N330DL, cancelled Mar 13, 2007

Service difficulty reports · 23

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 = 'N330DL' AND deregistration_id = 'N330DL-2007-03-13'
  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 DL73S060013Skin · crackedA CRACK WAS FOUND IN THE FUSELAGE SKIN. CRACK IS 3 INCH LONG LOCATED JUST AFT OF BS 727B, JUST BELOW S-18L. INSTALLED A DOUBLER IAW ER/A 452077-14AD.Dec 13, 2005 · N330DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73S050097Frame · crackedA FASTENER HOLE COMMON TO THE OUTER CHORD OF THE AFT FRAME OF THE L2 DOOR CUTOUT (FS 992, BETWEEN STRINGERS 7L & 8L) WAS FOUND CRACKED. THE HOLE WAS OVERSIZED AND AN INSURANCE CUT MADE TO REMOVE THE CRACK. THE OVERSIZED HOLE WAS REPAIRED WITH AN ALUMINUM BUSFeb 8, 2005 · N330DL · Boeing 737232 · Fuselage Main, FrameSDR DL73S031040Skin Panel · crackedDURING ACCOMPLISHMENT OF 03-058543-03, ME-01 EXISTING REPAIRS AND NEW CRACK DAMAGE WERE NOTED ON THE KEEL BEAM LOWER SKIN PANEL. THE SUBJECT SKIN PANEL WAS REPLACED PER INSTRUCTIONS CONTAINED IN ERA 385772-14.Nov 21, 2003 · N330DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73S031039Attach Fitting · corrodedDURING ACCOMPLISHMENT OF 03-069697-03 NUMEROUS ATTACHMENT LUGS REQUIRED MACHINING BEYOND THE LIMITS PROVIDED, IN ORDER TO REMOVE ALL CORROSION DAMAGE FOUND. LUGS WERE REWORKED PER INSTRUCTIONS CONTAINED IN ERA 385802-14AD.Nov 21, 2003 · N330DL · Boeing 737232 · Horizontal Stabilizer, Attach FittingsSDR DL73S031033Floorbeam · corrodedDURING MODIFICATION OF THE BL 24 FLOORBEAMS PER EO 03-056673-03AD ADDITIONAL WORK WAS REQUIRED DUE TO ADDITIONAL DAMAGE INCURRED. ERA 385831-14AD IMPLEMENTS THE LBL 24 BEAM MOD, PROVIDES NEW REPAIRS FOR THE BEAM WEBS AND ADDRESSES INCURRED DAMAGE.Nov 20, 2003 · N330DL · Boeing 737232 · Fuselage Main, Floor BeamSDR DL73S031028Fitting · corrodedCORROSION DAMAGE WAS FOUND ON THE VERTICAL STAB NR 2 FIN LUG AND THE NR 11 BODY CLEVIS LUG. CORROSION WAS REMOVED AND REWORKED PER ERA 385810-14.Nov 19, 2003 · N330DL · Boeing 737232 · Vertical Stabilizer, Attach FittingsSDR DL73S031036Skin · damagedTHE FUSELAGE SKIN WAS FOUND DAMAGED AROUND 2 NUT PLATE HOLES USED FOR ATTACHMENT OF A WING TO FUSELAGE FAIRING PANEL AT FS 760 BETWEEN STRINGERS 19R & 20R. THE DAMAGED HOLES WERE REMOVED WITH 1.5 X 1 INCH LOCAL CUTOUTS. THE CUTOUTS WERE REPAIRED WITH A SINGLNov 17, 2003 · N330DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73S031035Skin · gougedTHE FUSELAGE SKIN WAS FOUND DENTED AND GOUGED NEAR FS 178 AND STRINGER 24R. THE DAMAGED SECTION OF SKIN WAS CUT OUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 087582-14, REV A.Nov 17, 2003 · N330DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73S031025Skin · dentedA DENT WAS NOTED IN THE FUSELAGE SKIN AT BS 380, BETWEEN S17L AND S18-L. THE DENT WAS CUT OUT AND REPAIRED PER ERA 385827-14.Nov 17, 2003 · N330DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73S031010Floorbeam · crackedTHE FS 520 FLOORBEAM WAS FOUND WITH 1 INCH TO 2 INCH CRACKS NEAR THE UPPER CAP FLANGE AT RBL & LBL 24 & 45. THE CRACKS WERE TYPICAL OF BAC S/B 737-53-1120. THE UPPER CAP WAS TRIMMED OFF TO REMOVE ALL CRACKS. A NEW CAP WAS FABRICATED FROM ALUMINUM EXTRUSIONNov 12, 2003 · N330DL · Boeing 737232 · Fuselage Main, Floor BeamSDR DL73S030975Stop Fitting · damagedDURING ACCOMPLISHMENT OF EO 3-059252-3AD, OPN 0301, (S/B 737-52A1100), A 65-46861-0) FITTING WAS FOUND. EO INSTRUCTIONS REQUIRE ENGINEERING EVALUATION. EVALUATION FOUND THAT FITTING REQUIRED REPLACEMENT PER S/B 737-52-1065. FITTING REPLACED PER S/B 737-52-1Oct 29, 2003 · N330DL · Boeing 737232 · Cargo/Baggage DoorsSDR DL73K030896Frame · crackedTHE LOWER FORWARD FRAME OF THE C1 DOOR HAD A TIME-LIMITED REPAIR PREVIOUSLY INSTALLED AND NEEDED PERMANENT REPAIR INSTRUCTIONS. PERMANENT REPAIR ISSUED VIA ERA 377407-14AD, REV A.Oct 2, 2003 · N330DL · Boeing 737232 · Cargo/Baggage DoorsSDR DL73K011340Keelbeam · crackedTHE LT STRINGER 18A SHEAR BEAM AT FS 727 WAS FOUND WITH A 1 INCH CRACK EMANATING FROM THE EDGE OF THE WEB. THE CRACK IS TYPICAL OF THOSE SHOWN IN BAC S/B 737-53-1066, HOWEVER THE S/B IS NOT EFFECTIVE FOR THIS AIRCRAFT. THE CRACK WAS STOP DRILLED AND REPAIRED Aug 14, 2001 · N330DL · Boeing 737232 · Fuselage Main, KeelSDR DL73K010377Keelbeam · crackedTHE RT STRINGER 18A SHEAR BEAM WAS FOUND WITH A WEB CRACK AT FS 727. THE CRACK IS TYPICAL OF THOSE FOUND IN BAC S/B 737-53-1066, HOWEVER THE S/B IS NOT EFFECTIVE FOR THIS AIRCRAFT. THE CRACK WAS STOP DRILLED AND REPAIRED WITH A STEEL REPAIR CHANNEL PER ER/Mar 6, 2001 · N330DL · Boeing 737232 · Fuselage Main, KeelSDR DL73K002530Relay · failedDURING CLIMB RIGHT CENTER LOW PRESSURE LIGHT ILLUMINATED. CB POPPED RETURNED TO EWR. - REPLACED CONTROL RELAY FOR RT CENTER FUEL BOOST PUMPDec 29, 2000 · N330DL · Boeing 737232 · Fuel Boost PumpSDR DL73K001620Light · inoperativeON LAYOVER, EMERGENCY LIGHT INOP AT ROW 10 DEF. REPLACED LIGHT ASSY, CKS GOOD.Aug 21, 2000 · N330DL · Boeing 737232 · Emergency LightingSDR DL73K000674Seat · crackedSEAT ROW 3 DEF LOOSE ON MOUNTS LIKE A ROCKING CHAIR. FOUND SEAT FRAME CRACKED. REPLACED SEAT ASSEMBLY.Apr 8, 2000 · N330DL · Boeing 737232 · Passenger Compartment EquipmentSDR DL73K990542Frame · crackedTHE AFT DOOR JAMB FRAME OF THE R1 DOOR OPENING WAS FOUND WITH A 3 INCH LONG CRACK UNDER UPPER DOOR STOP FITTING. THE CRACKED FRAME WAS REPAIRED PER THE REQUIREMENTS OF B737 SRM 53-10-4, FIG 1 AND DOCUMENTED PER ER/A 366934-14AD.Mar 11, 1999 · N330DL · Boeing 737232 · Fuselage Main, FrameSDR DL73S981794Actuator · failedRUNAWAY STAB TRIM ON SHORT FINAL. GO-AROUND MADE. REPLACED STAB TRIM ACTUATOR.Aug 30, 1998 · N330DL · Boeing 737232 · Stabilizer ActuatorSDR DL73S980538Skin · gougedSEVERAL GOUGES AND NICKS WERE FOUND IN THE EDGE OF THE SKIN O THE AFT SIDE OF THE C1 DOOR CUTOUT AT APPROX FS 489, BETWEEN S21R AND S23R. REPAIRED PER ERA 331462-14.Mar 9, 1998 · N330DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR DL73S980537Intercostal · crackedDURING INSPECTION PER SI 3-55852-12, THE R1 DOOR AFT FRAME INTERCOSTALS BETWEEN FS 332 AND 344 WERE FOUND CRACKED AT 3 LOCATIONS S8A, 10A, AND 11A. REPAIRED PER ERA 331432-14AD.Mar 9, 1998 · N330DL · Boeing 737232 · Fuselage Miscellaneous StructureSDR DL73S960651Blkhd Web · crackedTHE BS 178 BULKHEAD WEB WAS FOUND CRACKED BENEATH THE VERTICAL STIFFENERS AT LBL 5.7 AND RBL 5.7. DAMAGE REMOVAL RESULTED IN A 1.45 INCH LEFT AND RIGHT BY 1.2 INCH UP AND DOWN CUTOUT ON THE LT SIDE AND A 1.5 INCH LEFT AND RIGHT BY 5.1 INCH UP AND DOWN CUTOUT Mar 14, 1996 · N330DL · Boeing 737232 · Fuselage Main, BulkheadSDR DL73S953838Cowl · dentedDURING SHOP VISIT, ENGINE NOSE COWL ASSEMBLY WAS RESTORED PER CMM 65-85378. OUTER SKIN DENTED AT 5:30 POSITION. REPAIRED PER SRM 51-40-2.Sep 8, 1995 · N330DL · Boeing 737232 · Engine Cowling System
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