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 05FDEA00228Slat Track · wornM-TYPE-MOD 716-27-80-0264, NR 8 SLAT TRACK HAS SIDE ROLLER WEAR SPOTS. BLENDED AND POLISHED TRACK ROLLER WEAR SPOTS FOUND ONE AREA OUT OF ALLOWABLE DAMAGE LIMITS IAW A-300 SRM 57-40-00 3.A.(3)(D). THE TRACK MAYBE RETURNED TO SERVICE PROVIDED THE AREA IS INSFeb 2, 2005 · N716FD · Airbus A300B4622SDR SWAA050274Skin · debondedDURING SCHEDULED C4 CHECK, FOUND LT WING NR 2 L/E SLAT DISBONDED. REMOVED AND REPLACED NR 2 L/E SLAT PER MM.Feb 1, 2005 · N617SW · Boeing 7373H4SDR SWAA050272Skin · delaminatedDURING SCHEDULED SERVICE CHECK, FOUND RT WING NR 4 L/E SLAT DELAMINATED. REMOVED AND REPLACED NR 4 L/E SLAT PER MM.Feb 1, 2005 · N507SW · Boeing 7375H4SDR AWXA200500226Skin · delaminatedMCN - MAJOR REPAIR - DURING C-18 CHECK THE UPPER SURFACE SKIN OF THE NR 2 SLAT WAS FOUND DELAMINATED AT THE OUTBOARD END, SLAT STA 251. MAINTENANCE CUT OUT DAMAGED AREA OF UPPER NR 2 SLAT SKIN FROM SS 249.77 TO SS 254.27; FABRICATED A CORE FILLER AND EXTERNALJan 31, 2005 · N326AW · Boeing 737301SDR 05FDEA00197Skin · damagedCOMPLY WITH EA 8-5710-55426 WINGS - BASIC, LT, LEADING EDGE NR 7 SLAT SKIN REPAIR AT XOS=947.65. COMPLIED WITH EA 8-5710-55426.Jan 29, 2005 · N363FE · Doug MD1010FSDR AWXA200500243Skin · crackedDURING C-16 CHECK 4 EACH .25 INCH CRACKS WERE FOUND AT FASTENER HOLES ON LOWER NR 2 SLAT SKIN. MAINTENANCE FASTENERS AND PREVIOUS REPAIR IN LOWER NR 2 SLAT SKIN FROM SLAT STA 158.5 T0 SLAT STA 165; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REPAIR PARTSJan 28, 2005 · N303AW · Boeing 7373G7SDR 0500145523Skin · crackedDURING H-CHECK FOUND CRACKED COVE SKIN PANELS AT NR 9 LEADING EDGE SLAT OUTBOARD DRIVE TRACK. REPAIRED PER EA 55-202250.Jan 25, 2005 · N523US · Boeing 757251SDR SWAA050185Attach Fitting · crackedDURING SCHEDULED D-CHECK, FOUND LT WING L/E NR 3 SLAT ACTUATOR ATTACH FITTING CRACKED. REPAIRED SLAT FITTING PER SRM.Jan 24, 2005 · N602SW · Boeing 7373H4SDR ASAA0540046Skin · crackedOKC - NR3 SLAT LOWER SKIN CRACKED AT FASTENER OB END .6 INCHES LONG. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IAW SRM. (K)Jan 23, 2005 · N771AS · Boeing 7374Q8SDR ASAA0540045Skin · crackedOKC - NR 2 SLAT LOWER SKIN CRACKED 2 PLACES IB END AT FASTENER (.73 INCH LONG) AND CENTER (1.6 INCHES LONG). REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IAW SRM. (K)Jan 23, 2005 · N771AS · Boeing 7374Q8SDR AWXA200500225Skin · delaminatedMCN - MAJOR REPAIR - DURING C-18 CHECK THE LOWER SURFACE SKIN OF THE NR 3 SLAT WAS FOUND DELAMINATED AT SLAT STA 14.5. MAINTENANCE REMOVED PREVIOUS REPAIR AND DAMAGED AREA OF LOWER NR 3 SLAT SKIN; FABRICATED A CORE FILLER AND EXTERNAL DOUBLER; BONDED REPAIR PJan 21, 2005 · N326AW · Boeing 737301SDR 05FDEA00138Hinge · corrodedLEFT WING INBOARD FLAP HINGE INBOARD PIVOT BUSHING GALLED AND PITTED. MEASURED BORE DIAMETER, FOUND TO BE OUT OF LIMITS IAW DAC CMM 57-52-01, ALODINE AND PRIMED BORE IAW DC10-10 SRM 51-21-01 VOL 2, FABRICATED, INSTALLED AND HONED BUSHING TO A FINAL INSIDE DIAJan 21, 2005 · N395FE · Doug DC10SDR ASAA0540037Wedge · delaminatedOKC - RT WING NR 5 LE SLAT TRAILING EDGE WEDGE HAS SMALL AREA OF DELAMINATION AND DETERIORATED EDGE POTTING ON OB EDGE. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER AND REPORTED IAW SRM. (K)Jan 18, 2005 · N771AS · Boeing 7374Q8SDR UPS05243707Skin · crackedINSPECTION TYPE: C, LE SLAT ACCESS PANEL (NR 6 SLAT) HAS 1/2 INCH CRACK ON SKIN. REPAIR CARRIED OUT IAW SRM 51-10-01, 51-40-02 AND 51-30-02.Jan 13, 2005 · N940UP · Boeing 727185CSDR 05FDEA00084Skin · warpedLEFT WING, NR 5 SLAT LEADING EDGE SURFACE IS EXCESSIVELY WARPED THE ENTIRE WIDTH DUE TO TOO MUCH HEAT. LT WING NR 5 SLAT REMOVED AND REPLACED.Jan 12, 2005 · N384FE · Doug MD11SDR USAA050064Skin · delaminatedPIT - FOUND TOP SKIN CORE BOND DELAMINATED 2.5 INCH BY 2.5 INCH AREA, NR 3 SLAT INBOARD TRAILING EDGE. REMOVED DAMAGED SKIN AND CORE, INSTALLED NEW CORE, DOUBLERS PER SRM 51-70-10. (M)Jan 11, 2005 · N374US · Boeing 7373B7SDR UPS05243698Rib · crackedINSPECTION TYPE: C, NR 8 LE SLAT STRUCTURE HAS CRACKED RIB JUST O/B OF ACTUATOR ATTACH POINT. REPAIR CARRIED OUT IAW SRM 57-50-03.Jan 11, 2005 · N940UP · Boeing 727185CSDR UPS05243697Rib · crackedINSPECTION TYPE:C NR 5 LE SLAT STRUCTURE HAS THREE RIBS CRACKED BETWEEN O/B TRACK AND O/B EDGE OF SLAT. REPAIRED CRACKED RIBS 3 PLACES AT NR 5 LE SLAT IAW SRM 57-50-03 FIG 9.Jan 11, 2005 · N940UP · Boeing 727185CSDR UPS05243687Hook · crackedINSPECTION TYPE:C SUSPECT CRACK ON NR 2 SLAT O/B HOOK UPPER FASTENER. HFEC CARRIED OUT IAW NDTM 51-00-00 FIG 4. RESULT - CRACK CONFIRMED. REPAIR CARRIED OUT IAW SRM 57-50-3 FIG 10.Jan 11, 2005 · N940UP · Boeing 727185CSDR USAA050006Skin · crackedCLT - FOUND SLAT SKIN CRACKED 1 INCH, LOWER TRAILING EDGE OF SKIN, 6 INCHES OUTBOARD OF ACTUATOR ON THE NR 4 LE SLAT. INSTALLED DOUBLER. (M)Jan 10, 2005 · N574US · Boeing 737301SDR UPS05243686Bracket · crackedINSPECTION TYPE:C, NR 1 KRUEGER FLAP TRUNNION BRACKET IS CRACKED ON O/B SIDE. BRACKET REPLACED IAW DRG 65-16275.Jan 10, 2005 · N940UP · Boeing 727185CSDR USAA050063Skin · delaminatedPIT - FOUND TOP SKIN CORE BOND DELAMINATED 3 INCHES BY 3 INCHES, NR 5 SLAT OUTBOARD TRAILING EDGE. REMOVED DAMAGE, INSTALLED NEW CORE, FILLERS, DOUBLERS PER SRM 51-70-10. (M)Jan 7, 2005 · N514AU · Boeing 7373B7SDR UPS05243710Casting · corrodedINSPECTION TYPE:C, NR 3 KRUEGER FLAP INBOARD HINGE, FIXED LEADING EDGE CASTING HAS EVIDENCE OF INTERGRANULAR CORROSION. REPLACED AND INSTALLED NEW CASTING IAW DRG 64-8343.Jan 7, 2005 · N940UP · Boeing 727185CSDR ASMF200501004Skin · damagedDURING TRANSIT CHECK WERE DETECTED FUEL PANEL AND SLAT NR 2 DAMAGED. INSPECTION WAS PERFORMED AND DAMAGES WERE DETECTED OUT OF LIMITS, THEREFORE AIRCRAFT WAS SENT TO THE HANGAR. SLAT NR 2 AND FUEL PANEL WERE REPLACED IAW MM 27-80-01 AND 57-30-03, RESPECTIVELJan 7, 2005 · N205AM · Doug DC987SDR AWXA200500028Wedge · delaminatedMCN - MAJOR REPAIR - DURING C-17 CHECK A DISBOND AREA WAS FOUND IN NR 5 SLAT WEDGE ON UPPER SURFACE AT INBOARD END BETWEEN SS 131.50 AND SS 132.50. MAINTENANCE CUT OUT DAMAGE IN NR 5 SLAT WEDGE AT UPPER INBOARD END; FABRICATED A FILLER AND DOUBLER; BONDED REPJan 6, 2005 · N327AW · Boeing 7373Q8SDR AWXA200500154Wedge · delaminatedMCN - MAJOR REPAIR - DURING C-18 CHECK, FOUND THE A PREVIOUS REPAIR ON UPPER INBOARD END OF NR 4 SLAT WEDGE DELAMINATED BETWEEN SLAT STA 12.25 AND 16.25. MAINTENANCE REMOVED DAMAGED SKIN ON UPPER INBOARD END OF NR 4 SLAT WEDGE; FABRICATED A FILLER AND REPAIR Jan 5, 2005 · N156AW · Boeing 7373G7SDR USAA050198Skin · delaminatedPIT - FOUND TOP SKIN CORE BOND DELAMINATED 2.5 INCH BY 1.5 INCH AREA, NR 3 SLAT TOP SURFACE OUTBOARD T/E. BONDED IN NEW CORE, BOND ON TOP DOUBLER PR SRM 51-70-10. (M)Jan 4, 2005 · N426US · Boeing 7374B7SDR AWXA200500139Wedge · delaminatedMCN - MAJOR REPAIR - DURING C-18 CHECK, THE LOWER SURFACE OF NR 1 SLAT WEDGE WAS FOUND DELAMINATED FROM SLAT STA 358 TO 369. MAINTENANCE REMOVED DAMAGE FROM LOWER SURFACE OF NR 1 SLAT WEDGE; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW B737-300Jan 4, 2005 · N156AW · Boeing 7373G7SDR SWAA050025Structure · delaminatedDURING SCHEDULED C4 CHECK, FOUND RT WING NR 4 L/E SLAT DELAMINATED. REMOVED AND REPLACED NR 4 L/E SLAT PER MM.Jan 4, 2005 · N527SW · Boeing 7375H4SDR 05FDEA00019Rib · crackedSECOND INBOARD RIB IS CRACKED IN LEADING EDGE OF NR 5 SLAT. REMOVED AND REPLACED RIB IAW SRM 51-10-1.Jan 4, 2005 · N151FE · Boeing 727100SDR LCQ18Skin · chafedNR 2 L/E SLAT UPPER T/E LOWER SURFACE CHAFING NEAR ACTUATOR AND O/B ENDJan 4, 2005 · N943UA · Boeing 737SDR 05FDEA00009Slat Track · crackedLEFT HAND WING, SLAT TRACK NR 16 INBOARD RIB FOUND CRACKED. REMOVED AND REPLACED PER SRM 51-33-01 AND SRM 51-35-01. NR 16 SLAT TRACK ADJUSTMENT AND TEST CARRIED OUT PER AMM 27-80-00-2. OUTBOARD SLAT OPERATIONAL TEST CARRIED OUT PER AMM 27-80-00-5.Jan 3, 2005 · N605FE · Doug MD11SDR 05FDEA00006Skin · damagedLT WING, NR 2 SLAT EXTERIOR, FOUND 2EA DOUBLER REPAIR AND 1EA CUTOUT REPAIR. REMOVED AND REPLACED AS PER AMM 27-80-20 AND FUNCTIONAL CHECK CARRIED OUT AS PER AMM 27-80-00, FOUND SATISFACTORY.Jan 3, 2005 · N577FE · Doug MD11SDR USAA050206Skin · crackedPIT - FOUND SLAT CRACKED .5 INCH, FORWARD OF INBOARD AUX TRACK LOWER SURFACE AFT FASTENER. INSTALLED DOUBLER PER SRM 57-43-01 FIG 206. (M)Jan 1, 2005 · N436US · Boeing 7374B7SDR USAA050176Skin · chafedPIT - FOUND LOWER SKIN SURFACE WITH CHAFE DAMAGE, 1.5 INCH BY 2.5 INCH, NR 2 SLAT INBOARD CORNER AND OUTBOARD CORNER LOWER SURFACE. (M)Jan 1, 2005 · N521AU · Boeing 7373B7SDR USAA050170Skin · bentPIT - FOUND SLAT EXT SKIN BENT AREA 3.5 INCH BY 1.5 INCH AREA, NR 1 SLAT UPPER T/E SURFACE INBOARD END. REMOVED DAMAGED AREA, INSTALLED FILLER AND INTERNAL DOUBLER PER SRM 51-70-10. (M)Jan 1, 2005 · N522AU · Boeing 7373B7SDR USAA050168Skin · delaminatedPIT - FOUND TOP SKIN/CORE BOND DELAMINATED 3 INCHES BY 2 INCHES AREA, NR 3 SLAT INBOARD T/E. REMOVED DELAMINATED TOP SKIN AND CORE MATERIAL, BONDED IN NEW CORE, INSTALLED TOP DOUBLER PER SRM 51-70-10. (M)Jan 1, 2005 · N521AU · Boeing 7373B7SDR USAA050053Skin · crackedPIT - FOUND NR 1 SLAT WITH .125 INCH CRACKS ON 6 RIVET HOLES, CENTER OF SLAT BY ACTUATOR MOUNT LOWER SKIN. INSTALLED DOUBLER PER SRM 57-43-01 FIG 206. (M)Jan 1, 2005 · N522AU · Boeing 7373B7SDR USAA050068Panel · delaminatedPIT - FOUND PANEL DELAMINATED, INBOARD AND OUTBOARD ENDS OF NR 5 SLAT PANEL. INSTALLED DOUBLER PER SRM 51-70-10. (M)Jan 1, 2005 · N522AU · Boeing 7373B7SDR USAA050051Skin · crackedPIT - FOUND NR 3 SLAT CRACKED .125 INCH, LOWER SURFACE AT MID SPAN RIVET HOLE. INSTALLED DOUBLER PER SRM 57-43-01 FIG 206. (M)Jan 1, 2005 · N522AU · Boeing 7373B7SDR USAA050069Skin · delaminatedPIT - FOUND SLAT DELAMINATED 4 INCHES BY 6 INCHES, NR 3 SLAT. REMOVED TOP SKIN CORE AND DAMAGE, INSTALLED FILLER, DOUBLER PER SRM 51-70-09. (M)Jan 1, 2005 · N522AU · Boeing 7373B7SDR USAA050160Skin · crackedPIT - Q6 - NR 6 SLAT, .5 INCH CRACK; LOWER SKIN AFT ROW RIVET 4 INCHES FROM OB END; INSTALLED DOUBLER IAW SRM. (K)Jan 1, 2005 · N521AU · Boeing 7373B7SDR USAA050156Skin · crackedPIT - Q6 - NR 1 SLAT, 1 INCH CRACK; LOWER SKIN AFT ROW RIVETS AT NR 2 AUX TRACK. INSTALLED DOUBLER IAW SRM. (K)Jan 1, 2005 · N521AU · Boeing 7373B7SDR USAA050112Skin · delaminatedPIT - Q6 - SKIN, 6.5 INCH X 4.5 INCH AREA DELAMINATION; NR 5 SLAT OB END; REMOVED TOP SKIN AND CORE AND REPLACED IAW SRM. (K)Jan 1, 2005 · N517AU · Boeing 7373B7SDR USAA050111Skin · delaminatedPIT - Q6 - SKIN, 4 INCH X 4 INCH AREA DELAMINATION; NR 5 SLAT IB END; REMOVED TOP SKIN, CORE, REPLACED CORE AND TOP SKIN IAW SRM 57-70-10. (K)Jan 1, 2005 · N517AU · Boeing 7373B7SDR USAA050110Skin · delaminatedPIT - Q6 - SKIN, 4 INCH X 4 INCH AREA DELAMINATION; NR 2 SLAT, OB END; REMOVED TOP SKIN, CORE, REPLACED CORE, TOP SKIN IAW SRM 51-70-10. (K)Jan 1, 2005 · N517AU · Boeing 7373B7SDR USAA050109Skin · delaminatedPIT - Q6 - SKIN - CORE, 4 INCH X 4 INCH DELAMINATION, NR 2 SLAT IB END. REMOVED DAMAGE, INSTALLED INTERNAL DOUBLER, CORE, TOP EXT DOUBLER IAW SRM 51-70-10. (K)Jan 1, 2005 · N517AU · Boeing 7373B7SDR USAA050107Structure · crackedPIT - Q6 - NR 2 SLAT, .1250 INCH CRACKS (3 EA); LOWER T CHORD AFT ROW OF FASTENERS AT ACTUATOR MOUNT; INSTALLED DOUBLER IAW SRM 57-43-01, FIG 206. (K)Jan 1, 2005 · N517AU · Boeing 7373B7SDR USAA050095Structure · crackedPIT - Q6 - NR 1 SLAT, .1250 INCH CRACKS-2 EA; LOWER T-CHORD, AFT ROW OF FASTENERS, APPROX 40 INCHES FROM IB EDGE. INSTALLED DOUBLER IAW SRM. (K)Jan 1, 2005 · N517AU · Boeing 7373B7SDR USAA050093Skin · crackedPIT - Q6 - RIVET HOLES, .1250 INCH TO .2500 INCH - 7 RIVET HOLES, CRACKED; LWR SKIN AFT FASTENER ROW CENTERED ON SLAT ACT. AREA. INSTALLED DOUBLER IAW SRM 57-43-01.(K)Jan 1, 2005 · N517AU · Boeing 7373B7
Back to JASC 5754