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 DALA2016090906475Intercostal · crackedCRACK ON INTERCOSTAL STA Y=1076 X=-19 Z=5 AT AFT CABIN PRESSURE BULKHEAD. INTERCOSTAL WAS REPLACED IAW DWG 5917579, REV, ED ITEM -325, SRM 51-41-05 AND SRM 51-41-02.SDR DALA2016090906474Frame · crackedCRACK ON FRAMES STA Y=674 AND Y=696 AT LT KEELBEAM AREA, SM NRC 00306. FRAMES WERE REPAIRED IAW SRM 51-70-11, 51-41-02, 51-41-05, AND 51-10-04 PAR 15, 21, 26, AND 37. HFEC INSPECTION WAS ACCOMPLISHED ON FRAMES STA Y=674 AND Y=696 AT LEFT KEELBEAM AREA. NO CSDR DALA2016090906473Frame · crackedCRACK ON FRAMES STA Y=674 AND Y=696 AT RT KEELBEAM AREA, SM NRC 308. FRAMES WERE REPAIRED IAW SRM 51-70-11, 51-41-02, 51-41-05, AND 51-10-04 PAR 15, 21, 26, AND 37. HFEC INSPECTION WAS ACCOMPLISHED ON FRAMES, STA Y=674 AND Y=696 AT RT KEELBEAM AREA. NO CRACSDR DALA2016090906472Frame · crackedCRACKED FRAME 715 BETWEEN LONGERON 27/28 AT KEELBEAM AREA, SM, NRC 00552. FRAME WAS REPAIRED IAW SRM 51-70-11, FIG 201, 51-41-02, 51-41-05, AND 51-10-04, PAR 15,21,26 AND 37. HFEC INSPECTION WAS ACCOMPLISHED ON FRAME STA Y=715 BETWEEN LONGERON 27/28 AT KEEL SDR DALA2016090806456Battery Pack · dischargedMAINTENANCE DETERMINED THAT THE BATTERY FOR THE EMERGENCY PATHWAY LIGHTING IN THE TAIL COMPARTMENT WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK FOR THE NOTED AREA AND THE OPS CHECK WAS GOOD.SDR DALA2016090806455Pan · gougedFORWARD CARGO DOOR PAN GOUGED ABOVE FORWARD DOOR HOLD OPEN HOOK. CLEANED UP GOUGES ON FORWARD CARGO DOOR PAN ABOVE FORWARD DOOR HOLD OPEN HOOK IAW SRM 52-00-00, FIG 103, 52-30-02, PG 1. REMOVED .014 OF .050 BEYOND ALLOWABLE LIMITS, TAG 2721. REPAIRED DOOR PSDR DALA2016090806454Channel · crackedCRACK ON GENERATION FLOOR CHANNEL NR 221, TF, SM, NRC 00226. CRACK WAS STOP DRILLED. DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-41-02, SRM 51-20-09, AND SRM 53-20-50, REPAIR 5, FIG 202. HFEC INSPECTION WAS PERFORMED AT END OF CRACK. NO CRACKS WERE FOUSDR DALA2016090706402Battery Pack · dischargedDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 19, IN THE CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK FOR THE NOTED LIGHTED AREA AND THE OPS CHECK WAS GOOD.SDR DALA2016110208150Cusp Web · corrodedEXCESIVE CORROSION ON CUSP WEB BS 911-913 AND X -54 TO -60 . DAMAGE WAS REMOVED AND A REPAIR WAS FABRICATED IAW SRM 53-00-55 RAPAIR 4 FIG 216.SDR DALA2016090706457Battery · dischargedDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGN FOR THE AFT EXIT DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY SUPPLY AND THE OPS CHECK WAS GOOD.SDR DALA2016090706401Access Panel · damagedELONGATED HOLE ON FUEL ACCESS PLATE 520LB, SN 575. HOLE WAS REWORKED IAW SRM 57-10-01, PAR 5, CONDITION II, 3. HOLE AND COUNTERSINK WERE MEASURED WITH ID 0.3435" AND COUNTERSINK 0.613" THEREFORE WITHIN LIMITS OF REPAIR IAW SRM 57-10-01, PAR 5 CONDITION II. SDR DALA2016090706400Web · wornWEAR ON LOWER WEB LT SIDE INTERNAL STRUCTURE AT AFT CABIN BULKHEAD VENTRAL DOOR, SN 594, DUE TO EXCESSIVE DAMAGE, WEAR ON LOWER WEB LT SIDE INTERNAL WILL BE REPAIRED. RETAINERS WERE REMOVED IAW SRM 51-41-01, LOWER WEB ON LT SIDE. INTERNAL STRUCTURE WAS MEASUSDR DALA2016090606471Skin · damagedFUSELAGE SKIN BS 207-220 18R-21R DAMAGED. INSTALLED PERMANENT SKIN REPAIR IAW ER/A 549610-14, REV 0.SDR DALA2016090606452Skin · crackedREPAIRED LT FUSELAGE EXTERIOR SKIN CRACK AT STA 1095 JUST ABOVE LONGERON 14L IAW ER/A 547512-14. FAA STAGE III APPROVAL REQUIRES INITIAL AND RECURRING GENERAL VISUAL INSPECTIONS THAT BEGIN AND ARE REPEATED EVERY 3000 CYCLES IAW ER/A 547512-14. ACCOMPLISH SECSDR DALA2016090606385Cusp Web · corrodedWHILE GAINING ACCESS TO L/L REPAIR, FOUND CUSP WEB MEMBRANE CORRODED AT STA 200-218, RBL 56-RBL44. FABRICATED NEW CUSP WEB IAW DWG 9936535. ALODINED, PRIMED, TOP COATED NEW CUSP WEB IAW AMM 51-10-00 370-803. INSTALLED NEW WEB IAW SRM 51-41-02, SEC 4 AND 51-4SDR DALA2016090506384Cusp Web · corrodedEXCESSIVE CORROSION ON CUSP WEB BETWEEN STA 478-STA 481 BETWEEN X-54--60 ON REF SN CARD 300, SN 00548. DAMAGE WAS REMOVED IAW SRM 53-00-55, HFEC INSPECTION WAS ACCOMPLISHED IAW NDT, SPM 06-10-01.001 ALONG TRIM LINE AND NO CRACKS WERE FOUND. REPAIR PARTS WAS SDR DALA2016090606386Battery Pack · dischargedDURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING AT ROW 20 WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.SDR DALA2016090506383Angle · damagedDAMAGED ON LOWER ANGLE AT RT CUSP WEB BETWEEN STA Y=579 AND STA Y=598 AND X=-54 AND X=-60 AT PASSENGER CAB, SN 00300. SPLICE WAS REMOVED DUE TO EXCESSIVE CORROSION IAW SRM 51-41-05, AND NEW SPLICE WAS FABRICATED AND INSTALLED IAW SRM 53-20-01, FIG 51-20-09 ANSDR DALA2016090706453Cusp Web · corrodedCUSP WEB MEMBRANE CORRODED BEYOND LIMITS AT STA 200-160, RBL 54. REMOVED AND TRIMMED CUSP MEMBRANE STA 160-200 IAW SRM CHAPTER S1 & ER/A 549606-14. PERFORMED HFEC OF CUTOUT AREA IAW NON DESTRUCTIVE TESTING STANDARD PRACTICE MANUAL PART 6 PRECEDURE 06-10-01.0SDR DALA2016090506399Floor Support · corrodedFLOOR SUPPORT AT STA HAS CORROSION AT MARKED LOCATIONS ON REPAIR RACK BLEND CHECK LIMITS. BLEND FLOOR SUPPORT STA 200 IAW SRM 51-10-04. ORIGINAL .070 REMAINING .042 OUT OF LIMITS IAW B DWG S00074, TAG 6887. FABRICATED FLOOR SUPPORT IAW SRM 51-20-09. TREATESDR DALA2016090506382Cusp Web · corrodedCUSP WEB RBL 44-58, STA 218-237 IS CORRODED AT MARKED LOCATIONS. CLEAN AND RE-EVALUATE. CUSP WEB, RBL 44-58, STAS 218-237 WAS BLENDED AND FOUND TO BE OUT OF LIMITS. REPLACED CUSP WEB IAW SRM 51-41-02, PG 3, PAR F, TAG 12663.SDR DALA2016090406378Pan · crackedCRACK ON RT RING PAN AFT UPPER CORNER, STA Y= 832 AT CABIN PASSENGER RT SIDE, SN 00206. DAMAGE WAS REMOVED IAW SRM 56-20-02, REPAIR 1, FIG 202, SHEET 3 AND INSPECTION NDT CHECK FOR CRACKS ON STA Y=832 CABIN PASSENGER RT SIDE. NO CRACKS WERE FOUND. REPAIR PASDR DALA2016090406377Pan · crackedCRACK ON LT RING PAN FWD LOWER CORNER, STA Y= 598 AND Y= 889 AT CABIN PASSENGER LEFT SIDE, S/N 00207. DAMAGE WAS REMOVED IAW SRM 56-20-02 REPAIR 1, FIG 202, SHEET 3 AND INSPECTION NDT CHECK FOR CRACKS ON STA Y=598 AND 889 AT CABIN PASSENGER LT SIDE. NO CRACKSDR DALA2016090406376Pan · crackedCRACK ON RT RING PAN FORWARD UPPER CORNER, STA Y= 636 AND Y= 696 AT CABIN PASSENGER RT SIDE, SN 00203. DAMAGE WAS REMOVED, IAW SRM 56-20-02, REPAIR 1, FIG 202, SHEET 3 AND INSPECTION NDT CHECK FOR CRACKS ON STA Y=636 AND 696 AT CABIN PASSENGER RT SIDE, NO CRASDR DALA2016090406375Door Frame · crackedFORWARD RT SERVICE DOOR LOWER HORIZONTAL FRAME CRACKED AT LOWER DOOR HINGE. REPLACE LOWER FRAME. REMOVED CRACKED FRAME AND REPLACED WITH FABRICATED FRAME, PN 9911582-21 IAW DWG 9911582, REV T AND SRM 57-41-01, FABRICATION CERTIFICATE OF CONFORMANCE AMES REF SDR DALA2016090506388Attach Angle · corrodedSEAT TRACK ATTACH ANGLE RBL 56, STA 200-214 HAS CORROSION AND DAMAGED FASTENER HOLES. BLEND CHECK LIMITS. SEAT TRACK ATTACH ANGLE RBL 56, STA 200-214 FASTENER HOLES FOUND TO BE OUT OF LIMITS. REPLACEMENT ATTACH ANGLE WAS MATCH DRILLED IAW SRM 51-40-08, PG 1,SDR DALA2016090506381Attach Fitting · corrodedBULKHEAD TO LONGERON ATTACH CLIP AT STA 1087, LONGERON 20R CORRODED. BLEND CHECK LIMITS. REPLACED BULKHEAD TO LONGERON ATTACH CLIP -51 AT STA 1087, L20R IAW SRM 51-41-02 AND 51-10-04, PARA 26 AND 51-41-05, PG 17, PARA 8.SDR DALA2016090506380Tip Cap · damagedL/E RT WING OTBD OF NR 5 SLAT AT WING TIP HAS SLAT, WING TIP, AND WING L/E CHAFING. CHECK LIMITS. L/E R/W OTBD NR 5 SLAT REMOVED IAW SRM 51-41-02 DUE TO GOUGE AND WAS OUT OF LIMITS .025. REMOVED ORIGINAL THICKNESS WAS .063, TAG 2721 IAW SRM 57-00-00, FIG 103SDR DALA2016090506379Slat · gougedL/E RT WING OTBD OF NR 5 SLAT AT WING TIP HAS SLAT, WING TIP, AND WING L/E CHAFING. CHECK LIMITS. L/E RT WING OTBD NR 5 SLAT REMOVED IAW SRM 51-41-02 DUE TO GOUGE AND WAS OUT OF LIMITS .025. REMOVED ORIGINAL THICKNESS WAS .063, TAG 2721 IAW SRM 57-00-00, FISDR DALA2016090306374Former · crackedALL 3 RT CANTED KEEL FORMERS ARE CRACKED ON OTBD ENDS AT STA 674, 696, AND 714. REMOVED AND REINSTALLED FOR CANTED KEEL FORMERS ON OTBD ENDS AT STATIONS 674, 696, AND 714 IAW SRM 51-41-02 AND SRM 51-41-05. REPAIRED DAMAGE TO CANTED KEEL FORMERS ON OTBD ENDS SDR DALA2016090206349Beam · crackedCRACK AT FWD CARGO COMPARTMENT DOOR PAN UPPER EDGE ON STA 389, UPPER EDGE OF BEAM 5, SN 00529. PAN UPPER EDGE ON STA 389 UPPER EDGE OF BEAM 5 WAS REPAIRED IAW SRM 52-30-02, REPAIR 1, FIG 201, LENGTH CRACK: 2.100".SDR DALA2016090206348Beam · crackedCRACK AT FWD CARGO COMPARTMENT DOOR PAN UPPER EDGE STA 408 UP OF BEAM 5 SN 00530. PAN UPPER EDGE ON STA 408 UP OF BEAM 5 WAS REPAIRED SRM 52-30-02, REPAIR 1, FIG 201, LENGTH CRACK: 2.400".SDR DALA2016090106318Frame · crackedCRACKED FRAME BS 1474 AND X -20. THE FRAME WAS REPAIRED IAW SRM 53-01 FIG. 2, 51-30-2 AND 51-30-5.SDR DALA2016090106317Frame · corrodedCORROSION ON LOWER SECTION OF A FRAME AT BS 889, LONGERONS 25 - 28R IN THE AFT CARGO. BLENDED TO REMOVE CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-00-00 FIG 103. FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM 53-20-07 REPAIR 3.SDR DALA2016F00176Spoiler · delaminatedDURING UNSCHEDULED MAINTENANCE CHECK RT OTBD SPOILER, FOUND DELAMINATED.SDR DALA2016090206398Rib · crackedFORWARD CARGO DOOR HAS CRACKED RIBS ON LOWER SIDE IN 2 PLACES. MARKED, FABRICATED, -41 WEB AND -43 ANGLE FOR LOWER FORWARD AND AFT RIBS IAW BP 9957664. PROTECTIVE TREATMENT APPLIED IAW SRM 51-10-04, TABLE 1 AND DPSM 900-3-6, NR 34. INSTALLED FORWARD AND AFTSDR DALA2016083106292Longeron · damagedAFTER REMOVAL OF LIFE LIMITED REPAIR, FOUND LONGERON 19R HOLES TO BE DAMAGED AT STA 207-218. REPLACED LONGERON 19R STA 188-218 IAW SRM 51-41-02 AND 51-41-05 FABRICATED NUT CHANNEL AND .063 SPLICE IAW SRM 53-00-55, REPAIR 2.SDR DALA2016083006264Stringer · damagedPROTECTIVE COATING MISSING FROM LONGERON L-29L, STA 932. POSSIBLE CORROSION. REPAIRED DAMAGED AREA BY BLENDING IAW 53-00-00, FIG 103 AND INSTALLING REPAIR U-CHANNEL DOUBLER OVER AREA IAW SRM 53-00-05, REPAIR 3, FIG 201. ORIGINAL THICKNESS .125" REMOVED .031SDR DALA2016083006263Shear Tie · crackedSHEER TIE CLIP ON THE FWD SIDE OF STA 1002, BULKHEAD AT LONGERON 14R IS CRACKED. REPLACED SHEAR TIE CLIP ON THE FWD SIDE OF STA 1022 BULKHEAD 14R IAW SRM 51-41-05, 51-41-02, PAL-4.SDR DALA2016083006262Cusp Web · crackedRIGHT CUSP WEB CRACKED AT LIGHTNING HOLE FUSELAGE STA 807, MARKED. REPLACED CUSP WEB AT RT FLOOR FUSELAGE STA 807 IAW SRM 51-41-01, 51-41-05, 51-41-08.SDR HALA2016082800337Proximity Sensor · out of adjustAFTER TAKE OFF WHEN GEAR WAS RETRACTED LEFT MAIN GEAR "UNSAFE" "RED" LIGHT ILLUMINATED WITH GEAR HANDLE IN UP POSITION. FOUND LEFT MLG UP AND LATCHED PROXIMITY SENSOR SPRING BROKEN. REMOVED AND REPLACED SPRING. ADJUSTED PROXIMITY SENSOR IAW AMM 32-61-00. OPSDR DALA2016082806240Light · missingDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY EXIT IDENTIFIER IN THE FLOOR AT SEAT 19AB IN THE CABIN WAS MISSING, AND INOPERATIVE. MAINTENANCE INSTALLED THE FLUORESCENT STRIP FOR THE NOTED AREA AND THE OPS CHECK WAS GOOD.SDR DALA2016082706239Cusp Web · corrodedRIGHT CUSP WEB RBL 60, STA 389-STA 408 CORROSION FOUND TO BE OUT OF LIMITS. REPAIR CORRODED CUSP WEB BY REMOVING AND REPLACING DAMAGE SECTION OF CUSP WEB FROM FS 370 TO FS 440 IAW SRM 53-00-55, REPAIR 4, FIG 223, USING SECTION OF CUSP WEB, PN 9930538475. APPSDR DALA2016082606209Shear Tie · crackedSHEAR TIE CRACKED AT LONGERON L15, STA 1022, MARKED. REPLACED SHEAR TIE AT LONGERON 14L, STA 1022 BULKHEAD IAW SRM 51-41-05, PG 1.SDR DALA2016082606208Frame · crackedFRAME FORMER ON THE AFT SIDE OF STA 1022, BULKHEAD AT LONGERON 7L IS CRACKED. REPAIRED FRAME FORMER ON THE AFT SIDE OF STA 1022, BULKHEAD AT 7L LONGERON IAW SRM 51-70-11, REPAIR 1 .SDR DALA2016082606207Shear Tie · crackedSHEER TIE CLIP ON THE FWD SIDE OF STA 1022 BULKHEAD AT LONGERON 7L IS CRACKED. REPLACED SHEAR TIE CLIP ON FWD SIDE OF STA 1022 BULKHEAD AT LONGERON 7L IAW SRM 51-41-05, PG 1.SDR DALA2016082606206Intercostal · crackedFORWARD CARGO FUSELAGE STA 636, BL0 INTERCOSTAL CRACKED. REPAIRED CRACK IAW SRM 53-00-00, REPAIR 1, FIG 201 & SRM 51-41-05, PG. 17, NR 8.SDR DALA2016082506196Door Frame · crackedRIGHT FORWARD GALLEY SERVICE DOOR, LOWER FORWARD CORNER, LOWER HORIZONTAL FRAME CRACKED. REPLACED GALLEY SERVICE DOOR LOWER HORIZONTAL FRAME IAW SRM 51-41-02, 51-41-05, B DWG 5910084, REINSTALLED R1 DOOR IAW AMM 52-42-01 000-801, 52-42-01 400-801, PRESSURE CHSDR DALA2016082506195Cusp Web · corrodedRIGHT CUSP WEB STA 936-946, RBL 60 HAS CORROSION. BLENDED OUT ALL SIGNS OF CORROSION. TREATED AND PRIMED AREAS OF REPAIR, BLEND IAW SRM 51-10-04, MATERIAL LOSS WAS OUT OF LIMITS AT RT CUSP WEB STA 936-946, RBL60, FABRICATED, DRILLED, AND INSTALLED A PRIMARY SDR DALA2017010500109Seal Depressor · damagedFOUND AFT LOWER SEAL DEPRESSOR TO BE DAMAGED. COMPLIED WITH PRI 549608-14, AND ER/A 549608-14. BY FABRICATING PROTECTING & INSTALLATION OF AFT SEAL DEPRESSOR ON AFT CARGO DOOR CUTOUT.
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