Boeing 727-232
Service difficulty reports · 6,539
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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 = '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 DL72S961721Skin · corrodedTHREE AREAS OF CORRODED SKIN WERE FOUND, ONE AT FS 720 STRINGER 28L, ONE AT FS 720, STRINGER 28R AND ONE AT FS 700 STRINGER 28R. THERE IS AN EXISTING REPAIR AT FS 700 STRINGER 28L. TWO DOUBLERS WILL BE INSTALLED TO REPAIR THE DAMAGE. THE REPAIR DOUBLERS ARESDR DL72S961720Skin · corrodedA PUNCTURE REPAIR WAS FOUND CORRODED. THE CORROSION LED TO A 1 BY 2 CUT OUT AT STA 695 OUTBOARD OF STRINGER 28R. DAMAGE WAS REPAIRED PER B727 SRM 53-30-3, FIGURE 1.SDR CALA9600998Skin · crackedINSPECTION FOUND A 5 INCH CRACK WITH CORROSION IN SKIN LAP JOINT AT STA 520, S24L. REPAIRED IAW SRM 53-30-03, FIGURE 5.SDR DL72K961733Angle · crackedA .25 INCH CRACK EXTENDING FROM NR 2 SLAT O/B TRACK UPSTOP PAD IN COVE SKIN ATTACH ANGLE. INSTALLED DOUBLER PER M/M 57-54-0 PG 816.SDR DL72K961717Stiffener · crackedFOUND 1 CRACK IN WING L/E SPAR STIFFENERS OF NR 2 O/B TRACK. REPAIRED PER M/M 57-20-21 PG 813.SDR DL72K961716Bracket · crackedFOUND NR 7 SLAT ACTUATOR CRACKED I/B BRACKET UPPER LOBE. REPAIRED PER ERA 303841-14.SDR DL72K961715Stiffener · crackedFOUND 1.25 INCH CRACKS AT WING L/E SPAR STIFFENERS AFT OF NR 3 SLAT I/B TRACK TWO EACH. REPAIRED BY REPLACING STIFFENERS PER M/M 57-20-21 PG 813.SDR DL72K961714Cove Skin Angle · crackedFOUND .25 INCH CRACK EXTENDING FROM NR 2 SLAT O/B TRACK UP STOP PAD, IN COVE SKIN ATTACH ANGLE. REPAIRED PER M/M 57-54-0 PG 816.SDR DL72S961695Floor Beam · corrodedFOUND CORROSION ON FLOOR BEAM STA 344 AT SEAT TRACK ATTACH POINT RBL 21. REPAIRED PER SRM 53-10-8 FIG 11.SDR DL72S961650Light · crackedR1 DOOR SLIDE LIGHT INOP. REPLACED REFLECTOR LIGHT ASSEM.SDR DL72S961641Start Duct · failedNUMBER ONE ENGINE FIRE INDICATION AT CRUISE, WHEN THROTTLE WAS MOVED TO IDLE, INDICATION EXTINGUISHED. ENGINE WAS SHUT DOWN PRECAUTIONARY. ENGINE WINDMILLED FOR APPROX 20 MINUTES N-2 RPM WAS APPROX 15 PERCENT, OIL PRESSURE WAS APPROX 20 PSI, ON APPROACH. FOSDR CALA9600970Actuator · leakingTHE A-SYSTEM HYDRAULIC QUANTITY WAS LOST DURING CLIMBOUT. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 LEADING EDGE FLAP ACTUATOR LEAKING. THE ACTUATOR WAS REMOVED AND REPLACED. IN ADDITISDR DL72S961632Window · failedON CLIMBOUT, AT 27,000 PASSENGER CABIN WINDOW AT ROW 2A CRACKED AND CABIN PRESSURE WAS MAINTAINED AT 7.6 PSI. FLT WAS CONTINUED AT FL200 AND CABIN PRESS AT 6.0 PSI. ON ARRIVAL PBI FOUND OUTER WINDOW PANE BROKEN, INNER PANE INTACT. REPLACED 2A WINDOW, INSPECSDR CALA9600960Skin · crackedINSPECTION FOUND A 6 INCH CRACK ON LEFT ELEVATOR BOTTOM SKIN, INBOARD. THE LT ELEVATOR WAS REMOVED AND REPLACED IAW MM 27-30-1. AN ADJUSTMENT/TEST WAS PERFORMED ON ELEVATOR AND CONTROL TAB SYSTEM PER MM 27-30-0, PAGE 501 TO 532 AND OPERATION CHECKED GOOD.SDR CALA9600956Floorbeam · corrodedINSPECTION FOUND THE FLOORBEAM CORRODED AT STA 1130, RBL 34 DURING FLIGHT PHONE INSTALLATION. THE FLOORBEAM WAS REPAIRED IAW SRM 5310-03300.SDR DL72S961580Stiffener · crackedTHE OUTBOARD ACTUATOR ATTACH RIB STIFFENER ON THE NR 2 SLAT ACTUATOR WAS FOUND CRACKED. THE DAL MFG PART NUMBER FOR THE INBOARD AND OUTBOARD STIFFENERS IS (57-0367-002). THE ERA REPLACED BOTH THE INBOARD AND OUTBOARD ATTACH RIB STIFFENERS PER EO 4-59271-3AD.SDR DL72S961601Transverse Beam · crackedA CRACK WAS FOUND IN THE UPPER FWD TRANSVERSE BEAM ANGLE AT STA 1273. THIS AREA OF THE TORQUE BOX IS THE SUBJECT OF AN AIRWORTHINESS DIRECTIVE 94-07-08 WHICH REQUIRES INSPECTION PER S/B 53-0129. THIS ER/A WILL REPLACE THE DAMAGED PART IN ACCORDANCE WITH THE SDR DL72S961573Web · crackedWEB IS CRACKED AT LIGHTENING HOLE LT SIDE STA 1323. REPAIRED PER M/M 53-11-0 PG 828 NR 15.SDR DL72L961582Stringer · crackedVERTICAL STABILIZER STRINGER 9R WAS FOUND CRACKED OUTSIDE RIB 7 AT STA 133.8 DURING EXECUTION OF EO 4-59253-12 AD. EO CALLS FOR A REPAIR PER B727 SRM 55-30-4, HOWEVER STR 9R CANNOT BE REPAIRED PER THIS SRM PROCEDURE DUE TO SPACE LIMITATIONS ON IBOARD FLANGE. SDR DL72S961537Doubler · crackedPREVIOUS DOUBLER CRACKED 1.5 INCH AT FASTENER. LOWER RT ELEVATOR I/B END. REPAIRED PER SRM 55-20-3 FIG 4.SDR DL72S961532Pwr Contl Unit · malfunctionedA/C PORPOISED AND VIBRATES ON CLIMB/CRUISE WITH A/P OFF. FEELS LIKE THERE IS PLAY IN CONTROL COLUMN IN PITCH. CONTROL COLUMN KICKS BACK OCCASIONALLY. REPLACED ELEVATOR POWER CONTROL UNIT, PERFORMED AUTO-PILOT AUTH CHECK, ALL INDICATIONS NORMAL.SDR DL72S961528Rib · crackedFOUND A .5 INCH CRACK IN RADIUS OF NOSE RIB INBD SIDE OF INBD TRACK, NR 6 SLAT. REPAIRED PER MM 57-54-0.SDR DL72S961515Web · crackedA 1.25 IN CRACK IN TORQUE BOX WEB UPPER RT CORNER AT STA 1213 AT UPPER CORD. INSTALLED DOUBLER PER MM 53-11-0 PG 832.SDR DL72L961647Skin · corrodedFUSELAGE SKIN AFT OF FS 700 FOUND TO BE WITH CORROSION DAMAGE BETWEEN STR 28L AND 28R. A 3.25 BY .375 INCH LONG CUTOUT WAS REQUIRED TO REMOVE THE DAMAGE BETWEEN STR 28R AND 28L. SKIN MACHINED FROM 2024-T3 WITH A LOCAL THICKNESS OF 0.050.SDR DL72S961563Skin · corrosionCORROSION WAS DISCOVERED IN THE FUSELAGE SKIN AT STA 1050, STR 28L. THE RESULTING DAMAGE CUTOUT IS 10 INCH FWD/AFT, BY 4.75 INCH I/B AND O/B AND IS CENTRALLY LOCATED AT THE INTERSECTION OF THE FRAME AT STA 1050 AND STR 28L. ALSO, STR 28L IS CORRODED AND WILLSDR DL72L961547Floor Beam · corrodedFOUND ON MV1 CHECK, CORROSION ON TOP SIDE OF FLOOR BEAM STA 1070 O/B OF RT O/B SEAT TRACK. REPAIRED PER M/M 53-20-11.SDR DL72S961497Stiffener · crackedA 1.5 INCH CRACK WING FRONT SPAR VERTICAL STIFFENER AT NR 3 SLAT INBD TRACK CUTOUT. REPLACED SPAR STIFFENER PER M/M 57-20-21.SDR DL72S961496Web · crackedONE CRACK 48 SECTION TORQUE BOX WEB AT UPPER EDGE STA 1223 LT. REPAIRED PER M/M 53-11-0.SDR DL72L961546Frame · crackedFOUND ON MV1 CHECK, 1 CRACK IN LT AFT SERVICE DOOR CUTOUT FWD FRAME AT INBD RADIUS ADJACENT TO UPPER STOP PAD CASTING. REPAIRED PER SRM REPAIR REF LIA ENG 06/26/96, 53-13-0.SDR DL72S961562Doubler · crackedTHE AFT VENTRAL STAIRWAY TORQUE BOX RIGHT HAND HORIZONTAL WEB HAS A .5 INCH CRACK IN A PREVIOUS REPAIR DOUBLER INSTALLED BY ER/A 06896-14, AT STA 1263 ON APPROXIMATELY BL 20.5. THIS DOUBLER WILL BE REMOVED AND THE WEB WILL BE TRIMMED IN A RECTANGULAR FASHION.SDR DL72S961482Battery Pack · dischargedRT FWD OVERWING EMERGENCY LIGHT IS INOP. REPLACED BATTERY PACK (P/N 9008-3-58), (S/N 8751).SDR DL72S961485Channel · crackedFOUND A .875 INCH CRACK IN THE CHANNEL AT FS 1263. REPAIRED PER DELTA ER/A 303744-14AD.SDR DL72S961486Skin · crackedFOUND CRACK AT STA 1060, ON STRINGER 28R. REPAIRED PER DELTA ER/A 303739-14.SDR DL72S961451Web · crackedA .5 INCH CRACK IN TORQUE BOX WEB EXTENDING FROM RT FWD LIGHTENING HOLE. REPAIRED PER M/M 53-11-0.SDR DL72S961450Angle · crackedA 2 INCH AND 1.5 INCH CRACK IN TORQUE BOX WEB AT UPPER CHORD RT END. REPAIRED PER M/M 53-11-0.SDR DL72S961453Skin · corrodedDURING INSPECTION, FOUND FUSELAGE SKIN BULGED AT STATION 1030, STRINGER 28R. REPAIRED IN ACCORDANCE WITH B727 SRM 53-30-3, FIG 1.SDR DL72S961439Line · brokenTHE B-SYS HYD FAILURE IN FLT, RETURNED SLC. FOUND B-SYS PRESS LINE FROM PUMP TO B-PRESS MOD BROKEN. REPLACED LINE, BOTH HYD B-PUMPS AND FILTERS.SDR CALA9600838Floor Beam · corrodedINSPECTION FOUND FLOOR BEAM CORRODED AT CEILING OF AFT CARGO COMPARTMENT, STA 1130 AND 1148, RT SIDE OF AIRCRAFT. THE FLOOR BEAM WAS REPAIRED IAW ECRA 5310-03288.SDR DL72S961432Prox Sensor · malfunctionedON T/O WITH GEAR RETRACTED, HANDLE IN UP POSITION, GOT LT MAIN GEAR RED UNSAFE LIGHT. REPLACED LT MAIN GEAR UP PROX SENSOR. ALSO, AS A PRECAUTIONARY REPLACED LDG MOD.SDR DL72S961423Tq Box Web · crackedDURING INSPECTION, FOUND TWO, .5 CRACKS IN LT FWD TORQUE BOX WEB AT UPPER CHORD ATTACH POINT STA 122. REPAIRED PER M/M 53-11-0.SDR DL72K961455Anti-Fret Strips · wornDURING INSPECTION, FOUND THE MICARTA ANTI FRETSTRIP FOR THE RIGHT WING INBD T/E FLAP, I/B TRACK WORN. REPLACED STRIP IN ACCORDANCE WITH AD 90-07-05.SDR DL72S961473Frame · crackedFOUND CRACK IN THE INBOARD FLANGE OF STA 784 FRAME JUST ABOVE THE MAIN CABIN FLOOR. REPAIRED PER B727 S/B 727-53-0197.SDR DL72S961472Skin · corrodedFUSELAGE SKIN JUST AFT OF FUSELAGE STA 700 HAD CORROSION DAMAGE AT STRINGER 28L AND STR 28R. REPAIRED PER B727 SRM 53-30-3, FIGURE 1 IN ACCORDANCE WITH B727 S/B 727-53A0203, REV 2.SDR DL72S961425Swivel · leakingDURING CLIMB, A-HYD QTY WENT TO ZERO AND A PUMP LIGHT FLICKERED, RETURNED TO SHV. REPLACED CASE DRAIN FILTERS, NO METAL FOUND. FOUND THE NR 4 SLAT ACTUATOR SWIVEL LEAKING. REPLACED O-RING, REFILLED HYD SYS, RAN ENGINES AND B-PUMPS, OPERATED ALL FLT CONTROLSSDR DL72S961422Trunnion Fitting · corrodedFOUND CORROSION ON THE INNER FACE OF THE FWD TRUNNION BEARING SUPPORT FITTING ON THE RT MLG. REPAIRED PER MM 57-43-0.SDR DL72S961529Angle · corrodedFOUND CORROSION AT ANGLE UNDER AND AROUND THE HINGES FOR PANEL 3348. REPAIRED PER MM 53-30-1, PG 807 TO 808.SDR DL72S961454Skin · dentedFOUND A DEEP, SHARP RADIUS DENT AND GOUGE IN THE C-3 DOOR EXTERIOR SKIN APPROX 15 INCHES LONG, 8 INCHES ABOVE THE HANDLE CUTOUT. REPAIRED PER SRM 52-00-3, FIG 3.SDR DL72S961410Support · corrodedFOUND CORROSION ON THE FLAP TRACK SUPPORT IN LARGE BEARING BORE. REPAIRED PER M/M 57-42-0, PG 806.SDR DL72S961409Track · corrodedFOUND CORROSION ON THE NR 4 FLAP TRACK FWD SUPPORT FITTING INSIDE THE BORES. REPAIRED PER M/M 57-42-0.SDR DL72S961408Trunnion · corrodedFOUND CORROSION ON LEFT GEAR FWD TRUNNION FACE. REPAIRED PER M/M 57-43-0 PG 803.
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