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 HALA2016030000072Skin · crackedA .2500" FUSELAGE SKIN CRACKED BETWEEN LONGERON 14R AND 15R AT BS 1096. INSTALLED EXTERNAL DOUBLER.SDR HALA2016030100064Landing Gear · malfunctionedON FIRST ATTEMPT, GEAR DID NOT COME DOWN. GEAR INDICATIONS ALL RED, ALSO ALL RED ON CONFIGURATION PAGE. 2ND ATTEMPT OK. COMPLIED WITH INSPECTION OF NLG AND MLGS AND SENSORS. COMPLIED WITH RETURN TO SERVICE TEST OF PROXIMITY SENSING ELECTRONIC UNIT. OPS CHECSDR DALA2016030201570Web · corrodedAFT PIT FORWARD DOOR CUTOUT THRESHOLD WEB CORRODED IN SEVERAL LOCATIONS BETWEEN STATIONS 947 AND 954. LONGERONS 26-25R MARKED. BLENDED OUT CORROSION ORIGINAL .040" REMAINING .028", LOSS .012". FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00, PG 105. FABRICATED SDR DALA2016102807820Angle · corrodedRIGHT WHEEL WELL FORWARD BULKHEAD UPPER ANGLE IS CORRODED 20 INCHES OUTBOARD OF INBOARD WHEEL WELL. REMOVED CORROSION. ROTO PEENED AND RESTORED FINISH IAW PIR ER/A 540747-14 REV O AND ER/A 540747-14 ORIGINAL.SDR DALA2016102807819Angle · corrodedLEFT WHEEL WELL FORWARD BULKHEAD UPPER ANGLE IS CORRODED 19 INCHES OUTBOARD OF INBOARD WHEEL WELL BULKHEAD. REMOVED CORROSION. ROTO PEENED AND RESTORED FINISH IAW ER/A 540747-14 ORIG. AND PRI ER/A 540747-14 REV O.SDR DALA2016102807818Angle · corrodedLEFT WHEEL WELL FORWARD BULKHEAD UPPER ANGLE IS CORRODED 30 INCHES OUTBOARD OF INBOARD WHEEL WELL BULHEAD. REMOVED CORROSION. ROTO PEENED AND RESTORED FINISH IAW PRI ER/A 540747-14 REV 0 AND ER/A 540747 ORIGINAL.SDR DALA2016030102572Cusp Web · corrodedCORROSION FOUND AT CUSP WEB SKIN APPROXIMATELY FROM BS 208 TO BS 215 AND RBL 56. INSTALLED EWIS PROTECTION IAW AMM 20-30-00, REMOVED CUSP WEB IAW SRM 51-40-02, DUE TO 100 PERCENT MATERIAL LOSS, LOCATED, AND DRILLED AND DEBURR NEW CUSP WEB IAW SRM 51-40-08. ALOSDR DALA2016030102571Support Fitting · crackedMAIN CABIN TANK BS 737, RBL 44. SEAT TRACK SUPPORT FITTING CRACKED. REMOVED CRACKED SEAT TRACK SUPPORT FITTING AT STR 737, RBL 44, IAW SRM 51-41-05. LOCATED, DRILLED, AND DEBURRED NEW SUPPORT IAW SRM 51-40-08. ALODINED AND PRIMED NEW HOLES IAW 51-10-04. INSSDR DALA2016030701684Floor Support · corrodedWEB FLOOR SUPPORT FWD OF R1 DOOR AND WATER LINE PAN IS CORRODED, M ON REPAIR RACK. BLEND & CHECK LIMITS. REF ORNRC 64480-0200-0140. CORRODED BEYOND LIMITS IAW SRM 53-00-00. REPLACED FLOOR SUPPORT MATCH DRILLED NEW FLOOR SUPPORT IAW SRM 51-40-08, PG 1 TO BE INSDR DALA2016030101538Strap · corrodedAFT CARGO STRAP AT BS 892, LONGERON 30 IS CORRODED NEAR FASTENER ON UPPER SURFACE. BLENDED OUT CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00, PG 105. FABRICATED NEW SPLICE ON WO 033609-1600-0006 INSTALLED IAW DWG 5919707.SDR DALA2016102807817Bulkhead · corrodedAFT CARGO BAY BILGE AREA BS 813 BETWEEN LONGERON 28 AND 29R BULKHEAD HAS CORROSION. REPAIRED IAW ER/A 540745-14 REV O.SDR DALA2016022901488Frame · crackedAFT CARGO DOOR INTERNAL STRUCTURE AFT FRAME CRACKED ABOVE CENTER STOP FITTING. STOP DRILLED CRACKS, REMOVED FASTENERS, REMOVED FILLER FROM PAN. VERIFIED MATERIAL FOR REPAIR DOUBLER ATAG 27991, CUT, FIT, LOCATED NEW DOUBLER & SHIMS IAW SRM 52-30-02 REPAIR 6. SDR DALA2016022901487Frame · crackedAFT CARGO DOOR INTERNAL STRUCTURE UPPER FWD CORNER FRAME CRACKED AT UPPER STOP FITTING. REMOVED DOOR SEAL, STOP DRILLED CRACKS, REMOVED FASTENER IN REPAIR AREA, REMOVED FILLER FROM PAN, VERIFIED MATERIAL FOR REPAIR DOUBLER ATAG A63804, CUT, TRIMED AND LOCATEDSDR DALA2016022901485Floor Panel · damagedFLOOR PANEL 222SF DAMAGED. FABRICATED NEW HAT CHANNEL IAW DWG NR 9952521, REV BB ID:1, FRAME 1 OF 1. TREATED & PRIMED NEW HAT CHANNEL IAW SRM 51-10-04, STEP 15 & 21. REPLACED NEW HAT CHANNEL TO FLOORBOARD IAW DWG 9952521, REV BB, ID: 1, FRAME 1 OF 1.SDR DALA2016022802570Support Fitting · crackedMAIN CABIN BS 737, LBL 44 SEAT TRACK SUPPORT FITTING CRACKED. REPLACED MAIN CABIN CENTER WING TANK BS 737, LBL 44 SEAT TRACK SUPPORT FITTING IAW SRM 51-41-02 AND SRM 51-41-05.SDR DALA2016022901537Slide · damagedINSPECTION DISCOVERED THAT THE EMERGENCY ESCAPE SLIDE IN THE TAILCONE WAS NO LONGER IN AN ACCEPTABLE CONFIGURATION. A MISRIGGED, IMPROPERLY MISSING BUSTLE CABLE CLIP FOR THE SLIDE COVER WOULD PREVENT PROPER DEPLOYMENT OF THE ESCAPE SYS AND IS NOT INCOMPLIANCE SDR DALA2016102807816Angle · corrodedLEFT WHEEL WELL FORWARD BULKHEAD UPPER ANGLE IS CORRODED 19 INCHES OUTBOARD OF INBOARD WHEEL WELL BULKHEAD. REMOVED CORROSION, ROTOR PEENED AND RESTORED FINISH IAW ER/A 540747-14 ORIGINAL AND PRI ER/A540747-14 REV 0.SDR DALA2016022701484Hinge Fitting · crackedAFT CARGO COMPARTMENT DOOR JAMB UPPER SILL FWD HINGE FITTING LOWER FWD AND AFT ATTACH CLIPS CRACKED. REMOVED OLD, FABRICATED NEW, TREAT, PRIMED, APPLIED TOP COAT, APPLIED CIC. INSTALLED NEW AFT CARGO COMPARTMENT DOOR JAMB UPPER SILL FWD HINGE FITTING LOWER FSDR DALA2016022701483Skin · crackedBS 1153, 3" INBD OF STR 3R, SKIN HAS .2500" CRACK AT SHEAR TIE FASTENER LOCATION. HFEC VERIFIED IAW NDT SPM 06-10-01. 001 PROCEDURE 1, REF: ORNRC 64480-0300-0006. REPAIRED DAMAGE AREA AT BS 1153 3" INBD OF STR 3R IAW ER/A 543583-14. AMDS CONTINUATION FORM PSDR DALA2016022701482Cusp Web · corrodedLEFT CUSP WEB BETWEEN BS 465-484 HAS 3 AREAS OF CORROSION. LEFT CUSP WEB, FS 465-484 HAS 3 AREAS OF CORROSION. REMOVED CORROSION MECHANICALLY. ORIGINAL "T" .020, LOSS OF .004, .016 REMAINING. FOUND TO BE OUT OF LIMITS. ACCESSED AREA TO BE REPAIRED. DRILLEDSDR DALA2016022701481Cusp Web · corrodedLEFT CUSP WEB BETWEEN BS 446-465 HAS 2 AREAS OF CORROSION. LEFT CUSP WEB, FS 446-FS 465, 2 AREAS CORROSION. REMOVED CORROSION MECHANICALLY. ORIGINAL "T" .020, LOSS OF .005, .015 REMAINING. FOUND TO BE OUT OF LIMITS. ACCESSED AREA TO BE REPAIRED. DRILLED &SDR DALA2016022601444Longeron · crackedLEFT PYLON APRON, FRAME BS 1076 UPPER LONGERON REPAIR CRACKED AT UPPER COWLING HINGE FITTING CUTOUT. INSTALLED FABED NEW DOUBLER FROM 2024-T3- .071 QQ-A- 250/S. 2024-T3 IS A PERMITTED SUBSTITUTION FOR 2024-T42 IAW SRM 51-30-08, FIG 1, TABLE A IAW SRM 54-50-02SDR DALA2016022601443Floorboard · damagedPASSENGER FLOORBOARD 222AFF CRACK IN MIDDLE OF PANEL VERFIED MATERIAL FOR NEW HAT CHANNEL A TAG A53914 FABRICATED NEW HAT CHANNEL IAW DWG 9952521, REV BB ID1 FRAME 1 OF 1. TREATED AND PRIMED NEW HAT CHANNEL IAW SRM 51-10-04, STEP 21 AND STEP 25 INSTALLED NEW SDR DALA2016022501398Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE LOWER EMERGENCY EXIT SIGNS AT BOTH OF THE OVERWING HATCHES AND AT THE AFT CABIN DOOR WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.SDR DALA1704899547Spar Cap · not reportedSTABILIZER / VERTICAL / RT SPAR CAP FORWARD FLANGE,ZFS = 49-50 REPAIRED IAW ERA 543293-14.SDR DALA2016022501439Slide · unserviceableINSPECTION DISCOVERED THAT THE EMERGENCY ESCAPE SLIDE IN THE TAILCONE WAS NO LONGER IN AN ACCEPTABLE CONFIGURATION. THE SLIDE BECAME UNRAVELED INSIDE THE COVER. AN OUT OF POSITION, MISRIGGED, POOR CONDITION, OR ILL-ARRANGED SLIDE ASSEMBLY COULD PREVENT PROPESDR DALA2016022501397Bulkhead · crackedUPPER CABIN LT ENGINE PYLON SUPPORT BULKHEAD, BS 1022 IS CRACKED ON AFT SIDE AT LONGERON 7L. MARKED, VERIFIED WITH EDDY CURRENT. CUT OUT DAMAGE AS MARKED BS 1022 L7L IAW SRM 51-70-11, FIG 201. HFEC OF CUTOUT SHOWED NO DEFECTS IAW NOT SPM 06-10-01. 001 TAG 678SDR DALA2016022401396Cover · unsecureINSPECTION DISCOVERED THAT THE EMERGENCY ESCAPE SLIDE IN THE TAILCONE WAS IMPROPERLY INSTALLED. THE SLIDE COVER WAS NOT SECURED AS DESIGNED. THIS WOULD PREVENT PROPER DEPLOYMENT OF THE ESCAPE SLIDE AND IS NOT IN COMPLIANCE WITH 14 CFR, PART 121.703. THE TAISDR DALA2016022401395Skin · crackedAFT FUSELAGE SKIN IS CRACKED, 1.0" AT STA 1133 BETWEEN STR 2RT AND STR 3RT, HFEC -M-. SEE NR FOR ADDITIONAL INFORMATION 001-0219:0593-2005, 012 00102. REPAIRED BY CUTOUT AND INSTALLATION OF DOUBLER. STA LOCATION IAW ENGINEERING IS ACTUALLY BS 1152 NOT BS 1133SDR DALA2016022401364Cusp Web · corrodedLH OUTER CUSP WEB HAS CORROSION AROUND SEVERAL FASTENER HEADS BETWEEN BS 813 & 832. REPAIRED LT OUTER CUSP WEB AT BS 813 TO 832 IAW SRM 53-00-55, PG 101, 102 AND 104, AND FIG 216, REPAIR 4.SDR DALA2016022401363Cusp Web · corrodedLEFT OUTER CUSP WEB HAS CORRODED LAP JOINT AT ATTACH ANGLE AT BS 589. MARKED. BLENDED CORROSION ON LEFT UPPER CUSP ANGLE SPLICE AT BS 589 AND FOUND TO BE OUT OF LIMITS. ORIGINAL 0.080", REMAINING 0.055". REMOVED UPPER CUSP ANGLE SPLICE AND FABRICATED NEW CUSSDR DALA2016022401362Cusp Web · corrodedLEFT OUTER CUSP WEB HAS CORRODED LAP JOINT AT ATTACH ANGLE, BS 635. MARKED. BLENDED CORROSION ON LT UPPER CUSP ANGLE SPLICE AT BS 635 AND FOUND TO BE OUT OF LIMITS. ORIGINAL 0.080", REMAINING 0.060". FABRICATED NEW UPPER CUSP ANGLE SPLICE AND HEAT TREATED SDR DALA2016102807815Cusp Web · corrodedLEFT OUTER CUSP WEB HAS TWO SPOTS OF CORROSION BETWEEN BS 794 - 813. BLENDED CORRODED AREAS AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-55 PG 101 & 102 FIG 101. FABRICATED & INSTALLED A REPAIR DOUBLER IAW SRM 53-00-55 REPAIR 4 FIG 216.SDR DALA2016102807814Cusp Web · corrodedLEFT OUTER CUSP WEB CORRODED AT BS 544. CORRISION BLENDED BEYOND ALLOWABLE LIMITS. REPAIRED THE CUSP WEB IAW SRM 53-00-55 ALLOWABLE DAMAGE 1 AND 53-00-55 REPAIR 4.SDR DALA2016102807813Cusp Web · corrodedLEFT OUTER CUSP WEB CORRODED AT BS 488. CORRISION BLENDED AND FOUND BEYOND ALLOWABLE LIMITS. REPAIRED THE CUSP WEB IAW SRM 53-00-55 ALLOWABLE DAMAGE 1 AND 53-00-55 REPAIR 4.SDR DALA2016022301313Seat Track · corrodedPASSENGER CABIN INBD SEAT TRACK CORRODED AT BS 522, RBL 22". REMOVED CORROSION ON PASSENGER CABIN INBD SEAT TRACK BS 522, RBL 22", CHECK MATERIAL ORIG "T" .115, LOSS OF .033, REMAINING MATERIAL OF .082 FOUND TO BE OUT OF LIMITS IAW SRM 53-20-52, FIG 101, NEW SSDR DALA2016022301312Seat Track · corrodedPASSENGER CABIN INBD SEAT TRACK CORRODED AT BS 488, RBL 22". REMOVED CORROSION OF CABIN SEAT TRACK AT BS 488, RBL 22 IAW SRM 53-20-52, PG 103, FIG 101 AND 51-10-04; FOUND TO BE WITH OUT LIMITS IAW SRM 53-20-52, FIG 101. REPLACEMENT OF SEAT TRACK REF WORK CASDR DALA2016022301311Seat Track · corrodedPASSENGER CABIN INBD SEAT TRACK CORRODED AT BS 551, RBL 22". REPLACED PASSENGER CABIN INBD SEAT TRACK FROM BS 470 TO 580, RBL 22". TREATED AND PRIMED, TOPCOATED SEAT TRACK IAW SRM 51-10-04, PG 20,29, AND 49 AND INSTALLATION OF SEAT TRACK REF SRM 53-20-52 REPSDR DALA2016022301309Floor Panel · corrodedPASSENGER CABIN FLOOR PANEL 221ER HAS AREAS OF CORROSION ON FWD END OF PANEL. REMOVED CORROSION FROM FLOOR PANEL 221ER. PANEL WAS OUT OF LIMITS. NEW PANEL WAS LOCATED AND DRILLED TO FIT ACFT IAW DWG 9957828, REV AB ID:1 FRAME 2 OF 3, PANEL WAS TREATED & PRIMSDR DALA2016022301308Seat Track · not reportedREPLACE MAIN CABIN SEAT TRACK BS 200-588, RBL 44.5. REPLACED SEAT TRACK BS 200-588, RBL 44.5 IAW DWG 5930547.SDR DALA2016022301310Drain Mast · corrodedELECTRONIC EQUIPMENT COMPARTMENT A LOWER DRAIN MAST IS CORRODED, FWD OF 218 BULKHEAD BETWEEN S27-S28R. VERIFIED DRAIN MAST DOUBLER WAS OUT OF LIMITS BY VISUAL INSPECTION. ZERO THICKNESS REMAINING. REMOVED 2 EA INTERCOSTALS TO GAIN ACCESS REMOVED DRAIN MAST ANSDR DALA2016022201276Fuel Tank · corrodedLEFT WHEEL WELL TO RT WHEEL WELL FUEL TANK SKIN PLANK PANEL T/E CORRODED AT SEVERAL LOCATIONS. CLEAN/ EVAL, TREAT & PAINT REF OR NRC 62937-0100-0065. BLENDED OUT CORROSION ON RT WHEEL WELL FUEL TANK SKIN PLANK PANEL. MEASURED THICKNESS LOSS OF .015 TAG 3310SDR DALA2016022201273Vane · puncturedRIGHT WING, INBD FLAP VANE, INBD END HAS A PUNCTURE HOLE. REMOVED DAMAGE ON RT WING INBD FLAP VANE INBD END IAW SRM 57-53-01 REPAIR NR 1. MATERIAL REMOVED .75" DIA CIRCLE. FABRICATED .75" FILLER FROM 7075-T6 BARE .016", FABRICATED 11.5" X 4.25" DOUBLER FROMSDR DALA2016022201272Strap · crackedFORWARD CARGO COMPARTMENT DOOR JAMB LOWER SILL 4.5" SPLICE STRAP CORRODED 5" FWD OF LOWER FWD STOP FITTING. REMOVED CORROSION IN SPECIFIED AREA FOUND BLENDED LIMITS TO BE BEYOND ACCPTABLE LIMITS ORGINAL MATERIAL .080 REF SRM 53-20-15, FIG 1, MATERIAL LOSS OF SDR DALA2016022201271Door Frame · corrodedFORWARD CARGO COMPARTMENT DOOR JAMP LOWER SILL 4.5" SPLICE STRAP CORRODED 5" AFT STOP FITTING. REMOVED CORROSION IN SPECIFIED AREA FOUND BLENDED LIMITS TO BE BEYOND ACCEPTABLE LIMITS, ORGINAL MATERIAL .080, REF SRM 53-20-15, FIG 1. MATERIAL LOSS OF .040 USSDR DALA2016102807812Cargo Track · corrodedFWD CARGO BAY. CARGO TRACK CORRODED AT BS 427 - 655. REMOVED CORROSION IAW SRM 51-10-04. FOUND TO BE BEYOND LIMITS IAW SRM 53-20- 52. REPLACED THE CARGO TRACK IAW SRM 53-20-52 AND DWG 5965411 REV AW.SDR DALA2016102707783Seat Track · corrodedPASSENGER CABIN CENTER SEAT TRACK CORRODED BS 295 RBL 43. THE SEAT TRACK WAS REMOVED AND REPLACED.SDR DALA2016102707782Seat Track · corrodedPASSENGER CABIN CENTER SEAT TRACK CORRODED BS 400 RBL 43. THE SEAT TRACK WAS REMOVED AND REPLACED.SDR DALA2016102707781Seat Track · corrodedPASSENGER CABIN CENTER SEAT TRACK CORRODED BS 522 RBL 43. THE SEAT TRACK WAS REMOVED AND REPLACED.SDR DALA2016102707780Seat Track · corrodedPASSENGER CABIN CENTER SEAT TRACK CORRODED BS 551 RBL 43. THE SEAT TRACK WAS REMOVED AND REPLACED.
Back to Boeing 717-200