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 DALA2017031001921Frame · crackedFRAME CRACKED RT SIDE BS 1076 AFT FLANGE IN RADIUS. REPAIRED IAW PRI 556132-14, REVISION O, AND COMPLIED WITH ER/A 556132-14 REVISION ORIGINAL.SDR DALA2017030901920Door Frame · corrodedAFT CARGO BAY LOWER DOOR FRAME CORRODED. REPAIRED IAW SRM 53-20-15, FIG 201, REPAIR 7.SDR DALA2017032002226Floor Support · corrodedFORWARD FUSELAGE FLOOR SUPPORT BS 202-218, 221-239, LBL 14 CORRODED. REPLACED THE FLOOR SUPPORT IAW DWG 9936535.SDR DALA2017030901925Frame · damagedBS 237 FRAME BETWEEN LONGERONS 17 AND 18L IS CRACKED AND BENT. REMOVED AND REPLACED THE FRAME IAW SRM 51-41.SDR DALA2017030801866Cusp Web · corrodedFUSELAGE, CABIN, RT CUSP WEB, STA 487 R54.5, UNDERSIDE, CORROSION. REPAIRED CUSP WEB STA 389-503 RT SIDE IAW SRM 53-00-55 2R-4. FABRICATED AND INSTALLED 7075-T6. 032 DOUBLER AND 7075-T6. 020. FILLER WET WITH SEALANT IAW SRM 53-00-55 2R-4. ALODINED, PRIMED, ANDSDR DALA2017030801865Cusp Web · corrodedFUSELAGE, CABIN, RT CUSP WEB, STA 584 R56.0 AT DOUBLER, UNDERSIDE CORROSION. REPAIRED DAMAGED CUSP 584 RT SIDE, IAW SRM 53-00-55 REPAIR 4.SDR DALA2017031802190Seat Track · corrodedRIGHT INBOARD SEAT TRACK BL22R STATIONS 465-565 HAS AREAS OF GOUGES AND CORROSION. BLENDED AREA AT VL 22R STA 489-491 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-20-52-1A WITH .036" REMOVED REMAINING MATERIAL .079" WITH NOMINAL AT .115". INSTALLED 3-LUG REPAIR ISDR DALA2017030701919Battery Pack · inoperativeOVERWING EMERGENCY LIGHT BATTERY PACK INOPERATIVE.SDR DALA2017030701861Circuit Board · burnedOVERWING EMERGENCY LIGHT BATTERY POWER SUPPLY CIRCUIT BOARD BURNT. REPLACED OVERWING EMERGENCY LIGHT BATTERY POWER SUPPLY PER AMM 33-51-03 OPS CHECK GOOD. AC OK FOR SERVICE.SDR DALA2017030701860Doubler · corrodedFUSELAGE, CABIN, RT STA 889 TO 908 R56.0, SPLICE DOUBLER, UNDERSIDE, CORROSION. REPLACED LOWER SKIN SPLICE DOUBLER AT STA 889-908 IAW SRM 51-41-05.SDR DALA2017030701859Structure · corrodedSUB FLOOR AT STA 157 BL5R CORRODED ON LOWER SURFACE. REPAIRED CORRODED AREA ON SUB FLOOR STA 157 BL5R IAW 51-70-10-2R-2 AND SRM 51-41-02 PG 3 PAR F.SDR DALA2017030501766Skin · corrodedMLG & W/W, CORROSION ON CENTER TANK UPPER SKIN AFT EDGE BTW STA 755 Z=-9 FROM X=O TO X=-53. AS VIEWED FROM RT FWD BULKHEAD. CORROSION ON UPPER SKIN OF CENTER FUEL TANK WAS REMOVED PER ETI 17-17-032 REV 2 AND ER/A 555628-14 REV ORIGINAL.SDR DALA2017030501764Frame · corrodedCORROSION ON FRAME Y=1022 BTW LONG 28L AND 27R AFT CARGO COMPARTMENT. FRAME WAS REPAIRED PER SRM 53-20-07 2R-3. HFEC INSPECTION WAS PERFORMED PER NDT SPM 06-10-01.001 AND NO CRACKS WERE FOUND ALONG TRIM LINE.SDR DALA2017030501763Cargo Track · corrodedAFT CARGO COMPARTMENT HAS CORROSION ON RT TIE TRACK FROM Y=813 TO Y=954, Y=994 TO Y=1022. RT TIE TRACK FROM Y=813 TO Y=954, Y=994 TO Y=1022 WAS REPLACED PER SRM 51-41-01 0G.SDR DALA2017030801862Doubler · corrodedSTA 870-889 CORROSION WAS FOUND ON EXISTING CUSP WEB REPAIR DOUBLER AND WAS FOUND TO BE OUT OF LIMITS IAW 51-00-00 .015" MATERIAL REMOVED. REMOVED AND INSTALLED NEW DOUBLER IAW SRM 51-41-02 AND 53-00-55 2R-4 FIG 215.SDR DALA2017030701857Membrane · crackedFWD FLOOR CUSP MEMBRANE CRACKED IN EXISTING REPAIR DOUBLER AT FS190 RBL8. MARKED. REPLACED FWD FLOOR CUSP MEMBRANE REPAIR DOUBLER AT FS 190RBL 8 IAW SRM 51-40-03-0G PAR 16 STEP A, SRM 51-40-03-0G PAR 6 STEP A, SRM 53-00-55-2R-4 NOTE 27, SRM 51-41-08-0G PAR 7 ASDR DALA2017030501765Cusp Web · corrodedLT CUSP WEB CORRODED BOTH SIDES STA 617-655. REPLACED LT CUSP WEB AT STA 617-655 IAW SRM 51-40-02 SEE 75663-0500-0047 FOR HOLD DOWN ACTUATOR. CUSP WEB P/N 8910151.SDR DALA2017033102582Skin · damagedFUSELAGE SKIN STA 235, ABOVE L-18L "FOUR CORNERS" AREA DENT AND GOUGE. PERMANENT REPAIR RESTRICTION. ER/A 539814-14 REV B IS CURRENT. REMOVED TIME LIMITED REPAIR AT STA 235 LONGERON 18LT AND ACCOMPLISHED A CLASS 1 PERMANENT REPAIR IAW SRM 53-10-01 REPAIR 10 FISDR DALA2017030801864Cusp Web · corrodedSTA 908-927 CORROSION ON BOTH SIDES OF CUSP LT SIDE. INSTALLED EXTERNAL AND RING DOUBLER REPAIR LT CUSP WEB STA 913 FOR BLENDS OUT OF LIMITS REF SRM 53-00-55-2R-4.SDR DALA2017030801863Former · crackedFORMER IS CRACKED JUST ABOVE LONGERON 15L AND STA 1022. REPLACED SHEAR TIE / FORMER WITH NEW SHEAR TIE / FORMER IAW SRM 51-41-02, 51-41-05, AND DRAWING 99122434197.SDR DALA2017030501767Skin · corrodedMLG & W/W, CORROSION ON CENTER TANK UPPER SKIN AFT EDGE BTW STA STA 755 Z=-9 FROM X=O TO X=-53. AS VIEW FROM LT FWD BULKHEAD. CORROSION ON UPPER SKIN OF CENTER FUEL TANK WAS REMOVED PER ETI-17-17-032 REV 2 AND ER/A 555628-14 REV ORIGINAL.SDR DALA2017030301724Skin · damagedSEVERAL LOOSE FASTENERS WITH ELONGATED HOLES IN L/E VERTICAL WRAP AROUND SKIN PANEL ZFS 148.858. LT AND RT SIDES. REPAIRED THE SKIN PANEL IAW ER/A 553690-14 REV 0.SDR DALA2017030301721Rub Strip · corrodedCORROSION ON LEFT UPPER RUBTRIPS BETWEEN BS 775 TO 813 AND BETWEEN BS 579 TO 696. THE RUB STRIPS WERE REPLACED IAW SRM 51-20-05 0G.SDR DALA2017030701858Longeron · crackedLONGERON 16L CRACKED AT 1022 BULKHEAD. INSTALLED REPAIR ON L16L STA 1022 IAW SRM 53-00-05 REPAIR 2 TRIMMED PYLON ANGLE TO REMOVE TRAPPED FASTENERS IAW ER/A 553686-14 REV O.SDR DALA2017030201699Seat Track · corrodedCORROSION ON INBD & OTBD F.O. SEAT TRACK , ALSO ON FLOOR SUPPORT RBL 54 BTW BS 140 TO 110. REPAIRED IAW ETI-17-17-034 REV. 1 AND ER/A 555629-14 REV.ORIGINAL.SDR DALA2017030201693Channel · crackedCRACK ON CHANNEL BS 749 INBD EDGE AT RT MLG INNER DOOR. THE CHANNEL WAS REPAIRED IAW ETI-17-17-025, REV 5, AND ER/A 554172-14, REV ORIG.SDR DALA2017030201691Longeron · corrodedCORROSION ON LONGERON 30 BS 946 - 974. REPLACED THE LONGERON FROM BS 908 - 965 IAW SRM 51-41-05, AND 51-41-02.SDR DALA2017030201690Longeron · crackedFOUND LONGERON 17L TO BE CRACKED AT BS 1022. PERFORMED A LONGERON HAT SECTION SPLICE REPAIR IAW SRM 53-00-05 2, REPAIR 2.SDR DALA2017030201689Shear Tie · crackedLEFT BS 1022 FRAME SHEAR TIE CRACKED ON END BETWEEN LONGERONS 16 - 17L. REPLACED THE FRAME IAW SRM 53-00-06 2, REPAIR 3.SDR DALA2017030201687Skin · corrodedCORROSION ON FUSELAGE SKIN AREA BELOW FILLET PANEL RUBSTRIP UPPER SECTION BETWEEN BS 760 - 800. CORROSION REMOVED IAW SRM 51-10-04 0G PAR. 26, 21, AND 15. UT WAS ACCOMPLISHED IAW NDT SPM 04-00-07 PAR 5 FIG 3 SHEET 1 AND 2.SDR DALA2017030201686Angle · crackedANGLE CRACKED ON REPAIR ON FWD CARGO BAY BULKHEAD BS 674, LONGERON 24L. REPLACED IAW SRM 51-41-05 AND SRM 51-40-08 0G.SDR DALA2017030201698Pan · crackedFLC DOOR LOWER FWD CORNER HAS A CRACK ON DOOR PAN.SDR DALA2017030201692Angle · crackedSKIRT ANGLE CRACKED AT UPPER FWD HINGE POINT JUST FWD OF YOKE. REMOVED DAMAGE IAW SRM 54-50-02 2B-1 STEP 6. FABRICATED A REPAIR IAW SRM 54-50-02 2R-1, REPAIR 1 THRU STEP 6.SDR DALA2017030101649Angle · corrodedCORROSION ON CUSP ANGLE FROM BS 465 - 470, LONGERON 18R. THE CUSP ANGLE WAS REPAIRED IAW ETI-17-17-028 REV.2, AND ER/A 555636-14 REV. ORIGINAL.SDR DALA2017030101640Door Frame · crackedCRACK IN WEB OF THE AFT CABIN PRESSURE BULKHEAD EMERGENCY EXIT DOOR JAMB AT 2 HRS POSITION (CPAX). REPAIR WAS ACCOMPLISHED PER INSTRUCTIONS OF ETI 17-17-023 REV 3 AND ER/A 554168-14 REV ORIGINAL.SDR DALA2017030101639Skin · corrodedTO ACCOMPLISH REMOVAL OF CORROSION ON CENTER TANK UPPER SKIN, CUT/REPAIR WEB/ANGLE AS REQUIRED FROM STA Y=727, 737, AND X=0. AREA WAS REPAIRED ON CENTER TANK UPPER SKIN (WEB/ANGLE) FROM STA Y=726, 755, AND X=0 PER 51-70-11 2R, 51-40-02, AND 51-40-05.SDR DALA2017030101638Floor Panel · damagedCORROSION ON FLOOR PANELS 222XF AND 222AQF (SM). DUE TO EXCESSIVE DAMAGE FLOOR PANELS WERE REPLACED PER SRM 51-40-08 06 AND DWG 9952521 REV BB.SDR DALA2017030101637Structure · corrodedWING BOX CABIN AREA CORROSION ON UPPER FACE WING BOX RT BTW STA Y=674 TO 696 X=-54 TO X=-60 (WING BOX). REPAIR WAS ACCOMPLISHED PER ETI-17-17-022 REV 4 AND ER/A 554158-14 REV ORIGINAL.SDR DALA2017030101636Skin · corrodedRT MLG WHEEL WELL CORROSION ON CTR FUEL TANK SKIN STA Y=755 AND X=-50 AT SLANT PRESSURE PANEL AREA 5310-2003 (FYT). CORROSION WAS ATTENDED PER ETI-17-17-022 REV 4 AND ER/A 554158-14 REV ORIGINAL.SDR DALA2017030301725Angle · corrodedCUSP ANGLE AT THE R1 DOOR IS CORRODED. REPLACED THE ANGLE FROM BS 146 TO 239 IAW SRM 51-41-02 0G AND SRM 53-00-55 2R-3.SDR DALA2017030301723Frame · corrodedCORROSION ON FRAME BS 927 BETWEEN LONGERONS 29L-29R. REPAIRED THE FRAME IAW SRM 53-00-06, REPAIR 2.SDR DALA2017022801635Floor Support · corrodedFORWARD CABIN FLOOR SUPPORT AT STA 178, RBL 14 - RBL 32 CORRODED SEVERAL PLACES. REPLACED FORWARD FLOOR SUPPORT IAW SRM 51-41-05. DAMAGE WAS OUT OF LIMITS IAW SRM 53-00-00-1A AND 53-10-51.SDR DALA2017022801610Beam · crackedFWD R1 DOOR AREA HAS A CRACKED NR 4 BEAM AT FWD EDGE. A NEW BEAM WAS FABRICATED AND REPLACED IAW SRM 51-41-02, 51-41-05,AND DWG 911582 REV T.SDR DALA2017022701609Lens · missingSIDEWALL LIGHT LENS MISSING OVER RIGHT SIDE EMERGENCY EXIT WINDOWS. INSTALLED A NEW LENS. OK FOR SERVICE.SDR DALA2017022701570Beam · crackedCRACKED LATERAL BEAM LBL 60- 18 AND RBL 18 IN THE NOSE LANDING GEAR WHEEL WELL. HFEC INSPECTION WAS ACCOMPLISHED IAW NDT SPM 06-10-01.001. REPAIRED IAW SRM 53-10-14-2R PROCEDURE 2.SDR DALA2017022701569Seal Depressor · crackedCRACK ON AFT CARGO DOOR FRAME SEAL DEPRESSOR BS 994 BETWEEN LONGERONS 24 AND 25R. THE SEAL DEPRESSOR WAS REPAIRED IAW SRM 53-20-15 2R.SDR DALA2017022701568Cargo Track · corrodedCORROSION ON CARGO TRACK BS 812 - 1022. THE CORROSION WAS REMOVED IAW SRM 51-10-04 PAR 26 AND FOUND OUT OF LIMITS IAW SRM 53-20-52 101. A NEW CARGO TRACK WAS INSTALLED IAW SRM 51-41-01, AND SRM 51-41-02.SDR DALA2017022701608Floor Support · corrodedCORROSION ON FLOOR SUPPORT UNDER FIRST OFFICER`S SEAT TRACK, BS 120 TO 145, RBL 28. THE SEAT TRACK WAS REPLACED IAW 51-41-01 AND 53-10-51 FIG1.SDR DALA2017022701607Rub Strip · corrodedCORROSION ON ACCESS PANEL CUT OUT RUB STRIPS ON THE LT WING THE RUB STRIPS WERE REPLACED IAW SRM 57-10-01 2R PROCEDURE 3.SDR HALA2017022500046Relay · failedBURNING ODOR NOTICED AFTER LANDING. PERFORMED FIM 21-22-815 FOR ODOR. RAN NR 1 & 2 ENGINES SPERATELY. AS NR 1 AND 2 PACKS ISOLATED, COULD NOT DUPLICATE ON GROUND. OPS OF PACKS NORMAL ON GROUND. OK TO CONTINUE. NO EVIDENCE OF ODOR. ON SUBSEQUENT FLIGHT F
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