N592SW
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.
58 reports on file, 2002-06-02 – 2007-11-08.
Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 21,682 hrs · 18,496 cycles
FLIGHT 5308 - EN ROUTE CVG-LGA RECEIVED FLAP FAIL MESSAGE. DIVERTED TO JFK, DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C) FLAP SYSTEM WAS RESET WITH NO FURTHER MESSAGES.
Part: CONTROL HANDLE — FAULTY (COCKPIT) · airframe 20,664 hrs · 17,659 cycles
AT 4000FT AND 210KTS RECEIVED GEAR HORN, TERRAIN WARNING AND GEAR DOWN AMBER. CLEARED AFTER 45 SECONDS. GEAR IND TURNED WHITE AFTER 10 SECONDS. 2ND INCIDENT, FIRST HAD NO TERRAIN WARNING. PERFORMED OPERATIONAL TEST. REPLACED LANDING GEAR CONTROL ASSEMBLY. NO FURTHER DEFECTS.
Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 20,506 hrs · 17,536 cycles
FLIGHT 5067 - FLAP FAIL AT GATE. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER MESSAGES.
Part: FLAP — MALFUNCTIONED (WING) · airframe 20,245 hrs · 17,329 cycles
AFTER LANDING DURING FLAP RETRACTION RECEIVED A FLAP FAIL MESSAGE AT 27 DEGREES. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES.
Part: WINDOW — CRACKED (COCKPIT) · airframe 20,027 hrs · 17,155 cycles
FLIGHT 9438 - F/O'S SIDE WINDOW CRACKED PASSING THROUGH 26,000 FT. REPLACED WINDOW.
Earlier reports · 2002–2006 · 53 reports
2006
Part: SENSOR — FAULTY (E/E BAY) · airframe 18,447 hrs · 15,910 cycles
FLIGHT 5480 - AFTER TAKEOFF RECEIVED A RIGHT PACK OVERPRESSURE WARNING, FLIGHT RETURNED TO THE FIELD. REPLACED THE DUCT TEMPERATURE SENSOR.
Part: CONNECTOR — DIRTY (OIL TEMP BULB) · airframe 18,418 hrs · 15,888 cycles
FLIGHT 5506 - RECEIVED APU TEMP MASTER CAUTION IN FLIGHT/ DIVERTED TO ORF AND LANDED WITHOUT INCIDENT. FOUND APU OIL SERVICED PROPERLY. CLEANED CONNECTOR ON OIL TEMP BULB AND RESECURED. PERFORMED APU RUN, NO FURTHER DEFECTS.
2005
Part: PIN — LOOSE (CONNECTOR) · airframe 17,352 hrs · 15,034 cycles
STAB TRIM CH 1 STATUS MESSAGE OCCURRED TWICE, ONCE ON CLIMB-OUT, ONCE ON TAXI IN. REPLACED HSTA AND MCU IAW AMM 27-40-00, 27-42-05 AND RECONNECTED LOOSE PINS AT P268. OPERATIONAL CHECK GOOD, PN: 7062-3, SN OFF: 934, PN: 8396-3 SN OFF: 794.
Part: TRIM SWITCH — MALFUNCTIONED (STAB TRIM) · airframe 17,314 hrs · 15,007 cycles
CA STAB TRIM INTERMITTENT, BOTH DIRECTIONS. REPLACED CAPTIANS TRIM SWITCH. IAW 27-41-05. OPERATIONAL CHECK GOOD IAW 27-41-01.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 17,140 hrs · 14,876 cycles
NR 2 CEILING EMERGENCY FLOODLIGHT INOP. RELAMPED NR 2 CEILING EMERGENCY FLOODLIGHT. OPERATIONAL CHECK GOOD.
Part: BOLT — LOOSE (SPOILER) · airframe 16,767 hrs · 14,581 cycles
ABORTED T/O DUE TO "CONFIG SPOILERS" WARNING MSG. REPLACED BOLT AND BUSHINGS AT ROD END ATTACH POINT RIGHT FLIGHT SPOILER OB PCU AND ADJUSTED PCU IAW MM 27-62-01. OPERATIONAL CHECK GOOD.
Part: PCU — MALFUNCTIONED (FLT SPOILERS) · airframe 16,402 hrs · 14,305 cycles
FLIGHT SPOILERS FAULT STATUS MSG ON ED2. REPLACED RIGHT NR 2 OUTBOARD FLIGHT SPOILER PCU IAW MM 29-62-01. OPERATIONAL CHECK GOOD.
Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 15,730 hrs · 13,780 cycles
OVERHEAD EMERGENCY EXIT SIGN AT OVERWING EXITS INOP. RESECURED LOOSE CONNECTOR. OPERATIONAL CHECK GOOD IAW AMM SUBTASK 33-51-00-720-801.
Part: ANGLE — CRACKED (BS 625) · airframe 16,580 hrs · 14,441 cycles
FS 625 LT ANGLE STR 14L CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 15,730 hrs · 13,780 cycles
FS 280 BELOW FLOOR RBL 9.0 OUTBOARD ANGLE CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-13, 51-42-21, 51-23-00, 51-25-00.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 15,730 hrs · 13,780 cycles
FLOOR ANGLE CORRODED IN NUMEROUS LOCATIONS FROM FS 409 +128 TO FS 559 AND LBL 36 TO 47, ITEM FOUND AT C-CHECK INSPECTION. BLENDED OUT DAMAGE IAW CRJ SRM 53-41-45 PAGE 101-108. FOUND TO BE WITHIN LIMITS IAW SRM 53-41-45.
Part: FLOOR SUPPORT — CORRODED (FUSLEAGE) · airframe 15,730 hrs · 13,780 cycles
FLOOR ANGLE CORRODED IN NUMEROUS LOCATIONS FROM FS 409 +128 TO FS 559 AND RBL 36 TO 47, ITEM FOUND AT C-CHECK INSPECTION. BLENDED OUT DAMAGE IAW CRJ SRM 53-41-45 PAGE 101-108, FOUND TO BE WITHIN LIMITS IAW SRM 53-41-45.
Part: STEP — CORRODED (PAX DOOR) · airframe 15,730 hrs · 13,780 cycles
PAX DOOR TOP STEP HAS CORROSION ON HINGE, ITEM FOUND AT C-CHECK INSPECTION. HINGE REPLACED IAW CRJ SRM 51-41-02.
Part: FLOOR PANEL — CRACKED (E/E BAY) · airframe 15,730 hrs · 13,780 cycles
FS 193 - LEFT SIDE ELECTRICAL BAY FLOOR CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED CRACK IAW CRJ REO 601R-53-11-001 REV NC.
Part: LIGHT — BURNED OUT (EXTERIOR) · airframe 15,134 hrs · 13,294 cycles
ONE CEILING LEVEL EMERGENCY FLOODLIGHT INOPERATIVE. RELAMPED, OPERATIONAL CHECKS GOOD.
Part: PCU — MALFUNCTIONED (SPOILERS) · airframe 15,098 hrs · 13,265 cycles
SPOILERON FAULT STATUS MESSAGE UPON LANDING. REPLACED RIGHT OUTBOARD PCU IAW 22-61-05, OPERATIONAL CHECK GOOD.
2004
Part: CONVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 14,253 hrs · 12,613 cycles
EMERGENCY TRACK LIGHTING AT SEAT 12AB IS NOT ILLUMINATING. REMOVED AND REPLACED CONVERTER IAW 33-00-00. OPERATIONAL CHECK GOOD.
Part: ACTUATOR — MALFUNCTIONED (HORIZONTAL STAB) · airframe 13,967 hrs · 12,384 cycles
COULD NOT GET STAB CHANNEL NR 2 TO ENGAGE. REMOVED AND REPLACED THE HORIZONTAL STAB TRIM ACTUATOR AND THE MOTOR CONTROL UNIT. OPERATIONAL CHECK GOOD. P/N 7062-3, S/N OFF 1095.
Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB TRIM) · airframe 13,928 hrs · 12,354 cycles
STAB CHANNEL 2 WILL NOT ENGAGE. REMOVED AND REPLACED HSTCU IAW AMM 27-41-01. OPERATIONAL CHECK GOOD.
Part: TRIM SWITCH — MALFUNCTIONED (STAB TRIM) · airframe 13,850 hrs · 12,287 cycles
STAB TRIM CHANNEL 2 WILL NOT ENGAGE. REMOVED AND REPLACED BOTH TRIM SWITCHES IAW MM 27-41-30. OPERATIONAL CHECK GOOD.
Part: CONTROL UNIT — MALFUNCTIONED (TRIM MOTOR) · airframe 13,627 hrs · 12,110 cycles
STAB TRIM CHANEL 1 INOPERATIVE. REMOVED AND REPLACED STAB TRIM ACTUATOR AND MOTOR CONTROL UNIT IAW MM 27-42-01 AND 27-42-05. OPERATIONAL CHECK GOOD. P/N: 8396-3 S/N OFF: 682
Part: SWITCH — MALFUNCTIONED (STAB TRIM) · airframe 13,592 hrs · 12,080 cycles
STAB CH 1 INOP MESSAGE. REMOVED AND REPLACED CAPTIANS STAB TRIM DISCONNECT SWITCH IAW MM 27-41-30. OPERATIONAL CHECK GOOD.
Part: PCU — MALFUNCTIONED (FLIGHT SPOILER) · airframe 13,150 hrs · 11,727 cycles
SPOILERON FAULT MESSAGE ON TAXI OUT WITH BOTH ENGINES RUNNING. REMOVED AND REPLACED LT NR 1 SPOILERON PCU IAW MM 27-62-01. OPERATIONAL CHECK GOOD.
Part: PCU — MALFUNCTIONED (SPOILERS) · airframe 13,080 hrs · 11,672 cycles
SPOILERON FAULT STATUS MESSAGE WOULD NOT CLEAR. REMOVED AND REPLACED LEFT WING INBOARD FLIGHT SPOILER INBOARD PCU IAW MM 27-61-00. LEAK AND OPS CHECK GOOD.
Part: CONTROL UNIT — FAILED (SPOILERONS) · airframe 12,471 hrs · 11,203 cycles
LEFT SPOILERON FAULT MESSAGE ON EICAS. REMOVED AND REPLACED NR 1 SECU IAW MM 27-61-05. OPS CHECK GOOD. P/N 49-164-06, S/N OFF 0929.
Part: BPSU — MALFUNCTIONED (T/E FLAP) · airframe 12,371 hrs · 11,124 cycles
RECEIVED A FLAPS FAIL WHEN SELECTING FLAPS 20 DURING APPROACH. REMOVED AND REPLACED LEFT BPSU IAW CRJ MM 27-51-10. OPS CHECK GOOD. P/N: 855D100-9, S/N ON: 316B, S/N OFF: 0811B.
Part: SENSOR — MALFUNCTIONED (AOA) · airframe 12,354 hrs · 11,108 cycles
STALL FAIL AFTER ROTATION. REMOVED AND REPLACED LEFT AOA SENSOR IAW CL600 MM 27-35-05. OPS CHECKS GOOD.
Part: PDU — MALFUNCTIONED (TE FLAPS) · airframe 11,974 hrs · 10,813 cycles
FLAP FAIL MESSAGE WHEN SELECTING FLAPS AT 45 DEGREES. REMOVED AND REPLACED FLAP PDU IAW MM 27-52-01. OPS CHECKS GOOD.
2003
Part: BEAM — CRACKED (RT NACELLE) · airframe 11,768 hrs · 10,653 cycles
ENGINE SUPPORT BEAM LOWER WEB RIGHT SIDE RBL 34 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. WEB REPAIRED IAW CRJ REO 601R-53-61-366 REV ''D'', RII 53-401.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 11,768 hrs · 10,653 cycles
FS 280 RT FLOORBEAM RBL 90 INBOARD AND OUTBOARD ATTACH ANGLE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11 & RII 53-401.
Part: BEAM — CRACKED (FUSELAGE) · airframe 11,768 hrs · 10,653 cycles
FS 280 TRANSVERSE BEAM LBL 11 LOWER FLANGE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. CUT-OUT AND REPAIRED DAMAGED SECTION OF TRANSVERSE BEAM IAW CRJ REO 601R-53-11-171 REV ''NC''.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 11,768 hrs · 10,653 cycles
FS 460 RIGHT FLOORBEAM RBL 9.0 O/B FITTING CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED FITTING IAW CRJ SRM 51-40-11, 51-23-00, 51-42-06, 51-42-21 & RII 53-401.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 11,768 hrs · 10,653 cycles
FS 625 RIGHT INTERCOSTAL STRINGER 14R CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED INTERCOSTAL IAW CRJ SRM 51-40-11, 51-42-06.
Part: BEAM — CRACKED (LT NACELLE) · airframe 11,768 hrs · 10,653 cycles
ENGINE SUPPORT BEAM LOWER WEB LT SIDE LBL 34 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. WEB REPAIRED IAW CRJ REO 601R-53-61-366 REV ''D'' AND RII 53-401.
Part: BEAM — CRACKED (CARGO BAY) · airframe 11,768 hrs · 10,653 cycles
TRANSVERSE BEAM REMOTE ANGLE FOR DOOR STOP FITTING IS CRACKED; FS 589.00; LBL 42.0. DISCOVERED DURING C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40-11 & RII 53-401.
Part: SILL — CRACKED (CARGO PIT) · airframe 11,768 hrs · 10,653 cycles
CARGO PIT CARGO DOOR FLOOR LANDING SILL IS CRACKED UNDER STEP PLATE ASSY PIN STOP FITTING; FS 576.00; LBL 42.0. DISCOVERED DURING C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40-11 & RII 53-401.
Part: SUPPORT — CRACKED (ENGINE) · airframe 11,768 hrs · 10,653 cycles
ENGINE SUPPORT BEAM UPPER WEB RBL 6 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. UPPER WEB REPAIRED IAW CRJ REO 601R-53-61-345 REV ''C'' AND RII 53-401.
Part: BEAM — CRACKED (FUSELAGE) · airframe 11,768 hrs · 10,653 cycles
FS 280 TRANSVERSE BEAM RBL 11 LOWER FLANGE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. CUT-OUT AND REPAIRED DAMAGED SECTION OF TRANSVERSE BEAM IAW CRJ REO 601R-53-11-171 REV ''NC''.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 11,974 hrs · 10,813 cycles
FS 484 LT INTERCOSTAL O/B FLANGE LBL 36 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED INTERCOSTAL IAW CRJ REO 601R-53-41-059 REV A AND RII 53-401.
Part: FRAME — CRACKED (FUSELAGE) · airframe 11,974 hrs · 10,813 cycles
OUTER FLANGE ON FUSELAGE FRAME AT FS 220 AND STR 23L IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED FLANGE IAW CRJ DWG 600-34013 & RII 53-401.
Part: RIB — CRACKED (LT PYLON) · airframe 11,974 hrs · 10,813 cycles
LT PYLON FS 605 RIB CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED RIB IAW CRJ SRM 51-40-11. P/N: 601-37004-85.
Part: HEATER — MALFUNCTIONED (GALLEY) · airframe 10,988 hrs · 10,046 cycles
THE NR 1 GALLEY HTR CAUSES A SMOKEY SMELL WHEN ON. CREW REPORTS THAT THERE IS A STRONG BURNT ELECTRICAL SMELL IN THE GALLEY OR FLIGHT DECK JUST AFTER PUSHBACK. REMOVED AND REPLACED NR 1 GALLEY HEATER IAW CRJ AMM 21-23-05. P/N: 2831-45 S/N OFF: 584. ALSO REMOVED AND REPLACED GALLEY VENTILATION FAN. SYSTEM OPS CHECK GOOD. NO TRACE OF ELECTRICAL BURNING SMELL.
Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 10,754 hrs · 9,861 cycles
LEFT ENGINE FAILED ON DESCENT. JUST PRIOR TO FAILURE, ''L MAIN EJECTOR'' AND ''L SCAV EJECTOR'' MSG DISPLAYED ON EICAS. REMOVED AND REPLACED LEFT POWER PLANT IAW CRJ MM 72-00-00. OPS AND LEAK CHECKS GOOD.
2002
Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 9,479 hrs · 8,864 cycles
ENGINE NR 2 FAILURE INFLIGHT. DURING CRUISE FLIGHT THE RT ITT WAS 50 DEGREES HIGHER THAN ENGINE NR 1 WITH A REDUCTION OF N1 ON ENGINE NR 2 OF 4 PERCENT. REMOVED AND REPLACED RIGHT ENGINE ASSEMBLY IAW CRJ MM 71-00-00 DUE TO COMPRESSOR BLADE DAMAGE.
Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 9,146 hrs · 8,611 cycles
STAB TRIM CHANNELS 1 AND 2 FAILED ON TAKEOFF. STAB TRIM AND MACH TRIM CAUTION MESSAGES. RETURNED TO MEM. PERFORMED BITE CHECK OF HSTCU. HSTCU SHOWS NO FAULTS IAW AMM 7-41-00. SYSTEM OPS CHECK GOOD.
Part: STRUT — DEFECTIVE (NLG) · airframe 9,146 hrs · 8,611 cycles
AFTER DEPARTURE WE RECEIVED GEAR DISAGREE NOSE DOOR WARNINGS. NOSE GEAR REMAINS GREEN WHILE MAINS TURN WHITE. RETURNED TO YYC. REMOVED AND REPLACED NLG ASSEMBLY IAW CRJ MM TASK 2-21-00-000-801. GEAR SWINGS COMPLETED IAW CRJ MM 32-30-00-720-801. OPS CHECK GOOD. REMOVED AND REPLACED NLG STEERING ECU IAW MM 32-51-10-401-801.
Part: PDU — MALFUNCTIONED (RT ENGINE T/R) · airframe 9,058 hrs · 8,534 cycles
DURING FLIGHT AT FL 350 WE RECEIVED AN ''R REV UNLOCK'' MESSAGE. FOLLOWED MEMORY ITEMS AND THEN QRH. ENGINE WAS SHUT DOWN PER QRH. NORMAL SINGLE ENGINE LANDING WAS MADE. REMOVED AND REPLACED PDU IAW MM 78-32-03 AND RIGGED LOWER INBOARD BALLSCREW ACTUATORS IAW MM 78-32-03. OPS GOOD.
Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 8,469 hrs · 8,077 cycles
ABORTED TAKEOFF FOR INBOARD OUTBOARD GROUND SPOILER FAULT. CLEARED MESSAGES BY POWER DOWN. NO FURTHER PROBLEMS.
Part: BRACKET — BENT (NLG) · airframe 7,973 hrs · 7,661 cycles
NOSE GEAR WON'T RETRACT. RETURNED TO DFW. INSPECTED NOSE GEAR FOUND GEAR PROX SENSOR BENT. STRAIGHTENED BRACKET, SWUNG GEAR AND OPS CHECK GOOD.
Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB) · airframe 7,973 hrs · 7,661 cycles
STAB CH 1 INOP STATUS MESSAGE TRIM NR 1 WON'T ENGAGE. REMOVED AND REPLACED STAB TRIM MOTOR CONTROL UNIT AND ACTUATOR, OPS CHECK GOOD.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 8,091 hrs · 7,759 cycles
FLOOR SUPPORT ANGLES AT FS 621 ON LEFT AND RIGHT SIDES ARE CRACKED. REPAIR CARRIED OUT IAW CRJ REO 601R-53-61-117, REV A.
Part: CONTROL CABLE — CORRODED (AILERON) · airframe 8,091 hrs · 7,759 cycles
RIGHT WING AILERON CABLES FROM THE TENSION REGULATOR INBOARD TO THE WHEEL WELL ARE CORRODED. RIGHT WING AILERON CABLES REPLACED IAW CRJ MM 27-00-00-960-802.
Part: OVERHEAT LOOP — MALFUNCTIONED (LT ENGINE) · airframe 7,822 hrs · 7,545 cycles
RECEIVED BLEED AIR DUCT AURAL WARNING AND RED LEFT 14TH DUCT LEAK WARNING MESSAGE IN FLIGHT. COMPLETED MEMORY ITEMS AND QRH PROCEDURES. SHUTDOWN LEFT ENGINE. REPLACED LEFT 14TH PYLON LOOP. OPS CHECK GOOD.