N812SK
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.
74 reports on file, 2007-09-10 – 2018-10-22.
Part: CONTROL UNIT — FAILED (FUEL SYSTEM) · airframe 31,633 hrs · 19,592 cycles
EN-ROUTE AFTER LEVEL OFF, RECEIVED CROSS FLOW PUMP CAUTION MSG PER QRH SHUT DOWN ENGINE NR 2. DECLARED EMERGENCY RETURNED TO FIELD IN SLC. (FLT 3708) CLOSED REMOVED AND REPLACED FQCU IAW AMM. ALSO REMOVED AND REPLACED BI-CROSS FLOW CARTRIDGE PUMP IAW AMM. OPS AND LEAK CHECK GOOD AT THIS TIME.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 30,872 hrs · 19,066 cycles
PITTING CORROSION ON STRINGER JOINT AT STR25L FS333. (C-CHECK) 07/06/2018 INSTALLED NEW STRINGER JOINT AT STR 25L, FS333 IAW SRM. PRESSURE CHECK GOOD.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 30,872 hrs · 19,066 cycles
STRINGER 26L BETWEEN FS280 AND FS310 HAS CORROSION. (C-CHECK) 07/06/2018 INSTALLED STRINGER 26L LOCATED BETWEEN FS280.00-FS333.00 IAW REO. PRESSURE CHECK GOOD.
Part: FRAME — CORRODED (FUSELAGE) · airframe 30,872 hrs · 19,066 cycles
FRAME AT FS349 BETWEEN STR 26L AND STR 26R HAS CORROSION. (C-CHECK) 07/06/2018 INSTALLED FRAME FS349 BETWEEN STR 23L AND STR 24R IAW SRM. PRESSURE CHECK GOOD.
Part: FRAME — CORRODED (FUSELAGE) · airframe 30,872 hrs · 19,066 cycles
FRAME AT FS364 BETWEEN STR 26L AND STR 26R HAS CORROSION. (C-CHECK) 07/06/2018 INSTALLED FRAME SECTOR LOCATED AT FS364.00 BETWEEN STR 24L & STR 24R IAW REO. PRESSURE CHECK GOOD.
Part: LONGERON — CORRODED (FUSELAGE) · airframe 30,872 hrs · 19,066 cycles
LT LONGERON BETWEEN FS333 AND FS349, STR 25L HAS CORROSION. (C-CHECK) 07/06/2018 INSTALLED NEW SERVICEABLE LT LONGERON COMMON TO STR 25L BETWEEN FS333 AND FS364 IAW SRM. PRESSURE CHECK GOOD.
Part: FRAME — CORRODED (FUSELAGE) · airframe 30,872 hrs · 19,066 cycles
FRAME AT FS333 BETWEEN STR 27 AND STR 26R HAS CORROSION. (C-CHECK) 07/06/2018 REPLACED FRAME SECTOR AT FS333.00 BETWEEN STR 25R TO STR 25L IAW REO. PRESSURE CHECK GOOD.
Earlier reports · 2007–2017 · 67 reports
2017
Part: WIRE HARNESS — FAILED (PROXIMITY SENSOR) · airframe 29,155 hrs · 17,981 cycles
RETURNED TO THE FIELD DUE TO A GEAR DISAGREE. GEAR DID NOT RETRACT. REMOVED AND REPLACED THE PROXIMITY SENSOR HARNESS IAW AMM. OPS CHECKED GOOD.
2016
Part: FRAME — CORRODED (BS 349) · airframe 24,913 hrs · 15,333 cycles
BS 349 LOWER FUSELAGE FRAME SECTOR IS CORRODED. R & R THE FRAME SECTION IAW SRM.
Part: DOUBLER — CORRODED (BS 297-308) · airframe 24,913 hrs · 15,333 cycles
AVIONICS BAY,TCAS ANTENNA DOUBLER FS 297 - 308, STRINGER 27, CORRODED. R & R TCAS ANTENNA DOUBLER IAW SRM. PRESSURE CHECK OF THE TCAS ANTENNA DOUBLER GOOD IAW AMM.
Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 24,913 hrs · 15,333 cycles
INTERCOSTAL CORRODED IN AVIONICS BAY BS 364 - 349, LBL 2. R & R INTERCOSTAL IAW SRM. R
Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 24,913 hrs · 15,333 cycles
INTERCOSTAL CORRODED IN AVIONICS BAY FS 364 - FS 349, RBL2. R & R INTERCOSTAL ON FS 364-FS 349, RBL 2 IAW SRM. R & R RT GUSSET FS 364 IAW SRM. REMOVED AND INSTALLED CLEAT ON FS 349 STR 26R IAW SRM. PRESSURE LEAK CHECK OF THE REPAIR AREA GOOD IAW AMM.
Part: INTERCOSTAL — CORRODED (BS 897-913) · airframe 24,913 hrs · 15,333 cycles
INTERNAL FUSELAGE, INTERCOSTAL CORRODED FS 897 - 913, STRINGER 21R. REPLACED THE INTERCOSTAL IAW EA AND SRM.
Part: FRAME — CORRODED (BS 333) · airframe 24,913 hrs · 15,333 cycles
AVIONICS BAY, FRAME FS 333 CORRODED STR 26L-STR 26R. REPAIRED IAW EA. PRESSURE CHECKED GOOD.
Part: PANEL — CHAFED (LT WING) · airframe 24,913 hrs · 15,333 cycles
PANEL 584EB CHAFED. REPLACED OUT OF LIMITS PANEL 584EB IAW SRM.
Part: PANEL — CHAFED (LT WING TE FLAP) · airframe 24,913 hrs · 15,333 cycles
PANEL 584ET AT INBD END OF LT FLAP VANE IS CHAFED. R & R PANEL IAW SRM.
2015
Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 23,652 hrs · 14,549 cycles
LT AND RT PACK FAULT STATUS MESSAGE DURING CLIMBOUT, CABIN WOULD NOT MAINTAIN PRESSURIZATION. RECEIVED A CABIN ALTITUDE CAUTION MESSAGE AND CABIN WARNING. PERFORMED TEST OF THE ASCS AND R & R NR 1 ASCS IAW AMM, OPS CHECKED GOOD.
2014
Part: LUG — CORRODED (NLG) · airframe 19,983 hrs · 12,106 cycles
CORROSION FOUND ON INNER DIAMETER OF BOTH NLG LOWER PISTON-AXLE TORQUE LINK LUGS. C-CHECK, REPAIRED IAW REO.
Part: FRAME — CORRODED (BS 295) · airframe 19,983 hrs · 12,106 cycles
FUSELAGE FRAME AT BS 295 AT LOWER SKIN PANEL IS CORRODED. C-CHECK, PERFORMED REPAIR ON FRAME IAW REO.
Part: ANGLE — CORRODED (THRESHOLD) · airframe 19,983 hrs · 12,106 cycles
PAX DOOR LOWER THRESHOLD AFT ANGLE CORRODED VISUALLY OUT OF LIMITS. C-CHECK, REPLACED ANGLE IAW SRM.
Part: ANGLE — CORRODED (THRESHOLD) · airframe 19,983 hrs · 12,106 cycles
PAX DOOR LOWER THRESHOLD FWD ANGLE CORRODED OUT OF LIMITS. C-CHECK, REPLACED ANGLE IAW SRM.
Part: THRESHOLD — CORRODED (BS 1000-1047) · airframe 19,983 hrs · 12,106 cycles
CORROSION FOUND AT AT AFT CARGO THESHOLD BS 1000 - 1047. C-CHECK, REMOVED CORROSION IAW REO.
Part: FLOOR SUPPORT — CORRODED (BS 1000-1051) · airframe 19,983 hrs · 12,106 cycles
AFT CARGO RT SIDE FLOOR SUPPORT HAS CORROSION AT VARIOUS NUT PLATES BENEATH STAINLESS STEEL FLASHING FROM BS 1000 - 1051. REMOVED CORROSION IAW REO.
Part: ANGLE — CORRODED (THRESHOLD) · airframe 19,983 hrs · 12,106 cycles
PAX DOOR LOWER THRESHOLD MID ANGLE CORRODED OUT OF LIMITS. C-CHECK, REPLACED ANGLE IAW SRM.
Part: PAN — CRACKED · airframe 19,983 hrs · 12,106 cycles
FWD EQUIPMENT BAY, RT SIDE JUST AFT OF ADG HANDPUMP FLOOR PAN IS CRACKED. C-CHECK, REPAIRED IAW REO.
Part: SLIDER — CORRODED (LT NACELLE) · airframe 19,983 hrs · 12,106 cycles
LEFT ENGINE UPPER TRANSCOWL INBD SLIDER CHAFED AT FWD END. C-CHECK, BLENDED DAMAGE AND RESTORED FINISH IAW REO.
Part: PANEL — CRACKED (UNKNOWN) · airframe 19,983 hrs · 12,106 cycles
PANEL 222QZ IS CRACKED. C-CHECK, REPAIRED PANEL IAW EA.
Part: HOUSING — CHAFED (DOOR HANDLE) · airframe 19,983 hrs · 12,106 cycles
AFT CARGO DOOR CHAFED IN OUTER HANDLE HOUSING. C-CHECK, BLENDED OUT DAMAGE IAW REO.
Part: ARM — CHAFED (CARGO DOOR) · airframe 19,983 hrs · 12,106 cycles
CENTER CARGO DOOR AFT COUNTER-BALANCE ARM CHAFED ON AFT SIDE. C-CHECK, REMOVED DAMAGE IAW REO.
Part: SKIN — DENTED (BS 310-349) · airframe 19,771 hrs · 11,954 cycles
DENT MEASURING 24 INCHES? IN LENGTH RUNNING DIAGONALLY BETWEEN BS 310 AND 349, STRINGERS 21-22R. REPAIRED SKIN IAW REO.
2013
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 19,437 hrs · 11,748 cycles
EMERGENCY OVERHEAD LIGHT AT ROW 6 IS BURNED OUT. REPLACED LAMP.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 18,482 hrs · 11,165 cycles
BACKLIGHT FOR PASS SIGNS IS BURNED OUT. FLT#4812 RELAMPED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,088 hrs · 10,898 cycles
EMERGENCY FLOOR FLOOD LIGHT HAS BULBS BURNED OUT. FLT#4558 RELAMPED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,346 hrs · 10,410 cycles
OVERHEAD EMERGENCY LIGHT NR 3 DOES NOT ILLUMINATE. (FLT 4695) RELAMPED EMERGENCY LIGHT.
Part: LENS — CRACKED (EXTERIOR) · airframe 17,291 hrs · 10,372 cycles
LEFT FUSELAGE EXTERIOR AFT EMERGENCY LIGHT LENS CRACKED. (SERVICE) INSTALLED AN EMERGENCY LIGHT LENS ON THE LEFT FUSELAGE EXTERIOR AFT.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 17,224 hrs · 10,316 cycles
NUMEROUS EMERGENCY LIGHTS DO NOT ILLUMINATE. (FLT 4489) REPLACED MIDDLE EMERGENCY LIGHT BATTERY PACK. P/N AD-2013-1A S/N ON 60185 S/N OFF 69440
Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,065 hrs · 10,200 cycles
LAST EMERGENCY OVERHEAD LIGHT IS BURNED OUT. (FLT 4799) RELAMPED EMERGENCY LIGHT.
2012
Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,718 hrs · 10,001 cycles
NR 6 EMERGENCY OVERHEAD LIGHT BURNED OUT. (FLT 4803) RELAMPED EMERGENCY LIGHT.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 16,292 hrs · 9,690 cycles
THE 280 FLOORBEAM CRACKED ON BOTH SIDES. (C-CHECK) REPLACED FS 280 FLOORBEAM IN REFERENCE TO REO.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,168 hrs · 9,603 cycles
EXIT LIGHT BULBS ARE OUT. (FLT 4780) RELAMPED EXIT LIGHT.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 15,680 hrs · 9,292 cycles
EMERGENCY EXIT SIGN AT ROW 12 IS OUT. (FLT 4596) RELAMPED EMERGENCY EXIT SIGN.
Part: BATTERY — DISCHARGED (CABIN) · airframe 15,623 hrs · 9,250 cycles
ROW 12 OVERHEAD AND SIDEWALL EMERGENCY EXIT LIGHTS ARE OUT. (FLT 4611) REPLACED NR 3 EMERGENCY BATTERY IN REFERENCE TO AMM. P/N: AD-2013-1A S/N OFF: 67883.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,371 hrs · 9,093 cycles
NR 6 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4600) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,352 hrs · 9,081 cycles
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4785) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,296 hrs · 9,043 cycles
NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4809) RELAMPED EMERGENCY LIGHT.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 15,169 hrs · 8,961 cycles
FLT 4720, AFT OVERHEAD EMERGENCY LIGHT IS OUT. RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,969 hrs · 8,818 cycles
NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4467) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,848 hrs · 8,745 cycles
NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4464) RELAMPED EMERGENCY LIGHT.
Part: COMPUTER — FAILED (AUTOPILOT SYS) · airframe 14,494 hrs · 8,511 cycles
AT FL370, THE AUTO PILOT PITCHED DOWN INTO AN 1100 FPM DESCENT AND THEN RECAPTURED FL370. (FLT 4681) REPLACED NR 1 & 2 FCC COMPUTERS. P/N: 822-1308-027 S/N OFF: 28HPX P/N: 822-1308-027 S/N OFF: 28HHX
2011
Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,306 hrs · 8,387 cycles
NR 1 EMERGENCY LIGHT OUT. (FLT 4690) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,262 hrs · 8,350 cycles
NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4727) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,743 hrs · 8,000 cycles
OVERHEAD EMERGENCY LIGHT AT ROW 8 IS OUT. (FLT 4646) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,580 hrs · 7,890 cycles
NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,443 hrs · 7,796 cycles
OVERHEAD EMERGENCY LIGHT AT ROW 8 IS OUT. (FLT 4671) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,314 hrs · 7,717 cycles
NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4701) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,264 hrs · 7,682 cycles
AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4558) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,200 hrs · 7,646 cycles
NR 4 CEILING EMERGENCY LIGHT IS INOPERATIVE. (FLT 4785) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,162 hrs · 7,614 cycles
AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4616) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,715 hrs · 7,321 cycles
AFT CEILING EMERGENCY LIGHT IS OUT. (FLT 4567) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,204 hrs · 7,034 cycles
NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4632) RELAMPED EMERGENCY LIGHT.
Part: LONGERON — CRACKED (FUSELAGE) · airframe 11,743 hrs · 6,772 cycles
FS 274 RBL 12.0 LONGERON WEB IS CRACKED. (C-CHECK) REPAIR PER REO.
Part: LONGERON — CRACKED (FUSELAGE) · airframe 12,168 hrs · 7,006 cycles
WEB OF THE LONGERON AT FS 274 IS CRACKED. (C-CHECK) REPAIRED PER REO.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 12,168 hrs · 7,006 cycles
FS 280 FLOORBEAM IS CORRODED. (C-CHECK) REPLACED FS 280 FLOORBEAM.
2010
Part: DOOR — MALFUNCTIONED (CABIN) · airframe 9,722 hrs · 5,554 cycles
MAIN CABIN DOOR HARD TO OPEN. (FLT 4484) OPERATION CHECKS NORMAL.
2009
Part: LINK — CORRODED (ENGINE MOUNT) · airframe 7,583 hrs · 4,381 cycles
LEFT FORWARD ENGINE MOUNT LINK BUSHINGS AND SPHERICAL BEARING CORRODED. (SVC CHECK) REPLACED LEFT FORWARD ENGINE MOUNT LINK.
Part: RELAY — DEFECTIVE (CABIN) · airframe 7,309 hrs · 4,241 cycles
EMERGENCY LIGHT STATUS MESSAGE DISPLAYED WITH SYSTEM CONFIGURED CORRECTLY. (FLT 4474) REPLACED K135 RELAY.
Part: FUSE — BLOWN (CABIN) · airframe 7,309 hrs · 4,241 cycles
CEILING EMERGENCY EXIT SIGN ROW 12 INOP. (FLT 1010) REPLACED FUSES ON EPSU NR 3 AND EPSU NR 5.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,300 hrs · 4,237 cycles
CABIN EMERGENCY LIGHT INOP IN AFT CABIN. (FLT 4646) RELAMPED EMERGENCY LIGHT.
Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 6,425 hrs · 3,726 cycles
FLT 4615 - 2ND EMERGENCY LIGHT FROM AFT INOP. RELAMPED.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 6,019 hrs · 3,459 cycles
FLT 4688 - SKIN DENTED, IS INSIDE RVSM CRITICAL AREA. REPAIRED PER REO.
2008
Part: OXYGEN MASK — UNWANTED DEPLOY (FLT ATTENDENT) · airframe 3,818 hrs · 2,188 cycles
AFT FLIGHT ATTENDANT O2 MASK DEPLOYED ON LANDING. INSPECTED AND REINSTALLED O2 MASK.
Part: SIGN — LOOSE (EMERGENCY LIGHTS) · airframe 3,726 hrs · 2,145 cycles
FLT 1994 - EXIT SIGN ABOVE GALLEY SERVICE DOOR IS INOP. RESECURED EXIT SIGN. OPS CHECKS GOOD.
2007
Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 2,684 hrs · 1,595 cycles
FLT 4000 - OVERHEAD EMERGENCY LIGHT AT ROW 13 IS INOP. REPLACED NR 3 EMERGENCY LIGHT BATTERY AS NEEDED PER CRJ MM 33-50-00. OPS CHECK GOOD.
Part: CONTROL PANEL — FAULTY (CABIN PRESSURE) · airframe 1,985 hrs · 1,193 cycles
"ALT LIMITER" CAUTION MESSAGE, FOLLOWED BY DEPLOYING OF OXYGEN MASKS IN CABIN. REMOVED AND REPLACED CABIN PRESSURE CONTROL PANEL REF CRJ 900 MM 21-31-04. RESTOWED ALL CABIN OXYGEN MASKS. OPS CHECK OF CPCP GOOD. NO FURTHER DEFECTS NOTED, PN: GG670-98001-11, SN ON: 00488 SN OFF: 80606.