N997DL
Service difficulty reports · 244
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 = 'N997DL' AND registry_match = 'registration' 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 = 'N997DL' AND registry_match = 'registration' 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 DALA2016040702685Cusp Web · corrodedSEVERE CORROSION ON RT CUSP WEB BETWEEN BS 370-389 AND X=-54 TO X=-60. DAMAGE WAS REPAIRED IAW SRM 53-05, FIG 131A AND 51-30-2, 51-10-3 PAR 14 AND 21.SDR DALA2016040702684Pan · crackedCRACK ON RING PAN AFT LOWER CORNER BETWEEN BS 237-258 LT AT PASSENGER CABIN. FASTENERS AND DAMAGE WERE REMOVED, WAS PERFORMED IAW SRM 06-10-01-001. NO CRACKS. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-30-5, 53-05, FIG 122.SDR DALA2016040702683Pan · crackedCRACK ON RING PAN STRUCTURE UPPER FWD AND LOWER AFT CORNERS BETWEEN BS 788 AND BS 769 LT SIDE. DAMAGE AND FASTENERS WERE REMOVED, WAS PERFORMED IAW NDT SPM 06-10-01-001, WO CRACKS. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-30-5, 51-30-2, 53-05, SDR DALA2016040702682Pan · crackedCRACK ON RING PAN FWD UPPER CORNER BETWEEN BS 351-370 RT AT PASSENGER CABIN. FASTENERS AND DAMAGE WERE REMOVED REPAIR PARTS WERE FABRICATED. REPAIR PARTS WERE INSTALLED IAW SRM 53-05, FIG 122, 51-30-2, 51-30-5.SDR DALA2016040702681Pan · crackedCRACK ON RING PAN FWD UPPER CORNER BETWEEN BS 617-636 RT AT CABIN PAX. FASTENERS AND DAMAGE WERE REMOVED REPAIR PARTS WERE FABRICATED REPAIR PARTS WERE INSTALLED IAW SRM 53-05, FIG 122, 51-30-2, 51-30-5.SDR DALA2016040702680Pan · crackedCRACK ON RING PAN FWD UPPER CORNER BETWEEN BS 769-788 RT AT CABIN PAX. DAMAGE WAS REMOVED IAW SRM 53-05, FIG 122. REPAIR PARTS WERE FABRICATED IAW SRM 53-05, FIG 122. REPAIR PARTS WERE INSTALLED IAW SRM 51-30-5, 51-30-2.SDR DALA2016040702679Pan · crackedCRACK ON RING PAN AFT LOWER CORNER BETWEEN BS 294-275 LT AT CABIN PAX. FASTENERS AND DAMAGE WERE REMOVED IAW SRM 51-30-2 AND 53-05, FIG 122. REPAIR PARTS WERE FABRICATED ANS INSTALLED IAW SRM 51-30-5, 51-30-2.SDR DALA2016040702678Pan · crackedCRACK ON RING PAN FWD UPPER CORNER BETWEEN BS 788-807RT CABIN PASSENGER. FASTENERS AND DAMAGE WERE REMOVED, REPAIR PARTS WERE FABRICATED, REPAIR PARTS WERE INSTALLED IAW SRM 53-05, FIG 122, 51-30-2, 51-30-5.SDR DALA2016040702677Pan · crackedCRACK ON RING PAN FWD UPPER CORNER BETWEEN BS 655-674, RT AT CABIN PASSENGER DAMAGE AND FASTENER WERE REMOVED IAW SRM 53-05, FIG 122 AND 51-30-2.SDR DALA2016040902746Pan · crackedCRACKED PAN ABOVE FRAME NR 4 FROM AREA AT R1 DOOR. PAN WAS REPAIRED IAW SRM 52-03 D FIG. 3.SDR DALA2016040702690Pan · crackedCRACK ON RING PAN STRUCTURE AT UPPER FWD CORNER BETWEEN BS 788 AND 807 ALSO UPPER FWD CORNER BETWEEN BS 807 AND 826 LT SIDE. RING PAN WERE REPAIRED IAW SRM 53-05, FIG 122, 51-30-2 AND 51-30-5 CRACK LONG WAS 0.125" HFEC WAS PERFORMED NO CRACKS WERE FOUND AFTERSDR DALA2016040702692Skin · wornWEAR ON UPPER SKIN T/E OF OTBD VANE OTBD FLAP BS XV2-297 CANT AT LT WING. WEAR ON UPPER SKIN T/E OF OTBD VANE OTBD FLAP BS XV2=297 LT WING WAS REPAIRED IAW ERA 521199-14MA REV ORIGINAL.SDR DALA2016041402910Cusp Web · crackedCORROSION ON LT CUSP WEB, OUT LIMITS, BETWEEN BS 674 TO 693. CORROSION OUT LIMITS WAS REPAIRED IAW SRM 53-05, FIG 131A-14 51-30-5, 51-30-2, 51-10-3 PAR 14, 21, 26, 38.SDR DALA2016040402520Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENTAREAOF FUEL ACCESS PLATE NR 1303C AND 1409C. FUEL ACCESS PLATE NR 1303C AND 1409C WERE REPLACED IAW SRM 51-22-2A CONDTION III.SDR DALA2016040402507Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE NR 1303C AND 1409C. FUEL ACCESS PLATE NR 1303C AND 1409C WERE REPLACED IAW SRM 51-22-2A, CONDTION III.SDR DALA2016033102489Channel · crackedCRACKED CHANNEL ON FLOOR PANEL 927E. FLOOR PANEL WAS REPAIRED IAW SRM 53-05, PAR 145.SDR DALA2016033102488Channel · crackedCRACK ON CHANNEL, AFT SIDE AT FLOOR PANEL 1003A. FLOOR PANEL WAS REPAIRED IAW SRM 53-05, PAR 145.SDR DALA2016033102487Channel · crackedCRACK ON CHANNEL AT FLOOR PANEL 1003F. FLOOR PANEL WAS REPAIRED IAW SRM 53-05, AR 145.SDR DALA2015102606484Fairing · crackedTAIL TOP, RT UPPER BANANA FAIRING UPPER EDGE HAS A 15 INCH LONG CRACK ABOVE AFT ATTACH POINT. REPAIRED IAW ER/A 464895-14MA REV F.SDR DALA2015102606482Fairing · crackedTAIL TOP, RT LWR BANANA FAIRING LWR EDGE HAS TWO 1 INCH LONG CRACKS AT 36 & 40 INCHES AFT OF FWD END. REPAIRED IAW ER/A 464895-14MA, REV F.SDR DALA2015102606480Longeron · damagedTAIL INTERIOR A .2500" ALUMINUM LINE IS CONTACTING LONGERON 13R AT BS 1341. REPAIRED IAW SRM 53-02, FIG 18 AS A REF.SDR DALA2015102506445Skin · gougedVERTICAL STABILIZER TIP MID SECTION RT AFT SKIN HAS 2 DEEP 3" LONG GOUGES, ABOVE HORIZONTAL STABILIZER HINGE. REPAIRED IAW PRI 540664-14, REV 0 AND C/W ERA 540664-14, REV A.SDR DALA2015102506446Skin · wornVERTICAL STABILIZER LT SIDE SKIN IS WORN AT HORIZONTAL STABILIZER SIDE LOAD ROLLER. REPAIRED IAW PRI 540677-14, REV 0 AND WAITING FOR FINAL ER/A.SDR DALA2015102306375Skin · crackedSKIN BENEATH DIAMOND DOUBLER CRACKED BS 1410 AT LONGERON 2L. REPAIRED IAW PRI 540097-14, REV 0 AND WAITING FOR FINAL ER/A.SDR DALA2015102206334Doubler · crackedTAIL INTERIOR - DIAMOND SHAPED ACFT SKIN DOUBLER AT BS 1410 IB OF L2L IS CRACKED 2 PLACES. SEE NR FOR ADDITIONAL INFORMATION 001-0279:5300-2551/018 00077, WORK TO BE ACCOMPLISHED ON NR 137 AND PRI/ERA 540097-14AD, REV ORIG.SDR DALA2015061203758Wire · brokenDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING AT SEAT 24D IN THE CABIN WAS INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE IN THE UNDERSEAT HARNESS. THE WIRE HARNESS WAS REPAIRED AND THE SYSTEM RETURNED TO NORMAL OPERATION. LP 7126129.SDR DALA2015032002295Connector · damagedMAINTENANCE FOUND EMERGENCY LIGHTS FROM ROWS 1-12 FLOOR LIGHTS INOPERATIVE AFTER ERA 531288-14MA WAS COMPLETED. MAINTENANCE R & R CONNECTOR PLUG P1-791 ON B5-211 IAW WDM 33-51-14 AND REPLACED B5-211 POWER SUPPLY AND BATTERY. OPS CKS NML IAW AMM 33-53.SDR DALA2015031702235Slide · no testMAINTENANCE DEPLOYED THE TAILCONE IAW TAILCONE DEPLOYMENT WC 2562-7267. THE SLIDE INITIALLY FAILED TO INFLATE. APPROXIMATELY 45 SECONDS AFTER TAILCONE DEPLOYMENT, THE SLIDE DID INFLATE COMPLETELY AND REMAINED INFLATED FOR OVER 10 MINS. MAINTENANCE INSTALLESDR DALA2014122906826Pbe · damagedMAINTENANCE DISCOVERED THAT THE COCKPIT PROTECTIVE BREATHING EQUIPMENT BEHIND THE CREW SEATS WAS DAMAGED. THE PBE WAS REPLACED.SDR DALA2014100705429Battery Pack · inoperativeOVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE AT ROWS 27-30. REPLACED BATTERIES IAW AMM 33-53-00. OPS CHECKED NORMAL.SDR DALA2014092205209Wire · brokenMAINTENANCE FOUND THE EMERGENCY AISLE LIGHTS ON SEAT 25ED WERE INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE AT THE CONNECTOR. THE CONNECTOR WAS REPLACED AND THE OPS CHECK WAS GOOD.SDR DALA2014072104200Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS AT ROWS 22-30 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.SDR DALA14027530997Wire · brokenDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHT AT SEAT 13D WAS INOPERATIVE. FOUND A BROKEN WIRE, REPAIRED AND SYSTEM RETURNED TO NORMAL OPERATION.SDR DALA13050700997Cable · wornDURING SCHEDULED CHECK, TAILCONE TELEFLEX CABLE WAS NOTED TO BE WORN. SPIRAL WRAP WAS SHOWING WEAR & COMING OFF OF THE CABLE. REPLACED TELEFLEX CABLE IAW AMM 53-53-02-201-1.SDR DALA13050690997Skin · crackedMULTIPLE CRACKS NOTED ON SKIN BS 1380, 14R JUST ABOVE PYLON. REPAIRED IAW ER/A 519023-14 AND THE REQUIRED INSPECTION WAS COMPLETED.SDR DALA13050680997Frame · crackedWEB ON LEFT SIDE OF CANTED FRAME BS 1485 CRACKED AT 10:00 POSITION. REPAIRED IAW ER/A 519100-14, REV O.SDR DALA13050050997Sill · corrodedCORROSION FOUND AT THE AFT CARGO DOOR SILL. CORROSION WAS BLENDED AND EXCEEDED SRM MINIMUMS. REPLACED C3 CARGO BEAM IAW DWG 5930483.SDR DALA13050030997Skin · corrodedCORROSION FOUND ON THE AFT CARGO SKIN UNDER THE SEAL DEPRESSOR FROM STA 1155-1212. REPAIRED IAW ER/A 519203-14.SDR DALA13049450997Gauge · obstructedDURING SCHEDULED CHECK, THE TAILCONE SLIDE PRESSURE GAUGE WAS FOUND TO BE OBSTRUCTED FROM VIEW BY TAPE. TAILCONE SLIDE COVER WAS REPLACED IAW AMM 25-62-01 AND WC 2500-4484. REQUIRED INSPECTION COMPLETED.SDR DALA13049440997Hook And Loop · missingDURING SCHEDULED CHECK, HOOK AND LOOP FOR THE RELEASE LANYARD NORMALLY LOCATED ON THE TOP OF THE TAILCONE SLIDE COVER WAS MISSING. TAILCONE SLIDE COVER WAS REPLACED IAW AMM 25-62-01 & WC 2500-4484. THE REQUIRED INSPECTION WAS ALSO COMPLETED.SDR DALA13049430997Pin · corrodedDURING SCHEDULED INSPECTION, THE TAILCONE TEE PIN AND BUSHINGS WERE FOUND TO BE RUSTED. THE TEE PIN BUSHINGS AND ASSOCIATED HARDWARE WERE REPLACED IAW AMM 53-53 AND THE REQUIRED FUNCTIONAL CHECKED AND INSPECTION WAS ACCOMPLISHED.SDR DALA13049420997Cable · wornDURING SCHEDULED CHECK, PLASTIC COATED TAILCONE RELEASE CABLE WAS FOUND TO BE WORN WHERE IT PASSES THROUGH THE CONDUIT CONNECTION TO THE TEE PIN. CABLE REPLACED IAW AMM 53-53 AND THE FUNCTIONAL CHECKED AND INSPECTION WAS COMPLETED.SDR DALA13049110997Gusset · corrodedDURING SCHEDULED CHECK, AFT CARGO DOOR FRAME CORNER GUSSET AT BS 1212 FOUND CORRODED AND OUT OF LIMITS. REPAIRED IAW SRM 51-30-05.SDR DALA13049100997Skin · crackedDURING SCHEDULED CHECK, A SKIN CRACK WAS NOTED AT BS 1437 BETWEEN LONGERON 2 & 3L. REPAIRED IAW ER/A 519049-14.SDR DALA13050040997Floor Support · corrodedAFT CARGO DOOR FRAME FLOOR SUPPORT TEE BS 1136-1218-CORROSION. REPLACED T-SECTION DUE TO CORROSION OUT OF LIMITS. REPLACED IAW DWG 5936660.SDR DALA13046440997Release Mech · failedACFT FAILED INITIAL DROP CHECK OF THE TAILCONE RELEASE SYS. RELEASE MECHANISM CAM EXCEEDED 45 POUNDS ALLOWABLE PULL LIMIT. TEE PIN ADJUSTED IAW MANUAL AND THE SYSTEM RECHECKED. TAILCONE DROPPED AT 10 POUNDS OF MEASURED PULL FORCE. THE RII STEPS WERE COMPLETESDR DALA13032930997Wire Harness · looseDURING LINE INSPECTION IN MEM, THE FLOOR ESCAPE PATH LIGHT WAS FOUND TO BE INOPERATIVE AT ROW 12. MX ADJUSTED AND SECURED A LOOSE WIRING HARNESS IAW AMM 33-53 AND THE SYS CHECKED GOOD.SDR DALA13032920997Wire Harness · looseDURING LINE INSPECTION, THE FLOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE AT ROW 20. MX ADJUSTED AND SECURED A LOOSE WIRING HARNESS IAW AMM 33-53 AND THE SYS CHECKED GOOD.SDR DALA13020070997Connector · looseSEAT MOUNTED EMERGENCY PATH LIGHT INOPERATIVE AT ROW 13D. SECURED LOOSE CONNECTOR AT SIDEWALL OPERATION CHECKS OK.SDR DALA1235530997Seat Track · corrodedCORROSION ON SEAT TRACK LBL 44 BS 218 MAIN CABIN. REMOVED EXISTING SEAT TRACK SPLICE FROM BS 198-228-LBL 44 PER DC9/MD80 SRM 51-30-5 STEP 8 A,B. INSTALLED SEAT TRACK P/N 5936566-75 LBL 44 BS 198 BS 228 IAW MD88 SRM 53-05 PAR 32 VIEW A. REPAIR ACCOMPLISHED A
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