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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR UPS06146132Rib · crackedRT WING KRUEGER FLAP WELL HAS RIB CRACKED APPROX 1.5" IN LOWER RADIUS. REMOVED AND REPLACED RIB PER A300 SRM 51-40-00.SDR 06FDEA0446Doubler · crackedRIGHT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT XORS 542. REPAIR CARRIED OUT AT CRACK FOUND AT RIGHT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER AT XORS 542 AS PER FEDEX EA 1-5730-90735, TITLE: WING - LEADING EDGE BEADED DSDR 06FDEA0444Doubler · crackedLEFT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT XORS 528. REPAIR CARRIED OUT AT CRACK FOUND AT LEFT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER AT XORS 528 AS PER FEDEX EA 1-5730-90733, TITLE: WING - LEADING EDGE BEADED DOUSDR 06FDEA0443Doubler · crackedLEFT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT XORS 520. REPAIR CARRIED OUT AT CRACK FOUND AT LEFT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER AT XORS 520 AS PER FEDEX EA 1-5730-90733, TITLE: WING - LEADING EDGE BEADED DOUSDR USAA060161Skin · wornFOUND LEADING EDGE WORN AREA OUTBOARD MID FLAP AT INBOARD END OF LEADING EDGE SKIN. REMOVED DAMAGE, FABRICATED AND INSTALLED FILLER IAW SRM 57-53-01 REPAIR 7, DEFECT SIZE: 3.5" BY .25".SDR WRNA200600021Rib · damagedDURING INSPECTION, DAMAGE WAS FOUND ON RT WING NR 3 SLAT INBOARD END AT RIB 3 LEADING EDGE. REPAIRED PER AVBORNE REPAIR REFERENCE 25599-8-01-06, (AIRBUS TECHNICAL DISPOSITION #FOK/036/2006) CUT OUT DAMAGED AREA, MODIFIED NOSE RIB 3, MANUFACTURED AND INSTALLEDSDR PIDA06012Skin · crackedNUMBER 6 SLAT HAS A CRACK BETWEEN FASTENERS ON THE LOWER SKIN JUST I/B OF THE I/B AUX TRACK. REPAIRED PER SRM 57-43-01.SDR PIDA06011Skin · crackedNUMBER 5 SLAT HAS A CRACK BETWEEN FASTENERS ON THE LOWER SKIN. REPAIRED PER SRM 57-43-01.SDR PIDA06010Skin · crackedNUMBER 1 SLAT HAS A CRACK BETWEEN SIX FASTENERS ON THE LOWER SKIN JUST BELOW THE ACTUATOR. REPAIRED PER SRM 57-43-01.SDR IXXA06SMN059SPan · crackedDURING ROUTINE C CHECK INSPECTION, RT WING CTR L/E, ZEE-PAN CRACKED 1" AT STA XS 526.000. REMOVED CRACKED ZEE PAN IAW DC8 SRM 51-1-20D ATI REPAIR SPECIFICATION NR 2003-05, DWG DOUGLAS NR 5769 857. PERFORMED HEAT TREATMENT IAW DC8 SRM 51-1-1 PAGES 1, 13, 17. SDR DHL2006804512Bracket · crackedLEFT WING OUTBOARD SLOT MECHANISM NR 8 BRACKET CRACKED. REMOVED AND REPLACED BRACKET NR 8 FROM LT OUTBOARD SLOT MECHANISM IAW MM 20-16-0 PG 201-202, 207. REFER TO NR 044174 FOR OPS CHECK.SDR 06FDEA0375Flap · corrodedNR 5 K-FLAP HAS CORROSION AT OB BULLNOSE TO K-FLAP BONDING WIRE BOTH ATTACH POINTS. REPAIRED NR 5 K FLAP BULLNOSE PER SR DRAWING SR 27-57-010 REV C.SDR USAA060136Skin · wornLEADING EDGE SKIN OF MIDFLAP AT INBOARD END WORN. FABRICATED AND INSTALLED DOUBLER IAW SRM 57-53-01 REPAIR 8, DEFECT SIZE: 8 X 4 INCHES.SDR SWAA060253Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND RT WING NR 5 L/E SLAT DELAMINATED AT OUTBOARD END. REPAIRED SLAT PER SRM.SDR USAA060116Skin · crackedOUTBOARD END OF NR 6 SLAT, LOWER, TRAILING EDGE SKIN CRACKED. REMOVED DAMAGED, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 57-43-01, DEFECT SIZE: 1.5 INCH.SDR QXEA200600323Skin · chafedYYC - C3 RIGHT HAND LEADING EDGE PANEL 631AR HAS CHAFE MARK FROM SLAT. REPAIRED IAW CRJ700/900 SRM 51-12-00-001-001-A01, SRM 57-41-01-101-001-A01 AND SRM 51-25-16-001-001-A01.SDR QXEA200600322Skin · chafedYYC - C3 RIGHT HAND LEADING EDGE PANEL 622BR HAS CHAFED MARK FROM SLAT. REPAIRED IAW CRJ700/900 SRM 51-12-00-001-001-A01, SRM 57-41-01-101-001-A01 AND SRM 51-25-16-001-001-A01.SDR QXEA200600321Skin · chafedYYC - C3 RIGHT HAND LEADING EDGE PANEL 622AR HAS CHAFED MARK FROM SLAT. REPAIRED IAW CRJ700/900 SRM 51-12-00-001-001-A01, SRM 57-1-01-101-001-A01 AND SRM 51-25-16-001-001-A01.SDR QXEA200600301Skin · chafedYYC - C3 LEFT HAND WING, MID SECTION LEADING EDGE PANEL 522BL FROM SS144.94 TO SS249.04 NUMEROUS CHAFE MARKS ON SKIN. REPAIRED IAW CRJ700/900 SRM 51-12-00-001-001-A01, SRM 51-25-01-001-001-A01 AND SRM 57-41-01-101-001-A01.SDR QXEA200600302Skin · chafedYYC C3 LEFT HAND WING, LEADING EDGE 531AL PANEL FROM SS249.04 TO SS337.66 NUMEROUS CHAFE MARKS. REPAIRED IAW CRJ700/900 SRM 51-12-00-001-001-A01 AND SRM 51-25-01-001-001-A01.SDR QXEA200600300Skin · chafedYYC - C3 LEFT HAND WING, INBOARD LEADING EDGE SKIN PANEL FROM SS 57.00 TO SS 144.00 (522AL) NUMEROUS CHAFE MARKS ON SKIN. REPAIRED IAW CRJ700/900 SRM 51-12-00-001-001-A01 AND SRM 51-25-01-001-001-A01.SDR AWXA200600269Skin · crackedMCN - DURING C19 DISCOVERED 9 CRACKS, 1.0 INCHES IN LENGTH, ON THE BOTTOM OF THE NR 2 SLAT SKIN OUTBOARD OF THE INBOARD AUXILARY TRACK, BELOW THE OUTBOARD MAIN TRACK, AND BELOW THE OUTBOARD AUXILARY TRACK FROM SLAT STATION (SS) 164L TO SS 248L. MAINTENANCE CUSDR AWXA200600268Skin · crackedMCN - DURING C19 DISCOVERED 4 CRACKS, 1.0 INCHES IN LENGTH, ON THE BOTTOM OF THE NR 6 SLAT SKIN BELOW THE OUTBOARD MAIN TRACK AND BELOW THE OUTBOARD AUXILIARY TRACK FROM SLAT STATION (SS) 322R TO SS 356R. MAINTENANCE CUT OUT AND REMOVED DAMAGED PART OF LOWER SDR USAA060057Skin · delaminatedFOUND NR 1 SLAT DELAMINATION UPPER OTBD END OF T/E WEDGE. REMOVED DAMAGE, INSTALLED CORE AND DOUBLER IAW SRM 51-70-10, DEFECT SIZE: 4.750" BY 5.250".SDR USAA060059Skin · delaminatedFOUND SLAT DELAMINATION RT WING NR 5 LE SLAT OUTBD END. INSTALLED DOUBLER IAW SRM 51-70-10, DEFECT SIZE: 1 INCH DELAMINATION.SDR USAA060064Structure · crackedFOUND SLAT CRACKED OTBD END, LOWER SURFACE AT AFT FASTENER ROW, 3.5" BY 8" DOUBLER ON OUTBD END INSTALLED IAW SRM 57-43-01 AND 57-56-22, DEFECT SIZE: APPROX TOT ACCUMULATIVE LENGTH 0.375".SDR USAA060037Wedge · unknownFABRICATED DOUBLER THAT MEASURES 3" BY 5" IAW 57-42-02, NR 2 SLAT UPPER O/B T/E WEDGE SURFACE, DEFECT SIZE: 3" BY 5".SDR USAA060039Wedge · unknownUPPER I/B T/E WEDGE SURFACE, FABRICATED DOUBLER THAT MEASURES 3" BY 5" IAW 57-42-01, DEFECT SIZE: 3" BY 5".SDR USAA060055Skin · delaminatedFOUND DELAMINATION UPPER OTBD END OF T/E WEDGE. REMOVED DAMAGE INSTALLED CORE AND DOUBLER IAW SRM 51-70-10, DEFECT SIZE: 4.750" BY 5.250.SDR USAA060043Skin · crackedFOUND NR 1 SLAT CRACKED, FASTENER HOLES LOWER SURFACE T/E. INSTALLED EXTERNAL DOUBLER IAW BOEING SRM 57-43-01, DEFECT SIZE: .050".SDR USAA060048Skin · crackedFOUND NR 1 SLAT CRACKED, FASTNER HOLE LOWER SURFACE T/E. INSTALLED EXTERNAL DOUBLER IAW SRM 57-43-01, DEFECT SIZE: .050".SDR AALA20060105Skin · crackedAFW - NUMBER EIGHT SLAT LEADING EDGE SKIN INBOARD EDGE HAD SMALL CRACK AT STATION OSS418.426. AREA IS 1 11/16 INCH BY 15/16 INCH AND 1 AND 11/16 INCHES LONG. CUTOUT DAMAGE. INSPECT CUTOUT EDGES FOR CRACKS. ENSURE CUTOUT DOES NOT EXCEED CONDITION DESCRIPTION.SDR DHL2006804501Frame · crackedRIGHT WING OUTBOARD L/E UPPER FORMER CRACKED 0.250" XFS 741.250. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-20D. FABRICATED (2EA) ANGLE DOUBLER (AL7075T6 0.032") IAW SRM 57-2-0 PG 9-10. PERFORMED STOP HOLE IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMSDR IXXA06SMN040SSkin Panel · corrodedDURING ROUTINE C-CHECK INSPECTION, OUTBOARD OUTER L/E CORRODED XFS 710.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-1 FIG 38, TR 5785 DATED 11-22-00. REMOVED CORROSION IAW DC8 SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW DC-8 SRM 57-2-1 FIG 2G. REMOVED SDR DHL2006752513Rib · crackedFOUND NR 111076; NR 2 SLAT, RIB 7 SLAT STA 190 IS CRACKED. REMOVED DAMAGED PART IAW B727 SRM 51-30-2 AND FABBED NEW RIB AREA NR 2 SLAT RIB 7 SLAT STA 180 DIM 16 X 5 INCH MAT USED 7075.0:0.40 PO 9001602 IAW B727 SRM 57-50-2 FIG 2 & 51-20-1. PART TREATED AND PSDR AWXA200600307Skin · crackedMCN - DURING C24 CHECK DISCOVERED 6 CRACKS, .189 INCHES LONG, ON THE BOTTOM OF THE NR 4 SLAT SKIN BELOW THE OUTBOARD AUXILIARY TRACK FROM SS 80R TO SS 100R. MAINTENANCE REMOVED DAMAGED AREA OF SKIN ON THE NR 4 SLAT IAW BOEING 737-300 SRM 57-43-01-2R6. FABRICSDR DHL2006752512Skin · crackedNR 2 SLAT RIB NR 1 AT SLAT STA 234.0 IS CRACKED. REMOVED DAMAGED PART IAW B727 SRM 51-30-2 AND FABBED NEW RIB AREA NR 2 SLAT RIB NR 1 SLAT 180 DIM 16 BY 5 MAT USE 7075.0 0.40 PO 9001602 IAW B727 SRM 57-50-2 FIG NR 2 AND 51-20-1 PART TREATED AND PRIMED IAW B7SDR DL764060041Bolt · missingLE SLAT ASYM MSG WHILE EXTENDING FLAPS TO 15 AFTER ENG START. FOUND SLAT 9 INBD TARGET MISSING. REPLACED SAME PER M/M. OPS CK NML.SDR 06FDEA0178Skin · damagedPDIS: AFTER LANDING IN NARITA, THE MECHANIC AND THE NEW BOARDING OUTBOUND CREW REPORTED A HOLE IN THE LEADING EDGE OF THE LEFT SLAT OUTBOARD OF NUMBER ONE ENGINE. THE AIRPLANE FLEW AND FELT FINE ON A HAND FLOWN APPROACH TO 34L. PANEL MISSING ON OUTBOARD NR 1SDR DHL2006804500Support Angle · crackedRIGHT WING INBOARD L/E UPPER SUPPORT ANGLE CRACKED 2 INCHES, STA XFS 7.500. REMOVED CRACKED ANGLE IAW SRM 51-3-0. FABRICATED NEW ANGLE (AL7075T6 0.080") IAW SRM 57-2-0 PG 1. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW ANGLE IAW SRM 51-3-0. SDR DL764060037Washer · missingON TAXI OUT FLAPS AT 5 GOT L/E SLAT ASYM, RTB. FOUND NR 8 SLAT INBOARD TARGET/WASHER ASSY MISSING. REPLACED TARGET ASSY PER MM.SDR 2006FA0000128Plate · crackedSEAL CLAMPING PLATE IS CRACKING AND BREAKING OFF AT THE 6TH AND 7TH SCREWS, (FROM IB TO OB) ON THE INSIDE OF THE OB SLOTS. SUBSEQUENT FOD DAMAGE TO THE NUT AND SAFETY WIRE OF THE BLEED AIR TUBE, AND ALSO THE LEADING EDGE OF THE WING BEHIND THE SLAT IS OCCURRISDR 2006FA0000127Plate · crackedSEAL CLAMPING PLATE IS CRACKING AND BREAKING OFF AT THE 6TH AND 7TH SCREWS, (FROM IB TO OB) ON THE INSIDE OF THE OB SLATS. SUBSEQUENT FOD DAMAGE TO THE NUT AND SAFETY WIRE OF THE BLEED AIR TUBE, AND ALSO THE LEADING EDGE OF THE WING BEHIND THE SLAT IS OCCURINSDR AWXA200600045Skin · debondedMCN - DURING C15 CHECK DISCOVERED DISBOND AT UPPER AND LOWER SURFACE OF THE NR 5 SLAT WEDGE OUTBOARD END, FROM SS 233.0 TO SS 254.0. MAINTENANCE REMOVED THE DISBOND SKIN IAW BOEING 737-300 SRM 51-70-10-2R4. FABRICATED CORE AND DOUBLER IAW BOEING 737-300 SRM SDR DHL2006752510Skin · dentedDENT ON NR 1 SLAT UPPER SURFACE WSTA 720. CUTOUT SKIN SIZE 4 5/8 X 1 1/2 AND INNER SKINS SIZES 8 1/2 X 3 1/4 AND 8 1/2 X 3 1/2 IAW B727 SRM 57-50-3 FIG 1 AND FIG 44. FIBBED SKIN DOUBLERS FROM 2024 T3 .080 SIZE 8 1/2 BY 5 1/8 POX 9002459 AND INNER SKIN FROM 2SDR DHL2006572510Slat · dentedFOUND NR 111042; DENT ON NR1 SLAT UPPER SURFACE WSTA 720. CUTOUT SKIN SIZE 4.6250 X 1.5 AND INNER SKINS SIZES 8.5 X 3.25 AND 8.5 X 3.5 IAW SRM 57-50-3 FIG 1 AND FIG 4 FABBED SKIN DOUBLER FROM 2024 T3 .080 SIZE 8.5 X 5.1250 PO 9002459 AND INNER SKIN FROM 2024SDR 06FDEA0087Skin · dentedFOUND LEFT WING, NR 8 SLAT OUTBOARD LEADING EDGE FOUND DENT. REPAIR CARRIED OUT AT LEFT HAND WING, #8 SLAT OUTBOARD LEADING EDGE SKIN AS PER SRM 57-10-00 VOLUME I, FIGURE 5. REPAIR CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.SDR SWAA060086Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND NR 2 L/E SLAT UPPER SKIN DELAMINATED AT OB END. REMOVED AND REPLACED SLAT IAW MM.SDR IXXA06SMN022SSkin · crackedDURING C CHECK, RT WING OTBD L/E LWR PART SKIN CRACKED ½, XFS 710.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 06014 DATED 01-11-06, SEMAN DWG ED-4144 DATED 01-06-06, EO SEMAN NR 20051569 DATED 01-11-06. REMOVED FASTENERS IAW DC8 SRM 51-1-21, DC8 SRM 5SDR SWAA060060Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND NR 5 L/E SLAT UPPER WEDGE DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED SLAT PER MM.
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