N248LR
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.
80 reports on file, 2013-05-16 – 2026-07-20.
Part: WINDSHIELD — CRACKED (ZONE 200) · airframe 24,868 hrs · 19,098 cycles
CAPT WINDSHIELD CRACK INFLIGHT. WINDOW STARTED ARCHING FROM THE CAPT SIDE UPPER WINDOW HEATER. THE AIRCRAFT WAS EXPERIENCING ELMOÃâ¬â¢S FIRE DUE TO STORMS IN THE AREA AT THE SAME TIME. THE CREW USED A FLASHLIGHT AND OBSERVED A CRACK FROM TOP CENTER TO ALMOST THE BOTTOM. THE AREA AROUND THE UPPER HEATER IS ALSO CRACKED.QRH PROCEDURES WERE FOLLOWED INCLUDING A LOWER ALTITUDE AND MANUAL PRESSURE CHANGE. AIRCRAFT LANDED AT THE DESTINATION AIRPORT WITH NO FURTHER PROBLEMS. (FLIGHT 5009) OPEN
Earlier reports · 2013–2025 · 79 reports
2025
Part: STRINGER — CORRODED (ZONE 100) · 17,975 cycles
CORROSION FOUND UNDER BRACKET ON STR 20R, 6 INCHES AFT OF FS280. REMOVED AND REPLACED DAMAGED STR SECTION FROM FS 280 TO FS 300 STR 20R.PEFORMED ANGLE SPLICE REPAIR AT FS 300 STR 20 IN REF TO CRJ 900 SRM 53-00-03-201-001-A01 FIG. 53-00-03--95-806 SOLUTION 1.COMPLIED WITH TASK CARD 51-900-1002-SKY. LEAK CHECKED GOOD.WEIGHT STATEMENT: 1 FOR 1 REPLACEMENT OF DISCREPANT ITEMS.. NO WEIGHT CHANGE.
Part: STRINGER — CORRODED (ZONE 100) · 17,975 cycles
DUCT CLAMP BRACKET ON STR22R NEER FS280 HAS CORROSION. INSTALLED NEW STGR 22R & BRACKET @ FWD BETWEEN FS. 280 TO FS. 333.0 IAW CRJ900 SRM 51-42-06-001-001-A01 NO WEIGHT CHANGE, ITEMS REMOVED, REPLACED WITH NEW SAME ITEMS.STRUCTRAL REPAIR TASK CARD 51-900-1002-SKY COMPLIED WITH. LEAK CHECKED GOOD. REFER TO CONTINUATION SHEET FOR WORK PERFORMED.
Part: SKIN — CORRODED (ZONE 100) · 17,975 cycles
MULTIPLE SPOTS OF COROSION ON INTERNAL SKIN BETWEEN FS280 AND FS295 FROM STR24R TO 25L. REPAIRED CORRODED AREAS ON INTERNAL SKIN BTW BS 280 AND BS 295 FROM STRINGERS 24R TO 25L IAW REO 690-53-21-2000, REV--, AND REO 690-53-21-2001, REV--.
Part: STRINGER — CORRODED (ZONE 100) · 17,975 cycles
STRINGER 21R LOCATED 5.5" FWD FS 349.0 HAS CORROSION. REMOVED AND REPLACED NEW STGR 21R @ FWD BETWEEN FS. 333 TO FS. 349.0 IAW CRJ900 SRM 51-42-06-001-001-A01NO WEIGHT CHANGE, ITEMS REMOVED, REPLACED WITH NEW SAME ITEMS.STRUCTRAL REPAIR TASK CARD 51-900-1002-SKY COMPLIED WITH. LEAK CHECKED GOOD. REFER TO CONTINUATION SHEET FOR WORK PERFORMED.
Part: STRINGER — CORRODED (ZONE 100) · 17,975 cycles
STRINGER 22R LOCATED 5.5" FWD FS 349.0 HAS CORROSION. REMOVED AND REPLACED NEW STGR 22R , BRACKET, & JOINT SPLICE, AT FWD BETWEEN BS 280 TO 349 IAW SRM 51-42-06-001-001-A01. ITEMS REMOVED, REPLACED WITH NEW COMPLIED WITH STRUCTRAL REPAIR TASK CARD 51-900-1002-SKY.
Part: STRINGER — CORRODED (ZONE 100) · 17,975 cycles
STRINGER 21R LOCATED 7" FWD FS 333.0 HAS CORROSION. REMOVED AND REPLACED NEW STGR 21R @ FWD BETWEEN FS. 280 TO FS. 333.0 IAW CRJ900 SRM 51-42-06-001-001-A01WEIGHT CHANGE: NO WEIGHT CHANGE NOTED, SAME ITEMS REPLACED AS REMOVED.COMPLIED WITH TASK CARD 51-900-1002-SKY
Part: FLOORBEAM — GOUGED (ZONE 200) · 17,975 cycles
DEEP GOUGE ON FLOORBEAM AT F.S 677, WL 72 RT SIDE. BLENDED AND EVALUATED DEEP GOUGE ON FLOOR BEAM AT RH SIDE FS 677.00 WL 72.00 AND FOUND WITHIN LIMITS IAW REO 690-53-31-1029. REV. -.
Part: ROLLER — WORN (ZONE 600) · 17,975 cycles
RIGHT SLAT TRACK 3-2 FWD IB, AFT IB, AND AFT OB SIDE ROLLERS WORN OUT OF LIMITS. REMOVED AND REPLACED RH SLAT TRACK 3-2 FWD IB, AFT IB, AND AFT OB SIDE ROLLERS PER CRJ 900 AMM 27-81-44-000-803 CONF A01 AND AMM 27-81-44-400-803 CONF A01.
Part: ROLLER — WORN (ZONE 600) · 17,975 cycles
RH SLAT TRACK 2-2 AFT IB SIDE ROLLER WORN OUT OF LIMITS (C-CHECK RO 11/06/2025)REMOVED AND REPLACED RH SLAT TRACK 2-2 AFT IB SIDE ROLLER PER CRJ 900 AMM 27-81-44-400-802 (CONFIG A01)
Part: SLAT TRACK — WORN (ZONE 500) · 17,975 cycles
LEFT SLAT TRACK 2-2 FWD IB SIDE ROLLER WORN OUT OF LIMITS. REMOVED AND REPLACED LH SLAT TRACK 2-2 FWD IB SIDE ROLLER PER CRJ900 AMM 27-81-44-000-802-A01
Part: SLAT TRACK — WORN (ZONE 500) · 17,975 cycles
LEFT SLAT TRACK 3-2 FWD OB SIDE ROLLER WORN OUT OF LIMITS. REMOVED AND REPLACED LH SLAT TRACK 3-2 FWD OB SIDE ROLLER PER CRJ900 AMM 27-81-44-400-803-A01
2023
Part: FRAME — DAMAGED (FS280) · airframe 23,398 hrs · 17,974 cycles
INCIDENT WHERE THE NOSE POINT JACK PUNCTURED THE SKIN ADJACENT TO THE JACK POINT. DAMAGE IS JUST FORWARD OF FS280 AT OR NEAR BL?? 3-8R EXTENDING FORWARD APPROXIMATELY 10-12 INCHES. PERMANENT REPAIR ACCOMPLISHED IAW RO# CRJ9-53-5309.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 23,365 hrs · 17,984 cycles
R PAX DR FLR LVL EXIT SIGN (1) BULB INOP- RELAMPED
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 23,365 hrs · 17,948 cycles
PAX DR FLR LVL EXIT SIGN (1) BULB INOP- RELAMPED
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 23,116 hrs · 17,741 cycles
GALLEY FWD MID EXIT SIGN 1 BULB INOP- RELAMPED
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 22,611 hrs · 17,363 cycles
EMERGENCY LIGHTS INOP- REPLACED EMERGENCY LIGHT BATTERIES
Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 22,248 hrs · 17,068 cycles
SVC DR FLR LVL EMER FLOOD LT (2) BULBS INOP RELAMPED, OPS CHECK GOOD
2022
Part: NONE — NONE · airframe 21,079 hrs · 16,181 cycles
LH BLEED DUCT WARNING IN FLIGHT. MX IS CURRENTLY TROUBLE SHOOTING.
Part: NONE — NONE · airframe 20,806 hrs · 15,973 cycles
FWD SVC DOOR LWR EXIT LIGHT 4 BULBS OUT. RELAMP.
Part: NONE — NONE · airframe 20,470 hrs · 15,728 cycles
FWD LAV EMER EXIT SIGN INOP. CHARGED EMER BATTS WITH GPU. OPS CHECK GOOD.
Part: NONE — NONE · airframe 20,470 hrs · 15,728 cycles
RH EMER DOOR EXIT SIGN INOP. CHARGED EMER BATTS WITH GPU. OPS CHECK GOOD.
Part: NONE — NONE · airframe 20,470 hrs · 15,728 cycles
RH OVERWING EMER EXIT SIGN INOP. CHARGED EMER BATTS WITH GPU. OPS CHECK GOOD.
Part: NONE — NONE · airframe 20,470 hrs · 15,728 cycles
LH EMER DOOR EXIT SIGN INOP. CHARGED EMER BATTS WITH GPU. OPS CHECK GOOD.
Part: NONE — NONE · airframe 20,470 hrs · 15,728 cycles
LH OVERWING EMER EXIT SIGN INOP. CHARGED EMER BATTS WITH GPU. OPS CHECK GOOD.
Part: NONE — NONE · airframe 20,470 hrs · 15,728 cycles
MAIN CABIN DOOR EMER EXIT SIGN INOP. CHARGED EMER BATTS WITH GPU. OPS CHECK GOOD.
Part: NONE — NONE · airframe 20,470 hrs · 15,728 cycles
ROW 3 RH EMER EXIT SIGN INOP. CHARGED EMER BATTS WITH GPU. OPS CHECK GOOD.
Part: NONE — NONE · airframe 20,470 hrs · 15,728 cycles
ROW 12 CEILING EMER EXIT SIGN INOP. CHARGED EMER BATTS WITH GPU. OPS CHECK GOOD.
Part: NONE — NONE · airframe 20,470 hrs · 15,728 cycles
ROW 13 RH EMER EXIT SIGN INOP. CHARGED EMER BATTS WITH GPU. OPS CHECK GOOD.
Part: BULB — INOPERATIVE (ZONE 200) · airframe 20,255 hrs · 15,583 cycles
R1 DOOR FLOOR EMER LIGHT INOP LIGHT OPS NORMAL
2021
Part: FRAME — CORRODED (BS 319 S26L/R) · airframe 19,571 hrs · 15,109 cycles
FRAME CORRODED FS319 - STGR 26L- 26R. REMOVED AMO REPLACED FRAME IAW SRM 53-00-06.
Part: FRAME — CORRODED (BS 310 S27L) · airframe 19,571 hrs · 15,109 cycles
MAIN AVI COMPARTMENT CORRODED AT FS310 - STGR 27. REMOVED AND REPLACED FRAME FS310 BETWEEN STGR 27L IAW SRM 53-00-06
Part: FLOORBEAM — CRACKED (BS 280) · airframe 19,571 hrs · 15,109 cycles
COMPLY WITH SB 670BA-53-041 PART B ONLY 280 BEAM SB. THE BEAM WAS FOUND TO BE CRACKED, WHICH IS THE ORIGINAL REASON FOR THIS. DUE TO EFFECTIVITY VIA THE SERIAL NUMBER, THE SB WAS ALREADY COMPLIED WITH. HOWEVER, THE BEAM WAS REPLACED FROM THE SRM ON A SEPARATE RO.
Part: STRINGER — CORRODED (FS280-295 S27R) · airframe 19,571 hrs · 15,106 cycles
STRINGER CORROSION AT FS295 BETWEEN STGR 27. R+R STRINGER FS280-295 BETWEEN STGR27R IAW SRM 51-42-06.
Part: FLOORBEAM — CORRODED (BS 280 LBL 14) · airframe 19,571 hrs · 15,109 cycles
CRACK AT FS280 CROSS BEAM LBL 14 |R&R UH 280 CROSS BEAM AT LBL 14
Part: WEB — CORRODED (FS280) · airframe 19,571 hrs · 15,109 cycles
LH COCKPIT WEB AT FS280 LBL 12 CORRODED |REMOVED AMO REPLACED FABRICATED WEB IAW SRM 51-42-06
Part: FLOORBEAM — CORRODED (BS 280) · airframe 19,571 hrs · 15,109 cycles
MAIN FORWARD CABIN RH FLOOR SILL CORRODED AT FS280 R&R RH FLOOR SILL IAW SRM 51-42-06
Part: CROSSBEAM — CRACKED (BS 280) · airframe 19,571 hrs · 15,109 cycles
CRACK AT FS280 CROSSBEAM GUSSET AT RBL 9 |RR CROSSBEAM IAW SRM 51-42-06
Part: CROSSBEAM — CRACKED (FS280) · airframe 19,571 hrs · 15,109 cycles
CRACK AT FS280 CROSSBEAM GUSSETT AT LBL 9 |RR CROSSBEAM IAW SRM 51-42-06
Part: SEAT TRACK — CORRODED (BS 661-677) · airframe 19,571 hrs · 15,109 cycles
SEAT TRACK FS661+32 TO FS677 RBL9 CORRODED. REMOVE CORRODED SEAT TRACK, INSTALL FABRICATED SEAT TRACK IAW SRM 53-00-49
Part: CROSSBEAM — CRACKED (BS 280) · airframe 19,571 hrs · 15,109 cycles
CRACK AT FS280 CROSSBEAM GUSSET AT RBL 14| RR CROSSBEAM IAW SRM 51-42-06
Part: FRAME — CORRODED (BS 349 S26R-26L) · airframe 19,571 hrs · 15,109 cycles
CORROSION AT FS349 STGR 26R-26L IN FWD E&E BAY |R&R FRAME SECTOR IAW SRM 51-42-06
Part: INTERCOSTAL — CORRODED (BS 349-364 S27L) · airframe 19,571 hrs · 15,109 cycles
INTERCOSTAL CORRODED AT FS349 TO FS364 LH SIDE STGR 27L R&R INTERCOSTAL IAW SRM 51-42-06
Part: STRINGER — CORRODED (BS 280-333 S26R) · airframe 19,571 hrs · 15,109 cycles
STRINGER 26R CORRODED FS280-FS333 IN FWD E&E BAY |R&R STRINGER IAW SRM 51-42-06
Part: FRAME — CORRODED (BS 319 S25L-25R) · airframe 19,571 hrs · 15,109 cycles
CORROSION AT FS319 STGR 25L-25R IN FWD E&E BAY. R&R FRAME SECTOR AND FRAME SPLICE IAW SRM 51-42-06
Part: INTERCOSTAL — CORRODED (BS 349-364 S26R) · airframe 19,571 hrs · 15,109 cycles
NTERCOSTAL CORRODED AT FS349 TO FS364 RH SIDE STGR 26R R&R INTERCOSTAL IAW SRM 51-42-06
Part: INTERCOSTAL — CORRODED (BS 349-364 S27R) · airframe 19,571 hrs · 15,109 cycles
INTERCOSTAL CORRODED AT FS349 TO FS364 RH SIDE STGR 27R R&R INTERCOSTAL IAW SRM 51-42-06
Part: STRINGER — CORRODED (BS 280-333) · airframe 19,571 hrs · 15,109 cycles
STRINGER CORRODED FS280-FS333 IN FWD E&E BAY |R&R STRINGER IAW SRM 51-42-06
Part: DOUBLER — CORRODED (BS 295-310) · airframe 19,571 hrs · 15,109 cycles
TCAS ANTENNA DOUBLER CORRODED. R&R TCAS ANTENNA DOUBLER IAW 51-42-06
Part: FRAME SPLICE — CORRODED (BS 333 S26R) · airframe 19,571 hrs · 15,109 cycles
CORROSION AT FS333 STGR 26R SPLICE IN FWD E&E BAY | R&R FRAME SPLICE IAW SRM 51-42-06
Part: FRAME — CORRODED (FS295) · airframe 19,571 hrs · 15,106 cycles
CORROSION AT FS295 BETWEEN STGR 26L AND 26R |R+R FRAME FS295 BETWEEN STGR25R AND STGR 25L IAW SRM 51-42-06
2020
Part: SIGN — INOPERATIVE (R2 DOOR) · airframe 19,535 hrs · 15,083 cycles
PAX DOOR EMERG EXIT SIGN SALIDA INOP R2 SIGN.
2019
Part: CENTERING CAM — OUT OF ADJUST (NLG) · airframe 18,130 hrs · 14,077 cycles
GEAR DISAGREE W/N RETRACT RE-RIGGED NOSE WHEEL STEERING CENTERING CAM
Part: NOT REPORTED — MALFUNCTIONED (LANDING GEAR) · airframe 16,338 hrs · 12,707 cycles
GEAR DISAGREE W/N RETRACT. PLACED ON MEL.
2018
Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 15,446 hrs · 12,039 cycles
FWD FA FLASHLIGHT INOP. PLACED ON MEL
2017
Part: OXYGEN BOTTLE — INOPERATIVE (CABIN) · airframe 11,810 hrs · 9,205 cycles
AFT PORTABLE O2 BOTTLE VALVE W/N OPEN DURING MEDICAL EMERGENCY. REPLACED BOTTLE.
Part: FLOORBEAM — CORRODED (BS 349) · corrosion level 2 · airframe 11,622 hrs · 9,058 cycles
CORROSION FOUND ON RT FLOORBEAM AT BS 349 JUST AFT OF SERVICE DOOR LOWER CORNER. REPAIRED THE AREA.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 11,622 hrs · 9,058 cycles
DURING REPLACEMENT OF THE FS 280.00 TRANSVERSE FLOORBEAM, THE COCKPIT FLOORBEAM AT RBL 12, WAS FOUND TO BE CRACKED. REPAIR WAS MADE IAW REO 670-53-11-896, REV-, DATED 2015-03-17.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 11,622 hrs · 9,058 cycles
DURING THE REPLACEMENT OF THE FS 280.00 TRANSVERSE FLOORBEAM, THE COCKPIT FLOORBEAM AT LBL 12, WAS FOUND TO BE CRACKED. REPAIR WAS MADE IAW BOMBARDIER REO 670-53-11-896, REV-, DATED 2015-03-17.
Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 11,622 hrs · 9 cycles
LT FS 280 CROSSBEAM IS CRACKED AT LBL12.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 11,622 hrs · 9,058 cycles
FLOORBEAM ANGLE IS CORRODED.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 11,622 hrs · 9,058 cycles
RIGHT SIDE FLOOR SUPPORT IS CORRODED FROM BS 280 TO SERVICE DOOR.
Part: STRINGER SPLICE — CORRODED (BS 333) · airframe 11,622 hrs · 9,058 cycles
STRINGER SPLICE 26R IS CORRODED AT BS 333.
Part: FLOORBEAM — CORRODED (BS 280) · corrosion level 2 · airframe 11,622 hrs · 9,058 cycles
BS 280 FLOORBEAM J CHANNEL IS CORRODED AROUND FLOORBOARD FASTNER HOLES.
Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,622 hrs · 90,558 cycles
LOWER FLOORBOARD SUPPORT ANGLE AT PAX DOOR CUTOUT IS CORRODED.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 11,622 hrs · 9,058 cycles
BS 280 FLOORBEAM IS CRACKED AT LBL 12.
2016
Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 10,580 hrs · 8,266 cycles
AFT FA FLASHLIGHT INOPERATIVE. REPLACED THE BATTERY. OPS GOOD
Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 10,544 hrs · 8,239 cycles
AFT FLASHLIGHT INOPERATIVE. REPLACED BATTERY
Part: FLASHLIGHT ASSY — INOPERATIVE (FWD CABIN) · airframe 10,348 hrs · 8,094 cycles
FWD FA FLASHLIGHT NOT BLINKING.
Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 9,450 hrs · 7,424 cycles
FWD F/A FLASHLIGHT INOPERATIVE. REPLACED BATTERIES. OPS GOOD.
2015
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 8,402 hrs · 5,697 cycles
FWD SERVICE DOOR EMERGENCY EXIT SIGN BULBS BURNED OUT. REPLACED BULB.
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 8,402 hrs · 5,697 cycles
MAIN CABIN DOOR EMERGENCY EXIT LIGHT BULB BURNED OUT. REPLACED BULB.
Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 8,138 hrs · 6,389 cycles
FWD F/A FLASHLIGHT INOPERATIVE.
Part: FLASHLIGHT — INOPERATIVE (ZONE 200) · airframe 7,853 hrs · 6,159 cycles
AFT F/A FLASHLIGHT INOPERATIVE.
Part: WARNING MESSAGE — ILLUMINATED (LT ENGINE) · airframe 6,832 hrs · 5,343 cycles
LEFT ENGINE FADEC, CAUTION RTF.
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 6,824 hrs · 5,335 cycles
GALLEY EXIT SIGN TWO BULBS INOPERATIVE.
Part: A/C PACK — SMOKE (LEFT) · airframe 6,706 hrs · 5,228 cycles
AT GATE, COCKPIT & CABIN FILLED WITH SMOKE, LT PACK.
2014
Part: TAB — GOUGED (HORIZONTAL STAB) · airframe 3,954 hrs · 3,114 cycles
FOUND GOUGE DAMAGE TO RT ANTI-ROTATION TAB WHILE PERFORMING LUBRICATION ON TASK 73510 LUBRICATION HORIZONTAL STAB HINGE FITTING & 71142 LUBRICATION OF HORIZONTAL STAB HINGE FITTING COMPLETED TEMPORARY REPAIR IAW CRJ-55-4021, REO 690-55-11-005 & 690-55-11-006, PERMANENT REPAIR IS DUE WITHIN 6000 FLIGHT HOURS.
Part: TAB — GOUGED (HORIZONTAL STAB) · airframe 3,954 hrs · 3,114 cycles
FOUND A GOUGE ON THE RT ANTI-ROTATION TAB. COMPLETED TEMPORARY REPAIR IAW CRJ-55-4021, REO 690-55-11-005 & 690-55-11-006.
2013
Part: UNKNOWN — UNKNOWN (EMERGENCY LIGHTS) · airframe 1,950 hrs · 1,410 cycles
EVERY OTHER EMERGENCY FLOOD LIGHT INOPERATIVE. LIGHTS OPS NORMAL