N329DL, cancelled Dec 21, 2007
Service difficulty reports · 40
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 = 'N329DL' AND deregistration_id = 'N329DL-2007-12-21' 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 = 'N329DL' AND deregistration_id = 'N329DL-2007-12-21' 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 DL73S060242Bear Strap · crackedTHE UPPER AFT CORNER OF THE L2 DOOR OPENING HAS A FATIGUE CRACK IN THE BEAR STRAP AND ONE IN THE FUSELAGE OUTER SKIN AND DOUBLER. CUTOUT IS 3.5 X 1.5 INCH. INSTALLED REPAIR DOUBLER PER SRM.SDR DL73S050615Floorbeam · crackedTHE RBL 24 LONGITUDINAL OVERWING FLOORBEAM HAS BEEN PREVIOUSLY MODIFIED PER 3-056673-3AD. THE C-CHANNEL INSTALLED PER THIS EO DOES NOT MEET EXISTING AD REQUIREMENTS. CRACKS WERE FOUND IN THE UPPER CHORD, BEAM AFT WEB, AND WEB DOUBLERS. THE C-CHANNEL WAS REPSDR DL73S050614Floorbeam · crackedTHE LBL 24 LONGITUDINAL OVERWING FLOORBEAM WAS MODIFIED USING A PREVIOUSLY ACCEPTALBE C-CHANNEL THAT IS NOT ACCEPTABLE PER AD 2001-17-18. CRACKS WERE FOUND IN THE BEAM AFT WEB AND WEB DOUBLER. C-CHANNEL WAS REPLACED. WEB REPAIR DOUBLER WAS INSTALLED, AND CRSDR DL73S041012Shear Beam · crackedA 1 INCH CRACK WAS FOUND EMANATING FROM A FASTENER HOLE AT THE AFT END OF THE STRINGER 18A SHEAR BEAM WEB AT FS 727 ON THE LT SIDE OF THE AIRCRAFT. THE CRACK EXTENDED TO THE AFT EDGE OF THE PART AND FWD OF THE END FASTENER HOLE. THE CRACK WAS REPAIRED WITH ASDR DL73S040229Relief Valve · failedDURING APPROACH PHASE AFTER PLACING THE FLAP LEVER TO 5 SYSTEM A PRESSURE WENT TO ZERO WITH ASSOCIATED SYSTEM A LOW PRESSURE LIGHTS ILLUMINATED. REPLACED SEVERAL LINES AND RESERVOIR PRESSURE RELIEF VALVE.SDR DL73S040191Regulator · leakingLOSS OF A-SYSTEM HYDRAULIC PRESSURE. FOUND NO RESERVOIR HEAD PRESSURE. REPLACED RESERVOIR PRESSURE REGULATOR AND BOTH CHECK VALVES.SDR DL73S030630Insulation · out of positionSMOKE SMELL IN AFT CABIN. FOUND INSULATION TOUCHING APU BLEED DUCT CAUSING SMELL. REPOSITIONED INSUL. FWD APU AIR TO MCO AND PLAC AS PRECAUTION.SDR DL73S030508Frame · crackedMTC FOUND CRACKS IN THE FRAME AT S6L, 3L, 2L, 1, 2R, AND 3R EXTENDING FROM THE STRINGER PASS THRU CUTOUTS. THE CRACKS WERE CUTOUT AND A REPAIR SIMILAR TO B737-200 SRM 53-10-04, F14, WAS INSTALLED TO EXTEND FROM O/B OF STR 6L TO O/B OF STR 4R. FUSELAGE SKIN WSDR DL73S030505Frame · crackedTHE SUBJECT DOOR FRAME WAS FOUND CRACKED AT THE INTERSECTION OF FS 440 AND STR 24R. THE FRAME WAS ORIGINALLY 0.071 INCH 7075-T6 CLAD. THE CRACK WAS TRIMMED OUT, STEEL REPAIR ANGLES WERE INSTALLED, AND TWO DOOR STOP FITTINGS WERE MODIFIED TO ALLOW FOR THE INSSDR DL73S030495Attach Fitting · corrodedSTABILIZERS / HORIZONTAL / ATTACH FITTINGS / LT, RT AND CENTER SECTION - CORROSION: WHILE ACCOMPLISHING AN INSPECTION OF THE HORIZONTAL STABILIZER ATTACH LUGS PER EO 3-69697-3. MAINTENANCE DISCOVERED CORROSION IN ALL FUSELAGE AND STABILIZER LUGS AND ON MOST SDR DL73S030485Skin · dentedFUSELAGE SKIN FS 344, S-19R TO S-20R - DENT: A DENT WAS REPORTED APPROXIMATELY 2 INCHES BELOW THE LOWER EDGE OF THE UPPER SKIN OF THE LAP SPLICE AT S-19R. THE DENT MEASURED 2.2 X 1.5 X 0.057 INCH DEEP. THE SKIN PANEL IS 0.036 INCH SKIN WITH A 0.036 INCH INSDR DL73S030479Attach Fitting · corrodedFUSELAGE ATTACH FITTINGS: VERTICAL STABILIZER CLEVIS LUGS - CORROSION. THE NR 11 CLEVIS LUG FWD FACE WAS FOUND GOUGED. THE DAMAGE WAS CLEANED UP USING A SPOTFACE, WITH A MIN REMAINING LUG THICKNESS OF 0.940 INCH IAW DAL ER/A 412535-14, INITIAL RELEASE.SDR DL73K010986Bleed Valve · malfunctionedSHORTLY AFTER T/O NR 2 ENGINE EGT REACHED 640 FOR 3 TO 4 SECONDS. INSPECTED INLET AND EXHAUST, NO DEFECTS. CHECKED EPR SYSTEM WITH P/S TEST BOX INDICATION GOOD. NO LEAKS. LUBED BLEED VALVES AND REPLACED PRBC PERFORMED PFHB TEST E - J AND X. TESTS GOOD. RSDR DL73K010840Skin · crackedA 1 INCH LONG CRACK WAS FOUND IN THE FUSELAGE SKIN AT FS 750 JUST ABOVE STRINGER 18R. THE CRACK WAS REMOVED WITH A CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER B737-200 SRM 53-30-3, FIG 17 AND ER/A 380916-14.SDR DL73K010004Skin · crackedTHE LOWER HINGE CUTOUT OF THE FWD ENTRY DOOR CUTOUT WAS FOUND WITH A 1 INCH CRACK. THE CRACK WAS ROUTED OUT AND REPAIRED WITH AN EXTERNAL STEEL DOUBLER PER B737 SRM 53-30-3 FIG 31 AND ER/A 379680-14, REV A.SDR DL73K002113Power Supply · inoperativeON MTC CK FOUND R2 OVER DOOR EMERGENCY LIGHT AND AFT EXIT LOCATOR EMERGENCY LIGHT NOT ILLUMINATING ON TEST. REPLACED POWER SUPPLY.SDR DL73K001234Bulkhead · damagedINSPECTIONS OF THE FS 178 BULKHEAD STRUCTURE PER AD 2000-05-19, REVEALED CRACKS IN THE BULKHEAD STRUCTURE COMMON TO THE COCKPIT FLOOR (REF. DAL ER/A 377636-14AD). IN ORDER TO ACCESS THE AREA FOR REPAIR, AN ACCESS HOLE HAD TO BE CUT IN THE BULKHEAD WEB AT SDR DL73K001221Web · crackedWHILE ACCOMPLISHING AD 2000-05-29 INSPECTIONS OF THE FS 178 BULKHEAD AND ADJACENT STRUCTURE, A 1 INCH CRACK WAS FOUND EMANATING FROM A LIGHTNING HOLE IN THE WEB OF THE HORIZONTAL FLOOR CLOSEOUT AT WL 207 ON BOTH THE LT AND RT SIDES OF THE AIRCRAFT. THE LT SDR DL73K001222Bulkhead · crackedA TYPICAL CRACK WAS FOUND IN THE FS 178 BULKHEAD WEB AT WL 233.5, RBL 7 DURING INSPECTIONS MANDATED PER AD 2000-05-29. THE CRACK WAS REPAIRED PER B737-200 SRM 53-10-11, FIG. 1 AND DOCUMENTED PER ER/A 377622-14AD.SDR DL73K000791Warning Light · false indicationLEFT, RIGHT AND APU FAULT DET ILLUMINATED. REPLACED COCKPIT FIRE CONTROL PANEL. GROUND CHECKS NORMAL. REPLACED FIRE DETECTOR MODULE PRECAUTIONARY OPS NORMAL. RAN ENGS, NO FAULT DET LIGHTS. OK FOR SERVICE.SDR DL73K992655Turbine Wheel · damagedAT APPROX 400 FT AGL, LOUD BANG, NR 1 ENGINE FAILED 700 DEGREES EGT, WINDMILLING N1 AND N2 WAS BLOF T/O DUE TO GROSS WT. FOUND 3RD STAGE OF LPT DAMAGED. REPLACED ENGINE.SDR DL73K991837Bulkhead Web · crackedWHILE ACCOMPLISHING LFEC INSPECTIONS OF THE AFT PRESSURE BULKHEAD WEB, A CRACK INDICATION WAS NOTED NEAR STRINGER 6R. INTERNAL HFEC INSPECTION CONFIRMED TWO CRACKED FASTENER HOLES AT THE WEB TO CAP INTERFACE AT STRINGER 6R. THE CRACKED AREA OF WEB WAS CUTOUTSDR DL73K991563Support · wornDURING INSP PER OPN 5264, FOUND BUSHING MIGRATED RT FWD ENG MOUNT SUPPORT FITTING. REPLACED SUPPORT FITTING PER EO 03-073535-12AD ME-04. FWD MOUNT SUPPORT ASSY PN 713701203.SDR DL73K991330Tire · failedEXPERIENCE NOSE WHEEL TIRE FAILURE AT ROTATION. CONTINUED TAKEOFF. INSPECTED AIRCRAFT AND FOUND RT NOSE TIRE TREAD CAP MISSING. REPLACED LEFT AND RIGHT NOSE WHEEL ASSYS PER MM. PERFORMED OVERWEIGHT LANDING INSP. NO DAMAGE TO FUSELAGE AND WINGS. ENGINE INSDR DL73K990925Tire · failedA/C BLEW NR 2 TIRE ON T/O FROM EWR. UPON LANDING IN MCO, LOST ALL 'A' SYSTEM HYDS AND HAD TO BE TOWED IN AFTER TIRE REPLACEMENT. REPLACED NR 1 AND 2 TIRES AND BRAKES, AFT FLAP, ANTI-SKID WIRING HARNESS, AND ASSOCIATED HARDWARE.SDR DL73K990453Compressor · damagedDURING CRUISE AT FL370 FROM MCO-BOS, CREW EXPERIENCED HEAVY COMPRESSOR STALLS ON THE NR 2 ENGINE. CREW REDUCED POWER AND LANDED IN RDU. CONTRACT MTC INSPECTED ENGINE AND FOUND EXTENSIVE COMPRESSOR AND FAN BLADE DAMAGE. REPLACED ENGINE.SDR DL73K982610Fitting · corrodedFUSELAGE LT AND RT MLG SIDE STRUT SUPPORT FITTING, BS 685. REPAIR FOR OVERSIZE LUG BORES. THE LUG BORES OF THE LT AND RT MLG SIDE STRUT SUPPORT FITTINGS AT BS 685 WERE FOUND CORRODED. THE LUG BORES WERE OPENED A MAX OF .11 IN DIAMETER. STEEL REPAIR SLEEVES SDR DL73K982498Actuator · failedLEADING EDGE AMBER LIGHT ON SLAT NR 5. REPLACED NR 5 SLAT AND ACTUATOR.SDR DL73K981632Bulkhead Chord · crackedA 0.5 INCH CRACK WAS FOUND IN THE MLG WHEEL WELL BLKHD AT STA 727. THE CRACK WAS LOCATED IN THE UPPER FLANGE OF THE COMPRESSION CHORD AT BL 0.0 AND RUNS THRU A FASTENER HOLE. REPAIRED PER ERA 365406-14.SDR DL73S981294Skin · dentedFUSELAGE SKIN AND BONDED DOUBLER WERE FOUND DENTED BETWEEN S17L AND 18L AT FS 400. REPAIRED PER ERA 331844-14.SDR DL73S981289Skin · crackedUPON HFEC AND LFEC INSPECTIONS OF THE UPPER AFT CORNER OF THE FWD GALLEY DOORWAY PER 3-58715-3AD, A CRACK WAS INDICATED. REPAIRED PER ERA 331849-14AD.SDR DL73S972195Skin · damagedFUSELAGE SKIN FS 460-480 STR 27R - 28L GROUND DAMAGE REPAIR. THE FUSELAGE SKIN BETWEEN FS 460 AND 480 AND BETWEEN STRG 27R AND 28L WAS DAMAGED BY A CARGO LOADER. DAMAGE CUT OUT RESULTED IN A 4 BY 7 CUTOUT AND A 2 BY 17 CUT OUT. DOUBLER AND TRIPLER REPAISDR DL73S970640Coalescer Bag · dirtySTRONG ODOR NOTED IN COCKPIT AND CABIN. REPLACED BOTH LT AND RT WATER BAGS, RAN PACKS OFF ENG AND NO SMELLS NOTED.SDR DL73S980089Hyd Line · rupturedON CLIMBOUT AT 12000, THE MASTER CAUTION AND HYD LIGHTS ILLUMINATED ON GLARESHIELD PANEL. ENG NR 2 HYD PUMP LOW PRESSURE ILLUMINATED ON OVERHEAD PANEL, QTY WENT TO 0. RETURNED TO ATLANTA. MTC IN PROGRESS, BROKEN HYD PRESS LINE RT ENG PUMP. REPLACED LINE.SDR DL73S961969burned outEMERGENCY LIGHTS AT 1L DOOR AND ROWS 17 ABC, 21 ABC, AND 25 ABC INOPERATIVE.SDR DL73S961461Bulkhead Web · crackedDURING SPECIAL INSPECTION 3-69482-12, CRACKS WERE DISCOVERED ON THE FWD FACE OF THE FS 178 BULKHEAD WEB. THE FIRST CRACK IS LOCATED NEAR THE LBL 5.7 VERTICAL STRAP AT APPROX WL 203. THE SECOND IS NEAR THE RBL 5.7 VERTICAL STRAP AT APPROX WL 203. THE 3RD IS SDR DL73S960158Valve · leakingON CLIMBOUT, LOST A/B HYDRAULIC SYSTEM PRESSURE. FLIGHT RETURNED MSP. FOUND PARKING BRAKE VALVE LEAKING. REPLACED VALVE, SERVICED SYSTEM AND OPERATION NORMAL.SDR DL73S952205Door · crackedFWD B/B DOOR PAN CRACKED AT FWD AND AFT CORNERS INSIDE RADIUS. REPAIRED PER DL ERA 301812-14.SDR DL73S952204Skin · delaminatedNR 6 SPOILER UPPER SURFACE DELAMINATED. REPAIRED PER SRM 57-50-5 FIG 5. FOUND AT M1 LTR CK.SDR DL73S952203Skin · delaminatedRUDDER DELAMINATED AT TOP LEFT SIDE T/E NEXT TO PREV REPAIR. ACCOMPLISHED REPAIRS PER SRM 51-40-9 FIG 1 AND ERA 301817-14.
Back to N329DL, cancelled Dec 21, 2007