N409DA, cancelled Feb 16, 2001
Service difficulty reports · 48
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 = 'N409DA' AND deregistration_id = 'N409DA-2001-02-16' 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.
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 = 'N409DA' AND deregistration_id = 'N409DA-2001-02-16' 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 DL72S992761Skin · crackA .75 INCH LONG CRACK WAS FOUND EMANATING FROM A FASTENER HOLE NEAR THE UPPER FORWARD CORNER OF THE R1 DOOR CUTOUT (FS 380). THE CRACK WAS ROUTED OUT OF THE SKIN AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER. THE REPAIR WAS ACCOMPLISHED PER ER/A 368954-14, SDR DL72S992751Skin · crackedFOUND ON C1 LETTER CK, .375 INCH CRACK ON SKIN AT THE LOWER I/B FASTENER OF THE L4 WINDOW CUTOUT. REPAIRED PER SRM 53-30-3.SDR DL72S992447Light · inopFWD CABIN OVERHEAD EMERGENCY LIGHT INOP. ON LAYOVER CK. REPLACED RACK.SDR DL72S992080Antenna · failedWEATHER RADAR INOP, RESET CB, LEFT IN STANDBY FOR 5 MIN. WORKED 10 MIN, THEN INOP AGAIN, REPEAT WRITE-UP. REPLACED RADAR ANTENNA AND CONTROL PANEL. TRANSMITTED RADAR FOR 20 MIN. RADAR CKS OK.SDR DL72S991438Switch · failedAFTER TAKEOFF APPROX 3000 FT, GEN NR 2 BKR AND FIELD LIGHT ON. RAN POM PROCEDURES AND RETURNED TO BOS. REPLACED NR 2 ENG GEN RESIDUAL VOLTAGE SWITCH.SDR DL72S990675Battery Pack · dischargedFWD AISLE EMERGENCY LIGHT STAYED ON. REPLACED EMERGENCY LIGHT RACK AND BATTERY, OPS CK OK.SDR DL72S982664Compressor · stalledNR 2 ENGINE COMPRESSOR STALLS AND VIBRATIONS ON CLIMBOUT. ACFT RETURNED TO DFW. NR 2 ENGINE CHANGED.SDR DL72S982253Skin · repairedDURING SHOP INSP, THE COVE SKIN WAS FOUND CRACKED AT THE I/B AFT CORNER OF I/B AFT FLAP DRIVE ROD CUTOUT. THE SKIN WAS REPAIRED BY REMOVING THE DAMAGE AND INSTALLING A DOUBLER PER MM 57-52-0, FIG 09.SDR DL72S982093Fitting · crackedCRACKING WAS DETECTED IN FOUR OF EIGHT HOLES ON S18A, LT SIDE. HOLES WERE OVERSIZED THROUGH THE SKIN, STRINGER AND FITTING. REPAIRED PER ERA 332264-14.SDR DL72S982092Skin · crackedLT SIDE OF THE VERT STAB SKIN IS CRACKED AT THE INTERSECTIONOF S10 AND FUSE CREASE LINE. REPAIR PER ERA 332292-14.SDR DL72S982056Frame · crackedWHILE PERFORMING INSPECTION PER SI 4-61904-12AD A CRACK WAS FOUND IN THE FS 761 RT FRAME ABOVE THE FIRST BOLT HOLE BELOW THE FLOOR LINE IN THE INBD FLANGE. REPAIRED PER ERA 332248-14AD.SDR DL72S981987Frame · crackedA CRACK WAS FOUND IN THE FS 761 RT FRAME DURING ACCOMPLISHMENT OF S/B 727-53-0197. THE CRACK IS TYPICAL OF THAT SHOWN IN SUBJECT S/B AND IS DUE TO FATIGUE. REPAIRED PER ERA 332248-14AD.SDR DL72S982321Angle · crackedDURING SHOP INSPECTION, THE AFT CHORD ANGLE WAS FOUND CRACKED 34 INCHES FROM I/B END OF FLAP. THE ANGLE WAS REPAIRED BY INSTALLING A DOUBLER PER MM 57-52-0 FIG 802.SDR DL72S982320Angle · crackedDURING SHOP INSP, THE AFT CHORD ANGLE WAS FOUND CRACKED 33 INCHES FROM IB END OF FLAP. THE ANGLE WAS REPAIRED PER MM 57-52-0, FIG 809 BY INSTALLING A DOUBLER.SDR DL72S982319Angle · crackedDURING SHOP INSPECTION, THE AFT CHORD ANGLE WAS FOUND CRACKED 33 INCHES FROM O/B END OF FLAP. THE ANGLE WAS REPAIRED PER MM 57-52-0 BY REPLACING A SECTION OF THE ANGLE AND INSTALLING A DOUBLER.SDR DL72S982135Spar · crackedLWR AFT SPAR RAIL CRACKED TWO PLACES AT I/B DRIVE ROD CUTOUT. REPAIRED PER MM 57-52-0 FIG 802.SDR DL72S982077Rib · crackedAT HMV, FOUND RIB NR 5 AND RIB NR 15 CRACKED. ROUTED FRAME 5. REPAIRED DOUBLER AND FILLER AS PER M/M 57-54-0 FIG 814. OK TO INST REPAIR NR 5 RIB. INSTALLED REPAIR ON NR 5 RIB PER M/M 57-54-0 FIG 814. BEGAN MAKING DOUBLER. FINISHED ROUTING RIB NR 15. REPSDR DL72S982076Frame · crackedAT HMV, FOUND FRAME CRACKED FS 930 BETWEEN STR 13R - 14R JUST ABOVE REPAIR. REMOVED DAMAGED PORTION OF FRAME. BEGAN DRILLING FRAME REPAIR, DRILLED FRAME REPAIR. TREATED AND PAINTED PER PS 900-3-6 NR 3. OK TO INSTALL, BEGAN INSTALL. COMPLETED INSTALL OF FRSDR DL72S981226Light · inoperativeL2 DOOR EMERG LIGHT INOP. REPLACED CHARGER.SDR DL72S981142Skin · crackedFOUND AT A2 LETTER CK, FUSELAGE SKIN HAS A .25 INCH CRACKED AT LWR I/B FASTENER HOLE FOR R-4 WINDOW CUTOUT. REPAIRED PER SRM 53-30-3.SDR DL72S981141Skin · delaminatedLT ELEV T/E SEPARATING I/B SIDE, REPAIRED PER MM 55-20-0 P801.SDR DL72S980492Battery Pack · dischargedEMERGENCY LIGHTS ON AFT CARGO DOOR AND ABOVE EMERGENCY EXITS LFT SIDE FLASHING. REPLACED BOTH BATTERY PACKS.SDR DL72S972652Skin · cracked.75 IN CRACK AT NR 2 LE FLAP SKIN AT INBD LIP HINGE CUTOUT. REPAIRED PER ERA 363453-14 AND M/M 57-30-0.SDR DL72S972452Battery Pack · dischargedF/C OVRHD EMERGENCY LIGHTS INOP. REPLACED BATTERIES.SDR DL72S970978Battery Pack · dischargedRIGHT CABIN EMERGENCY WINDOW EXIT SIGN WILL NOT TEST. REPLACED BATTERY PACK, CHECKS GOOD.SDR DL72S971028Skin · crackedTHE FUSELAGE SKIN AND UNDERLYING DOUBLER WAS FOUND TO HAVE A .625 INCH CRACK IN THE UPPER FWD CORNER OF THE L-1 DOOR CUTOUT. THE SKIN IS M/F FROM 0.040 2024-T3 CLAD AND THE BONDED DOUBLER IS COMPOSED OF 0.036 2024-T3 CLAD. TEMPORARY - LISTED ON SHTS 2-4 OF ESDR DL72S970281Stringer · crackedS-8L CRACKED AT FIN STA 110.40. FABRICATED REPAIR PER M/M 55-30-0 FIG 803, STOP DRILLED CRACKS AND INSTALLED REPAIR PER M/M 55-30-0 FIG 803.SDR DL72S970280Web · crackedWEB CRACKED AT STA 1303 LWR RT CORNER. DRILLED NEW REPAIR DOUBLER PER SRM 53-10-4 FIG 17.SDR DL72S970259Support · damagedAT MV-2, FOUND TOP SLOTTED MOUNTS FOR UPRIGHT SUPPORTS FOR AFT B/B PANEL STA 720D, LBL 24 AND RBL 24 TO BE DAMAGED. REMOVED BOTH LEFT AND RIGHT SUPPORTS, FABRICATED AND DRILLED UP REPAIR DOUBLERS AS PER SRM 53-10-9 FIG 9. INSTALLED REPAIR AND L/R SUPPORTS PESDR DL72S970291Blkhd Stiffener · crackedWHILE ACCOMPLISHING EO 4-59275-12, 2.5 INCH CRACK WAS FOUND ON I/B FLANGE OF VERT STIFFENER LOCATED AT RBL 8. A SECOND 1.5 INCH CRACK WAS FOUND ON O/B FLANGE IN VERT STIFFENER FOUND AT LBL 8. BOTH CRACKS FOUND AT WL 100. MTC WILL ACCOMPLISH ONLY OPER 0240/0SDR DL72S970224Flap · crackedAT MID VISIT, THE NR 2 MID FLAP I/B CONTROL CABLE CUTOUT WAS FOUND TO BE CRACKED. REPAIRED WITH A DOUBLER PER MM 57-52-0 PAGE 802.SDR DL72S962764Battery Pack · dischargedCABIN EMERGENCY LIGHTS INOP.SDR DL72S961214Light · inoperativeFLIGHT ENGINEER TESTED EMER EXIT SYS AFT AIRSTAIR UPPER LT DID NOT TEST. FWD TO MCO AND PLAC PER M3L 33-00-16.SDR DL72S961027Battery Pack · dischargedEMERGENCY ESCAPE FLOOD LIGHT ON CENTER CARGO DOOR IS ON ALL THE TIME. REPLACED RT OVERWING BATTERY PACK RACK. OPS CHECKS GOOD.SDR DL72S960577Vert Beam · crackedVISIBLE CRACK, 1.50 INCHES, IN VERT BEAM, STA 1183, RBL 8 AT WL 182. FOUND DURING E-2 LTR CK TPAMM. REPAIRED PER M/M 53-11-0.SDR DL72S960392Web · damagedDURING INSPECTION PER S/B 727-53-0129 IN ACCORDANCE WITH AD 94-07-08, THE INBD WEB WAS CUT TO THE BOTTOM EDGE OF THE WEB, THUS SEVERING. ALSO, SEVERAL OBLONG HOLES IN THE WEB WERE FOUND. ACCOMPLISHED REPAIRS PER FORM 8110-3, DATED 12-02-92, BACP TWX DA; -AT;SDR DL72S954599Angle · crackedDURING SHOP INSPECTION, FOUND NR 4 L/E SLAT WITH LOWER COVE PANEL SUPPORT ANGLE CRACKED AT RIB NR 9. REPAIRED PER MM 57-54-0.SDR DL72S954598Rib · crackedDURING SHOP INSPECITON, NR 4 L/E SLAT WAS FOUND WITH CRACKED RIB AT O/B SIDE OF THE O/B SLAT TRACK. REPAIRED PER MM 57-54-0.SDR DL72S954597Rib · crackedDURING SHOP INSPECTION, NR 4 L/E SLAT WAS FOUND WITH CRACKED RIB ON O/B OF ACTUATOR ATTACH FITTING. REPAIRED PER MM 57-54-0 PG 805.SDR DL72S960253Rib · crackedDURING SHOP INSPECTION FOR NR 6 LEADING EDGE SLAT, RIBS NR 16 AND NR 18 WERE FOUND TO BE CRACKED. REPAIRED PER MM 57-54-0 FIG 809.SDR DL72S960251Rib · crackedDURING SHOP INSPECTION FOR LEADING EDGE SLAT NR 6, RIBS NR 5 AND NR 13 FOUND TO BE CRACKED. REPAIRED RIBS PER M/M 57-54-0 FIG 805.SDR DL72S954596Rib · crackedDURING SHOP INSPECITON, NR 4 L/E SLAT WAS FOUND WITH CRACKED RIB AT I/B SIDE OF ACTUATOR ATTACH FITTING. REPAIRED PER MM 57-54-0 FIG 805.SDR DL72S954558Skin · bentLOWER SKIN BENT AND A PIECE MISSING AT THE ACTUATOR RIBS LOCATION. INSTALLED DOUBLER PER M/M 57-54-0, FIG. 815, DURING SHOP VISIT, FOR NR 4 L/E SLAT.SDR DL72S960582Rib · crackedLOWER AFT CORNER OF NR 2 RIB FROM OUTBOARD END CRACKED. REPAIRD PER MM 57 54 0, FIG 814, DURING SHOP INSPECTION FOR NR 5 L/E SLAT.SDR DL72S953360Skin · crackedNR 2 ENGINE INLET HOUSING CRACKED .5 RT SIDE AT PANEL 9524. FOUND DURING E-1 LTR CK TPAMM, REPAIRED PER MM 54-30-00.SDR DL72S953359Angle · crackedNR 7 SLAT COVE SKIN SUPPORT ANGLE HAS .5 CRACK BELOW THERMAL ANTI-ICE DUCT. FOUND DURING E-1 LTR CK TPAMM, REPAIRED PER M/M 57-54-0.SDR DL72S950656Wire · looseDURING CRUISE, UNABLE TO MAINTAIN CABIN PRESSURE, INITIATED EMERGENCY DESCENT. REGAINED CONTROL AT FL 180 IN MANUAL MODE. FOUND INTERMITTENT WIRES AT RIGHT PACK FLOW CONTROL AND SHUT OFF VALVE. REPLACED 3 WIRES AT CANNON PLUG D870, WDM 21-61-02 PG.4. OPERASDR DL72S950571Skin · crackedDURING LETTER CHECK, FOUND 2 CRACKS IN PANEL FWD OF SADDLE PLATE LEFT SIDE VERTICAL STABILIZER. REPAIRED PER MM 54-30-0 PG 801-802.
Back to N409DA, cancelled Feb 16, 2001