Boeing 737-228
Service difficulty reports · 371
Newest first. General aviation reporting is voluntary.
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 = '737228' 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 aircraft_model_key = '737228' 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 EF2R2000311Frame · crackedDURING ROUTINE INSPECTION, THE BS 178 BULKHEAD VERTICAL CHORD AT LBL 5.7 WAS FOUND CRACKED AT WL 184 OB RADIUS. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR.SDR EF2R2000310Rib · crackedDURING ROUTINE INSPECTION, THE LT HORIZONTAL STABILIZER LEADING EDGE IB RIB WAS FOUND TO BE CRACKED. REMOVED DAMAGED RIB. FABRICATED REPAIR, INSTALLED REPAIR AND REINSTALLED RIB.SDR EF2R2000309Intercostal · crackedDURING ROUTINE INSPECTION, THE INTERCOSTAL AT BS 500B, STR27L WAS FOUND TO BE CRACKED. REMOVED DAMAGED INTERCOSTAL. FABRICATED REPLACEMENT INTERCOSTAL AND INSTALLED.SDR EF2R2000308Intercostal · corrodedDURING ROUTINE INSPECTION, THE INTERCOSTAL FROM BS747-767 AT STR25R WAS FOUND CORRODED BEYOND ALLOWED LIMITS. REMOVED THE DAMAGED INTERCOSTAL. FABRICATED REPLACEMENT INTERCOSTAL AND INSTALLED.SDR EF2R2000307Intercostal · corrodedDURING ROUTINE INSPECTION, THE INTERCOSTAL BETWEEN STR 26R-27R, FROM BS727A-727B WAS FOUND CORRODED BEYOND ALLOWED LIMITS. REMOVED DAMAGED INTERCOSTAL. FABRICATED REPLACEMENT INTERCOSTAL AND INSTALLED.SDR EF2R2000306Rib · wornDURING ROUTINE INSPECTION, THE LT ELEVATOR HINGE RIB WEB AT ELEV STA66.54 WAS FOUND TO BE WORN BEYOND ALLOWED LIMITS. REMOVED ELEVATOR HINGE RIB WEB. REPAIRED AND REINSTALLED ELEVATOR HINGE RIB WEB.SDR EF2R2000305Bulkhead · crackedDURING ROUTINE INSPECTION, THE BS178 BULKHEAD FLOOR WEB AT WL207, RBL26 WAS FOUND CRACKED. REMOVED DAMAGED FLOOR WEB. FABRICATED, AND INSTALLED REPLACEMENT FLOOR WEB.SDR EF2R2000304Bulkhead · crackedDURING ROUTINE INSPECTION, THE BS178 BULKHEAD FLOOR WEB AT WL207,LBL26 WAS FOUND TO BE CRACKED. REMOVED DAMAGED WEB. FABRICATED, AND INSTALLED REPLACEMENT WEB.SDR EF2R2000303Intercostal · crackedDURING ROUTINE INSPECTION, THE RT BS178 BULKHEAD INTERCOSTAL AT WL195, WAS FOUND TO BE CRACKED. REMOVED DAMAGED INTERCOSTAL. FABRICATED AND PERFORMED PREVENTATIVE MODIFICATION TO REPLACEMENT INTERCOSTAL, INSTALLED.SDR EF2R2000302Intercostal · crackedDURING ROUTINE INSPECTION, THE LT BS178 BULKHEAD INTERCOSTAL AT WL195, WAS CRACKED. REMOVED DAMAGED INTERCOSTAL. FABRICATED AND MADE PREVENTATIVE MODIFICATION TO INTERCOSTAL, INSTALLED.SDR EF2R2000298Panel · corrodedDURING ROUTINE INSPECTION, THE LT TRANSISTION PANEL IN THE FORWARD BAG BIN WAS FOUND TO BE CORRODED BEYOND ALLOWED LIMITS FROM BS 500A-500B. REMOVED DAMAGED LT TRANSITION PANEL FROM BS 480-520. REPLACED WITH NEW PANEL.SDR EF2R2000297Tie Clip · crackedDURING ROUTINE INSPECTION, THE TIE CLIP AR BS 460, STR 27R WAS FOUND TO BE CRACKED. REMOVED DAMAGED TIE CLIP. INSTALLED FABRICATED REPLACEMENT TIE CLIP.SDR EF2R2000296Floor Panel · crackedDURING ROUTINE INSPECTION, THE FLOOR PANEL BENEATH THE CAPTAINS RUDDER PEDALS WAS FOUND TO BE CRACKED. REMOVED DAMAGED PANEL. INSTALLED REPLACEMENT PANEL.SDR EF2R2000295Cowling · gougedDURING ROUTINE INSPECTION, THE NR 2 ENGINE INBOARD COWL SIXTH RIB FROM FORWARD WAS FOUND TO BE GOUGED BEYOND ALLOWED LIMITS. REMOVED DAMAGED AREA FROM RIB. INSTALLED FABRICTED A REPAIR ANGLE.SDR F3LA200000257Hinge · crackedDURING C-5 CHECK, INSPECTION REPORTED CENTER HINGE FOR RT AILERON CASTING CRACKED AT WING FIXED TRAILING EDGE PANEL SCREW HOLE. MAINTENANCE REMOVED CASTING PER SRM 51-30-2, LOCATED AND DRILLED NEW CASTING PER SRM 51-10-1 AND INSTALLED PER SRM 51-30-2.SDR F3LA200000254Charger · failedDURING C-5 CHECK, INSPECTION REPORTED FORWARD CEILING BULLNOSE EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE REPLACED BATTERY CHARGER.SDR F3LA200000252Web · chafedDURING C-5 CHECK, INSPECTION REPORTED VERTICAL STABILIZER FORWARD BULKHEAD AT STA 1010 DAMAGED. REMOVED AND REPLACED DAMAGED WEB PER SRM 51-30-2 AND BOEING DRAWING 65-52913.SDR F3LA200000251Angle · crackedDURING C-5 CHECK, INSPECTION REPORTED SUPPORT ANGLE UNDER LT WING-TO-BODY FAIRING AT STA 540, STR 21-L CRACKED. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR ANGLE PER SRM 51-30-2 AND 51-40-3.SDR F3LA200000250Angle · crackedDURING C-4 CHECK, INSPECTION REPORTED SUPPORT ANGLE UNDER RT WING-TO-BODY FAIRING AT STA 540, STR 21-R CRACKED. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED REPAIR ANGLE AND DOUBLER AND INSTALLED PER SRM 51-4-3.SDR F3LA99130Skin · crackedDEN - DURING SERVICE CHECK, INSPECTION REPORTED A 2.5 INCH CRACK AT THE LOWER AFT CORNER OF THE R-1 DOOR CUTOUT. MAINTENANCE REPAIRED PER SRM 53-30-3, FIG 26, PAGE 90 THROUGH PAGE 92B. CYCLES: 187. (X)SDR F3LA99128Detent Arm · out of adjustDEN - FLT 416 - FLIGHT CREW REPORTED AIRCRAFT ROLLED TO RIGHT WITH FLAPS EXTENDED AND REQUIRED 10 DEGREES AILERON TO COMPENSATE. MAINTENANCE ADJUSTED NR 1 AND NR 6 LEADING EDGE SLAT DETENT ARM TENSION PER MM 27-81-21. FOUND LT WING OUTBOARD TRAILING EDGE FLA
Back to Boeing 737-228