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 jasc_code = '5755' 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 jasc_code = '5755' 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 GAIA9911Panel · crackedEN ROUTE FROM CLT-TOL - DURING CRUISE AT FL280 BETWEEN MACH .74 TO .80, THE AIRCRAFT EXIBITED A MODERATE VIBRATION. (CONTROL WHEEL CENTERED AND SPEED BRAKE HANDLE IN FORWARD DETENT). MOVING SPEED HANDLE BACK APPROXIMATELY 2 INCHES WOULD MAKE THE VIBRATION GOSDR CALA9900116Brace · crackedINSPECTION FOUND A CRACK OF UNSPECIFIED LENGTH IN THE LT GROUND SPOILER ACTUATOR I/B ATTACH BRACKET CROSS BRACE. A NEW CROSS BRACE WAS INSTALLED IAW SRM 51-30-5.SDR UPS99228632Fitting · corrodedINSPECTION TYPE:SI NR 3 FLIGHT SPOILER ACTUATOR SUPPORT FITTING HAS EXCESSIVE PITTING CORROSION ON I/B FACES OF BOTH I/B MOUNTING LUGS FOR SPOILER CENTER HINGE. REPLACED MOUNT (SUPPORT FITTING PN 65-21622-22) PER 727 MM 27-61-81.SDR UPS99228610Skin · corrodedINSPECTION TYPE-SI, NR 7 SPOILER PANEL HAS SEVERAL SMALL AREAS OF CORROSION ON LOWER SURFACE AT TRAILING EDGE 7 INCHES I/B OF O/B END. REPLACED SPOILER IAW MM 27-62-1.SDR GTIA9900884Skin · delaminatedLEFT WING UPPER SURFACE OUTBOARD SPOILER IS DELAMINATED AT UPPER INBOARD SECTION APPROX 6 INCH BY 5 INCH OF DELAM ON PART RACK. DELAMINATION AREA IS LARGER THAN ALLOWED LIMITS IN SRM REQUIRES OUTSIDE VENDOR REPAIR REMOVED AND REPLACED. (M)SDR ABXA9900146Bracket · crackedLEFT WING SPOILER ACTUATOR BRACKET, LOWER SURFACE CRACKED. REPAIRED UNIT COMPLETE.SDR EISA99011Skin · delaminatedDURING ACCOMPLISHED ROUTINE C-CHECK WORK CARD, CORROSION WAS FOUND SKIN DISBOND RIGHT WING INBOARD SPOILER, INBOARD TRAILING EDGE TOP SKIN. REMOVED DAMAGED AREA, REPAIRED HONEYCOMB PER SRM 57-04 FIG 4, AND INSTALLED NEW SKIN SECTION PER SRM 51-70-2. (M)SDR P2EA99052Skin · delaminatedSJO - Q-CHECK ITEM. NR 4 GROUND SPOILER DELAMINATED. DEFECT SIZE: LENGTH 10 INCHES WIDTH 20 INCHES. REPAIRED SPOILER PER COOPESA B.O. COO-CMP-3-57-010-99 DATED JAN 19, 1999. DOCUMENTED ON FAA FORM 8110-3. APPROVED AND SUBMITTED BY FAA DER ROBERT M. MANASSDR DHL9980686CPanel · delaminatedAT C-CHECK, LT WING NR 4 SPOILER PANEL DELAMINATED. REMOVED AND REINSTALLED PER MM 27-5-13. N/R 90SDR P2EA99039Skin · delaminatedSJO - Q-CHECK ITEM. NR 5 SPOILER DELAMINATED. DEFECT SIZE: LENGTH 4.0 INCHES WIDTH 3.0 INCHES. REPAIRED NR 5 SPOILER PER SRM 57-50-5, FIG 2, SHEET 9. SEE COOPESA W.O. M1-0005-6-21, VAM 100 NR 189 FOR TECHNICAL INFORMATION. (X)SDR DHL9971222CPanel · delaminatedAT C-CHECK, NR 9 SPOILER PANEL DELAMINATED AT TOP SURFACE I/B CORNER. INSTALLED BONDING REPAIR PER SRM 51-40-6, 15 X 11.SDR DHL9971220CSkin · delaminatedAT C-CHECK, LEFT WING NR 6 SPOILER PANEL UPPER SURFACE AREA DELAMINATED AND HOLES DRILLED. INSTALLED BONDED REPAIR PER SRM 51-40-6, 16 X 11.SDR UPS99228450Skin · delaminatedINSPECTION TYPE-C, NR 9 SPOILER PANEL LOWER SKIN DELAMINATED. REPAIRED IAW SRM 57-50-6 FIG 5.SDR UPS99228432Skin · delaminatedINSPECTION TYPE-C, NR 9 SPOILER PANEL LOWER SKIN DELAMINATED. REPAIRED IAW SRM 57-50-6 FIG 5.SDR QXEA9900144Skin · damagedPDX - LEFT-HAND SPEED BRAKE HAS SEVERAL RIVETS PULLING THROUGH SKIN ON BACK MIDDLE FRAME. REPAIRED IAW FOKKER SRM 51-31-05 AND SRM 53-02-01, PAGE 11 FIGURE 9.SDR QXEA9900146Rivet · loosePDX - RIGHT-HAND SPEED BRAKE HAS THREE LOOSE RIVETS JUST BELOW SKID PLATE. REPAIRED IAW FOKKER SRM 51-31-05.SDR AU981662Bracket · broken(AUS) WING GROUND SPOILER PANEL'S LT OUTBOARD ATTACHMENT BRACKET FOUND BROKEN AT ACTUATOR LINK ATTACHMENT. SUSPECT A POSSIBLE CAUSE OF THE FAILURE WAS DUE TO INCORRECT RIGGING ASSEMBLY AT LAST FITMENT AS THE ACTUATOR ROD END REQUIRED ADJUSTMENT TO RECONNECT TSDR P5CA9801618Spoiler · holeRIGHT WING NR 12 SPOILER HAS SMALL HOLE IN TOP SIDE SURFACE. CLEANED, POTTED DAMAGED AREA AND REPAIRED PER SRM 51-40-06.SDR P2EA98296Slat · delaminatedSJO - NR 5 SLAT DELAMINATED, DEFECT SIZE TOTAL 400 SQ INCH. REPAIRED NR 5 SLAT PER COOPESA EO COO-3-57-719-98 DATED DEC 2, 1998. DOCUMENTED ON FAA FORM 8110-3. (M)SDR P2EA98307Skin · delaminatedSJO - NR 5 SPOILER DELAMINATED, DEFECT SIZE TOTAL 234 SQUARE INCH. REPAIRED NR 5 SPOILER PER COOPESA EO C00-3-57-709-98 DATED NOV 30, 1998. (M)SDR P2EA98306Skin · delaminatedSJO - NR 2 SPOILER DELAMINATED, DEFECT SIZE TOTAL 6 SQUARE INCH. REPAIRED NR 2 SPOILER PER COOPESA EO COO-3-57-710-98 DATED NOV 30, 1998. (M)SDR P2EA98303Skin · delaminatedSJO - NR 7 SPOILER DELAMINATED, DEFECT SIZE TOTAL 325 SQUARE INCH. REPAIRED NR 7 SPOILER PER COOPESA EO COO-3-57-711-98 DATED NOV 30, 1998. (M)SDR P2EA98298Spoiler · delaminatedSJO - NR 8 SPOILER DELAMINATED, DEFECT SIZE TOTAL 320 SQ IN. REPAIRED NR 8 SPOILER PER COOPESA EO C00-3-57-713-98 DATED NOV 30, 1998. DOCUMENTED ON FAA FORM 8110-3. (M)SDR P2EA98295Spoiler · delaminatedSJO - NR 6 SPOILER DELAMINATED, DEFECT SIZE TOTAL 160 SQ INCH. REPAIRED NR 6 SPOILER PER COOPESA EO COO-3-57-712-98 DATED NOV 30, 1998. DOCUMENTED ON FAA FORM 8110-3. (M)SDR CALA9802075Cover · crackedINSPECTION FOUND A .1875 AND .125 CRACK IN LT WING UPPER T/E HINGE COVER OF NR 2 SPOILER HINGE. THE T/E HINGE COVER WAS REMOVED AND A NEW T/E HINGE COVER WAS INSTALLED IAW SRM 51-30-2, PARAGRAPH 7.SDR ASAA9880237Fitting · corrodedLCQ - DURING 30K CHECK, CORROSION WAS FOUND ON RIGHT WING INBOARD FLIGHT SPOILER HINGE FITTING. REPAIRED IAW ASA EA 2760-01026. (M)SDR DHL9980108CSkin · delaminatedAT C-CHECK, LT WING T/E LOWER AREA NR 2 SPOILER PANEL DELAMINATED. REMOVED, REPAIRED AND REPLACED PANEL PER DAC MM 27-61-1.SDR EISA98269Skin · damagedROUTINE C-CHECK WORKCARD ACCOMPLISHMENT REVEALED A REPAIR DOUBLER OUTBOARD OF NR 1 SPOILER CRACKED. FABRICATED AND INSTALLED NEW DOUBLER PER SRM 51-30-1 AND 51-30-7. (M)SDR QXEA9801692Link · chafedSPEED BRAKE LEFT-HAND SUPPORT LINK CHAFING ON COMPOSITE TAIL CONE AT UPPER AND LOWER ARMS. REPAIRED IAW HORIZON AIR EA 4-55-103.SDR CALA9802036Skin · delaminatedINSPECTION FOUND TOP SURFACE OF NR 8 SPOILER DELAMINATED. THE NR 8 SPOILER WAS REMOVED AND REPLACED IAW MM 27-62-81.SDR DHL9872090DSkin · crackedAT D CHECK, RT WING NR 11 SPOILER ACTUATOR SUPPORT FITTING, INBD HINGE WING CUT OUT IS CRACKED. CUT OUT DAMAGED AREA, INSTALLED DOUBLER REPAIR PER SRM 57-30-4, 6 BY 3, N/R 2864.SDR CA981109046Fitting · cracked(CAN) PILOT REPORTED AN UNCOMMANDED DEPLOYMENT OF RT FLIGHT SPOILER ON APPROACH 'FLT SPLR' STATUS MSG. DURING APPROACH WITH FLAPS 45 DEGREES AFTER 10 SECONDS, 'FLT SPLRS DEPLOY' MSG STRONG AILERON TO LEFT REQUIRED TO KEEP DIRECTIONAL CONTROL. INSPECTION FOUNSDR TWAA9816804Angle · crackedDURING OP 16 MAINT CHECK, FOUND RT WING OTBD SPOILER, OTBD DOWN STOP ANGLE WAS CRACKED ON THE INBD SIDE. INSTALLED NEW TEE ANGLE, MFG 5918134-1, PER SRM 51-01, PG 1 ITEM C. INSTALLED RIVETS PER SRM 51-30-02. INSTALLED FASTENERS PER SRM 51-30-0.SDR QXEA9801510Bushing · wornRIGHT-HAND SPEED BRAKE A FRAME PUSHROD FORWARD BUSHINGS WORN. REPAIRED IAW FOKKER SRM 27-61-05 PAGE 402 PARAGRAPH 3 AND HORIZON AIR EA 4-55-96.SDR ABXA9800900Fitting · crackedDURING C-CHECK, FOUND RIGHT INBOARD SPOILER TORSION BAR OUTBOARD SUPPORT FITTING CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-3 AND 51-30-5.SDR ABXA9800899Fitting · crackedDURING C-CHECK, FOUND RIGHT OUTBOARD SPOILER TORSION BAR SUPPORT INBOARD FITTING CRACKED. REPAIRED IAW DC9 SRM 51-30-3 AND 51-30-5.SDR DHL9980117CSkin · delaminatedAT C-CHECK, RT WING T/E UPPER AREA NR 5 SPOILER PANEL DELAMINATED. REMOVED, REPAIRED AND REINSTALLED PANEL.SDR DHL9980113CSkin · delaminatedAT C-CHECK, RT WING T/E SPOILER PANEL DELAMINATED. REMOVED AND REPLACED SPOILER PER MM 27-61-1.SDR QXEA9801498Bearing · looseBEARING LOOSE IN FITTING FOR SPEED BRAKE LEVER ATTACHMENT AT LEFT-HAND UPPER POSITION. REPAIRED IAW FOKKER SRM PAGE 215, E3 FIGURE 9.SDR QXEA9801497Bearing · looseBEARING LOOSE IN FITTING FOR SPEED BRAKE LEVER ATTACHMENT AT LEFT -HAND LOWER POSITION. REPAIRED IAW FOKKER SRM PAGE 215, E3 FIGURE 9.SDR CALA9801932Skin · wornRT WING NR 8 SPOILER CENTER CHAFE PAD WORN AND TE WORN/MISSING. DENTS OUT OF LIMITS PER SRM 57-50-1 FIG 5. REMOVED SPOILER PANEL AND SENT OUT FOR REPAIR PER MM 27-62-1.SDR CALA9801919Skin · delaminatedINSPECTION FOUND THE RT WING NR 8 SPOILER DELAMINATED. THE SPOILER WAS REMOVED AND REPLACED IAW MM 27-62-1, PAGE 401-404.SDR UPS98227946Support · crackedINSPECTION TYPE:C SUPPORT CHANNEL FOR NR 5 SPOILER PANEL INB DOWNSTOP CASTING CRACKED. NR 5 SPOILER CHANNEL REPLACED IAW SRM 51-30-02.SDR QXEA9801503Fitting · wornSPEED BRAKE LEFT-HAND LEVER UPPER BUSHING HOLE FOR STRAIGHT PUSHROD IS ENLARGED AND OUT OF ROUND. REPAIRED IAW HORIZON AIR EA 4-55-86.SDR MZZA98248Skin · delaminatedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON NR 7 SPOILER T/E UPPER SKIN. THE DAMAGED SKIN 6 INCH BY 2.4 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. (M)SDR QXEA9801505Fitting · damagedSPEED BRAKE CROSSHEAD ASSEMBLY DAMAGE TO RIGHT-HAND PUSHROD BOLT HOLE AREA, LOWER EAR OF CROSSHEAD. REPAIRED IAW HORIZON AIR EA 4-55-85.SDR MZZA98252Skin · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON NR 11 SPOILER UPPER SKIN AT WBL 317 AND WBL 327. THE DAMAGED SKIN 18 INCH BY 7 INCH AND 9 INCH DIAMETER WERE TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. (M)SDR DL72S981976Panel · delaminatedFOUND ON A1 LETTER CK, NR 1 SPOILER PANEL DELAMINATED. REPAIRED PER SRM 57-50-6.SDR CALA9801844Skin · corrodedINSPECTION FOUND NR 5 SPOILER CORRODED ALONG TOP EDGES. THE NR 5 SPOILER WAS REMOVED AND REPLACED IAW MM 27-61-1.SDR CALA9801843Skin · delaminatedINSPECTION FOUND THE NR 2 SPOILER DELAMINATED AFT OF INBOARD HINGE. THE NR 2 SPOILER WAS REMOVED AND REPLACED IAW MM 27-61-1.
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