Boeing 727-212
Service difficulty reports · 405
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 = '727212' 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 = '727212' 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 R5KB2013031150569Door Frame · damagedOTBD STRUCTURE AT DOOR FRAME, BS 950E DAMAGED AT STR 27R.SDR R5KB2013031150559Doubler · corrodedFRAME DOUBLER CORRODED AT BS 1166, BETWEEN STR 25L AND 25R.SDR R5KB2013031150544Web · corrodedWEB AT BS 990 CORRODED FROM RBL 27 TO RBL 29.SDR R5KB2013031150365Floorbeam · corrodedCORROSION ON BOTTOM CORD OF FLOORBEAM AT STA 1130, LBL 28.SDR R5KB2013031150525Frame · corrodedFRAME AT BS 950B CORRODED ABOVE STR 28L.SDR R5KB2013031146434Floor Support · corrodedFLOOR SUPPORT, CORRODED BETWEEN STA 950E AND 960E AT STR 27R.SDR R5KB2013031146431Stringer · corrodedSTRINGER 29L, CORRODED BETWEEN STA 950F AND 960F.SDR R5KB2013031150504Stringer · crackedSTRINGER 29R CRACKED AT BS 985.SDR R5KB2013031150428Frame · corrodedFRAME AT BS 990, RBL 22 AREA OF CORROSION.SDR R5KB2013031146390Shear Tie · corrodedSHEAR TIE CORRODED ON AFT SIDE STA 1148 BETWEEN STR 28R AND 29R.SDR R5KB2013031146430Skin · corrodedEVIDENCE OF CORROSION AT LOWER AFT CORNER CUTOUT STA 990, STR27R.SDR R5KB2013031150507Skin · corrodedSKIN CORRODED UNDER EDGE OF DOUBLER AT STA 950E, STR 27R.SDR R5KB2013031150373Door Frame · corrodedDOOR FRAME AT BS 950F HAS AREA OF CORROSION ABOVE STR 27R ON WEB.SDR R5KB2013031146428Intercostal · corrodedINTERCOSTAL CORRODED AT STR 28R BETWEEN STA 950F AND 970.SDR PCSA2012072101Connector · damagedENGINE NR 2 FIRE WARNING BELL AND LIGHT ACTUATED IN FLIGHT.SDR SPUY20120628024Support · corrodedAFTER REMOVAL OF LT MLG FWG TRUNNION SUPPORT FITTING FOUND INBD SUPPORT ASSY RUSTED.SDR SPUY20120628023Support · corrodedAFTER REMOVAL OF RT MLG FWD TRUNNION SUPPORT FITTING FOUND INBD SUPPORT ASSY RUSTED.SDR SPUY20120627022Support · corrodedRT WING REAR SPAR AREA. REAR SUPPORT TO FLAP TRACK NR 5 SHOWS CORROSION AT WS 224.50 (FWD PART).SDR SPUY20120627021Support · corrodedLEFT WING REAR SPAR AREA. REAR SPAR SUPPORT TO FLAP TRACK NR 4 SHOWS CORROSION AT WS 224.50. (FWD PART)SDR SPUY20120620020Trunnion · corrodedRT WING MLG FORWARD TRUNNION ATTCH FITTING INBD FLANGE SHOWS CORROSION.SDR SPUY20120620019Trunnion · corrodedLEFT WING MLG FOWARD TRUNNION ATTACH FITTING INBD FLANGE SHOWS CORROSION.SDR SPUY20120620018Frame · deformedMAIN CARGO BAY FRAME DEFORMED, BS 380.SDR SPUY20120620017Floorbeam · corrodedMAIN CARGO BAY AFT UPPER FLANGE OF FLOORBEAM SHOWS CORROSION RBL 10 BS 950.SDR SPUY20120620016Floorbeam · corrodedMAIN CARGO BAY FLOORBEAM UPPER FLANGE SHOWS CORROSION BS 1070 BETWEEN LBL 45" AND LBL 62.5.SDR SPUY20120620015Cargo Track · corrodedCARGO TRACK SHOWS CORROSION BS 1010, LBL 62.5.SDR SPUY20120620014Cargo Track · corrodedCARGO TRACK SHOWS CORROSION BS 950 LBL 24.5.SDR SPUY20120620013Cargo Track · corrodedCARGO TRACK UPPER AND LOWER LT FLANGE SHOWS CORROSION BETWEEN BS 950C AND BS 950D, RBL 24.5.SDR SPUY20120620012Cargo Track · corrodedCARGO TRACK LOWER PART BOTH FLANGES SHOW CORROSION BS 1130, RBL 24.5.SDR SPUY20120620011Cargo Track · corrodedCARGO TRACK RT FLANGE SHOWS CORROSION BETWEEN BS 950C AND BS 950F LBL 24.5.SDR SPUY20120620010Cargo Track · corrodedCARGO TRACK SHOWS CORROSION UPPER LBL 62.5 BS 445.000, BS 485.000 AND BS 502.00.SDR SPUY20120620009Beam · corrodedMAIN CARGO BAY BEAM FWD LOWER FLANGE SHOWS POINTS OF CORROSION AT STA 890, RBL 35".SDR SPUY20120620008Beam · corrodedMAIN CARGO BAY BEAM FWD LOWER FLANGE SHOWS CORROSION AT STA 900 RBL 45"SDR SPUY20120620007Floorbeam · corrodedMAIN CARGO BAY FLOORBEAM LOWER FLANGE SHOWS CORROSION STA 890, LBL 30".SDR SPUY20120620006Cargo Track · corrodedNR 1 CARGO TRACK LOWER PART CORRODED AT BS 950, LBL 62.5.SDR SPUY20120620005Skin · corrodedCENTER SECTION LOWER SKIN SHOWS CORROSION STA 804-5 - STA 825.95, LBL25.SDR SPUY20120620004Spar · corrodedLT WING FRONT SPAR LOWER CHORD SHOWS CORROSION BETWEEN WS 304.0 AND WS 320.5SDR SPUY20120620003Frame · deformedFWD CARGO BAY FRAME DEFORMED BS 560, STRINGER 24L TO 25L.SDR SPUY20120620001Frame · crackedFWD CARGO BAY FRAME CRACKED .5" BS 580, STRINGER 23L TO 25L.SDR SPUY20120620002Frame · deformedFWD CARGO BAY FRAME DEFORMED BS 520, S22-26L.SDR FY4Y201203070001Bear Strap · corrodedDURING PERFORMED 6C-CHECK, CORROSION WAS FOUND ON AFT ENTRY DOOR CUTOUT BEAR STRAP AT STATION BS 1067 TO 1073 BETWEEN S-12L AND S-15L (DIMENSIONS OF CORROSION AREA:8.750 × 2.250 AND 7.000 × 2.250). AFTER BLEND OUT CORROSION, THE PENETRATION DEPTH WAS OVER LIMSDR FY4Y201202226Spar · corrodedDURING PERFORMED 6C CHECK, CORROSION WAS FOUND ON FUSELAGE WING CENTER SECTION REAR SPAR WEB BS 870 LBL 25 AND 35 TO 39 WL 184. AFTER CORROSION REMOVED, CLEAN UP DEPTH WAS OVER LIMITS PER SRM 57-10-1 PAGE 12.SDR FY4Y201202225Spar · corrodedDURING PERFORMED 6C CHECK, CORROSION WAS FOUND ON FUSELAGE WING CENTER SECTION REAR SPAR WEB BS 870 RBL 35 TO 43 WL 184. AFTER CORROSION REMOVED, THE CLEAN UP DEPTH WAS OVER LIMIT PER SRM 57-10-1 PAGE 12.SDR FY4Y201202224Structure · corrodedDURING PERFORMED 6C CHECK, LOWER FUSELAGE BS 348 TO 351 S27R WAS FOUND CORRODED. AFTER CORROSION REMOVED, CLEAN UP DEPTH WAS OUT OF LIMIT PER SRM 53-10-1 PAGE 1.SDR FY4Y201202223Structure · corrodedDURING PERFORMED 6C CHECK , LOWER FUSELAGE BS 348 TO 351 S27L WAS FOUND CORRODED. AFTER CORROSION REMOVED, CLEAN UP DEPTH WAS OUT OF LIMIT PER SRM 53-10-1 PAGE 1.SDR FY4Y201202172Spar · corrodedDURING PERFORMED 6C CHECK, FOUND RT HORIZONTAL STABILIZER REAR SPAR LOWER CHORD CORRODED AT ELEV STA 173 PER SRM 55-10-01 FIG 1 SHEET 3 ITEM 4, PENETRATED DEPTH OUT OF LIMITS. OPENSDR FY4Y201202151Beam · corrodedDURING PERFORMED 6C CHECK (ASIA PACIFIC AIRLINES N86425), CARD NO. C55-300-10 PART 2 OF 2, FOUND RT HORIZONTAL STABILIZER T/E UPPER BEAM CORRODED AT ELEV STAT 17 & 68.5 PER B727 SRM 55-10-01 FIG 1 SHEET 3 ITEM 5 PENETRATED DEPTH OUT OF LIMIT. THE ITEM HAS BEESDR FY4Y20120215Skin · corrodedDURING PERFORMED 6C CHECK. FOUND RT WING LWR SKIN CORRODED AT WS 196 TO WS 201 JUST UNDER FRONT SPAR, PER B727 SRM 57-30-1 PAGE 6 PENETRATED DEPTH OUT OF LIMIT. THE ITEM HAS BEEN REPORTED TO DER FOR REQUESTING THE REPAIR APPROVAL DATA.SDR FY4Y197M20110919Beam · corrodedDURING PERFORM THE MAINTENANCE WORK (7C CHECK CARD NO.:C53-300-10 PART 1 OF 2), CORROSION WAS FOUND ON THE AFTER FLANGE OF THE LT HORIZONTAL STABILIZER T/E LOWER BEAM AT ELEV STA 156~160 AND ELEV STA 186.5~190. THE DEPTH AFTER BLENDOUT IS OUT OF LIMIT. THE ASDR 2011FA0000045Stringer · corrodedLT RAM AIR INLET LOWER FUSELAGE SKIN BULGED STA 720A. CORROSION FOUND AT STRINGER AT KEELBEAM.SDR PCSA2011012201Actuator · leakingDURING CLIMBOUT, LOST HYDRAULIC SYSTEM "A" QUANTITY AND PRESSURE. T/S FOUND LEAKING NR 5 KRUEGER FLAP ACTUATOR. REMOVED AND REPLACED ACTUATOR AND OPS AND LEAK CHECK GOOD.
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