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 HNAA2026061700545Floor Support · corrodedDURING A DOUBLER INSTALL FOUND ADDITIONAL CORROSION ON LH FLOOR SILL AT FR 40. FABRICATED AND INSTALLED DOUBLER ON MID CABIN LH FLOOR SILL AT FR40 IAW ETD 2026-145-008549 REV: B. SEE MAJOR EO# EO1-53-26-0243SDR ASAA2026052166732Shield · corrodedAFT CARGO SHIELD FWD OF CARGO DOOR IS CORRODED. GROUNDED - YES. REMOVED AND REPLACED AFT CARGO SHIELD FWD OF CARGO DOOR IAW B737-800 SRM 51-40-02-0G-0.SDR ASAA2026052166730Shield · corrodedFWD CARGO SHIELD AFT OF DOOR HAS CORROSION. GROUNDED - YES. REMOVED AND REMPLACED FWD CARGO SHIELD AFT OF DOOR IAW SRM 51-40-02-0G-0 STEP 7.SDR MASA20260608146Floor Support · corrodedDURING HEAVY CHECK INSPECTIONS OF THE INTERNAL FWD FUSE FLOOR SUPPORT CORRODED FLOOR SUPPORT ANGLE AT FR 16 RT, RBL 28 REMOVED AND REPLACED IAW SRM 51-41-01, REV 45, CORROSION LEVEL2SDR HNAA2026060500490Support Bracket · crackedLEFT PACK FUSELAGE SUPPORT (ANTI-ROTATION SUPPORT) BRACKET CRACKED. R & R SUPPORT BRACKET IAW SRM 51-40-02.SDR CALA2026052816589Transition Panel · corrodedFWD PIT TRANSITION PANEL UPPER SURFACE HAS CORROSION FROM APPROX STA 500+15 - 500D, LH SIDE. REMOVED CORROSION IAW B737-900ER SRM 51-10-02. ORIGINAL THICKNESS 0.040, MATERIAL LOSS 0.005, REMAINING THICKNESS 0.035 FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMSDR DALA2026052803220Cusp Web · crackedCRACK ON LH SIDE FLOOR CUSP WEB BTW STA Y= 655 AND STA Y=674 AND STA X=60. CRACK ON LT SIDE FLOOR CUSP WEB BTW STA Y= 655 AND STA Y=674 AND STA X=60 WAS REPAIRED PER B717-200 SRM 53- 00-55 (1606007) (AIRCRAFT GROUNDED)SDR 2026FA0000443Structure · degradedPROBLEM: A ZIP DRONE RETURNED TO DOCK AT PEA RIDGE WITH A BROKEN PROPELLER AND BOOM ARM AFTER A LOUD POPPING NOISE WAS HEARD ON APPROACH. IMPACT: ONE ZIP AT PEA RIDGE SUFFERED A BROKEN PROPELLER AND BOOM ARM (AFT LEFT). THERE HAVE BEEN NO INJURIES, AND ALL PESDR DALA2026052403132Floor Support · corrodedLEVEL 2 CORROSION FLOOR SUPPORT -Y1292-1162.5 LOC. FR 66 TO FR 68 AT AFT GALLEY AREA. REPLACED FLOOR SUPPORT -Y1292, -Y1162.5 AND LOCATED BETWEEN FR66 TO FR68 AT AFT GALLEY AREA IAW SRM 51-42-11 AND SRM 51-72-11 AND DWG D53472816, ISSUE F, AND DWG D53472780 ISDR DALA2026052403127Floor Support · corrodedLEVEL 2 CORROSION, FLOOR SUPPORT -Y1162.5 FROM FR68 TO FR69 AT AFT GALLEY AREA. REPLACED FLOOR SUPPORT -Y1162.5 LOCATED BETWEEN FR68 TO FR69 AT AFT GALLEY AREA IAW SRM 51-42-11 AND A319 SRM 51-72-11 AND DWG D53472780.SDR 2A6R2026052275501Angle · crackedA CRACK WAS DISCOVERED ON THE EQUIPMENT DECK COVER. THE DAMAGE IS APPROXIMATELY 10MM IN LENGTH. AN APPROXIMATE LOCATION OF THE DAMAGE IS AT F.S. 6100MM, W.L. 2600MM, AND L.B.L. 200MM. A DETAILED DESCRIPTION OF THE PERFORMED TYPICAL DAMAGE REPAIR AND APPROVED RSDR VNAA202607010013Fitting · corrodedCORROSION FLOOR FITTING IN FWD ACCESS 107 (1EA) ON GALLEY 1. NEW FLOOR FITTING P/N: CDSP2019-7C-620 IN FWD ACCESS 107 (1EA) ON GALLEY 1. WAS REPLACED IAW CMM 25-33-44SDR SWAA2026062204623Intercostal · crackedCRACKED INTERCOSTAL BS 344 - 360, RBL 12, WL 200. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-40-02 AND DWG 141A5400, REV -.SDR SWAA2026062204622Intercostal · crackedCRACKED INTERCOSTAL BS 344 TO 360, BL 0, WL 200. REMOVED AND REPLACED THE INTERCOSTAL BS 344 - 360, BL 0 IAW SRM 51-40-02 AND DWG 141A5400, REV -.SDR HNAA2026060400485Support Angle · cracked53-2222 CARGO DOOR MECHANISM MIDDLE SUPPORT CRACKED AT BTW FR67-68 AND BTW STR4-5R. RAR SUPPORT IAW SRM 51-40-02SDR HNAA2026060400486Support · crackedCARGO DOOR MECHANISM LWR SUPPORT CRACKED AT BTW FR67-68 AND AT S5R. RAR SUPPORT IAW SRM 51-40-02SDR HNAA2026060400465Support · crackedCARGO DOOR MECHANISM MIDDLE SUPPORT CRACKED AT BTW FR67-67 AND BTW 4-5R. RAR SUPPORT IAW SRM 51-40-02SDR HNAA2026060400484Support · crackedCARGO DOOR MECHANISM UPPER SUPPORT CRACKED AT BTW FR67-68 AT STR4R. RAR SUPPORT IAW SRM 51-40-02SDR CALA2026052216475Baffle · corrodedFWD PIT LOWER BAFFLE HAS CORROSION ON LOWER SURFACE OF UPPER FLANGE AT APPROX STA 500J+3, RBL 25. REMOVED AND REPLACED BAFFLE FROM STA 500J+3 RBL25 IAW B737-900 SRM 51-40-02 AND BAC DWG 143A7505.SDR CALA2026052216473Baffle · corrodedFWD CARGO COMPARTMENT R/H SIDE STA 500I-STA 500J RBL 21.0 BAFFLE HAS CORROSION. REMOVED BAFFLE IAW B737-900 SRM 51-40-02 AND RECEIVED NEW BAFFLE, FABRICATED REPAIR ANGLE AND INSTALLED BAFFLE IAW B737-900 SRM 53-30-53-2R-1 AND 51-40-02.SDR CALA2026052216471Baffle · corrodedFWD CARGO COMPARTMENT RT SIDE BS 500H - 500I, RBL 21. BAFFLE HAD CORROSION. REMOVED BAFFLE IAW SRM 51-40-02 AND RECEIVED NEW BAFFLE, LOCATED AND DRILLED IAW SRM 51-40-05 AND INSTALLED IAW SRM 51-40-02 AND BAC DWG 143A7505.SDR CALA2026052116448Stiffener · crackedDURING REMOVAL OF FASTENERS BETWEEN BS 955 AND 977 RBL 54.75 ON THE ZEE CHORD CRACKS WERE FOUND IN TWO FASTENERS. . THE STEPS OF REPAIR HAVE BEEN PERFORMED ON NON ROUTINE 3389289. FOR THIS REPAIR WAS ISSUED ECRA 5350-02639. NO MORE MAINTENANCE IS REQUIRED. ALLSDR CALA2026052116446Bracket · brokenDURING OK TO INSTALL, FOUND SUPPORT BRACKET BROKEN. REMOVED AND REPLACED SUPPORT BRACKET AT L2 DOOR UNDER SCUFF PLATE IAW SRM 51-40-02.SDR CALA2026052116442Transition Panel · corrodedCORROSION FOUND AT AFT CARGO TRANSITION PANEL RT SIDE BS 1140 - 1500. UPON REMOVAL OF FLOOR PANEL 153CF. REMOVED TRANSITION PANEL RT BTW STA 1440 TO BS 1530 SIDE IAW SRM 51-40-02-0G AND FABRICATED NEW TRANSITION PANEL AND INSTALLED NEW TRANSITION PANEL FROM SDR VNAA202607300011Web · crackedCRACK ON WEB BTW BS 195 TO BS 205 & WL79.5(RT SIDE) ON INTERNAL STRUCTURE AT FWD EQUIPMENT COMPARTMENT. WEB BTW FS195 TO FS 205 & WL 79.5 RT SIDE ON INTERNAL STRUCTURE AT FWD EQUIPMENT COMPARTMENT WAS REPAIRED PER REO 670-53-11-509 REV. E. AND REO 690-53-11-2SDR REXA2026070301064Plate · corrodedCORROSION ON BRACKET MACHINED (4E/A) AND PLATE (2E/A) AT FWD CARGO COMPARTMENT. BRACKET MACHINED FS517 BTW STGR 22LH TO STGR 23LH AND PATE BTW FS 645 TO FS 661 WERE CLEANED PER CRJ900 SRM 51-26-00-001-001-A01 AND PAINT WAS REMOVED PER CRJ-900 SRM 51-26-01-001-SDR SWAA2026062204620Shield · corrodedCORROSION ON ACB FWD SHIELD WEB BETWEEN BS 767 - 792, RBL 25, WL 156. REMOVED AND REPLACED THE SHIELD IAW SRM 51-40-02-0G-0, AND DWG 146A0081, REV A.SDR SWAA2026062204523Threshold Web · corrodedCORROSION ON FCB SUB THRESHOLD WEB BETWEEN BS 440 - 492, RBL 25, WL 156. P 5 REJECT DUE TO COMMON STRUCTURE TO SUB-THRESHOLD HAS BEEN COUNTERSINK. REMOVED AND REPLACED FCB THRESHOLD WEB IAW SRM 51-40-02-0G-0, DWG 143A8330, REV B.SDR SWAA2026061804517Floor Support · crackedCRACKED ANGLE FLOOR STRUCTURE, BS 380 TO 400, LBL 50 IN PASSENGER CABIN. REPLACED ANGLE FLOOR STRUCTURE IAW DWG 143A5400, SHEET 140, REV- AND SRM 51-40-02-0G-0.SDR SWAA2026061804516Floor Support · crackedCRACKED FLOOR SUPPORT LOCATED BETWEEN BS 380 - 400, LBL 13. REPLACED FLOOR SUPPORT IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A5400, SHEET 184, REV -.SDR AALA202606132655Angle · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON THS COMPARTMENT ACCESS DOOR 312AR CUTOUT INTERNAL STRUCTURE ANGLE AT FR 71 BETWEEN S27R AND S32R. REPLACED ANGLE PER SRM 51-42-11.SDR SWAA2026061004183Baffle · crackedFWD CARGO RT TRANSITION ANGLE SUPPORT BAFFLE BETWEEN STA.500G TO 500H IS CRACKED. REMOVED AND REPLACED NEW FWD CARGO R/H TRANSITION ANGLE SUPPORT BAFFLE BETWEEN BS 500G TO 500H PER SRM 51-40-02.SDR HNAA2026060300482Floor Support · corrodedLEFT OMEGA BEAM CORRODED AT 2 ANCHOR NUT LOCATIONS BTW FR 59-61. REPAIRED IAW SRM 53-24-10.SDR 2026FA0000447Stiffener · crackedAFT FUSELAGE LOWER SKIN STIFFENER FOUND CRACKED. REPLACED WITH NEW STIFFENER.SDR AALA202605271314Threshold · out of positionAIRCRAFT WAS NOT GROUNDED: AFT RIGHT LAVATORY DOOR IS DIFFICULT TO OPEN. VERIFIED LAVATORY-E DOOR IS JAMMING. MAINTENANCE ADJUSTED RIGHT AFT LAV DOOR THRESHOLD PER CMM 25-40-65.SDR AALA202605222166Shear Plate · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 68 AND FR 70 AT +Y1162. REPLACED SHEAR PLATE PER SRM 51-42-11.SDR CALA2026052216469Cusp Web · damagedAFTER REMOVAL OF L2 LOWER SILL CHORD FOUND MAIN CABIN BS 927 TO 951 LT CUSP WEB HAS DOUBLE DRILLED HOLE. REMOVED, REPLACED AND INSTALLED NEW WEB AT BS 927 TO 947+ 4 LBL 58.6 WL208. IAW SRM 51-40-02-0G-0, AND DWG 147A8501, REV-.SDR CALA2026052216465Door Sill · corrodedMAIN CABIN L-2 DOOR SILL IS CORRODED ON THE UPPER SURFACE BETWEEN APPROX STA 947.5 AND 986.5 IN MULTIPLE SPOTS APPROX LBL53. REMOVED REPLACED AND INSTALLED NEW DOOR SILL FROM STA 887+6 TO STA 1006 WL208 LBL58. IAW SRM 51-40-02-0G-0 AND DWG 147A8501 REV C.SDR CALA2026052216463Floor Support · corrodedMAIN CABIN FLOOR SUPPORT IS CORRODED ON THE UPPER SURFACE BETWEEN BS 947.5 & 967 AT APPROX LBL50 . REMOVED, REPLACED, AND INSTALLED NEW FLOOR SUPPORT IAW SRM 51-40-02-0G-0, DWG 147A5650, REV -.SDR CALA2026052216461Floor Support · corrodedMAIN CABIN FLOOR SUPPORT CHANNEL BETWEEN BS 947.5 & 967 IS CORRODED ON THE UPPER SURFACE AT APPROX RBL50. REMOVED, REPLACED AND INSTALLED NEW FLOOR SUPPORT IAW SRM 51-40-02-0G-0 AND DWG 147A5760, REV -. 194SDR CALA2026052216457Web · gougedMAIN CABIN RH STA 927-951 WEB IS GOUGED ON UPPER SURFACE. REMOVED REPLACED AND INSTALLED NEW WEB AT STA 927 TO STA 951 RBL 58.6 WL208. IAW SRM 51-40-02-0G-0. DWG 147A8501 REV B.SDR CALA2026052116438Baffle · crackedFWD CARGO PIT RT SIDE BAFFLE CLIP (AFT) AT STA500J IS CRACKED. REMOVED AND REPLACED FWD CARGO PIT RT BAFFLE CLIP IAW DWG 143A7505, REV-, AND SRM 51-40-02. LOCATED AND DRILLED IAW SRM 51-40-05.SDR CALA2026052116436Baffle · crackedFWD CARGO PIT RT SIDE BAFFLE CLIP (FWD ) AT BS 500K IS CRACKED. REMOVED AND REPLACED FWD CARGO PIT RT BAFFLE CLIP IAW DWG 143A7505, REV-, & SRM 51-40-02. LOCATED AND DRILLED IAW SRM 51-40-05.SDR CALA2026052116434Shield · corrodedFWD CARGO DOOR CUTOUT AFT OF DOOR TRANSITION STRIP HAS SEVEREAL AREAS OF CORROSION. REMOVED CORROSION FROM FWD CARGO AFT SHIELD, ORIGINAL MATERIAL 0.032, MAT REMOVED 0.020, REMAINING THICKNESS IN BLENDED AREA MEASURED .012, FOUND OUT OF LIMITS IAW SRM 53-00-SDR CALA2026052116432Intercostal · corrodedDURING REMOTION OF AFT CARGO SIDEWALLS PANELS, FOUND CORROSION ON INTERCOSTAL BTW BS 747 - 767, RBL 21, REQUIRES REPLACEMENT. REMOVED, LOCATED, DRILLED, APPLIED ALODINE, PRIMER AND INSTALLED NEW INTERCOSTAL IAW SRM 51-40-02-0G-0, 51-40-05-0G-0, AMM 51-21-4SDR AALA202605224971Transition Panel · wornAIRCRAFT IN BASE MAINTENANCE: RIVET PULLED THROUGH ON AFT CARGO COMPARTMENT TRANSITION PANEL AT STA 727G AND LBL 23. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.SDR WX0A2026052032819Profile · corroded(AIRCRAFT NOT GROUNDED) (DEFECT DISCOVERED DURING THE AC HEAVY MX VISIT) NR-00058 CORROSION ON PROFILE LOCATED AT FR 59, BTW STGR 35LH - STGR 38LH, FT CARGO COMPARTMENT. REPLACED LOCATED AT FR 59, BTW STGR 35LH - STGR 38LH, FT CARGO COMPARTMENT AS PER SRM 51-SDR CALA2026052016401Support Channel · crackedFWD CARGO, BS 680, RT SIDE, BTWN CEILING TO UPPER SIDEWALL, CHANNEL HAS CRACKS. REMOVED AND REPLACED SUPPORT CHANNEL AT FWD CARGO STA 680 RH SID E BETWEEN CEILING TO UPPER SIDEWALL IAW B757-200 SRM 51-10-02 AN D SRM 51-40-02.SDR F3LA202605190417Shear Plate · crackedAIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. FOUND CRACK ON RH SHEAR PLATE AFT WET AREA AND REQUIRES REPLACEMENT IAW SRM 51-72-11 REV 49. PERFORMED REPLACEMENT OF RT SHEAR PLATE IAW SRM 51-72-11 REV 49. MX ACTION IS ACCEPTABLE.SDR F3LA202605190415Shear Plate · crackedAIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. FOUND CRACK ON LT SHEAR PLATE AFT WET AREA AND REQUIRES REPLACEMENT IAW SRM 51-72-11 REV 49. PERFORMED REPLACEMENT OF LT SHEAR PLATE IAW SRM 51-72-11 REV 49. MX ACTION IS ACCEPTABLE.
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