N26SW, cancelled Sep 30, 1997

Service difficulty reports · 18

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 = 'N26SW' AND deregistration_id = 'N26SW-1997-09-30'
  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 97ZZZX4360Stringer · crackedTHREE ATTACHMENT HOLES CRACKED BEYOND LIMITS, LOWER SKIN LAP ROW AT STA 269 THROUGH STA 285, STR 19L. LIMITS BASED ON AD 64-25-05. REPAIRED PER DALFORT AVIATION XEA NR X2-53-176 DATED 7-1-97 AND XEA NR X2-53-173 REV 3 DATED 7-1-97. APPROVAL DATA: FAA FORM Sep 8, 1997 · N26SW · Boeing 7372H4 · Fuselage Main, Longeron/StringerSDR 97ZZZX4359Stringer · out of limitsONE EACH 0.233 INCH DIAMETER HOLE OUT OF ALLOWABLE LIMITS PER DALFORT AVIATION XEA NR X2-53-168. LOCATED AT STR 10L, STA 393. REPAIRED PER DALFORT AVIATION XEA NR X2-53-168, REV 3 DATED 6-30-97. APPROVAL DATA: FAA FORM 8110-3 DATED 6-27-97.Sep 8, 1997 · N26SW · Boeing 7372H4 · Fuselage Main, Longeron/StringerSDR 97ZZZX4358Floor Beam · crackedFLOOR BEAM CRACKED, STA 685, STR 62R. REPAIRED PER DALFORT AVIATION XEA NR X2-53-180 REV 1 DATED 7-18-97. APPROVAL DATA: FAA FORM 8110-3 DATED 7-29-97.Sep 8, 1997 · N26SW · Boeing 7372H4 · Fuselage Main, Floor BeamSDR 97ZZZX4357Stringer · doubler crackedPREVIOUS REPAIR IS NOT IN C/W SB 737-53-A 1177 AND THE INNER DOUBLER IS CRACKED AT STA 380, STR 19R. REPAIRED PER DALFORD AVIATION XEA NR X2-53-182 REV 1 DATED 7-31-97. APPROVAL DATA: FAA 8110-3 DATED 8-18-97.Sep 8, 1997 · N26SW · Boeing 7372H4 · Fuselage Main, Longeron/StringerSDR 97ZZZX4356Stringer · holes wornTWO EACH ATTTACHMENT HOLES CRACKED BEYOND ALLOWABLE LIMITS. LOCATED IN LOWER ROW SKIN LAP ON STR 14L, STA 540. LIMITS BASED ON AD 94-25-05. REPAIRED PER DALFORT AVIATION XEA NR X2-53-184 REV 1 DATED 8-20-97. APPROVAL DATA: FAA FORM 8110-3 DATED 8-19-97.Sep 8, 1997 · N26SW · Boeing 7372H4 · Fuselage Main, Longeron/StringerSDR 97ZZZX4355Stringer · crackedONE EACH ATTACHMENT HOLE CRACKED BEYOND ALLOWABLE LIMITS, LOWER ROW SKIN LAP. LOCATED AT STA 344, STR 14R. LIMITS BASED ON AD 95-25-05. REPAIRED PER DALFORT AVIATION XEA NR X2-53-177 REV 1 DATED 7-17-97 AND XEA NR X2-53-17 REV 3 DATED 7-1-97. APPROVAL DATASep 8, 1997 · N26SW · Boeing 7372H4 · Fuselage Main, Longeron/StringerSDR 97ZZZX4354Stringer · cracksTHREE EACH ATTACHMENT HOLES OUT OF ALLOWABLE LIMITS. LOCATED AT STR 10L AT STATIONS 445, 485, AND 507. LIMITS BASED ON DALFORT AVIATION XEA NR X2-53-168, REV 2, DATED 6-30-97. TWO ATTACHMENT HOLES CRACKED BEYOND ALLOWABLE LIMITS. LOCATED ON LOWER ROW SKIN Sep 8, 1997 · N26SW · Boeing 7372H4 · Fuselage Main, Longeron/StringerSDR 97ZZZX4353Stringer · crackedONE EACH ATTACHMENT HOLE CRACKED BEYOND LIMITS, STR 14R, STA 734 AND STR 10L, STA'S 498 AND 500. ONE EACH ATTACHMENT HOLE CRACKED BEYOND LIMITS, STR 14L, STA 416 AND STA 443, AND, STR 20L, STA 827 AND STA 887. ABOVE MENTIONED LIMITS BASED ON AD 94-25-05. RESep 8, 1997 · N26SW · Boeing 7372H4 · Fuselage Main, Longeron/StringerSDR 97ZZZX4352Stringer · crackedNUMEROUS FASTENER HOLES CRACKED BEYOND LIMITS, STR 4L, STA 360 TO STA 908, AND STR 4R, STA 360 TO STA 908. NUMEROUS FASTENER HOLES CRACKED BEYOND LIMITS, STR 10R, STA 727 TO STA 908, AND STR 10L, STA 360 TO STA 540, AND STA 727 TO STA 908. ABOVE MENTIONED LIMSep 8, 1997 · N26SW · Boeing 7372H4 · Fuselage Main, Longeron/StringerSDR SWAA961238Bulkhead · crackedDURING SCHEDULED SERVICE VISIT CHECK, FOUND BS 727 BULKHEAD CRACKED. REPAIRED PER BOEING SRM.Nov 8, 1996 · N26SW · Boeing 7372H4 · Fuselage Main, BulkheadSDR SWAA961016Skin · crackedDURING SCHEDULED C1 CHECK, FOUND NOSE W/W CEILING SKIN CRACKED AFT OF MANUAL EXTENSION RETURN SPRING BRACKET. REPAIRED PER BOEING SRM.Sep 22, 1996 · N26SW · Boeing 7372H4 · Fuselage Miscellaneous StructureSDR SWAA960738Battery · dischargedDURING SCHEDULED SERVICE CHECK, FOUND FWD EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M.Jul 27, 1996 · N26SW · Boeing 7372H4 · Emergency LightingSDR SWAA960570Web · crackedDURING SCHEDULED B2 CHECK, FOUND FWD CARGO DOOR LOWER WEB CRACKED ORIGINATING FROM RIVET HOLE, ADJACENT TO AFT/LOWER STOP FITTING. REPAIRED PER BOEING SRM.Jun 20, 1996 · N26SW · Boeing 7372H4 · Cargo/Baggage DoorsSDR SWAA960151Retract Mech · malfunctionedAFTER TAKEOFF, CREW WAS UNABLE TO RAISE GEAR WITHOUT USING OVERRIDE TRIGGER. AIRCRAFT RETURNED TO DAL AND MADE AN UNEVENTFUL LANDING. CYCLED GEAR SEVERAL TIMES, NO DEFECTS NOTED. RESET LANDING GEAR POSITION LIGHTS C/B.Mar 11, 1996 · N26SW · Boeing 7372H4 · Landing Gear Retraction/Extension SystemSDR SWAA950553Web · crackedDURING SCHEDULED CHECK, FOUND NOSE WHEELWELL LEFT VERTICAL WEB CRACKED 3.1 INCHES, BELOW FWD LEFT ACCESS PANEL. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.Jul 22, 1995 · N26SW · Boeing 7372H4 · Fuselage Miscellaneous StructureSDR SWAA950488Skin · crackedDURING SCHEDULED MAINT VISIT, FOUND FUSELAGE SKIN CRACKED AT AFT LOWER CORNER OF FORWARD AIRSTAIRS DOORWAY CUTOUT AT DOUBLER. REPAIRED PER DALFORT XEA X2-53-153.Jun 24, 1995 · N26SW · Boeing 7372H4 · Fuselage Main, Plate/SkinSDR SWAA950487Skin · crackedDURING SCHEDULED MAINT VISIT, FOUND FUSELAGE SKIN CRACKED AT AFT LOWER CORNER OF FORWARD AIRSTAIRS DOORWAY CUTOUT AT THREE PLACES AT BS 227.8, BETWEEN S13 AND 16L. REPAIRED PER DALFORT XEA X2-53-154.Jun 24, 1995 · N26SW · Boeing 7372H4 · Fuselage Main, Plate/SkinSDR SWAA950486Skin · crackedDURING SCHEDULED MAINT VISIT, FOUND FUSELAGE SKIN CRACKED THREE PLACES AT BS 227.8, BETWEEN S13 AND 16L. REPAIRED PER DALFORT XEA X2-53-154.Jun 24, 1995 · N26SW · Boeing 7372H4 · Fuselage Main, Plate/Skin
Back to N26SW, cancelled Sep 30, 1997