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.

SDR DALA2016041802984Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE NR 1472C. ACCESS WAS REPLACED IAW SRM 51-22-2A, COND. II.Apr 16, 2016 · N997DL · Doug MD88 · Wing, Plate/SkinSDR DALA2016041802980Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE NR 2302C. FOUND NR 1 HOLE OUT OF LIMITS WITH .671" BUSHING WAS FABRICATED AND INSTALLED WITH OD .439" AND COUNTERSINK .635" IAW SRM 51-22-2A PAR 6, COND. II.Apr 16, 2016 · N997DL · Doug MD88 · Wing, Plate/SkinSDR DALA2016041802979Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE NR 1464C. FOUND NR NR 1 HOLE OUT OF LIMITS WITH .540" BUSHING WAS FABRICATED AND INSTALLED WITH OD .329" AND COUNTERSINK .517" IAW SRM 51-22-2A, PAR 6 COND II.Apr 16, 2016 · N997DL · Doug MD88 · Wing, Plate/SkinSDR DALA2016041802978Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA AT FUEL ACCESS PLATE 1335 C. CORROSION WAS REMOVED, ACCESS WAS MEASURED AND WAS FOUND NR 1 HOLE OUT OF LIMITS WITH .675", BUSHING WAS FABRICATED AND INSTALLED WITH OD .439", COUNTERSINK .635" IAW SRM 51-22-2A, PAR Apr 16, 2016 · N997DL · Doug MD88 · Wing, Plate/SkinSDR DALA2016041802977Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE 1478C. FOUND 5 HOLE OUT OF LIMITS, MAXIMUM HOLE MEASURED WITH .543" BUSHING WAS FABRICATED AND INSTALLED WITH OD .329" COUNTERSINK .509" IAW SRM 51-22-2A, PAR 6, CONDITION II.Apr 16, 2016 · N997DL · Doug MD88 · Wing, Plate/SkinSDR DALA2016041802976Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE NR 1436C. ACCESS WAS REPLACED IAW SRM 51-22-2A CONDITION II.Apr 16, 2016 · N997DL · Doug MD88 · Wing, Plate/SkinSDR DALA2016041802975Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE NR 1307C. ACCESS WAS REPLACED IAW SRM 51-22-2A CONDITION II.Apr 16, 2016 · N997DL · Doug MD88 · Wing, Plate/SkinSDR DALA2016041802974Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE NR 2301C. ACCESS WAS REPLACED IAW SRM 51-22-2A, CONDITION II.Apr 16, 2016 · N997DL · Doug MD88 · Wing, Plate/SkinSDR DALA2016041802973Access Panel · corrodedCORROSION ON SETTLEMENT AREA AND COUNTERSINK OF FUEL ACCESS PLATE NR 1410C. ACCESS WAS REPLACED IAW SRM 51-22-2A, CONDITION II.Apr 16, 2016 · N997DL · Doug MD88 · Wing, Plate/SkinSDR DALA2016041702972Cusp Web · corrodedCORROSION ON RT CUSP WEB PREVIOUS REPAIR BETWEEN BS 1231-1250 AND X=-54 TO X=-60. CORROSION WAS REPAIRED IAW SRM 53-05, 51-30-5, 51-10-3, PAR 14, 21, 38. REPAIR DOUBLER WAS REPLACED.Apr 16, 2016 · N997DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2016041702969Cusp Web · corrodedCORROSION ON CUSP WEB UPPER AND LOWER SURFACE BS 541-560 BETWEEN X=54-X=60 LT SIDE. DAMAGE AREA WAS REPAIRED IAW SRM 53-05, FIG 131A-14 , 51-10-3 PAR 14/21, 51-30-1, 51-30-2 AND 51-30-5.Apr 16, 2016 · N997DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2016041803000Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 769G. THE FLOOR PANEL WAS REPAIRED SRM 53-01, FIG 4 , 51-30-2.Apr 15, 2016 · N997DL · Doug MD88 · Fuselage Floor PanelSDR DALA2016041802995Skin · damagedDAMAGE METALIZED ON RUDDER. DAMAGE METALIZED WAS REPAIRED IAW ERA NR 092613-14MA.Apr 15, 2016 · N997DL · Doug MD88 · Rudder, Plate/SkinSDR DALA2016041702970Floor Panel · crackedCRACKED FLOOR PANEL 693A. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-05,51-30-2.Apr 15, 2016 · N997DL · Doug MD88 · Fuselage Floor PanelSDR DALA2016041702968Floor Panel · corrodedCORROSION ON FLOOR PANEL 160G. THE FLOOR PANEL WAS REPLACED IAW SRM 51-10-2, DWG 9957828, REV: Y.Apr 15, 2016 · N997DL · Doug MD88 · Fuselage Floor PanelSDR DALA2016041702967Cusp Web · corrodedSURFACE CORROSION ON RT CUSP WEB BETWEEN BS 579-598 AND X=-54 TO X=-60, CARD 83, ZONE 201. CUSP WEB RT 503 TO 598 WAS REPLACED IAW SRM 51-30-1, AMM 20-30-1, 51-30-2, 51-30-5, DWG 9930538, REV BF.Apr 15, 2016 · N997DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2016041702966Floor Panel · crackedCRACK ON FLOOR PANEL NR 389A AND DISBONDED RUBSTRIP AT CAB PAX. CRACK WAS REPAIRED AND STRIP WAS BONDED IAW SRM 53-01, FIG 4 , 51-30-2 , 51-20-0.Apr 15, 2016 · N997DL · Doug MD88 · Fuselage Floor PanelSDR DALA2016041602962Cusp Web · corrodedCORROSION ON CUSP WEB, UPPER AND LOWER, BS 1028 TO 1030 BETWEEN X=54-X=60 LT SIDE. CORROSION WAS REPAIRED IAW SRM 53-05, FIG 131-A -13 , 51-30-2, 51-30-5 , 51-10-3 PAR 14, 21, 38.Apr 15, 2016 · N997DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2016041802998Bearing · corrodedCORROSION ON RUDDER YOKE BEARING. BEARING WAS REPLACED IAW AMM 27-20-03.Apr 14, 2016 · N997DL · Doug MD88 · Rudder Control SystemSDR DALA2016041502934Cusp Web · crackedCRACK ON CUSP WEB BS 864-868 BETWEEN X=+54 TO X=+60. REMOVED DAMAGE AND FABRICATE A REPAIR IAW SRM 53-05, FIG 131, A-1, SH 1.Apr 14, 2016 · N997DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2016041502932Cusp Web · corrodedCORROSION ON CUSP WEB PREVIOUS REPAIR FROM BS 948 - 961, X 54 - X 60, LT SIDE. DOUBLER PREVIOUS REPAIR WAS REMOVED IAW SRM 51-30-5, PAR 8. REPAIR PARTS WERE FABRICATED IAW SRM 53-05, FIG 131, A-13. REPAIR PARTS WERE INSTALLED IAW SRM 51-30-5, PAR 7. CIC WAApr 14, 2016 · N997DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2016041502931Bolt · damagedDAMAGED UPPER YOKE BOLT TREADS TO ATTACH FWD VIBRATION ABSORBER. UPPER YOKE BOLT WAS REPLACED IAW AMM 71-20-03-201.Apr 14, 2016 · N997DL · Doug MD88 · Engine Mount SectionSDR DALA2016041502930Longeron · crackedCRACK ON LONGERON 7R, BS 1338. LONGERON REMOVED AND REPLACED IAW SRM 51-30-5, FABRICATED IAW SRM 53-14-3, FIG 4.Apr 14, 2016 · N997DL · Doug MD88 · Fuselage Main, Longeron/StringerSDR DALA2016041402913Pan · crackedCRACK ON RING PAN FWD UPPER CORNER BETWEEN BS 886-905, RT AT CABIN PAX. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-05, FIG 122 AND ERA 487747-14MA, REV: ORIGINAL.Apr 13, 2016 · N997DL · Doug MD88 · Fuselage Main, StructureSDR DALA2016041402912Pan · crackedCRACK ON RING PAN STRUCTURE AT AFT LOWER CORNERS BETWEEN BS 1022-1041 AND BS 1041-1060 LT SIDE. REPAIR PARTS WERE FABRICATED, AND INSTALLED IAW SRM 53-05, FIG 122 AND ER/A 487747-14MA, REV ORIGINAL AND REV A.Apr 13, 2016 · N997DL · Doug MD88 · Fuselage Main, StructureSDR DALA2016041402911Pan · crackedCRACK ON RING PAN STRUCTURE AT FWD LOWER CORNERS BETWEEN BS 1174-1193 RT SIDE. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-30-5, 53-05 FIG 122 AND ERA 487747-14MA REV ORIGINAL AND REV A.Apr 13, 2016 · N997DL · Doug MD88 · Fuselage Main, StructureSDR DALA2016041402906Vane · wornWEAR ON PREVIOUS REPAIR UPPER SURFACE ON OTBD VANE, OTBD FLAP, BS XV2-371 AT RT WING. UPPER SURFACE ON OUTBD VANE, OUTBD FLAP, BS XV2-371 RT WING WAS REPAIRED IAW SRM 57-03 PAR II.Apr 13, 2016 · N997DL · Doug MD88 · Trailing Edge FlapsSDR DALA2016041402907Web · corrodedCORROSION ON WEB, BS 139-140, X=15 LT. WEB WAS REPAIRED IAW SRM 53-01, FIG 4, 51-30-2 , 51-10-3, PARA 21, 14, 36.Apr 12, 2016 · N997DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2016041302861Longeron · crackedCRACKED LONGERON 4R, BS 541 AT PAX CABIN. REPAIR THE LONGERON IAW SRM 53-02, FIG 18 AND 51-30-2 , 51-30-5.Apr 12, 2016 · N997DL · Doug MD88 · Fuselage Main, Longeron/StringerSDR DALA2016041302862Skin · damagedLIGHTNING STRIKE ON WINDOW BELT FWD AREA FROM STA 370-389, 346-365 AND 731-750. LIGHTNING STRIKES WERE REPAIRED BY BLENDED OUT AND DIMENTIONS AS FOLLOW: (UT) WAS ACCOMPLISHED IAW NDT-SPM 04-00-07, PAR 5, FIG 3 ON 370-389 RT AT FWD SECTION, ORIGINAL THICKNESS 0Apr 11, 2016 · N997DL · Doug MD88 · Fuselage Main, Plate/SkinSDR DALA2016041202825Cusp Web · corrodedCORROSION ON CUSP WEB UPPER AND LOWER SURFACE FROM BS 826-845 BETWEEN X=44-X=60 LT SIDE. CORROSION WAS REPAIRED IAW SRM 53-05, FIG 131A-6 , 51-10-3, PAR 14, 21, 51-30-5, 51-30-2.Apr 11, 2016 · N997DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2016041202821Seat Track · corrodedCORROSION ON SEAT TRACK -22 BETWEEN BS 200 -256. SEAT TRACK WAS REPLACED IAW SRM 51-30-1, 51-30-5, 51-10-4, 51-10-3 PAR 14 AND 21.Apr 11, 2016 · N997DL · Doug MD88 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016041202820Cusp Web · corrodedCORROSION ON RT CUSP WEB PREVIOUS REPAIR BETWEEN BS 722-731 AND X=-54 TO X=-60, CARD 86 ZONE 201. TRACK WAS REMOVED, DOUBLER WAS REMOVED, DOUBLER AND RING DOUBLER WERE FABRICATED, REPAIR PARTS WERE TREATED AND PAINTED, DOUBLERS AND RING DOUBLERS WERE INSTALLEApr 11, 2016 · N997DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2016041202815Cusp Web · corrodedCORROSION ON RT CUSP WEB, PREVIOUS REPAIR BETWEEN BS 788-807 AND X=-54 TO X=-60. PREVIOUS DOUBLER WAS REMOVED, REPAIR PARTS WERE FABRICATED, REPAIR PARTS WERE INSTALLED, CIC WAS APPLIED, IAW SRM 51-30-2, 53-05, FIG 131A-2, 51-10-3, PAR 14, 21, 38.Apr 10, 2016 · N997DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2016041102764Beam · crackedCRACKED BEAM NR 1 AFT EDGE AT PASSENGER ENTRANCE DOOR L1. BEAM WAS REPAIRED IAW SRM 52-05-D, FIG 97, SHEET 3, 51-30-2, 51-30-5, 51-10-3 PAR 14/21 AND 51-10-2.Apr 10, 2016 · N997DL · Doug MD88 · Passenger/Crew DoorsSDR DALA2016041102763Cusp Web · corrodedCORROSION ON CUSP WEB PREVIOUS REPAIR FROM BS 522-541 BETWEEN X=54-X=60 LT SIDE. REPLACED IAW SRM 51-30-1, 51-30-5, 51-30-2, 53-05, FIG 131A-7, 51-10-3 PAR 21, 14 AND 38.Apr 10, 2016 · N997DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2016041102762Cusp Web · corrodedCORROSION ON RT CUSP WEB PREVIOUS REPAIR BETWEEN BS 598-617 AND X=-54 TO X=-60. CUSP WEB WAS ATTENDED IAW SRM 51-30-2, 51-30-5 AND 53-05, FIG 131A-7, 51-10-3 PAR 14, 21 AND 38.Apr 9, 2016 · N997DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2016040902750Seat Track · corrodedCORROSION ON RT SEAT TRACK PLUG X=-54 BETWEEN BS 370 TO BS 389. PLUG WAS REMOVED, NEW PLUG WAS INSTALLED, CIC WAS APPLIED IAW SRM 51-10-3 PAR 38, 51-30-1, 53-05 FIG 4A, SH 1.Apr 8, 2016 · N997DL · Doug MD88 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016040902748Seat Track · corrodedCORROSION ON SEAT TRACK PLUGS BS 316-982 AT X=22. SEAT TRACK PLUGS REPLACED IAW SRM 51-30-1, 53-05, FIG 4A, SH 1 AND 51-10-3, PAR 38.Apr 8, 2016 · N997DL · Doug MD88 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016040902747Cusp Web · corrodedCORROSION ON RT CUSP WEB PREVIOUS REPAIR BETWEEN BS 996 AND X=-54 TO X=-60. REMOVE AND INSTALLED REPAIR PARTS ON RT CUSP WEB BETWEEN BS 996 AND X=-54 TO X=-60 IAW SRM 51-30-3 AND 51-30-2.Apr 8, 2016 · N997DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2016040902751Skin · crackedCRACKED EXTERNAL REPAIR DOUBLER FWD LOWER CORNER AT PASSENGER ENTRANCE DOOR. REPAIR DOUBLER WAS REPLACED IAW SRM 51-30-2, 52-05D FIG 37, 51-10-3, PAR 14/21.Apr 7, 2016 · N997DL · Doug MD88 · Passenger/Crew DoorsSDR DALA2016040802705Cusp Web · puncturedPUNCTURED RT CUSP WEB BETWEEN BS 484-492 AND X=-44 TO X=-54. PUNCTURED ON RT CUSP WEB WAS REPAIRED IAW SRM 51-30-2, 51-10-3 PAR 19 AND 21 AND 38, 53-05, FIG 131A-17.Apr 7, 2016 · N997DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2016040802703Bushing · corrodedCORROSION ON INNER SURFACE OF FITTING BUSHING RT MLG. CORROSION ON BUSHING BORE RT WAS REMOVED IAW DWG SR 09570087, REV B, NOTE II, MEASURE AFTER REWORK ID 2.337", THEREFORE IS WITHIN LIMITS FOR REPAIR IAW DWG SR09570087, REV: B, NOTE II.Apr 7, 2016 · N997DL · Doug MD88 · Fuselage, Landing Gear Attach FittingsSDR DALA2016040902749Cusp Web · corrodedCORROSION ON CUSP WEB PREVIOUS REPAIR FROM BS 984-1003 BETWEEN X=54-X=60 LT SIDE. CUSP WEB PREVIOUS REPAIR WAS REPLACED IAW SRM 51-30-5 AND 53-05, FIG 131A-14.Apr 6, 2016 · N997DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2016040702695Skin · crackedCRACK ON MID CARGO COMPARTMENT DOOR SKIN NEXT TO OPEN, CLOSE HANDLE HSG MID CARGO COMPARTMENT DOOR SKIN WAS REPAIRED IAW ER/A 486446, MA REV ORIGINAL.Apr 6, 2016 · N997DL · Doug MD88 · Cargo/Baggage DoorsSDR DALA2016040702694Doubler · wornWORN PREVIOUS REPAIR DOUBLERS ON AFT AND FWD LOWER CORNER AT FWD CARGO COMPARTMENT DOOR. REPAIR DOUBLERS WERE REPLACED IAW SRM 51-30-2 AND ER/A 486624-14 REV ORIGINAL.Apr 6, 2016 · N997DL · Doug MD88 · Cargo/Baggage DoorsSDR DALA2016040702689Seat Track · corrodedCORROSION ON SEAT TRACK PLUG BS 419 TO 422, 455 TO 458, 671 TO 674, 701 TO 703 AT X=54 ON CABIN PASSENGER PLUGS WERE REMOVED, NEW PLUGS WERE INSTALLED IAW SRM 51-30-1, 53-05 FIG 4A, SH 1.Apr 6, 2016 · N997DL · Doug MD88 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016040702688Cusp Web · corrodedSEVERE CORROSION ON RT CUSP WEB BETWEEN BS 389-408 AND X=-54 TO X=-60. CUSPS WEB WERE REPAIRED IAW SRM 53-05, FIG 131A AND 51-10-3, PAR 14, 21, 38.Apr 6, 2016 · N997DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2016040702687Seat Track · corrodedCORROSION ON RT SEAT TRACK PLUG X=-22 BETWEEN BS 1231 TO 1212. PLUG WAS REMOVED. NEW PLUG WAS INSTALLED IAW SRM 51-30-1, 53-05, FIG 4A, SH1.Apr 6, 2016 · N997DL · Doug MD88 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016040702686Tab · delaminatedDELAMINATED ON INBD AT ANTI-FLOAT TAB UPPER, LOWER SURFACE LT ELEVATOR. DUE TO EXCESSIVE DAMAGE REPLACED IAW SRM 55-04, PAR 2C.Apr 6, 2016 · N997DL · Doug MD88 · Elevator, Tab Structure
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