JASC 5754
Service difficulty reports · 17,348
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 SWAA000893Skin · crackedDURING SCHEDULED BC1 CHECK, FOUND BOTH LT AND RT WING O/B KRUEGER FLAPS HAVE .25 INCH CRACKS ON INNER SKIN ACROSS T/E OF VERTICAL STIFFENER RIB. REMOVED AND REPLACED BOTH KRUEGER FLAPS PER MM.SDR DL72S000939Bracket · crackedFOUND ON F2 LETTER CK, INBOARD ATTACH BRACKET CRACKED NR 8 SLAT ACTUATOR. REPAIR PER MM 57-20-21.SDR 0001929880Skin · crackedFLAP LEADING EDGE JUST AFT OF NR 2 FLAP HINGE IS CRACKED. REPAIRED PER EA 98-172453. L/P 1437664SDR TWAA0007703Skin · dentedDURING OP 16 MAINT CHECK ON LT WING, FOUND DENTS IN LEADING EDGE OF NUMBER 3 LEADING EDGE SLAT, DENT LOCATED 13 INCHES I/B FROM O/B END OF SLAT WAS 1 INCH WIDE BY 1 INCH LONG AND 0.050 INCH DEEP, DENT LOCATED 18 INCHES I/B FROM O/B END OF SLAT WAS .75 INCH LONSDR RRXA001755Skin · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK ON THE UPPER SIDE OF THE RT WING LE SKIN 2 INCHES FWD OF THE WING SPAR AT XFS 615, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8.SDR RRXA001754Skin · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK ON THE UPPER SIDE 2 INCHES FWD OF THE WING SPAR ON THE RT WING LE SKIN AT XFS 603.75, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8.SDR RRXA001753Skin · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK 2 INCHES FWD OF THE WING SPAR ON THE RT WING LE SKIN ON UPPER SIDE AT XFS 615, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8.SDR RRXA001752Skin · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE SKIN ON UPPER SIDE 2 INCHES FWD OF THE WING SPAR AT THE RT WING LEADING EDGE AT XFS 603.75, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8.SDR UPS00832655Angle · crackedINSPECTION TYPE:C123, LEFT WING L/E RIB ANGLE IS CRACKED AT XS 467.323. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 5770170 AND SRM 51-1-20D.SDR UPS00832654Doubler · crackedINSPECTION TYPE:C123, LEFT WING L/E INTERNAL DOUBLER IS CRACKED AT XFS 572.5. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769600 AND SRM 51-1-20D, 51-1-21, 51-1-21A.SDR UPS00832653Angle · crackedINSPECTION TYPE:C123, LEFT WING L/E VERTICAL ANGLE IS CRACKED AT XS 256. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 9753294 AND SRM 51-1-20D.SDR DL72K000919Stiffener · crackedFOUND ON B1 LETTER CK, L/E SPAR STIFFENERS CRACKED L/E SPAR I/B AND O/B OF NR 7 SLAT ACTUATOR. REPAIRED PER MM 57-20-21.SDR MALA000315Rib · crackedRIB 3 & 4 CRACKED ON ENDS LEADING EDGE PNL 511 BL. REMOVED DAMAGE, FABRICATED REPAIR DOUBLERS IAW SRM 57-10-30. LOCATED AND DRILLED ROW HOLES IAW 57-10-30. NDT PER FFUNDT006, NO CRACKS NOTED. INSTALLED DOUBLERS ON LEADING EDGE IAW SRM 57-10-30.SDR RRXA002240Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACKS AT RIVETS ON THE LT WING O/B SLOT LEADING EDGE VANE AT STA XS 472 AND XS 478, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED RIVETS IAW DC-SDR RRXA002238Skin · damagedDURING A MAINTENANCE VISIT FOUND SCREWS PULLING THROUGH SKIN ON THE LT WING O/B SLOT L/E VANE AT STA XFS 428 34 TO 48 INCHES FWD OF SPAR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSDR AALA20005710Structure · wornTUL - FOUND RIGHT KRUEGER FLAP BLOCKER DOOR WORN 2 INCHES BY .080 DEEP IN FLANGE. REPAIRED FLAP BLOCKER DOOR PER ESO 30595 DATED 5/5/2000. (M)SDR CALA0000635Access Panel · crackedINSPECTION FOUND A 1 INCH CRACK IN NR 1 RIGHT SLAT LOWER CUTOUT DOOR. THE CUTOUT DOOR WAS REMOVED AND REPLACED.SDR UPS00832636Skin · crackedINSPECTION TYPE:C123, RIGHT WING L/E SKIN IS CRACKED AT XFS 710. REPAIRED IAW SRM 57-2-1 FIG 2H.SDR DL72L000884Skin · wornUPPER SURFACE IS WORN ON NR 5 SLAT. BURNISHED WEAR AREA, MADE STAINLESS DOUBLER. INSTALLED DOUBLER PER MM 727 57-54-0 FIG 81.SDR CALA0000612Skin · gougedLEFT NUMBER 5 FLAP LEADING EDGE IS GOUGED. REMOVED AND REPLACED RUB STRIP PER EC/RA 5750-01579 AND SRM 51-30-2.SDR UPS00232786Rib · crackedINSPECTION TYPE:C, CRACK FOUND AT NR 3 RIB AT INNER SKIN CONNECTING NR 7 SLAT. REPAIR CARRIED OUT IAW SRM 57-50-3, FIGURE 9.SDR QXEA0001187Skin · chafedYYC- SPAN WISE CHAFE DAMAGE ON UPPER SURFACE OF LEFT HAND INBOARD FLAP LEADING EDGE. REPAIRED IAW HORIZON AIR EA 9-57-501, DHC-8 SRM 51-2036 AND SRM 51-20-51.SDR DL72K000868Stiffener · crackedA 2 INCH CRACK IN NR 3 SLAT O/B TRACK O/B SPAR STIFFENER. REPLACED STIFFENER PER M/M 57-20-21.SDR RAAA00B1003Rib · crackedDURING SCHEDULED C2 CHECK, FOUND NR 3 SLAT ACTUATOR BUSHING/BOLT WORN. UPON FURTHER INVESTIGATIION FOUND RIB CRACKED. REPLACED BOLT AND BUSHING WITH NEW RIB IAW M/M 27-81-11 & 27-81-32, SRM 51-20-4, 51-10-1 & 51-30-2.SDR RRXA002239Skin · damagedDURING A MAINTENANCE VISIT FOUND ATTACH SCREWS PULLING THROUGH SKIN AT LT WING O/B SLOT L/E VANE AT STA XFS 508.000 34 INCHES TO 48 INCHES FWD OF SPAR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABSDR GAIA00258Rib · crackedDURING HEAVY C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND, NR 5 SLAT 3RD RIB FROM INBOARD END RIB CRACKED. REPAIRED RIB PER IAW SRM 57-50-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR DL72S000806Stiffener · crackedA 1 INCH CRACK IN SPAR STIFFENER I/B SIDE OF NR 6 SLAT I/B TRACK. REPLACED STIFFENER PER M/M 57-20-21. TPA D-1 LETTER CHECK.SDR DL72K000980Skin · damagedDURING SHOP VISIT, THE LEADING EDGE SKIN WAS FOUND WORN AT THE I/B END OF THE MIDFLAP. THE SKIN WAS REPAIRED BY REMOVING THE DAMAGE AND INSTALLING A DOUBLER AND FLUSH FILLER PER MM 57-52-0, FIG 803.SDR DL72K000979Skin · damagedDURING SHOP VISIT, THE LEADING EDGE SKIN WAS FOUND WORN AT THE I/B END. THE SKIN WAS REPAIRED BY REMOVING THE DAMAGE AND INSTALLING A DOUBLER AND FLUSH FILLER PER MM 57-52-0, FIG 803.SDR 00FDEA00284Cap · crackedNR 5 LEADING EDGE SLAT I/B END CRACKED. REMOVED AND REPLACED I/B END CAP ON NR 5 SLAT IAW SRM 51-30-2.SDR TWAA0006434Skin · debondedDURING CHECK-C MAINT, THE LT WING NUMBER 6 LEADING EDGE SLAT TOP SIDE AT MID SPAN HAD THE HOT BOND LIFTED AND HAD BEEN SEALED WITH SPEED TAPE PER SRM 57-43-02. APPLIED HOT BOND REPAIR ON NUMBER 6 SLAT APPROX 3 .75 BY 4.75 INCH DOUBLER PER SRM 57-43-20 AND 51-SDR RRXA002500Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LEADING EDGE LT WING AT XFS 566, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 51-1-21 AND EO NR 00SDR DL757000771Skin · puncturedAFTER ACCOMPLISHMENT OF S/B 757-57A0043, THE I/B LEADING EDGE SLAT, TRAILING EDGE WEDGE, UPPER SKIN WAS DAMAGED. DAMAGE LOCATED 1 AFT OF THE FWD EDGE OF THE TRAILING EDGE WEDGE UPPER SKIN AND 46 I/B FROM THE O/B EDGE. REPAIR PER ER/A 387545-14.SDR DL757000770Skin · puncturedAFTER ACCOMPLISHMENT OF BCAG S/B 757-57A0043, THE I/B LEADING EDGE SLAT, TRAILING EDGE WEDGE UPPER SKIN WAS DAMAGED. DAMAGE WAS LOCATED 2 INCHES FWD OF THE AFT EDGE OF THE TRAILING EDGE WEDGE UPPER SKIN AND 61 O/B FROM I/B EDGE. REPAIR PER ER/A 387546-14.SDR UPS00832606Skin · crackedINSPECTION TYPE:C2, LEFT WING L/E LOWER SKIN IS CRACKED AT FASTENER HOLES BETWEEN XFS 640 - 649. REPAIRED IAW EO DC8-5720-4087-B.SDR UPS00832565Rib · crackedINSPECTION TYPE:C-2, RIGHT WING L/E UPPER RIB CRACKED STA XS 250.089. STOP DRILLED CRACKED IAW SRM 57-2-0 FIG 2. FAB AND INSTALLED ANGLE DOUBLERS IAW SRM 51-1-20D & 51-3-0.SDR UPS00832557Skin · crackedINSPECTION TYPE:C-2, LEFT WING CENTER L/E LWR SKIN CRACKED STA XW 257. STOP DRILLED CRACK IAW ADDUM DC8-5720-4087-B. FAB AND INSTALLED DOUBLER IAW DC8-5720-4087-B.SDR UPS00832546Doubler · corrodedINSPECTION TYPE:C2, RIGHT WING L/E BETWEEN STA 772.500 TO XFS 760.00. THE INTERNAL DOUBLER HAS HEAVY CORROSION. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 3641257.SDR UPS00832545Skin · crackedINSPECTION TYPE:C2, RIGHT WING L/E (NR 3 STUB WING) AT STA XS207.500. THE L/E SKIN IS CRACKED AT FRONT SPAR. REPAIRED AREA IAW DC8-5720-7767-A.SDR UPS00832536Rib · crackedINSPECTION TYPE:C2, RIGHT WING L/E EXTERIOR SKIN IS CRACKED AT STA XFS288.00 ON THE L/E. REPAIRED AREA IAW SRM 57-2-1 FIG 2H.SDR UPS00832534Rib · crackedINSPECTION TYPE:C2, RIGHT WING L/E AT STA XFS.792.250. THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS00832532Rib · crackedINSPECTION TYPE:C2, LEFT WING L/E UPPER RIB IS CRACKED AT STA XS.00. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS00832531Skin · corrodedINSPECTION TYPE:C2, RIGHT WING L/E SKIN HAS INTERNAL CORROSION AT STA XFS710.00. REPAIRED AREA IAW 8110-3 APPROVED DH SK 700-025.SDR UPS00832421Rib · crackedINSPECTION TYPE:C2, LEFT WING L/E UPPER RIB IS CRACKED AT XFS 646. REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS00832420Rib · crackedINSPECTION TYPE:C2, RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 283.25. REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS00832417Rib · crackedINSPECTION TYPE:C2, LEFT WING L/E UPPER RIB IS CRACKED AT XFS 660. REPAIRED IAW SRM 57-2-0 FIG 2.SDR RIVA0000011Rib · crackedNR 5 SLAT LEADING EDGE RIBS (2 EACH) CRACKED AT SLAT STATION 61 AND 63. REPAIRED IAW BOEING SRM 57-50-3, FIGURE 9. FABRICATED AND INSTALLED DOUBLERS (2 EACH) FROM .032 CRES A1S1,321 ANNEALED CONDITION. DOUBLER AT SLAT STATION 63 INSTALLED WITH SHIM AND RADISDR RRXA002276Skin · damagedDURING A MAINTENANCE VISIT FOUND SCREWS PULLING THROUGH THE SKIN I/B SLOT LEADING EDGE VANE AT STA XS 250.000, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRSDR UPS00832535Rib · crackedINSPECTION TYPE:C2, LT WING CENTER L/E UPPER RIB IS CRACKED AT STA XFS 410.250. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS00832419Rib · crackedINSPECTION TYPE:C2, LEFT WING L/E UPPER RIB IS CRACKED AT XFS 610. REPAIRED IAW SRM 57-2-0 FIG 2.
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