N176CA
Service difficulty reports · 109
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 = 'N176CA' 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 = 'N176CA' 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 U2RA201406020001Slide Raft · unserviceableRIGHT DOOR NR 1, SLIDE RAFT FOUND UNSERVICEABLE DUE TO THE RT SIDE BULGING OUT & BENDING RELEASE PINS.SDR U2RA201405270003Battery Pack · dischargedDURING ACCOMPLISHMENT OF TASK CARD 33-004-01-01, THE L2 DOOR EMER LIGHT FAILED THE EMER LIGHT TEST. FOUND BATTERY PACK DEPLETED.SDR U2RA201405270002Stringer · crackedDURING ACCOMPLISHMENT OF ERO 5330ERO1712, INSPECTION NOTED A CRACKED STRINGER. STRINGER 16 LEFT BODY STATION 613. CRACK LENGHT .5".SDR U2RA201405270001Frame · corrodedRIGHT WING TO BODY FAIRING, ATTACH FRAME, HAS CORROSION AT SEVERAL AREAS BS 870, AREAS WERE BLENDED IAW SRM 51-10-02. ORIGINAL MATERIAL THICKNESS OF 0.063 INCHES, LOSS OF MATERIAL .002 INCHES & REMAINING MATERIAL THICKNESS OF .061 INCHES. ALODINED PRIMED & TSDR U2RA201403180003Light · inoperativeEMERGENCY EXIT AISLE LIGHTS INOPERATIVE.SDR U2RA201403180002Battery Pack · dischargedEMERGENCY EXIT LIGHT AT RT NR 2 DOOR INOPERATIVE. FOUND BATTERY PACK DISCHARGED.SDR U2RA201403180001Battery Pack · dischargedEMERGENCY EXIT LIGHT AT L4 DOOR INOPERATIVE. FOUND BATTERY PACK DISCHARGED.SDR U2RA201401270001Battery Pack · dischargedDURING SERVICE CHECK RIGHT NR 4 DOOR EMERGENCY EXIT LIGHT IS INOPERATIVE. FOUND BATTERY PACK DISCHARGED. R & R BATTERY PACK IAW AMM33-51-07. CHECK GOOD.SDR U2RA201310230001Light · inoperativeEMERGENCY EXIT LIGHT ABOVE L1 DOOR INOPERATIVE.SDR U2RA2013F00100Access Door · missingON ARRIVAL, FOUND GROUND AIR SUPPLY ACCESS DOOR MISSING FROM ACFT. NO OTHER DAMAGE NOTED TO ACFT.SDR U2RA201303130001Signal Cond Unit · failedNR 2 ENGINE HIGH VIBRATION INDICATION IN FLIGHT, PRECAUTIONARY ENGINE SHUTDOWN OF THE NR 2 ENGINE ACCOMPLISHED OIL PRESSURE NORMAL. ENGINE WINDMILLED APPROXIMATELY 20 MINUTES. SIGNAL COND. UNIT REPLACEDSDR U2RA2012012126801Lamp · inoperativeEMERGENCY LIGHT OVER SEAT 34ABC INOPERATIVE. REPLACED LAMP IAW AMM 33-21-10. OPS CHECKED GOOD.SDR U2RA201202164861Lever · lack of lubeL1 DOOR DISARMING LEVER HARD TO MOVE BETWEEN ARM AND DISARM. CLEANED AND LUBED DOOR LINKAGE FOR ARMING LEVER IAW MM 12-21-18. OPS CHECKED GOOD AT THIS TIME.SDR U2RA2012113026801Lever · lack of lubeL1 DOOR DISARMING LEVER HARD TO MOVE BETWEEN ARM AND DISARM. CLEANED AND LUBED DOOR LINKAGE FOR ARMING LEVER IAW MM 12-21-18. OPS CHECK GOOD AT THIS TIME.SDR U2RA201211210002Sill · corrodedDURING INSPECTION, FOUND CORROSION AT RT NR 4 PASSENGER DOOR LOWER MAIN SILL. REPAIR PERFORMED IAW SR 2-2346032878.SDR U2RA201211210001Wedge · delaminatedDURING INSPECTION, FOUND NR 1 SLAT T/E WEDGE, FOUND DEBONDED. AREA OF DISBOND 4.5" DIAMETER.SDR U2RA2012112000001Bracket · crackedFOUND BRACKET, CRACKED AT BS 1540.SDR U2RA201211160001Stiffener · crackedSTIFFNER AT LT STRUT ACCESS PANEL 433CL CUTOUT PP STA 153.9, FOUND CRACKED. CRACK LENGTH .7" STIFFNER.SDR U2RA201211150005Scuff Plate · crackedFORWARD CARGO DOOR LOWER SILL SCUFF PLATE, FWD EDGE OTBD CORNER HAS CRACK, CRACK LENGTH 2".SDR U2RA201211150004Fairing · crackedLEFT HORIZONTAL STABILIZER L/E INBD FAIRING 332AL UPPER SURFACE AFT AREA FOUND CRACK.SDR U2RA201211150003Battery Pack · dischargedEMERGENCY LIGHT BATTERY PACK CAN NOT BE DEEP CHARGED.SDR U2RA201211150002Stringer · corrodedMAIN CABIN BS 1600-1620, STRINGER 17R, STRINGER HAS CORROSION, CORROSION LENGTH 1.6", WIDTH .8" DEPTH .016", ORIGINAL MATERIAL THICKNESS .063", REMAINING MATERIAL .047". STRINGER REPAIRED IAW INSTRUCTIONS.SDR U2RA201211150001Retainer · crackedNR 2 ENGINE THRUST REVERSER "C" DUCT T/E UPPER FORWARD RETAINER HAS TWO CRACKS. CRACK ONE LENGTH .25" CRACK TWO LENGTH .5". REPAIRED IAW DWG 5430D1519.SDR U2RA201211140008Floor Support · corrodedFORWARD CARGO BS 640-660, RBL 2.9, FLOOR SUPPORT HAS CORROSION AT ANCHOR NUT ATTACH AREAS, LENGTH 2.5", WIDTH 1", DEPTH .037" ORIGINAL MATERIAL THICKNESS .063", REMAINING MATERIAL THICKNESS .026". FLOOR SUPPORT REPLACED IAW DWG 143N5370.SDR U2RA201211140007Floor Support · corrodedFORWARD CARGO BS 640-660, LBL 7.55", FLOOR SUPPORT HAS CORROSION AT ANCHOR NUT ATTACH AREAS, LENGTH 2.5", WIDTH 1", DEPTH .017", ORIGINAL MATERIAL THICKNESS .063", REMAINING MATERIAL THICKNESS .046", FLOOR SUPPORT REPLACED IAW DWG 143N5370.SDR U2RA201211140006Floor Support · corrodedFORWARD CARGO BS 640-660 LBL 2.9", FLOOR SUPPORT HAS CORROSION AT ANCHOR NUT ATTACH AREAS, LENGTH 2.5", WIDTH 1",DEPTH .023" ORIGINAL MATERIAL THICKNESS .063", REMAINING MATERIAL THICKNESS .040". FLOOR SUPPORT REPLACED IAW DWG 143N5370.SDR U2RA201211140005Frame · corrodedAFT CARGO BS 1640, STRINGER 29L TO 29R FRAME WEB HAS HEAVY CORROSION. REPLACED FROM STRINGER 24L TO S24R IAW DWG 146N1032. REF NRC HFL6086. GENERATED FROM TASK CARD 53-222-00-01.SDR U2RA201211140004Floor Support · corrodedFORWARD CARGO BS 640-660 RBL 7.55" FLOOR SUPPORT HAS CORROSION AT ANCHOR NUT ATTACH AREAS, LENGTH 2.5", WIDTH 1", DEPTH .018", ORIGINAL MATERIAL THICKNESS .063", REMAINING MATERIAL THICKNESS .045". FLOOR SUPPORT REPLACED IAW DWG 143N5370.SDR U2RA201211140003Floor Support · corrodedFORWARD CARGO BS 640-660, LBL 10.45", FLOOR SUPPORT HAS CORROSION AT ANCHOR NUT ATTACH AREAS, LENGTH 2.5" WIDTH 1", DEPTH .029" ORIGINAL MATERIAL THICKNESS .063", REMAINING MATERIAL THICKNESS .034". FLOOR SUPPORT REPLACED IAW DWG 143N5370.SDR U2RA201211140002Fairing · scratchedLEFT HORIZONTAL STABILIZER L/E MID FAIRING 332CL 2 EA AREAS SCRATCHED, (AREA 1 LENGTH 1.2" WIDTH .9", DEPTH .017", ORIGINAL MATERIAL THICKNESS .063", REMAINING MATERIAL THICKNESS .046"). (AREA 2 LENGTH 1.2", WIDTH .9", DEPTH .013" ORIGINAL MATERIAL THICKNESSSDR U2RA201211140001Doubler · corrodedNR 2 PYLON ACCESS PANEL 443LL CUT OUT SKIN DOUBLER HAS CORROSION LENGTH 2.5", WIDTH 1.1", DEPTH .065", ORIGINAL MATERIAL THICKNESS .090", REMAINING MATERIAL THICKNESS .065".SDR U2RA201211130011Floor Support · corrodedAFT CARGO BS 1450-1490, RBL 10.45", FLOOR SUPPORT HAS CORROSION AT ANCHOR NUT ATTACH AREAS, LENGTH 2.5", WIDTH 1" DEPTH .038", ORIGINAL MATERIAL THICKNESS .063", REMAINING MATERIAL THICKNESS .025". REPAIRED IAW SRM 51-70-11.SDR U2RA201211130010Floor Support · corrodedAFT CARGO BS 1460-1490, LBL 70. 55, FLOOR SUPPORT HAS CORROSION AT ANCHOR NUT ATTACH AREAS, LENGTH 1.5",WIDTH 1", DEPTH .038", ORIGINAL MATERIAL THICKNESS .063", REMAINING MATERIAL THICKNESS .025". FLOOR SUPPORT REPAIRED IAW SRM 51-70-11.SDR U2RA201211130009Floor Support · corrodedAFT CARGO BS 1350-1380, RBL 16.1", FLOOR SUPPORT HAS CORROSION AT ANCHOR NUT ATTACH AREAS, LENGTH 1.5",WIDTH 1", DEPTH .021", ORIGINAL MATERIAL THICKNESS .063", REMAINING MATERIAL THICKNESS .042". FLOOR SUPPORT REPLACED5 IAW DWG 146N5417.SDR U2RA201211130008Support · corrodedAFT CARGO BS 1360-1380, LBL 2.9, FLOOR SUPPORT HAS CORROSION AT ANCHOR NUT ATTACH AREAS, LENGTH 1.5, WIDTH 1", DEPTH .038", ORIGINAL MATERIAL THICKNESS .063", REMAINING MATERILA THICKNESS .025". REPLACED FLOOR SUPPORT IAW DWG 146N5417.SDR U2RA201211130007Floor Support · corrodedAFT CARGO BS 1450-1500 RBL 2.9, FLOOR SUPPORT HAS CORROSION AT ANCHOR NUT ATTACH AREAS, LENGTH 1.5", WIDTH 1" DEPTH .038" ORIGINAL MATERIAL THICKNESS .063", REMAINING MATERIAL THICKNESS .025". FLOOR SUPPORT, REPLACED IAW DWG 146N5447.SDR U2RA201211130006Floor Support · corrodedAFT CARGO BS 1460-1500, RBL 7.55" FLOOR SUPPORT HAS CORROSION AT ANCHOR NUT AREAS, LENGTH 1.5, WIDTH 1", DEPTH .038", ORIGINAL MATERIAL THICKNESS .063", REMAINING MATERIAL THICKNESS .025". SUPPORT REPLACED FROM STATION 1450-1500 IAW DWG 146N5447.SDR U2RA201211130005Floor Support · corrodedAFT CARGO BS 1380-1400, RBL 7.55" FLOOR SUPPORT HAS CORROSION AT ANCHOR NUT ATTACH AREAS, LENGTH 1.5", WIDTH 1", DEPTH .038", ORIGINAL MATERIAL THICKNESS .063", MATERIAL THICKNESS REMAINING .025". REPLACED SUPPORT FROM STATION 1340-1445 IAW DWG 146N5417.SDR U2RA201211130004Floor Support · corrodedAFT CARGO BS 1450-1500 RBL 2.9", FLOOR SUPPORT HAS CORROSION AT ANCHOR NUT ATTACH AREAS, LENGTH 1.5", WIDTH 1", DEPTH .038" ORIGINAL MATERIAL THICKNESS .063", REMAINING MATERIAL THICKNESS .025". SUPPORT REPLACED IAW DWG 146N5447.SDR U2RA201211130003Floor Support · corrodedAFT CARGO BS 1360-1380 RBL 10.45", FLOOR SUPPORT HAS CORROSION AT ANCHOR NUT AREAS, LENGTH 1.5", WIDTH 1", DEPTH .035", ORIGINAL MATERIAL THICKNESS .063", REMAINING THICKNESS .028". SUPPORT REPLACED FROM STATION 1340-1445 IAW DWG 146N5417.SDR U2RA201211130002Floor Support · corrodedAFT CARGO BS 1460-1480, LBL 10.45" FLOOR SUPPORT HAS CORROSION ON AT ANCHOR NUT ATTACH AREAS, LENGTH 1.5", WIDTH .5", DEPTH .038" ORIGINAL THICKNESS .063", REMAINING THICKNESS .025". SUPPORT, REPLACED IAW DWG 146N5447. REF NRC HFL5781.SDR U2RA201211130001Floor Support · corrodedAFT CARGO BS 1390-1410, RBL 2.9", FLOOR SUPPORT HAS CORROSION AT ANCHOR NUT ATTACH AREAS, LENGTH 1.5", WIDTH 1", DEPTH .014" ORIGINAL MATERIAL THICKNESS .063", REMAINING MATERIAL THICKNESS .049". SUPPORT REPLACED IAW DWG 146N5417. REF NRC HFL5880.SDR U2RA201211120005Sill · corrodedFORWARD CARGO DOOR CUT OUT BS 560-620 LOWER SILL HAS CORROSION IN NUT PLATE AREA. LENGTH 3.2", WIDTH 1", DEPTH .042". ORIGINAL MATERIAL THICKNESS .300", REMAINING MATERIAL THICKNESS .258".SDR U2RA201211120004Nose Cowl · corrodedNR 1 ENGINE NOSE COWL FOUR O'CLOCK ARE INNER SANDWICH PANEL FOUND CORRODED. NOSE COWL REPLACED.SDR U2RA201211120003Blades · debondedNR 1 ENGINE, NR 14 FAN BLADE FOUND TAP DISPLAY MORE THAN 600 DB AT SEC "C" OUT OF LIMITS IAW SB RB211-72-9660. GENERATED FROM TASK CARD 72-136-01-01.SDR U2RA201211120002Nose Cowl · corrodedNR 1 ENGINE NOSE COWL 11 O'CLOCK POSITION AREA INNER SANDWICH PANEL FOUND CORROSION. REF NRC HFL0717, COWL REPLACED. GENERATED FROM TASK CARD 71-802-50-01.SDR U2RA201211120001Fitting · chafedNR 1 PYLON MID-BULKHEAD RT FITTING, CHAFING, LENGTH 3", WIDTH 1" DEPTH .095", ORIGINAL MATERIAL THICKNESS .388", REMAINING MATERIAL THICKNESS .293". MFG FOUND CONDITION ACCEPTABLE AS IS.SDR U2RA201211110005Web · crackedMAIN DECK BS 400-420 RBL 45" FLOOR SUPPORT INTERCOSTAL WEB, TWO LOCATIONS, CRACKED. CRACK LENGTH .5 INCHES ON AFT UPPER CORNER OF WEB. REPLACED WEB IAW DWG 141N5150.SDR U2RA201211110004Seat Track · corrodedMAIN DECK BS 365-440 RBL 40", SEAT TRACK CORRODED, LENGTH = 4.1", WIDTH = .7", DEPTH = .098", ORIGINAL THICKNESS .225" REMAINING THICKNESS = .127". SEAT TRACK, REPLACED FROM BS 365-440 IAW DWG 141N5131.SDR U2RA201211110003Attach Angle · crackedFORWARD LOWER BODY FAIRING SUPPORT FRAME STA 900. LBL 4 ATTACH CLIP CRACKED, REPLACED IAW DWG 149N7130.
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