N938SW
Registered owner: SKYWEST AIRLINES INC, UT (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| SKYWEST AIRLINES, INC. (SWIA) | Operator | on 2010-10-18 | Operator named in NTSB report |
Accident & incident history
Operated by SkyWest Airlines (per NTSB report)
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.
128 reports on file, 2004-03-12 – 2019-11-12.
Part: LANDING GEAR — LEAKING (NOSE) · airframe 43,204 hrs · 36,671 cycles
GEAR DISAGREE ON CLIMB OUT. NOSE GEAR WOULDNÃâ¬â¢T COME UP. COMPLIED WITH QRH AND RECEIVED 3 GREEN DOWN LOCKED INDICATION. LANDED NORMALLY. FLIGHT 5240 CLOSEDTHIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 19884985 WITH THE FOLLOWING CORRECTIVE ACTION: "FOUND NLG STRUT WOULD NOT RETAIN HYDRAULIC FLUID. REMOVED AND REPLACED NLG DRESSED ASSY. IAW AMM. OPS CHECK GOOD WITH NO LEAKS NOTED.
Part: WARNING MESSAGE — FALSE ACTIVATION (MLG) · airframe 43,082 hrs · 36,558 cycles
AFTER GEAR RETRACTION ON DEPARTURE FROM DEN, NOSE GEAR DID NOT RETRACT (MAIN GEAR RETRACTED NORMALLY) & GOT GEAR DISAGREE WARNING MESSAGE. FLIGHT # 5975 CLOSED. COMPLIED WITH FIM FOR GEAR DISAGREE WARNING MESSAGE. PERFORMED GEAR SWINGS AND EMERGENCY EXTENSION AS REQUIRED WITH NO DISCREPANCIES NOTED. NO TEN DAY HISTORY NOTED FOR A GEAR DISAGREE. AIRCRAFT OKAY FOR CONTINUED SERVICE.
Earlier reports · 2004–2018 · 126 reports
2018
Part: ANGLE — CORRODED (CABIN) · airframe 39,722 hrs · 33,611 cycles
FOUND CORROSION BETWEEN THE RIGHT SIDE WINDSCREEN FLOOR SUPPORT FITTING AND THE BS 349 FLOORBEAM. REMOVED AND REPLACED THE ANGLE IAW SRM.
Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 39,722 hrs · 33,611 cycles
FOUND CORROSION BETWEEN THE LEFT SIDE WINDSCREEN FLOOR SUPPORT FITTING AND BS 349 FLOORBEAM. REMOVED AND REPLACED THE FLOOR SUPPORT ANGLE IAW SRM.
Part: ANGLE — CORRODED (BS 718) · airframe 39,722 hrs · 33,611 cycles
CORROSION FOUND ON THE ANGLE AROUND THE AFT EQUIPMENT DOOR CUT OUT, BS 718. REMOVED THE CORROSION FROM THE AFT ANGLE IAW SRM AND REO.
Part: SPAR — CHAFED (RT PYLON) · airframe 39,722 hrs · 33,611 cycles
RIGHT PYLON, A SMALL CHAFE WAS FOUND ON THE LOWER FORWARD SIDE OF THE PYLON SPAR. BLENDED THE CHAFE IAW SRM.
2016
Part: DOWNLOCK SENSOR — FAILED (NR 2) · airframe 35,676 hrs · 29,911 cycles
GEAR DISAGREE WARNING. REPLACED THE NR 2 DOWNLOCK SENSOR.
Part: SKIN — CORRODED (FUSELAGE) · airframe 35,115 hrs · 29,398 cycles
FRETTING CORROSION NEAR MOUNT HOLES UNDER ADF ANTENNA. COMPLIED WITH STS EA PRESSURE LEAK CHECK GOOD.
Part: BULKHEAD — GOUGED (BS 621) · airframe 35,115 hrs · 29,398 cycles
BS 621, BULKHEAD 30" ABOVE FLOOR AT RBL36.20 GOUGED & NICKED. REPAIRED THE BULKHEAD IAW REO. PRESSURIZATION CHECKED GOOD.
Part: BULKHEAD — GOUGED (BS 621) · airframe 35,115 hrs · 29,398 cycles
BS 621, BULKHEAD 30" ABOVE FLOOR AT RBL 27.50 GOUGED & NICKED. REPAIRED THE BULKHEAD IAW REO. PRESSURIZATION CHECKED GOOD.
Part: BULKHEAD — GOUGED (BS 621) · airframe 35,115 hrs · 29,398 cycles
FS 621, BULKHEAD 30" ABOVE FLOOR AT RBL 18.00 DUE TO GOUGED & NICKED. REPAIRED THE BULKHEAD IAW REO. COMPLIED WITH PRESSURIZATION CHECKED GOOD.
Part: VANE — CHAFED (RT WING TE FLAP) · airframe 35,115 hrs · 29,398 cycles
RT INBD FLAP VANE CHAFED ON OTBD SIDE L/E. R & R WITH NEW FABRICATED VANE CAP, PN 601R14303-44 IAW SRM.
Part: VANE — CHAFED (LT WING TE FLAP) · airframe 35,115 hrs · 29,398 cycles
LT INBD FLAP VANE CHAFED ON CENTER SIDE L/E. REMOVED CHAFED VANE CAP AND INSTALLED NEW VANE CAP IAW SRM AND STS EA.
2015
Part: DRAG BRACE — UNKNOWN (NLG) · airframe 32,740 hrs · 27,263 cycles
SELECTED GEAR DOWN AND THE NOSE GEAR STAYED RED WITH NO AURAL MESSAGES, AFTER GO AROUND, SELECTED GEAR; GEAR SLOW TO GO GREEN AND NO GEAR DISAGREE MESSAGE. R & R NLG DRAG BRACE IAW AMM. PERFORMED OPS CHECK OF THE NLG EXTENSION AND RETRACTION SYSTEM IAW AMM, AND POWER UP CHECK OF THE PSS IAW AMM. OPS CHECK GOOD AT THIS TIME, NO FURTHER DEFECTS NOTED AT THIS TIME. ACFT OK FOR SERVICE.
2014
Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 30,616 hrs · 25,493 cycles
CABIN EMERGENCY LIGHTS FOUND IN THE ON POSITION DURING PRE-FLIGHT. FOUND BATTERIES DEAD. CHARGED EMERGENCY LIGHT BATTERIES AND PERFORMED OPS CHECK OF EMERGENCY LIGHTS IAW AMM.
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,473 hrs · 25,358 cycles
EMERGENCY LIGHTS INOPERATIVE, SWITCH ON LT SIDE EXTERIOR FORWARD OVERWING EXIT BULB INOPERATIVE AND INTERIOR CEILING PANEL FORWARD EMERGENCY EXIT SIGN INOPERATIVE. C-CHECK, R & R BATTERY ASSY IAW AMM.
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,473 hrs · 25,358 cycles
SERVICE DOOR EXIT LIGHT HAS ONE BULB INOPERATIVE. C-CHECK, REPLACED SERVICE DOOR EXIT BULB.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,473 hrs · 25,358 cycles
CENTER EXIT LIGHT, AFT, INOPERATIVE. C-CHECK, PERFORMED ADJUSTMENT TEST ON THE CENTER EXIT LIGHT, AFT IAW AMM.
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,473 hrs · 25,358 cycles
SIX BULBS INOPERATIVE IN CENTER CEILING FORWARD EMERGENCY EXIT. C-CHECK, INSTALLED BULBS IN FWD CENTER CEILING EMERGENCY EXIT LIGHT.
Part: LIGHT — CRACKED · airframe 30,473 hrs · 25,358 cycles
PAX DOOR PULL IN LEVER EMERGENCY EXIT BETAS LIGHT IS CRACKED. C-CHECK, R & R EMERGENCY EXIT BETA LIGHT, IAW SRM.
Part: STRUCTURE — CRACKED (TAILCONE) · airframe 30,473 hrs · 25,358 cycles
TAIL CONE HAS A CRACK ON LT SIDE, 11 O'CLOCK, AT APPROXIMATE BS 830. C-CHECK, REPAIRED DAMAGE IAW REO.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 30,473 hrs · 25,358 cycles
FS 280 FLOORBEAM, AFT ANGLE CRACKED AT RBL 9 AND LBL 9. C-CHECK, AFT FLOORBEAM ANGLE REPLACED IAW SRM.
Part: POST — CRACKED (BS 409) · airframe 30,473 hrs · 25,358 cycles
LT VERTICAL POST AT FS 409.0+128, BL 0 IS CRACKED. C-CHECK, LOCATED AND DRILLED NEW LT VERTICAL POST AT FS 409.0-128 BL 0 AND INSTALLED IAW SRM.
Part: STIFFENER — CRACKED (BS 409) · airframe 30,473 hrs · 25,358 cycles
VERT POST AT FS 409.0+128, BL 0 HAS CRACKS ON RT SIDE. C-CHECK, RO: REPLACED VERTICAL POST FS 409+128 BL0 IAW SRM.
Part: SKIN — DAMAGED (PAX DOOR) · airframe 30,473 hrs · 25,358 cycles
PAX DOOR INNER SKIN CORRODED AND HAS MULTIPLE CRACKS. C-CHECK, REMOVED AND INSTALLED NEW PAX DOOR INNER SKIN IAW SRM.
Part: EXHAUST DUCT — CRACKED (RT) · airframe 30,473 hrs · 25,358 cycles
CRACK NOTED BY NDT IN UPPER FWD STIFFENER OF THE RT EXHAUST NOZZLE FAIRING. REPLACE STIFFENER. C-CHECK, R & R RT EXHAUST NOZZLE FAIRING UPPER FWD STIFFENER AND RESTORED FINISH IAW SRM.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 30,473 hrs · 25,358 cycles
INBD AND OTBD FLOORBEAM ANGLE AT FS 280, RBL 9 CRACKED. C-CHECK, FABRICATED INBD AND OTBD FLOORBEAM ANGLE IAW REO AND SRM.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 30,473 hrs · 25,358 cycles
FLOORBEAM FS 280, CRACKED AT LBL9 AND RBL9. C-CHECK, REPLACED WITH NEW IAW SRM.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 30,473 hrs · 25,358 cycles
INBD AND OTBD FLOORBEAM ANGLES AT BS 280, LBL 9 CRACKED. C-CHECK, R & R INBD AND OTBD FLOORBEAM ANGLES IAW REO AND SRM.
Part: VANE — CHAFED (LT WING TE FLAP) · airframe 30,473 hrs · 25,358 cycles
LEFT FLAP VANE CHAFED TO METAL ON CENTER. C-CHECK, BLENDED CHAFE ON LT FLAP VANE CENTER IAW SRM AND REO.
Part: VANE — CHAFED (LT WING TE FLAP) · airframe 30,473 hrs · 25,358 cycles
LT FLAP VANE CHAFED TO METAL ON INBD SIDE. C-CHECK, BLENDED CHAFE ON LT FLAP VANE IB SIDE IAW SRM AND REO.
Part: ANGLE — CRACKED (BS 625) · airframe 30,473 hrs · 25,358 cycles
LEFT EQUIPMENT BAY BS 625, ANGLE AT APPROXIMATELY STRINGER 14 IS CRACKED. C-CHECK, R & R ANGLE IAW SRM.
Part: DOOR — CRACKED (NLG) · airframe 30,473 hrs · 25,358 cycles
AFT NOSE GEAR DOOR RT LOWER CORNER CRACKED. C-CHECK, REPAIRED AFT NOSE GEAR DOOR RT LOWER CORNER IAW EA.
Part: VANE — CHAFED (LT WING TE FLAP) · airframe 30,473 hrs · 25,358 cycles
LEFT FLAP VANE CHAFED TO METAL ON OTBD SIDE. C-CHECK, BLENDED CHAFE ON LT FLAP VANE OTBD SIDE IAW REO AND SRM.
Part: VANE — CHAFED (RT WING TE FLAP) · airframe 30,473 hrs · 25,358 cycles
RIGHT FLAP VANE CHAFED TO METAL ON OTBD SIDE. C-CHECK, BLENDED CHAFE ON RT FLAP VANE INBD SIDE IAW SRM AND REO.
Part: FAIRING — CHAFED (RT WING TE FLAP) · airframe 30,473 hrs · 25,358 cycles
RT FLAP FAIRING METAL CHAFED ON INBD SIDE OF VANE. C-CHECK, BLENDED RT FLAP FAIRING CHAFE ON INBD SIDE OF VANE IAW SRM AND REO.
Part: VANE — CHAFED (RT WING TE FLAP) · airframe 30,473 hrs · 25,358 cycles
RIGHT FLAP VANE CHAFED TO METAL ON CENTER. C-CHECK, BLENDED RT FLAP VANE CHAFE ON CENTER IAW SRM AND REO.
Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 30,140 hrs · 25,093 cycles
CEILING EXIT SIGN LENS BY ROW 8 IS BROKEN. REPLACED BROKEN LENS IAW AMM.
2013
Part: WIRE — INOPERATIVE (CABIN) · airframe 28,262 hrs · 23,665 cycles
NR 1 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. FLT#5584 RELAMPED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,262 hrs · 23,665 cycles
RT WING AFT EMERGENCY EXIT LIGHT IS BURNED OUT. FLT#6367 RELAMPED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,233 hrs · 23,639 cycles
NR 3 OVERHEAD EMERGENCY LIGHT IS BURNED OUT. FLT#6337 RELAMPED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,416 hrs · 23,032 cycles
ONE EMERGENCY LIGHT BULB IS BURNED OUT AT MAIN CABIN DOOR ENTRY. (FLT 6208) RELAMPED EMERGENCY LIGHT.
Part: SIGN — INOPERATIVE (CABIN) · airframe 27,382 hrs · 23,006 cycles
CENTER CEILING AFT EMERGENCY EXIT SIGN DOES NOT ILLUMINATE. (FLT 5436) REPLACED CENTER CEILING AFT EMERGENCY EXIT SIGN.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,730 hrs · 22,506 cycles
GALLEY SERVICE AREA EMERGENCY LIGHT HAS ONE LIGHT OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,730 hrs · 22,506 cycles
NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5624) RELAMPED EMERGENCY LIGHT.
2012
Part: INVERTER — FAILED (CABIN) · airframe 26,459 hrs · 22,291 cycles
EMERGENCY FLOOR LIGHT STRIPS NR 2, 3, 4 AND 5 INOPERATIVE AND FLOOR LEVEL EMERGENCY EXIT ROW EXIT LIGHT INOP WHEN EMERGENCY LIGHT SWITCH ON. (FLT 6493) REPLACED NR 2 INVERTER, NR 2 BATTERY CHARGER AND BATTERY PACK IAW AMM PN AD-2013-1A S/N ON 72485 S/N OFF 50480.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,340 hrs · 22,203 cycles
NR 2 EMERGENCY OVERHEAD LIGHT BURNED OUT. (FLT 6430) RELAMPED EMERGENCY LIGHT.
Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 26,123 hrs · 22,024 cycles
MAIN AVIONIC COMPARTMENT CUTOUT HAS CORROSION WHERE DOOR SEAL MEETS AIRFRAME. (C-CHECK) REPAIRED AVIONIC COMPARTMENT CUTOUT AS PER REO.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 26,123 hrs · 22,024 cycles
CRACK ON FS 621 BULKHEAD WEB, FORWARD FACE, ABOVE UPPER CARGO DOOR TRACK FITTING AT LBL 27.5. (C-CHECK) REPAIRED CRACK ON FS 621.0 BULKHEAD WEB AT TOP OF AFT CARGO DOOR TRACK IN REFERENCE TO REO.
Part: CONNECTOR — DIRTY (CABIN) · airframe 26,074 hrs · 21,980 cycles
FLOOR EMERGENCY EXIT LIGHT AT ROW 2, 3, 4, AND 5 ARE OUT. (FLT 6514) CLEANED CONNECTOR FOR CONTACTS ON NR 1 BATTERY PACK CHARGER ASSEMBLY IN REFERENCE TO CRJ MM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 26,038 hrs · 21,948 cycles
LOWER EXIT LIGHT AT SEAT 8A IS INOPERATIVE. (FLT 5515) REPLACED NR 3 ELBP P/N: AD-2013-1A S/N OFF: 69303.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,918 hrs · 21,858 cycles
NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5389) RELAMPED EMERGENCY LIGHT.
Part: WIRE — OUT OF ADJUST (CABIN) · airframe 25,918 hrs · 21,858 cycles
EMERGENCY FLOOR LIGHTING, OVERHEAD LIGHTING, AND SIDEWALL LIGHTING IS INTERMITTENT. (FLT 5512) ADJUSTED WIRES FOR AFT FLOOR EMERGENCY LIGHTING.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,959 hrs · 21,147 cycles
NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5556) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,520 hrs · 20,775 cycles
NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5539) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,191 hrs · 20,515 cycles
OVERHEAD FORWARD EMERGENCY LIGHT IS OUT. (FLT 5246) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,177 hrs · 20,502 cycles
NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5249) RELAMPED EMERGENCY LIGHT.
2011
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,984 hrs · 20,356 cycles
NR 3 CEILING EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.
Part: CONNECTOR — UNSECURE (CABIN) · airframe 23,943 hrs · 20,328 cycles
GALLEY EMERGENCY LIGHTS ARE OUT. (FLT 5561) RESECURED LOOSE GALLEY EMERGENCY LIGHT CONNECTOR.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,537 hrs · 19,994 cycles
AFT CEILING EMERGENCY LIGHT IS BURNED OUT. (FLT 6477) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,483 hrs · 19,945 cycles
NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6301) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,360 hrs · 19,853 cycles
NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5306) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,297 hrs · 19,799 cycles
NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5518) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,297 hrs · 19,799 cycles
AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5372) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,237 hrs · 19,740 cycles
NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5490) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,237 hrs · 19,740 cycles
NR 3 LEFT EXTERIOR EMERGENCY LIGHT IS OUT. (FLT 5483)RELAMPED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,063 hrs · 19,590 cycles
FORWARD OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,943 hrs · 19,501 cycles
NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5496) RELAMPED EMERGENCY LIGHT.
Part: BELLCRANK — OUT OF ADJUST (CABIN DOOR) · airframe 22,675 hrs · 19,305 cycles
MAIN CABIN DOOR DIFFICULT TO OPEN. (FLT 5652) ADJUSTED MAIN CABIN DOOR UPPER AND LOWER BELLCRANK.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,675 hrs · 19,305 cycles
NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5652) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,675 hrs · 19,305 cycles
NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.
Part: STRUCTURE — CRACKED (CABIN DOOR) · airframe 22,643 hrs · 19,281 cycles
MAIN CABIN DOOR IS DIFFICULT TO OPEN. (FLT 5256) REPLACED PAX DOOR FLAPPER DOOR BELLCRANK MOUNTING STRUCTURE.
Part: CAM — LACK OF LUBE (CABIN DOOR) · airframe 22,595 hrs · 19,241 cycles
MAIN CABIN DOOR DIFFICULT TO OPEN. (FLT 6231) LUBED CABIN DOOR CENTERING CAM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,525 hrs · 19,187 cycles
NR 2 AND NR 4 CEILING OVERHEAD EMERGENCY LIGHTS ARE OUT. (SERVICE) RELAMPED EMERGENCY LIGHTS.
Part: SKIN — DAMAGED (AILERON) · airframe 22,180 hrs · 18,928 cycles
LEFT AILERON, LOWER OUTBOARD LEADING EDGE SKIN IS DAMAGED. (C-CHECK) REPLACED LEFT AILERON LOWER OUTBOARD LEADING EDGE SKIN PER SRM.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 22,180 hrs · 18,928 cycles
FS 559.0 PRESSURE BULKHEAD CRACKED AT LEFT AND RIGHT SIDES. (C-CHECK) REPAIR PER REO.
Part: CAM — LACK OF LUBE (PAX DOOR) · airframe 22,125 hrs · 18,882 cycles
MAIN CABIN DOOR HARD TO OPEN. (FLT 6615) LUBED PAX DOOR CENTERING CAM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,464 hrs · 18,375 cycles
AFT EMERGENCY FLOOD LIGHT IN CABIN INOPERATIVE. (FLT 6850) RELAMPED EMERGENCY LIGHT.
2010
Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,283 hrs · 18,211 cycles
CABIN EMERGENCY LIGHT CEILING LEVEL IS OUT. (FLT 6726) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,241 hrs · 18,171 cycles
AFT CEILING EMERGENCY LIGHT INOPERATIVE. (FLT 6707) RELAMPED EMERGENCY LIGHT.
Part: PIN — SCORED (ENGINE MOUNT) · airframe 20,871 hrs · 17,864 cycles
RIGHT ENGINE FORWARD MOUNT PIN SCORED. (ENGINE CHANGE) REPLACED RIGHT ENGINE FORWARD MOUNT PIN.
Part: CABLE — BINDING (CABIN DOOR) · airframe 20,835 hrs · 17,834 cycles
MAIN CABIN DOOR DIFFICULT TO OPEN. (FLT 6522) REPLACED POWER ASSIST CABLE.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 20,052 hrs · 17,167 cycles
FORWARD PRESSURE BULKHEAD IS CRACKED AT PARKING BRAKE CONTROL ACTUATION ROD. (A CHECK) INSTALLED DOUBLER PER REO.
Part: DOOR — BINDING (PAX DOOR) · airframe 19,603 hrs · 16,798 cycles
PASSENGER DOOR VERY DIFFICULT TO OPEN. (FLT 5873) REPOSITIONED AIRCRAFT ON RAMP, OPERATIONAL CHECK NORMAL.
Part: INVERTER — INOPERATIVE (CABIN) · airframe 19,554 hrs · 16,764 cycles
EMERGENCY LIGHTS IN FRONT OF RIGHT OVERWING EXIT INOP. (FLT 6595)REPLACED INVERTER.
Part: CABLE — DIRTY (CABIN DOOR) · airframe 19,311 hrs · 16,563 cycles
MAIN CABIN DOOR WILL NOT OPEN. (FLT 6551) REMOVED DIRT FROM DOOR CABLE.
2009
Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,479 hrs · 15,868 cycles
NR 2 OVERHEAD EMERGENCY LIGHT INOP. (FLT 4606) RELAMPED EMERGENCY LIGHT.
Part: LENS — MISSING (CABIN) · airframe 17,250 hrs · 14,851 cycles
RED LIGHT LENS COVER ON OVERHEAD EMERGENCY LIGHT PANEL MISSING. (FLT 6005) REPLACED LENS.
Part: FITTING — CRACKED (FUSELAGE) · airframe 17,337 hrs · 14,912 cycles
AFT PRESSURE BULKHEAD CLIPS CRACKED. (C CHECK) REPLACED PER SRM.
Part: SUPPORT BEAM — CRACKED (FUSELAGE) · airframe 17,337 hrs · 14,912 cycles
FORWARD TRACK SUPPORT BEAM FOR CARGO DOOR TRACK CRACKED. (C CHECK) REPLACED PER SRM.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 17,337 hrs · 14,912 cycles
LEFT SIDE FS 484 INTERCOSTAL CRACKED. (C CHECK) REPAIRED PER REO.
Part: WEB — CRACKED (AIRSTAIR) · airframe 17,337 hrs · 14,912 cycles
FORWARD WEB OF AIRSTAIR CRACKED. (C CHECK) REPAIRED PER REO.
Part: FRAME — CRACKED (FUSELAGE) · airframe 17,337 hrs · 14,912 cycles
FS 605 FRAME CRACKED. (C CHECK) REPAIRED PER REO.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 17,094 hrs · 14,728 cycles
FLT 6562 - MAIN CABIN DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 17,075 hrs · 14,714 cycles
FLT 6686 - NR 2 EMERGENCY OVERHEAD FLOOD LIGHT INOP. RELAMPED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,948 hrs · 14,613 cycles
REAR EMERGENCY LIGHT INOP. (FLT 6553) RELAMPED EMERGENCY LIGHT.
Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 16,235 hrs · 14,060 cycles
FLT 6161 - MAIN CABIN DOOR FLOOR LEVEL EXIT LIGHT HAS ONE BULB INOP. RELAMPED.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 15,986 hrs · 13,876 cycles
FLT 6020 - NR 1 EMERGENCY LIGHT ON OVERHEAD INOP. RELAMPED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,846 hrs · 13,772 cycles
FLT 6070 NR 2 CEILING EMERGENCY LIGHT INOP. RELAMPED.
2008
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 15,578 hrs · 13,551 cycles
FLT 6445 - RIGHT SIDE FORWARD EMERGENCY LIGHT INOP. RELAMPED.
Part: WINDOW — CRACKED (COCKPIT) · airframe 15,442 hrs · 13,441 cycles
FLT 5836 - CAPTAIN'S SIDE WINDOW CRACKED. REPLACED WINDOW.
Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 15,263 hrs · 13,289 cycles
FLT 6014 - OVERHEAD EXIT SIGN IN CABIN MISSING RED/LENS COVER. REPLACED RED/LENS COVER.
Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 13,028 hrs · 11,390 cycles
OVERWING EMERGENCY EXIT SIGN DOES NOT ILLUMINATE, FLIGHT NR 6369. INSPECTED AND SECURED CONNECTOR ON ELBP 2 CHARGER IAW CRJ 200 MM 33-51-05.
2007
Part: FLOORBEAM — CRACKED (BS 280) · airframe 13,082 hrs · 11,432 cycles
LBL 9 AT FS 280 SHOWS SIGNS OF CRACKING, FOUND AT C-CHECK. COMPLIED WITH REPAIR OF CRACKED ANGLE AT FS 280 AND LBL 9 FLOORBEAM IAW CRJ200 REO 601R-53-11-138 REV NC.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 13,082 hrs · 11,432 cycles
LBL9 AT FS 280 IS CRACKED AT LOWER RADIUS, FOUND AT C-CHECK. COMPLIED WITH FLOORBEAM REPAIR IAW CRJ200 REO 601R-53-11-171 REV C.
Part: STRUCTURE — CRACKED (TE FLAPS) · airframe 13,082 hrs · 11,432 cycles
LEFT OUTBOARD FLAP IS CRACKED ALONG TRAILING EDGE, FOUND AT C-CHECK. REPLACED FLAP ASSEMBLY PER CRJ200 AMM 27-54-05-400-801.
Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 12,121 hrs · 10,634 cycles
FLT 6445 - EMERGENCY LIGHTING ALONG FLOOR STRIP IS INOP. REPLACED NR 2 EMERGENCY LIGHT INVERTER IAW 33-51-07. OPS CHECK GOOD.
Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 12,121 hrs · 10,634 cycles
FLT 5967 - THE EMERGENCY FLOOR LIGHTING BETWEEN ROWS 2 AND 5 DOES NOT WORK. ALSO, THE EMERGENCY EXIT SIGN BELOW THE LEFT WING EMERGENCY EXIT DOES NOT WORK. SECURED PLUG AT LIGHT STRIP. OPS CHECK GOOD FOR ALL LIGHTS IAW AMM 33-25-00.
Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 11,674 hrs · 10,266 cycles
FORWARD PORTION OF PAX DOOR IS CRACKED UNDERNEATH TOP STEP. REPAIRED CRACK IAW AMM REO 601R-52-11-279.
Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 11,674 hrs · 10,266 cycles
AFT PORTION OF PAX DOOR IS CRACKED UNDERNEATH TOP STEP. REPAIRED CRACK IAW REO 601R-52-11-279.
2006
Part: WINDOW — CRACKED (COCKPIT) · airframe 9,164 hrs · 8,082 cycles
ON DESCENT THROUGH 8000' FIRST OFFICER'S SIDE WINDOW CRACKED. REPLACED FIRST OFFICER'S SIDE WINDOW IAW 56-12-01 AND RII 56-220-1000. OPERATIONAL CHECKS GOOD, SN OFF: 02196H1120.
Part: B-NUT — LOOSE (SHUTOFF VALVE) · airframe 8,898 hrs · 7,843 cycles
FUEL ODOR IN COCKPIT DURING APU USEAGE. SECURED LOOSE (B) NUT ON APU FUEL SHUTOFF VALVE. OPERATIONAL CHECKS GOOD.
Part: FITTING — CRACKED (FUSELAGE) · airframe 8,766 hrs · 7,728 cycles
MAIN FWD AVIONICS COMPARTMENT FS 280 LBL9 FRAME CLIP CRACKED INBD, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP PN 601R31113-57 PO#58390 IAW CRJ200 REO 601R-53-11-136.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 8,766 hrs · 7,728 cycles
CRACK IN FLOOR SUPPORT FS 621 WL73.5 RBL44, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REO 601R 53-117-4. REPAIR ANGLE AND REO 601R 53-61-117-6 STRAP IAW REO 601R 53-61-117 REV 'C'.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 8,766 hrs · 7,728 cycles
CRACK IN FLOOR SUPPORT FS 621 WL73.5 LBL44, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PIECES IAW CRJ200 REO 601R-53-61-117 REV 'C'.
Part: FITTING — CRACKED (FUSELAGE) · airframe 8,766 hrs · 7,728 cycles
MAIN FWD AVIONICS COMPARTMENT FS 280.00 RBL9 FRAME CLIP CRACKED INBD AND OTBD, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED (2 EA) PN 601R31113-58 CLIPS AT FS 280 RBL9 INBD AND OTBD PER CRJ200 SRM 51-42-21 AND BOMBARDIER REO 601R-53-11-136.
Part: ANGLE — CRACKED (PAX DOOR) · airframe 8,766 hrs · 7,728 cycles
PAX DOOR; AFT DRAG ANGLE CRACKED BELOW POWER ASSIST MOTOR, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED MADE REPAIR PARTS ON PAX DOOR AFT DRAG ANGLE IAW AREO 601R 52-11-513 REV 'A'. A.INFANTI 03-26-06.
2005
Part: CONTROL UNIT — MALFUNCTIONED (STAB TRIM) · airframe 6,447 hrs · 5,688 cycles
STAB CHANNEL ONE WILL NOT ENGAGE. REPLACED MOTOR CONTROL UNIT IAW MM27-42-05. OPERATIONAL CHECK GOOD.
Part: SWITCH — MALFUNCTIONED (F/O TRIM) · airframe 5,401 hrs · 4,847 cycles
F/O'S TRIM SWITCH IS STICKY. REPLACED F/O'S TRIM SWITCH IAW MM 27-41-05. OPERATIONAL CHECK GOOD.
Part: CONTROL PANEL — MALFUNCTIONED (RUDDER TRIM) · airframe 5,077 hrs · 4,561 cycles
ON CLIMB, RIGHT RUDDER TRIM WAS USED MOMENTARILY, FOLLOWED BY UNCOMMANDED FULL RIGHT RUDDER TRIM ACTIVATION, AIRCRAFT WAS RETURNED TO TRIMMED CONDITION EASILY OPPOSITE RUDDER AND CORRECTED ALL TOGETHER WITH TRIM SWITCH. NORMAL FOR REMAINDER OF FLIGHT. REPLACED AILERON/RUDDER TRIM PANEL IN REFERENCE TO CRJ 200 MM ATA CHPT 27-00-00. OPERATIONAL CHECK GOOD.
2004
Part: WINDOW — FAILED (COCKPIT) · airframe 4,103 hrs · 3,745 cycles
LEFT SIDE WINDOW SHATTERED. REMOVED AND REPLACED LEFT SIDE WINDOW REF MM 56-12-01. P/N OFF 601R33033-11, S/N OFF 02201H1672.
Part: POSITION SENSOR — MALFUNCTIONED (BRAKE) · airframe 4,060 hrs · 3,712 cycles
FLAP FAIL MESSAGE ON TAXI OUT AT 13 DEGREES. REMOVED AND REPLACED RIGHT BPSU PER CRJ MM 27-51-10. REMOVED AND REPLACED NR 2 INBOARD FLAP ACTUATOR AND NR 1 RIGHT INBOARD FLAP ACTUATOR IAW CRJ MM 27-53-01. OPERATIONAL CHECK GOOD. NR 1 P/N 852D100-19, S/N OFF 4483. NR 2 P/N 852D100-19, S/N OFF 4487.
Part: CONTROL UNIT — MALFUNCTIONED (TE FLAP) · airframe 4,036 hrs · 3,694 cycles
FLAPS FAIL MESSAGE APPEARED WHEN FLAPS SELECTED TO 45 DEGREES. REMOVED AND REPLACED FECU IAW CRJ MM 27-51-05. OPERATIONAL CHECK GOOD.
Part: ANGLE — CRACKED (APU BAY) · airframe 3,720 hrs · 3,418 cycles
APU COMPARTMENT FS 625.00 STR 14L HAS A CRACKED ATTACH ANGLE. ITEM FOUND AT C-CHECK INSPECTION. REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-25-16.
Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 3,720 hrs · 3,418 cycles
FUSELAGE FLOORBEAM TO TRANSVERSE BEAM ATTACH CLIP IS CRACKED FS 280.00 LBL 9.0 O/B CLIP. ITEM FOUND AT C-CHECK INSPECTION. CLIP REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-01, 51-42-13, 51-21-11, 51-25-16.
Part: ANGLE — CRACKED (APU BAY) · airframe 3,720 hrs · 3,418 cycles
APU COMPARTMENT FS 625.00 STR 14R HAS A CRACKED ATTACH ANGLE. ITEM FOUND AT C-CHECK INSPECTION. REPLACED IAW CRJ SRM 51-40-11, 51-42-06 AND 51-25-16.
Part: BEAM — CRACKED (FUSELAGE) · airframe 3,720 hrs · 3,418 cycles
FUSELAGE TRANSVERSE BEAM LOWER FLANGE IS CRACKED; FS 280.00 RBL 12.0. ITEM FOUND AT C-CHECK INSPECTION. LOWER FLANGE REPAIRED IAW CRJ REO #601R-53-11-171 REV A.
Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 2,680 hrs · 2,504 cycles
EMERGENCY LIGHTS STRIP INSIDE CABIN HAS APPROX 12 FEET OF LIGHTS NOT WORKING BETWEEN ROW 2 AND ROW 5. INSTALLED SERVICEABLE CONNECTOR P38LZ AT ROW 5. OPS CHECKS GOOD.