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 DALA2017052504209Lens · detachedL1 DOOR EXIT SIGN LENS DETACHED. SECURED THE LENS.SDR DALA2017052504208Window Frame · crackedCRACKS ON WINDOW PANE, BS 870. THE WINDOW PANE WAS REPAIRED IAW SRM 56-20-02 REPAIR 1.SDR DALA2017052404207Seat Track · corrodedSEAT TRACK AT BS 587 TO 656, LBL 17 HAS CORROSION IN SCREW HOLES. MECHANICALLY BLENDED CORROSION, AND FOUND TO BE OUT OF LIMITS IAW SRM 53-20-52-1A, FIG 101. THE SEAT TRACK WAS REPLACED WITH NEW.SDR DALA2017052304108Light · contaminatedOVERWING AISLE OVERHEAD EMERGENCY EXIT SIGN PARTIALLY OBSCURED. REMOVED DEBRIS FROM INSIDE BOTH LENS, OPS CHECKED GOOD.SDR DALA2017052304107Cusp Web · crackedON REMOVAL OF THE FIRST OFFICER`S OTBD SEAT TRACK, FOUND A CRACKED CUSP WEB FROM ATTACH FASTENER HOLE. REPAIRED THE CUSP WEB IAW SRM 53-00-00-2R, EX B, AND 51-41-02.SDR DALA2017052304106Skin · crackedLEFT FUSELAGE SKIN CRACKED, BS 1022, LONGERON 14L. REPAIRED SKIN IAW ER/A 555612-14, REV O.SDR DALA2017052304105Skin · crackedRIGHT FUSELAGE SKIN CRACKED, BS 1087, ABOVE LONGERON 14R. REPAIRED THE SKIN IAW ER/A 557984-14, REV OR.SDR DALA2017052304104Skin · crackedRIGHT FUSELAGE SKIN CRACKED, BS 1076, LONGERON 14R. REPAIRED THE SKIN IAW ER/A 557983-14, REV OR.SDR DALA2017052304103Skin · crackedRIGHT FUSELAGE SKIN CRACKED AT BS 1037, LONGERON 14R. REPAIRED THE SKIN IAW ER/A 555611-14, REV OR.SDR DALA2017052304102Door Frame · damagedFWD LOWER FUSELAGE, FWD CARGO DOOR FRAME, BS 408 TO 434.5, LONGERON 18R, UPPER SILL, LOWER CUSP WEB PANEL. REPAIRED IAW SRM 53-00-55-2R-4 .SDR DALA2017052304101Frame · corrodedCORROSION AT BS 974 FRAME FWD SIDE LONGERON 29L - 29R. PERFORMED FRAME REPAIR IAW SRM 53-20-07-2R-2.SDR DALA2017052104055Battery · dischargedEMERGENCY EXIT SIGN IN CEILING FORWARD OF 1ST CLASS IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY IN B5-259 POWER PACK REF AMM 33-51. OPERATIONAL CHECK IS GOOD.SDR DALA2017052104056Battery Pack · dischargedTHE OVERWING EMERGENCY EXIT LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK PER AMM 33-50. OPERATIONAL CHECK IS GOOD.SDR DALA2017051803979Charger · inoperativeEMERGENCY EXIT SIGNS AT THE AFT OVER WING EXITS INOPERATIVE. REPLACED BATTERY CHARGER PB5-230. CHECKS GOOD REF AMM 33-51.SDR DALA2017051803978Power Supply · inoperativeON SERVICE CHECK FOUND FORWARD CABIN CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY B5-227 AND BATTERY PACK REF AMM 33-51. OPERATIONAL CHECK IS GOOD.SDR HALA2017051500119Stick Shaker · malfunctionedSTICK PUSHER FAILED. PERFORMED FCC 1 & 2 RTS AND SYSTEM TEST. NO FAULTS.SDR DALA2017051603896Lens · looseEMERGENCY EXIT COVER DIFFUSER LENS LOOSE AT LOCATION 602. SECURED THE LOOSE LENS. CHECKED OK.SDR DALA2017051603895Battery Pack · inoperativeDURING A SERVICE CHECK, OVERWING EMERGENCY EXIT LIGHTS WOULD NOT STAY ILLUMINATED. R & R THE BATTERY PACK AT 22CDE IAW AMM 33-51. OPS CHECKED GOOD.SDR DALA2017051503867Battery Pack · dischargedEMERG ESCAPE LIGHT INOP BY C1 DOOR. REPLACED BATTERY PACK B5-235 REF AMM 33-51. OPS CHECK GOOD. OK FOR SERVICE.SDR DALA2017051503897Fan · failedF/A REPORTED STRONG ODOR IN AFT CABIN DURING APPROACH. FOUND GASPER VENT FAN INOPERATIVE AND CAUSING A BURNING ODOR. COMPLIED WITH NO GO ODI PREV. 2172. CABIN ODOR WAS DETERMINED TO BE ELECTRICAL NOT APU, PERFORMED A DUCT BURNOUT & REPLACED THE COALESCER BSDR DALA2017051503893Door Frame · corrodedAFT CARGO BAY HAD CORROSION ON DOOR FRAME PAN. A REPAIR WAS ACCOMPLISHED IAW ETI 17-17-062, REV 3 AND ER/A 558101-14, REV ORIGINAL.SDR DALA2017051403866Repair · damagedELONGATED SEVERAL HOLES ON PREVIOUS REPAIR DOUBLER AT VERTICAL STABILIZER LE SPLICE AT STA ZFS=52.267. REPAIR WAS ACCOMPLISHED PER ETI-17-17-060 REV 3 AND ER/A 535894-14AD REV A.SDR DALA2017051503868Cover · looseEMERGENCY EXIT SIGN COVER LOOSE, LOCATION 604. ADJUSTED EXIT SIGN, OK FOR SVC.SDR DALA2017051303865Skin · crackedCRACK ON PRODUCTION DOUBLER UPPER SKIN STA Y=1176 CANT BTW LONG 1 TO 3 RT AFT ACCESSORY COMPARTMENT. REPAIR WAS ACCOMPLISHED PER ETI-17-17-052 REV ORIGINAL AND ER/A 558094-14 REV ORIGINAL.SDR DALA2017051303864Cusp Web · corrodedRT STA 389 UNDERSIDE OF CUSP WEB HAS CORROSION. REPAIRED DAMAGED CUSP WEB IAW SRM 53-00-55-2R-4. TREAT, PRIMED, TOPCOATED, AND INSTALLED REPAIR DOUBLERS IAW SRM 51-41-05, 53-00-55-2R-4, AND AMM 51-10-00-370-803.SDR DALA2017051303863Cusp Web · corrodedRT STA 434 CUSP WEB HAS CORROSION ON TOP AND BOTTOM. REPAIRED DAMAGED CUSP WEB IAW SRM 53-00-55-2R-4. TREATED, PRIMED, TOPCOATED, AND INSTALLED REPAIR DOUBLERS IAW SRM 51-41-05, 53-055-2R-4, AND AMM 51-10-00 370-803.SDR DALA2017051303862Cusp Web · corrodedTHE RT CUSP WEB AT STA 737-756, RBL 55 HAS CORROSION AROUND THE UNDERSIDE OF LIGHTENING HOLE(S). BLENDED CUSP WEB AT STA 737-756 ORIGINAL THICKNESS .040 REMAINING THICKNESS .028. FOUND TO BE OUT OF LIMITS. INSTALLED DOUBLER IAW SRM 53-00-55 REPAIR 4.SDR DALA2017051203816Battery · dischargedAFT CABIN OVERHEAD EMERGENCY LIGHTS INOP. REPLACED EMERGENCY BATTERY AND BATTERY POWER SUPPLY PER AMM 33-51. OPS CHKS GOOD. NO FAULTS NOTED. OK FOR SVC.SDR DALA2017051203815Skin · crackedCRACKS ON PRODUCTION DOUBLER UPPER SKIN STA Y=1176 CANT BTW LONGS 3L TO 3R AFT ACCESSORY COMPARTMENT. CRACK ON PRODUCTION DOUBLER UPPER SKIN STA Y=1176 CANT BTW LONGS 1 TO 3 LT AFT ACCESSORY WAS REPAIRED PER SRM 53-30-08-2R PROCEDURE 10 REPAIR 10. HFEC INSPECTSDR DALA2017051203814Frame · crackedCRACK ON MAIN FRAME AFT LT STA 1022 LONG 7L. CRACK ON MAIN FRAME AFT LT STA 1022 LONG 7L WAS REPAIRED PER ETI-17-17-052 REV. ORIGINAL AND ER/A 558094-14 REV ORIGINAL.SDR DALA2017051203813Door · wornWEAR ON INNER SURFACE OF LT MLG STRUT DOOR. RT MLG DOOR STRUT WAS REPAIRED IN ACCORDING ETI. 17-17-060 REV ORG AND ER/A 558089-14 REV ORIG.SDR DALA2017051103808Floor Support · corrodedAFT WET AREA STA 1022-1053, LBL 46 FLOOR SUPPORT HAS CORROSION IN MULTIPLE AREAS INCLUDING OUTBD FLANGE. REMOVED CORROSION BY BLENDING ON FLOOR SUPPORT AT LBL46 STA 1041 .025" MATERIAL REMOVED .055" REMAINING .080" ORIGINAL THICKNESS OUT OF LIMITS IAW SRM 53-0SDR DALA2017051103807Seat Track · corrodedRIGHT INBOARD SEAT TRACK RBL 22, BS 200 - 256, HAS AREAS OF CORROSION. BLENDED THE SEAT TRACK, AND FOUND AREAS OUT OF LIMITS. A NEW SEAT TRACK WAS INSTALLED IAW SRM 53-20-52-2R.SDR DALA2017051103806Longeron Splice · corrodedCORROSION AT BS 891 - 906, LONGERON 30 SPLICE FITTING. REMOVED AND REPLACED THE DAMAGED LONGERON SPLICE IAW SRM 51-41-01, 51-41-05, AND DRAWING 5924878.SDR DALA2017051103764Lens · unsecureEMERGENCY EXIT DIFFUSER LENS FOUND UNSECURE. SECURED THE LENS.SDR DALA2017051103763Lens · missingAFT EMERGENCY LIGHT LENS MISSING ABOVE AFT LAVATORY DOOR. INSTALLED A NEW LENS.SDR DALA2017051103761Bulkhead · gougedAFT CABIN PRESSURE BULKHEAD EMERGENCY EXIT DOOR INTERNAL STRUCTURE IS GOUGED IN SEVERAL AREAS AT LOWER RT SECTION WHERE FLIGHT ATTNANTS SEAT IS MOUNTED. REPAIRED IAW SRM 52-10-02-2R, OPTION 2.SDR DALA2017051103760Cusp Web · corrodedCORROSION ON TOP AND BOTTOM SIDE OF LEFT CUSP WEB BETWEEN BS 737-756, LBL 60. REPAIRED THE CUSP WEB IAW SRM 53-00-55-4R-2, REPAIR 4.SDR DALA2017051103759Longeron · corrodedCORROSION AT BS 954 - 908, L30. BLENDED THE CORROSION AND FOUND TO BE OUT OF LIMITS AT STA 931. REPAIR THE AREA. TREATED, PRIMED, TOP COATED, INSTALLED FASTENERS, IAW SRM 51-41-02, 53-00-00, FIG 103, 53-00-05-2R-3, AND AMM 51-10-00-370-803.SDR DALA2017051103758Cusp Web · crackedCRACKS AROUND RIVET HEADS ON LT SIDE CUSP WEB BS 716, LBL 44 - 54. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R4, REPAIR 4.SDR DALA2017051203810Frame · crackedFWD LT STA 1022 FRAME FORMER CRACKED BETWEEN LONGERON 5L-6L. REPAIRED FWD LT STA 1022 FRAME FORMER BETWEEN 5L-6L IAW SRM 53-00-06-2R REPAIR 3.SDR DALA2017051003726Frame · corrodedCORROSION ON FRAME ANGLE BS 974 BETWEEN LONGERONS 24L - 29R IN THE AFT CARGO BAY. THE FRAME ANGLE WAS REPLACED IAW SRM 53-20-07-01-3, AND DWG 9958215, REV AM.SDR DALA2017051203861Cusp Web · corrodedCUSP WEB LT AT STA 427-446 CORRODED. REPAIRED LT CUSP WEB AT STA 427-446 IAW SRM 53-00-55-2R-4. BLENDED CORROSION ON WEB. NOMINAL .020 REMOVED .005 REMAINING .015. OUT OF LIMITS IAW SRM 53-00-55-1A-1.SDR DALA2017051103762Seat Track · corrodedCORROSION ON THE F/O'S OTBD SEAT TRACK. CORROSION ON SEAT TRACK FOUND TO BE BEYOND DWG TOLERANCE OF .015 WITH 50% MATERIAL LOSS IAW BOEING DWG 5971207. REPLACED THE SEAT TRACK IAW AMM 53-22-01.SDR DALA2017050903674Cover · damagedEMERGENCY EXIT COVER DIFFUSER LENS DAMAGED. R & R THE COVER. OK FOR SERVICE.SDR DALA2017050903673Door Frame · crackedCRACKED DOOR FRAME BEAM LT SIDE OF NOSE GEAR WHEEL WELL NEAR BS 69.550. REPAIRED IAW ETI-17-17-057, REV 3, AND ER/A 558076-14, REV ORIGINAL.SDR DALA2017050703611Hinge · wornFREE PLAY ON AFT HINGE AT FWD CARGO DOOR. REPAIRED AIW ER/A 558081-14, REV ORIGINAL.SDR DALA2017050703610Door Frame · crackedCRACK DOOR JAMB BEAM RT SIDE OF NOSE GEAR WHEEL WELL NEAR STA Y=69.550. REPAIR WAS ACCOMPLISHED PER SRM 53-10-14-2R.SDR DALA2017051203812Seat Track · gougedRT I/B SEAT TRACK GOUGED STA 890. GOUGED AREA ON SEAT TRACK WAS OUT OF LIMITS ORIG 0.115" REMAINING 0.090" IAW SRM 53-20-52-1A. REPLACED RT IB SEAT TRACK FROM STA 822 TO 897 IAW SRM 53-20-52-2R-5 FIG 201.SDR DALA2017050903725Cargo Track · corrodedCORROSION BS 995 - 1022, RT CARGO TRACK, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00-1A, FIG 103. REPLACED THE CARGO TRACK IAW SRM 51-41-01.
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