JASC 5754
Service difficulty reports · 17,344
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 UPS06847406Rib · crackedLT CENTER LE UPPER RIB CRACKED AT XFS 334. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLES 2 IAW SRM 57-02-00 FIG 002, 57-03-03 FIG 005 AND 51-1-20D.SDR UPS06847405Rib · crackedFOUND LT CENTER LE UPPER RIB CRACKED AT XS454. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0 FIG 2 AND 51-1-20A.SDR UPS06847376Rib · crackedC1, 3 RT CENTER LEADING EDGE UPPER RIB AT XFS 415 IS CRACKED. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0 FIG 002, 51-1-21 AND 51-1-20D.SDR UPS06847371Rib · crackedC1, 3 RT CENTER LEADING EDGE UPPER RIB CRACKED AT XFS409. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 51-1-21, 57-02-00 FIG 2, 57-03-03 FIG 5.SDR 06FDEA02547Attach Fitting · damagedEXISTING REPAIR AT LT NR 8 L/E SLAT RIB DRIVE TRACK ATTACH LUG HOLES AT OSS 1065.695(ER/A372144-14) SNRM N00313: EXISTING REPAIR AT LT NR 8 L/E SLAT RIB DRIVE TRACK ATTACH LUG HOLES OSS 1065.695 EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED PER DELTA ENG'G REPAISDR UPS06847370Rib · crackedC1, 3 LT OB LEADING EDGE RIB CRACKED AT XFS 746 UPPER RIB. STOP DRILLED CRACK, FABRICATED AND INSTALLED 2 EACH DOUBLERS IAW SRM 57-02-00 FIG 2 SHT 2, 51-01-20D AND 51-01-15.SDR UPS06847367Rib · crackedC1,3 LT OB LEADING EDGE UPPER RIB CRACKED AT XFS 752. FABRICATED AND INSTALLED 2 EACH DOUBLERS IAW SRM 57-02-00 FIG 2 SHT 2, 21-1-20D AND 51-1-15.SDR SWAA062413Skin · crackedDURING SCHEDULED C4 CHECK, FOUND RT WING NR 6 L/E SLAT SKIN CRACKED AT LOWER T/E. REPAIRED L/E SLAT SKIN PER SWA EA.SDR UPS06847411Rib · crackedRT OB LE LWR RIB CRACKED AT XFS 796. STOP DRILLED CRACK, FABRICATED AND INSTALLED 2 DOUBLERS IAW SRM 57-02-00 AND 51-1-21.SDR UPS06847408Rib · crackedRT OB LE UPPER RIB CRACKED AT XFS 834. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-02-00 FIG 002, 51-1-21 AND 51-1-20D.SDR UPS06847377Rib · crackedC1, 3 RT OB LEADING EDGE UPPER RIB CRACKED AT XFS834. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-02-00 FIG 002, 51-1-21 AND 51-1-20D.SDR UPS06847372Rib · crackedC1, 3 RT OB LEADING EDGE LWR RIB CRACKED AT XFS 734. FABRICATED AND INSTALLED STACK ANGLE REPAIR IAW SRM 57-02-00 AND 51-1-20D.SDR 06FDEA2528Finger Doubler · crackedRIGHT WING LEADING EDGE CAVITY THROUGH ACCESS PANEL 619CB CEILING AREA FINGER DOUBLER AS MARKED AT XOS 625. REPAIRED AS PER FEDEX E.A. 1-5730-100703.SDR 06FDEA2524Finger Doubler · crackedRIGHT WING LEADING EDGE CAVITY THROUGH ACCESS PANEL 619CB CEILING AREA FINGER DOUBLER AS MARKED. REPAIRED AS PER FEDEX EA 1-5730-100703.SDR 06FDEA2514Rib · crackedFOUND LT WING NR 16 SLAT TRACK I/B RIB CRACKED AS MARKED.SDR 06FDEA2513Rib · crackedFOUND RT WING NR 16 SLAT TRACK I/B RIB CRACKED AS MARKED.SDR 06FDEA2491Skin · damagedFOUND RT WING NR 3 SLAT LE SURFACE FOUND DAMAGED. REPAIR CARRIED OUT ON RT WING NR 3 SLAT L/E SURFACE AS PER SRM 57-10-00 FIG.33 VOL.I.REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR UPS06247520Rib · crackedSUSPECT CRACK ON NR 6 SLAT ON 4TH RIB OB OF ACTUATOR AT UPPER AFT CORNER RIB REPLACED IAW SRM 51-30-02.SDR UPS06247518Rib · crackedSUSPECT CRACK ON NR 6 SLAT ON 1ST RIB O/B OF I/B TRACK ALONG AFT FLANGE. RIB REPLACED IAW SRM 51-10-02, AND INSTALLED IAW SRM 51-30-02.SDR UPS06247437Rib · crackedINSPECTION TYPE:C SUSPECT CRACK ON NR 5 SLAT 3RD RIB O/B OF IB TRACK AT AFT UPPER CORNER. SLAT REPLACED.SDR ASAA0680747Skin · dentedRIGHTHAND NR 1 SLAT LEADING EDGE DENTED. REMOVED DAMAGED AREA. INSTALLED REPAIR DOUBLER PER SRM 57-09.SDR 06FDEA2459Skin · crackedFOUND CRACKED FASTENER HOLE AT UPPER SURFACE OF RT WING DROOP LE SLAT. WORK CARRIED OUT AS PER E.A.1-5740-99695 REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR DU4R2006546Skin · chafedRIGHT WING NR 2 SLAT AT MID TRACK, L/E CHAFED ON I/B SIDE. FABRICATED AND INSTALLED REPAIR DOUBLER 6 X 6.5 INCHES FROM 7075-T6 .063 IAW MD80 SRM 51-10-3, 51-30-5, AND 51-30-2.SDR DHL2006762501Frame · crackedNR 6 SLAT AT ACT ROD END ATTACHMENT WS 515 HAS BOTH I/B & O/B FRAMES CRACKED FWD. REMOVED I/B & O/B NR 6 SLAT FRAMES AT WS 515 IAW B727 SRM 51-30-2, FAB NEW I/B & O/B FRAMES FROM 20024-0 .040 PO 9003230 DIM. FOR BOTH FRAMES 6 X 16 INCHES IAW B727 SRM 57-50-2SDR AWXA200601106Skin · crackedFOUND CRACKS, BOTTOM NR 2 SLAT SKIN AT OUTBD AUX TRACK. REMOVED FIVE CRACKS, BOTTOM NR 2 SLAT SKIN AT OUTBD AUX TRACK, VERIFIED ALL CRACKS REMOVED, FABRICATED FILLER AND DOUBLER FOR REPAIR AND INSTALLED REPAIR IAW B 737-300 SRM 57-43-01-2 RG FIG 201.SDR AWXA200601105Skin · crackedFOUND FIVE CRACKS, BOTTOM NR 1 SLAT BLOW INBD AUX TRACK. REPAIRED FIVE CRACKS BOTTOM NR 1 SLAT SKIN BELOW INBD AUX TRACK IAW B737-300 SRM 57-43-01-2RG FIG 201.SDR UIEA200600147Skin · puncturedLEFT AFT T/E FLAP LOWER SKIN HAS A PUNCTURE MARK LOCATED 125 INCHES FROM I/B & 9 INCHES FWD OF AFT EDGE. PUNCTURE MARKS REPAIRED IAW ATLAS AIR SRM 747-400F 57-53-01 PG 102 REF D & F REVISION 43 FIG 101.SDR UIEA200600145Skin · puncturedRIGHT I/B FORE FLAP LOWER SKIN 4 PUNCTURE MARKS ALL APPROX .100 DIA LOCATED AT 1) 65.5 INCHES FROM I/B EDGE & 6.75 INCHES FROM AFT. 2) 64.5 INCHES FROM I/B EDGE & 9.5 INCHES FROM AFT EDGE. 3) 60 INCHES FROM I/B EDGE & 14 INCHES FROM AFT EDGE. 4) 56.5 INCHES SDR 06FDEA2415Skin · crackedSNRM N02174: RT WING NR 7 SLAT INTERIOR SURFACE MID SECTION SUSPECT SKIN CRACK. REPAIRED AS PER SRM 57-10-00 FIG.10 VOL.I. REPAIR CLASSIFIED AS MAJOR REPAIR PER GMM 6-2-100.SDR PIDA06048Skin · delaminatedDURING A-5 CHECK, WHILE ACCOMPLISHING INSPECTION IN ACCORDANCE WITH AD 90-23-06, FOUND NR 10 LEADING EDGE SLAT DELAMINATED ON UPPER SURFACE 15 INCHES FROM INBOARD END JUST BEHIND A PREVIOUS REPAIR. REPLACED SLAT PER MM 27-81-02.SDR USAA060861Skin · crackedNR 9 SLAT COVE SKIN AT D/B TRACK CUT-OUT AREA. FABRICATED AND INSTALLED NEW 966 AND 967 ANGLES IAW BOEING DWG 114N4003 AND SRM 57-43-01 FIG 01. DEFECT SIZE: 1.50"SDR USAA060862Skin · crackedNR 10 SLAT COVE SKIN AT I/B TRACK CUTOUT ANGLE. FABRICATED AND INSTALLED NEW PANEL IAW BOEING DWG 114N4002 AND SRM 57-43-01 DEFECT SIZE: .75"SDR USAA060863Skin · crackedNR 10 SLAT COVE SKIN OUTBD TRACK. FABRICATED AND INSTALLED NEW PANEL IAW BOEING DWG 114N4002 SRM 57-43-01. DEFECT SIZE: .125SDR DU4R2006516Skin · dentedS/O 291016 NR 20089 LT WING L/E SLAT NR 1 HAS SEVERAL DENTS ON TOP. CUT OUT DENTED AREA OF SKIN. FABRICATED AND INSTALLED SLAT NOSE REPAIR 14.25" X 2.55" AND 2.25" X 2.80" FROM 2014-T6 .050", AND 2.25" DIAMETER FROM 2024-T3 .100" AND SLAT LEADING EDGE REPAIRSDR SWAA062146Skin · crackedDURING SCHEDULED 20Y CHECK, FOUND RT WING NR 5 L/E SLAT LOWER SKIN CRACKED AT INBOARD RIB ATTACHMENT. REPAIRED SKIN PER SRM.SDR SWAA062127Structure · delaminatedDURING SCHEDULED C4 CHECK, FOUND RT WING NR 5 L/E SLAT DELAMINATED. REMOVED AND REPLACED NR 5 L/E SLAT PER MM.SDR MWEA060066Fitting · corrodedRIGHT NR 2 SLAT HAD CORROSION ON TRACK IDLER NR 6 FITTING. FABRICATED AND INSTALLED SLAT.SDR MWEA060065Fitting · corrodedRIGHT NR 2 SLAT HAS CORROSION ON NR 7 TRACK IDLER FITTING. FABRICATED AND INSTALLED SLAT.SDR MWEA060064Fitting · corroded7 RIGHT LEADING EDGE NR 2 SLAT CORROSION OUT BOARD FITTING BOLTS HOLTS. FABRICATED AND INSTALLED SLAT.SDR MWEA060063Skin · corrodedRIGHT LEADING EDGE SLAT HAS LIGHT SURFACE CORROSION ON OUTBOARD ECCENTRIC HOLE FITTING NR 8. FABRICATED AND INSTALLED SLAT.SDR ASAA0640718Structure · delaminatedNUMBER 2 SLAT IS BULGED AND DELAMINATED AT TRAILING EDGE INBOARD CORNER. PREPPED DELAMINATED AREA, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 51-70-10.SDR UPS06247273Rib · crackedNR 6 SLAT SUPPORT RIB CRACKED, ABOUT 9 INCHES FROM SLAT I/B END. REMOVED DAMAGE IAW SRM 51-10-01. HFEC CARRIED OUT AROUND CUTOUT IAW B7 27-NDTM 51-00-00 PT 6 FIG 4, NDF. REPAIR DOUBLER FORMED IAW SRM 57-50-3. NR 6 SLAT SUPPORT RIB CAD PLATING CARRIED OUT ISDR UPS06247210Rib · crackedINSPECTION TYPE:C NR 6 SLAT SUPPORT RIB CRACKED, ABOUT 9 INCHES FROM THE SLAT O/B END. REMOVED DAMAGE IAW SRM 51-10-1. HFEC CARRIED OUT AROUND CUTOUT IAW B72 7NDTM 51-00-00 PT 6 FIG 4. REPAIR DOUBLER FORMED IAW SRM 57-50-3. DRILLED AND SHAPED DOUBLER IAW SRSDR UPS06247207Rib · crackedINSPECTION TYPE:C NR 6 SLAT SUPPORT RIB CRACKED ABOUT 9 INCHES FROM SLAT I/B END. REMOVED DAMAGE IAW SRM 51-10-1. HFEC CARRIED OUT AROUND CUTOUT IAW B72 7NDTM 51-00-00 PT 6 FIG 4. SUPPORT RIB REPAIR DOUBLER FORMED IAW SRM 57--50-3. DOUBLER SHAPED AND DRILLSDR ASAA0640705Structure · delaminatedNR 2 SLAT DELAMINATED AT OUTBOARD TRAILING EDGE CORNER. PREPPED DELAMINATED AREA, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 51-70-10.SDR AWXA200601041Wedge · debondedDURING C15 CHECK DISCOVERED DISBOND AREA ON THE UPPER SURFACE OF THE NR 5 SLAT WEDGE, OUTBOARD END AT SLAT STATION (SS) 252.27 TO SS 254.27. MAINTENANCE REMOVED PREVIOUS REPAIR DOUBLER AND DISBOND AREA ON UPPER SURFACE OF THE NR 5 SLAT WEDGE. FOUND LOWER SURSDR AWXA200601040Wedge · debondedMCN - MAJOR REPAIR - NR 5926347 - DURING C-15 CHECK DISCOVERED DISBOND AT NR 4 SLAT UPPER AND LOWER SURFACE OF WEDGE AT INBOARD END. MAINTENANCE REPAIRED UPPER AND LOWER SURFACE OF NR 4 SLAT WEDGE END IAW BOEING 737-300 SRM 51-70-10-2R4 REPAIR 4.SDR UPS06247285Intercostal · crackedINSPECTION TYPE:C NR 3 SLAT AT O/B TRACK ATTACHMENT TO SLAT, CRACK ON INTERCOSTAL. FASTENERS REMOVED IAW SRM 51-30-02 AND CRACK CUTOUT IAW SRM 57-50-03. O/B SLAT TRACK DISPLACED AT FWD ATTACHMENT AREA IAW OHM 57-51-51. REPAIR DOUBLER FABRICATED IAW SRM 57-5SDR UPS06247278Intercostal · crackedNR 3 SLAT AT O/B TRACK ATTACHMENT TO SLAT CRACK ON INTERCOSTAL. FASTENERS REMOVED IAW SRM 51-30-02 AND CRACK CUT OUT IAW SRM 57-50-03. REPAIR DOUBLER FABRICATED IAW SRM 57-50-03. CAD PLATING CARRIED IAW SO PM 20-42-10. REPAIR INSTALLED IAW SRM 57-50-03. FSDR UPS06M47135Structure · crackedINSPECTION TYPE:N/A RIGHT WING INBOARD SLAT HAS A 16 INCH CRACK ON THE INBOARD END. A/C FERRIED TO SDF FOR REPAIR. REMOVED RT INBD SLAT PER MM 27-80-20-4. OK TO INSTALL NEW SLAT. INSTALLED RT NR 1 SLAT TO STEP NR 1 ALL BOLTS REQUIRE TORQUE AND SECURE PERFORM
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