JASC 5300
Service difficulty reports · 8,206
Reports filed under 5300 · Fuselage Structure (General), 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 = '5300' 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 = '5300' 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 EIA2003018StrapLap repairs from STA 1460-2180 at Stringer 19R requires an additional strap. CORRECTIVE ACTION: Install external strap per ECRA 481-53-169-2 Rev ASDR EIA2003017BeltframeCracked frame at STA 1740. Stringer 4 left. CORRECTIVE ACION: Repaired cracked frame at STA 1740 stringer 4 left per ECRA 481-53-173-2SDR EIA2003036SpliceMAIN CABIN L/H INTERIOR CORROSION ALONG SKIN LONGITUDINAL SPLICE AT STRINGER 19L, BS 1960 to 2180. CORRECTIVE ACTION: REMOVED DAMAGE, NDT & VISUAL INSPECTION, FAB'D AND INSTALLED REPAIR PER ECRA 481-53-169-2 Rev ASDR EIA2003035SpliceFUSELAGE RIGHT SIDE INTERIOR CORROSION ALONG SKIN LONGITUDINAL SPLICE AT STRINGER 19R, FROM STA 1760-2180 CORRECTIVE ACTION: REMOVED DAMAGE, NDT AREA & VISUALLY IINSPECT, FAB'D AND INSTALLED REPAIR PER ECRA 481-53-169-2 Rev ASDR C2XA03SH031Strap · crackedSHV-DURING C CHECK A SPLICE ANGLE ON THE CENTER BEAM TO BUTTSTRAP BETWEEN FRAMES 14 AND 16 WAS FOUND CRACKED. MAINTENANCE PERFORMED AN ANGLE SPLICE REPAIR TO AFFECTED BEAM IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR DHL2003367513Skin · dentedItem Ref. N/R 0029727:External skin at STA. 4925 dented at six oclock position. Corrective action:Removed damaged area IAW A300 SRM 53-10-10 mat. ID IAW A300 SRM 53-10-10 fabbed doubler IAW A300 SRM 53-10-10 alodined an primed filler IAW SRM 51-40-12. InstalleSDR DHL2003367510Doubler · corrodedItem Ref. N/R 0029435:AT lower fusl. skin around static drain ports is corroded. Corrective action: Removed existing repair doubler and fab new 2 ea. mat. ID 2024T3 .071 treated and primed and installed it IAW A300 SRM 51-30-30,mat. ID IAW A300 SRM 53-10-10 alSDR EIA2003020BeltframeR/H STA 1740 between Stringer 12R & 13R frame bent and gouged. CORRECTIVE ACTION: Repaired R/H STA 1740 Frame @ Sringer 12R- 13R per ECRA 481-53-176-2SDR EIA2003015Skin PanelR/H Lower fuselage at STA 400, lower lap skin has evidence of damage and corrosionCORRECTIVE ACTION: Repaired area per ECRA 481-53-182-2SDR EIA2003013Support FittingL/H Main Gear Wheel @ STA 1241 BL) to 43" WL 175" (approx) longitudinal support fitting has two double drilled holes (1 ea) in the flanges. CORRECTIVE ACTION: Complied with ECRA # 481-53-190-2 (Removed & Replaced Support Fitting)SDR EIA2003012Skin PanelImproper Fastener on lap Seam at STA. 615 and S-47R on Fuselage below FWD. Lower Cargo Compt. CORRECTIVE ACTION: Removed fastener and existing doubler, cut overlapping skin, requested NDT, fabricated, alondined, primed and installed -1 repair doubler and -2 fSDR EIA2003011Skin PanelExternal Skin Repair, at Station 1580 Stringer 35L to 36L is not per S.R.M. CORRECTIVE ACTION: Removed external skin repair, fabricated new fillers,(2 ea.) and doubler. Alodined, primed and installed per Boeing SRM 51-30-03, Page 2A-2F, and SOPM Ch. 20-41-0SDR EIA2003010StiffenerSTIFFENER CRACKED AT STA 291, LBL 10 ON TOP OF NOSE WHEEL WELL BO. CORRECTIVE ACION: INSTALLED KIT # 65B28266-5 AND SUB KIT 65B28266-6 PER E.O. 53-747-1138-91 REV C, PER S.B. B747SRM 51-30-02 PGS 1-15SDR ABXA030112Longeron · crackedLONGERON 17 RIGHT CRACKED AT STA. 389, APPROXIMATELY 1/4" LONG. INSTALLED NEW FABRICATED LONGERON (P/N 2777922-1) AND SPLICE (P/N 7637813-3) IAW DC-9 SRM 53-02.SDR EIA2003034Door FrameBULK PIT DOOR CUT OUT HAS BENT AND GOUGED EDGE APPROXIMATELY 14 IN. UP FROM FORWARD LOWER CORNER. CORRECTIVE ACTION: REMOVED DAMAGE, NDT & VISUAL INSPECTION OF AREA, FAB'D AND INSTALLED REPAIR PER ECRA 481-53-157-2 Rev ASDR C2XA03SH023Beam · corrodedSHV-DURING C-CHECK THE LEFT HAND OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25.MAINTENANCE REMOVED THE DAMAGED SECTION OF THE OMEGA BEAM AND INSTALLED A REPAIR DOUBLER IAW EMB 145 SRM 53-21-10.THE AIRCRAFT WAS APPROVED FOR RETURN TO SEVICE.SDR C2XA03SH024Beam · corrodedSHV-DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25.MAINTENANCE REMOVED THE DAMAGED SECTION OF THE OMEGA BEAM AND INSTALLED A REPAIR DOUBLER IAW EMB 145 SRM 53-22-10.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03SH025Beam · corrodedSHV-DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 17 AND 24.MAINTENANCE REMOVED AND REPLACED THE AFFECTED OMEGA BEAM IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03SH026Beam · corrodedSHV-DURING C-CHECK CARGO DOOR CUT OUT LOWER BEAM WAS FOUND TO HAVE CORROSION.MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-06.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03SH027Butt Strap · corrodedSHV-DURING C-CHECK BUTT STRAP BETWEEN FRAMES 18 AND 23 WAS FOUND TO HAVE CORROSION.MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03SH028Angle · corrodedSHV-DURING C-CHECK RAMP ANGLE ON CENTER OMEGA BEAM BETWEEN FRAMES 18 AND 20 WAS FOUND TO HAVE CORROSION.MAINTENANCE REMOVED AND REPLACED THE AFFECTED RAMP ANGLE IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03SH029Butt Strap · corrodedSHV-DURING C-CHECK LEFT HAND BUTT STRAP BETWEEN FRAMES 19 AND 23 WAS FOUND TO HAVE CORRSION.MAINTENANCE REMOVED AND REPLACED AFFECTED BUTT STRAP IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR EIA2003014BeltframeFrame Cracked STA 340 1" below Sringer 16 left. CORRECTIVE ACTION: Repaired per ECR # 481-53-175-2SDR EIA2003008Frame · crackedFRAME CRACKED STA 340, 1 INCH BELOW STRINGER 16 LEFT. REMOVED DAMAGE, FABRICATED DOUBLER -2 DOUBLER, FILLER-4 DOUBLER, PER ECRA 481-53-1752 & 51-10-02 PG 7, SOPM PER 20-41-02 PG 10SDR C2XA03SH022Strap · corrodedSHV-DURING C-CHECK THE LEFT HAND STRAP AT FRAME 61 WAS FOUND TO BE CORRODED.MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRAP IAW EMB 145 SRM 53-31-19 AND 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03SH021Sill · corrodedSHV-DURING C-CHECK THE RIGHT HAND SILL BETWEEN FRAMES 18 AND 20 WAS FOUND TO BE CORRODED.MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03SH020Sill · corrodedSHV-DURING C-CHECK THE RIGHT HAND SILL AT FRAME 61 WAS FOUND TO BE CORRODED.MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03SH010Sill · corrodedSHV-DURING C-CHECK THE LEFT HAND SILL WAS FOUND TO BE CORRODED AT FRAME 61.MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03SH019Crossbeam · corrodedSHV-DURING C-CHECK THE CROSSBEAM AT FRAME 61 BETWEEN THE LEFT HAND SILL AND THE LEFT HAND FLOOR BEAM WAS FOUND TO BE CORRODED.MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03SH018Crossbeam · corrodedSHV-DURING C-CHECK THE CROSSBEAM AT FRAME 61 BETWEEN THE LEFT HAND AND CENTER FLOOR BEAMS WAS FOUND TO BE CORRODED.MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03SH017Crossbeam · corrodedSHV-DURING C-CHECK THE CROSSBEAM AT FRAME 61 BETWEEN THE CENTER AND LEFT HAND FLOOR BEAMS WAS FOUND TO BE CORRODED.MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03SH016Crossbeam · corrodedSHV-DURING C-CHECK THE CROSSBEAM AT FRAME 61 BETWEEN THE CENTER AND RIGHT FLOOR BEAMS WAS FOUND TO BE CORRODED.MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03SH015Crossbeam · corrodedSHV-DURING C-CHECK THE CROSSBEAM AT FRAME 61 BETWEEN THE RIGHT SILL AND RIGHT FLOOR BEAM WAS FOUND TO BE CORRODED.MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03SH014Butt Strap · corrodedSHV-DURING C-CHECK THE CENTER BUTT STRAP BETWEEN FRAMES 59 AND 61 WAS FOUND TO BE CORRODED.MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB 145 SRM 51-40-01.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03SH013Butt Strap · corrodedSHV-DURING C-CHECK THE RIGHT HAND BUTT STRAP AT FRAME 61 WAS FOUND TO BE CORRODED.MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03SH012Butt Strap · corrodedSHV-DURING C-CHECK THE RIGHT HAND BUTT STRAP WAS FOUND TO BE CORRODED BETWEEN FRAMES 59 AND 61.MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03SH011Butt Strap · corrodedSHV-DURING C-CHECK THE LEFT HAND BUTT STRAP WAS FOUND TO BE CORRODED AT FRAME 61.MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB 145 SRM 51-40-02.THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03SH009Butt Strap · corrodedSHV-DURING C CHECK AFT BUTT STRAP AT FRAME 17 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED THE AFFECTED AFT BUTT STRAP IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR ABXA030103Spacer · crackedVERT. STAB. RIGHT ATTACH ANGLE WAS CRACKED BELOW RAM AIR OPENING. REPAIRED IAW DC-9 SRM 53-05.SDR DHL2003804537Skin · crackedITEM REF N/R 2660; iterim repair on fwd lwr. corner of the aft pax entry door ref srm53-2-0 pgs. 125/126 fig. 18 sheet 2m (major repair) corr: performed major repair iaw srm53-2-0 fig 18 , removed interim repair from aft pax entry door fwd. lwr. corner iawSDR C2XA03SH005Support · corrodedSHV-DURING C CHECK THE CENTER FLOOR BEAM RAMP ANGLE SUPPORT WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR CXA03SH002Gusset · corrodedSHV-DURING C CHECK FOWARD FLOOR GUSSET WAS FOUND TO HAVE NUMEROUS AREAS OF CORROSION AND GOUGING. MAINTENANCE REMOVED DAMAGE AREAS AND PERFORMED A SPLICE REPAIR IAW EMB 145 SRM 51-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA03SH001Gusset · corrodedSHV-DURING C CHECK THE AFT FLOOR GUSSET WAS FOUND TO HAVE NUMEROUS AREAS OF CORROSION AND GOUGING. MAINTENANCE REMOVED AND REPLACED THE AFFECTED GUSSET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA03BT029Skin · dentedBTV---CO2002, MAJOR REPAIR WAS PERFORMED AFT OF MAIN CABIN DOOR BETWEEN STRINGER 12L AND 13L AND FRAME 18 AND FRAME 20, HAD DENT (OUT OF LIMITS), DENT REPAIRED IAW EMB145 SRM #53-21-01. SEAL AND PAINTED IAW EMB145 SRM CHAPTER #51. PRESSURIZATION CHECK PERFORMESDR DHL2003804541Fitting · crackedITEM REF. N/R 1308 AFT CARGO COMPT.- FITTING CRACKED @ STA 1320 , L31L (MAJOR REPAIR) CORR: PERFORMED MAJOR REPAIR IAW 53-1-0 PG 1 AND BOEING FAX SEU-LIM-03-0002H DATED JAN 20TH , 2003 REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21, CLEANED , TREATED AND PRIMESDR ABXA030092Former · crackedSHEAR TIE AT F.S. 1019, LONGERON 14 - 15 LEFT, CRACKED. REPLACED SHEAR TIE IAW DC-9 SRM.SDR ABXA030091Shear Tie · crackedSHEAR TIE AT F.S. 1019, LONGERON 14 - 15 RIGHT, CRACKED. REPLACED SHEAR TIE IAW DC-9 SSRM K05159.SDR SWAA030258Tie Clip · crackedDURING SCHEDULED SPECIAL VISIT, FOUND TIE CLIPS CRACKED (2 EA) AT STR 4L, BS 727B AND BS 807. REMOVED AND REPLACED TIE CLIPS PER SRM.SDR AWXA200300101Structure · vibrationLAS - EMERGENCY LANDING - FLT 0048 - ON APPROACH INTO LAS EN ROUTE FROM DCA WITH FLAPS AT 5, LANDING GEAR DOWN, AND SPEED BRAKES ARMED, A VIBRATION DEVELOPED THROUGHOUT THE AIRCRAFT. HYDRAULICS AND ENGINE INDICATIONS APPEARED NORMAL, AND AIRCRAFT CONTROL WAS NSDR ABXA030090Doubler · corrodedCORROSION ON RIGHT WHEEL WELL UPPER PRESSURE PANEL DOUBLER STATION 722, RIGHT BUTT LINE 56. FABRICATED NEW DOUBLER IAW DWG #9910155 AND DC-9 SRM.
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