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 SWAA042141Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND LT WING NR 2 L/E SLAT DELAMINATED. REMOVED AND REPLACED NR 2 L/E SLAT PER MM.SDR AWXA200400880Skin · crackedMCN - MAJOR REPAIR - DURING C-19 CHECK 2 EACH CRACKS WERE FOUND IN NR 3 SLAT LOWER SKIN BELOW AUXILIARY TRACK. MAINTENANCE CUT OUT DAMAGED AREA OF NR 3 SLAT LOWER SKIN; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REPAIR PARTS IAW B737-300 SRM 57-43-01 FIGSDR 2004UALA00713Skin · delaminatedT/E WEDGE DELAMINATED, SLAT NR 5. REPLACED TRAILING EDGE WEDGE.SDR DHL2004804527Skin · wornRIGHT WING OUTBOARD FLAP L/E UPPER SKIN WORN, XF 226.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW ED-EDW27.5, DWG W27-R05 REV 1R. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. TRIMMED OUT DAMAGED PLATING IAW ED-EDW 27.5, DWG W27-R05. FABRICATESDR 2004UALA00783Skin · bird strikeOUTBOARD END L/E SKIN DAMAGED BY BIRD STRIKE. REPLACED SECTION OF L/E SKIN.SDR USAA040392Skin · delaminatedPIT - FOUND TOP SKIN AND CORE BOND 3 INCH BY 3.5 INCH AREA DELAMINATED, NR 1 SLAT OUTBOARD T/E. REMOVED DELAMINATED, SKIN CORE 7 INSTALLED NEW AND TOP DOUBLER PER BOEING SRM 51-70-10. (M)SDR USAA040449Skin · delaminatedPIT - FOUND SKIN TO CORE BOND DELAMINATION 2 INCH BY 3 INCH AREA, NR 5 SLAT TOP SURFACE OUTBOARD END. REMOVED DAMAGED SKIN AND CORE MATERIAL, INSTALLED NEW CORE AND TOP DOUBLER PER SRM 51-70-10. (M)SDR USAA040386Skin · delaminatedFOUND SKIN AND CORE BONDED 3 INCH BY 5 INCH AREA, UPPER OUTBOARD T/E CORNER OF NR 5 SLAT. REMOVED DELAMINATED SKIN AND CORE, INSTALLED NEW CORE AND TOP SKIN PER BOEING SRM 51-70-10. (M)SDR USAA040391Skin · delaminatedPIT- FOUND TOP SKIN/CORE BOND DELAMINATED 3 INCH BY 3 INCH AREA, NR 6 SLAT TOP SURFACE OUTBOARD T/E. REMOVED DELAMINATED SKIN, INSTALLED NEW SECTION AND DOUBLER PER BOEING SRM 51-70-10. (M)SDR USAA040387Skin · delaminatedPIT - FOUND SKIN AND CORE BOND DELAMINATED 3 INCH BY 4 INCH AREA, UPPER INBOARD END T/E CORNER OF NR 5 SLAT. REMOVED DELAMINATED, UPPER SKIN AND CORE, INSTALLED NEW CORE AND TOP DOUBLER PER BOEING SRM 51-70-10. (M)SDR AWXA200400892Skin · crackedMCN - MAJOR REPAIR - DURING C-19 CHECK 4 EACH .5 INCH CRACKS WERE FOUND AT RIVET HOLES IN NR 4 SLAT BETWEEN SLAT STA 64.25 AND 78.25. MAINTENANCE CUT OUT CRACKS IN NR 4 SLAT 45.5 TO 61.5 INCHES FROM INBOARD END; FABRICATED A FILLER AND SPLICE PLATE; INSTALLEDSDR AWXA200400889Skin · crackedMCN - MAJOR REPAIR - DURING C-19 CHECK 2 EACH .5 INCH CRACKS WERE FOUND EMANATING FROM RIVET HOLES IN NR 6 SLAT INBOARD AUXILIARY GUIDE ATTACH AREA 42 INCHES AND 45 INCHES FROM INBOARD END. MAINTENANCE CUT OUT CRACKED NR 6 SLAT SKIN 42 INCHES TO 57 INCHES FROSDR AWXA200400881Skin · crackedMCN - MAJOR REPAIR - DURING C-19 CHECK 5 EACH CRACKS WERE FOUND EMANATING FROM RIVET HOLES IN SKIN AT NR 5 SLAT ACTUATOR ATTACHMENT AREA. MAINTENANCE CUT OUT DAMAGED AREA OF NR 5 SLAT SKIN 42 INCHES TO 51 INCHES FROM INBOARD SIDE; FABRICATED A FILLER AND SPLISDR SWAA042001Skin · delaminatedDURING SCHEDULED D-CHECK, FOUND LT WING NR 3 L/E SLAT WEDGE OUTBOARD UPPER END, DELAMINATED. REPAIRED LT WING NR 3 L/E SLAT PER SRM.SDR USAA040447Skin · delaminatedPIT - FOUND SKIN AND CORE BOND DELAMINATION WITH CHAF DAMAGE 1 INCH BY 2 INCH AREA, UPPER INBOARD T/E AFT CORNER OF NR 2 SLAT. REMOVED DELAMINATED, UPPER SKIN AND CORE, INSTALLED FILLER, INTERNAL AND TOP DOUBLER PER SRM 51-70-10. (M)SDR USAA040448Skin · delaminatedPIT - FOUND EXT SKIN AND CORE BOND DELAMINATED AND CHAFE WEAR 3 INCH BY 5 INCH AREA, UPPER OUTBOARD T/E AFT CORNER OF NR 2 SLAT. REMOVED DELAMINATED SKIN AND CORE, INSTALLED FILLER AND INTERNAL AND UPPER DOUBLER PER SRM 51-70-10. (M)SDR CALA0400573Skin · crackedINSPECTION FOUND A 2 INCH CRACK IN NR 3 SLAT SKIN LOWER EDGE AT RIVET HOLES ADJACENT TO ACTUATOR. THE CRACKED AREA WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW SRM 57-43-01, FIGURE 206.SDR USAA040446Skin · delaminatedPIT - FOUND LOEWR SKIN AND CORE WITH DELAMINATED AND CHAF DAMAGED 3 INCH BY 4 INCH, NR 3 SLAT T/E CORNER. REMOVED DELAMINATED SKIN AND CORE MATERIAL, INSTALLED NEW AND LOWER SKIN DOUBLER REPAIR PER SRM 51-70-10. (M)SDR USAA040368Skin · delaminatedPIT - FOUND TOP SKIN AND CORE MATERIAL DELAMINATED 3 INCH BY 4 INCH AREA, NR 3 SLAT INBOARD T/E CORNER. INSTALLED NEW CORE, INSTALLED FILLER AND UPPER DOUBLER PER BOEING SRM 51-70-10. (M)SDR USAA040367Skin · chafedPIT - FOUND LOWER SKIN SURFACE CHAFED 2 INCH BY 1 INCH, NR 4 SLAT INBOARD TRAILING EDGE. REMOVED CHAFED AREA, BONDED, SEALED EDGE AND REFINISHED PER BOEING SRM 51-70-10. (M)SDR DHL2004804518Fitting · crackedITEM REF. NR.2095: LT IB STUB WING ZEE PAN FITTING CRACK 4.000, STA XILD 43.188. REMOVED AND REPLACED CRACKED ZEE PAN FITTING, STA XILD 43.188 (LT IB STUB WING) IAW SRM 51-1-20D PG. 21, SRM 51-1-21 PG.1.SDR SWAA041940Skin · delaminatedDURING SCHEDULED 1/2D CHECK, FOUND RT WING NR 4 L/E SLAT DELAMINATED. REMOVED AND REPLACED RT WING NR 4 L/E SLAT PER MM.SDR DHL2004745519Frame · crackedDURING A C-CHECK, NR 3 SLAT INT FRAME BOTTOM AFT WS 525 IS CRACKED IN RADIUS. REMOVED NR 3 SLAT FOR SHEET METAL ACCESS IAW B727 M/M 27-81-11. REMOVED CRACKED RIB ON NR 3 SLAT IAW B727 SRM 51-30-2. FABRICATED RIB FROM 7075-T6 .032 SIZE 15 X 5.5 INCHES PO 90SDR SWAA041899Skin · delaminatedDURING SPV, FOUND LT WING OUTBOARD FOREFLAP DELAMINATED. REMOVED AND REPLACED LT WING OUTBOARD FOREFLAP PER MM.SDR 04FDEA01926Track · chafedRIGHT WING LOWER SURFACE, LEADING EDGE DIRECTLY INBOARD OF NR 9 SLAT DRIVE TRACK IS CHAFED. BLENDED AREA, FOUND TO BE OUT OF LIMITS IAW DC10 SRM 57-55-01 FIGURE 1 PARAGRAPH 2 VOL 3 AND 57-00-01 VOL I FIG 1A, PARAGRAPH 5. FABRICATED AND INSTALLED OUTER SLAT SSDR 04FDEA01927Skin · gougedRIGHT HAND WING LOWER SURFACE, LEADING EDGE ADJACENT TO NR 8 SLAT IS GOUGED. BLENDED GOUGE IAW DC10 SRM 57-00-01 VOL I, FABRICATED AND INSTALLED DOUBLER IAW DC10 SRM 57-10-00 VOL I, 51-21-01 VOL 2, AND 51-33-01 VOL 2.SDR 151AW0022Skin · crackedNR 2 SLAT HAS CRACKS AT TWO FASTENERS ON LOWER SURFACE NEAR O/B AUX TRACK. REPAIRED PER SRM 57-43-01.SDR 151AW00220Structure · crackedNR 2 SLAT HAS CRACKS AT TWO FASTENERS ON LOWER SURFACE NEAR O/B AUX TRACK. REPAIRED PER SRM 57-43-01.SDR SWAA041871Skin · delaminatedRIGHT WING NR 6 L/E SLAT DELAMINATED. REMOVED AND REPLACED NR 6 L/E SLAT PER MM.SDR 04FDEA01881Support Angle · crackedRIGHT WING SLAT TRACK NR 16 LOWER FAIRING PANEL INBOARD SUPPORT ANGLE IS CRACKED. REMOVED AND REPLACED CLIP IAW SRM 51-31-01 AT MAE.SDR IXXA060404SSkin · corrodedDURING ROUTINE C CHECK, FOUND LEFT WING LEADING EDGE SKIN CORRODED BETWEEN STATION XW257 AND XW408. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060403SSkin · corrodedDURING ROUTINE C CHECK, FOUND LEFT WING LEADING EDGE SKIN CORRODED BETWEEN STATION XW454 AND XW485. REPAIRED PER ALL APPLICABLE DATA.SDR USAA040388Skin · delaminatedPIT - FOUND SKIN AND CORE BOND WITH DELAMINATION 2 INCH AREA, LEFT WING NR 3 SLAT INBOARD AFT CORNER TOP SURFACE. REMOVED DAMGAED SKIN AND CORE, INSTALLED INTERNAL AND TOP DOUBLER AND NEW CORE MATERIAL PER BOEING SRM 51-70-10. (M)SDR ABXA040261Support · crackedLEFT SLAT DRIVE LOWER INBOARD BOLT ATTACHMENT SUPPORT FITTING CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-5 AND 51-30-1.SDR UPS04242737Web · crackedINSPECTION TYPE: C, NR 6 KRUEGER FLAP ACTUATOR TRUNNION SUPPORT BOX L + R WEB CRACKED. REMOVED NR 6 KRUEGER FLAP ACTUATOR IAW MM 27-81-22. REMOVED BOTH CRACKED WEBS FOR FABRICATION IAW SRM 51-30-02. FABRICATED LT & RT WEBS AS PER DRAWING 65-16275. INSTALLESDR UPS04242736Web · crackedINSPECTION TYPE:C, NR 2 KRUEGER FLAP ACTUATOR TRUNNION SUPPORT BOX LT WEB CRACKED. REMOVED LT WEB TO FACILITATE IN FABRICATION OF NEW ONE IAW SRM 51-30- 02. FABRICATED NEW LT WEB IAW DRAWING 65-16269 AND INSTALLED ON NR 2 KRUEGER FLAP ACTUATOR TRUNNION SUPPOSDR SWAA041804Bolt · shearedON APPROACH NR 4 L/E SLAT INDICATED INTRANSIT, RECYCLED PER QRH WITH NORMAL DEPLOYMENT. UPON LANDING CYCLE FLAPS/SLATS AND NOTED A LOUD BANG AND ASYMMETRICAL RATE OF DEPLOYMENT ON NR 4 L/E SLAT, NR 4 L/E SLAT OUTBOARD SIDE STICKS. REMOVED AND REPLACED NR 4 LSDR 2004UALA00620Skin · delaminatedDURING WALK AROUND, FOUND SLAT NUMBER 9 DELAMINATED AT TRAILING EDGE WEDGE. *S/D* REPLACED NUMBER 9 SLAT. DURING DISASSEMBLY OF THE SLAT WEDGE FOR REPAIR, THE SHOP FOUND THAT INADEQUATE FILM ADHESIVE (RESIN) WAS USED DURING THE PERVIOUS REPAIR WHICH LEAD TOSDR SWAA041787Wedge · delaminatedDURING SCHEDULED C2 CHECK, FOUND LT WING NR 2 L/E SLAT T/E WEDGE DELAMINATED. REPAIRED NR 2 L/E SLAT WEDGE PER EA.SDR UPS04242675Skin · crackedINSPECTION TYPE:C, NR 6 L/E SLAT O/B UPSTOP HAS CRACK ON SURROUNDING SKIN. REPAIR CARRIED OUT IAW MM 27-81-11 & SRM 57-30-4 FIG 4.SDR UPS04242677Bracket · crackedINSPECTION TYPE:C, NR 7 SLAT O/B TRACK TO SKIN ATTACH BRACKETS ARE CRACKED. NEW BRACKETS INSTALLED IAW SRM 51-30-02, OHM 57-51-61.SDR UPS04242676Bracket · crackedINSPECTION TYPE:C, NR 5 SLAT, O/B UPSTOP BOLT RETAINING BRACKET IS CRACKED. BRACKET REMOVED IAW SRM 51-30-02, BRACKET FABRICATED IAW SRM 51-30-01, BRACKET INSTALLED IAW SRM 51-30-1 & MM 20-80-01. STOP ADJUSTED TO WITHIN LIMITS IAW MM 27-81-11.SDR AWXA200400790Skin · crackedLCQ - MAJOR REPAIR - DURING C-12 CHECK 5 EACH CRACKS WERE FOUND EMANATING FROM RIVET HOLES IN LEFT L/E SLAT JUST OUTBOARD OF ENGINE PYLON, STAB STA 55.75. MAINTENANCE CUT OUT CRACK IN LEFT L/E SLAT AT STAB STA 55.75; PERFORMED HFEC INSPECTION OF CUTOUT TO VERSDR UPS04242705Skin · crackedINSPECTION TYPE: C, NR 3 LEADING EDGE FLAP ANTI ICE SKIN IS CRACKED IN TWO AREAS, ALSO LOOSE RIVETS IN ANTI ICE SKIN. REPAIRED CRACKS IAW EO B727-5750-3082. REPLACED LOOSE RIVETS IAW SRM 51-30-2.SDR UPS04242683Structure · crackedINSPECTION TYPE:C, NR 3 LEADING EDGE FLAP, O/B BONDING WIRE ATTACH SCREW HOLE IS CRACKED. REPAIR CARRIED OUT IAW AAAE EO 2004-061-002, UPS ENGINEERING FILE NR 727-57-20113.SDR SWAA041717Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND LT WING NR 2 L/E SLAT UPPER T/E CORNER DELAMINATED. REMOVED AND REPLACED NR 2 L/E SLAT PER MM.SDR 2004UALA00640Wedge · delaminatedLEADING EDGE DELAMINATED NR 6 SLAT WEDGE. MAJOR REPAIR. REPLACED WEDGE.SDR UPS04242674Skin · crackedINSPECTION TYPE:C NR 6 L/E SLAT UPPER SKIN HAS SCRATCHES 2 OF WHICH ARE SUSPECT CRACKS NR 1 IS 3 INCHES O/B OF ACTUATOR, NR 2 IS 4 INCHES I/B OF ACTUATOR AND FROM PREVIOUS REPAIR CUTOUT. HFEC INSP CARRIED OUT ON THE ABOVE AREAS IAW B727 NDTM PT6 51-00-00 FIG SDR MWEA040101Vane · chafedRIGHT FLAP NR 2 FIXED VANE LEADING EDGE IS CHAFED. FABRICATED AND INSTALLED PATCH FOR REPAIR.SDR USAA040295Skin · delaminatedPIT - FOUND SKIN TO CORE DELAMINATED AND KNIFE EDGE WEAR, RT WING NR 4 SLAT INBOARD TRAILING EDGE. INSTALLED FILLER AND INTERNAL DOUBLER REPAIR COREW, TOP REPAIR DOUBLER PER SRM 51-70-10. (M)
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