JASC 5320
Service difficulty reports · 216,095
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 AALA202605229367Web · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR STRUCTURE WEB BETWEEN STA 986 AND STA 992, BETWEEN RBL 50 AND RBL 54. REPLACED WEB PER AARD 51-00-05-1.SDR SWAA2026052294704Support Angle · crackedCRACKED SUPPORT ANGLE LOCATED BS867 LBL19 AT AFT CARGO COMPARTMENT. REPLACED SUPPORT ANGLE LOCATED BS867 LBL19 AT AFT CARGO COMPARTMENT IAW SRM 51-40-02-0G-0; DWG 149A8102 SHEET 19 REV A AND DWG 149A8104 SHEET 1 REV B. MEASUREMENT OF CRACK IS L= 1.435? INCH.SDR IPXA2026050679318Profile · crackedMCD FR75 RH CRACK FOUND IN THE Z-PROFILE. INSTALLED NEW Z- PROFILE. MCD FR75 RH: I.A.W. A300-600 SRM 51-40-21-001SDR IPXA2026050779287Tee Angle · crackedMCD FR80/82 RT CRACK IN THE TEE PROFILE AT THE CORNER. REMOVED TEE PROFILE CRACKED IAW0 SRM 51-40-21-001. INSTALLED NEW TEE PROFILE IAW SRM 51-40-21-001.SDR AALA202605086490Shear Plate · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23R. REPLACED SHEAR PLATE PER SRM 51-72-11.SDR CALA2026050515973Splice Angle · corrodedACCESS PANEL 139CL FORWARD KEEL BEAM REQUIRE FURTHER CLEANING AT PANEL ATTACH FRAMES AND CHECK ON CORROSION. CLEANED AREA IAW BOEING SOPM 20-30-03, REMOVED CORROSION ON LH A ND RH TEE BEAM BTW 995-1040 IAW B757-200 SRM 51-10-02-0G-0. ORIG INAL THICKNESS .130SDR CALA2026050515971Splice Angle · corrodedACCESS PANEL 139AL FORWARD KEEL BEAM REQUIRE FURTHER CLEANING AT PANEL ATTACH FRAMES AND CHECK ON CORROSION. CLEANED AREA IAW SOPM 20-30-03. REMOVED CORROSION IAW SRM 51-10-02-0G-0. ORIGINAL THICKNESS .130", REMAINING THI CKNESS .123" FOUND TO BE WITHIN LIMISDR CALA2026050515969Splice Angle · corrodedACCESS PANEL 139BL FORWARD KEEL BEAM REQUIRE FURTHER CLEANING AT PANEL ATTACH FRAMES AND CHECK ON CORROSION. CLEANED AREA IAW BOEING SOPM 30-30-03, REMOVED CORROSION ON LH A ND RH TEE BEAM BTW STA 965-995 IAW 51-10-02-0G-0. ORIGINAL THICK NESS .130" REMAININGSDR CALA2026050515966Support · crackedLEFT CEILING SUPPORT AT STA 1640-1681 CRACKED IN NUMEROUS LOCATIONS. REMOVED AND REPLACED LT CEILING SUPPORT AT BS 1640-1681, IAW SRM 51-40-02-0G -0 AND SRM 51-40-05-0G-0.SDR CALA2026050415964Support · crackedRT CEILING SUPPORT AT STA 1640-1681 CRACKED. REMOVED AND REPLACED L/H CEILING SUPPORT AT BS 1640-1681 BY NEW PART IAW B757-200 SRM 51-40-02AND SRM 51-40-05.SDR DALA2026050402804Floor Support · corrodedCORROSION ON INTERCOSTAL BTW BS 1580 TO 1600, S29R OF FLOOR STRUCTURE AT AFT CARGO COMPARTMENT. CORROSION LEVEL 2. INTERCOSTAL BTW BS 1580 - 1600, S29R OF FLOOR STRUCTURE AT AFT CARGO COMPARTMENT WAS REPLACED IAW SRM 51-40-02-0G PAR 7.D. (1572695) AIRCRAFT WASDR DALA2026050402801Floor Support · corrodedCORROSION AROUND FASTENER HOLE ON FLOORBOARD SUPPORT STRUCTURE R/H SIDE BETWEEN FR 76 AND FR78 APPROX RBL 37.5 SECOND FROM FORWARD FASTENER HOLE. REMOVED AND REPLACED FLOORBOARD SUPPORT STRUCTURE R/H SIDE BETWEEN FR76 AND FR78 APPROX RBL 37.5 I.A.W. A220 ASRP SDR DALA2026050302787Floor Support · corrodedLEVEL 2 CORROSION FLOOR BEAM +Y254 LOCATED BTW FR 16 TO FR 21 FWD GALLEY AREA (SSI 531189). REPLACED FLOOR BEAM Y254 AND FASTENERS LOCATED BTW FR12 TO FR 24 AT FWD GALLEY AREA AS PER A320 SRM 51-72-11, A320 SRM 51-42-11 AND DWG D53212367 RELEASE DATE 18-MAY-2SDR DALA2026050302786Web · corrodedLEVEL 2 CORROSION WEB LOCATED AT FR 16 LEVEL STR 23R AT FWD GALLEY AREA. REPLACED WEB LOCATED ON FR12 TO FR16 AT LEVEL STR 23R AT FWD GALLEY AREA IAW SRM 51-72-11; A320 SRM 51-42-11, DWG D53114392 ISSUE B00, RELEASE DATE 01-FEB-19, DWG D53112781 ISSUE E00, RESDR REXA2026070301039Intercostal · corrodedCORROSION ON INTERCOSTALS (3 EAS) BTW FS 349 TO FS 364 NEAR STGR 27 ALSO STGR 26R AT MAIN AVIONICS COMPARTMENT INTERCOSTALS BTW 7LH AND 27RH, BTW FS 349 TO FS 364 NEAR STGR 27R WERE REPAIRED PER EA CRJ953-22320 REV IR AND EA NO: CRJ953-22321 REV IR AND INTERCSDR REXA2026070301037Intercostal · corrodedCORROSION ON INTERCOSTALS (3 EAS) BTW FS 394 TO FS 409 NEAR STGR 27 ALSO STGR 26L AT MAIN AVIONICS COMPARTMENT INTERCOSTALS (3 EAS) BTW FS 394 TO FS 409 NEAR STGR 27 ALSO STGR 26L AT MAIN AVIONICS COMPARTMENT WERE REPAIRED PER EA NO: CRJ953-20508 REV ASDR VNAA202606120004Bracket · corrodedCORROSION ON BRACKET (FWD SURFACE) OF CONNECTOR HARNESSES AT LT (PX19P1 AND PX34P1) RT (PX17P1 AND PX33P1) MLG WHEEL WELL. CORROSION ON BRACKET (FWD SURFACE) OF CONNECTOR HARNESSES AT LH(PX19P1 AND PX34P1) / RH(PX17P1 AND PX33P1) MLG WHEEL WELL WAS REMOVED PSDR SWAA2026060394137Scuff Plate · crackedCRACK ON FWD CORNER SCUFF PLATE LOC ON AFT CARGO COMPARTMENT. REPAIRED FWD CORNER SCUFF PLATE LOC ON AFT CARGO COMPARTMENT IAW SRM 53-60-15-2R-1 REPAIR 1; AND BAC 5975.SDR SWAA2026060194290Angle · crackedCRACK ON ANGLE LOCATED BS 500H AFT SIDE AND S-26R AT FWD CARGO COMPARTMENT. REPLACED ANGLE LOCATED BS 500H AFT SIDE AND S-26R AT FWD CARGO COMPARTMENT IAW SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 143A7505; SHEET 138; REV -.SDR SWAA2026060194294Angle · crackedCRACKED ANGLE LOCATED BS500G FWD SIDE AND S-26L AT FWD CARGO COMPARTMENT. REPLACED ANGLE LOCATED BS500G FWD SIDE AND S-26L AT FWD CARGO COMPARTMENT IAW SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 143A7505; SHEET 137; REV -.SDR SWAA2026060194297Angle · crackedCRACKED ANGLE LOCATED BS 500G FWD SIDE AND S-26R AT FWD CARGO COMPARTMENT. REPLACED REPAIR ANGLE AND FASTENERS LOCATED BS 500G FWD SIDE AND S-26R AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02 ; SRM 51-10-02 ITEM 9 AND DWG 143A7505; SHEET 139; REV-.SDR SWAA2026060194298Angle · crackedCRACK GUSSET ANGLE LOCATED BS 500I AT LEVEL STR 19R AT FWD CARGO COMPARTMENT. REPLACED GUSSET ANGLE AND FASTENERS LOCATED ON BS 500I AT LEVEL STR 19R AT FWD CARGO BAY IAW SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 143A7902; SHEET: 256 AND 257; REV: B.SDR SWAA2026060194289Angle · crackedCRACKED ANGLE LOCATED BS 500H FWD SIDE AND S-26R AT FWD CARGO COMPARTMENT. REPLACED ANGLE AND FASTENERS LOCATED BS 500H FWD SIDE AND S-26R AT FWD CARGO COMPARTMENT IAW SRM 51-10-02 ITEM 9, SRM 51-40-02 AND DWG 143A7505, SHEET 137; REV-.SDR SWAA2026060194296Angle · crackedCRACKED ANGLE LOCATED BS 500G AFT SIDE AND S-26R AT FWD CARGO COMPARTMENT. REPLACED ANGLE AND FASTENERS LOCATED BS 500G AFT SIDE AND S-26R AT FWD CARGO COMPARTMENT IAW SRM 51-10-02 ITEM 9 ; SRM 51-40-02 AND DWG 143A7505; SHEET 139; REV-.SDR SWAA2026052794302Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BTW BS 500I TO BS 520 LBL 1 WL 208.1 AT PASSENGER CABIN . REPLACED SUPPORT ANGLE LOCATED BTW BS 500I TO BS 520 LBL 1 WL 208.1 AT PASSENGER CABIN IAW BOEING 737-800 SRM-51-10-02 ITEM 9 AND DGW 143A5400 SHEET: 189 AND 190 REV-.SDR AALA202605250280Attach Angle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE AT STA 663 BETWEEN LBL 18 AND LBL 72. REPAIRED ANGLE PER SRM 57-10-10-2R-5 AND EA 374988.SDR AALA202605223005Floor Support · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL AT STA 950 AND RBL 48. REPLACED INTERCOSTAL PER AARD 51-00-05-1.SDR R61A2026051800139Floor Support · corrodedWHILE IN HEAVY CHECK - RT COCKPIT FLOOR DOUBLER BETWEEN FR. 11-12 HAS SMALL AREAS OF CORROSION. REPAIRED RT COCKPIT FLOOR DOUBLER BETWEEN FR. 11-12 IAW ETD2026-170-007951 REV.: B AND SRIIM CHAPTER 51.SDR SWAA2026051994317Baffle · crackedFCB BAFFLE BS 500 - 500A, LBL 21 CRACKED. REMOVED AND REPLACED ON FCB BAFFLE IAW SRM 51-40-02, AND DWG 143A7505 0117, REV -.SDR SWAA2026051994319Baffle · damagedFCB BAFFLE BS 500A - 500B, LBL 21 HAS ELONGATED FASTENER HOLES. REMOVED AND REPLACED ON FCB BAFFLE IAW SRM 51-40-02 AND DWG 143A7505 0118, REV -.SDR ASAA2026043066184Skate Angle · crackedAFT TOP SIDE OF ECS BAY AT STA.661.95 SKATE ANGLE IS CRACKED AT RIVET ON RIGHT SIDE OF KEEL BEAM. GROUNDED - YES. REPAIRED SKATE ANGLE AT STA 661.95 RBL9 IAW B737-900ER SRM 57-10-10-2R-5. ACCOMPLISHED LEAK CHECK OF REPAIR IAW B737-900 AMM 28-11-00-400-801. LEASDR SWIA2026043076015Doubler · corrodedCOCKPIT RT INBD FLOOR DOUBLER HAS CORROSION AT MULTIPLE LOCATIONS, FR 10-12. REPAIRED RT COCKPIT FLOOR DOUBLER WITH FILLER/DOUBLER REPAIR IN 2 LOCATIONS REF ETD2026-170-007956 REV. A.SDR MASA20260512105Floor Support · corrodedDURING HEAVY CHECK, INSPECTIONS OF THE INTERNAL FUSELAGE FLOOR STRUCTURE AT FWD WET AREA., CORROSION FOUND AT FR 16, LBL 45.HAS BEEN REMOVED BY BLENDING, IAW ERJ 175 SRM 51-10-03, FOUND TO BE WITH IN LIMITS IAW ERJ 175 SRM 53-10-10, TABLE 101, AD06, 10X MAG C/SDR MASA20260512099Web · corrodedDURING HEAVY CHECK, INSPECTIONS OF THE INTERNAL FUSELAGE FLOOR STRUCTURE AT FWD WET AREA., CORROSION FOUND ON WEB BETWEEN FR 12TO FR 14, BETWEEN RBL 36 AND RBL 45. HAS BEEN REMOVED BY BLENDING IAW ERJ 175 SRM 51-10-03, FOUND TO BE WITH IN LIMITS IAW SRM 53-10-SDR IPXA2026043058730Intercostal · corrodedFS 1042, LBL 45, PAX AREA OTBD INTERCOSTAL HAS CORROSION ON UPPER OTBD LIP UNDER NUTPLATE. INSTALLED INTERCOSTAL P/N 149N7559-2 SERIAL NUMBER: TAG058576. AT STA 1042 TO STA 1060 LBL 45 PER SRM 51-40-02-0GSDR AALA202605050896Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN AFT CARGO COMPARTMENT WEB FITTING AT STA 727 AND LEFT HAND S18A. REPAIRED FITTING PER AARD 51-00-05-1.SDR CALA2026050415960Transition Panel · corrodedFWD CARGO FWD OF DOOR CUTOUT TRANSITION STRIP HAS SEVERAL AREAS OF CORROSION. REMOVED CORROSION ON FWD CARGO FWD OF DOOR CUTOUT TRANSITION PANEL. FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02 STEP 9. REMOVED AND REPLACED TRANSITION STRIP IAW SRM 51-40-02 AND BASDR REXA2026050400452Stringer · damagedSTRINGER 16R AT F.S. 193 - F.S. 202 P/N CC670-33350-4 REQUIRES FABRICATION FOR USE ON HN00305790. FABRICATED, LOCATED AND DRILLED NEW SERVICEABLE STRINGER 16R LOCATED AT F.S. 193 - F.S. 202 (P/N CC670-33350-4) PER SAMPLE AND IAW CRJ-900 SRM 51-24-36-001-001-A0SDR DALA2026050102771Angle · crackedCRACKED ANGLE AT WING CENTER, STA 663 RBL 11. REPAIRED CRACK ON ANGLE AT WING CENTER, STA 663 RBL 11 IAW B737 SRM 57-10-10-2R PROCEDURE 5. (LOG 1571072 - AIRCRAFT WAS GROUNDED).SDR DALA2026050102767Floor Support · corrodedCORROSION OUT OF LIMITS, SUPPORT FLOOR NEXT TO LOWER SILL AT L4 DOOR WITH ORIGINAL THICKNESS: 0.071 IN AND MINIMUM REMAINING THICKNESS 0.050IN THEREFORE IT IS OUT LIMITS PER B757-300 SRM 53-60-15-1A PROCEDURE 1 ALLOWABLE DAMAGE 1 FIG. 101 DETAIL V. CORROSIOSDR DALA2026050102765Shear Plate · corrodedCORROSION LEVEL 2 SHEAR PLATE STR 23R BTW FR69 AND FR70 AT AFT GALLEY AREA. REPLACED SHEAR PLATE AND FASTENERS LOC. STR 23R BTW FR69 AND FR70 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM 51-72-11. (LP 1571111- AIRCRAFT WAS GROUNDED)SDR DALA2026050102764Web · corrodedCORROSION LEVEL 2 WEB BTW FR69 TO FR70 AND STR23R AT AFT GALLEY AREA (SSI 534 147). REPLACED WEB, AND FASTENERS BTW FR69 TO FR70 AND STR23R AT AFT GALLEY AREA AS PER A319 SRM 51-72-11, A319 SRM 51-42-11. (LP 1571108 - AIRCRAFT WAS GROUNDED)SDR DALA2026050102763Web · corrodedCORROSION LEVEL 2 WEB FRAME 20 RH SIDE AT LEVEL STR 23 AT FWD GALLEY AREA. REPLACED WEB AND FASTENERS LOC ON FR20 TO FR24 RH SIDE AT LEVEL STR 23 AT FWD GALLEY AREA AS PER A319 SRM 51-72-11 AND SRM 51-42-11. (LP 1570957 - AIRCRAFT WAS GROUNDED)SDR DALA2026043002739Strip · corrodedAFT CARGO STRIP FOUND CORROSION AT STA 1109 S-36R. REPAIRED AS PER ER/A 633828-14 (1570144) (AIRCRAFT GROUNDED)SDR 2026F00091Bracket · corrodedMECHANICALLY REMOVED 8 AREAS OF CORROSION WHERE 8 LOCK FASTENERS WERE PREVIOUSLY REMOVED ON FWD BRACKET INSIDE NLG WHEEL WELL, ON FWD FACE OF UP-LOCK BRACKET IAW SRM 51-70-02. FOUND CORROSION BLENDS TO BE BEYOND LIMITS IAW SRM 51-70-02 EXCEEDING .002" OF MATESDR SWIA2026042977015Floor Support · corrodedRBL 9 FLOOR BEAM CAP ANGLE IS CORRODED AT MULTIPLE LOCATIONS BETWEEN F.S.409+128 TO F.S.559 (C-CHECK RO 08/28/2026)CUTAWAY CORRODED FLOORBEAM CAP ANGLE AT FS409+118 & FS559.00+10 AND INSTALLED NEW FABRICATED CAP ANGLE AT SAME LOCATION IAW ALL STEPS MHIRJ REOSDR SWAA2026060193943Intercostal · crackedFAULT RAISED TO CAPTURE RII LABOR OF CRACK ON WEB INTERCOSTAL LOCATED BTW BS 344 TO BS 360 LBL 10 WL 208.1 AT FWD GALLEY AREA. REPLACED INTERCOSTAL AND FASTENERS LOCATED BTW BS 344 TO BS 360 LBL 10 WL 208.1 AT FWD GALLEY AREA IAW SRM 53-10-15; SRM 51-40-02 ASDR REXA2026052900878Attach Angle · corrodedCORROSION ON ATTACHMENT ANGLE OF BONDING JUMPER ON TOILET SERVICE DOOR AT FWD LOWER FUSELAGE CORROSION ON ATTACHMENT ANGLE OF BONDING JUMPER ON TOILET SERVICE DOOR AT FWD LOWER FUSELAGE. WAS REMOVED AND EVALUATED OUT OF LIMITS PER CRJ900 SRM 51-21-06-001-001-SDR SWAA2026052794062Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 BL 0 WL 208.1 AT PASSENGER CABIN. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BETWEEN BS 380 TO BS 400 BL 0 AND WL 208.1 AT FLOOR STRUCTURE OF PASSENGER CABIN AREA IAW SRM 51-10-02-0G-0 PARAGRAPH 9; SRM 51SDR SWAA2026052794060Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 10 WL 208.1 AT PASSENGER CABIN. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BETWEEN BS 380 TO BS 400 RBL 10 AND WL 208.1 AT FLOOR STRUCTURE OF PASSENGER CABIN AREA IAW B737-800 SRM 51-10-02-0G-0 PARAGR
Back to JASC 5320