JASC 5350
Service difficulty reports · 6,121
Reports filed under 5350 · Aerodynamic Fairings, 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 = '5350' 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 = '5350' 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 AALA202403195459Tail Cone · corrodedAIRCRAFT IN BASE MAINTENANCE: EXFOLIATION CORROSION IN THE ADVANCED STAGE OF DETERIORATION FOUND ON THE RIGHT HAND SIDE OF THE UPPER FORWARD TAIL CONE. LOCATED AT AFT OF RUB STRIP AND JUST UNDER HORIZONTAL STAB. REPAIRED PER AARD 11-20-00-1 REPAIR 1.SDR AALA202403155459Tail Cone · deterioratedAIRCRAFT IN BASE MAINTENANCE: EXFOLIATION CORROSION IN THE ADVANCED STAGE OF DETERIORATION FOUND ON THE RIGHT HAND SIDE OF THE UPPER FORWARD TAIL CONE. LOCATED AT AFT OF RUB STRIP AND JUST UNDER HORIZONTAL STAB. Ï¿½ **SUPPLEMENTAL REPORT WILL BE SUBMITTED**(OPSDR DALA2024031203274Fairing · degradedSHIP 5810 -DIV- TO MEM DUE TO VIBRATION FELT IN CABIN. FOUND LEFT OVERWING TO BODY PANEL SEAL DEGRADED. PERFORMED TIME LIMITED REPAIR. R/R LH WING TO BODY FAIRING OVERWING PANEL 191DL SEAL REF ERA 616536-14, REV ORG, SEC III PERMANENT REPAIR.SDR SWAA2024031161273Radome · delaminatedON THE NOSE CONE IF FACING THE AIRCRAFT FROM THE FRONT AT THE 11 OCLOCK POSITION THERE APPEARS TO BE SUBSTANTIAL DELAMINATING WHERE THE LIGHTNING STRIP ATTACHES TO THE NOSE CONE. THE WEAR AND TEAR IS SIGNIFICANTLY MORE THAN THE PAINT FADING IN THE SURROUNDING SDR DALA2024030803186Release Cable · out of limitsTHE KEVLAR CABLE FOR THE TAIL CONE EMERGENCY EXIT RELEASE IS TORN BEYOND ALLOWABLE LIMITS. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REPLACED THE TAILCONE JETTISON KEVLAR CABLE REF SDR VNAA202404080009Strap · crackedCRACK ON STRAP AT FAIRING PANEL 196DR. STRAP AT FAIRING PANEL 196DR WAS REPAIRED PER REO 690-53-82-052 REV. --SDR JR2R20240302397Frame · crackedLH SIDE MAIN WING STUB BOX FR52 WING TO BODY CRACKED. REPAIRED PER SRMSDR SWAA2024041557779Fairing · delaminatedWING TO BODY PANEL 193CL EDGE IS DELAM<[01] REMOVED DAMAGE IAW B737 SRM 53-40-70-2R-1;[02] REPAIRED DAMAGED PANEL 193CL IAW B737 SRM 53-40-70; 51-70-05.;[03] 04 - REPAIRED PER [SRM 53-40-70-2R-1-B00375 (REPAIR 1 - SECTION 44 WING-TO-BODY FAIRING SKIN PANELS MASDR SWAA2024031958141Fairing · delaminatedFAIRING 194BR IS DELIMITED MARKED FAIRING PANEL 194BR IS DELAMINATED MARKED<[01] DELAMINATION ON FAIRING 194BR WAS REPAIRED IAW SRM 51-70-05-2R-10.;[02] VERIFIED FAIRING 194BR WAS REPAIRED IAW SRM 51-70-05-2R-10.SDR YENA2024030500312Skin · dentedDURING HEAVY MAINTENANCE:FUSELAGE / REAR / TAILCONE/DENT BTWN FRAME 78-80 BETWEEN LH STR 1 AND 2 SPLICE - PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)SDR YENA2024022900301Tail Cone · dentedDURING HEAVY MAINTENANCE: FUSELAGE / REAR / TAILCONE/DENT BTWN FRAME 78-80 BETWEEN LH STR 1 AND 2 SPLICE - PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)SDR VNAA202404160013Channel · crackedWING/FUSELAGE FAIRING, RH (PANEL 196DR) SUPPORT CHANNEL HAS A 1.33" CRACK, 7.4" FROM FWD END OF CHANNEL. PN:BA690-39311-1.SDR SCNA20240401171Support · corrodedAFT WING TO BODY FAIRING SUPPORTS PANEL AT STA 727 + 2.7 BETWEEN BL"0" AND LBL 25" AND BETWEEBN BL "0" AND RBL 25" WITH CORROSION (2EA). REPLACED SUPPORT FRAMESSDR DALA2024030102891Radome · dentedSHIP 3128 DENTED RADOME RH SIDE AT LOWER FUSELAGE. CORRECTIVE ACTION: REPLACED RADOME PER A319 AMM 53-51. (0219762)SDR DALA2024022702759Fairing · crackedSHIP 3128 CRACK BELLY FAIRING STRUCTURE WEB LH SIDE LOCATED AT FR 52 AT LOWER FUSELAGE. CORRECTIVE ACTION: REPAIRED PER ER/A 615516-14. (0219747)SDR SWAA2024022655688Radome · out of limitsNOSE RADOME OUT OF LIMITS<[01] RR NOSE RADOME ASSY PER AMM 53-52-00.SDR SWAA2024030754502Boot · crackedNOSE RADOME BOOT HAS MULTIPLE CRACKS AND HOLES EXPOSING COMPOSITE UNDERLAYER<[01] REMOVED AND REPLACED RADOME PER AMM 53-52-00;[02] 02 - INSPECTED PER [AMM 53-52-00-400-801-NG (NOSE RADOME INSTALLATION - PERMANENT)]SDR SWAA2024022053276Radome · crackedDURING LIGHTNING STRIKE CONDITIONAL INSPECTION: MULTIPLE CRACKS AND PIN HOLES ON NOSE AND BOTTOM STRIP OF THE RADOME<[01] REMOVED AND REPLACED RADOM PER AMM 53-52-00.;[02] C/WSDR DALA2024021201954Fairing · crackedSHIP 3124 CRACK WEB BELLY FAIRING AT LEVEL FR52 LH SIDE AT LOWER FUSELAGE. CORRECTIVE ACTION: REPAIRED PER ER/A 615016 -14. (0196222)SDR IPXA2024020609795Tail Cone · damagedRH FWD UPPER TAIL CONE PATIO DOOR DAMAGED C/W EO-89416-REQ1. FINISHED CLOSING UP THE TAILCONE IAW AMM 53-52-01.MATCH DRILLED EXTRUSION. INSTALLED EXTRUSION AND SEAL RETAINER REF SRM 51-35-01.SDR IPXA2024021805797Tee Angle · corrodedFAULT: AFT FUSELAGE WTB FAIRING T CHORD SUPPOR AT STA 1240 R/H HAS CORROSION INSTALLED T-CORD SUPPORT AT STA 1240 R/H IAW B757-200 SRM 51-70-12-0G-0, FIG 1. AUDIT COMPLETE.SDR IPXA2024021789430Tee Angle · corrodedFAULT: WING TO BODY T CHORD SUPPORT STA 1200 R/H HAS CORROSION INSTALLED T CHORD SUPPORT STA 1200 IAW B757-200 SRM 51-40-02 REVIEWEDSDR IPXA2024021589259Support · corroded*** SDR FILED OPEN *** FAULT: WING TO BODY T CHORD SUPPORT AT STA 1220 R/H IS CORRODED AUDIT COMPLETESDR CALA2024020700340Radome · damagedLIGHTNING STRIKE APPEARED TO BE ON RIGHT NOSE AREA.TOMC CONSULTED NO DAMAGE NOTED LIGHTNING STRIKE INSPECTIONS CARRIED OUT AS PER AMM 05-51-19 PHASE 1A, 1B AND PHASE 2. FINDINGS RAISED IN LOGBOOK REFER TO LP''S 6972633, 6972329,6973095, 6972860, 6972725, & 697SDR SWAA2024020547859Panel · damagedWING TO BODY PANEL 193B HAS NUMEROUS ELONGATED HOLES.<[01] REPLACED 193B PANEL REF AMM 53-51-21SDR IPXA2024021960150Tee Angle · corrodedEVIDENCE OF CORROSION BEHIND PANEL 198LR ON FUSELAGE. INSTALLED T CHORD BEHIND PANEL 189 IAW B757-200 SRM 51-40-02. INSTALLED PANEL 198LR IAW B757-200 SRM 51-40-02. AUDIT COMPLETE.SDR SWAA2024020546666Panel · debondedFUSELAGE BODY PANEL #193B IS CHAFED AND DISBONDED AROUND FASTENER HOLES<[01] LOCATE AND DRILLED A NEW PANEL 193B PER SRM 51-40-02.SDR DALA2024012901332Radome · crackedSHIP 6817 COMPLY WITH ER/A 615106-14 REV A DURING ANTENNA AND RADOME IDTV REMOVAL MTC FOUND FOUR HOLES WITH CRACK INDICATIONS. CORRECTIVE ACTION: COMPLIED WITH ER/A 615106-14 REV A REFERENCE LOG # 0166433. (0176275)SDR DALA2024012901334Radome · crackedSHIP 6817 DURING ANTENNA AND RADOME, IDTV REMOVAL, MTC FOUND FOUR HOLES WITH CRACK INDICATIONS. DTE, ER/A 615106-14 - SECTION I REPAIR REQUIRES DTE WITHIN 12 MONTHS OF AIRCRAFT RETURN TO SERVICE. CORRECTIVE ACTION: REF ERA 615106-14. (0173520)SDR DALA2024012501111Fairing · damagedSHIP 3161 1 BY 1 HOLE IN COMPOSITE FAIRING JUST BELOW REFUEL PANEL ON BELLY OF A/C RT SIDE PANEL 192KB. CORRECTIVE ACTION: REPAIRED PANEL PER SRM 53-35-11-300-007. (0170481)SDR DALA2024012401095Longeron · crackedWHILE PERFORIMING W/C 5352-01038-01A WTBF INSP FOUND APPROX 3 INCH CRACK IN LEFT LONGERON ON BOTTOM FLANGE. AD RELATED. REMOVED 2 EA O/B FILLET PANELS L/H SIDE.(309252) REMOVED AND BEGAN DRILLING LONGERON PER WORKCARD 5352-01038-07A (373696) LONGERON SOFT MOUNSDR IPXA2024030778103Longeron · corroded*MAJOR REPAIR* (STR) RH FUSELAGE BODY FAIRING AREA STA 1305 EXTERNAL "T" BAR LONGERON HAS CORROSION. 74-127 ACCOMPLISHED REPAIR PER EA 011-5310-01-B0156 REV I/R AND UPS EO-89562-REQ1 REV1. REVIEWEDSDR SWAA2024020543680Panel · crackedCRACK - AT UPPER AFT CORNER (PANEL 192BR FAIRING- UNDERWING RIGHT FAIRING ABOVE A/C DOOR)<[01] REPAIRED PANEL #192BR AT DAMAGD AREA PER B737 SRM 51-70-04-2R-2; SRM 51-70-04-2R-0 PARA 4.L.7. MATERIALS USED RESIN P/O#1791128; CLOTH P/O#1690463; GRAPHI P/O#204306SDR SWAA2024012242897Fairing · delaminatedWING-TO-BODY FAIRING PANEL 194CL HAS PUNCTURE DAMAGE WITH DELAM IN OUTER SKIN. -MARKED-<[01] REMOVED AND REPLACED PANEL 194CL IN REF WITH AMM 20-50-11.SDR SWAA2024012242899Panel · delaminatedWING-TO-BODY FAIRING PANEL 194CR HAS TWO PUNCTURE DAMAGED AREAS WITH DELAM. -MARKED-<[01] REMOVED AND REPLACED 194CR PANEL IN REF WITH AMM 20-51-11 AND TASK CARD 5351-E-16723-NG.SDR SWAA2024012242898Fairing · pulledWING-TO-BODY FAIRING PANEL 193AR SEVERAL SCREWS PULLED THROUGH AT THE IB END OF PANEL.<[01] REMOVED AND REPLACED 193AR PANEL IN REF WITH AMM 20-51-11 AND TASK CARD 5351-E-16723-NG.SDR SWAA2024012242900Fairing · pulledWING-TO-BODY FAIRING PANEL 194CR HAS A SCREW PULLED THROUGH AT THE FWD IB MOST CORNER.<[01] REMOVED AND REPLACED 194CR PANEL IN REF WITH AMM 20-51-11 AND TASK CARD 5351-E-16723-NG.SDR SWAA2024012242901Fairing · bulgedWING-TO-BODY FAIRING PANEL 193AR HAS TWO BULGED AREAS IN EXTERIOR SKIN WITH TAP TEST SOUND OF DELAM. -MARKED-<[01] REMOVED AND REPLACED 193AR PANEL IN REF WITH AMM 20-51-11 AND TASK CARD 5351-E-16723-NG.SDR SWAA2024013042679Support · crackedFWD L/H FAIRING SUPPORT FOR PANEL 192E IS CRACKED<[01] REMOVED AND REPLACED SUPPORT BRACKET P/N 149A7712-41 PER SRM 51-40-02 AND DWG 149A7701;[02] VERIFIED MEASUREMENT FIELD.SDR IPXA2024011791927Fairing · punctured*** SDR FILED OPEN *** PUNCTURE IN THIRD WING TO BODY FAIRING PANEL AFT OF RH BODY GEAR 194DL REMOVED FOD. DAMAGE IS 1/4" IN DIAMETER APPROXIMATELY 10' AFT OF FWD EDGE. TAP TEST FOR DELAM. NONE NOTED. DAMAGE IS WITHIN DEFERRABLE LIMITS PER SRM 53-00-70-1A-1 DESDR SWAA2024022241604Access Panel · crackedCRACK ACCESS PANEL 191D BODY FAIRING AT LOWER FUSELAGE 2024-61171<[01] TOOL USED: CALIPER P/N:500-197-30 S/N:15120589 DUE DATE: 13-FEB-24.;[02] TOOL USED: HOT BONDER PN: HCS9200B; SN: 15102320; DUE DATE: 25-JAN-25.;[03] TOOL USED: SCALE PN: CR5200; SN: 8343110SDR NACA2024011700002Fairing · damagedIMPACT DAMAGE FOUND AT LH AFT WING/BODY FAIRING 195PL, STA 1222-1230, WL-160. COMPLETED TEMP REPAIR PER NAC EO 767-53-0040. DVI OF TAPE ONCE PER FLIGHT DAY, REPLACE IF DETERIORATED. ONCE PER WEEK TAP TEST, ANY GROWTH IN DAMAGE MUST NOTIFY NAC ENGINEERING.SDR DALA2024011200547Unknown · unknownSHIP 697 CORROSION ON FAIRING SUPPORTS (2EA) BTW STA 860 TO STA 900 BL0 AND LBL25 AT BODY FAIRING SUPPORT. CORRECTIVE ACTION: SUMMARY OF NRC 00293: FAIRING SUPPORTS (2EA) BTW STA 860 TO STA 900 BL0 AND LBL25 AT BODY FAIRING SUPPORT.WERE REPLACED PER B757-200 SSDR IPXA2025030469862Tail Cone · damagedTAIL CONE R/H FWD UPPER PRODUCTION DOUBLER IS DAMAGED. FABRICATED REPAIR FILLER, AND TREATED AND PRIMED IAW SREO-66790-REQ002 REV 1 OK TO INSTALL REPAIR FILLER. WORK ACCOMPLISHED ON SREO-66790-REQ002 REV1, T3F18E003QKC3, LINE 1307.SDR IPXA202401174392Radome · crackedRADOME HAS 2 CRACKS TOTALING 18 INCHES LONG. R/R RADOME IAW AMM 53-10-61/ 401. ADJUSTMENTS AND CHECKS GOOD.SDR SWAA2024011539650Bracket · crackedCRACK ACCESS PANEL 192CR BODY FAIRING AREA ON BRACKET IN APU DUCT AT LOWER FUSELAGE 2023-758510<[01] REPLACED BRACKET LOCATED ON PANEL 192CR BODY FAIRING AREA IN APU DUCT AT LOWER FUSELAGE IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 ; MEASURES OF CRACK ISDR IPXA2024011169862Unknown · unknownTAIL CONE R/H FWD UPPER PRODUCTION DOUBLER IS DAMAGED. OK TO WORKSDR IPXA2024011174392Unknown · unknownRADOME HAS 2 CRACKS TOTALING 18 INCHES LONG.SDR DALA2024011100502Unknown · unknownWORKING AD RELATED WORK CARD 5352-01038-01B FOUND LONGERON P/N C02383111-001 AT LBL 4010 CRACKED FROM FRAME C02383123-001 TO FRAME C02383037-001 25" ALONG THE NUT PLATE FLANGE THEN VERTICAL 1.5" FROM FRAME 02383037-001 UP 2.25" FROM NUT PLATE FLANGE. REMOVED SSDR IPXA2024032049912Fairing · crackedRH BODY FAIRING UPR AREA STA 1341 STRUCTURAL FRAME HAS CRACKED. 74-089 TREATED AND PRIMED REPAIR PARTS IAW MD11 SRM 51-21-01-OG-0 PARA 26-33. REINSTALLED RIB ON R\H BODY FAIRING UPR AERA STA 1341 IAW MD11 SRM 51-35-01-OG-0
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