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 DL72S990311Frame · crackedFOUND ON D1 LETTER CK AFT ENTRY DOOR FRAME CUTOUT CRACKED RT SIDE APPROX 10 INCHES FROM THE TOP. REPAIRED PER SRM 53-10-9.SDR DL72S990310Frame · crackedFOUND ON D1 LETTER CK AFT ENTRY DOOR FRAME CUTOUT CRACKED LEFT SIDE APPROX 10 INCHES FROM TOP OF CUTOUT. REPAIRED PER SRM 53-10-9.SDR DL72S990477Skin · crackedAT HMV2, FOUND SKIN CRACKED - EMPENNAGE EXIT, LOC AT FWD RT CORNER OF AFT AIRSTAIRS CUTOUT. FABRICATED DOUBLER PER MM 53-30-00 PG 803. STOP DRILLED CRACK, INSTALLED DOUBLER.SDR DL72S990450Frame · dentedFRAME DENTED AFT CARGO COMPT LT FRAME DENTED AT STA 950C SEVERAL PLACES FROM STR 27L TO 25L. REMOVED DAMAGE PER SRM 53-10-4 FIG 27, FABRICATED DOUBLER PER SRM 53-10-4 FIG 27. REMOVED FACTORY SPLICE. INSTALLED REPAIR PER SRM 53-10-4 FIG 27 REV NR 1170.SDR DL72S990416Frame · dentedFRAME DENTED AFT CARGO COMPT RT FRAME DENTED AT STA 950C SEVERAL PLACES FROM STR 25R TO STR 26R. CUT OUT DAMAGE PER SRM 53-10-4 FIG 27. DYE PENETRANT INSPECTED CUTOUT PER PS 900-6-3 NO 1 AND FOUND OK. DRILLED DOUBLER AND FILLER PER SRM 53-10-4 FIG 27 AND TRSDR DL72S990379Skin · crackedSKIN CRACKED EMPENNAGE EXT LOC AT AFT I/B CORNER OF ACCESS PNL 3903 CUTOUT. FABRICATED DOUBLER PER M/M 53-30-0 PG 803. STOP DRILLED CRACK, INSTALLED DOUBLER PER MM 53-30-0 PG 803, IDENTIFIED PER PS 900-5-1 NR 4.SDR DL72K990295Slide · dislodgedDURING TAKEOFF ROLL, L1 SLIDE PACK DISLODGED FROM DOOR. ACFT RETURNED TO BLOCK. RESECURED SLIDE PACK, CKS NORMAL.SDR DL72S990294Light · inopLEFT AFT ENTRY DOOR OVERHEAD EMERGENCY LIGHT INOP. REPLACED RACK, NOW CKS NORMAL.SDR DL72S990293Battery Pack · dischargedMID CABIN SEAT EMERGENCY LIGHTS INOP. REPLACED BATTERY RACK AND BATTERY PACK, ALL OPS NORMAL.SDR DL72L990318Frame · damagedFUSELAGE LT OVERWING EXIT CUTOUT FRAME FS 784, REPAIR FOR DISCREPANT FASTENER HOLES. WHILE ACCOMPLISHING INSPECTIONS OF THE LT OVERWING EXIT CUTOUT FRAME AT FS 784, SEVERAL FASTENER HOLES WERE FOUND OVERSIZED DAMAGED. THE MODIFICATION PER BAC S/B 727-53-0197SDR DL72L990317Frame · damagedFUSELAGE RT OVERWING EXIT CUTOUT FRAME FS 783.95, REPAIR FOR DAMAGED HOLES. UPON INSPECTION FOR TYPICAL CRACKS IN THE INNER CHORD OF THEFS 783.95 OVERWING EXIT CUTOUT FRAME, SEVERAL HOLES WERE FOUND MISDRILLED. THE PREVENTATIVE MODIFICATION PER BAC S/B 727-5SDR DL72L990316Frame · crackedFUSELAGE RT OVERWING EXIT FRAME, FS 761, FRAME CHORD REPAIR. THE FS 761 FRAME FOR THE RT OVERWING EXIT CUTOUT WAS FOUND WITH A TYPICAL CRACK IN THE INNER CHORD. THE FRAME WAS REPAIRED/MODIFIED PER BAC S/B 727-53-0197 WITH MODIFICATIONS REQUIRED DUE TO EXSDR DL72S990304Skin · crackedFUSELAGE SKIN FS 481-681 STRINGER 4R SKIN LAP SPLICE, REPAIR FOR CRACKS. LFEC INSPECTION REVEALED CRACKS IN THE LOWER SKIN OF THE STRINGER 4R LAP SPLICE BETWEEN FS 481 AND 681. INTERNAL HFEC INSPECTION CONFIRMED 14 CRACKS ALONG THE LOWER FASTENER ROW OF TSDR DL72S990303Skin · crackedFUSELAGE SKIN FS 681-740, STRINGER 4R, SKIN LAP SPLICE, REPAIR FOR CRACKS. LFEC INSPECTION REVEALED CRACKS IN THE LOWER SKIN OF THE STRINGER 4R LAP SPLICE BETWEEN FS 681 AND 740. INTERNAL HFEC INSPECTION VERIFIED 15 CRACKS ALONG THE LOWER ROW OF FASTENERSSDR DL72K990282Frame · crackedFOUND AT C-1 LETTER CHECK, .5 INCH VISIBLE CRACK ON AFT ENTRYWAY LT FRAME APPROX 6 INCHES BELOW UPPER STOP PAD. REPAIRED PER SRM 53-10-9.SDR DL72K990279Skin · wornWEAR IN FUSELAGE SKIN AT STA 1096 AT STR-1. REPAIRED PER ERA 332760-14AD.SDR DL72L990376Bulkhead Chord · corrodedFOUND DURING MV2 CORROSION VISIT NRC 221, CORROSION ON LOWER CHORD OF STA 950 BULKHEAD JUST O/B OF STR 29 RT. REPAIRED PER SRM 53-10-9 FIG 12.SDR DL72L990275Support · corrodedWING MLG SUPPORT BEAM, LT AFT ATTACH LUG, REPAIR FOR CORRODED LUG. THE AFT ATTACH LUG OF THE LT MLG SUPPORT BEAM WAS FOUND CORRODED. THE CORROSION WAS REMOVED BY OVERSIZING THE LUG HOLE BORE AND SPOTFACING THE SURFACE OF THE LUG. THE LUG WAS REPAIRED BY INSSDR DL72S990274Skin · crackedFUSELAGE SKIN FS 481-681, STRG 4R SKIN LAP SPLICE REPAIR FOR CRACKS. EXTERNAL LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE REVEALED CRACK INDICATIONS IN THE PANEL BETWEEN FS 481 AND 681. INTERNAL HFEC INSPECTION CONFIRMED A TOTAL OF 48 CRACKS ALONG THESDR DL72S990273Skin · crackedFUSELAGE SKIN FS 360-481, STRG 4L, SKIN LAP SPLICE, REPAIR FOR CRACKS. EXTERNAL LFEC INSPECTION REVEALED CRACK INDICATIONS IN THE LOWER SKIN OF THE STRINGER 4L LAP SPLICE BETWEEN FS 360-481. INTERNAL HFEC INSPECTION CONFIRMED 10 CRACKS ALONG THE LOWER ROW OFSDR DL72S990272Skin · crackedFUSELAGE SKIN FS 360-481, STRG 4R, SKIN LAP SPLICE REPAIR FOR CRACKED FASTENER HOLES. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360-481 REVEALED CRACK INDICATIONS. HFEC INTERNAL INSPECTION CONFIRMED A TOTAL OF 4 CRACKS IN TWO SEPERATE FRASDR DL72S990268Rib · crackedVERTICAL FIN RIB CHORD CRACKED 1.25 INCH FIN STA 133.800, AT STR 8 ATTACH BOLT RT SIDE. REPAIR PER M/M 55-30-0 FIG 802.SDR DL72S990267Clip · cracked1 IN CRACK IN LT VERT FIN SKIN TO RIB ATTACH CLIP, STA 180.600 ABOVE STR 10. REPAIR PER M/M 55-30-0 FIG 803.SDR DL72S990266Panel · cracked2 INCH CRACK NR 2 BALANCE BOARD CLOSE OUT PANEL, RT ELEVATOR. REPAIR PER SRM 55-20-3.SDR DL72K990261Spar · corrodedWEAR WAS FOUND ON THE I/B AND O/B PIVOT LUG FACES OF THE REAR SPAR CENTER FORGIN OF THE HORIZ STAB. ADDITIONALLY CORROSION WAS FOUND IN THE BORES OF EACH OF THE TWO LUGS. REWORKED PER ERA 332761-14.SDR DL72K990260Rib · corrodedCORROSION FOUND ON THE INBD FACE OF THE INBD LUG ON THE LT FIN CLOSURE RIB CLEVIS. DAMAGE REMOVED WITH A 1.6 DIA SPOTFACE W/DEPTH OF 0.062. REWORKED PER ERA 332753-14.SDR DL72K990256Skin · crackedA SKIN PANEL REPAIR WAS FOUND ON THE RHS VERT STAB WHICH WAS INSTALLED W/ BLIND RIVETS PER SRM. REPAIRED PER ERA 332755-14.SDR DL72K990255Skin · damagedDURING ACCOMPLISHMENT OF EO 4-69078-3AD, THE BONDED INTERNAL DOUBLER WAS DAMAGED (TOOLING DAMAGE). REPAIRED PER ERA 332737-14.SDR DL72K990254Skin · crackedWHILE ACCOMPLISHING LFEC INSPECTION PER SI 4-74176-12, REV B ON THE S4R LAP JOINT, CRACK INDICATIONS WERE FOUND BETWEEN BS 640 AND BS 740. AFTER GAINING INTERNAL ACCESS AND ACCOMPLISHING THE REQUIRED HFEC INSPECTIONS; ONE CRACK WAS CONFIRMED AT A FASTENER LOCSDR DL72S990258Skin · crackedFUSELAGE SKIN, FS 528, STRG 4, REPAIR FOR SKIN CRACK. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE GAVE A CRACK INDICATION. HFEC INTERNAL INSPECTION WAS THEN ACCOMPLISHED ALONG THE ENTIRE LENGTH OF THE PANEL WITH ONLY ONE CRACK FINDING. THE CRACK WAS SDR DL72K990252Switch · brokenAFTER FLAP RETRACTION FROM 5 DEGREES TO 2 AMBER FLAP ANNUNCIATOR ILLUMINATED ON FWD PANEL. IN POSITION TEST, THE NR 5 SLAT INDICATED EXTEND. RAN V-LIST PER POM NR 5 SLAT WOULD NOT RETRACT. TROUBLESHOT SYSTEM, FOUND SWITCH S12 ROCKER ARM MISSING. REPLACED SSDR DL72S990354Frame · crackedSTA 620 FRAME UPPER FLANGE AT RBL 8 HAS CRACK IN RADIUS. CRACK TRIMMED OUT AND REPAIR DOUBLER INSTALLED PER ERA 332727-14. ACTION TAKEN, ERA 332727-14.SDR DL72S990248Gearbox · leakingON APPROACH INTO CVG PASSING THROUGH APPROX 9000 AGL, NR 2 LOW OIL PRESS LIGHT ILLUMINATED. OIL QTY WAS AND NOW OBSERVED TO DECREASE, OIL TEMP NORMAL, INCREASED ABOVE 105 DEG C. ENGINE SHUT DOWN PER POM PROCEDURES. FOUND NR 2 ENG GEARBOX LEAKING AT 6 O'CLOCSDR DL72S990243Skin · crackedDURING INSP PER SI 4-74176-12 ON S4R, LAP JOINT CRACK INDICATIONS WERE NOTED FROM BS 481 TO BS 681 APPROX 19 CRACK INDICATIONS WERE NOTED BY HFEC INSP. LAP JOINT CUT OUT AND REPAIRED PER ERA 332726-14.SDR DL72K990245Spar · damagedFOUR FASTENER HOLES WERE MISDRILLED DURING ACCOMPLISHMENT OF EO 4-72440-3AD. HOLES WERE OVERSIZED TO 0.312 DIA. REPAIRED PER ERA 332757-14AD.SDR CALA9900110Actuator · inoperativeTHE LT MLG DOOR WOULD NOT RETRACT AFTER TAKEOFF FROM SFO. THE AIRCRAFT WAS RETURNED TO SFO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LT MLG DOOR ACTUATOR IAW MM 32-32-81. LEAK AND OPERATIONAL CHECKS WERE GOOD.SDR DL72S990231Engine · failedNR 1 ENG FAILED IN FLIGHT AT APPROX FL305. AIRCRAFT SHUTTERED FOR ABOUT 10 SEC THEN ENG FLAMED OUT, EGT ROSE TO ABOUT 780C, OIL TEMP ROSE TO 140C. RETURNED TO SLC. FOUND METAL IN TAILPIPE. REPLACED ENGINE.SDR DL72S990230Rib · crackedMULTIPLE CRACKS FOUND IN THE WING RIB UPPER CHORD AT BS 760 AT R/LBL 70.85 DURING INSPECTIONS PER SI 4-58560-12AD. ALL CRACKS FOUND WERE TYPICAL OF PER SB727-57-0112, R5. ALSO, TOOLING DAMAGE WAS DONE DURING REPAIR INSTALLATION. REPAIRED PER ERA 332730-14ADSDR DL72K990976Skin · damagedDURING SHOP INSPECTION, A HOLE WAS FOUND IN COVE SKIN PANEL AT 2ND FROM I/B AFT FLAP TRACK. THE SKIN WAS REPAIRED PER MM 57-52-0, FIG 809.SDR DL72S990234Skin · crackedLFEC INSPECTION OF THE LOWER ROW OF FASTENERS IN THE STR 4R LAP SPLICE GAVE TWO CRACK INDICATIONS. INTERNAL HFEC INSPECTION CONFIRMED ONLY TWO CRACKS, ONE AT FS 513, AND ONE AT FS 632. FASTENERS WERE REMOVED FWD AND AFT OF EACH CRACK AND HFEC SURFACE INSPECTSDR DL72S990222Batteries · discharged2L EMERG EXIT LIGHT INOP. REPLACED BATTERIES, OPS CHECK GOOD.SDR DL72K990229Blkhd Stiffener · crackedCRACK FOUND IN VERT STIFFENER AT RBL 36.83 ON THE FWD SIDE OF BS 1183 BLKHD, CRACK IS LOCATED AT APPROX WL 238 AND IS NO LONGER THAN 2. REPAIRED PER ERA 332741-14.SDR DL72K990228Blkhd Stiffener · crackedCRACK FOUND IN THE LBL 36.83 VERT STIFFENER ON THE FWD SIDE OF BS 1183. CRACK LOCATED AT APPROX WL 238 AND WAS APPROX 2 INCHES LENGTH. REPAIRED PER ERA 332750-14.SDR DL72K990227Skin · wornGOUGE/WORN AREA WAS FOUND IN THE FUSELAGE SKIN CAUSED BY THE ENGINE INLET SKATE ANGLE. REPAIRED PER ERA 332760-14AD.SDR DL72K990226Stringer · damagedS7L WAS GOUGED DURING INSTALLATION OF NEW GALLEY, DAMAGE IS IN INNER RADIUS AT BS 1018. REPAIRED PER ERA 332697-14.SDR DL72K990225Skin · damagedEXISTING TRIM OUTS AND ADDITIONAL GROUND DAMAGE WAS FOUND IN THE SKIN AT THE AFT EDGE OF THE C2 DOOR CUTOUT AT BS 990. THE DAMAGED AREAS ARE NEAR S24R. REPAIRED PER ERA 332684-14.SDR DL72K990224Bulkhead Ring · damagedDURING INITIAL INSPECTION, A FASTENER AFT OF BS 1183 AT RBL 24 WAS FOUND LOOSE. DURING REMOVAL OF THE FASTENER, TOOLING DAMAGE WAS DONE TO THE TENSION FITTING AND THE SKIN AND ATTACH RING OF THE BS 1183 BLKHD. THE FITTING WAS REPLACED. REPAIRED PER ERA 3327SDR DL72S990188Light · inopEMERGENCY PATH LIGHT OUT ROW 26DEF. REPAIRED EMERGENCY PATH LIGHTS ROW 26DEF.SDR DL72S990187Battery Pack · dischargedTWO AISLE EMERGENCY EXIT SIGNS INOP AT AFT GALLEY AND AFT ENTRY DOOR. REPLACED BATTERY PACKS, OPS NORMAL.SDR DL72K990298Track · corrodedINB'D FLAP / INB'D TRACK / MLG BEAM ATTACH PAD: CORROSION AD 90-07-05 AND 90-06-09. CORROSION TO (1) MLG BEAM ATTACH HOLES AND (2) MLG DOOR AFT ATTACH FITTING BOLT HOLES. BOTH HOLES ARE WITHIN AD AREA. MLG BEAM ATTACH HOLES OVERSIZED AND LEFT AS IS. MLG D
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