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 AALA202406176628Shield · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT TRANSITION SHIELD FROM STA 847 TO STA 867, S24R. REPLACED TRANSITION SHIELD PER AARD 51-00-05-1.SDR ASAA2024052950230Baffle · crackedFWD PIT, L/H BAFFLE CLIP AT STA 500G AFT SIDE IS CRACKED. GROUNDED - YES. REMOVED & REPLACED FWD PIT, L/H BAFFLE CLIP AT AT STA 500G WITH PN: 143A 7502-159 PO: 1092414.1 IAW B737-800 SRM 51-40-02 & SRM 51-40-05.SDR SWAA2024061391070Panel · crackedFOUND PANEL BRAKE CRACKED AT STA 537.45 BL 0 TO RBL 24.75 FOUND PANEL BREAK CRACKED AT MAIN CABIN STA 537.45 BL0 TO RBL 24.75<[01] REMOVED AND REPLACEDPANEL BRAKE AT STA 537 BL0 TO RBL24.75 PER SRM 51-40-02 AND DWG 143A5240;[02] CORRECTION: REMOVED AND REPLACESDR JJBA20240611017Floor Support · crackedLH OMEGA BEAM #5 FOUND CRACKED AT FR 39. LH OMEGA BEAM #5 CRACK AT FR39 REPAIREDSDR JJBA20240610016Support Plate · corrodedRF1, ABOVE FLOOR, LH SUPPORT PLATE AT FR61 FOUND CORRODED AT FLOOR LEVEL. AT RF1, ABOVE FLOOR LH SUPPORT PLATE AT FR61 BLENDED AND FOUND OUT OF LIMIT AND REMOVED FOR REPLACEMENT. AT RF1, ABOVE FLOOR, LH SUPPORT PLATE AT FR61 REPLACEDSDR FDEA202405290783Floor Support · corrodedMAIN DECK FLOOR STRUCTURE SUPPORT UPPER SURFACE WAS FOUND CORROSION AT FR11 PLUS14"~FR11 PLUS 16", Y730 REPLACED THE DAMAGE SUPPORT WITH NEW AT MAIN DECK FLOOR STRUCTURE SUPPORT SURFACE FR11 PLUS 14" ~FR11 PLUS 16", Y730 I.A.W A300-600 SRM 51-72-10-001, PASDR ASAA2024052950090Transition Panel · corrodedFWD PIT R/H TRANSITION PANEL STA 500E+10 TO 500I HAS CORROSION. GROUNDED - YES. REMOVED THE CORROSION FROM THE FWD PIT R/H TRANSITION PANEL AT STA 500E+10 TO 500I IAW B737-800 SRM 53-00-53-1A-2.2.D. ORIG THICKNESS IS .040" IAW B737-800 SRM 53-30-53-01-2 TABLE SDR ASAA2024052950089Transition Panel · corrodedFWD CARGO LT TRANSITION PANEL STA 500G+2 TO 500I HAS CORROSION. GROUNDED - YES. REMOVED CORROSION FROM THE FWD PIT L/H TRANSITION PANEL AT STA 500G+2 TO 500I IAW B737-800 SRM 53-00-53-1A-2.2.D ORIG THICKNESS IS .040 IAW B737-800 SRM 53-30-53-01-2 TABLE 2. REMOSDR AALA202406068315Door Sill · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON L2 DOOR ENTRY AREA LOWER SILL INNER CHORD (CREASE ANGLE) AT STA 984, LBL 52. REPARED INNER CHORD PER EA 354931.SDR DALA2024060405763Shield · corroded(LOG 0375054) CORROSION ON UNDERSIDE OF AFT CARGO COMPARTMENT AFT SHIELD STA 847-867. REMOVED AND REPLACED AFT CARGO CORMPARMENT AFT SHIELD STA 847 TO 867 RBL 21 WL 165 IAW B737-800 SRM 51-40-02-0G AND DWG 146A0081 REV A.SDR JJBA20240603064Support Plate · corrodedRF1, ABOVE FLOOR, RH SUPPORT PLATE AT FR61 FOUND CORRODED AT FLOOR LEVEL. AT RF1, ABOVE FLOOR AT RH FR61, SUPPORT PLATE BLENDED AND FOUND OUT OF LIMIT AND REMOVED FOR REPLACEMENT. AT RF1, ABOVE FLOOR AT RH FR61, SUPPORT PLATE REPLACED.SDR DALA2024053005655Web · corroded(LOG 0366620) FWD CARGO DOOR THRESHOLD WEB CORRORED. REMOVED AND REPLACED FWD CARGO DOOR TRESHOLD WEB IAW B737 SRM 51-40-05 AND DWG 143A8122.SDR DALA2024053005654Floor Support · damaged(LOG 0366200) PASSENGER COMP. FLOOR SUPPORT DAMAGE STA 540 RBL 2 WL 208. REMOVED, REPLACED AND INSTALLED NEW FLOOR SUPPORT (PANEL BREAK) @ BSTA 540 BL0 TO RBL 42.5 WL 208. IAW DWG 143A5240 REV-B AND 737-900 SRM 51-40-02-0G.SDR ASAA2024052852596Floorboard · damagedMAIN CABIN FLOORBOARD 231VF DAMAGED. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOORBOARD P/N E5367190600000 AT FR 36 TO FR 42. STGR 23L TO STRGR 23R BUTT LINE 10L TO BUTT LINE 10R IAW A320 AMM 53-00-00-00-801-A AND AMM 53-00-00-400-801-A.SDR SWIA2024F00639Door Sill · corrodedPASSENGER DOOR FLOOR SILL AT STGR17L BETWEEN FS310.00 AND FS349.00 HAS MULTIPLE SPOTS OF CORROSION AS MARKED (C-CHECK RO 8/4/2024) REMOVED AND INSTALLED NEW PAX DOOR LOWER SILL (KICKPLATE) PN SH670-31875-7 REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG SH6SDR ASAA2024052851404Threshold · corrodedFWD CARGO THRESHOLD CORROSION FR 26+10 +28Y GROUNDED - YES. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW A320 SRM 53-21-29-283-001. REMOVED AND REPLACED THRESHOLD P/N D5323132220003 P.O. #1095256.2. IAW A320 SRM 51-42-11 AND AIRBUS DWG D53231761 ISSUE F. REMOSDR SWAA2024071690670Bracket · crackedCRACK ON BRACKET LOCATED BS 540 AIR CONDITIONING BLEED DUCT RT SIDE 2024-345627<[01] REPLACED BRACKET LOCATED BS 540 AIR CONDITIONING BLEED DUCT RT SIDE IAW B737-700 SRM 51-10-02-0G-0 PARAGRAPH 9 AND SRM 51-40-02-0G-0;DWG 212A1101 SHEET 3 REV -.TOOL USED DIGITSDR SWAA2024070390955Angle · corrodedCORRODED CLIP ON BS946 S-28L AT ACB (MARKED) UPON FURTHER EVALUATION ACTUAL LOCATION OF THE CORRODED CLIP IS BS 947 S-26 L/H<[01] REMOVED AND REPLACED CLIP AT ACB BS 947 STR 26L PER SRM 51-40-02 AND DWG 147A1047;[02] CORRECTION=REMOVED AND REPLACED CLIP AT ACBSDR VNAA202407020007Support · crackedCRACK ON AFT REFUEL DUCT MOUNTING SUPPORT BTW FS 677.00 TO FS 669.40, BTW STGR 22RH AND 21RH. CRACK ON AFT REFUEL DUCT MOUNTING SUPPORT BTW FS 677.00 TO FS 669.40, BTW STGR 22RH AND 21RH WAS REPAIRED PER REO 690-28-25-020 REV.--SDR SWAA2024070290507Floor Support · crackedCRACKS FOUND AROUND FASTENERS ON 2 INTERCOASTALS ON FLOOR STRUCTURE BETWEEN RBL 13 TO RBL 8; BS 907-927; WL 156.<[01] UPON FURTHER INVESTIGATION NO ALLOWABLE DAMAGE FOUND PER SRM; REPAIR BY REPLACEMENT OF PARTS. REMOVED AND REPLACED 2EA INTERCOSTALS BETWEEN RBSDR SWAA2024070290510Sidewall Support · corrodedCORROSION ON AFT CARGO FLOOR TO SIDEWALL SUPPORT BS 727D-787; LBL 21; WL 156.<[01] REPLACED AFT CARGO FLOOR TO SIDEWALL SUPPORT BS 727D-787; LBL 21; WL 156 PER SRM 51-40-02-0G-0; SRM 53-60-53-0I-2; SRM 53-00-53-1A-2; SRM 51-40-05-0G-09; SRM 53-00-53-2R-5; DWG SDR SWAA2024070290506Sidewall Support · corrodedCORROSION ON AFT CARGO FLOOR TO SIDEWALL SUPPORT BS 727D-767; RBL 21; WL 156.<[01] REPLACED AFT CARGO FLOOR TO SIDEWALL SUPPORT BS 727D-767; RBL 21; WL 156 PER SRM 51-40-02-0G-0; SRM 53-00-53-1A-2 & BOEING DWG 146A7502; AMM 51-21-72-370-804.;[02] VERIFIED CORRSDR SWAA2024070290505Shield · corrodedCORROSION ON AFT CARGO DOOR SHIELD BS 847+8; RBL 21; WL 156<[01] REPLACED AFT CARGO DOOR SHIELD BS 847+8; RBL 21; WL 156 PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; SRM 51-40-08-0G-00; DWG 146A0081; APPLIED WHITE ENAMEL TOPCOAT AND CIC PER AMM 51-21-73-370-804; SDR ASAA2024052850617Floor Support · corrodedR2 DOOR UNDER FLOOR PANEL 262LG HAS CORROSION ON FLOOR STRUCTURE. GROUNDED - YES. REMOVED AND REPLACED LONGITUDINAL BEAM AT R2 DOOR FR67 TO FR69, Y=-765 IAW SRM 51-72-11-911-001 AND SRM 51-42-11/001 REV. 149SDR ASAA2024052850426Floor Support · corrodedFWD WET AREA STA 328 - 344 LBL11 FLOOR STIFFNER HAS CORROSION. GROUNDED - YES. REMOVED CORROSION FROM FWD WET AREA, STA 328-344, LBL 11 FLOOR STIFFENER (PANEL BREAK) REF B737-800 SRM 53-10-51-0I-2. TABLE 3. ITEM 8 PER. B737-800 SRM 53-10-51-1A-A. PAR 4.F,(2) OSDR ASAA2024052850425Floor Support · corrodedFWD WET AREA STA 312 - 328 LBL 11 FLOOR STIFFNER HAS CORROSION. GROUNDED - YES. REMOVED CORROSION FROM FWD WET AREA, STA 312-328, LBL 11 FLOOR STIFFENER (PANEL BREAK) REF B737-800 SRM 53-10-51-OI-2, TABLE 3 ITEM (8)PER B737-800 SRM 53-10-51-1A-1, PAR. 4.F (2) SDR ASAA2024052850411Web · corrodedR1 DOOR AFT FLOOR STRUCTURE HAS CORROSION AT FR20. GROUNDED - YES. REMOVED AND REPLACED R1 DOOR AFT FLOOR STRUCTURE P/N: D5311816020000 AT FR C20R-FR C23R IAW SRM 51-72-911-00 REV 149 AND SRM 51-23-12 REV. 149.SDR SWAA2024061990889Angle · crackedFWD PIT RIGHT SIDE; ANGLE HAS CRACK INDICATION AROUND THE FASTENERS AT BS 500H APPROX. STRINGER S-25R.<[01] REMOVED AND REPLACED BS500H; STRINGER S-25R ANGLE IAW BOEING DWG 143A7505 REV:B AND B737-800 SRM 51-40-02.;[02] VERIFIED REMOVAL AND REPLACEMENT ANGLE BSDR SWAA2024061990890Angle · crackedFWD PIT LEFT SIDE; ANGLE HAS CRACK INDICATION AROUND THE FASTENERS AT BS 500H APPROX. STRINGER S-25L.<[01] REMOVED AND REPLACED BS500H; STINGER S-25L ANGLE IAW BOEING DWG 143A7505 REV:B AND B737-800 SRM 51-40-02.;[02] VERIFIED REMOVAL AND REPLACEMENT BS. 500H SDR ASAA2024052850372Web · corrodedL2 DOOR AFT OF FR C69 AT FLOOR LEVEL A TRIANGLE WEB HAS CORROSION. GROUNDED - YES. REMOVED AND REPLACED TRIANGLE WEB (SHEAR PLATE) P/N: D534742420200 AT L2 DOOR AFT OF C69 FRAME AT FLOOR LEVEL IAW SRM 51-72-911-001 REV. 149 AND SRM 51-42-11/001 REV. 149.SDR ASAA2024052850371Web · corrodedR2 DOOR BETWEEN FR C69-C70 AT FLOOR LEVEL. A TRIANGLE WEB HAS CORROSION. GROUNDED - YES. REMOVED AND REPLACED TRIANGLE WEB (SHEAR PLATE) P/N: 53-47112420300 AT R2 DOOR BETWEEN FR C69-C79 AT FLOOR LEVEL IAW SRM 51-72-11-911-001 REV. 149 AND SRM 51-42-11/001 RESDR IPXA2024061485833Floor Support · corrodedFWD SIDE OF RCB WALL FLOOR PANEL # WSP0786-501 HAS CORROSION BETWEEN FITTING # 4 & 5. REMOVED AND REPLACED FLOOR FITTING P/N WSP0750-507 PER DAC DWG WSP0750, DWG SP11250221, AND PER MD11 SRM CHAPTER 51 GUIDELINES. USE ORIGINAL PART AS SAMPLE IN ACCORDANCE WITHSDR IPXA2024061482250Sidewall Panel · corrodedNEED TO REMOVE RCB WALL TO ACCESS CORROSION ON LOWER SIDE OF WALL. INSTALLED RCB WALL, 18EA FITTINGS, 8EA HYDROSTATIC STRAP, 4EA SUPPORT RODS, 20EA FLOOR FITTING BOLTS, 3EA COVERS AND RCB WALL NETS 2EA IN REF TO MD11 AMM 25-59-13-400-801.SDR SWAA2024061390688Scuff Plate · crackedACB FWD CORNER SCUFF PLATE IS CRACKED<[01] EDIT: ADDED CALIBRATED WELDING EQUIPMENT USED IN STEP 2;[02] REPAIRED ACB FWD CORNER SCUFF PLATE PER BAC5975 PT INSPECTED WELDED AREA IAW SOPM 20-20-02. NO DEFECTS NOTED. SANDED THE REWORKED SURFACES AND EDGES OF THE SDR JJBA20240607009Support · corrodedRF1, UNDERFLOOR, RH SILL BTW FR 61-65 FOUND CORRODED. RH SILL BTW FR 61-65 BLENDED AND FOUND OUT OF LIMIT. RH SILL BTW FR 61-65 REMOVED AND INSTALLED.SDR DALA2024060605818Floor Support · corroded(LOG 0374986) AFT CARGO FLOOR SUPPORT STRAP FROM BS 787 TO BS 855, RBL 20, WL 160 CORRODED IN SEVERAL AREAS. REMOVED AND REPLACED AFT CARGO STRAP TO STA 767+4 TO 847+14 RBL 20 WL 160 IAW B737-800 SRM 51-40-02-0G AND DWG 146A8120 REV B.SDR ASAA2024052850049Floor Support · corrodedL2 DOOR FLOOR SUPPORT UNDER PANEL 261 LG HAS CORROSION GROUNDED - YES. REMOVED AND REPLACED FLOOR BEAM P/N: D5347219220200 AT L2 DOOR BETWEEN FR67 TO FR70 AND Y=765 IAW SRM 51-72-11-911-001 AND SRM 51-42-11/001 PARA 2F REV 149.SDR JJBA20240603065Support · corrodedRH SILL BTW FR 59-61 FOUND CORRODED. RH SILL BTW FR 59-61 FOUND CORRODED OUT OF LIMIT. RH SILL BTW FR 59-61 REMOVED AND REPLACED.SDR JJBA20240603063Support · corrodedLH SILL BTW FR 59-61 FOUND CORRODED. LH SILL BTW FR 59-61 BLENDED OUT OF LIMITS AND REMOVED FOR REPLACEMENT. LH SILL BTW FR 59-61 REPLACEDSDR DALA2024053105703Floor Support · corroded(LOG 0368257) CORROSION AT CABIN FLOOR INTERCOSTAL, STA947+1, & 941+7, RBL49, WL208. REMOVED AND REMPLACED INTERCOSTAL, STA 947+1, & 941+7. RBL 49, WL 208 PER B737-900 SRM 51-40-02-0G AND DWG. 147A5650.SDR DALA2024052905613Plate · corrodedSHIP 6806 IN REF. NRC 0168: CORROSION ON RH SIDE PLATE (UPPER AND LOWER SURFACE) 1380 TO 1440 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00654. RH SIDE PLATE (UPPER AND LOWER SURFACE) 1380 TO 1440 AT AFT CARGO COMPARTMENT WAS REPLACED PER B757SDR DALA2024052905612Intercostal · corrodedSHIP 6806 IN REF. TO NRC 00165: CORROSION ON INTERCOSTAL 30 BTW STA 1300 AND 1320 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 744: INTERCOSTAL 30 BTW STA 1300 AND 1320 AT AFT CARGO COMPARTMENT. WAS REPLACED" PER B757-200 SRM. (0364846)SDR DALA2024052905611Floor Support · corrodedSHIP 6806 IN REF TO NRC S/N 00162: CORROSION OUT LIMITS ON FLOOR SUPPORTS (JOOGLE AREA) BTW STA 1328 TO 1331 AND LBL 16.10, LBL 10.45, RBL 2.90 RBL 7.55 RBL 10.45 RBL 16.10 AT AFT CARGO. CORRECTIVE ACTION: SUMMARY OF NRC 724: CHANNELS 6 (E/AS) WERE REPLACED PESDR DALA2024052905596Floor Support · corrodedSHIP 3132 CORROSION FLOOR BEAM -Y1292 LOCATED FR 64 TO FR 66 AT AFT GALLEY AREA (SSI 534147). CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y1292 LOCATED FR 64 TO FR 66 AT AFT GALLEY AREA AS PER A319 SRM 51-72-11. (0365313)SDR DALA2024052905595Floor Support · corrodedSHIP 3132 CORROSION FLOOR BEAM +Y1292 LOCATED FR 16 AND FR 20 AT FWD GALLEY ARE A (SSI 531189). CORRECTIVE ACTION: REPLACED FLOOR BEAM Y1292 LOC. FR12 TO FR24 AT FWD GALLEY AREA AS PER A319 SRM 51- 42-11 AND A319 SRM 51-72-11. (0365217)SDR SWAA2024070390387Attach Angle · corrodedFWD CARGO DOOR UPPER SILL WEB ATTCHMENT CLIP AT BS 460 PN 143A8114-23 IS CORRODED<[01] REMOVED AND REPLACED CLIP <BR>IAW SRM 51-40-02 & DWG 143A0081<BR>FCD UPPER SILL WEB ATTCHMENT CLIP AT BS 460;[02] VERIFIED CORRECTIVE ACTION #1SDR SWAA2024062890207Angle · corrodedFWD CARGO COMPT LH TRANSITION ANGLE CORRODED STA 500A-500B. REMOVED DAMAGE IAW SRM 51-10-02. MEASURED DAMAGE DEPTH TO BE .009. DAMAGE FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-53-1A-2. CUTOUT & REMOVED DAMAGE SECTION OF TRANSITION ANGLE FROM STA 480SDR SWAA2024062890214Angle · corrodedFWD CARGO COMPT RH TRANSITION ANGLE CORRODED STA 500F-500G. REMOVED CORROSION AT FWD CARGO R/H TRANSITION ANGLE FROM STA 500A TO STA 500I PER SRM 51-10-02. MEASURED BLEND AREAS OUT OF LIMITS PER SRM 53-00-53-1A-2 FIG.103; DETAIL E. FWD CARGO R/H TRANSITION SDR SWAA2024062890215Angle · corrodedFWD CARGO COMPT RH TRANSITION ANGLE CORRODED STA 500E-500F. REMOVED CORROSION AT FWD CARGO R/H TRANSITION ANGLE FROM STA 500A TO STA 500I PER SRM 51-10-02. MEASURED BLEND AREAS OUT OF LIMITS PER SRM 53-00-53-1A-2 FIG.103; DETAIL E. FWD CARGO R/H TRANSITIONSDR SWAA2024062890216Angle · corrodedFWD CARGO COMPT RH TRANSITION ANGLE CORRODED STA 500D-500E. REMOVED CORROSION AT FWD CARGO R/H TRANSITION ANGLE FROM STA 500A TO STA 500I PER SRM 51-10-02. MEASURED BLEND AREAS OUT OF LIMITS PER SRM 53-00-53-1A-2 FIG.103; DETAIL E. REPLACED IAW SRM 51-10-02
Back to JASC 5320