N922EV
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.
159 reports on file, 2004-08-08 – 2020-12-28.
Part: SKIN — DENTED (FUSELAGE) · airframe 34,933 hrs · 35,113 cycles
TRANSFER FROM EAML 550059. DENT BETWEEN FS 640 AND 672.2 HAS LARGE DENT APPROXIMATELY 6.4 X 6.3 INCHES WITH HOLE IN CENTER APPROXIMATELY 2.6 X 1.8 INCHES. LT FUSELAGE STRUCTURE DAMAGE BETWEEN FS 640.00 AND FS 672.20, STR 13L AND 16L WAS REPAIRED BY BOMBARDIER MOBILE REPAIR TEAM, IAW REO 601R-53-61-7522 REV DATED 1/3/21. REF ATTACHED BOMBARDIER WORK ORDER. C/W 51-900-1003-SKY AND FORM M-337.
Part: BULKHEAD — DAMAGED · airframe 34,700 hrs · 34,802 cycles
EVALUATE CENTER 9G BULKHEAD AFT SIDE DAMAGE AT INSERT/RIV NUT LOCATIONS, REFERENCE RIL 5378. REPAIR IF NEEDED, IAW ENGINEERING INSTRUCTIONS. C-CHECK RO 10/18/2020. COMPLIED WITH MHIRJ EO IN REPAIR OF TOOLING DAMAGE TO CENTER 9G BULKHEAD AFT WALL. REPAIR DOUBLER MATERIAL 2024-T3 .040 P/O W58363. DEPTH GAGE WVACT 204441 CAL DUE 28 FEB 2021. COMPLETED TASK CARD, FORM M-337 ATTACHED. NO WEIGHT REMOVED, TOTAL WEIGHT ADDED .826 LBS.
Part: BULKHEAD — DAMAGED · airframe 34,700 hrs · 34,802 cycles
EVALUATE LT 9G BULKHEAD AFT SIDE DAMAGE AT INSERT/RIV NUT LOCATIONS, REFERENCE RIL NR 5378. REPAIR IF NEEDED, IAW ENGINEERING INSTRUCTIONS. C-CHECK RO 10/18/2020. COMPLIED WITH MHIRJ EO IN REPAIR OF TOOLING DAMAGE TO LT 9G BULKHEAD AFT WALL. REPAIR DOUBLER MATERIAL 2024-T3 .040 P/O W58363. INSERT 2 EACH P/N CDSP5905-3-44. NEW P-SEAL P/N 1024. P/O W72038. DEPTH GAGE WVACT 204441 CAL DUE 28 FEB 2021. COMPLETED TASK CARD, FORM M-337 ATTACHED. NO WEIGHT REMOVED, TOTAL WEIGHT ADDED 1.715 LBS.
Part: BULKHEAD — DAMAGED (ZONE 200) · airframe 34,700 hrs · 34,802 cycles
EVALUATE RT 9G BULKHEAD AFT SIDE DAMAGE AT INSERT/RIV NUT LOCATIONS, REFERENCE RIL 5378. REPAIR IF NEEDED, IAW ENGINEERING INSTRUCTIONS. C-CHECK RO 10/18/2020. COMPLIED WITH MHIRJ EO IN REPAIR OF TOOOLING DAMAGE TO RT 9G BULKHEAD AFT WALL. REPAIR DOUBLER MATERIAL 2024-T3 .040 P/O W58363. INSERT 2 EACH P/N CDSP5905-3-44. NEW P-SEAL P/N 1024 P/O W72038. DEPTH GAGE WVACT 204441 CAL DUE 28 FEB. 2021. COMPLETED TASK CARD, FORM M-337 ATTACHED. NO WEIGHT REMOVED, TOTAL WEIGHT ADDED .822 LBS.
Part: FLOORBEAM — CORRODED (BS 559) · airframe 34,700 hrs · 34,802 cycles
FLOOR SUPPORT PLATE AT FS 559+48 BETWEEN RBL 9 AND RBL 27 IS CORRODED. C-CHECK RO 10/18/2020. REMOVED AND REPLACED FLOOR SUPPORT PLATE AT FS 559+48 BETWEEN RBL 9 AND RBL 27, IAW CRJ 200 SRM. REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
Part: CONTROL ROD — CORRODED (RT ELEVATOR) · airframe 34,700 hrs · 34,802 cycles
RT ELEVATOR SYSTEM MECHANICAL CONTROL PATH INPUT ROD BEARING AND HARDWARE LOCATED AFT END OF VERTICAL STABILIZER CANTED RIB APPEARS TO HAVE CORROSION (RUST). C-CHECK RO 10/18/2020. REMOVED AND REPLACED LT ELEVATOR CONTROL PATH INPUT ROD AND FWD AND AFT HARDWARE, IAW CRJ 200 AMM. OPERATIONS CHECK GOOD AT THIS TIME.
Part: CONTROL ROD — CORRODED (LT ELEVATOR) · airframe 34,700 hrs · 34,802 cycles
LT ELEVATOR SYSTEM MECHANICAL CONTROL PATH INPUT ROD BEARING AND HARDWARE LOCATED AFT END OF VERTICAL STABILIZER CANTED RIB APPEARS TO HAVE CORROSION (RUST). C-CHECK RO 10/18/2020. REMOVED AND REPLACED LT ELEVATOR CONTROL PATH INPUT ROD AND FWD AND AFT HARDWARE, IAW CRJ 200 AMM. OPERATIONS CHECK GOOD AT THIS TIME.
Part: WINDOW POST — CRACKED (WINDSHIELD) · airframe 34,700 hrs · 34,802 cycles
RT WINDSHIELD SIDE POST LOWER AFT FITTING IS CRACKED. C-CHECK RO 10/18/2020. REMOVED DAMAGED RT WINDSHIELD SIDE POST LOWER AFT FITTING. LOCATED, DRILLED, AND INSTALLED NEW SERVICEABLE FITTING, IAW CRJ200-SRM.
Part: WINDOW POST — CHAFED (WINDSHIELD) · airframe 34,700 hrs · 34,802 cycles
STRAP ON WINDSHIELD CENTER POST, ATTACHING CENTER POST TO CENTER SUPPORT CLIPS FOUND TO BE CHAFED. CAUSED BY CRACKED LT SUPPORT CLIP, P/N 601R34012-25. C-CHECK RO 10/18/2020. REMOVED DAMAGED WINDSHIELD CENTER POST STRAP AND INSTALLED NEW SERVICEABLE STRAP, IAW CRJ200-SRM.
Part: FITTING — CRACKED (WINDSHIELD) · airframe 34,700 hrs · 34,802 cycles
WINDSHIELD CENTER SUPPORT CLIPS ON THE LT AND RT SIDE ARE CRACKED. C-CHECK RO 10/18/2020. REMOVED DAMAGED WINDSHIELD CENTER SUPPORT CLIPS ON THE LT AND RT SIDE AND INSTALLED NEW SERVICEABLE CLIPS, IAW CRJ200.
Part: ANGLE — CRACKED (LT WING) · airframe 34,700 hrs · 34,802 cycles
UPPER ANGLE COMMON TO THE LT INBOARD BATTERY RIB AT WS 48.30 IS CRACKED. C-CHECK RO 10/18/2020. REMOVED AND REPLACED ANGLE, IAW CRJ 200 SRMS. REFER TO CONTINUE CARD FOR WORK PERFORMED.
Part: COUNTERBALANCE — CRACKED (PAX DOOR) · airframe 34,700 hrs · 34,802 cycles
AFT ANCHOR FITTING FOR PASSENGER DOOR COUNTERBALANCE IS CRACKED. C-CHECK RO 10/18/2020. REMOVED AND REPLACED PAX DOOR ANCHOR FITTING, IAW CRJ 200 AMM.
Part: FLOORBEAM — CORRODED (BS 559) · airframe 34,700 hrs · 34,802 cycles
FS 559.0+80 CROSS BEAM RBL 9 TO RBL 27 IS CORRODED. C-CHECK RO 10/18/2020. REMOVED AND REPLACED FLOOR SUPPORT PLATE AT FS 559.0+80 ON TOP OF CROSS BEAM RBL 9 TO RBL 27, IAW CRJ 200 SRM.
Part: SEAT TRACK — CORRODED (BS 364-400) · airframe 34,700 hrs · 34,802 cycles
SEAT TRACK SEGMENT AT RBL 9 BETWEEN FS 364 TO FS 400 IS CORRODED. C-CHECK RO 10/18/2020. REMOVED, FABRICATED, AND REPLACED SEAT TRACK, IAW CRJ 200 SRM & REO. REFER TO CONTINUE CARD FOR WORK PERFORMED.
Part: SEAT TRACK — CORRODED (BS 559) · airframe 34,700 hrs · 34,802 cycles
LBL 27 FLOOR SEAT RAIL IS CORRODED BETWEEN FS 559.0+80 TO 559.0+96. C-CHECK RO 10/18/2020. REMOVED AND REPLACED SEAT RAIL BETWEEN LBL 27 BETWEEN FS 559.0+80 TO 559.0+96, IAW CRJ 200 AMM.
Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 34,700 hrs · 34,802 cycles
FLOOR BEAM AT RBL 9 UPPER INBOARD FLANGE IS CORRODED AT MULTIPLE LOCATIONS BETWEEN FS 409+128 TO FS 559 AND OUTBOARD FLANGE IS CORRODED AT 1 LOCATION AT FS 559. C-CHECK RO 10/18/2020. REPAIRED FLOOR BEAM AT RBL 9 UPPER INBOARD FLANGE CORROSION AT MULTIPLE LOCATIONS BETWEEN FS 409+128 TO FS 559 AND OUTBOARD FLANGE CORROSION AT 1 LOCATION AT FS 559, IAW MHIRJ REO. REFERENCE ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED. MAJOR REPAIR TASK CARD & FORM M337 COMPLETED AND ATTACHED. NO MEASURABLE WEIGHT CHANGE TO RECORD.
Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 34,700 hrs · 34,802 cycles
RIGHT SIDE FLOOR SILL HAS MULTIPLE AREAS OF CORROSION BETWEEN FS 409+128 TO FS 559. C-CHECK RO 10/18/2020. REPAIRED RT SIDE PRESSURE FLOOR SILL CORROSION AT MULTIPLE LOCATIONS BETWEEN FS 409+128 TO FS 559, IAW REO. MAJOR REPAIR TASK CARD & FORM M337 COMPLETED AND ATTACHED. NO MEASURABLE WEIGHT CHANGE. NOTE REPAIR REQUIRES A DETAILED VISUAL INSPECTION EVERY 8260 FLIGHT CYCLES WITH A REPEAT EVERY 8260 FLIGHT CYCLES FIRST INSPECTION IS DUE AT 43061 FLIGHT CYCLE. REFERENCE ATTACHED CONTINUATION CARD FOR DETAILS OF LOCATIONS OF BLENDING AND WORK PERFORMED.
Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 34,700 hrs · 34,802 cycles
FLOOR BEAM AT LBL 9 UPPER INBOARD FLANGE IS CORRODED AT MULTIPLE LOCATIONS BETWEEN FS 409+128 TO FS 559. C-CHECK RO 10/18/2020. REPAIRED FLOORBEAM, IAW REO. WEIGHT CHANGE +1.55 LB. MAJOR REPAIR TASK & FORM M337 COMPLETED AND ATTACHED. REFER TO CONTINUE CARD FOR WORK PERFORMED.
Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 34,700 hrs · 34,802 cycles
SEAT TRACK SEGMENT AT LBL 9 BETWEEN FS 409+128 TO FS 559 IS CORRODED MULTIPLE LOCATIONS. C-CHECK RO 10/18/2020. REMOVED, FABRICATED, AND INSTALLED SEAT TRACK, IAW CRJ 200 AMM & REO. REFER TO CONTINUATION CARD FOR WORK PERFORMED.
Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 34,700 hrs · 34,802 cycles
SEAT TRACK SEGMENT AT RBL 9 BETWEEN FS 409+128 TO FS 559 IS CORRODED AT MULTIPLE LOCATIONS. C-CHECK RO 10/18/2020. REMOVED, FABRICATED, AND INSTALLED SEAT TRACK, IAW CRJ 200 AMM & REO. REFER TO CONTINUE CARD FOR WORK PERFORMED.
Part: SEAT TRACK — CORRODED (BS 559) · airframe 34,700 hrs · 34,802 cycles
FLOOR SEAT TRACK ON RBL 9 BETWEEN FS 559.0+80 TO FS 559.0+96 IS CORRODED. C-CHECK RO 10/18/2020. REMOVED AND REPLACED SEAT TRACK ON RBL 9 BETWEEN FS 559.0+80 TO FS 559.0+96, IAW CRJ 200 AMM.
Part: FLOOR SUPPORT — CORRODED (BS 409) · airframe 34,700 hrs · 34,802 cycles
FLOOR BEAM LBL 9 UPPER INBOARD FLANGE IS CORRODED AT APPROXIMATELY FS 409+30, FS 409+60 AND FS 409+118. C-CHECK RO 10/18/2020. REMOVED, FABRICATED, AND REPLACED/INSTALLED FLOORBEAM CAP, IAW REO CRJ 200 SRMS. MAJOR REPAIR TASK & FORM 337 COMPLETED AND ATTACHED. NO MEASUREABLE WEIGHT CHANGE.
Part: SEAT TRACK — CORRODED (BS 559) · airframe 34,700 hrs · 34,802 cycles
RBL 27 SEAT TRACK IS CORRODED FROM FS 559.0+80 TO FS 559.0+96. C-CHECK RO 10/18/2020. REMOVED AND REPLACED SEAT TRACK FROM FS 559.0+80 TO FS 559.0+96 AT RBL 27, IAW CRJ 200.
Part: ATTACH ANGLE — CRACKED (BS 484) · airframe 34,700 hrs · 34,802 cycles
INBOARD AND OUTBOARD ANGLE ATTACHING TO FS 484 INTERCOSTAL BETWEEN PRESSURE FLOOR BEAM LBL 27 AND LBL 36 ARE CRACKED AT UPPER EDGE AT FASTENER HOLE. C-CHECK RO 10/18/2020. REMOVED AND REPLACED ANGLES, IAW CRJ 200 SRM. REFER TO CONTINUE CARD FOR WORK PERFORMED.
Part: SEAT TRACK — CORRODED (BS 364-400) · airframe 34,700 hrs · 34,802 cycles
SEAT TRACK SEGMENT AT LBL 9 BETWEEN FS 364 TO FS 400 IS CORRODED. C-CHECK RO 10/18/2020. REMOVED AND REPLACED SEAT TRACK SEGMENT AT LBL 9 BETWEEN FS 364 AND FS 400, IAW CRJ 200 AMM. REFERENCE ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
Part: SEAT TRACK — CORRODED (BS 559-574) · airframe 34,700 hrs · 34,802 cycles
LBL 9 CARGO SEAT TRACK IS CORRODED BETWEEN FS 559.00+112 TO FS 574. C-CHECK RO 10/18/2020. REMOVED AND REPLACED LBL 9 CARGO SEAT TRACK, IAW AMM.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 34,700 hrs · 34,802 cycles
INBOARD AND OUTBORD ANGLES ATTACHING THE LBL 9 FLOOR BEAM AT FS 280 CROSSBEAM ARE CRACKED IN UPPER RADIUS. C-CHECK RO 10/18/2020. REMOVED AND REPLACED CRACKED CLIPS 2 EA AT STA 280 LBL 9, IAW CRJ200 SRM.
Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 34,700 hrs · 34,802 cycles
LEFT SIDE PRESSURE FLOOR SILL HAS CORROSION AT MULTIPLE LOCATIONS BETWEEN FS 409+128 TO FS 559. C-CHECK RO 10/18/2020. REPAIRED LEFT SIDE PRESSURE FLOOR SILL CORROSION AT MULTIPLE LOCATIONS BETWEEN FS 409+128 TO FS 559, IAW REO. COMPLETED AND ATTACHED TASK CARD & FORM M337. WEIGHT & BALANCE NOT AFFECTED. NOTE REPAIR REQUIRES A DETAILED VISUAL INSPECTION EVERY 8260 FLIGHT CYCLES WITH A REPEAT EVERY 8260 FLIGHT CYCLES FIRST INSPECTION IS DUE AT 43061 FLIGHT CYCLE. REFERENCE ATTACHED CONTINUATION CARD FOR DETAILS OF LOCATIONS OF BLENDING AND WORK PERFORMED.
Part: ATTACH ANGLE — CRACKED (BS 484) · airframe 34,700 hrs · 34,802 cycles
INBOARD AND OUTBOARD ANGLE ATTACHING TO FS 484 INTERCOSTAL BETWEEN PRESSURE FLOOR BEAM RBL 27 AND RBL 36 ARE CRACKED AT UPPER EDGE AT FASTENER HOLE. C-CHECK RO 10/18/2020. REMOVED AND REPLACED ANGLES, IAW CRJ 200 SRM. REFER TO CONTINUE CARD FOR WORK PERFORMED.
Part: SEAT TRACK — CORRODED (BS 559-574) · airframe 34,700 hrs · 34,802 cycles
RBL 9 FLOOR SEAT TRACK IS CORRODED BETWEEN FS 574 TO FS 559.0+112. C-CHECK RO 10/18/2020. REMOVED AND REPLACED CORRODED SEAT TRACK, IAW CRJ200 AMM. USED TOOL WVACT 6025 CAL DUE 31 MAR 2021.
Part: FRAME — CORRODED (BS 349) · airframe 34,700 hrs · 34,802 cycles
FRAME SECTOR FS 349 IS CORRODED BETWEEN STRINGERS 25L TO 26R. C-CHECK RO 10/18/2020. REMOVED AND REPLACED FRAME SECTOR FS 349 BETWEEN STRINGERS 25L AND 26R, IAW CRJ 200 SRM. REFERENCE ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 34,700 hrs · 34,802 cycles
RBL 9 FLOOR BEAM IS CORRODED BETWEEN FS 559.0+96 TO FS 559.0+112. C-CHECK RO 10/18/2020. REMOVED FABRICATED OUT OF N126-1577 EXTRUSION AND INSTALLED NEW RBL 9 FLOOR BEAM CAP BETWEEN FS 559.0+96 TO FS 559+112, IAW CRJ 200 SRM & IAW MHIRJ REO. REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
Part: BRACKET — CRACKED (BS 621) · airframe 34,700 hrs · 34,802 cycles
OBLIQUE ANGLE IS CRACKED IN RADIUS AT STRINGER 14R AFT SIDE OF FS 621 BULKHEAD. C-CHECK RO 10/18/2020. REMOVED AND REPLACED OBLIQUE ANGLE AT STRINGER 14R ON AFT SIDE OF FS 621 BULKHEAD, IAW BOMBARDIER REO.
Part: ANGLE — CRACKED (BS 621) · airframe 34,700 hrs · 34,802 cycles
OBLIQUE ANGLE IS CRACKED IN RADIUS AT STRINGER 14L AFT SIDE OF FS 621 BULKHEAD. C-CHECK RO 10/18/2020. REMOVED AND REPLACED OBLIQUE ANGLE AT STRINGER 14L AFT SIDE OF FS 621 BULKHEAD, IAW BOMBARDIER REO.
Part: GUSSET — CORRODED (DOOR FRAME) · airframe 34,700 hrs · 34,802 cycles
PAX DOOR SURROUND STRUCTURE GUSSET CORRODED AT FS 349 AT STGR 15L. C-CHECK RO 10/18/2020. REMOVE AND REPLACED PAX DOOR SURROUND STRUCTURE GUSSET AT FS 349 AT STR 15L, IAW CRJ SRM.
Part: GUSSET — CORRODED (DOOR FRAME) · airframe 34,700 hrs · 34,802 cycles
PAX DOOR SURROUND STRUCTURE GUSSET CORRODED BETWEEN STGR 15L AND STGR 16L AT FS 310. C-CHECK RO 10/18/2020. REMOVED AND REPLACED GUSSET, IAW CRJ 200 SRM. REFER TO CONTINUE CARD FOR WORK PERFORMED.
Part: FLOORBEAM — CORRODED (BS 349) · airframe 34,700 hrs · 34,802 cycles
SERVICE DOOR FLOOR BEAM ANGLE CORRODED AT STGR 18 AND AT FS 349. C-CHECK RO 10/18/2020. REPAIRED SERVICE DOOR FLOOR BEAM ANGLE AT STGR 18 AT FS 349, IAW REO. SEE ATTACHED STRUCTURAL MAJOR REPAIR TASK CARD AND CONTINUE CARD FOR DETAILS OF WORK PERFORMED. NO WEIGHT CHANGE NOTED.
Part: HINGE — CORRODED (PAX DOOR) · airframe 34,700 hrs · 34,802 cycles
PAX DOOR FWD AND AFT HINGE CUPS CORRODED. C-CHECK RO 10/18/2020. REMOVED AND REPLACED FWD AND AFT HINGE CUPS AT PAX DOOR LOWER SILL, IAW CRJ 200 SRM.
Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 34,700 hrs · 34,802 cycles
PAX DOOR INTERCOSTAL DD6 CORRODED. C-CHECK RO 10/18/2020. REPAIRED IAW REO. MAJOR REPAIR TASK CARD AND FORM M337 ATTACHED. NO MEASURABLE WEIGHT CHANGE REQUIRED. REFER TO CONTINUE CARD FOR WORK PERFORMED.
Part: BRACKET — CRACKED (LT MLG WW) · airframe 34,700 hrs · 34,802 cycles
LT MLG WHEEL WELL FWD HYDRAULIC FUSE BRACKET IS CRACKED. C-CHECK RO 10/18/2020. REMOVED AND REPLACED HYD FUSE BRACKET, IAW CRJ200 SRM. REFER TO CONTINUE CARD FOR WORK PERFORMED.
Part: BRACKET — CRACKED (RT MLG WW) · airframe 34,700 hrs · 34,802 cycles
RT MLG WHEEL WELL FWD HYDRAULIC FUSE BRACKET IS CRACKED. C-CHECK RO 10/18/2020. REMOVED AND REPLACED BRACKET AT RT MLG WHEEL WELL FWD HYDRAULIC FUSE, IAW CRJ200 SRM.
Part: SUPPORT — CRACKED (WINDSHIELD LFT) · airframe 34,700 hrs · 34,802 cycles
LEFT WINDSHIELD SIDE POST SUPPORT P/N 601R34032-21 IS CRACKED AT THE RADIUS ABOVE STRINGER. C-CHECK RO 10/18/2020. REMOVED AND REPLACED SUPPORT, IAW CRJ 200 SRM. MAJOR REPAIR TASK AND FORM M337 COMPLETED AND ATTACHED. NO WEIGHT CHANGE, WAS A PART FOR PART REPLACEMENT. REFER TO CONTINUE CARD FOR WORK PERFORMED.
Part: SUPPORT — CRACKED (WINDSHIELD) · airframe 34,700 hrs · 34,802 cycles
RIGHT WINDSHIELD SIDE POST SUPPORT P/N 601R34032-22 IS CRACKED IN THE RADIUS ABOVE THE STRINGER. C-CHECK RO 10/18/2020. REMOVED AND REPLACED SUPPORT, IAW CRJ 200 SRM. MAJOR REPAIR TASK AND FORM M337 COMPLETED AND ATTACHED. NO WEIGHT CHANGE, WAS A PART FOR PART REPLACEMENT. REFER TO CONTINUE CARD FOR WORK PERFORMED.
Part: ANGLE — CRACKED (RT WS 50.54) · airframe 34,700 hrs · 34,802 cycles
RT WHEEL WELL AT WS 50.54 THERE IS A CRACKED ANGLE. C-CHECK RO 10/18/2020. REMOVED DAMAGED ANGLE IN RT WHEEL WELL AT WS 50.54. LOCATED, DRILLED, AND INSTALLED NEW SERVICEABLE ANGLE, IAW CRJ200-SRM.
Part: SKIN — CORRODED (BS 559) · airframe 34,700 hrs · 34,802 cycles
FOUND MINOR EXTERNAL SKIN CORROSION ON BELLY SKIN PANEL FS 559.00+92 TO FS 559.00+112 BETWEEN STGR 26L AND 26R. C-CHECK RO 10/18/2020. REPAIRED IAW REO. MAJOR REPAIR TASK & FORM M337 COMPLETED AND ATTACHED. NO MEASURABLE WEIGHT CHANGE. REFER TO CONTINUE CARD FOR WORK PERFORMED.
Part: SKIN — CHAFED (BS 513) · airframe 34,700 hrs · 34,802 cycles
LOWER WING PLANK HAS MINOR CHAFING DAMAGE FROM FUSELAGE FAIRING AT AT BOTH LBL 45 AND RBL 45 AT APPROXIMATELY FS 513. C-CHECK RO 10/18/2020. REPAIRED IAW REO. NO MEASUREABLE WEIGHT CHANGES. MAJOR REPAIR TASK CARD & FORM M337 COMPLETED AND ATTACHED. REFER TO CONTINUE CARD FOR WORK PERFORMED.
Part: ACCESS PANEL — CORRODED (RT WING) · airframe 34,700 hrs · 34,802 cycles
RT WING LOWER SKIN FUEL PANEL ACCESS PANEL CUT OUT 640BB IS CORRODED AROUND CIRFUMFERENCE. C-CHECK RO 10/18/2020. REPAIRED RT WING LOWER SKIN FUEL PANEL ACCESS PANEL CUT OUT 640BB IS CORRODED AROUND CIRFUMFERENCE. BOMBARDIER REO IT WAS IN THE CRITICAL AREA. AWL INSPECT DUE AT 42742 CYCLES WITH A REPEAT AT 51705 CYCLES. MAJOR REPAIR TASK & FORM M337 COMPLETED AND ATTACHED. NO MEASUREABLE WEIGHT CHANGE REQUIRED.
Part: ACCESS PANEL — CORRODED (LT WING) · airframe 34,700 hrs · 34,802 cycles
LT WING LOWER WING PLANK ACCESS PANEL CUTOUT AT 510AB IS CORRODED AROUND THE CIRCUMFERENCE. C-CHECK RO 10/18/2020. REPAIRED LT WING PLANK ACCESS PANEL CUTOUT AT 510AB CORROSION, IAW MHIRJ REO AND BOMARDIER REO. SPECIAL INSPECTION PER NDTM IS DUE AT 62883 FLIGHT CYCLES WITH A REPEAT EVERY 28,082 WHICH WOULD BE AT 90965 CYCLES. NO MEASUREABLE WEIGHT CHANGE. MAJOR REPAIR TASK & FORM M337 COMPLETED AND ATTACHED,
Part: BULKHEAD — CHAFED (RT ENGINE INLET) · airframe 34,700 hrs · 34,802 cycles
RT ENGINE NOSE INLET AFT BULKHEAD INSPECTION HOLES AT 7, 10, AND 12 O`CLOCK POSITIONS ARE CHAFED AND HAVE BENT/MISSING INSPECTION DOORS. C-CHECK RO 10/18/2020. REPAIRED RT ENGINE NOSE INLET AFT BULKHEAD INSPECTION HOLES AT 7, 10, AND 12 O`CLOCK POSITIONS ARE CHAFED AND HAVE BENT/MISSING INSPECTION DOORS, IAW MHIRJ REO. REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED. COMPLETED AND ATTACHED MAJOR REPAIR TASK CARD & FORM M337. NO WEIGHT CHANGE REQUIRED.
Part: SKIN — DENTED (BS 262) · airframe 34,700 hrs · 34,802 cycles
ADM NR N922EV-6861. THE DENT IS ON THE LT SIDE OF THE FUSELAGE AT FS 262.00 AND APPROXIMATELY 35 INCHES DOWN FROM WL 73.50. THE DAMAGE IS A DENT WITH A LENGTH OF 0.975 INCHES AND A WIDTH OF 0.446 INCHES. THE DEPTH OF THE DENT IS 0.012 INCHES. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED. ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES. C-CHECK RO 10/18/2020. REPAIRED DENT ON THE LT SIDE OF THE FUSELAGE AT FS 262.00 AND APPROXIMATELY 35 INCHES DOWN FROM WL 73.50 BETWEEN STR 23L AND STR 24L, IAW MHIRJ REO AND BOMBARDIER REO. REFERENCE ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED. NO WEIGHT CHANGE REQUIRED. MAJOR REPAIR TASK & FORM M337 COMPLETED AND ATTACHED.
Part: FLOORBEAM — DAMAGED (BS 559) · airframe 34,700 hrs · 34,802 cycles
COMPLY WITH REO 601R-53-41-1116 REPAIR & REINFORCEMENT FOR FS 559.00 LOWER CAP ANGLES BL 9.00 & 18.00 LT & RT. C-CHECK RO 10/18/2020. COMPLIED WITH REO. MAJOR REPAIR TASK & FORM M337 COMPLETED AND ATTACHED. WEIGHT CHANGE OF +4.3 LBS. REFER TO ATTACHED CONTINUE CARD FOR DETAILS OF WORK PERFORMED.
Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 34,700 hrs · 34,802 cycles
COMPLY WITH SCHEDULED MAINTENANCE CODE: AD-COMPLY WITH PARAGRAPH (J) OF AD: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION FS 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWL. (J)(2) MODIFYING THE RPB AND DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FS 621 PRESSURE BULKHEAD WEB, IN ACCORDANCE WITH BOMBARDIER REPAIR ENGINEERING ORDER (REO) AND MARKING THIS CAMP AS "STRUCTURAL REPAIR," WHICH WILL GENERATE AN RA FOR TRACKING THE SDIR FOR THIS REO ON THIS AIRPLANE, PART NUMBER: -, SERIAL NUMBER: 7822, POSITION. C-CHECK RO 10/18/2020. COMPLIED WITH PARAGRAPH (J) OF AD BY: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION FS 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWL. (J)(2) MODIFYING THE RPB AND DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FS 621 PRESSURE BULKHEAD WEB, IN ACCORDANCE WITH BOMBARDIER REPAIR ENGINEERING ORDER (REO). AND; MARKING THIS CAMP AS "STRUCTURAL REPAIR," WHICH WILL GENERATE AN RA FOR TRACKING THE SDIR FOR THIS REO ON THIS AIRPLANE. COMPLIED WITH SERIAL NUMBER 7822. COMPLETED MAJOR REPAIR TASK AND FORM M337. REFER TO CONTINUE CARD FOR WORK PERFORMED. WEIGHT CHANGE DOCUMENTED ON CONTINUE CARD.
Earlier reports · 2004–2017 · 107 reports
2017
Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 29,962 hrs · 29,432 cycles
CRACK INDICATION NOTED AT BS 621 REAR PRESSURE BULKHEAD FWD FACE AT RBL 27.5, WL 136. .250 IN LENGTH AND 100% FULL SCREEN HEIGHT FAILING NDT. REPAIRED THE PRESSURE BULKHEAD IAW REO.
Part: SKIN — DENTED (RT WING TE FLAP) · airframe 29,962 hrs · 29,432 cycles
RIGHT INBOARD FLAP LOWER SKIN HAS THREE DENTS ALONG INBOARD EDGE MEASURING .027 INCH DEEP, .072 INCH DEEP AND .041 INCH DEEP. REPAIRED IAW REO.
Part: SKIN — DENTED (LT WING TE FLAP) · airframe 29,962 hrs · 29,432 cycles
LEFT INBOARD FLAP LOWER SKIN HAS A DENT .041 INCH DEEP AT THE INBOARD TRAILING EDGE. REPAIRED IAW REO.
2016
Part: WARNING SYSTEM — OUT OF ADJUST (SERVICE DOOR) · airframe 28,913 hrs · 28,227 cycles
OTBD COOL CAUTION MESSAGE AFTER TAKE OFF. QRH LED TO EMERGENCY DECOMPRESS. ADJUSTED SERVICE DOOR INDICATION SYSTEM IAW 52-70-06, OPS CHECKED GOOD.
Part: LANDING GEAR — MALFUNCTIONED · airframe 27,981 hrs · 27,217 cycles
HYDRALIC 3 CAUTION AND APU ON SELECTING GEAR DOWN LT AND MLG CAUTION MSG EMERGENCY ACTIONS, LANDING GEAR RETRACTION SYSTEM, PERFORMED FUNCTIONAL TEST OF LANDING GEAR EXTENSION/RETRACTION SYS IAW AMM 32-30-00. OPS CK GOOD AT THIS TIME. REMOVED AND STOWED GEAR PINS IAW AMM 10-11-00.
2015
Part: CIRCUIT BOARD — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 25,774 hrs · 24,859 cycles
F/A NOTIFICATION LIGHT AT 11C & 11D AND ALSO EXIT SIGN ILLUMINATED MULTIPLE TIMES AT RANDOM. R & R PSU CIRCUIT BOARD IAW MM 25-28-54. OP'S CHECK GOOD.
Part: LIGHT — BROKEN (CABIN) · airframe 25,628 hrs · 24,710 cycles
WARDROBE FLOOR EMERGENCY FLOODLIGHT HAS BROKEN LENS AND BASE ASSEMBLY. DISCONNECTED THE ELECTRICAL LEADS TO THE WARDROBE EMERGENCY FLOODLIGHT. REMOVED THE BASE BY REMOVING 2 SCREWS. REMOVED THE LIGHT ASSY FROM THE WARDROBE. INSTALLED A NEW BASE BY SECURING TO THE WARDROBE WITH 2 SCREWS. INSTALLED IAW AMM TASK 20-21-00-910-801. INSTALLED NEW LENS COVER BY PRESSING IT ONTO THE BASE TO SECURE IT. INSTALLED THE ELECTRICAL CONNECTORS BY INSERTING THE PLUG END INTO THE RECEPTACLE END. OPS TEST IS GOOD IAW CRJ 200 AMM TASK 33-51-00-710-801.
Part: ANGLE — CRACKED (CARGO DOORWAY) · airframe 25,628 hrs · 24,710 cycles
CARGO DOOR SURROUND, CARGO SILL, FS 605.00 FLOOR ANGLE IS CRACKED. REMOVED CRACKED ANGLE AT FS 605 FLOOR CARGO DOOR STRUCTURE. TRANSFERED HOLES TO NEW ANGLE & DEBURRED IAW SRM 51-40-11 PG 1-2. INSTALLED NEW FLOOR ANGLE AT FS 605.00 IAW SRM 51-42-06, 51-42-10 & 51-42-20.
Part: STRAP — CORRODED (BS 559 FLOORBEAM) · airframe 25,628 hrs · 24,710 cycles
FLOORBEAM STRAP FROM RBL 18 TO RBL 36 AT FS 559.00 IS CORRODED. REMOVED CORRODED STRAP IAW SRM 51-42-06. DRILLED NEW SERVICEABLE STRAP IAW SRM 51-40-11. INSTALLED STRAP IAW SRM 51-42-06.
Part: SKIN — CORRODED (BS 559) · airframe 25,628 hrs · 24,710 cycles
2 EA FASTENERS, LOCATED AT JUST FWD OF FS 559+112, STR 23R ON EXTERNAL SKIN HAVE FILOFORM CORROSION AROUND FASTENER HEADS. FOUND CORROSION UNDER 6 MORE ROWS OF FASTENERS FWD OF FS 559+112. REMOVED 12 EA RIVETS AND REMOVED CORROSION IAW SRM 51-21-06. MAX MATERIAL REMOVED .0035". REPAIRED DAMAGE IAW EA 32-2015-121. FOUND CORROSION ON DOUBLER AT FS 559+112 JUST ABOVE STR 23R. REMOVED 2 EA FASTENERS AND REMOVED CORROSION IAW SRM 51-21-6. REPAIRED DAMAGE IAW EA 32-2015-122. EA 32-2015-121 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUTINE WORK CARD.
Part: BRACKET — CRACKED (E/E BAY) · airframe 25,628 hrs · 24,710 cycles
AFT EQUIPMENT BAY RT SIDE DIRECTLY UNDER ACM HAS CRACKED BRACKET. REMOVED BRACKET IAW SRM 51-42-06. INSTALLED NEW BRACKET, IAW SRM 51-42-06.
Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 25,628 hrs · 24,710 cycles
LBL 27, FLOORBEAM IN CARGO COMPARTMENT HAS AREAS OF EXFOLIATION CORRSION FS 559+80- FS 559+112. COMPLIED WITH EC/TC REO:601R-53-00-005.
Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 25,628 hrs · 24,710 cycles
LEFT FS 621-625 INTERCOSTAL 601-35012-51, CRACKED AT STR 14L. REMOVED CRACKED INTERCOSTAL AT FS 621-FS 625, STR 14L IAW SRM 51-42-21. LOCATED AND DRILLED NEW SERVICEABLE INTERCOSTAL AT FS 621-FS 625, STR 14L IAW SRM 51-40-11 AND INSTALLED INTERCOSTAL IAW SRM 51-42-21.
Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 25,628 hrs · 24,710 cycles
RIGHT FS 621-625 INTERCOSTAL 601-35012-52 CRACKED AT STR 14R. REMOVED CRACKED INTERCOSTAL AT FS 621-FS 625 STR 14R IAW SRM 51-42-21. LOCATED AND DRILLED NEW SERVICEABLE INTERCOSTAL AT FS 621-FS 625, STR 14R IAW SRM 51-40-11 AND INSTALLED INTERCOSTAL IAW SRM 51-42-21.
Part: POST — CRACKED (409) · airframe 25,627 hrs · 24,709 cycles
FS 409+128, BL 0, VERT POST RT SIDE HAS AN INDICATION NOTED IN THE AFT FLANGE RADIUS AT WL 69 .250" LONG X 50 PERCENT FSH. FAILED NDT INSP. REMOVED FS 409+128, BL 0 VERTICAL POST IAW SRM 51-42-06, 51-42-22. LOCATED, DRILLED AND SUBASSEMBLED NEW SERVICEABLE RT VERTICAL POST, PN:601R32208-230S TO LT POST IAW SRM 51-40-11, SRM 51-42-60. SUB ASSEMBLED NEW AND SERVICEABLE INBD & OTBD VERTICAL POST, PN:601R32208-230 AND REQUIRES INSTALL. INSTALLED NEW AND SERVICEABLE SUBASSEMBLED INBD AND OTBD VERTICAL POST AT FS 409+128, BL 0 IAW REO 601R-53-41-889 AND SRM 51-42-06, REO REV A DATED 01/28/10.
Part: POST — CRACKED (BS 409) · airframe 25,627 hrs · 24,709 cycles
FS 409+128, RBL 18 VERT POST INBD AND OTBD SIDES HAVE INDICATIONS NOTED IN THE AFT FLANGE RAD II AT WL 69 .250" LONG X 50 PERCENT FSH. BOTH FAILED NDT INSP. REMOVED VERTICAL POST ASSY AT FS 409+128, RBL 18. INSTALLED RBL 18 FS 409 POST IAW REO 601R-53-41-889, REV A AND SRM 51-42-06. FABRICATED REPLACEMENT STIFFENER SAME AS PN 601R32208-32 USING 7075-0.063" PO W34348 IAW EO EO1R32208.
Part: POST — CRACKED (BS 409) · airframe 25,627 hrs · 24,709 cycles
FS 409+128, LBL 18 VERT POST INBD AND OTBD SIDES HAVE INDICATIONS NOTED IN THE AFT FLANGE RAD II AT WL 69 BOTH APPROX .250" LONG X 50 PERCENT FSH. BOTH FAILED NDT INSP. REMOVED FS 409+128, LBL 18 VERTICAL POST IAW SRM 51-42-06 AND 51-42-22. INSTALLED NEW POST IAW REO 601R-53-41-889 AND SRM 51-42-06. LOCATED, DRILLED AND SUB-ASSEMBLED FS 409+128 LBL 18.00 VERTICAL POSTS IAW SRM 51-40-11, 51-42-06, TR 51-32. COMPLIED WITH EC/TC REO 601R-53-41-889 AND MET ALL THE REQUIREMENTS OF REO 601R-53-41-889, REV A.
Part: FLOOR SUPPORT — CORRODED (BS 568-621) · airframe 25,627 hrs · 24,709 cycles
LBL 9 FLOORBEAM HAS SEVERAL AREAS EXFOLIATION AROUND SCREW HOLES FS 568-FS 621. REMOVED FLOORBEAM LBL 9, FS 568-FS 621. REMOVED, 3 FILLERS, 2 SEAT TRACK LUGS AND 1 SEAT TRACK SECTION AND INBD RIVETS ON FLOORBEAM LBL 9, FS 568-FS 621 IAW SRM 51-41-02 AND 51-42-06. REMOVED FLOORBEAM LBL 9, FS 568-FS 621 IAW SRM 51-42-06 AND 51-42-20. LOCATED AND DRILLED NEW FLOORBEAM, LBL 9, FS 568-FS 621, PN 601R-35031-263 IAW SRM 51-40-11. INSTALLED ALL FASTENERS IN 601R-35031-263 FLOORBEAM IAW REO 601R-53-61-3780, REV A EXCEPT FOR 3 EA AT AFT END OF BEAM MIDDLE ROW, FS 610. INSTALLED 3 EA FASTENERS AFT OF BEAM MIDDLE ROW FS 610 IAW REO 601R-53-61-5468. COMPLIED WITH EC/TC REO 601R-53-61-3780 AND REO 601R-53-61-3780, REV A DATED 07/15/2011, AS WRITTEN. SDR CLOSED.
Part: SEAT TRACK — CORRODED (BS 559-567) · airframe 25,627 hrs · 24,709 cycles
RBL 9 CARGO FLOOR SEAT TRACK FS 559+110 - FS 567 CORRODED AROUND SCREW HOLES. REMOVED CORRODED SEAT TRACK AT RBL 9 CARGO FLOOR AT FS 559+110 - FS 567 IAW SRM 51-41-04. LOCATED, DRILLED AND INSTALLED NEW CARGO SEAT TRACK PT 601R38779-49 AT RBL 9, FS 559+110 - FS 567 IAW SRM 51-40-11 AND 51-41-04.
Part: SEAT TRACK — CORRODED (BS 559-569) · airframe 25,627 hrs · 24,709 cycles
LBL 9 FLOOR SEAT TRACK FROM FS 559+110-FS 569 CORRODED AROUND SCREW HOLES. R & R LBL 9 FROM FS 559+110-FS 569 W/601R38779-5 IAW AMM 53-01-11-000-802 & 53-01-11-400-802.
Part: SEAT TRACK — CORRODED (BS 559) · airframe 25,627 hrs · 24,709 cycles
RBL 9, FLOOR SEAT TRACK FS 559+4 - 559+80 CORRODED AROUND SCREW HOLES. REMOVED RBL 9 FLOOR SEAT TRACK BETWEEN FS 559+4 - 559+80 IAW SRM 51-41-02. LOCATED AND DRILLED NEW SEAT TRACK IAW REO 601R-53-00-485. INSTALLED SERVICEABLE SEAT TRACK AT RBL 9, FS 559+4 TO 559+80 IAW REO 601R-53-00-485. FABRICATED SEAT RAILS IAW GREO 601R-53-00-485, REV A.
Part: SEAT TRACK — CORRODED (BS 549) · airframe 25,627 hrs · 24,709 cycles
RT SIDE SEAT RAIL FS 549 AFT HAS SEVERAL AREAS OF HEAVY INTERGRANULAR CORROSION. COMPLIED WITH EC/TC REO 601R-53-00-055 REV A DATED 11/18/2011 AS WRITTEN. R & R SEAT TRACK.
Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 25,627 hrs · 24,709 cycles
RBL 27, FLOORBEAM IS CORRODED AROUND SCREW HOLES FS 559+82-FS 559+104. COMPLIED WITH EC/TC REO 601R-53-00-005.
Part: SEAT TRACK — CORRODED (BS 559) · airframe 25,627 hrs · 24,709 cycles
LBL 27 FLOOR SEAT TRACK FS 559+80-FS 559+96 CORRODED AROUND SCREW HOLES. REMOVED LBL 27 FLOOR SEAT TRACK FS 559+80 - 559+86 IAW SRM 51-42-02. REPLACED LBL 27 FLOOR SEAT TRACK W/601R38779-9 IAW AMM 53-01-11-400-802.
Part: SEAT TRACK — CORRODED (BS 559) · airframe 25,627 hrs · 24,709 cycles
LBL 9, FLOOR SEAT TRACK FS 559 - 559+88 IS CORRODED AROUND MOUNT SCREWS. REMOVED LBL 9 FLOOR SEAT TRACK FS 559+96-FS 559+88 IAW SRM 51-41-02. REPLACED LBL 9, FLOOR SEAT TRACK FROM FS 559+96 -559+88, W/601R38779-13 IAW AMM 53-01-05.
Part: FLOOR SUPPORT — CORRODED (BS 559-621) · airframe 25,627 hrs · 24,709 cycles
LBL 27 FLOORBEAM IN CARGO COMPARTMENT HAS AREAS OF EXFOLIATION CORROSION FS 621-FS 559+96. REMOVED FLOORBEAM CAP AT LBL 27 FOR REPLACEMENT IAW SRM 51-42-21 AND 51-42-06. LOCATED AND DRILLED NEW FLOORBEAM CAP AT LBL 27, PN 601R35031-263 IAW SRM 51-42-21 AND 51-42-22. INSTALLED FLOORBEAM CAP, PN 601R-35031-263 IAW REO 601R-53-61-5468. COMPLIED WITH EC/TC REO 601R-53-61-5468. REO 601R-53-61-5468 REV A HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUTINE WORK CARD.
Part: FRAME — CORRODED (BS 589) · airframe 25,627 hrs · 24,709 cycles
FS 589 FRAME HAS LIGHT CORROSION ON LOWER FLANGE STR 27-25L. REMOVED FLOORBEAM AT FS 589 TO GAIN ACCESS IAW AMM 21-22-01-000-801. INSTALLED FLOORBEAM AT FS 589 IAW AMM 21-22-01-400-801. BLENDED FRAME 589 BETWEEN STR 27-25L SMOOTH REMOVING CORROSION IAW SRM 53-21-00. BLEND WITHIN ALLOWABLE LIMITS IAW SRM TEMP REV 53-27.
Part: FLOOR SUPPORT — CORRODED (BS 559-562) · airframe 25,627 hrs · 24,709 cycles
RIGHT CARGO FLOOR SILL HAS CORROSION AROUND SCREW HOLES FS 559+87-FS 562. COMPLIED WITH ECTC REO 601R-53-00-526 AND GREO 601R-53-00-526 REV DATED 05/22/2013 AS WRITTEN.
Part: SEAT TRACK — CORRODED (BS 559) · airframe 25,627 hrs · 24,709 cycles
RBL 9 FLOOR SEAT TRACK, CARGO, FS 559+84 - FS 559+96 CORRODED AROUND MOUNT SCREW HOLES. REMOVED RBL 9 FLOOR SEAT TRACK FS 559+84 -FS 559+96 IAW SRM 51-41-02. REPLACED RBL 9 SEAT TRACK W/601R38779-13 IAW SRM 51-40-11 AND AMM 53-01-05.
Part: SEAT TRACK — CORRODED (BS 559) · airframe 25,627 hrs · 24,709 cycles
RBL 27, CARGO FLOOR SEAT TRACK FS 559+80-FS 559+96 CORRODED AROUND SCREW HOLES. REMOVED RBL 27 CARGO FLOOR SEAT TRACK FS 559+80-FS 559+96 IAW SRM 51-41-2. REPLACED RBL 27 FLOOR SEAT TRACK W/601R38779-9 IAW AMM 53-01-05.
Part: SEAT TRACK — CORRODED (BS 559) · airframe 25,627 hrs · 24,709 cycles
LBL 9, FLOOR SEAT TRACK, FS 559+4 - 559+80 CORRODED AROUND SCRW HOLES. REMOVED FLOOR SEAT TRACK AT LBL 9, FS 559+4 TO 559+80 IAW AMM 53-01-11-000-802. DRILLED UP NEW SERVICEABLE SEAT TRACK IAW SRM 51-40-11. INSTALLED SERVICEABLE SEAT TRACK AT LBL 9 FS 559+4 TO 559+80 IAW REO 601R-53-00-485. FABRICATED SEAT RAILS IAW GREO 601R-53-00-485 REV A.
Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 25,627 hrs · 24,709 cycles
FOUND REAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING HAS INDICATION NOTED APPROX .500 IN LENGTH 90 PERCENT FSH FAILED NDT INSPECTION. COMPLIED WITH EC/TC REO:601R-53-61-1230 AND GREO:601R-53-61-1230, REV F, DATED 10/31/2011 AS WRITTEN.
Part: BULKHEAD WEB — CRACKED (BS 280) · airframe 25,627 hrs · 24,709 cycles
FS 280 WEB IS CRACKED OTBD OF RBL 9 IN RADIUS OF LOWER FLANGE. C/W ECTC REO 601R-53-11-171 AND MET ALL THE REQUIREMENTS OF REO 601R-53-11-171.
Part: FLOORBEAM — CRACKED (BS 621) · airframe 25,627 hrs · 24,709 cycles
FS 621, LEFT FLOOR SUPPORT ANGLE CRACKED AT LBL 36. LOCATED AND DRILLED NEW FLOOR SUPPORT ANGLE, PN 601R53-61-117-1 IAW SRM 51-40-11. REPAIRED FS 621 LT FLOOR SUPPORT IAW REO 601R-53-61-5465. REO 601R-53-61-5465 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON ROUTINE WORK CARD.
Part: DOOR SILL — CORRODED (CARGO DOORWAY) · airframe 25,627 hrs · 24,709 cycles
CARGO DOOR SILL HAS SEVERAL AREAS OF CORROSION AROUND, +1 BETWEEN, NUTPLATE HOLE. REMOVED DAMAGED FLOOR SILL IAW SRM 51-42-02 AND 51-42-21. LOCATED AND DRILLED CARGO DOOR SILL IAW SRM 51-40-11. INSTALLED FABRICATED DOOR SILL IAW REO 601R-53-61-1574 AND SRM 51-42-06.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 25,612 hrs · 24,694 cycles
FS 280.00 INBD AND OTBD FLOOR SUPPORT CLIP AT RBL 9 ARE CRACKED IN RADIUS. R & R INBD RBL 9.0 FLOOR SUPPORT CLIP AT FS 280.00, PN:601R31113-58 IAW SRM 51-42-21.
Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 25,627 hrs · 24,709 cycles
LEFT PRESSURE FLOOR SILL HAS FILIFORM CORROSION IN MULTIPLE LOCATIONS BETWEEN FS 409+128 TO FS 559.00. C/W ECTC REO 601R-53-41-666 AND REO 601R-53-41-666, REV C, DATED 11/06/12 AS WRITTEN. REO 601R-53-41-1892 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NRI WORK CARD.
Part: ISOLATOR — CRACKED (BS 621 BULKHEAD) · airframe 25,612 hrs · 24,694 cycles
FS 621 BULKHEAD, PANEL MOUNT ISOLATORS, 4, ARE CRACKED AT: LBL 27 BOTTOM, RBL 27 BOTTOM AND RBL 43 1ST AND 3RD FROM BOTTOM. IN ADDITION FOUND 6 MORE ISOLATORS CRACKED. R & R 10 ISOLATORS IAW SRM 51-42-10.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 25,612 hrs · 24,694 cycles
FS 280.0 INBD FLOOR SUPPORT CLIP AT LBL 9 IS CRACKED IN UPPER RADIUS. R & R FLOOR SUPPORT CLIP AT LBL 9 IAW SRM 51-42-21.
Part: ATTACH ANGLE — CRACKED (BS 484) · airframe 25,612 hrs · 24,694 cycles
ANGLE ATTACHING TO INTERCOSTAL AT FS 484.0 AND RBL 27 IS CRACKED. REMOVED DAMAGED ANGLE AT FS 484 AND RBL 27 AND INSTALLED NEW SERVICEABLE ANGLE IAW SRM 51-42-06 & 51-42-21.
Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 25,612 hrs · 24,694 cycles
SEAT TRACK RAIL AT LBL 9 BETWEEN FS 364. TO FS 409+32 HAS PITTING AND INTERGRANULAR CORROSION IN MULTIPLE LOCATIONS. REMOVED SEAT TRACK AT LBL 9 BETWEEN FS 364.00 TO FS 409+32 IAW AMM TASK 53-01-11-000-802. INSTALLED NEW SERVICEABLE SEAT TRACK AT LBL 9 BETWEEN FS 364.00 TO FS 409+32 IAW AMM TASK 53-01-11-400-802.
Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 25,627 hrs · 24,709 cycles
RIGHT PRESSURE FLOOR SILL HAS FILIFORM CORROSION IN MULTIPLE LOCATIONS BETWEEN FS 409+128 TO FS 559. AREA AT FS 559, RBL 39 FOUND TO BE OUT OF LIMITS GREO 601R-53-4-666. COMPLETED CORROSION REMOVAL IAW GREO 601R-53-41-666.
Part: ATTACH BRACKET — CRACKED · airframe 25,612 hrs · 24,694 cycles
PAX DOOR 3L LINTEL, ATTACH BRACKET JUST AFT OF FS 280 BULKHEAD IS CRACKED. REMOVED UNSERVICEABLE ANGLE AND LOCATED, DRILLED AND INSTALLED SERVICEABLE ANGLE PT 600-31057-19 IAW SRM 51-40-11, 51-42-06 AND 51-42-21.
Part: ATTACH ANGLE — CRACKED (BS 484) · airframe 25,612 hrs · 24,694 cycles
ANGLE ATTACHING TO INTERCOSTAL AT FS 484.0 AND LBL 27 IS CRACKED. REMOVED DAMAGED ANGLE AT FS 484, LBL 27 AND INSTALLED NEW SERVICEABLE ANGLE IAW SRM 51-42-06 & 51-42-21.
Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 25,627 hrs · 24,709 cycles
SEAT TRACK RAIL AT RBL 9 BETWEEN FS 364.0 TO FS 409+32 HAS PITTING AND INTERGRANULAR CORROSION IN MULTIPLE LCOATONS. REMOVED SEAT TRACK AT RBL 9 BETWEEN FS 364.00 TO FS 409+32 IAW AMM TASK 53-01-11-000-802. INSTALLED NEW SERVICEABLE SEAT TRACK, 601R31032-15, AT RBL 9 BETWEEN FS 364.00 TO FS 409+32 IAW AMM TASK 53-01-11-400-802.
2014
Part: FUSE — BLOWN (EMERGENCY LIGHT) · airframe 24,366 hrs · 23,417 cycles
MAIN CABIN ENTRANCE EMERGENCY FLOOR FLOOD LIGHT INOPERATIVE. R & R FUSES ON BATTERY PACK 2 IAW AMM 33-51-04, OPS CK GOOD.
Part: FUSE — BLOWN (EMERGENCY LIGHTS) · airframe 24,366 hrs · 23,417 cycles
CABIN EXIT SIGN 50 PERCENT INOPERATIVE ABOVE ROW 8. R & R FUSES ON BATTERY PACK NR 2 IAW AMM 33-51-04. OPS CK GOOD, DEFER CLEARED PLACARD REMOVED.
Part: BULKHEAD — CRACKED (AFT) · airframe 23,682 hrs · 22,752 cycles
AFT PRESSURE BULKHEAD CRACKED AT LBL 27.50, WL 132. CRACK APPEARS TO EXTEND UNDER DOOR TRACK. INSTALLED REPAIR IAW REO 601R-53-61-1541, REV E. MAJOR REPAIR IAW GMM 5-3.
2013
Part: BULKHEAD — CRACKED · airframe 22,427 hrs · 21,453 cycles
FOUND BULKHEAD CRACKED. REPAIRED IAW REO 601R-53-11-563, REV C. CLASSIFIED AS A MAJOR REPAIR IAW GMM 5-3.
Part: SILL — CORRODED (CARGO DOORWAY) · airframe 21,486 hrs · 20,504 cycles
CARGO DOOR SILL CORRODED AROUND NUTPLATE. REMOVED CORROSION ON CARGO DOOR SILL AT NUTPLATES IAW SRM 51-21-06-00.
Part: FLOOR SUPPORT — CORRODED (BS 570-621) · airframe 21,486 hrs · 20,504 cycles
RT FLOOR SUPPORT CORRODED FROM FS 621 TO 570. REMOVED CORROSION ON RT FLOOR SUPPORT IAW SRM 51-21-06-00. C
Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 21,486 hrs · 20,504 cycles
PAX DOOR AFT DRAG ANGLE CRACKED. COMPLIED WITH EC/TC REO 601R-52-11-5/3.
2012
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 20,893 hrs · 19,867 cycles
RT OVERWING FWD EMEGRENCY LIGHT AND LT OVERWING FWD EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY IAW AMM 33-51-04.
Part: INVERTER — UNSERVICEABLE (EMERGENCY LIGHTS) · airframe 20,767 hrs · 19,729 cycles
FLOOR LEVEL EMERGENCY LIGHT INOPERATIVE AT ROW 8A EMERGENCY EXIT. REMOVED AND REPLACED THE POWER INVERTER FOR THE EMERGENCY LIGHT IAW AMM 33-51-07. OPS CHECKED GOOD.
Part: TRANSDUCER — FAILED (OIL PRESSURE) · airframe 19,798 hrs · 18,645 cycles
OIL PRESSURE FLUCTUATION ON CLIMB OUT, THEN DROPPED BELOW 25 PSI. RAN QRH WITH THRUST LEVER AT IDLE, PRESSURE STARTED TO INDICATE NORMAL. ACFT RETURNED, EMERGENCY DECLARED. R & R RT ENGINE OIL PRESSURE TRANSDUCER IAW AMM 79-31-05 (IPC 79-30-00 ITEM 35A). OPS AND LEAK CHECKS GOOD.
Part: SWITCH — BROKEN (FLASHLIGHT) · airframe 19,581 hrs · 18,401 cycles
F/O FLASHLIGHT SWITCH BROKEN. R & R F/O'S FLASHLIGHT IAW AMM 25-61-02. NO DEFECTS NOTED.
2011
Part: BULKHEAD — CRACKED (BS 559) · airframe 19,248 hrs · 18,037 cycles
FS 559 BULKHEAD FAILS NDT WITH INDICATION IN RBL 18 WEB, GREATER THAN 50 PERCENT SCREEN HEIGHT, APPROX .100 LONG. REPAIRED IAW REO 601R-53-41-260 AND REO 601R-53-41-260, REV E.
Part: BATTERY — WEAK (FLASHLIGHT) · airframe 18,801 hrs · 17,532 cycles
F/A FLASHLIGHT NOT BRIGHT. R & R F/A FLASHLIGHT BATTERIES, IAW AMM 25-61-02, OPS CHECKED GOOD.
Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 17,618 hrs · 16,205 cycles
CAPTAINS WINDSHEILD SHATTERED ENROUTE. ACFT DIVERTED DUE TO MX -- EMERGENCY DECLARED. R & R CAPT'S WINDSHIELD IAW AMM 56-11-01 LEAK AND OPS CHECK GOOD.
Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 17,342 hrs · 15,888 cycles
F/O COCKPIT FLASHLIGHT BROKEN. R & R F/O COCKPIT FLASHLIGHT IAW AMM 25-60-00. OK FOR SERVICE.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,278 hrs · 15,816 cycles
CABIN CEILING NR 4 EMERGENCY LIGHT INOP. R & R CABIN CEILING NR 4 EMERGENCY LIGHT. OPS CHECK GOOD. R & R CABIN CEILING NR 4 EMERGENCY LIGHT. OPS CHECK GOOD.
2010
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 17,131 hrs · 15,644 cycles
LEFT FWD OVERWING EMERGENCY LIGHT INOP. REPLACED THE LAMP FOR THE LT FWD OVERWING EMERGENCY EXIT. OPS CHECKED GOOD. DONE IAW THE AMM CHAPTER 33-51-21.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 16,975 hrs · 15,460 cycles
CABIN CEILING NR4 EMERGENCY LIGHT INOP. RELAMPED CABIN CEILING NR 4 EMERGENCY LIGHT IAW CMM 33-22-89. OPS CK GOOD. RELAMPED CABIN CEILING NR4 EMERGENCY LIGHT IAW CMM 33-22-89. OPS CK GOOD.
Part: HANDLE — BINDING (SERVICE DOOR) · airframe 16,899 hrs · 15,373 cycles
SERVICE DOOR OUTER HANDLE WILL NOT TURN. LUBED SERVICE DOOR IAW AMM 12-50-52. OP CK GOOD, ACFT OK FOR SERVICE. (CLOSED)
Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 16,506 hrs · 14,929 cycles
GALLEY TRIM PNL EXIT LIGHT IS INOP. REMOVED GALLEY EMERGENCY LIGHT TRIM PANEL IAW AMM 25-31-01-400-802. T/S AND FOUND NR 1 BATTERY PACK TO BE BAD IAW WDM 33-00-00. NR1 BATTERY PACK NEEDS REPLACED AND GALLEY PNL INSTALL. R & R THE EMERGENCY LIGHT BATTERY PACK IAW AMM TASK 33-51-04-000-801 AND 33-51-04-400-801. OP TEST IS GOOD IAW AMM TASK 33-51-00-710-801. REINSTALLED GALLEY TRIM PANEL IAW AMM TASK 25-31-01-400-802. OK TO INSTALL GALLEY TRIM PANEL.
Part: POST — CRACKED (BS 409) · airframe 16,477 hrs · 14,898 cycles
FS 409+128 VERT POST, BL 0 (CTR) FAILS NDT WITH A INDICAITON IN AFT LT RADIUS GREAT THAN 50 PERCENT SCREEN HEIGHT (APPROX .2 LONG). REMOVED VERT POST IAW SRM 51-42-06, 51-42-20. LOCATED AND DRILLED VERT POST AT BL 0 FS 409+128 IAW SRM 51-40-11. INSTALLED POST IAW SRM 51-42-06, ASA ECTC REO 601R-53-41-889. COMLIED WITH EC/TC REO 601R-53-41-889 AND MET ALL THE REQUIREMENTS OF REO 601R-53-41-889 REVISION A.
Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 16,477 hrs · 14,898 cycles
THE PAX DOOR AFT DRAG ANGLE IS CRACKED IN AN EXISTING REPAIR BY THE DOOR ASSIST PULLEY BRACKET. REMOVED DAMAGED SECTION OF ANGLE AND PREVIOUSLY INSTALLED SPLICE ANGLES IAW SRM 51-42-06 & SRM 51-42-13. COMPIED WITH EC/TC REO 601R-52-11-53 & VERIFIED THAT ALL REQUIREMENTS OF REO 601R-52-11-513 HAVE BEEN MET.
Part: SEAT TRACK — CORRODED (BS 364-599) · airframe 16,477 hrs · 14,898 cycles
LT FLOOR SEAT TRACK HAS CORROSION IN SEVERAL AREAS FROM FS 364 TO FS 559 LBL 9. REMOVED LT FLOOR SEAT TRACK IAW SRM 53-01-11-000-802. LOCATED, DRILLED AND COUNTERSUNK NEW SEAT TRACK IAW SRM 51-40-11. INSTALLED SEAT TRACK IAW AMM 53-01-11-400-802.
Part: SEAT TRACK — CORRODED (BS 364-559) · airframe 16,477 hrs · 14,898 cycles
RT FLOOR SEAT TRACK HAS CORROSION IN SEVERAL AREAS FROM FS 364 TO FS 559 RBL 9. REMOVED RT SEAT TRACK IAW 53-01-11-000-802. NEW TRACK REQUIRES INSTALL. LOCATED, DRILLED & COUNTERSINK NEW SEAT TRACK IAW SRM 51-40-11. INSTALLED SEAT TRACK IAW AMM 53-01-11-400-802. INSTALLED NEW SERVICEABLE SEAT TRACK IAW AMM 53-01-11-400-802 STEP 2B.
Part: FLOOR SUPPORT — CRACKED (BS 484) · airframe 16,477 hrs · 14,898 cycles
FS 484 FLOOR SUPPORT INTERCOSTAL ANGLE CRACKED .1" LONG AT RBL 27. REMOVED ANGLE AT RBL 27 AT FS 484 IAW SRM 51-42-06 AND 51-42-21. INSTALLED NEW ANGLE IAW SRM 51-42-06 AND 51-42-21. (CLOSED)
Part: LIGHT — BROKEN (GALLEY) · airframe 16,477 hrs · 14,898 cycles
GALLEY TRIM STRIP EXIT LIGHT ASSY IS BROKEN. REMOVED AND REPLACED GALLEY TRIM STRIP EXIT LIGHT ASSY IAW CRJ 200 AMM TASK 33-51-10-000-801 AND TASK 33-51-10-400-801. OP CHECK GOOD IAW AMM 33-51-00-710-801.
Part: FLOOR SUPPORT — CRACKED (BS 484) · airframe 16,477 hrs · 14,898 cycles
FS 484, FLOOR SUPPORT INTERCOSTAL ANGLE CRACKED .1" LONG AT LBL 27. REMOVED AND REPLACED ANGLE IAW SRM 51-42-06 AND 51-42-21. (CLOSED)
Part: FLOORBEAM — CRACKED (BS 484) · airframe 16,477 hrs · 14,898 cycles
FS 484, FLOOR SUPPORT INTERCOSTAL ANGLE CRACKED .1" LONG AT LBL 27. R & R ANGLE IAW SRM 51-42-06 AND 51-42-21.
Part: FITTING — CRACKED (FLOORBEAM) · airframe 16,477 hrs · 14,898 cycles
FS 460 FLOOR SUPPORT FITTING CRACKED APPROX 1" LONG OTBD SIDE OF RBL 9. REMOVED DAMAGED FLOOR SUPPORT FITTING AT FS 460 O/B OF RBL 9 AND INSTALLED NEW SERVICEABLE FITTING IAW SRM 51-42-06, 51-42-21 & 51-40-11.
Part: INTERCOSTAL — CRACKED (BS 484) · airframe 16,477 hrs · 14,898 cycles
FS 484 FLOOR SUPPORT INTERCOSTAL CRACKED .1" LONG AT RBL 36. REPAIR TO THE INTERCOSTALS AT F.S. 484 BETWEEN BL 27.0 AND BL 36.00 IS COMPLETED IAW REO 601R-53-41-059 AND MEETS WITH ALL THEIR REQUIREMENTS.
Part: LIGHT — BROKEN (CABIN) · airframe 16,477 hrs · 14,898 cycles
PANEL 232DZ HAS A BROKEN EMERGENCY LIGHT HOUSING AND COVER. REMOVED AND REPLACED PANEL 232DZ EMERGENCY LIGHT HOUSING AND COVER IAW AMM TASK 33-51-13-000-801 AND 33-51-13-400-801. OP CHECK GOOD IAW AMM 33-51-00-710-801 ON PANEL 232DZ.
Part: ANGLE — CRACKED (BS 621-625) · airframe 16,477 hrs · 14,898 cycles
AFT EQUIPMENT COMPARTMENT LT & RT F.S. 621.00 TO F.S. 625.00 OBLIQUE ANGLES ARE CRACKED IN AFT RADIUS 1" LONG. REMOVED UNSERVICEABLE ANGLES ON AFT EQUIPMENT COMPARTMENT LT & RT FS 621.00 TO 625.00, PN 601-35012-51 AND 601-35012-52 AND INSTALLED NEW ANGLES. INSTALLED ANGLES PN 601-35012-51 AND 601-35012-52 IAW SRM 51-42-21.
Part: SKIN — CORRODED (BS 559) · airframe 16,477 hrs · 14,898 cycles
EXTERNAL FUSELAGE SKIN HAS CORROSION AROUND SEVERAL FASTENER HEADS BETWEEN FS 559+96 AND FS 559+112, STR 27. REMOVED FASTENERS FROM SKIN BETWEEN FS 559+96 TO FS 559+112 STR 27 PER SRM 51-42-06. REMOVED CORROSION PER CRJ 200 SRM 53-00-31 FIG 103. REMOVED APPROX 0.003"" OF MATERIAL FROM OUTER SURFACE OF SKIN FS 559+96 TO FS 559+112 STR 27. THIS EQUALS APPROX 5 PERCENT OF TOTAL SKIN THICKNESS. BLENDOUT IS WITHIN ALLOWABLE LIMITS PER SRM 53-00-31 FIG 103 (SHEET 3). TREATED, PRIMED, AND PAINTED. INSTALLED SERVICEABLE FASTENERS AT F.S. 559+112 STR 27 IAW SRM 51-25-01 AND 51-42-06.
Part: RELAY — FAILED (EMERGENCY LIGHTS) · airframe 16,039 hrs · 14,406 cycles
EMERGENCY LIGHTS REMAIN ON IN ARMED POSITION ( CABIN EMERGENCY LIGHTS, NON REVENUE FLIGHTS ONLY, MAY BE INOPERATIVE PROVIDED, FLIGHT CREW ARE THE ONLY OCCUPANTS, NO CREW OCCUPIES AREA OF THE AFFECTED LIGHTS, ALTERNATE PROCEDURES ARE ESTABLLISHED AND USED ) R & R K1XD RELAY IAW AMM 24-51-27-000-801. PERFORMED OPS TEST OF AC ESSENTIAL BUS SENSE RELAY K1XD IAW AMM 24-52-27-700-801. DEFER CLEARED PLACARD REMOVED (SDR CLOSED)
2009
Part: FLAP — FAILED (WING) · airframe 14,277 hrs · 12,467 cycles
FLAPS FAIL AFTER T/O WHEN SELECTING FLAPS TO ZERO V2 250 ON LANDING 50000 LBS, EMERGENCY DECLARED. A/C RETURNED TO CVG AFTER T/O. FLT 5570 DEL 215 MINS.
Part: WARNING LIGHT — ILLUMINATED (COCKPIT) · airframe 13,884 hrs · 12,073 cycles
FLAPS FAIL CAUTION MESSAGE ILLUMINATED IN FLIGHT. EMERGENCY DECLARED. A/C RETURNED TO ATL AFTER T/O.
2008
Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,769 hrs · 11,040 cycles
LT SIDE EXT EMERGENCY LIGHTS FWD CENTER FUSELAGE INOP. RESOLVED ON W/O 101005 TASKCARD NR 00002. WORK COMPLETED IN COMPLIANCE WITH AMM R&R LT SIDE EMERGENCY LIGHT FWD CENTER OF FUSELAGE IAW CRJ 200 AMM 33-51-21. OPS CHECK GOOD.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,769 hrs · 11,040 cycles
EXT RT SIDE EMERGENCY CENTER LIGHT INOP. RESOLVED ON W/O 101005 TASKCARD NR 00006. WORK COMPLETED IN ACCORDANCE WITH AMM. R&R EMERGENCY LIGHT ON RT SIDE IAW CRJ 200 33-51-21. OPS CHECK GOOD.
Part: BEAM — CRACKED (FUSELAGE)
BOTTOM ATTACH ANGLE FOR BAGGAGE DOOR LINTEL BEAM MEMBER IS CRACKED IN AREA OF OUTBOARD FASTENER APPROX .50" LONG. REMOVED CRACKED BOTTOM ATTACH ANGLE FOR BAGGAGE DOOR LINTEL BEAM. LOCATED, DRILLED AND INSTALLED A NEW SERVICEABLE ANGLE IAW CRJ200 SRM 51-40-11 AND 51-42-21. (A)
Part: FLOORBEAM — CRACKED (BS 621) · airframe 12,428 hrs · 10,718 cycles
FS 621.00 FLOORBEAM IS CRACKED 1/2 IN LONG ON O/B RADIUS. REMOVED DAMAGED SECTION OF FLOORBEAM AND REPAIRED IAW REO 601R-53-61-117. NEEDS PAINT AND DINITROL. NEEDS LEAK CHECK. LEAK CHECK GOOD IAW CRJ 200 MM 21-32-00-863-801. TOUCH UP FLOOR SUPPORT ANGLE AT RT FS 621 IAW CRJ SRM 51-21-16. NEEDS DINITROL IAW MM 51-25-56-390-802. C/W ECTC REO 601R-53-61-117. RII C/W 5300005. (S)
Part: ATTACH FITTING — CRACKED (BS 280) · airframe 12,428 hrs · 10,718 cycles
FS 280.00 CLIP AT LBL 9 O/B SIDE IS CRACKED 1/2" LONG IN UPPER RADIUS. OPEN (B)
Part: LIGHT — INOPERATIVE (CABIN) · airframe 1,210,051 hrs · 10,430 cycles
EMERGENCY FLOOR LIGHTS AFT OF RT EMERGENCY EXIT INOP. REMOVED AND REPLACED EMERGENCY FLOOR LIGHT SEGEMENT NR 11 IAW AMM 33-51-01. OPS CHECK GOOD. (B)
2007
Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 10,605 hrs · 9,176 cycles
EMERGENCY LIGHTS ARE ON IN THE ARMED POSITION. FLT 4766 DEL 17 MINS.
Part: LIGHT — INOPERATIVE (LT WING) · airframe 10,447 hrs · 9,010 cycles
LEFT WING EMERGENCY LIGHT IS INOP.
Part: STEP — BROKEN (PAX DOOR) · airframe 10,109 hrs · 8,641 cycles
PAX DOOR BOTTOM STEP BROKEN.
2006
Part: UNKNOWN — ODOR (CABIN) · airframe 8,747 hrs · 7,388 cycles
WHEN TRANSFERRING APU BLEEDS TO THE ENGINE THERE IS A STRONG ODOR OF OIL SMELL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,282 hrs · 6,979 cycles
AFT CEILING EMERGENCY LIGHT AT ROW 12 INOP.
Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 7,944 hrs · 6,721 cycles
RT FS 625 OBLIQUE ANGLE CLIP IS CRACKED.
Part: RIB — CRACKED (RT WING) · airframe 7,944 hrs · 6,721 cycles
RANRC NR 163// RT BATT RIB CRACKED.
Part: ATTACH FITTING — CRACKED (BS 625) · airframe 7,944 hrs · 6,721 cycles
FOUND LT FS 625 OBLIQUE ANGLE CLIP IS CRACKED.
Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 7,944 hrs · 6,721 cycles
RANRC NR 194// RT OB 280 CLIP CRACKED.
Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 7,944 hrs · 6,721 cycles
RANRC NR 195// LT IB 280 CLIP CRACKED.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 7,944 hrs · 6,721 cycles
RANRC NR 165// LT FS621.00 FLOOR SUPPORT ANGLE IS CRACKED.
Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 7,944 hrs · 6,721 cycles
RANRC NR 193// RT IB 280 CLIP CRACKED.
Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 7,944 hrs · 6,721 cycles
FOUND PAX DOOR AFT DRAG ANGLE CRACKED.
Part: LAMP — UNKNOWN (EMERGENCY LIGHT) · airframe 7,375 hrs · 6,266 cycles
RELAMPED SERVICE DOOR EMERGENCY EXIT LIGHT.
2005
Part: FLASHLIGHT — INOPERATIVE (COCKPIT)
FLT 4290 - DURING A GROUND INSPECTION IN ATL, THE FIRST OFFICERS FLASHLIGHT WAS FOUND TO BE DIFFICULT TO OPERATE. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS FLASHLIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
Part: ANCHOR FITTING — CRACKED (PAX DOOR)
DURING HANGAR MAINTENANCE, THE REAR ANCHOR FITTING ON THE PASSENGER DOOR WAS FOUND TO BE CRACKED. UPON INSPECTION, MAINTENANCE DETERMINED THE CRACKED REAR ANCHOR FITTING TO BE WITHIN LIMITS. A REPEAT INSPECTION OF THE ANCHOR FITTING IS TO BE PERFORMED AT EVERY SUBSEQUENT SERVICE CHECK FOR PROPAGATION OF THE CRACK IAW MFG REO 601R-11-272. MAINTENANCE REMOVED AND REPLACED THE ASD AFT ANCHOR FITTING IAW AMM. (CLOSED)
Part: CONTROL VALVE — DEFECTIVE (A/C BAY)
FLT 4918 - DURING CLIMB-OUT FROM TYS-TPA, AT APPROXIMATELY 4,000 FEET WITH THE AUXILIARY POWER UNIT DEFERRED, THE CREW NOTICED A SMELL OF SMOKE IN THE COCKPIT FOLLOWED BY SMOKE FILLING THE COCKPIT. THE CREW IMMEDIATELY DONNED THEIR OXYGEN MASKS AND SUBSEQUENTLY RECEIVED A LEFT PACK OVERTEMP MESSAGE. THE QRH WAS COMPLIED WITH, AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED TO TYS. DURING DESCENT SMOKE DRIFTED INTO THE CABIN AND THEN CLEARED IN THE COCKPIT AND CABIN. THE AIRCRAFT LANDED SAFELY IN TYS. MAINTENANCE REMOVED AND REPLACED THE AIR CYCLE MACHINE DUCT ASSEMBLY DUAL BYPASS CONTROL VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
Part: LIGHT — MISSING (CABIN)
DURING A HANGAR CHECK, SEVERAL SECTIONS OF THE EMERGENCY FLOOR LIGHT STRIP WERE FOUND MISSING. MAINTENANCE INSTALLED EMERGENCY FLOOR LIGHTING STRIPS IN THE MISSING SECTION. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)
2004
Part: SCAVENGE PUMP — CLOGGED (RT ENGINE)
DURING CRUISE FROM AEX-DFW, AT APPROXIMATELY 22,000 FT WHILE FERRYING THE AIRCRAFT TO DFW THE CREW RECEIVED A RT ENGINE OIL PRESSURE WARNING. THE QRH WAS COMPLIED WITH AND THE CREW WAS ABLE TO MAINTAIN ADEQUATE THRUST TO MAINTAIN LEVEL FLIGHT AT 22,000 FT. THE AIRCRAFT LANDED SAFELY IN DFW. AS A PRECAUTION FIRE AND MEDICAL VEHICLES FOLLOWED THE AIRCRAFT DURING A SAFE TAXI TO THE GATE. MAINTENANCE R & R THE RT ENGINE OIL LUBE AND SCAVENGER PUMP ASSEMBLY. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
Part: WARNING SYSTEM — FALSE INDICATION (RT ENGINE OIL)
DURING CRUISE, AT APPROX 31,000 FT THE CREW RECEIVED A RT ENGINE OIL PRESSURE WARNING MESSAGE. OIL PRESSURE BEGAN FLUCTUATING BETWEEN 30-32 PSI & THEN DROPPED TO 19 PSI. THE CREW REDUCED ENGINE TO IDLE WITH OIL PRESSURE CONTINUING TO FLUCTUATE BETWEEN 35-40 PSI. ALL OTHR ENGINE IDICATIONS REMAINED NORMAL. QRH PROCEDURES COMPLIED WITH AND AN EMERGENCY DECLARED. AIRCRAFT DIVERTED INTO AEX. DURING FINAL APPROACH AT APPROXIMATELY 5,000 FT THE OIL PRESSURE RETURNED TO NORMAL AND REMAINED THERE DURING A SAFE LANDING AND TAXI. LOCAL MAINTENANCE INSPECTED THE CHIP DETECTOR INDICATOR, OIL LEVEL AND THE OIL PRESSURE TRANSDUCER ON THE RIGHT ENGINE. ALL OPERATIONAL CHECKS WERE GOOD. AIRCRAFT OK FOR SERVICE. (M)