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 DALA2026042002471Fitting · crackedCRACK INTERNAL STRUCTURE FITTING LOCATED BTW FR 11 TO FR 12 AND -Y765 IN COCKPIT. REPLACED FITTING LOCATED BTW FR 11 TO FR 12 AND -Y765 IN COCKPIT IAW SRM 51-42-11, SRM 51-72-11, AND DWG D53110097, (LP: 1551681). AIRCRAFT WAS GROUNDEDSDR IPXA2026042970084Profile · crackedM.C.DECK LH FR#79 Z-PROFILE CRACKED DOT#58-07. REMOVED CRACKED Z-PROFILE BTW C77 TO C79 LH SIDE MAIN DECK IAW A300-600 SRM 51-40-21-001. INSTALLED NEW Z-PROFILE AT M.C. DECK LH FR#79 IAW A300-600 SRM 51-40-21.SDR IPXA2026050267681Profile · corrodedAFT CARGO-FRAME 57 CEILING STRUCTURE FROM LH TO RH SIDE HAS CORROSION AROUND MULTIPLE HOLES. SH 91148554. REMOVED DAMAGE (02 EA) ON ANGLE SUPPORT, CEILING STRUCTRURE FR-57, BETWEEN Y1959 AND Y450 IAW A300-600 SRM 51-74-10-201. INSTALLED NEW PROFILE (CEILING STSDR SWAA2026052090784Stiffener · crackedCRACKED STIFFENER FRONT SPAR LOCATED BS 540, LBL 24.75 AT CENTER SECTION. REPLACED STIFFENER FRONT SPAR, IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, DWG 111A6000, SHEET 245, REV-, AND DWG 111A2001, SHEET 77, REV-.SDR IPXA2026051567636Profile · corrodedAFT CARGO-FRAME 54-54.2 CEILING STRUCTURE RUNNING FWD AND AFT, LH AND RH STRUCTURE HAS CORROSION AROUND MULTIPLE HOLES. REMOVED DAMAGE (01 EA) ON ANGLE SUPPORT, CEILING ESTRUCTRURE BETWEEN CROSS BEAM 54 TO 54.2 , Y-450. IAW SRM 51-74-10-201. INSTALLED NEW PLSDR IPXA2026042968001Bracket · crackedAFT CARGO- FRAME 54 RH SIDEWALL BRACKET IS CRACKED. INSTALLED BRACKET AT FRAME 54 RH SIDEWALL, IAW A300-600- SRM 51-40-21-001. NEW PART NUMBER A53410765218PNSU, IAW GMM 09.08.01.04.SDR SWAA2026050690771Angle · crackedCRACK ANGLE LOCATED BS 695 RBL1 AT CENTER WING BOX . REPLACED ANGLE AND FASTENERS LOCATED BS 695 RBL1 AT CENTER WING BOX IAW SRM 51-10-02 ITEM 9, SRM 51-40-02 AND DWG 273A9110; SHEET 6, REV A.SDR IPXA2026050170017Web · crackedMAIN CARGO DECK RT FR 77 OTBD OF SIDEWALL LOWER WEB HAS A CRACK. REMOVED CRACKED WEB BTW C76 TO C77 RT SIDE MAIN DECK IAW SRM 51-40-21-001. INSTALLED NEW WEB 2 ANGLES AND 1 PROFILE ON MAIN CABIN BETWEEN C76 TO C77 SIDEWALL LOWER I.A.W AIRBUS SRM 51-40-21.SDR IPXA2026042968063Bracket · crackedAFT CARGO- FRAME 54 LT SIDEWALL BRACKET IS CRACKED. INSTALLED BRACKET AT FRAME 54 LH SIDEWALL, IAW SRM 51-40-21-001.SDR IPXA2026042870068Profile · crackedMAIN CARGO DECK RH FR 74 Z PROFILE CRACKED. REMOVED CRACKED Z-PROFILE BTW C73 TO C76 RH SIDE MAIN DECK IAW SRM 51-40-21-001. INSTALLED NEW Z-PROFILE TRAVELER NUMBER:T26/1862656 BTW C73 TO C76 RH SIDE MAIN DECK IAW SRM 51-40-21-001. OK TO TOP COAT HEAD OF FASTSDR IPXA2026042870092Profile · crackedMAIN CARGO DECK LT FR 74 Z-PROFILE CRACKED. REMOVED CRACKED Z-PROFILE BTW C73 TO C76 LH SIDE MAIN DECK IAW SRM 51-40-21-001. INSTALLED NEW Z-PROFILE AT MAIN CABIN L/H C73 TO C76 IAW SRM 51-40-21-001.SDR SWAA2026042890560Web · crackedAPB APEX DOME HAS SURFACE WEB CRACK AT STR23R FROM UPPER LH RIVET GOING TO CENTER EDGE OF DOME. REPAIRED PER EA 26-153-01061 WITH AN INSPECTION THRESHOLD DEFINED IN 26-153-01061-DTI..SDR DALA2026042202560Intercostal · crackedSHIP 9571 CRACK ON INTERCOSTAL ON UPPER AFT CORNER ALSO CRACK NEAR FASTENERS ON CLIP IN THE SAME INTERCOSTAL X=0 ON STA Y=1022 AT CPAX. REPAIRED PER B717-200 SRM 53-00-00 (1550325) (AIRCRAFT GROUNDED)SDR N6WA2026042004Floor Support · corrodedCORROSION ON FLOOR SILL AT FS280-FS319. REMOVED AND REPLACED RH SILL AT FS280-319.00 IAW CRJ SRM 51-42-06.SDR DALA2026042002470Web · corrodedCORROSION WEB FRAME 16 RH SIDE AT FWD GALLEY AREA. REPLACED WEB, LOC. BTW FR12 TO 16 RH SIDE AT FWD GALLEY AREA IAW SRM 51-42-11, SRM 51-72-11 AND DWG D53112780, & DWG D53918884. TOOK MEASURES OF CORROSION ON WEB ARE: L= 3.832IN W=1.570 IN. (LP: 1551636). ASDR DALA2026042002468Fitting · crackedCRACKED FITTING. LOCATED BTW FR 11 TO FR 12 AND -Y 765 IN COCKPIT. REPLACED FITTING (1 EA) LOCATED BTW FR 11 TO FR 12 AND -Y 765 IN COCKPIT TOOK MEASURES OF CRACK L:0.468 INCH IAW SRM 51- 42-11, SRM 51-72-11, AND DWG D53110097. (LP: 1551630). AIRCRAFT WAS SDR JR2R20260418660Floor Support · corrodedL/H FLOOR SILL AT FR16 LBL40 IS CORRODED. REPLACED PER SRM.SDR VNAA20260418012Bracket · crackedCRACKS ON SUPPORT BASE MAIN BATTERY DIRECT BUS AT FWD EQUIPMENT COMPARTMENT. SUPPORT BASE MAIN BATTERY DIRECT BUS AT FWD EQUIPMENT COMPARTMENT WAS REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01.SDR VNAA20260418011Web · crackedCRACK ON WEB BTW FS195 TO FS205 AND WL79.50 INTERNAL STRUCTURE AT FWD EQUIPMENT COMPARTMENT. CRACK ON WEB BTW FS195 TO FS205 AND WL79.50 INTERNAL STRUCTURE AT FWD EQUIPMENT COMPARTMENT. WAS REPAIRED PER CRJ-900 SRM 53-11-43-201-001-A01.SDR VNAA20260418010Bracket · crackedCRACK FWD ANGLE SUPPORT (2EAS) ON ACUMULATOR AT INTERNAL NOSE HYD COMPARTMENT. CRACK FWD ANGLE SUPPORT (2EAS) ON ACUMULATOR AT INTERNAL NOSE HYD COMPARTMENT WERE REPLACED PER CRJ900 SRM 51-42-21-001-001-A01 AND SRM 51-41-02-001-001-A01.SDR VNAA20260418006Diaphragm · crackedCRACK ON SUPPORT STRUCTURE ON FS 849 AND STGR 24L BELLOW FUSELAGE FAIRING 195DL. CRACK ON SUPPORT STRUCTURE ON FS 849 AND STGR 24L BELLOW FUSELAGE FAIRING 195DL WAS REPAIRED REO 690-53-82-277 REV. -.SDR SWIA2026041776850Floor Support · corrodedRBL 9 FLOOR SUPPORT HAS MULTIPLE AREA OF CORROSION FROM BS 409+128 TO 559. PERFORMED A MAJOR REPAIR BY REPLACING THE RT RBL 9 FLOOR SUPPORT FROM BS 409+128 - 559 IAW REO 601R-53-00-005 IAW 601R-53-51-3428. COMPLETED STRUCTURAL MAJOR REPAIR TASK CARD 51-900-10SDR SWIA2026041776847Floor Support · corrodedLBL 9 FLOOR SUPORT HAD MULTIPLE AREAS OF CORROSION ON INBD AND OTBD FLOOR SUPPORT BS 409+128 - 559. PERFORMED A MAJOR REPAIR BY REPLACING THE UPPER CAP OF THE LBL 9 FLOOR SUPPORT BTWN BS 409+128 & 559 IAW REO 601R-53-41-3427, REV-. COMPLETED TASK CARD 51-900-SDR IPXA2026061056670Fitting · gougedMAIN CARGO DECK RH FRAME 47 SPLICE FITTING BETWEEN STRG 24 AND STRG 26 HAS GOUGES ON FWD FACE OF SPLICE FITTING. ACCOMPLISHED PERMANENT REPAIR PER EO-97689-REQ1 AND EA 300-5236-27-A4484 REV. -.SDR CALA2026052116424Support Angle · corrodedCORROSION-FWD WET AREA L-1 CUTOUT THRESHOLD I/B SUPPORT ANGLE. REMOVED AND REPLACED SUPPORT ANGLE AT L1 DOOR THRESHOLD I/B POSITION IAW SRM 51-40-02-0G-0, AND DWG 141A8110,SDR SWAA2026050690234Scuff Plate · crackedCRACK FWD CORNER SCUFF PLATE AT AFT CARGO DOOR CUT-OUT. REPAIRED FWD CORNER SCUFF PLATE AT AFT CARGO DOOR CUT OUT IAW SRM 53-60-15-2R-1, REPAIR 1, & BAC 5975.SDR SWAA2026050690233Scuff Plate · crackedCRACK AFT CORNER SCUFF PLATE AT AFT CARGO DOOR CUT-OUT. REPAIRED AFT CORNER SCUFF PLATE AT AFT CARGO DOOR CUT OUT IAW B737-700 SRM 53-60-15-2R-1 REPAIR 1. AND BAC 5975.SDR SWAA2026042490498Scuff Plate · crackedCRACK ON AFT SCUFF PLATE AT AFT CARGO COMPARTMENT DOOR CUTOUT. REPAIRED AFT CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IN ACCORDING WITH SRM 53-60-15-2R-1; REPAIR 1.SDR CALA2026042215592Transition Panel · corrodedFWD CARGO LEFT SIDE TRANSITIONAL PANEL FROM STA 500E-500B HAVE SIGN OF CORROSION AT MULTIPLE PLACES. TRANSCRIBED FROM AAR GSO NON-ROUTINE 9288805 ORIGINATED BY AAR GSO MECH V899802 COMPLETED ESFR AREA OF CORROSION FOUND TO BE EXFOLIATED ON FWD CARGO LH TRANSISDR DALA2026042202590Stiffener · crackedCOCKPIT FLOOR STRUCTURE STIFFENER FOUND CRACK AT STA 246, LBL 40. REPAIRED AS PER B767-300 SRM53-10-51 (1548932) (AIRCRAFT GROUNDED)SDR DALA2026042102511Floor Support · crackedCRACKED INTERCOSTAL OF FLOOR STRUCTURE BTW STA Y= 1002 TO 1022 X=0 AT CPAX. REPAIRED PER B717-200 SRM 51-70-11 (1549483) (AIRCRAFT GROUNDED)SDR CALA2026042015542Floor Support · corrodedMAIN CABIN AFT WET AREA, INTERCOSTAL CORRODED ON UPPER SURFACE BETWEEN BS 927 AND 947.5 APPROX RBL10. REMOVED, LOCATED, DRILLED AND INSTALLED NEW INTERCOSTAL IAW SRM 51-40-05 AND DWG 147A5760 REV-.SDR DALA2026042002480Floor Support · corrodedCORROSION AROUND FASTENER HOLE ON FLOOR SUPPORT STRUCTURE R/H SIDE BETWEEN FR 76 AND FR78 APPROX RBL 37.5 SECOND FROM FORWARD FASTENER HOLE. C/W ER/A 633633-14 REV ORIGINAL ASSOCIATED ER/A 14-633633 ADDED FOR AC 8135. (LP# 1549486)SDR F3LA202604200401Shear Plate · crackedREFERENCE LTPR NR 5001479409-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. FOUND CRACK ON RH SHEAR PLATE AND REQUIRES REPLACEMENT AS PER A320N SRM 51-72-11 REV.48. PERFORMED REPLACEMENT OF R/H SHEAR PLATE AS PER A320N SRM 51-72-11 REV. 48 MSDR F3LA202604200400Shear Plate · crackedREFERENCE LTPR NR 5001479408-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. FOUND CRACK ON LH SHEAR PLATE AND REQUIRES REPLACEMENT AS PER A320N SRM 51-72-11 REV.48. RERFORMED REPLACEMENT OF LT SHEAR PLATE AS PER A320N SRM 51-72-11 REV. 48 MX SDR DALA2026042002467Floor Support · damagedMISSING MATERIAL FLOOR SUPPORT LOCATED BTW FR 14 TO FR 16 AND Y940 AT FWD GALLEY AREA. REPLACED FLOOR SUPPORT LOCATED BTW FR 14 TO FR 16 AND Y940 AT FWD GALLEY AREA AS PER A320 SRM 51-72-11; A320 SRM 51-42-11 AND DWG D53112823; ISSUE: F00; RELEASE DATE:14-MARSDR JR2R20260417667Support Bracket · corrodedAFT WET AREA FLOOR SUPPORT AT FR87 RBL24 IS CORRODED. REPLACED PER SRM.SDR JR2R20260417663Gusset · corrodedAFT WET AREA GUSSET AT FR90 BL0 IS CORRODED. REPLACED PER SRM.SDR AALA202606040950Shear Plate · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23L. REPLACED SHEAR PLATE PER SRM 51-72-11.SDR AALA202606034032Shear Plate · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR SHEAR PLATE AT FR 69 AND S23R. REPLACED SHEAR PLATE PER SRM 51-42-11.SDR AALA202605260376Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSENGER / CREW DOOR CUTOUT LOWER SILL CENTER SHAPE FITTING AT FR 67 AND S23R. REPLACED CENTER SHAPE FITTING PER SRM 51-72-11.SDR ASAA2026041665820Intercostal · crackedPASS CABIN, FWD WET AREA, INTERCOSTAL BETWEEN STA 360-344 IS DAMAGED. GROUNDED - YES. REMOVED AND REPLACED PASS CABIN, FWD WET AREA INTERCOSTAL BETWEEN STA 360-344 I.A.W. B737-800 SRM 51-40-02-06-0.SDR IXXA20260428001Stiffener · crackedSTA. 246 FLOORBEAM HAS A CRACKED VERTICAL STIFFENER ON FWD SIDE OF BEAM AT LBL 26, AS SEEN FROM LEFT TUNNEL OF MEC.SDR IPXA2026042428172Scuff Plate · dentedDENTED SCUFF PLATE, BULK CARGO DOOR CUTOUT LOWER AFT CORNER AREA. REPLACED IAW AMM 53-13-02-404-007 REV.147 TO INSTALL SCUFF PLATE. IAW AMM 53-13-02-404-007 REV.147 TO INSTALL SCUFF PLATE.SDR IPXA2026042227994Support Angle · brokenFOUND MAIN DECK CARGO CREW ENTRY DOOR LOWER SILL DAMAGE UNDER SCUFF PLATE. (REPLACE) INSTALL NEW LLIPLAY I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO: 141T8310 SHEET.4 REV.HSDR AALA202604224749Shield · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT SHIELD BETWEEN STA 767 AND STA 787 AT RBL 25. REPLACED SHIELD PER AARD 51-00-05-1.SDR DALA2026042002487Support · corrodedCORROSION ON SIDEPLATE SUPPORT ZEE LH SIDE FROM STA 727A - 787, LBL 21. AT AFT CARGO COMPT. SIDEPLATE SUPPORT ZEE REPLACED IAW SRM 51-40-02-0G. (LOG 1547983 - -AIRCRAFT WAS GROUNDED).SDR CALA2026041715436Insulation · contaminatedFWD CARGO BAY LT FROM BS 718 - 755, AND BELOW CARGO FLOOR PANEL INSULATION ARE SOAKED WITH WATER DUE TO POTABLE WATER LEAKING FROM LAV C. REMOVED INSULATION BLANKETS . REINSTALLED NEW INSULATION IAW AMM 53-01-01-000-808.SDR DALA2026041702445Floor Support · corrodedCORROSION FLOOR BEAM -Y1162.5 LOCATED BTW FR 68 TO FR 69 AT AFT GALLEY AREA (SSI 534147). REPLACED FLOOR BEAM -Y1162.5 LOCATED BTW FR 68 TO FR 69 AT AFT GALLEY AREA AS PER A320 SRM 51-42-11 , A320 SRM 51-72-11 AND DWG D53472780; RELEASE DATE: 26-APR-18; ISSUESDR DALA2026041702443Web · corrodedCORROSION WEB LOCATED AT FR 20 AND -Y1732 AT FWD GALLEY AREA. REPLACED WEB LOC. BTW FRAME 20 AND -Y1732 AT FWD GALLEY AREA AS PER A320 SRM 51-42-11, A320 SRM 51-72-11 AND DWG: D53114392, ISSUE: B00, RELEASE DATE:01/ FEB/19. CORROSION MEASURE WERE: L= 1.442 I
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