JASC 5754
Service difficulty reports · 17,348
Reports filed under 5754 · Leading Edge Devices, newest first.
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 = '5754' 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 = '5754' 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 UPS97222126Rib · crackedINSPECTION TYPE-D, SLAT 5 CRACK ON RIB AT WS 464 SLAT STA 120. CRACK APPROX .75 INCH LONG. *S/D* HFEC CARRIED OUT IAW NDT PT 6 51-00-00 FIG 4. CRACK FOUND TO BE CONTAINED WITHIN FASTENER HOLE. REPAIR CARRIED OUT IAW SRM 57-50-3 FIG 9.SDR DHL9771257DRib · crackedAT D-CHECK, NR 6 SLAT INBOARD TRACK, OUTBOARD RIB IS CRACKED. REPLACED RIB PER SRM 51-10-1.SDR DHL9771250DRib · crackedAT D-CHECK, NR 4 SLAT NR 3 RIB FROM OUTBOARD END CRACKED. REMOVED DAMAGED AREA AND INSTALLED RIB REPAIR PER SRM 57-50-3, DOUBLER 4.375 BY 3.SDR CALA9700201Skin · crackedINSPECTION FOUND A .5 INCH CRACK AT RIVET HOLE OF LT WING NR 2 SLAT LOWER SKIN BETWEEN NR 6 AND NR 7 TRACKS. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-01.SDR UPS97222136Skin · corrodedINSPECTION TYPE-C, NR 1 KREUGER FLAP CORRODED CORROSION BEYOND LIMITS PER SRM 57-50-1. KREUGER FLAP REPLACED IAW MM 27-81-01.SDR CALA9700253Skin · dentedINSPECTION FOUND A DENT IN INBOARD END OF NR 1 RT SLAT SKIN. A DOUBLER, SPLICE STRAP AND SKIN INSERT WERE FABRICATED AND INSTALLED IAW SRM 57-10-00, FIGURE 43, 51-21-01 AND 51-31-01.SDR 97ZZZM613Flap Track · corrodedRIGHT WING REAR SPAR OUTBOARD FLAP INBOARD TRACK MOUNT RIGHT HOLE HAS PITTING IN INSIDE DIAMETER. REMOVED CORROSION. FABRICATED BUSHINGS AND INSTALLED BUSHINGS IAW EO NR 97-457.SDR UPS97222109Skin · crackedINSPECTION TYPE-D, OUTER SKIN ON LOWER SURFACE OF NR 5 SLAT OUTBOARD END CRACKED APPROX 6 CM. HFEC INSPECTED PER NDT PT6 51-00-00 FIG 4, CRACK CONTAINED BY FASTENER HOLE AND STOP DRILL HOLE. REPAIR CARRIED OUT PER SRM 57-30-3 FIG 1.SDR UPS97222135Skin · corrodedINSPECTION TYPE-C, PAINT BLISTERING FROM NR 3 KREUGER FLAP. SUSPECT CORROSION ON INVESTIGATION CORROSION FOUND TO BE OUTSIDE. REPAIR LIMITS OF SRM 57-50-1. NR 3 KREUGER FLAP REPLACED IAW MM 27-81-01.SDR DHL9771268DRib · crackedAT D-CHECK, NR 3 SLAT THIRD RIB FROM OUTBOARD END CRACKED. INSTALLED REPAIR PER SRM 57-50-3.SDR GTIA9700225Skin · crackedYIP - LEFT WING, OUTBOARD SLAT - RIVETS PULLED AT CENTER TRACK FAIRING AND OUTER SKIN CRACKED. REMOVED AND REPLACED SKIN IAW DC-9 SRM 51-01, PAGE 1. (X)SDR GTIA9700221Fairing · crackedYIP - LEFT WING INBOARD SLAT, INBOARD TRACK FAIRING CRACKED. REPLACED DAMAGED (CRACKED) SLAT FAIRING WITH NEW PER DC-9 SRM 51-01, PAGE 1. (X)SDR DL757970211Te Wedge · delaminatedT/E WEDGE DELAMINATED. REPLACED T/E WEDGE PER SRM 57-43-02.SDR 97UAL900094Flap · crackedDURING C-CHECK. EXTENSIVE CRACKING WAS DISCOVERED ON THE 114W4160-8 SLAT ASSEMBLY. CRACKS EXISTED IN THE 114W4562-4 COVE SKIN ASSEMBLY AND THE 114W6640 NOSE BEAM ASSEMBLY. PRELIMINARY FINDINGS INDICATE THAT CRACKING APPEARS TO BE THE RESULT OF HIGH CYCLE SONSDR UPS97222169Angle · crackedINSPECTION TYPE-C, NR 3 SLAT INBD TRACK INBD VERTICAL SUPPORT ANGLE IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW SRM 51-30-2, 51-10-1.SDR UPS97221923Hinge Lug · crackedNR 1 KREUGER FLAP HAS CRACK ON CENTER HINGE LUG AT BOTTOM BOLT HOLE. REPLACED NR 1 KREUGER FLAP IAW MM 27-81-01. SYS OP/C NORMAL. LANDING LIGHT OP/C NORMAL.SDR UPS97222173Angle · crackedINSPECTION TYPE-C, RT WING L/E NR 5 K-FLAP ACTUATOR I/B SUPPORT ANGLE IS CRACKED AT UPPER AND LWR ENDS. FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW SRM 51-10-1 AND 51-30-2.SDR UPS97222154Angles · crackedINSPECTION TYPE-C, RT WING NR 6 SLAT I/B TRACK BOTH I/B AND O/B VERT MOUNT ANGLE STIFFENERS ARE CRACKED AT LWR END. REMOVED, FABRICATED AND INSTALLED ANGLES IAW SRM 57-10-2, 51-30-2.SDR DL72S970182Rib · crackedONE INCH CRACK IN NOSE RIB NR 5 SLAT ACT ATTACH OUTBOARD SIDE. CORRECTION - DRILLED, TREATED, PRIMED AND INSTALLED DOUBLER PER M/M 57-54-0.SDR CALA9700184Skin · disbondedINSPECTION FOUND TRAILING EDGE OF NR 1 L/E SLAT DISBONDED ALONG ENTIRE LOWER TRAILING EDGE SECTION. THE SLAT WAS REMOVED AND REPAIRED IAW SRM 51-40-5 AND REINSTALLED.SDR COMA9710088Rollers · dirtyOUTBOARD FLAPS FAILED TO RETRACT. REPLACED THE ROLLERS ON THE RT OUTBOARD FLAP.SDR UPS97821912Angle · crackedINSPECTION TYPE: C. LT WING L/E SLOT VANE ATTACH ANGLE I/B END IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW SRM'S 51-1-21, 57-1-1, 51-1-4, 51-1-21, AND DOUGLAS DWG 5769891.SDR CALA9700119Skin · crackedINSPECTION FOUND A .3750 INCH CRACK IN NR 8 SLAT ON BOTH SIDES OF OUTBOARD UPSTOP PAD. THE CRACKED AREA WAS CUT OUT. AN ANGLE AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 51-40-4.SDR UPS97222101Bullnose · corrodedINSPECTION SI-CHECK, NR 1 K-FLAP BULLNOSE CORRODED AT LUGS. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW MM 27-81-01. INSTALLED NEW BULLNOSE IAW MM 27-81-01.SDR UPS97222100Bullnose · corrodedINSPECTION SI-CHECK, NR 3 K-FLAP BULLNOSE CORRODED UNDER OUTBOARD ATTACH POINT. FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 57-50-10. REMOVED CORRODED BULLNOSE AND REPLACED WITH SERVICEABLE IAW SRM 27-81-01.SDR P5CA9700098Bull Nose · corrodedLEVEL 1 CORROSION ON LEFT WING NR 12 LEADING EDGE SLAT BULL NOSE INBOARD END. REPAIRED PER BOEING SRM'S 51-10-01 AND 51-10-02.SDR P5CA9700149Skin · corrodedLIGHT CORROSION/BARE METAL ON SLAT NR 22 AS MARKED LOWER EDGE OF EXTERIOR SKIN. REMOVED CORROSION IAW 51-10-01 AND 51-10-02.SDR P5CA9700079Panel · damagedDAMAGED METAL ON NR 1 LEFT LEADING EDGE PANEL BULLNOSE. BURNISHED AND TRIMMED PANEL PER BAC SRM 51-40-01.SDR DL757971172Wedge · delaminatedT/E WEDGE DELAMINATED, REPLACED WEDGE PER SRM 57-43-2.SDR CALA9700121Rib · crackedINSPECTION FOUND A 1 INCH CRACK IN INBOARD AND OUTBOARD ACTUATOR ROD END ATTACH RIBS OF NR 5 SLAT. THE CRACKS WERE STOP DRILLED IAW SRM 51-10-1. A DOUBLER AND ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2 AND 51-10-1.SDR CALA9700120Skin · crackedINSPECTION FOUND A .75 INCH CRACK IN NR 7 SLAT ON BOTH SIDES OF INBOARD DOWN STOP. A NEW SECTION OF CAP AND CHORD WERE SPLICED IN IAW SRM 51-40-4.SDR UPS97221819Slat · crackedINSPECTION TYPE-N/A, NR 5 SLAT CRACKED AT OUTBOARD STOP THROUGH STOP MOUNTING POINTS. REPLACED NR 5 LEADING EDGE SLAT WITH A BORROWED PART FROM DELTA AIRLINES. WITH REF TO M/M 27-81-11. GRND CHKS GOOD. REMOVED (P/N 65-1 6221-2) (S/N BN46) OFF, (P/N 65-16221-SDR UPS97221840Hinge · corrodedINSPECTION TYPE-C, NR 5 K-FLAP CENTER HINGE FITTING HAS SEVERAL SPOTS OF CORROSION. REMOVED AND INSTALLED NEW HINGE ASSY, WORK DONE IAW SRM 51-30-2, 51-30-5, 51-30-8, 51-10-2, 51-20-04, MM 27-87-01.SDR UPS97221839Rib · crackedINSPECTION TYPE-C, NR 3 SLAT 1ST RIB I/B OF ACTUATOR ROD END CRACKED. REPLACED WITH NEW SLAT ASSY, WORK DONE IAW MM 27-81-11.SDR UPS97221814Spar · crackedINSPECTION TYPE-C, NR 4 SLAT AFT SPAR CRACKED AT O/B END. INSTALLED DOUBLERS PER SRM 51-40-4.SDR RRXA97014Skin · wornDURING A-MAINTENANCE VISIT, FOUND RT WING O/B FLAP LEADING EDGE ASSEMBLY (P/N 5655752-345) WAS CHAFED AND WORN UNDER RIB STRIP, AT XF=244.263. DAMAGE ROUTED OUT IN 2 EACH PLACES, FABRICATED AND INSTALLED FILLERS AND REINFORCING INTERNAL DOUBLER ADDED ON LEADISDR DL72W970034Stiffener · crackedL/E VERTICAL SPAR STIFFENER CRACKED AT NR 3 SLAT O/B TRACK I/B STIFFENER. REPLACED STIFFENER PER MM 57-20-21.SDR 97UAL900049Fitting · crackedDURING ROUTINE L-CHECK, THE LT SLAT NR 1 FAIRING ATTACH FITTING WAS FOUND CRACKED AND NOT REPAIRABLE. MANUFACTURED A NEW FITTING PER DRAWING ARB7131501. INSTALLED FITTING ON AIRCRAFT.SDR DL72E970031Bracket · crackedFOUND ON E1 LETTER CK, NR 1 L/E FLAP ACTUATOR O/B MOUNT BRACKET CRACKED. REPAIRED PER M/M 57-20-21.SDR DL757970023Wedge · delaminatedREPLACED DELAMINATED WEDGE PER SRM 57-43-02.SDR UPS97821845Slot Brace · crackedINSPECTION TYPE-C/CK, LT CENTER LE SLOT BRACE CRACKED AT FWD END O/B OF PANEL 522A TOP SIDE OF LE. REMOVED CRACKED BRACE IAW DC8 SRM 51-1-24 AND DC8 SRM 51-1-20D MATERIAL ID IAW DC8 SRM 57-30D, FABRICATED DOUBLER IAW DC8 SRM 57-2-0 AND DC8 SRM 51-1-24, ALODISDR UPS97221802Ribs · crackedINSPECTION TYPE-C, R/W NR 6 SLAT ACTUATOR RIBS CRACKED AT AFT FASTENER HOLE BOTH SIDES OF ACTUATOR. SLAT WAS REPLACED ON NRC 494364 IAW M/M 27-81-11.SDR CALA9700091Skin · crackedINSPECTION FOUND A 7 INCH CRACK IN NR 2 SLAT LOWER SKIN NEAR ACTUATOR. THE SLAT SKIN WAS REPAIRED IAW ECRA 5750-01159.SDR CALA9700078Skin · crackedINSPECTION FOUND A 8.5 INCH CRACK IN LOWER SLAT SKIN NEAR ACTUATOR. THE AREA WAS REPAIRED IAW ECRA 5750-01159.SDR UPS97222171Fitting · corrosionINSPECTION TYPE-C, RT WING L/E NR 5 K-FLAP ACTUATOR HINGE SUPPORT CASTING HAS HEAVY CORROSION. REMOVED AND REPLACED HINGE FITTING (P/N 65-18532-8) PER DWG NR 65-18532 AND SRM 51-30-2 AND DWG NR 65-16269.SDR 96UAL900987Skin · crackedNR 5 LEADING EDGE SLAT LOWER SKIN CRACK. *S/D* INSPECTED SLAT AND FOUND THREE ADDITIONAL CRACKS ON LOWER SKIN ATTACH ANGLE. STOP DRILLED ALL CRACKS AND SECURED AREA.SDR CALA9601902Skin · crackedINSPECTION FOUND A .5 INCH CRACK AT RIVET IN LOWER SKIN OF NR 6 SLAT AT ACTUATOR. THE SKIN WAS REPAIRED IAW ECRA 5750-01159.SDR CALA9700040Channel · crackedINSPECTION FOUND A .125 INCH CRACK IN AFT SUPPORT CHANNEL AT LT WING NR 4 LEADING EDGE FLAP. THE CHANNEL WAS REPAIRED IAW SRM 51-40-03, FIGURE 2.SDR DL72W962735Skin · crackedINNER SKIN CRACKED BETWEEN RIBS 10/11. REPAIRED PER M/M 57-54-0.SDR CALA9700106Slat · gougedINSPECTION FOUND RT NR 6 SLAT CHAFED AND GOUGED AT INBOARD END, 12 INCHES UP FROM L/E TIP. THE SLAT WAS REPAIRED IAW ECRA 5750-02573.
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