Boeing 727-2J7
Service difficulty reports · 117
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 = '7272J7' 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 = '7272J7' 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 96ZZZX4865Control Valve · crackedFLIGHT RETURN. LOST A-SYSTEM HYDRAULICS IN-FLIGHT DUE TO LOSS OF FLUID. FOUND OUTBOARD FLAP CONTROL VALVE LEAKING (DUE TO CRACK IN CASE). THE OUTBOARD FLAP CONTROL VALVE WAS REPLACED TO CORRECT THE PROBLEM.SDR 96ZZZX3519Fitting · corrodedDURING C-CHECK INSPECTION, NOTED THE FORWARD TIE-DOWN MOUNT FITTING HAD INTERGRANULAR CORROSION AT STA 560, AT S26R.SDR 96ZZZX3518Fitting · corrodedDURING C-CHECK INSPECTION, NOTED THE SECOND FROM FRONT TIE-DOWN MOUNT FITTING HAD INTERGRANULAR CORROSION AT STA 570 AND STA S26R.SDR 96ZZZX3517Web · corrodedDURING C-CHECK INSPECTION, INTERGRANULAR CORROSION WAS NOTED ON FORWARD BAG PIT LOWER SILL CUT-OUT WEB. FROM STA 560 TO STA 620, LOCATED AT S26R.SDR 96ZZZX3666Stringer · corrodedWHILE PERFORMING CPCP TASK CARD NR C53-113-01.01, FOUND CORROSION BLEEDING FROM FASTENERS ON STR 26L BETWEEN STA 500 - STA 520 IN ZONE 1-13. OPEN AREA FOUND LEVEL 2 CORROSION ON STRINGER. REPLACED SECTION OF STRINGER FROM STA 480 TO STA 515. THE REMAINDER OSDR 96ZZZX3665Spar Fitting · corrodedFOUND LEVEL 2 CORROSION WHILE PERFORMING TASK NR C57-581-03. THE CORROSION EFFECTED A FITTING ON THE RIGHT WING REAR SPAR LOWER CHORD AT WBL 94 INCHES, AT ZONE 6-85. REPLACED FITTING AND CLEANED CHORD PER SRM 51-10. MAINTENANCE ACCOMPLISHED BY PROFESSIONAL SDR 96ZZZX3664Chord · corrodedWHILE PERFORMING CPCP TASK CARD NR C55-300-10.01, FOUND INDICATION OF LEVEL 2 CORROSION. THIS CORROSION EFFECTED THE LEFT HORIZONTAL STABILIZER UPPER TRAILING EDGE CHORD AROUND FASTENERS FOR THE NR 2 ELEVATOR HINGE FITTING AT STABILIZER STA 118.65, ELEVATOR SSDR 96ZZZX3663Chord · corrodedWHILE PERFORMING CPCP TASK CARD NR C55-300-10.01, FOUND INDICATION OF LEVEL 2 CORROSION. THIS CORROSION EFFECTED THE LEFT HORIZONTAL STABILIZER UPPER TRAILING EDGE CHORD AROUND FASTENERS FOR THE NR 3 ELEVATOR HINGE FITTING AT STABILIZER STA 151, ELEVATOR STA SDR 95ZZZZ274Stringer · corrodedIN THE PROCESS OF COMPLYING WITH S/B 53-159 BELLY SKIN REPLACEMENT, STRINGER (P/N 65-56441-8) WAS FOUND CORRODED ALONG TOPSIDE. STRINGER WAS REPLACED.SDR 95ZZZX4159Stringer · corrodedIN THE PROCESS OF COMPLYING WITH SB 53-159 BELLY SKIN REPLACEMENT, SOME CORROSION WAS FOUND ON LEFT SIDE OF STRINGER PN 65-56129-10. THE STRINGER HAD TO BE REPLACED. THIS STRINGER RUNS ALONG THE LOWER END OF NR 2 CARGO DOOR. SUBMITTER STATED CAUSE OF THIS CSDR 95ZZZX4158Stringer · corrodedIN THE PROCESS OF COMPLYING WITH SB 53-159, BELLY SKIN REPLACEMENT STRINGER P/N 65-56441-8 WAS FOUND CORRODED ALONG TOP SIDE. STRINGER WAS REPAIRED. SUBMITTER STATED CAUSE OF CORROSION WAS EITHER MOISTURE BUILD-UP OR LACK OF FINISH ON THE PART.SDR 95ZZZZ273Stringer · crackedIN THE PROCESS OF COMPLYING WITH S/B 53-159 BELLY SKIN REPLACEMENT STRINGER (P/N 65-56441 WAS FOUND TO BE CRACKED AT BOLT HOLES FWD END OF STRINGER.SDR 95ZZZZ270Stringer · crackedIN THE PROCESS OF COMPLYING WITH SB 53-159 BELLY SKIN REPLACEMENT, STRINGER (P/N 65-56441-7) WAS FOUND TO BE CRACKED AT BOLT HOLES FWD END OF STRINGER.SDR 95ZZZX4162Blkhd Web · corrodedDURING A C-CHECK INSPECTION, CORROSION WAS FOUND AT STA 351.2 FORWARD BULKHEAD WEB SHEAR TIE AND ADJACENT AREA. AS THE CORROSION WAS FOUND IN NUMEROUS AREAS, THE BULKHEAD WEB WAS REPLACED. THE REPAIR WAS ACCOMPLISHED WITH THE HELP OF BOEING AIRCRAFT COMPANY.SDR 95ZZZX4160Structure · corrodedDURING A C-CHECK INSPECTION, FOUND SEVERAL STRINGERS AND DOUBLERS CORRODED IN LOWER BELLY AREA FROM STA 320 - STA 360. INTERNAL DOUBLER CORRODED ON SKIN PANEL STA 351 TO STA 360, STR 27L TO STR 27R. STRINGER SEGMENT CORRODED STA 351 TO STR 360, STR 26R. FRAMSDR 95ZZZZ271Stringer · crackedIN THE PROCESS OF COMPLYING WITH S/B 53-159 BELLY SKIN REPLACEMENT, CHORD STRINGER (P/N 65-56441-7) WAS FOUND TO BE CRACKED AT FWD BOLT HOLES. THE ED IN THAT AREA SEEMS TO BE MARGINAL.SDR 95ZZZX1490Chord · corrodedDURING BELLY SKIN REPLACEMENT, CHORD, PN 65-56441-7, WAS FOUND CORRODED. FROM EXAMINATION, IT APPEARS THERE WAS NOT ENOUGH CORROSION PREVENTION AND, ALSO, MOISTURE BUILD-UP. CHECKING DRAIN HOLES IN LOWER SKIN AND MORE EFFORT USED DURING INSPECTION.
Back to Boeing 727-2J7