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.
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 HALA2023031400008Unknown · unknownANTI SKID FAIL - ON APPROACH TO OGG. OK TO CONTINUE PER MEL 32-45-01 MDDR #401785. PLACARD INSTALLED. MIC UPDATED. PERFORMED FIM 32-41 TASK 805. RTS PASSED NO CURRENT FAULTS NOTED. THIS CLEARS MEL. PLACARD REMOVED, MIC SHEET UPDATED. OK FOR SERVICE.SDR DALA2023031401857Unknown · unknownTHE R1 EXIT EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE.MAINTENACE REPLACED THE BATTERY B5-259 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #4072112)SDR DALA2023031401847Unknown · unknownCORROSION ON LONGERON 18RH AT R1 PASSENGER DOOR (AFT EDGE). SUMMARY OF NRC 00479: CORROSION LEVEL: 2. LONGERON 18RH AT R1 PASSENGER DOOR (AFT EDGE) WAS REPAIRED PER ER/A 605807-14 REV ORIGINAL SECTION I, PERMANENT REPAIR AND PRI 605807-14 REV 4. ASSOCIATED ER/SDR DALA2023031401846Unknown · unknownAFT SPLICE BTW L-28R TO L-28L REMOVAL, FOUND CRACK ON SPLICE FRAME AT STA 636. SUMMARY OF NRC 00244: SPLICE FRAME AT STA 636 WAS REPAIRED PER B-717-200 SRM 51-70-11-2R PROCEDURE 2 REPAIR 2. (LP #2664206)SDR DALA2023031001761None · noneLMLG FIXED STRUT O/B ATTACH FITTING WORN ON FWD AND AFT FACES. SUMMARY SEE NRC 008-0003:3211-4001/001 00006: REPAIRED PER CMM 57-40-1. (LP #2663943)SDR DALA2023031001760None · noneRMLG FIXED STRUT O/B ATTACH FITTING WORN ON FWD AND AFT FACES. SUMMARY SEE NRC 006-0003:3211-4004/001 00007: REPAIRED PER CMM 57-40-1. (LP #2663936)SDR DALA2023031401845Unknown · unknownCORROSION WAS FOUND ON FWD PASSENGER DOOR STAIRWELL INTERNAL STRUCTURE IN REF NRC 2060-1001. SUMMARY OF NRC 00572: CORROSION LEVEL 2. FWD PASSENGER DOOR STAIRWELL WAS REPLACED WITH SERVICEABLE STAIRWELL PER B717-200 AMM 52-63-01. TOOL USED CALIBRATED STD DUE DSDR DALA2023031001759None · noneCRACKED RH CUSP WEB BTW STA Y=918-925 AND Y=935-942 AT PASSENGER CABIN. SUMMARY OF NRC 00489: CORROSION LEVEL 2. CUSP WEB RH BTW STA Y=918-925 AND Y=935-942 WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 REPAIR 4 PAR 5 B FIG 216. (LP #2661740)SDR DALA202303094717DDisc · cracked1 AXIAL CRACK IN AIR SEAL F AREA (ABOVE DIA 15-2) MEASURING ~0.340 INCH
1 CIRCUMFERENTIAL CRACK IN AIR SEAL F AREA (BELOW DIA 15-2) MEASURING ~0.100 INCHSDR DALA2024071807235Skin · dentedDENT & 3/8" HOLE IN FLAP SKIN AFT OF LT MAIN LANDING GEAR. PER ERA 606778-14 REV ORIGINAL, SEC 1 ACCOMPLISHED DETAILED VISUAL INSPECTION, NO DAMAGE BEYOND PUNCTURE, NO LOOSE, MISSING, OR PULLED FASTNERS. COMPLIED WITH PERMANENT REPAIR OF FLAP OF ERA 606778-14 SDR HALA2023031400006Unknown · unknownINTERMITTENT L HYD PUMP FAIL. REMOVED AND REPLACED LH ENGINE DRIVEN HYD PUMP PER B717 AMM 29-11-01. CONDITION SAME. REMOVED AND REPLACED LH ENGINE EDP LOW PRESSURE SWITCH PER B717 TSM 29-10 TASK 801. NO FAULTS NOTED. OPS CHECK NORMAL. OK FOR SVC.SDR DALA2023030801720None · noneAFTER DOOR ASSEMBLY, CORROSION WAS FOUND ON SETTLEMENT AREA AT DOOR PANEL P/N 5971074. SUMMARY OF NRC 0240: LEVEL CORROSION 2. (UT) THICKNESS MEASUREMENT WAS ACCOMPLISHED ON SETTLEMENT AREA AT DOOR PANEL. WAS MEASURED WITH AN ORIGINAL THICKNESS OF 0.090 IN. RESDR DALA2023030701661None · noneCORROSION ALONG LONGERON L30 FROM STA Y=900 TO Y=1022 AT AFT CARGO COMPARTMENT C2. SUMMARY OF NRC 00178: CORROSION LEVEL 2. NEW SECTION LONGERON L30 FROM STA Y=900 TO Y=1022 WAS INSTALLED PER B717-200 SRM 51- 41-05-0G. (LP #2658653)SDR DALA2023030701660None · noneCORROSION ON LONGERION 30 RH BTW STA Y=1031 TO STA Y=1053 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00195: CORROSION LEVEL 2. LONGERON SECTION 30 FROM STA Y=1022 TO Y=1053 AT AFT CARGO COMPARTMENT C2 WAS REPLACED PER B717-200 SRM 51-41-05-0G STEP 8. AND 51-41-0SDR DALA2023030701659None · noneCORROSION ON RH/LH TRACKS (RH) FROM STA Y=813 TO STA Y=896 AND (LH) TRACK FROM STA Y=813 TO STA Y=947 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00682: CORROSION LEVEL 2. RH/LH TRACKS (RH) FROM STA Y=813 TO STA Y=896 AND (LH) TRACK FROM STA Y=813 TO STA Y=947 ATSDR DALA2023030801721None · noneSHIP 9571 -HYD/DE- THE FLIGHT CREW DECLARED AN EMERGENCY INTO ATL DUE TO THE "RIGHT HYDRAULIC LOW-PRESSURE" MESSAGE. THE ALTERNATE GEAR EXTENSION PROCEDURES WERE UTILIZED, AND THE LANDING WAS UNEVENTFUL. CORRECTIVE ACTION: MAINTENANCE REPLACED THE RIGHT HYDRAUSDR DALA2023030701662None · noneTHE AISLE OVERHEAD EMERGENCY LIGHT COVER IS MISSING AT ROW 3. MAINTENANCE INSTALLED A NEW COVER. OK FOR SERVICE. (LP #9677521)SDR DALA2023030801719None · noneFOUR (4) CRACKS WERE DISCOVERED ON THE FUSELAGE SKIN. SUMMARY OF NRC 00157: PERMANENT REPAIR ON FUSELAGE SKIN WAS ACCOMPLISHED PER ER/A 566828-14 REV. B SECTION III: DAMAGE TOLERANCE PERMANENT REPAIR AND PRI 566828-14, REV. 3 AND ACCOMPLISH SECTION IV: GENERALSDR DALA2023030701658None · noneCORROSION ON FUSELAGE SKIN ON STA Y=1053 BTW STR 29 LH TO STR 29 RH AT AFT CARGO COMPARTMENT. CORROSION WAS FOUND ON PRODUCTION DOUBLER. SUMMARY OF NRC 00241: CORROSION LEVEL 2. DOUBLER ON STA 1053 BTW LONGERON 28RH TO 28LH WAS REPLACED PER B717 SRM 51-41-02-0SDR DALA2023030701657None · noneCORROSION ON FINGER DOUBLER ADJACENT TO L-26LH, STA Y=1010 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00673: CORROSION LEVEL 2. FINGER DOUBLER ADJACENT TO L-26LH, STA Y=1010 AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-03-01-2R PROCEDURE 1 REPAIR 1 SDR DALA2023030301615None · noneCORROSION ON FRAME CLIP ON AFT CARGO COMPARTMENT C2 STA Y=908 BTW LONG L30/L29. SUMMARY OF NRC 00174: CORROSION LEVEL 2. SECTION ON FRAME CLIP ON AFT CARGO COMPARTMENT C2 STA Y=908 BTW LONG L30/L29 WAS REPAIRED PER B717-200 SRM 53-00-06-2R-2. (LP #2652378)SDR DALA2023030201557None · noneCABIN STANDBY EMERGENCY LIGHTING IS MISSING TWO LENS COVERS (LOC ROW 22 AND 26). FORWARD MISSING CABIN STANDBY EMERGENCY LIGHTING TO MEL 33-52-01. PLACARDS INSTALLED. (LP #4154618)SDR DALA2023030201556None · noneCORROSION ON LONGERON 30, BTW STA Y:946 AND STA Y:974 AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00255: CORROSION LEVEL 2: LONGERON 30 BTW STA Y:946 AND STA Y:974 AT AFT CARGO COMPARMENT WAS PERMANENTLY REPAIRED PER B-717-200 SRM 53-20-05 REPAIR 1 PAR. 4 FIG. 201SDR DALA2023030201555None · noneSKIN PANELS BTW STA 954 TO STA 974 LONG 30 TO R29 ARE CORRODED OUT OF LIMITS. WITH ORIGINAL THICKNESS OF 0.071 IN. AND THE MAXIMUM REMOVED MATERIAL FOUND IS 0.033 IN. THEREFOR AREA IS OUT OF LIMITS IN REF NRC 00192 AT AFT CARGO (C2). SUMMARY OF NRC 00512: CORRSDR DALA2023030201554None · noneCORROSION ON INTERCOSTAL AT STR 30 BTW STA Y=1022 TO STA Y=1037 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00193: CORROSION LEVEL 2. INTERCOSTAL AT STR 30 BTW STA Y=1022 TO STA Y=1037 WAS REPLACED PER B-717 SRM 51-41-02-0G AND SRM 51-41-05-0G. (LP #2651008)SDR DALA2023030201553None · noneCORROSION ON FRAME CLIP AND SKIN ON AFT CARGO COMPARTMENT C2 STA Y=1022 BTW LONG L30. SUMMARY OF NRC 00182: CORROSION LEVEL 2. SECTION ON FRAME CLIP AFT CARGO COMPARTMENT C2 STA Y=1022 BTW LONG 29RH TO 29LH WAS REPAIRED PER B717-200 SRM 53-00-06-2R-2 FIG 201 ASDR HALA2023031400007Unknown · unknownGEAR WOULD NOT COME UP ALONG WITH LOUD GRINDING LIKE NOISE AND VIBRATION COMING FROM NOSE GEAR. RETURNED TO HNL. PERFOMED EXT/RET OF NOSE GEAR MULTIPLE TIMES PER AMM 32-30-00. LUBRICATED NOSE GEAR AMM 12-21-01. FOUND NOSE TIRES UNEVEN. REPLACED TIRES PER AMSDR DALA2023030201551None · noneFOUND DAMAGE AFT CARGO DOOR OPENING. AFT SIDE SEAL RETAINER SPLICE ANGLE CRACKED NEAR TEFLON GUIDE. REMOVED AFT DEPRESSOR SPLICE PER B717 SRM 53-20-15-2R-10. REPAIRED JAMB SEAL DEPRESSOR PER B717 SRM 53-20-15-2R-4. OK FOR SERVICE. (LP #9493774)SDR DALA2023030101525None · noneSEVERAL DENTS ON AFT MOVABLE FLAP VANE (LOWER SURFACE) AT LH WING (AI). SUMMARY OF NRC 00160: DENTS (26 EAS) ON AFT MOVABLE FLAP VANE (LOWER SURFACE) AT LH WING WERE FOUND AND EVALUATED AS FOLLOWS, WHERE, L=LENGTH, W=WIDTH, Y=DEPTH, AND W/Y MUST BE 10 OR MORE,SDR DALA2023022701429None · noneTHE R1 DOOR EMERGENCY INDENTIFIER SIGN LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY ASSEMBLY PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #9493766)SDR DALA2023030101526None · noneFOUND LOWER AFT CORNER OF L1 DOOR DAMAGED AFTER AIRCRAFT ARRIVAL. INSPECTED DAMAGE AREA. REMOVED REQ FASTENERS AND CUT OUT DAMAGE PER B717 SRM 52-10-01-2R-1. PREFORMED DAMAGE CONTAINMENT REF NDT SPM 06.10.01.001 PROCEDURE 1 NO DEFECTS AND OPEN HOLE REF NDTSPM SDR DALA2023022701431None · noneFOUND 2 HOLES WITH CRACK INDICATIONS ON LH VERT STAB FRONT SPAR CAP FWD FLANGE, REF AA 5530-01048 AND AD 2018-10-08. REMOVED LH FASTENERS FROM VERT LEADING EDGE. REMOVED VERT LEADING EDGE PER B717 AMM 55-32-01. C/W BHEC OF SEPERATED LAYERS, FOUND CRACK INDICATSDR DALA2023022701428None · noneCRACKED PAN ON AFT EDGE BELOW STOP FITTING #2 AT PASSENGER ENTRANCE DOOR INTERNAL STRUCTURE. SUMMARY OF NRC 00235: PAN ON AFT EDGE BELOW STOP FITTING #2 AT PASSENGER ENTRANCE DOOR INTERNAL STRUCTURE WAS REPAIRED PER B717-200 SRM 52-10-02-2R REPAIR 3. (LP #2644SDR DALA2024121311699Skin · damaged-AD- AMOC 606161-14AD - B717-200 VERTICAL STABILIZER LEADING EDGE SKIN ZFS 52.267 OVERSIZE HOLES. REPAIR APPROVAL IS LIMITED TO TWENTY-FOUR (24) MONTHS SERVICE FROM DATE OF APPROVAL ONLY. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIRED FOR CONSDR DALA2023022701430None · noneFLOOR NEAR 1ST CLASS COAT CLOSET SEEMS SOFT. REMOVED AND FABRICATED FLOOR PANEL PER B717 AMM 53-21 AND SRM 53-20-50 PG 2. FIG 3. FOUND SUPPORT ANGLE BROKEN AT STA 237. REMOVED, FABRICATED, DRILLED UP, PRIMED, AND PAINTED A NEW SUPPORT ANGLE. INSTALLED FLOOR SUSDR DALA2023022501420None · noneCRACKED BEAM ON AFT SECTION BELOW STOP FITTING #2 AT PASSENGER ENTRANCE DOOR INTERNAL STRUCTURE. SUMMARY OF NRC 00236: BEAM ON AFT SECTION BELOW STOP FITTING #2 AT PASSENGER ENTRANCE DOOR INTERNAL STRUCTURE WAS REPAIRED PER B717-200 SRM 52-10-02-2R REPAIR 8. (SDR DALA2023030201550None · noneFOUND SKIN DAMAGE AT C-2 DOORWAY JAMB EDGE AT DOOR CUT OUT SURROUND AREA BELOW DOOR STOP #2. SUMMARY SEE NRC 003-0001:0514-2001/003 00003: COMPLIED WITH ER/A PRI 606111-14 REV'S "0","1","2","3" AND ALL REPAIR INSTRUCTIONAL STEPS ARE COMPLETED, ENSURED FINAL ERSDR DALA2023022501422None · noneLT SLANT PANEL HAS CORROSION ON IT AT NUT PLATE LOCATION SEEN FROM THE INSIDE. BOTTOM ROW APPROX. LBL27. SUMMARY SEE NRC 001-0196:5300-2005/001 00276: COMPLIED WITH ER/A PRI 606032-14 REV "0","1" INSTRUCTIONAL STEPS. ENSURED FINAL ER/A 606032-14 REV ORIG SECTISDR DALA2023022501419None · noneRE-WRITE TO NRC #00493: DUE TO INADEQUATE STEERING OF THE RELATED STATIONS. THIS NRC IS TO CLARIFY THE CORRECT LOCATION FOR EACH STRUCTURAL ELEMENT. CORROSION ON FLOOR STRUCTURE SUPPORTS ALONG FWD DIAPHRAGM AT CPAX BTW STA. Y=157 TO Y=200; AND BTW BL (X)=45 (-SDR DALA2023022501418None · noneAFTER REMOVAL OF FORWARD JAM PAN SEALS,CRACK WAS FOUND ON THE FWD SEAL. SUMMARY OF NRC 00626: REPAIR DOUBLER WAS INSTALLED PER B717-200 SRM 53-00-00-2R PROCEDURE 1 REPAIR 1 AND SRM 51-41-02-0G. (LP #2642198)SDR DALA2023022501417None · noneCORROSION ON FLOOR STRUCTURE SUPPORTS ALONG FWD DIAPHRAGM AT CPAX, BTW STA Y=200 TO Y=237 AND BL (-X)=55. SUMMARY OF NRC 00518: CORROSION LEVEL 2. FLOOR STRUCTURE SUPPORTS ALONG FWD DIAPHRAGM AT CPAX, BTW STA Y=200 TO Y=237 AND BL (-X)=55 WERE REPLACED PER B71SDR DALA2023022401416None · noneCRACKS (3 EA) ON FRAMES AT LH CANTED KEEL STA Y=674, Y=696, AND Y=715, (-X)=27. SUMMARY OF NRC 00319; FRAMES (3 EA) AT LH CANTED KEEL STA Y=674, Y=696, AND Y=715, (-X)=27. WERE REPAIRED PER B717-200 SRM 51-70-11-2R REPAIR 1. (LP #2642292)SDR DALA2023022401413None · noneCRACKS (2 EA) ON FRAMES AT RH CANTED KEEL STA Y=696 AND Y=715, (X)=27. SUMMARY OF NRC 00320: FRAMES (2 EA) AT RH CANTED KEEL STA Y=696 AND Y=715, (X)=27. WERE REPAIRED PER B717-200 SRM 51-70-11-2R REPAIR 1. (LP #2642050)SDR DALA2023022701432Panel · damagedPANEL DAMAGED AND BENT. REPAIRED AND FABRICATED PANEL.SDR DALA2023022401415None · noneCORROSION ON SEAT TRACKS STA Y=200-237 X=-22, STA Y=200-218 X=-44.5 AND STA Y=200 X=22 (CPAX)( W1). SUMMARY OF NRC 00425: CORROSION LEVEL 2. CORROSION WAS REMOVED ON SEAT TRACKS STA Y=200-237 X=-22, STA Y=200-218 X=-44.5 AND STA Y=200 X=22 PER B717-200 SRM 51-SDR DALA2023022401414None · noneCRACK ON PAN, FWD/UPPER INNER SIDE NEAR TO BEAM 5 OF FWD CARGO COMPARTMENT DOOR. (C1) SUMMARY OF NRC 00541: PAN FWD/UPPER OF FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1 FIGURE 201. (LP #2640421)SDR DALA2023022201326None · noneCORROSION ON FLOOR SUPPORT 4 (EA) STA Y=218 AND X=0 TO X=13.5, STA Y=200 X=16 TO X=-6, STA Y=200-210 X=-10.5 (CPAX)(W1). SUMMARY OF NRC 00433: CORROSION LEVEL 2. FLOOR SUPPORT 4 (EA) STA Y=218 AND X=0 TO X=13.5, STA Y=200 X=16 TO X=-6, STA Y=200-210 X=-10.5 WESDR HALA2023022200003None · noneSMOKE & FUMES IN CKPT ORIGINATING CAPT'S SIDE WINDOW UPPER NEAR GRAB HANDLE, O2 MASK USED ( WINDSHIELD HEAT SYSTEM-ANTI-ICE SYSTEM ) MX FOUND WINDSHIELD HEAT TERMINAL BLOCK MELTING AND DAMAGED WIRE BUNDLE. WAITING ON SEVERAL PARTS REQUISITIONS.SDR DALA2023022201324None · noneSECONDARY IN REF TO AMDS 5310-01436-01A: CRACK ON CUSP MEMBRANE WEB AT STA 674 L-18 LH. SUMMARY NRC 00198: CUSP MEMBRANE WEB AT STA 674 L-18 LH WAS REPAIRED PER B717-200 SRM 53-00-55-2R REPAIR 4 FIGURE 203. (LP #2637942)SDR DALA2023022201323None · noneCORROSION ON CUSP WEB BETWEEN STA Y=200 TO STA Y=218 AND BL (-X)=55. SUMMARY OF NRC 00519: CUSP WEB WAS FABRICATED PER DWG 9936535 REV CS AND CUSP WEB BETWEEN STA Y=200 TO STA Y=218 AND BL (-X)=55 WAS REPLACED PER B-717-200 SRM 51-41-02-0G PAR 4, 51-41-05-0G P
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