N792CP
Service difficulty reports · 24
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 = 'N792CP' 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.
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 = 'N792CP' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR SROM2025120479202Tire · separatedDURING TAKEOFF THE NR 1 MAIN LANDING GEAR TIRE TREAD SEPARATED FROM THE TIRE CASING IN SEVERAL LARGE PIECES AND WAS LEFT ON THE RUNWAY. WHEN THE TIRE TREAD SEPARATED IT CAUSED MINOR DAMAGE (DENTS) TO TWO OF THE SHOCK STRUT FAIRINGS REQUIRING THEM TO BE REPLACSDR SROM202311210001Threshold · corrodedMED THRESHOLD MEMBER PN: 85329539 CORRODED AT SCREW HOLES AND BEYOND MANUFACTURES LIMITS. PART REPLACEMENT IS REQUIRED.SDR SROM09122022Bracket · looseTHE THIRD OCCURRENCE OF N. DOOR GEAR DOOR ADVISORY LIGHT ILLUMINATED AFTER NORMAL GEAR EXTENSION OR RETRACTION. THE FOLLOWING TROUBLESHOOTING AND COMPONENT REPLACEMENTS/MAINTENANCE ACTIONS WERE TAKEN.
FIRST OCCURRENCE; FOUND NOSE GEAR CLOSED PROXIMITY SENSORSDR SROM0523202204Cleat · corrodedFUSELAGE FRAME UNDERFLOOR FS X156.00 STR. 24P CORROSION ON UPPER AND LOWER SURFACES OF BRACKET. CORROSION BEYOND MANUFACTURES LIMITS, PART REPLACEMENT REQUIRED. NOTE: RESUBMITTING THIS SDR DUE TO A CORRECTED PN. PN 85328131-120 WAS LISTED ON ORIGINAL SDR ASDR SROM06222022Cleat · corrodedFUSELAGE FRAME UNDERFLOOR FS X236.00 STR. 27P, LIGHT CORROSION FOUND ON BRACKET SURFACE. POSSIBLE CORROSION UNDER FASTENER. DISASSEMBLY MAY BE REQUIRED. AFTER DISASSEMBLY, IT WAS DETERMINED THAT CLEAT PN 85328131-164 NEEDED TO BE REPLACED DUE TO CORROSION.SDR SROM06142202Bracket · corrodedLH OUTBD FLAP, AFT FAIRING 526AB ATTACHMENT BRACKET INBD LUG HAS CHAFFING MARK, BOLTS FOUND LOOSE. AREA 1. DAMAGE DEPTH 0.003", LENGTH 0.570", WIDTH 0.200". AREA 2. DAMAGE DEPTH 0.015", LENGTH 0.100", WIDTH 0.400". AREA 3. DAMAGE DEPTH 0.025", LENGTH 1.300"SDR SROM06142201Hinge · corrodedRH INBD SPOILER, INBD HINGE, CHAFING WEAR ON BOTH AIRCRAFT FITTING AND SPOILER FITTING. DAMAGE MAX DEPTH IS 0.018", MAX WIDTH IS 0.600" AND DAMAGE LENGTH IS 1.700".SDR SROM060820221Skin · corrodedUPPER FUSELAGE OUTER SKIN AT FS X469 TO FS X553 BETWEEN STR. 12S AND 3S CHAFED ALONG WITH TO FUSELAGE FAIRING SEAL (AFT RG WING TO FUSELAGE FAIRING).SDR SROM060720223Hinge Bracket · corrodedCHAFING DAMAGE ON LOWER HINGE BRACKET OF RUDDER FITTING OF AIRCRAFT (LOWER FITTING).SDR SROM060720222Skin · corrodedUPPER FUSELAGE OUTER SKIN AT FS X321 TO FS X373 AND STR 12P AND 12S CHAFED.SDR SROM060720221Skin Panel · corrodedUPPER FUSELAGE OUTER SKIN AT FSX69 TO FSX553 AND STR12P TO STR3P CHAFED ALONG WING TO FUSELAGE FAIRING SEAL (AFT LH WING TO FUSE FAIRING).SDR SROM06012022Intercostal · corrodedCORROSION FOUND ON FLOOR PANEL SUPPORT INTERCOSTAL STA. X1.000 AND LBL33. CORROSION OUT OF LIMITS AND REQUIRES AN RD TO SPLICE A REPLACEMENT SECTION.SDR SROM0523202208Bracket · corrodedFUSELAGE FRAME FS X216.00, STRINGER Y24P FLOORBOARD BRACKET MOUNT HOLE CORROSION DAMAGE. CORROSION BEYOND MANUFACTURES LIMITS, REPLACEMENT REQUIRED.SDR SROM0523202207Cleat · corrodedFUSELAGE FRAME UNDERFLOOR FS X236.00 CORROSION ON BRACKET SURFACE UNDER FASTENER AT STR. 24S, 25S, AND STR. 26S. CORROSION BEYOND MANUFACTURES LIMITS, PART REPLACEMENT REQUIRED.SDR SROM0523202206Cleat · corrodedFUSELAGE FRAME FS X 216.00, STR. 24P, CORROSION BETWEEN CLEAT AND STR. 24P. CORROSION BEYOND MANUFACTURES LIMITS, PART REPLACEMENT REQUIRED.SDR SROM0523202205Cleat · corrodedFUSELAGE FRAME UNDERFLOOR FS X156.0 STR. 24S CORROSION ON LOWER SURFACE OF BRACKET. CORROSION BEYOND MANUFACTURES LIMITS, REPLACEMENT REQUIRED.SDR SROM0523202203Cleat · corrodedFUSELAGE FRAME UNDERFLOOR FS X136.00 STR. 24P CORROSION ON UNDERSIDE OF BRACKET. CORROSION BEYOND MANUFACTURES LIMITS, PART REPLACEMENT REQUIRED.SDR SROM0523202202Cleat · corrodedFUSELAGE FRAME UNDERFLOOR FS X236.00, STR. 25P, CORROSION FOUND ON SURFACE OF BRACKET. CORROSION OUT OF MFG. LIMITS, REPLACEMENT REQUIRED.SDR SROM051220223Shear Web · corrodedBAGGAGE COMPARTMENT AFT SHEAR WEB PN: 85339527-107SP CORRODED AT FS STA. X707 AND LBL 35. THIS CORROSION FALLS OUTSIDE THE ALLOWABLE BLEND AREA OF SRM 53-40-43. REPLACEMENT IS REQUIRED.SDR SROM051220222Shear Web · corrodedBAGGAGE COMPARTMENT AFT SHEAR WEB PN: 85339627-111 CORRODED AT MULTIPLE SPOTS BETWEEN FS STA. X712 - X788. SRM 53-40-43 ALLOWS SOME BLENDING BUT DOES NOT ALLOW BLENDING AROUND THE RADIUS OF A LIGHTNING HOLE. CORROSION AT STA. X771 IS IN THE STAY-OUT AREA OFSDR SROM05122022Threshold · corrodedPASSENGER MAIN ENTRANCE DOOR THRESHOLD SUPPORT CHANNEL PN: 85329540-001 CORRODED ON UPPER AND LOWER SURFACE. SRM 53-20-23-02-01 ONLY ALLOWS BLENDING OF THE UPPER SURFACE, REPLACEMENT REQUIRED.SDR SROM042722None · corrodedLH AFT SEAT FLOOR RAIL P/N: 85338210-111 CORRODED AT AFT TIE DOWN RING IN AFT BAGGAGE COMPARTMENT. MEASURED AT 0.060" BEFORE BLENDING AND LIMIT IS 0.040" PER SRM 53-40-49. NEW REPLACEMENT FLOOR RAIL WILL BE INSTALLED.SDR SROM03022022Power Supply · failedLEFT AFT PAX DOOR EMERGENCY EXIT SIGN INOP. CORRECTION: REPLACED EMERGENCY LIGHTS POWER SUPPLY IAW Q400 AMM 33-51-01-400-801. OPERATIONAL CHECK GOOD.SDR SROM020200718201I/O Module · malfunctionedRIGHT FUEL TANK TEMP INDICATED +99°C WITH FIRE BELL. REMOVED AND REPLACED THE RT FUEL HEATER THERMAL ACTUATOR INAW DHC-8-400 AMM 73-11-05 (FOR THE FUEL OVERHEAT). SWAPPED INPUT/OUTPUT MODULE (IOM) POSITIONS IAW Q400 AMM 31-41-11 (FOR TROUBLE SHOOTING THE F
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