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 CA050316003Arm · punctured(CAN) DURING GROUND HANDLING, MAINTENANCE DISCOVERED A SIGNIFICANT FUEL LEAK ON THE RT WING. FUEL WAS RUNNING DOWN THE OB FLAP CANOE AND DRIPPING ONTO GROUND. AIRCRAFT WAS REMOVED FROM SERVICE AND PLACED INTO HANGAR FOR FURTHER INSPECTION AND FUEL DRAINING. AMar 14, 2005 · Boeing 737522SDR SWAA050782Wedge · delaminatedDURING SCHEDULED D-CHECK, FOUND RT WING, NR 4 L/E SLAT, INBOARD END T/E WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.Mar 14, 2005 · N607SW · Boeing 7373H4SDR SWAA050777Slat Track · corrodedDURING SCHEDULED D-CHECK, FOUND RT WING, NR 4 L/E SLAT, OUTBOARD MAIN TRACK, LOWER SURFACE CORRODED. REPAIRED TRACK PER OHM.Mar 14, 2005 · N605SW · Boeing 7373H4SDR SWAA050763Skin · crackedDURING SCHEDULED C4 CHECK, FOUND OUTBOARD END NR 2 L/E SLAT LOWER SKIN CRACKED. REPAIRED SKIN PER SWA EA.Mar 11, 2005 · N639SW · Boeing 7373H4SDR ASAA0540166Skin · dentedPAE - NR 6 SLAT TRAILING EDGE HAS A DENT. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IAW SRM, REPAIR 21. (K)Mar 10, 2005 · N764AS · Boeing 7374Q8SDR DHL2005782523Skin · crackedSKIN CRACKED ON UPPER SKIN CUT OUT FOR NR 5 SLAT IB TRACK, RT WING LE WS 375. STOP DRILLED CRACK SIZE 1/4 AT UPPER SKIN CUT OUT NR 5 SLAT IB TRACK RT WING LE IAW B727 SRM 51-10-1. FABRICATE DOUBLER REPAIR USING 2024T3 .063 PO NR 9001634 SIZE 7 1/2 INCH BY 6.Mar 10, 2005 · N782DH · Boeing 727227SDR DHL2005782520Skin · dentedNR 2 SLAT EXTERNAL SKIN DENTED (3) PLACES. MEASURED DENT AT WS 656.3 ON NR 2 SLAT AND FOUND IN LIMITS A.2/Y.005=40 IAW SRM 53-30-1 FIG 1. MEASURED DENT AT WS 684.3 ON NR 2 SLAT AND FOUND TO BE OUT OF LIMITS A.4/Y.32=28.1 IAW B727 SRM 53-30-1 FIG 1 AND REPAIMar 10, 2005 · N782DH · Boeing 727227SDR DHL2005782501Skin · crackedCRACK ON NR 4 SLAT SKIN AT I/B UP STOP BLOCK FASTENER. STOP DRILLED CRACK AT NR 4 SLAT SKIN AT I/B UPSTOP IAW B727 SRM 51-10-1. ACCOMPLISHED 727 HFEC INSPECTION 51-00-00 CRACK CONTIMENT CONFIRMED. FABRICATED REPAIR DOUBLER MAT USED 2024-T3 .80 DIMENSION 11 Mar 10, 2005 · N782DH · Boeing 727227SDR AWXA200500377Skin · delaminatedMCN - MAJOR REPAIR - DURING C-05 CHECK, FOUND THE UPPER SURFACE OF THE NR 3 SLAT WEDGE DELAMINATED AT INBOARD END, SLAT STA 14. MAINTENANCE CUTOUT DAMAGE IN UPPER SURFACE OF NR 3 SLAT WEDGE FROM SS 12.25 TO SS 15.25; FABRICATED A CORE FILLER AND DOUBLER; BONDMar 10, 2005 · N336AW · Boeing 737375SDR USAA050344Skin · crackedCLT - Q2 - NR 5 SLAT SKIN, 38 INCH CRACK, NR 5 SLAT LE SKIN. INSTALLED REPAIR DOUBLER IAW SRM. (K)Mar 7, 2005 · N519AU · Boeing 7373B7SDR USAA050343Skin · crackedCLT - Q2 - NR 5 SLAT SKIN, SEVERAL .250 INCH CRACKS, NR 5 SLAT LOWER SKIN L/E. INSTALLED REPAIR DOUBLER. (K)Mar 7, 2005 · N519AU · Boeing 7373B7SDR USAA050342Wedge · wornCLT - Q2 - NR 4 SLAT, 2 INCH X 2 INCH, WEAR. NR 4 SLAT T/E WEDGE LOWER SKIN IB. ACCOMPLISHED COMPOSITE REPAIR IAW EA. (K)Mar 7, 2005 · N519AU · Boeing 7373B7SDR SWAA050681Wedge · delaminatedDURING SCHEDULED D-CHECK, FOUND RT WING, NR 5 L/E SLAT, I/B END T/E WEDGE DELAMINATED. REMOVED AND REPLACED NR 5 L/E SLAT ASSY PER MM.Mar 6, 2005 · N607SW · Boeing 7373H4SDR 05FDEA00374Structure · damagedREPAIR ON LT O/B SLAT UPPER SURFACE NEEDS EVALUATION FOR FAA APPROVED DATA AND MAJOR OR MINOR CLASSIFICATION, REF CONFORMITY INSPECTION RECORD SHEET 3 ITEM 24. REPAIR DETERMINED TO BE ACCOMPLISHED IAW A310-200 SRM 57-40-00 FIG 201. CLASSIFIED AS A MINOR REPAMar 4, 2005 · N446FE · Airbus A310222SDR DHL2005781563Rib · crackedDURING A C-CHECK, RT WING NR 6 SLAT I/B RIB AT ACTUATOR ROD ATTACH POINT IS CRACKED. REMOVED DAMAGED RIB IAW B727 SRM 51-30-2, FABRICATED NEW RIB, MATERIAL USED 2024 T3, .040 PO 9002012 DIM 15 BY 5.50 INCHES IAW B727 SRM 57-50-2 FIG 2 AND 51-20-1 FIG 7. ALODMar 3, 2005 · N781DH · Boeing 727227SDR SWAA050652Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND LT WING, NR 2 SLAT, OUTBOARD T/E WEDGE PANEL DELAMINATED. REMOVED AND REPLACED NR 2 SLAT PER MM.Mar 3, 2005 · N383SW · Boeing 7373H4SDR 05FDEA00325Skin · chafedLEFTHAND WING NR 3 SLAT, LOWER SURFACE, MOST LOWER, FAIRING FOUND CHAFING DAMAGE AGAINST THE FAIRING DOOR OF THE ANTI-ICE TELESCOPIC DUCT. LEFTHAND WING NR 3 SLAT, LOWER SURFACE REPAIRED AS PER FEDEX EA 1-5740-78105. TITLE: WINGS - LEADING EDGE AND LEADINMar 2, 2005 · N577FE · Doug MD11SDR ASAA0580159Skin · chafedHV - CHECK - RT IB FLAP L/E PANEL IS CHAFED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER. (K)Mar 1, 2005 · N965AS · Doug DC983SDR AWXA200500391Skin · crackedMCN - MAJOR REPAIR - DURING C-16 CHECK 7 EACH .3125 INCH CRACKS WERE FOUND IN LOWER SURFACE SKIN OF NR 5 SLAT BETWEEN SLAT STATIONS 166 - 215. MAINTENANCE CUT OUT DAMAGE IN LOWER SURFACE SLAT SKIN FROM SS 166 TO SS 215 RT; FABRICATED A FILLER AND SPLICE PLATEMar 1, 2005 · N305AW · Boeing 7373G7SDR USAA050306Skin · crackedCLT - FOUND NR 5 SLAT WITH 4 INCH CRACK, LOWER LE SKIN NR 5. INSTALLED REPAIR DOUBLER IAW SRM 57-43-01. (M)Feb 28, 2005 · N519AU · Boeing 7373B7SDR CA050308012Bracket · cracked(CAN) FLAP SLAT BRACKET FOUND CRACKED DURING MAINTENANCE, CHECK THE CRACKS IN THOSE 3 BRACKETS ARE 1 INCH LONG LOCATED IN THE FORWARD RADIUS OF THE BENDS.Feb 24, 2005 · Bag JETSTM3212SDR USAA050353Skin · chafedPIT - Q4 - SLAT, 8 INCH LONG X 3 INCH WIDE AREA, CHAFED. NR 4 SLAT IB T/E LOWER SKIN SURFACE. INSTALLED FILLER AND INTERNAL DOUBLER, KEY CORE AND TOP DOUBLER, SEALED EDGE AND REFINISHED IAW SRM. (K)Feb 24, 2005 · N438US · Boeing 7374B7SDR DHL2005805506Frame · crackedLEFT OUTER WING INBOARD L/E UPPER FORMER CRACKED 0.500, XFS 603.750. REMOVED FASTENERS IAW SRM 51-1-20D PG 21, SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END AND FABRICATED ANGLE DOUBLERS (AL7075-T6 0.032) (2EA) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED Feb 24, 2005 · N805DH · Doug DC873FSDR DHL2005805512Frame · crackedLEFT OUTER WING INBOARD L/E UPPER FORMER CRACKED 0.500 XFS 591.500. REMOVED FASTENERS IAW SRM 51-1-20D PG 21. PERFORMED STOP DRILL ON CRACK END AND FABRICATED ANGLE DOUBLERS (2EA) (AL7075-T6 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA ANFeb 23, 2005 · N805DH · Doug DC873FSDR DHL2005805505Frame · crackedLEFT OUTER WING INBOARD L/E UPPER FORMER CRACKED 0.500, XFS 678.750. REMOVED FASTENERS IAW SRM 51-1-20D PG 21. FABRICATED (2EA) ANGLE DOUBLERS (AL7075-T6 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLERS IAW SRM 51-1-8B. INFeb 23, 2005 · N805DH · Doug DC873FSDR SWAA050512Skin · delaminatedDURING SCHEDULED D-CHECK, FOUND NR 3 L/E SLAT DELAMINATED. REPAIRED NR 3 L/E SLAT PER SRM.Feb 21, 2005 · N662SW · Boeing 7373Q8SDR USAA050285Skin · crackedCLT - FOUND SLAT SKIN CRACKED .025 INCH, NR 6 SLAT LOWER L/E. INSTALLED DOUBLER. (M)Feb 17, 2005 · N519AU · Boeing 7373B7SDR DHL2005781513Skin · crackedDURING A "C" CHECK, CRACKED PANEL SURROUNDING NR 7 SLAT I/B UPSTOP BOLT STOP PAD. REMOVED CRACKED PANEL IAW B727 SRM 51-30-2. FABRICATED PANEL SURROUNDING NR 7 SLAT I/B UPSTOP BOLT STOP PAD MAT USED 2024T3 .050 PO NR 9001684 DIM 18 3/4 INCH BY 8 1/4 INCH IAWFeb 17, 2005 · N781DH · Boeing 727227SDR SWAA050455Wedge · delaminatedDURING SCHEDULED C4 CHECK, FOUND RT WING NR 4 L/E SLAT WEDGE DELAMINATED. REPAIRED PER MM.Feb 17, 2005 · N316SW · Boeing 7373H4SDR AWXA200500317Wedge · delaminatedMCN - MAJOR REPAIR - DURING C-14 CHECK FOUND THE NR 4 SLAT WEDGE DELAMINATED ON LOWER SURFACE AT INBOARD END, SLAT STA 14. MAINTENANCE REMOVED DELAMINATED AREA OF NR 4 SLAT FROM SLAT STA 12.25 TO 15.25 RT; FABRICATED A FILLER AND DOUBLER; BONDED REPAIR PARTS Feb 16, 2005 · N307AW · Boeing 7373G7SDR AWXA200500316Wedge · delaminatedMCN - MAJOR REPAIR - DURING C-14 CHECK FOUND THE NR 5 SLAT WEDGE DELAMINATED AT INBOARD END, SLAT STA 257. MAINTENANCE REMOVED DELAMINATED AREA OF NR 5 SLAT WEDGE; FABRICATED A FILLER AND DOUBLER; BONDED REPAIR PARTS TO SLAT IAW B737-300 SRM 51-70-10 FIG 31.Feb 16, 2005 · N307AW · Boeing 7373G7SDR DHL2005781503Skin · gougedDURING A C-CHECK, ACCOMPLISH INDENTIFICATION OF EXISTING REPAIR ON LT WING NR 4 SLAT SKIN, WS 436, PER ASTAR J/C FCD 500001-018-B. REMOVED PREVIOUS REPAIR WITH NON-COMPLIANT PER SRM AT LT WING NR 4 SLAT SKIN WS 434 IAW B727 SRM 51-30-2. FABRICATED NEW REPAIRFeb 16, 2005 · N781DH · Boeing 727227SDR USAA050291Skin · crackedPIT - NR 1 SLAT WITH FIVE CRACKS .1875 INCH CRACKS, LOWER SKIN UNDER OUTBOARD SLAT FITTING, AFT RIVET ROW. INSTALLED DOUBLER PER SRM 57-43-01. (M)Feb 15, 2005 · N438US · Boeing 7374B7SDR DHL2005781532Skin · crackedDURING A C-CHECK, NR 4 SLAT CRACKED AT I/B & O/B OF ACTUATOR ROD ATTACH POINT (IN LIGHTENING HOLE). REMOVED AND REPLACED NR 4 SLAT WEB (RIBS) IAW B727 SRM 51-30-2, P/N 65-17276-9, PO441715 & P/N 65-17276 PO441715.Feb 14, 2005 · N781DH · Boeing 727227SDR DHL2005781522Rib · crackedDURING A "C" CHECK, RT WING LEADING EDGE RIB AT SLAT, STA 260 IS CRACKED. REMOVED AT RT WING LEADING EDGE RIB AT STA 260 FOR FAB IAW B727 SRM 51-30-2, FABRICATED NEW RIB, MAT'L USED 2024-T3 .050 PO NR 9001873,DIM.15 INCH BY 1 1/2 INCH IAW B727 SRM 57-20-2 FIFeb 13, 2005 · N781DH · Boeing 727227SDR QXEA200500281Skin · chafedYYC - LT AILERON UPPER SKIN LEADING EDGE HAD CHAFED MARKS FROM SEAL. REPAIRED IAW CRJ700 SRM 51-41-01-101-001-A01, SRM 51-12-00-001-001-A01, 51-21-11-001-001-A01, 51-25-03-001-001-A01, 51-25-01-001-001-A01 AND CRJ700 AMM 57-52-32-000-809-A01.Feb 12, 2005 · N609QX · Cndair CL6002C10SDR DHL2005781531Skin · crackedDURING A C-CHECK, NR 1 SLAT SKIN CRACKED AT I/B TRACK ATTACH POINT (MARKED). STOP DRILLED WITH .25 INCH DIAMETER DRILL IAW B727 SRM 51-10-1 FAB. DOUBLER REPAIR WITH 2024T3 0.80 SIZE 6.5 X 6.5 INCH PO 9001502 IAW B727 SRM 57-50-3 FIG 1 & 57-50-2 FIG 2. TREATFeb 11, 2005 · N781DH · Boeing 727227SDR DHL2005781530Skin · gougedDURING A C-CHECK, NR 2 SLAT SKIN GOUGED AT I/B SLAT HOOK (MARKED). REMOVED FASTENERS FOR ACCESS AT NR 2 SLAT SKIN AT I/B SLAT HOOK IAW B727 SRM 51-30-2. FABRICATED DOUBLER REPAIR MAT USED 2024T3 .125 PO 9001068 DIM 5.5 X 3.5 INCH IAW B727 SRM 57-50-3 FIG 10.Feb 11, 2005 · N781DH · Boeing 727227SDR DHL2005781525Skin · dentedDURING A "C" CHECK, NR 1 SLAT L/E EXTERIOR SKIN DENTED AND SCRATCHED AT WSTA 760 (MARKED). CUT OUT DAMAGED AREA APROX 1 INCH BY 2 1/4 INCH AT NR 1 SLAT LE EXT SKIN W STA 760 IAW B727 SRM 57-50-3. FAB DOUBLER REPAIR WITH 2024T3 .080 SIZE 5 1/4 INCH BY 4.5 INFeb 11, 2005 · N781DH · Boeing 727227SDR USAA050298Skin · chafedPIT - FOUND RIGHT OUTBOARD MID FLAP CHAFED .25 INCH BY 2 INCH BY .016 INCH, OUTBOARD 4 EDGE SURFACE. DOUBLER INSTALLED PER SRM 57-53-01 FIG 208. (M)Feb 11, 2005 · N520AU · Boeing 7373B7SDR DHL2005781516Skin · dentedDURING A "C" CHECK, LT L/E SKIN DENTED 15 INCH I/B OF NR 4 SLAT I/B TRACK. CUT OUT DAMAGED AREA AT LT WING L/E SKIN I/B NR 4 SLAT, I/B TRACK DIM.3/4 BY 3/4 IAW B727 SRM 57-30-4 FIG.1. FABRICATED DOUBLER REPAIR MAT'L 2024 T3 .050 PO 9001873 DIM 3 1/4 BY 3 3Feb 11, 2005 · N781DH · Boeing 727227SDR DHL2005781505Skin · crackedDURING A C-CHECK, NR 3 SLAT SKIN AT TRACK ATTACH POINT CRACKED. MAKE 2 EA STOP DRILLS WITH .25 DIA DRILL AT NR 3 SLAT SKIN AT I/B TRACK IAW B727 SRM 57-5-3 FIG 1. ACCOMPLISHED 727 HFEC INSPECTION 51-00-00 FIG 4, CRACK CONTAINMENT CONFIRMED. FAB REPAIR DOUBLFeb 11, 2005 · N781DH · Boeing 727227SDR DHL2005781502Skin · dentedDURING A C-CHECK, LT WING L/E SKIN DENTED 15 INCHES I/B OF NR 4 SLAT I/B TRACK. CUT OUT DAMAGED AREA LT WING LEADING EDGE SKIN I/B NR 4 SLAT I/B TRACK DIM .75 X .75 INCH IAW B727 SRM 57-30-4 FIG 1. FABRICATED DOUBLER REPAIR MATL USED 2024-T3 .050 PO 9001873 Feb 11, 2005 · N781DH · Boeing 727227SDR DHL2005781501Skin · gougedDURING AN C-CHECK, NR 2 SLAT SKIN GOUGED AT I/B SLAT HOOK. REMOVED FASTENERS FOR ACCESS AT NR 2 SLAT SKIN AT I/B SLAT HOOK IAW B727 SRM 51-30-2, FABRICATED DOUBLER REPAIR, MAT USED 2024-T3 .125 PO 9001068, DIM 5.5 X 3.5 INCHES IAW B727 SRM 57-50-3 FIG 10. ALFeb 11, 2005 · N781DH · Boeing 727227SDR USAA050299Skin · crackedPIT - FOUND NR 5 SLAT SKIN CRACKED 1 INCH, OUTBOARD FORWARD EDGE ABOVE UPSTOP. INSTALLED DOUBLER PER SRM 57-43-01. (M)Feb 8, 2005 · N520AU · Boeing 7373B7SDR ASAA0540120Skin · crackedPAE - L/W NR 1 SLAT LOWER L/E SKIN CRACKED. ACCESSED AREA, FABRICATED REPAIR, INSTALLED REPAIR PARTS, CLOSED AREA. (K)Feb 6, 2005 · N772AS · Boeing 7374Q8SDR ABXA050034Wedge · delaminatedWHILE PERFORMING LINE MAINTENANCE, FOUND LEFT WING NR 4 SLAT WEDGE DELAMINATED BEYOND LIMITS AT INBOARD END. REPLACED NR 4 SLAT IAW B767 MM 27-81-02-4.Feb 6, 2005 · N775AX · Boeing 767281SDR SWAA050329Bearing · wornMOVING FLAPS FROM 5 TO 10 DEGREES BOTH PILOTS HEARD A LOUD POP AND A THUMP, ALL INDICATIONS NORMAL. REMOVED AND REPLACED NR 6 L/E SLAT BEARINGS PER SERVICE LETTER AND MM.Feb 6, 2005 · N300SW · Boeing 7373H4SDR USAA050352Skin · delaminatedPIT - C5 - SLAT, 3 INCH LONG X 2.5 INCH WIDE - 2 AREAS, DELAMINATION. NR 5 SLAT TOP SURFACE IB AND OB T/E. INSTALED NEW CORE, TOP DOUBLERS, SEAL AND REFINISH IAW SRM. (K)Feb 3, 2005 · N436US · Boeing 7374B7SDR QXEA200500371Skin · chafedYYC - LEFTHAND OUTBOARD SLAT IS CHAFING THE UPPER WING SHROUD. REPAIRED IAW DHC-8 SRM 51-21-10 AND 51-25-10.Feb 2, 2005 · N539DS · Bombdr DHC8401
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