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 CALA9800230Skin · crackedINSPECTION FOUND SEVERAL .375 INCH CRACKS FROM FASTENER HOLE AT NR 4 SLAT UPPER SKIN WHERE INBOARD HOOK MOUNTS. TWO .375 INCH CRACKS WERE FOUND AT NR 4 SLAT UPPER SKIN WHERE OUTBOARD HOOK MOUNTS. DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 57-50-3.SDR CALA9800226Rib · crackedINSPECTION FOUND A 2 CRACK IN NR 2 LEADING EDGE SLAT RIB OUTBOARD OF ANTI-ICE DUCT. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 57-50-3.SDR DHL9872445CTrack · crackedAT C-CHECK, CRACK AT R/W L/E AT NR 6 I/B TRACK. CUT OUT DAMAGED AREA, INSTALLED DOUBLER PER SRM 57-30-4, 3 X 6, FILLER 1 X 1.5. N/R 2383.SDR UPS98225874Rib · crackedINSPECTION TYPE-SI, WHILE WORKING CARD NR 465720 FOUND CRACKED RIB ON L/W NR 3 SLAT AT SLAT STA 128 TO 950. REMOVED CRACKED RIB, REPLACED WITH NEW RIB IAW SRM 51-30-2.SDR EISA98038Guide · chippedDURING C-CHECK, FOUND NR 2 SLAT GUIDE CHIPPED AT WS 620 LT TOP OF FLAT TRAILING EDGE. INSTALLED SLAT TRAILING EDGE DOUBLER PER SRM 57-50-03. (M)SDR DHL9872458CAngle · crackedAT C-CHECK, NR 3 SLAT ACTUATOR DOOR, I/B ATTACH ANGLE ON THE UPPER SIDE CRACKED AT FWD FASTENER. REPLACED ANGLE PER SRM 51-30-2. N/R 1081.SDR DHL9872408CSkin · crackedAT C-CHECK, NR 4 SLAT LOWER SKIN IS CRACKED AT CUTOUT FOR O/B UP STOP PAD. STOP DRILLED CRACK, FABRICATED REPAIR DOUBLER AND INSTALLED PER SRM 51-40-2, 6 X 4.5. N/R 1086.SDR DL72L980307Rib · crackedFOUND AT F1 LETTER CK, 1.25 INCH CRACK AT NR 6 SLAT I/B ACTUATOR ATTACH RIB. REPAIRED PER M/M 57-54-0.SDR DL72L980306Angle · crackedFOUND AT F1 LETTER CHECK, .5 INCH CRACK AT NR 7 SLAT COVE SKIN ANGLE AT I/B UPSTOP PAD. REPAIRED PER M/M 57-54-0.SDR DL757980302Wedge · delaminatedTHE NR 7 SLAT TRAILING EDGE WAS FOUND WITH A 4 X 5.5 AREA OF DELAMINATION ON THE LOWER SURFACE. THE DAMAGE WAS REPAIRED PER THE B757 SRM 51-70-10 AND DOCUMENTED PER ER/A 363912-14.SDR DL72S980292Stiffener · crackedL/E SPAR STIFFENER CRACKED NR 2 SLAT O/B TRACK I/B SIDE. REPAIRED PER MM 57-20-21 PG 813.SDR DL72S980291Stiffener · crackedFOUND AT E1 LETTER CK, L/E SPAR STIFFENER CRACKED I/B SIDE OF 7 SLAT I/B TRACK. REPAIRED PER M/M 57-20-21.SDR DL72S980290Stiffener · crackedFOUND AT LETTER CHECK E1, L/E SPAR STIFFENER CRACKED O/B SIDE NR 7 SLAT O/B TRACK. REPAIRED PER M/M 57-20-21.SDR CALA9800175Skin · dentedINSPECTION FOUND A 2 X 3 DENT IN LT INBOARD LEADING EDGE SLAT WITH SIX POPPED RIVETS AT STA XIS 240.844. REPAIRED IAW ECRA 5750-02897 AND PLACED ON DIP TO REPLACE RIB WITHIN 365 DAYS OR NEXT C-CHECK.SDR P2EA98020Rib · crackedSJO - DURING C-CHECK, LEFT WING NR 1 SLAT AREA, INBOARD RAIL, OUTBOARD RIB CRACKED. REPAIRED IAW BOEING DRAWING 65C25658. (M)SDR DL757980247Wedge · delaminatedTHE NR 9 SLAT ON THE RT WING WAS FOUND WITH 1.25 AREA OF DELAMINATION ON THE TRAILING EDGE WEDGE, 39 FROM THE OUTBD END. THE WEDGE WAS REPAIRED PER B757 SRM 51-70-10 AND DOCUMENTED PER ER/A 363885-14AD.SDR CALA9800135Angle · crackedINSPECTION FOUND, A 2.25 INCH AND 1.5 INCH CRACK AT INBOARD UPSTOP AREA BELOW TELESCOPING ANTI-ICE DUCT OF LT WING NR 2 SLAT CHORD ANGLE. THE ANGLE WAS REPAIRED IAW SRM 51-40-3.SDR CALA9800115Skin · crackedINSPECTION FOUND A .375 INCH CRACK IN LT WING NR 4 SLAT LOWER SKIN JUST OUTBOARD OF INBOARD TRACK AREA. THE CRACKED AREA WAS BLENDED OUT. A PATCH REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-50-1, 51-10-2, AND 57-50-3.SDR MZZA98073Angle · crackedKUL - Q-CHECK - NR 2 SLAT LOWER SKIN ATTACH ANGLE FOUND WITH TWO CRACKS AT TAI DUCT CUT-OUT AT SLAT STA 271. FORMED SECTION REPAIR CUT-OUT IAW ECRA 5750-02901. (X)SDR TWAA9804010Skin · delaminatedLAX - DURING C-CHECK MAINTENANCE, FOUND THE RT WING NR 8 LE SLAT REPAIR DELAMINATED AT INBOARD UPPER EDGE. INSTALLED HOT BOND REPAIR PER SRM 51-70-10 PAGE 23. (M)SDR DL757980198Wedge · delaminatedTHE NR 10 SLAT WAS FOUND WITH A 2 X 2 AREA OF DELAMINATION ON THE TRAILING EDGE WEDGE. THE WEDGE WAS REPAIRED PER B757 SRM 51-70-10 AND DOCUMENTED PER ER/A 363806-14AD.SDR DL72S980279Stiffeners · cracked2 EA WING L/E SPAR STIFFENERS CRACKED NR 3 L/E SLAT OUTBD TRACK ROLLER FITTING ATTACH. INSTALLED NEW ANGLES PER M/M 57-20-21.SDR P5CA9800149Bracket · crackedNR 15 L/E FLAP BULLNOSE ATTACH ARM BRACKET MOST I/B IS CRACKED. REPLACED ARM BRACKET PER SRM 51-10-01.SDR P5CA9800135Web · crackedNR 16 L/E FLAP O/B WEB UPPER RADIUS CRACKED. STOP DRILLED AND REPAIRED PER SRM 51-40-03 FIG 1.SDR P5CA9800111Web · crackedNR 13 L/E FLAP PANEL I/B WEB UPPER RADIUS CRACKED. REPAIRED PER SRM 51-40-03 FIG 3.SDR P5CA9800110Bracket · crackedNR 13 L/E FLAP BULLNOSE MOST I/B ATTACH ARM BRACKET ON FLAP PANEL IS CRACKED. REPLACED BRACKET PER SRM 51-10-01.SDR P5CA9800109Bracket · crackedNR 14 LE FLAP BULNOSE FAIRING MOST I/B AND MOST O/B ATTACH ARM TO FLAP PANEL BRACKETS ARE CRACKED. REPLACED BRACKETS PER SRM 51-10-01.SDR P5CA9800108Rib · crackedNR 14 L/E FLAP PANEL I/B WEB LOWER RADIUS CRACKED. REPLACED FLAP SUPPORT RIB PER SRM 51-10-01.SDR MWEA98077Slat · dentedTHE NR 5 RT SLAT LEADING EDGE HAS 3 DENTS OUT OF SERVICEABLE LIMITS. MTC INSTALLED REPAIR IAW TEL-X ISC-MIS-005/DC/RBH.SDR MZZA98064Rib · crackedTNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, 2 SUB-STANDARD REPAIR WERE FOUND IN RT WING L/E NR 6 SLAT ACTUATOR OUTBOARD RIB. THE DAMAGED SLAT ACTUATOR OUTBOARD RIB WAS REMOVED AND REPLACED WITH NEW RIB PER B727 SRM 57-50-2 AND 51-30-2. (M)SDR AALA980126Structure · corrodedTUL - KRUEGER FLAP RT WING, UPPER SECTION HAS MODERATE CORROSION ON RIBS AND SKIN INTERNALLY. REMOVED AND REPLACED KRUEGER FLAP WITH SERVICEABLE PART PER SRM 51-72-10-0. FIT CHECK AND OPS CHECK PERFORMED ON E-58 NR 2376654. (X)SDR MZZA98063Skin · crackedTNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A SUB-STANDARD EXTERNAL REPAIR WAS FOUND ON RT WING NR 6 SLAT NOSE AREA AT SS 122. THE EXISTING EXTERNAL REPAIR WAS REMOVED AND REPLACED WITH NEW STANDARD EXTERNAL REPAIR PER B727 SRM 57-50-3 FIGURE 1SDR DL72S980097Angle · crackedFOUND DURING F-2 LETTER CHECK, NR 7 SLAT COVE SKIN ANGLE CRACKED O/B OF I/B UPSTOP PAD. REPAIRED PER M/M 57-54-0.SDR UPS98225467Lug · corrodedINSPECTION TYPE-SI, NR 4 K-FLAP HAS CORROSION ON O/B UPPER LUG WHERE BONDING JUMPER ATTACHES. REMOVED AND REPLACED NR 4 K-FLAP IAW OHM 57-51-21 AND MM 27-81-01.SDR VJ9800021Plate · damagedDURING C CHECK, FOUND NR 2 SLAT REQUIRED REPLACEMENT. FABRICATED AND INSTALLED IAW DC9 SRM 57-09 FIG 10A AND AEROCORP EO 98-795.SDR DL72S980063Skin · crackedNUMBER 4 L/E SLAT HAD A CRACK FROM THE FENCE MOUNTING BOLT HOLE. INSTALLED A REPAIR DOUBLER PER M/M 57-54-0.SDR DL72L980021Spar · crackedFRONT SPAR CRACKED. REPAIRED SPAR PER SRM 51-40-3 (REF 57-50-2) ENG SIG.SDR DL72L980020Skin · crackedCRACK IN LWR T/E SKIN AT ACTUATOR FITTING. REPAIRED SKIN PER SRM 57-50-3.SDR UPS98225402Bonding Jumper · corrodedINSPECTION TYPE-SI, NR 5 K-FLAP O/B LOWER BONDING JUMPER HAS CORROSOION WHERE JUMPER ATTACHES. CORROSION FOUND OUT OF LIMITS PER SRM 57-50-01. CORROSION DAMAGE REMOVED AND STANDARD REPAIR COMPLETED PER SRM 57-50-3, SRM 51-20-2 AND SRM 51-30-00.SDR DL757980002Skin · delaminatedAIR TURNBACK, A PORTION OF THE NR 6 L/E SLAT DELAMINATED AND RIPPED OFF. INSPECTION FOUND UPPER AFT PORTION OF THE NR 6 L/E SLAT DID DELAMINATE RIPPING OFF A QTY OF THE UPPER SLAT. ALSO, FOUND WAS A HOLE IN THE L/E OF THE WING APPROX 4.5 FT INBD OF THE RT ENSDR DHL9871748CRib · crackedAT C CHECK, NR 4 SLAT INBD RIB CRACKED AT ACTUATOR ATTACH. INSTALLED RIB REPAIR PER SRM 57-50-3, 4 BY 5 FT, N/R 1227.SDR DHL9871742CCasting · corrodedAT C CHECK, FITTING ON CASTING AT NR 1 KRUEGER FLAP CENTER ATTACHMENT TO WING. REMOVED AND REPLACED CASTING PER SRM 51-10-1, N/R 1200.SDR DHL9871734CAngle · crackedAT C CHECK, NR 8 SLAT OUTBD SLAT ATTACH ANGLE CRACKED. REPLACED ANGLE PER SRM 51-10-1, N/R 2088.SDR DL72S972745Skin · holeNR 1 SLAT HAS HOLE IN TAI BAFFLE. REPAIRED PER MM 57-54-0 P. 804A.SDR UPS98225438Rib · crackedINSPECTION TYPE-SI, NR 6 SLAT O/B RIB END 2ND IN FROM O/B END IS CRACKED. REMOVED AND REPLACED IAW SRM 51-30-2, 51-20-01.SDR UPS98225437Fitting · corrodedINSPECTION TYPE-SI, NR 4 K-FLAP CENTER L/E HINGE FITTING IS CORRODED. REMOVED AND REPLACED PER SRM 51-30-2.SDR MZZA98024Skin · crackedKUL - NR 2 SLAT ASSY HAS TWO CRACKS AT THERMAL ANTI-ICE DUCT CUTOUT IN AFT LOWER SKIN ATTACH ANGLE AT SLAT STATION 271. CRACKS STOP DRILLED AND DOUBLER INSTALLED IAW ECRA 5750-02875. (M)SDR MZZA98009Support · crackedKUL - FIXED L/E SUPPORT STRUT SITUATED AT WS 175 (AT OUTBOARD END OF NR 3 L/E FLAP ACTUATOR MOUNTING TORQUE BOX) IS CRACKED AT AFT END, THROUGH HI-LOCK HOLES. LEFT WING FIXED L/E SUPPORT STRUT AT NR 3 KRUEGER FLAP ACTUATOR MOUNTING TORQUE BOX, REPLACED IAW SRSDR DL72S980109Web · crackedNR 6 L/E SLAT INTERNAL WEB CRACKED ON O/B SIDE OF SLAT TRACK MT FITTING. REPAIRED PER MM 57-40-00.SDR DL72S980050Web · crackedWEB CRACKED NR 1 SLAT ACTUATOR ATTACH HOUSING WEBS BOTH CRACKED I/B AND O/B SIDE. FABRICATED AND DRILLED I/B REPAIR PER M/M 57-54-0 FIG 804. FABRICATED AND DRILLED UP O/B REPAIR AS PER M/M 57-40-0 FIG 804. OK TO INSTALL. INSTALLED REPAIRS PER M/M 57-54-0
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