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 SWAA2025090804488Floor Support · corrodedCORROSION ANGLE FLOOR STRUCTURE ON BS 716 AT LEVEL STR 18L AND LBL 64 AT PASSENGER CABIN. REPLACED ANGLE FLOOR STRUCTURE ON BS 716 AT LEVEL STR 18L AND LBL 64 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 144A7730 SHEET 7 REV -.SDR SWAA2025090804739Angle · corrodedCORROSION ANGLE LOCATED BS716 RBL64 WL203.1 AT PASSENGER CABIN. REPLACED ANGLE AND FASTENERS LOCATED BS716 RBL64 WL203.1 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 144A7730 SHEET 8 REV:-.SDR SWAA2025090804490Floor Support · corrodedCORROSION ANGLE FLOOR STRUCTURE ON BS 685 AT LEVEL STR 18L AND LBL 64 AT PASSENGER CABIN. REPLACED ANGLE AND FASTENERS LOCATED ON FLOOR STRUCTURE ON BS 685 AT LEVEL STR 18L AND LBL 64 AT PASSENGER CABIN IAW SRM 51-40-02-0G-0 AND DWG 144A7730, SHEET 9, REV-.SDR SWAA2025090804742Angle · corrodedCORROSION ANGLE LOCATED BS706 RBL64 WL203.1 AT PASSENGER CABIN. REPLACED ANGLE AND FASTENERS LOCATED BS706 RBL64 WL203.1 AT PASSENGER CABIN IAW SRM 51-40-02 AND DWG 144A7700 SHEET 130 REV-.SDR SWAA2025090804744Web · corrodedCORROSION WEB LOCATED BS663.5 RBL64 WL203.1 AT PASSENGER CABIN. REPLACED WEB LOCATED BS663.5 RBL64 WL203.1 AT PASSENGER CABIN IAW SRM 51-40-02 AND DRAWING #144A7730 SHEET 12 REV -.SDR SWAA2025090404740Angle · corrodedCORROSION ANGLE LOCATED BS705 RBL64 WL203.1 AT PASSENGER CABIN . REPLACED ANGLE AND FASTENERS LOCATED BS705 RBL64 WL203.1 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 144A7730 SHEET 8 REV:-.SDR IPXA2025090270617Strap · corrodedFWD CARGO COMPT, BS 800-820 CEILING DECOMPRESSION PANEL SUPPORT HAS CORROSION AND (1EA) NUTPLATE LOOSE. STRAP INSTALLED ACCORDING TO IAW SRM 51-40-02. INSTALLED ANGLES (4 EA) ON FWD CARGO COMPT, STA 800-820 CEILING DECOMPRESSION PANEL, IAW B757-200PF, SRM 51-SDR IPXA2025090271962Tee Fitting · corrodedLOWER CENTER FUSELAGE, STA 1040-1060 LBL 40, LT PACK EXHAUST SUPPORT INTERCOSTAL TEE FITTING HAS EXFOLIATION. INSTALLED 1 NEW TEE FITTING IAW SRM-51-40-02.SDR IPXA2025082770574Support · corrodedFWD CARGO COMPT, BS 580 - 600 CEILING DECOMPRESSION PANEL SUPPORT HAS CORROSION. INSTALLED NEW SUPPORT PANEL IN FWD CARGO COMPT BS 580 - 600 CEILING DECOMPRESSION IAW B757-200 SRM 51-40-02-0G SRM 51-70-13-0G-0.SDR AALA202509024926Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND AFT PASSENGER / CREW DOOR CUT OUT LOWER FORWARD CORNER SHAPE FITTING AT FR 66 AND S23R. REPLACED FORWARD CORNER SHAPE FITTING PER SRM 51-72-11.SDR AALA202509022610Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND AFT PASSENGER / CREW DOOR CUT OUT LOWER AFT CORNER SHAPE FITTING AT FR 68 AND S23R. REPLACED AFT CORNER SHAPE FITTING PER SRM 51-72-11.SDR CALA2025081807905Scuff Plate · corrodedFWD CARGO DOOR LOWER SCUFF PLATE AREA IS CORRODED. REF AAR N/R 97524634. REMOVED AND REPLACED FWD CARGO THESHOLD WEB PER SRM 51-40-02-0G-0 AND DWG#143A8120 ,SDR AALA202508180558Baffle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT BAFFLE ASSEMBLY LOCATED AT BS 500A PLUS 10 INCHES, AT RBL 25. REPLACED BAFFLE ASSEMBLY PER AARD 51-00-05-1SDR AALA202508188026Baffle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT BAFFLE ASSEMBLY LOCATED AT BS 500B PLUS 10 INCHES, AT RBL 25. REPLACED BAFFLE ASSEMBLY PER AARD 51-00-05-1SDR AALA202508189017Baffle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT BAFFLE ASSEMBLY LOCATED AT BS 500C PLUS 10 INCHES, AT RBL 25. REPLACED BAFFLE ASSEMBLY PER AARD 51-00-05-1SDR AALA202508189685Baffle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT BAFFLE ASSEMBLY LOCATED AT BS 500D PLUS 10 INCHES, AT RBL 25. REPLACED BAFFLE ASSEMBLY PER AARD 51-00-05-1.SDR DALA2025081506116Web · crackedCRACKED WEB FR20, S23R, FWD GALLEY. INSTALLED SPLICE 1(E/A) LOC. FR 24 AT LEVEL S23R AT FWD GALLEY AREA IAW SRM 51-42-11.SDR DALA2025081506107Angle · corrodedCORROSION ON LONGITUDINAL ANGLE FROM STA 312 TO STA 323.7 AND STRG S-23L AT E/E COMPARTMENT. LONGITUDINAL ANGLE FROM STA 312 TO STA 323.7 AND STRG S-23L AT E/E COMPARTMENT WAS REPAIRED PER ERA 628115-14 REV. ORIGINALSDR SWAA2025092904008Angle · crackedCRACK ON ANGLE LOCATED FWD FACE BS 685 BL 0 WL 208.1 RT SIDE AT PASSENGER CABIN. REPLACED ANGLE LOCATED FWD FACE BS 685 BL 0 WL 208.1 RT SIDE AT PASSENGER CABIN; IAW B737-800 SRM 51-40-02; SRM 51-10-02 PARAGRAPH 9 AND DWG # 273A9110; SHEET: 6; REV: A.SDR SWAA2025092904010Angle · crackedCRACK ON ANGLE LOCATED BS 685 RBL 24.75, WL 208.1 IN PASSENGER CABIN. REPLACED ANGLE IAW SRM 51-10-02, PARAGRAPH 9, SRM-51-40?02, AND DWG 273A91100, SHEET 6, REV A.SDR SWAA2025092904006Intercostal · crackedCRACK ON INTERCOSTAL LOCATED BS 540 BTW LBL 0 TO LBL 24.75 WL 208.1 AT PASSENGER CABIN . REPLACED INTERCOSTAL LOCATED BS 540 BTW LBL 0 TO LBL 24.75 WL 208.1 AT PASSENGER CABIN IAW SRM 51-40-02 AND SRM 51-10-02 PARAGRAPH 9 AND DWG # 143A0060 SHEET:64 REV:-.SDR SWAA2025092604005Plate · elongatedELONGATED HOLE ON PLATE LOCATED BS 540 BTW RBL 45.5 TO RBL 56 WL 208.1 AT PASSENGER CABIN. REPLACED PLATE LOCATED ON BREAK PANEL LOCATED BS 540 BETWEEN RBL 45.5 TO RBL 65 WL 208.1 AT PASSENGER CABIN IAW SRM 51-40-02 AND SRM 51-10-02 PARAGRAPH 9 AND DWG # 143SDR SWAA2025092204253Stiffener · crackedFWD CARGO COMPARTMENT 540 BULKHEAD VERTICAL STRUCTURE STIFFENER HAS CRACK STA 540 LBL 24.97. REPLACED BULKHEAD VERTICAL STIFFENER STA 540 LBL 24.97 ON FWD CARGO COMPARTMENT THIS REPAIR IS CATEGORY A; IAW EA 25-157-02272.SDR AALA202509225873Shear Plate · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23R. REPLACED SHEAR PLATE PER SRM 53-42-11,SDR SWAA2025091504266Strap · corrodedCORROSION ON TENSION STRAP AT BS 1006, LBL 7, AND BS 1016+7, LBL 3, WL 208.1. REMOVED AND REPLACED AFT WET AREA TENSION STRAP FROM BS 1006 TO 1016+7; LBL 3 TO LBL 7, WL 208.1 IAW SRM 51-40-02-0G-0, AND DWG 147A5600 REV B.SDR SWAA2025091503994Scuff Plate · crackedAFT CARGO FWD CORNER SCUFF PLATE IS CRACKED. REPAIRED THE CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1.SDR SWAA2025091504267Web · corrodedMULTIPLE CORROSION AREAS ON LT SHIELD WEB AT BS 1016, LBL 4, BS 1016+12, LBL 4, BS 1016+14, LBL10 & LBL 13, BS 1016+12, LBL 18 AND BS 1016+5, LBL 30, WL 208.1. REPAIR PER EA 25-153-02201.SDR SWAA2025091504004Intercostal · crackedFED INTERCOSTAL BETWEEN BS294.5-BS303.9 STR 16L WL216 IS CRACKED. REMOVED AND REPLACED FED INTERCOSTAL FROM BS 294.5 TO BS 303.9, S16L IAW SRM 51-40-02 AND DWG 141A8180 ID: 0027 REV C.SDR SWAA2025091104028Support Plate · corrodedCORROSION FWD CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS500A+1' TO BS500C+10' LBL22 WL156. EVALUATED; LOCATED AND DRILLED; REMOVED AND REPLACED FWD CARGO BAY L/H NEW SECTION FLOOR SIDEWALL SUPPORT PLATE BS480+10 TOSDR SWAA2025091104029Support Plate · corrodedCORROSION AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 LBL22 WL156. CORROSION EVALUATION ON ACB L/H FLOOR TO SIDEWALL SUPPORT BS727B TO BS767 LBL22 WL156 WAS FOUND TO BE OUT OF LIMITS PER SRM 53-00-5SDR SWAA2025091104351Strap · corrodedCORROSION AFT CARGO BAY FLOOR SPLICE STRAP AROUND NUT PLATE HOLE BS727D+6' RBL11.5 WL156. EVALUATED CORROSION ON AFT CARGO BAY FLOOR STRAP BS 727D+6 RBL 11.5 WL 156; FOUND TO BE OUT OF LIMITS; RECEIVED NEW STRAP AND APPLIED ENAMEL; ALL PER SRM 51-10-02-0G-0;SDR AALA202509109293Shear Plate · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR SHEAR PLATE BEYWEEN FR 69 AND FR 70 AT S23L. REPLACED SHEAR PLATE PER SRM 51-42-11.SDR AALA202509093761Floor Support · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL LOCATED FROM BS 947 TO BS 967 AT LBL 24. REPLACED INTERCOSTAL PER AARD 51-00-05-1.SDR IPXA2025082957732Strap · corrodedAFT CARGO COMPARTMENT CEILING DECOMPRESSION PANEL SUPPORT AT STA 1220 -1240 LBL 40 HAS EXFOLIATION CORROSION. INSTALLED AFT CARGO COMPARTMENT CEILING 153AC IAW B757-200 AMM 25-50-01-404-008.SDR IPXA2025082757796Strap · corrodedAFT CARGO COMPARTMENT CEILING DECOMPRESSION PANEL SUPPORT AT STA 1580 LBL 40 HAS CORROSION. INSTALLED CEILING PANEL 161DC AFT CARGO PIT L/H STA 1520-1600 IAW B757-200 SRM 51-40-02.SDR IPXA2025082857775Strap · corrodedAFT CARGO COMPARTMENT CEILING DECOMPRESSION PANEL SUPPORT AT STA 1400-1420 RBL 45 HAS EXFOLIATION CORROSION. INSTALLED CEILING PANEL 154EC IAW B757-200 AMM 25-50-01-404-008.SDR IPXA2025082944844Support Bracket · crackedRH WW, FWD CUTOUT, STA. APPROX 1060, BRACKET #6 (I/B TO O/B) HAS A CRACK. INSTALLED NEW BRACKET AT RH WW, FWD CUTOUT, STA. APPROX 1060 IAW B757-200PF SRM 51-40-02.SDR IPXA2025082741605Support Channel · crackedRIGHT MLG WW FWD SEAL RETAINER ATTACHMENT FRAME CRACKED AT OTBD END. INSTALLED NEW SUPPORT CHANNEL AT RT MLG WW IAW SRM 51-40-02.SDR IPXA2025082752325Strap · corrodedMAJOR REPAIR. AFTER REMOVAL OF APU INLET FOUND CORROSION ON UPPER AFT STRAP PREVIOUSLY REPAIRED. INSTALLED REPAIR PARTS (2) STRAP AND (4) FILLER AT AT AFT OF APU INLET SURRAND STRUCTURE STA 1825, IAW B757-200 SRM 53-80-15-2R-1 REPAIR 1 PAR.4. ACCOMPLISHED SDR ASAA2025081360255Nut Plate · corrodedLH SIDEPLATES ( TRANSITION ) NUTPLATES FALLING OFF DUE TO CORROSION ON SIDEPLATE STA 727-787. GROUNDED - YES. REPAIRED TRANSTION PANEL IAW B737-9MAX SRM 53-00-53-2R-5W:3 O:.040 R:.020 L:10 D:.020.SDR IPXA2025082141090Stiffener · crackedCRACK - ANGLE, FWD MEC AT STA 246 LBL 40 FLOOR STRUCTURE. .ACCOMPLISHED REPAIR I.A.W SRM 53-10-51-2R-4 REV.92 AND EGAT WORK SHEET NO.50647SDR AALA202508205383Fitting · chafedAIRCRAFT IN BASE MAINTENANCE: FORWARD GALLEY SERVICE DOOR FUSELAGE CUTOUT FORWARD FRAME MOUNTED LOWER LATCH TRACK FITTING HAS A CHAFE. REPLACED FITTING PER SRM 51-40-02.SDR AALA202508182229Baffle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT BAFFLE ASSEMBLY LOCATED FROM BS 500B TO BS 500C A LBL 25. REPLACED BAFFLE ASSEMBLY PER AARD 51-00-05-1SDR AALA202508183951Web · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR STRUCTURE K WEB LOCATED AT BS 1004, RBL 32. REPLACED WEB PER EA 367156 AND SRM 51-40-02.SDR F3LA202508130278Floor Support · corrodedFLOOR SUPPORT Y765 AT FR 66-70 FOUND CORRODED. REPLACEMENT IS REQUIRED IAW SRM 51-72-11 REV 44. FLOOR SUPPORT Y-765 AT FR66-FR67 INSTALLED IAW SRM 51-72-11 REV 44.SDR F3LA202508130275Floor Support · crackedAIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION FOUND CABIN FLOOR SUPPORT Y-1292 CORRODED. REQUIRES REPLACEMENT AS PER SRM 51-72-11 REV 44. FLOOR SUPPORT AT Y-1292 WAS REPLACED AS PER SRM 51-72-11 REV 44. FLOOR SUPPORT AT Y-129SDR SWI2025F01449Floor Support · corrodedUPON REPEAT INSPECTION OF THE L/H FLOOR SILL FOUND ADDITIONAL CORROSION AT, FS 413, FS 480, AND FS 537 ON L/H FLOOR SILL (C-CHECK RO 10/19/2025)REPAIRED CORRSION ON LH FLOOR SILL AT FS 413, FS 480, AND FS 537 IAW REO 601R-53-41-666 REV C DATED 2012-11-06. COSDR SWIA2025102000812Floor Support · corrodedUPON REPEAT INSPECTION OF L/H FLOOR SILL FOUND CORROSION ON PREVIOUS REPAIRED LOCATIONS, FS 428, FS 518, AND 541 AROUND SCREW HOLES. (C-CHECK RO 10/19/2025)REMOVED CORROSION FROM LH FLOORSILL AT FS 428, 518, AND 541 AND FOUND IN LIMITS IAW REO 601R-53-41-666SDR JJBA20250916022Support · corrodedCENTER FUSELAGE IV. LH SILL CORRODED BTW FRAME 60-61. CENTER FUSELAGE IV, LH SILL CORRODED BTW FRAME 60-61 BLENDED OUT OF LIMIT. CENTER FUSELAGE IV, LH SILL AT FR 60-61 REMOVED AND REPLACEDSDR ASAA2025081260556Web · corrodedFWD CARGO DOOR SCUFF PLATE SUB FRAME HAS CORROSION IN MULTIPLE LOCATION. GROUNDED - YES. REMOVED CORROSION ON FWD CARGO THRESHOLD WEB ORIGINAL THICKNESS .045, REMOVED .012, REMAINING .033, FOUND TO BE OUT OF LIMITS IAW B737-900ER SRM 53-30-15. REMOVED DAMAGE W
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