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 = '5751' 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 = '5751' 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 TWAA0009614Skin · delaminatedDURING OP 15 MAINT CHECK ON THE LT WING, THE I/B AILERON HAD SEPARATION AND DELAMINATION AT THE L/E UPPER SURFACE, TWO PLACES. REPAIRED PER DWG 113T6002.SDR 20001004AP005Skin · crackedON ROUTINE MAINTENANCE PREFLIGHT, A TECHNICIAN DISCOVERED A SMALL AREA OF BUBBLED PAINT. AN INVESTIGATION REVEALED A CRACK IN THE TRAILING EDGE OF THE LEFT AILERON THE AILERON TRAILING EDGE WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR LR7A0079Skin · corrodedDURING SCHEDULED C2 INSPECTION PER JOB CARD HC2704, FOUND RT AILERON UPPER SKIN CORRODED AT AIL STA 15. REPAIRED PER SRM SMP 583-57-10.SDR AU000885Rib · damaged(AUS) RT AILERON DAMAGED DURING GROUND HANDLING. RIB 20 AND FAIRING DAMAGED.SDR TSAA0027157Skin · corrodedREPAIRED RIGHT AILERON CONTROL QUADRANT AT WING STATION 519 BY BLENDOUT AND TREATING CORROSION IAW ECO 3147. AIRCRAFT RETURNED TO SERVICE. (M)SDR QXEA0001623Fastener · looseYYC- RIGHT HAND ELEVATOR OUTBOARD END HAS LOOSE FASTENERS. REPAIRED IAW FOKKER SRM 51-31-05 AND 51-70-0.SDR 20000608SH016Sleeve · crackedOVER 50 PERCENT OF THE FLANGE ON THE SLEEVE IS CRACKED IN THE RADIUS, WHERE IT SEATS AGAINST SUPPORT ITEM 60 FIGURE 1101 PN 65-75928-4. SLEEVE IS WORN AND STRESSED UNDER SPACER ITEM 55 FIGURE 1101 PN 69-41647-2. POSSIBLE CAUSE: FATIGUE AND STRESS. (X)SDR 20000608SH011Sleeve · crackedOVER 50 PERCENT OF THE FLANGE ON THE SLEEVE IS CRACKED IN THE RADIUS WHERE IT SEATS AGAINST SUPPORT ASSY ITEM 2 FIGURE 1101 PN 65-50555-5. SLEEVE IS WORN AND STRESSED UNDER SPACER ITEM 6 FIGURE 1101 PN 69-41647-2. (X)SDR 20000516SH002Channel · crackedAFTER REMOVAL OF BOTH RT AND LT AILERON INBOARD HINGE ASSEMBLIES, FOUND BOTH AILERON ''U'' CHANNELS HAD CRACKS IN THE WEB AROUND THE LOWER HINGE ATTACH BOLTS. SUBMITTER RECOMMENDED INSTALLING A REINFORCING PLATE ON AFT SIDE OF WEB IAW AC 43.131B PAR 4-58, 4-5SDR 20000516SH001Channel · crackedAFTER REMOVAL OF BOTH RT AND LT AILERON INBOARD HINGE ASSEMBLIES, FOUND BOTH AILERON ''U'' CHANNELS HAD CRACKS IN THE WEB AROUND THE LOWER HINGE ATTACH BOLTS. SUBMITTER RECOMMENDED INSTALLING A REINFORCING PLATE ON AFT SIDE OF WEB IAW AC 43.131B PAR 4-58, 4-5SDR 20000515SH014Bracket · shearedFOUND 2 OF 6 RIVETS THAT HOLD THE OUTBOARD AILERON HINGE TO THE WING SPAR SHEARED OFF. (X)SDR P2EA00173Skin · delaminatedSJO - DURING C-CHECK, FOUND THE LEFT AILERON FORWARD OUTBOARD LOWER SURFACE WITH DELAMINATED. REPAIRED THE LEFT AILERON FORWARD OUTBOARD LOWER SURFACE IAW BOEING SRM 51-40-6 PAR 11. (M)SDR RRXA001897Panel · delaminatedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LT WING LWR AILERON POWER PACK AT PANEL NR 540, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED PANEL NR 540 IAW DC-8 SRM, SDR MWEA00269Skin · dentedRIGHT AILERON HAS A DENT ON LOWER SURFACE, 4 INCHES FROM OUTBOARD END. FABRICATED AND INSTALLED REPAIR DOUBLER.SDR RRXA001934Skin · crackedDURING A MAINTENANCE VISIT FOUND A CRACK IN 3 PLACES TO THE LEFT I/B AILERON O/B END, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 51-1-21 AND EO NR 00-055SDR RRXA001799Skin · crackedDURING A MAINTENANCE VISIT FOUND A CRACK IN 3 PLACES TO THE LT I/B AILERON O/B END, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 51-1-21 AND EO NR 00-055 SDR RRXA001907Skin · tornDURING A MAINTENANCE VISIT FOUND TORN SKIN 8 INCHES AFT OF AILERON L/E LEFT O/B AILERON UPPER SURFACE O/B EDGE AT STA XA 747, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBSDR RRXA001771Skin · tornDURING A MAINTENANCE VISIT, FOUND A TEAR 8 INCHES AFT OF AILERON LE ON LT OB AILERON UPPER SURFACE OB EDGE SKIN AT STA XA 747, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLEDSDR 20000512SH020Nose Rib · crackedDURING ACFT''S FIRST 100-HR INSP, A .25 INCH LONG CRACK WAS FOUND IN A NOSE RIB OF THE LT AILERON. NOSE RIB IS AT THE AILERON''S CUT-OUT IN THE LEADING EDGE FOR THE INBD HINGE ATTACH POINT, ON THE OTBD SIDE. THE CRACK IS AT THE UPPER FWD CORNER OF THE NOSE SDR 20000512SH019Nose Rib · crackedDURING ACFT''S FIRST 100-HR INSP, A .25 INCH LONG CRACK WAS FOUND IN A NOSE RIB OF THE LT AILERON. NOSE RIB IS AT THE AILERON''S CUT-OUT IN THE LEADING EDGE FOR THE INBD HINGE ATTACH POINT, ON THE OTBD SIDE. THE CRACK IS AT THE UPPER FWD CORNER OF THE NOSE SDR 20000426SH033Counterweight · corrodedTHE LEFT AILERON PN 6524113-809, SN 258, HAD WEIGHTS (BALANCE) LOOSE IN THE INBOARD END CAP AND WERE BOUNCING AROUND LOOSE. THE LAST BALANCE WEIGHT CAME OFF OR PULLED THROUGH THE SMALL WASHER AND NUT THAT HOLD THE WEIGHT ON. THERE WAS SOME CORROSION, BUT NOTSDR 2000UALA00150Housing · fodTHE CONTROL WHEELS STUCK IN THE FULL RIGHT AILERON POSITION. THE RIGHT AILERON AND FLIGHT SPOILERS WERE FULLY EXTENDED. *S/D* THE TRANSFER MECHANISM (P/N: 65-54200-15) WAS FOUND TO HAVE RECENT WITNESS MARKS ON THE LOWER BEARING HOUSING WHICH SUGGESTS THE JASDR F3LA00034Skin · damagedDEN - DURING C-7 CHECK, INSPECTION REPORTED HOLE IN LOWER SURFACE OF AILERON AT OUTBOARD END. MAINTENANCE REMOVED AILERON. REPAIRED HOLE PER SRM 51-70-04 AND 51-70-03 AND PAINTED AND BALANCED PANEL. INSTALLED AILERON PER MM 27-11-11. PERFORMED OPERATIONAL SDR CALA0000295Skin · gougedINSPECTION FOUND LEFT AILERON LOWER SURFACE SKIN GOUGED. THE AILERON WAS REPAIRED IAW ECRA 5750-03367.SDR 20000424SH022Skin · crackedPRE-FLIGHT INSPECTION REVEALED A SMALL PORTION OF THE AILERON SKIN CRACKED AT THE INBOARD SECTION, TOP SKIN, TRAILING EDGE ADJACENT TO THE MOVABLE TRIM. FURTHER INSPECTION REVEALED EXTENSIVE CORROSION RELATED CRACKING MOSTLY ALONG THE TRAILING EDGE. REMOVED SDR UPS00832138Fitting · crackedINSPECTION TYPE: C123, LT O/B AILERON I/B HINGE FITTING IS CRACKED. REMOVED & REPLACED FITTING IAW DC8 SRM 51-1-21 & 51-3-0.SDR DHL200080373CTrim Tab · delaminatedAT C-CHECK, LT WING I/B AILERON TRIM TAB UPPER SKIN DELAMINATED. REMOVED AND REPLACED TRIM CONTROL TAB IAW MM 27-13-1, OPERATIONAL CHECK GOOD IAW MM 27-10-0. N/R 1007SDR UPS00232199Fitting · corrodedINSPECTION TYPE: C, CORROSION ON LT O/B AILERON, I/B CENTER HINGE FITTING AROUND FASTENER HOLES. REMOVED AND INSTALLED NEW HINGE FITTING PER SRM 51-30-2SDR QXEA0000620Skin · tornPDX - BEHIND PANEL 83D LEFT AILERON COVER PANEL IS TORN AND DENTED. REPAIRED IAW HORIZON AIR EA 4-57-371.SDR P5CA0000093Skin · damagedOUTBOARD AILERON UPPER SURFACE ONE OFF LOCATION DAMAGED. REPAIRED PER SRM 51-40-15.SDR TWAA0003025Skin · damagedDURING CHECK-C MAINTENANCE, THE RT WING INBD AILERON UPPER SURFACE, 38.75 IN FWD OF TE, 16 INCHES OTBD OF INBD END, HAD A DENT. INSTALLED 2 LAYER GRAPHITE 4.5 INCH DIAMETER HOT BOND PER SRM 51-70-05. PRIMED AND PAINTED AREA.SDR MWEA00067Skin · crackedRIGHT AILERON INBOARD SECTION OF OUTBOARD TRAILING EDGE UPPER SKIN IS CRACKED. MTC FABRICATED AND INSTALLED REPAIR DOUBLER AND FILTER.SDR P2EA00054Skin · delaminatedSJO - DURING Q-CHECK, LEFT WING AILERON INBOARD TOP SECTION DELAMINATED. REPAIRED AILERON IAW COOPESA EO COO-CMP-3-57-072-00, DATED 2/7/2000. (M)SDR 20000405SH006Bearing · failedBEARINGS (76) SHATTER WHEN SUBMITTED TO HIGH TORQUE LOADS. THE BEARING FAILURE CAUSES UNIT TO BIND AND BECOME INOPERATIVE. SUBMITTER SUGGESTED LOAD RATING OF THE BEARING IS TOO LOW. (X)SDR QXEA0000270Skin · corrodedYYC - AREAS OF LIGHT CORROSION ON UPPER AND LOWER SKIN OF RIGHT AILERON. REPAIRED IAW DHC 8 SRM 51-20-00 AND SRM 51-20-11.SDR QXEA0000269Skin · corrodedYYC - CORROSION ON AND AROUND FASTENERS ON RIGHT AILERON. REPAIRED IAW DHC 8 SRM 51-20-00, SRM 51-20-11, SRM 51-40-00 AND SRM 57-60-16, PAGE 2, TABLE 1.SDR AU000203014Hinge · cracked(AU) DURING SCHEDULED MAINTENANCE, THE AILERON OUTBOARD HINGE MOUNTING BRACKET WAS FOUND CRACKED 1/2 WAY THROUGH THE CENTER LUG.SDR DHL200080339CSkin · deformedAT C-CHECK, LT WING AILERON T/E UPPER SKIN DEFORMED AT XW 627. REMOVED FASTENERS AND PERFORMED ANTI-CORROSION TREATMENT IAW SRM 51-1-8, PG 11, INSTALLED SKIN IAW SRM 51-1-21 PG 7. N/R 1078SDR TWAA0001705Skin · separatingDURING CHECK-C MAINT FOUND ON RT WING THE TRAILING EDGE SEPARATING ON THE O/B AILERON. BLENDED AND SMOOTHED. APPLIED TEFLON COATING TO TE PER SRM 51-20-01. AREA WAS NOT SEPARATING.SDR UPS00231509Rib · crackedINSPECTION TYPE:C, RIGHT O/B AILERON L/E NOSE RIB NR 2 I/B OF TAB ACTUATING MECHANISM CRACKED. REPAIR CARRIED OUT IAW SRM 51-40-3, FASTENERS INSTALLED IAW SRM 51-30-2.SDR CA000120018Hinge · loose(CAN) WHILE CARRYING OUT A 100 HR INSP. ON THE LT WING, THE ENGINEER NOTICED THAT THE AILERON HINGE ON THE INBOARD AND OUTBOARD END OF THE AILERON HAD LOOSE RIVETS. THE END RIB AND HINGE FITTING WERE REMOVED FROM THE AILERON AND THE ARE INSPECTED. THE RIVET HOSDR UPS00231467Skin · delaminatedINSPECTION TYPE:C, LT O/B AILERON DELAM ON UPPER AND LWR SKIN AT T/E O/B OF TAB. REPAIRED IAW SRM 51-40-6 FIG 39.SDR MWEA00015Skin · corrodedRIGHT HAND AILERON ON INBOARD SKIN IS CORRODED UNDER CHAFE PLATE IN SEVERAL AREAS. MTC FABRICATED AND INSTALLED FILLER AND DOUBLER.SDR UPS00231339Skin · delaminatedINSPECTION TYPE:C EVIDENCE OF DELAMINATION TO RT O/B AILERON TE AREA JUST O/B OF AILERON TAB. REPAIRED IAW SRM 510 FIG 40.SDR UPS00831311Weight · corrodedINSPECTION TYPE:C1 THE RT OTBD AILERON INBD BALANCE WEIGHT HAS MODERATE CORROSION ON AND UNDER THE WEIGHT. REMOVED AND REPLACED THE RT OTBD AILERON IAW M/M 27-10-02.SDR CALA9901704Skin · gougedINSPECTION FOUND LEFT O/B AILERON LOWER EDGE GOUGED. THE GOUGED AREA WAS REPAIRED IAW SRM 57-50-5, FIGURE 2 AND 51-20-0.SDR GAIA99248Skin · gouged'NO FLIGHT' - FOUND DURING 'HEAVY C-MAINTENANCE CHECK' AT TIMCO HEAVY MAINTENANCE FACILITY (WINSTON/SALEM, NC). FOUND RIGHT WING, INBOARD AILERON, UPPER FIXED LEADING EDGE GOUGED AND CHAFED. REPAIRED IAW BOEING SRM 51-40-5. AIRCRAFT WAS RETURNED TO SERVICE.SDR AALA991957Skin · crackedLAX - DURING B-CHECK, THE RIGHT OUTBOARD TRAILING EDGE FLAP ASSEMBLY JUST INBOARD OF OUTBOARD AILERON HAD 12 INCH CRACK. REPAIRED UPPER AND LOWER SIDE RIGHT OUTBOARD TRAILING EDGE FLAP ASSEMBLYJUST INBOARD OF OUTBOARD AILERON. SYSTEM GROUND CHECKED, NORMAL OSDR CA000118045Support · cracked(CAN) DURING AN ANNUAL INSPECTION, A 1 INCH CRACK WAS DETECTED IN THE FORWARD RADIUS.SDR TWAA0000403Seal · missingDURING CHECK-C MAINT, THE LT WING OTBD AILERON, OTBD TE WEDGE HAD MISSING FILLER SEALANT APPROX 5 INCHES LONG, FROM THE TE TIP.. REPLACED MISSING SEALANT PER SRM 51-10-00.
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