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 SWAA2024070898044Intercostal · crackedCRACK WEB - INTERCOSTAL FLOOR STRUCTURE BETWEEN BS 277 TO BS 294.5 AND BL 0 FWD GALLEY AND LAV 2024-361597<[01] REPLACED WEB-INTERCOSTAL AND FASTENERS LOCATED FLOOR STRUCTURE BETWEEN BS 277 TO BS 294.5 AND BL 0 FWD GALLEY AREA IAW BOEING 737-700 SRM 51-40-02; SDR SWAA2024070810383Web · crackedCRACK WEB - INTERCOSTAL FLOOR STRUCTURE BETWEEN BS 277 TO BS 294.5 AND BL 0 FWD GALLEY AND LAV 2024-361597<[01] REPLACED WEB-INTERCOSTAL AND FASTENERS LOCATED FLOOR STRUCTURE BETWEEN BS 277 TO BS 294.5 AND BL 0 FWD GALLEY AREA IAW BOEING 737-700 SRM 51-40-02; SDR ASAA2024060350503Floor Support · corrodedMAIN CABIN SUPPORT P/N 147A5676-16 STA 927 - STA 947 LBL16 CORRODED. GROUNDED - YES. BLENDED CORROSION SUPPORT HAS 100% MAT LOSS FOUND OUT OF LIMITS ALLOWABLE DAMAGE IAW B737-800 SRM 53-70-51-1A-1. DRILLED TO FIT NEW SUPPORT IAW B737-800 SRM 51-40-05 AND BAC DSDR ASAA2024060350501Floor Support · corrodedMAIN CABIN INTERCOSTAL P/N 147A5676-13 STA 947.5 TO 967 CORRODED. GROUNDED - YES. CORROSION IS AROUND SEVERAL FASTENERS HOLE FOUND OUT OF LIMITS ALLOWABLE DAMAGE IAW B737-800 SRM 53-70-51-1A-1, 100% MAT LOSS. DRILLED NEW SUPPORT IAW B737-800 SRM 51-40-05 AN BASDR FDEA202406030867Angle · crackedFWD CARGO COMP'T UNDER FLOOR AREA LH SIDE PLATE CRACK AT S-43L~S-44L,FR26 POSITION. INSTALLED THE NEW PLATE ANGLE WITH FASTENERS AT UNDER FWD CARGO FLOOR AREA FR26 S-43L~44L I.A.W A300-600 SRM 51-72-10-001, PAGE.2 & 51-40-21-001, PARA.6, PAGE.7B-23, THE RESDR SWAA2024062497585Panel · corrodedFWD PIT PANEL 120AF IS CORRODED. A177-019<[01] C/WSDR SWAA2024062497586Scuff Plate · crackedFWD CARGO DOOR SURROUND; FWD CORNER SCUFF PLATE IS CRACKED FWD CARGO DOOR SURROUND FWD CORNER SCUFF PLATE IS CRACKED<[01] FWD CARGO DOOR SURROUND; FWD CORNER SCUFF PLATE REPAIRED ON BACKSHOP W/O# 45805-1000-0001 IAW SRM 53-30-15-2R-1;[02] VERIFIED STEP 1<BR>AUSDR SWAA2024062497976Shield · corrodedA225-002 FWD CARGO RH AFT SHIELD BS500 + 10' TO 500A RBL 25' WL 156 HAS AREAS OF CORROSION<[01] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-D00069 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)]<BR>FWD CARGO RH AFT SHIELD BS500 + 10'SDR SWAA2024062497979Support Angle · corrodedA225-005 FWD CARGO AFT BLKD LOWER SUPPORT ANGLE BS 500I CORRODED FROM RLB 20' TO LBL 20' WL 156.<[01] REMOVED; REPAIRED; AND REINSTALLED FWD CARGO AFT BLKD LOWER SUPPORT ANGLE AT STA 500I IAW EA 24-153-01577;[02] COMPLETE<BR>AUDIT C/WSDR ASAA2024060350430Sidewall Support · corrodedMAIN CABIN WALL SUPPORT STA 990 - 1016 LBL 32 CORRODED. GROUNDED - YES. CORROSION IS AROUND SEVERAL FASTENER HOLES, 100% MATERIAL LOSS. OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1. DRILLED TO FIT NEW SUPPORT IAW B737-800 SRM 51-40-05 AND BAC DWG 147A5700 REV.SDR ASAA2024060350429Support · corrodedMAIN CABIN SUPPORT STA 990 - 1016 RBL 32 CORRODED. GROUNDED - YES. BLENDED OUT CORROSION. SUPPORT HAS 100% MATERIAL LOSS. OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1. DRILLED TO FIT NEW SUPPORT IAW B737-800 SRM 51-40-05 AND BAC DWG 147A5700 REV.- SUPPORT INSTSDR SWAA2024061497825Stiffener · crackedCRACKED STIFFENER BS 540 LBL 1.5 WL 208 (MARKED)<[01] VERIFIED STEP 2 IN PARTIAL.;[02] REMOVED AND REPLACED PASSENGER CABIN STIFFENER AT BS 540 BL0 TO LBL 25 WL 208 IAW SRM 51-40-02 AND DWG 143A524;[03] VERIFIED STEPS 1;2 COMPLETE.;[04] REMOVED AND REPLACED PASDR SWAA2024061497824Stiffener · crackedCRACKED STIFFENER BS 540 RBL 1.5 WL 208 (MARKED)<[01] VERIFIED STEP 3 IN PARTIAL.;[02] VERIFIED STEPS 2;3 COMPLETE; STEP 1 IN PARTIAL.;[03] REMOVED AND REPLACED STIFFENER BS 540 BL 0 TO RBL 25 WL 208 IAW SRM 51-40-02-0G-0 DWG 143A5240;[04] REMOVED AND REPLACEDSDR ASAA2024060350203Floor Support · corrodedWHILE PERFORMING REPAIR TO STA 986 FLOOR STRUCTURE FOUND FLOOR SUPPORT @ STA 967-STA 986 RBL 16 TO HAVE CORROSION. P/N 140A9872-10. GROUNDED - YES. REMOVED AND REPLACED (INSTALLED) NEW FLOOR SUPPORT AT STA 967-986 RBL 16 I.A.W B737-800 SRM 51-40-02 AND PER BACSDR DALA2024060605808Floor Support · corrodedCORROSION FLOOR SUPPORT +Y254 LOCATED BTW FR 16 TO FR 18 AT FWD GALLEY AR EA (SI 531189). C/A: REPLACED FLOOR SUPPORT Y254 LOCATED BTW FR 12 TO FR 24 AT FWD GALLEY AREA (SI 531189) AS PER A320 SRM 51-42-11 AND SRM 51-72- 11 DWG D53112816 ,ISSUE G00 ,RELEASE DASDR CALA2024060701713Strap · crackedREF AMES NON ROUTINE 171415-0100-0024.GENERATING ITEM B757-06-3- 0228: FLOORBEAM STRAP IS CRACKED, LOCATED IN LEFT TUNNEL OF MEC, FRAME STA. 377.7 AND LBL 26 (MARKED WITH STREAMER 70878). CATEGORY A REPAIR. NO ADDITIONAL SUPPLEMENT INSPECTIONS REQUIRED . REMOVSDR DALA2024060605826Floor Support · corroded(LOG 0376553) DAMAGED INTERCOSTAL AT STA 312 TO STA 328 LBL 46 WL 208. REMOVED AND REPLACED DAMAGE INTERCOSTAL AT STA 312 TO STA 328 LBL 46 WL 208 IAW B737-800 SRM 51-40-02-0G AND DWG 141A5400.SDR DALA2024060605816Floor Support · corroded(LOG 0373973) CORROSION** CABIN FLOOR INTERCOSTAL, STA868+18, LBL49, AT FWD O/B LAV MOUNT AREA. REMOVED AND REPLACED INTERCOSTAL AT STA 868+18, LBL49 IAW B737-900 SRM 51-40-02-0G, 51-40-05-0G.SDR DALA2024060405788Strap · crackedAIRCRAFT 6814, MAIN CABIN BS 1640 FLOOR BEAM LOWER STABILIZER STRAP IS CRACKED AT RBL 45.5. DOT 050. REPAIRED MAIN CABIN BS 1640 FLOOR BEAM LOWER STABILIZER STRAP CRACK AT RBL 45.5. PER B757 SRM 53-00-51-2R REPAIR 12. (LP 0374646)SDR N6WA2024060401Mount · crackedJB6 MOUNTING TRAY CRACKED. REMOVED AND REPLACED JB6 MOUNTING TRAY IAW CRJ SRM 51-42-06.SDR UIEA2024052400436Floor Support · corrodedLOWER FUSELAGE AFT CARGO COMPARTMENT, FLOOR STRUCTURE AREA, FROM STA 727+10" TO STA 793, LBL 3" FLOOR SUPPORT CHANNEL WITH CORROSION AT SEVERAL PLACES(<P>REPLACED FLOOR BEAM SUPPORT RAIL CHANNEL P/N: BAC1509-100146 FROM STA 727+10" TO STA 797.5" WITH TWO SPLICSDR DALA2024060405774Floor Support · corrodedSHIP 3137 CORROSION FLOOR BEAM +Y1227 FROM FRAME 66 TO FRAME 68 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM Y1227 AND SPLICE (3 E/A) LOC BTW FR 66 TO FR 68 AT AFT GALLEY AREA AS PER A319 SRM 51-72-11 AND AS PER A319 SRM 51-42-11. (0375111)SDR DALA2024060405773Floor Support · corrodedSHIP 3137 CORROSION FLOOR BEAM -Y1227 FROM FRAME 66 TO FRAME 68 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM AND REINSTALLED SPLICE 4 E/A -Y1227 FROM FR 66 TO FR 68 AT AFT GALLEY AREA AS PER A319 SRM 51- 42-11. (0374946)SDR DALA2024060405772Floor Support · corrodedSHIP 3137 CORROSION FLOOR BEAM +Y765 FROM FRAME 66 TO FRAME 70 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM Y765 AND SPLICE (2 E/A) HARD POINT (2 E/A) BRACKETS (2 E/A) AS PER A319 SRM 51-42-11 AND SRM 51-72-11. (0374942)SDR DALA2024060405764Channel · corroded(LOG 0375205) AFT CARGO COMPARTMENT Z CHANNEL AT STA 727-847 LBL 24 IS CORRODED. REPAIRED AFT CARGO COMPARTMENT Z CHANNEL FROM STA 727 TO STA 847, LBL 24 PER B737-900 SRM 53-00-53-2R-6, SRM 51-40-05-0G, SRM 51-40-02-0G AND DWG# 146A7502 REV-A.SDR SWAA2024071697652Intercostal · crackedCRACK ON INTERCOSTAL LOCATED BTW BS 294.5 TO BS 303.9 AT LEVEL 16L AT FWD GALLEY AREA 2024-357313<[01] REPLACED INTERCOSTAL LOCATED BTW BS 294.5 TO BS 303.9 AT LEVEL 16L AT FWD GALLEY AREA IAW B737-700 51-10-02 PARAGRAPH 9 AND INSTALLED FASTENERS IAW B737-700 SDR SWAA2024071697655Intercostal · crackedCRACK ON INTERCOSTAL LOCATED BTW BS 294.5 TO BS 303.9 AT LEVEL STR 15L AT FWD GALLEY AREA 2024-357319<[01] TOOLS USED TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25 AND TEMPERATURE CONTROLLED P3015GOES00000; S/N: 142811019; DUESDR VNAA202407110003Floor Support · corrodedCORROSION ON FLOOR PANEL SUPPORT ANGLE UPPER FACE AT FS280.00 BTW RBL 9.00 AND LBL 9.00, DUE EXCESSIVE CORROSIÓN ON FLOOR SUPPORT ANGLE UPPER FACE AT FS 280 BTW RBL 9.00 AND LBL 9.00 ITS OUT OF LIMITS PER CRJ-900 SRM 53-00-00-101-001-A01. PER SRM 51-42-06-001SDR SWAA2024071097642Scuff Plate · crackedFSD; SCUFF PLATE AFT SIDE IS CRACKED 3 INCHES.<[01] FUSION WELDED THE DAMAGED AREA ON SCUFF PLATE IAW SRM53-10-15-2R-2. PT INSPECTED WELDED AREA PER SOPM 20-20-02. NO CRACKS NOTED. SANDED THE REWORKED SURFACES AND EDGES OF SCUFF PLATE AS NECESSARY TO GET A SURSDR SWAA2024070897673Support Angle · crackedCRACK SUPPORT ANGLE LOCATED BS693 RBL25 AND WL202 AT PASSENGER CABIN 2024-361562<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811019; DUE DATE 23-JAN-25.SDR SWAA2024070810382Support Angle · crackedCRACK SUPPORT ANGLE LOCATED BS693 RBL25 AND WL202 AT PASSENGER CABIN 2024-361562<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811019; DUE DATE 23-JAN-25.SDR SWAA2024062797261Strip · corrodedTHE AFT CARGO CAP STRIPS HAVE NUMEROUS AREAS OF CORROSION.<[01] REMOVED AND REPLACED DAMAGED CAP STRIPS AT AFT CARGO I/A/W AMM 25-52-10.;[02] INSPECTED AS REQUIRED. CORRECTIVE ACTION #1SDR SWAA2024062797262Strip · corrodedTHE FWD CARGO CAP STRIPS HAVE NUMEROUS AREAS OF CORROSION.<[01] REPLACED CAP STRIPS IN FWD CARGO IAW SRM 51-40-02 AND PER TASK CARD 'TTG8Q00S2BCS';[02] C/W INSPECTIONSDR CALA2024061301792Floor Support · corrodedCORROSION UNDEER THE NUTPLATES ON THE LOWER SURFACE OF THE ALC FLOOR SUPPORT FROM STA 1329 TO STA 1351 LBL19 NO 3447. REF AMES NR 170098-0100-0131 BLENDED CORROSION FOUND TO BE OUT OF LIMITS HAD TO FABRICATE NEW FLOOR SUPPORT IAW 47613FAAB01. SEE PARTIAL WORKSDR IPXA2024061061446Angle · crackedCRACK -ANGLE BULK CARGO COMPARTMENT LEFT AREA STA 1578 LBL60 OUTBOARD.I.A.W AMM 53-01-06-400-801 REV.142 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL. I.A.W AMM 25-57-05-404-006 AND AMM 25-58-04-404-015 REV.142 INSTALLED MAIN DECK CARGO HANDSDR IPXA2024061060582Angle · crackedCRACK - ANGLE BULK CARGO COMPARTMENT RIGHT AREA STA 1578 RBL 60 OUTBOARD I.A.W AMM 53-01-06-400-801 REV.142 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL. I.A.W AMM 25-57-05-404-006 AND AMM 25-58-04-404-015 REV.142 INSTALLED MAIN DECK CARGO HASDR DALA2024060605828Channel · corroded(LOG 0376662) FWD CARGO BAY L/H 'Z' CHANNEL IS CORRODED FROM STA 500-500L, LBL 25. REPAIRED ZEE CHANNEL L/H STA 500-500L, LBL 25 IAW B737 SRM 53-00-53-2R-6.SDR CALA2024060401695Floor Support · damagedFWD PIT TORSION BOX COVER SHEET REQUIRES REPLACEMENT DUE TO SHOR T REINSPECTION INTERVALS. REMOVED AND REPLACED TORSION BOX COVER SHEET AT FWD CARGO PIT IA W A320 SMR 51-42-11-001.SDR AALA202406039832Floor Support · damagedAIRCRAFT IN BASE MAINTENANCE: UNSPECIFIED DAMAGE TO PASSENGER CABIN FLOORBOARD SUPPORT FROM STA 947 TO STA 967, RBL 16. REPLACED SUPPORT PER AARD 51-00-05.SDR U2RA2024081500026Web · crackedDURING C CHECK IN GMF FOUND CRACK AT MED#1 RH UPPER SILL WEB CRACK AT STA 480 STR 16R CATEGORY B REPAIR WAS ACCOMPISHED IN ACCORDANCE WITH SRM 53-10-15 REPAIR 1 (REV 59/20 FEB 2024SDR U2RA2024081500025Reveal · crackedWHILE PERFORMING C CHECK IN GMF FOUND CRACK AT MED#5 CUTOUT DOOR REVEAL AT STA 2240 STR 21 NEAR DOOR LOCK RELEASE THIS REPAIR IS ACCOMPLISHED ANS CATOGORIZED AS CAT A REPAIR IN ACCORDANCE WITH SRM 53-60-15 REPAIR 7 (REV 59/20 FEB 2024SDR SWIA202408130680Door Sill · gougedFORWARD BAGGAGE BAY SILL BETWEEN FS533.00 AND FS581.00 STGR26L CORRODED AND GOUGED IN MULTIPLE AREAS AS MARKED (C-CHECK RO 8/11/2024) REPAIRED CORROSION/GOUGE DAMAGE TO THE FWD BAGGAGE BAY DOOR SURROUND INNER CLOSING SKIN BETWEEN FS533.00-FS581.00 AND SSDR SWIA202408130679Tee Angle · corrodedCENTER FUSELAGE T CAP CORRODEDIN MULTIPLE LOCATIONS ON LBL9 BETWEEN APPROXIMATELY F697.00 AND FS841.00 AS MARKED (C-CHECK RO 8/11/2024) BLENDED CORROSION FROM MULTIPLE LOCATIONS ON LBL9 T-CAP FLOOR STRUCTURE BETWEEN FS697 AND FS841. REPAIRED T-CAP REFSDR SWIA202408130678Intercostal · chafedINTECOSTAL IS CHAFED STGR9R BETWEEN FS1144.00 & FS1162.00. (FLAGGED) (C-CHECK RO 8/11/2024) BLENDED OUT CHAFE ON INTERCOSTAL LOCATED ON STGR9R BETWEEN FS1144.00 & FS1162.00. REF CRJ 700 SRM 51-12-00-001-001-A01REMOVED DAMAGED INTERCOSTAL BETWEEN FS 1144SDR SWIA202408130677Tee Angle · corrodedCENTER FUSELAGE T CAP CORRODED ON RBL9 BETWEEN APPROXIMATELY FS685.00 AND FS697.00 AS MARKED (C-CHECK RO 8/11/2024) REMOVED CORROSION FROM CENTER FUSELAGE T CAP CORRODED ON RBL9 BETWEEN APPROXIMATELY FS685.00 AND FS697.0. PERFORMED ALL STEPS OF REO 670-SDR SWIA20240813601Plate · corrodedFORWARD BAGGAGE BAY JOINT PLATE AT APPROXIMATELY FS581.00 BETWEEN STGR25L AND STGR26L CORRODED (C-CHECK RO 8/11/2024) REMOVED CORROSION FROM FORWARD BAGGAGE BAY JOINT PLATE AT APPROXIMATELY FS581.00 BETWEEN STGR25L AND STGR26L REF. CRJ-700 SRM 51-21-06-SDR SWAA2024071697034Angle · crackedCRACK ON ANGLE LOCATED BTW BS 380 UP TO 400 RBL 43 WL 208.1 2024-345758<[01] REPLACED ANGLE <BR>LOCATED BTW BS 380 UP TO BS400 RBL 43 WL 208.1<BR>IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02<BR>DWG: 143A5400 SHEET: 38 REV: A<BR>SEE INDIVIDUAL SIGN OFFS BESDR SWAA2024071697354Angle · crackedCRACK ON ANGLE LOCATED BS 685 RBL 24.75 AT PASSENGER CABIN 2024-357284 ANGLE LOCATED BS 692.10 RBL 24.75 AT PASSENGER CABIN<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25; TEMPERATURE CONTROLLER: P/N: P3015GOESDR SWAA2024071197346Floorboard · delaminatedPASSENGER CABIN FLOOR BOARD 232RF IS DELAMINATED<[01] PASSENGER CABIN FLOOR BOARD 232RF WITH DELAMINATED WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0 AND BDWG: 144A5810 ID: 0004 DUE TO AMOUNT OF ALL DAMAGE;[02] VERIFIED CORRECTIVE ACTSDR VNAA202407110002Intercostal · corrodedINITIAL INSPECTION: CORROSION ON INTERCOSTAL ATTACHED TO STRINGER 20RH IN STA. FS=333.00 TO FS= 364.00 AT MAIN AVIONICS COMPARTMENT. SUMMARY:EVALUATED, DUE TO EXCESIVE DAMAGE ON INTERCOSTAL ATTACHED TO STRINGER 20RH IN STA. FS=333.00 TO FS= 364.00 PER CRJ-900
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