N174GJ
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.
65 reports on file, 2010-11-07 – 2019-11-21.
Part: WARNING MESSAGE — MULTIPLE FAIL · airframe 27,068 hrs · 18,340 cycles
GPWS FAIL STATUS MSG, TERRAIN FAIL STATUS MSG, WINDSHEAR FAIL STATUS MESSAGES CAME ON SIMULTANEOUSLY. PERFORMED OPS TEST OF THE GPWS SYSTEM IAW CRJ 700 AMM 34-42-01. NO DEFECTS NOTED. PART.
Part: SMOKE WARNING — FALSE ACTIVATION (AFT LAVATORY) · airframe 27,068 hrs · 18,340 cycles
SMOKE AFT LAV MASTER WARNING IN FLIGHT. INSPECTED AFT LAV AND PERFORMED OPS TEST OF LAV SMOKE DETECTION SYSTEM IAW CRJ 700 AMM 26-16-00. NO DEFECTS NOTED.
Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 27,013 hrs · 18,300 cycles
SMOKE DETECT WARNING AFT LAV IN FLT. OPS CHECKED GOOD IAW CRJ 700AMM 26-16-00.
Part: BEAM — CORRODED (FUSELAGE) · airframe 25,924 hrs · 17,546 cycles
FS280.00 BEAM LT SIDE CRACKED. INSTALED CENTER FWD SUPPORT ANGLE IAW SRM 51-40-206.
Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,924 hrs · 17,546 cycles
FS280 BEAM CENTER FWD SUPPORT ANGLE HAS CORROSION. INSTALED CENTER FWD SUPPORT ANGLE IAW SRM 51-40-206.
Part: BEAM — CRACKED (FUSELAGE) · airframe 25,924 hrs · 17,546 cycles
FS280.00 BEAM RT SIDE CRACKED. INSTALLED FS280.00 BEAM RT SIDE DRIP TRAY AND INSTALED 280 BEAM IAW SRM 51-40-206.
Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,924 hrs · 17,546 cycles
FS280 BEAM CENTER FWD SUPPORT ANGLE HAS CORROSION.
Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 25,481 hrs · 17,249 cycles
GEAR DISAGREE WARNING IN FLT. DEFERRED LANDING GEAR RETRACTION SYS ON OCN 70052422 PER MEL 32-30-01 CAT A AUTH BY MXC.
Earlier reports · 2010–2018 · 57 reports
2018
Part: UNKNOWN — SMOKE (LAVATORY) · airframe 24,622 hrs · 16,679 cycles
SMOKE AFT LAV WARN MSG APPEARED IN FLT WITH ELECTRICAL SMOKE. PERFORMED FIM TASK 26-16-00. INSPECTED WIRE BEHIND LIGHT LENS IAW AMM 25-42-06 NO DEFECTS NOTED. INSPECTED TEMP INDICATOR ON LAVITORY WASTE DOOR IAW AMM 26-26-03 NO TEMP INDICATION. OK RAN NR 1 AND NR 2 PACKS IAW AMM 21-51-06. FOR 40 MIN COULD NOT REPLICATE. PERFORMED OPS CHECK OF SMOKE DETECTION SYSTEM. OPS CHECK GOOD IAW AMM 26-16-00. A/C OK FOR SERVICE.
2017
Part: LIGHT — UNSECURE (CABIN) · airframe 20,098 hrs · 13,457 cycles
EMERGENCY LIGHTING STRIP FOUND LOOSE. SECURED THE EMERGENCY LIGHT STRIP IAW AMM 25-25-01.
2015
Part: ANGLE — CORRODED (FUSELAGE) · airframe 16,045 hrs · 10,525 cycles
SPLICE ANGLE ON AFT WING TO BODY FAIRING SUPPORT WEB IS CORRODED. R & R SPLICE ANGLE IAW SRM 51-42-06.
Part: FRAME — CORRODED (FUSELAGE) · airframe 16,045 hrs · 10,525 cycles
FRAME AT FS 295, BETWEEN STRINGER 25L & 25R HAS SIGNS OF CORROSION. CUT OUT CORRODED SECTION OF FRAME. CUT & DRILLED NEW FRAME SECTION, FABRICATED REPAIR SPLICES & INSTALLED WITH TWO ANGLES, PN S6144-13 & S1710-4, IAW REO 670-53-21-799, DATED 30 JAN 2012.
Part: ESCAPE ROPE — FRAYED (CABIN) · airframe 16,045 hrs · 10,525 cycles
LEFT & RIGHT OVERWING EXIT SAFETY ROPES HAVE LOOSE STITCHING. R & R ROPES IAW AMM 25-63-04.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 16,045 hrs · 10,525 cycles
PASSENGER DOOR INTERNAL SURROUND STRUCTURE LINTEL STRINGER 3 IS CRACKED AT FS 280. CUT OUT DAMAGED AREA & REPAIRED IAW SB 670BA-53-040 REV B DATED 02 MAY 2012. WO 80289 & WC 2157.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 15,942 hrs · 10,451 cycles
SKIN DAMAGED BETWEEN FS 376.00 - 409.0 & STRINGER 14R - 19R. REPAIRED FUSELAGE SKIN DAMAGE IAW REO 670-53-21-1184.
Part: LIGHT — LOOSE (CABIN) · airframe 15,916 hrs · 10,433 cycles
LEFT EXIT ROW ESCAPE PATH EMER LIGHTING STRIP LOOSE. SECURED EXIT ROW STRIP IAW AMM 33-51-01.
Part: ESCAPE ROPE — DETACHED · airframe 15,510 hrs · 10,148 cycles
RIGHT EMER ESCAPE ROPE COVER WILL NOT STAY ATTACHED. REATTACHED RT ESCAPE ROPE COVER IAW AMM 51-22-61.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 15,220 hrs · 9,963 cycles
LEFT BLEED DUCT MASTER WARNING IN FLIGHT. INSPECTED LOOPS MT137L & MT203L. PERFORMED OPERATIONAL CHECK OF THE LT BLEED SYS IAW AMM 36-12-05. NO MSGS AT THIS TIME.
Part: COVER — MISSING (ESCAPE ROPE) · airframe 15,193 hrs · 9,943 cycles
LEFT EMER OVERWING DOOR ESCAPE ROPE COVER MISSING. SECURED LT COVER IAW AMM 25-53-04.
Part: COVER — MISSING (ESCAPE ROPE) · airframe 15,020 hrs · 9,830 cycles
LEFT EMER ROPE COVER MISSING. DEFERRED LT ROPE COVER IAW NEF 25-100-1 CAT 5.
2014
Part: ESCAPE ROPE — LOOSE (CABIN) · airframe 14,946 hrs · 9,781 cycles
EMERGENCY EXIT ROPE COVER AT ROW 18 LOOSE. SECURED EMER ROPE COVER AT EXIT ROW 18 IAW AMM 25-26-09.
Part: GLOWSTRIP — UNSECURE (CABIN) · airframe 14,347 hrs · 9,372 cycles
PHOTO LUMINESCENT STRIPS ARE PULLING UP BY THE RT OVERWING EXIT. SECURED PHOTO LUMINESCENT STRIP ON OVERWING EXIT RT SIDE OF ACFT IAW AMM 33-51-01.
Part: LIGHT — UNSECURE (CABIN) · airframe 13,732 hrs · 8,996 cycles
EMERGENCY PATH LIGHT STRIP CAME OFF IN EXIT ROW. REINSTALLED EMER LIGHT STRIP IN EXIT ROW AMM 33-51-01. OPERATIONS CHECKED GOOD AT THIS TIME.
Part: HOOK AND LOOP — MISSING (ESCAPE ROPE) · airframe 13,595 hrs · 8,919 cycles
EXIT ROW 18 RT EMER ROPE COVER MISSING HOOK AND LOOP. INSTALLED NEW HOOK AND LOOP ON RT EXIT ESCAPE ROPE COVER IAW AMM 51-22-61.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 13,562 hrs · 8,897 cycles
RED PAX DOOR WARNING MSG. INSPECTED & VERIFIED PAX L1 DOOR CLOSES, LATCHES & GREEN DOOR WITNESS MARKS FOUND ALIGNED. ACFT SAFE FOR A ONE TIME FLIGHT.
Part: ADC — FAULTY (NR 1) · airframe 13,026 hrs · 8,547 cycles
ERRATIC ALTIMETER READINGS NR 1 POSITION. R & R NR 1 ADC IAW AMM 34-13-01, OPERATIONS CHECKED GOOD WITH NO FAULTS NOTED.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 12,356 hrs · 8,130 cycles
STEERING INOPERATIVE CAUTION MESSAGE IN FLIGHT. PERFORMED NLG STEERING ECU BIT TEST IAW AMM 32-50-00, OPERATIONS CHECKED GOOD AT THIS TIME.
Part: INDICATION SYS — FAULTY (COCKPIT) · airframe 12,277 hrs · 8,076 cycles
PASSENGER DOOR OUTER HANDLE CAUTION MESSAGE. DEFERRED INDICATION ON OPEN CONTROL 31869 IAW MEL 52-70-01 CAT A.
2013
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 12,077 hrs · 7,959 cycles
PASSENGER DOOR OUTER HANDLE MASTER CAUTION. PERFORMED OPERATIONS TEST OF PAX DOOR PROX WARNING SYSTEM IAW CRJ700 AMM 52-70-00, NO FAULTS NOTED.
Part: PROXIMITY SENSOR — OUT OF ADJUST (NLG) · airframe 12,003 hrs · 7,910 cycles
NOSE LANDING GEAR DOOR OPEN WARNING MESSAGE AFTER TAKEOFF. ADJUSTED NLG PROX SENSOR PX30 IAW CRJ700 AMM 32-61-05. OPERATIONS CHECKED GOOD AT THIS TIME.
Part: BEAM — CORRODED (FUSELAGE) · airframe 12,000 hrs · 7,908 cycles
RIGHT 280 BEAM HAS PITTING CORROSION. R & R RT 280 BEAM WITH SERVICEABLE PN C6670-34094-25 IAW CRJ 700 SRM 51-42-06, 51-21-11, 51-23-00, 51-42-21, 51-40-11 & CRJ 700 AMM 51-21-01.
Part: WEB — CORRODED (FUSELAGE) · airframe 12,000 hrs · 7,908 cycles
RIGHT WEB AT FS 280 CORRODED. REPAIRED RT WEB AT FS 280 IAW REO 670-53-11-594 DATED 27 APR 2011, CRJ 700 SRM 51-23-00, 51-42-06, 51-25-06, 51-25-16, 51-21-11 & CRJ 700 AMM 51-21-01.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 12,000 hrs · 7,908 cycles
280 BEAM QUARTER TURN ANGLE CORRODED. R & R 280 BEAM QUARTER TURN ANGLE PN CC670-34095-3 IAW CRJ 700 SRM 51-42-06, 51-42-22, 51-42-21 & 51-42-13.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 12,000 hrs · 7,908 cycles
LEFT BUTT LINE 12.00 AT FS 276 FLOOR BEAM CRACKED. REPAIRED LBL 12.00 COCKPIT FLOOR BEAM IAW REO 670-53-11-881 REV A 2013-12-16 & CRJ 700 SRM 51-21-11.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 12,000 hrs · 7,908 cycles
RIGHT BUTT LINE 12 COCKPIT FLOOR BEAM CRACKED AT FS 276. PERFORMED REPAIR ON RBL 12.00 COCKPIT FLOOR BEAM IAW REO 670-53-11-881 REV A 2013-12-16 & CRJ 700 SRM 51-21-11.
Part: SILL — CORRODED (FUSELAGE) · airframe 12,000 hrs · 7,908 cycles
RIGHT HAND SILL FROM FS 280 TO 319.70 HAS CORROSION AROUND DRAIN HOLE FWD OF SERVICE DOOR. R & R RT SILL FROM FS 280 TO 319.70 WITH SERVICEABLE PART IAW CRJ 700 SRM 51-42-06, 51-42-21, 51-42-13 & 51-23-00.
Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 12,000 hrs · 7,908 cycles
MAIN PAX DOOR AFT DRAG ANGLE CRACKED. REMOVED DAMAGED PORTION OF AFT DRAG ANGLE. INSTALLED FABRICATED SPLICES 2 & ANGLE IAW CRJ 700 SRM 51-32-59 & 52-11-04.
Part: PANEL — CRACKED (PAX DOOR) · airframe 12,000 hrs · 7,908 cycles
MAIN PASSENGER DOOR AFT SIDE PANEL CRACKED IN ZONE NR 1. CUT OUT DAMAGED PORTION IN ZONE NR 1 OF MAIN PAX DOOR AFT SIDE PANEL. INSTALLED FABRICATED DOUBLER & ANGLE IAW BOMBARDIER REO 670-52-11-104 REV F, DATED 2010-10-21.
Part: HOOK AND LOOP — MISSING (EMERGENCY EXIT) · airframe 11,982 hrs · 7,896 cycles
HOOK AND LOOP MISSING FROM LT EXIT HANDLE COVER. REPLACED HOOK AND LOOP ON EMERGENCY COVER IAW CRJ700 AMM 51-22-61.
Part: WARNING SYSTEM — ACTIVATED (PAX DOOR) · airframe 11,881 hrs · 7,826 cycles
PASSENGER DOOR MASTER WARNING ON GROUND. R & R PX101 IAW AMM 52-70-04, NO FIX.
Part: SPLICE — DAMAGED (PAX DOOR) · airframe 11,881 hrs · 7,826 cycles
PASSENGER DOOR MASTER WARNING ON GROUND. REPAIRED SPLICE ON SP528 OF PX101 IAW CRJ700 ESPM 20-33-00, OPERATIONS CHECKED GOOD AT THIS TIME, NO DEFECTS NOTED.
Part: WARNING SYSTEM — FALSE ACTIVATION (PAX DOOR) · airframe 11,881 hrs · 7,826 cycles
PASSENGER DOOR MASTER WARNING ON GROUND. INSPECTED ALL PROX SENSORS FOR PAX DOOR, NO DEFECTS NOTED AT THIS TIME IAW CRJ52-70-04. INSPECTED WIRING HARNESS FOR PROX SENSOR DEFECTS, NONE FOUND IAW CRJ700 AMM 20-70-00. CYCLED DOOR & RE RACKED PSEU IAW CRJ700 AMM 32-61-01 NO FIX.
Part: COVER — LOOSE (EMERGENCY EXIT) · airframe 11,077 hrs · 7,279 cycles
LEFT EMERGENCY EXIT HANDLE COVER LOOSE. SECURED COVER IAW AMM 51-22-61.
Part: HOOK AND LOOP — FAILED (EMERGENCY EXIT) · airframe 11,031 hrs · 7,254 cycles
LEFT EMERGENCY DOOR COVER WILL NOT STAY UP. APPLIED NEW HOOK AND LOOP AS REQUIRED IAW AMM 51-22-61.
Part: PROXIMITY SENSOR — OUT OF ADJUST (PAX DOOR) · airframe 10,989 hrs · 7,226 cycles
PAX DOOR LATCH MESSAGE AND PROX SYS FAULT 2 STATUS MESSAGE IN FLIGHT. ADJUSTED PAX DOOR PROXIMITY SENSOR PX46 IAW CRJ700 52-70-04. PERFORMED OPS TEST OF PAX DOOR WARN SYSTEM IAW AMM 52-70-00. NO FAULTS NOTED OK FOR SERVICE AT THIS TIME.
Part: PROXIMITY SWITCH — OUT OF ADJUST (PAX DOOR) · airframe 10,990 hrs · 7,226 cycles
PAX DOOR LATCH CAUTION MESSAGE AND PROXIMITY 2 STATUS MESSAGE IN FLIGHT. ADJUSTED PAX DOOR PROXIMITY SWITCH PX46, IAW AMM 52-70-04, OP'S CHECKED GOOD.
Part: WARNING MESSAGE — ILLUMINATED (BRAKE TEMP) · airframe 10,918 hrs · 7,172 cycles
BRAKE OVERTEMP WARNING.
Part: HOOK AND LOOP — UNSECURE (EMERGENCY EXIT) · airframe 10,844 hrs · 7,123 cycles
HOOK AND LOOP LOOSE ON OVERWING EMERGENCY EXIT DOOR HANDLE COVER. RESECURED EMERGENCY ROPE COVER IAW AMM 51-21-61, NO FURTHER DEFECTS NOTED AT THIS TIME.
Part: PROXIMITY SENSOR — OUT OF ADJUST (PAX DOOR HANDLE) · airframe 9,835 hrs · 6,450 cycles
PAX DOOR HANDLE CAUTION MEAASGE WITH PROX 2 STATUS MESSAGE. ADJUSTED PX46 PASSENGER DOOR PROXIMITY SENSOR, OP'S CHECK GOOD IAW AMM 52-70-04.
Part: PROXIMITY SENSOR — INOPERATIVE (PAX DOOR) · airframe 9,747 hrs · 6,397 cycles
PAX DOOR OUTER HANDLE MESSAGE ON EICAS DISPLAY IN FLIGHT. R & R PX46 PROX SENSOR IAW AMM 52-70-04, OP'S CHECK OF PAX DOOR WARNING SYS GOOD AT THIS TIME FOR SERVICE.
Part: SENSOR — OUT OF ADJUST (PAX DOOR) · airframe 9,745 hrs · 6,395 cycles
PAX DOOR LATCH CAUTION MESSAGE. ADJUSTED PAX DOOR LATCH SENSOR IAW AMM 52-71-04, OPS CHECK OK FOR SERVICE.
Part: CABLE — BROKEN (PAX DOOR) · airframe 9,723 hrs · 6,383 cycles
CABLE ON MAIN CABIN DOOR BROKEN. DEFERED DOOR POWER ASSIST CABLE SYS ON DMI 23839 IAW MEL 52-11-00.
2012
Part: PROXIMITY SENSOR — INOPERATIVE (PAX DOOR) · airframe 7,465 hrs · 4,917 cycles
PASSENGER DOOR WARNING MESSAGE. R & R PX101 PROXIMITY SENSOR IAW AMM 52-70-04, OPS CHECKED GOOD.
Part: PROXIMITY SENSOR — OUT OF ADJUST (PAX DOOR) · airframe 7,456 hrs · 4,911 cycles
PASSENGER DOOR WARNING MESSAGE. INSPECTED AND ADJUSTED PROXIMITY SENSOR PX101 IAW AMM 52-70-00. OPS CHECKED GOOD, NO MESSAGES NOTED.
Part: PROXIMITY SENSOR — FALSE INDICATION (PAX DOOR) · airframe 7,456 hrs · 4,911 cycles
PASSENGER DOOR WARNING MESSAGE. ADJUSTED PAX DOOR PROX SENSOR IAW AMM 52-70-04. PERFORMED OPS CHECK IAW AMM 52-70-00. OPS CHECK GOOD AT THIS TIME.
Part: WARNING MESSAGE — FALSE ACTIVATION (PAX DOOR) · airframe 7,456 hrs · 4,911 cycles
PASSENGER DOOR WARNING MESSAGE. INSPECTED AND OPERATED MAIN CABIN DOOR WARNING SYS OPS CHECKED GOOD IAW AMM 52-70-00 NO MESSAGES NOTED AT THIS TIME.
Part: PROXIMITY SENSOR — OUT OF ADJUST (PAX DOOR) · airframe 7,446 hrs · 4,905 cycles
PAX DOOR WARNING. ADJUSTED SENSOR PX101 AND PERFORMED OPS CHECK OF CABIN MAIN DOOR NO DEFECTS NOTED IAW AMM 52-70-04
Part: PROXIMITY SWITCH — FAULTY (PAX DOOR) · airframe 7,440 hrs · 4,901 cycles
PAX DOOR LATCH CAUTION IN FLIGHT WITH PROX SYS FAULT 1 STATUS MESSAGE. R & R PROXIMITY SWITCH PX107 OPS CHECKED GOOD IAW AMM 52-70-04.
Part: WEB — CRACKED (PAX DOOR) · airframe 6,644 hrs · 4,375 cycles
PAX DOOR AFT WEB CRACKED AT MOTOR BRACKET. REPAIRED IAW REO670-52-11-104, REV E.
Part: LANYARD — FRAYED (PAX DOOR) · airframe 6,644 hrs · 4,375 cycles
BOTH PAX DOOR HAND RAIL QUICK RELEASE PIN LANYARD CABLES FRAYED. REMOVED DAMPNER LANYARD AND INSTALLED NEW IAW AMM 52-11-00.
2011
Part: SIGN — LOOSE (CABIN) · airframe 5,737 hrs · 3,787 cycles
LIGHTED EMERGENCY EXIT SIGN AT 1C LOOSE ON TOP. RESECURED HARDWARE ON EMERGENCY EXIT SIGN IAW AMM 20-21-00.
Part: PLACARD — WORN (CABIN) · airframe 5,246 hrs · 3,467 cycles
PASSENGER DOOR OPEN PLACARD WORN. R & R OPEN PLACARD ON PASSENGER DOOR IAW AMM 20-60-04.
Part: SENSOR — FAULTY (BRAKE TEMP) · airframe 4,547 hrs · 3,011 cycles
BRAKE OVER HEAT MASTER WARNING. TURNED INTO BRAKE TEMP SENSOR UNAVAILABLE. INSPECTIED AND FOUND FAULTY BRAKE TEMP READOUT. DEFFERED NR 4 BRAKE TEMP READOUT ON DMI 24399 IAW MEL 32-46-01D, CAT C, AUTHORIZED.
Part: PANEL — CRACKED (PAX DOOR) · airframe 3,819 hrs · 2,580 cycles
PAX DOOR LOWER STOW PANEL CRACKED. R & R PAX DOOR BOTTOM STOW PANEL IAW AMM 52-11-04
2010
Part: UNKNOWN — ODOR (CABIN) · airframe 2,826 hrs · 1,940 cycles
F/A REPORTED ODOR OF SMOKE NEAR ROW 17 LEFT SIDE. INSPECTED AND OPS CHECKED CABIN AND LAV LIGHTS, OVERHEAD BINS, GALLEY COMPARTMENT, AND TRASH CANS. ALSO OPS CHECKED GALLEY HEATER, PERFORMED BOTH ENGINE POWER RUNS AND CHECKED LT AND RT BLEED AND PACKS. NO SIGNS OF ODOR FOUND IN CABIN, LAV, OR COCKPIT AT THIS TIME. IAW AMM 33-20-00, 33-25-00, 21-23-64, 21-51-00, 36-10-00, AND 72-00-00.