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.

SDR DL72W950406Rib · crackedDURING SHOP INSPECTION, FOUND NR 6 RIB FOR NR 3 SLAT CRACKED. REPAIRED PER SRM 57-54-0.Jan 29, 1995 · N2807W · Boeing 727247SDR DL72L951017Angle · wornNR 6 SLAT, ITEM NR 1, INNER CLOSE OUT PANEL LOWER ATTACH ANGLE HAS ELONGATED HOLE 4.5 INCHES FROM I/B END. ITEM NR 2, REPAIR INSUFFICIENT AT LOWER ATTACH ANGLE T-DUCT CUTOUT. REPAIRED BOTH ITEMS PER SRM 57-54-0 FIG 805A.Jan 29, 1995 · N507DA · Boeing 727232SDR DL72L951016Rib · crackedNR 6 SLAT, SECOND RIB FROM I/B END CRACKED AT LOWER END. INSTALLED DOUBLER PER M/M 57-54-0 FIG 814. DAMAGE FOUND DURING SHOP INSPECTION.Jan 29, 1995 · N507DA · Boeing 727232SDR DL733950457Skin · crackedAT HMV, NR 5 SLAT LOWER T/E SKIN WAS FOUND CRACKED AT RIVET HEADS ON BOTH SIDES OF SLAT ACTUATOR. REPAIRED PER SRM 57-43-01 FIG 205.Jan 28, 1995 · N307WA · Boeing 737347SDR DL76S952035Te Wedge · delaminationFOUND T/E DAMAGE DURING INSPECTION, REPLACE T/E WEDGE PER CMM 57-43-45, FOR NR 2 L/E SLAT PANEL.Jan 27, 1995 · N117DL · Boeing 767332SDR DL72S950380Angle · crackedDURING CORROSION INSPECTION, RIGHT WING NR 6 SLAT WAS FOUND WITH A .5 INCH CRACK IN O/B ATTACH ANGLE, JUST I/B OF O/B STOP. REPAIRED PER MM 57-54-0 PG 816.Jan 26, 1995 · N411DA · Boeing 727232SDR DL72S950379Rib · crackedDURING CORROSION INSPECTION, RIGHT WING NR 6 SLAT WAS FOUND WITH A 1 INCH CRACK IN L/E RIB, JUST OUTBOARD OF INBOARD SLAT TRACK. REPAIRED PER MM 57-54-0 PG 815-815A.Jan 26, 1995 · N411DA · Boeing 727232SDR DL72S950378Skin · crackedDURING CORROSION INSPECTION, RT WING NR 6 SLAT WAS FOUND WITH A 2.25 INCH CRACK IN LOWER AFT SKIN. REPAIRED PER MM 57-54-0 PG 801.Jan 26, 1995 · N411DA · Boeing 727232SDR DL72S950377Angle · crackedDURING CORROSION ISNPECTION, FOUND NR 6 SLAT WITH A .5 INCH CRACK IN ATTACH ANGLE BELOW ANTI-ICE DUCT TEE. REPAIRED PER MM 57-54-0 PG 807A.Jan 26, 1995 · N411DA · Boeing 727232SDR YAUA9502Bolts · looseCOMPLY WITH INSPECTION FOR LOOSE OR BROKEN BOLTS IAW SB 727-57-171. INSPECTION FOUND NR 1 L/E SLAT STRUCTURAL STOP WITH 2 EACH BOLTS LOOSE. IN ORDER TO COMPLY FULLY WITH SB 727-57-171, REMOVED ALL SLATS INCLUDING NR 6 AND NR 7 SLATS MODIFIED IAW SB USING KITJan 25, 1995 · N590CA · Boeing 727231SDR DL72W952140Lug · crackedDURING INSP, A CRACK WAS FOUND IN THE NOSE FLAP AT THE INBD LUG. THIS WAS REPAIRED PER SRM 57-50-3 PG 20.Jan 25, 1995 · N2825W · Boeing 727247SDR DL72W952139Skin · crackedDURING INSP, A CRACK WAS FOUND IN THE SKIN AT THE INBD SIDE. THIS WAS REPAIRED PER SRM 57-50-3, FOR L/E KRUGER FLAP PANEL.Jan 25, 1995 · N2825W · Boeing 727247SDR DL72W950484Web · gougedFOUND DURING HMV, GOUGE IN WEB FWD OF ATTACH BOLT NR 7 SLAT O/B. REPAIRED PER M/M 57-54-0 PG 807.Jan 25, 1995 · N293WA · Boeing 727247SDR DL72W950483Fitting · crackedAT HMV, LEFT WING NR 4 SLAT WAS FOUND WITH THE INBOARD AND OUTBOARD SLAT ACTUATOR FITTING SUPPORT RIB DOUBLERS CRACKED AT THE LOWER FORWARD FLANGE RADIUS. REPAIRED BY INSTALLING NEW DOUBLERS PER MM 57-54-0 PG 805.Jan 25, 1995 · N293WA · Boeing 727247SDR DL72W950426Rib · crackedNR 2 SLAT RIB AND NR 3 CRACKED AT RADIUS FORM LWR RIB CAP. FABRICATED REPAIR PER MM 57-54-0 PG 806-807. FOUND DURING HMV.Jan 25, 1995 · N293WA · Boeing 727247SDR 95ZZZX1046Bolts · looseCOMPLY WITH INSPECTION FOR LOOSE OR BROKEN BOLTS IAW SB 727-57-171. INSPECTION FOUND NR 8 L/E SLAT STRUCTURAL STOP WITH 1 EACH BOLTS LOOSE. IN ORDER TO COMPLY FULLY WITH SB 727-57-171, REMOVED ALL SLATS INCLUDING NR 6 AND NR 7 SLATS MODIFIED IAW SB USING KITJan 25, 1995 · N590CA · Boeing 727231SDR 95ZZZX1045Bolts · looseCOMPLY WITH INSPECTION FOR LOOSE OR BROKEN BOLTS IAW SB 727-57-171. INSPECTION FOUND NR 5 L/E SLAT STRUCTURAL STOP WITH 3 EACH BOLTS LOOSE. IN ORDER TO COMPLY FULLY WITH SB 727-57-171, REMOVED ALL SLATS INCLUDING NR 6 AND NR 7 SLATS MODIFIED IAW SB USING KITJan 25, 1995 · N590CA · Boeing 727231SDR 95ZZZX1044Bolts · looseCOMPLY WITH INSPECTION FOR LOOSE OR BROKEN BOLTS IAW SB 727-57-171. INSPECTION FOUND NR 4 L/E SLAT STRUCTURAL STOP WITH 1 EACH BOLTS LOOSE. IN ORDER TO COMPLY FULLY WITH SB 727-57-171, REMOVED ALL SLATS INCLUDING NR 6 AND NR 7 SLATS MODIFIED IAW SB USING KITJan 25, 1995 · N590CA · Boeing 727231SDR 95ZZZX1043Bolts · looseCOMPLY WITH INSPECTION FOR LOOSE OR BROKEN BOLTS IAW SB 727-57-171. INSPECTION FOUND NR 3 L/E SLAT STRUCTURAL STOP WITH 3 EACH BOLTS LOOSE. IN ORDER TO COMPLY FULLY WITH SB 727-57-171, REMOVED ALL SLATS INCLUDING NR 6 AND NR 7 SLATS MODIFIED IAW SB USING KITJan 25, 1995 · N590CA · Boeing 727231SDR 95ZZZX1042Bolts · looseCOMPLY WITH INSPECTION FOR LOOSE OR BROKEN BOLTS IAW SB 727-57-171. INSPECTION FOUND NR 2 L/E SLAT STRUCTURAL STOP WITH 2 EACH BOLTS LOOSE. IN ORDER TO COMPLY FULLY WITH SB 727-57-171, REMOVED ALL SLATS INCLUDING NR 6 AND NR 7 SLATS MODIFIED IAW SB USING KITJan 25, 1995 · N590CA · Boeing 727231SDR DL72S950682Rib · crackedDURING INITIAL INSPECTION OF THE NR 7 LEADING EDGE SLAT, RIB MARKED NR 11 WAS FOUND TO HAVE A CRACK. THE RIB WAS REPAIRED PER MM 57-54-0.Jan 20, 1995 · N421DA · Boeing 727232SDR DL72S950680Slat · crackedDURING THE INITIAL INSPECTION OF THE NR 7 LEADING EDGE SLAT, THERE WAS A CRACK FOUND THE UPPER I/B CORNER OF THE 'T' DUCT OPENING. THE CRACK WAS REPAIRED PER MM 57-54-0 PG 802A.Jan 20, 1995 · N421DA · Boeing 727232SDR DL72S950679Skin · damagedUPON INITIAL INSPECTION OF THE NR 7 LEADING EDGE SLAT, THERE WAS A TEMPORARY REPAIR FOUND ON THE OUTER SKIN 45 INCHES FROM THE OUTBOARD END. THE DAMAGE WAS REPAIRED PER SRM 57-50-3.Jan 20, 1995 · N421DA · Boeing 727232SDR DL72S950261Attach Angle · crackedDURING LETTER CHECK, THE LEFT WING NR 4 LEADING EDGE SLAT LOWER FORWARD SKIN ATTACH ANGLE WAS FOUND WITH A .5 INCH CRACK IN ITS RADIUS BEHIND THE INBOARD SLAT UPSTOP. REPAIRED PER MM 57-54-0 FIG 812.Jan 18, 1995 · N421DA · Boeing 727232SDR DL72W950285Angle · crackedDURING HMV, FOUND AN ANGLE CRACKED AT TAI CUTOUT ON THE NR 7 LEADING EDGE SLAT, REPAIRED PER M/M 57-54-0 PG 807A.Jan 15, 1995 · N291WA · Boeing 727247SDR DL72S951146Rib · crackedDURING SHOP INSPECTION, RIB AT ACTUATOR FITTING WAS FOUND CRACKED ON L/WING NR 3 L/E SLAT. REPAIRED PER SRM 57-54-0.Jan 14, 1995 · N517DA · Boeing 727232SDR DL72L950167Le Rib · crackedDURING HMV, FOUND RIB INSIDE NR 3 L/E SLAT CRACKED. REPAIRED PER SRM 57-50-3 FIG 9.Jan 13, 1995 · N514DA · Boeing 727232SDR DL72S951003Slat · crackedDURING INSPECTION OF NR 5 L/E SLAT, N/R CARD WAS WRITTEN TO COMPLY WITH EO NR 4-55122-3AD. THIS EO WAS COMPLIED WITH AND N/R CARD SIGNED OFF.Jan 12, 1995 · N526DA · Boeing 727232SDR DL757950524Skin · delaminatedNR 9 LE SLAT, TRAILING EDGE WAS FOUND TO BE DELAMINATED WEDGE WAS REPLACED DURING SHOP 38O VISIT PER SRM 57-43-02 AND AD 90-23-06.Jan 11, 1995 · N635DL · Boeing 757232SDR DL72S950533Skin · wornDURING INSPECTION ON A B727 NR 5 L/E SLAT, A HOLE WAS FOUND TO BE ELONGATED UNDER WHERE THE FENCE IS MOUNTED. IN ADDITION, THE OUTER SKIN WAS FOUND TO BE WORN AT THE SAME LOCATION. AN EXTERNAL DOUBLER WAS INSTALLED PER THE M/M 57-54-00 PG 817.Jan 11, 1995 · N526DA · Boeing 727232SDR DL72S950532Rib · crackedON NR 5 L/E SLAT DURING INSPECTION A CRACK WAS FOUND ON A RIB. A REPAIR DOUBLER WAS INSTALLED PER M/M 57-54-00 FIG 809.Jan 11, 1995 · N526DA · Boeing 727232SDR DL72S950194Kruger Flap · crackedDURING SHOP INSPECTION, A CRACK WAS FOUND ON THE NR 3 KRUGER FLAP NEAR THE I/B HINGE. REPAIRED CRACK PER SRM 57-50-3.Jan 11, 1995 · N493DA · Boeing 727232SDR DL72S950370Skin · dentedDURING SHOP INSPECTION, RIGHT WING NR 8 SLAT WAS FOUND WITH THE LEADING EDGE SKIN DENTED AT 51 INCHES TO 57 INCHES FROM THE I/B END OF SLAT. REPAIRED PER SRM 57-50-3 FIG 1.Jan 10, 1995 · N419DA · Boeing 727232SDR DL72S950216Ribs · crackedDURING SHOP INSPECTION, LEFT WING NR 3 LEADING EDGE SLAT WAS FOUND WITH INTERNAL SUPPORT RIBS NR 7 AND NR 9 CRACKED. REPAIRED PER SRM 57-54-0.Jan 10, 1995 · N484DA · Boeing 727232SDR DL72S960038Rib · crackedNR 3 RIB CRACKED AT I/B TRACK ATTACH POINT. REPAIRED PER M/M 57-54-0 PG 807. FOUND DURING NR 3 L/E SLAT AT SHOP INSPECTION.Jan 5, 1995 · N518DA · Boeing 727232SDR DL72S960037Angle · crackedCOVE ANGLE CRACKED AT I/B UP STOP ATTACH POINT. REPAIRED PER M/M 57-54-0, FOR NR 3 L/E SLAT AT SHOP INSPECTION.Jan 5, 1995 · N518DA · Boeing 727232SDR DL72S950857Skin · crackedUPON INSPECTION OF THE NR 3 SLAT, THE SKIN WAS FOUND TO BE CRACKED AT THE ACTUATOR. A REPAIR WAS PERFORMED PER THE SRM 57-50-3, FIGURE 1.Jan 5, 1995 · N8875Z · Boeing 727225SDR DL72L950424Skin · crackedDURING SHOP ISNPECTION, LEFT WING NR 4 SLAT UPPER SKIN WAS WORN AT FENCE. ALSO, A TIME LIMITED REPAIR WAS FOUND ON LOWER SKIN AT FENCE AREA. REPAIRED PER MM 57-54-0 FIG 813 AND SRM 57-50-3 FIG 1.Jan 5, 1995 · N503DA · Boeing 727232SDR DL72L950423Rib · crackedDURING SHOP INSPECTION, FOUND LEFT WING NR 4 SLAT WITH RIB NR 12 AND NR 18 CRACKED. REPAIRED PER MM 57-54-0.Jan 5, 1995 · N503DA · Boeing 727232SDR DL72L950422Rib · crackedDURING SHOP INSPECTION, LEFT WING NR 4 SLAT WAS FOUND WITH RIB NR 11 CRACKED. REPAIRED PER SRM 57-54-0.Jan 5, 1995 · N503DA · Boeing 727232SDR DL72L950421Rib · crackedDURING SHOP INSPECTION, FOUND LEFT WING NR 4 SLAT WITH THE RIB CHORD CRACKED AT THE O/B END, AND WORN AT THE I/B TRACK. REPAIRED PER MM 57-54-0 FIG 812.Jan 5, 1995 · N503DA · Boeing 727232SDR DL72L950420Skin · crackedDURING SHOP INSPECTION, LEFT WING NR 4 SLAT WAS FOUND WITH CRACKED LOWER SKIN AT INBD TRACK FAIRING. REPAIRED PER MM 57-54-0 FIG 15.Jan 5, 1995 · N503DA · Boeing 727232SDR DL733950212Le Slat · crackedAT HMV, FOUND NR 5 LEADING EDGE SLAT CRACKED ON BOTTOM ALONG FASTENERS. REPAIRED PER SRM 57-43-01 FIG 205.Jan 4, 1995 · N308WA · Boeing 737347SDR DL72S950048Slat Rib · crackedDURING LETTER CHECK, FOUND LEFT WING NR 4 LEADING EDGE SLAT WITH A .5 INCH CRACK IN THE NOSE RIB JUST OUTBOARD OF ACTUATOR ROD ATTACH FITTING. REPAIRED PER MM 57-54-0.Jan 4, 1995 · N484DA · Boeing 727232SDR DL72S950046Slat · crackedDURING LETTER CHECK, LEFT WING NR 4 LEADING EDGE SLAT WAS FOUND WITH TWO .5 INCH CRACKS ON THE LOWER SKIN IN THE RADIUS OF THE INBOARD SLAT TRACK FAIRING. REPAIRED PER MM 57-54-0.Jan 4, 1995 · N484DA · Boeing 727232SDR DL72L950264Angle · crackedDURING HMV, NR 5 SLAT CLOSEOUT ATTACH ANGLE CRACKED. REPAIRED PER M/M 57-54-0.Jan 4, 1995 · N514DA · Boeing 727232SDR DL72L950192Rib · crackedDURING HMV, FOUND NR 7 L/E SLAT ACT ATTACH RIBS CRACKED AT LWR FWD RADIUS. FABRICATED PART AND REPAIRED PER M/M 57-54-0.Jan 4, 1995 · N514DA · Boeing 727232SDR DL72S950288Ribs · crackedDURING SHOP INSPECTION, LEFT WING NR 3 SLAT WAS FOUND WITH NR 3, NR 7, NR 9 AND NR 10 RIBS CRACKED. REPAIRED PER SRM 57-50-3 AND SRM 57-54-0 FIG 804.Jan 2, 1995 · N524DA · Boeing 727232
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