N934SW
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.
142 reports on file, 2002-12-31 – 2019-12-10.
Part: STRINGER — CORRODED (BS 589) · airframe 42,794 hrs · 36,693 cycles
WHILE REMOVING FRAME AT FS 589.00 IT WAS NOTICED CORROSION ON STGR 21L AT APPROX. FS 581.00. REPAIRED THE STRINGER IAW SRM. ALL CHECKED GOOD.
Part: STRUCTURE — CHAFED (BS 621) · airframe 42,794 hrs · 36,693 cycles
FS621 LBL9.50 CHAFE AREA REQUIRES REPAIR PER REO (C-CHECK) RO 12/23/2019 PERFORMED REPAIR TO FS621 LBL9.50 CHAFE AREA REF REO. CHECKS GOOD
Part: STRAP — CORRODED (BS 559) · airframe 42,794 hrs · 36,693 cycles
THE CROSSBEAM/STRAP AT BS 559 FROM LT EDGE MEMBER, SILL TO LBL 27 HAD CORROSION. REMOVED AND INSTALLED A NEW SERVICEABLE CROSSBEAM STRAP AT BS.559 IAW DWG. PERFORMED PRESSURE CHECK IAW AMM. PRESSURE CHECKED GOOD. PERFORMED OPS TEST OF THE MLG OVERHEAT DETECTION AND WARNING SYSTEM IAW AMM. OPS TESTED GOOD.
Part: STRAP — CORRODED (BS 559) · airframe 42,794 hrs · 36,693 cycles
THE CROSSBEAM/STRAP AT BS 559 +80 FROM RBL 9 TO RBL 27 HAD CORROSION. REMOVED CORROSION FROM THE CROSSBEAM/STRAP IAW SRM. MATERIAL LOSS FOUND TO BE WITHIN LIMITS IAW SRM.
Part: DOUBLER — CORRODED (BS 605-621) · airframe 42,794 hrs · 36,693 cycles
THE AFT DRAIN DOUBLER BETWEEN BS 621 AND 605, BETWEEN STRINGERS 26R AND 25R HAD MULTIPLE AREAS OF CORROSION. REMOVED AND INSTALLED NEW DRAIN MAST DOUBLER IAW SRM AND DWG. ALL CHECKED GOOD.
Part: FRAME — CORRODED (BS 605) · airframe 42,794 hrs · 36,693 cycles
THE FRAME AT BS 605 FROM STRINGERS 25R TO 20L HAD CORROSION AT MULTIPLE LOCATIONS. REMOVED CORROSION AND RESTORED FINISH IAW SRM. REMAINING MATERIAL THICKNESS IS WITHIN LIMITS. . LEAK CHECKED GOOD.
Part: FRAME — CORRODED (BS 589) · airframe 42,794 hrs · 36,693 cycles
THE FRAME AT BS 589 FROM STRINGERS 24R TO 20L HAD MULTIPLE LOCATIONS OF CORROSION. REMOVED AND REPLACED THE FRAME IAW SRM. PRESSURE CHECKED GOOD,
Part: FRAME — CORRODED (BS 589) · airframe 42,794 hrs · 36,693 cycles
THE FRAME AT BS 589 FROM STRINGERS 20L TO 17L HAD CORROSION AT MULTIPLE AREAS. REMOVED CORROSION IAW SRM. REMAINING MATERIAL THICKNESS IS WITHIN LIMITS IAW SRM. RESTORED FINISH IAW SRM. . PRESSURE CHECKED GOOD.
Part: ANGLE — CRACKED (BS 280 FLOORBEAM) · airframe 42,794 hrs · 36,693 cycles
CRACKED CLIP AT BS 280, LBL 9 INBD SIDE. REMOVED, AND INSTALLED A NEW INBD ATTACHMENT CLIP IAW REO, AND SRM.
Part: STRAP — CORRODED (BS 559) · airframe 42,794 hrs · 36,693 cycles
THE CROSSBEAM/STRAP AT BS 559 FROM RT EDGE MEMBER, SILL TO RBL 27 HAD CORROSION. REMOVED CORROSION AT CROSSBEAM/STRAP IAW SRM 51-21-06, AREA IS WITHIN LIMITS IAW SRM 53-00-00.
Part: ANGLE — CRACKED (BS 280 FLOORBEAM) · airframe 42,794 hrs · 36,693 cycles
CRACKED CLIP AT BS 280, RBL 9 OTBD SIDE. REMOVED AND INSTALLED A NEW FABRICATED ATTACHING CLIP IAW REO AND SRM.
Part: FRAME — CORRODED (BS 589) · airframe 42,794 hrs · 36,693 cycles
THE FRAME AT BS 589 FROM STRINGERS 17R TO 19R HAD CORROSION. REMOVED CORROSION IAW SRM. MATERIAL LOSS FOUND TO BE WITHIN ALLOWABLE LIMITS IAW SRM. RESTORED FINISH AND CIC.
Part: FLOOR SUPPORT — CORRODED (PRESSURE DECK) · airframe 42,794 hrs · 36,693 cycles
LH PRESSURE FLOOR SILL ANGLE HAS MULTIPLE AREAS OF CORROSION. BLENDED OUT CORROSION ON L/H FLOOR SILL ANGLE AND REPLACED FASTENERS A REQUIRED IAW REO. ALL CHECKED GOOD
Part: ANGLE — CORRODED (BS 621) · airframe 42,794 hrs · 36,693 cycles
THE FS 621.00 BELOW FLOOR ANGLE FROM STRINGER 24R TO 19L HAD CORROSION IN MULTIPLE LOCATIONS. REMOVED CORROSION IAW SRM. REMAINING MATERIAL THICKNESS IS WITHIN LIMITS IAW SRM. RESTORED FINISH TO AREA IAW SRM. PRESSURE CHECKED GOOD.
Part: PANEL — DIRTY (BS 559) · airframe 42,794 hrs · 36,693 cycles
THE FLAPPER DRAIN PANEL BETWEEN BS 559+80 TO 559+96, STRINGERS 26L AND 27 HAD CORROSION. CLEANED AREA IAW SRM. UPON CLEANING, FOUND NO CORROSION ON FLAPPER DRAIN PANEL.
Part: FRAME — CORRODED (BS 605) · airframe 42,794 hrs · 36,693 cycles
THE FRAME AT BS 605 FROM STRINGERS 20L TO 17L HAD CORROSION. REMOVED CORROSION AND RESTORED FINISH IAW SRM. REMAINING MATERIAL THICKNESS IS WITHIN LIMITS. LEAK CHECKED GOOD.
Part: STRINGER — DIRTY (BS 589-574) · airframe 42,794 hrs · 36,693 cycles
STRINGER 26R BETWEEN BS 589 AND 574 HAD CORROSION. CLEANED AREA IAW SRM. UPON CLEANING, FOUND NO CORROSION ON THE STRINGER.
Part: FLOORBEAM — CRACKED (BS 461) · airframe 42,794 hrs · 36,693 cycles
*PRESSURE FLOOR SKIN IS CRACKED AT FS 461 BETWEEN BL 0 AND LBL 9. REPAIRED CRACKED PRESSURE FLOOR SKIN AT APPROX FS461 BETWEEN LBL9 AND RBL9 IAW REO. ALL CHECKED GOOD
Part: ANGLE — CRACKED (BS 484) · airframe 42,794 hrs · 36,693 cycles
CLIP ON INTERCOSTAL AT FS 484 OTBD OF RBL27 IS CRACKED. (C-CHECK) RO 12/23/2019 REMOVED AND REPLACED CRACKED CLIP WITH NEW CLIP (P/N 601R31171-9) ON INTERCOSTAL AT FS 484.00, OTBD RBL 27 REF CRJ-200 SRM. RESTORD FINISH AND APPLIED CIC TO REWORKED AREA REF CRJ-200 SRM. SEE CONTINUATION FOR DETAILS.
Part: FRAME — CORRODED (BS 574) · airframe 42,794 hrs · 36,693 cycles
* THE FRAME AT FS 574.00 FROM STRINGER 17L TO 18L HAS CORROSION. (C-CHECK) RO 12/23/2019 REMOVED CORROSION FROM FS 574.00 FRAME BETWEEN STRINGER 17L AND18L AND RESTORED FINISH. REF CRJ200 SRM. REMAINING MATERIAL THICKNESS IS WITHIN LIMITS. SEE CONTINUE CARD FOR DETAILS. LEAK CHECK GOOD.
Part: FRAME — CORRODED (BS 574) · airframe 42,794 hrs · 36,693 cycles
THE FRAME AT FS 574.00 FROM STRINGER 24L TO 25R HAS CORROSION. REMOVED CORROSION AND RESTORED FINISH IAW SRM. REMAINING MATERIAL THICKNESS IS WITHIN LIMITS. OPS CHECKED GOOD.
Part: ANGLE — CRACKED (BS 484) · airframe 42,794 hrs · 36,693 cycles
CLIP ON INTERCOSTAL AT FS 484 OTBD OF LBL27 IS CRACKED. REMOVED AND REPLACED CRACKED CLIP WITH NEW CLIP ON INTERCOSTAL AT FS 484.00, OTBD LBL 27 IAW SRM. RESTORD FINISH AND APPLIED CIC TO REWORKED AREA REF SRM.
Part: ANGLE — CRACKED (BS 280 FLOORBEAM) · airframe 42,794 hrs · 36,693 cycles
CRACKED CLIP BS 280, LBL 9 OTBD SIDE. FABRICATED, LOCATED, DRILLED AND INSTALLED A NEW CLIP IAW REO, AND LOCATION AND MATERIAL, AND IAW SRM.
Part: BRACKET — CRACKED (BS 625) · airframe 42,794 hrs · 36,693 cycles
AFT EQUIPMENT COMPARTMENT HAS CRACKED CLIP ATTACHED TO FS 625.00 FRAME NEAR R/H STGR 14. REMOVED AND REPLACED CLIP P/N: 601-35012-52 AT FS 625.00 FRAME NEAR R/H STGR 14R IAW SRM.
Part: BRACKET — CRACKED (BS 625) · airframe 42,794 hrs · 36,693 cycles
* AFT EQUIPMENT COMPARTMENT HAS CRACKED CLIP ATTACHED TO FS 625.00 FRAME NEAR L/H STGR 14. REMOVED AND REPLACED CLIP P/N: 601-35012-51 AT FS 625.00 FRAME NEAR L/H STGR 14L IAW SRM.
Part: UPLOCK — FAILED (NLG) · airframe 42,167 hrs · 36,113 cycles
GEAR DISAGREE IN FLIGHT. COMPLIED WITH QRH. DECLARED EMERGENCY. LANDED WITHOUT INCIDENT. (FLT#5045) CLOSED REMOVED AND REPLACED NLG UPLOCK ASSEMBLY AND NLG UPLOCK HARNESS ASSEMBLY IAW AMM. LEAK CHECK GOOD AT THIS TIME. OPS TEST OF PSS SYSTEM GOOD AT THIS TIME.
Earlier reports · 2002–2017 · 116 reports
2017
Part: STRUCTURE — CHAFED (RT AILERON) · airframe 38,526 hrs · 32,822 cycles
RIGHT AILERON INBOARD FIXED LEADING EDGE IS CHAFED. REMOVED AND REPLACED THE AILERON INBOARD FIXED LEADING EDGE IAW SRM.
Part: SKIN — DENTED (BS 654-672) · airframe 38,526 hrs · 32,822 cycles
FUSELAGE SKIN DENTED BS 654 & 672 BETWEEN STRINGERS 26L & 26R. REPAIRED THE SKIN IAW REO.
2015
Part: VANE — CHAFED (LT WING TE FLAP) · airframe 33,950 hrs · 28,606 cycles
LEFT SIDE INBD FLAP, MOVABLE VANE OTBD L/E HAS CHAFE. REMOVED, FABRICATED, INSTALLED NEW LT INBD FLAP, OTBD FLAP VANE CAP IAW SRM.
Part: UNKNOWN — SMOKE (CABIN) · airframe 31,913 hrs · 26,797 cycles
DURING CLIMB OUT, CREW RECEIVED SMOKE TOILET CAUTION MESSAGE. F/A REPORTED NO EVIDENCE OF SMOKE OR ODOR IN THE CABIN. RAN ACFT ABOUT 15 MIN AND TRIED EVER COMBINATION OF BLEED AIR AND ELECTRICAL BUT UNABLE TO DUPLICATE. NO INDICATION IN COCKPIT OR VISUAL.
2014
Part: DOOR FRAME — DENTED (BS 310) · airframe 31,764 hrs · 26,672 cycles
DENT ON THE FWD PAX DOOR FRAME BS 310 S16L. REPAIRED IAW REO.
Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 30,733 hrs · 25,810 cycles
F/A FLASHLIGHT IS INOPERATIVE. R & R BATTERY ON F/A FLASHLIGHT IAW AMM. OPS CHECKED GOOD.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 30,229 hrs · 25,424 cycles
EXTERIOR OVERWING EXIT EMERGENCY LIGHT ON RT SIDE FUSELAGE IS BURNED OUT, REPLACED LAMP.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,720 hrs · 25,035 cycles
NR 4 EMERGENCY POD LIGHT IS BURNED OUT. FLT 5641 RELAMPED.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 29,559 hrs · 24,903 cycles
AFT OVERHEAD EMERGENCY EXIT SIGN IS BURNED OUT. SERVICE RELAMPED.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 29,559 hrs · 24,903 cycles
FLOOR LEVEL EMERGENCY EXIT SIGN IS BURNED OUT AT MCD ENTRY. SERVICE RELAMPED.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 29,519 hrs · 24,877 cycles
TWO EACH CRACKS NOTED ON FS 621 AFT PRESS BULKHEAD FWD FACE AT LBL 27.50 BETWEEN WL 120.00 & WL 75.00. C-CHECK CUT AWAY DAMAGE, FABRICATED NEW PARTS & INSTALLED ON FS 621 AFT PRESS BULKHEAD IAW REO.
Part: VANE — CHAFED (TE FLAP) · airframe 29,519 hrs · 24,877 cycles
LT INBD FLAP, OTBD FLAP VANE IS CHAFED. C-CHECK BLENDED CHAFE ON LT INBD FLAP, OTBD FLAP VANE LE IAW REO.
Part: POST — CRACKED (FUSELAGE) · airframe 29,519 hrs · 24,877 cycles
FS 409.0+128 BL 0.00 FWD RADIUS OF VERTICAL POST CRACK INDICATION NOTED. C-CHECK REPLACED FS 409+128 BL 0 VERTICAL POST IAW SRM & REO.
Part: VANE — CHAFED (TE FLAP) · airframe 29,519 hrs · 24,877 cycles
RT INBD FLAP, OTBD FLAP VANE IS CHAFED. C-CHECK NEW CAP WAS INSTALLED IAW REO.
Part: VANE — CHAFED (TE FLAP) · airframe 29,519 hrs · 24,877 cycles
RT INBD FLAP, MIDDLE FLAP VANE IS CHAFED. C-CHECK REPAIRED IAW REO.
Part: VANE — CHAFED (TE FLAP) · airframe 29,519 hrs · 24,877 cycles
LT INBD FLAP, MIDDLE FLAP VANE IS CHAFED. C-CHECK BLENDED CHAFE ON LT INBD FLAP, MIDDLE FLAP VANE LE IAW REO.
Part: VANE — CHAFED (TE FLAP) · airframe 29,519 hrs · 24,877 cycles
RT INBD FLAP, INBD FLAP VANE IS CHAFED. C-CHECK BLENDED CHAFE ON RT INBD FLAP, INBD FLAP VANE LE IAW REO.
Part: VANE — CHAFED (TE FLAP) · airframe 29,519 hrs · 24,877 cycles
LT INBD FLAP, INBD FLAP VANE IS CHAFED. C-CHECK BLENDED CHAFE ON LT INBD FLAP, INBD FLAP VANE LE IAW REO.
2013
Part: CONTROL HANDLE — FAILED (COCKPIT) · airframe 29,112 hrs · 24,579 cycles
RECEIVED ANTI-SKID INBD CAUTION MESSAGE, FOLLOWED BY PARKING BRAKE SOV CAUTION MESSAGE. GEAR DID NOT RETRACT, FOLLOWED QRH WITH GEAR SELECTED DOWN, ALL MESSAGES CLEARED. FLT 6405 REPLACED LANDING GEAR SELECTOR HANDLE ASSEMBLY IAW AMM. PERFORMED GEAR SWINGS, SYSTEM OPERATIONS CHECKED GOOD PN 601R51008-33.
Part: SHUTOFF VALVE — FAILED (PARKING BRAKE) · airframe 29,078 hrs · 24,557 cycles
UPON SELECTING GEAR UP AFTER TAKEOFF RECEIVED ANTI-SKID INBD CAUTION, THEN A PARK BRAKE SOV CAUTION MESSAGE & GEAR WOULD NOT RETRACT. UPON SELECTING GEAR DOWN BOTH MESSAGES CLEARED & LANDING GEAR REMAINED DOWN. FLT 6427 REPLACED PARKING BRAKE SOV, PERFORMED LEAK CHECK, NO LEAKS, PERFORMED GEAR EXTENSION & RETRACTION IAW AMM, OPERATIONS CHECKED GOOD.
Part: BUTTON — DIRTY (CABIN DOOR) · airframe 29,033 hrs · 24,513 cycles
MAIN CABIN DOOR JAMMED COULD NOT OPEN. FLT 6252 INSPECTED MAIN CABIN DOOR & FOUND CABIN DOOR PUSH BUTTON ASSIST MOTOR STUCK. CLEANED DEBRIS FROM PUSH BUTTON. DOOR NO LONGER JAMMED SHUT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,834 hrs · 24,375 cycles
NR 2 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. FLT#6217 RELAMPED.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 28,102 hrs · 23,808 cycles
FLT 6308, NR 4 EMERGENCY OVERHEAD LIGHT BURNED OUT. REPLACED LAMPS.
Part: GUIDE — LACK OF LUBE (CABIN DOOR) · airframe 27,760 hrs · 23,546 cycles
MAIN CABIN DOOR IS DIFFICULT TO OPEN. LUBED THE HANDLE ROLLER GUIDE. REPLACED MAIN CABIN DOOR ICE BREAKER CABLE, IAW AMM.
2012
Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,917 hrs · 22,038 cycles
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6465) RELAMPED EMERGENCY LIGHT.
Part: INVERTER — FAILED (CABIN) · airframe 25,595 hrs · 21,794 cycles
FLOOR EMERGENCY LIGHT STRIP FROM ROW 8 AFT IS INOPERATIVE. (FLT 5537) REPLACED EMERGENCY LIGHT INVERTER FOR THE NR 4 POSITION IN REFERENCE TO CRJ AMM.
Part: CAP — DAMAGED (TE FLAP VANE) · airframe 25,070 hrs · 21,381 cycles
(C-CHECK) RIGHT FLAP VANE CENTER LEADING EDGE CAP IS DAMAGED. REPLACED PER SRM.
Part: STRUT — LOW (NLG) · airframe 24,925 hrs · 21,250 cycles
GEAR DISAGREE WARNING FOR 10 SECONDS THEN GEAR CAME UP NORMALLY. (FLT 6340) PERFORMED A FULL SERVICE ON THE NOSE GEAR SHOCK STRUT ASSEMBLY IAW CRJ 200 AMM.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 24,740 hrs · 21,102 cycles
FLT 5416, NR 1 AND NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,652 hrs · 21,026 cycles
NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5576) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,509 hrs · 20,895 cycles
NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6434) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,509 hrs · 20,895 cycles
NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6434) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,326 hrs · 20,756 cycles
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6209) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,264 hrs · 20,703 cycles
NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.
2011
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,959 hrs · 20,487 cycles
NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6387) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,959 hrs · 20,487 cycles
RIGHT WING AFT EXTERIOR EMERGENCY EXIT LIGHT IS OUT. (FLT 6486) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,522 hrs · 20,135 cycles
AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6347) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,482 hrs · 20,107 cycles
NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6404) RELAMPED EMERGENCY LIGHT.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 22,866 hrs · 19,588 cycles
FLOOR SUPPORT ANGLE AT FS 621 LBL 41 IS CRACKED. (C-CHECK) REPLACE PER SRM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,477 hrs · 19,293 cycles
MIDDLE CEILING LEVEL CABIN EMERGENCY LIGHT IS OUT. (FLT 6229) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,188 hrs · 19,064 cycles
NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6907) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,709 hrs · 18,690 cycles
NR 2 CEILING EMERGENCY LIGHT IS OUT. (FLT 6869) RELAMPED EMERGENCY LIGHT.
2010
Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,165 hrs · 18,237 cycles
AFT CEILING EMERGENCY LIGHT OUT. (FLT 6402) RELAMPED EMERGENCY LIGHT.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 20,989 hrs · 18,104 cycles
FS 280 FLOORBEAM IS CRACKED AT MULTIPLE LOCATIONS. (C-CHECK) REPLACED FS 280 FLOORBEAM PER SRM.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 20,989 hrs · 18,104 cycles
FS 621 PRESSURE BULKHEAD WEB AT LINTEL FITTING CRACKED. (C-CHECK) REPAIR PER REO.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 20,989 hrs · 18,104 cycles
FS 599.0 BULKHEAD CRACKED ON LEFT SIDE. (C-CHECK) REPAIR PER REO.
Part: FITTING — CRACKED (FUSELAGE) · airframe 21,139 hrs · 18,221 cycles
FS 200 BULKHEAD AT LEFT PARKING BRAKE FITTING CRACKED. (C-CHECK) REPAIRED PER REO.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 20,852 hrs · 17,990 cycles
RIGHT AFT EXTERIOR EMERGENCY LIGHT IS INOPERATIVE. (FLT 6403) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,840 hrs · 17,980 cycles
THE 3RD CEILING EMERGENCY LIGHT IS INOPERATIVE. (FLT 6640) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,647 hrs · 17,802 cycles
LAST EMERGENCY LIGHT IN CABIN IS INOPERATIVE. (FLT 6834) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,050 hrs · 17,300 cycles
AFT EMERGENCY CEILING LIGHT NR 4 INOP. (FLT 6826) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,388 hrs · 16,743 cycles
NR 4 OVERHEAD EMERGENCY LIGHT INOP. (FLT 6534) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,256 hrs · 16,619 cycles
NR 4 CEILING LEVEL FLOOD LIGHT INOP. (FLT 6038) RELAMPED FLOOD LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,226 hrs · 16,591 cycles
CEILING LEVEL EMERGENCY FLOODLIGHT NR 3 INOP. (FLT 6484) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,793 hrs · 16,230 cycles
MOST AFT EMERGENCY CEILING LIGHT INOP. (FLT 6303) RELAMPED EMERGENCY LIGHT.
Part: WARNING MESSAGE — FALSE ACTIVATION (LAVATORY SMOKE) · airframe 18,608 hrs · 16,066 cycles
FLT 6476 - SMOKE TOILET CAUTION MESSAGE DISPLAYED ON CLIMB. MESSAGE CLEARED WITH NO ACTION TAKEN.
Part: COALESCER BAG — DIRTY (AC BAY) · airframe 18,525 hrs · 16,002 cycles
SMOKE TOILET CAUTION ON TAKEOFF. (FLT 6014) REPLACED RIGHT PACK COALESCER BAG.
2009
Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,525 hrs · 16,002 cycles
NR 2 CEILING LEVEL EMERGENCY FLOODLIGHT INOP. (FLT 6586) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,173 hrs · 15,709 cycles
NR 3 EMERGENCY OVERHEAD LIGHT INOP. (FLT 6734) RELAMPED EMERGENCY LIGHT.
Part: INVERTER — MALFUNCTIONED (CABIN) · airframe 17,605 hrs · 15,247 cycles
RIGHT SIDE LOWER EMERGENCY WING SIGN PARTIALLY ILLUMINATED. (FLT 5777) REPLACED NR 2 INVERTER.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,605 hrs · 15,247 cycles
AFT OVERHEAD EMERGENCY LIGHT IN CABIN INOP. (FLT 6494) RELAMPED EMERGENCY LIGHT.
Part: STRUT — LOW (NLG) · airframe 17,474 hrs · 15,143 cycles
GEAR DISAGREE MESSAGE DISPLAYED. (FLT 5961) ACCOMPLISHED FULL SERVICE OF NLG STRUT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,370 hrs · 15,042 cycles
CEILING EMERGENCY LIGHT INOP. (FLT 6701) RELAMPED EMERGENCY LIGHT.
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 17,050 hrs · 14,789 cycles
FLT 6380 - FLOOR LEVEL EMERGENCY LIGHTS INOP. RESET POWER SUPPLY.
Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 16,797 hrs · 14,591 cycles
FLT 6127 - RIGHT WING AFT EMERGENCY EXIT LIGHT INOP. RELAMPED.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 17,267 hrs · 14,960 cycles
FS 625 INTERCOSTALS CRACKED. (C CHECK) REPLACED PER SRM.
Part: FITTING — CRACKED (FUSELAGE) · airframe 17,267 hrs · 14,960 cycles
FS 400-500 CLIPS CRACKED. (C CHECK) REPLACED PER REO.
Part: FITTING — CRACKED (FUSELAGE) · airframe 17,267 hrs · 14,960 cycles
FS 280 CLIPS CRACKED. (C CHECK) REPLACED PER SRM.
Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 16,580 hrs · 14,407 cycles
FLT 6511 - EMERGENCY LIGHTING STRIP BY EXIT ROW INOP. REPAIRED BROKEN WIRE.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 16,563 hrs · 14,393 cycles
FLT 5892 - EMERGENCY LIGHT AT ROW 5 INOP. RELAMPED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,486 hrs · 14,327 cycles
FLT 6351 - ONE SEGMENT OF FLOOR EMERGENCY LIGHT INOP. REPLACED FLOOR STRIP.
Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 16,392 hrs · 14,257 cycles
FLT 6001 - LOWER EMERGENCY EXIT RIGHT SIDEWALL LIGHT INOP. RESEATED CONNECTOR.
Part: CONNECTOR — DIRTY (EMERGENCY LIGHTS) · airframe 16,140 hrs · 14,057 cycles
FLT 6453 - EMERGENCY LIGHTS ON FLOOR FROM ROW 5 TO ROW 8 INOP. CLEANED AND RESECURED CONNECTORS.
Part: CONNECTOR — DIRTY (EMERGENCY LIGHT) · airframe 16,084 hrs · 14,008 cycles
FLT 6265 - RIGHT SIDE LOWER EMERGENCY SIGN AND RIGHT SIDE FLOOR ILLUMINATION STRIPS INOP. CLEANED CONNECTION ON EMERGENCY BATTERY PACK NR 4.
Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 15,975 hrs · 13,917 cycles
FLT 6435 - FLOOR ILLUMINATION STRIP ROWS 6-8 IN INOP. RESEATED CONNECTOR.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 15,975 hrs · 13,917 cycles
FLT 6621 - EMERGENCY LIGHT CENTER CEILING ROW 10 INOP. RELAMPED.
2008
Part: ACM — SMOKE (RIGHT) · airframe 15,568 hrs · 13,592 cycles
FLT 6514 - SMOKE TOILET MESSAGE AND SMOKE IN CABIN. REPLACED RIGHT ACM,
Part: SENSOR — FAILED (RT A/C PACK) · airframe 15,514 hrs · 13,546 cycles
FLT 6550 - "SMOKE TOILET" MESSAGE AFTER TAKE OFF. REPLACED RIGHT PACK TEMPERATURE SENSOR.
Part: SMOKE WARNING — MALFUNCTIONED (LAVATORY) · airframe 15,316 hrs · 13,374 cycles
ON CLIMBOUT "SMOKE TOILET" CAUTION MESSAGE, F/A REPORTED SMOKE (FLT 6269). INSPECTED LAV AND COMPONENTS COULD NOT FIND ANY DEFECTS. RAN BOTH ENGINES AND PRESSURIZED AIRCRAFT WITH ENGINE BLEEDS, NO SMOKE OR SMOKE SMELL NOTED ANYWHERE IN CABIN.
Part: CONNECTOR — DIRTY (EMERGENCY LIGHT) · airframe 15,252 hrs · 13,319 cycles
FLT 6456 - RIGHT WING EXIT EMERGENCY SIGN INOP. CLEANED ELECTRICAL CONNECTION ON LIGHTING STRIP.
Part: OXYGEN MASK — UNWANTED DEPLOY (CABIN) · airframe 14,888 hrs · 13,009 cycles
THE O2 MASKS IN PAX COMPARTMENT DROPPED WHILE AT THE GATE. FLIGHT 6759. RESTOWED ALL O2 MASKS AND PERFORMED OPERATIONAL TEST OF THE PASSENGER OXYGEN SYSTEM PER AMM 35-20-00-946-01. SYSTEM TEST GOOD.
Part: CONTROL PANEL — MALFUNCTIONED (AILERON TRIM) · airframe 14,605 hrs · 12,772 cycles
AILERON TRIM STICKS AND WILL NOT TRIM TO THE RIGHT. (FLIGHT NR 6052) REPLACED AILERON/RUDDER TRIM CONTROL PANEL IAW AMM 27-12-10.
Part: OXYGEN MASK — UNWANTED DEPLOY (CABIN) · airframe 14,540 hrs · 12,718 cycles
FLT 6562 - ALL OXYGEN MASKS DROPPED IN CABIN WHILE STARTING APU. RESTOWED OXYGEN MASKS PER AMM 35-20-00.
Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 14,262 hrs · 12,483 cycles
RECEIVED A "SMOKE TOILET" CAUTION MESSAGE AFTER TAKE OFF. (FLIGHT #6647)INSPECTED AND OPERATED THE LEFT AND RIGHT ACM IAW AMM 21-51-13. NO DISCREPENCIES NOTED.
Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 13,999 hrs · 12,247 cycles
FLT 5987 - OVERHEAD EMERGENCY LIGHT IN CABIN IS OUT. RELAMPED EMERGENCY LIGHT IN CABIN IAW AMM 33-51-01.
Part: HEATER — INOPERATIVE (COCKPIT WINDOW) · airframe 13,494 hrs · 11,819 cycles
FLT 5929 - "L WINDOW HEAT" CAUTION MESSAGE IN FLIGHT. REPLACED CAPTAINS SIDE WINDOW IAW AMM 56-12-01, P/N OFF: NP-139322-9, S/N OFF: 04023H4007.
2007
Part: UNKNOWN — ODOR (CABIN) · airframe 12,330 hrs · 10,818 cycles
FLT 6593 - DURING DESCENT, DETECTED AN ELECTRIC BURNING ODOR. THE ODOR LASTED FOR 10 SECONDS WITH NO SMOKE SEEN. INSPECTED CABIN AND COCKPIT FOR BURN INDICATIONS. NO DISCREPANCIES NOTED. COULD NOT DUPLICATE.
Part: THRESHOLD — CRACKED (FUSELAGE) · airframe 12,724 hrs · 11,167 cycles
ANGLE BELOW CARGO DOOR THRESHOLD HAS EVIDENCE OF CRACKING, FOUND AT C-CHECK. REPLACED ANGLE BELOW CARGO DOOR THRESHOLD PER CRJ200 SRM 51-42-06 PAGE 18.
Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 12,724 hrs · 11,167 cycles
SERVICE DOOR THRESHOLD SHOWS SIGNS OF CORROSION, FOUND AT C-CHECK. REPLACED SERVICE DOOR THRESHOLD PER CRJ200 SRM 51-41-02 PG 1-7.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 12,724 hrs · 11,167 cycles
STA280 AT LBL9 UPPER BEAM IS CRACKED, FOUND AT C-CHECK. REPAIRED UPPER BEAM CRACK PER CRJ200 REO 601R-53-11-138.
Part: NUT CLIP — CRACKED (BS 280) · airframe 12,724 hrs · 11,167 cycles
STA 280 AT RBL 9 INBOARD AND OUTBOARD CLIPS ARE CRACKED, FOUND AT C-CHECK. REPLACED CLIPS AT STA 280 RBL9 PER CRJ200 SRM 51-42-21 PG 17.
Part: ADC — FAILED (NR 1) · airframe 11,156 hrs · 9,813 cycles
"EFIS COMP MON" CAUTION MESSAGE AND "IAS" FLAG ON BOTH DISPLAYS. DETERMINED ADC 1 FAILED. PURGED PITOT/STATIC SYSTEMS NR 1 AND NR 2 IAW AMM 34-11-00, AND REPLACED NR 1 ADC IAW AMM 34-13-01.
Part: UNKNOWN — ODOR (CABIN) · airframe 10,650 hrs · 9,375 cycles
FOUND OVERHEATING ODOR IN VICINITY OF ROW 9C-10C. RAN PACK AND COULD NOT DETECT ANY ODOR IN CABIN. OPERATIONAL CHECKS GOOD.
2006
Part: ANCHOR — CRACKED (PAX DOOR) · airframe 9,776 hrs · 8,646 cycles
PAX DOOR AFT COUNTER BALANCE ANCHOR IS CRACKED. REMOVED AND REPLACED PAX DOOR AFT COUNTER BALANCE ANCHOR FITTING IAW CRJ 200 MM 52-11-17. OPERATIONAL CHECKS GOOD.
Part: YOKE — MALFUNCTIONED (COCKPIT) · airframe 8,492 hrs · 7,484 cycles
CONTROL YOKE MAKES CLICKING NOISE WHEN ELEVATOR IS DEFLECTED UP AND DOWN. REPLACED BOLTS AND NUTS CONNECTING RIGHT CONTROL COLUMN TORQUE TUBE TO ELEVATOR DISCONNECT MECHANISM IAW AMM 27-32-01. OPERATIONAL CHECK GOOD.
2005
Part: LIGHT — INOPERATIVE (CABIN) · airframe 6,810 hrs · 5,982 cycles
2ND OVERHEAD CABIN EMERGENCY LIGHT INOP. REPLACED 2ND OVERHEAD CABIN EMERGENCY LIGHT. OPERATIONAL CHECK GOOD.
Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB TRIM) · airframe 6,591 hrs · 5,810 cycles
WHILE ON THE GROUND, "STAB CH 1 INOP" AND "MACH TRIM" MSG'S APPEARED. REMOVED AND REPLACED HSTCU. OPERATIONAL CHECK GOOD.
Part: TRIM SWITCH — STICKING (COCKPIT) · airframe 6,622 hrs · 5,842 cycles
FO'S STAB TRIM SWITCH STICKS. REPLACED F/O'S STAB DISCONNECT SWITCH PER MM 27-41-30.
Part: CONTROL UNIT — MALFUNCTIONED (MOTOR) · airframe 6,591 hrs · 5,810 cycles
STAB CHANNEL 1 WOULD NOT ENGAGE. REPLACED MCU IAW MM 27-42-05. OPERATIONAL CHECK GOOD.
Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB TRIM) · airframe 6,559 hrs · 5,772 cycles
BOTH STAB TRIM CHANNELS WON'T ENGAGE. REPLACED USING HSTCU. OPERATIONAL CHECK GOOD.
Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 6,374 hrs · 5,629 cycles
EMERGENCY OVERHEAD POD LIGHT INOP BY ROW 12. RELAMPED OVERHEAD EMERGENCY LIGHT. OPERATIONAL CHECK OK.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 6,135 hrs · 5,435 cycles
OVERHEAD AISLE LIGHT INOP, LOCATION FORWARD. RELAMPED OVERHEAD EMERGENCY LIGHT "FWD". OPERATIONAL CHECK GOOD.
Part: TRIM SWITCH — MALFUNCTIONED (ELEVATORS) · airframe 6,032 hrs · 5,347 cycles
F/O`S TRIM SWITCH STICKS (RIGHT SIDE OF SWITCH). REPLACED F/O`S ELEVATOR TRIM SWITCH ON F/O`S YOKE. OPERATIONAL CHECK GOOD PER MM 27-40-00.
2004
Part: MOTOR-BRAKE UNIT — MALFUNCTIONED (TE FLAPS) · airframe 4,886 hrs · 4,404 cycles
FLAPS HALFSPEED STATUS MESSAGE WHEN FLAPS SELECTED ON APPROACH. REMOVED AND REPLACED LEFT MOTOR/BRAKE ASSY IAW AMM TASK 27-52-05. OPERATIONAL CHECK GOOD.
Part: PCU — MALFUNCTIONED (SPOILERS) · airframe 4,040 hrs · 3,609 cycles
ON TAXI OUT, DURING FLIGHT CONTROL CHECK, SPOILERON FAULT MESSAGE ILLUMINATES. REPLACED RT SPOILERON IB PCU IAW MM 27-62-01. REPLACED SECU NR 1 AS IAW MM 27-61-05. OPERATIONAL CHECK GOOD.
Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 4,006 hrs · 3,583 cycles
MAIN CABIN DOOR ENTRYWAY EMERGENCY LIGHT LENS BROKEN. REMOVED AND REPLACED ENTRYWAY EMERGENCY FLOOR FLOODLIGHT FIXTURE, REF CHAP 33-51-19 CRJ AMM. OPERATIONAL CHECK GOOD.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 3,982 hrs · 3,557 cycles
RT SIDE EXTERNAL EMERGENCY LIGHT BURNED OUT. RELAMPED RT SIDE EXTERNAL EMERGENCY LIGHT. OPERATIONAL CHECK GOOD.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 3,848 hrs · 3,427 cycles
FS 280 RIGHT HAND FLOORBEAM RBL 9.0 O/B ATTACH ANGLE CRACKED. ITEM FOUND AT C-CHECK.
Part: CONTROL UNIT — MALFUNCTIONED (SPOILERS) · airframe 3,409 hrs · 3,068 cycles
RECEIVED O/B GROUND SPOILER FAULT AND FLT SPOILERS FAULT STATUS MSGS WHILE ON SHORT APPROACH TO SLC. REMOVED AND REPLACED NR 1 AND NR 2 SECU'S REF AMM 27-61-05. OPS CHECK GOOD. NR 2 SECU S/N OFF: 01715.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 3,112 hrs · 2,792 cycles
EMERGENCY EXIT TIP LIGHTS INOP ON OVERHEAD SIGN AT ROW 8. REMOVED AND REPLACED TIP LIGHTS ON OVERHEAD SIGN AT ROW 8 IN REF TO AMM 33-51-00. OPS CHECK GOOD AT THIS TIME.
Part: ACTUATOR — MALFUNCTIONED (HORIZONTAL STAB) · airframe 2,977 hrs · 2,662 cycles
STAB CHANNEL NR 2 CIRCUIT BREAKER 3A5 KEEPS TRIPPING. REMOVED AND REPLACED THE HORIZONTAL STAB TRIM ACTUATOR AND THE MOTOR CONTROL UNIT. OPS CHECK GOOD FOR CRJ MM 27-42-01 AND 27-42-05. MOTOR CONTROL UNIT P/N 7062-3, S/N OFF 1009.
Part: WINDOW — CRACKED (COCKPIT) · airframe 3,031 hrs · 2,714 cycles
LEFT WINDOW CRACKED AT 17,000 FT. INSTALLED SERVICEABLE LEFT WINDOW ASSEMBLY IAW CRJ MM 56-12-01 AND RII 56-402. NO LEAKS NOTED. P/N OFF: NP139322-001, S/N OFF: 02218H3041.
Part: BATTERY — DISCHARGED (CABIN) · airframe 2,814 hrs · 2,500 cycles
FORWARD OVERWING EMERGENCY EXIT SIGN INOP. INSTALLED SERVICEABLE BATTERY AND POWER SUPPLY. OPS CHECK GOOD.
Part: CHARGER — FAILED (CABIN) · airframe 2,814 hrs · 2,500 cycles
ROW 8 CEILING EXIT SIGN DOES NOT ILLUMINATE ON FORWARD SIDE. REPLACED AND SECURED BATTERY CHARGER ASSY AT SECTION 2 OF EMERGENCY BATTERY PACKS. OPS CHECK GOOD.
2003
Part: PUMP — MALFUNCTIONED (LT HYD SYSTEM) · airframe 292 hrs · 294 cycles
RECEIVED A HYDRAULIC NR 1 LOW PRESSURE CAUTION MESSAGE CLIMBING THROUGH 14,000 FT. TURNED ON HYDRAULIC 1B AS PER QRH, HYDRAULIC PRESSURE STILL SHOWED ZERO. RETURNED TO PHX. REMOVED AND REPLACED LT ENGINE HYDRAULIC PUMP IAW MM 29-11-01 AND LT HYD PUMP CASE DRAIN LINE. OPERATIONAL CHECKS AND LEAK CHECKS GOOD. NO DEFECTS OR LEAKS NOTED AT THIS TIME. S/N OFF: MX661187.
2002
Part: BLADE — BIRD STRIKE (LT ENGINE) · airframe 176 hrs · 177 cycles
AFTER TAKEOFF FROM SMF, THE LEFT NOSE SECTION WAS STRUCK BY BIRD. SHORTLY AFTER BIRD IMPACT, THE LEFT ENGINE FAILED DUE TO BIRD INGESTION. NO FIRE INDICATIONS. FOLLOWED QRH PROCEDURE. C/W BIRDSTRIKE INSPECTION CHECKLIST IAW ST12-413. NO DAMAGE TO RADOME. FOUND DAMAGE TO NR 1 ENGINE FAN BLADES. REMOVED DAMAGED FANS FROM LEFT ENGINE BLADES AND REPLACED WITH SERVICEABLE UNITS. DAMAGED BLADES ARE 1, 2, 3, 4, 5,14,15, 22, 25, 26, 27 & 28. REINSTALLED SPINNER AND NOSE CONE, ENGINE COWLINGS. BOROSCOPED FIRST, SECOND AND THIRD COMPRESSORS. NO DAMAGE FOUND IN COMPRESSOR SECTION. RAN ENGINE TO TAKEOFF POWER. ALL CHECKS GOOD. FAN BLADES CHECK IAW SEI-756 SP 50.