N373DL, cancelled Dec 20, 2006
Service difficulty reports · 36
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 = 'N373DL' AND deregistration_id = 'N373DL-2006-12-20' 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 = 'N373DL' AND deregistration_id = 'N373DL-2006-12-20' 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 DL73S060004Power Supply · inoperativeL1 AND R1 EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AND POWER SUPPLY.SDR DL73S050625Floorbeam · crackedDURING INSPECTION PER SI 3-56673-12, AN EXISTING REPAIR/MODIFICATION WAS FOUND TO BE CRACKED IN THE UPPER FORWARD HOLE OF THE WEB DOUBLER, WEB, UPPER CHORD, AND MOD CHANNEL AT RBL 24.8 AND LBL 24.8. CRACKS WERE REMOVED, WEB DOUBLERS, CHORDS, AND MOD CHANNELS SDR DL73S050233Tire · damagedNR 2 MAIN TIRE LOST CAP ON OUTBOUND HOU /AFTER LOSS OF A-SYSTEM HYDRAULICS, CREW MANUALLY EXTENDED GEAR, LANDED IN ATL WITHOUT INCIDENT. TIRE REMAINED INFLATED /DAMAGE TO LEADING EDGE OF MID FLAP AND HYDRAULIC LEAK PRESENT DUE TO DAMAGED LINES IN WHEEL WELL. SDR DL73S041119Pump · failedLOSS OF A-SYSTEM HYDRAULIC PRESSURE IN FLIGHT. REPLACED BOTH ENGINE PUMPS DUE A-SYSTEM CONTAMINATION.SDR DL73S040840Socket · burnedON GO-AROUND IN ATL STRONG BURNING ODOR WAS DETECTED IN CABIN AND COCKPIT. ODOR DISSIPATED IN APPROX 3 MIN. REPLACED LIGHT SOCKET AT SEAT 13A.SDR DL73S040566Web · crackedFUSELAGE SHEAR BEAM WEB CRACKED AT STRINGER 18A AND STA 727. AREA REPAIRED IAW ERA 090776-14.SDR DL73S040571Attach Fitting · damagedVERTICAL STABILIZER ATTACH LUG FOUND TO HAVE A THINNER FLANGE THAN BLUEPRINT. AREA REPAIRED IAW ERA 090968-14AD.SDR DL73S040570Attach Fitting · corrodedHORIZONTAL STABILIZER FRONT AND REAR SPAR ATTACH LUGS CORRODED. AREA REPAIRED IAW ERA 090805-14AD.SDR DL73S040564Skin · crackedFUSELAGE SKIN AND STRINGER CRACKED AT STA 525 AND STR 16L. ERA 091121-14 COMPLIED WITH FOR REPAIR.SDR DL73S040560Frame · dentedINNER FLANGE OF FRAME AT STATION 500 DENTED BETWEEN STRINGERS 24R AND 25R. AREA REPAIRED IAW 090636-14.SDR DL73S040559Skin · crackedFUSELAGE SKIN AT THE R1 DOOR LOWER AFT CORNER WAS FOUND WITH A FATIGUE CRACK. AREA HAD BLIND FASTENER REPAIR INSTALLED AND PERMANENT REPAIR INSTALLED PER ER/A 363957-14.SDR DL73S040558Skin · crackedCRACKS IN FUSELAGE SKIN AT STATION 380 BETWEEN S-17L AND 18L. AREA REPAIRED IAW ERA 090754-14.SDR DL73S040557Floorbeam · crackedFUSELAGE CABIN FLOORBEAM AT STATION 520 FOUND WITH A CRACK AT THE UPPER CHORD. AREA REPAIRED IAW ERA 090614-14.SDR DL73S040555Fitting · corrodedCORROSION ON THE MLG SIDE STRUT ATTACH AT FUSELAGE STA 685 MLG FITTING. AREA REPAIRED IN ACCORDANCE WITH ERA 090842-14.SDR DL73S030404Skin · crackedTHE FUSELAGE SKIN WAS FOUND WITH A 3 INCH CRACK JUST BELOW STRINGER 18R AT FS 750. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER THE B737-200 SRM AND PER ER/A 384987-14.SDR DL73K021468Transceiver · failedWX RADAR INOP. ANT FAULT MSG DISPLAYED. REPLACED RADAR TRANSCEIVER. RADAR TEST NORMAL.SDR DL73K021333Hydraulic System · lowSYSTEM A HYD QTY INDICATOR DROPPED TO 1.5 GALLONS FOLLOWED BY ILLUMINATION OF SYSTEM B LOW QTY LIGHT. ABNORMAL PROCEDURES FOLLOWED. A/C ARRIVED WITH A SYSTEM AT 2.5 GAL. SERVICED TO FULL EXERCISED FLAPS/SLATS AND SPOILERS OPERATED GEAR HANDLE. PERFORMED YASDR DL73K021315Tire · separatedON WALK AROUND FOUND TIRE TREAD MISSING ON NR 4 MAIN TIRE. TREAD SEPARATION CAUSED DAMAGE TO THE RT INBD UNDERWING FIXED PANEL, RT TRAILING EDGE MID FLAP AND BROKE THE INNER AND CENTER RT GEAR DOORS. REPLACED WHEEL ASSY AND REPAIRED DAMAGE.SDR DL73K021167Skin · crackedTHE FUSELAGE SKIN WAS FOUND WITH A 1.375 CRACK ALONG THE MILL LINE JUST ABOVE STRINGER 16L AT FS 525, AFT OF THE WING SCANNING LIGHT CUTOUT. THE CRACK WAS REMOVED WITH A CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL DOUBLER PER B737 SRM AND ERSDR DL73K020182Torque Link · failedAT 100 KTS LANDING ROLLOUT, NOSE WHEEL HAD SEVERE SHIMMY. REPLACED TORQUE LINK ASSY.SDR DL73K011916Skin · crackedFUSELAGE / SKIN / FS 727B / STRG. 18R : CRACK REPAIR INSPECTION OF THE FUSELAGE SKIN REVEALED A 5" CRACK JUST ABOVE STRINGER 18R AT FS 727B. THE CRACK WAS REMOVED WITH A CUTOUT IN THE SKINSDR DL73K011846Power Supply · discharged2L EMERGENCY EXIT LIGHT INOP. REPLACED POWER SUPPLY.SDR DL73E010629Light · corrodedAFT LEFT SLIDE EMERGENCY LT INOPERATIVE. REPLACED LIGHT ASSYSDR DL73E010628Battery · dischargedAFT RT SLIDE EMERGENCY LT INOPERATIVE AND 1 CABIN AISE EMER. LT I INOPERATIVE. REPLACED BATTERYSDR DL73E001322Frame · tool damageTHE LT SIDE FRAME AT STA 747 WAS GOUGED DURING FASTENER REMOVAL. DAMAGE LOCATED AT THE UPPER END OF THE FRAME AND LOCATED IN THE RADIUS. ER/A 334653-14.SDR DL73E001321Skin · fatiguedDURING ACCOMPLISHMENT OF S/B 737-53-1116 REV 3, SEVERAL DEVIATIONS WERE REQUIRED TO ACCOMPLISH REPAIR (FASTENER SUB). ER/A 334616-14AD.SDR DL73E001320Frame · tool damageTHE SIDE FRAME AT STA 907 ON LHS SUSTAINED TOOLING DAMAGE BETWEEN THE 3RD AND 4TH FASTENERS FROM THE UPPER EDGE OF THE FRAME SPLICE. ER/A 334646-14 REV A.SDR DL73E001327Frame · tool damagePILOT HOLE FOUND IN THE I/B FLANGE OF THE FS 927 FRAME AT S-14R. HOLE COMMON TO LOWER FRAME AND STRAP. ER/A 334668-14.SDR DL73E001024Skin · crackedTHE FUSELAGE SKIN, BONDED DOUBLER, AND BEAR STRAP WERE FOUND WITH A TYPICAL CRACK IN THE LOWER FORWARD CORNER OF THE AFT ENTRY DOOR CUTOUT (L2). THE CRACK WAS REMOVED IN ALL THREE MEMBERS WITH A 1.9 CUTOUT. THE CUTOUT WAS REPAIRED WITH THREE EXTERNAL ALUMISDR DL73E991540Power Supply · inoperativeWHITE EMERGENCY TRACK LIGHTS OUT ROW 16 TO ROW 21. FOUND MID AND AFT BATTERY PACK AND PWR SUPPLY BAD. REPLACED SAME, OPS NORMAL.SDR DL73E990719Coffeemaker · smokingABOUT 15 MIN AFTER T/O AT APPROX 20,000 ALT, F/A REPORTED A STRONG ELECT SMELL IN AFT LAV AREA. SHUT OFF GALLEY PWR AND PULLED AFT LAV C/B. RETURNED TO CVG. ON DESCENT, F/A REPORTED SMELL DIMINISHING. INSPECTED, SUSPECT BURNING COFFEE.SDR DL73E981814Hinge · failedRT I/B LEADING EDGE FLAP SKIN BENT/CRACKED AT UPPER I/B EDGE DUE TO FAILURE OF I/B HINGE.SDR DL73E981677Skin · crackedTHE UPPER OUTBD CORNER OF THE L1 COCKPIT WINDOW WAS FOUND WITH A .75 INCH LONG CRACK IN THE SKIN AND UNDERLYING GUSSET ALONG THE C-D WINDOW POST. THE GUSSET CRACK WAS STOP DRILLED AND THE SKIN CRACK TRIMMED OUT. AN EXTERNAL STEEL DOUBLER AND ALUMINUM TRISDR DL73E970098Dnlock Light · malfunctionedLT MAIN LANDING GEAR DOWN AND LOCKED LIGHT DID NOT ILLUMINATE ON LANDING. A/C ARRIVED GATE LT GREEN LIGHT ON. SLUGGED LEFT GEAR LIGHT, CHECKED GOOD. READJUSTED LANDING GEAR ASSY UNIT AS PRECAUTIONARY. PERFORMED TEST PFHB PER CHAPTER 32 OF M/M, ALL CHECKED SDR DL73E961584Bulkhead Web · crackedDURING ACCOMP OF SI 3-69482-12, TWO CRACKS WERE DISCOVERED ON THE FORWARD FACE OF THE BS 178 BULKHEAD WEB. FIRST CRACK IS LOCATED UNDER THE RBL 5.7 VERTICAL STRAP AT APPROXIMATELY WL 202 AND THE SECOND IS LOCATED UNDER THE LBL 5.7 VERTICAL STRAP, RANGING BETWSDR DL73E952016Le Skin · dentedDURING SHOP INSPECTION, VERTICAL STABILIZER L/E WAS FOUND DENTED BEYOND LIMITS. REPAIRS ACCOMPLISHED PER SRM 55-30-6.
Back to N373DL, cancelled Dec 20, 2006