Boeing 717-200
Service difficulty reports · 18,771
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 = '717200' 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 = '717200' 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 DALA2016111508809Access Panel · corrodedCORROSION ON FUEL ACCESS PANEL ON COUNTERSINK 520DT ON LT WING. THE ACCESS PANEL WAS REPLACED IAW SRM 57-10-01.SDR DALA2016111508808Access Panel · corrodedCORROSION ON FUEL ACCESS PANEL ON SETTLEMENT AREA AND COUNTERSINK 520 CT AT RT WING. THE ACCESS PANEL REPLACED IAW SRM 57-10-01.SDR DALA2016111408796Lens · looseTHE PILOT DISCOVERED THAT THE MAIN CABIN DOOR EMERGENCY EXIT SIGN HAD A LOOSE LENS/COVER. MAINTENANCE RE-ATTACHED THE LENS/COVER AND THE OPERATIONAL CHECK WAS GOOD.SDR DALA2016111408747Battery Pack · dischargedDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPERATIONAL CHECK WAS GOOD.SDR DALA2016111308745Power Supply · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT SEATS 1B & 1C IN THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.SDR DALA2016111408744Splice · damagedAFT SILL SPLICE IS CORRODED AND BENT. REMOVED AND REPLACED THE SILL SPLICE IAW SRM 53-00-00 FIG 103 AND DWG 5910142 REV DJ.SDR DALA2016111408743Cusp Web · crackedCRACKED CUSP WEB BETWEEN BS 1002 AND 1020, RBL 54 TO 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55 REPAIR 4 FIG. 216. AND 51-41-05.SDR DALA2016111408795Engine · making metalTHE FLIGHT CREW DIVERTED THE AIRCRAFT TO JFK AFTER THE NR 1 ENGINE EXPERIENCED A STALL DURING INITIAL CLIMBOUT AND WAS SHUTDOWN. MAINTENANCE FOUND METAL IN THE TAILPIPE AND HAS REPLACED THE ENGINE.SDR DALA2016111408793Beam · crackedCRACK AT BEAM NR 6 ON FWD PASSENGER DOOR L1. BEAM NR 6 ON FWD PASSENGER DOOR WAS REPAIRED PER ER/A 551749-14 REV ORIGINAL AND ETI-17-16-156 REV ORIGINAL.SDR DALA2016111208742Vane · dentedSEVERAL DENTS ON AFT MOVABLE FLAP VANE ON THE LT WING. THE FLAP VANE WAS REPAIRED IAW SRM 57-53-01 REP.1 PARAGRAPH 4.SDR DALA2016111508794Seat Track · corrodedCORROSION ON UPPER SURFACE OF LT CENTER SEAT TRACK, AROUND FASTENER HOLES AT STA 1026 AND STA 1057 LEFT AFT LAV AREA. CORROSION ON UPPER SURFACE LT CENTER SEAT TRACK STA 1026-1057 BLENDED IAW SRM 53-00-00 FIG 103 ORIGINAL THICKNESS 0.080, 0.030 FOUND REMAININGSDR DALA2016111408746Battery Pack · dischargedDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPERATIONAL CHECK WAS GOOD.SDR DALA2016111208741Skin · crackedCRACKED FUSELAGE SKIN BS 1133 BETWEEN LONGERONS 2-3L. THE SKIN WAS REPAIRED IAW ETI-17-16-139 REV. 3 AND ER/A 551722-14AD REV. ORIGINAL.SDR DALA2016111208740Channel · crackedCRACKED FWD CHANNEL OF THE LT MLG DOOR CUTOUT BS 764 AT LT WW AREA. THE CHANNEL WAS REMOVED PER B-717 SRM 51-41-02. A NEW CHANNEL WAS DRILLING IAW SRM 51-40-08. THE CHANNEL WAS TREATED AND PAINTED IAW SRM B717 51-10-04 PART 15 & 21. THE CHANNEL WAS INSTALLSDR DALA2016111108739Cargo Track · corrodedCORROSION ON LT CARGO TRACK BETWEEN BS 899 TO 813 AT AFT CARGO BAY. THE DAMAGE SECTION WAS REPLACED IAW SRM 53-20-51 FIG 1.SDR DALA2016111108715Seat Track · damagedLT INBOARD SEAT TRACK HAS MULTIPLE AREAS OF GOUGES AND CORROSION FROM STA 856 TO STA 956 (AREAS MARKED IN RED). REMOVED CORROSION AND GOUGES FROM SEAT TRACK LT IB STA 856-956. ORIGINAL THICKNESS .115" REMOVED .025" REMAINING .090" SEAT TRACK OUT OF LIMITS. REPSDR DALA2016111108713Channel · crackedCRACKED CHANNEL ON FLOOR PANEL 222AFF AND 222AF, ALSO CRACKED WEB ON FLOOR PANEL 222XF AND CRACK ON STRAP ON FLOOR PANEL 223EF (S/N 00242). CRACKS ON FLOOR PANELS 222AFF, 222AF, 222XF AND 223EF WERE REPAIRED PER SRM 53-20-50 REPAIR 5, 53-00-00 REPAIR 1, AND 51SDR DALA2016111108712Cusp Web · crackedDURING CORROSION REMOVAL CRACK WAS FOUND AT CUSP WEB STA Y=660 X=60. IN REF CARD 00278. (S/N 00525). CUSP WEB WAS REPAIRED PER SRM 53-00-55 FIG 126 HFEC WAS ACCOMPLISHED AND NO CRACKS WAS FOUND AFTER CUT OUT PER NDT SPM 06-10-01.001.SDR DALA2016111108711Angle · crackedCRACK ON ANGLES 2EAS AT AFT PASSENGER EMERGENCY EXIT DOOR JAMB LT SIDE LOWER AND MIDDLE STOP AREA. (S/N 00506) FITTINGS WERE REPLACED PER SRM 51-41-02 AND 51-41-01.SDR DALA2016111108710Fitting · crackedCRACKED TEE AND CLIP AT FWD CARGO DOOR LOWER ANGLE BEAM INTERNAL STRUCTURE STA Y=410 APPROX. TEE AND CLIP WERE REPLACED PER SRM 51-41-01, 51-41-02, 51-41-05, AND DPS 4.710-3.SDR DALA2016111108709Skin · crackedCRACK IN SKIN AT TOP FASTENER AT STA 1152 JUST BELOW DORSAL FIN ON RIGHT SIDE. REPAIRED SKIN CRACK AT STA 1152 RT IAW ER/A 549635-14 REV 0.SDR DALA2016111108708Skin · crackedCRACK IN SKIN AT TOP FASTENER AT STA 1152 JUST BELOW DORSAL FIN ON LEFT SIDE. REPAIRED SKIN CRACK AT STA 1152 L/H IAW ERA 549634-14 REV 0.SDR DALA2016111108707Fitting · crackedCRACKED FRAME CLIP STA Y 1037 BTW LONG 16-17R AT RT AFT LAVATORY AREA. CLIP WAS REPAIRED PER ETI-17-16-145 REV 1 AND ER/A 551734-14 REV ORIG.SDR DALA2016111108706Fitting · crackedCRACKED FRAME CLIP STA Y=1037 LONG 16L TO 17L AT W2. CLIP WAS REPAIRED PER ETI-17-16-145 REV 1 AND ER/A 551734-14 REV ORIG.SDR DALA2016111108705Fitting · crackedCRACKED FITTING AT LT AFT OVERWING EMERGENCY EXIT DOOR BEAM 1 FWD EDGE. CLIP WAS REPLACED AND INSTALLED PER SRM 51-41-02, 51-41-05, AND DRAWING 9957735 REV G.SDR DALA2016111108704Fitting · crackedCRACKED CLIPS AT Z=41.375 STA 196.8 AND STA 172.5 ON FWD GALLEY DOOR. CLIPS WERE REPLACED PER SRM 51-41-02, 51-41-05, AND DRAWING 9911581 REV U.SDR DALA2016111108703Frame · crackedCRACKED FRAMES STA 680, 696, 715 BTW LONG 28/25 LT AT KEEL BEAM AREA. FRAMES WERE REPAIRED PER SRM 51-70-11 REPAIR 1, 51-41-05, 51-41-02, AND 51-10-04 PAR 37. HFEC INSPECTION WAS ACCOMPLISHED AND NO CRACKS WERE FOUND AFTER THE REMOVED DAMAGE FRAME Y=696 LT PERSDR DALA2016111108714Seat Track · corrodedCORROSION ON THE F/O O/B SEAT TRACK. SEAT TRACK FOUND TO BE BEYOND LIMITS. REPLACED WITH NEW SEAT TRACK. INSTALLED NEW SEAT TRACK IAW SRM 51-41-01.SDR DALA2016111008443Shear Tie · crackedFRAME SHEAR TIE CRACKED BS 1152 STRINGERS 2R AND 2L. REPLACED THE SHEAR TIE IAW SRM 51-41-05.SDR DALA2016111008442Cargo Track · corrodedCORROSION ON RT CARGO TRACK BS 899 - 1022 IN AFT CARGO BAY . THE CARGO TRACK WAS REPLACED IAW SRM 53-20-51 FIG 1.SDR DALA2016111008441Cargo Track · corrodedCORROSION ON THE LEFT CARGO TRACK BS 899 - 1022. THE CARGO TRACK WAS REPLACED IAW SRM 53-20-51 FIG 1.SDR DALA2016111008440Pan · crackedCRACK ON PAN AT BS 170 AND Z 11.063 ON FWD R1 SERVICE DOOR. HFEC INSPECTION WAS ACCOMPLISHED AND A CRACK OF 0.312" WAS FOUND IAW NDTSPM 06-10-01. THE CRACK WAS STOP DRILL IAW SRM 52-00-00 FIG. 202. NO CRACKS FOUND AFTER STOP DRILL, IAW NDTSPM 06-10-01 .001SDR DALA2016111008439Skin · bentFWD LOWER CORNER OF DOOR SKIN BENT. CUT OUT DAMAGED AREA IAW SRM 52-00-01 FIG 202, FABRICATED REPAIR DOUBLER AND REPAIR FILLER IAW SRM 52-00-01 REPAIR 8 AND INSTALLED IAW SRM 52-00-01 REPAIR 8.SDR DALA2016111008438Frame · crackedCRACKED FRAMES BS 680 BETWEEN LONGERON 25-28R. THE FRAME WAS REPAIRED IAW SRM 51-70-11 REPAIR 1, 51-41-05, 51-41-02, AND 51-10-04 PAR 37.SDR DALA2016111008437Seat Track · corrodedRIGHT INBOARD SEAT TRACK IS CORRODED ON TOP FORWARD END. FOUND TO BE OUT OF LIMITS IAW SRM 53-20-52. REPLACED THE SEAT TRACK IAW SRM 53-20-52 REPAIR 5.SDR DALA2016111008436Frame · crackedCRACKED FRAME ANGLE BS 1022 BETWEEN LONGERON 13 & 14L, REPLACED IAW SRM 51-41-02, 51-41-05 AND DRAWING 9912243 REV JS.SDR DALA2016111008435Frame · crackedCRACKED FRAME BS 1037 LONGERON 17L. THE FRAME WAS REPAIRED IAW SRM 53-20-07 FIG 201 REPAIR 4.SDR DALA2016110908367Power Supply · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS IN THE TAIL COMPARTMENT INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND THE LIGHTS RETURNED TO NORMAL OPERATIONAL CONDITION.SDR DALA2016110908365Access Panel · crackedRIGHT WING FUEL ACCESS PANEL 620MB FOUND CRACKED. THE ACCESS PANEL WAS REPLACED, NO LEAK WAS FOUND.SDR DALA2016110908364Skin · damagedSEVERAL FASTENER HOLES OF THE VERTICAL STABILIZER LEADING EDGE STRUCTURE EXHIBIT EVIDENCE OF DISTRESS AT SPLICE STATION ZFS-52.267 IAW JC 5530-01048-01. REPAIRED IAW DRAWING SG95550001 AND WORK CARD 5530-01048-03.SDR DALA2016110908363Floor Panel · damagedDAMAGED FLOOR PANEL. FLOOR PANEL REPLACED IAW DWG 9936639 REV: P.SDR DALA2016110808338Sign · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGN FOR THE AFT RIGHT OVERWING HATCH WAS INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.SDR DALA2016110808337Structure · crackedCRACK ON GROUND CONDITIONED AIR ACCESS CUT OUT. REPLACED PER ETI-17-16-147 REV ORIGINAL, ER/A 551737-14 REV ORIGINAL, AND SRM 51-41-02 AND 51-41-08.SDR DALA2016110808336Longeron · corrodedCORROSION ON LONGERON 30 FROM STA Y=908-Y=993 AT AFT CARGO COMPARTMENT. SECTION LONGERON 30 FROM STA Y=905-993 WAS REPLACED PER SRM 51-41-01, SRM 51-41-02, SRM 51-41-05, AND SRM 53-20-05 FIG 201 REPAIR 1.SDR DALA2016110808335Longeron · corrodedCORROSION ON LONGERON 30 FROM STA Y=988 TO Y=1009 AT AFT CARGO COMPARTMENT. SECTION LONGERON 30 FROM STA Y=900 TO Y=1012 WAS REPLACED PER SRM 51-41-01, SRM 51-41-02, SRM 51-41-05, AND SRM 53-20-05 FIG 201 REPAIR 1.SDR DALA2016110808334Pan · crackedHIDDEN DAMAGE, CRACK ON INNER PAN STA Y=370 BTW BEAMS 1 AND 2 AT FWD CARGO COMPARTMENT DOOR. HFEC WAS ACCOMPLISHED ON CONFIRMED CRACK NDT SPM 06-10-01.001 IS 1.593". CRACK WAS STOPPED PER SRM 51-00-07 PAR 5-16 HFEC OK NO CRACKS AFTER STOP DRILL PER SRM 51-00SDR DALA2016110808333Angle · corrodedCORROSION ON ANGLES (2EA) STA Y=383 AND Y=415 FRONT OF LOWER DOOR JAMB PAN AT FWD CARGO COMPARTMENT. ANGLES (2EA) STA Y=383 AND Y=415 FRONT OF LOWER DOOR JAMB PAN AT FWD CARGO COMPARTMENT WERE REPLACED PER SRM 51-41-02 AND DWG 5910142 REV DJ.SDR DALA2016110708319Doubler · damaged2 EA 3/16TH DOUBLER ATTACHMENT FASTENER HOLES DAMAGED. COMPLIED WITH PRI 552498-14 REV 0 IAW ER/A 552498-14 REV ORG.SDR DALA2016110708316Floor Support · corrodedCORROSION ON FLOOR SUPPORT X=0 STA AND Y= 218 AT W1 AREA (S/N 00489). NEW SUPPORT FLOOR PANEL WAS INSTALLED PER SRM 51-41-02.SDR DALA2016110708315Window · crackedCRACKED UPPER FWD CORNER WINDOW BETWEEN BS 427 AND 446. REPAIRED IAW SRM 56-20-02 REPAIR 1 TYPE C FIG 203. HFEC INSPECTION WAS ACCOMPLISHED AND NO CRACKS WERE FOUND AFTER TRIM OUT IAW NDT SPM 06-10-01. 001. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 56-2
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