Boeing 737-2H4
Service difficulty reports · 4,801
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 = '7372H4' 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 = '7372H4' 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 SWAA950644Bulkhead · gougedDURING SCHEDULED D-CHECK, FOUND GOUGE IN FWD SIDE OF BS 1156 BULKHEAD AND ON ADJOINING WEB BEHIND RT CENTER SECTION HINGE. REPAIRED PER TRAMCO EWO 95-0560 AND BOEING STRUCTURAL REPAIR MANUAL.SDR SWAA950643Chord · crackedDURING SCHEDULED D-CHECK, FOUND T-CHORD CRACKED AT AFT CARGO BAY, BS 726 RBL 8.5 WL 203. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.SDR SWAA950642Skin · dentedDURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 842 TO 857 BETWEEN 26R AND 27L, BS 480 BETWEEN S27 AND 28R AND AT BS 306 ABOVE S25L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.SDR SWAA950641Skin · gougedDURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 963, BETWEEN 20 AND 21L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.SDR SWAA950640Keel Beam · corrodedDURING SCHEDULED D-CHECK, FOUND KEEL BEAM FASTENER HOLE CORROSION AT LBL 5.5, AT BS 673.75, 677, 687.5, 692.25, 706.75 AND 708.25. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.SDR SWAA950639Keel Beam · corrodedDURING SCHEDULED D-CHECK, FOUND KEEL BEAM LOWER O/B FLANGE CORRODED AT BS 707 TO 727, LBL 7 WL 149. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.SDR SWAA950638Frames · crackedDURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 663 S4R, BS 500 LBL 2 WL 155, BS 344 LBL 46 WL 170 AND BS 294 WL 209 RBL 55. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.SDR SWAA950637Angle · crackedDURING SCHEDULED D-CHECK, FOUND SKATE ANGLE CRACKED AT BS 570 LBL 42 TO 55 WL 170. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.SDR SWAA950636Stringer · crackedDURING SCHEDULED D-CHECK, FOUND STRINGERS CRACKED AT BS 747, BS 767 S9R AND AT BS 639 S3L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.SDR SWAA950635Splices · corrodedDURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CORROSION AT BS 905, LBL 21.5 WL 168, BS 907, S5R AND BS 360, S4L AND S14L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.SDR SWAA950618Sensor · inopDURING CLIMB-OUT, NR 1 KRUGER FLAP TRANSIT LIGHT REMAINED ILLUMINATED. AIRCRAFT DIVERTED INTO MDW AND MADE AN UNEVENTFUL LANDING. REPLACED NR 1 KRUGER FLAP POSITION SENSOR PER BOEING M/M.SDR SWAA950603Skin · crackedDURING SCHEDULED SERVICE CHECK, FOUND 3 SKIN CRACK ALONG S25L AT BS 720. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.SDR SWAA950601Fire Loop · malfunctionedDURING CLIMBOUT, CREW EXPERIENCED APU FIRE WARNING AND THE APU WAS OFF. FIRE BOTTLE WAS ACTIVATED AND THE FIRE WARNING LIGHT REMAINED ILLUMINATED. AIRCRAFT RETURNED TO HOU AND MADE AN UNEVENTFUL LANDING. INSPECTED AND NOTED NO EVIDENCE OF FIRE OR OVERHEAT CSDR SWAA950600Retract Mech · malfunctionedAFTER TAKEOFF, CREW WAS UNABLE TO RAISE LANDING GEAR POSITION LEVER PAST THE OFF POSITION TO RETRACT GEAR. AIRCRAFT RETURNED TO MCI AND MADE AN UNEVENTFUL LANDING. AIRCRAFT WAS MX FERRIED TO MDW WHERE THEY RIGGED THE GROUND SHIFT CABLE AND REPLACED THE LANDISDR SWAA950599Blkhd Web · crackedDURING SCHEDULED 1/4 D-CHECK, FOUND CRACKS AT BS 178 BULKHEAD WEB AT LBL 5.7 AND RBL 5.7, ALONG SIDE I/B ROW OF FASTENER HOLES BETWEEN WL 207 AND 218. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.SDR SWAA950595Eel Battery · dischargedDURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT ABOVE FWD SERVICE DOOR INOP. REPLACED BATTERY PACK PER BOEING M/M.SDR SWAA950594Eel Battery · dischargedDURING SCHEDULED SERVICE CHECK, FOUND MAIN ENTRY AND SERVICE DOORS OUTSIDE EMERGENCY EXIT LIGHTS WEAK. REPLACED BATTERY PACK PER BOEING M/M.SDR SWAA950609Blkhd Strap · crackedDURING SCHEDULED 1/4 D-CHECK, FOUND WEB AND STRAP CRACKS AT BS 178 BULKHEAD, INBOARD ROW OF FASTENERS, LBL 5.7 FROM WL 184 TO 201. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.SDR SWAA950608Blkhd Web · crackedDURING SCHEDULED 1/4 D-CHECK, FOUND WEB AND STRAP CRACKS AT BS 178 BULKHEAD, INBOARD ROW OF FASTENERS, RBL 5.7 FROM WL 184 TO 201. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.SDR SWAA950607Blkhd T-Chord · crackedDURING SCHEDULED 1/4 D-CHECK, FOUND TWO CRACKS AT T-CHORD BS 178 BULKHEAD AFT SIDE, WL 184, ONE I/B AND ONE O/B. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.SDR SWAA950606Nlg Panel · crackedDURING SCHEDULED 1/4 D-CHECK, FOUND NOSE WHEEL WELL CEILING CRACKED AT SPRING ATTACH POINT, BS 277 RBL 10. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.SDR SWAA950605Angle · crackedDURING SCHEDULED 1/4 D-CHECK, FOUND CHORD CRACKED IN AFT EDGE AT I/B FASTENER OF 18A CHORD ANGLE, LEFT MAIN WHEEL WELL, BS 727 S18A. INSTALLED CHORD ANGLE REPAIR PER DRAWING 65-29228.SDR SWAA950572Fire Contl Pnl · malfunctionedAFTER TAKEOFF, EXPERIENCED APU FIRE WARNING. CREW ACTIVATED APU FIRE BOTTLE, FIRE WARNING LIGHT EXTINGUISHED. AIRCRAFT RETURNED TO LBB AND MADE AN UNEVENTFUL LANDING. INSPECTED AND FOUND NO EVIDENCE OF FIRE OR OVERHEAT CONDITION. REPLACED FIRE CONTROL PANESDR SWAA950571Press Ind · inopEN ROUTE TO MDW, EXPERIENCED B-SYSTEM PRESSURE DROP. AIRCRAFT DIVERTED TO IND AND MADE AN UNEVENTFUL LANDING. INSPECTED AND FOUND PRESSURE INDICATOR INOP, DEFERRED INDICATOR AND CONTINUED PER MEL 29-3.SDR BJNA95815Blkhd Web · crackedREPAIRED FUSELAGE BULKHEAD WAS DUE TO CRACKS AT BS 294.5 LBL 3.5 TO LBL 9.5 AND RBL 5 TO RBL 11 BETWEEN WL 172.5 TO WL 150.5 IAW FAX BOEING M-7272-953780 DATED JULY 21, 1995 AND SKETCH CIN FAAX952195 1/1, DOCUMENTED ON FAA FORM 8110-3. (M)SDR BJNA95814Stringer · crackedREPAIRED LEFT WING DUE TO CRACK AT WBL 279.5 UPPER STRINGER NR 9 ON THE RIB ATTACHMENT FLANGE IAW CASINO DRAWING NR CEX3-57-3 DATED JULY 20, 1995, DOCUMENTED ON FAA FORM 8110-3. (M)SDR BJNA95813Chord · corrodedREPLACED CHORD SECTION DUE TO CORROSION ON NOSE GEAR TORQUE BOX AT BS 267 WL 144 BETWEEN LBL 20 TO RBL 20 IAW SRM 51-10-1 AND 51-30-2. (M)SDR BJNA95812Floor Beam · corrodedREPAIRED FLOOR BEAM UPPER CHORD DUE TO CORROSION AT BS 312 WL 208.1 BETWEEN LBL 18 TO RBL 5 IAW SRM 53-10-9, FIG 5. (M)SDR BJNA95811Floor Beam · corrodedREPAIRED FLOOR BEAM UPPER CHORD DUE TO CORROSION AT BS 344 WL 208.1 BETWEEN LBL 12 TO LBL 58 IAW SRM 53-10-9, FIG 5. (M)SDR BJNA95810Floor Beam · corrodedREPAIRED FLOOR BEAM UPPER CHORD DUE TO CORROSION AT BS 947.5 WL 208.1 RBL 7 TO RBL 54 IAW SRM 53-10-9, FIG 2. (M)SDR BJNA95809Stringer · crackedREPAIRED STRINGER NR 9 LEFT DUE TO CRACK BETWEEN BS 1035 TO BS 1045 IAW SRM 53-10-3, FIG2. (M)SDR BJNA95808Floor Beam · corrodedREPAIRED FLOOR BEAM WWEB DUE TO CORROSINO AT BS 277 WL 194 BETWEEN LBL 9.50 TO LBL 12.50 IAW SRM 51-40-2, FIG 1. (M0SDR BJNA95807Stringer · crackedREPAIRED LEFT WING DUE TO CRACK AT WBL 227 UPPER STRINGER NR 11 AND STRINGER NR 12 ON THE RIB ATTACHMENT FLANGE IAW CASINO DWG NR CEX3-57-4, DATED JULY 20, 1995, DOCUMENTED ON FAA FORM 8110-3.SDR BJNA95806Stringer · crackedREPLACED SPLICE IN RIGHT STRINGER NR 4 DUE TO CRACK BETWEEN BS 903 TO BS 913 IAW SRM 51-10-1, 51-30-2 AND 51-20-1. (M)SDR BJNA95805Floor Beam · corrodedREPAIRED FLOOR BEAM UPPER CHORD DUE TO CORROSION AT BS 967 WL 208.1 BETWEEN LBL 1 TO LBL 16 IAW SRM 53-10-9, FIG 7. (M)SDR BJNA95804Floor Beam · corrodedREPAIRED FLOOR BEAM WEB DUE TO CORROSION AT BS 328 WL 200 BETWEEN LBL 52 TO LBL 64 IAW SRM 51-40-2, FIG 1. (M)SDR BJNA95803Floor Beam · corrodedREPAIRED FLOOR BEAM UPPER CHORD DUE TO CORROSION AT BS 1006 WL 208.1 BETWEEN BL 0 TO LBL 23 IAW SRM 53-10-9, FIG 7. (M)SDR BJNA95802Skin · crackedREPAIRED FUSELAGE SKIN DUE TO CRACK AT BS 727 BETWEEN STRINGER NR 20 AND STRINGER NR 19 RIGHT IAW DRAWING NR CEX3-53-1 DATED JULY 15, 1995, DOCUMENTED ON FAA FORM 8110-3. (M)SDR BJNA95801Blkhd Web · dentedREPAIRED FUSELAGE AFT BULKHEAD WEB DUE TO DENT AT BS 1016 BETWEEN STIFFENERS NR 6 LEFT AND NR 7 LEFT IAW SRM 53-10-4, FIG 12. (M)SDR SWAA950561Compressor · stalledDURING CLIMBOUT, EXPERIENCED NUMBER 2 ENGINE COMPRESSOR STALL. AIRCRAFT RETURNED TO MDW AND MADE AN UNEVENTFUL LANDING. INSPECTED AND REPLACED NUMBER 2 ENGINE PER BOEING M/M.SDR SWAA950567Eel Battery · dischargedDURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHTS AT FWD ENTRY AND FWD SERVICE DOORS INOP. REPLACED BATTERY PACK PER BOEING M/M.SDR SWAA950563Blkhd Web · crackedDURING SCHEDULED C2 CHECK, FOUND WEB CRACKED AT FASTENER HOLE IN UPPER RIGHT CORNER OF BS 178 BULKHEAD. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.SDR SWAA950566Eel Battery · dischargedDURING SCHEDULED A1 CHECK, FOUND RIGHT AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK PER BOEING M/M.SDR SWAA950568Eel Battery · dischargedDURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRYWAY EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY CHARGER AND BATTERY PACK PER BOEING M/M.SDR SWAA950556Prox Sensor · inopAFTER GEAR RETRACTION, RIGHT MAIN GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED. CYCLED GEAR AND LIGHT EXTINGUISHED, THEN ILLUMINATED AGAIN. AIRCRAFT RETURNED TO MDW AND MADE AN UNEVENTFUL LANDING. REPLACED GEAR PROXIMITY SENSOR, RIGHT GEAR UPLOCK SWITCH AND SSDR SWAA950555Blkhd Skin · crackedDURING SCHEDULED C1 CHECK, FOUND 1 CRACK AT BS 178, BULKHEAD BETWEEN WL 218 AND S2L. REPAIRED PER SWA RA 1-253-1320.SDR SWAA950557Eel Battery · dischargedDURING SCHEDULED SERVICE CHECK, FOUND CABIN FLOOR TRACK LIGHTING INOP. REPLACED AFT BATTERY PACK AND REWIRED TRACK LIGHTING PER BOEING M/M.SDR 95ZZZM599Rotating Beacon · defectiveWHILE PUSING BACK FROM GATE AT JAX, FLIGHT ATTENDANT REPORTED SMOKE FROM OVERHEAD BIN AROUND ROW NR 9. AIRCRAFT WAS TOWED BACK TO THE GATE AND PASSENGER DEPLANNED. ALL POWER WAS REMOVED, UPPER BEACON CIRCUIT BREAKER WAS FOUND POPPED. MAINTENANCE IN JAX FOUNSDR 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.SDR SWAA950552Skin · crackedDURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT LOWER HINGE CUTOUT OF AFT SERVICE DOOR. REPAIRED PER BOEING S/B 737-53-1074 AND STRUCTURAL REPAIR MANUAL.
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