N367DL, cancelled Apr 16, 2003

Service difficulty reports · 31

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 = 'N367DL' AND deregistration_id = 'N367DL-2003-04-16'
  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 DL73E011295Battery · dischargedON INSPECTION FOUND AFT LEFT OVER DOOR EMERGENCY EXIT SIGN INOP. REPLACED BATTERIES PER MM. OPN NORMALAug 6, 2001 · N367DL · Boeing 7372S3 · Emergency LightingSDR DL73E010864Indicator · failedNR 1 INST XMFR C/B POPPED ON PRE-DEPARTURE. REPLACED CAPTS RMI DUE TO OFF FLAG IN VIEW.May 29, 2001 · N367DL · Boeing 7372S3 · Visual Omnirange (VOR) SystemSDR DL73E010557Frame · crackedCRACKS WERE FOUND IN THE FS 178 BULKHEAD LT AND RT SIDE CHORDS. ADDITIONALLY, TWO CRACKS WERE FOUND IN THE CENTER WEB AT LBL 12/WL 218 AND RBL 12/WL 234. THE WEB WAS REPAIRED PER SRM 53-10-11, FIG. 1 AND THE CHORDS WERE REPLACED PER ERA 397408-14AD. THE DApr 4, 2001 · N367DL · Boeing 7372S3 · Fuselage Main, FrameSDR DL73E010555Skin · crackedTWO CRACKS WERE FOUND IN THE FUSELAGE SKIN NEAR FS 727B, STR 17 RT AND 727A, STR 18 RT. THE CRACKS WERE CUT OUT AND AN EXTERNAL DOUBLER WAS INSTALLED PER B737-200 SRM 53-30-3, FIG6. THE DAMAGE WAS FOUND AT HMV.Apr 4, 2001 · N367DL · Boeing 7372S3 · Fuselage Main, Plate/SkinSDR DL73E010554Skin · crackedA CRACK WAS FOUND IN THE LOWER HINGE CUTOUT OF THE AFT GALLEY DOOR. THE CRACK WAS COMMON TO THE SKIN, BONDED DOUBLER AND THE BEAR STRAP. THE CRACK WAS CUT OUT AND A DOUBLER / TRIPLER INSTALLED AT HMV.Apr 4, 2001 · N367DL · Boeing 7372S3 · Fuselage Main, Plate/SkinSDR DL73E010518Floorbeam · crackedDURING ACCOMPLISHMENT OF INSPECTION PER S/B 737-57-1210. A CRACK WAS FOUND IN THE PANEL ATTACH HOLE AT FS 660. THE CRACK WAS CUT OUT AND THE AREA REPAIRED BY S/B 737-57-1210.THE DAMAGE WAS FOUND AT HMV.Mar 30, 2001 · N367DL · Boeing 7372S3 · Fuselage Main, Floor BeamSDR DL73E010499Skin · crackedA CRACK WAS FOUND IN THE FUSELAGE SKIN AT FS 727B AND STR 16L. THE CRACK WAS CUT OUT AND REPAIRED PER SRM 53-30-3. THE DAMAGE WAS FOUND AT HMV.Mar 27, 2001 · N367DL · Boeing 7372S3 · Fuselage Main, Plate/SkinSDR DL73E010466Frame · crackedA CRACK WAS FOUND IN THE WEB OF THE FS 795 FRAME BETWEEN STR 23R AND 24R. THE CRACK WAS CUT OUT AND REPAIRED PER SRM 51-40-3, FIGURE 1. THE DAMAGE WAS FOUND AT HMV.Mar 22, 2001 · N367DL · Boeing 7372S3 · Fuselage Main, FrameSDR DL73E001723Support Fitting · corrodedTHE LUG BORE OF THE FS 685 LT MLG SIDE SUPPORT FITTING WAS FOUND WITH CORROSION. THE CORROSION WAS REMOVED BY OVERSIZING THE LUG BORE. AN OVERSIZE BUSHING WAS INSTALLED. THE REPAIR WAS ACCOMPLISHED PER ER/A 378436-14.Sep 6, 2000 · N367DL · Boeing 7372S3 · Main Landing Gear Attach SectionSDR DL73E001722Beam · tool damageTHE AFT TRUNNION BORE OF THE LT WING MLG SUPPORT BEAM SUFFERED TOOLING DAMAGE IN THE HOLE BORE. THE BORE WAS OVERSIZED TO REMOVE THE TOOLING DAMAGE, ROTO PEENED, AND AN OVERSIZE BUSHGING INSTALLED. THE REPAIR WAS ACCOMPLISHED PER ER/A 378444-14.Sep 6, 2000 · N367DL · Boeing 7372S3 · Wing SparSDR DL73E001670Link · corrodedMLG TRUNNION LINK PITTED AND RUSTY RUST COMING OUT OF MATING SURFACES OF TRUNNION LINK ASSY AND TRUNNION PIN I/B OF MLG ACTUATOR. RIGHT MLG TRUNNION LINK PITTED/CORRODED ON I/B AND O/B FACES. RT MLG UPPER STRUT TRUNNION LUG CORROSION. RT MLG UPPER STRUT CYLAug 23, 2000 · N367DL · Boeing 7372S3 · Landing Gear Retraction/Extension SystemSDR DL73E001623Pcu · malfunctionedNOTICED A SHARP ABRUPT YAW INPUT SHORTLY AFTER NOSE WHEEL LIFT OFF. NO ABNORMAL WINDS OR AIRCRAFT WAKE EXISTING. YAW WAS SIGNIFICIANT, NO INPUTS NOTED IN RUDDER PEDALS BY PILOT FLYING. CHECKED YAW DAMP FOR FAULTS, NONE. REPLACED RUDDER PCU PER M/M RII. CAug 19, 2000 · N367DL · Boeing 7372S3 · Rudder Control SystemSDR DL73E001600Actuator · malfunctionedNOTICED A SHARP ABRUPT YAW INPUT SHORTLY AFTER NOSE WHEEL LIFTOFF. NO ABNORMAL WINDS OR AIRCRAFT WAKE EXISTING. YAW WAS SIGNIFICANT NO INPUTS NOTED IN RUDDER PEDALS BY PILOT FLYING. REPLACING RUDDER PACK.Aug 19, 2000 · N367DL · Boeing 7372S3 · Rudder ActuatorSDR DL73E991786Light · inopEMERGENCY LTS INOP LT AND RT FWD ENTRY DOOR ON OUTSIDE OF AIRCRAFT REF WDM 33-51-01. REPLACED M571. OPS NORMAL.Aug 10, 1999 · N367DL · Boeing 7372S3 · Emergency LightingSDR DL73E991322Skin · crackedDURING THE INSP OF THE R1 DOOR UPPER CORNERS SEVERAL CRACKS WERE FOUND IN THE SKIN ASSY AND BEARSTRAP. REPAIRED PER ERA 367544-14, REV A.Jun 11, 1999 · N367DL · Boeing 7372S3 · Service DoorsSDR DL73E990846Connector · looseEMERGENCY EXIT LIGHTS ALONG AISLE AND LOWER DOORS COME ON AND GO OFF ON THEIR OWN. FOUND WIRE LOOSE ON AFT FLT ATTENDANT PANEL EMERGENCY SWITCH. TIGHTENED CONNECTOR ON SWITCH. LIGHTS OPS CHK NML.Apr 16, 1999 · N367DL · Boeing 7372S3 · Emergency LightingSDR DL73E990133Battery · dischargedEMERGENCY EXIT LIGHT BATTERIES DEAD DUE TO GND POWER LOSS. REPLACED EMERGENCY EXIT BATTERIES AND BASE ASSY.Jan 21, 1999 · N367DL · Boeing 7372S3 · Emergency LightingSDR DL73E982302Skin · crackedTHE FUSELAGE SKIN WAS FOUND WITH A 1.875 INCH CRACK BELOW THE L1 DOOR AT APPROX FS 335. THE CRACK IS TYPICAL OF BAC S/B 737-53-1083. THE CRACK WAS STOP DRILLED AND REPAIRED WITH AN INTERIM DOUBLER REPAIR PER THE S/B. THE REPAIR WILL BE REPLACED WITH A PERMANov 6, 1998 · N367DL · Boeing 7372S3 · Fuselage Main, Plate/SkinSDR DL73E982128Floorbeam · crackedTHE UPPER CAP OF THE RBL 24.82 OVERWING PASSENGER FLOORBEAM WAS FOUND WITH A .5 INCH CRACK EMANATING FROM A CUTOUT FOR A SEAT TRACK ATTACH POINT. THE CRACK WAS STOP DRILLED AND REPAIRED WITH AN ALUMINUM REPAIR DOUBLER AND TRIPLER PER ER/A 365847-14, REV B.Oct 12, 1998 · N367DL · Boeing 7372S3 · Fuselage Main, Floor BeamSDR DL73E982127Skin · crackedTHE UPPER HINGE CUTOUT OF THE L1 DOOR OPENING WAS FOUND WITH A TYPICAL CRACK IN THE SKIN AND BONDED DOUBLER. THE CRACK WAS ROUTED OUT AND REPAIRED WITH AN EXTERNAL STEEL DOUBLER PER THE B737 SRM 53-30-3 FIG 21. THE REPAIR WAS DOCUMENTED PER ER/A 365839-14, ROct 12, 1998 · N367DL · Boeing 7372S3 · Fuselage Main, Plate/SkinSDR DL73E981894Audio Acc Unit · failedCOMM RADIO FAILURE IN FLIGHT OCCURED 5 MIN AFTER T/O. RADIOS RESTORED AFTER APU STARTED AND TRANSFERED NR 2 BUS TO APU. RAN ENGS ALL COMRADIOS CK GOOD. INSPECTED STATIC WICKS AND ANTS. ALL OK. REPLACED AUDIO ACC UNIT. ALL RADIO FUNCTIONS NORMAL.Sep 12, 1998 · N367DL · Boeing 7372S3 · Audio Integrating SystemSDR DL73E981449Clip · crackedA SKIN AND STRINGER REPAIR WERE ACCOMPLISHED AT FS 597 STR 2L. THE FRAME-TO-STRINGER CLIP INSPECTION REQUIRED PER BAC S/B 737-53-1085 (AD 93-08-04) WAS ACCOMPLISHED AT THIS LOCATION AND RESULTED IN FINDING A CRACKED CLIP. A NEW CLIP HAD TO BE MODIFIED TO ALLJul 9, 1998 · N367DL · Boeing 7372S3 · Fuselage Miscellaneous StructureSDR DL73E981447Clips · crackedWHILE ACCOMPLISHING REPLACEMENT OF CRACKED FRAME-TO-STRINGER CLIPS PER BAC S/B 737-53-1085 (AD 93-08-04), MTC. WAS UNABLETO INSTALL THE REQUIRED RIVETS. THE RIVETS WERE SUBSTITUTED WITH STEEL HI-LOKS PER ER/A 365196-14AD, REV A.Jul 8, 1998 · N367DL · Boeing 7372S3 · Fuselage Miscellaneous StructureSDR DL73E980037Skin · crackedFUSELAGE/SKIN, FS 727A-727B, S-16R-17R, REPAIRED FOR SKIN CRACKS. THE FUSELAGE SKIN BETWEEN FS 727A AND 727B AND BETWEEN STRINGER 16R AND 17R WAS FOUND WITH A 3.25 LONG CRACK AND A 2.25 LONG CRACK. THE CRACKS WERE CUT OUT AND A REPAIR DOUBLER WAS INSTALLED PJan 6, 1998 · N367DL · Boeing 7372S3 · Fuselage Main, Plate/SkinSDR DL73E970290Intercostal · crackedTHE R-1 DOOR FRAME INTERCOSTALS AT STR 8A,10A, 11A WERE FOUND CRACKED IN THE TYPICAL MANNER SHOWN IN S/B 737-53A1108, REV 5. THIS ER/A ACCOMPLISHED A REPAIR AT THIS LOCATION WITH THE LISTED S/B AND AD 88-03-03. REPETITIVE INSPECTIONS PER EO 3-55852-12AD MUSFeb 12, 1997 · N367DL · Boeing 7372S3 · Fuselage Miscellaneous StructureSDR DL73E970200Uplock Sensor · malfunctionedLEFT GEAR RED ON RETRACTION. RETURNED TO CVG. CORRECTIVE ACTION NECESSARY TO DO GEAR SWING. CHECKING UPLOCK. REPLACED UPLOCK SENSOR. CHECKS OK.Feb 1, 1997 · N367DL · Boeing 7372S3 · Landing Gear Position and WarningSDR DL73E962787Pwr Supply · inoperativeBOTH LT AND RT LOWER EMERG DOOR EXIT IDENTIFIERS INOP. REPLACED EMERG LIGHT PWR SUPPLY PACK M9027, OPS GOOD PER MM.Dec 30, 1996 · N367DL · Boeing 7372S3 · Emergency LightingSDR DL73E962403Transmitter · inoperativeFLAPS FAILED TO EXTEND. REPLACED LT FLAP POS TRANSMITTER AND INDICATOR, OPER CK OK.Oct 28, 1996 · N367DL · Boeing 7372S3 · Trailing Flap Position Indicating SystemSDR DL73E954745Rib · crackedDURING SHOP INSPECTION, C-2 CARGO DOOR WAS FOUND WITH CRACKS TO A RIB AND SUPPORT ANGLE AT ACCESS HOLE NR 23. ACCOMPLISHED REPAIRS PER ERA 271679-14AD AND SRM 52-30-2.Dec 21, 1995 · N367DL · Boeing 7372S3 · Cargo/Baggage DoorsSDR DL73E954496Frame · crackedAIRWORTHINESS DIRECTIVE 90-06-02, DOOR AFT CARGO, LOWER AFT CORNER, FRAME AND BEAM REPAIR. DURING ROUTINE OVERHAUL, THE LOWER AFT CORNER OF THE AFT CARGO DOOR WAS FOUND DAMAGED. THE FRAME WAS CRACKED AXIALLY ALONG THE RADIUS APPROX 20 INCHES. THE LOWER BEAMSep 22, 1995 · N367DL · Boeing 7372S3 · Cargo/Baggage DoorsSDR DL73E952649Skin · crackedDURING INSPECTION, THE FUSELAGE SKIN AT STA 303.9 BETWEEN STR 10 AND STR 14 WAS CRACKED AT THE LOWER FORWARD CORNER OF THE FORWARD ENTRY DOORWAY (L-1) LOWER HINGE CUTOUT. THE CRACK MEASURED APPROX 1.8 LONG. FAA FORM 8110-3 DATED 6/7/95, THE DAMAGE WAS CUT OUJun 7, 1995 · N367DL · Boeing 7372S3 · Fuselage Main, Plate/Skin
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