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 DL72L982470Stop · looseWING NR 7 SLAT, DOWNSTOP FITTING, REPAIR FOR LOOSE BOLT. THE NR 7 SLAT DOWNSTOP FITTINGS WERE FOUND WITH LOOSE BOLTS. DURING INSPECTIONS PER S/B 727-57-171. THE STOP FITTINGS FOR THE SLAT WERE MODIFIED PER THE REQUIREMENTS OF THE S/B. THE MODIFICATION OF Nov 27, 1998 · N505DA · Boeing 727232SDR TWAA9818808Skin · delaminatedFOUND 12 INCH BY 12 DELAMINATION ON UPPER SURFACE OF NR 6 L/E DEVICE, AT O/B END. INSTALLED METAL TO METAL HOT BOND REPAIR PER 767 SRM 51-70-10. CHECK-C 10-28-98 LAX.Nov 24, 1998 · N650TW · Boeing 767205SDR CALA9802104Chord · crackedINSPECTION FOUND A 2.25 INCH CRACK IN LT WING NR 3 SLAT AT LOWER CHORD BELOW OUTBOARD STOP PAD. THE CHORD WAS REMOVED AND A NEW CHORD WAS INSTALLED IAW SRM 51-10-2 AND 51-30-2.Nov 24, 1998 · N17407 · Boeing 727243SDR P2EA98309Rib · crackedSJO - NR 5 SLAT OUTBOARD RIB CRACKED AT FSS 480, DEFECT SIZE LENGTH 1.125 INCH. REPLACED LEADING EDGE CAVITY MAIN TRACK OUTBOARD RIB AT FSS 480 PER 51-10-1 PAGE 1 AND SRM 51-30-2. (M)Nov 17, 1998 · N219US · Boeing 737281SDR CALA9802072Angle · crackedINSPECTION FOUND A .375 INCH CRACK IN LT WING NR 2 SLAT LOWER CHORD ANGLE BELOW TELESCOPING ANTI-ICE DUCT AREA. THE CRACK WAS STOP DRILLED AND A REPAIR ANGLE WAS INSTALLED IAW SRM 51-40-4, PAGE 16.Nov 17, 1998 · N27783 · Boeing 727232SDR CALA9802070Skin · crackedINSPECTION FOUND TWO 1 INCH CRACKS AT SCREW HOLE TO RIVET HOLES OF NR 2 SLAT UPPER TRAILING EDGE WHERE I/B HOOK MOUNTS. THE FASTENERS WERE REMOVED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-10-2, PAGE 3 AND 57-50-3, PAGES 27-28.Nov 17, 1998 · N27783 · Boeing 727232SDR CALA9802069Skin · crackedINSPECTION FOUND A 4 INCH CRACK IN SKIN AT AFT FACE OF LT WING NR 1 SLAT, INBOARD OF INBOARD TRACK AREA. THE NR 1 LE SLAT WAS REMOVED AND REPLACED IAW MM 27-81-11.Nov 17, 1998 · N27783 · Boeing 727232SDR DL72W982368Angle · crackedFOUND ON D2 LETTER CK, NR 6 SLAT LOWER COVE SKIN ATTACH ANGLE CRACKED AT THE I/B STOP PAD. REPAIRED PER MM 57-54-0.Nov 16, 1998 · N290WA · Boeing 727247SDR DHL9872059DRib · crackedAT D CHECK, LEFT WING NR 4 L/E SLAT RIB MARKED NR 11 CRACKED. REPLACED RIB PER SRM 57-50-2, N/R 1979.Nov 16, 1998 · N720DH · Boeing 727228SDR ASAA9880235Skin · dentedLCQ - DURING 15K CHECK, DENTS WERE FOUND ON LEFT WING NR 2 L/E SLAT SKIN. REPAIRED IAW ASA EA 5750-01299. (M)Nov 16, 1998 · N932AS · Doug DC982SDR ASAA9880234Skin · gougedLCQ - DURING 15K CHECK, GOUGES WERE FOUND ON RIGHT WING NR 0 L/E SLAT SKIN. REPAIRED IAW ASA EA 5750-01298. (M)Nov 16, 1998 · N932AS · Doug DC982SDR EISA98258Rib · crackedDURING ROUTINE C-CHECK WORK CARD ACCOMPLISHMENT REVEALED NR 3 SLAT HAD CRACKED RIB INBOARD OF INBOARD TRACK. REPLACED RIB ASSEMBLY PER SRM 57-50-3 AND 51-30-2. (M)Nov 14, 1998 · N313NE · Boeing 727223SDR EISA98257Rib · crackedDURING ROUTINE C-CHECK WORK CARD ACCOMPLISHMENT, FOUND NR 7 SLAT OUTBOARD TRACK RIB CRACKED. BLENDED OUT CRACK IAW SRM 51-10-1. FABRICATED AND INSTALLED DOUBLER PER SRM 57-50-2 AND 51-40-3. (M)Nov 14, 1998 · N313NE · Boeing 727223SDR EISA98256Rib · crackedDURING ROUTINE C-CHECK WORKCARD ACCOMPLISHMENT REVEALED NR 3 SLAT INBOARD RIB CRACKED. STOP DRILLED CRACK. FABRICATED AND INSTALLED DOUBLER PER SRM 51-10-1. (M)Nov 14, 1998 · N313NE · Boeing 727223SDR EISA98272Skin · delaminatedROUTINE C-CHECK WORK CARD ACCOMPLISHMENT REVEALS LEFT OUTBOARD FOREFLAP HAS DELAMINATION AT INBOARD LOWER CORNER. REPAIRED DELAMINATION PER SRM 51-40-5, 51-40-8 AND 51-40-9. (M)Nov 13, 1998 · N313NE · Boeing 727223SDR EISA98271Skin · delaminatedROUTINE C-CHECK WORK CARD ACCOMPLISHMENT REVEALS LEFT INBOARD FOREFLAP DELAMINATED AT INBOARD CORNER. REPAIRED DELAMINATION PER SRM 51-40-6, FIGURE 26. (M)Nov 13, 1998 · N313NE · Boeing 727223SDR DL72S982341Stop · looseDURING INSPECTION PER REQUIREMENTS OF AD 94-07-08, LOOSE SLAT STOP ATTACH BOLTS WERE FOUND LOOSE FOR THE NR 6, 7 & 8 SLATS. EACH OF THESE SLAT LOCATIONS WERE MODIFIED PER THE REQUIREMENTS OF BAC S/B 727-57-171. THE MODIFICATION WAS DOCUMENTED PER ER/A 366092Nov 12, 1998 · N519DA · Boeing 727232SDR DL72E982337Angle · crackedNR 2 SLAT LWR COVE SKIN ATTACH ANGLE CRACKED AT I/B STOP PAD. REPAIRED PER M/M 57-54-0 PG 816.Nov 12, 1998 · N831WA · Boeing 727247SDR DL767982344Wedge · delaminatedTHE UPPER SKIN OF THE TRAILING EDGE WEDGE ON THE NR 6 SLAT WAS FOUND WITH A 5 X 4 AREA OF DELAMINATION APPROXIMATELY 62 INCHES FROM THE O/B EDGE OF THE SLAT. THE DAMAGE WAS TRIMMED AWAY AND REPAIRED PER THE B767 SRM 51-70-10 AND DOCUMENTED PER ER/A 366072-14ANov 11, 1998 · N106DA · Boeing 767232SDR TWAA9818405Skin · delaminatedDURING CHECK-C MAINT, FOUND REPAIR AT NR 6 LEADING EDGE SLAT HAD DELAMINATED AT EDGE WHERE SEAL IS MISSING. INSTALLED A METAL TO METAL HOT BOND PER SRM 51-70-10.Nov 10, 1998 · N607TW · Boeing 767231SDR DL72S982323Bracket · crackedNR 6 L/E FLAP ACT ATTACH BRACKET CRACKED AT UPPER AND LWR ENDS. REPAIRED PER M/M 57-20-21 FIG 807.Nov 10, 1998 · N494DA · Boeing 727232SDR CALA9802051Casting · crackedINSPECTION FOUND A 1.62 INCH CRACK IN LT WING NR 3 LEADING EDGE FLAP MAIN CASTING AT O/B HINGE MOUNT AREA. THE NR 3 LEADING EDGE FLAP WAS REMOVED AND REPLACED IAW MM 27-81-1.Nov 10, 1998 · N59792 · Boeing 727232SDR DL72S982275Rib · crackedFOUND ON A1 LETTER CK, 1 INCH CRACK L/E RIB O/B OF ACTUATOR ON NR 4 SLAT. REPAIRED PER MM 57-54-0 AND ERA 366036-14.Nov 5, 1998 · N8882Z · Boeing 727225SDR 98ZZZX4295Skin · corrodedDURING A C-CHECK, CORROSION NOTED ON RT WING NR 4 LE FLAP. PITTING AROUND BOLT HOLE.Nov 5, 1998 · N64319 · Boeing 727231SDR SWAA982748Skin · crackedDURING SCHEDULED D-CHECK, FOUND FIXED L/E AT NR 4 SLAT O/B AUX TRACK, CUTOUT HAS A STOP DRILLED CRACK. REMOVED CRACK AREA, FABRICATED DOUBLER AND FILLER PER SWA TR T1-251-008.Nov 4, 1998 · Boeing 7372H4SDR DL72S982273Rib · crackedFOUND ON C1 LETTER CK, NR 4 SLAT L/E NOSE RIB I/B SIDE OF ACTUATOR CRACKED .5 INCH. REPAIRED PER MM 57-54-0.Nov 4, 1998 · N520DA · Boeing 727232SDR DHL9872029DSkin · damagedAT D CHECK, NR 1 L/E FLAP HAS CORNER BROKEN OFF T/E OUTBD. BURNISHED EDGES, HFEC AND INSTALLED DOUBLER AND FILLER PER SRM 51-10-1 AND AVITAS ENGINEERING, 98MSI.241D-1, N/R 1921.Nov 4, 1998 · N720DH · Boeing 727228SDR DL72S982363Angle · damagedNR 4 SLAT, ANGLE CRACKED IN CORNER. DYE CHECKED PER PS 900-6-3. NO CRACK FOUND. BURNISHED AREA, TREATED AND PAINTED PER PS 900-2 NR 5.Nov 3, 1998 · N406DA · Boeing 727232SDR DHL9872095DRib · crackedAT D CHECK, L/W NR 4 L/E SLAT RIBS 12, 19, 21 CRACKED. REMOVED AND REPLACED L/E SLAT RIBS PER SRM 57-30-2. REPLACED NR 12 SLAT RIB PER SRM 57-50-2, N/R 1891.Nov 3, 1998 · N720DH · Boeing 727228SDR DHL9872074DRib · crackedAT D CHECK, L/W NR 3 L/E SLAT RIBS NR 1, 16, 19 ARE CRACKED. REMOVED AND REPLACED RIBS PER SRM 57-50-2 .Nov 3, 1998 · N720DH · Boeing 727228SDR DHL9872028DSkin · crackedAT D CHECK, LEFT WING NR 4 L/E SLAT I/B AND O/B TRACK CUT OUTS CRACKED. CUT OUT DAMAGED AREA, INSTALLED DOUBLER AND FILLER REPAIR 6 INCH BY 4 PER SRM 57-30-4, N/R 1892.Nov 3, 1998 · N720DH · Boeing 727228SDR DHL9872026DSkin · damagedAT D CHECK, NR 1 LE FLAP HAS CORNER BROKEN OFF. BURNISHED ROUGH EDGES, HFEC, FABRICATED DOUBLER AND FILLER, INSTALLED, PER SRM 51-10-1 AND AVITAS DRAWING, 98MST241D-1, N/R 1865.Nov 3, 1998 · N720DH · Boeing 727228SDR DHL9872025DRib · crackedAT D CHECK, NR 4 L/E SLAT RIB NR 19 CRACKED. REMOVED AND REPLACED RIB PER SRM 57-50-2, N/R 1839.Nov 3, 1998 · N720DH · Boeing 727228SDR CALA9802031Chord · crackedINSPECTION FOUND A .3125 INCH CRACK IN LOWER CHORD OF LT WING NR 2 SLAT AT CUTOUT BELOW TELESCOPING ANTI-ICE TUBE. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW SRM 51-40-4 PAGE 11 AND 51-10-1 PAGE 6B.Nov 3, 1998 · N59792 · Boeing 727232SDR TWAA9818409Skin · delaminatedDURING CHECK-C MAINT, FOUND NR 6 LEADING EDGE SLAT, O/B SIDE REPAIR DELAMINATED. REPLACED CORRODED HONEYCOMB AND INSTALLED 12.5 IN BY 13 IN METAL OVERLAY PER SRM 51-70-10.Nov 1, 1998 · N650TW · Boeing 767205SDR SWAA982706Roller · looseAIR TURNBACK DUE TO NR 5 L/E SLAT INTRANSIT INDICATION OCCURS INTERMITTENTLY OF FWD PANEL AND OVERHEAD LED PANEL WITH FLAPS EXTENDED INFLIGHT. FOUND LOOSE ROLLER ON NR 5 SLAT INBOARD TRACK. REINSTALLED ROLLER PER BOEING MM. (LPG 243950)Nov 1, 1998 · Boeing 7372H4SDR CLCA9801Skin · damagedFLT 56 - BOG-MIA - UPON APPROACH, CREW LOGGED 'FLAPS MAKE LOUD GRINDING NOISE IN FLIGHT WHEN FLAPS MOVING FROM POSITION 0 TO 1.' UPON GROUND INSPECTION AT MAI, FOUND NR 6 INBOARD SLAT TRAILING EDGE WEDGE DAMAGED, PORTIONS OF MATERIAL MISSING. ALSO, FOUND MINNov 1, 1998 · N572CA · Boeing 75723APFSDR 98ZZZX4799Rib · corrodedWHILE ACCOMPLISHING AN ANNUAL INSPECTION, FOUND CORROSION ON THE SMALL AREAS OF THE RIB. AFTER REMOVING LEADING EDGE OF THE FLAP, FOUND SEVERE CORROSION.Nov 1, 1998 · N3602Q · Beech A23ASDR TWAA9818410Skin · delaminatedDURING CHECK-C MAINT, FOUND RT WING NR 10 LEADING EDGE SLAT TOP DELAMINATED O/B OF CENTER, AND I/B OF OLD PATCH, 2 IN WIDE BY 4 IN LONG. REMOVED PREVIOUS REPAIR AND ADDITIONAL DELAMINATED SKIN. REMOVED DAMAGED CORE. MADE 10 IN BY 25 IN CORE AND SKIN METAL TOct 31, 1998 · N650TW · Boeing 767205SDR AU981610Wedge · disbonded(AUS) LEADING EDGE SLAT TRAILING EDGE WEDGES FOUND DISBONDED ON A TOTAL OF EIGHT SLATS: SLAT 3 - P/N 114T4103-25P, 8 DISBONDED AREAS. SLAT 4 - P/N 114T4104-21C, 1 DISBONDED AREA. SLAT 5 - P/N 114T4105-37, 1 DISBONDED AREA. SLAT 6 - P/N 114T3100-1A, 2 DISBOOct 31, 1998 · Boeing 767277SDR TWAA9818411Skin · delaminatedDURING CHECK-C MAINT, FOUND NR 6 LEADING EDGE SLAT I/B REPAIR HAD DELAMINATION. REMOVED DELAMINATED DOUBLER AND REPAIRED DAMAGED CORE AND INSTALLED 10 BY 12 IN HOT BOND REPAIR PER 51-70-10.Oct 30, 1998 · N650TW · Boeing 767205SDR DL72S982214Bracket · crackedFOUND ON C-1 LETTER CK, NR 1 SLAT I/B ACTUATOR ATTACH BRACKET CRACKED. REPAIRED PER MM 57-20-21.Oct 26, 1998 · N496DA · Boeing 727232SDR SWAA982611Angle · crackedDURING SCHEDULED TRAN CHECK, FOUND LT WING ANGLE CRACKED ON FIXED LEADING EDGE O/B END OF K-FLAP AT AIRLOAD RIB. REMOVED AND REPLACED PER BOEING SRM.Oct 21, 1998 · N661SW · Boeing 7373H4SDR AALA981843Mount · corrodedTUL - NR 3 SLAT ACT INBOARD AND OUTBOARD MOUNTS CORRODED. REMOVED AND INSTALLED INBOARD AND OUTBOARD MOUNTS, REPAIRED DAMAGED AREA INSIDE TANK PER ESO 11697, DATED 10-2-98 AND 9-18-98. (M)Oct 21, 1998 · N720AA · Boeing 727227SDR SWAA982539Skin · crackedDURING SCHEDULED 1/4D CHECK, FOUND NR 4 SLAT SKIN CRACKED AT ACTUATOR. REPAIRED CRACK PER TI-A57-015.Oct 13, 1998 · N678SW · Boeing 7373A4SDR DL76G982163Skin · delaminatedWING NR 3 AND NR 5 SLATS, TRAILING EDGE WEDGES, DELAMINATION REPAIR. THE UPPER SKIN OF THE TRAILING EDGE WEDGES ON THE NR 3 AND NR 5, SLATS WERE FOUND WITH A 2 BY 4 AREA OF DELAMINATION ON EACHWEDGE. THE DISBONDED AREAS WERE TRIMMED AWAY AND REPAIRED PER B7Oct 13, 1998 · N1501P · Boeing 7673P6SDR P2EA98249Skin · damagedSJO - NR 5 SLAT DELAMINATED UPPER AND LOWER SKIN. REPAIRED NR 5 SLAT PER COOPESA EO COO-3-57-573-98 DATED OCT 17, 1998. (M)Oct 11, 1998 · N620PC · Boeing 737244SDR SWAA982432Skin · crackedDURING SCHEDULED D CHECK, FOUND CRACKED NR 6 SLAT LWR SKIN AT CENTER AUX TRACK. REPAIRED PER BOEING SRM.Oct 6, 1998 · N339SW · Boeing 7373H4SDR CALA9801909Rib · crackedINSPECTION FOUND A 1.25 INCH CRACK AT AFT LOWER END OF NR 3 SLAT LEADING EDGE RIB AND A 1.25 INCH CRACK WAS FOUND AT FORWARD LOWER END OUTBOARD OF ACTUATOR ROD MOUNT. THE CRACKS WERE STOP DRILLED IAW SRM 51-30-2, A DOUBLER WAS INSTALLED IAW SRM 57-50-3, PAGE Oct 5, 1998 · N579PE · Boeing 727243SDR P2EA98241Skin · wornSJO - RIGHT WING OUTBOARD FOREFLAP LEADING EDGE SECTION WORN. REPAIRED RIGHT WING OUTBOARD FOREFLAP LEADING EDGE SECTION FROM WS 493 TO WS 505 PER SRM 57-50-4 FIG 1. (M)Oct 4, 1998 · N620PC · Boeing 737244
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