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 I5PA2016022642502Drag Brace · crackedAFTER FURTHER ASSESSMENT, WE IDENTIFIED THE PROBLEM THAT CAUSED THE AIRCRAFT'S NLG ASSEMBLY NOT TO EXTEND. WE FOUND THAT THE NOSE GEAR DRAG BRACE CTR LOCK ARM SPLINE HAD CRACKED, WHICH DID NOT ALLOW THE SYS TO UNLOCK NORMALLY OR MANUALLY FOR THE NOSE GEAR TOSDR I5PA2015102631902Line · unknownNUMBER 3 ENG EXPERIENCED OIL LOSS. OIL PRESS AT APPROX 10 PSI ON IDLE PRIOR TO SHUT DOWN. DUE TO WEATHER ACFT DIVERTED TO ALTERNATE, FLIGHT ARRIVED SAFELY. TROUBLESHOOTING IN PROGRESS. ENG HAD APPROX 1 GAL IN THE SYS & SERVICED APPROX 3 GAL. FOUND OIL SUPSDR I5PA2015102631901Engine · leakingNR 3 ENG EXPERIENCED OIL LOSS. OIL PRESSURE AT APPROX 10 PSI ON IDLE PRIOR TO SHUT DOWN. DUE TO WEATHER ACFT DIVERTED TO ALTERNATE, FLIGHT ARRIVED SAFELY. TROUBLESHOT NR ENG OIL LOSS, ENG INITIALLY HAD APPROX 1 GAL IN THE SYS & SERVICED APPROX 3 GAL FOR TRSDR PCSA2014122201Engine · making metalENGINE NR 3 HAD A COMPRESSOR STALL & A FLAMEOUT AT FL320. METAL FOUND IN TAIL PIPE.SDR 3FMR20140903001Skin · corrodedDURING ACCOMPLISHMENT OF AD 85-24-02, CORROSION WAS FOUND IN LOWER SKIN BS 870, RBL 3 - 8, WATERLINE 160.8.SDR 3FMR20140903006Skin · corrodedDURING ACCOMPLISHMENT OF AD 82-24-02, CORROSION WAS FOUND IN THE LT AIR CONDITIONING PLENUM AREA ON THE LOWER SURFACE SKIN AT BS 826 - 848 AT LBL 32, W/L 160.8. FOUND TO BE OUT OF SRM LIMITS. REPAIRED IAW DWG AMJ-N598AJ - 04/ 14.SDR 3FMR20140903004Structure · corrodedDURING ACCOMPLISHMENT OF AD 2005-05-19, CORROSION WAS FOUND ON THE LT FRONT SPAR LOWER ANGLE AT WS 383 - 465. FOUND TO BE OUT OF SRM LIMITS. REPAIRED.SDR 3FMR20140903005Spar Cap · corrodedCORROSION WAS FOUND ON THE RT HORIZONTAL STABILIZER. CORROSION IS LOCATED AT HORIZONTAL STAB STATION 78.13. FOUND TO BE OUT OF MFG SRM LIMITS. REPAIRED IAW DWG 55-14215-1A.SDR 3FMR20140903003Skin · corrodedRIGHT WING LOWER SKIN WAS FOUND CORRODED AROUND FRONT SPAR ATTACH FASTENERS LOCATED AT WING STA 509 - 519. CORROSION WAS FOUND TO BE OUT OF SRM LIMITS. REPAIRED IAW DWG AMJN598AJ 3/14.SDR 3FMR20140903002Spar · corrodedDURING ACCOMPLISHMENT OF AD 2005-05-19, CORROSION WAS FOUND ON THE RIGHT HAND WING, FRONT SPAR, LOWER CHORD AT WING STATION 509 TO 519. CORROSION WAS FOUND OUTSIDE OF MANUFACTURER SRM LIMITATIONS. A DESIGNATED ENGINEERING REPRESENTATIVE REPAIR HAS BEEN SOUGHT.SDR I5PA201405010002Gearbox · leakingAT APPROX 0730Z, THE CREW EXPERIENCED NR 3 ENG LOSS OF OIL QTY, FOLLOWED BY LOW OIL
PRESS, HIGH ENG EMP AT FL 330. DECLARED AN EMER AT 0738Z & AIR RETURNED BACK SAFELY AT 0908Z. TROUBLESHOOTING IN PROGRESS. R & R NR 3 ENG GEARBOX IAW AMM 72-63-00. INSPECTESDR I5PA201405010001Gearbox · unknownAT APPROXIMATELY 0730Z, THE CREW EXPERIENCED NR 3 ENG LOSS OF OIL QTY FOLLOWED BY LOW OIL PRESS, HIGH ENG TEMP AT FL 330. THEY DECLARED AN EMERGENCY AT 0738Z & AIR RETURNED BACK TO HNL STATION SAFELY AT 0908Z. TROUBLESHOOTING IN PROGRESS. R & R NR 3 ENG GEASDR I5PA2013101600053Frame · corrodedCORROSION WAS FOUND AT BS 720D FRAME BETWEEN S25-26R. CORROSION REMOVED IAW SRM 53-10-1, FIG 1.SDR FY4Y2013101600005Skin · corrodedDURING 7C CHECK & CPCP INSPECTION, INSPECTOR PERFORMED VISUAL INSPECTION AND FOUND CORROSION ON CENTER WING LOWER SURFACE BETWEEN STRINGER 4C & 5C, WING LBL 24 TO LBL 28, AFTER BLEND OUT OF CORROSION, FOUND OUT OF LIMITS IAW SRM 57-30-1, TABLE 1.SDR FY4Y201310160001Skin · corrodedDURING CPCP INSPECTION, INSPECTOR PERFORMED VISUAL INSPECTION AND FOUND CORROSION ON FUSELAGE EXTERNAL SURFACE OF BS 640 TO 660, FOUND OUT OF LIMITS IAW SRM 53-30-1, FIG 2.SDR PCSA2013092501Duct · rupturedLOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. FOUND DUCT RUPTUREDSDR FY4Y201307180003Bulkhead · corroded8C CHECK. DURING CPCP INSPECTION, CORROSION WAS FOUND. THE CORROSION DAMAGE THROUGH THE PART ON THE NOSE WHEEL WELL BS 294.5 BULKHEAD WEB.SDR FY4Y20130718197Frame · corroded8C CHECK. DURING CPCP INSPECTION, PERFORMED VISUAL INSPECTION AND FOUND LEVEL 2 CORROSION ON LOWER ANGLE OF BS 950 CANTED BULKHEAD BETWEEN S22-23L. BLENDED OUT CORROSION, PENETRATION DEPTH WAS OVER LIMITS IAW SRM 53-10-1, FIG 1.SDR FY4Y20130718002Skin · corroded8C CHECKK. DURING PERFORMED CPCP INSPECTION, CORROSION WAS FOUND ON THE UPPER SKIN UPPER SURFACE OF THE WING CENTER SECTION, AT BS 783.95, BETWEEN RBL 63.0 AND RBL 65.5. CORROSION BLENDED OUT. THE DAMAGE CONDITION HAD EXCEEDED THE ALLOWABLE LIMITATION IAWSDR PCSA2013051001Fuel Control · faultyENGINER 2 FLAMEOUT AT CRUISE. ALL PARAMETERS NORMAL. ENG WINDMILL FOR ABOUT 15 MIN. 20 PSI OIL PRESS. THE NR 2 ENGINE OIL FILTER WAS CHECKED, FOUND NORMAL, THE NR 2 FUEL PUMP AND FUEL CONTROL UNIT REPLACED AND TESTED PER THE B727 AMM AND THE AIRCRAFT RETURNSDR R5KB2013013150501Mount · corrodedNR 2 ENGINE, UPPER FORWARD MOUNT ASSY CORRODED.SDR R5KB46252Pin · corrodedRIGHT WING AFT BOTTLE PIN CUP HAS EVIDENCE OF CORROSION UNDER PIN CUP.SDR R5KB2013013150398Seat Track · corrodedLEFT BUTTLINE 55 SEAT TRACK HAS SEVERAL AREAS OF CORROSION BETWEEN STA 991 TO 1030.SDR R5KB2013013150353Seat Track · corrodedLEFT BUTTLINE 56, STA 344 SEAT TRACK CORRODED.SDR R5KB2013013150349Seat Track · corrodedSEAT TRACK CORRODED BETWEEN STA 800 TO 815, LEFT BUTTLINE 25.SDR R5KB2013013150258Stringer · corrodedEVIDENCE OF CORROSION BETWEEN STA 950E AND 950E, STRINGER 15L.SDR R5KB2013013146411Intercostal · corrodedINTERCOSTAL CORRODED AT STA 1060 STRINGER 20 LEFT.SDR R5KB2013013150363Floorbeam · corrodedTOP CORD OF FLOORBEAM CORRODED ON FLOORBEAM AT STA 1110, LEFT BUTTLINE 24 TO 52.SDR R5KB2013013150432Support · corrodedSEAT TRACK SUPPORT CORRODED AT LEFT BUTTLINE 45.5, STA 1090 TO 1110.SDR R5KB2013013150369Web · corrodedCORROSION AROUND PINS IN FLOOR WEB AT STA 1146 BETWEEN RIGHT BUTTLINE 54 AND 58.SDR R5KB2013013150368Web · corrodedCORROSION AROUND EDGE OF WALL AND FLOOR WEB AT STA 1148, RIGHT BUTTLINE 63.SDR R5KB46410Intercostal · corrodedINTERCOSTAL AT STA 1060, LEFT BUTTLINE 26 AREA OF CORROSION.SDR R5KB2013012850324Web · crackedFLOOR TO SKIN WEB CRACKED, .25' AT EDGE OF LIGHTENING HOLE AT STA 490, RIGHT BUTTLINE 72.SDR R5KB2013012850439Floorbeam · corrodedFLOORBEAM CORRODED ON UPPER AND LOWER SURFACE AT STA 1110 LEFT BUTTLINE 1 TO RIGHT BUTTLINE 12.SDR R5KB2013012846287Skin · corrodedCORROSION ON RIGHT SIDE OF UPPER RUDDER TRAILING EDGE AT RS 175.SDR R5KB2012012846190Skin · corrodedCORROSION ON LEFT SIDE OF UPPER RUDDER TRAILING EDGE BETWEEN RS 220 AND 242.SDR R5KB2013012846405Shear Tie · corrodedSHEAR TIE CORRODED AT STA 1130 BETWEEN STR 29 AND 30 LEFT.SDR R5KB2013012846406Shear Tie · corrodedSHEAR TIE CORRODED AT STA 1110, BETWEEN STR 28 AND 29 LEFT.SDR R5KB2013012850560Panel · delaminatedLEFT UPPER RUDDER PANEL BETWEEN STA 212 AND 220 HAS ONE AREA OF DELAMINATION.SDR R5KB2013012850553Web · crackedSUPPORT WEB CRACKED LEFT BUTTLINE 25 FROM STA 1130 TO 1110.SDR R5KB2013012846189Structure · corrodedCORROSION ON LEFT SIDE OF UPPER RUDDER BETWEEN STA 212 AND 220.SDR R5KB2013012850361Floorbeam · corrodedFLOORBEAM CORRODED STA 1110 LEFT BUTTLINE 12 TO LEFT BUTTLINE 24 TOP AND BOTTTOM.SDR R5KB2013012846194Skin · damagedUPPER RUDDER SKIN CORRODED RIGHT SIDE TRAILING EDGE BETWEEN STA 220-247.SDR R5KB2013012846281Skin · damagedSKIN DAMAGED ON LOWER RUDDER LEFT SIDE BETWEEN STA 113-118.SDR R5KB2013012846403Shear Tie · corrodedSHEAR TIE CORRODED AT STA 1130 BETWEEN STR 27 AND 28 RIGHT.SDR R5KB2013012850568Frame · damagedFRAME DAMAGED AT STA 1130 BETWEEN STR 27 AND 28 RIGHT.SDR R5KB2013012846170Structure · crackedCRACK ON TOP OF NR 1 PYLON OUTBD FASTENER HOLE"P" OF S/B 727-54A0010R6, FROM HOLE TO OTBD EDGE OF LOWER ANGLE.SDR R5KB2013012846396Frame · corrodedFRAME AT STA 1148 CORRODED AT STR 26R.SDR R5KB2013012846404Shear Tie · corrodedSHEAR TIE CORRODED AT STATION 1130 BETWEEN STR 27 AND 28 LEFT.SDR R5KB2013012846435Shear Tie · corrodedSHEAR TIE CORRODED STA 1166 BETWEEN STR 29 AND 30 LEFT.
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