N331DL, cancelled May 26, 2009
Service difficulty reports · 34
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 = 'N331DL' AND deregistration_id = 'N331DL-2009-05-26' 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 = 'N331DL' AND deregistration_id = 'N331DL-2009-05-26' 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 DL73S050399Duct · perforatedON T/O AT 3500FT, NR 2 ENG OVHT LIGHT ILLUMINATED. WHEN THRUST LEVER PULLED TO IDLE IAW QRK PROCEDURE LIGHT WENT OUTMADE RETURN LANDING AT CVG. REPLACED BLOWN ANTI-ICE DUCT.SDR DL73S050154Apu · smokeDURING APU START CABIN FILLED WITH SMOKE. RAN PACKS USING EXT CART, NO SMELL NOTED. STARTED ENGINES, NO SMELL WITH PACKS ON / OFF. FWD APU MCO PLACARD MEL 49-00-01A.SDR DL73S041071Skin · crackedA 1 INCH CRACK WAS FOUND IN THE BONDED SKIN ASSY AND UNDERLYING BEAR STRAP AT THE UPPER AFT CORNER OF THE L2 DOOR CUTOUT. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH 3 EXTERNAL ALUMINUM REPAIR DOUBLERS PER B737 SRM AND ER/A 095399-14, REV A.SDR DL73S040401Housing · crackedLOST A HYDRAULIC SYSTEM ON TAXI IN TO GATE AT ORD. FOUND NR 8 GROUND SPOILER ACTUATOR BODY CRACKED. REPLACED NR 8 GROUND SPOILER PER AMM 27-62-101, PB 401. LEAK AND OP. CHECK GOOD. RII PERFORMED.SDR DL73S030688Attach Fitting · corrodedDURING ACCOMPLISHMENT OF INSPECTIONS IAW SB 737-55-1028 (DAL EO 3-85220-3), CORROSION WAS FOUND ON FIVE (5) VERT STABILIZER CLEVIS LUGS AND THREE (3) VERT STABILILZER ATTACH LUGS. THE BORES WERE OVERSIZED AND THE LUG FACES MACHINED TO REMOVE CORROSION. O/S BSDR DL73S030681Skin · dentedA SCRATCH AND DENT WAS FOUND IN THE FUSELAGE SKIN JUST BELOW THE C1 CARGO DOORWAY EXTENDING FROM FS 460 TO FS 500. AN EXISTING REPAIR WAS FOUND AT THE FORWARD LOWER CORNER OF THE DOORWAY. THIS REPAIR WAS REMOVED AND AN EXTERNAL ALUMINUM DOUBLER TRIPLER AND FILSDR DL73S030680Spar · gougedRT WING / MLG AFT SUPPORT FITTING / WBL 157, TOOLING DAMAGE. THE MLG AFT SUPPORT FITTING ON THE RT WING SUFFERED TOOLING DAMAGE DURING REMOVAL OF FASTENERS FOR INSPECTION. THE BORE OF ONE OF THE FASTENERS WAS DAMAGED IN THE AFT FITTING, REAR SPAR UPPER CHORDSDR DL73S030674Floorbeam · damagedDURING ACCOMPLISHMENT OF EO 03-062982-03AD, MTC ADDED ADDITIONAL FASTENER HOLES THROUGH THE UPPER CAP AND SPLICE ANGLES OF THE CENTER WING BOX FLOORBEAMS FROM BS 650 TO 675 AT BL 0.07. REPAIR PER ER/A 385423-14AD.SDR DL73S030666Pressure Panel · crackedFUSELAGE STA 727 BLKHD, MLG WW, UPPER CHORD - REPAIR: A 0.5 INCH CRACK WAS PREVIOUSLY REPAIRED IN TEH UPPER CHORD OF THE SUBJECT BULKHEAD NEAR BL 0. THE CRACK WAS IN THE UPPER FLANGE OF THE COMPRESSION CHORD AND RAN THROUGH A FASTENER HOLE. DURING THE CURRENSDR DL73S030665Frame · crackedFUSELAGE SKIN STA 663, S2R TO S1 - MISALIGNMENT: DURING INSPECTION OF THE FS 663 FRAME, MTC FOUND CRACKS IN THE FRAME AT S2R AND S1R. THESE WERE WITHIN THE AREA ADDRESSED BY B737-200 SRM 53-10-4, FIG 14. DURING INSTALLATION OF SRM FRAME REPAIR, SKIN ATTACH SDR DL73S030664Skin · damagedFUSELAGE SKIN STA 255, S-23R TO S-24R - CUTOUT: EXISTING TEMPORARY (BLIND FASTENER) SRM REPAIR REMOVED AND PERMANENT SKIN REPAIR INSTALLED IAW DAL ER/A 385263-14.SDR DL73S030658Attach Fitting · corrodedHORIZ STAB LT, RT, AND CENTER SECTIONS ATTACH FITTINGS :LUG CORROSION, INSPECTION OF THE HORIZONTAL STABILIZER ATTACH LUGS ON THE LT, RT, AND CENTER SECTIONS OF THE STAB PER BAC S/B 737-55- 1055, CORROSION WAS FOUND IN SEVERAL OF THE LUG BORES AND ON THE LUG SDR DL73S030623Sill · crackedFUSELAGE C-2 DOOR UPPER SILL FS 818 WEB CORROSION. DURING INSPECTION OF A TIME LIMITED REPAIR TO THE C-2 DOORWAY UPPER SILL WEB, CRACKING OF THE WEB WAS NOTED AS WELL AS A SHORT ED FASTENER IN THE SILL OUTER CHORD. THE WEB WAS REPAIRED WITH A DOUBLER AND THESDR DL73K030517Skin · crackedFS 661 - 727, KEEL BEAM SKIN PANEL FABRICATION: DURING INSPECTIONS PER EO 3-58542-3, THE SUBJECT PANEL WAS FOUND CRACKED. BAC SB 737-53-1104 PROVIDES REPAIR INSTRUCTIONS TO REFABRICATE THE PANEL, HOWEVER ER/A 385214-14 WAS ISSUED TO CUT AN ACCESS HOLE IN THESDR DL73K010980Door Frame · crackedTHE UPPER SILL BEAM OF THE C2 DOOR CUTOUT SURROUND STRUCTURE WAS FOUND WITH A CRACK IN THE BEAM WEB AT FS 818.SDR DL73K010795Antenna · failedWX RADAR ANTENNA FAULT. REPLACED WX RADAR ANTENNA, TEST GOOD. THIS WAS AN AIR TURNBACK.SDR DL73K002275Wire · shortedNR 2 ENG OIL TEMP IN YELLOW BAND. FOUND NR 2 FUEL HEAT VALVE C/B POPPED. FOUND WIRE 058-20 INSIDE FIREWALL CANNON PLUG SHORTED TO GROUND. REPAIRED SAME.SDR DL73K001897Coffeemaker · shortedFLT ATT REPORTED STRONG ELECTRICAL SMELL IN AFT GAL. TURNED OFF AFT GALLEY PWR IN COCKPIT SMELL WENT AWAY. FOUND SHORTED AFT NR 1 COFFEE DISPENSER. REPLACED SAME, CKS OK.SDR DL73K001755Skin · gougedTHE FUSELAGE SKIN AT THE C1 DOOR CUTOUT FWD EDGE (FS 440) WAS FOUND WITH SEVERAL GOUGES AND SCRATCHES BETWEEN STRINGERS 21R & 25R. THE SKIN WAS CUT OUT TO REMOVE THE DAMAGE. THE CUTOUT WAS REPAIRED WITH AND EXTERNAL ALUMINUM DOUBLER AND TRIPLER PER ER/A 3784SDR DL73K001689Floor Panel · crackedTHE COCKPIT FLOOR WEBS AT WL 207 THAT EXTEND FROM FS 178 TO FS 188 O/B OF LBL AND RBL 24 WERE FOUND CRACKED. THE CRACKS WERE FOUND DURING INSPECTION AND MODIFICATION OF THE FS 178 BULKHEAD WEB PER BAC S/B 737-53A1173, REVISION 3. THIS ER/A INSTRUCTS TO REPLASDR DL73K001037Engine · malfunctionedON T/O ROLL, LT ENG WOULD ONLY ACHIEVE 2.02 EPR. DISCONTINUEDT/O ROLL AT 60 KTS. TRIMMED 01/02 ENGS PER PFHB. PART PWR AND T/O PWR CHECKS GOOD. ALL ENG PARAMETERS NORMAL ON ENG RUN.SDR DL73K990454Ballast · failedSMOKE AND FUMES IN FWD CABIN AND FLT DECK. DIVERTED TO ATL. REPLACED FWD GALLEY CEILING LIGHT BALLAST.SDR DL73S981396Bulkhead Web · cracked8 CRACKS FOUND IN THE BS 178 BULKHEAD WEB. REPAIRED PER ERA 331867-14.SDR DL73S981392Skin · damagedLWR AFT CORNER OF THE C2 DOOR CUTOUT WAS ROUTED OUT TO REMOVE DAMAGE. REPAIRED PER ERA 331876-14.SDR DL73S981391Frame · corrodedC2 DOOR CUTOUT FWD FRAME LWR CORNER AT FS 800 WAS FOUND CORRODED IN THE UPPER RADIUS NEAR S25R. REPAIRED PER ERA 331884-14AD.SDR DL73S981390Frame · crackedLT AND RT INBD CHORD OF THE FS 616 FRAME BOTH HAVE A CRACK IN THE LOWEST FASTENER HOLE BELOW THE FLOOR LINE. REPAIRED PER ERA 331885-14.SDR DL73S981388Frame · dentedTHE STA 747 FRAME WAS FOUND DENTED ON THE INBOARD FLANGE BETWEEN STR 24L AND 25L. THE STA 827 FRAME WAS FOUND DENTED ON THE INBOARD FLANGE AT STR 24L. THE DAMAGE WAS CAUSED IN SERVICE. REPAIRED PER ERA 331894-14.SDR DL73S981153Line · rupturedSYS 'A' LOSS INDICATIONS LOW HYD QTY AND NR 2 SYS 'A' LOW PRESS LIGHT. FOUND PRESSURE LINE ON RT ENG HYD PUMP RUPTURED. REPLACED LINE. SERVICED SYS BLEED SYS. ALL CK GOOD PER M/M.SDR DL73S972356Intercostal · crackedTHE R1 DOOR SURROUND AFT FRAME INTERCOSTAL AT STR 8A WAS FOUND WITH A TYPICAL CRACK PER S/B 737-53A1108. THE INTERCOSTAL WAS REPAIRED PER THE S/B AND ER/A 363174-14AD WHICH ALLOWED SUBSTITUTION OF ALODINE FOR CHROMIC ANODIZE.SDR DL73S971459Fan · failedDURING DESCENT, A STRONG ELECTRICAL ODOR STARTED, VERY STRONG IN COCKPIT. FLT ATT REPORTED STRONG ELECTRICAL ODOR ROW 14. REPLACED GASPER FAN AND BOTH WATER SEPARATOR BAGS, CKS OK.SDR DL73S970262Hydraulic Fluid · lostLOSS OF A-SYSTEM HYDRAULIC QTY AND PRESSURE. ACCOMPLISHED SYSTEM A-HYDRAULIC LOSS PROCEDURES PER POM. RETURNED TO ATL, LANDING WEIGHT 102,000 POUNDS.SDR DL73S960620Door · jammedDURING EVAC OF AIRCRAFT, THE LEFT NR 1 DOOR WOULD NOT OPEN ALL OF THE WAY. DOOR CHECKS GOOD PER MM 52-11-00, OPENED DOOR DEPLOYED AND INFLATED SLIDE OPS NORMAL. REPLACED SLIDE.SDR DL73S960031Relay · inoperativeAT ALTITUDE MAIN STAB TRIM MOTOR WOULD NOT WORK, A/P MOTOR WORKS OK. APPLICABLE C/B WERE CYCLED TO NO AVAIL, RETURNED TO ATL PER DISPATCH. INSPECTED STAB TRIM ACT, CLEANED CONNECTORS, INSPECTED LIMIT SWITHCES, CUTOUT SWITHCES AND ALL CHECK NORMAL. REPLACED SDR DL73S954032Floorbeam · crackedTHE BL 0.07 FLOORBEAM OF THE WING CENTER SECTION IS CRACKED AT STA 661 AND THE UPPER CAP OF THE BEAM IS COMPLETELY CRACKED THROUGH, INCLUDING TWO FASTENER HOLES. THIS AREA WILL BE TRIMMED OUT. NO CRACKS WERE FOUND IN THE WEB. THE CRACK IS TYPICAL PER BOEING
Back to N331DL, cancelled May 26, 2009