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 2004UALA00054Wedge · delaminatedT/E WEDGE DELAMINATED AND DENTED. REMOVED, REPAIRED AND REINSTALLED.Jan 6, 2004 · N774UA · Boeing 777222SDR DHL2004806533Angle · crackedRT WING STUB WING SUPPORT ANGLE CRACKED 2.000 AT STA XILD 42.000. REMOVED CRACKED SUPPORT ANGLE IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. FABRICATED NEW SUPPORT ANGLE AL7075-T6 0.063 IAW SRM 57-2-0 PG 1-2. CLEANED, TREATED AND PRIMED AREA AND SUPPORT ANGLE IAWJan 6, 2004 · N806DH · Doug DC873FSDR DHL2004752504Skin · delaminatedDURING C-CHECK, LT INBOARD FOREFLAP UPPER INBOARD SURFACE PREVIOUS REPAIR DELAMINATED. REMOVED DELAMINATED PREVIOUS REPAIR. FABRICATED FILLER APPROX 13 INCH X 13 INCH AND DOUBLER APPROX 13 INCH X 5 INCH FROM 2024 T3 .016 PO 900291. CLEANED, PREPPED, APPLIEDJan 6, 2004 · N752DH · Boeing 727223SDR DHL2004752508Angle · crackedDURING C-CHECK, RT WING WBL 130.7 HAS CRACK IN L-ANGLE OF L/E FLAP AREA. STOP DRILLED CRACK IAW 727 SRM 51-10-1 & FABBED REPAIR ANGLE FROM 2024T3050 DIM 6 INCH X 2 INCH PO 900471 IAW 727 SRM 51-40-3 FIG 1. REPAIR TREATED & PRIMED IAW 727 SRM 51-10-2 & INSTALJan 6, 2004 · N752DH · Boeing 727223SDR 04FDEA00030Fillet · crackedLEFT WING HIGH PERFORMANCE FILLET O/B RIB FOUND CRACKED APPROX 1.5 INCH LENGTH AT UPPER STUD AREA.Jan 5, 2004 · N584FE · Doug MD11SDR DHL2004753508Frame · crackedNR 2 SLAT OUTBOARD FRAME AT ACT ROD END ATTACH HAS THE FWD LOWER CORNER CRACKED. REMOVED NR 2 SLAT ASSY FOR S/M REPAIR IAW B727 M/M 27-81-11. REMOVED INT ACCESS PNL & 3 RIBS AT O/B FRAME AT ACT IAW B727 SRM 51-30-2. DRILLED NEW HOLES AT RIB'S P/N 65-17310-4Jan 2, 2004 · N753DH · Boeing 727223SDR AWXA200400085Wedge · delaminatedMCN - MAJOR REPAIR - DURING C-18 CHECK NR 2 SLAT WEDGE LOWER SURFACE WAS FOUND DELAMINATED INBOARD OF ANTI-ICE TELESCOPING TUBE. MAINTENANCE CUT OUT DELAMINATED SKIN ON LOWER SURFACE OF NR 2 SLAT; FABRICATED A DOUBLER & FILLER; BONDED REPAIR PARTS IAW B737-30Jan 1, 2004 · N324AW · Boeing 737301SDR 04FDEA00001Strut · looseINBOARD SLAT MECHANICAL RT STRUT ASSY BEARING FOUND MIGRATED. I/B SLAT MECHANICAL RT STRUT ASSY REMOVED & REPLACED AS PER CMM 27- 03-20.Jan 1, 2004 · N621FE · Doug MD11SDR UPS04841723Rib · crackedINSPECTION TYPE: C3, LEFT WING NR 2 STUB WING UPPER RIB IS CRACKED AT XS 250.089. CUT OUT DAMAGED AREA, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 57-2-0 FIG 2.Dec 30, 2003 · N702UP · Doug DC871FSDR DHL2003753512Rib · crackedN/R 65147 NR 8 SLAT AT ACTUATOR ATTACH MOUNT IB. RIB IS CRACKED ABOUT 2.5 INCHES LONG SLAT STA. 390. REMOVED NR 8 SLAT IAW M/M 27-81-11. REMOVED NR 8 SLAT ACTUATOR IAW MM 27-81-22. REMOVED ACCESS PANELS AND RIBS AT NR 8 SLAT IAW SRM 51-30-2. REMOVED RIBS Dec 29, 2003 · N753DH · Boeing 727223SDR SWAA032822Skin · crackedDURING SCHEDULED C2 CHECK, FOUND NR 3 L/E SLAT LOWER T/E SKIN CRACKED AT FASTENER'S ROW. REPAIRED SKIN PER SWA EA.Dec 28, 2003 · N646SW · Boeing 7373H4SDR AWXA200400051Attach Bracket · crackedLCQ - MAJOR REPAIR - DURING C-17 CHECK A 1.1875 INCH CRACK WAS FOUND ON LT WING LEADING EDGE NR 3 SLAT ACTUATOR DOOR FORWARD ATTACH BRACKET AT WBL 328. MAINTENANCE REMOVED CRACKED NR 3 SLAT ACTUATOR DOOR ATTACH BRACKET AT WBL 328; FABRICATED A NEW REPLACEMENTDec 24, 2003 · N332AW · Boeing 7373B7SDR SWAA032764Wedge · delaminatedNR 1 SLAT T/E WEDGE DELAMINATED. REMOVED AND REPLACED NR 1 SLAT PER MM.Dec 17, 2003 · Boeing 7372H4SDR 03FDEA02209Fitting · crackedLT WING, FOUND NR 16 SLAT TRACK, INBOARD FITTING CRACKED, APPROX 0.250 INCH IN LENGTH. NR 16 SLAT TRACK, INBOARD FITTING REMOVED AND REPLACED NEW RIB FITTING ARB2850-505 AS PER SRM 51-33-01 VOL. II AND OPERATION CHECK CARRIED OUT AS PER AMM 27-80-30.Dec 17, 2003 · N584FE · Doug MD11SDR SWAA032733Wedge · delaminatedDURING SCHEDULED D CHECK, FOUND NR 5 L/E SLAT T/E WEDGE INBOARD END DELAMINATED. REPAIRED WEDGE PER SRM.Dec 15, 2003 · N303SW · Boeing 7373H4SDR 03FDEA02184Fairing · wornRT WING FIX LEADING EDGE FAIRING ADJACENT TO NR 8 SLAT OUTBOARD END FOUND WORN. COMPLIED WITH FEDEX EA 1-5720-73367, OUTER WING, FIXED LEADING EDGE SKIN.Dec 14, 2003 · N608FE · Doug MD11SDR 03FDEA02183Fairing · wornLT WING FIX LEADING EDGE FAIRING ADJACENT TO OUTBOARD END OF LEADING EDGE SLAT FOUND WORN AT 02 LOCATIONS. COMPLIED WITH FEDEX EA 1-5720-73368, OUTER WING FIXED LEADING EDGE SKIN.Dec 14, 2003 · N608FE · Doug MD11SDR CALA0300708Skin · crackedINSPECTION FOUND A 3 INCH CRACK IN NR 1 SLAT INTERIOR SKIN BETWEEN NR 4 AND NR 5 SLAT TRACKS OF LT WING, STA XFS 167. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5752-01134, PART 1, STEP 13.Dec 11, 2003 · N16806 · Doug DC982SDR DHL2003742549Access Panel · crackedDURING C-CHECK, NR 4 SLAT IS CRACKED AT ACCESS PANEL LOWER ATTACH ANGLE AT THE RIB INBD OF ANTI ICE DUCT. REMOVED DAMAGED AREA DIM 1.125 INCHES AND FABRICATED NEW DOUBLER FROM 2024 T3 .050 PO 900274 DIM 6 X 1 INCH AND FILLER FROM 2024-T3 .040 PO 900471, 1.12Dec 9, 2003 · N742DH · Boeing 727225SDR DHL200374249Skin · crackedDURING C-CHECK, NR 4 SLAT IS CRACKED AT ACCESS PANEL LOWER ATTACH ANGLE AT THE RIB INBD OF ANTI ICE DUCT. REMOVED DAMAGED AREA DIM 1.125 INCH AND FABRICATED NEW DOUBLER FROM 2024 T3 .050 PO 900274 DIM 6 X 1 INCH AND FILLER FROM 2024-T3 .040 PO 900471 1.125 X Dec 9, 2003 · N742DH · Boeing 727225SDR SWAA032691Structure · delaminatedPHX - DURING SCHEDULED C4 CHECK, FOUND NR 6 SLAT TRAILING EDGE DELAMINATED AT INBOARD END. REPAIRED PER SRM. (M)Dec 9, 2003 · N669SW · Boeing 7373A4SDR AWXA200301621Slat · delaminatedMCN - MAJOR REPAIR - DURING C-18 CHECK THE NR 3 SLAT WAS FOUND DELAMINATED AT THE INBOARD UPPER TRAILING EDGE. MAINTENANCE REMOVED DELAMINATION ON INBOARD UPPER TRAILING EDGE OF NR 3 SLAT; FABRICATED REPAIR DOUBLERS; BONDED DOUBLERS ON SLAT IAW B737-300 SRM 5Dec 9, 2003 · N325AW · Boeing 737301SDR AWXA200301601Skin · delaminatedMCN - MAJOR REPAIR - DURING -18 CHECK THE NR 2 SLAT INBOARD UPPER TRAILING EDGE WAS FOUND DELAMINATED AROUND PREVIOUS REPAIR. MAINTENANCE REMOVED EXISTING REPAIR AND DELAMINATED SKIN ON NR 2 SLAT INBOARD UPPER TRAILING EDGE; FABRICATED REPAIR DOUBLERS; INSTALDec 9, 2003 · N325AW · Boeing 737301SDR DHL2003745027Skin · crackedNR 6 LEADING EDGE SLAT BOTTOM SKIN CRACKED 30 INCHES FROM INBOARD EDGE. REMOVED AND REPLACED NR 6 LEADING EDGE SLAT ASSEMBLY IAW B-727 M/M 27-81-11, OPS CHECKED GOOD IAW B-727 M/M 27-81-0. P/N OFF: 65-16222-2, S/N:BN939, P/N ON: 65-16222-92, S/N: BN3.Dec 8, 2003 · N745DH · Boeing 727224SDR AWXA200400058Wedge · delaminatedMCN - MAJOR REPAIR - DURING C-18 CHECK FOUND THE NR 3 SLAT OUTBOARD END UPPER WEDGE SKIN DELAMINATED. MAINTENANCE CUT OUT DELAMINATED AREA NR 3 SLAT OUTBOARD END UPPER WEDGE SKIN; CLEANED AND PREPARED AREA; FABRICATED REPAIR DOUBLERS; INSTALLED BOND REPAIR IADec 5, 2003 · N174AW · Boeing 73733ASDR AWXA200301592Skin · delaminatedDURING C-18 CHECK THE NR 1 SLAT TRAILING EDGE WEDGE UPPER SKIN WAS FOUND DELAMINATED AT OUTBOARD MAIN TRACK. MAINTENANCE REMOVED DAMAGED NR 1 SLAT TRAILING EDGE WEDGE UPPER SKIN; FABRICATED A DOUBLER AND FILLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-10Dec 5, 2003 · N174AW · Boeing 73733ASDR AWXA200301591Skin · delaminatedDURING C-18 CHECK THE NR 1 SLAT TRAILING EDGE UPPER SKIN WAS FOUND DELAMINATED AT OUTBOARD AUXILIARY TRACK. MAINTENANCE REMOVED DAMAGED NR 1 SLAT TRAILING EDGE UPPER SKIN; FABRICATED A DOUBLER AND FILLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-10, FIG. Dec 5, 2003 · N174AW · Boeing 73733ASDR AWXA200301589Wedge · delaminatedDURING C-18 CHECK THE NR 5 SLAT OB END UPPER WEDGE TRAILING EDGE SKIN WAS FOUND DELAMINATED AROUND PREVIOUS REPAIR. MAINTENANCE REMOVED PREVIOUS REPAIR AND DELAMINATED SKIN; FABRICATED A DOUBLER AND FILLER; INSTALLED REPAIR PARTS IAW 737-300 SRM 51-70-10, FIG.Dec 5, 2003 · N174AW · Boeing 73733ASDR MWEA030474Slat Track · brokenSLATS WERE RETRACTED, THE AMBER SLAT DISAGREEMENT LIGHT STAYED ON. FOUND SLAT TRACK DOOR AT NUMBER TWO AND NUMBER THREE SLAT JUNCTION BENT AND BROKEN. REMOVED AND REPLACED SLAT TRACK DOOR.Dec 5, 2003 · N202ME · Doug DC932SDR DHL200374247Skin · delaminatedDURING C-CHECK, LEFT HAND INBOARD FORE FLAP UPPER SKIN DELAMINATED AT OUTBOARD END. CUT OUT UPPER SKIN DELAMINATION APPROX 1.7 INCH DIA & DOUBLER APPROX 4 X 4.75 INCH FROM 2024-T3 .016 PO900291. FURTHER EVALATION FOUND 1 PUNCTURE & 1 SHARP DENT ON LOWER SKINDec 4, 2003 · N742 · Piper PA18150SDR 03FDEA02041Fitting · gougedWINGS BASIC- REWORK OF SLIGHT GOUGE IN L/E SLAT ACTUATOR FITTING. COMPLIED WITH ALL ASPECTS OF EA 7-5740-73855.Dec 4, 2003 · N257FE · Boeing 727200SDR AWXA200301634Skin · delaminatedMCN - MAJOR REPAIR - DURING C-18 CHECK THE RIGHT WING NR 4 SLAT WAS FOUND DELAMINATED AT INBOARD LOWER TRAILING EDGE. MAINTENANCE CUT OUT DELAMINATED SECTION OF SKIN AT INBOARD LOWER TRAILING EDGE; FABRICATED REPAIR DOUBLERS; BONDED REPAIR PART TO SLAT SKIN IDec 3, 2003 · N325AW · Boeing 737301SDR AWXA200301633Skin · delaminatedDURING C-18 CHECK THE LT WING NR 3 SLAT WAS FOUND DELAMINATED AT OUTBOARD UPPER TRAILING EDGE, SLAT STA 329.75. MAINTENANCE REMOVED DELAMINATED SECTION OF SKIN AT OUTBOARD UPPER TRAILING EDGE; FABRICATED REPAIR DOUBLERS; BONDED REPAIR PART TO SLAT SKIN IAW B7Dec 3, 2003 · N325AW · Boeing 737301SDR AWXA200301629Wedge · delaminatedMCN - MAJOR REPAIR - DURING C-18 CHECK THE LT WING NR 2 SLAT WAS FOUND DELAMINATED AT OUTBOARD UPPER TRAILING EDGE, SLAT STA 246.27-254.27. MAINTENANCE CUT OUT DELAMINATED SKIN AT OUTBOARD UPPER TRAILING EDGE; FABRICATED REPAIR DOUBLERS; BONDED REPAIR PART TODec 3, 2003 · N325AW · Boeing 737301SDR AWXA200301593Skin · debondedDURING C-18 CHECK FOUND THE NR 2 LEADING EDGE SLAT DISBONDED AT OUTBOARD CORNER. MAINTENANCE CUTOUT DAMAGED AREA NR 2 LEADING EDGE SLAT AT OB CORNER; FABRICATED REPAIR DOUBLERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-10, FIG. 16, PG. 67-69.Dec 2, 2003 · N174AW · Boeing 73733ASDR DHL2003802568Door · crackedRIGHT WING OTBD SLOT UPPER DOOR CRACKED 3.000. REMOVED AND REPLACED UPPER DOOR ON RIGHT WING OTBD SLOT IAW MM 27-80-2 PG 201-203, SRM 51-3-0 PG 1, SRM 51-3-1 PG 2A. FOR OPS CHECK SEE NR 1456.Dec 2, 2003 · N802DH · Doug DC873SDR DHL2003802555Skin · damagedLT OUTER WING CENTER EXTENDED L/E SLOT LWR PLATING ELONGATED HOLES AROUND STA XFS 526.000 (MAJOR REPAIR). REMOVED FASTENERS. TRIMMED OUT THE DAMAGED SKIN AREA IAW ED EDU38-2 AND DWG U38-R02. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06,10-01-001. CLEANDec 1, 2003 · N802DH · Doug DC873SDR DHL2003802556Skin · damagedRIGHT WING EXTENDED L/E INBD VANE FWD OUTER PLATING ELONGATED HOLES AROUND STA XS 247.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW ED EDU38-3 AND DWG U38-R03. REMOVED FASTENERS, TRIMMED OUT THE DAMAGED SKIN AREA. PERFORMED NDT INSPECTION. CLEANED, TREATENov 30, 2003 · N802DH · Doug DC873SDR DHL2003802554Skin · damagedELONGATED HOLES IN RT WING EXTENDED L/E INBD VANE FORWARD PLATING AROUND STA XILD 7095 (MAJOR REPAIR). REMOVED FASTENERS. TRIMMED OUT THE DAMAGED SKIN AREA. PERFORMED NDT INSPECTION. CLEANED, TREATED AND PRIMED AREA. FABRICATED AND EXTERNAL REPAIR DOUBLERNov 30, 2003 · N802DH · Doug DC873SDR DHL2003802574Rib · damagedRIGHT OUTBD STUB WING RIB HOLES ELONGATED STA XOLDO 67.750 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, ATM 201846, DWG 9753297. REMOVED DAMAGED RIB IAW SRM 51-3-0 PG 1, SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. FABRICATED RIB IAW ATM 201846, DWGNov 28, 2003 · N802DH · Doug DC873SDR 03FDEA02112Hinge · corrodedLT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD HOLE SPOT FACE CORRODED. LT WING OUTBD FLAP INBD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD HOLE SPOT FACE CORROSION REMOVED AS PER EA 1-5750-73348, WINGS - TRAILING EDGE AND TNov 28, 2003 · N608FE · Doug MD11SDR DHL2003742560Mount Bracket · crackedDURING C-CHECK, NR 2 SLAT INBD TRACK UPPER MOUNT INBD L-ANGLE IS CRACKED. REMOVED DAMAGED ANGLE AND FABRICATED NEW FROM BAC1505-100617 PO 900411 DIM 9.25 X 1.25 INCH AS PER SAMPLE IAW 727 SRM 57-10-2 FIG 3. NEW ANGLE TREATED AND PRIMED IAW 727 SRM 51-10-2, Nov 25, 2003 · N742DH · Boeing 727225SDR DHL2003742558Rib · crackedDURING C-CHECK, NR 4 SLAT HAS SEVERAL CRACKS IN RIB INBD SIDE OF THE ACTUATOR, VIEWED THRU THE ACCESS HOLE. REMOVED DAMAGED RIB & INSTALLED NEW, P/N 65-17276-9 PO 3348104 IAW 727 SRM 51-30-2. REMOVED AND REPLACED THE NR 4 SLAT FOR STRUCTURAL ACCESS IAW B727 Nov 25, 2003 · N742DH · Boeing 727225SDR DHL200374260Mount Bracket · crackedDURING "C" CHECK, NR 2 SLAT IB TRACK UPPER MOUNT IB (L) ANGLE IS CRACKED; CA: REMOVED DAMAGED ANGLE AND FABRICATED NEW FROM BAC1505-100617 PO NR 900411 DIM. 9.2500 X 1.2500 IAW SAMPLE IAW 727 SRM57-10-2 FIG.3 NEW ANGLE TREATED AND PRIMED IAW 727 SRM51-10-2,INov 25, 2003 · N742DH · Boeing 727225SDR DHL200374258Rib · crackedDURING "C" CHECK, NR 4 SLAT HAS SEVERAL CRACKS IN RIB IB SIDE OF THE ACTUATOR, VIEWED THRU THE ACCESS HOLE. CA: REMOVED DAMAGED RIB AND INSTALLED NEW, PN 65-17276-9 PO NR 3348104 IAW 727 SRM 51-30-2, REMOVED AND REPLACED THE NR 4 SLAT FOR STRUCTURAL ACCESS IANov 25, 2003 · N742DH · Boeing 727225SDR DHL200342538Bracket · crackedDURING C-CHECK, NR 6 KRUEGER FLAP INBOARD ACT MOUNT CRACKED 2 PLACES. REMOVED SUPPORT BRACKETS IAW B727 SRM 51-30-02, FABRICATED AT 2 EA SUPPORT BRACKETS, 7075-T6 .063 PO 900226 PER SAMPLE DIM 3.5 X 7 INCHES IAW B727 SRM 57-20-02. ALODINED AND PRIMED IAW B72Nov 24, 2003 · N742DH · Boeing 727225SDR DHL200342540Mount · crackedDURING C-CHECK; N/R60111 NR 5 KRUEGER FLAP ACT MOUNT IS CRACKED INBD 2 PLACES, OTBD 1 PLACE. REMOVED NR 5 L/E FLAP ACT SUPPORT BRACKETS IAW B727 SRM 51-30-02, FABRICATED PER SAMPLE I/B & O/B SUPPORT BRACKETS 7075-T6, .063 PO900226 (6 X 8 INCH) IAW B727 SRM 57Nov 24, 2003 · N742DH · Boeing 727225SDR UIEA200300070Skin · bird strikeRIGHT INBOARD FLAP FOREFLAP DAMAGE. BIRD STRIKE ON RIGHT WING L/E FLAPS. PERFORMED INSPECTION PER MM 5-51-14, FOUND RIGHT INBOARD FLAP FOREFLAP DAMAGED OUT OF SRM LIMITS. REMOVED FLAP AND REPAIRED IAW SRM 51-70-07 AND MM 57-52-31. INSTALLED FLAP AS EPR MM Nov 24, 2003 · N415MC · Boeing 74747UFSDR DHL2003742515Skin · crackedDURING C-CHECK, NR 5 SLAT OUTBOARD HOOK CUTOUT IN UPPER L/E SKIN AFT OUTBOARD CORNER IS CRACKED. REMOVED PAINT AT AFFECTED AREA IAW MM 51-20-1 AND STOP DRILLED CRACK IAW SRM 51-10-1 HFEC VERIFIED STOP DRILL IAW B-727 NDT MM PT 6 51-00-00 FIG 23. FABRICATED PNov 24, 2003 · N742DH · Boeing 727225SDR 03FDEA01962Structure · corrodedRT OUTBOARD FLAP FOUND VANE TO TRACK ATTACHMENT NR 5 WITH SLOT CORRODED AS MARKED. RT OUTBOARD FLAP VANE TO TRACK ATTACHMENT NR 5 CORROSION REPAIRED AS PER FEDEX EA 1-5750-74257, WING RT OUTBOARD FLAP NR 5 FITTING SUPPORT VANE TO TRACK CORROSION.Nov 21, 2003 · N583FE · Doug MD11
Back to JASC 5754