GOJET AIRLINES, LLC

Operated by GoJet Airlines (per NTSB report)

The elevator control restriction was caused by the failure of the elevator autopilot servo control cable, which failed due to cyclic fatigue. The slack in the broken cable wrapped around the elevator autopilot servo mount in such a way that it was bound between the servo mount and the servo mount cable guide pins. The bound cable interfered with the rotation of the servo mount, which remained connected to the aft side of the elevator control quadrant by the intact aft cables. This condition resulted in the limited rotation of the elevator control quadrant in one direction.

Operated by GoJet Airlines, LLC. (per NTSB report)

The probable cause of the uncontained No. 1 (left) engine failure was a separated high pressure turbine 2nd stage blade that failed due to a fatigue crack that originated below the blade platform from an area of corrosion.

Operated by GOJET AIRLINES LLC (per NTSB report)

The nose landing gear’s failure to fully extend due to missing and damaged fastening hardware on the drive arm assembly.

Operated by GOJET AIRLINES LLC (per NTSB report)

The malfunction of the airplane’s aileron control system due to ice accumulation.

Sanction: $24,750 · case closed 2017-02-09

Sanction: $75,000 · case closed 2015-11-09

Sanction: $40,000 · case closed 2015-01-29

Sanction: $18,000 · case closed 2014-11-07

Sanction: $15,000 · case closed 2013-06-20

Sanction: $100,000 · case closed 2013-12-16

Sanction: $175,000 · case closed 2013-11-18

Sanction: $11,000 · case closed 2013-02-11

Sanction: $30,000 · case closed 2013-02-11

Sanction: $6,000 · case closed 2013-04-15

Sanction: $10,000 · case closed 2012-12-05

Sanction: $77,000 · case closed 2012-11-14

Sanction: $20,000 · case closed 2012-10-03

Sanction: $10,000 · case closed 2012-09-13

Sanction: 2500 · case closed 2012-03-05

Sanction: $13,500 · case closed 2010-04-29

Sanction: $5,000 · case closed 2009-10-20

Sanction: $7,500 · case closed 2009-12-09

Sanction: $5,000 · case closed 2009-12-01

Sanction: $25,000 · case closed 2011-04-14

Sanction: $22,000 · case closed 2010-06-02

Sanction: 50000 · case closed 2012-03-05

Sanction: $20,000 · case closed 2008-01-18

Part: SENSOR — FAULTED (BRAKE TEMP) · airframe 47,183 hrs · 37,743 cycles

BRAKE OVERHEAT WARNING MESSAGE IN FLIGHT, LEFT OTBD (RED ZEROS WHEN MESSAGE, LOWERED GEAR FOLLOWING QRH AND SAW YELLOW DASHES, ON DECENT RECIEVED 11, ON TOUCH DOWN EVERYTHING IN LIMITS // B1 CODES - 007469, 006058, 007475, 007470. DEFERRED L OB BRAKE TEMP SENSOR, IAW MEL 32-46-01 D, CATEGORY C, ON OCN 70103271.

Part: INTERCOSTAL — CORRODED (ZONE 800) · corrosion level 2 · airframe 34,667 hrs · 21,910 cycles

CORROSION ON CLIP AND SILL BETWEEN FS 349 TO FS364, STGR 20R. INSTALLED NEW SILL BETWEEN FS 349 TO FS364, STGR 20R IAW CRJ700 SRM 51-42-20.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,667 hrs · 21,910 cycles

CORROSION AND HOLE DAMAGE ON CLIP AND STGR 23R, NEAR TO FS 379. INSTALLED NEW CLIP AND STGR 23R, BETWEEN FS 333-364 IAW CRJ 700 SRM 51-42-06.

Part: CONTROL VALVE — FAULTED (RT ENGINE) · airframe 37,674 hrs · 28,164 cycles

RT THRUST LEVER WILL NOT ADVANCE ABOVE IDLE WITH ENG RUNNING FOR TAKEOFF. REMOVED AND REPLACED T/R DCV IAW AMM 78-32-01 LEAK AND OPS CHECK GOOD. FAULT PERSISTS. REF LOG PAGE 645688 ITEM 2 FOR CORRECTIVE ACTION.

Part: SLEEVE — UNSECURE (ZONE 400) · airframe 33,837 hrs · 26,691 cycles

LEFT BLEED DUCT WARNING. RESECURED HASOV HEAT SLEEVE IAW AMM 21-61-08. NO LEAKS NOTED AT THIS TIME. OPS CHECKED GOOD.

Part: DOOR FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,179 hrs · 37,469 cycles

PASSENGER DOOR FRAME AT FS320.00 HAS CORROSION. INSTALLED FITTING INTERNAL FRAME AND INTERCOSTAL DD7A, FRAME BS 320 WAS REMOVED AND INSTALLED IAW SRM 51-42-06 AND 51-42-21.

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,667 hrs · 21,910 cycles

CORROSION ON FWD FUSE FAIRING SUPPORT TEE ATTACHMENT AT BS 629 - 661 NEEDS EVALUATED. REMOVED AND REPLACED FWD FUSELAGE FAIRING SUPPORT TEE ATTACHMENT AT BS 629 - 661 IAW SRM 51-42-06.

Part: CONTROL UNIT — FAULTED (ZONE 300) · airframe 37,664 hrs · 28,151 cycles

RUDDER LIMITER CAUTION DURING CLIMB (B1 - 233334, 060059). SWAPPED NR 1 AND NR 2 SSCU. OPS CHECKED GOOD IAW AMM 27-61-05. NO DEFECTS NOTED.

Part: UNKNOWN — ODOR (CABIN) · airframe 47,856 hrs · 37,893 cycles

FUMES IN COCKPIT SMELLS LIKE METAL BURNING UNKNOWN SOURCE IN INITIAL DESCENT 15-20 MINUTES FOLLOWED QRH AND FUMES STARTED TO DISSAPATE. PERFORMED SMOKE INSPECTION IAW FIM 21-21-00 TROUBLESHOT AND FOUND TO BE COMING FROM GALLEY HEATER. REFER TO LOG PAGE 640989 ITEM 2. STOWED CREW O2 MASKS IAW AMM 35-11-12.

Part: WARNING MESSAGE — ILLUMINATED (SPOILERS) · airframe 45,847 hrs · 35,391 cycles

INBD FLT SPOILERS MASTER CAUTION AND IB SPOILERONS MASTER CAUTION CAME ON IN FLIGHT. RESET IAW FCOM 2 CH 10.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,667 hrs · 21,910 cycles

MIDDLE INTERCOSTAL HAS CORROSION AT FS 364 R/H. REMOVED AND REPLACED MIDDLE INTERCOSTAL AT BS 364 RT IAW SRM 51-42-06, & 51-42-20.

Part: ANGLE — CORRODED (ZONE 800) · corrosion level 2 · airframe 34,667 hrs · 21,910 cycles

CRACK ON ANGLE OF PAX DOOR AFT SIDE PANEL. SECTIONAL REPAIR INSTALLED OF ANGLE WAS PERFORMED IAW SRM 52-11-04, FIGURE 52-11-04-991-814, SHEET 1-2.

Part: MANIFOLD — FAULTED (ZONE 700) · airframe 36,945 hrs · 27,718 cycles

STEERING INOPERATIVE CAUTION MESSAGE, ABORTED TAKE OFF AT 70 KTS (B1 007465 NWS MANIFOLD, NWS EHSV FAILED). PERFORMED FIM 32-51-50-810-802-AO1 NO MESSAGES AT THIS TIME.. PERFROM OPS CHECK OF NLG STEERING IAW AMM 32-50-00.

Part: ANTI-ICE VALVE — WARNING MESSAGE (ZONE 400) · airframe 32,606 hrs · 29,992 cycles

LEFT COWL ANTI-ICE CAUTION MSG IN FLIGHT(B1-039268/ L COWL A/ICE SOV/ SOV SW POSITION MISMATCH). DEFERRED COWL ANTI-ICE VALVE ON OCN 70102844 PER MEL 30-22-01 CAT C. CORRECT PRIOR TO 08/12/2026. AUTHORIZED BY MXC.

Part: SELECTOR VALVE — INOPERATIVE (ZONE 700) · airframe 1,318 hrs · 1,806 cycles

GEAR DISAGREE AFTER TAKEOFF (B1-007697) RT MLG UPLOCK SENSOR OUT OF RIG (B1-007249) MLG UPLOCK SENSOR OUT OF RIG, REMOVED AND REPLACED MLG SELECTOR VALVE IAW AMM 32-32-10. NO FURTHER DEFECTS AT THIS TIME.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 34,667 hrs · 21,910 cycles

CORROSION ON SEAT TRACK, RBL 9 BETWEEN BS 319 - 430. REMOVED & REPLACED SEAT TRACK IAW AMM 53-00-49.

Part: ENGINE — DEGRADED (LEFT) · airframe 33,364 hrs · 26,327 cycles

LEFT ENG DEGRADED CAUTION, ITT SPIKED, THRUST REDUCED ON LEFT ENGINE. REMOVED AND REPLACED LT ENG IAW AMM 71-00-00 ALL LEAK & OPS CHKD GOOD.

Part: RADIO ALTIMETER — FAULTED · airframe 40,754 hrs · 38,635 cycles

GLD UNSAFE CAUTION MESSAGE. RERACKED RADIO ALT TRANSCEIVERS 1 AND 2 IAW AMM 34-44-01 CLEANED RAD ALT ANTENNAS AND PERFORMED RADIO ALT OPS TEST NO FAULTS FOUND AT THIS TIME. PERFORMED PER FLEET RELIABILITY.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 34,667 hrs · 21,910 cycles

LH SIDE SEAT TRACK HAS CORROSION AT FS 797 - FS863 STRINGER 15L. REMOVED AND REPLACED LH SIDE SEAT TRACK AT FS797 - FS 863 STRINGER 15L IAW CRJ 700 AMM 53-0049.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,667 hrs · 21,910 cycles

POSSIBLE CORROSION ON RT INBD SEAT TRACK AT BS 349 - 477. REMOVED AND REPLACED RT INBD SEAT TRACK AT BS 349 - 477 IAW AMM 53-00-49.

Part: FMS — FAILED (ZONE 200) · airframe 33,742 hrs · 26,605 cycles

FMS STOPPED WORKING MID FLIGHT NO NAVIGATION (B1 006719 FMC 1 / INTERNAL FAULT). PERFORMED RESET AND OPS CHECK OF FMC OPS CHECK GOOD.REF CRJ 550 AMM 34-61-07. AND 34-61-01.

Part: DOOR SEAL — DAMAGED (ZONE 800) · airframe 45,905 hrs · 34,294 cycles

LOUD SQUEALING NOISE FROM MAIN CABIN DOOR SEAL IN ALL PHASES OF FLIGHT. FOUND DAMAGE TO MAIN DOOR SEAL. PERFORMED GVI OF AIRCRAFT AND FOUND TO BE SAFE FOR ONE TIME FERRY FLIGHT FROM KGSO TO KRIC.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 34,667 hrs · 21,910 cycles

POSSIBLE CORROSION ON LT INBD SEAT RAIL AT FS 379 - FS 477. REMOVED AND REPLACED LT INBD SEAT RAIL AT FS 379-FS477 IAW AMM 53-00-49.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 34,667 hrs · 21,910 cycles

POSSIBLE CORROSION ON R/H SIDE SEAT RAIL AT FS 797 - FS 863 STGR 15R. CORROSION ON RH SIDE SEAT RAIL AT FS797-FS863 STGR 15R FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49. REMOVED AND REPLACED RH SIDE SEAT RAIL AT FS797-FS863 15R IAW AMM 53-00-49.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 34,667 hrs · 21,910 cycles

CORROSION ON FLOOR RAIL LBL9 BETWEEN FS 437-FS445. REMOVED AND REPLACED DAMAGED FLOOR RAIL WITH CORROSION AT LBL9 BETWEEN FS437-FS445 IAW CRJ700 AMM 53-00-49.

Part: LIGHT — LOOSE (ZONE 200) · airframe 45,899 hrs · 34,289 cycles

EMERGENCY EXIT LIGHT STRIP ON RT EMERGENCY EXIT DOOR IS LOOSE. RESECURED EMERGENCY EXIT LIGHT STRIP ON RT EMERGENCY EXIT IAW AMM 25-25-00.

Part: PROXIMITY SENSOR — INOPERATIVE (SPOILERS) · airframe 45,774 hrs · 35,318 cycles

IB GND SPLRS CAUTION MSG AND GND SPOILER DEPLOY CAUTION MSG IN FLIGHT. R/R RHIB GND SPOILER PROXIMITY SENSOR IAW CRJ-AMM-27-63-07. OP CHECKS GOOD.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 34,667 hrs · 21,910 cycles

CORROSION ON SEAT TRACK LBL 9 BETWEEN FS 427 - 437. REMOVED AND REPLACED DAMAGED FLOOR RAIL AT LBL 9 BETWEEN FS 427-437 IAW AMM 53-00-49.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 34,667 hrs · 21,910 cycles

RIGHT SIDE SEAT TRACK HAS CORROSION AT BS 581 - 677 STR 15R. REMOVED AND REPLACED RT SIDE SEAT TRACK AT BS 581 - 677, STR 15R IAW AMM 53-00-49.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 34,667 hrs · 21,910 cycles

POSSIBLE CORROSION ON LT INBD SEAT TRACK AT BS 477 - 581. INSTALLED NEW LT SEAT TRACK IAW AMM 53-00-49.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 34,667 hrs · 21,910 cycles

POSSIBLE CORROSION ON LT INBD SEAT TRACK AT BS 581 - 693. INSTALLED NEW L/H SEAT TRACK IAW AMM 53-00-49.

Part: SEAT BACK — OUT OF ADJUST (ZONE 200) · airframe 35,142 hrs · 28,709 cycles

RH OVERWING EXIT RUBS ON THE BACK OF SEAT 10D. ADJUSTED SEAT BACK AT 10D IAW CMM 25-26-24. OPS CHECKED GOOD.

Part: WARNING LIGHT — ILLUMINATED (ZONE 800) · airframe 25,746 hrs · 24,920 cycles

LEFT EMERGENCY DOOR CAUTION. IAW TELECON WITH MXC DEFERRED LT EMERGENGY DOOR INDICATION IAW MEL 52-70-03 CAT -C- ON OCN 70102521.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 34,667 hrs · 21,910 cycles

POSSIBLE CORROSION ON RT INBD SEAT TRACK AT BS 477 - 581. INSTALLED THE NEW RT SEAT TRACK AT IAW AMM 53-00-49.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 34,667 hrs · 21,910 cycles

POSSIBLE CORROSION ON RT INBD SEAT TRACK AT BS 581 - 693. INSTALLED NEW RT SEAT TRACK IAW AMM 53-00-49.

Part: STRIP — FAULTED (ZONE 800) · airframe 33,338 hrs · 26,300 cycles

RIGHT EMERGENGY DOOR CAUTION ON LANDING. REMOVED AND REPLACED TEFLON STRIP FOR RT EMERGENCY DOOR IAW AMM 52-70-10. OPS CHECKED GOOD IAW AMM 52-70-10.

Part: COMPUTER — FAULTED (STALL SYS) · airframe 35,142 hrs · 28,709 cycles

STALL FAIL CAUTION MESSAGE IN FLIGHT. R & R STALL PROTECTION COMPUTER IAW AMM 27-35-01. OPS CHECKED GOOD, NO CURRENT FAULTS AT THIS TIME.

Part: O-RING — DAMAGED (HYD SYSTEM) · airframe 36,402 hrs · 27,785 cycles

HYD 1 LOW PRESSURE CAUTION MESSAGE IN FLIGHT (QTY 0). R & R HYD NR 1 PRESSURE TRANSDUCER O-RING IAW AMM 29-31-01. OPS CHECKED GOOD. NO LEAKS NOTED. OK FOR SERVICE AT THIS TIME.

Part: CLAMP — GROUND DAMAGE (ZONE 800) · airframe 48,787 hrs · 38,917 cycles

GROUND CREW HIT PAX DOOR STAIRS WITH BOARDING RAMP TWICE. REMOVED AND REPLACED MAIN PAX DOOR AFT COUNTER BALANCE ACTUATOR CLAMP IAW AMM 52-11-17, OPS CHECKED GOOD.

Part: ANTENNA — DIRTY (ZONE 100) · airframe 40,681 hrs · 38,565 cycles

GLD USAFE CAUTION MESSAGE 65 KIAS LOW ENERGY.( MOMENTARILY.) CLEANED ANTENNAS AND PREFORMED OPS TEST OF RADAR ALTIMETER SYSTEM. NO DEFECTS NOTED IAW AMM 34-44-01. MESSAGE NO LONGER PRESENT.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 34,667 hrs · 21,910 cycles

LEFT SIDE SEAT RAIL HAS CORROSION AT FS 677 THROUGH FS 761. REMOVED AND REPLACED LT SIDE SEAT RAIL AT FS677-FS761 IAW AMM 53-00-49.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 34,667 hrs · 21,910 cycles

LEFT SIDE SEAT RAIL HAS CORROSION AT FS 379-FS 485 STGR 15L. REMOVED AND REPLACED LT SIDE SEAT RAIL AT FS379- FS485 STGR 15L IAW AMM 53-00-49.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 34,667 hrs · 21,910 cycles

LEFT SIDE SEAT RAIL HAS CORROSION AT FS 565-FS 677 STGR 15L. REMOVED AND REPLACED LT SIDE SEAT RAIL AT BS 565 - 677, STGR 15L IAW AMM 53-00-49.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,667 hrs · 21,910 cycles

LEFT SIDE SEAT TRACK HAS CORROSION AT FS 485-FS 565 STGR 15L. REMOVED AND REPLACED LT SIDE SEAT TRACK AT BS485 - 565 IAW AMM 53-00-49.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,667 hrs · 21,910 cycles

POSSIBLE CORROSION ON RT SIDE SEAT TRACK STRUCTURE FROM BS 485 - 565 STGR 15R NEEDS EVAL. REMOVED AND INSTALLED NEW SEAT TRACK IAW SRM 53-31-49.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 36,864 hrs · 34,591 cycles

ROW 7 EMERGENCY FLOODLIGHT INOPERATIVE. IAW TELECON WITH MXC DEFERRED ROW 7 CEILING EMERGENCY FLOOD LIGHT IAW MEL 33-51-01B, CAT C ON OCN 70102340.

Part: FAULT MESSAGE — ILLUMINATED (NR 1 IDG) · airframe 45,984 hrs · 35,386 cycles

IDG 1 FAULT MESSAGE B1-007096, IDG1, INTERNAL FAULT. AS PER TELECON WITH MXC, DEFERRED IDG 1 FAULT MESSAGE ON OCN 70102179 PER MEL 24-11-01A CATEGORY A.

Part: FAULT MESSAGE — ILLUMINATED (NR 1 IDG) · airframe 45,984 hrs · 35,386 cycles

IDG 1 FAULT 1 MESSAGE (REPEAT). ALREADY ON DEFERRAL PER MEL 24-11-01A CAT A OCN 70102171.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 46,320 hrs · 341,565 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT IS INOPERATIVE. R & R RT OVERWING EMERGENCY EXIT LIGHT IAW AMM 33-51-15.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 46,000 hrs · 35,439 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT IS INOPERATIVE. R & R RT OVERWING EMERGENCY EXIT LIGHT IAW AMM 33-51-15.