N927HA

Service difficulty reports not matched to an aircraft · 18

They name N927HA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N927HA' AND registry_match IS NULL
  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 HNAA0200083Windshield · crackedL/H Forward Sindshield shattered in flight at 16,000 FT. A/C diverted to GSP the windshield fram was inspected and the windscreen replaced.Nov 21, 2002 · N927HA · Dhav DHC8102 · Flight Compartment WindowsSDR HNAA0200081Windshield · crackedAfter Take-off F/O's windshield cracked. A/C returned to DCA where windshield was replaced.Nov 19, 2002 · N927HA · Dhav DHC8102 · Flight Compartment WindowsSDR HNAA0200024Cable · brokenDuring aircraft taxi from terminal to hanger by maintenance, there was a loss of right brake control. Subsequent inspection found broken cable at #1 brake valve.Mar 2, 2002 · N927HA · Dhav DHC8102 · BrakeSDR HNAA0200014Frame · corrodedAT LEFT HAND EMERGENCY EXIT CORROSION FOUND ON FRAME AT STATION X366 AFT SIDE BELOW EMERGENCY EXIT. FRAME THICKNESS IS .040. DEPTH OF CORROSION AT EDGE OF FRAME IS .012. REPAIRED FRAME AREA IAW EO8-53-02-0141. BLEND OUT CORROSION, FABRICATED A REPAIR STRAP Feb 2, 2002 · N927HA · Dhav DHC8102 · Fuselage Main, FrameSDR HNAA0200013Skin Panel · corrodedSkin corroded and cracked at station x182 and stringer 33. Replaced skin panel.Jan 19, 2002 · N927HA · Dhav DHC8102 · Fuselage Main, StructureSDR HNAA0200016Seat Track · corrodedRT INBOARD SEAT RAIL CORRODED BETWEEN STATION X182 TO X222. REMOVED AND REPLACED SEAT RAIL IN ACCORDANCE WITH RD8-53-3074.Jan 18, 2002 · N927HA · Dhav DHC8102 · Fuselage, Seat/Cargo Attach FittingsSDR HNAA0200015Gusset · corrodedFOUND CORROSION ON GUSSET AT STATION X354 STRINGER 21 RT. MFG NEW GUSSET AND INSTALLED.Jan 18, 2002 · N927HA · Dhav DHC8102 · Fuselage Miscellaneous StructureSDR HNAA0100025Engine · defectiveSMOKE IN CABIN AND FLIGHT COMPARTMENT, SMELLED LIKE HOT DUCT. DECLARED EMERGENCY AND DIVERTED TO BUFFALO. AIRCRAFT FERRIED TO SBY. FOUND OIL IN HEAT EXCHANGER AND AIR CYCLE MACHINE DUCTING. REMOVED AND REPLACED ACM AND HEAT EXCHANGER. ON 15 APRIL PROBLEM Apr 13, 2001 · N927HA · Dhav DHC8102 · Engine (Turbine/Turboprop)SDR HNAA0100024Ballast · overheatedF/A NOTICED SMOKE AND ELECTRICAL SMELL IN CABIN. FOUND CENTER OVERHEAD LIGHT AT ROW 8 DIM AND BALLAST EXTREMELY HOT TO THE TOUCH. REPLACED THE LUMINAIRE/BALLAST ASSY.Apr 11, 2001 · N927HA · Dhav DHC8102 · Passenger Compartment LightingSDR HNAA9900140Smoke Detector · malfunctionedBAGGAGE SMOKE WARNING LIGHT ILLUMINATED INFLIGHT AND EXTINGISHED ON LANDING. COULD NOT DUPLICATE PROBLEM ON GROUND. REMOVED AND REPLACED NUMBER 1 SMOKE DETECTOR, OPS CHECK GOOD.Oct 29, 1999 · N927HA · Dhav DHC8102 · Smoke DetectionSDR HNAA9900019Retract Mech · malfunctionedLANDING GEAR DOORS WOULD NOT CLOSE UNTIL NOSE GEAR TOUCHED DOWN ON LANDING. REPLACED 3261-K9 (P/N DSC182-2) RELAY.Jan 27, 1999 · N927HA · Dhav DHC8102 · Landing Gear Door Retract SectionSDR HNAA9892794Skin · corrodedUNDER COCKPIT FLOOR MINOR SURFACE CORROSION TO THE SKIN ADJACENT TO STRINGER 31 RT, .020 DEPTH CORROSION TO THE SKIN APPROXIMATELY 3 INCHES LONG AT STRINGER 32 RT. STRINGER 31 RT BETWEEN STATION 167.00 AND STATION 182.00 CORRODED APPROXIMATELY 11 INCHES EXCEEDec 21, 1998 · N927HA · Dhav DHC8102 · Fuselage Main, Plate/SkinSDR HNAA9892793Stringer · corrodedJAX - FOUND CORROSION ON STRINGER 31 RT BETWEEN STATION 167 AND 182 WITH A LOSS OF 50 PERCENT OF MATERIAL. REPAIRED IAW RD8-53-1243. (M)Nov 28, 1998 · N927HA · Dhav DHC8102 · Fuselage Main, Longeron/StringerSDR HNAA9892792Stringer · corrodedJAX - CORROSION WAS REPAIRED ON STRINGER 32 RT IAW EO8-53-98-385. (M)Nov 28, 1998 · N927HA · Dhav DHC8102 · Fuselage Main, Longeron/StringerSDR 95ZZZX4242Eel Batt Packs · failedPHN/BWI - FLT 3260 - DURING PRE-FLIGHT WALK-AROUND, FOUND NUMEROUS INTERIOR AND EXTERIOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED THE EMERGENCY BATTERY PACKS AT LOCATIONS PS6 AND PS3.Jul 29, 1995 · N927HA · Dhav DHC8102 · Emergency LightingSDR 95ZZZM130Auto Feather Lts · malfunctionedFLT 3068 - PHL-LYH - AIRCRAFT RETURNED TO THE GATE WHEN THE AUTO FEATHER LIGHTS WOULD NOT ILLUMINATE DURING STATIC TEST WHILE ENGINES WERE RUNNING, BUT THE PROPELLERS WERE FEATHERING. REMOVED AND REPLACED THE DC REMOTE CONTROL CIRCUIT BREAKER, NO FIX. PULLEDMay 12, 1995 · N927HA · Dhav DHC8102 · Propeller Indication SystemSDR 95ZZZZ94Prop · out of balanceFLT 72 - ORF-PHF - AIRCRAFT HAS VIBRATION ABOVE 180 KNOTS. AIRCRAFT TURNED BACK TO ORF AND LANDED WITHOUT INCIDENT. PERFORMED PROP BALANCE AND ADJUSTED PROP BALANCE WEIGHTS ON NR 1 PROP.Jan 22, 1995 · N927HA · Dhav DHC8102 · Propeller AssemblySDR 95ZZZZ93Oil · req'd serviceFLT 3264 - EWN-CLT - NR 2 ENGINE OIL PRESSURE CAUTION LIGHT AND ENGINE OIL PRESSURE GAUGE ILLUMINATED AFTER TAKEOFF. AIRCRAFT TURNED BACK AND LANDED IN EWN WITHOUT INCIDENT. CHECKED NR 2 ENGINE FOR OIL LEAKS, NO LEAKS FOUND. SERVICED WITH 2 QUARTS OF OIL. Jan 20, 1995 · N927HA · Dhav DHC8102 · Turbine Engine Oil System
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