Boeing 727-232
Service difficulty reports · 6,539
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 = '727232' 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 = '727232' 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 DL72S950082Regulator · faultyDURING CRUISE, WITH NR 2 GENERATOR INOP NR 3 BUS-TIE BREAKER TRIPPED. DIVERTED FLIGTH TO DFW. FOUND NR 3 VOLTAGE REGULATOR FAULTY. REPLACED REGULATOR OPERATION NORMAL.SDR DL72S950066Bulkhead · crackedDURING LETTER CHECK, FOUND A .75 INCH CRACK IN FS 1183 BULKHEAD WEB AT UPPER EDGE OF HORIZONTAL STIFFENER AT WL 168 AT RBL 25. REPAIRED PER SRM 53-10-9 FIG 6.SDR DL72L950187Stiffiners · crackedDURING INSPECTION (L/C), THE RT TORQUE BOX WAS FOUND TO HAVE CRACKED STIFFENERS AT FS 1263. THE DAMAGED PART WILL BE REPLACED IN ACCORDANCE WITH B727 S/B 53-0129, REV 4.SDR DL72L950168Web · crackedDURING HMV, FOUND WEB CRACKED INSIDE LT WING L/E O/B OF NR 2 SLAT ACTUATOR. REPAIRED PER M/M 57-54-0.SDR DL72S960038Rib · crackedNR 3 RIB CRACKED AT I/B TRACK ATTACH POINT. REPAIRED PER M/M 57-54-0 PG 807. FOUND DURING NR 3 L/E SLAT AT SHOP INSPECTION.SDR DL72S960037Angle · crackedCOVE ANGLE CRACKED AT I/B UP STOP ATTACH POINT. REPAIRED PER M/M 57-54-0, FOR NR 3 L/E SLAT AT SHOP INSPECTION.SDR DL72S950190Stiffeners · crackedDURING INSPECTION AT LETTER CHECK, THE RT TORQUE BOX HAD STIFFENERS/BEAMS CRACKED AT BOTH FS 1263 AND FS 1273. THE DAMAGED PART WILL BE REPLACED IN ACCORDANCE WITH B727 S/B 53-0129, REV 4.SDR DL72L950424Skin · crackedDURING SHOP ISNPECTION, LEFT WING NR 4 SLAT UPPER SKIN WAS WORN AT FENCE. ALSO, A TIME LIMITED REPAIR WAS FOUND ON LOWER SKIN AT FENCE AREA. REPAIRED PER MM 57-54-0 FIG 813 AND SRM 57-50-3 FIG 1.SDR DL72L950423Rib · crackedDURING SHOP INSPECTION, FOUND LEFT WING NR 4 SLAT WITH RIB NR 12 AND NR 18 CRACKED. REPAIRED PER MM 57-54-0.SDR DL72L950422Rib · crackedDURING SHOP INSPECTION, LEFT WING NR 4 SLAT WAS FOUND WITH RIB NR 11 CRACKED. REPAIRED PER SRM 57-54-0.SDR DL72L950421Rib · crackedDURING SHOP INSPECTION, FOUND LEFT WING NR 4 SLAT WITH THE RIB CHORD CRACKED AT THE O/B END, AND WORN AT THE I/B TRACK. REPAIRED PER MM 57-54-0 FIG 812.SDR DL72L950420Skin · crackedDURING SHOP INSPECTION, LEFT WING NR 4 SLAT WAS FOUND WITH CRACKED LOWER SKIN AT INBD TRACK FAIRING. REPAIRED PER MM 57-54-0 FIG 15.SDR DL72L950165Skin · dentedAT HMV, FOUND DENT IN FUSELAGE SKIN BETWEEN STA 450-460 AND STR 17R AND 18R. ROUTED OUT DAMAGE PER SRM 53-30-3.SDR DL72S950215Nose Cowl · wornDURING SHOP INSPECTION, NR 1 ENGINE NOSE COWL WAS FOUND WITH THE AFT LIP WORN TO A KNIFE EDGE AT THE 6:30 TO 7:30 POSITION. REPAIRED PER SRM 54-10-3.SDR DL72S950048Slat Rib · crackedDURING LETTER CHECK, FOUND LEFT WING NR 4 LEADING EDGE SLAT WITH A .5 INCH CRACK IN THE NOSE RIB JUST OUTBOARD OF ACTUATOR ROD ATTACH FITTING. REPAIRED PER MM 57-54-0.SDR DL72S950046Slat · crackedDURING LETTER CHECK, LEFT WING NR 4 LEADING EDGE SLAT WAS FOUND WITH TWO .5 INCH CRACKS ON THE LOWER SKIN IN THE RADIUS OF THE INBOARD SLAT TRACK FAIRING. REPAIRED PER MM 57-54-0.SDR DL72S950045Skin · crackedDURING LETTER CHECK, THE NR 2 ENGINE S DUCT HOUSING RIGHT SIDE OUTER SKIN WAS FOUND WITH A 1.25 INCH CRACK EXTENDING UP FROM ACCESS PANEL 9524. REPAIRED PER MM 54-30-0 PG 803.SDR DL72S950044Stiffener Angle · crackedDURING LETTER CHECK, A 3 INCH CRACK WAS FOUND IN THE VERTICAL STIFFENER ANGLE ON THE WING FRONT SPAR ON THE OUTBOARD SIDE OF NR 3 SLAT OUTBOARD TRACK ROLLER FITTING. REPAIRED PER MM 57-20-21 PG. 813.SDR DL72L950264Angle · crackedDURING HMV, NR 5 SLAT CLOSEOUT ATTACH ANGLE CRACKED. REPAIRED PER M/M 57-54-0.SDR DL72L950192Rib · crackedDURING HMV, FOUND NR 7 L/E SLAT ACT ATTACH RIBS CRACKED AT LWR FWD RADIUS. FABRICATED PART AND REPAIRED PER M/M 57-54-0.SDR DL72L950170Rib · crackedDURING HMV, FOUND NR 2 L/E SLAT ACTUATOR ATTACH RIBS CRACKED, REPAIRED PER MM 57-54-0.SDR DL72L950126Te Skin · delaminatingDURING HMV, FOUND NR 2 SPOILER TE DELAMINATING. REPAIRED PER SRM 51-40-6.SDR DL72L950121Skin · bentDURING HMV, SKIN IS BENT ON L-1 DOOR AT THE FWD LOWER ATTACH POINT AND UPPER AFT CORNER. REPAIED PER SRM 52-11-01 FIG 804.SDR DL72S950144Skin · damagedDURING LETTER CHECK, THE RIGHT ELEVATOR UPPER SKIN WAS FOUND WITH A SMALL HOLE JUST FWD OF TAB, DAMAGE WAS DUE TO LIGHTNING STRIKE. REPAIRED ELEVATOR SKIN PER SRM 52-20-3.SDR DL72S950033Angle · crackedDURING LETTER CHECK, THE LEFT ELEVATOR INTERNAL SUPPORT ANGLE INSIDE ACCESS PANEL 9307 WAS FOUND CRACKED. REPAIRED PER SRM 55-21-4 FIG 1.SDR DL72L950498Nose Cowl · worn and bentDURING SHOP INSPECTION, FOUND PREVIOUS REPAIR DAMAGED AT THE EIGHT O'CLOCK POSITION ON ENGINE NOSE COWL. REPAIRED DAMAGE AS PER SRM 54-10-3.SDR DL72L950173Longeron · crackedDURING HMV, FOUND RIGHT WING UPPER STRINGER CRACKED AT STRINGER TO RIB ATTACH HOLE AT WS 629. REPAIRED PER MM 57-13-0.SDR DL72L950172Longeron · crackedDURING HMV, FOUND RIGHT WING UPPER STRINGER NR 13 WITH A CRACK AT FASTENER HOLE AT ATTACH POINT TO WING RIB AT WS 629. REPAIRED PER MM 57-13-0.SDR DL72L950169Longeron · crackedDURING HMV, FOUND RIGHT WING UPPER STRINGER NR 10 AT STA 686.5 CRACKED AT THE STRINGER TO RIB ATTACH FASTENER HOLE. REPAIRED PER MM 57-13-0.SDR DL72L950166Frame · crackedAT HMV, FOUND FRAME 700 CRACKED BETWEEN STR 22 AND 23 R. FABRICATED PARTS AND REPAIRED DAMAGE PER SRM 53-10-4.SDR DL72L950124Frame · crackedDURING HMV, FOUND FRAME 804.5 CRACKED. REPAIRED PER SRM 53-10-4 FIG 17.SDR DL72S950288Ribs · crackedDURING SHOP INSPECTION, LEFT WING NR 3 SLAT WAS FOUND WITH NR 3, NR 7, NR 9 AND NR 10 RIBS CRACKED. REPAIRED PER SRM 57-50-3 AND SRM 57-54-0 FIG 804.SDR DL72S950214Center Frame · crackedDURING SHOP INSPECTION, THE AFT CENTER FRAME ON FWD GALLEY DOOR WAS FOUND CRACKED. REPAIRED PER SRM 51-40-3.SDR DL72L950174Frame · corrodedDURING HMV, FOUND FRAME AND SKIN CLIPS CORRODED AT FS 1148 AT STR 28L-30. REPAIRED PER M/M 53-11-0.SDR DL72L950123Stringer · corrodedDURING HMV, FOUND STR 26 R CORRODED FROM FS 1140 - 1166. REPAIRED PER ERA 300913-14.SDR DL72L950096Angle · wornDURING HMV, NR 2 PYLON COWLING SUPPORT ANGLE WORN AT 6 O'CLOCK POSITION. REPAIRED PER M/M 53-11-0.SDR DL72L950053Stringer · crackedDURING HMV, STRINGER 15L CRACKED AT STA 720C. REPAIRED PER SRM 53-10-3 FIG 1.SDR DL72L950040Skin · crackedDURING HMV, NR 2 INLET SKIN IS DAMAGED INSIDE 'S' DUCT AT THE 1 O'CLOCK POSITION. REPAIRED PER SRM 54-10-3 FIG 13.SDR 96ZZZX1397Floor Beam · corrodedSTA 420.0 FLOOR BEAM UPPER CHORD HAS LEVEL 2 CORROSION AT SEVERAL AREAS FROM RBL 10 TO RBL 60. REMOVED CORROSION PER SRM 51-10-6. WITHIN LIMITS PER SRM 53-10-1 EXCEPT AT RBL 14. REPAIRED WITH NESTED ANGLES PER SRM 51-40-4.
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