Boeing 727-247
Service difficulty reports · 2,669
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 = '727247' 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 = '727247' 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 UPS204855Eel · misinstalledCREW REPORTED, EMERGENCY EXIT LIGHTS REMAIN ILLUMINATED AFTER DEPARTURE, FOR REMAINDER OF FLIGHT. MAINTENANCE USED THE WRONG TYPE OF LIGHT ASSY FOR THE COCKPIT POSITION, TESTED OK.SDR DL72W954394Angle · crackedAT HMV-1, INSP FOUND CHORD ANGLE CRACKED AT 48 SECTION LT SIDE STA 1342. THE HORIZONTAL CHORD ANGLE IS CRACKED JUST I/B OF FIN TERMINAL FITTING. FITTING IS PREVIOUSLY STOP DRILLED. REPAIRED CRACK PER M/M 53-11-0 PG 808.SDR DL72W954393Angle · crackedAT HMV-1, INSPECTION FOUND THE CHORD ANGLE CRACKED AT STA 134248 SECTION HORIZONTAL CHORD ANGLE LOC ABOVE S-DUCT. IT IS CRACKED JUST I/B OF RT FIN TERMINAL FITTING. CHORD HAS BEEN PREVIOUSLY STOP DRILLED, CRACK APPEARS TO HAVE CONTINUED PAST STOP DRILL HOLESDR DL72W954244Stringr · crackedATL - HMV, RT WING TANK AFT VENT BOX STRINGER EAR AT RIB 656.5 CRACKED. REPAIRED PER MM 57-13-0.SDR DL72W954148Spar · crackedDURING SHOP INSPECTION, NR 3 MID-FLAP, LOWER AFT SPAR RAIL FOUND CRACKED 19 INCHES FROM INBOARD END OF FLAP. REPAIRED PER MM 57-54-0.SDR DL72W954103Floorbeam · corrodedAT HMV, FS 344 FLOORBEAM UPPER CAP CORRODED AT BL 0 TO LBL 60. REPAIRED UPPER CAP PER SRM 53-10-8 FIG 10.SDR DL72W954337Angle · wornAT HMV, FOUND ACCESS PANELS 9601 AND 9602 MOUNTING SCREW WORN THROUGH SUPPORT ANGLE. INSTALLED DOUBLER PER SRM 51-40-4 PG 14.SDR DL72W954326Skin · crackedAT HMV, FOUND .25 INCH CRACK AT AFT INBD CORNER OF PNEU AIR CONNECTION ACCESS DOOR CUTOUT. STOP DRILLED CRACK IAW M/M 53-30-0 PG 803, LOCATED AND DRILLED REPAIR DOUBLER IAW M/M 53-30-0 PG 803, INSTALLED REPAIR.SDR DL72W954303Stringer · crackedFOUND AT HMV REF OPN 8502AD LT WING STRINGER TO RIB HFEC INSP, SHOWS FWD TAB OF FWD VENT BOX, STRINGER S-14 CRACKED AT STRINGER TO RIB ATTACH POINT AT WS 629. REPAIRED VENT BOX STRINGER PER MM 57-13-0.SDR DL72W954239Doubler · crackedDURING HMV, INSP FOUND FUS EXT SKIN DOUBLER CRACKED AT FWD UPPER CUTOUT RADIUS FOR R-1 DOOR UPPER HINGE. HFEC VERIFIED AND MARKED END OF CRACK, REMOVED DOUBLER. HFEC HOLES CRACK END AT FASTENER HOLE, LOC A PER 53-30-0. MANUFACTURED DOUBLER PER M/M 53-30-0, SDR DL72W954277Duct Housing · damagedDURING HMV, FOUND TEMP REPAIR ON RT SIDE OF NR 2 ENGINE INLET DUCT HOUSING. REPAIRED PER SRM 54-10-3 FIG 4.SDR DL72W954132Skin · crackedAT HMV ATL, TEMP REPAIR INSTALLED. RT FWD CORNER OF AFT AIR STAIR CUT-OUT. REPAIR NOT MARKED PERMANENT. CORRECTION: REMOVED OLD REPAIR AND STARTED MAKING NEW REPAIR IAW M/M 53-30-0. OK TO INSTALL. VERIFIED TERMINATION OF CRACK PER P.S. 900-6-3 NR 1. INSTSDR DL72W954071Lines · crackedFUEL VENTED OUT OF RT VENT BOX ON ACTIVE RUNWAY, FUEL MIGRATING FROM OTHER TANK CAUSING THE NR 3 TANK TO OVERFILL. FOUND CRACK LINES MFG (P/N 65-22731-2 AND 65-16710-52) REF IPC 28-30-0-16 ITEMS 120 AND 140. BOTH LINES SENT TO SHOP FOR REPAIRS.SDR DL72W954041Battery · dischargedAFT RIGHT SERVICE DOOR OVERHEAD EMERGENCY LIGHT INOP. REPLACED BATTERIES, CHECKS NORMAL.SDR DL72W954040Battery Pack · dischargedFWD RT SERVICE DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REPLACED RACK AND BATTERIES, OPERATION NORMAL.SDR DL72W954005Fuel Heat Vlv · failedNR 1 FUEL HEAT VALVE FAILED OPEN AFTER TAKEOFF, OIL TEMP HIT 120 DEGREES CENT, PULLED FUEL DE-ICE C/B. REPLACED FUEL HEAT VALVE, OPS CKS OK.SDR DL72W954002Eel Battery Pack · dischargedLT AFT OVER WING EMERGENCY LIGHT INOP. REPLACED LEFT OVER WING BATTERY PACK, OPS CHECK NORMAL.SDR DL72W954693Skin · gougesMTC REPORTS, 3 GOUGES IN THE FUSELAGE SKIN BELOW AND JUST AFT OF THE L2 DOOR LWR AFT CORNER. THE FIRST GOUGE IS LOCATED JUST AFT OF FS 1070, IT IS 7 INCHES LENGTH, HAS A MAX DEPTH OF 0.010, AND RUNS PERPENDICULAR TO S-18L. IT WILL BE BLENDED AND TREATED PER SDR DL72E954266Doubler · crackedTHE LT MAIN LANDING GEAR WHEEL WELL PRESSURE DECK WAS FOUND WITH A PREVIOUS MODIFICATION DOUBLER INSTALLED FOR A CRACK AT LBL 55 AND STA 938. THE PREVIOUS DOUBLER WILL BE REMOVED AND A NEW DOUBLER INSTALLED PER REVISION 4 OF THE SERVICE BULLETIN E0 4.61537-3ASDR DL72E954027Bushing · looseAT HMV, FOUND BUSHING LOOSE IN LT MLG PORK CHOP FTG IN AFT HOLE FOR NR 4 FLAP TRACK. REPAIRED AND INSTALLED NEW BUSHING PER MM 57-42-0.SDR DL72E953991Fitting · corrodedFOUND AT HMV, FRETTING CORROSION ON I/B FACE OF LT MLG PORK CHOP FITTING AT FLAP TRACK ATTACH HOLE. REPAIRED PER MM 57-42-0 PG 814.SDR DL72E953977Rib · crackedAT HMV, NR 4 SLAT RIB NR 18 CRACKED. REPAIRED PER MM 57-54-00.SDR DL72E960315Rib · crackedDURING SHOP INSPECTION, RIBS NR 2 AND NR 3 WERE FOUND TO BE CRACKED. REPAIRS WERE MADE AS PER M/M 57-54-0. ALSO, THE LOWER FORWARD SKIN ATTACH ANGLE WAS FOUND TO BE CRACKED. REPAIRED PER M/M 57-54-0, FOR NR 7 L/E SLAT.SDR DL72E953945Stringer · crackedDURING A HANGAR INSPECTION, A CRACK WAS DISCOVERED IN THE FWD STRINGER OF THE NR 1 ENGINE LWR COWL. A REPAIR WAS INSTALLED PER THE S.R.M. 51-40-3.SDR DL72E954116Skin · corrosionAT HMV IN ATLANTA, MTC FOUND CORROSION IN FUSELAGE SKIN AT STA 950 PLUS 10 INCHES JUST OUTBOARD OF STR 30. FINAL CUT-OUT DIMENSIONS ARE 2.75 INCHES BY 3.75 INCHES. THE SKIN IS FABRICATED FROM 2024-T3 CLAD AND HAS A NOMINAL THICKNESS OF 0.183 INCH AT THE FWD SDR DL72E954117Vent Access Hole · mislocatedDURING ACCOMPLISHMENT OF THE LT WING UPPER STRINGER 13/14 TAB ONLY REPAIR AT WS 656.5 RIB, THE VENTB OX ACCESS HOLE WAS INADVERTENTLY CUT INBD OF THE RIB INSTEAD OF OTBD. THIS REPAIR WAS BEING ACCOMPLISHED PER B727 M/M 57-13-0 FIG. 804, REPAIR FOR TAB CRACKS SDR DL72E954025Skin · crackedAT HMV, FOUND VERT STABILIZER SKIN STOPPED DRILLED 3 TIMES AT RT FS 1333 AT BOTTOM OF VERT FIN. REPAIRED PER MM 55-30-0 PG 801.SDR DL72E953976Angle · crackedNR 1 L/E FLAP ACTUATOR ATTACH ANGLE CRACKED I/B SIDE. WORKED AT HMV, REPAIRED ANGLE PER M/M 57-20-21.SDR DL72E953915Angle · crackedDURING F-1 LETTER CHECK, FOUND 1 INCH CRACK NR 3 L/E SLAT COVE SKIN ATTACH ANGLE BELOW ACTUATOR ATTACH POINT. REPAIRED PER M/M 57-54-0.SDR DL72E954069Frame · crackedAT HMV, FOUND FUSELAGE FRAME CRACKED AT REPAIR DOUBLER, UPPER FASTENER HOLE FS 930 RT SIDE. REPAIRED PER SRM 53-10-04 FIG 25 TYP B.SDR DL72E954023Web · crackedAT HMV, FOUND WEB CRACKED VERT STAB INT STA 1303. FABRICATED AND INSTALLED NEW DOUBLER PER SRM 53-10-4 FIG 17.SDR DL72E954022Web · crackedAT HMV, FOUND WEB CRACKED VERT STAB INT STA 1303. FABRICATED AND INSTALLED NEW DOUBLER PER SRM 53-10-4 FIG 17.SDR DL72E953974Vent Box Tab · crackedREF OPN 8602 AD HFEC INSP OF RT OUTER WING UPPER STRINGER-TO-RIB CRACK INDICATED FWD VENT BOX AFT TAB W.S. 686.5, MARKED NR 2.SDR DL72E953973Rib · crackedNR 5 SLAT-RIB NR 20 CRACKED UNDER LEADING EDGE AT NUTPLATE. WORKED AT HMV. REPAIRED PER M/M 57-54-00.SDR DL72E953972Heat Shield · crackedNR 6 SLAT-INTERIOR HEAT SHIELD CRACKED BETWEEN RIBS 11 AND 12. WORKED AT HMV. REPAIRED PER M/M 57-54-00, PG 804A.SDR DL72E953971Stringer · crackedHFEC CHECKED ON STR-TO-RIB HOLES SHOWS CRACK INDICATION ON STRINGER NR 10 AND NR 14 AT W.S. 656.5. WORKED AT HMV. INSTALLED REPAIR DOUBLER PER M/M 57-13-00.SDR DL72E953970Support · crackedRT ELEVATOR-HINGE SUPPORT FRAME CRACKED AT BOLT, INSIDE 3RD BALANCE BAY FROM O/B END, WORKED AT HMV. REPAIRED PER SRM 55-10-04, FIG 6.SDR DL72E953969Rib · crackedNR 4 SLAT-RIB NR 2 CRACKED. WORKED AT HMV. REPAIRED PER M/M 57-40-00, FIG 805.SDR DL72E953968Vent Box Tab · crackedTAB CRACKED. VENT BOX TAB CRACKED STA. 686.5 AT HOLE MARKED NR 4. WORKED AT HMV. REPAIRED TAB PER M/M 57-13-00.SDR DL72E953906Angle · crackedDURING A-1 LETTER CHECK, FOUND 2 INCH CRACK NR 2 L/E SLAT COVE SKIN ATTACH ANGLE AT O/B STOP PAD. REPAIRED PER M/M 57-54-0.SDR DL72E953905Angle · crackedDURING A-1 LETTER CHECK, FOUND .25 INCH CRACK NR 7 L/E SLAT COVE SKIN ATTACH ANGLE AT I/B STOP PAD. REPAIRED PER M/M 57-54-0.SDR DL72W953887Door · crackedAFT FRAME SECTION CRACKED AT AFT TORQUE TUBE CRANK ARM CUTOUT OF C-1 DOOR. REPAIRED PER SRM 51-40-3.SDR DL72E954067Stringer · crackedAT HMV, FOUND STRINGER CRACKED VERTICAL STAB INTERIOR STR 8R LOC IN 5TH BAY UP FROM ACCESS HOLE. REPAIRED PER M/M 55-30-00 FIG 803.SDR DL72E954024Skin · crackedAT HMV, FOUND SKIN CRACKED NR 2 ENG INLET AT 3 O'CLOCK POS, 10 INCHES AFT OF LIP. FABRICATED AND INSTALLED NEW REPAIR PER MM 54-30-0 PG 801.SDR DL72E954020Skin · crackedAT HMV, FOUND .375 CRACK AT AFT INBD CORNER OF PNEU AIR CONNECTION ACCESS DOOR CUOUT. REPAIRED PER MM 53-30-0 PG 803.SDR DL72E954017Web · crackedAT HMV, FOUND .5 INCH CRACK IN LT TORQUE BOX WEB IN 48 SECT STA 1223 AT UPPER RIVET ROW. FABRICATED AND INSTALLED REPAIR PER MM 53-11-0 PG 833.SDR DL72E954016Web · crackedAT HMV, FOUND .5 INCH CRACK IN WEB AT STA 1303 RT SIDE ABOVE S-DUCT. FABRICATED AND INSTALLED DOUBLER REPAIR PER SRM 53-10-4 FIG 17.SDR DL72E954015Web · crackedAT HMV, FOUND .5 INCH CRACK IN WEB AT STA 1303 LT ABOVE S-DUCT. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 53-10-4 FIG 17.SDR DL72E953975Stringer · crackedSTRINGER CRACKED VERT STAB INTERIOR STR 8R CRACKED, LOCATED IN 3RD BAY UP FROM ACCESS HOLE. WORKED AT HMV, REPAIRED PER M/M 55-30-00.SDR DL72E953967Web · crackedWORKED AT HMV. PERFORM PERMANENT REPAIR, CRACK STA 913.5 LT, PER M/M 53-11-00, PG 816. REMOVED AND INSTALLED REPAIR PER M/M 53-11-00.
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