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 UPS00832418Rib · crackedINSPECTION TYPE:C2, LEFT WING L/E LOWER RIB IS CRACKED AT XOLDI 6.225. REPAIRED IAW SRM 57-2-0 FIG 2.SDR TWAA0006302Skin · delaminatedDURING CHECK-C MAINT, THE LT WING NUMBER 2 L/E SLAT O/B END, THE T/E WEDGE HAD A BULGE THAT WAS DELAMINATING. APPLIED HOT BOND REPAIR ON NR 2 SLAT APPROX 4 IN BY 3.5 DOUBLER PER SRM 57-43-02 AND 51-70-10.SDR TWAA0006301Structure · damagedDURING CHECK-C MAINT, THE LT WING NUMBER 4 L/E SLAT ASSY HAD A HOLE IN THE INSIDE SURFACE. FILLED DAMAGED AREA AND APPLIED 2 IN BY 2 IN METAL TO METAL HOT BOND. PRIMED AND PAINTED PER SRM 51-70-10.SDR TWAA0006206Skin · delaminatedDURING CHECK-C MAINT THE RH WING NUMBER 10 L/E SLAT HAD 5 INCH SQUARE DOUBLER THAT WAS DELAMINATING, ON TOP SURFACE, 5 FT I/B FROM THE O/B END. REMOVED DELAMINATED PATCH. CLEANED AREA, FABRICATED NEW DOUBLER 5 INCH BY 6 INCH AND HOT BOND PER SRM 51-70-10. SSDR TWAA0006205Skin · delaminatedDURING CHECK-C MAINT, FOUND RT WING NUMBER 7 L/E SLAT REPAIR HAD A 6 INCH BY 4 INCH DELAMINATION, 4 INCHES FROM THE I/B END, ON TOP. APPLIED HOT BOND REPAIR ON NUMBER 7 SLAT, APPROX 5.5 INCH BY 5.5 INCH DOUBLER PER SRM 57-43-02 AND 51-70-10. SEALED EDGES PERSDR 2000UALA00514Skin · damagedRIGHT WING LEADING EDGE (L/E) SKIN DAMAGE FROM LEADING EDGE STATION 140 TO LE STA 149, AND KRUEGER FLAP HINGE RIB DAMAGE AT L/E STA 149. THE KRUEGER FLAP HINGE RIB WAS REPLACED AND THE L/E SKIN WAS REPLACED FROM L/E STA 139 TO L/E STA 149.SDR RRXA002277Skin · damagedDURING A MAINTENANCE VISIT FOUND SCREWS PULLING THROUGH SKIN LT WING I/B SLOT LEADING EDGE VANE AT STA XS 220.000, 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-SDR DL72K000857Rib · crackedAT HMV, THE RIB OF THE NR 2 SLAT WAS FOUND CRACKED JUST O/B OF ANTI-ICE DUCT. REMOVED DAMAGE AND MADE DOUBLER AND FILLER. INSTALLED DOUBLER AND FILLER PER MM 57-54-0 FIG 814.SDR CALA0000499Skin · dentedINSPECTION FOUND LT WING NR 1 SLAT DENTED. THE DENTED AREA WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 57-06, FIGURE 1.SDR MZZA00008Bracket · failedFLT 911 - GUM - NR 4 LED WON''''T RETRACT AFTER TAKEOFF, PERFORMED ABNORMAL PROCEDURES AND RETURNED FOR LANDING. MAINTENANCE REMOVED NR 4 LED RETRACT SWITCH AND MOUNT BRACKET AND ARM, AND INSTALLED SERVICEABLE MOUNT BRACKET AND ARM AND INSTALLED SERVICEABLE SSDR ABXA000240Fitting · corrodedDURING D-CHECK, FOUND NR 1 SLAT TRACK FITTING CORRODED. REPLACED FITTING IAW DC9 SRM 51-30-2.SDR P2EA00174Skin · wornSJO - DURING C-CHECK, FOUND THE RIGHT OUTBOARD FORE FLAP INBOARD LEADING EDGE SKIN WBL 191-205 HAS WEAR BEYOND LIMITS. REPAIRED THE RIGHT OUTBOARD FORE FLAP INBOARD LEADING EDGE SIN WBL 191-205 IAW BOEING FAX NR COO-SJO-00-00439H DATED APR 27, 2000. (M)SDR P2EA00175Skin · wornSJO - DURING C-CHECK, FOUND THE RIGHT OUTBOARD FORE FLAP INBOARD LEADING EDGE SKIN WBL 409-394 HAS WEAR BEYOND LIMITS. REPAIRED THE RIGHT OUTBOARD FOREFLAP INBOARD LEADING EDGE SKIN WBL 409-394 IAW BOEING FAX NR COO-SJO-00-00439H DATED APR 27, 2000. (M)SDR P2EA00176Rib · crackedSJO - DURING C-CHECK, FOUND THE NR 6 SLAT OUTBOARD SLIDING RAIL BEARINGS SUPPORT RIB WBL 523.5 CRACKED. REPAIRED THE NR 6 SLAT OUTBOARD SLIDING RAIL BEARINGS SUPPORT RIB WBL 523.5 CRACKED IAW COOPESA EO NR COO-3-57-287. (M)SDR RRXA002480Skin · crackedDURING A MAINTENANCE VISIT FOUND A CRACK EMANATING FROM SCREW HOLE ON THE RIGHT I/B SLOT LEADING EDGE BOTTOM SIDE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 51-1-7SDR DL72S000702Skin · crackedLOWER EXT SKIN CRACKED AT RIB ATTACH FASTENER HOLES 8.5 INCHES FROM I/B END. REPAIRED PER MM 57-54-0 FIG 801.SDR CALA0000462Skin · chafedINSPECTION FOUND LT WING LEADING EDGE OF NR 1 FORE FLAP CHAFED DUE TO CONTACT WITH SPOILER ACTUATOR HYDRAULIC LINE. THE LEADING EDGE OF NR 1 FORE FLAP WAS REPLACED IAW ECRA 5753-01100.SDR AALA20000671Skin · corrodedTUL - NR 6 LEADING EDGE FLAP CORRODED AT 11B GROUND WIRE ATTACH BELT. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 57-50-03-9. (X)SDR DL72S000693Rib · crackedRIB NUMBER 7 CRACKED MANUFACTURED DOUBLER. INSTALLED DOUBLER PER 57-54-0 FIG 814 MM.SDR 20000622AP002Bolt · shearedFLT 9424 - EYW/MIA - ON APPROACH TO MIA, THE FLAPS WERE SELECTED TO THE LANDING POSITION. THE AIRCRAFT WENT TO THE LEFT. PERFORMED MISSED APPROACH PROCEDURES. UNABLE TO RAISE THE FLAPS OUT OF LANDING POSITION, SUSPECTED DIFFERENTIAL FLAP LOCKOUT, RETRIMMED SDR DL72L000809Rib · crackedRIB CRACKED AT LWR RADIUS NR 5 SLAT TRACK SUPPORT BOX. REMOVED SLAT TRACK. REMOVED DAMAGE, FABRICATED REPAIR DOUBLER AND FILLER PER MM 57-54-0 FIG 808. OK TO INSTALL DOUBLER AND FILLER. INSTALLED REPAIR PER MM 57-54-0 FIG 808 AND BEGAN INSTALLING SLAT TRACSDR 00FDEA00213Skin · crackedA/C ARRIVED TO EWR WITH DAMAGE TO LH WING OUTBD FORE FLAP. ** S/D ** R&R LT OTBD VANE ASSY PER MM 27-50-03-2. PER OPS CK NO DEFECT NOTED.SDR RRXA001779Skin · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO THE SCREW HOLE ON THE UPPER SURFACE RT LE STUB WING AT STA XFS 550, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. INSTALLED FASTENER PER E.O. 00SDR RRXA001797Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AROUND SCREW HOLES AT LT WING I/B LEADING EDGE UPPER SURFACE AT STA XFS 113.750 TO XFS 10.750, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATEDSDR DHL200072617CAngle · crackedNR 7 SLAT O/B TRACK TO SLAT ATTACH ANGLE IS CRACKED. REMOVED CRACKED ANGLE FROM NR 7 SLAT O/B TRACK TO SLAT ATTACH ANGLE PER SRM 51-30-2. REPLACED ANGLE PER SRM 51-30-2 & 51-10-2 FIG 4.SDR DHL200072612CAngle · crackedNR 2 SLAT O/B TRACK TO SLAT ATTACH ANGLE IS CRACKED. REMOVED AND REPLACED ATTACH BRACKET AT NR 2 SLAT O/B TRACK PER SRM 51-30-2. ALODINED AND PRIMED AREA PER SRM 51-10-2.SDR AWXA0000226Skin · chafedC-CHECK, LEFT WING NR 3 SLAT ACTUATOR CUTOUT CHAFED. REMOVED DAMAGE IAW 737 SRM 57-30-4 FIG 5, FABRICATED REPAIR SKIN IAW 737 SRM 57-30-4 FROM 2024T3 .032, SPLICE PLATES FROM 2024 T3 .050 AND FILLER FROM 2024T3 .063 IAW 737 SRM 57-30-4, ALODINED AND PRIMED PSDR AWXA0000225Skin · chafedC-CHECK, LEFT WING NR 1 SLAT ACTUATOR CUTOUT CHAFED. REMOVED DAMAGE IAW 737 SRM 57-30-4 FIG 5, FABRICATED SKIN FROM 2024 T3 .040, SPLICE PLATES FROM 2024T5 .050 IAW 737 SRM 57-30-4, ALODINED AND PRIMED IAW 737 SRM 51-10-2, INSTALLED IAW 737 SRM 57-30-4.SDR RRXA001750Skin · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK ON THE LWR SURFACE AT THE LT WING LE SKIN 5 INCHES FWD OF THE WING SPAR AT XFS 335, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAWSDR 20000511SH030Structure · corrodedDURING A C-CHECK, CORROSION WAS NOTED IN SEVERAL AREAS, RIGHT - INBOARD FORE FLAP. (X)SDR RRXA000831Skin · damagedDURING A MAINTENANCE VISIT, FOUND TWO SCREWS NOT INSTALLED IN RT WING L/E BETWEEN STA XFS 26.250 AND 63.750 (EO), DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8, INSTALLED FASTENERS IAW DC-8 SRM 51-1-20C AND EO NR 9SDR P2EA00086Skin · delaminatedYXD - DURING C-CHECK, FOUND THE RIGHT OUTBOARD FORE FLAP INBOARD END BL 334 WITH DELAMINATED, LENGTH 1.5 INCH, WIDTH .500 INCH, DEPTH .089 INCH. REPAIRED RIGHT OUTBOARD FORE FLAP INBOARD END DELAMINATED WITH DOUBLER PER SRM 51-40-6 WORK ACCOMPLISHED ON NON-ROSDR ABXA000244Fitting · corrodedRIGHT OUTBOARD SLAT IDLER TRACK FITTING HAD HEAVY CORROSION/EXFOLIATION AT 3 MOUNT HOLES. REPLACED RIGHT NR 1 LEADING EDGE SLAT.SDR AT0000196Doubler · dentedFOUND LEFT WING NR 4 SLAT WITH 2 DENTS OUT OF LIMITS. CUT OUT DENTS, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC9 SRM 57-09 FIGURE 10.SDR AWXA0000198Skin · delaminatedC-CHECK, LEFT O/B FORE FLAP DELAMINATED AT I/B END LOWER SURFACE. REMOVED DAMAGED AREA IAW 737 SRM 51-70-10, FABRICATED FILLER AND HOT BONDED PARTS IAW 737 SRM 57- 53-02, PRIMED AND SEALED REPAIR IAW 737 SRM 51-70-10.SDR 00FDEA00201Rib · crackedLT WING NR 3 SLAT I/B RIB FOUND CRACKED, LENGTH 6 INCHES.SDR DHL200080484CRib · crackedLEFT WING L/E RIB LOWER PART CRACKED AT XFS 347.750. STOP DRILLED PER SRM 57-2-0. FABRICATED DOUBLER PER SRM 57-2-0. CLEANED,TREATED AND PRIMED PER SRM 51-1-8. INSTALLED DOUBLER PER SRM 57-2-0.SDR DHL200080483CRib · crackedLT WING LEADING EDGE RIB LOWER PART CRACKED 3 INCHES AT XES 329.343. FABRICATED DOUBLER PER SRM 57-2-0. CLEANED, TREATED AND PRIMED PER SRM 51-1-8. INSTALLED DOUBLER PER SRM 51-1-21.SDR SWAA000589Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND NR 1 LE SLAT DELAMINATED, 12 X 5 X 10 SECTION NEAR INBD AND TE. R&R SLAT ASSY PER MM.SDR SWAA000585Skin · crackedDURING SCHEDULED C2 CHECK, FOUND NR 1 LE SLAT LOWER SKIN CRACKED 3 INCHES LONG NEAR TE AND INBD ACTUATOR. R&R SLAT PER MM.SDR RRXA001922Skin · crackedDURING A MAINTENANCE VISIT FOUND A CRACK IN THE SKIN UPPER SURFACE LT CENTER SECTION L/E AT STA XFS 366, 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-SDR RRXA001786Skin · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK IN THE SKIN UPPER SURFACE AT THE LT CENTER SECTION LE AT STA XFS 366, 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 DCSDR MWEA00185Skin · damagedRIGHT WIND LEADING EDGE SKIN DAMAGED AT CUTOUT FOR NUMBER ONE SLAT INBOARD IDLER TRACK. MAINTENANCE FABRICATED AND INSTALLED WING SKIN REPAIR.SDR USAA000446Skin · crackedCLT - FOUND SLAT EXTERNAL SKIN CRACKED 1 INCH, NR 3 SLAT LOWER SKIN TRAILING EDGE AT ACTUATOR ATTACH LOCATION. REPAIRED PER BOEING DWG 65C30133. (M)SDR P2EA00102Skin · delaminatedYXD - DURING C-CHECK, FOUND NR 5 SLAT TRAILING EDGE WITH DELAMINATED AT RWBL 317, LENGTH 4 INCHES, WIDTH 2 INCHES, WL 232, LENGTH 4.5 INCH. REPLACED NR 5 SLAT WITH SERVICEABLE SLAT P/N NR 65-46-422-282 IAW BOEING MM 27-81-12 WORK COMPLETED ON VAM 100-0374.(M)SDR SWAA000563Skin · crackedDURING SCHEDULED QUARTER D CHECK, FOUND NR 5 LE SLAT LOWER SURFACE CRACKED INBD OF OUTBD AUX TRACK CUT-OUT. REPAIRED SKIN PER TI-657-012.SDR DL72K000638Skin · wornAT HMV THE 5 SLAT LEADING EDGE WAS FOUND WORN AT FENCE. DRILLED REPAIR DOUBLER PER MM 57-54-0. DYE PEN INSP AREA UNDER FENCE FOUND 2 CRACKS STOP DRILLED. INSTALLED DOUBLER PER MM 57-54-0 FIG 817.SDR DL72K000585Rib · crackedNR 5 SLAT I/B RIB CRACKED. INSTALLED REPAIR DOUBLER PER B727 MM 57-54-0, FIG 814.SDR ASAA0040038Skin · damagedSEAT - DURING SCHEDULED C-CHECK, THE FIXED LEADING EDGE COMPOSITE SKIN BETWEEN NR 2 AND NR 3 SLAT WAS FOUND TO BE DAMAGED. REPAIRED PER EA 5740-01195. (M)SDR RRXA001931Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE UPPER RIB AT LT CENTER L/E AT STA XFS 297.500, 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 57-
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