JASC 5320
Service difficulty reports · 216,159
Reports filed under 5320 · Fuselage Miscellaneous Structure, 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 = '5320' 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 = '5320' 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 AALA202405203564Floor Support · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT FLOOR STRUCTURE TRANSITION PANEL AT STA 412, S25L. REPLACED TRANSITION PANEL PER AARD 53-00-05.SDR DALA2024050905080Shield · corroded(LOG 0331582) AFT CARGO COMPARTMENT SHIELD FWD OF DOOR HAS CORROSION STA767-787 RBL23 WL160. REMOVED AND REPLACED SHIELD ON AFT CARGO COMPARTMENT FWD OF DOOR STA 767-787 RBL23 WL160 I.A.W B737-800 SRM 51-40-02-0G AND DWG 146A0081 REV A.SDR DALA2024050905078Drain · corroded(LOG 0331556) R2 DOOR MOP SILL HAS CORROSION FROM STA 947-986+ 3" RBL46-RBL55 WL208. REMOVED AND REPLACED R2 DOOR MOP SILL FROM STA 887+6 TO STA 1016 RBL 46-RBL55 WL208 I.A.W B737 SRM 51-40-02-0G AND DWG# 147A5700.SDR DALA2024050805031Strap · crackedSHIP 6700 CRACK ON STABILIZATION STRAP BSTA 350 LBL 45 .CPAX.W1. CORRECTIVE ACTION: SUMMARY OF NRC 00400; STABILIZATION STRAP BSTA 350 LBL 45. CPAX.W1 WAS REPAIRED PER B757-200 SRM 53-00-51-2R PROCEDURE 13 REP. 13 AND B757-200 SRM 53-00-51-2R PROCEDURE 12 REP.SDR DALA2024050805030Floor Support · corrodedSHIP 6700 CORROSION ON FLOOR SUPPORT RH SIDE UNDER FLOOR PANEL 900E AT RBL 64 BTW STA 1000/1040. CORRECTIVE ACTION: SUMMARY OF NRC 00334: CORROSION LEVEL 2: FLOOR SUPPORT RH SIDE UNDER FLOOR PANEL 900E AT RBL 64 BTW STA 1000/1040 WAS REPAIRED PER B757-200 SRM SDR CALA2024050701365Panel · crackedREF AMES NR 170224-0100-0068 GEN ITEM EA 5100-02244 REV G OP 003 ALC PANEL 151AF HAS A CRACKSDR A6WA202405068741Floor Support · corrodedCABIN RH FLOOR SILL SUPPORT PN 601R31133-102 AND PLATE PN 601R31133-101 AT FS559.00 + 85 TO FS559.00 + 116 AND RBL42 TO RBL44 HAS EXFOLIATION CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED CABIN RH FLOOR SILL SUPPORT PN 601R31133-102 AND PLASDR DALA2024050704973Cusp Web · corrodedCORROSION ON CUSP WEB LOWER AND UPPER SIDE STA Y=526 AND Y=571 APPROX X=58 LH SIDE AT PAX CABIN (CPAX). SUMMARY OF NRC 00728: CORROSION LEVEL 2. CUSP WEB STA Y=526 AND X=58 WAS MEASURED ON LIGHTENING HOLE AND MATERIAL REMOVAL IS 0.100IN THERFORE IS WITHIN LIMISDR DALA2024050704972Cusp Web · crackedCRACK ON LOWER SURFACE OD CUSP WEB ON STAY 655 UNDER SEAT TRACK -X44 AT PAX CABIN. SUMMARY OF NRC 00591: CUSP WEB ON STAY 655 UNDER SEAT TRACK -X44 AT CABIN PAX WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #0329495)SDR DALA2024050704971Cusp Web · crackedTWO CRACKS WERE FOUND ON RH CUSP WEB BTW STA Y=715 TO Y=737 AND -X=45 TO -X=60 IN PAX CABIN. SUMMARY OF NRC 00534: RH CUSP WEB BTW STA Y=715 TO Y=737 AND -X= 45 TO -X=60 IN CABIN PAX WAS REPAIRED PER B717 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #0329432)SDR R61A2024050600196Stiffener · crackedDURING INSPECTION: CRACKED CROSS BEAM STIFFNER FOUND ON FWD FUSELAGE COCKPIT FLOOR FR12,LBL 37. REPLACED CRACKED CROSS BEAM STIFFNER ON FWD FUSELAGE COCKPIT FLOOR, FR12, LBL 37 WITH NEW IAW SRM 51-41-01SDR R61A2024050600194Pan · corrodedDURING INSPECTION FWD WET AREA, CORROSION FOUND ON RH FLOOR PAN BETWEEN FR12-FR14, FWD OF SERVICE DOOR. FWD WET AREA, RH FLOOR PAN BETWEEN FR12-FR14 HAS BEEN REPLACED IAW SRM CH 51-43-02, PARA 4, PARA 5 AND IAW SRM CH 51-41-02, PARA 4, PARA 6.SDR SWAA2024061282755Support Angle · crackedCRACK REAR SPAR ON SUPPORT ANGLE LOCATED BS1016 BTW STR3L TO STR3R AT VERTICAL STABILIZER 2024-294662<[01] REPLACED SUPPORT ANGLE LOCATED ON REAR SPAR; BS1016 BTW STR3L TO STR3R AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 176ASDR AALA202406103911Door Sill · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON L2 DOOR ENTRY AREA SILL INNER CHORD (CREASE ANGLE) FROM STA 981 TO STA 974, LBL 48. REPLACED INNER CHORD PER AARD 51-00-05-1.SDR SWAA2024053082766Floor Support · corrodedAFT GALLEY FLOOR STRUCTURE SUPPORT ANGLE AT STA 986.5 +8' APPROXIMATELY 12' I/B OF AFT SERVICE DOOR OPENING HAS SMALL AREA OF SURFACE CORROSION ON FASTENER HOLE. REMOVED CORROSION PER SRM 53-70-51-1A-1. FOUND TO BE OUT OF LIMITS. BLENDED CORROSION ON AFT GSDR DALA2024050905073Channel · corroded(LOG 0331396) R1 DOOR MOP SILL HAS CORROSION FROM STA 294+11"- STA328 RBL58 WL208. INSTALL NEW MOPSILL ON R1 DOOR MOP SILL FROM STA 294+ 11 TO STA 328 RBL 58 WL 208 IAW B737 SRM 51-40-02-0G DWG 141A8310.SDR GTIA2024050738106Door Sill · corrodedINSIDE CABIN AFT WET AREA-R-2 DOOR SILL HAS CORROSION AROUND NUTPLATE HOLE. FR 68 STR 23R-REPAIRED AREA INSIDE CABIN AFT WET AREA R-2 DOOR SILL BEAM FR 68 STR 23R IAW A320 SRM 53-41-14-300-001SDR FDEA202405050581Web · crackedMAIN DECK CARGO UNDER FLOOR WEB FR47 -Y953~-Y1456 FOUND 1EA CRACK REPAIRED THE MAIN DECK CARGO UNDER FLOOR CRACKED WEB FR47 -Y953 ~ -Y1456 PER A300- 600F SRM53-15-15-201 FIG.201. THIS IS A CAT B REPAIR. THE INSPECTION THRESHOLD WAS 24000FC AFTER REPAIR EMBSDR SWAA2024061782257Support Angle · crackedCRACK ON SUPPORT ANGLE AFT POSITION LOCATED BTW BS 907 TO BS 927 AND BTW STR 25R TO STR 27R AT AFT CARGO COMPARTMENT 2024-295399<[01] REPLACED SUPPORT ANGLE AFT POSITION LOCATED BTW BS 907 TO BS 927 AND BTW STR 25R TO STR 27R AT AFT CARGO COMPARTMENT IAW B737-SDR SWAA2024061782258Web · crackedCRACK ON WEB LOCATED BTW BS 927 TO BS 947.5 AT LEVEL STR 25R AT CARGO COMPARTMENT 2024-295400<[01] REPLACED WEB LOCATED BTW BS 927 TO BS 947.5 AT LEVEL STR 25R AT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9 ; SRM 51-40-02 AND DWG 147A7500 REV -. SESDR SWAA2024061782259Angle · crackedCRACK ON ANGLE LOCATED BS 867 AT LEVEL STR 26L AT AFT CARGO COMPARTMENT 2024-295402<[01] REPLACED ANGLE LOCATED BS 867 AT LEVEL STR 26L AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 AND SRM 51-40-02-0G;[02] REPLACED ANGLE LOCATED BS 867 AT LEVEL SDR SWAA2024061782260Web · corrodedCORROSION ON SHEILD WEB LOCATED BTW BS 847 TO BS 867 AT LEVEL STR 25R WL 156.1 AT AFT CARGO COMPARTMENT 2024-295403 CORROSION ON SHIELD WEB LOCATED BTW BS 847 TO BS 867 AT LEVEL STR 25R WL 156.1 AT AFT CARGO COMPARTMENT<[01] REPLACED SHIELD WEB LOCATED BTW BS SDR SWAA2024061782255Web · corrodedCORROSION ON SHEILD WEB LOCATED BTW BS 787 TO BS 767 AT LEVEL STR 25R WL 156.1 AT AFT CARGO COMPARTMENT 2024-295404<[01] REPLACED SHEILD WEB AND FASTENERS LOCATED BTW BS 767 TO BS 787 AT LEVEL STR 25R WL 156.1 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02SDR SWAA2024061702571Fastener · corrodedCORROSION ON SHEILD WEB LOCATED BTW BS 787 TO BS 767 AT LEVEL STR 25R WL 156.1 AT AFT CARGO COMPARTMENT 2024-295404<[01] REPLACED SHEILD WEB AND FASTENERS LOCATED BTW BS 767 TO BS 787 AT LEVEL STR 25R WL 156.1 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02SDR SWAA2024061782261Support · corrodedCORROSION SUPPORT ZEE BTW BS 727 TO BS 807 LBL 22 WL 156.1 AT AFT CARGO COMPARTMENT 2024-295406<[01] REPLACED SUPPORT ZEE AND FASTENERS BTW BS 727 TO BS 847 LBL 22 WL 156.1 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 146A750SDR SWAA2024061702572Support · corrodedCORROSION SUPPORT ZEE BTW BS 727-807 LBL 22 WL 156.1 AT AFT CARGO COMPARTMENT. REPLACED SUPPORT ZEE AND FASTENERS BTW BS 727 TO BS 847 LBL 22 WL 156.1 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 146A7500 SHEET 61 REV -.SDR SWAA2024061782262Support · corrodedCORROSION SUPPORT ZEE BTW BS 727B TO BS 767 RBL 22 WL 156.1 AFT CARGO COMPARTMENT. REPLACED SUPPORT ZEE LOCATED BS 727-767 RBL 22 WL 156.1 IAW SRM 51-40-02; SRM 51-10-02, ITEM 9 AND DWG 146A7500 SHEET 61 REV -.SDR SWAA2024053182344Angle · corrodedFWD CARGO STA 500D TO 500E AT TRANSITION ANGLE ON LEFT SIDE HAS CORROSION AROUND NUT PLATE HOLES.<[01] BLENDED AREAS; REMOVED .010' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. THIS SECTION TO BE REPLACED ON NR# TTG8Q00T572F FROM STA. 480 + 10 TOSDR SWAA2024053182349Angle · corrodedFWD CARGO STA 500E TO 500F AT TRANSITION ANGLE ON LEFT SIDE HAS CORROSION AROUND NUT PLATE HOLES. BLENDED AREAS; REMOVED .023' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. THIS SECTION TO BE REPLACED ON NR TTG8Q00T572F FROM BS 480 + 10 TO 500E +SDR SWAA2024053182601Web · corrodedAFT CARGO THRESHOLD WEB HAS CORROSION IN AND AROUND NUTPLATE HOLES AT NUMEROUS LOCATIONS. REMOVED SURFACE CORROSION AROUND DISCREPANT NUTPLATE HOLE LOCATIONS PER SRM 51-10-02; FOUND TO BE OUT OF ALLOWABLE LIMITS PER SRM 53-60-12-1A-1. MATERIAL REMOVED .010' SDR SWAA2024053082597Web · corrodedAFT CARGO RIGHT INTERCOSTAL WEB AT STRINGER 25R BS 767 TO 787 HAS CORROSION IN AND AROUND NUT PLATE HOLES(MARKED).<[01] 01 - REMOVED AND REPLACED PER [SRM 51-10-02-0G-0-B00070 (GENERAL - INSPECTION AND REMOVAL OF DAMAGE - AIRFRAME - PERMANENT)] REMOVED SURFACESDR SWAA2024053082603Angle · corrodedAFT CARGO RIGHT TRANSITION ANGLE HAS CORROSION IN AND AROUND NUT PLATE HOLES AT BS 747 TO 767. REMOVED SURFACE CORROSION ON AFT CARGO RH TRANSITION ANGLE FROM STA 747 TO 767. REMAINING THICKNESS IS 0.035. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.SDR SWAA2024053082598Angle · corrodedAFT CARGO RIGHT TRANSITION ANGLE HAS CORROSION IN AND AROUND NUT PLATE HOLES AT BS 727J TO 747. REMOVED SURFACE CORROSION ON AFT CARGO RH TRANSITION ANGLE FROM STA 727J TO 747. REMAINING THICKNESS IS 0.032. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.SDR SWAA2024053082604Angle · corrodedAFT CARGO RIGHT TRANSITION ANGLE HAS CORROSION IN AND AROUND NUT PLATE HOLES AT BS 727I TO 727J. REMOVED SURFACE CORROSION ON AFT CARGO RH TRANSITION ANGLE FROM STA 727I TO 727J. REMAINING THICKNESS IS 0.036. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.SDR SWAA2024053082337Web · damagedFWD CARGO DOORWAY THRESHOLD WEB HAS NUMEROUS AREAS OF MISSING PRIMER.<[01] 01 - REMOVED AND REPLACED PER [SRM 51-20-01-0G-0-B00331 (GENERAL - PROTECTIVE TREATMENT OF METALLIC AND COMPOSITE MATERIALS - AIRFRAME - PERMANENT)]PREPPED ;TREATED AND PRIMED THE AREA SDR SWAA2024053082341Angle · corrodedFWD CARGO STA 500A TO 500B AT TRANSITION ANGLE ON LEFT SIDE HAS CORROSION AROUND NUT PLATE HOLES.<[01] BLENDED AREAS; REMOVED .008' MATERIAL. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] C/W INSPECTION CA #1.;[03] REMOVED AND REPLACED L/H TRANSITION ASDR SWAA2024053082343Angle · corrodedFWD CARGO STA 500B TO 500C AT TRANSITION ANGLE ON LEFT SIDE HAS CORROSION AROUND NUT PLATE HOLES.<[01] BLENDED AREAS; REMOVED .012' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. THIS SECTION TO BE REPLACED ON NR# TTG8Q00T572F FROM STA. 480 + 10 TOSDR SWAA2024052982241Angle · crackedCRACK ANGLE LOCATED STA947.5 AND LBL10 AFT CARGO COMPARTMENT 2024-286829<[01] REPLACED ANGLE AND FASTENERS LOCATED BS947.5 AT LEVEL STR26L LBL10 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DRAWING 149A8103 SHEET: 7 REV: A SSDR SWAA2024052982238Strap · damagedELONGATED HOLE STRAP LOCATED BTW STA 847 TO 856 AND RBL18 AT LEVEL FLOOR STRUCTURE AT AFT CARGO COMPARTMENT 2024-286831<[01] REPLACED STRAP LOCATED BTW STA 847 TO 856 AND RBL18 AT LEVEL FLOOR STRUCTURE AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND SRMSDR SWAA2024052982239Strap · damagedELONGATED HOLE STRAP LOCATED BTW STA 794.3 TO STA 807 RBL18 AT LEVEL FLOOR STRUCTURE AT AFT CARGO COMPARTMENT 2024-286832<[01] REPLACED STRAP LOCATED BTW STA 794.3 TO STA 807 RBL18 AT LEVEL FLOOR STRUCTURE AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02-0SDR SWAA2024052982551Angle · crackedCRACK BRACKET ANGLE LOCATED BS 540 PLUS 3 INCHES LBL18 AT AIR CONDITIONING BAY. REPLACED THE BRACKET ANGLE IAW SRM 51-10-02 ITEM 9 AND SRM 51-40-02. CRACK LENGTH IS: 0.367.SDR AALA202405245364Shield · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT FLOOR STRUCTURE SHIELD LOCATED FROM STA 767 TO STA 787, S25R. REPLACED SHIELD PER AARD 51-00-05-1.SDR AALA202405244516Angle · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT FLOOR STRUCTURE TRANSITION PANEL CLIP AT STA 767, S25R. REPLACED CLIP PER AARD AARD 51-00-05.SDR AALA202405214839Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT TRANSITION PANEL FROM STA 727H TO STA 727I, RBL 24. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.SDR AALA202405218692Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT TRANSITION PANEL FROM STA 727G TO STA 727H, RBL 24. REPLACED TRANSITION PANEL PER ARM 53-00-53.SDR AALA202405202612Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT FLOOR STRUCTURE TRANSITION PANEL FROM STA 727 TO STA 767, S25R. REPLACED TRANSITION PANEL PER AARD 51-00-05.SDR AALA202405203733Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT FLOOR STRUCTURE TRANSITION PANEL FROM STA 727 TO STA 767, S25R. REPLACED TRANSITION PANEL PER AARD 51-00-05.SDR AALA202405201163Floor Support · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT FLOOR BOARD SUPPORT FROM STA 787 TO STA 807, LBL 6. REPAIRED FLOOR BOARD SUPPORT PER SRM 53-00-53.SDR AALA202405209078Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT FLOOR STRUCTURE TRANSITION PANEL FROM STA 727 TO STA 767, S25R. REPLACED TRANSITION PANEL PER AARD 51-00-05.SDR AALA202405208803Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT FLOOR STRUCTURE TRANSITION PANEL FROM STA 727F TO STA 727G, RBL 24. REPLACED TRANSITION PANEL PER AARD 51-00-05.
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