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 WVE2003F00020Panel · misriggedLT WING LEADING EDGE PANEL 531AL AFT OUTBOARD SIDE IS CHAFED .3750 INCH LONG, .3750 INCH WIDE, .003 INCH DEEP. MISRIG OF LEADING EDGE SLAT CAUSING CONTACT ON UNDERLYING PANEL. RECOMMENDATION: BLEND CHAFED AREA TO SMOOTH THE SURFACE, PERFORM EDDY CURRENT TO Nov 16, 2003 · N613QX · Cndair CL6002C10SDR SWAA032489Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND #6 L/E SLAT DELAMINATED AT MID SPAN AREA. REMOVED AND REPLACED SLAT ASSY PER MM.Nov 10, 2003 · N306SW · Boeing 7373H4SDR DL757030995Skin · gougedNR 2 SLAT GOUGED. COMPLETED PERMANENT REPAIR PER SRM 51-70-10D REF SRM 57-43-02D. C/W PERMANENT REPAIR ON OPN 1000 CARDS 1135-1143.Nov 9, 2003 · N618DL · Boeing 757232SDR DL757030994Skin · dentedNR 9 SLAT DENTED ON I/B END. COMPLETED PERMANENT REPAIR PER SRM 51-70-10D REF SRM 57-42-02D. C/W REPAIR ON OPN 1000 CARDS 1126-1134.Nov 8, 2003 · N618DL · Boeing 757232SDR DL73S030983Wedge · dentedFOUND ON W-1 LETTER CK, REPAIR LIFTING NUMBER 6 L/E SLAT T/E WEDGE 6 INCHES FROM O/B EDGE. REPAIRED PER SRM 51-40-20 AND OPERATION 1000.Nov 6, 2003 · N312DL · Boeing 737232SDR AWXA200301508Skin · crackedDURING C-15 CHECK 2 EACH CRACKS WERE FOUND ON NR 6 SLAT LOWER SKIN BELOW CENTER AUXILIARY TRACK. MAINTENANCE REMOVED AND REPLACED NR 6 LEADING EDGE SLAT PER BMM 27-81-21.Nov 3, 2003 · N305AW · Boeing 7373G7SDR AWXA200301457Angle · crackedDURING C-13 CHECK A .375 INCH CRACK WAS FOUND IN ZEE ANGLE AT RT WING LEADING EDGE, INSIDE ACCESS PANEL 5848, ON OUTBOARD SIDE AT SLAT STA 2.5. MAINTENANCE REMOVED DAMAGED ZEE ANGLE AT RT WING LEADING EDGE INSIDE ACCESS PANEL 5848; FABRICATED A NEW REPLACEMENOct 28, 2003 · N307AW · Boeing 7373G7SDR GAIA03120STRib · crackedDURING C-CHECK INSPECTION, FOUND NR 5 SLAT RIBS CRACKED INBOARD AND OUTBOARD SIDES OF ACTUATOR ATTACH POINT. REF FASI N/R NR 61216, REPLACED CRACKED RIBS 2024 T-3 .063 INCH PO NR 900103 IAW B727 SRM 57-50-2. (M)Oct 24, 2003 · N1269Y · Boeing 727243SDR 2003UALA00837Wedge · delaminatedT/E WEDGE DELAMINATED, SLAT NR 6. MAJOR REPAIR ACCOMPLISHED. REPLACED WITH NEW T/E WEDGE.Oct 24, 2003 · N527UA · Boeing 757222SDR WVE2003F00019Vane · chafedRT OUTBOARD FLAP VANE IS CHAFED ON THE OUTBOARD LEADING EDGE OF THE VANE CAP APPROXIMATELY 2 INCHES FROM THE END. THE CHAFE IS .025 INCHES X .003 INCHES DEEP. CHAFING AGAINST THE BUTE DOORS WHEN FLAPS EXTEND AND RETRACT. RECOMMENDATION: BLEND CHAFED AREA TOct 21, 2003 · N612QX · Cndair CL6002C10SDR AWXA200301341Slat · delaminatedMCN - MAJOR REPAIR - DURING C-21 CHECK THE NR 1 LEADING EDGE SLAT WAS FOUND DELAMINATED AT THE INBOARD UPPER SURFACE WS 510 TO WS 512 LT. MAINTENANCE CUT OUT DELAMINATED AREA ON NR 1 L/E SLAT; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW B737-2Oct 20, 2003 · N182AW · Boeing 737277SDR DHL2003807543Skin · corrodedRT WING INBD VANE SLOT UPPER SKIN CORRODED AT STA XILD 0.7095. (MAJOR REPAIR) PERFORMED MAJOR REPAIR. REMOVED FASTENERS. REMOVED CORROSION. FOUND OUT OF LIMITS. TRIMMED OUT AND REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION IAW NDT STANDARD PRACTICE MANOct 19, 2003 · N807DH · Doug DC873FSDR SWAA032289Slat · delaminatedDURING SCHEDULED D CHECK, FOUND NR 2 AND NR 3 L/E SLATS DELAMINATED. REPAIRED NR 2 AND NR 3 L/E SLATS PER MM.Oct 19, 2003 · N379SW · Boeing 7373H4SDR 03FDEA01766Link · wornSLATS NR 14 SLAT TRACK INBOARD LINK (RT WING) WEAR REWORK P/N ARB1468-2. COMPLIED WITH EA 8-5750-73213 WINGS - SLATS NR 14 SLAT TRACK INBOARD LINK (RT WING) WEAR REWORK P/N ARB 1468-2.Oct 18, 2003 · N397FE · Doug DC1010SDR ASAA0380682Panel · puncturedOAK - FOUND 15K CHECK, LEFT WING SLAT NR 1 INBOARD LOWER PANEL IN PUNCTURED. REPLACED SLAT PANEL. (M)Oct 15, 2003 · N948AS · Doug DC983SDR 2003UALA00779Skin · delaminatedNR 4 SLAT DELAMINATED AT OB END LOWER SURFACE OF T/E WEDGE. AREA 2.2 INCH CHORDWISE X 3.0 INCH SPANWISE LOCATED 1.5 INCH FROM OB END AND 3.0 INCH FROM T/E. THE ABOVE NOTED DELAM CONDITION WAS DUE TO WEAR FROM NORMAL LOADS EXPERIENCED DURING A FLIGHT OVER A PEROct 15, 2003 · N775UA · Boeing 777222SDR 2003UALA00778Skin · delaminatedNR 2 SLAT DELAMINATED AT OB END LWR SURFACE OF T/E WEDGE. AREA IS 1.6 INCHES CHORDWISE X 1.3 INCHES SPANWISE AT 1.3 INCHES FROM OB END AND 1.6 INCHES FROM T/E. THE ABOVE NOTED DELAM CONDITION WAS DUE TO WEAR FROM NORMAL LOADS EXPERIENCED DURING A FLIGHT OVER Oct 15, 2003 · N775UA · Boeing 777222SDR 2003UALA00777Skin · delaminatedNR 1 SLAT DELAMINATED OB END OF LOWER SURFACE OF T/E WEDGE OF AREA 3.3 INCHES CHORDWISE X 1.6 INCHES SPANWISE. THE ABOVE NOTED DELAM CONDITION WAS DUE TO WEAR FROM NORMAL LOADS EXPERIENCED DURING A FLIGHT OVER A PERIOD OF TIME. THE TRAILING EDGE WEDGE OF THEOct 15, 2003 · N775UA · Boeing 777222SDR CALA0300594Skin · crackedINSPECTION FOUND A .7500 INCH CRACK IN NR 6 SLAT LOWER SKIN. A DOUBLER REPAIR WAS INSTALLED IAW SRM 57-43-01.Oct 14, 2003 · N12313 · Boeing 7373T0SDR ABXA030406Rib · crackedRIGHT WING LEADING EDGE NOSE RIB INBOARD SIDE OF NR 1 SLAT DRIVER HAD 2 CRACKS ON REPAIR MARKED, REA 43261, CRACKED IN FORWARD RADIUS AND AFT BETWEEN HI-LOKS. REPLACED LEADING EDGE RIB IAW DC-9 SRM 51-30-5 AND 51-30-2.Oct 13, 2003 · N979AX · Doug DC941SDR SWAA032248Wedge · delaminatedDURING SCHEDULED C4 CHECK, FOUND NR 2 L/E SLAT T/E WEDGE DELAMINATED AT OUTBD END. REPAIRED WEDGE PER SRM.Oct 13, 2003 · N635SW · Boeing 7373H4SDR CALA0300592Skin · crackedINSPECTION FOUND A 2 INCH CRACK IN LT WING NR 3 SLAT PANEL LOWER SKIN. A DOUBLER WAS INSTALLED IAW SRM 57-43-01.Oct 13, 2003 · N12319 · Boeing 7373T0SDR SWAA032239Skin · crackedDURING SCHEDULED 1/4D CHECK, FOUND NR 6 L/E SLAT SKIN CRACKED OUTBD OF MAIN TRACK. REPAIRED SLAT SKIN PER SRM.Oct 12, 2003 · N625SW · Boeing 7373H4SDR DHL2003807520Skin · corrodedRIGHT WING L/E SLOT UPPER SKIN CORRODED BETWEEN STA XFS 220.000 - XFS 232.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 38 TR 57-85. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17, 18. FOUND OUT OF LIMITS IAWOct 10, 2003 · N807DH · Doug DC873FSDR 0301899868Bearing · lack of lubeDURING APPROACH FOR LANDING AFTER SLATS WERE SELECTED TO EXTEND, THE FLIGHT CREW NOTICED THE AIRCRAFT ROLLING AND ONE SLAT DID NOT EXTEND. THE SLAT DISAGREEMENT LIGHT ILLUMINATED AND COM PROCEDURES WERE FOLLOWED. LANDING AT DTW WAS UNEVENTFUL. MAINTENANCE FOUNOct 8, 2003 · N777NC · Doug DC951SDR 03FDEA01715Fitting · crackedRIGHT WING - SLAT TRACK NR 16 I/B FITTING FOUND CRACKED. RIGHT WING - SLAT TRACK NR 16 I/B FITTING REMOVED AND REPLACED AS PER DRAWING ARB 7565 AND SRM 51-33-01 VOL II.Oct 7, 2003 · N614FE · Doug MD11SDR 03FDEA01714Fitting · crackedLEFT WING - FOUND NR 16 SLAT TRACK INBOARD FITTING WITH CRACK. LEFT WING NR 16 SLAT TRACK INBOARD FITTING CRACK RIB REMOVED AND REPLACED AS PER DWG ARB7565, SRM 51-33-01 VOL II AND SRM 51-35-01 VOL II.Oct 7, 2003 · N614FE · Doug MD11SDR QXEA200301318Skin · chafedRIGHT WING INBOARD FLAP LEADING EDGE MOVEABLE VANE INBOARD LEADING EDGE CHAFED. REPAIRED IAW EO 601R-57-44255 AND HORIZON AIR EA R-57-49.Oct 7, 2003 · N611QX · Cndair CL6002C10SDR QXEA200301319Panel · chafedRIGHT WING PANEL 622DB LEADING EDGE OF PANEL IS CHAFED. REPAIRED IAW CRJ-700 AMM 27-81-25-820-901 AND EO 601R-57-4253 AND HORIZON AIR EA R-57-48.Oct 7, 2003 · N611QX · Cndair CL6002C10SDR DL75K030905Wedge · dentedFOUND ON PSV-2 CK DENT ON NUMBER 8 SLAT T/E WEDGE. REPAIRED PER SRM 57-43-02D, SRM 51-70-10D AND OPERATION 1000.Oct 6, 2003 · N6715C · Boeing 757232SDR 2003UALA00739Skin · delaminatedNR 4 SLAT OUTBOARD ON THE LOWER SURFACE OF TR EDGE DELAMINATED 1.7 INCH CHORDWISE BY .7 INCH SPAN WISE. MAJOR REPAIR ACCOMPLISHED. INJECTED STRUCTURAL ADHESIVE INTO DELAMINATED AREA.Oct 3, 2003 · N217UA · Boeing 777222SDR GTIA030879Cap · crackedFOUND RIGHT WING NR 5 SLAT OUTBOARD END CAP IS CRACKED. REMOVED END CAP. LOCATED AND DRILLED NEW PART. INSTALLED NEW END CAP. (M)Oct 2, 2003 · N820NK · Doug DC982SDR SWAA032182Skin · delaminatedDURING SCHEDULED A1 CHECK, FOUND NR 5 L/E SLAT DELAMINATED AT OUTBOARD END UPPER SURFACE. REMOVED AND REPLACED NR 5 L/E SLAT PER MM.Oct 1, 2003 · N366SW · Boeing 7373H4SDR 250TR0025Skin · delaminatedNR 1 LEADING EDGE SLAT FOUND DELAMINATED. REPLACED NR 1 LEADING EDGE SLAT ASSY PER MM 27-81-21.Oct 1, 2003 · N250TR · Boeing 7372K5SDR AWXA200301346Wedge · debondedMCN - MAJOR REPAIR - DURING C-17 CHECK THE NR 4 SLAT WEDGE WAS FOUND DISBONDED AT THE LOWER INBOARD END. MAINTENANCE CUT OUT DAMAGE ON NR 4 SLAT WEDGE; FABRICATED A REPAIR DOUBLER; BONDED REPAIR DOUBLER TO SLAT IAW B737-300 SRM 51-70-10, REPAIR 7, FIG 16, PG Sep 30, 2003 · N156AW · Boeing 7373G7SDR XGN2003F00003Hinge · brokenLT WING LEADING EDGE ASSY SAGGING AND FLEXING BETWEEN W/S 49.131 AND 91.131. WE WERE UNABLE TO DISASSEMBLE LEADING EDGE ASSEMBLY FROM THE FORWARD SPAR CAP DUE TO BROKEN (105774C-ZG18700) HINGE PIN. NOT ABLE TO DISASSEMBLE THE LEADING, COULD ONLY GUESS THAT TSep 29, 2003 · N5740V · Beech 95C55SDR 2004F00071Skin · dentedDURING SERVICE CHECK, FOUND DENT ON LEADING EDGE OF SKIN OF LEFT WING AT STATION 180 ABOVE NR 3 KRUGER FLAP. CUT OUT DENTED SECTION OF WING, FIXED LEADING EDGE SKIN AND INNER SKIN AT STATION 180. FABRICATED A FLUSH REPAIR FILLER AND DOUBLER. FABRICATED SKINSep 26, 2003 · N801EA · Boeing 727225SDR SWAA032108Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND NR 5 L/E SLAT DELAMINATED AT LOWER SURFACE. REMOVED AND REPLACED NR 5 L/E SLAT PER MM.Sep 20, 2003 · N662SW · Boeing 7373Q8SDR UPS03841357Rib · crackedINSPECTION TYPE: C1, RT WING LE. UPPER RIB IS CRACKED AT XFS 835. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM. 57-2-0 FIG. 2Sep 19, 2003 · N866UP · Doug DC873FSDR UPS03241247Doubler · corrodedFOUND CORROSION ON NR 3 KRUEGER FLAP EXTENDING UNDER DOUBLER REPAIR R&R REQUIRED. REMOVED AND REPLACED NR 3 KRUEGER FLAP IAW MM 27-81-01.Sep 19, 2003 · N945UP · Boeing 72722CSDR SWAA032065Skin · delaminatedDURING SCHEDULED C1 CHECK, FOUND NR 5 L/E SLAT DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED NR 5 L/E SLAT PER MM.Sep 16, 2003 · N605SW · Boeing 7373H4SDR UPS03241369Rib · crackedINSPECTION TYPE:C NR 6 SLAT IB TRACK IB FLAP RIB CRACK AT FWD CORNER NR 6 FLAT IB TRACK REMOVED IAW OHM 57-51-51 REPAIR CARRIED OUT IAW SRM 51-40-3. NR 6 SLAT IB TRACK INSTALLED IAW OHM 57-51-51. FUNCTION TEST CARRIED OUT IAW MM 27-81-00. OPS. OKSep 15, 2003 · N935UP · Boeing 7271A7CSDR UPS03241356Rib · crackedINSPECTION TYPE: C, NR 6 SLAT RIB 2ND FROM O/B END CRACKED AT AFT END. REPAIR CARRIED OUT IAW SRM 57-50-03 FIG 9.Sep 15, 2003 · N935UP · Boeing 7271A7CSDR AWXA200301060Panel · crackedDURING C-16 CHECK .1875 INCH CRACK WAS FOUND ON CLOSE OUT PANEL BELOW NR 2 SLAT INBOARD MAIN TRACK AT WBL 355. MAINTENANCE REMOVED CRACKED NR 2 SLAT CLOSE OUT PANEL AT WBL 355; FABRICATED A NEW REPLACEMENT PANEL IAW DWG 69-53316; INSTALLED REPAIR PART IAW B737Sep 14, 2003 · N186AW · Boeing 737277SDR AUS20030930Bolt · failed(AUS) LEADING EDGE SLAT BOLT FAILED.Sep 11, 2003 · Boeing 767338SDR ASAA0380581Fitting · wornOAK LINE CHECK, FOUND LT NR 4 SLAT CABLE FOUND TO BE WEARING INTO WING LEADING EDGE. REPLACED LEADING EDGE STRUCTURE IAW EA 5740-01361. (M)Sep 10, 2003 · N973AS · Doug DC983SDR C1HA200386004Wedge · gougedNR 3 SLAT TRAILING EDGE WEDGE GOUGED.Sep 8, 2003 · N686CA · Boeing 7272S7SDR C1HA200386003Wedge · gougedNR 7 SLAT TRAILING EDGE WEDGE GOUGED.Sep 8, 2003 · N686CA · Boeing 7272S7SDR 03FDEA01487Rib · crackedLT WING SLAT TRACK NR 16, INBOARD SUPPORT RIB CRACKED. LT WING SLAT TRACK NR 16, INBOARD SUPPORT RIB REMOVED AND REPLACED AS PER SRM 51-33-01 VOL. 2 & SRM 51-35-01 VOL. 2.Sep 7, 2003 · N591FE · Doug MD11SDR 03FDEA01488Rib · crackedRT WING SLAT TRACK NR 16, INBOARD SUPPORT RIB CRACKED. RT WING SLAT TRACK NR 16, INBOARD SUPPORT RIB REMOVED AND REPLACED AS PER SRM 51-33-01 VOL. 2 & SRM 51-35-01 VOL. 2Sep 7, 2003 · N591FE · Doug MD11
Back to JASC 5754