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 2001UALA00144Web · crackedNR 2 INBOARD SLAT WEB CUTOUT AT INBOARD THERMAL ANTI ICE DUCT CRACKED. REPAIRED WEB PER MM 57-45-19.SDR SWAA010359Slat · delaminatedDURING SCHEDULED SERVICE CHECK, FOUND NR 2 L/E SLAT INBD EDGE OF T/E WEDGE DELAMINATED. REPAIRED SLAT PER SRM.SDR EISA20010020Angle · crackedDURING ROUTINE C-CHECK INSPECTION FOUND ANGLE CRACKED IN LEFT WING LEADING EDGE OF NR 3 KRUEGER FLAP. REMOVED ANGLE, FABRICATED AND INSTALLED REPAIR ANGLE, ALODINED AND PRIMED IAW SRM 51-40-3 FIG 1, 51-30-2.SDR EISA20010005Former · crackedDURING ROUTINE C-CHECK INSPECTION FOUND CRACK AT NR 4 SLAT ACTUATOR INBOARD FORMER. STOP DRILLED CRACK, FABRICATED, REPAIR DOUBLER, ALODINED, PRIMED, AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-3, 51-30-2, 51-10-2.SDR DHL2001712502Skin · crackedC-CHECK, FORE FLAP CRACKED 2.0 INCH AT WBL 440. PERFORMED STOP DRILL IAW SRM 57-50-4, FIG 1. FABRICATED DOUBLER (ALCLAD 2024, T3, 0.050 INCH) IAW 57-50-4, FIG 1. CLEANED, TREATED AND PRIMED IAW 51-10-2, PAGE 1 AND 2. INSTALLED DOUBLER IAW SRM 57-50-4, FIG SDR DL72W010178Slat Track · corrodedDURING OVERHAUL THE INBD TRACK, CORROSION AND WEAR WAS FOUND, WHICH WERE BEYOND ALLOWABLE LIMITS, AT MLG BEAM ATTACH BOLT HOLE AND SPOTFACES, SPOILER BEAM ATTACH HOLES, THE MLG DOOR AFT HINGE FITTING HOLES, THE TOGGLE DETENT HOLE AND THE CLIP ASSEMBLY ATTACH BSDR DL72S011907Slat · damagedNR 3 SLAT, B727 REPAIRED PER M/M 57-54-000-8 FIG. 814 AND 804, S/N: BN29, P/N: 65-16222-91SDR AALA20010157Structure · corrodedTUL - FOUND LEFT KRUEGER FLAP HAS CORROSION IN NUMEROUS AREAS INTERNALLY THROUGHOUT VANE. INSTALLED KRUEGER FLAP DOOR. OPS CHECK AND RIGGED OK IAW MM 27-87-11-4. (M)SDR SWAA010313Slat · crackedDURING SCHEDULED C1 CHECK, FOUND 2 INCH CRACKAT NR 6 L/E SLAT EXTENDING FROM AFT ROW OF RIVETS, NEAR CENTER AUX TRACK, OTBD OF PREVIOUS REPAIR. REMOVED AND REPLACED SLAT ASSY PER MM.SDR SWAA010301Slat · delaminatedDURING SCHEDULED C2 CHECK, FOUND RT WING NR 6 L/E SLAT DELAMINATED. REPAIRED L/E SLAT PER SRM.SDR SWAA010300Slat · delaminatedDURING SCHEDULED C2 CHECK, FOUND RT WING NR 5 L/E SLAT DELAMINATED. REMOVED AND REPLACED L/E SLAT PER MM.SDR DL72S010167Angle · crackedFOUND ON C1 LETTER CK, TWO .25 INCH CRACKS IN THE NUMBER 6 SLAT LOWER COVE SKIN ATTACH ANGLE. REPAIRED PER MM 57-54-000-8.SDR UPS01834845Doubler · brokenINSPECTION TYPE:C1&3, LEFT WING L/E LOWER INTERNAL DOUBLER HAS A CORNER BROKEN OFF AT XS 520. REMOVED AND REPLACED DOUBLER AND SKIN IAW DWG 5769759, AND SRM 51-1-20D, 51-1-21.SDR UPS01834844Attach Angle · crackedINSPECTION TYPE:C1&3, LEFT WING CENTER L/E VERTICAL ATTACH ANGLE IS CRACKED AT XS 520. REMOVED, FABRICATED, AND REPLACED ANGLE IAW DWG 9753297, AND SRM 51-1-20D.SDR DHL2001740C14Attach Angle · corrodedNR 5 L/E SLAT I/B TRACK ROLLER SUPPORT O/B VERTICAL ATTACH ANGLE HAS CORROSION AT LOWER SPAR. INSTALLED NEW VERTICAL ATTACH ANGLE PER B727 SRM 57-10-2 AND 51-30-2.SDR DL72W010122Skin · crackedA 1 INCH CRACK AT NR 2 SLAT LWR COVE SKIN ANGLE O/B END. REPAIRED PER MM 57-54-0.SDR DL757010175Skin · delaminatedSLAT DELAMINATED. NUMBER ONE SLAT SEALER CRACKED AND T/E WEDGE DELAMINATED AT UPPER OUTBD T/E. REF SUPPLEMENTAL CARD ATTACHMENT A.SDR SWAA010194Skin · debondedDURING SCHEDULED C1 CHECK, FOUND LT WING OUTBOARD FORE FLAP DISBONDED AT T/E, INBOARD SECTION. REMOVED AND REPLACED FORE FLAP PER MM.SDR SWAA010183Skin · damagedDURING SCHEDULED 1/4D CHECK, FOUND LT WING L/E INBOARD FORE FLAP HAS 10 INCH CREASE ON UPPER SURFACE. REMOVED AND REPLACED INBOARD FORE FLAP PER MM.SDR DL72S010101Skin · crackedA .5 INCH CRACK AT NR 6 SLAT I/B TRACK CUTOUT. REPAIRED PER MM 57-20-021-8.SDR DL72S010100Stiffener · crackedFWD SPAR STIFFENERS CRACKED AT I/B AND O/B SIDES OF NR 7 L/E SLAT I/B TRACK. BOTH REPAIRED PER MM 57-20-021-8.SDR DL72S010099Stiffener · crackedFWD SPAR STIFFENERS CRACKED AT I/B AND O/B SIDES OF NR 6 L/E SLAT I/B TRACK. BOTH REPAIRED PER MM 57-20-021-8.SDR DHL2001740C22Structure · gougedLEFT WING INBOARD FORE FLAP OUTBOARD END HAS DEEP GOUGE IN PREVIOUS REPAIR DOUBLER. INSTALLED DOUBLER PER B727 SRM 51-30-2. SIZE OF MATERIAL USED 5 X 6 INCHES.SDR SWAA010153Skin · delaminatedDURING SCHEDULED 1/4D CHECK, FOUND LEFT WING L/E OUTBOARD FORE FLAP T/E DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.SDR SWAA010142Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND NR 2 L/E SLAT AFT OUTBOARD EDGE DELAMINATED. REPAIRED SLAT PER RA 1-357-0946.SDR COMA0160119Vane · chafedTHE RIGHT AND LEFT FLAP VANES, I/B LEADING EDGE SKINS WERE DAMAGED AND CHAFED WHERE THE FLAP VANE COMES IN CONTACT WITH THE RESTRAINING PADS. ALSO THE LEFT I/B FLAP VANE, MID LEADING EDGE WAS DAMAGED AND CHAFED. PERFORMED A MAJOR REPAIR BY REPLACING CHAFED VSDR DHL2001740C21Skin · dentedLEFT WING INBOARD FORE FLAP HAS DENT AT CENTER ACCESS PANEL 8442 MAKING CONTACT WITH NR 6 SPOILER ACTUATOR ROD END. INSTALLED NEW ACCESS PANEL PER B727 SRM 51-30-2. SIZE OF REPAIR 8 X 8 INCHES.SDR SWAA010050Skin · crackedDURING SCHEDULED 1/4D CHECK, FOUND NR 2 L/E SLAT LOWER SKIN CRACKED NEAR OUTBOARD END. REPAIRED SKIN PER SRM.SDR SWAA010035Slat · crackedDURING SCHEDULED 1/4D CHECK, FOUND NR 1 L/E SLAT CRACKED AT TWO ADJOINING RIVET HOLES, INBOARD OF INBOARD MAIN TRACK AND OUTBOARD OF INBOARD AUX TRACK. REPAIRED SLAT PER SRM.SDR RRXA10791Spoiler Panel · delaminatedDURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO R/H #3 SPOILER AT #3 R/H SPOILER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 MM 27-61-1 ASDR RRXA10790Spoiler Panel · delaminatedDURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO R/H #4 SPOILER AT #4 SPOILER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 MM 27-61-1.SDR UPS01434807Channel · crackedINSPECTION TYPE:C, LT WING L/E LEADING EDGE FLAP DRIVE UNIT SUPPORT CHANNEL CRACKED AT POSITION NR 2 LEFDU. SUPPORT CHANNEL REPAIRED IAW SRM 51-40-03.SDR RRXA10776Panel · delaminatedDURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO LT. WING #1 SPOILER AT #1 PANEL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 MM 27-61-1.SDR UPS01434806Mount · crackedINSPECTION TYPE:C, R WING L/E KRUEGER FLAP NR 15 INBOARD HINGE MOUNT CRACKED. NEW FLAP ASSY FITTED IAW MM 27-81-01.SDR UPS01234770Angle · crackedINSPECTION TYPE:C, RT WING NR 6 LE SLAT, I/B TRACK RECESS CUTOUT 2 ANGLES CRACKED, I/B AND O/B AT LWR END OF ANGLE. REMOVED AND REPLACED 2 ANGLES IAW SRM 57-10-2.SDR UPS01234767Angle · crackedINSPECTION TYPE:C, RT WING NR 6 LE SLAT, O/B TRACK RECESS CUTOUT, I/B VERT ANGLE CRACKED AT LWR END. REMOVED AND REPLACED I/B VERT ANGLE IAW SRM 51-30-2.SDR UPS01434856Hinge · crackedINSPECTION TYPE:C, RT WING L/E NR 15 KRUEGER FLAP O/B FOLDING FAIRING ATTACH HINGE FITTING IS CRACKED. P/N 65B02471-10. DUE TO ADDITIONAL DAMAGE ON FLAP, FLAP REPLACED.SDR DL72S010010Angle · crackedFOUND ON MV2 CHECK, .75 INCH CRACK NR 8 SLAT COVE SKIN ANGLE BELOW THE ANTI-ICE DUCT. REPAIRED PER MM 57-54-000-8.SDR SWA002790Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND LT WING L/E OUTBOARD FORE FLAP DELAMINATED AT INBOARD T/E. REMOVED AND REPLACED FORE FLAP PER MM.SDR AU001288Slat · debonded(AUS) RT WING NR 7 LEADING EDGE SLAT TRAILING EDGE WEDGE DISBONDING ON UPPER AND LOWER SURFACES.SDR SWA002775Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND 15 X 17 DELAMINATION ON RT WING L/E INBOARDD FORE FLAP. REMOVED AND REPLACED FORE FLAP PER MM.SDR RAIA0012059Skin · damaged7108-STL-DURING TAXI OUT AIRFRAME ANTI ICE FAULTED. MAINTENANCE REMOVED AND REPLACED LEFT HAND CENTER LEADING EDGE IAW J41 MAINTENANCE MANUAL.SDR SWAA002758Structure · crackedDURING SCHEDULED 1/4D CHECK, FOUND NR 2 L/E SLAT CRACKED AT RIVET HOLES OUTBOARD OF ACTUATOR. REPAIRED SLAT PER SRM.SDR DL72W002523Slat · missingDURING APPROACH CONTROLS REQUIRED 20 DEGREES RIGHT AILERON AND 2 UNITS RIGHT RUDDER TO TRACK CENTER LINE. CA FOUND SECTION OF FOREFLAP MISSING FROM LT OUTBD T.E FLAP - REPLACED FLPA PER M/M. OPS CHK OKSDR SWAA002734Flap Track · brokenLT WING L/E INBOARD FORE FLAP TRACK ARM BROKEN. R&R FORE FLAP PER MM.SDR USAA002195Skin · crackedCLT - FOUND SLAT SKIN .375 INCH, LOWER SKIN NR 3 L/E SLAT MID SPAN. INSTALLED DOUBLER PER TR 57-50-01 DRAWING 65C30133. (M)SDR AWXA0001117Skin · dentedDENT ON RT IB FOREFLAP LOWER SKIN SURFACE AT WBL 120. DENT OUT OF LIMITS IAW SRM 57-53-02; REMOVED DAMAGED SKIN; CLEANED AREA; FABED REPAIR PARTS; HF/ALODINED AND APPLIED BONDING PRIMER TO BOND SURFACES; INSTALLED REPAIR PARTS WITH METAL TO METAL HOT BOND REPASDR ASAA0070005ASlat · wornSEA - DURING MAINTENANCE CHECK, TWO DEEP WEAR MARKS WERE FOUND IN THE NR 2 SLAT TRAILING EDGE AT SLAT STATION 382.5. REPAIRED PER EA 5740-01237. (M)SDR ASAA0070005Skin · damagedSEA - DURING MAINTENANCE CHECK, TWO DEEP WEAR MARKS WERE FOUND IN THE NR 3 SLAT TRAILING EDGE AT SLAT STATION 259.2. REPAIRED PER EA 5740-01236. (M)SDR AWXA0001114Stiffener · crackedLT WING LWBL 184 TE AT NR 3 FLAP TRACK FAIRING INBOARD FORMER/STIFFENER CRACKED. REMOVED AND REPLACED STIFFENER IAW SRM 51-40-02
Back to JASC 5754