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.

SDR CALA0001196Rib · crackedINSPECTION FOUND A CRACK IN RT WING LEADING EDGE SLAT MID RIB AT WS XRS 267-295. THE RIB WAS REPAIRED IAW EA 9-5720-2-A0742 AND ECRA 5720-01810.Aug 2, 2000 · N33817 · Doug DC982SDR USAA001113Skin · crackedCLT - FOUND SLAT SKIN WITH 7 CRACKS, .5 INCH EACH, NR 5 SLAT LOWER SKIN SURFACE INBOARD OF HEAT TUBE. INSTALLED DOUBLER PER DWG 65C30133. (M)Aug 1, 2000 · N353US · Boeing 737301SDR SWAA001445Wedge · delaminatedDURING SCHEDULED D-CHECK, FOUND NR 2 AND NR 3 LEADING EDGE SLAT T/E WEDGES DELAMINATED. REPAIRED WEDGES PER SRM.Aug 1, 2000 · N508SW · Boeing 7375H4SDR SWAA001433Skin · crackedDURING SCHEDULED C2 CHECK, FOUND NR 6 L/E SLAT SKIN CRACKED AT MID AUX TRACK CUT OUT. REPAIRED SLAT PER SWA RA.Jul 31, 2000 · N341SW · Boeing 7373H4SDR ABXA000354Rib · crackedLEFT WING LEADING EDGE RIB CRACKED AT AFT END BETWEEN STATION X0S 481 AND X0S 530. REPAIRED IAW DC9 SRM.Jul 28, 2000 · N965AX · Doug DC941SDR UPS00233588Fitting · crackedINSPECTION TYPE:SI, NR 1 K-FLAP O/B ATTACH LUG FITTING ON K-FLAP UPPER O/B SIDE IS CRACKED. REMOVED AND INSTALLED NEW K-FLAP ASSY PER MM 27-81-01.Jul 27, 2000 · N933UP · Boeing 72725CSDR ABXA000377Skin · crackedLEFT WING NR 4 SLAT END FITTING WAS CRACKED. REPLACED NR 4 SLAT IAW DC9 MM 27-80-01.Jul 27, 2000 · N907AX · Doug DC931SDR EISA20000093Web · puncturedDURING ROUTINE C-CHECK INSP, FOUND HOLE IN LEADING EDGE INTERNAL WEB AT NR 6 SLAT. FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR WEB IAW SRM 51-40-2, 57-30-4, 51-10-2, 51-30-2, AND M/M 27-81-11, 20-50-1.Jul 24, 2000 · N311NE · Boeing 727223SDR EISA20000092Skin · gougedDURING ROUTINE C-CHECK INSP, RIGHT WING OUTBOARD FORE FLAP LEADING EDGE HAS GOUGE AT WS 577. FABRICATED DOUBLER, ALODINED, PRIMED, AND INSTALLED IAW SRM 57-50-4, 51-10-2, 51-30-2.Jul 24, 2000 · N311NE · Boeing 727223SDR TWAA0011801Rib · crackedTHE RT WING NUMBER 4 SLAT O/B NUMBER 12 SLAT RIB WAS CRACKED. REPLACED THE SLAT PER M99-27-02. CHECKK-C 8-21-99 STL.Jul 24, 2000 · N925TW · Doug DC982SDR 20000912SH016Bracket · crackedAFTER LANDING AND SHUT-DOWN AT OFFSHORE PLATFORM MC268. MOUNTING BRACKETS FOR THE LEFT CENTER SLAT WERE CRACKED AND BROKEN ALLOWING SLAT TO DEPART THE AIRCRAFT. LEFT VERTICAL FINLET WAS DAMAGED BY THE MISSING SLAT. (X)Jul 22, 2000 · N647AL · Bell 407SDR 20000912SH015Bracket · crackedPILOT NOTICED THE LEFT CENTER SLAT MISSING AFTER LANDING AND SHUT-DOWN AT OFFSHORE PLATFORM MC268. MOUNTING BRACKETS FOR THE LEFT CENTER SLAT WERE CRACKED AND BROKEN ALLOWING SLAT TO DEPART THE AIRCRAFT. LEFT VERTICAL FINLET WAS DAMAGED BY THE MISSING SLAT. Jul 22, 2000 · N647AL · Bell 407SDR UPS00833627Angle · crackedINSPECTION TYPE:C123, LEFT WING L/E UPPER RIB ANGLE IS CRACKED AT XS 467.323. REMOVED, FABRICATED, AND REPLACED RIB ANGLE/DOUBLER IAW DWG 5770170, AND SRM SRM 51-1-20D.Jul 22, 2000 · N806UP · Doug DC873FSDR USAA001060Skin · crackedPIT - FOUND SLAT OUTER SKIN CRACKED 1.9 INCH, NR 6 SLAT LOWER T/E SKIN, .0008 INCH FORWARD OF T/E. HFEC, REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER PER TR 57-50-01 AND BOEING DRAWING 65C30133. (M)Jul 21, 2000 · N517AU · Boeing 7373B7SDR SWAA001325Skin · delaminatedDURING SCHEDULED SERVICE CHECK, FOUND LT WING NR 1 L/E SLAT I/B TRAILING EDGE DELAMINATED. REMOVED AND REPLACED L/E SLAT PER MM.Jul 19, 2000 · Boeing 7372H4SDR USAA001059Skin · crackedPIT - FOUND SLAT OUTER SKIN CRACKED .6 INCH, NR 6 SLAT LOWER T/E SKIN 1.125 INCH FORWARD OF TRAILING EDGE. REMOVED CRACKED AREA, HFEC, INSTALLED DOUBLER AND FILLER PER TYP 57-50-01. (M)Jul 17, 2000 · N517AU · Boeing 7373B7SDR 00FDEA00474Rib · crackedDURING ROUTINE INSPECTION, NR 4 LEAD EDGE SLAT FOUND CRACKED AT I/B ACTUATOR ATTACH RIB. STOP DRILL, FAB AND INSTALLED PER IAW SRM 51-40-3 & SRM 51-30-2.Jul 17, 2000 · N189FE · Boeing 72722SDR 00FDEA00470Structure · corrodedDURING ROUTINE INSPECTION, NR 6 LEAD EDGE FLAP CORRODED BEYOND ALLOWED LIMITS ON THE OUTER SURFACE. REMOVED AND REPLACED PER IAW MM 27-81-1. OPS CK GOOD IAW MM 27-81-1.Jul 17, 2000 · N189FE · Boeing 72722SDR 00FDEA00465Rib · crackedDURING ROUTINE INSPECTION, THE NR 5 LEAD EDGE SLAT FOUND CRACKED AT O/B ACTUATOR ATTACH RIB. STOP DRILLED CRACK, FAB REPAIR, AND INSTALLED IAW SRM 51-40-3 & SRM 51-30-2.Jul 17, 2000 · N189FE · Boeing 72722SDR CALA0001081Panel · corrodedINSPECTION FOUND RT WING L/E SLAT ACCESS PANEL NR 1278 COUNTER SUNK HOLES CORRODED WITH INNER SKIN LINER CRACKED AND EDGE SEAL CHAFED. THE SEALANT WAS REPLACED IAW SRM 51-20-0. A DOUBLER WAS INSTALLED IAW SRM 57-03-1, FIGURE 3, 51-10-2, 51-10-4, 51-60-00, FIJul 16, 2000 · N72825 · Doug DC982SDR DHL200070905CCover · brokenRT WING NR 7 L/E SLAT ACTUATOR COVER BROKEN AND MISSING BOLT. REPLACED ANGLES SUPPORTS FROM ACTUATOR COVER PANEL PER SRM 51-40-4 FOR FWD ANGLE AND 51-40-3 FOR AFT ANGLE. INSTALLED WITH NEW FASTENERS PER SRM 51-30-2. TREATED AND PRIMED PER SRM 51-30-2.Jul 15, 2000 · N709DH · Boeing 72782CSDR P2EA00227Mount · wornYYC - DURING C-CHECK, WHILE COMPLYING WITH VANGUARD EO NR 963727A065 FRUEGER FLAP FITTING INSPECTION FOUND THREE ACTUATOR MOUNT LUGS WORN DUE TO MISSING RUB STRIPS. NR 1 LEFT FSS 180.36, NR 3 RIGHT FSS 129.80 AND NR 4 RIGHT FSS 180.36. WEAR DEPTH MEASURED NRJul 14, 2000 · N123NJ · Boeing 737230SDR GAIA00415Skin · crackedDURING A C-CHECK INSPECTION, RIGHT SLAT, WS 100 HAS A SKIN CRACK AT NR 5 L/E SLAT OUTBOARD TRACK CUT OUT. REPAIRED TRACK CUT OUT PER SRM 57-30-4. (M)Jul 14, 2000 · N858AA · Boeing 727223SDR GAIA00422Skin · gougedDURING A C-CHECK INSPECTION, FOUND GOUGE AT THE UNDER SIDE WING SKIN JUST BELOW NR 5 SLAT, RIGHT WING. REPAIRED GOUGE PER B727 SRM 57-50-3. (M)Jul 14, 2000 · N858AA · Boeing 727223SDR CA000804017Track · broken(CAN) DURING THE WALK AROUND AND INSPECTION FOR AN A CHECK THE MECHANIC NOTICED EXCESSIVE MOVEMENT IN THE NR 6 SLAT. FURTHER INVESTIGATION REVEALED THAT THE CENTER AUX RACK HAD BROKEN AT THE ATTACH POINT TO THE SLAT. THE SLAT ASSEMBLE WAS REPLACED WITH A SERVIJul 12, 2000 · Boeing 737297SDR RIVA0000015Skin · wornDURING C CHECK INSPECTION, IT WAS NOTED THAT THE RIGHT WING OUTBOARD FOREFLAP HAS A WEAR MARK IN SKIN AT LEADING EDGE, INBOARD OF INBOARD SEQUENCE CARRIAGE ATTACH BEARING. INSTALLED PATCH ON RIGHT WING OUTBOARD FOREFLAP LEADING EDGE (INBOARD OF INBOARD SEQUENJul 12, 2000 · N367PA · Boeing 727221SDR RIVA0000014Structure · crackedDURING C CHECK INSPECTION, IT WAS NOTED THAT THE NR 2 SLAT HAS TWO CRACKS AT EDGE OF LIGHTENING HOLES. REMOVED FASTENERS IN THE NR 2 SLAT COVE PANEL IAW B727 SRM 51-30-2. BLENDED OUT ONE CRACK IAW SRM 57-50-1, REMOVED DAMAGED AREA OF OTHER CRACK IAW SRM 51-4Jul 12, 2000 · N367PA · Boeing 727221SDR CALA0001056Skin · crackedINSPECTION FOUND A .75 INCH CRACK AND LOOSE RIVETS IN RT WING SLAT NR 3 AT AFT SIDE. THE CRACK WAS STOP DRILLED IAW SRM 57-01, FIGURE 3. A DOUBLER REPAIR WAS INSTALLED IAW SRM 57-01, FIGURE 3 AND 51-10-04.Jul 11, 2000 · N33817 · Doug DC982SDR CALA0001041Angle · crackedINSPECTION FOUND A 12 INCH CRACK IN RT WING FIXED L/E RIB SUPPORT ANGLE AT PANEL O/B OF TRACK NR 8. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-05, 51-10-02, 51-10-04, AND 51-10-03.Jul 11, 2000 · N33817 · Doug DC982SDR DL72S001538Attach Angle · crackedFOUND DURING MV4 VISIT, .75 INCH CRACK AT I/B UPPER CORNER NR 5 L/E FLAP ACT ATTACH ANGLE. REMOVED L/E SUPPORT ROD AND INSTALLED DOUBLER PER MM 57-20-21 FIG 807. INSTALLED L/E SUPPORT ROD.Jul 10, 2000 · N518DA · Boeing 727232SDR DHL200070906CRib · crackedLEFT WING NR 1 L/E STAT 4TH INTERNAL RIB FROM O/B END CRACKED AT LOWER AFT SIDE. REMOVED 4TH RIB FROM O/B END OF NR 1 L/E SLAT TO BE REPAIRED PER SRM 51-30-2. INSTALLED REPAIR PER SRM 51-30-2. INSTALLED RIB AND DOUBLER PER SRM 51-30-2.Jul 10, 2000 · N709DH · Boeing 72782CSDR DL72S001364Rib · crackedA 2 INCH CRACK IN NR 5 SLAT L/E RIB LWR AFT CORNER I/B OF ACT ROD END. REPAIRED PER 727 M/M 57-54-0 PG 805.Jul 10, 2000 · N518DA · Boeing 727232SDR TWAA0010903Skin · delaminatedDURING CHECK-C MAINT ON THE LT WING FOUND DELAMINATION ON TOP O/B SIDE OF NUMBER 2 SLAT. INSTALLED A 3 INCH DIAMETER METAL HOT BOND REPAIR PER SRM 51-70-10.Jul 10, 2000 · N606TW · Boeing 767231SDR TWAA0010902Structure · damagedDURING CHECK-C MAINT ON LT WING FOUND A HOLE IN THE NUMBER 2 SLAT ON BOTTOM O/B SIDE. INSTALLED A 2 INCH DIAMETER METAL HOT BOND REPAIR PER SRM 51-70-10.Jul 10, 2000 · N606TW · Boeing 767231SDR AWXA0000454Skin · gougedLT OUTBD MID FLAP GOUGED ON LEADING EDGE. FABRICATED REPAIR DOUBLER, TREATED AND PRIMED AND INSTALLED IAW 737 SRM 51-40-02, SRM 51-20-2, AND SRM 52-55-01.Jul 10, 2000 · N336AW · Boeing 737375SDR DHL200070952DFitting · crackedLEFT WING NR 1 L/E FLAP CENTER HINGE FITTING ON L/E CRACKED AROUND SUPPORT ROD. REMOVED CENTER HINGE FITTING PER SRM 51-30-2. INSTALLED NEW HINGE FITTING PER SRM 57-50-2.Jul 8, 2000 · N709DH · Boeing 72782CSDR TWAA0010802Panel · delaminatedDURING CHECK-C MAINT, FOUND ON LT WING, DELAMINATION ON BULL NOSE PANEL UNDER THE I/B SIDE OF NUMBER 5 SLAT. CLEANED UP DAMAGE, FILLED AND INSTALLED A 4 INCH BY 6 INCH HOT BOND REPAIR PER SRM 51-70-07, AND APPLIED PROTECTIVE COATING AND PAINTED.Jul 8, 2000 · N606TW · Boeing 767231SDR 2000709001CSkin · crackedNR 2 L/E FLAP INNER ANTI-ICE SKIN IS CRACKED AT ATTACH RIVET LOCATED AT THE THIRD BAY FROM THE O/B END. REMOVED INNER ANTI-ICE SKIN AT NR 2 L/E FLAP AS PER SRM 51-30-2. REPAIRED ANTI-ICE SKIN AT NR 2 L/E FLAP AS PER SRM 57-30-1. TREATED WITH ALODINE AND PRIJul 6, 2000 · N709DH · Boeing 72782CSDR 00FDEA00425Rib · crackedDURING ROUTINE INSPECTION, NR 6 LEADING EDGE SLAT WAS FOUND CRACKED AT INBD ACTUATOR ATTACH RIB. R&R PER IAW SRM 57-50-3.Jul 3, 2000 · N262FE · Boeing 727233SDR 00FDEA00424Rib · crackedDURING ROUTINE INSPECTION, NR 4 LEADING EDGE SLAT WAS FOUND CRACKED AT OTBD ACTUATOR ATTACH RIB. R&R IAW SRM 57-50-3.Jul 3, 2000 · N262FE · Boeing 727233SDR 00FDEA00423Rib · crackedDURING ROUTINE INSPECTION, NR 6 LEADING EDGE SLAT WAS FOUND CRACKED AT THE OTBD ACTUATOR ATTACH RIB. R&R PER IAW SRM 57-50-3.Jul 3, 2000 · N262FE · Boeing 727233SDR GAIA00378Flange · crackedDURNIG ROUTINE C-CHECK, FOUND THE NR 4 SLAT ACTUATOR INBOARD ATTACHMENT FLANGE WAS CRACKED BETWEEN TWO MOUNTING BOLTS. REMOVED AND REPLACED ACTUATOR FLANGE AND LOCATED HOLES IN NEW FLANGE. INSTALLED AND REPAIRED IAW B727 SRM 51-30-5 AND 51-30-2. OPERATIONALJun 30, 2000 · N751US · Boeing 727214SDR DL72S001236Stiffener · crackedIB SPAR STIFFENER CRACKED NR 7 SLAT OB TRACK. REPAIR PER M/M 57-20-21Jun 29, 2000 · N537DA · Boeing 727232SDR F3LA00129Skin · corrodedDEN - DURING C-7 CHECK INSPECTION, REPORTED CORROSION ON LEFT WING OUTBOARD FORE FLAP, INBOARD MOUNT SUPPORT. MAINTENANCE REPLACED FORE FLAP. (M)Jun 24, 2000 · N270FL · Boeing 7372L9SDR CALA0000962Bracket · crackedINSPECTION FOUND A 1 INCH CRACK IN RT WING NR 1 SLAT TRACK LOWER FAIRING I/B BRACKET. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-30-01, 51-10-04, 51-10-3.Jun 24, 2000 · N819NY · Doug DC982SDR USAA000961Flap Track · crackedPIT - FOUND OUTBOARD TRACK CRACKED .5 INCH, NR 2 OUTBOARD TRACK CUTOUT LE AT STA 750. TYPICAL REPAIR PER 57-20-08 REV A. (M)Jun 22, 2000 · N375US · Boeing 7373B7SDR 20001204AP003Skin · gougedLEFT WING LEADING EDGE 36 INCHES FROM INBOARD NR 4 SLAT HAS A 7 INCH GOUGE OF .22 INCH DEEP. REMOVED DAMAGED AREA AND FABRICATED DOUBLER AND FILLER IAW SRM 57-30-4 PAGE 1. TREATED PRIMED AND INSTALLED IAW SRM 57-30-4. (M)Jun 21, 2000 · N804MA · Boeing 727225SDR 00FDEA00394Rib · crackedDURING INSPECTION, NR 4 L/E SLAT WAS FOUND CRACKED AT INBOARD ACTUATOR ATTACH RIB. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR IAW SRM 51-40-3 & 51-30-2.Jun 19, 2000 · N480FE · Boeing 727227SDR 00FDEA00393Rib · crackedDURING INSPECTION, NR 5 L/E SLAT WAS FOUND CRACKED AT INBOARD ACTUATOR ATTACH RIB. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR IAW SRM 51-40-3 & 51-30-2.Jun 19, 2000 · N480FE · Boeing 727227SDR 00FDEA00392Rib · crackedDURING ROUTINE INSP, NR 5 L/E SLAT WAS FOUND CRACKED AT O/B ACTUATOR ATTACH RIB. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR IAW SRM 51-40-3 & 51-30-2.Jun 19, 2000 · N480FE · Boeing 727227
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