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"

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SDR EISA20000162Skin · crackedRT WING NR 5 SLAT I/B HOOK SEAL CUTOUT L/E SKIN HAS CRACKS BOTH CORNERS. FABRICATED FILLER AND DOUBLER, PASSIVATED, PRIMED AND INSTALLED IAW B727-200 SRM 57-30-4 AND 51-30-2.Sep 9, 2000 · N12305 · Boeing 727231SDR UPS00434113Frame · crackedINSPECTION TYPE: C, LT WING CRACK FOUND ON UPPER AND LOWER CHORD AND WEB ON L/E AT ILES 1110. NEW CHORDS FABRICATED IAW EO206770 AND EO206774 AND REFITTED IAW QUERY NOTE 100/2000.Sep 9, 2000 · N691UP · Boeing 747121SDR DHL200070801CDuct · crackedEVIDENCE OF CRACK AT NR 6 L/E SLAT WELL UPPER STRAP I/B OF TELESCOPING DUCT. REMOVED UPPER STRAP AT NR 6 L/E SLAT I/B OF TELESCOPING DUCT PER SRM 51-30-2. TREATED AND PRIMED AREA PER SRM 51-10-2. REPLACED UPPER STRAP AT NR 6 L/E SLAT I/B OF TELESCOPING DUCTSep 8, 2000 · N708DH · Boeing 72725SDR DHL2000708026Strap · crackedEVIDENCE OF CRACK AT NR 6 L/E SLAT WELL UPPER STRAP I/B OF TELESCOPING DUCT. REPAIRED PER B727 SRM 51-10-2, 51-30-2. MATERIAL USED 12 X 20 INCH.Sep 8, 2000 · N708DH · Boeing 72725SDR TWAA0015003Skin · delaminatedDURING CHECK-C MAINT, THE NUMBER 8 L/E SLAT, I/B END T/E WEDGE REPAIR I/B EDGE HAD DELAMINATED. RE-BONDED EDGES ON SLAT PER SRM 51-70-03, PAGE 27 TO 48.Sep 8, 2000 · N604TW · Boeing 767231SDR CALA0001404Skin · dentedINSPECTION FOUND THE LT NR 5 SLAT LEADING EDGE DENTED. THE SLAT WAS REMOVED, REPAIRED, AND REINSTALLED IAW MM 27-80-01, SRM 57-06, FIGURE 1, AND 51-30-2.Sep 8, 2000 · N35832 · Doug DC982SDR TWAA0014101Skin · delaminatedDURING CHECK-C MAINT, THE LEFT WING L/E SLAT NUMBER 2, THE I/B CORNER OF THE AFT WEDGE HAD DELAMINATION. INSTALLED A 3 INCH BY 3.5 INCH METAL BOND REPAIR PER SRM 51-70-10.Sep 8, 2000 · N604TW · Boeing 767231SDR AWXA0000637Skin · nickedC-CHECK, NR 3 SLAT T/E SKIN OUT OF LIMITS AFTER BLEND OUT OF NICK. COMPLIED WITH ER 15-5742-00236-551, NDT NO CRACKS NOTED.Sep 8, 2000 · N149AW · Boeing 7372U9SDR TWAA0013903Seal · tornTHE NUMBER 8 L/E SLAT DID NOT RETRACT AFTER TAKEOFF. FLIGHT RETURNED TO STL. REPLACED THE NUMBER 8 SLAT SEAL, WHICH IMPEDED THE SLAT OPERATION. CHECK-C 10-25-99 MCI.Sep 7, 2000 · N54349 · Boeing 727231SDR CALA0001401Skin · gougedINSPECTION FOUND LT WING NR 5 SLAT LOWER SKIN GOUGED AT I/B END. A DOUBLER WAS INSTALLED IAW SRM 57-03, FIGURE 4, 51-10-3, AND 51-30-8.Sep 6, 2000 · N13891 · Doug DC982SDR CALA0001368Slat Track · gougedINSPECTION FOUND RT WING NR 5 SLAT TRACK GOUGED. THE SLAT TRACK WAS REMOVED AND REPLACED IAW MM 27-80-01.Sep 2, 2000 · N35832 · Doug DC982SDR AALA20001537Skin · gougedTUL - FOUND 2 DEEP GOUGES IN FIXED L/E AFT OF NR 2 SLAT INBOARD OF NR 7 SLAT TRACK. REPAIRED AFT DAMAGED AREA PER AARD 57-30-00-8. (M)Sep 1, 2000 · N565AA · Doug DC983SDR CALA0001356Fitting · crackedINSPECTION FOUND TWO 1 INCH CRACKS AT FASTENER HOLE OF RT WING NR 5 SLAT END FITTING. THE SEAL AND RETAINER ON END FITTING WERE REMOVED IAW SRM 51-30-3. THE CRACKS WERE WELDED IAW DPS 10.225. THE SEAL AND RETAINER WERE REINSTALLED IAW SRM 51-30-2.Sep 1, 2000 · N35832 · Doug DC982SDR CA001006006Bolt · corroded(CAN) WHILE REPLACING BOTH NR 1 FLAP CARRIAGE LINK ASSEMBLIES BADLY PITTED AND CORRODED ATTACHMENT BOLTS WERE DISCOVERED. THEIR CONDITION RENDERED THEM UNSERVICEABLE AND WERE REPLACED WITH NEW BOLTS.Aug 30, 2000 · Bag BAE146200ASDR DL72W001762Rib · crackedAT MV2, RIB CRACKED NR 7 SLAT O/B RIB AT ACTUATOR ATTACH POINT. FABBED DBLR PER 727 MM 57-54-0 FIG 804, INSTALLED DBLR PER 727 MM 57-54-0 FIG 804, INSTALLED COVER PNL ON R/C 636.Aug 29, 2000 · N292WA · Boeing 727247SDR DL72W001761Rib · crackedAT MV2 FOUND RW RIB CRACKED NR 7 SLAT I/B RIB AT ACTUATOR ATTACH POINT. FABBD DBLR PER MM 727-57-54-0 FIG 804. INSTALLED DBLR PER MM 57-54-0 FIG 804.Aug 29, 2000 · N292WA · Boeing 727247SDR DL72W001754Rib · crackedAT MV2 FOUND RW RIB CRACKED NR 6 L/E SLAT, I/B RIB AT ACTUATOR ATTACH POINT. REMOVED PREV REPAIR AND FABBD REPLACEMENT DBLR PER MM 51-540 FIG 804. REPAIRED PER CMM 57-54-0 FIG 804, INSTALLED AND REMOVED ON R/C 634.Aug 29, 2000 · N292WA · Boeing 727247SDR DL72W001733Rib · crackedRIB-CRACKED NR 7 SLAT I/B RIB AT ACTUATOR ATTACH POINT W/W NRC 303. FABRICATED DOUBLER PER MM 727-57-54-0 FIG 804. OK TO INSTALL DOUBLER. INSTALLED DOUBLER PER 727 MM 57-54-0 FIG 804. REMOVED AND INSTALLED ON RC 636.Aug 29, 2000 · N292WA · Boeing 727247SDR DL72W001732Rib · crackedRIB CRACKED NR 7 SLAT O/B RIB AT ACTUATOR ATTACH POINT W/W NRC 342. FABRICATED DOUBLER PER 727 MM 57-54-0 FIG 804 OK TO INSTALL DOUBLER. INSTALLED DOUBLER PER 727 MM 57-54-0 FIG 804. OK TO INSTALL PANEL. INSTALLED COVE PANEL. REMOVED AND INSTALLED ON RC 6Aug 29, 2000 · N292WA · Boeing 727247SDR UPS00833724Vane · corrodedINSPECTION TYPE:C123, LEFT WING LEADING EDGE O/B SLOT VANE IS CORRODED BEYOND LIMITS AT XOLDI 6.225. REPAIRED VANE SKIN IAW SRM 57-2-1 FIG 2H.Aug 29, 2000 · N729UP · Doug DC871FSDR SWAA001615Skin · crackedDURING SCHEDULED 1/4D CHECK, FOUND NR 2 L/E SLAT LOWER SKIN CRACKED I/B OF PREVIOUS REPAIR. REPAIRED SKIN PER BAC DRAWING AND SRM.Aug 27, 2000 · N332SW · Boeing 7373H4SDR L1GA200000286Skin · chafedA 1 BY 1 INCH CHAFED AREA. REPAIRED WITH REPAIR DOUBLER ON RT WING FLAP LEADING EDGE.Aug 25, 2000 · N12507 · Doug DC932SDR ERYA682DPanel · dentedBIRD STRIKE TO RIGHT WING TKS PANEL. MANUFACTURES ENGINEERING TO APPROVE REPAIR. REPLACED TKS PANEL.Aug 25, 2000 · N731DL · Hawker BAE125700BSDR TWAA0013318Skin · delaminatedDURING CHECK-C MAINT, ON RT WING L/E SLAT NUMBER 11, O/B END LOWER SURFACE OF THE WEDGE HAD DELAMINATION. INSTALLED REPLACEMENT HONEYCOMB CORE AND 3 INCH BY 9 INCH EXTERNAL DOUBLER PER SRM 51-70-10.Aug 25, 2000 · N610TW · Boeing 767231SDR CALA0001314Skin · dentedINSPECTION FOUND THREE DENTS IN NR 1 SLAT T/E BETWEEN XOS 166 AND XOS 147. THE DENTED AREA WAS REMOVED AND A REPAIR WAS INSTALLED IAW ECRA 5750-03426.Aug 25, 2000 · N35832 · Doug DC982SDR TWAA0013406Skin · delaminatedDURING CHECK-C, MAINT ON LT WING, FOUND NUMBER 5 L/E SLAT TRAILING EDGE WEDGE I/B AFT CORNER, TOP SURFACE DELAMINATED. INSTALLED 6 INCH BY 8 INCH HOT BOND EXTERIOR DOUBLER PER SRM 51-70-10.Aug 24, 2000 · N610TW · Boeing 767231SDR TWAA0013320Skin · delaminatedDURING CHECK-C MAINT, ON RT WING THE L/E SLAT NUMBER 11, I/B END LOWER SURFACE T/E WEDGE HAD DELAMINATION. INSTALLED HOT BOND REPAIR PER SRM 51-70-10. REPLACED SKIN, CORE AND APPLIED DOUBLER OF 12 INCH BY 12 INCH, 0.020 THICK AND SEALED EDGES.Aug 24, 2000 · N610TW · Boeing 767231SDR TWAA0013319Skin · delaminatedDURING CHECK-C MAINT ON RT WING, THE L/E SLAT NUMBER 12 I/B END LOWER SURFACE OF THE T/E WEDGE HAD DELAMINATION. INSTALLED REPLACEMENT HONEYCOMB CORE AND 12 INCH BY 10 INCH EXTERNAL DOUBLER PER SRM 51-70-10.Aug 24, 2000 · N610TW · Boeing 767231SDR 00FDEA00594Rib · crackedDURING ROUTINE INSP, NR 4 SLAT RIB FOUND CRACKED JUST O/B OF THE I/B TRACK. CUT OUT DAMAGED AREA, FAB DOUBLER AND FILLER, AND INSTALLED REPAIR PER IAW SRM 57-50-3.Aug 24, 2000 · N499FE · Boeing 727232SDR P2EA00238Structure · bird strikePIT - FLT 408 - ON POST FLIGHT WALKAROUND, NOTED BIRD STRIKE ON NR 2 ENIGNE INLET AND ON NR 3 SLAT INBOARD SIDE. PERFORMED BIRD STRIKE INSPECTION PER MM 05-51-201. NO DAMAGE OR OTHER DEFECTS NOTED. ENGINE RUN PERFORMED AND TAKEOFF POWER ACHIEVED. OK TO CONAug 22, 2000 · N5WM · Boeing 737297SDR 00FDEA00576Skin · crackedDURING ROUTINE INSP, NR 4 SLAT FOUND TO HAVE 2 INCH CRACK ON INTERIOR RADIUS 5 INCHES O/B OF THE ACTUATOR. REMOVED AND REPLACED PER IAW MM 27-81-011-04.Aug 22, 2000 · N489FE · Boeing 727227SDR 00FDEA00575Skin · crackedDURING ROUTINE INSP, NR 4 SLAT FOUND CRACKED AT O/B ACTUATOR ATTACH ANGLE. REMOVED AND REPLACED PER IAW MM 27-81-11-04.Aug 22, 2000 · N489FE · Boeing 727227SDR 00FDEA00574Skin · crackedDURING ROUTINE INSP, NR 5 SLAT FOUND CRACKED BEYOND PREVIOUS STOP DRILL IN O/B ANGLE AT THE ACTUATOR ROD END. STOP DRILLED CRACK, FAB, INSTALLED PER IAW SRM 57-50-3.Aug 22, 2000 · N489FE · Boeing 727227SDR 00FDEA00572Skin · crackedDURING ROUTINE INSP, LEFT I/B FOREFLAP FOUND CRACKED ON I/B END. REMOVED AND REPLACED FOREFLAP PER IAW SRM 51-40-6.Aug 22, 2000 · N489FE · Boeing 727227SDR TWAA0013003Skin · delaminatedDURING CHECK-C MAINT ON THE RT WING LEADING EDGE THE NUMBER 10 SLAT HAD DELAMINATION ON TOP SIDE OF THE TRAILING EDGE WEDGE, SEVENTEEN INCHES FROM THE O/B END OF THE SLAT. INSTALLED METAL TO METAL HOT BOND 12 INCHES BY 27 INCHES, ON OUTER SKIN AND 6 INCHES BYAug 21, 2000 · N651TW · Boeing 767205SDR DLM88001596Cover · looseAIR TURNBACK, ON SLAT RETRACT HEARD CONTINUOUS LOW FREQUENCY NOISE. SLATS EXTENDED WITH NO NOISE OR ABNORMAL FLIGHT CONTROL RESPONSES. RAN FLAPS AND FOUND LT INBOARD LEADING EDGE SLAT TRACK COVER LOOSE. TIGHTENED SAME.Aug 19, 2000 · N914DL · Doug MD88SDR RRXA003819Skin · puncturedDURING A MAINTENANCE VISIT FOUND PUNCTURE DAMAGE TO O/B END OF #2 GROUND SPOILER ON L/H WING AT STA. XRS162.263, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTAAug 18, 2000 · N811AL · Doug DC871SDR AWXA0000556Skin · gougedC-CHECK, LEFT O/B FORE FLAP LEADING EDGE GOUGED AND CORRODED. CUT OUT DAMAGE, FABRICATED DOUBLER AND FILLER, INSTALLED REPAIR PARTS IAW 737 SRM 57-50-4.Aug 18, 2000 · N184AW · Boeing 737277SDR AWXA0000545Skin · tornC-CHECK, RT INBOARD FORE FLAP L/E SKIN DAMAGE. CUT OUT DAMAGE, FABED, AND INSTALLED REPAIR DOUBLER IAW 737 SRM 57-50-1 FIG 1.Aug 17, 2000 · N184AW · Boeing 737277SDR UPS00233660Rib · crackedINSPECTION TYPE:C, NR 4 L/E SLAT 2 RIBS CRACKED OUTBOARD OF OUTBOARD TRACK. RIBS REPAIRED IAW SRM 57-50-3 FIG 9 & SRM 51-30-2.Aug 15, 2000 · N925UP · Boeing 72731CSDR DL757001592Skin · damagedTHE TRAILING EDGE WEDGE OF THE NR 7 SLAT WAS MODIFIED PER EO 6-59305-AD. ADDITIONAL DAMAGE TO THE SLAT WAS FOUND RESULTING IN THE REMOVAL OF SEVERAL FASTENERS THAT ATTACH THE T/E WEDGE TO THE SLAT INNER SURFACE. SEVERAL HOLES WERE OVERSIZED. REPAIRED PER ERAug 15, 2000 · N601DL · Boeing 757232SDR DL72W001705Rib · crackedA .5 INCH CRACK ON NR 5 SLAT LT NOSE RIB UPPER LEG AT FWD SIDE OF AC ROD END. REPAIRED PER MM 57-54-0.Aug 14, 2000 · N297WA · Boeing 727247SDR EISA20000122Skin · delaminatedDURING ROUTINE C-CHECK INSPECTION, I/B FORE FLAP DELAMINATED ON I/B LOWER SIDE. REMOVED DELAMINATED COVER, CLEANED, PREPPED AND POTTED CORE. BONDED FIBERGLASS OVERLAY, ALODINED AND PRIMED SURROUNDING AREA. WORK DONE IAW B727 SRM 51-40-6 AND 51-10-2.Aug 10, 2000 · N6815 · Boeing 727223SDR DL73K001515Guide · damagedNR 2 SLAT INBOARD GUIDE BROKE ON TAKEOFF. PUNCTURED SLAT AND CAUSED SHEET METAL DAMAGE ON A/C AND SLAT ITSELF. REPLACED SLAT AND REPAIRED DAMAGE.Aug 9, 2000 · N242WA · Boeing 737247SDR AWXA0000514Skin · chafedC-CHECK, LT WING O/B FOREFLAP I/B LEADING EDGE CHAFED. REMOVED DOUBLER IAW 737 SRM 57-53-01, FAB''D DOUBLER IAW B737 SRM 57-53-01 FIG 202, INSTALLED REPAIR IAW B737 SRM 57-40--2.Aug 9, 2000 · N150AW · Boeing 7373G7SDR AWXA0000512Skin · puncturedC-CHECK, LT MID FLAP AT WBL 73-96 HAS SEVERAL PUNCTURES IN SKIN, THIRD SCREW FROM I/B EDGE, TOP. REMOVED DAMAGE AND SPLICED DOUBLERS IAW 737 SRM 57-53-01 FIG 203.Aug 9, 2000 · N150AW · Boeing 7373G7SDR MWEA00642Doubler · corrodedMKE - RIGHT NR 0 SLAT INBOARD SECTION HAS LIGHT TO MODERATE CORROSION AROUND ALL SLAT TO SEAL ATTACH FASTENERS. FABRICATED AND INSTALLED REPAIR DOUBLER. (M)Aug 4, 2000 · N805ME · Doug DC981SDR P2EA00245Skin · delaminatedDURING C-CHECK, RIGHT OUTBOARD FORE FLAP UPPER SKIN IS DELAMINATED (16 INCHES) AND DENTED. REPAIRED FORE FLAP IAW SRM 51-40-6 PAGE 8 PARA 11 AND SRM 51-40-6 PAGE 45. (M)Aug 4, 2000 · N122NJ · Boeing 737230SDR 00FDEA00531Skin · gougedRIGHT WING I/B FOREFLAP O/B END LEADING EDGE GOUGED. *S/D* REMOVED AND REPLACED PER IAW FEDEX SRM 57-50-4, 51-20-151.Aug 4, 2000 · N263FE · Boeing 727233SDR ABXA000378Fitting · crackedNR 5 SLAT OUTBOARD ATTACH FITTING WAS CRACKED. REPLACED NR 5 SLAT IAW DC9 MM 27-80-1.Aug 3, 2000 · N907AX · Doug DC931
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