JASC 5714
Service difficulty reports · 1,451
Reports filed under 5714 · Wing, Center Box, 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 = '5714' 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 = '5714' 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 UPS00832540Doubler · corrodedINSPECTION TYPE:C2, STA 730 - 780 ,LBL 8 -RBL 8, THE CENTER WING UPPER EXTERNAL DOUBLER HAS HEAVY CORROSION IN SEVERAL PLACES. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5643130.SDR EIAA2000101Shear Tie · crackedHAECO-HKG - D6/D-CHECK - WING CENTER TANK FORWARD LBL 10 INCHES BS 1000 UPPER SHEAR TIE CRACKED. TRIMMED OFF, NDT INSPECTED OK, REPLACED CRACKED SHEAR TIE PER SRM 51-10-01. (X)SDR EIAA2000100Shear Tie · crackedHAECO-HKG - C6/D-CHECK - WING CENTER TANK FORWARD LBL 50 INCHES BS 1000 UPPER SHEAR TIE CRACKED. TRIMMED OFF, NDT INSPECTED OK, REPLACED CRACKED SHEAR TIE PER SRM 51-10-01. (X)SDR EIAA2000099Shear Tie · crackedHAECO-HKG - WING CENTER TANK FORWARD LBL 30 INCHES BS 1000 UPPER SHEAR TIE CRACKED. TRIMMED OFF, NDT INSPECTED OK, REPLACED CRACKED SHEAR TIE PER SRM 51-10-01. (X)SDR UPS00432864Frame · corrodedINSPECTION TYPE: C, CORROSION ON UPPER SURFACE OF CENTER WING AT BS 1100 RBL 106. NEW SECTION OF CHORD AND REPAIR ANGLES FABRICATED AND FITTED PER Q/NOTE 6/00.SDR RRXA002048Skin · damagedDURING A MAINTENANCE VISIT FOUND SCREWS PULLING THROUGH THE LT L/E CENTER SECTION AT STA XFS 310 TO 422, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-20DSDR RRXA000499Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO CENTER AUX TANK LOWER SKIN AT XFS 107.5. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA DER APPROVED ENGINEERING SKETCHSDR RRXA000498Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO CENTER TANK LOWER SKIN AT XFS 102.5. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED IAW FAA DER ENGINEERING SKETCH SK 831-231. CORROSSDR AALA20004003Skin · corrodedAFW - WING BOX UPPER SKIN HAS CORROSION ON UPPER SURFACE. REMOVED FASTENERS, HFEC THE BLENDED AREA, SHOT/FLAP PEEN THE AFFECTED AREA PER SRM. APPLY ALODINE AND 2 COATS OF PRIMER TO AREA. REWORK EXISTING COUNTERSINK PER 767SRM 51-40-08 PER REF /C/. INSTALL SDR RRXA000269Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO EXTERNAL CENTER TANK ATTACHMENT ANGLE BETWEEN STA 710 TO STA 720 AND BL 47R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAWSDR 99T64R472EWAWeb · misdrilledFOUND DURING D-CHECK, HOLE MISDRILLED INSIDE LEFT CENTER TANK AT XCW 69.5 UPPER SURFACE, FUSELAGE STATION 761. BLENDED OUT DRILL START, SPOT FACED. TREATED AND PRIMED. INSTALLED FACTORY FASTENER. IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO NR 99-186 WITH SDR 2000ZZZM38Panel · corrodedCENTER WING DRY BAY PAREL NR 52105 HAS CORROSION, UNIT TRANSFERED FROM CRIC NR 7860. BLENDED CORROSION IAW ATR SRM 53-14-12. INSTALLED NEW CENTER WING DRY BAY PANEL IAW ATR 72 AMM/JIC 57-00-00 OAC. (M)SDR SCNA99582Endcap · corrodedDURING A HEAVY MAINTENANCE CHECK, THE CENTER WING LOWER BARREL AT STA 1521 LGR 50 RIGHT END CAP FITTING WAS FOUND TO BE CORRODED. REMOVED AND FABRICATED NEW FITTING AND INSTALLED PER SRM 513101.SDR SCNA99581Endcap · corrodedDURING A HEAVY MAINTENANCE CHECK, THE CENTER WING LOWER BARREL AT STA 1521 LGR 49 LEFT END CAP FITTING WAS FOUND TO BE CORRODED. REMOVED AND FABRICATED NEW FITTING AND INSTALLED PER SRM 513101.SDR SCNA99580Endcap · corrodedDURING A HEAVY MAINTENANCE CHECK, THE CENTER WING LOWER BARREL AT STA 1521 LGR 49 RIGHT END CAP FITTING WAS FOUND TO BE CORRODED. REMOVED AND FABRICATED NEW FITTING AND INSTALLED PER SRM 513101.SDR SCNA99579Endcap · corrodedDURING A HEAVY MAINTENANCE CHECK, THE CENTER WING LOWER BARREL AT STA 1521 LGR 48 LEFT END CAP FITTING WAS FOUND TO BE CORRODED. REMOVED AND FABRICATED NEW FITTING AND INSTALLED PER SRM 513101.SDR SCNA99578Endcap · corrodedDURING A HEAVY MAINTENANCE CHECK, THE CENTER WING LOWER BARREL AT STA 1521 LGR 48 RIGHT END CAP FITTING WAS FOUND TO BE CORRODED. REMOVED AND FABRICATED NEW FITTING AND INSTALLED PER SRM 513101.SDR SCNA99577Endcap · corrodedDURING A HEAVY MAINTENANCE CHECK, THE CENTER WING LOWER BARREL AT STA 1521 LGR 51 RIGHT END CAP FITTING WAS FOUND TO BE CORRODED. REMOVED AND FABRICATED NEW FITTING AND INSTALLED PER SRM 513101.SDR SCNA99576Endcap · corrodedDURING A HEAVY MAINTENANCE CHECK, THE CENTER WING LOWER BARREL AT STA 1521 LGR 52 RIGHT AND LEFT END CAP FITTING WAS FOUND TO BE CORRODED. REMOVED AND FABRICATED NEW FITTING AND INSTALLED PER SRM 513101.SDR SCNA99575Endcap · corrodedDURING A HEAVY MAINTENANCE CHECK, THE CENTER WING LOWER BARREL AT STA 1521 LGR 51 END CAP FITTING WAS FOUND TO BE CORRODED. REMOVED AND FABRICATED NEW FITTING AND INSTALLED PER SRM 513101.SDR SCNA99574Endcap · corrodedDURING A HEAVY MAINTENANCE CHECK, THE CENTER WING LOWER BARREL AT STA 1521 LGR 50 END CAP FITTING WAS FOUND TO BE CORRODED. REMOVED AND FABRICATED NEW FITTING AND INSTALLED PER SRM 513101.SDR ABXA9900842Fitting · corrodedDURING D-CHECK, FOUND FITTING JUST BELOW CENTER WING TANK FRONT SPAR IN FORWARD LOWER CARGO COMPARTMENT CORRODED. REPLACED FITTING IAW DC9 SRM 51-30-5 AND 51-20-0.SDR USAA990421Angle · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT LOWER END OF INBOARD CHORD ANGLE OF FRAME RBL 65 AT TOP OF WING CENTER SECTION FRAME. INSTALLED FILLER, STIFFENING ANGLE AND TAPERED SHIM PER EA 64331 AND TR 53-62-01. (M)SDR LR7A99130Beam · corrodedDURING C CHECK/BRIDGING INSPECTION NR 420 WORK, FOUND CENTER WING BOX BEAM UPPER REAR CAP CORRODED AT CWS 61R. REPAIRED IAW SMP S83 AND MPP L100-404-99-060. NR 981.SDR LR7A9982Web · crackedDURING SCHEDULED C1 INSPECTION PER HC2704, FOUND FWD CENTER WING WEB CRACKED 1.25 INCH AT RBL 20 RADIATING FROM FASTENER HOLE UNDER SUPPORT FITTING. REPAIRED PER MPP 401-1999-L100-57-107.SDR 99FDEA00115Spar · corrodedWHILE WORKING NR 654, FOUND VERTICAL FLANGE OF LWR WING CTR SECTION SPAR CHORD TO BE CORRODED RBL 55-LBL 55, BS 870.SDR AU990031Web · cracked(AUS) WING CENTER SECTION REAR SPAR WEB CRACKED IN THE AREA BETWEEN RBL 12 AND RBL 13. THE CRACK WAS LOCATED JUST BELOW THE TANGENT POINT OF THE MACHINED LAND RADIUS OF THE WEB. CRACK LENGTH 19.05 MM (0.750 INCH). FOUND DURING NDT INSPECTION IAW AD/B727/152SDR 20010426CW001Spar Cap · corrodedFOUND CORROSION ON FORWARD SIDE OF MAIN WING SPAR LOWER CAP BOND ASSEMBLY. THE AFFECTED AREA IS UNDER THE CABIN FLOOR IN THE CABIN. CORROSION DAMAGE FOUND TO REQUIRE REPLACEMENT OF THE SPAR CAP BOND ASSEMBLY.SDR CA980810023Bolt · corroded(CAN) ON 40,000 CYCLES INSPECTION, LOCKBOLTS WERE FOUND FACTORY INSTALLED WITH STEEL WASHERS. 20 ON THE RIGHT SIDE AND 16 ON THE LEFT SIDE. GALVANIC CORROSION HAD STARTED TO DEVELOP. BRAD CONTACTED FOR REPAIR. LOCKBOLTS REMOVED AND WING BOX SKIN TREATED FOSDR GAIA9875Wing Box · corrodedDURING ACCOMPLISHMENT ON AD 85-24-02, RAM AIR PLENUM CORROSION INSPECTION. CORROSION WAS FOUND ALONG THE LEFT SIDE WING BOX CENTER SECTION AT STRINGER 5C. THE CORROSION WAS BLENDING OUT AND A DOUBLER WAS INSTALLED. THE AREA WAS REPAIRED IAW BOEING ENGINEERISDR GAIA9867Wing Box · corrodedDURING ACCOMPLISHMENT OF AD 85-24-02, RAM AIR PLENUM CORROSION INSPECTION. CORROSION WAS FOUND ALONG THE LEFT SIDE WING BOX CENTER SECTION AT STR 4C AND LBL 36.5. THE CORROSION WAS BLENDED OUT AND A DOUBLER WAS INSTALLED. THE AREA WAS REPAIRED IAW BOEING ESDR GAIA9866Wing Box · corrodedDURING ACCOMPLISHMENT OF AD 85-24-2, RAM AIR PLENUM CORROSION INSPECTION. CORROSION WAS FOUND ALONG THE RT SIDE WING BOX CENTER SECTION AT STRINGERS S-3C AND S-4C, RBL 36.5 AND STRINGERS 3C AND S-4C, RBL 20.0. THE CORROSION WAS REMOVED BY BLENDING OUT. THE SDR UPS98826397Web · crackedINSPECTION TYPE-C, UPPER WING BOX AREA AT STA 850 RBL 65, BULKHEAD TO FUSELAGE WEB HAS A 3 INCH CRACK. REMOVED PRESSURE PANEL, FABRICATED REPLACEMENT PANEL AND INSTALLED IAW DWG 5646674.SDR UPS98826396Fitting · crackedINSPECTION TYPE-C, LOWER FUSELAGE EXTERIOR CENTER WING BOX AT STA 704, RBL 3, THE FITTING IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW DWG 4750718.SDR DL72E980585Web · crackedTHE CENTER WING FUEL TANK SPANWISE BEAM NR 1 WEB WAS FOUND CRACKED AT APPROX LBL 3, JUST BELOW THE CHEM-MILL RADIUS. THE RESULTING CUTOUT IS 2.9 (INB'D-OUTB'D) BY 0.5. REPAIRED PER ERA 331472-14.SDR CKSA97379Ctr Wing Box · corrodedDURING ACCOMPLISHMENT OF AD 94-26-09 FOUND LEVEL 2 CORROSION: STA 1000 RT TOP OF CENTER WING BOX CORRODED AT WALL/FUSE. CLEANED CORROSION AND FOUND TO BE OUT OF LIMITS IAW L1011 SRM 51-50-02 FIG 1 AND 2. REPAIRED IAW INSTRUCTION ON SKETCH NBR AIA/E/2563. NSDR ARWA970502Fitting · corrodedMIA - DURING INSPECTION, FOUND LEFT WHEELWELL FORWARD AREA CENTER WING BOX OUTBOARD UPPER AREA SUPPORT FITTING AND AREA FORWARD HAVE LEVEL 2 CORRISION BEYOND LIMITS. REMOVED FASTENERS AND CORRODED MATERIAL. TREATED AND PRIMED AREA. FABRICATED AND INSTALLED SDR RRXA97099Plating · corrosionDURING A MAINTENANCE VISIT, FOUND SKIN CORROSION ON TOP OF CENTER TANK, AT Y=780 & X=+8. AWAITING ON ZANTOP AND COTNEY ENGINEERING TO DETERMINE REPAIR PROCEDURE. *S/D* REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED SPLICE REPAIR IAW DER APPROVED ENGINEERSDR 96FDEA01661Ctr Wing Sect · corrosionSNRM 345. CORROSION FOUND ON TOP OF CTR TANK, BELOW MAIN CABIN FLOOR, LT SIDEWALL AREA, STA 1210. CLEANED CORROSION REF. SRM 57-20-00. COMPLIED WITH HFEC INSP. NO DEFECTS NOTED. MEASURED REMAINING SKIN THICKNESS. REWORKED PER EA 8-5710-31746 WORK INSTRUSDR 96FDEA01645Ctr Wing Section · corrodedSNRM 232, MAIN CABIN, UPPER SURFACE OF CENTER WING SECTION CORROSION AT LT SIDE APPROX STA 1185, SIDEWALL AREA. *S/D* REWORKED PER EA 8-5710-31746 WORK INSTRUCTIONS.SDR 96FDEA01644Ctr Wing Section · corrodedSNRM 227, MAIN CABIN, UPPER SURFACE OF CENTER WING SECTION CORROSION AT LT SIDE APPROX STA 1341, SIDEWALL AREA. *S/D* REWORKED PER EA 8-5710-31746 WORK INSTRUCTIONS.SDR 96FDEA01643Ctr Wing Section · corrodedSNRM 222, MAIN CABIN, UPPER SURFACE OF CTR WING SECTION CORROSION AT RT SIDE APPROX STA 1205, SIDEWALL AREA. *S/D* REWORKED PER EA 8-5710-31746 WORK INSTRUCTIONS.SDR 96FDEA01642Ctr Wing Section · corrosionSNRM 211, MAIN CABIN, UPR SURFACE OF CTR WING SECTION CORROSION AT LT SIDE APPROX STA 1205. *S/D* REWORKED PER EA 8-5710-31746 WORK INSTRUCTIONS.SDR 96FDEA01510Web · corrodedCENTER WING BOX 3RD BAY WEB AT STA 870 RBL 25.08 TO 45.61 POPPED FASTENER. REMOVED CORRODED AREA AND INSTALLED DOUBLER PER EA 7-5771-28858.SDR P5CA9600178Frame · crackedFOUND CRACKED FRAME IN INBOARD LEADING EDGE BETWEEN STA 570 TO 590 AT LOWER CENTER POSITION. REPAIRED IAW SRM 51-40-03.SDR UPS805143Skin · crackedMAINT REPORTED, CRACK AT BOX ROOT AREA LT WING. STOP PER EO DC8-5750-7635C.SDR DL73S954118Floor Beam · crackedDURING LAYOVER AT ATLANTA, THE BL ZERO FLOOR BEAM OF THE WING CENTER SECTION WAS FOUND CRACKED AT STA 662. NO CRACKS WERE FOUND IN THE WEB. THE CRACK IS TYPICAL PER BOEING SERVICE BULLETIN 737-57-1210. REPAIRED DAMAGE PER S/B.SDR DL73S953421Floor Beam · crackedTHE BL0.07 FLOOR BEAM OF THE WING CENTER SECTION IS COMPLETELY CRACKED. THE WEB AND WEB DOUBLER ARE CRACKED APPROXIMATELY 2.0 INCHES IN LENGTH IN THE SAME LOCATION. THE ORIGINAL 65-45410-104 ANGLE IS REINSTALLED TO REPAIR DAMAGE. REPAIRS ACCOMPLISHED PER DLSDR DLL10951817Web · corrodedWEB CORRODED AND PITTED INTERIOR OF CTR WING AT FS 1103, BETWEEN RBL 22 AND RBL 42 WITHIN 4 INCHES OF CTR BOX UPPER SKIN FWD SIDE 4 AREAS OF CORROSION AT FASTENERS. FOUND DURING HMV/CORROSION VISIT. REPAIRED PER SRM 57-11-00 FIG 811.SDR UPS202922Rib · crackedDURING 'D' CHECK, MAINTENANCE FOUND CORROSION AND CRACKS IN FORWARD TWO AND AFT UPPER HOLES AND RIB CHORD AT STATION 760.5 AND RBL 70.5. MAINTENANCE REMOVED AND REPLACED FAIL SAFE STRAP AND T-CLIP AND REPAIRED RIB CHORD PER UPS EO B727-5710-6847A AND UPS EO B
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