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 DALA2016051103851Cusp Web · corrodedAT BS 370 RT CORRODED CUSP WEB. CORROSION CUT-OUT AND REPAIRED IAW SRM 53-00-55, REPAIR 4, FIG 216 & 223. CORROSION AT FASTENER HOLE REMOVED, BLEND OUT, & WITHIN ALLOWABLE LIMITS, REMOVED .001 ALLOWED REMOVING .002 IAW SRM 53-00-55. ALLOWABLE DAMAGE 1, PARA SDR DALA2016051103849Hinge Fitting · damagedSCRATCHES ON BUSHINGS ON RT ELEVATOR HINGE FITTINGS BS XE=49. AYP, CARD 1, ZONE 340. UPPER BUSHING AT BS XE=49 ON RT ELEVATOR HINGE FITTING WAS CLEANED IAW PS 900-1-2-1 NR 001 AND DAMAGE WAS NOT FOUND. LOWER BUSHING AT BS XE=49 ON RT ELEVATOR HINGE FITTING WSDR DALA2016051103848Hinge Fitting · wornFREEPLAY ON EYEBOLT NR 6 ON HINGE FITTING ON RT HORIZONTAL STAB. AYP, CARD 14, ZONE 340. EYEBOLT NR 6 ON HINGE FITTING ON RT HORIZONTAL STABILIZER WAS REPLACED IAW CMM 27-30-2 AND FREE PLAY WAS CORRECTED. RII COMPLETEDSDR DALA2016051103847Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA ON RT WING FUEL ACCESS PLATE NR 620JB, 620LB, 620MB, AND 620PB, AYP. DUE TO CORROSION OUT OF LIMITS FUEL ACCESS NR 620JB, 620LB, 620MB, AND 620PB WERE REPLACED IAW SRM 57-10-01 UNDER CONDITION III. TOOL USED, PN 1SDR DALA2016051103846Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA ON LT WING FUEL ACCESS NR 520CB, 520DB, 520EB, AND 520GB, AYP. CORROSION ON COUNTERSINK AND SETTLEMENT AREA ON FUEL ACCESS 520CB, 520DB, 520EB, AND 520GB WAS REMOVED, COUNTERSINK HOLES AT FUEL ACCESS 520CB AND 520ESDR DALA2016051103845Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA ON LT WING FUEL ACCESS PLATE NR 620DB AND 620HB, AYP, IN REF OR NRC 48, ZONE 000. FUEL ACCESS PLATES 620DB AND 620HB WERE REPAIRED UNDER CONDITION II IAW SRM 57-10-01.SDR DALA2016051103844Access Panel · corrodedCORROSION ON LT FUEL ACCESS PLATE COUNTERSINK NR 520CB AND 520EB. CORROSION ON LT FUEL ACCESS PLATE 520CB AND 520EB WAS REMOVED AND FUEL ACCESS WERE REPAIRED IAW SRM 57-10-01.SDR DALA2016051303916Skin · gougedVERTICAL STABILIZER SKIN RT GOUGED UNDER PANEL 360AT. REPLACED NEW VERTICAL STABILIZER SKIN RT IAW DWG 5936143 AND 51-41-02, PARA 4 AND 51-41-05, PARA 2.SDR DALA2016051003834Seat Track · corrodedLOWER FUSELAGE, AFT CARGO, RT SEAT TRACK FOR BS 995-1021, FASTENER HOLES CORRODED. FABRICATED NEW AFT CARGO RT SEAT TRACK F/S 995-1021 IAW SRM 51-40-08, TABLE 1. NEW SEAT TRACK TO BE INSTALLED ON NR 66647-0100-077, PARTIAL 4.SDR DALA2016051103852Wire Harness · damagedTHE FLIGHT WAS DIVERTED FOLLOWING THE SHUTDOWN OF THE NR 2 ENGINE. ALSO, ALL OF THE ENGINE COWLING EXITED THE ACFT WHILE IN FLIGHT. MAINTENANCE REPAIRED THE FUSELAGE DAMAGE AND REPLACED THE NR 2 ENGINE DUE TO WIRE HARNESS DAMAGE.SDR DALA2016051103850Cusp Web · corrodedCUSB WEB AT BS 585 RT CORRODED. REPLACED LOWER CUSP TEE SPLICE CORRODED OUT OF LIMITS 50 PERCENT. REPLACED UPPER CUSP TEE SPLICE AND DAMAGED CUSP WEB AT BS 575 TO 595 IAW SRM 53-00-00, FIG 103, SRM 51-41-05, SRM 51-41-02.SDR DALA2016051003833Floor Support · damagedMULTIPLE DISCREPANCIES NOTED ON THE FORE TO AFT FLOORBEAMS BS 1022-1053. REPLACED FORE TO AFT FLOORBEAMS BS 1022-1053 RT AND LT BL 445 IAW SRM 51-41-05, PG 17, PARA 8, ER/A 545674-14. COMPLIED WITH ASSOCIATED ER/A 54-567414 ADDED FOR AC 9516.SDR HALA2016050700175Hf Comm · malfunctionedHF RADIO UNABLE TO UNDERSTAND TRANSMISSIONS FROM OTHER ACFT AND FROM ATC, VERY GARBLED. TRIED 3 DIFFERENT FREQUENCIES ALL SAME. SET HF FOR USB OPERATION. OPS CHECKED NR 1 HF IAW AMM 23-11-00-710-801. OPS CHECKED GOOD. OK FOR SERVICE.SDR HALA2016050500172Cylinder · malfunctionedUPON GEAR EXTENSION, NOSE GEAR UNSAFE LIGHT ILLUMINATED. CREW USED THE ALT METHOD, MANUALLY EXTENDING GEARS). ACCOMPLISHED BITE CHECK, NO FAULTS NOTED. ACFT TO BE MAINTENANCE FERRIED BACK TO HOME BASE, IN, GEAR DOWN CONFIGURATION, TO BE JACKED AND OPS CHECKSDR DALA2016050603719Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA OF RT WING FUEL ACCESS PLATE NR 620AT AND 620DT, AYP IN REF ORNRC 50, ZONE 000, CARD 55, ZONE 000. FUEL ACCESS 620AT WAS REPAIRED UNDER CONDITION II IAW SRM 57-10-01.SDR DALA2016050603718Spring · missingDURING THE TAILCONE RELEASE SYSTEM FUNCTIONAL CHECK, MAINTENANCE FOUND THAT THE TAIL CONE FAILED TO DROP BECAUSE A SINGLE SPRING WAS MISSING FROM A RELEASE CABLE SYSTEM PIN. THE SPRING WAS INSTALLED AND THE SYSTEM WAS SUCCESSFULLY FUNCTIONALLY CHECKED IAW AMMSDR DALA2016050603714Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA OF RT WING FUEL ACCESS PLATE 620DT. CORROSION ON COUNTERSINK HOLES AND SETTLEMENT AREA AT FUEL ACCESS WAS REMOVED, COUNTERSINK HOLES AND SETTLEMENT AREA ON FUEL ACCESS 620DT WERE MEASURED THIS IS OUT OF LIMITS. ASDR DALA2016050603713Hinge Fitting · damagedNICK ON LOWER HOUSING ON RT ELEVATOR HINGE FITTING XE=49. REPAIR WAS PERFORMED IAW ER/A 545166-14, REV ORIGINAL.SDR DALA2016050603712Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA ON LT WING FUEL ACCESS PLATE NR 520FT CARD 52, ZONE 000. DUE TO EXCESSIVE DAMAGE AT FUEL ACCESS 520FT THIS WAS REPLACED IAW SRM 57-10-01.SDR DALA2016050603711Support Fitting · crackedCRACKED FITTING SUPPORT ON BS 737, X=-44, AND Z=5 AT PASSENGER STRUCTURE WING BOX AREA, SM, CARD 23, ZONE 140. FITTING SUPPORT WAS REPLACED IAW DWG 3925812, REV A, SRM 51-41-02, 51-40-05, 51-10-04 PAR 15, 21.SDR DALA2016050603710Attach Angle · crackedPYLON BULKHEAD BS 1022 AFT ATTACH ANGLE CRACKED AROUND 2 FASTENERS LONGERON 7L. REPAIRED ATTACH ANGLE AT 1022 L7L IAW SRM 51-70-11, REPAIR 1, FIG 201.SDR DALA2016050603709Attach Angle · crackedPYLON BULKHEAD BS 1022 AFT ATTACH ANGLE CRACKED AROUND 2 FASTENERS, LONGERON 7R. REPAIRED ATTACH ANGLE AT 1022 L7R IAW SRM 51-70-11, REPAIR 1, FIG 201.SDR DALA2016050603708Tee Fitting · crackedCRACK ON TEE FITTING ON LOWER SECTION OF FWD CARGO DOOR BS 401 APPROXIMATELY C1, SM, CARD 12, ZONE 810. TEE FITTING WAS REPLACED IAW SRM 51-41-01 AND 51-41-02.SDR HALA2016050300171Warning Light · false activationON APPROACH, DURING GEAR EXTENSION, NOSE GEAR UNSAFE LIGHT ILLUMINATED AND CREW USED THE ALT METHOD, MANUALLY EXTENDING GEARS. ACCOMPLISHED BITE CHECK, NO FAULTS NOTED. ACFT TO BE MAINTENANCE FERRIED BACK TO HOME BASE, IN GEAR DOWN CONFIGURATION,TO BE JACK ASDR DALA2016050503661Bracket · crackedINTERCOSTAL BRACKETS ARE CRACKED, VERIFIED WITH HFEC ON THE FWD SIDE OF FRAME AT BS 237. JUST OTBD OF LONGERON 28L ABD OTBD OF LONG .28R LOCATED UNDER CARGO TIE-DOWN TRACKS. REMOVED CRACKED INTERCOSTAL BRACKETS AT BS 237, STR 28R AND 28L. FABRICATED ANGLES 9SDR DALA2016050503659Skin · puncturedPUNCTURE AND CRACK ON UPPER SKIN, LT ELEVATOR, BS PROYECTION XE=13.213, APPROACH. SM VHS. UPPER SKIN LT ELEVATOR WAS REPAIRED IAW SRM 51-41-02, 41-41-08, 51-70-13, PAGE 201, SHT 1-3, REPAIR 2, RII COMPLETEDSDR DALA2016050503658Intercostal · crackedCRACKED INTERCOSTAL ON LT ELEVATOR INTERNAL STRUCTURE BS XE=13.213, SM, IN REF ORNRC 4, ZONE 300. CRACKED INTERCOSTAL WAS REPAIRED IAW SRM 51-41-02, 55-00-00, FIG 201. RII COMPLETED BY INSPECTION.SDR DALA2016050603715Former · crackedFORMER CRACKED BS 660. REPAIRED IAW ER/A 545665-14, REV 0 AND NDT SPM PORT 606-10-01.SDR DALA2016050503660Former · cracked2 FORMERS CRACKED INTERNAL STRUCTURE OF THE CANTED KEEL, RT OTBD SIDE AT BS 660.0 AND 675.5. REMOVED R1 AND R2 WING TO BODY FRAMES, HYD LINES, AND FORMERS AT BS 660 AND 675.5 RT. FABRICATED REPAIR ANGLES AND FILLERS. HEAT TREATED REPAIR ANGLES AND FILLERS TSDR DALA2016050403610Skin · crackedEXTERNAL FUSELAGE SKIN CRACKED, BS 1076, LONGERON 14R. REPAIRED CRACKED AREA WITH FILLER END DOUBLER RT PANEL DUCT REMOVED AND REINSTALLED LEAK CHECK COMPLETED IAW AMM 36-00-00-863-804 IAW PRI 545666-14, REV 2.SDR DALA2016050403609Skin · damagedDURING RUDDER INSTALL LOWER LT SKIN WAS CRACKED AND BENT. LOWER LT SKIN WAS REPAIRED IAW SRM 51-70-13, REPAIR 1.SDR DALA2016050403608Access Panel · corrodedCORROSION ON RT FUEL ACCESS PLATE NR 620CT. FUEL ACCESS PLATE NR 620CT WAS REPLACED IAW SRM 57-10-01.SDR DALA2016050303563Cusp Web · corrodedCORROSION FOUND ON CUSP WEB, BS 193, LBL56. REPAIRED CUSP WEB IAW SRM 53-00-55 REPAIR 4.SDR DALA2016050303561Skin · corrodedCORROSION ON UPPER WING SKIN AFT EDGE FROM BS XCW=16 TO XCW=50 AT RT MLG WHEEL WELL. DAMAGE WAS REPAIRED IAW ER/A 545128-14, REV ORIGINAL, AND ETI 17-16-013, REV 2. RII COMPLETED.SDR DALA2016050303560Access Panel · corrodedCORROSION ON COUNTERSINK OF FUEL ACCESS DOOR. FUEL ACCESS DOOR REPLACED IAW IPC 57-23-01.SDR DALA2016050303559Web · puncturedPUNCTURE AT FLOOR WEB, UNDER FLOOR PANEL. WEB WAS REPAIRED IAW 53-00-00, FIG 102.SDR DALA2016050303558Access Panel · corrodedCORROSION OUT OF LIMITS IN COUNTERSINK, 3 HOLES NON ADJACENT AT FUEL ACCESS DOOR 620JB. FUEL ACCESS DOOR WAS REPAIRED IAW SRM 57-10-01, CONDITION II.SDR DALA2016050303557Access Panel · corrodedCORROSION ON COUNTERSINK OF FUEL ACCESS DOOR 620AT. FUEL ACCESS DOOR WAS REPAIRED IAW AMM 51-10-01, CONDITION II.SDR DALA2016050303556Access Panel · corrodedCORROSION ON COUNTERSINK OF FUEL ACCESS DOOR 520CB. FUEL ACCESS DOOR WAS REPAIRED IAW AMM 51-10-01, CONDITION II.SDR DALA2016050203476Pan · crackedCRACKS ON LOWER PAN BETWEEN STOP 1 AND 2 BS 373 APPROXIMATELY AT FWD CARGO COMPARTMENT DOOR. 1, SM CARD 11, ZONE 810. PAN BETWEEN STOP 1 AND 2 WAS REPAIRED IAW SRM 52-30-02, FIG 201.SDR DALA2016050203475Bracket · crackedCRACKED AFT BRACKET SUPPORT TOP AREA OF L1 DOOR. BRACKET WAS REPLACED IAW SRM 51-41-02 AND DWG 5961804, REV 2F.SDR DALA2016050203474Beam · crackedCRACK ON BEAM 1, AFT EDGE AT L1 DOOR. BEAM WAS REPAIRED IAW SRM 52-10-2, FIG 201, SHEET 3.SDR DALA2016050203473Access Panel · corrodedCORROSION ON COUNTERSINK OF FUEL ACCESS DOOR 620DT. CORROSION ON COUNTERSINK OF FUEL ACCESS PLATE NR 620DT WAS REMOVED. COUNTERSINK WERE MEASURED AND WERE FOUND 4 COUNTERSINK OUT OF LIMITS IAW SRM 57-10-01. ACCESS PLATE WAS REPAIRED IAW SRM 51-10-01 AND TREASDR DALA2016050203472Access Panel · corrodedCORROSION ON COUNTERSINK OF FUEL ACCESS DOOR 620MB. CORROSION WAS REMOVED. COUNTERSINK WERE MEASURED AND WERE FOUND 3 COUNTERSINK OUT OF LIMITS IAW SRM 57-10-01. ACCESS WAS REPAIRED IAW SRM 51-10-01 AND TREATED IAW SRM 51-10-04.SDR DALA2016050103469Floor Panel · crackedCRACKED FLOOR PANEL. FLOOR PANEL REPAIRED IAW SRM 53-20-50.SDR DALA2016050103465Frame · crackedCRACKED FRAME BS 1037 LONGERON 17R AT PAX CABIN. FRAME WAS REPAIRED IAW SRM 53-20-07, FIG 201, 51-41-03 PAR 11, AND 51-41-02, 51-41-05. RII INSPECTOR SGMR ID 796792.SDR DALA2016050103464Door Frame · crackedCRACK ON DOOR FRAME LT SIDE BETWEEN BS 35 TO BS 46 NOSE GEAR WHEEL WELL. THE DOOR FRAME WAS REPAIRED IAW SRM 53-14-4, FIG 201, 51-41-02, 51-41-03, 51-41-05, 51-20-09, AND 51-10-4 PAR 21 AND 15.SDR DALA2016050103463Door Frame · crackedCRACK ON DOOR FRAME RT SIDE BETWEEN BS 35 TO BS 46 AT NOSE GEAR WHEEL WELL. DOOR FRAME WAS REPAIRED IAW SRM 53-10-14, FIG 201, 51-41-02, 51-41-03, 51-41-05, 51-20-09, AND 51-10-4 PAR 21 AND 15.SDR DALA2016050103462Cusp Web · corrodedCORROSION OUT OFF LIMITS ON CUSP WEB UPPER/LWR SURFACE ON BS 874 . REPAIRED IAW SRM 53-00-55, FIG 212, SRM 51-10-04 PAR 15, 21, 37, 26, SRM 51-41-01, 51-41-02, AND 51-41-05.SDR DALA2016050103461Cusp Web · corrodedCORROSION ON RT CUSP WEB UPPER, LWR SURFACE BETWEEN BS 397-405 AND 465 TO 477, SM, IN REF OR NRC 37, ZONE 200, CARD 57, ZONE 200. CUSP WEB BS 397 TO 405 AND 465 AND 465 TO 477 WERE REPAIRED IAW SRM 53-00-55, FIG 219 AND FIG 216 AND 51-41-02, 51-41-01, 51-41-05
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