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 DALA2017100207219Door Frame · crackedL1 DOOR FRAME CRACKED. THE DOOR FRAME WAS REPAIRED AND REFURBISHED IAW ER/A 534742-14 REV. ORIGINAL.SDR DALA2017100207218Panel · crackedCRACK ON TRAILING EDGE PANEL XRS 164, LT WING UPPER SURFACE. THE PANEL WAS REPAIRED IAW SRM 57-00-00-2R-2.SDR DALA2017092907178Structure · wornWORN ON LOWER RT CORNER INTERNAL STRUCTURE AT THE AFT EMERGENCY EXIT BULKHEAD DOOR. DAMAGED AREA WAS REPAIRED IAW SRM 52-10-02-2R, 16, FIG 201.SDR DALA2017092907177Doubler · corrodedCORROSION ON PREVIOUS REPAIR DOUBLER ON THE AFT CARGO DOOR FRAME BS 954. THE REPAIR DOUBLER WAS REPLACED IAW SRM 53-20-15-2R-7, FIG 201.SDR DALA2017092807137Beam · crackedCRACKED RT NOSE LANDING GEAR BEAM. REPAIRED IAW SRM 53-10-14-2R-2.SDR DALA2017092807136Beam · crackedCRACKED LEFT NOSE LANDING GEAR BEAM. REPAIRED IAW SRM 53-10-14-2R-2.SDR DALA2017092807135Skin · crackedTWO CRACKS ON THE RT WING FIXED TRAILING EDGE PANEL UPPER AREA XRS 137. REPAIRED IAW SRM 57-00-00-2R-2.SDR DALA2017092807134Skin · crackedCRACK ON FUSELAGE SKIN AROUND AFT HINGE OF THE LT AFT NLG DOOR. THE SKIN WAS REPAIRED IAW SRM 53-10-01-2R-11.SDR DALA2019091005259Spar · crackedER/A 561912-14AD SECTION I ISSUED FOR CRACK REPAIR ON VERTICAL STABILIZER FRONT SPAR RT CHORD AND WEB. AD 2016-09-05 AFFECTED. ASSOCIATED ER/A 00-561912 ADDED FOR AC 9507. ASSOCIATED AA 5530-01048 ADDED FOR AC 9507. REF NEW LP 1262502FOR DTA, THIS LP TERMINATESDR DALA2017092707110Angle · crackedCRACKED ANGLE BELOW THE NR 1 BEAM AFT EDGE ON FWD SERVICE DOOR. REPLACED IAW SRM 51-41-05, AND DRAWING 9911579, REV L.SDR DALA2017092707109Beam · crackedCRACKED NR 1 BEAM, AFT EDGE ON THE L1 DOOR. THE BEAM WAS REPAIRED IAW SRM 52-10-02, FIG 201, REPAIR 7.SDR DALA2017092707108Spar Cap · crackedVERTICAL STABILIZER LEADING EDGE SPAR CAP WEB CRACKED. REPAIRED REF ER/A 561912-14AD, REV ORIGINAL.SDR DALA2017092707107Spar · crackedVERTICAL STAB, FOUND RIGHT SPAR CRACKED AT ZFS=52.267 REPAIRED IAW ER/A 561912-14AD REV ORIGINAL.SDR DALA2017092707106Spar Cap · damagedVERTICAL STABILIZER RIGHT FRONT SPAR CAP FORWARD FLANGE HAS CRACK INDICATIONS IN FIVE HOLES BELOW THE LEADING EDGE SKIN SPLICE ZFS=52.267. REPAIRED ER/A 561912-14AD, REV ORIGINAL.SDR DALA2017092707105Structure · damagedVERTICAL STAB LEFT AND RIGHT SIDE ZFS 52.267 UPPER TWO ROWS FASTENERS 85 LOOSE AND ELONGATED HOLES. COMPLIED WITH PRI 560974-14AD REV. 0, REV. 1, AND REV. 2. REPAIRED REF ER/A 560974-14AD REV ORIG. COMPLIED WITH ER/A 560974-14AD REV A.SDR DALA2017092607090Power Supply · inoperativeOVERWING EMERGENCY EVACUATION LIGHTS WERE INOPERATIVE. REPLACED THE OVERWING EMERGENCY EVACUATION LIGHT POWER SUPPLY AND BATTERY IAW AMM 33-51. OPS CHECKED NORMAL.SDR DALA2017092507089Battery Pack · inoperativeFOUND THE AFT EMERGENCY LIGHTS INOPERATIVE. TROUBLESHOT IAW FIM 33-50-00 810-801. FOUND EMERGENCY FLOOR LIGHTS POWER SUPPLY BATTERY B5-119 INOPERATIVE. REPLACED THE BATTERY PER B717 AMM 33-51-03. OPS CHECKED OK. AIRCRAFT IS OK FOR SERVICE.SDR DALA2017092507088Sign · looseCREW REPORTED THE CEILING EXIT SIGN AT ROW 1 WAS LOOSE. SECURED THE SIGN.SDR DALA2017092507087Floor Support · corrodedCORROSION ON FLOOR SUPPORT BETWEEN BS 180 - 200, LBL. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-41-02-0G, AND SRM 51-41-05-0G.SDR DALA2017092207033Lens · detachedEMERGENCY EXIT SIGN LENS FELL OFF. REINSTALLED THE LENS ON THE EMERGENCY EXIT SIGN AT ROW 20. OPS NORMAL IAW AMM 33-51.SDR DALA2017092207032Power Supply · inoperativeAFT EMERGENCY DOOR EXIT SIGN IS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY BATTERY POWER SUPPLY IAW AMM 33-51.SDR DALA2017092207031Attach Fitting · corrodedCORROSION ON GALLEY FLOOR AT GALLEY SERVICE DOOR AFT GIRT BAR LATCH ATTACH FITTING. . REPLACED THE GIRT BAR ATTACH FITTING IAW SRM 51-00-07.SDR DALA2017092207030Fitting · corrodedCORROSION ON GALLEY FLOOR AT GALLEY SERVICE DOOR FWD. GIRT BAR LATCH ATTACH FITTING. REMOVED AND REPLACED THE GIRT BAR ATTACH FITTING IAW SRM 51-00-07.SDR DALA2017092207029Floor Support · corrodedCORROSION 0N GALLEY FLOOR SUPPORT ANGLE LBL 52 BETWEEN STA. 168 AND 193. M. NR 000-0001:5300-0116/029 00165 REMOVED CORROSION REF B717 SRM 53-00-00-1A. INSTALLED NEW GALLEY FLOOR SUPPORT. (LP #0222753)SDR DALA2017092207028Attach Angle · corrodedCORROSION ON GALLEY FLOOD ATTACH ANGLE LBL 44 BETWEEN BS 172 AND 199. REMOVED CORROSION IAW STM 53-00-00-1A. INSTALLED A NEW GALLEY FLOOR ATTACH ANGLE.SDR DALA2017092207027Structure · corrodedCORROSION ON PRINTER ENCLOSURE IN THE COCKPIT. THE DAMAGED AREA FOR THE PRINTER ENCLOSURE WAS FABRICATED AND REPLACED IAW DWG 5991370, REV ORIGINAL, AND SRM 51-41-02.SDR DALA2017092106998Lens · unsecureEMERGENCY EXIT DIFFUSER LENS UNSECURE. SECURED THE LENS IAW AMM 33-51. OPS CHECKED NORMAL. OK FOR SERVICE.SDR DALA2017092106999Lens · unsecureEMERGENCY EXIT DIFFUSER LENS UNSECURE. SIGN COVER SECURED. OK FOR SERVICE.SDR DALA2017092106997Angle · crackedCRACKED ANGLE ON THE RH AFT ENGINE PYLON SUPPORT BULKHEAD BS 1022, LONGERON 7R. REPAIRED IAW ETI 17-17-164, REV ORIGINAL, AND ER/A 560925-14, REV ORIGINAL.SDR DALA2017091806960Lens · detachedEMERGENCY EXIT SIGN IS MISSING THE LENS. FOUND EXIT SIGN LENS, INSPECTED THE LENS, NO DAMAGE NOTED AND INSTALLED.SDR DALA2017091906959Skin · crackedCRACKED FUSELAGE SKIN BS 1022, BETWEEN LONGERONS 13R TO 14R. REPAIRED IAW ETI-17-17-148, REV 2, AND ER/A 560890-14, REV ORIGINAL.SDR DALA2017091906958Skin · crackedCRACKED FUSELAGE SKIN BS 1022, BETWEEN LONGERONS 13L TO 14L. REPAIRED IAW ETI-17-17-149, REV 2, AND ER/A 560891-14, REV ORIGINAL.SDR DALA2017091806934Lens · missingR1 DOOR EMERGENCY LIGHT MISSING THE LENS. REPLACED THE LENS, CHECKED GOOD.SDR DALA2017091906979Lens · missingDURING SVC CHECK FOUND EMERGENCY LIGHT DIFFUSER LENS MISSING AT SEAT 12B. FWD TO NEF 33-51-02. REPLACED MISSING LENS COVER.SDR DALA2017091806931Longeron · crackedCRACKED LONGERON 3R, BS 1152. HFEC WAS ACCOMPLISHED IAW NDT SPM 06-10-01.001. THE CRACKS WERE CONFIRMED ON THE LONGERON. TRIMMED OUT AND NO CRACKS WERE FOUND NDT SPM 06-10-01.001. LONGERON WAS REPAIRED IAW SRM 53-00-05, REP 2.SDR DALA2017092507133Stud · corrodedCORROSION ON RT FLAP HINGE FITTING AROUND OF OUTBD LOWER STUD XW 251. RT CENTER FLAP HINGE FITTING, WING FLAP HINGE MOUNTING STUD WERE REPLACED IAW AMM 57-55-25 AND HYDRAULIC LINES AND ACTUATOR CYLINDER WERE REMOVED AND INSTALLED IAW AMM 27-55-03 AND LEAK ANSDR DALA2017091806932Charger · inoperativeAFT EMERGENCY LIGHT ON INTERMITTENTLY. ALL EMERGENCY LIGHTS FLASHED ON LOADING. FOUND B5-260 CHARGER INOPERATIVE. R & R IAW AMM 33-51. ALL CHECKED GOOD. OK FOR SERVICE.SDR DALA2017091706930Spar Cap · crackedCRACKED VERTICAL STABILIZER FRONT SPAR CAP LT SIDE BELOW ZFS=52.267. THE VERTICAL STAB FRONT SPAR CAP WAS REPAIRED IAW ER/A 560934-14AD, REV ORIGINAL AND ETI-17-17-169, REV 3.SDR DALA2017091706929Skin · crackedCRACK ON FUSELAGE SKIN BS 1037, LONGERON 14R. THE SKIN WAS REPAIRED IAW ER/A 560879-14, REV ORIGINAL, AND ETI-17-17-142, REV 6.SDR DALA2017091706928Fitting · crackedCRACKED FITTING ON THE LT FLAP INTERNAL STRUCTURE XCW 65. THE FITTING WAS REPLACED IAW SRM 51-41-02-0G, SRM 51-41-05-0G, AMM 20-00-02, AND AMM 20-50-01.SDR DALA2017091806933Cover · unsecureEMERGENCY EXIT SIGN COVER LOOSE. INSTALLED EXIT SIGN. OPS CHECKED GOOD.SDR DALA2017091606927Frame Angle · corrodedCORROSION ON FRAME ANGLE BS 927, BETWEEN LONGERONS 29L - 30L IN THE AFT CARGO BAY. REPAIRED IAW SRM 53-00-06-2R, REP 2.SDR DALA2017091606926Fitting · crackedCRACK ON MAIN FRAME WING TO FUSELAGE FITTING BS 661, LONGERON 22L. REPAIRED IAW ETI-17-17-155, REV ORIGINAL, AND ER/A 560940-14, REV ORIGINAL.SDR DALA2017091606925Door Frame · corrodedCORROSION ON DOOR FRAME WEB BS 200, LONGERON 18L. A REPAIR WAS ACCOMPLISHED IAW ETI-17-17-160, REV 3, AND ER/A 560920-14, REV ORIGINAL.SDR DALA2017091606924Frame · crackedCRACK ON FRAME BS 1225, 7 HRS POSITION. THE FRAME WAS REPAIRED IAW ETI17-17-165, REV ORIGINAL. AND ER/A 590926-14, REV ORIGINAL.SDR DALA2017091606923Pan · crackedCRACKS FOUND ON THE AFT CARGO DOOR INNER PAN AND OUTER PAN AROUND UPPER STOP. REPAIRED IAW ER/A 560875-14, REV ORIGINAL, AND ETI-17-17-140, REV 4.SDR DALA2017091506902Fitting · crackedCRACKED VERTICAL FITTING BS 663 RBL 22 Z=-12, THE FITTING WAS REPLACED IAW DWG 9910009-123, REV BB, AND SRM 51-41-05. LEAK CHECKED IAW AMM 28-00-00, NO LEAKS FOUND.SDR DALA2017091506922Skin · corrodedCORROSION THE UPPER SKIN BETWEEN BS 660 AND 756, LBL 40 AND 60. REPAIRED IAW ER/A 560894-14, REV ORIGINAL. AND ETI-17-17-151, REV 1.SDR DALA2017091506903Longeron · crackedCRACKED LONGERON 2R, BS 1133. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R, PROCEDURE 2. HFEC INSPECTION WAS ACCOMPLISHED, NO CRACKS WERE FOUND IAW NDT SPM 06-10-01.SDR DALA2017091506901Intercostal · crackedCRACKED INTERCOSTAL ON LT FLAP, XCW 65. THE INTERCOSTAL WAS REPLACED IAW SRM 51-41-05-0G, SRM 51-41-02-0G, AND DWG 9958001, REV U.
Back to Boeing 717-200