N311DL, cancelled Jan 26, 2007
Service difficulty reports · 74
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 = 'N311DL' AND deregistration_id = 'N311DL-2007-01-26' 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 = 'N311DL' AND deregistration_id = 'N311DL-2007-01-26' 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 DL73S060308Skin · crackedTHE FUSELAGE SKIN WAS FOUND CRACKED AT THE LAP JOINT AT S-14L BETWEEN BS 380 AND 500A. THE DAMAGED SKIN WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED.SDR DL73S060307Skin · crackedTHE FUSELAGE SKIN WAS FOUND WITH CRACKS IN THE LAP JOINT AT S-4L BETWEEN BS 727A+19 TO 762. THE DAMAGED SKIN WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED.SDR DL73S060306Skin · crackedTHE FUSELAGE SKIN WAS FOUND WITH CRACKS IN THE LAP JOINT AT BS 400-410. THE DAMAGED SKIN WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED.SDR DL73S060305Skin · crackedTHE FUSELAGE SKIN WAS FOUND WITH CRACKS IN THE LAP JOINT AT S-4L BETWEEN BS 380 AND 500. THE DAMAGED SKIN WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED.SDR DL73S060304Skin · crackedTHE FUSELAGE SKIN WAS FOUND WITH CRACKS IN THE LAP JOINT AT S-4R BETWEEN BS 727A+1 AND 752. THE DAMAGED SKIN WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED.SDR DL73S050574Engine · bird ingestionON T/O AT 1000 FT, HEARD LOUD BANG AND AIRCRAFT YAWED MOMENTARLLY LT AND RT. PASSENGER REPORTED BLUE FLAME FROM FWD OF LT ENGINE. FOWL SMELL IN CABIN. ENGINE PARAMETERS NORMAL. RETURNED TO CVG. FOUND EVIDENCE OF BIRD INGESTION IN NR 1 ENGINE. INSPECTED SSDR DL73S050202Fire Loop · failedCLIMBING THRU 18,000 FT WHEEL WELL FIRE INDICATION. LOWERED GEAR AND INDICATION REMAINED ON. REPLACED DETECTOR LOOP.SDR DL73S050029Shaft · failedFUEL PUMP SHAFT SHEARED AT ROTATION. RUNWAY EXCURSION ON RETURN IN BAD WEATHER. REPLACING NR 2 ENGINE FUEL PUMP AND CONTROL.SDR DL73S040842Skin · crackedINSPECTION OF THE STRINGER 4L SKIN LAP JOINT PER AD 2003-08-15 REVEALED A CRACKED FASTENER LOCATION AT FS 700. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER B737-200 SRM AND PER ER/A 092798-14AD.SDR DL73S040841Skin · crackedINSPECTION OF THE STRINGER 4R SKIN LAP JOINT PER AD 2003-08-15 REVEALED A CRACKED FASTENER HOLE AT FS 631. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER B737-200 SRM AND ER/A 092799-14.SDR DL73S040839Skin · crackedINSPECTION OF THE STRINGER 4R SKIN LAP JOINT PER AD 2003-08-15 REVEALED A CRACKED FASTENER HOLE AT FS 848. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN ALUMINUM REPAIR DOUBLER PER B737-200 SRM AND PER ER/A 092824-14AD.SDR DL73S040838Skin · crackedINSPECTION OF THE STRINGER 4L SKIN LAP JOINT PER AD 2003-08-15 REVEALED A CRACKED FASTENER LOCATION AT FS 500. THE CRACK WAS REMOVED WITH A CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER B737-200 SRM AND PER ER/A 092SDR DL73S040498Pin · brokenFOUND ON SERVICE CHECK, AISLE LIGHTS AT SEAT 22L AND 24L INOP. FOUND PIN BROKE ON M1136 AT STATION L753. REPLACED AND TESTED PER M/M.SDR DL73S040412Battery · inoperativeFWD BULLNOSE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY. CHECKS OK.SDR DL73S040411Fuse · failedAFT LT BULLNOSE EMERGENCY LIGHTS INOPERATIVE, REPLACED BATTERY. NO HELP. REPLACED FUSES ON CHARGER. CHECKS GOOD.SDR DL73S031097Doubler · damagedFOUND ON W-2 LETTER CK, STRINGER 22RT CUT AT STA 957, 977, 996 FOR OUTFLOW VALVE DOUBLER REPLACEMENT. REPAIR PER SRM 53-10-3 FIG 1.SDR DL73S031096Frame · corrodedFOUND ON W2 LETTER CK, CORROSION ON FORMER STA 967 O/B OF STR 27 RIGHT. REPAIRED PER SRM 53-10-4 FIG 11.SDR DL73S031095Frame · corrodedFOUND ON W-2 LETTER CK, CORROSION ON FORMER STA 967 AT SKIN ATTACH ANGLE BETWEEN STR 27 LEFT AND 27 RIGHT. REPAIRED PER SRM 53-10-4 FIG 11.SDR DL73S031094Frame · corrodedFOUND ON W-2 LETTER CK, SKIN BULGED/ RIVETS SHEARED AT FRAME STA 847 BETWEEN STR 27 LEFT AND 27 RIGHT. FOUND FORMER CORRODED AT THIS LOCATION. REPAIRED PER SRM 53-10-4 FIG 9A.SDR DL73S031024Wire · shortedON L/O FOUND EMERGENCY LIGHTS AT SEAT ROWS 22-25 INOP AND L2 EXIT IDENTIFIER INOP. REPAIRED DAMAGED WIRE.SDR DL73K030507Skin · crackedA 3 INCH CRACK WAS FOUND IN THE FUSELAGE SKIN AT FS 525 JUST ABOVE STRINGER 16L RUNNING ALONG THE EDGE OF THE INTERNAL BONDED WAFFLE DOUBLER. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER B737-200 SRM AND PER ERSDR DL73K030504Engine · malfunctionedENG FUEL FLOWS WERE 1500 SPLIT AFTER TAKEOFF. TRIED ENG ANTIICE ON AND MISMATCH ON THROTTLES REVERSED. EPR ON LEFT ENG 1.40 AND ON RIGHT ENG WAS 1.77. AFTER CONSULTATION WITH MAINTENANCE COORDINATOR AND DISPATCH, DIVERTED TO MCO. DUPLICATED ITEM ON R/U. RSDR DL73K021318Skin · corrodedFUSELAGE / SKIN / AFT LAV SERVICE CUTOUT / FS 986.5 / STRG. 27R : CORROSION CUTOUT REPAIR AN AREA OF CORROSION WAS FOUND IN THE SKIN AT THE FWD INBD CORNER OF THE AFT LAVATORY SERVICE DOOR CUTOUT. THE CORROSION WAS REMOVESDR DL73K021215Spar · corrodedTHE CENTER SECTION OF THE HORIZONTAL STAB WAS PREVIOUSLY REWORKED FOR CORROSION IN SEVERAL LUGS. THE REWORK WAS APPROVED FOR A 24 MONTH LIMIT WHICH HAS BEEN REACHED. THE HORIZONTAL STAB WAS REMOVED FROM THE AIRCRAFT AND THE REAR SPAR LOWER CHORD REPLACESDR DL73K020047Warning System · malfunctionedLEFT WING BODY OVERHEAT LIGHT ON IN FLT. DIVERTED TO MCO. REPAIRING OVERHEAT SYSTEM. TRIED CONTROLLER AND OVERHEAD PANEL, NO HELP. RE-INSTALLED ORIGINAL. INSPECTED FOR LEAKS, NONE FOUND. INSPECTED LOOPS FROM NR 1 ENGINE TO AC PACK BAY CONNECTORS. CHECKESDR DL73K011994Skin · crackedTHE FWD LOWER CORNER OF THE AFT GALLEY DOOR OPENING WAS FOUND WITH A CRACK IN THE SKIN AND UNDERLYING BEAR STRAP. THE CRACK WAS REMOVED WITH A 1.5 INCH X 1.5 INCH CUTOUT IN ALL LAYERS. THE CUTOUT WAS REPAIRED WITH 3 EXTERNAL ALUMINUM REPAIR DOUBLER PER B73SDR DL73K011993Skin · crackedTHE UPPER HINGE CUTOUT OF THE AFT ENTRY DOOR OPENING WAS FOUND WITH A SMALL CRACK IN THE BONDED SKIN ASSY. THE CRACK WAS REMOVED WITH A TRIM-OUT. THE DAMAGE WAS REPAIRED WITH AN EXTERNAL STEEL DOUBLER PER B737 SRM 53-30-3 AND PER ER/A 382354-14, REV A.SDR DL73K011290Fan · unserviceableON LANDING, COCKPIT FILLED WITH SMOKE, TURNED GASPER AND PACKS OFF. AT GATE DETERMINED SMOKE WAS COMING IN WHEN RT PACK WAS TURNED ON. CA FOUND CONTROL CABIN AIR FLOW FAN C/B POPPED. FWD TO MCO AND PLACARD PER MEL 21-00-30ASDR DL73K011157Pump · defectiveHYD SYSTEM A PUMP 2/ LOW PRESSURE. REMOVED AND REPLACED RT EDP, REPLACED CASE DRAIN AND A SYS FILTERS SERV HYD, LEAK CKS GOOD.SDR DL73K011051Circuit Breaker · burnedSMOKE IN COCKPIT FOUND LEFT SIDE WINDOW ANTI-ICE C/B C392 AND C848 STANBY HYD PUMP ALTERNATE C/B BURNEDSDR DL73K010667Light · inoperative3 BULLNOSE EMERGENCY EXIT LIGHTS INOP C/A RELAMPEDSDR DL73K002088Frame · wornTHE FS 440 FRAME HAS A WORN AREA AT THE FORWARD LOWER CORNER OF THE C1 DOORWAY. THE WEAR IS LOCATED ON THE VERTICAL WEB OF THE Z-FRAME. THE DAMAGE WAS BLENDED SMOOTH AND A REPAIR DOUBLER WAS INSTALLED PER ERA 396283-14 AT HMV.SDR DL73K002066Floorbeam · crackedCRACK INDICATIONS WERE FOUND ON THE BL 0.07 LONGITUDINAL FLOORBEAM BETWEEN FS 700 AND FS 717. THE CRACKS WERE REMOVED AND REPAIRED SIMILIAR TO THAT OF B737 S/B 57-1210 PER ERA 396272-14 AT HMV.SDR DL73K002065Floorbeam · corrodedTHE FS 294 FLOORBEAM WAS CORRODED ON THE UPPER CAP AT LBL 10 AND RBL 49. REPAIRED PER ERA 396233-14AD AT HMV.SDR DL73K002062Frame · crackedTHE FS 400 RT SIDE FRAME WAS FOUND CRACKED IN THE SKIN ATTACH FLANGE IN THE BEND RADIUS ADJACENT TO THE FIRST FASTENER ABOVE STR 14R. THE DAMAGE WAS TRIMMED OUT AND A REPAIR INSTALLED PER ERA 396241-14 AT HMV.SDR DL73K002057Attach Fitting · corrodedTHE RT AND LT HORIZONTAL STABILIZER ATTACH FITTINGS WERE FOUND CORRODED. MATERIAL WAS REMOVED FROM THE FACES AND THE BORES WERE OVERSIZED TO REMOVE CORROSION. THE DAMAGE WAS FOUND AT HMV.SDR DL73K002056Fitting · corrodedTHE RT HORIZONTAL STABILIZER CLEVIS LUG WAS FOUND CORRODED THE BORES WERE OVERSIZED AND SOME LOCAL BLENDED WAS APPLIED TO THE FACES PER ERA 396224-14 AT HMV.SDR DL73K002055Fitting · corrodedCORROSION WAS FOUND ON MULTIPLE LUGS ON THE VERTICAL STABILIZER ATTACHMENT LUGS AND FUSELAGE ATTACH LUGS. ALL CORROSION WAS REMOVED AND REPAIRED PER ERA 396259-14 AT HMV.SDR DL73K002053Frame · corrodedCORROSION WAS FOUND ON THE INBOARD CHORD OF THE FS 500B FRAME AT STR 25R. THE DAMAGE WAS REMOVED AND A FACTORY SPLICE EXTENDED TO REPAIR THE DAMAGE. THE DAMAGE WAS FOUND AT HMV.SDR DL73K001895Skin · damagedSKIN AT AFT GALLEY DOOR LWR HINGE CUTOUT CRACKED. DAMAGE IS TRIMMED OUT AND REPAIRED. ER/A 300224-14 REV.ASDR DL73K001865Floorbeam · corrodedSTA 328 FLOORBEAM - PREVIOUS REPAIR CORROSION ON SURFACE TASK NR C53-107-02 OPN 58101AD NRC 416. FLOORBEAM REPAIRED PER SRM 53-10-9 FIG 9.SDR DL73K001917Floorbeam · corrodedSTA 328 FLOORBEAM PREVIOUS REPAIR CORROSION ON SURFACE, TASK NR C53-107-02. REMOVED FASTENERS. TRIMMED BEAM AND PICKED UP HOLES. TREATED AND PAINTED PER SRM 53-10-9 PG 21. OK TO INSTALL. BEGAN INSTALLING REPAIR PER SRM 53-10-9 FIG 9. INSTALLED REPAIR PERSDR DL73K000705Skin · crackedTHE FUSELAGE SKIN ASSY BELOW THE L1 DOOR CUTOUT LOWER SILL NEAR THE AFT CORNER WAS FOUND WITH A 1 INCH CRACK. THE CRACK IS TYPICAL OF BAC S/B 737-53-1083. THE CRACK WAS ROUTED OUT AND REPAIRED WITH TWO REPAIR STRAPS ON A TIME-LIMITED BASIS PER THE S/B. THSDR DL73K000255Fitting · corrodedTHE LT & RT MAIN LANDING GEARS SIDE STRUT SUPPORT FITTING LUGS AT FS 685 WERE FOUND WITH CORROSION IN THE LUG BORES AND ON THE LUG FACES. THE CORROSION WAS REMOVED BY OVERSIZING THE BORES AND MACHINING THE LUG FACES. REPAIR BUSHINGS WERE INSTALLED SDR DL73K992329Power Supply · inopAT DEPARTURE TIME, EMERGENCY LIGHTS ROWS 1 THRU 16 WOULD NOT TURN OFF. REPLACED POWER SUPPLY AND BATTERY LIGHTS OPERATION NORMAL.SDR DL73K991589Valve · failedENGINE OIL TEMP WAS IN THE YELLOW ZONE AROUND 150 DEG C FOR 15 MINUTES. WHEN THE ENGINE WAS IN IDLE THE TEMP WENT UP TO THE RED LINE. REPLACED NR 1 ENGINE FUEL HEAT VALVE (FOUND OPEN/CLOSE IND TANG HANGING UP ON VALVE BODY IN BOTH DIRECTIONS) PER PFHB DRAINESDR DL73K991432Skin · crackedTHE FUSELAGE SKIN WAS FOUND WITH A 2 INCH CRACK AT FS 750 AND STRINGER 19R. THE CRACK WAS ROUTED OUT OF THE SKIN AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER. THE REPAIR WAS ACCOMPLISHED PER B737 SRM 53-30-3, FIG 6 AND ER/A 367661-14.SDR DL73K990795Valve · stuckNR 1 ENG OIL TEMP IN YELLOW BAND. ENG FUEL HEAT VLV STUCK IN THE OPEN POSITION. SHUT DOWN ENG AS PRECAUTIONARY. FLIGHT DIVERTED INTO CAE. VLV DEFERRED PER MEL. AT BDL LAYOVER, THE VLV WAS REPLACED.SDR DL73K990233Skin · crackedTHE FUSELAGE SKIN WAS FOUND WITH A 1 INCH LONG CRACK JUST ABOVE STRINGER 16R AT FS 522. THE CRACK WAS ROUTED OUT AND A REPAIR DOUBLER INSTALLED PER B737 SRM 53-30-3, FIG 1. BECAUSE THE REPAIR EXTENDED UNDR A WING-TO-FUSELAGE PANEL THE REPAIR WAS DOCUMENTEDSDR DL73K982285Module · failedCOCKPIT FIRE CONTROL PANEL SHORTED. POPPING NOISE COMING FROM PEDESTAL AREA. REMOVED AND REPLACED ENG/APU FIRE CONTROL MODULE.
Back to N311DL, cancelled Jan 26, 2007