N279MQ

Service difficulty reports · 18

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N279MQ' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR SIMA202511140001Battery · no testCEILING PANEL AT ROW 9 HAS EMERGENCY LIGHT THAT FAILED TO LIGHT UP DURING OPS CHECK. FOUND EMERGENCY LIGHT AT ROW 9 INOPERATIVE. R & R EMERGENCY LIGHT POWER UNIT IAW AMM 33-50-01 OPS CHECKED GOODNov 10, 2025 · N279MQ · Emb ERJ170200LR · Emergency LightingSDR SIMA20250714001Module · failedDURING TAKEOFF AND BELOW 80 KNOTS MASTER CAUTIONS GND PROX FAIL, TERRAIN FAIL, AND WINDSHEAR FAIL APPEARED. REJECTED TAKEOFF INITIATED AND AIRCRAFT REACHED A SPEED OF 110KIAS MAX. MASTER CAUTIONS EXTINGUISHED AS THRUST LEVERS WERE PULLED BACK TO IDLE. THRUST RJul 14, 2025 · N279MQ · Emb ERJ170200LR · Navigation SystemSDR SIMA20250130002Seat Track · corrodedRH SEAT TRACK IN FWD WET AREA HAS CORROSION AT FR13 Y+10. (MAJOR REPAIR) INSTALLED EWIS PROTECTION PER EMB 175 SWPM 20-67-00.REMOVED CORROSION PER EMB 175 SRM 51-10-03, BLENDED AREA MEASURES L=.5 W=.25 H=.030. DAMAGE FOUND TO BE OUT OF ALLOWABLE LIMITS PER EMBJan 30, 2025 · N279MQ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR SIMA20250110005Seat Track · corrodedCORROSION ON RIGHT HAND LONGITUDINAL SEAT TRACK AT FR 84+2. (MAJOR REPAIR) INSTALLED EWIS PROTECTION PER EMB 175 SWPM 20-67-00 BLENDED AREA AT RH LONGITUDINAL SEAT TRACK AT FR84+2 IAW EMB 175 SRM 51-10-03. DIMENSIONS L=1?, W=2?, H-.020?. UPON FURTHER EVALUATIOJan 10, 2025 · N279MQ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR SIMA20250110004Seat Track · corrodedCORROSION ON RIGHT HAND LONGITUDINAL SEAT TRACK AT FR 84+2. (LEVEL 2 CORROSION) INSTALLED EWIS PROTECTION PER EMB 175 SWPM 20-67-00 BLENDED AREA AT RH LONGITUDINAL SEAT TRACK AT FR84+2 IAW EMB 175 SRM 51-10-03. DIMENSIONS L=1?, W=2?, H-.020?. UPON FURTHER EVALJan 10, 2025 · N279MQ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR SIMA20250110002Floor Support · corrodedRH FLOOR BEAM AT FR 12 TO 13 HAS DAMAGED AND ELONGATED HOLES. (LEVEL 2 CORROSION) DAMAGED AND ELONGATED HOLES DETERMINED TO BE OUT OF LIMITS IAW EMB 175 SRM 51-75-16. REMOVED FLOOR BEAM ON RH PASSENGER FLOOR STRUCTURE FROM FRAME 12 TO 13 IAW EMB 175 SRM 51-40-Jan 10, 2025 · N279MQ · Emb ERJ170200LR · Elevator StructureSDR SIMA20250110003Floor Support · damagedRH FLOOR BEAM AT FR 12 TO 13 HAS DAMAGED AND ELONGATED HOLES. (MAJOR REPAIR) DAMAGED AND ELONGATED HOLES DETERMINED TO BE OUT OF LIMITS IAW EMB 175 SRM 51-75-16. REMOVED FLOOR BEAM ON RH PASSENGER FLOOR STRUCTURE FROM FRAME 12 TO 13 IAW EMB 175 SRM 51-40-08. LJan 10, 2025 · N279MQ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR SIMA20250109001Seat Track · corrodedRH SEAT TRACK IN FWD WET AREA HAS CORROSION AT FR13 Y+10 (LEVEL 2 CORROSION) INSTALLED EWIS PROTECTION PER EMB 175 SWPM 20-67-00. REMOVED CORROSION PER EMB 175 SRM 51-10-03, BLENDED AREA MEASURES L=.5 W=.25 H=.030. DAMAGE FOUND TO BE OUT OF ALLOWABLE LIMITS PEJan 9, 2025 · N279MQ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR SIMA20240703001Light · fadedEMERGENCY PHOTOLUMINESCENT LIGHT STRIP BY SEATS 1FD FADED RAR EMERGENCY PHOTOLUMINESCENT LIGHT STRIP BY 1FD IAW ERJ 175 33-50-21 OPS CHK GOOD NO DEFECTS NOTEDJul 3, 2024 · N279MQ · Emb ERJ170200LR · Emergency LightingSDR SIMA202308072001Unknown · unknownPARKING BRAKE WILL NOT SET-C/A-FOUND EMERGENCY BRAKE HANDLE RELEASE BUTTON STICKY CLEANED BUTTON IAW AMM 12-22-01 OPERATIONAL TEST OF EMERGENCY BRAKE SYSTEM GOOD IAW AMM 32-44-00 -C/A-FOUND EMERGENCY BRAKE HANDLE RELEASE BUTTON STICKY CLEANED BUTTON IAW AMM 12Aug 2, 2023 · N279MQ · Emb ERJ170200LR · Landing Gear Brake SystemSDR SIMA20230414001Unknown · unknownRIGHT MAIN LANDING GEAR WHEEL WELL ELECTRIC FUMES/ ACID ODOR ALSO LIQUID SPILL/ HIDRAULICS-C/A-RESECURED HYD LINE ON #1 BRAKE VALVE & REMOVED AND REPLACED O-RINGS IAW AMM - 32-44-01. NO LEAKS NOTED.Apr 14, 2023 · N279MQ · Emb ERJ170200LR · Master Cylinder/Brake ValveSDR SIMA20221218001Heat Exchanger · fodDURING DESCENT CABIN BECAME HOT FOR ABOUT ONE MINUTE WHICH CAN BE NORMAL BUT FLIGHT ATTENDANT SAID CABIN HAD SMOKEY HAZE FOR ABOUT TWO MINUTES. "TRANSFERRED FROM AML PAGE 4944502 ITEM 1"-C/A-WHILE PERFORMING FIM TASK 21-20-00 FOUND COFFEE RESIDUE ON THE R/H HEDec 18, 2022 · N279MQ · Emb ERJ170200LR · Air Distribution SystemSDR SIMA20220506002Flap · failedAIR INTERRUPT/FLAPS FAIL/OVR WT LANDING/EMERGENCY DECLARED FLAP FAIL CAUTION MSGAPPEARED ON EICAS AFTER TAKE OFF WHEN RETRACTING FLAPS FROM 2 TO 1. RAN QRH FLAP FAIL CHECKLIST FLAP FROZEN AT FLAP 2 SLAT 3 . WINDSHIER FAIL GROUND PROX FAIL ASSOCIATED ON EICAS."May 6, 2022 · N279MQ · Emb ERJ170200LR · Trailing Flap Position Indicating SystemSDR SIMA20220425004Spar · crackedRIGHT WINGTIP IS CRACKED.-C/A-COMPLETE:C/W RAR OF RH WINGLET ASSY IAW AMM 57-30-00Apr 25, 2022 · N279MQ · Emb ERJ170200LR · Wing, Plate/SkinSDR SIMA20220419002Spar · crackedLH WINGLET AT FWD SPAR CRACKED.-C/A-COMPLETE:INSTALLED SERVICEABLE LH WINGLET IAW AMM 57-35-00. REF BOW360927 FOR LH WINGLET FWD SPAR REPAIR.Apr 19, 2022 · N279MQ · Emb ERJ170200LR · Wing, Plate/SkinSDR SIMA2020073026003Processor · malfunctionedMULTI FLT CNTRL FAIL ON DESCENT. EMERGENCY DECLARED. LANDED SAFELY. FOUND FAULT CODE 45452147 CMC. R & R NIC PROC 5 (MAU 3 NIC PROC1) IAW AMM 31-41-02DATA LOAD OK IAW AMM 45-45-00. OPS CHECKED GOODJul 26, 2020 · N279MQ · Emb ERJ170200LR · Central ComputersSDR SIMA201911252002Light · inoperativeEMERGENCY FLOR STRIP 1 LH SIDE INOP-C/A-REMOVED AND REPLACED EMERGENCY FLOOR STRIP 1 LH SIDE IAW ERJ 175 AMM 33-50-21. NO FURTHER DEFECTS FOUND.Nov 22, 2019 · N279MQ · Emb ERJ170200LR · Emergency LightingSDR SIMA201906265002Control Lever · failedFLAPS FAIL ON DEPARTURE. OVERWEIGHT LANDING AT APPOX 79,000 LBS SINK RATE 200 FT PER OR LESS. PERFORMED GVI OF FLAP ACTUATOR TORQUE LIMITER IAW AMM 27-51-01. R & R SLAT/FLAP CONTROL LEVEL UNIT IAW AMM 27-53-01 OPS CHECKED GOOD.Jun 25, 2019 · N279MQ · Emb ERJ170200LR · Trailing Edge Flap Control System
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