REF CRJ 700 SRM. REMOVED AND INSTALLED NEW 4EA ANGLES ON SERVICE DOOR LOWER SILL ATTACHED TO FLOOR WEB PROTECTOR FROM FS310 TO FS349 REF CRJ 700 SRM.
Part: ANGLE — CORRODED (SERVICE DOOR) · airframe 41,889 hrs · 26,872 cycles
SERVICE DOOR MID CAP ANGLE CORRODED (C-CHECK) RO 3/25/2020 SERVICE DOOR MID CAP ANGLE OUT OF LIMITS REF- CRJ-700 SRM. REMOVED AND INSTALLED NEW SERVICE DOOR MID CAP ANGLE REF CRJ 700 SRM.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,889 hrs · 26,872 cycles
*LEFT HAND SIDE SEAT RAIL FS675.00-713.00 IS CORRODED. (C-CHECK) RO 3/25/2020 LH SIDE SEAT RAIL FROM APROX FS675.00 TO FS713.00 EVALUATED AND FABRICATED ON JOB 710196114 OP 60 MX TRANS# 20496818 INSTALLED NEW LH SIDE SEAT RAIL FROM APROX FS675.00 TO FS713.00 REF CRJ700 AMM.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,889 hrs · 26,872 cycles
*RIGHT HAND SIDE SEAT RAIL FS675.00-713.00 IS CORRODED. (C-CHECK) RO 3/25/2020 RH SIDE SEAT RAIL FROM APROX FS675 TO FS 713 CORROSION FOUND TO BE OUT OF LIMITS. REF CRJ700 SRM. REMOVED AND FABRICATED NEW REPLACEMENT PART. REF CRJ700 AMM AND CRJ700 SRM. INSTALLED NEW REPLACEMENT PART. REF CRJ700 AMM. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,889 hrs · 26,872 cycles
*RIGHT HAND SIDE SEAT RAIL FS713.00 ̉‰ 761.85 IS CORRODED. (C-CHECK) RO 3/25/2020 RH SIDE SEAT RAIL FROM APROX FS713.00 TO FS761.85 CORROSION FOUND TO BE OUT OF LIMITS. REF CRJ700 SRM. REMOVED AND FABRICATED NEW REPLACEMENT PART. REF CRJ700 AMM AND CRJ700 SRM. INSTALLED NEW REPLACEMENT PART. REF CRJ700 AMM. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,889 hrs · 26,872 cycles
*RIGHT HAND SIDE SEAT RAIL FS785.00 - FS861.00 IS CORRODED. (C-CHECK) RO 3/25/2020 RH SIDE SEAT RAIL FROM APROX TO FS785.00 TO FS861.00 CORROSION OUT OF LIMITS. SEE JOB 710196114 OP 61 MX TRANS# 20496830 FOR EVALUATION. REMOVED FABRICATED AND REPLACED WITH NEW RH SIDE SEAT TRACK REF CRJ700 AMM SEE ATTACHED CONTINUATION CARD FOR WORK PERFORMED.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,889 hrs · 26,872 cycles
*RIGHT HAND SIDE SEAT RAIL FS861.00 ̉‰ FS969 IS CORRODED. (C-CHECK) RO 3/25/2020 RH SIDE SEAT RAIL FROM FS861 TO FS969 CORROSION OUT OF LIMITS. SEE JOB 710196114 OP 61 MX TRANS# 20496830 FOR EVALUATION. REMOVED FABRICATED AND REPLACED WITH NEW RH SIDE SEAT TRACK. SEE CONTINUE CARD FOR DETAILS. REF CRJ700 AMM. REF CRJ700 SRM.
Part: SKIN — GOUGED (FUSELAGE) · airframe 41,889 hrs · 26,872 cycles
*TWO DENTS WITH A GOUGE AND MULTIPLE GOUGES IN EXTERNAL SKIN. FS1031.00 ̉‰ FS1051.00 STGR22R ̉‰ STGR26R. (C-CHECK) RO 3/25/2020 DRESSED BACK DENTS AND BLENDED MULTIPLE GOUGES IN THE EXTERNAL SKIN AT FS1031.00 ̉‰ FS1051.00 STGR22R ̉‰ STGR26R. ALL REWORKED AREAS ARE WITH A SMOOTH IN COUNTOUR WITH NO CREASES AND NO OIL CANNING OCURRED POST REWORK REF-CRJ-700 REO. DRESS BACK ONLY THUS NO WEIGHT CHANGE.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,889 hrs · 26,872 cycles
*LEFT HAND SIDE SEAT RAIL FS713.00 ̉‰ 761.85 IS CORRODED. (C-CHECK) RO 3/25/2020 LH SIDE SEAT RAIL FROM APROX TO FS713.00 TO FS761.00 CORROSION OUT OF LIMITS. SEE JOB 710196114 OP 60 MX TRANS# 20496818 FOR EVALUATION AND FABRICATION. REMOVED AND REPLACED WITH NEW LH SIDE SEAT TRACK REF CRJ700 AMM.
Part: HINGE — GROOVED (FUSELAGE) · airframe 41,889 hrs · 26,872 cycles
PAX DOOR HINGE ON FUSELAGE SIDE AFT LAND IS GROOVED. (C-CHECK) RO 3/25/2020 REMOVED AND REPLACED PAX DOOR HINGE FUSELAGE SIDE REF-CRJ-700 SRM ,LEACK CHECK GOOD.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,889 hrs · 26,872 cycles
LH SIDE SEAT RAILS FS 675 TO 761 APPROX AS MARKED HAVE CORROSION. (C-CHECK) RO 3/25/2020 EVALUATION OF 2EA SEAT TRACK SEGMENTS FROM FS675.00-714.00 AND FS714-761 DETERMINED CORROSION TO BE OUT OF LIMITS. REF CRJ700 SRM. FABRICATED 2EA NEW SEAT TRACKS SEE CONTINUATION CARD FOR WORK PROFORMED. REF CRJ700 SRM. INSTALLED NEW SIDE SEAT TRACK FS675.00-714 ON JOB 710196114 OP 80 MX TRANS# 20515347. INSTALLED NEW FS714.00-761 ON JOB 710196114 OP 81 MX TRANS# 20515369.
Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 41,889 hrs · 26,872 cycles
SERVICE DOOR SURRROUND STRUCTURE ANGLE LOWER SILL HAS CORROSION RH FS319.70 TO 349 (C-CHECK) RO 3/25/2020 SERVICE DOOR SURROUND STRUCTURE ANGLE LOWER SILL R/H FS319.70 TO FS349 OUT OF LIMITS REF CRJ 700 SRM. REMOVED AND INSTALLED NEW SERVICE DOOR SURROUND STRUCTURE ANGLE LOWER SILL R/H FS319.70 TO FS349 REF CRJ 700 SRM.
Part: GUSSET — CORRODED (FUSELAGE) · airframe 41,889 hrs · 26,872 cycles
GUSSET @ STGR21R AND FS349.00 IS CORRODED (C-CHECK) RO 3/25/2020 REMOVED AND REPLACED WITH NEW GUSSET FS349 STR21R REF CRJ 700 SRM AND BOMBARDIER DWG. COMPLIED WITH FORM M-337.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 41,889 hrs · 26,872 cycles
* CORROSION ON STR 25L BETWEEN FS333 ̉‰ FS349 (C-CHECK) RO 3/25/2020 REMOVED CORROSION ON STGR 25L BETWEEN FS333-FS349 REF CRJ 700SRM. REMOVED AND INSTALLED NEW LONGERON STGR25L FS333 TO FS364 REF CRJ 700 SRM, DWG. PERFORMED LEAK CHECK OF OUTER SKIN IN REPAIR AREA LEAK CHECK GOOD NO DEFECTS NOTED REF CRJ 700 AMM.
Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 41,889 hrs · 26,872 cycles
* FLOOR SUPPORT ANGLE CORRODDED FROM LBL9 TO RBL 9 AT FS 280 MARKED (C-CHECK) RO 3/25/2020 REMOVED CORROSION FROM FLOOR SUPPORT ANGLE FROM LBL9 - RBL9 AT FS280 AND FOUND REWORKED AREA TO BE OUT OF LIMITS. REPLACED ANGLE REF CRJ-700 SRM , AND DWG. COMPLIED WITH TASK CARD STRUCTURAL MAJOR REPAIR (**RII**)
Part: ANGLE — CORRODED (PAX DOOR) · airframe 41,889 hrs · 26,872 cycles
*PASSENGER DOOR FRAME ANGLE KICKPLATE (P/N SH670-31875) HAS EVIDENCE OF CORROSION (C-CHECK) RO 3/25/2020 REMOVED AND REPLACED DOOR FRAME ANGLE KICKPLATE P/N SH670-31875. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED. REF CRJ700 SRM. OPS TEST OF PAX DOOR FAILED. SEE JOB 710196115 OP 175 MX TRANS# 20696094 FOR CORRECTIVE ACTION. COMPLIED WITH TASK CARD AND M337
Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 41,889 hrs · 26,872 cycles
* RH FLOOR SILL CORRODDED FS 280- FS 319 MARKED (C-CHECK) RO 3/25/2020 REPLACED RH FLOOR SILL AT FS280 - FS319 REF CRJ-700 SRM AND DWG. COMPLIED WITH TASK CARD. LEAK CHECK GOOD
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,889 hrs · 26,872 cycles
* RBL 9 SEAT RAIL CORRODDED FROM APROX FS 477.0 TO FS 693.0 MARKED (C-CHECK) RO 3/25/2020 RBL 9 SEAT RAIL FROM APROX FS477.0 TO FS 693.0 CORROSION FOUND TO BE OUT OF LIMITS. REF CRJ700 SRM. REMOVED AND FABRICATED NEW REPLACEMENT PART. REF CRJ700 AMM AND CRJ700 SRM. INSTALLED NEW REPLACEMENT PART. REF CRJ700 AMM. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 41,889 hrs · 26,872 cycles
CORROSION ON INTERCOSTAL AT STR 20R FS319 ̉‰ FS333 (C-CHECK) RO 3/25/2020 REPLACED INTERCOSTAL AT STR 20R FS319 ̉‰ FS333 REF CRJ-700 SRM AND BOMBARDIER DWG. COMPLIED WITH TASK CARD
Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 41,889 hrs · 26,872 cycles
* A-BAY CRAWL BOARD SUPPORT ANGLE AT FS 280 IS CORRODED (C-CHECK) RO 3/25/2020 REMOVED AND INSTALLED NEW SUPPORT ANGLE AT AVIONICS BAY CRAWL BOARD AT FS280 REF-CRJ-700 SRM & DWG, SEE CONTINUATION CARD FOR DETAILS.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 41,889 hrs · 26,872 cycles
* CORROSION ON STR 26R BETWEEN FS333 - FS349 (C-CHECK) RO 3/25/2020 STGR26R HAS PITTING AT FASTENER HOLE AND 100% MATERIAL LOSS AT 2EA LOCATIONS ON STRINGER OUT OF LIMITS REF CRJ 700 SRM. REMOVED AND INSTALLED NEW STRINGER STGR26R REF CRJ 700 SRM AND DWG. PERFORMED LEAK CHECK OF OUTER SKIN IN REPAIR AREA LEAK CHECK GOOD NO DEFECTS NOTED REF CRJ 700 AMM.
Part: ANGLE — CORRODED (SERVICE DOOR) · airframe 41,889 hrs · 26,872 cycles
SERVICE DOOR SUPPORT STRUCTURE LOWER SEAL STRICKER ANGLE RH FS 319.70 TO 349.00 HAS CORROSION AROUND FASTENER HOLE FOR COVER PLATE AS MARKED. (C-CHECK) RO 3/25/2020 SERVICE DOOR SUPPORT STRUCTURE LOWER SEAL STRICKER ANGLE R/H FS319.70 TO FS349 OUT OF LIMITS REF CRJ 700 SRM. REMOVED AND INSTALLED SERVICE DOOR SUPPORT STRUCTURE LOWER SEAL STRICKER ANGLE R/H FS319.70 TO FS349 REF CRJ 700 SRM. LEAK CHECK OF OUTER SKIN IN REPAIR AREA LEAK CHECK GOOD NO DEFECTS NOTED REF CRJ 700 AMM.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 41,889 hrs · 26,872 cycles
* CORROSION ON STR 21R AT APPROX. FS345 (C-CHECK) RO 3/25/2020 REMOVED AND REPLACED STRINGER 21R APPROX FS345 REF-CRJ-700 SRM, DWG. LEAK CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS.
Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 41,889 hrs · 26,872 cycles
* LH FLOOR SILL CORRODDED FS 280 ̉‰FS 310 MARKED (C-CHECK) RO 3/25/2020 LH FLOOR SILL FS 280.00 ̉‰ FS 310.00 OUT OF LIMITS EXFOLIATED 100% MATERIAL LOSS REF CRJ 700 SRM. LH FLOOR SILL P/N SH670-32171 BTW FS 280.00 ̉‰ FS 310.00 WAS REPLACED AND NEW ONE INSTALLED PER REF CRJ-700 SRM & BOMBARDIER DWG AND COMPLIED WITH TASK. PERFORMED LEAK CHECK OF OUTER SKIN IN REPAIR AREA LEAK CHECK GOOD NO DEFECTS NOTED REF CRJ 700 AMM.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,889 hrs · 26,872 cycles
* 280 FLOOR BEAM CORRODDED FROM LBL 9 TO RBL 9 MARKED (C-CHECK) RO 3/25/2020 ONLY FS280 CROSSBEAM UPPER SPLICE STRIP FOUND TO BE CORRODED. FOUND UPPER SPLICE STRIP TO BE OUT OF LIMITS REPLACED REF CRJ-700 SRM.
Part: FITTING — CORRODED (PAX DOOR) · airframe 41,889 hrs · 26,872 cycles
PASSENGER DOOR AFT CLOSING FITTING HAS EVIDENCE OF CORROSION (STR18, FS342.00) (C-CHECK) RO 3/25/2020 PASSENGER DOOR AFT CLOSING FITTING (STR18, FS342.00) WAS REMOVED AND NEW ONE INSTALLED, PER REF CRJ-700 SRM, BOMBARDIER DRAWING AND COMPLIED WITH TASK.
Part: FRAME — CORRODED (FUSELAGE) · airframe 41,889 hrs · 26,872 cycles
* CORROSION ON FWD SIDE OF FS379 FRAME BETWEEN STR 22R AND 23R (C-CHECK) RO 3/25/2020 REPLACED FRAME SECTOR AT FS379 REF CRJ-700 SRM, DWG. COMPLIED WITH TASK CARD STRUCTURAL MAJOR REPAIR (RII). LEAK CHECK GOOD
Part: FITTING — CORRODED (PAX DOOR) · airframe 41,889 hrs · 26,872 cycles
*PASSENGER DOOR FWD CLOSING FITTING HAS EVIDENCE OF CORROSION (STR18, FS314.00) (C-CHECK) RO 3/25/2020 PASSENGER DOOR FWD CLOSING FITTING WAS REMOVED AND NEW ONE INSTALLED, PER REF CRJ-700 SRM, DRAWING AND COMPLIED WITH TASK
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,889 hrs · 26,872 cycles
* LBL 9 SEAT RAIL CORRODDED FROM APROX FS 477.0 TO FS 693.0 MARKED (C-CHECK) RO 3/25/2020 LBL 9 SEAT RAIL FROM APROX FS477.0 TO FS 693.0 CORROSION FOUND TO BE OUT OF LIMITS. REF CRJ700 SRM. REMOVED AND FABRICATED NEW REPLACEMENT PART. REF CRJ700 AMM AND CRJ700 SRM. INSTALLED NEW REPLACEMENT PART. REF CRJ700 AMM. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.
Part: FRAME — CORRODED (FUSELAGE) · airframe 41,889 hrs · 26,872 cycles
* CORROSION ON AFT SIDE OF FS 349 FRAME BETWEEN STR 26R AND 27 (C-CHECK) RO 3/25/2020 REPLACED LOWER FRAME SECTOR AT FS349 REF CRJ-700 SRM, DRAWING. COMPLIED WITH TASK CARD STRUCTURAL MAJOR REPAIR (**RII**). LEAK CHECK GOOD
Part: STRINGER — CORRODED (FUSELAGE) · airframe 41,889 hrs · 26,872 cycles
* CORROSION ON STR 26L BETWEEN FS333 ̉‰ FS349 (C-CHECK) RO 3/25/2020 STGR26L BETWEEN FS333-FS349 OUT OF LIMITS DEEP PITTING AT FASTENER HOLES REF CRJ 700 SRM. REMOVED AND INSTALLED NEW STGR26L BETWEEN FS333-FS349 REF CRJ 700 SRM AND DWG. PERFORMED LEAK CHECK ON REPAIR AREA LEAK CHECK GOOD REF CRJ 700 AMM.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 41,889 hrs · 26,872 cycles
* CORROSION ON INTERCOSTAL AT STR 20R FS310 ̉‰ FS319 (C-CHECK) RO 3/25/2020 REPLACED INTERCOSTAL LOCATED AT 20R FROM FS310-FS319 WITH NEW. REF CRJ-700 SRM AND BOMBARDIER DRAWING.
Part: ANGLE — CORRODED (PAX DOOR) · airframe 41,889 hrs · 26,872 cycles
PASSENGER DOOR FWD CAP ANGLE HAS EVIDENCE OF CORROSION (C-CHECK) RO 3/25/2020 PASSENGER DOOR FWD CAP ANGLE WAS REMOVED AND NEW ONE INSTALLED, PER REF CRJ-700 SRM, DRAWING AND COMPLIED WITH TASK
Part: ANGLE — CORRODED (LT MLG WW) · airframe 41,889 hrs · 26,872 cycles
*LEFT WHEEL WELL - ANGLE MOUNTED TO AFT SIDE OF THE AFT WING SPAR FOR THE BLOW-OUT PROTECTION PANEL IS CORRODED. (MARKED & FLAGGED (C-CHECK) RO 3/25/2020 REMOVED AND INSTALLED NEW LEFT WHEEL WELL ANGLE AT AFT SIDE OF THE AFT LEFT WING SPAR REF-CRJ-700 SRM AND DWG. SEE CONTINUATION CARD FOR DETAILS. LEAK CHECK GOOD. COMPLIED WITH TASK.
Part: SKIN — CHAFED (FUSELAGE) · airframe 41,889 hrs · 26,872 cycles
*EXTERNAL SKIN HAS FOUR CHAFES ALONG STGR27 BETWEEN FS969.00 ̉‰ FS977.00. (MARKED) (C-CHECK) RO 3/25/2020 REPAIRED EXTERNAL SKIN ALONG STGR27 BETWEEN FS969 - FS977 REF REO. COMPLIED WITH TASK CARD STRUCTURAL MAJOR REPAIR (**RII**). LEAK CHECK GOOD
Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 41,889 hrs · 26,872 cycles
* AFT CARGO ENTRY WAY FLOOR SILL HAS EVIDENCE OF CORROSION. (C-CHECK) RO 3/25/2020 REPLACED AFT CARGO FLOOR SILL REF CRJ700 SRM AND BOMBARDIER DWG. COMPLIED WITH TASK CARD. LEAK CHECK GOOD NO DEFECT NOTED.
Part: BOLT — CORRODED (LT WING) · airframe 41,889 hrs · 26,872 cycles
*LH OBD, AFT FLAP HINGE BOX ATTACHMENT HAS CORRODED HARDWARE. WS264.00 FLAGGED (C-CHECK) RO 3/25/2020 REMOVED AND REPLACED LH OB AFT FLAP HINGE BOX ATTACHMENT BOLT, 2EA WASHERS, NUT AND COTTER PIN WITH NEW REF CRJ 700 AMM. TOOL # TUC 8614 CAL DUE 30 NOV. 20. GAP CHECK GOOD.
Part: BOLT — CORRODED (LT WING) · airframe 41,889 hrs · 26,872 cycles
*LH OUTBOARD FLAP, INBD/AFT HINGE BOX ATTACHMENT HAS CORRODED HARDWARE. WS178.00 FLAGGED (C-CHECK) RO 3/25/2020 REMOVED BOLTS, WASHER NUT AND COTTER KEY REFERENCE CRJ700 AMM. INSTALLED NEW BOLT, WASHER, NUT, AND COTTER KET AT LH O/B FLAP I/B HINGE BOX ATTACHMENT REFERENCE CRJ700 AMM. TORQUE WRENCH: TUC4822 CAL DUE: 30-APR-20.
Part: FASTENER — CORRODED (RT WING) · airframe 41,889 hrs · 26,872 cycles
*RH OBD, AFT FLAP HINGE BOX ATTACHMENT HAS CORRODED HARDWARE. WS264.00 FLAGGED (C-CHECK) RO 3/25/2020 REMOVAL AND REPLACED HARDWARE P/N 601R14633-3, AN960C516, S1236P416L,MS17825-4, MS24665-136, WS 264.00 RH OBD, AFT FLAP HINGE BOX ATTACHMENT, REF CRJ 700 AMM TASK.
Part: FASTENER — CORRODED (LT WING) · airframe 41,889 hrs · 26,872 cycles
*LH INBD, AFT FLAP HINGE BOX ATTACHMENT HAS CORRODED HARDWARE. WS178.00 FLAGGED (C-CHECK) RO 3/25/2020 DISCREPANCY WRITTEN IN ERROR. SHOULD HAVE READ AS: *LH OTBD FLAP, INBD/ AFT HINGE BOX ATTACHMENT HAS CORRODED HARDWARE. WS178.00 FLAGGED.JOB:4 OP:10 CAMP#20466513
Part: SKIN — DENTED (TE FLAP) · airframe 41,889 hrs · 26,872 cycles
* LH INBD FLAP LOWER SKIN DENTED MARKED (C-CHECK) RO 3/25/2020 L/H I/B FLAP LOWER SKIN DENT HAS BEEN REPAIRED USING BOMBARDIER REO, ALSO COMPLIED W/SKYWEST TASK CARD AND COMPLETED M337. SEE CONTINUATION SHEET FOR DETAILS.
Part: STRUCTURE — DENTED (FUSELAGE) · airframe 41,889 hrs · 26,872 cycles
ADM 6394 - DENT LOCATED JUST BEFORE FS295 BETWEEN STRINGERS 19 AND 20. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES. (C-CHECK) RO 3/25/2020 DISCREPANCY WRITEN WITH INCORRECT LOCATION. DENT LOCATED BETWEEN STRINGERS 21R - 22R. PERFORMED REPAIR AT FS295 BETWEEN STRINGERS 21R AND 22R REF REO. COMPLIED WITH TASK CARD STRUCTURAL MAJOR REPAIR (**RII**). LEAK CHECK GOOD
2016
Part: LINE — FAILED (HYD SYSTEM) · airframe 34,408 hrs · 20,654 cycles
SYSTEM THREE LOST ALL HYDRAULIC QUANTITY. REMOVED AND REPLACED FLEXIBLE LINE AND SERVICED THE HYDRAULIC SYSTEM. LEAK AND OPS CHECK GOOD.
Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 34,096 hrs · 20,439 cycles
CORROSION ON PAX DOOR INTERCOSTAL. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM. PERFORMED PRESSURIZATION CHECK. PRESSURE CHECKED GOOD.
Part: ATTACH ANGLE — CORRODED (BS 310-333) · airframe 34,096 hrs · 20,439 cycles
FWD ATTACH ANGLE FOR INTERCOSTAL BETWEEN BS 310 AND 333 AT STRINGER 21L HAS CORROSION. REMOVED AND REPLACED THE ATTACH ANGLE IAW SRM.
Part: FLOOR SUPPORT — CORRODED (BS 485-501) · airframe 34,096 hrs · 20,439 cycles
LEFT FLOOR SUPPORT IS CORRODED FROM BS 485 TO 501. REPAIRED THE FLOOR SUPPORT IAW EA.
Part: FRAME — CORRODED (BS 364) · airframe 34,096 hrs · 20,439 cycles
FRAME BS 364 CORRODED. FOUND TO BE OUT OF LIMITS. SECTION OF THE FRAME WAS REPLACED IAW REO.
Part: VANE — CORRODED (LT WING TE FLAP) · airframe 34,096 hrs · 20,439 cycles
LEFT INBOARD FLAP VANE AT APPROX WS 121 IS CHAFED. REPAIRED IAW EA.
Part: VANE — CORRODED (LT WING TE FLAP) · airframe 34,096 hrs · 20,439 cycles
LEFT INBOARD FLAP VANE AT APPROX WS 51 IS CHAFED. REPAIRED IAW EA.
Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 34,096 hrs · 20,439 cycles
INTERCOSTAL LOCATED BETWEEN BS 349 AND 364, STRINGER 26L HAS CORROSION. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM.
Part: THRESHOLD — CORRODED (SERVICE DOOR) · airframe 34,096 hrs · 20,439 cycles
SERVICE DOOR THRESHOLD HAS CORROSION ON INBOARD BOTTOM EDGE. REMOVED AND REPLACED THE THRESHOLD IAW SRM.
Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 34,096 hrs · 20,439 cycles
INTERCOSTAL LOCATED BETWEEN BS 349 AND 364, STRINGER 26R HAS CORROSION. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 34,096 hrs · 20,439 cycles
CRAWLWAY FLOORBEAM ANGLE LOCATED AT LOWER BS 280 HAS CORROSION. REMOVED AND REPLACED THE FLOORBEAM ANGLE IAW SRM.
Part: PANEL — CHAFED (RT WING) · airframe 34,096 hrs · 20,439 cycles
RT WING PANEL 684GB IS CHAFED. REMOVED AND REPLACED THE PANEL IAW SRM.
Part: PANEL — CHAFED (RT WING) · airframe 34,096 hrs · 20,439 cycles
RT WING PANEL 684AB IS CHAFED. REPAIRED THE PANEL IAW EA.
Part: PANEL — CORRODED (RT WING) · airframe 34,096 hrs · 20,439 cycles
RT WING PANEL 642BZ HAS CORROSION AROUND FASTENER HOLES. REMOVED AND REPLACED THE PANEL IAW SRM.
2014
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 29,342 hrs · 17,534 cycles
EMERGENCY EXIT LIGHT JUST AFT OF FIRST CLASS INOPERATIVE AND THE FRONT HALF OF THE OVERHEAD EXIT SIGN BETWEEN THE OVERWING EXITS IS ALSO INOPERATIVE. REPLACED EMERGENCY BATTERIES, OPS CHECKED GOOD.
Part: CIRCUIT BOARD — FAULTY (EMERGENCY LIGHTS) · airframe 29,216 hrs · 17,472 cycles
EMERGENCY LIGHTS ARE FLASHING ON AND OFF. MX CHANGED PCB 5 IN JB11. CHECKED GOOD.
Part: SKIN — CHAFED (FUSELAGE) · airframe 29,185 hrs · 17,457 cycles
FUSELAGE CHAFED UNDER RT STUB FAIRING, PANEL 172DR. C-CHECK, REPAIRED DAMAGED AREA IAW EA.
Part: DOOR — CHAFED (LT NACELLE) · airframe 29,185 hrs · 17,457 cycles
LEFT LOWER FAN COWL DOOR HAS A CHAFE ON 3RD STIFFENER AFT OF L/E. C-CHECK, REPAIRED LT LOWER FAN COWL DOOR CHAFE ON 3RD STIFFENER AFT OF L/E IAW REO.
Part: DOOR — CHAFED (LT NACELLE) · airframe 29,185 hrs · 17,457 cycles
LEFT LOWER FAN COWL DOOR HAS A CHAFE ON STIFFENER NEAR INBD HINGE. C-CHECK, BLENDED OUT CHAFE ON STIFFENER NEAR INBD HINGE OF LT LOWER FAN COWL IAW REO.
Part: AXLE — CORRODED (LANDING GEAR) · airframe 29,185 hrs · 17,457 cycles
CORROSION FOUND MLG PISTON AXLE 1 ROOT RADIUS. C-CHECK, REPAIRED CORROSION OF MLG PISTON AXLE 1 ROOT RADIUS IAW REO.
Part: AXLE — CORRODED (MLG) · airframe 29,185 hrs · 17,457 cycles
CORROSION FOUND MLG PISTON AXLE 2 ROOT RADIUS. C-CHECK, REPAIRED CORROSION OF MLG PISTON AXLE, 2 ROOT RADIUS IAW REO.
Part: AXLE — CORRODED (MLG) · airframe 29,185 hrs · 17,457 cycles
CORROSION FOUND MLG PISTON AXLE, 4 ROOT RADIUS. C-CHECK, RO: REPAIRED CORROSION OF MLG PISTON AXLE, 4 ROOT RADIUS IAW REO.
Part: AXLE — CORRODED (MLG) · airframe 29,185 hrs · 17,457 cycles
CORROSION FOUND MLG PISTON AXLE, 3 ROOT RADIUS. C-CHECK, REPAIRED CORROSION OF MLG PISTON AXLE, 3 ROOT RADIUS IAW REO.
Part: ANGLE — CRACKED (BS 280) · airframe 29,185 hrs · 17,457 cycles
OTBD L ANGLE AT BS 280, LBL.10 FOUND CRACKED. C-CHECK INSTALLED ANGLE IAW REO.
Part: TUBE — BROKEN (SERVICE DOOR) · airframe 29,185 hrs · 17,457 cycles
SERVICE DOOR CONVOLEX TUBE BROKEN. C-CHECK, REPAIRED THE SERVICE DOOR CONVOLEX TUBING IAW REO.
Part: FLANGE — CRACKED (RT NACELLE) · airframe 29,185 hrs · 17,457 cycles
RT ENGINE AFT FLANGE WHERE RUBBER SEAL ATTACHED NEAR FIRE LOOP AT 10:00 POSITION.FLANGE HAS A CRACK. C-CHECK, REPAIRED RT ENGINE AFT FLANGE CRACK AT 10 O'CLOCK POSITION.
Part: RETAINER — DAMAGED (CARGO DOOR) · airframe 29,185 hrs · 17,457 cycles
FORWARD CARGO DOOR SEAL RETAINER DAMAGED IN 4 AREAS. C-CHECK, REPLACED DAMAGED SEAL RETAINERS.
Part: RETAINER — DENTED (PAX DOOR SEAL) · airframe 29,185 hrs · 17,457 cycles
PAX DOOR SEAL RETAINER IS DENTED AT HINGE LINE. C-CHECK, INSTALLED NEW PAX DOOR SEAL RETAINER IAW REO.
Part: LUG — CHAFED (PAX DOOR HINGE) · airframe 29,185 hrs · 17,457 cycles
PAX DOOR HINGE LUGS ON DOOR SIDE ARE CHAFED. C-CHECK, BLENDED OUT CHAFES ON PAX DOOR HINGE LUGS IAW REO.
Part: ROLLER — WORN (PAX DOOR) · airframe 29,185 hrs · 17,457 cycles
PASSENGER DOOR FWD PULL CLOSE ROLLER LEVER HAS WEAR AT LOWER AREA. C-CHECK, BLENDED CHAFE ON PAX DOOR FWD PULL IN LEVER IAW REO.
Part: SKIN — DENTED (PAX DOOR) · airframe 29,185 hrs · 17,457 cycles
PASSENGER DOOR UPPER INNER SKIN FWD CORNER IS DENTED AND FASTENER IS WORN FROM DOOR HANDLE HITTING AREA. C-CHECK, DRESSED DENT BACK TO ORIGINAL CONTOUR IAW REO.
Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 29,185 hrs · 17,457 cycles
AFT SIDE OF PASSENGER DOOR, VERTICAL TO HORIZONTAL SIDE ANGLE CRACKED BELOW DOOR ASSIST CABLE BRACKET. C-CHECK, REPAIRED PASSENGER DOOR STAIR AFT DRAG ANGLE IAW REO.
Part: DOOR — DAMAGED (NLG) · airframe 29,185 hrs · 17,457 cycles
NLG AFT GEAR DOOR HAS A CHIP OUT OF COMPOSITE ON RT SIDE FWD EDGE AREA. C-CHECK, REPAIRED AFT NLG DOOR IAW EA AND SRM.
Part: SKIN — DENTED (PAX DOOR) · airframe 29,185 hrs · 17,457 cycles
PASSENGER DOOR UPPER INNER SKIN AFT CORNER IS DENTED AND FASTENER IS WORN FROM DOOR HANDLE HITTING AREA. C-CHECK, DRESSED DENT BACK TO ORIGINAL CONTOUR IAW REO.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 29,185 hrs · 17,457 cycles
FS 280, FLOORBEAM CRACKED. C-CHECK, R & R THE FLOORBEAM IAW REO.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,386 hrs · 17,010 cycles
EMERGENCY OVERHEAD LIGHT INOPERATIVE. REPLACED THE LAMP.
Part: UNKNOWN — SMOKE (COCKPIT & CABIN) · airframe 28,344 hrs · 16,990 cycles
DURING DESCENT AND FINAL APPROACH, A STRONG SMOKE ODOR AND SMOKE IN THE COCKPIT AND CABIN. SMOKE DISSIPATED ON LANDING. INTERROGATED MDC AND FOUND NO CURRENT FAULTS. RAN APU WITH EACH PACK WHILE ENGINES OFF WITH NO FAULTS FOUND. ALSO RAN BOTH ENGINES WITH EACH PACK WHILE APU OFF WITH NO DEFECTS NOTED AFTER EXTENDED PERIOD OF TIME. COULD NOT DUPLICATE FAULT AT THIS TIME IAW AMM.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 27,717 hrs · 16,664 cycles
EMERGENCY EXIT SIGN BY SERVICE DOOR IS BURNED OUT, REPLACED LAMP.
2013
Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,420 hrs · 15,950 cycles
GALLEY SERVICE DOOR FLOOR LEVEL EMERGENCY FLOOD LIGHT HAS ONE BURNED OUT. FLT 5220 RELAMPED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,293 hrs · 15,881 cycles
GALLEY SERVICE DOOR LOWER EMERGENCY EXIT LIGHT & RT SIDE EMERGENCY EXIT ROW LIGHT LOWER RT ARE BURNED OUT. FLT#5181 RELAMPED.
Part: PRINTED CKT BOARD — FAULTY (EMERGENCY LIGHTS) · airframe 26,037 hrs · 15,727 cycles
CABIN EMERGENCY LIGHTS ILLUMINATE INTERMITTENTLY. FLT#4968 REPLACED JB-11 PCB-5 IAW AMM.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,161 hrs · 15,233 cycles
REPLACE LT SIDE SEAT TRACK AT FS 711 TO 761. C-CHECK, REPLACED LT SIDE SEAT TRACK IAW AMM AND REO.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,161 hrs · 15,233 cycles
REPLACE RT SIDE SEAT TRACK AT FS 711 TO 761. C-CHECK, REPLACED RT SIDE SEAT TRACK AT F/S 711 TO 761 IAW AMM AND REO.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,161 hrs · 15,233 cycles
REPLACE RT SIDE SEAT TRACK AT FS 673 TO 711. C-CHECK, REPLACED RT SIDE SEAT TRACK AT F/S 673 TO 711 IAW AMM AND REO.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,161 hrs · 15,233 cycles
SEAT TRACK HAS CORROSION AT FS 380 - FS 381 AT RBL 9. C-CHECK, REPAIRED SEAT TRACK AT FS 380 TO FS 381 AT RBL 9.0 IAW REO.
Part: WEB — CRACKED (FUSELAGE) · airframe 25,161 hrs · 15,233 cycles
REPAIR 280 RT LOWER WEB. C-CHECK, COMPLETED REPAIR TO 280 RT LOWER WEB IAW REO.
Part: WEB — CRACKED (FUSELAGE) · airframe 25,161 hrs · 15,233 cycles
REPAIR 280, LEFT LOWER WEB. C-CHECK, COMPLETED REPAIR TO 280 LT LOWER WEB IAW REO.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,161 hrs · 15,233 cycles
SEAT TRACK HAS CORROSION AT FS 517 -FS 522 AT LBL 9. C-CHECK, REMOVED CORROSION AT FS 517 TO 522 LBL 9 IAW SRM AND REO.
Part: BATTERY — DISCHARGED (CABIN) · airframe 25,052 hrs · 15,169 cycles
CABIN EMERGENCY LIGHTS WILL NOT REMAIN ON WHEN SELECTED. (FLT 6399) CHARGED EMERGENCY LIGHT BATTERIES. OPS CHECK GOOD.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,244 hrs · 14,680 cycles
EMERGENCY OVERHEAD LIGHT NR 5 BURNED OUT. (FLT 6245) RELAMPED EMERGENCY LIGHT.
2012
Part: SIGN — MISSING (CABIN) · airframe 23,753 hrs · 14,375 cycles
IN GALLEY AREA, EXIT SIGN IS MISSING. (FLT 6439) REPLACED FLOOR LEVEL EMERGENCY FLOOD LIGHT ASSEMBLY.
Part: CONTROL UNIT — FAILED (GENERATOR SYS) · airframe 23,412 hrs · 14,167 cycles
ADG DID NOT DEPLOY ON LOSS OF ALL AC POWER. (FLT 1300) REPLACED ADG GENERATOR CONTROL UNIT IN REFERENCE TO AMM. P/N OFF: 761341A S/N OFF: 1283.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,073 hrs · 13,976 cycles
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6387) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,996 hrs · 13,936 cycles
NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,143 hrs · 13,466 cycles
LAST OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,025 hrs · 13,407 cycles
NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5492) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,554 hrs · 13,137 cycles
NR 4, 5, AND 6 OVERHEAD EMERGENCY LIGHTS ARE OUT. (SERVICE) RELAMPED EMERGENCY LIGHTS.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,537 hrs · 13,127 cycles
NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5427) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,268 hrs · 12,977 cycles
NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5589) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,194 hrs · 12,940 cycles
NR 4 AND 5 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 5589) RELAMPED EMERGENCY LIGHTS.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,040 hrs · 12,842 cycles
NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5302) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,975 hrs · 12,806 cycles
OVERHEAD EMERGENCY LIGHT AT ROW 15 IS OUT. (FLT 5207) RELAMPED EMERGENCY LIGHT.
2011
Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,698 hrs · 12,633 cycles
THE 4TH OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5178) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,698 hrs · 12,633 cycles
OVERHEAD EMERGENCY LIGHT AT ROW 11 IS OUT. (FLT 6298) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,560 hrs · 12,555 cycles
NR 4 CEILING EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 22,189 hrs · 13,495 cycles
FS 280 FLOORBEAM CRACKED. (C-CHECK) REPLACED FLOORBEAM PER SRM.
Part: FITTING — CRACKED (FUSELAGE) · airframe 22,189 hrs · 13,495 cycles
CRACK AT STRINGER L3 PAX DOOR LINTEL AT 280 CIRCUMFERENTIAL JOINT. (C-CHECK) REPLACED PER REO.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,447 hrs · 12,495 cycles
NR 4 AND 5 OVERHEAD EMERGENCY LIGHT ARE OUT. (FLT 5196) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,359 hrs · 12,453 cycles
NR 5 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5452) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,232 hrs · 12,387 cycles
NR 5 OVERHEAD EMERGENCY LIGHT IS INOPERATIVE. (FLT 5510) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,160 hrs · 12,334 cycles
NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6198) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,113 hrs · 12,311 cycles
SECOND TO LAST CEILING EMERGENCY LIGHT IS OUT. (FLT 5439) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,113 hrs · 12,311 cycles
THE 3RD FROM AFT OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,835 hrs · 12,156 cycles
NR 4 EMERGENCY OVERHEAD LIGHT IS OUT. (FLT 6219) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,814 hrs · 12,147 cycles
OVERHEAD EMERGENCY LIGHT AT ROW 9 IS OUT. (FLT 5635) RELAMPED EMERGENCY LIGHT.
Part: BRAKE — DRAGGING (LT MLG) · airframe 19,678 hrs · 12,071 cycles
LEFT BRAKE NR 1 DRAGGING. (FLT 1180) REPLACED THE NR 1 BRAKE ASSEMBLY, NR 1 AND NR 2 WHEEL ASSEMBLIES. P/N: 5013642-1, S/N ON: DEC03-0971, S/N OFF: JUL05-1147.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,296 hrs · 11,866 cycles
AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5651) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,059 hrs · 11,724 cycles
OVERHEAD EMERGENCY LIGHT ABOVE ROW 9 IS OUT. (FLT 6254) RELAMPED EMERGENCY LIGHT.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 19,059 hrs · 11,724 cycles
LEFT EMERGENCY EXIT SIGN BY OVERWING EXIT DOOR IS OUT. (SERVICE) REPLACED NR 3 ELBP. P/N: AD-2013-1A, S/N OFF: 40211.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,934 hrs · 11,651 cycles
AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6714) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 18,668 hrs · 11,506 cycles
RIGHT AFT EXTERIOR EMERGENCY LIGHT IS OUT. (FLT 1140) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,621 hrs · 11,480 cycles
NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6447) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,539 hrs · 11,428 cycles
AFT OVERHEAD EMERGENCY EXIT LIGHT IS OUT. (FLT 1123) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,115 hrs · 11,174 cycles
OVERHEAD EMERGENCY LIGHT IS OUT AT ROW 9. (FLT 6552) RELAMPED EMERGENCY LIGHT.
2010
Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,653 hrs · 10,895 cycles
OVERHEAD EMERGENCY LIGHT AT ROW 9 OUT. (FLT 6878) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 17,036 hrs · 10,525 cycles
EMERGENCY EXIT SIGN ON LEFT SIDEWALL NEAR OVERWING EXTERIOR IS INOPERATIVE. (FLT 6761) RELAMPED EMERGENCY EXIT SIGN.
Part: BATTERY — DISCHARGED (CABIN) · airframe 16,826 hrs · 10,391 cycles
LOWER EMERGENCY EXIT LIGHT SIGN FORWARD OF LEFT OVERWING EXIT IS OUT. (FLT 6400) REPLACED NR 4 BATTERY AND BATTERY CHARGER ASSEMBLY.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 16,776 hrs · 10,364 cycles
FS 280 FLOOR SUPPORT BEAM IS CRACKED & HAS CORROSION. (C-CHECK) REMOVED AND REPLACED FS 280 FLOORBEAM PER SRM.
2009
Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,564 hrs · 9,051 cycles
NR 4 OVERHEAD EMERGENCY LIGHT INOP. (FLT 5837)RELAMPED.
Part: BUSHING — CORRODED (ENGINE MOUNT) · airframe 14,094 hrs · 8,788 cycles
RIGHT ENGINE FORWARD MOUNT LINK BUSHINGS AND BEARING CORRODED. (ENG CHG) REPLACED LINK AND BUSHINGS PER AMM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,887 hrs · 8,670 cycles
AFT CEILING EMERGENCY LIGHT INOP. (FLT 6647) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,418 hrs · 8,405 cycles
AFT CEILING EMERGENCY LIGHT INOP. (FLT 5127) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,126 hrs · 8,225 cycles
REAR CEILING EMERGENCY LIGHT INOP. (FLT 6431) RELAMPED EMERGENCY LIGHT.
Part: ACM — SMOKE (RIGHT) · airframe 12,732 hrs · 7,990 cycles
FLT 5896 - SMOKE IN CABIN. REPLACED RT PACK, PN: GG670-95009-5, SN OFF: 00905.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 11,838 hrs · 7,462 cycles
FLT 6072 - AFT CEILING MOUNTED EMERGENCY LIGHTS INOP. RELAMPED.
2008
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 11,610 hrs · 7,322 cycles
DURING C-CHECK, FS280 FLOORBEAM CRACKED RIGHT SIDE. REPAIRED PER REO.
Part: STIFFENER — CRACKED (BULKHEAD) · airframe 11,610 hrs · 7,322 cycles
DURING C-CHECK, FS 280 BULKHEAD WEB STIFFENER AT RBL 25.5 CRACKED. REPAIRED PER SRM.
Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 11,400 hrs · 7,194 cycles
FLT 6732 - RIGHT SIDE LOWER WALL MOUNTED EMERGENCY EXIT SIGN HAS ONE LIGHT BULB INOP. RELAMPED.
Part: BULB — LOOSE (EMERGENCY LIGHT) · airframe 11,382 hrs · 7,184 cycles
FLT 6547 - NR 4 EMERGENCY LIGHT INOP. RESEATED BULB.
2007
Part: FLOORBEAM — CRACKED (BS 280) · airframe 8,639 hrs · 5,590 cycles
FS 280 FLOORBEAM IS CRACKED AT LBL9, FOUND AT C-CHECK. INSTALLED FLOORBEAM REPAIR PER CRJ700/900 SRM 51-42-21 AND 51-42-06.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 8,639 hrs · 5,590 cycles
COCKPIT FLOORBEAM IS CRACKED AT FS 280 AND RBL 9, FOUND AT C-CHECK. INSTALLED COCKPIT FLOORBEA, PER CRJ700/900 SRM 51-42-06 AND 51-40-11.
Part: LIGHT — BROKEN (CABIN) · airframe 6,968 hrs · 4,542 cycles
EMERGENCY EXIT LIGHT NEAR SERVICE DOOR IS BROKE OFF. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY WITH A SERVICABLE UNIT. OPS CHECK GOOD.
Part: HANDLE — LACK OF LUBE (PAX DOOR) · airframe 6,825 hrs · 4,468 cycles
FLIGHT ATTENDANT REPORTS THAT MAIN CABIN DOOR IS DIFFICULT TO OPEN. LUBRICATED INNER HANDLE SPRING ROLLER AND OVER CENTER GROOVE. OPS CHECK GOOD.
Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 5,380 hrs · 3,564 cycles
FORWARD EMERGENCY EXIT LIGHT INOP. RELAMPED BULBS AT FORWARD EMERGENCY EXIT LIGHT. OPERATIONAL CHECKS GOOD.
Part: LIGHT — SMOKE (CABIN) · airframe 5,306 hrs · 3,518 cycles
SMOKE FROM FOS SIDE FLOOD LIGHTS. REPLACED RHEOSTAT AND LIGHT ASSEMBLY ABOVE LIGHTING PANEL. OPERATIONAL CHECKS GOOD IAW AMM 33-24-01.
2006
Part: SUPPORT — CRACKED (PAX DOOR) · airframe 4,294 hrs · 2,858 cycles
PAX DOOR FWD SIDE CRACKED AT HANDRAIL SUPPORT, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED P/N 670-52-11-104 -1;-3;-2 REPAIR PARTS ONTO FWD SIDE OF PAX DOOR PER CRJ 700 REO 670-52-11-104.
Part: SUPPORT — CRACKED (PAX DOOR) · airframe 4,294 hrs · 2,858 cycles
PAX DOOR AFT SIDE CRACKED AT HANDRAIL SUPPORT, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS PER CRJ700 REO 670-52-11-104 REV 'A'.
2005
Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 1,850 hrs · 1,274 cycles
RECEIVED A -SPLR/STAB FAULT- STATUS MSG. REPLACED SSCU 2 IAW CRJ MM27-61-05. OPERATIONAL CHECK GOOD.
Part: ACTUATOR — MALFUNCTIONED (RUDDER LIMITER) · airframe 1,472 hrs · 1,028 cycles
RUDDER LIMIT FAULT STATUS MESSAGE. REPLACED NR 1 RUDDER LIMITER ACTUATOR IAW CRJ MM 27-25-03. OPERATIONAL CHECK GOOD.
Part: TRANSMITTER — MALFUNCTIONED (LT ELEVATOR) · airframe 534 hrs · 369 cycles
ELEVATOR SPLIT CAUTION MSG ILLUMINATED IN FLIGHT. REPLACED LEFT ELEVATOR POSITION TRANSMITTER IAW 27-34-10, OPERATIONAL CHECK GOOD.
Part: CONTROL UNIT — MALFUNCTIONED (SPOILERS) · airframe 209 hrs · 150 cycles
RUDDER LIMIT FAULT STATUS MESSAGE DISPLAYED ON EICAS. REPLACED NR 1 SSCU IAW CRJ 700 MM 27-61-05. OPERATIONAL CHECK GOOD.