N435SW
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.
241 reports on file, 2002-03-06 – 2019-12-22.
Part: SUPPORT BRACKET — CRACKED (RT MLG) · airframe 41,811 hrs · 36,925 cycles
CRACKED RT MLG BRAKE TRANSDUCER SUPPORT BRACKET. REMOVED & REPLACED THE SUPPORT BRACKET IAW SRM. CHECKED GOOD.
Part: RIVET — CRACKED (LT ENG NOSE COWL) · airframe 41,811 hrs · 36,925 cycles
LEFT ENGINE NOSE COWL HAD ON CRACKED RIVET INSIDE THE INLET ON INBD SIDE. REPLACED THE RIVET ON THE LT ENG NOSE COWL IAW SRM.
Part: PLATE — BROKEN (BS 559) · airframe 41,811 hrs · 36,925 cycles
UPPER ATTACHMENT PLATE BROKEN FOR PRESSURE BOX / FUEL SHROUD AT F.S. 559.00. REMOVED BROKEN UPPER ATTACHMENT PLATE FOR PRESSURE BOX/FUEL SHROUD AT FS 559.0 AND LOCATED, DRILLED-UP AND INSTALLED WITH NEW ATTACHMENT PLATE PN C68C38.REF SRM AND TR51-42.
Part: HOUSING — CRACKED (T/R PDU) · airframe 41,811 hrs · 36,925 cycles
RIGHT THRUST REVERSER PDU HOUSING WAS CRACKED. REMOVED AND REPLACED THE THRUST REVERSER PDU IAW IAW AMM 78-32-03-000-801 AND AMM 78-32-03-400-801. OPS CHECKED GOOD.
Part: ANCHOR — BROKEN (RT WING TE FLAP) · airframe 41,811 hrs · 36,925 cycles
RH FLAP STUB FAIRING WING REAR SPAR FLAP FITTING (ANCHOR POINT) BROKEN. REMOVED AND REPLACED BROKEN RH FLAP STUB FAIRING WING REAR SPAR FLAP FITTING (ANCHOR POINT) WITH NEW FITTING INSTALLED WITH 2EA NEW LOCK FASTENERS AND NUTS. REF SRM.
Part: BOLT — CHAFED (RT ELEVATOR) · airframe 41,811 hrs · 36,925 cycles
RH ELEVATOR #1 HINGE MOUNT BOLT IB RETAINER CHAFED. REPLACED AND SAFTIED RH ELEVATOR #1 HINGE MOUNT BOLT IB RETAINER WITH NEW PLATE AND HARDWQARE 2EA BOLTS AND WASHERS REF SRM.
Part: ANGLE — DAMAGED (BS 280 FLOORBEAM) · airframe 41,811 hrs · 36,925 cycles
FS280 FWD ANGLE HAS ELONGATED HOLE BETWEEN LBL 9 AND RBL 9 (C-CHECK) RO 12/24/2019 REPAIRED FS280 FWD ANGLE ELONGATED HOLE BETWEEN LBL 9 AND RBL 9 REF CRJ200 SRM.
Part: STAND OFF — BROKEN (BS 625 BULKHEAD) · airframe 41,811 hrs · 36,925 cycles
FOUND 2EA BROKEN STANDOFFS. REMOVED AND REPLACED AT THE AFT SIDE OF REAR PRESSURE BULKHEAD FS625 IAW SRM.
Part: PULLEY BRACKET — CRACKED (BS 621) · airframe 41,811 hrs · 36,925 cycles
PULLEY BRACKET IS CRACKED AT BS 621 BETWEEN LBL 18 AND LBL 27. REMOVED AND REPLACED PULLEY BRACKET IAW SRM.
Part: FITTING — CRACKED (BS 460) · airframe 41,811 hrs · 36,925 cycles
FLOOR SUPPORT FITTING AT FS460.00 LBL27 INBOARD CASTING IS CRACKED AT FWD CORNER. REMOVED FLOOR SUPPORT FITTING AT FS460.00 LBL27 INBOARD CASTING IAW SRM. LOCATED, DRILLED EXISTING FASTENER HOLES TO REPLACEMENT SUPPORT FITTING IAW SRM. INSTALLED A NEW FLOOR SUPPORT FITTING IAW SRM.
Part: STIFFENER — CRACKED (BS 621) · airframe 41,811 hrs · 36,925 cycles
LEFT STIFFENER WAS CRACKED AT AFT SIDE OF BULKHEAD BS 621, STRINGER 16L INSTALLED A NEW STIFFENER IAW SRM.
Part: CROSSBEAM — CRACKED (BS 280) · airframe 41,811 hrs · 36,925 cycles
BS 280 CROSSBEAM WAS CRACKED AT 2 PLACES, LBL 9 AND RBL 9, PERFORMED A REPAIR IAW REO.
Part: FLOOR SUPPORT — DAMAGED (BS 409-559) · airframe 41,811 hrs · 36,925 cycles
FLOOR SUPPORT AT RBL 9 FROM BS 409+118 TO 559+10 DAMAGED. REPLACED THE DAMAGED SECTION OF THE FLOOR SUPPORT IAW REO.
Part: FLOOR SUPPORT — DAMAGED (BS 409-559) · airframe 41,811 hrs · 36,925 cycles
REPAIR FLOOR BEAM AT LBL9 FS409+118 TO FS559+10. REPLACED DAMAGED SECTION OF FLOOR BEAM PER REO 601R-53-41-2636 REV.
Part: FLOOR PANEL — CRACKED (BS 461) · airframe 41,811 hrs · 36,925 cycles
PRESSURE FLOOR PANEL WAS CRACKED AT FS 461 LBL 0 -9 AND FS 461 RBL 0 - 9. REPAIRED THE PRESSURE FLOOR PANEL IAW REO.
Part: MOUNT — CORRODED (GALLEY) · airframe 41,811 hrs · 36,925 cycles
CORROSION ON FORWARD AND AFT INBOARD MOUNT PLATES FOR GALLEY ATTACHMENT INBOARD OF RBL 9. REMOVED CORROSION FROM THE MOUNT PLATE IAW SRM. REPLACED THE MOUNT PLATE IAW SRM.
Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 41,811 hrs · 36,925 cycles
FLOOR SUPPORT BETWEEN BS 559+64 - 559+80, RBL 9, WAS CORRODED. EXFOLIATED BEYOND REPAIR. 100% MATERIAL LOSS. OUT OF LIMITS. FABRICATED AND INSTALLED A NEW REPLACEMENT FLOOR SUPPORT. INSTALLED IAW DWG.
Part: PANEL — CHAFED (LT WING TE FLAP) · airframe 41,811 hrs · 36,925 cycles
LEFT INBD FLAP PANEL 584JB IS CHAFFED AT ACTUATOR NOTCH . REPAIRED THE LT INBD FLAP PANEL.
Part: DOOR SILL — CORRODED (CARGO BAY) · airframe 41,811 hrs · 36,925 cycles
CARGO DOOR SILL WAS CORRODED AROUND SEVERAL SCREW HOLES. REMOVED CORROSION FROM THE CARGO DOOR SILL IAW SRM 51-21-06. ALL REWORKED AREAS ARE ACCEPTABLE IAW REO.
Part: FLOOR SUPPORT — CORRODED (BS 349-409) · airframe 41,811 hrs · 36,925 cycles
RIGHT FLOOR SUPORT BETWEEN BS 349 AND 409+5 WAS CORRODED. REMOVED CORROSION ON THE AFFECTED AREA IAW SRM.
Part: ISOLATOR — BROKEN (BS 621) · airframe 41,811 hrs · 36,925 cycles
BS 621 ISOLATOR BRACKET IS BROKEN, R/H SIDE, MARKED. (C-CHECK) RO 12/24/2019 REMOVED AND REPLACED BROCKEN ISOLATOR WITH NEW ISOLATOR FS621 R/H SIDE REF CRJ 200 SRM.
Part: SEAT TRACK — CORRODED (BS 364-394) · airframe 41,811 hrs · 36,925 cycles
CORROSION FOUND ON THE SEAT TRACK AT RBL 9 BETWEEN BS 364 AND 394. REMOVED CORROSION FROM THE AFFECTED AREA.
Part: FLOOR SUPPORT — CORRODED (BS 409) · airframe 41,811 hrs · 36,925 cycles
RBL 9 FLOOR SUPPORT CAP, INBOARD FLANGE WAS CORRODED AT MULTIPLE LOCATIONS BETWEEN BS 409+6 AND 409+118. REMOVED AND INSTALLED A NEW FLOOR SUPPORT CAP IAW DRAWING.
Part: PLATE — CORRODED (BS 308) · airframe 41,811 hrs · 36,925 cycles
CORROSION ON UPPER PLATE JUST INBOARD OF THE LT FLOOR SUPPORT AT APPROXIMATELY BS 308, LBL 41. REMOVED CORROSION ON THE AFFECTED AREA IAW SRM.
Part: FLOOR SUPPORT — CORRODED (BS 409) · airframe 41,811 hrs · 36,925 cycles
LBL 9 FLOOR SUPPORT CAP INBOARD FLANGE HAD CORROSION AT MULTIPLE LOCATIONS BETWEEN BS 409+118 AND 409+128. REMOVED CORROSION AND FOUND OUT OF LIMITS, REPAIRED.
Part: FLOOR SUPPORT — CORRODED (BS 409) · airframe 41,811 hrs · 36,925 cycles
RBL 9 FLOOR SUPPORT CAP INBOARD FLANGE HAD CORROSION AT MULTIPLE LOCATIONS BETWEEN BS 409+118 AND 409+128. REMOVED CORROSION AND FOUND OUT OF LIMITS, REPAIRED.
Part: SEAT TRACK — CORRODED (BS 409) · airframe 41,811 hrs · 36,925 cycles
RBL 9 SEAT TRACK BETWEEN BS 409+16 AND 409+120 WAS CORRODED. THE SEAT TRACK WAS REPLACED IAW REO.
Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 41,811 hrs · 36,925 cycles
*FLOOR BEAM AT 559.0 LBL 9 HAS CORROSION (C-CHECK) RO 12/24/2019 REMOVED CORROSION ON LBL 9 FLOOR BEAM CAP FROM FS409+118 TO FS559+10, OUT OF LIMITS. REPAIRED.
Part: ANGLE — BENT (AFT CARGO) · airframe 41,811 hrs · 36,925 cycles
AFT CARGO SURROUND FWD CAM TRACK SUPPORT LOWER FWD ANGLE BENT. REPLACED FWD CAM TRACK SUPPORT LOWER FWD ANGLE. REF SRM 51-42-06 AND DWG 601R35050 REV AC / COMPLIED WITH TASK CARD 51-900-1003 MAJOR REPAIR
Part: SEAT TRACK — CORRODED (BS 409) · airframe 41,811 hrs · 36,925 cycles
LBL 9 SEAT TRACK WAS CORRODED BETWEEN BS 409+48 AND 409+118. REPLACED THE SEAT TRACK IAW REO.
Part: ANGLE — CRACKED (CARGO BAY) · airframe 41,811 hrs · 36,925 cycles
AFT CARGO DOOR SURROUND AT FWD CAM TRACK SUPPORT LOWER ANGLE CRACKED. REPLACED FWD CAM TRACK SUPPORT LOWER ANGLE IAW SRM AND DWG. MAJOR REPAIR.
Part: DUCT — OUT OF ALIGNMENT (LT ACM RAM AIR) · airframe 41,811 hrs · 36,925 cycles
LEFT ACM RAM AIR DUCT. FIT CHECK FAILED. TOP HOLES OF RAM AIR DUCT DO NOT LINED UP WITH AIRCRAFT SIDE HOLES. REPAIRED THE RAM AIR DUCT IAW REO.
Part: FLOOR SUPPORT — CORRODED (BS 295-310) · airframe 41,811 hrs · 36,925 cycles
LEFT FLOOR SUPPORT HAD CORROSION BETWEEN FS 295 AND FS 310. REMOVED CORROSION ON THE AFFECTED AREA IAW SRM.
Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 41,811 hrs · 36,925 cycles
FLOOR SUPPORT AT BS 559, RBL 9 WAS CORRODED. REMOVED CORROSION FROM BS409+118 TO 559+10. FOUND OUT OF LIMITS, REPAIRED.
Part: FLOOR SUPPORT — CORRODED (BS 409) · airframe 41,811 hrs · 36,925 cycles
LBL 9 FLOOR SUPPORT CAP INBOARD FLANGE HAD CORROSION AT MULTIPLE LOCATIONS BETWEEN BS 409+6 AND 409+118. INSTALLED A NEW FABRICATED FLOOR SUPPORT CAP IAW SRM.
Part: SUPPORT — CORRODED (BS 574-605) · airframe 41,811 hrs · 36,925 cycles
BS 574 - 605, RT FLOOR EDGE MEMBER HAS CORROSION AROUND SEVERAL SCREW HOLES. REMOVED CORROSION IAW SRM. ALL REWORKED AREAS ACCEPTABLE IAW REO. .
Part: CUP — CORRODED (DOOR HAND RAIL) · airframe 41,811 hrs · 36,925 cycles
CORROSION ON FORWARD AND AFT PAX DOOR HANDRAIL CUPS. REMOVED AND REPLACED FWD AND AFT PAX DOOR HANDRAIL CUPS IAW SRM.
Part: FLOOR SUPPORT — CORRODED (BS 409) · airframe 41,811 hrs · 36,925 cycles
LH FLOOR SUPPORT WAS CORRODED BETWEEN BS 409+32 AND 409+80. REMOVED CORROSION ON THE AFFECTED AREA. IAW SRM.
Part: PANEL — CHAFED (LT WING TE FLAP) · airframe 41,811 hrs · 36,925 cycles
LEFT INBD FLAP PANEL 584MB IS CHAFED AT THE ACTUATOR NOTCH. REPAIRED LT INBD FLAP PANEL IAW EA934, CURED AND FINISHED.
Part: FLOOR SUPPORT — CORRODED (BS 409) · airframe 41,811 hrs · 36,925 cycles
RIGHT FLOOR SUPPORT BETWEEN BS 409+32 AND 409+48 WAS CORRODED. REMOVED CORROSION ON THE AFFECTED AREA IAW SRM.
Part: ISOLATOR — BROKEN (BS 621 BULKHEAD) · airframe 41,811 hrs · 36,925 cycles
* FS621 BULKHEAD HAS 8 EACH BROKEN ISOLATORS. REMOVED AND REPLACED 8 EACH BROKEN ISOLATORS WITH NEW ON FS621 BULKHEAD REF CRJ 200 SRM.
Part: DOUBLER — CORRODED (BS 559) · airframe 41,811 hrs · 36,925 cycles
NTERNAL FUSELAGE AT BS 559+80 TO 559+96 FOUND CORROSION ON THE BELLY DRAIN DOUBLERS LT AND RT. REMOVED CORROSION FROM 2EA FUSELAGE BELLY DRAIN DOUBLERS IAW SRM.
Part: ANGLE — CRACKED (BS 625.3) · airframe 41,811 hrs · 36,925 cycles
RIGHT BS 625.3 UPPER ANGLE WAS CRACKED. REMOVED AND REPLACED IAW SRM, DWG, AND REO.
Part: FLOOR PANEL — CORRODED (CABIN) · airframe 41,811 hrs · 36,925 cycles
RIGHT SIDE PRESSURE FLOOR PANEL WAS CORRODED AT MULTIPLE SPOTS. REPAIRED THE FLOOR PANEL IAW REO.
Part: FLOOR PANEL — CORRODED (CABIN) · airframe 41,811 hrs · 36,925 cycles
LEFT SIDE PRESSURE FLOOR SILL PANEL IS CORRODED IN MULTIPLE SPOTS. REPAIRED BY BLENDING IAW REO.
Part: FLOOR SUPPORT — CRACKED (BS 461) · airframe 41,811 hrs · 36,925 cycles
FLOOR SUPPORT BRACKET AT APPROX. BS 461 LBL 36, WAS CRACKED AT ITS FORWARD CORNER. REMOVED AND REPLACED THE FLOOR SUPPORT BRACKET IAW SRM AND DWG.
Part: STRAP — CORRODED (BS 559) · airframe 41,811 hrs · 36,925 cycles
FLOORBEAM STRAP AT BS 559, RBL 27 - 45 WAS CORRODED. REMOVED AND REPLACED THE STRAP IAW SRM AND DWG.
Part: FAIRING — CORRODED (FUSELAGE) · airframe 41,811 hrs · 36,925 cycles
FWD FUSELAGE UNDER FAIRINGS 191AB AND 192BB BETWEEN STRINGERS 24 LT AND RT AT BS 409+96 MOUNT HOLES WERE CORRODED. REMOVED CORROSION FROM FWD FUSELAGE UNDER FAIRINGS MOUNT HOLES, BLENDED AREAS FOUND TO BE OUT OF LIMITS, APPLICABLE REO FOR THIS AREA STATES THAT THE SUBJET CONDITION IS STRUCTURALLY ACCEPTABLE, COMPLIED WITH DISPOSITION STEPS 1-7.
Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 41,811 hrs · 36,925 cycles
LEFT SIDE PRESSURE FLOOR SUPPORT ANGLE WAS CORRODED AT MULTIPLE SPOTS. REPAIRED BY BLENDING IAW REO.
Part: ANGLE — CRACKED (BS 625.3) · airframe 41,811 hrs · 36,925 cycles
LEFT BS 625.3 UPPER ANGLE WAS CRACKED. REMOVED THE ANGLE IAW SRM. LOCATED AND DRILLED A NEW ANGLE IAW SRM, INSTALLED IAW DWG 601-35012, REV D, AND REO.
Part: STRAP — CORRODED (BS 559) · airframe 41,811 hrs · 36,925 cycles
FLOOR SUPPORT STRAP AT BS 559, LBL 27 - 45 WAS CORRODED. REMOVED CORROSION IAW SRM
Part: SKIN — DENTED (BS 256) · airframe 41,811 hrs · 36,925 cycles
FUSELAGE SKIN DENTED AT APPROXIMATELY BS 256, STRINGERS 25 - 26R. REPAIRED THE SKIN IAW REO, FOUND TO BE WITHIN LIMITS.
Part: SKIN — CORRODED (BS 559) · airframe 41,811 hrs · 36,925 cycles
FUSELAGE AFT BOTTOM OUTER SKIN HAS SEVERAL CORRODED FASTENERS FROM BS 559+80 TO 559+112, STRINGER 27. REMOVED THE CORROSION FROM THE EXTERNAL SKIN IAW SRM 51-21-06. ORIGINAL MATERIAL THICKNESS .058", MINIMUM MATERIAL REMAINING .051", MAX MATERIAL REMOVED .007", MAX ALLOWABLE .006". FOUND TO BE BEYOND ALLOWABLE LIMITS IAW SRM AND SRM . COMPLIED WITH REO
Part: PANEL — CRACKED (CARGO BAY) · airframe 41,811 hrs · 36,925 cycles
CARGO PANEL 281HLW TORN AND CRACKED AT FORWARD EDGE EVALUATED THE DAMAGE ON THE CARGO PANEL AND FOUND OUT OF LIMITS. A NEW CARGO PANEL WAS INSTALLED.
Part: PANEL — CRACKED (CARGO BAY) · airframe 41,811 hrs · 36,925 cycles
CARGO PANEL 281JLW CRACKED AT BOTTOM END REPAIRED THE CARGO PANEL IAW CMM.
Part: GEARBOX — FAILED (THROTTLE) · airframe 41,811 hrs · 36,925 cycles
LH ENGINE THROTTLE CONTROL GEARBOX ASSY FAILED FUNTIONAL TEST IAW TASK 76-10-00-830-801. REMOVED AND REPLACED THE LT THROTTLE CONTROL GEARBOX IAW AMM. RIGGING AND OPERATIONAL CHECKED GOOD.
Part: POST — CHAFED (PAX DOOR) · airframe 41,811 hrs · 36,925 cycles
PAX DOOR AFT HAND RAIL BOTTOM POST CHAFED ON AFT SIDE TOP. REPAIRED THE AFFECTED AREA. IAW SRM , TEMPORARY REVISION 51-44.
Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 41,811 hrs · 36,925 cycles
PAX DOOR POSSIBLE CORROSION ON INTERCOSTAL DD6. REPAIRED THE PAX DOOR INTERCOSTAL IAW SRM.
Part: GROUND STUD — CORRODED (PAX DOOR) · airframe 41,811 hrs · 36,925 cycles
PAX DOOR, UNDER TOP FOLDING STEP, POSSIBLE CORROSION AROUND THE GROUND STUD. REPLACED CORRODED GROUND STUD AND TOP STAIR PANEL IAW SRM.
Part: SPRING — BROKEN (NLG TORQUE LINK) · airframe 41,811 hrs · 36,925 cycles
NLG BOTTOM TORQUE LINK SPRING BROKEN. REMOVED AND REPLACED THE TORQUE LINK SPRING IAW AMM.
Part: ROD — WORN (NLG DOOR) · airframe 41,811 hrs · 36,925 cycles
NLG AFT DOOR LT ROD, BOTH ROD ENDS LOOSE AND WORN. REMOVED AND REPLACED THE LT AFT NLG DOOR ROD ASSY IAW AMM. OPERATIONAL TEST OF THE NLG DOORS CHECKED GOOD IAW AMM.
Part: SUPPORT — CRACKED (PAX DOOR) · airframe 41,811 hrs · 36,925 cycles
PAX DOOR SUPPORT WHEEL CRACKED. REMOVED AND REPLACED THE SUPPORT WHEEL IAW AMM.
Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 41,811 hrs · 36,925 cycles
PAX DOOR INTERCOSTAL DD4 CORRODED. REPAIRED PAX DOOR INTERCOSTAL IAW SRM.
Part: ROD END — LOOSE (NLG DOOR) · airframe 41,811 hrs · 36,925 cycles
NLG AFT DOOR RT ROD, AFT ATTACH BOLT LOOSE. REMOVED AND REPLACED THE RT AFT NLG DOOR ROD END IAW AMM. OPS TESTED GOOD IAW AMM
Part: RISER — CORRODED (PAX DOOR STEP) · airframe 41,811 hrs · 36,925 cycles
*PAX DOOR FWD STAIR RISER, TOP STEP, OUTBD TOP CORNER OF RISER CORRODED. THE RISER WAS REPAIRED IAW SRM.
Part: HANDLE — CHAFED (SERVICE DOOR) · airframe 41,811 hrs · 36,925 cycles
SERVICE DOOR INNER HANDLE HAD 2 GOUGES AND CHAFED. REMOVED CHAFE DAMAGE AND FOUND TO BE WITHIN LIMITS IAW REO.
Part: ATTACH ANGLE — CORRODED (PAX DOOR) · airframe 41,811 hrs · 36,925 cycles
PAX DOOR ATTACH ANGLE FOR STEP WAS CORRODED. REPLACED PAX DOOR ATTACH ANGLE IAW SRM.
Part: HINGE — CHAFED (SERVICE DOOR) · airframe 41,811 hrs · 36,925 cycles
SERVICE DOOR HINGE CHAFFED AT THE AFT UPPER INNER EDGE. REMOVED AND REPLACED PANEL IAW DWG 601R38440, REV-AF AND SRM .
Part: SKIN — CORRODED (SERVICE DOOR) · airframe 41,811 hrs · 36,925 cycles
*SERVICE DOOR HAS 2EA CORRODED FASTENERS ON INNER SKIN, UPPER FWD CORNER. REMOVED AND REPLACED 2 EACH FASTENERS AT THE SERVICE DOOR ON INNER SKIN, UPPER FWD CORNER REF. CRJ200-SRM
Part: PANEL — CORRODED (PAX DOOR STEP) · airframe 41,811 hrs · 36,925 cycles
PAX DOOR TOP FOLDING STEP BOTTOM ATTACH HOLES ON APRON WERE CORRODED. DOOR TOP STEP PANEL REPLACED.
Part: LEG ASSY — CRACKED (PAX DOOR) · airframe 41,811 hrs · 36,925 cycles
PAX DOOR SUPPORT WHEEL LEG CRACKED ON OTBD SIDE, CENTER. REMOVED AND REPLACED THE PAX DOOR SUPPORT WHEEL LEG, IAW AMM.
Part: LEVER — CHAFED (PAX DOOR) · airframe 41,811 hrs · 36,925 cycles
PAX DOOR FWD PULL IN LEVER CHAFED. REMOVED AND REPLACED PAX DOOR FWD PULL IN LEVER IAW AMM. PERFORMED AN OPS CHECK OF THE PASSENGER DOOR LATCH MECHANISM AND PASSENGER DOOR WARNING SYSTEM IAW AMM OPS CHECKED GOOD.
Part: FITTING — CRACKED (BS 349) · airframe 41,811 hrs · 36,925 cycles
*BACKUP FITTING FS349.00, BETWEEN STGR13 ̉‰ STGR14, PLASTIC GUARD IS CRACKED. REMOVED AND REPLACED 1EA. CABIN DOOR CABLE GUARD ASSEMBLY IAW AMM
Part: FAIRING — CRACKED (LT WING TE FLAP) · airframe 41,811 hrs · 36,925 cycles
LH FLAP STUB FAIRING CRACKED ON LEADING EDGE SIDE (C-CHECK) RO:12/24/2019 REPLACED LH FLAP STUB FAIRING WITH NEW FAIRING. LH FLAP STUB FAIRING IS INSTALLED ON JOB.2755581 OP.96 MX.19844954. SEE CONTINUATION FOR DETAILS
Part: CASCADE — CRACKED (RT ENGINE) · airframe 41,811 hrs · 36,925 cycles
*RH ENGINE TOP CASCADE HAS SEVERAL CRACKS. REMOVED AND REPLACED NEW TOP R/H ENGINE CASCADE REF CRJ-200 AMM CLEARANCE CHECK GOOD.
Part: SKIN — DELAMINATED (LT NOSE COWL) · airframe 41,811 hrs · 36,925 cycles
LH ENGINE NOSE COWL LEADING EDGE HAS NUMEROUS AREA OF DELAMINATION AND SEALANT GAPS ON THE INNER AND OUT TRAILING EDGE. REPAIRED LH ENGINE NOSE COWL LEADING EDGE SURROUND AND SEALANT GAPS ON INNER AND OUT TRAILING EDGE APPLIED REPAIR RESIN AND FILLET SEAL AND RESTORED FINISH IAW SRM AND CMM.
Part: COVER — CRACKED (RT EXHAUST LOOP) · airframe 41,811 hrs · 36,925 cycles
*RH ENGINE EXHAUST FAIRING FIRE LOOP COVER CRACKED (MARKED) (C-CHECK) RO:12/24/2019 REMOVED AND INSTALLED A NEW R/H ENGINE EXHAUST FAIRING FIRE LOOP COVER REF CRJ200 SRM NEW HARDWARE USED P/N 4 EA. WASHER NAS1149C0332R, SCREW 4 EA. NAS623-3-2 AND NUT 4EA. MS21043-3.
Part: RUB STRIP — CHAFED (RT NACELLE) · airframe 41,811 hrs · 36,925 cycles
* RH ENGINE COWL PANEL 442AT AFT RUB STRIP CHAFED THROUGH. (C-CHECK) RO:12/24/2019 R/H ENGINE FAN COWL 442AT'S AFT EDGE STRIP HAS BEEN REMOVED AND REPLACED PER BOMBARDIER CMM
Part: CASCADE — CRACKED (THRUST REVERSER) · airframe 41,811 hrs · 36,925 cycles
*LH ENGINE BOTTOM CASCADE CRACKED INBD SIDE. REMOVED AND REPLACED THE L/H ENGINE THRUST REVERSER LOWER INBOARD CASCADE WITH A SERVICEABLE PART REF AMMS OPERATIONAL AND CLEARANCE CHECKS GOOD.
Part: COVER — CORRODED (LT OVERWING DOOR) · airframe 41,811 hrs · 36,925 cycles
*LEFT WING OVER-WING EMERGENCY EXIT HAS CORRODED HARDWARE ON THE UPPER HANDLE COVER PLATE. REMOVED OVER-WING EMERGENCY EXIT HARDWARE ON THE UPPER HANDLE COVER PLATE REF AMM. AND INSTALLED NEW HARDWARE ON OVER-WING EMERGENCY EXIT ON THE UPPER HANDLE COVER PLATE. REF AMM
Part: CASCADE — CRACKED (THRUST REVERSER) · airframe 41,811 hrs · 36,925 cycles
*LH ENGINE INBD UPPER CASCADE CRACKED AT BOTTOM AREA. REMOVED AND REPLACED THE L/H ENGINE THRUST REVERSER UPPER INBOARD CASCADE WITH A SERVICEABLE PART REF CRJ 200 AMMS OPERATIONAL AND CLEARANCE CHECKS GOOD.
Part: ANCHOR FITTING — CORRODED (PAX DOOR) · airframe 41,811 hrs · 36,925 cycles
*PASSENGER DOOR ANCHOR FITTING, FS310.00 HAS CORRODED HARDWARE. REMOVED AND REPLACED, PASSENGER DOOR ANCHOR FITTING HARDWARE. NEW HARDWARE INSTALLED IAW SRM.
Part: EXHAUST CONE — CRACKED (LT ENGINE) · airframe 41,811 hrs · 36,925 cycles
*LH ENGINE EXHAUST FAIRING 2ND INNER RIB CRACKED ON INBRD SIDE (MARKED) (C-CHECK) RO:12/24/2019 ORDERED/RECEIVED LH ENG EXHAUST NOZZLE FAIRING ASSY. SEE CAMP 19772916 FOR MAINTENANCE PERFORMED
Part: RETAINER — MISSING (ACCESS PANEL) · airframe 41,811 hrs · 36,925 cycles
COCKPIT ACCESS PANEL 222BZ MISSING 1EA RETAINER RING ON FASTENER. REMOVED AND INSTALLED NEW COCKPIT ACCESS PANEL 222BZ FASTENER RING BY HOLDING FASTENER IN PLACE AND SLIDING RING DOWN SHAFT ON TO BASE OF FASTENER, AND SECURED IN POSITION.
Part: CONNECTOR — CRACKED (STICK SHAKER) · airframe 41,811 hrs · 36,925 cycles
COCKPIT ACCESS PANEL 221NZ HAS CRACKED COVER. (C-CHECK) RO:12/24/2019 ORDERED/RECEIVED 1EA CANNON PLUG SHIELD. REFER TO CAMP 19772913 FOR INSTALLATION. / LOCATED/DRILLED FASTENER HOLES. REF CRJ200 SRM
Part: LINK — CORRODED (SPOILER ACTUATOR) · airframe 41,811 hrs · 36,925 cycles
L/H OUTBD. GROUND SPOILER ACTUATOR LINK (LWR) AND BOLT RUSTED AND WORN (C-CHECK) RO:12/24/2019 INSTALLED NEW GRND ACTUATOR LINK AND ATTACHING HARDWARE FOR L/H OTBD GRND SPOILER ACTUATOR REF CRJ-200 AMM, OPS CHECK GOOD.
Part: LINK — CORRODED (SPOILER ACTUATOR) · airframe 41,811 hrs · 36,925 cycles
R/H INBD GROUND SPOILER ACTUATOR LINK (LWR.) AND BOLT RUSTED AND WORN (C-CHECK) RO:12/24/2019 INSTALLED NEW GRND ACTUATOR LINK AND ATTACHING HARDWARE FOR R/H INBD GRND SPOILER ACTUATOR REF CRJ-200 AMM OPS CHECK GOOD.
Part: LINK — CORRODED (SPOILER ACTUATOR) · airframe 41,811 hrs · 36,925 cycles
R/H OUTBD. GROUND SPOILER ACTUATOR LINK (LWR.) AND BOLT RUSTED AND WORN. INSTALLED NEW GRND ACTUATOR LINK AND ATTACHING HARDWARE FOR R/H OTBD GRND SPOILER ACTUATOR REF CRJ-200 AMM OPS CHECK GOOD.
Part: DOOR — CHAFED (PAX) · airframe 41,811 hrs · 36,925 cycles
* PASSENGER DOOR SURROUND ̉‰ STOP (ABOVE FWD CAM) AT FS 310 CHAFED (MARKED). (C-CHECK) RO:12/24/2019 REMOVED AND REPLACED DROP DOWN DOOR STOP REF. CRJ-200 SRM PERFORMED ADJUSTMENT AND FUNCTIONAL TEST OF DOOR STOP REF. CRJ-200 AMM CHECKED GOOD.
Part: DOOR — CHAFED (RT MLG) · airframe 41,811 hrs · 36,925 cycles
RH MLG DOOR FORWARD EDGE CHAFED AT PREVIOUS REPAIR LOCATION. RH MLG DOOR FORWARD EDGE CHAFED AT PREVIOUS REPAIR LOCATION, NO ALLOWABLE LIMITS PROVIDED FOR A PREVIOUS REPAIR, THE CHAFE WAS IN THE REPAIR FILLER OF THE PREVIOUS REPAIR, REMOVED PREVIOUS REPAIR FILLER, FABRICATED, LOCATED, DRILLED AND INSTALLED A NEW REPAIR FILLER REF REO AND REF CRJ200 SRM TEMORARY REVISION 51-42
Part: FITTING — DENTED (RT WING) · airframe 41,811 hrs · 36,925 cycles
OUTBD. OF R/H W.S. 148.019 FLAPGUIDE FITTING AT REAR SPAR DETENTED FROM - ALSO WORN FLAP GUIDE BEARING. REMOVED DAMAGED GUIDE FITTING AND INSTALLED NEW FITTING P/N 601R10156-2 PO: T52766 AND FLAP CAM FOLLOWER AT R/H OUTBOARD FLAP W.S 148.019. REF. SRM.
Part: STOP FITTING — GOUGED (ESCAPE HATCH) · airframe 41,811 hrs · 36,925 cycles
LH FORWARD STOP FITTING ON CREW ESCAPE HATCH DOOR HAS A GOUGE. REMOVED GOUGE FROM LH FORWARD STOP FITTING ON CREW ESCAPE HATCH DOOR REF CRJ200 SRM TEMPORARY REVISION REWORKED AREA IS WITHIN ALLOWABLE LIMITS PER REO ALL STEPS COMPLETED.
Part: DOOR — CHAFED (LT MLG DOOR) · airframe 41,811 hrs · 36,925 cycles
LH MLG DOOR FORWARD SIDE CHAFED AT PREVIOUS REPAIR LOCATION REMOVED PREVIOUS DAMAGED REPAIR FILLER, FABRICATED AND INSTALLED NEW REPAIR FILLER. REF BOMBARDIER REO. SEE CONTINUE CARD FOR DETAILS.
Part: LINK — CORRODED (SPOILER ACTUATOR) · airframe 41,811 hrs · 36,925 cycles
L/H INBD GROUND SPOILER ACTUATOR LINK(LWR.) AND BOLT RUSTED AND WORN ATTACHING TO SPOILER (C-CHECK) RO:12/24/2019 REMOVED AND INSTALLED NEW L/H INBD GROUND SPOILER ACTUATOR LINK WITH NEW HARDWARE REF CRJ-200-AMM AND CRJ-200-AMM OP CHECKS GOOD AND SEE CONTINUATION CARD FOR DETAILS
Part: PANEL — GOUGED (RT NACELLE) · airframe 41,811 hrs · 36,925 cycles
R/H LOWER NACELLE PANEL 422DB HAS KNIFE EDGE ON SEPERATOR PLATE (C-CHECK) RO:12/24/2019 REMOVED AND REPLACED 2 EA SEPARATOR PLATES ON RH LOWER NACELLE PANEL 422DB REF CRJ200 SRM.
Part: CAM — GOUGED (PAX DOOR FRAME) · airframe 41,811 hrs · 36,925 cycles
* PASSENGER DOOR SURROUND FWD CAM ON FRAME FS 310 AND AFT CAM ON FRAME FS 349 ARE GROOVED (MARKED). (C-CHECK) RO:12/24/2019 REMOVED AND REPLACED PASSENGER DOOR FWD AND AFT CAM FITTINGS WITH NEW CAM FITTINGS. INSTALLED WITH 10EA NEW HI-LOC AND NUTS. REF CRJ200 AMM PERFORMED ADJUSTMENT TEST OF THE PASSENGER DOOR REF CRJ200 AMM NO DEFECTS NOTED. REFERENCE THE CONTINUE CARD FOR DETAILS.
Part: LANDING — DAMAGED (E/E BAY DOOR) · airframe 41,811 hrs · 36,925 cycles
* LH FORWARD EQUIPMENT COMPARTMENT DOOR (211AL) LOWER LANDING HAS 2 CHAFE MARKS NEAR FWD LATCH AREA AND 1 NEAR AFT LATCH AREA. BLENDED OUT DAMAGE ON LH FORWARD EQUIPMENT COMPARTMENT DOOR (211AL) LOWER LANDING (CHAFE MARKS 3EA.) REF BOMBARDIER REO COMPLIED WITH REO.
Part: HINGE — CORRODED (DOOR) · airframe 41,811 hrs · 36,925 cycles
LOWER PANEL SIDE HINGE FOR DOOR 196AR HAS CORROSION. REMOVED AND INSTALLED LOWER PANEL SIDE HINGE FOR DOOR 196AR REF CRJ200 AMM AND REMOVED, LOCATED, DRILLED AND INSTALLED THE LOWER HINGE ARM FOR ACCESS DOOR AND 2EA HINGE ARM BRACKETS FOR 196AR REF DGW 601R35232, REV M, DATED 2000/01/01 AND REF SRM RESTORED FINISH REF SRM
Part: SHIM — DENTED (RT ENGINE COWL) · airframe 41,811 hrs · 36,925 cycles
* RH ENGINE Ãâ¬â DENT ON COWL 444AT AT APPROXIMATELY 2 OÃâ¬â¢CLOCK POSITION. INSTALLED ON JOB 2755580 OP 7008.
Part: PLATE — CORRODED (LT PYLON) · airframe 41,811 hrs · 36,925 cycles
LH UPPER PYLON TRAILING EDGE INBOARD BONDING PLATE HAS CORROSION . REMOVED AND REPLACED BONDING PLATE AT LH UPPER PYLON TRAILING EDGE INBOARD SIDE REF SRM AND DWG RESTORED FINISH REF SRM
Part: PANEL — CORRODED (PAX DOOR) · airframe 41,811 hrs · 36,925 cycles
PAX DOOR STAIR PANEL 832AT HAS CORROSION ON MOUNTING FLANGES. (C-CHECK) RO:12/24/2019 REPLACED PASSENGER DOOR STAIR PANEL 832AT. REF CRJ200 SRM.
Part: SKIN — CHAFED (RT MLG DOOR) · airframe 41,811 hrs · 36,925 cycles
RH MLG DOOR INNER SKIN CHAFED. BLENDED AFFECTED AREA REF CRJ200 SRM AFFECTED FOUND TO BE OUT OF LIMITS, RECEIVED FROM ENGINEERING REO AND ITS DISPOSITION STATES THAT THE SUBJET CONDITION IS STRUCTURALLY ACCEPTABLE. COMPLIED WITH DISPOSITIONS 1-4
Part: DOOR — EXCESS PLAY (LT MLG) · airframe 41,811 hrs · 36,925 cycles
* LH MLG DOOR HAS EXCESSIVE PLAY. REMOVED AND REPLACED LH MLG DOOR HARDWARE IAW AMM PERFORMED ADJUSTMENT OF LH MLG DOOR PER AMM. ADJUSTMENT GOOD AT THIS TIME.
Part: LINER — CRACKED (CARGO DOOR) · airframe 41,811 hrs · 36,925 cycles
CARGO DOOR LINER CRACKED. REPAIRED SEVERAL CRACKS IN THE CARGO DOOR LINER USING FG-778138-504
Part: DOOR — EXCESS PLAY (RT MLG DOOR) · airframe 41,811 hrs · 36,925 cycles
RH MLG DOOR HAS EXCESSIVE PLAY. REMOVED AND REPLACED RH MLG DOOR HINGE SECTOR HARDWARE IAW AMM FIT CHECK GOOD AT THIS TIME. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.
Part: PIN — MISSING (E/E DOOR LATCH) · airframe 41,811 hrs · 36,925 cycles
* LH FORWARD EQUIPMENT COMPARTMENT DOOR (211AL) MISSING LATCH PIN FOR HOLD OPEN ROD (MARKED). INSTALLED NEW LATCH PIN ON HOLD OPEN ROD FOR EQUIPMENT COMPARTMENT DOOR (211AL) BY INSERTING IT INTO THE ATTACHING LANYARD
Part: SKIN — DENTED (LT NACELLE) · airframe 41,811 hrs · 36,925 cycles
SMALL DENT FOUND ON L/H ENGINE LOWER TRANSLATING COWL ABOUT 6 O'CLOCK POSITION. (MARKED WITH YELLOW PAINT) (C-CHECK) RO:12/24/2019 REPAIRED DAMAGE TO L/H ENGINE LOWER TRANS COWL NEAR 6 O'CLOCK POSITION REF. BOMBARDIER CMM REPAIR NO. SRS030.
Part: SKIN — DENTED (SERVICE DOOR) · airframe 41,811 hrs · 36,925 cycles
AROUND AC SERVICING DOOR THERE ARE MULTIPLE DENTS. (MARKED WITH YELLOW PAINT) (C-CHECK) RO:12/24/2019 REPAIRED FUSELAGE SKIN BETWEEN FS574 AND FS605 REF REO SEE ATTACHED TASK SEE CONTINUE CARD FOR DETAILS.
Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 41,811 hrs · 36,925 cycles
CRACK NOTED AND MARKED ON FS621 BLKHD, FWD FACE AT LINTEL FITTING TO WEB INTERFACE. REPAIRED IAW REO 601R-53-61-1230. REINSPECT IAW SDIR REQUIREMENTS, FWD FACE AT LINTEL FITTING TO WEB INTERFACE. REPAIRED IAW REO. REINSPECTED IAW SDIR REQUIREMENTS NO DEFECTS NOTED
Earlier reports · 2002–2018 · 132 reports
2018
Part: CONTROL HANDLE — FAILED (MLG) · airframe 38,788 hrs · 34,052 cycles
AFTER DEPARTURE, GEAR REMAINED DOWN WITH GEAR SELECTED UP. REPLACED THE LANDING GEAR CONTROL HANDLE IAW AMM. OP CHECKED GOOD, OK FOR SERVICE.
2017
Part: BRACKET — BENT (NLG) · airframe 37,514 hrs · 32,530 cycles
NOSE DOOR WARNING ON TAKEOFF AND GEAR DISAGREE WARNING MESSAGES DURING TAKE OFF. REPLACED THE BENT NOSE BRACKET. OPS NORMAL.
2016
Part: WIRE HARNESS — FAILED (PROXIMITY SENSOR) · airframe 36,202 hrs · 31,018 cycles
RETURNED TO DEPARTURE WITH A GEAR DISAGREE AND NOSE GEAR DOOR OPEN MESSAGE. RECEIVED A THREE DOWN AND LOCKED AND RETURNED. REMOVED AND REPLACED THE NLG CENTERED EXTEND PROXIMITY SENSOR WIRE HARNESS AND BRACKET AND PERFORMED OPS CHECK NO DEFECTS NOTED.
Part: PRIORITY VALVE — MALFUNCTIONED (NLG) · airframe 36,065 hrs · 30,848 cycles
NOSE GEAR WAS EXTREMELY SLOW TO RETRACT WITH ASSOCIATED GEAR DISAGREE. REMOVED AND REPLACED THE NOSE GEAR PRIORITY VALVE IAW AMM. ALL CHECKS GOOD.
2015
Part: SELECTOR VALVE — FAILED (MLG) · airframe 34,296 hrs · 28,750 cycles
BOTH MAIN WOULD NOT EXTEND. EMERGENCY EXTENTION REQUIRE TO GET GEAR DOWN. R & R THE MLG SELECTOR VALVE IAW AMM. PERFORMED OPS CHECK OF THE MLG EXTENSION, RETRACTION SYSTEMS IAW AMM. ACFT EXTENSION, RETRACTION SYSTEMS, OPS CHECKED GOOD.
Part: SKIN — CHAFED (BS 700-736) · airframe 34,171 hrs · 28,603 cycles
GOUGE ON RT FUSELAGE SKIN UNDER PYLON T/E ASSEMBLY FROM FS 700.00 TO FS 736.00. BETWEEN STR 10R AND STR12R. REPAIRED RT SKIN PANEL CHAFE AT FS 700.00 AND FS 755.00 BETWEEN STR 9R AND STR 12R IAW REO AND SRM.
Part: DOOR FRAME — CORRODED (BS 311) · airframe 34,171 hrs · 28,603 cycles
PAX DOOR FWD FORMER BS 311.75 CORRODED. R & R PAX DOOR FORMER FS311.75 IAW SRM. PRESSURIZATION CHECK GOOD IAW AMM.
Part: FORMER — CORRODED (PAX DOOR) · airframe 34,171 hrs · 28,603 cycles
PAX DOOR AFT FORMER, FS347.25, REQUIRES REPLACEMENT DUE TO CORROSION. R & R PAX DOOR AFT FORMER, FS347.25 IAW SRM. COMPLIED WITH THE PRESSURIZATION OF THE ACFT IAW AMM. LEAK CHECK GOOD.
Part: DOOR FRAME — CORRODED (BS 313) · airframe 34,171 hrs · 28,603 cycles
PAX DOOR FRAME FS 313.56 CORRODED. R & R PAX DOOR FRAME AT FS 313.56 IAW SRM. COMPLIED WITH THE PRESSURIZATION LEAK CHECK IAW AMM. LEAK CHECK GOOD.
Part: SKIN — CRACKED (PAX DOOR) · airframe 34,171 hrs · 28,603 cycles
PAX DOOR INNER SKIN CRACKED AND CORROSION. R & R PAX DOOR INNER SKIN IAW SRM.
Part: SKIN — CHAFED (RT AILERON) · airframe 34,171 hrs · 28,603 cycles
RIGHT AILERON UPPER L/E SKIN CHAFED. R & R RT AILERON UPPER L/E SKIN IAW SRM.
Part: STRUCTURE — CHAFED (RT NACELLE) · airframe 34,171 hrs · 28,603 cycles
RIGHT ENGINE UPPER CORE COWL INNER T/E CHAFED. R & R NEW RT ENGINE UPPER CORE COWL IAW SRM.
Part: THRESHOLD — CORRODED (SERVICE DOOR) · airframe 34,171 hrs · 28,603 cycles
SERVICE DOOR THRESHOLD COVER IS CORRODED AT SEVERAL HOLE LOCATIONS. R & R NEW THRESHOLD PLATE, PN 601R38957-31 IAW SRM.
2014
Part: SKIN — DAMAGED (FWD FUSELAGE) · airframe 32,407 hrs · 27,010 cycles
BIRD STRIKE DAMAGE ON UPPER NOSE OF ACFT FROM JUST AFT OF RADOME TO 6 INCHES BELOW WINDSHIELD WIPERS, APPROXIMATELY 5 INCHES WIDE BY 8 INCHES LONG AND 0.3 INCHES DEEP. REPLACED NOSE SKIN PANEL ABOVE TRU COMPARTMENT IAW SRM.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,397 hrs · 26,018 cycles
LEFT AFT EXTERIOR EMERGENCY LIGHT IS INOPERATIVE. REPLACED THE LAMP IAW AMM.
Part: SENSOR — OUT OF ADJUST (WOW) · airframe 30,867 hrs · 25,516 cycles
GEAR DISAGREEMENT. ADJUSTED WOW SENSOR AT TORQUE LINKS. SWUNG GEAR SEVERAL TIMES.
2013
Part: POST — CRACKED (FUSELAGE) · airframe 30,341 hrs · 24,965 cycles
VERTICAL POST AT RBL 27 INBD HAS CRACK AT LOWER RADIUS. C-CHECK REMOVED & INSTALLED NEW 409+128 RBL27 POST IAW SRM & STS.
Part: ACTUATOR — CHAFED (TE FLAP) · airframe 30,341 hrs · 24,965 cycles
LT INBD FLAP, INBD FLAP VANE ACTUATOR TUBE IS CHAFED ON TOP SURFACE. C-CHECK REPAIRED LT INBD FLAP, INBD FLAP VANE ACTUATOR TUBE IAW REO.
Part: ACTUATOR — CHAFED (TE FLAP) · airframe 30,341 hrs · 24,965 cycles
RT INBD FLAP, INBD VANE ACTUATOR TUBE IS CHAFED ON BOTTOM SIDE UNDER AFT ROLLER IN DEPLOYED POSITION. C-CHECK REPAIRED RT INBD FLAP, INBD VANE ACTUATOR TUBE IAW REO.
Part: ACTUATOR — CHAFED (TE FLAP) · airframe 30,341 hrs · 24,965 cycles
LT INBD FLAP, INBD VANE ACTUATOR TUBE IS CHAFED UNDER TOP ROLLER AT DEPLOYED POSITION. C-CHECK REPAIRED LT INBD FLAP, INBD VANE ACTUATOR TUBE IAW REO.
Part: STRAP — CORRODED (FUSELAGE) · airframe 30,341 hrs · 24,965 cycles
FS 461.00 RT PRESS WEB STRAP UPPER SURFACE HAS CORROSION ON STRAP. C-CHECK PRESS FLOOR SKIN WEB STRAP AT FS 461.00 RT REPAIRED IAW REO.
Part: STRAP — CORRODED (FUSELAGE) · airframe 30,341 hrs · 24,965 cycles
FS 499.00 TO FS 510.00 RT PRESS WEB STRAP UPPER SURFACE HAS CORROSION ON STRAP. C-CHECK PRESS FLOOR SKIN WEB STRAP UPPER SURFACE AT FS 499.00 TO FS 510 RT REPAIRED IAW REO.
Part: STRAP — CORRODED (FUSELAGE) · airframe 30,341 hrs · 24,965 cycles
FS 461.00 RT PRESS WEB STRAP UPPER SURFACE HAS CORROSION ON STRAP AROUND FASTENERS. C-CHECK PRESS FLOOR SKIN WEB STRAP AT FS 461.00 RT REPAIRED IAW REO.
Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 30,341 hrs · 24,965 cycles
RT FLOOR EDGE MEMBER FS 589 TO FS 621 HAS CORROSION AROUND NINE NUT PLATE HOLES. C-CHECK REMOVED CORROSION AROUND NINE NUT PLATE HOLES ON RT FLOOR EDGE MEMBER FS 589 TO FS 621 IAW REO.
Part: FLOOR SKIN — CORRODED (FUSELAGE) · airframe 30,341 hrs · 24,965 cycles
PRESS FLOOR SKIN LT AT FS 424 HAS CORROSION ON UPPER SURFACE. C-CHECK PRESS FLOOR SKIN AT FS 424 LT REPAIRED IAW REO.
Part: STRAP — CORRODED (FUSELAGE) · airframe 30,341 hrs · 24,965 cycles
FS 538.00 TO FS 544.00 RT PRESS WEB STRAP UPPER SURFACE HAS CORROSION ON STRAP. C-CHECK PRESS FLOOR SKIN WEB STRAP AT FS 538.00 TO FS 544.00 RT REPAIRED IAW REO.
Part: FLOOR SKIN — CORRODED (FUSELAGE) · airframe 30,341 hrs · 24,965 cycles
PRESS FLOOR SKIN LT AT FS 439 HAS CORRODED ON UPPER SURFACE. C-CHECK PRESS FLOOR SKIN AT FS 439 LT REPAIRED IAW REO.
Part: STRAP — CORRODED (FUSELAGE) · airframe 30,341 hrs · 24,965 cycles
FS 493.00 RT PRESS WEB STRAP UPPER SURFACE HAS CORROSION. C-CHECK PRESS FLOOR SKIN WEB STRAP AT FS 493.00 RT REPAIRED IAW REO.
Part: STRAP — CORRODED (FUSELAGE) · airframe 30,341 hrs · 24,965 cycles
FS 513 RT PRESS WEB STRAP UPPER SURFACE HAS CORROSION ON STRAP. C-CHECK PRESS FLOOR SKIN WEB STRAP ANGLE AT FS 513.00 RT REPAIRED WITH DISPOSITION 2.2 IAW REO.
Part: FLOOR SKIN — CORRODED (FUSELAGE) · airframe 30,341 hrs · 24,965 cycles
PRESS FLOOR SKIN LT AT FS 449.85 HAS CORROSION ON UPPER SURFACE AROUND MAIN FRAME. C-CHECK PRESS FLOOR SKIN AT FS 449.85 LT REPAIRED IAW REO.
Part: FLOOR SKIN — CORRODED (FUSELAGE) · airframe 30,341 hrs · 24,965 cycles
PRESS FLOOR SKIN LT FROM FS 499 TO FS 513 HAS CORROSION IN SEVERAL AREAS. C-CHECK PRESS FLOOR SKIN REPAIRED LT FS 499- 513 IAW REO.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,341 hrs · 24,965 cycles
FS 621 BETWEEN LBL 9 & LBL 27 SEAT TRACKS, ANGLE HAS CORROSION AROUND TWO NUT PLATE HOLES. C-CHECK REMOVED CORROSION AT FS 621 BETWEEN LBL 9 & LBL 27 SEAT TRACKS IAW SRM & REO.
Part: FLOOR SKIN — CORRODED (FUSELAGE) · airframe 30,341 hrs · 24,965 cycles
PRESS FLOOR SKIN FROM FS 473 & 6" FWD HAS CORROSION ON IT. C-CHECK PRESS FLOOR SKIN LT FS 473 & 6"? FWD REPAIRED IAW REO.
Part: STRAP — CORRODED (FUSELAGE) · airframe 30,341 hrs · 24,965 cycles
FS 449.85 RT PRESS WEB STRAP UPPER SURFACE HAS CORROSION ON STRAP. C-CHECK PRESS FLOOR SKIN WEB STRAP AT FS 449.85 RT REPAIRED IAW REO.
Part: FLOOR SKIN — CORRODED (FUSELAGE) · airframe 30,341 hrs · 24,965 cycles
PRESS FLOOR SKIN LT FS 473 TO FS 484 HAS CORROSION ON IT. C-CHECK PRESS FLOOR SKIN LT FS 473- 484 REPAIRED IAW REO.
Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 30,341 hrs · 24,965 cycles
RT FLOOR EDGE MEMBER BETWEEN FS 559+64 & FS 559+48 HAS CORROSION AROUND TWO NUT PLATE HOLES & TWO FWD ATTACH RIVETS. C-CHECK REMOVED CORROSION ON RT FLOOR EDGE MEMBER BETWEEN FS 559+64 & FS 559+48 AROUND TWO NUTPLATE HOLES & TWO FWD ATTACH RIVETS IAW REO.
Part: STRAP — CORRODED (FUSELAGE) · airframe 30,341 hrs · 24,965 cycles
FS 521.00 TO FS 530.00 RT PRESS WEB STRAP UPPER SURFACE HAS CORROSION ON STRAP. C-CHECK PRESS FLOOR SKIN WEB STRAP AT FS 521.00 TO FS 530.00 RT REPAIRED IAW REO.
Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 30,341 hrs · 24,965 cycles
PRESS FLOOR PANEL SKIN LT FROM FS 513 TO FS 529 HAS CORROSION AROUND SEVERAL RIVETS. C-CHECK REPAIRED PRESS FLOOR SKIN LT FS 513 TO FS 529 IAW REO.
Part: STRAP — CORRODED (FUSELAGE) · airframe 30,341 hrs · 24,965 cycles
FS 484.00 RT PRESS WEB STRAP UPPER SURFACE HAS CORROSION ON STRAP. C-CHECK PRESS FLOOR SKIN WEB STRAP AT FS 484.00 RT REPAIRED IAW REO.
Part: POST — CRACKED (FUSELAGE) · airframe 30,341 hrs · 24,965 cycles
FS 409.0+128 BL 0 VERTICAL POST DEFECTS NOTED AT LT & RT AFT RADIUS OF POSTS. C-CHECK REPLACED CRACKED POST AT FS 409+128 BL 0 IAW REO.
Part: POST — CRACKED (FUSELAGE) · airframe 30,341 hrs · 24,965 cycles
VERTICAL BEAM RBL 18.0 AT FS 409.0+128 CRACKED, BOTTOM OTBD OF BEAM. C-CHECK REPLACED CRACKED POST AT FS 409+128 RBL 18 IAW REO.
Part: TRIM SWITCH — FAILED (COCKPIT) · airframe 29,666 hrs · 24,262 cycles
STAB TRIM RUNAWAY TO APPROXIMATELY 1.9. QRH COMPLETE & WAS ABLE TO RECONNECT STAB TRIM. FLT#2605 REPLACED PILOTS TRIM SWITCH IAW AMM.
Part: HYDRAULIC LINE — CHAFED (LT SPOILER) · airframe 29,382 hrs · 23,953 cycles
NR 2 HYDRAULIC SYSTEM LOST ALL FLUID WHILE STARTING ENGINES. HYDRAULIC SYNOPTIC PAGE INDICATES 0% FLUID RESERVOIR. FLT#2612 REPLACED CHAFED LT SPOILERS RETURN LINE & FLEXIBLE LINE IN LT WING ROOT FOR NR 2 SPOILER SYSTEM IAW AMM.
Part: SHUTOFF VALVE — FAILED (BRAKE SYS) · airframe 28,236 hrs · 22,708 cycles
CAUTION ANTI-SKID INBOARD FOLLOWED BY A CAUTION PARKING BRAKE SOV FAIL, FOLLOWED BY A WARNING GEAR DISAGREE ON THE MAINS. ALL MESSAGES SELF CLEARED 2 MINUTES INTO THE FLIGHT. (FLT 2607) REPLACED PARKING BRAKE SHUTOFF VALVE IAW AMM. UNABLE TO DUPLICATE DISCREPANCY, MESSAGE STILL CLEARED. NO LEAKS NOTICED ON THE SOV.
2012
Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,938 hrs · 22,382 cycles
SECOND OVERHEAD LIGHT BURNED OUT. (FLT 2681) RELAMPED OVERHEAD LIGHT.
Part: UNKNOWN — MALFUNCTIONED (FLIGHT CONTROL) · airframe 27,440 hrs · 21,835 cycles
RIGHT FLIGHT SPOILER CAUTION. AIRCRAFT PITCHED 15 DEGREES LEFT WING DOWN. (FLT 4461) COMPLIED WITH SPOILERS FIM PROCEDURES. COULD NOT DUPLICATE FAULTS.
Part: BUSHING — CORRODED (ENGINE MOUNT) · airframe 27,368 hrs · 21,772 cycles
RIGHT ENGINE FORWARD MOUNT YOKE LOWER BUSHING IS CORRODED. (C-CHECK) REPLACED RIGHT ENGINE FORWARD YOKE MOUNT ASSEMBLY IN REFERENCE TO AMM.
Part: BUSHING — CORRODED (ENGINE MOUNT) · airframe 27,368 hrs · 21,772 cycles
THE RIGHT ENGINE FORWARD YOKE MOUNT UPPER LINK HAS CORROSION ON THE BUSHINGS. (C-CHECK) REPLACED RIGHT ENGINE FORWARD YOKE MOUNT UPPER LINK IN REFERENCE TO AMM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,293 hrs · 21,702 cycles
NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4740) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,125 hrs · 21,541 cycles
THE 3RD FROM BACK OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4766) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,885 hrs · 21,306 cycles
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4685) RELAMPED EMERGENCY LIGHT.
Part: INERTIA REEL — FAILED (COCKPIT) · airframe 26,819 hrs · 21,242 cycles
CAPTAINS SHOULDER HARNESS IS LOCKING UP WITH NORMAL MOVEMENT. (FLT 4641) REPLACED PILOT SEAT INERTIA REEL AND SHOULDER STRAP ASSEMBLY IN REFERENCE TO CRJ200 AMM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,667 hrs · 21,103 cycles
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4696) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,407 hrs · 20,847 cycles
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4519) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,287 hrs · 20,736 cycles
NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4445) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,226 hrs · 20,686 cycles
NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4554) RELAMPED EMERGENCY LIGHT.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 27,249 hrs · 21,662 cycles
FS 202 BULKHEAD CRACKED AT PARKING BRAKE CABLE CUTOUT. (C-CHECK) REPAIR PER REO
2011
Part: VANE — CHAFED (TE FLAP) · airframe 272,494 hrs · 21,662 cycles
RIGHT FLAP VANE LEADING EDGE CHAFED. (C-CHECK) REPAIRED PER REO.
Part: SKIN — CHAFED (LT AILERON) · airframe 27,249 hrs · 21,662 cycles
LEFT AILERON UPPER LEADING EDGE SKIN CHAFED FROM INBOARD TO OUTBOARD HINGE. (C-CHECK) REPAIRED IN REFERENCE TO CRJ200 SRM.
Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 27,249 hrs · 21,662 cycles
CORROSION ON BL 9.0 AND BL 27.0 LEFT AT FS 621.00. (C-CHECK) REPAIRED IN REFERENCE TO CRJ 200 SRM.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 27,249 hrs · 21,662 cycles
ANGLE ON UPPER LEFT ENGINE BEAM TO FUSELAGE HAS A CRACK. (C-CHECK) REPAIRED PER CRJ200 SRM.
Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 27,249 hrs · 21,662 cycles
CORROSION ON FLOOR EDGE MEMBER AT RIGHT FS 559+80. (C-CHECK) REPAIRED IN REFERENCE TO CRJ200 SRM.
Part: HARNESS — STUCK (COCKPIT) · airframe 26,154 hrs · 20,626 cycles
CAPTAIN'S SHOULDER HARNESS LOCKED, WILL NOT RELEASE. (FLT 4674) REPLACED CAPTAIN'S RESTRAINT SYSTEM ASSEMBLY.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,056 hrs · 20,538 cycles
AFT MOST OVERHEAD EMERGENCY LIGHT INOPERATIVE. (SERVICE) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,720 hrs · 20,222 cycles
AFT EXTERIOR EMERGENCY LIGHT OVER RIGHT WING IS OUT. (FLT 4672) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,718 hrs · 20,221 cycles
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4446) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,554 hrs · 20,069 cycles
LEFT OVERWING FORWARD EMERGENCY LIGHT IS OUT. (FLT 4513) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,522 hrs · 20,039 cycles
FORWARD AND AFT EXTERIOR EMERGENCY LIGHTS OVER RIGHT WING ARE OUT. (SERVICE) RELAMPED EMERGENCY LIGHTS.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,462 hrs · 19,975 cycles
LEFT EXTERIOR FORWARD EMERGENCY LIGHT IS OUT. (FLT 4490) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,436 hrs · 19,951 cycles
RIGHT OVERWING AFT EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,228 hrs · 19,762 cycles
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4744) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,019 hrs · 19,577 cycles
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4704) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,837 hrs · 19,420 cycles
RIGHT SIDE OVERWING EMERGENCY LIGHTS ARE OUT. (FLT 4761) RELAMPED EMERGENCY LIGHTS.
Part: REGULATOR — OUT OF RIG (AILERON) · airframe 24,505 hrs · 19,143 cycles
AILERONS BINDING. (FLT 4479) RIGGED LEFT WING TENSION REGULATOR PER AMM.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 24,505 hrs · 19,143 cycles
LEFT AFT EMERGENCY LIGHT ON FUSELAGE IS OUT. (FLT 4690) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,986 hrs · 18,693 cycles
AFT CEILING EMERGENCY LIGHT OUT. (FLT 4582) RELAMPED EMERGENCY LIGHT.
2010
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,790 hrs · 18,536 cycles
LEFT FORWARD EXTERIOR EMERGENCY EXIT LIGHT OUT. (FLT 4483) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,651 hrs · 18,422 cycles
AFT CEILING EMERGENCY LIGHT INOPERATIVE. (FLT 4444) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,050 hrs · 17,908 cycles
EMERGENCY LIGHT ON CEILING 3RD BACK, INOP. (FLT 4442) INSTALLED A NEW LAMP.
Part: LINK — CORRODED (LT ENGINE) · airframe 22,527 hrs · 17,460 cycles
LEFT ENGINE FORWARD MOUNT YOKE LINK AND BUSHING CORRODED. (ENG CHANGE) REPLACED LEFT ENGINE FORWARD MOUNT YOKE LINK AND BUSHING PER AMM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,195 hrs · 17,149 cycles
LAST TWO OVERHEAD EMERGENCY LIGHTS INOP. (FLT 4534) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,025 hrs · 17,005 cycles
EMERGENCY FLOOR LIGHT TRACK INOP AT OVERWING DOOR. (FLT 4469) REPLACED EMERGENCY FLOOR LIGHTING STRIP.
Part: SKIN — CRACKED (FUSELAGE) · airframe 21,972 hrs · 16,960 cycles
LEFT TRU BAY FUSELAGE SKIN BELOW DOOR LATCH CRACKED. (C CHECK) RESKINNED PER SRM.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,982 hrs · 16,968 cycles
FS 621 BULKHEAD WEB CRACKED ABOVE CARGO DOOR TRACK FITTING. (C CHECK) REPAIRED PER REO.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 22,259 hrs · 17,206 cycles
FS 621 PRESSURE BULKHEAD CRACKED AT LINTEL FITTING INTERFACE. (C CHECK) REPAIRED PER REO.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 22,259 hrs · 17,206 cycles
FS 621 BULKHEAD WEB CRACKED ABOVE UPPER CARGO DOOR TRACK FITTING. (C CHECK) REPAIRED PER REO.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 22,259 hrs · 17,206 cycles
FS 559 PRESSURE BULKHEAD CAP ANGLE CRACKED. (C CHECK) REPAIRED PER REO.
2009
Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,637 hrs · 16,692 cycles
NR 3 EMERGENCY EXIT FLOOD LIGHT INOP. (FLT 4786)RELAMPED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,496 hrs · 16,576 cycles
OVERHEAD EMERGENCY LIGHT NR 3 INOP. (FLT 4867)RELAMPED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,199 hrs · 16,332 cycles
NR 8 EMERGENCY LIGHT INOP. (FLT 4513) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,876 hrs · 16,059 cycles
NR 3 EMERGENCY LIGHT ON CEILING INOP. (FLT 4657) RELAMPED EMERGENCY LIGHT.
Part: PRIORITY VALVE — FAILED (MLG) · airframe 20,848 hrs · 16,039 cycles
GEAR DISAGREE MESSAGE DISPLAYED. (FLT 4622) REPLACED MAIN GEAR PRIORITY VALVE.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,602 hrs · 15,847 cycles
EMERGENCY LIGHT AT THE TOP OF THE CABIN INOP. (FLT 4868) RELAMPED EMERGENCY LIGHT.
Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 20,027 hrs · 15,399 cycles
FLT 4420 - SECOND FROM THE AFT EMERGENCY FLOODLIGHT INOP. RELAMPED.
2008
Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT) · airframe 18,507 hrs · 14,233 cycles
EMERGENCY FLOOR LIGHTING AFT OF ROW 8 IS INOPERATIVE. (FLIGHT NR 3831) REPLACED FLOOR LIGHTING CONNECTOR AS REQUIRED. OPS CHECK GOOD.
Part: SUPPORT — CRACKED (FUSELAGE) · airframe 19,079 hrs · 14,674 cycles
RIGHT LOWER FLOORBEAM 280 SUPPORT CRACKED (C-CHECK). REPAIRED PER REO.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 19,079 hrs · 14,674 cycles
INTERCOSTAL CRACKED APPROX 18 INCHES BELOW ENGINE BEAM LEFT SIDE BETWEEN FS 621 AND FS 625 (C-CHECK). RE-INSPECT AT EVERY C-CHECK PER REO.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 19,079 hrs · 14,674 cycles
INTERCOSTAL CRACKED APPROX 12 INCHES BELOW ENGINE BEAM LEFT SIDE BETWEEN FS 621 AND FS 625 (C-CHECK). RE-INSPECT AT EVERY C-CHECK PER REO.
Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 19,079 hrs · 14,674 cycles
STA 280.0 FRAME RBL 9.0 INBOARD AND OUTBOARD SUPPORT CLIPS CRACKED (C-CHECK). REPLACED CLIPS.
Part: VALVE — MALFUNCTIONED (NLG SELECTOR) · airframe 17,357 hrs · 13,364 cycles
FLT 3760 - NOSE GEAR DID NOT RETRACT AFTER TAKEOFF. REPLACED NOSE GEAR SELECTOR VALVE. OPS AND LEAK CHECK GOOD, PN OFF 250006000, SN OFF 1644.
Part: GEARBOX — BINDING (THROTTLE CONTROL) · airframe 17,330 hrs · 13,341 cycles
FLT 4331 - LEFT THRUST LEVER WILL NOT COME OUT OF SHUTOFF POSITION. REPLACED LEFT ENGINE THROTTLE GEAR BOX. OPS CHECK GOOD, PN: 2100140-010, SN OFF: 2297.
2006
Part: ACTUATOR — MALFUNCTIONED (STALL PUSHER) · airframe 12,706 hrs · 9,871 cycles
BOTH STALL PUSHER/SHAKERS INOP. REPAIRED WIRE ON PILOT'S STICK SHAKER IAW W/M 27-35-00. REPLACED STALL PUSHER ACTUATOR IAW MM 27-35-15 AND REPLACED NR 2 MACH TRANSDUCER IAW CRJ MM 27-35-25 AND 34-11-00. OPERATIONAL CHECK GOOD. P/N 501-1259-04, S/N OFF 2168; P/N 60730-000-1, S/N OFF 180.
Part: PCU — MALFUNCTIONED (SPOILERONS) · airframe 12,662 hrs · 9,833 cycles
PRIOR TO DEPARTURE RECEIVE "LEFT SPOILERON CAUTION" MESSAGE. REPLACED LEFT SPOILERON PCU IAW MM 27-62-01 AND NR 2 SECU IAW MM 27-61-01, OPERATIONAL CHECK GOOD, PN 1 ON/OFF 49-164-05 SN 1 OFF 01362, PN 2 ON/OFF 27000-7, SN 2 OFF MAL5750.
Part: WINDOW — CRACKED (COCKPIT) · airframe 12,064 hrs · 9,373 cycles
DURING DESCENT INTO SLC THRU 12,000 FT, APPROX NOTICED CAPTAIN'S SIDE WINDOW WAS CRACKED. REPLACED LT SIDE WINDOW IAW MM 56-12-01, PN OFF NP-139322-5; SN OFF 02131R5990.
2005
Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 11,429 hrs · 8,865 cycles
SPOILERS FAULT. REPLACED NR 1 SECU IAW AMM 27-61-05. OPERATIONAL CHECK GOOD.
Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 11,410 hrs · 8,849 cycles
"FLIGHT SPOILER FAULT" MESSAGE ON EICAS. REPLACED SECU AS REQUIRED. OPERATIONAL CHECK GOOD IAW 27-61-05.
Part: CONTROL UNIT — MALFUNCTIONED (SPOILERS) · airframe 10,433 hrs · 8,097 cycles
AFTER FLIGHT SPOILER RETRACTION, RECEIVED FLIGHT SPOILER FAULT STATUS. REPLACED NR 1 SECU IAW 27-61-00. OPS CHECK GOOD.
Part: SWITCH — STICKING (TRIM SYSTEM) · airframe 10,263 hrs · 7,960 cycles
F/O'S TRIM SWITCH IS STICKING. REPLACED F/O'S TRIM SWITCH IAW MM 27-41-05.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,612 hrs · 7,462 cycles
LEFT FORWARD EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LEFT FORWARD EMERGENCY LIGHT IAW MM 33-51-21, OPERATIONAL CHECK GOOD.
Part: SWITCH — MALFUNCTIONED (PITCH TRIM) · airframe 9,596 hrs · 7,449 cycles
CAPTS TRIM SWITCH RIGHT HALF STICKS. REPLACED CAPTAINS PITCH TRIM SWITCH IAW MM 27-41-05-400-801.
Part: SERVO — CONTAMINATED (AUTOPILOT) · airframe 9,596 hrs · 7,449 cycles
WHEN AP (CAPT SIDE) WAS ENGAGED, REC'D AP TRIM IS LWD CAUTION, A/C BEGAN TO ROLL RIGHT WHILE FD WAS DIRECTING A LEFT TURN. DISCONNECTED IT FOR REMAINDER OF FLIGHT. CHECKED RIGGING OF RIGHT AND LEFT AILERON PCU'S IAW 27-11-00. REMOVED MOISTURE FROM AILERON/AUTOPILOT SERVO. AUTOPILOT OPERATIONAL CHECKS GOOD.
Part: PCU — MALFUNCTIONED (FLT SPOILERS) · airframe 9,254 hrs · 7,180 cycles
APPLIED HYDRAULICS AND GOT A LEFT SPOILERON CAUTION MESSAGE. REPLACED LEFT INBOARD AND OUTBOARD PCU IAW MM 27-62-01. REPLACED CB4CN. OPERATIONAL CHECK GOOD. P/N: 27000-7, S/N OFF: 5175, S/N OFF: MAL3758.
2004
Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 8,980 hrs · 6,963 cycles
CRACK IN RIGHT SIDE ADG VIEWING LIGHTENING HOLE ON FS 169.0. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR PARTS IAW CRJ REO 601R-53-11-834 REV "NC".
Part: CLIP — CRACKED (FUSLEAGE) · airframe 8,980 hrs · 6,963 cycles
FUSELAGE FLOORBEAM TO TRANSVERSE BEAM ATTACH CLIPS ARE CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIPS IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-25-16, 51-21-11.
Part: CLIP — CRACKED (FUSELAGE) · airframe 8,980 hrs · 6,963 cycles
AFT EQUIP COMPARTMENT INTERCOSTAL CLIP IS CRACKED; FS 625.00 STR 14R, ITEM FOUND AT C-CHECK INSPECTION. CLIP REPLACED IAW CRJ SRM 51-40-11, 51-42-06 & 51-25-16.
Part: CLIP — CRACKED (FUSELAGE) · airframe 8,980 hrs · 6,963 cycles
FUSELAGE FLOORBEAM TO TRANSVERSE BEAM ATTACH CLIPS ARE CRACKED INBOARD, ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIPS IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-25-16, 51-21-11, 51-42-13.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 8,980 hrs · 6,963 cycles
CARGO COMPARTMENT FLOOR SUPPORT ANGLE IS CRACKED; FS 621.00 RBL 38.0, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-61-117 REV "B" .
Part: CLIP — CRACKED (FUSELAGE) · airframe 8,980 hrs · 6,963 cycles
AFT EQUIP COMPARTMENT INTERCOSTAL CLIP IS CRACKED; FS 625.00 STR 14R, ITEM FOUND AT C-CHECK INSPECTION. CLIP REPLACED IAW CRJ SRM 51-40-11, 51-42-06, AND 51-25-16.
Part: PCU — MALFUNCTIONED (FLIGHT SPOILER) · airframe 8,060 hrs · 6,227 cycles
LT SPOILERON NR 1 PCU STATUS MESSAGE ON EICAS. REMOVED AND REPLACED LT IB SPOILERON PCU IAW MM 27-62-01. OPERATIONAL CHECK GOOD.
Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 7,821 hrs · 6,040 cycles
DURING CRUISE AT 33,000 RIGHT SIDE FRONT WINDSHIELD CRACKED. REPLACED RT WINDSHIELD PER MM 56-11-01. OPERATIONAL CHECK GOOD. P/N OFF: 601R33033-14, S/N OFF: 01123H7078.
2003
Part: PCU — MALFUNCTIONED (SPOILER) · airframe 5,404 hrs · 4,175 cycles
SPOILERON FAULT STATUS MSG ON TAXI OUT. REPLACED LEFT I/B FLT SPOILERON PCU IAW 27-60-00 & NR 1 SECU. OPS AND LEAKS CHECKS GOOD IAW 27-60-00. S/N OFF: 5587. SECU P/N: 49-164-20 S/N OFF: 01664 S/N ON: 03079.
Part: PCU — MALFUNCTIONED (RT SPOILERON) · airframe 5,050 hrs · 3,919 cycles
ON TAXI OUT, GOT ''R SPOILERON'' AND ''SPOILERON FAULT'' MSGS. REMOVED AND REPLACED RIGHT SPOILERON INBOARD PCU IAW 27-62-01. LEAK AND OPS CHECK GOOD.
Part: ROLLER — FROZEN (PAX DOOR) · airframe 4,904 hrs · 3,820 cycles
PAX DOOR WARNING MESSAGE ON DESCENT, NO PRESSURE DROP. INSPECTED PAX DOOR, FOUND INNER DOOR HANDLE DETENT ROLLER FROZEN IN RETRACTED POSITION. REMOVED AND REPLACED ROLLER SHAFT PER CRJ MM 52-11-02. OPS CHECK GOOD. P/N OFF: 582-20352.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 4,693 hrs · 3,657 cycles
FS 621 LEFT FLOORBEAM ANGLE LBL 42 CRACKED. DISCOVERED DURING C-CHECK. REPAIRED DAMAGED AREA IAW CRJ REO 601R-53-61-117 REV A.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 4,693 hrs · 3,657 cycles
FS 280 RIGHT FLOORBEAM RBL 9.0 ATTACH ANGLES CRACKED. DISCOVERED DURING C-CHECK. ANGLES REPLACED IAW CRJ SRM 51-40-11.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 4,693 hrs · 3,657 cycles
FLOORBEAM ANGLES AT STR 14 FS 625 ARE CRACKED BOTH SIDES. DISCOVERED DURING C-CHECK. REPLACED ANGLES IAW CRJ SRM 51-40-11 AND 51-42-06.
Part: PCU — MALFUNCTIONED (LT WING SPOILER) · airframe 4,384 hrs · 3,401 cycles
SPOILERONS FAULT STATUS MESSAGE ILLUMINATED IN FLIGHT. REMOVED AND REPLACED THE LEFT WING SPOILERON INBOARD PCU IAW CRJ MM 27-62-01. OPS AND LEAK CHECK GOOD. P/N OFF: 270007 S/N OFF: MAL 4704 S/N ON: MAL 5034.
Part: PROXIMITY SWITCH — MALFUNCTIONED (NLG) · airframe 4,240 hrs · 3,279 cycles
ON APPROACH RECEIVED A NOSE GEAR DISAGREEMENT ON THE EDI. RAN QRH, CLEARED DISAGREEMENT. SWUNG NOSE GEAR IAW MM CHAPTER 32. INSPECTED PROXIMITY SWITCHES. OPS CHECK GOOD.
2002
Part: DISPLAY — MALFUNCTIONED (ATTITUDE IND) · airframe 3,558 hrs · 2,748 cycles
AFTER TAKEOFF THE FIRST OFFICER'S ATTITUDE INDICATOR FAILED. ATT, FD, AND MAG FLAGS ILLUMINATED. QRH WAS INEFFECTIVE, RETURNED TO SLC. REMOVED AND REPLACED FIRST OFFICER'S PFD IAW MM 31-61-01. OPS CHECK GOOD IAW MM 34-25-00-710-901.
Part: DAMPER — MALFUNCTIONED (AUTOPILOT SYS) · airframe 2,643 hrs · 2,044 cycles
YAW DAMPER NR 2 INOP. REMOVED AND REPLACED NR 2 YAW DAMPER IAW 22-22-01. REPLACED NR 2 FCC CARD. OPS CHECK GOOD.
Part: WINDOW — CRACKED (COCKPIT) · airframe 1,847 hrs · 1,404 cycles
LEFT SIDE COCKPIT SIDE WINDOW SHATTERED AT FL350. DIVERTED TO GJT. REMOVED AND REPLACED LEFT SIDE WINDOW. OPS AND LEAK CHECKS GOOD.
Part: ACTUATOR — FAILED (HORIZ STAB) · airframe 1,243 hrs · 940 cycles
DURING INITIAL POWER UP IN FAT, STAB TRIM CH2 WOULD NOT ENGAGE. REMOVED AND REPLACED HORIZONTAL STAB TRIM ACTUATOR AND MCU IAW CRJ MM 27-42-01. OPS CHECK GOOD. AIRCRAFT OK FOR RETURN TO CAT II SERVICE.