Boeing 717-200

Service difficulty reports · 18,771

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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.

SDR DALA2017010500097Access Panel · corrodedCORROSION ON FUEL ACCESS PLATE 620QB COUNTERSINK. (1EA) CORROSION ON FUEL ACCESS PLATE 620QB COUNTERSINK WAS REMOVE AND MEASURED AND FOUND ONE HOLE OUT OF LIMITS .609". THEREFORE WAS REPAIRED WITH BUSHING PER SRM 57-10-01.Jul 13, 2016 · N958AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2017010500096Access Panel · corrodedCORROSION ON FUEL ACCESS PLATE 620LB COUNTERSINK. (2EA) CORROSION ON FUEL ACCESS PLATE 620LB COUNTERSINK WAS REMOVED AND MEASURED AND FOUND TWO HOLES OUT OF LIMITS .608" AND .613". THEREFORE WAS REPAIRED WITH BUSHINGS PER SRM 57-10-01.Jul 13, 2016 · N958AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016110108050Cusp Web · corrodedCUSP MEMBRANE AT STA 160-200 RBL 55 HAS CORROSION OUT OF LIMITS. REPAIRED CUSP MEMBRANE AT STA 160-200 IAW ER/A 547490-14 REV 0.Jul 13, 2016 · N960AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016110108049Access Panel · corrodedCORROSION ON DORSAL FIN JUST ON SETTLEMENT AREA OF ACCESS PANEL 370 AL. FABRICATED NEW AND REPLACED IAW SRM 51-41-02, 51-20-09, 51-10-04 PAR 15 AND 21, AND DWG 5911432 REV "CF".Jul 13, 2016 · N958AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2016071605337Shear Tie · crackedRIGHT FUSELAGE, STA 1022, BULKHEAD SHEAR TIE CRACKED IN UPPER RADIUS JUST BELOW LONGERON 16R. REMOVED SHEAR TIE, FABRICATED ATTACH ANGLE, INSTALLED ATTACH ANGLE AND NEW SHEAR TIE IAW SRM 51-41-02 AND PRI 547496-14, REV 0 AND ER/A 547496-14.Jul 13, 2016 · N960AT · Boeing 717200 · Fuselage Internal Mounting StructureSDR DALA2016071505291Frame · crackedDURING REMOVAL OF L17R FOUND CRACK ON FRAME AT STA 1037, L17R. REPAIRED CRACKED FRAME AT STA 1037 L-17R IAW SRM 53-20-07, REPAIR 4.Jul 13, 2016 · N960AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017010500095Access Panel · corrodedCORROSION ON SETTLEMENT AND COUNTERSINK LT FUEL TANK ACCESS PLATE 520FT. CORROSION ON SETTLEMENT AND COUNTERSINK AREA OF FUEL ACCESS PLATE 520FT WAS REMOVED AND MEASURED AND 4 COUNTERSINK WERE FOUND OUT OF LIMITS .664" .667" .665" .670" THEREFORE WERE REPAIREDJul 12, 2016 · N958AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016110108048Access Panel · corrodedCORROSION ON SETTLEMENT AND COUNTERSINK FUEL ACCESS PLATE 520HB. CORROSION ON SETTLEMENT AND COUNTERSINK AREA OF FUEL ACCESS PLATE 520HB WERE REMOVED AND MEASURED AND FOUND OUT OF LIMIT WITH 3 ADJACENT HOLES 0.563", 0.558", 0.555" THEREFORE WAS REPLACED PER SJul 12, 2016 · N958AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016110108047Access Panel · corrodedCORROSION ON SETTLEMENT AND COUNTERSINK FUEL ACCESS PLATE 520LB. CORROSION ON FUEL ACCESS PLATE 520LB WAS REMOVED IAW SRM 51-10-04 AND WAS MEASURED AND FOUND OUT OF LIMITS WITH 3 HOLES ADJACENT 0.553", 0.553", 0.553" THEREFORE WAS REPLACED PER SRM 51-10-04 ANJul 12, 2016 · N958AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016110108046Access Panel · corrodedCORROSION ON COUNTERSINK FUEL ACCESS PLATE 620GB. CORROSION ON SETTLEMENT AND COUNTERSINK AREA OF FUEL ACCESS PLATE NR 620GB WERE REMOVED AND MEASURED AND FOUND OUT OF LIMIT WITH 3 HOLES ADJACENT 0.540", 0.560", 0.560" THEREFORE WAS REPLACED PER SRM 51-10-04 Jul 12, 2016 · N958AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016110108045Access Panel · corrodedCORROSION ON SETTLEMENT AND COUNTERSINK FUEL ACCESS PLATE 620HB. CORROSION ON SETTLEMENT AND COUNTERSINK AREA OF FUEL ACCESS PLATE 620HB WERE REMOVED AND MEASURED AND FOUND OUT OF LIMITS WITH 3 HOLES ADJACENT "0.556" "0.556" "0.556" THEREFORE WAS REPLACED PERJul 12, 2016 · N958AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016071305265Power Supply · inoperativeDURING SERVICE CHECK, FOUND SEVERAL CABIN EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED TWO CABIN EMERGENCY POWER SUPPLIES AND BATTERIES IAW AMM 33-51.Jul 12, 2016 · N893AT · Boeing 717200 · Emergency LightingSDR DALA2016071305264Battery Pack · inoperativeEMERGENCY LIGHTS INOPERATIVE AT ROWS 1 - 14. REPLACED THE BATTERY PACK AT B5-227 IAW AMM 33-51-03.Jul 12, 2016 · N982AT · Boeing 717200 · Emergency LightingSDR DALA2016071305263Beam · crackedCRACKED FWD EDGE BEAM NR 7 AT L1 DOOR. BEAM WAS REPAIRED IAW SRM 52-10-02 REPAIR 13 FIGURE 202.Jul 12, 2016 · N958AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016071205262Frame · crackedCRACKED FRAME BS 693 BETWEE1 LONGERONS 26 & 27R. THE FRAME WAS REPLACED.Jul 12, 2016 · N958AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016110108044Seat Track · corrodedFO'S AFT O/B SEAT TRACK IS CORRODED. REPLACED FO'S AFT O/B SEAT TRACK IAW ER/A 547488-14 REV O.Jul 11, 2016 · N960AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016110108043Cusp Web · corrodedCUSP WEB CORRODED FROM STA 200-STA 218. FABRICATED NEW CUSP WEB MEMBRANE AT FS 200-218 RBL 25-56 IAW SRM 53-10-51 FIG 1 AND 51-40-08 AND PER SAMPLE INSTALLATION OF WEB WILL BE INSTALLED ON NRC 200-0049.Jul 11, 2016 · N960AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016110108042Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE 620JB. CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE 620JB WERE REMOVED AND FOUND OUT OF LIMITS WITH 3 ADJACENT HOLES .555" .545" .545" THEREFORE WAS REPLACED PER SRM 51-10-Jul 11, 2016 · N958AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016110108041Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE 620MB. CORROSION ON COUNTERSINK OF FUEL ACCESS PLATE 620MB WAS REMOVED IAW SRM 51-10-04 AND WAS MEASURED MAX DIAMETER ALLOWED IS 0.532" AND MAX DIAMETER MEASURE IS 0.58" IN 3 HOLES ADJACENT THEJul 11, 2016 · N958AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016110108040Access Panel · corrodedCORROSION ON SETTLEMENT AND COUNTERSINK FUEL ACCESS PLATE 520EB. CORROSION ON COUNTERSINK WAS REMOVED IAW SRM 51-10-04 AND WAS MEASURED AND FOUND OUT OF LIMITS WITH 3 ADJACENT HOLES 0.535" 0.554" AND .540" IAW SRM 57-10-01 MAGNETIC DRIPLESS FUEL MEASURING STIJul 11, 2016 · N958AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016110108039Access Panel · corrodedCORROSION ON SETTLEMENT AND COUNTERSINK FUEL ACCESS PLATE 520MB. CORROSION ON FUEL ACCESS PLATE WAS REMOVED IAW SRM 51-10-04 AND WAS MEASURED ON COUNTERSINK AND FOUND OUT OF LIMITS WITH 3 ADJACENT HOLES 0.554" 0.551" AND 0.549" IAW SRM 57-10-01. MAGNETIC DRIJul 11, 2016 · N958AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016110108038Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE 620EB. CORROSION ON COUNTERSINK OF FUEL ACCESS PLATE 620 EB WAS REMOVED IAW SRM 51-10-04 AND WAS MEASURED MAX DIAMETER ALLOWED IS 0.532 AND MAX DIAMETER MEASURED IS 0.565 IN 3 HOLES ADJACENT THJul 11, 2016 · N958AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016071205261Skin · crackedCRACK ON EXTERNAL FUSELAGE SKIN BS 1022 BETWEE1 LONGERONS 3 - 14L. THE SKIN WAS REPAIRED IAW ER/A 547827-14.Jul 11, 2016 · N958AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016071205260Skin · crackedCRACK ON EXTERNAL FUSELAGE SKIN BS 1037 BETWEEN LONGERONS 13 & 14L. THE SKIN WAS REPAIRED IAW ER/A 547828-14.Jul 11, 2016 · N958AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016071205259Cusp Web · crackedFOUND CUSP WEB CRACKED FROM EOP TRAVELING INBOARD TO LIGHTNING HOLE AT BS 245. CUT OUT THE DAMAGE & REPAIRED THE CUSP WEB IAW SRM 53-00-55, REPAIR 4.Jul 11, 2016 · N960AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016071205258Cusp Web · crackedON INSTALLING OTBD RT SEAT TRACK FOUND CUSP WEB CRACKED FROM EOP TRAVELING INBD TO LIGHTNING HOLE AT BS 245. CUT OUT THE DAMAGE & REPAIRED THE CUSP WEB IAW SRM 53-00-55, REPAIR 4.Jul 11, 2016 · N910AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016103107968Access Panel · corrodedCORROSION ON FUEL ACCESS PANEL COUNTERSINK & SETTLEMENT AREA. THE ACCESS PANEL CANNOT BE REPAIRED UNDER CONDITIONS I AND II THEREFORE WAS REPLACED IAW SRM 57-10-01 STEP 5, C(1).Jul 10, 2016 · N958AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016103107967Access Panel · corrodedCORROSION ON FUEL ACCESS PANEL COUNTERSINK & SETTLEMENT AREA. THE ACCESS PANEL CANNOT BE REPAIRED UNDER CONDITIONS I AND II THEREFORE WAS REPLACED IAW SRM 57-10-01 STEP 5, C(1).Jul 10, 2016 · N958AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016071105254Pan · crackedGALLEY SERVICE DOOR INTERNAL PAN TO WEB IS CRACKED. REPAIRED THE PAN IAW SRM 52-00-00 REP 3.Jul 10, 2016 · N960AT · Boeing 717200 · Galley DoorsSDR DALA2016071005252Frame · crackedCRACKED FRAME BS 674 BETWEEN LONGERONS 25 & 26R . FRAME REMOVED IAW SRM 51-41-02, 51-41-05 AND 51-41-03, REPAIRED IAW SRM 51-70-11 REPAIR 1 AND INSTALLED IAW SRM 51-41-02 AND 51-41-05.Jul 9, 2016 · N958AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016071005251Frame · crackedCRACKED FRAME BS 693 BETWEEN LONGERONS 26 & 27L AT INNER SURFACE OF LOWER FUSELAGE. DAMAGE FRAME WAS REMOVED IAW SRM 51-41-02, 51-41-05, 51-41-03, NEW FRAME WAS DRILLED IAW SRM 51-40-08 AND WAS TREATED AND PAINTED IAW SRM 51-10-04 PER 21 AND 15, NEW FRAME WASJul 9, 2016 · N958AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016071005253Frame · crackedCRACKED FRAME BS 674 BETWEEN LONGERONS 25 & 26L. THE FRAME WAS REMOVED IAW SRM 51-41-02, 51-41-05, 51-41-03, REPAIRED IAW SRM 51-70-11 REPAIR 1 AND INSTALLED IAW SRM 51-41-02 AND 51-41-05.Jul 8, 2016 · N958AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016070905250Longeron · crackedDURING REMOVAL OF SHEAR TIE AT BS 1022, FOUND LONGERON 16R CRACKED. REPAIRED THE LONGERON .Jul 8, 2016 · N960AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2016103107966Cusp Web · corrodedCORROSION ON RT CUSP WEB BS 368. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55 REP. 4 FIG. 212Jul 7, 2016 · N958AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016070805169Power Supply · inoperativeDURING SERVICE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGNS FOR THE OVERWING HATCHES WERE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY PACKS AND THE LIGHTS RETURNED TO AN OPS CONDITION.Jul 7, 2016 · N996AT · Boeing 717200 · Emergency LightingSDR DALA2016070805168Cusp Web · corrodedEXCESSIVE CORROSION ON RT CUSP WEB, STA Y=368, IN REF CARD 24, ZONE 200. CARD 77, ZONE 200. CUSP WEB WAS REPAIRED IAW SRM 53-00-55, REP 4, FIG 212, HFEC INSPECTION WAS ACCOMPLISHED AFTER DAMAGE REMOVAL, FITTING STRAP & SEAT TRACK WERE REMOVED AND INSTALLED IJul 7, 2016 · N958AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016070805167Former · crackedCORROSION ON AFT SIDE OF FRAME 446 AT LONGERON 30. ALSO, TOOLING MARKS ON AFT SIDE OF FRAME 446 FROM LONG 27, LT TO 27 RT. CORROSION ON FRAME AT STA 446, L30. REMOVED AND BLENDED IAW SRM 53-00-00, FIG 103, TOOL MARKS AT STA 446 L27, LT TO 27 RT BLENDED IAW Jul 7, 2016 · N960AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016070805166Pan · wornWEAR RT PAN INTERNAL STRUCTURE NEAR LOWER HINGE ALSO LT SIDE AT AFT CABIEN PRESSURE BULKHEAD EMERGENCY EXIT DOOR. SM, CARD 15, ZONE 820. LT PAN INTERNAL STRUCTURE WAS REPAIRED IAW SRM 52-10-02, REP 15, FIG 201 AND RT PAN INTERNAL STRUCTURE WAS BLENDED OUT, UTJul 7, 2016 · N958AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2016070805165Cusp Web · corrodedEXFOLIATE CORROSION ON LT CUSP WEB FROM STA 976 TO 986, ON REF CARD 32, ZONE 200, CARD 85, ZONE 200. DAMAGE AREA ON LT CUSP WEB FROM STA 976 TO 986 WAS REMOVED AND REPAIRED IAW SRM 53-00-55, REPAIR 4. RII COMPLETED.Jul 7, 2016 · N958AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016070805164Seat Track · corrodedCORROSION OUT OF LIMITS ON RT SEAT TRACK X=44 BETWEEN STA Y=589 TO 645 AT CABIN FLOOR STRUCTURE, CFS, IN REF TO ON RC 20, AC ZONE 200, CARD 74 ZONE 200. RT SEAT TRACK X=44, STA Y=589 TO 645 WAS REPLACED IAW SRM 53-20-52, FIG 1, 51-30-07, FIG 18, SRM 41-41-01.Jul 7, 2016 · N958AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016070805163Cusp Web · corrodedEXCESSIVE CORROSION ON RT CUSP WEB STA Y=401 IN REF CARD 24, ZONE 200, CARD 78, ZONE 200. DUE EXCESSIVE DAMAGE WAS REPAIRED IAW SRM 53-00-55 FIG 225, SHEET 7 OF 10. HFEC INSPECTION WAS ACCOMPLISHED ON RT CUSP WEB, STA Y=401, NO CRACKS WERE FOUND AFTER TRIMMIJul 7, 2016 · N958AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016070805162Cusp Web · corrodedEXCESSIVE CORROSION ON RT CUSP WEB, STA Y=460 IN REF CARD 24, ZONE 200. CARD 79, ZONE 200. DUE TO EXCESSIVE DAMAGE CUSP WEB MUST BE REPAIRED. FASTENERS WERE REMOVED IAW SRM 51-41-02, PAR 7C, DAMAGE WAS REMOVED IAW SRM 53-00-55, HFEC INSPECTION WAS ACCOMPLISHJul 7, 2016 · N958AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016070705155Access Panel · corrodedCORROSION ON SETTLEMENT AND COUNTERSINK OF FUEL ACCESS PLATE NR 520 DB, SM, LW, CARD 58, ZONE 000. CORROSION ON SETTLEMENT AND COUNTERSINK OF FUEL ACCESS PLATE NR 520DB WAS REMOVED AND MEASURED AND FOUND OUT OF LIMITS WITH 3 ADJANCENT HOLES 0.551", 0.540", 0.Jul 6, 2016 · N958AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016070705154Access Panel · corrodedCORROSION ON SETTLEMENT AND COUNTERSINK OF FUEL ACCESS PLATE 520CB, SM, LW, CARD 60, ZONE 000. CORROSION ON SETTLEMENT AND COUNTERSINK AREA OF FUEL ACCESS PLATE NR 520CB WAS REMOVED AND MEASURED AND FOUND OUT OF LIMITS WITH 3 ADJACENT HOLES 0.535", 0.535", 0.Jul 6, 2016 · N958AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016070705153Pan · crackedCRACK ON INNER PAN FORWARD SIDE BETWEEN BEAM 4 TO 5 AT FORWARD LT OVERWING EMERGENCY EXIT, SM, CARD 9, ZONE 820. PAN WAS REPAIRED IAW SRM 52-20-02, FIG 201, LENGTH OF CRACK 0.750".Jul 6, 2016 · N958AT · Boeing 717200 · Emergency ExitsSDR DALA2016070705152Longeron · crackedDURING REMOVAL OF SHEAR TIE AT STA 1022, FOUND LONGERON 17R CRACKED. REPAIRED DAMAGE BY REMOVING DAMAGE SECTION OF LONGERON 17R AT FS 1016- 1053 AND REPLACING WITH SECTION OF LONGERON EXTRUSION AND SPLICE ANGLE IAW SRM 53-00-05, REPAIR 2, FIG 201. APPLIED LOJul 6, 2016 · N960AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2016070705151Channel · crackedCRACKED CHANNEL OF FLOOR PANEL NR 222, SM, CARD 28, ZONE 000. FLOOR PANEL WAS REPAIRED IAW SRM 53-20-50 AND 51-41-02.Jul 6, 2016 · N958AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016070705150Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE 620 AT, AYP, CARD 32, ZONE 600. CORROSION ON COUNTERSINK WAS REMOVED ON FUEL ACCESS PLATE 620 AT IAW SRM 51-10-04 AND DAMAGE WAS FOUND AND FUEL ACCESS PLATE 620 AT WAS REPLACED DUE TO EXCESSIVEJul 6, 2016 · N958AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016070705149Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE 670DT, AYP, CARD 30, ZONE 600. CORROSION ON COUNTERSINK OF FUEL ACCESS PLATE 670DT WAS REMOVED IAW SRM 51-10-04 AND WAS MEASURED AND FOUND OUT OF LIMITS WITH 3 ADJACEND HOLES 0.670", 0.673 AND Jul 6, 2016 · N958AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016070705145Cusp Web · corrodedEXCESSIVE CORROSION ON RT CUSP WEB, STA Y=493 IN REF CARD 24, ZONE 200, CARD 80, ZONE 200. DAMAGED CUSP WEB WAS REPAIRED IAW SRM 53-00-55, FIG 215. HFEC INSPECTION WAS ACCOMPLISHED ON RT CUSP WEB, STA Y=493. NO CRACKS WERE FOUND AFTER TRIMMING OUT IAW NDT SJul 6, 2016 · N958AT · Boeing 717200 · Fuselage Miscellaneous Structure
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