Boeing 737-401

Service difficulty reports · 2,961

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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 aircraft_model_key = '737401'
  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 USAA011107Skin · crackedCLT - FOUND SKIN CRACKED 1 INCH, BS 727 D AND 3 INCHES AT STRINGER 23L. INSTALLED DOUBLER PER TR 53-60-03. (M)Aug 20, 2001 · N404US · Boeing 737401 · Fuselage Structure (General)SDR USAA011108Skin · crackedCLT - FOUND SKIN CRACKED 2 INCHES, BS 727D PLUS 17 INCHES STRINGER 24R. INSTALLED DOUBLER PER SRM 53-00-01. (M)Aug 20, 2001 · N404US · Boeing 737401 · Fuselage Structure (General)SDR USAA011096SkinCLT - FOUND SKIN OIL CAN IN AFT PRESSURE BULKHEAD, BS 1016. INSTALLED DOUBLER PER SRM 53-80-08 FIG 201. (M)Aug 15, 2001 · N411US · Boeing 737401 · Fuselage Structure (General)SDR USAASB01231Battery Pack · inoperativeCLT - MAINTENANCE FOUND THE AFT SECTION OF CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK. ALL EMERGENCY LIGHTS OPERATIONALLY CHECKED GOOD. (M)Aug 14, 2001 · N423US · Boeing 737401 · Emergency LightingSDR USAASB01223Socket · defectiveCLT - MAINTENANCE FOUND THE RIGHT OVERWING EMERGENCY EXIT LIGHT, THAT ILLUMINATES THE AREA AFT OF THE FLAPS, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT OVERWING EMERGENCY EXIT LIGHT SOCKET. OPS CHECK GOOD. (M)Aug 6, 2001 · N408US · Boeing 737401 · Emergency LightingSDR USAA010958Bulkhead · damagedCLT - FOUND PRESSURE WEB WITH ELONGATED HOLES, .281 INCH TO .321 INCH, BS 178, WL 207. DAMAGE REMOVED, INSTALLED ACCESS HOLE DOUBLER PER EA 85146. (M)Jul 27, 2001 · N413US · Boeing 737401 · Fuselage Main, BulkheadSDR USAA010959Bulkhead · crackedCLT - FOUND PRESSURE WEB CRACKED .5 INCH, BS 178 WL 217 AT LBL 6. DAMAGE REMOVED, REPAIR DOUBLER INSTALLED PER EO 5300V153. (M)Jul 27, 2001 · N413US · Boeing 737401 · Fuselage Main, BulkheadSDR USAA010960Stiffener · crackedCLT - FOUND VERTICAL CHORD CRACKED IN TWO PLACES .25 INCH EACH, BS 178, WL 184 AND 195 AT LBL 5.7. DOUBLER INSTALLED PER EO 5300V155. (M)Jul 27, 2001 · N413US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA010956Frame · crackedCLT - FOUND SIDE CHORDS .5 INCH, BS 178 WL 207 LEFT AND RIGHT SIDE. DAMAGE SECTION REMOVED, INSTALLED CHORD SPLICE REPAIR AND EXT SKIN STRAP PER EO 5300V157. (M)Jul 27, 2001 · N413US · Boeing 737401 · Fuselage Main, FrameSDR USAA010957Strap · damagedCLT - FOUND VERTICAL STRAP .125 INCH, BS 178, WL 208, LBL 25. DAMAGE SECTION REMOVED, REPLACEMENT SECTION SPLICED IN WITH DOUBLER PER EA 85114. (M)Jul 27, 2001 · N413US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA010927Bulkhead · crackedPIT - FOUND BULKHEAD WITH CRACKS, ONE AT 1 INCH, ONE AT 1.125 INCH, TWO AT 1.5 INCH AND TWO AT .125 INCH, BS 178 LBL 5.7 WL 216; BL 0, WL 184 - WL 195; RBL 5. CUT OUT DAMAGE, INSTALLED FILLER AND DOUBLER PER SRM 53-10-08, EO 5300V152, EO 5300V153. (M)Jul 19, 2001 · N412US · Boeing 737401 · Fuselage Structure (General)SDR USAA010929Frame · crackedPIT - FOUND VERTICAL CHORD CRACKED 1.5 INCHES, BS 178 RBL 5.7 WL 184. CUT OUT DAMAGED AREA, INSTALLED FILLER AND DOUBLERS PER SRM 53-10-08, FIG 205 EA 71759, EO 5300V155. (M)Jul 18, 2001 · N412US · Boeing 737401 · Fuselage Main, FrameSDR USAA010931Frame · crackedPIT - FOUND SIDE CHORD CRACKED TWO PLACES 1 INCH, LBL 24 WL 207 WL 195. CUT OUT DAMAGED SECTION AND SPLICED IN NEW PER SRM 53-10-08, EO 5300V157. (M)Jul 18, 2001 · N412US · Boeing 737401 · Fuselage Main, FrameSDR USAA010932Frame · crackedPIT - FOUND SIDE CHORD HAS TWO CRACKS 1 INCH EACH, RBL 24 WL 207 WL 195. CUT OUT DAMAGED SECTION AND SPLICED IN NEW PER SRM 53-10-08, EO 5300V157. (M)Jul 18, 2001 · N412US · Boeing 737401 · Fuselage Main, FrameSDR USAA010906Bulkhead · crackedCLT - FOUND NUMEROUS CRACK .2 INCH TO 1 INCH, BULKHEAD WEB BS 178 WL 198 TO 213, LBL 6.5 TO RBL 6.5. DAMAGE REMOVED, REPAIR DOUBLER INSTALLED PER SRM 53-10-08 FIG 211, EA 85068, AND EO 5300V153. (M)Jul 13, 2001 · N422US · Boeing 737401 · Fuselage Main, BulkheadSDR USAA010907Bulkhead · crackedCLT - FOUND TWO CRACKS 1 INCH LONG, BS 178, WL 195 AT RBL 7, WL 202 AT LBL 5.7. REMOVED AND REPLACED WEB STRAPS PER SRM 53-10-08, 53-10-02, 51-40-02 AND EO 5300V155. (M)Jul 13, 2001 · N422US · Boeing 737401 · Fuselage Main, BulkheadSDR USAA010908Bulkhead · damagedCLT - FOUND BULKHEAD WEB BLIND FASTENER INSTALLED DOUBLER, BS 178, WL 195 TO 203, RBL 17 TO RBL 27 APPROX 10 INCHES BY 12 INCHES. REMOVED DOUBLER, INSTALLED NEW DOUBLER PER SRM 53-10-08 FIG 211, EA 85068, AND EO 5300V153. (M)Jul 13, 2001 · N422US · Boeing 737401 · Fuselage Main, BulkheadSDR USAA010909Frame · crackedCLT - FOUND SIDE CHORD CRACKED 1 INCH, BS 178, RIGHT SIDE WL 207. REMOVED DAMAGED SECTION, SPLICED IN NEW CHORD SECTION PER EO 5300V157. (M)Jul 13, 2001 · N422US · Boeing 737401 · Fuselage Main, FrameSDR USAA010910Pressure Panel · crackedCLT - FOUND FLOORWEB CRACKED .25 INCH, BS 180, WL 207, RBL 28. REMOVED AND REPLACED FLOOR WEB PER SRM 51-40-02 AND EO 5300V157. (M)Jul 13, 2001 · N422US · Boeing 737401 · Fuselage Main, BulkheadSDR USAA010776Bulkhead · crackedCLT - FOUND BULKHEAD WEB CRACKED NUMEROUS AREAS .5 INCH TO 1.5 INCH, BS 178, WL 186 TO 234, LBL 12 TO RBL 6.5. DAMAGE REMOVED, INSTALLED REPAIR DOUBLER AND FILLERS PER EO 5300V153 AND EA 69888. (M)Jul 2, 2001 · N408US · Boeing 737401 · Fuselage Main, BulkheadSDR USAA010777Frame · crackedCLT - FOUND SIDE CHORDS CRACKED TWO PLACES 1.5 INCH EACH, BS 178 WL 207 LEFT AND RIGHT. DAMAGE REMOVED, SPLICED IN NEW CHORD SECTION PER EO 5300V157. (M)Jul 2, 2001 · N408US · Boeing 737401 · Fuselage Main, FrameSDR USAA010778Pressure Panel · crackedCLT - FOUND FLOORWEB CRACKED .5 INCH, BS 178 WL 207 LEFT SIDE. REMOVED AND REPLACED WEB PER EO 5300V157. (M)Jul 2, 2001 · N408US · Boeing 737401 · Fuselage Main, BulkheadSDR USAA010779Web · crackedCLT - FOUND WEB CRACKED .5 INCH, BS 178 WL 207 AT RIGHT SIDE CHORD. DAMAGE REMOVED, INSTALLED DOUBLER PER EO 5300V157. (M)Jul 2, 2001 · N408US · Boeing 737401 · Fuselage Structure (General)SDR USAASB01187Transmitter · faultyCLT - FLT 1157 - IN PREPARATION FOR LANDING AT CLT, FROM ORD, CREW REPORTED A SPLIT FLAP INDICATION AS FLAPS WERE STUCK AT 7 DEGREES. FLIGHT LANDED WITHOUT FURTHER INCIDENT WITH NO EMERGENCY BEING DECLARED. MAINTENANCE REMOVED AND REPLACED THE RIGHT FLAP POSJun 28, 2001 · N407US · Boeing 737401 · Flight Control SystemSDR USAA010761Skin · crackedCLT - FOUND AFT CARGO DOOR SKIN CRACKED .5 INCH, HANDLE CUTOUT, AFT UPPER CORNER. DAMAGE REMOVED, INSTALLED REPAIR DOUBLER PER SRM 52-30-03. (M)Jun 22, 2001 · N418US · Boeing 737401 · DoorsSDR USAA010756Skin · crackedTPA - FOUND FUSELAGE SKIN CRACKED .75 INCH, BS 294, MED LOWER HINGE CUTOUT BETWEEN S13L AND 14L. REPAIR DOUBLER INSTALLED PER SRM 53-10-01, FIG 205. (M)Jun 22, 2001 · N418US · Boeing 737401 · Fuselage Main, Plate/SkinSDR USAA010762Skin · crackedCLT - FOUND FUSELAGE SKIN CRACKED .75 INCH, BS 294.5, MED LOWER HINGE CUTOUT. INSTALLED REPAIR DOUBLER PER SRM 53-10-01, FIG 205. (M)Jun 21, 2001 · N418US · Boeing 737401 · Fuselage Structure (General)SDR USAASB01180Circuit Breaker · faultyCLT - FLT 682 - UPON DESCENT INTO CLT, FROM MIA, CAPTAIN DECLARED AN EMERGENCY WHEN HE HEARD A LOUD POP AND LOST HIS FLIGHT INSTRUMENTS. FIRST OFFICERS FLIGHT INSTRUMENTS SEEMED TO BE WORKING FINE. ONCE ON THE TAXI-WAY, THERE WAS REPORT OF A SMOKE SMELL. EVJun 19, 2001 · N405US · Boeing 737401 · AC Power Distribution SystemSDR USAA010754Bulkhead · crackedCLT - FOUND BULKHEAD WEB WITH 3 CRACKS ALL .5 INCHES LONG, BS 178, WL 198 AT LBL 5.7 AND RBL 5.7, WL 212 AT RBL 5.7. DAMAGED REMOVED, INSTALLED REPAIR DOUBLER PER EO 5300V153. (M)Jun 16, 2001 · N409US · Boeing 737401 · Fuselage Main, BulkheadSDR USAA010755Frame · crackedCLT - FOUND LEFT AND RIGHT SIDE CHORDS WITH 3 CRACKS, .25 INCH, 2 INCHES, AND 3 INCHES, BS 178, WL 207 AND LBL AND RBL 26, WL 202 AT LBL 27. DAMAGED REMOVED, INSTALLED SPLICE CHORD REPAIRS PER EO 5300V157. (M)Jun 16, 2001 · N409US · Boeing 737401 · Fuselage Main, FrameSDR USAA010750Bulkhead · crackedCLT - FOUND BULKHEAD WEB WITH FOUR CRACKS, 1 WAS .125 INCH, AND 3 WERE .5 INCH, BS 178 WL 189 TO 203, LBL 5.5 TO RBL 5.7. DAMAGE REMOVED, REPAIR DOUBLER INSTALLED PER EO 5300V153 AND SRM 53-10-08. (M)Jun 16, 2001 · N409US · Boeing 737401 · Fuselage Main, BulkheadSDR USAA010681Skin · crackedCLT - FOUND SKIN CRACKED, BS 727D, LEFT SIDE, EMERGENCY LIGHT AFT OF WHEEL WELL. DAMAGE REMOVED, INSTALLED DOUBLER PER SRM 53-00-01, FIG 202. (M)Jun 14, 2001 · N413US · Boeing 737401 · Fuselage Main, Plate/SkinSDR USAASB01171Switch · defectiveMIA - DURING PREFLIGHT, PILOT REPORTED THAT THE EMERGENCY EXIT LIGHTS ILLUMINATED WHILE NORMAL ELECTRICAL AC/DC POWER TO ALL BUSSES WAS AVAILABLE. LIGHTS WOULD NOT EXTINGUISH. MAINTENANCE REMOVED AND REPLACED A DEFECTIVE EMERGENCY LIGHT ARMING SWITCH ON THE Jun 11, 2001 · N423US · Boeing 737401 · Emergency LightingSDR USAA010621Web · crackedCLT - FOUND FLOOR WEB CRACKED .25 INCH, BS 179, LBL 27 WL 207. REMOVED AND REPLACED WEB PER EO 5300V157. (M)Jun 8, 2001 · N409US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA010623Web · crackedCLT - FOUND FLOOR WEB CRACKED .25 INCH, BS 179, RBL 27, WL 207. REMOVED AND REPLACED FLOOR WEB PER EO 5300V157. (M)Jun 8, 2001 · N409US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAASB01167Wire · brokenPVD - MAINTENANCE FOUND THE EMERGENCY LIGHT AT THE LAST SEAT ROW INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE BENEATH THE SEAT. OPS CHECK GOOD. (M)Jun 7, 2001 · N421US · Boeing 737401 · Light System WiringSDR USAA010567Bulkhead · crackedCLT - FOUND PRESSURE WEB .5 INCH, .75 INCH AND 1.5 INCH, BS 178 WL 199 AND 201, LBL 6.5 TO RBL 6.5. REMOVED DAMAGED, INSTALLED REPAIR FILLERS AND DOUBLER PER EO 5300V153. (M)May 25, 2001 · N407US · Boeing 737401 · Fuselage Main, BulkheadSDR USAA010568Doubler · crackedCLT - FOUND REPAIR DOUBLER CRACKED .5 INCH, NR 2 SLAT, OUTBOARD OF ACTUATOR ATTACH. REMOVED CRACKED DOUBLER, INSTALLED NEW DOUBLER PER SRM 57-43-01. (M)May 25, 2001 · N407US · Boeing 737401 · Leading Edge DevicesSDR USAA010586Skin · crackedPIT - FOUND SKIN CRACKED 2.5 INCHES, STRINGER 23R STATION 727D. CUT OUT DAMAGE, INSTALLED EXTERNAL DOUBLER PER EA 71032 AND SRM 53-00-01 FIG 202. (M)May 10, 2001 · N413US · Boeing 737401 · Fuselage Structure (General)SDR USAA010513Bulkhead · brokenCLT - FOUND PRESSURE BULKHEAD WEB WITH BROKEN AREA .5 INCH BY .5 INCH, BS 178 WL 183 AT RBL 17. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER. (M)May 7, 2001 · N423US · Boeing 737401 · Fuselage Main, BulkheadSDR USAA010511Bulkhead · crackedCLT - FOUND PRESSURE BULKHEAD WEB WITH THREE CRACKS, .125 INCH, .250 INCH AND .85 INCH, BS 178 WL 188 AND WL 234 RBL .5 TO LBL 12. DAMAGE CUTOUT, INSTALLED FILLERS AND REPAIR DOUBLER PER SRM 53-10-08 FIG 209, EO 5300V153 AND EA 69580. (M)May 7, 2001 · N423US · Boeing 737401 · Fuselage Main, BulkheadSDR USAA010510Frame · crackedCLT - FOUND LEFT SIDE CHORD CRACKED 1.2 INCH, BS 178 WL 207. DAMAGE REMOVED, SPLICED IN NEW CHORD SECTION PER EO 5300V157. (M)May 7, 2001 · N423US · Boeing 737401 · Fuselage Main, FrameSDR USAA010471Bulkhead · crackedCLT - FOUND PRESSURE WEB CRACKED TWO PLACES .125 INCH BOTH LOCATIONS, BS 178, WL 213 RBL 5.5 AND WL 234 RBL 10. DAMAGE REMOVED, INSTALLED REPAIR DOUBLER PER EO 5300V153 AND SRM 53-10-08 FIG 209. (M)Apr 27, 2001 · N423US · Boeing 737401 · Fuselage Main, BulkheadSDR USAA010404Frame · crackedCLT - FOUND SIDE CHORD CRACKED .25 INCH, BS 178, WL 207, LBL 26. CUTOUT DAMAGE, SPLICED IN NEW SIDECHORD SECTION. (M)Apr 16, 2001 · N421US · Boeing 737401 · Fuselage Main, FrameSDR USAA010403Frame · crackedCLT - FOUND SIDE CHORD CRACKED .5 INCH, BS 178, WL 207 RBL 26. CUT OUT DAMAGE, SPLICED IN NEW SIDE CHORD SECTION EO 5300V157. (M)Apr 16, 2001 · N421US · Boeing 737401 · Fuselage Main, FrameSDR USAA010402Bulkhead · crackedCLT - FOUND BULKHEAD WEB CRACKED 1 INCH, BS 178, LBL 5.7, WL 210. INSTALLED DOUBLER, EO5300V153 AND EA 69407. (M)Apr 16, 2001 · N421US · Boeing 737401 · Fuselage Main, BulkheadSDR USAA010401Bulkhead · crackedCLT - FOUND BULKHEAD WEB CRACKED 1 INCH, BS 178, RBL 5.7, WL 199. INSTALLED DOUBLER, EO5300V153 AND EA 69407. (M)Apr 16, 2001 · N421US · Boeing 737401 · Fuselage Main, BulkheadSDR USAA010400Bulkhead · crackedCLT - FOUND BULKHEAD WEB CRACKED 1 INCH, BS 178, RBL 5.7, WL 201.5. INSTALLED DOUBLER, EO5300V153 AND EA 69407. (M)Apr 16, 2001 · N421US · Boeing 737401 · Fuselage Main, BulkheadSDR USAA010399Bulkhead · crackedCLT - FOUND BULKHEAD WEB CRACKED 1 INCH, BS 178, LBL 5.7, WL 201.5. INSTALLED DOUBLER, EO 5300V153 AND EA 69407. (M)Apr 16, 2001 · N421US · Boeing 737401 · Fuselage Main, BulkheadSDR USAA010398Bulkhead · crackedCLT - FOUND BULKHEAD WEB CRACKED .25 INCH AND .5 INCH, BS 178, WL 189, LBL .5 AND RBL .5. INSTALLED 1 REPAIR DOUBLER FOR BOTH CRACKS, EO 5300V153 AND EA 69407.Apr 16, 2001 · N421US · Boeing 737401 · Fuselage Main, Bulkhead
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