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 DALA2016113009392Pan · crackedCRACKED RT RING PAN LOWER/FWD CORNER STA Y=927 INTERNAL STRUCTURE (FUS). DAMAGE AREA WAS REPAIRED PER SRM 56-20-02, REPAIR 1, FIG 202.SDR DALA2016113009391Pan · crackedCRACKED LT RING PAN LOWER/AFT CORNER STA Y=636 INTERNAL STRUCTURE (FUS). RING PAN WAS REPAIR PER B717 SRM 56-20-02 FIG 202.SDR HALA2016112900373Keelbeam · crackedLEFT SIDE UNDERWING BARREL KEEL BEAM AT BS 715 OB SIDE CRACKED. REPAIRED IAW E105-B10214-PERM AND DRAWING 9923454 REV F.SDR DALA2016112909363Battery Pack · dischargedDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS FOR THE AFT OVERWING EXITS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPERATIONAL CHECK WAS GOOD.SDR DALA2016121309811Seat Track · damagedUPPER CABIN RT INBD SEAT TRACK RBL 22 CORRODED & GOUGED AT BS 956-1022. BLENDED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-20-52. TRIMMED OUT SEAT TRACK IAW SRM 53-20-52 REPAIR 1.SDR DALA2016120709654Floor Panel · damagedAFT LAV WASTE DRAIN FLOOR PANEL HAS A MISSING INSERT AND DISBONDED HONEYCOMB CORE. REPAIRED IAW SRM 53-20-50 REPAIR 4.SDR DALA2016113009390Frame · corrodedVERIFY REPAIR DIMENSIONS PER SRM 53-20-07 REP3 FOR CORROSION ON LOWER LIP OF FRAME AT STA 908 L30 RT SIDE. VERIFIED REPAIR DID NOT CONFORM TO SRM 53-20-07 REP 3 DUE TO SHORT EDGE DISTANCE ON -17 PLATE AND -19 FILLER. FABRICATED NEW-17 PLATE AND -19 FILTERS, RESDR DALA2016112909362Seat Track · corrodedCORROSION ON RT SEAT TRACK X=54 FROM STA Y=984 TO Y=986 AT CABIN FLOOR STRUCTURE. DAMAGE AREA WAS REPAIRED PER B717 SRM 53-20-52 FIG 201 REPAIR 1.SDR DALA2016112609262Skin · crackedCRACK ON EXTERNAL FUSELAGE SKIN BS 1076 LONGERON 14L REPAIRED IAW ETI-17-16-154 REV.4 AND ER/A 551747-14 REV. A .SDR DALA2016112909389Support Angle · corrodedRIGHT WALKWAY SUPPORT ANGLE ATTACHED TO BOTTOM STIFFENER / FRAME IN AFT ACCESSORY AT STA 1133 IS CORRODED. RT WALKWAY SUPPORT STRUT WAS CORRODED TO 100%. REPLACED WALKWAY STRUT IAW B717 SRM 51-41-05.SDR DALA2016112809263Cusp Web · crackedLEFT CUSP WEB IS CRACKED BETWEEN BS 1002 AND 1022 LBL 44-55. CUT OUT THE DAMAGED SECTION OF CUSP WEB. FABRICATED AND INSTALLED DOUBLER, FABRICATED AND INSTALLED RING DOUBLER, AND FABRICATED AND INSTALLED FILLER REF B717 SRM 53-00-55 REPAIR 4.SDR DALA2016112409261Skin · crackedCRACKED INBD BUTTE DOOR INBD SKIN AT RT WING. REPAIRED IAW ETI-17-16-171 REV. 1 AND ER/A 551772-14 REV. ORIG.SDR DALA2016112909361Skin · dentedDENT DAMAGE TO FUSELAGE STA 579 BETWEEN L27L AND L28L REQUIRES SRM REPAIR. REPAIRED FUSELAGE SKIN STA 579 BETWEEN L27L AND L28L IAW ER/A 549357-14 REV A.SDR DALA2016112309128Cusp Web · crackedRIGHT CUSP WEB HAS MULTIPLE AREAS OF CORROSION BS 916, 930, 943, 955, 980, RBL 61. CLEANED CORROSION IAW SRM 53-00-55 FIG 101, REPAIRED IAW SRM 53-00-55 REPAIR 4.SDR DALA2016112309127Floor Panel · crackedFLOOR PANEL 211JF IS CRACKED. REPAIRED THE FLOOR PANEL IAW SRM 51-70-11, REPAIR 1 FIG 201. FABRICATED A REPAIR DOUBLER. APPLIED ALODINE AND PRIMER IAW SRM 51-22-01 PAGES 2 AND 3.SDR DALA2016112309126Floor Support · crackedFLOOR SUPPORT AT BS 617 - 636 BL 0 CRACKED. REPAIRED IAW SRM 53-00-00 REPAIR 1 FIG 201, AND DWG 9936580.SDR 2016F00242Skin · delaminatedDURING MAINTENANCE CHECK, THE RT OTBD SPOILER WAS FOUND DELAMINATED.SDR DALA2016112209067Door Frame · corrodedAFT CARGO DOOR FRAME HAS SEVERAL AREAS OF CORROSION. PAN SPLICE FOUND TO BE OUT OF LIMITS, MORE THAN 50% REMOVED. REPLACED LOWER PAN SPLICE IAW SRM 53-20-15 REPAIR 7.SDR DALA2016112209066Stringer · corrodedCORROSION ON STRINGER 24R BS 1002-1024. THE STRINGER WAS FOUND TO BE OUT OF LIMITS IAW IAW SRM 53-00-00. REPLACED THE STRINGER IAW SRM 51-41-02.SDR DALA2016112209068Frame · dentedDENT FOUND IN FRAME BS 579 BETWEEN LONGERONS 27 AND 28L. REPAIRED THE FRAME IAW SRM 53-00-06 REPAIR 3 PG 201-206.SDR DALA2016112008948Access Panel · crackedCRACK ON FUEL ACCESS PLATE 620MB. ACCESS PLATE 620MB WAS REPLACED PER AMM 28-00-00 AND IPC 57-23-01-01.SDR DALA2016112008947Doubler · corrodedCORROSION ON DOUBLER, STA Y=954 AND PROTECTION BTW LONG 26R TO 27R DOOR JAMB, AT AFTER CARGO COMPARTMENT. DOUBLER WAS REMOVED PER SRM 51-41-05 PAR 10 AND 51-41-07 PAR 10, DOUBLERS WERE MANUFACTURED PER SRM 51-20-09 AND 53-20-15 REPAIR 7 AND DOUBLER WAS INSTALLSDR HALA2016112900001Former · crackedLEFT UNDERWING BARREL KEEL BEAM AT BS 715 OTBD SIDE FORMER CRACKED. REPAIRED THE FORMER IAW DRAWING 9923454 REV F.SDR DALA2016112109065Cargo Track · corrodedCORRODED LT CARGO TRACK BETWEEN BS 813 - 1022. THE CORROSION WAS REMOVED IAW SRM 51-10-04 PAR 26. UT WAS ACCOMPLISHED IAW NDT SPM 04-00-07 PAR 5 FIG 3 (SHEET 1 AND 2) AND FOUND WITHIN LIMITS AT BS 813 TO 896 IAW SRM 53-20-52. FIG 101 (SHEET 1 OF 3). THE CASDR DALA2016112108949Power Supply · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING IN THE COCKPIT AND THE EXIT SIGN AT L1 DOOR WERE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.SDR DALA2016112008946Skin · crackedCRACK AROUND RIVET HEAD IN FUSELAGE SKIN AT L14 LT STA 1076 ABOVE NR 1 ENGINE PYLON, LOCATION MARKED. REPAIRED SKIN AT L14 LT STA 1076 IAW ER/A 551822-14 REV O.SDR DALA2016111908945Channel · crackedFLOOR PANEL 221SF HAS CRACKED HAT CHANNEL ON FORWARD END. REPAIRED CRACKED HAT CHANNEL ON FWD END OF FLOOR PANEL 221SF IAW SRM 53-20-50 REPAIR 5 DOUBLER FABBED FROM 6061-0-.032 HEAT TREATED TO 6061-T6 APPLIED ALODINE AND PRIMER IAW SRM 51-22-01 PAGES 2 & 3.SDR DALA2016111908944Channel · crackedFLOOR PANEL 222MF HAT CHANNEL IS CRACKED AT AFT END. REPAIRED AFT END OF HAT CHANNEL ON FLOOR PANEL 222MF IAW SRM 53-20-50 REPAIR 5. REPAIR DOUBLER FABBED FROM 6061-0=.032 HEAT TREATED TO 6061-T6. APPLIED ALODINE AND PRIMER TO DOUBLER IAW SRM 51-22-01 PAGES 2 SDR DALA2016111908943Channel · crackedFLOOR PANEL 222AJF HAT CHANNEL IS CRACKED AT AFT END AND SEPARATING FROM PANEL ON FORWARD END. REPAIRED CRACK ON AFT END OF HAT CHANNEL ON FLOOR PANEL 222AJF IAW B717 SRM 53-20-05 REPAIR 5. REPAIR DOUBLER FABBED FROM 6061-0-.032 HEAT TREATED TO 6061-T6 APPLIESDR DALA2016111908942Skin · crackedFS 1087 LONGERON 14R EMPENNAGE SKIN HAS 3 EA CRACKS, MARKED. HFEC VERIFIED IAW NDTSPM ETHF PROCEDURE 1, 06-10-01.001. CUT OUT CRACKED AREA; FABRICATED AND INSTALL FILLER/EXTERNAL REPAIR DOUBLER IAW ER/A 551823-14 REV, ORIGINAL AT F/S 1087 LONGERON 14R.SDR DALA2016111908941Skin · crackedCRACK ON INTERNAL FUSELAGE SKIN STA Y=1021 BTW LONG 13L-14L AT PAX CABIN. CRACKS ON FUSELAGE/SKIN AND DOUBLER/STA 1022 & L-13-L14 WERE REPAIRED WITH ETI-17-16-149 REV 3 AND ER/A 551741-14 REV ORIGINAL. PERFORM GVI ON EXTERNAL SURFACE, EVERY 3000 FLIGHT CYCLES SDR DALA2016111908940Floor Panel · damagedPANEL 223EF FORWARD CORNER IS BENT AND SEPARATED FROM BACKUP STRIP. FURTHER INSPECTION REVEALED A CRACK IN THE NR 2 FASTENERS HOLE. REPAIRED CRACK IAW SRM 53-00-00 REPAIR 1 DOUBLER FABBED. CRACK REPAIR SATISFIED SEPARATION REPAIR.SDR HALA2016111700516Valve · malfunctionedRT ENGINE COMPRESSOR STALL AFTER START. REMOVED AND REPLACED THE BYPASS AND VENT VALVE IAW TASK 73-13-04-000-801, 73-13-04-400-801.ENGINE
RUN AND LEAK CHECKED GOOD. OK FOR SERVICE.SDR DALA2016111808914Hinge · corrodedCORROSION AT HORIZONTAL STABILIZER CENTER SECTION HINGE BORE AT STRINGER 7 RT SIDE. THE REPAIR WAS ACCOMPLISHED PER ETI-17-16-155 REV 2 AND ER/A 551748-14 REV ORIG.SDR DALA2016111808913Cusp Web · crackedRT CUSP WEB JUST FORWARD OF FRAME STA 505 IS CRACKED AROUND RIVET AND AREA OF CORROSION. REMOVED DAMAGE PART OF CRACKED CUSP WEB. FABRICATED NEW PARTS. INSTALLED NEW PARTS IAW SRM 53-00-55 REPAIR 4 PG 257 & SRM 51-40-02 AT STA 505.SDR DALA2016111808939Panel · corrodedCORROSION AND DISBONDED VOR ANTENNA PANELS UPPER AND LOWER (4EA). VOR ANTENNA PANELS UPPER AND LOWER (4EA) WERE REMOVED PER AMM 34-32-03. VOR ANTENNAS (4 EA) WERE REPLACED PER AMM 34-32-03. FUNCTIONAL TEST WAS PERFORMED PER AMM 34-51-00. TEST OK.SDR DALA2016111808938Stiffener · crackedRT VERTICAL STIFFENER ON FWD FACE OF CENTER FUEL TANK IS CRACKED. VERIFIED WITH HFEC, MARKED. REMOVED CRACKED RT VERTICAL STIFFENER AND REPLACED WITH SERVICEABLE STIFFENER IAW SRM 51-41-05. LEAK CHECK WILL BE COMPLETED ON 72816-0100-0123.SDR DALA2016111808937Shear Tie · crackedSHEAR TIE AT STA 1020 BULKHEAD FWD SIDE IS CRACKED BETWEEN STRINGER 6LT& 7LT. VERIFIED WITH HFEC. REPLACED SHEAR TIE AT STA 1020 ON FWD SIDE OF BULKHEAD BETWEEN STRINGERS 6L AND 7L REF SRM 51-41-02 AND 51-41-05.SDR DALA2016111708912Pan · damagedELONGATED HOLE ON INNER PAN AT AFT SIDE BELOW HINGE ON AFT CARGO DOOR (C2) (S/N 00554). REPAIR ON INNER PAN AT AFT SIDE BELOW HINGE ON AFT CARGO DOOR (C2) WAS PERFORMED PER ETI-17-16-166 REV 1 AND ER/A 551752-14 REV ORIGINAL, AMM 52-31-03-000 802 AND SRM 51-41SDR DALA2016111708911Window Frame · crackedCRACK ON LWR FWD SECTION OF RT SLIDE WINDOW COUNTER FRAME AT COCKPIT. DAMAGE AREA WAS REPAIRED PER ETI -17-16-170 REV 1 AND ER/A 551770-14 REV ORIG.SDR DALA2016111708847Power Supply · inoperativeDURING THE TURN AROUND CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGN AT STA 706 WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY POWER SUPPLY FOR THE NOTED LIGHTED AREA AND THE OPERATIONAL CHECK WAS GOOD.SDR DALA2016121609950Power Supply · overheatedTHE F/A REPORTED A LOUD BANG FOLLOWED BY WHITE SMOKE WITH AN ELECTRICAL ODOR NEAR EXIT ROW 19. MAINTENANCE FOUND THAT THE UPPER BEACON POWER SUPPLY HAD OVERHEATED AND THAT THE WIRE HARNESS GOING TO THE BEACON WAS DISCOLORED. THE POWER SUPPLY, WIRE HARNESS, ANDSDR DALA2016111608848Lens · crackedTHE PILOT DISCOVERED THAT AN EMERGENCY EXIT SIGN DIFFUSER COVER WAS CRACKED. MAINTENANCE REPLACED THE LENS/COVER AND THE OPERATIONAL CHECK WAS GOOD.SDR DALA2016111608846Lens · brokenTHE PILOT DISCOVERED THAT AN EMERGENCY EXIT SIGN DIFFUSER COVER WAS BROKEN. MAINTENANCE REPLACED THE LENS/COVER AND THE OPERATIONAL CHECK WAS GOOD.SDR HALA2016111500513Compressor · stalledATB, OUT OF 1200 FT ENG R COMP STALL LOUD BANG, SHOOK VIOLENTLY RETURNED TO AIRPORT. FOUND POSSIBLE LIGHT BIRD MATERIAL ON NR 2 ENG INLET COWL AND TAIL CONE AREA. PERFORMED FIM 72-00 TASK 801 AND AMM 72-00-00-200-801 INSP OF THE ENGINE AFTER SURGE BORESCOPE HPSDR DALA2016111608813Retainer · wornWORN LOWER RETAINER AT FWD DOOR BARRIER. LOWER RETAINER WAS REPAIRED IAW ETI -17-16-168 REV. ORG. AND ER/A 551759-14 REV ORG.SDR DALA2016111608812Pan · crackedCRACK ON INBD AND OUTBD PAN LOWER EDGE BS 388 AT FWD CARGO DOOR. INBD & OUTBD PAN LOWER EDGE WAS REPAIRED IAW ETI-17-16-161 REV 1 AND ER/A 551739-14 REV ORIGINAL.SDR DALA2016111608811Beam · crackedCRACKED LT NLG DOOR FRAME BEAM BS 48. AREA DAMAGE WAS REPAIRED IAW SRM 53-10-14 FIG. 201 REP. 2, ETI-17-16-158 REV. 1 AND ER/A 551751-14 REV. ORIG.SDR DALA2016112209069Seat Track · corrodedCORROSION ON RT OTBD SEAT TRACK BS 215. BLENDED THE CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-20-52 FIG 101. REPLACED THE SEAT TRACK IAW SRM 51-41-01.SDR DALA2016111508810Access Panel · corrodedCORROSION ON FUEL ACCESS PANEL COUNTERSINK ON THE RT WING. THE ACCESS PANEL WAS REPLACED IAW SRM 57-10-01.
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