# Service difficulty reports: N26SW, cancelled Sep 30, 1997 A list on [N26SW, cancelled Sep 30, 1997](https://openairdocs.org/deregistered/N26SW-1997-09-30.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR 97ZZZX4360](https://openairdocs.org/sdr/97ZZZX4360.md): Stringer · cracked · Sep 8, 1997 · N26SW · Boeing 7372H4 · Fuselage Main, Longeron/Stringer > THREE 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 - [SDR 97ZZZX4359](https://openairdocs.org/sdr/97ZZZX4359.md): Stringer · out of limits · Sep 8, 1997 · N26SW · Boeing 7372H4 · Fuselage Main, Longeron/Stringer > ONE 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. - [SDR 97ZZZX4358](https://openairdocs.org/sdr/97ZZZX4358.md): Floor Beam · cracked · Sep 8, 1997 · N26SW · Boeing 7372H4 · Fuselage Main, Floor Beam > FLOOR 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. - [SDR 97ZZZX4357](https://openairdocs.org/sdr/97ZZZX4357.md): Stringer · doubler cracked · Sep 8, 1997 · N26SW · Boeing 7372H4 · Fuselage Main, Longeron/Stringer > PREVIOUS 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. - [SDR 97ZZZX4356](https://openairdocs.org/sdr/97ZZZX4356.md): Stringer · holes worn · Sep 8, 1997 · N26SW · Boeing 7372H4 · Fuselage Main, Longeron/Stringer > TWO 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. - [SDR 97ZZZX4355](https://openairdocs.org/sdr/97ZZZX4355.md): Stringer · cracked · Sep 8, 1997 · N26SW · Boeing 7372H4 · Fuselage Main, Longeron/Stringer > ONE 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 DATA - [SDR 97ZZZX4354](https://openairdocs.org/sdr/97ZZZX4354.md): Stringer · cracks · Sep 8, 1997 · N26SW · Boeing 7372H4 · Fuselage Main, Longeron/Stringer > THREE 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 - [SDR 97ZZZX4353](https://openairdocs.org/sdr/97ZZZX4353.md): Stringer · cracked · Sep 8, 1997 · N26SW · Boeing 7372H4 · Fuselage Main, Longeron/Stringer > ONE 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. RE - [SDR 97ZZZX4352](https://openairdocs.org/sdr/97ZZZX4352.md): Stringer · cracked · Sep 8, 1997 · N26SW · Boeing 7372H4 · Fuselage Main, Longeron/Stringer > NUMEROUS 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 LIM - [SDR SWAA961238](https://openairdocs.org/sdr/SWAA961238.md): Bulkhead · cracked · Nov 8, 1996 · N26SW · Boeing 7372H4 · Fuselage Main, Bulkhead > DURING SCHEDULED SERVICE VISIT CHECK, FOUND BS 727 BULKHEAD CRACKED. REPAIRED PER BOEING SRM. - [SDR SWAA961016](https://openairdocs.org/sdr/SWAA961016.md): Skin · cracked · Sep 22, 1996 · N26SW · Boeing 7372H4 · Fuselage Miscellaneous Structure > DURING SCHEDULED C1 CHECK, FOUND NOSE W/W CEILING SKIN CRACKED AFT OF MANUAL EXTENSION RETURN SPRING BRACKET. REPAIRED PER BOEING SRM. - [SDR SWAA960738](https://openairdocs.org/sdr/SWAA960738.md): Battery · discharged · Jul 27, 1996 · N26SW · Boeing 7372H4 · Emergency Lighting > DURING SCHEDULED SERVICE CHECK, FOUND FWD EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M. - [SDR SWAA960570](https://openairdocs.org/sdr/SWAA960570.md): Web · cracked · Jun 20, 1996 · N26SW · Boeing 7372H4 · Cargo/Baggage Doors > DURING SCHEDULED B2 CHECK, FOUND FWD CARGO DOOR LOWER WEB CRACKED ORIGINATING FROM RIVET HOLE, ADJACENT TO AFT/LOWER STOP FITTING. REPAIRED PER BOEING SRM. - [SDR SWAA960151](https://openairdocs.org/sdr/SWAA960151.md): Retract Mech · malfunctioned · Mar 11, 1996 · N26SW · Boeing 7372H4 · Landing Gear Retraction/Extension System > AFTER 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. - [SDR SWAA950553](https://openairdocs.org/sdr/SWAA950553.md): Web · cracked · Jul 22, 1995 · N26SW · Boeing 7372H4 · Fuselage Miscellaneous Structure > DURING SCHEDULED CHECK, FOUND NOSE WHEELWELL LEFT VERTICAL WEB CRACKED 3.1 INCHES, BELOW FWD LEFT ACCESS PANEL. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. - [SDR SWAA950488](https://openairdocs.org/sdr/SWAA950488.md): Skin · cracked · Jun 24, 1995 · N26SW · Boeing 7372H4 · Fuselage Main, Plate/Skin > DURING 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. - [SDR SWAA950487](https://openairdocs.org/sdr/SWAA950487.md): Skin · cracked · Jun 24, 1995 · N26SW · Boeing 7372H4 · Fuselage Main, Plate/Skin > DURING 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. - [SDR SWAA950486](https://openairdocs.org/sdr/SWAA950486.md): Skin · cracked · Jun 24, 1995 · N26SW · Boeing 7372H4 · Fuselage Main, Plate/Skin > DURING SCHEDULED MAINT VISIT, FOUND FUSELAGE SKIN CRACKED THREE PLACES AT BS 227.8, BETWEEN S13 AND 16L. REPAIRED PER DALFORT XEA X2-53-154. ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/deregistered/N26SW-1997-09-30/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. 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