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 DL72S982438Shear Tie · damagedSHEAR TIES AT BS 580 AND 620, S14R WERE DAMAGED DUE TO REWORK OF THE SKIN LAP JOINT. REPAIRED PER ERA 332452-14.SDR DL72S982199Battery Pack · dischargedRT OVERWING EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK.SDR DL72S982192Fitting · corrodedTHE REAR SPAR ATTACHMENT LUG OF THE LT MLG SUPPORT BEAM ATTACH FITTING WAS FOUND WITH CORROSION IN THE LUG HOLE BORE. THE HOLE WAS OVERSIZED TO 1.882 DIA TO REMOVE THE CORROSION AND AN OVERSIZE BUSHING WAS INSTALLED. THE REPAIR WAS ACCOMPLISHED PER ER/A 3659SDR DL72S982189Web · crackedREF SHIP 525 TPA LTR CHK A2 .5 INCH CRACK AT RT TORQUE BOX VERT, WEB STA 1233. REPAIRED PER MM 53-11-0 PG 832.SDR DL72S982182Support · corrodedWING LT MLG SUPPORT BEAM, OUTBD LUG AND LOWER SURFACE, REPAIR FOR O/S HOLE BORES. THE OUTBD LUG BORE ON THE LT MLG SUPPORT BEAM WAS OVERSIZED AND SPOT FACED TO REMOVE CORROSION. SEVERAL OF THE LOWER SURFACE PANEL ATTACH HOLES WERE ALSO OVERSIZED TO REMOVE SDR DL72S982193Skin · crackedA 1 INCH CRACK WAS FOUND IN THE SKIN AT THE UPPER HINGE CUTOUT OF THE FWD ENTRY DOOR CUTOUT. AN EXISTING EXTERNAL DOUBLER REPAIR WAS LOCATED MIDWAY BETWEEN THE UPPER HINGE CUTOUT ANDTHE LOWER HINGE CUTOUT. THE UPPER HINGE CRACK WAS REPAIRED PER SRM 53-30-3, SDR DL72S982180Skin · corrodedFUSELAGE SKIN FS 1070-109, STRG 28R, SKIN CORROSION CUTOUT REPAIR. THE FUSELAGE SKIN WAS FOUND CORRODED IN TWO AREAS NEAR S-28R BETWEEN FS 1070 AND 1091. THE CORRODED AREAS WERE CUTOUT WITH A 14.25 BY 3.25 CUTUOUT AND A .75 BY 1.5 CUTOUT. BOTH CUTOUTS WERE SDR DL72S982170Web · crackedREF SHIP 541 TPA LTR CHK D1, FOUND 1 IN CRACK AT LIGHTNING HOLE STA 1240 RT VERTICAL WEB TORQUE BOX AREA. REPAIRED PER MM 53-11-10.SDR DL72S982169Stringer · crackedCRACKS WERE FOUND IN THE SKIN, STRINGER AND BS 940 FITTING ON THE RT SIDE OF THE AC AT STRINGER 8A. STRINGER 18A CONTAINED AN APPROX 2 LONG CRACK, THE SKIN AND FITTING UPON BHEC INSPECTION YEILDED CRACK INDICATIONS. REPAIRED PER ERA 332374-14.SDR DL72S982162Battery · dischargedRT FWD ENTRY DOOR OVERHEAD EMEGENCY LIGHT WILL NOT TEST. REPLACED BATTERIES AND RACK NOW CKS NORMAL.SDR DL72S982206Bulkhead Web · crackedWEB AT STA 970 LOWER BULKHEAD WEB CRACKED RBL 10. REMOVED DAMAGED WEB AS PER SRM 51-40-2. FABRICATED REPAIR PARTS IAW SRM 53-10-9 FIG 4. OK TO INSTALL. STARTED INSTALLING REPAIR DOUBLER. COMPLETED REPAIR PER SRM 53-10-9 FIG 4.SDR DL72S982157Battery · dischargedSEAT ROW 25 OVERHEAD EMERGENCY LIGHT INOP. REPLACED BATTERY, OPS NOW OK.SDR DL72S982154Stringer · crackedS18 TAB ON THE RT WING VENT BOX AT WS 171.5 WAS FOUND CRACKED. ADDITIONAL DAMAGE INCURRED WHILE INSTALLING THE SRM REPAIR. REPAIRED PER ERA 332288-14.SDR DL72S982153Blkhd Stiffener · crackedTHE FS 1183 BULKHEAD VERTICAL STIFFENER AT RBL 36.83 WAS FOUND WITH TYPICAL CRACKING AT WL 240. THE CRACKED STIFFENER WAS REPAIRED PER BAC S/B 727-53-0192 AND DOCUMENTED PER ER/A 365894-14.SDR DL72S982151Stringer · crackedFUSE STR 29R WAS FOUND CRACKED AT FS 950E. REPAIRED PER ERA 332275-14.SDR DL72S982150Stringer · crackedRT WING UPPER SURFACE S18 AT WS 304 WAS FOUND CRACKED, REQUIRING A 2.5 INCH CUTOUT. REPAIRED PER ERA 332341-14.SDR DL72S982149Frame · crackedCRACK WAS FOUND IN THE VERT FLANGE OF THE WING TO FUSE UPPER ATTACH CHORD, LWR FRAME HOLE RBL 70.85, FS 760. REPAIRED PER ERA 332283-14AD.SDR DL72K982156Skin · crackedA .5 INCH CRACK FUSELAGE SKIN AT L-4 WINDOW I/B FWD ATTACH SCREW. REPAIRED PER SRM 53-30-3.SDR DL72K982155Web · crackedRT TORQUE BOX VERT WEB CRACKED AT LIGHTENING HOLES STA 1290 AND 1235 RT. REPAIRED PER MM 53-11-0 PG 832.SDR DL72S982208Panel · crackedA 1.25 INCH CRACK AT NR 1 RT BALANCE BOARD ACCESS PANEL O/B EDGE (MARKED).SDR DL72S982207Access Panel · crackedTWO INCH CRACK IN NR 2 LT BALANCE BOARD ACCESS PANEL AT O/B EDGE (MARKED). INSTALLED REPAIR DOUBLER PER SRM 55-20-3 FIG 5.SDR DL72S982139Skin · crackedFUSELAGE SKIN WAS FOUND WITH A TIME LIMITED EXT REPAIR DOUBLER FOR A CRACK IN THE SKIN AT FS 294.5, BELOW S15R. THE TIME LIMITED REPAIR WAS REMOVED AND ADDITIONAL DAMAGE FOUND. REPAIRED PER ERA 332347-14.SDR DL72L982142Support · crackedTHE DOUBLERS FOR THE NR 7 SLAT ACTUATOR SUPPORT STRUCTURE WERE FOUND WITH THE TYPICAL CRACKS PER BAC S/B 727-57-0130, REV 2. THE CRACKED DOUBLERS WERE REPAIRED/MODIFIED PER THE REQUIREMENTS OF THE S/B. THE REPAIR WAS DOCUMENTED PER ER/A 365879-14AD.SDR DL72S982136Skin · damagedTHE FUSELAGE SKIN AT STRINGER 22L BETWEEN FS 1110 AND 1166 WAS TORN AND GOUGED DUE TO CONTACT WITH GROUND EQUIPMENT. THE DAMAGE WAS REMOVED FROM THE SKIN WITH TWO CUTOUTS MEASURING 4 X 28.25 AND 3.25 X 16.5. THE CUTOUTS WERE REPAIRED WITH A SINGLE EXTERNAL ASDR DL72S982253Skin · repairedDURING SHOP INSP, THE COVE SKIN WAS FOUND CRACKED AT THE I/B AFT CORNER OF I/B AFT FLAP DRIVE ROD CUTOUT. THE SKIN WAS REPAIRED BY REMOVING THE DAMAGE AND INSTALLING A DOUBLER PER MM 57-52-0, FIG 09.SDR DL72S982174Skin · cracked1 INCH HOLE WITH CRACKS AT LT ELEVATOR UPPER SKIN AT INBD END. REPAIRED PER 727 SRM 55-20-3 FIG 4.SDR DL72L982108Skin · crackedCRACK AT NR 4 SLAT IB GUIDE CUTOUT AFT END. REPAIRED PER MM 57-20-21.SDR DL72L982107Stiffener · crackedSPAR STIFFENER CRACKED NR 3 SLAT IB TRACK. REPAIRED PER MM 57-20-21.SDR DL72L982106Skin · crackedCRACK AT NR 3 SLAT OB GUIDE CUT OUT AFT END. REPAIRED PER MM 57-20-21.SDR DL72S982094Skin · crackedFUSE SKIN HAD A TIME LIMITED REPAIR REMOVED AT FS294, S15R; AND ADDITIONAL DAMAGE WAS FOUND. REPAIRED PER ERA 332347-14.SDR DL72S982093Fitting · crackedCRACKING WAS DETECTED IN FOUR OF EIGHT HOLES ON S18A, LT SIDE. HOLES WERE OVERSIZED THROUGH THE SKIN, STRINGER AND FITTING. REPAIRED PER ERA 332264-14.SDR DL72S982092Skin · crackedLT SIDE OF THE VERT STAB SKIN IS CRACKED AT THE INTERSECTIONOF S10 AND FUSE CREASE LINE. REPAIR PER ERA 332292-14.SDR DL72S982085Spar · damagedDURING INSPECTION OF THE CTR WING REAR SPAR AND REPAIR MANY FASTENER LOCATIONS IN THE SPAR PANEL WERE OVERSIZED DUE TO TOOLING DAMAGE. REPAIRED PER ERA 332359-14AD.SDR DL72S982083Tab · cracked59R FLANGE TAB AT FIN STA 133.8 CRACKED, HORIZONTALLY THROUGH ATTACH BOLT. REF NRC515 MV2. REPAIRED PER MM 55-30-0 FIG 803.SDR CALA9801921Connector · shortedINSPECTION FOUND LT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE FOUND THE CANNON PLUG SHORTED AT POWER SUPPLY. THE PLUG WAS REPLACED AND EXIT LIGHT OPERATION WAS RESTORED.SDR DL72S982065Power Supply · inoperativeEMER TRACK LTS DAMAGED AT 26C. RELAMPED AND REPLACED LENS. ON TEST FOUND AFT FLOOR TRACK LTS INOP. FOUND AFT TRACK LIGHTING PWR SUPPLY BAD. REPLACED PWR SUPPLY. TEST GOOD.SDR DL72S982063Frame · crackedA CRACK WAS FOUND IN THE FS 784 RT FRAME INBD FLANGE. THE CRACK PROPAGATES FROM THE FIRST FASTENER HOLE ABOVE THE FLOOR LINE. REPAIRED PER ERA 300891-14AD, REV A.SDR DL72S982056Frame · crackedWHILE PERFORMING INSPECTION PER SI 4-61904-12AD A CRACK WAS FOUND IN THE FS 761 RT FRAME ABOVE THE FIRST BOLT HOLE BELOW THE FLOOR LINE IN THE INBD FLANGE. REPAIRED PER ERA 332248-14AD.SDR DL72S982037Pump · failedON DESCENT, HYD QUANTITY SYSTEM 'B' WENT TO .3 GALLONS AND SLOWLY CONTINUED DOWN. RAN SYSTEM 'B' FLUID LOSS INOP CHECKLIST. FOUND NR 2 'B' SYSTEM PUMP LEAKING. REPLACED SAME, SERVICED RESERVIOR. PUMP OPS NORMAL.SDR DL72S982075Bulkhead Beam · crackedFUSELAGE BULKHEAD FS 1183 LBL 18 VERTICAL BEAM, REPAIR FOR CRACK. A .75 INCH TYPICAL CRACK WAS FOUND IN RADIUS OF THE LBL 18 VERTICAL BEAM LOWER END ON THE FS 1183 BULKHEAD. THE CRACKED BEAM WAS REPAIRED PER BAC S/B 727-53-0202. THE REPAIR WAS DOCUMENTED PESDR DL72S982033Track · corrosionINBD FLAP INBD TRACK TYP CORROSION AT MLG BEAM ATTACH HOLES AND FWD LUG: AD 90-07-05: TYPICAL CORROSION WAS FOUND TO THE MLG BEAM ATTACH HOLES (WITHIN THE AD AREA) AND AT THE FWD ATTACH LUG. OVERSIZED CORRODED HOLES AND MACHINED LUG FACES.SDR DL72S982032Skin · misdrilledRT ELEVATOR, REAR SPAR MOD, OS HOLES: AD 96-06-05. DURING REAR SPAR MOD PER EO 4-70183-3AD, SEVERAL HOLES IN THE UPPER SKIN WERE OVERSIZED. REPAIR BONDED AN INTERNAL DOUBLER AND INSTALL OVERSIZED FASTENERS.SDR DL72K982040Frame · crackedFOUND ON B2 LETTER CK, LT AFT ENTRY DOOR FRAME CRACKED BELOW THE UPPER STOP CASTING WL 273. REPAIRED PER SRM 53-10-9. NR CARD 87. FOUND ON B2 LETTER CK, RT AFT ENTRY DOOR FRAME CRACKED BELOW THE UPPER STOP CASTING WL 273. REPAIRED PER SRM 53-10-9. NR CARD SDR DL72K982036Fitting · crackedRT I/B TENSION TIE BOLT FITTING CRACKED. REPLACED PER BAC DRAWING 65-17509.SDR DL72S982112Track · corrodedCORROSION FOUND AT FWD ATTACH LUG FACES AND BORE AND TO MLG BEAM ATTACH HOLES. BUSH LUG HOLES AND INSTALLED SPLICE PLATE REPAIR FOR MLG BEAM ATTACH HOLES.SDR CALA9801900Web · crackedINSPECTION FOUND A 1 INCH CRACK IN RT MLG FLYING DOOR WEB FORWARD OF AFT HINGE FITTING. THE HINGE WEB WAS REMOVED IAW SRM 51-30-2. A NEW HINGE WEB WAS INSTALLED IAW SRM 52-80-1, 51-10-2, 51-30-2, AND MM 51-20-11.SDR DL72S982318Angle · crackedDURING SHOP INSPECTION, THE AFT CHORD ANGLE WAS FOUND CRACKED 18 INCHES FROM I/B END OF FLAP. THE ANGLE WAS REPAIRED PER MM 57-52-0 FIG 802 BY REPLACING A SECTION OF THE ANGLE AND INSTALLING A SPLICE DOUBLER.SDR DL72S982316Skin · crackedDURING SHOP INSPECTION, THE COVE SKIN WAS FOUND CRACKED 34 INCHES FROM I/B END OF FLAP. THE SKIN WAS REPAIRED PER MM 57-52-0, FIG 809 BY REMOVING THE DAMAGE AND INSTALLING A DOUBLER.SDR DL72S982315Angle · repairedDURING SHOP INSPECTION, THE AFT CHORD ANGLE WAS FOUND CRACKED AT 2 PLACES APPROX 34 INCHES FROM I/B END OF FLAP. THE ANGLE WAS REPAIRED PER MM 57-52-00, FIG 802 BY REPLACING A SECTION OF THE ANGLE AND INSTALLING A SPLICE DOUBLER.SDR DL72S982143Strnger · crackedTAB CRACKED AT WING STRINGER TO FRAME ATTACHMENT STA 629 AT 4TH FROM FWD SIDE AND 2ND FROM FWD SIDE. REPAIRED PER MM 57-13-0 FIG 804 NRC 521 AND NRC 520.
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