JASC 5350
Service difficulty reports · 6,115
Reports filed under 5350 · Aerodynamic Fairings, 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 = '5350' 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 = '5350' 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 IPXA2026070420634Fairing · debondedDEBONDED PANEL, AFT WING TO BODY FAIRING PANEL 193CL EXTERNAL SURFACE. IAW AMM 20-51-01-912-008 REV.116 INSTALL PANEL 193CL. CONDITION CHECK NORMAL.SDR DALA2026070703964Support · corrodedCORROSION MULTIPLE FITTING HOLE AT WTBF SUPPORT STRUCTURE FROM LBL 11 TO RBL 20, FR 36. ACCOMPLISHED ER/A 635384-14 REV-ORIGINAL. ASSOCIATED ER/A 14-635384 ADDED FOR AC. (LP# 1675423; AIRCRAFT WAS GROUNDED)SDR DALA2026070703963Support · corrodedCORROSION MULTIPLE FITTING HOLE AT WTBF SUPPORT STRUCTURE FROM LBL 5 TO RBL 8, FR 40. ACCOMPLISHED ER/A 635384-14 REV-ORIGINAL. ASSOCIATED ER/A 14-635384 ADDED FOR AC. (LP# 1675417; AIRCRAFT WAS GROUNDED).SDR DALA2026070703962Support · corrodedCORROSION MULTIPLE FITTING HOLE AT WTBF SUPPORT STRUCTURE LONGERON AT TO RBL 9 FR 40. ACCOMPLISHED ER/A# 635349-14 REV-ORIGINAL ASSOCIATED ER/A 14-635349 ADDED FOR AC. (LP# 1675181; AIRCRAFT WAS GROUNDED)SDR DALA2026070703961Support · corrodedCORROSION FITTING HOLE AT WTBF SUPPORT STRUCTURE LONGERON AT TO LBL 9 FR 40. ACCOMPLISHED ER/A# 635349-14 REV-ORIGINAL ASSOCIATED ER/A 14-635349 ADDED. (LP# 1675166; AIRCRAFT WAS GROUNDED)SDR DALA2026070703960Support · corrodedCORROSION MULTIPLE FITTING HOLE AT WTBF SUPPORT STRUCTURE LONGERON AT LBL 9, FR 45 . ACCOMPLISHED ER/A 635349-14 REV-ORIGINAL, ASSOCIATED ER/A 14-635349 ADDED. (LP# 1675152; AIRCRAFT WAS GROUNDED)SDR DALA2026070703959Support · corrodedCORROSION MULTIPLE FITTING HOLE AT WTBF SUPPORT STRUCTURE LONGERON AT RBL 9 FR45. ACCOMPLISHED ER/A# 635349-14 REV-ORIGINAL ASSOCIATED ER/A 14-635349. (LP# 1675009; AIRCRAFT WAS GROUNDED)SDR AALA202607011817Fairing · missingAIRCRAFT WAS GROUNDED: FUSELAGE PANEL MISSING RIGHT AFT OF WING UNDER EMERGENCY EXIT FOR LIFE RAFT. MAINTENANCE INSTALLED ESCAPE SLIDE CONTAINER FAIRING 198LB PER AMM 25-62-47.SDR CALA2026062917387Angle · crackedRT WING TO BODY SPRT ANGLE IS CRACKED AT BS 1040, RBL64, (BEHIND PANEL 198AR). REMOVED CLIP ANGLE AT RT WING TO BODY SUPPORT BS 1040, RBL 64, (BEHIND PANEL 198AR) IAW SRM 51-40-02-0G-0, FABRICATED NEW ANGLE, IAW DWG 149N7553 AND AMM 51-21-14-370-801, AMM 51SDR IPXA2026070693040Angle · corrodedRIGHT WTB BS 1300 WTB SUPPORT BRACKET AT LWR SIDE IS CRACKED. INSTALLED ANGLE AT RT WTB BS 1300 IAW SRM 51-470-02-0G.SDR IPXA2026062578498Bracket · corrodedRIGHT WING TO BODY OVER WING BRACKET HAS SIGNS OF CORROSION. REMOVED BRACHET (1EA) AND ATTACHED NUTPLATES FOR ACCESS AT RT WING TO BODY OVER WING IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED ANGLE AT RT WING TO BODY OVER WING IAW SRM 51-40-05-0G-0 OK TO INSTALL SDR IPXA2026062578491Bracket · corrodedRIGHT WING TO BODY OVER WING BRACKET HAS SIGNS OF CORROSION. REMOVED BRACKET (1EA) AND ATTACHED NUTPLATES FOR ACCESS AT RT WING TO BODY OVER IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED ANGLE AT RT WING TO BODY OVER WING IAW SRM 51-40-05-0G-0 OK TO INSTALL ANGLESDR LR7A2026061903868Fairing · crackedDURING SCHEDULED C-3 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RADOME FAIRING CRACKED AT RIVET EDGE AT FS 80, LBL 12, WL 200 . REPAIRED IAW SRM 51-140-11.SDR HNAA2026072400622Panel · crackedPANEL 191ZB RT LEADING EDGE NR 1 STRAP ASSY ( HORSE COLLAR) IS CRACKED AT THE UPPER RADIUS BY FIRST FASTENER HOLE. COMPLIED WITH REPAIR TO THE RT WING-TO -FUSELAGE FAIRING PANEL 191ZB JOIN STRAP PER EMB 145 ETD2026-145-012463 REV.: / AND PIEDMONT EO1-05-26-03SDR REXA2026082601738Diaphragm · crackedCRACK IN LH/RH FAIRING SUPPORT DIAPHRAGM IN STA. FS= 797 TO FS= 807 AND 35LBL & 35RBL AT MLG WHEEL WELL. LH/RH FAIRING SUPPORT DIAPHRAGM IN STA. FS= 797 TO FS= 807 AND 35LBL & 35RBL AT MLG WHEEL WELL WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01SDR REXA2026082601737Diaphragm · crackedCRACK IN LH/RH FAIRING SUPPORT DIAPHRAGM IN STA. FS= 797 TO FS= 807 AND 35LBL & 35RBL AT MLG WHEEL WELL. LH/RH FAIRING SUPPORT DIAPHRAGM IN STA. FS= 797 TO FS= 807 AND 35LBL & 35RBL AT MLG WHEEL WELL WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01SDR SWAA2026072742350Panel · debondedPANEL 191FR L/E IN DISBONDED. REPAIRED IAW SRM 51-70-05-2R-6-B00323, REPAIR 6.SDR IPXA2026071106966Skin · debondedDEBONDED SKIN, LT AFT WING TO BODY FAIRING 193 BL. IAW SRM 53-60-70-2R-0 REFER TO SRM 53-00-70-2R-1 AND SRM 51-70-07-0G-0 REV.107. CONDITION CHECK IS SATISFACTORY.SDR DALA2026061503583Longeron · corrodedER/A 634632-14; A220-100, MID FUSELAGE WING TO BODY FAIRING LONGERONS BTWN FR36-38, FR42-FR45, & FR48-FR52 CORRODED. SUBJECT REPAIR REQUIRES FOLLOW-ON ACTION. ACCOMPLISH 634632-14, SECTION II REPETITIVE INSPECTION WITHIN EVERY 1,000 FLIGHT HOURS FROM 14,712 SDR SWAA2026062208736Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 193B (LEFT SIDE) BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED ACCESS PANEL 193B (LEFT SIDE) BODY FAIRING AT FUSELAGE EXTERIOR IAW SRM 51-70-05-2R-10 REPAIR 10.SDR SWAA2026060808355Panel · delaminatedWING TO BODY FAIRING PANEL 191FR WAS DELAMINATED AT FWD LOWER CORNER. REMOVED, REPAIRED AND REINSTALLED PANEL 191FR IAW SRM 51-70-05-2R-6, AMM 53-51-21-400-803, AMM 53-51-21-000-803, & SRM 51-70-05-2R-6.SDR SWAA2026070608238Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 193AR AT LOWER FUSELAGE. REPAIRED ACCESS PANEL 193AR AT LOWER FUSELAGE IAW SRM 51-70-05-2R-9 REPAIR 9.SDR IPXA2026061648877Support · crackedRIGHT LOWER WING TO BODY FAIRING SUPPORT STRUCTURE, INTERCOSTAL IS CRACKED AT BS 990. INSTALLED INTERCOSTAL IAW SRM 51-40-02-0G-0.SDR IPXA2026061148884Tee Angle · corrodedRIGHT LOWER WING TO BODY FAIRING SUPPORT STRUCTURE, TEE ANGLE HAS EXFOLIATED CORROSION, BTWN BS 1040 AND BS 1060 AT RBL 68. INSTALLED NEW TEE ANGLE RT LOWER WING TO BODY FAIRING SUPPORT STRUCTURE, BTWN BS 1040 AND BS 1060 AT RBL 68 IAW SRM 51-40-02-0G.SDR IPXA2026061249095Frame · corrodedRIGHT LOWER WING TO BODY FAIRING SUPPORT STRUCTURE, FRAME-WEB HAS CORROSION AT BS 1200 RBL 60. INSTALLED 1 EA FRAME WEB IAW SRM 51-40-02.SDR IPXA2026060949184Support Angle · crackedFAULT-STR-Z100- R/H WING TO BODY FAIRING SUPPORT STRUCTURE AT BS 1300, UPPER T-CHORD BRACKET SUPPORT IS CRACKED. DOT 21-14 INSTALLED NEW ANGLE SUPPORT P/N UP-149N7665-8 IAW 757-200 SRM 51-40-02SDR IPXA2026060248829Splice Plate · corrodedRT LOWER WING TO BODY FAIRING SUPPORT STRUCTURE, SUPPORT WEB HAS CORROSION AT BS 860 BL0. SURFACE PROTECTION RESTORATION COMPLIED WITH IAW SRM 51-20-01-0G-0, AMM 51-21-14-370-801 AND AMM 51-21-15-370-801.SDR IPXA2026060249026Angle · corrodedR/H LOWER WING TO BODY FAIRING SUPPORT STRUCTURE, T-CHORD "L" ANGLE HAS CORROSION AT BS 1040 AT RBL 68. VERIFIED STEP 3.INSPECTED SURFACE PROTECTION RESTORATION COMPLIED WITH IAW B757-200 SRM 51-20-01-0G-0, AMM 51-21-14-370-801 AND AMM 51-21-15-370-801.SDR SWAA2026070607857Access Panel · damagedELONGATED HOLE ACCESS PANEL 195CR BODY FAIRING AT LOWER FUSELAGE. REPAIRED ACCESS PANEL 195CR BODY FAIRING AT LOWER FUSELAGE IAW SRM 51-70-05-2R-9, REPAIR 9.SDR SWAA2026070607722Access Panel · elongatedELONGATED HOLES ON ACCESS PANEL 192HR BODY FAIRING AT LOWER FUSELAGE. REPAIRED ACCESS PANEL 192HR BODY FAIRING AT LOWER FUSELAGE IAW SRM 51-70-05-2R-10 REPAIR 10.SDR SWAA2026062207275Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 193B BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED ACCESS PANEL 193B BODY FAIRING AT FUSELAGE EXTERIOR IAW SRM 51-70-05-2R-10, REPAIR 10.SDR DALA2026052803247Support Angle · corrodedCORROSION LEVEL 2, WTB ANGLE SUPPORT BETWEEN FR57 AND FR58, STR33-L AND STR33-R. REMOVED DAMAGED WTB ANGLE SUPPORT BETWEEN FR57 AND FR58, STR 33-L AND STR 33-R AND REPLACED PER A220 ASRP BD500-A-J51-42-06-00AAA-0780A-A AND DWG# PL C01731500 REV-E. (LP 16158SDR REXA2026080401462Strap · corrodedCORROSION SEVERAL PLACES ON METAL STRIP AT FAIRING PANEL 193AB INNER AND OUTER FACE STRAPS ON FAIRING PANEL 193AB WERE REPLACED IAW SRM 51-42-10-001-001-A01.SDR REXA2026080401453Strap · corrodedCORROSION SEVERAL PLACES ON METAL STRIP AT FAIRING PANEL 193AB INNER AND OUTER FACE STRAPS ON FAIRING PANEL 193AB WERE REPLACED PER CRJ-900 SRM 51-42-10-001-001-A01.SDR SWAA2026062906694Access Panel · delaminatedDELAMINATED ACCESS PANEL 194CL BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED ACCES PANEL 194CL BODY FAIRING AT FUSELAGE EXTERIOR IAW SRM 51-70-04-2R-2, REPAIR 2.SDR SWAA2026062206541Access Panel · damagedELONGATED HOLE ON ACCESS PANEL 194E BODY FAIRING AT LOWER FUSELAGE. REPAIRED ACCESS PANEL 194E BODY FAIRING AT LOWER FUSELAGE IAW SRM 51-70-05-2R-8 REPAIR 8.SDR HNAA2026061100499Support Angle · crackedRH EXT CF3 WING TO BODY FAIRING UPPER ANGLE SUPPORT CRACKE AT BTW FR44-45. REPAIRED SUPPORT IAW SRM 53-23-12RE(3)SDR IPXA2026061744578Tail Cone · corrodedAPU EXTERNAL AREA NEXT TO TAIL CONE (STA. 1992) SHOWS EVIDENCE OF CORROSION. INSTALLED BOND ASSY SKIN LOWER PANEL 1 EA AT APU EXTERNAL AREA NEXT TO TAIL CONE BS 1992 IAW B757-200 SRM 51-40-02-0G-0SDR VNAA202608010004Seal · corrodedSEVERAL CORRSION ON SETTLEMENT AREA OF FAIRING ACCESS PANEL 194AB (AFT SIDE), ON SETTLEMENT AREA OF ACCESS PANELS 174BZ, 174DZ 173BZ AND 173DZ ALSO IN ANGLE OF KEEL BEAM NEAR FS 669.40 AT MLG WHEEL AREA. CORROSION WERE REMOVED ON SETTLEMENT AREA OF FAIRING ACSDR VNAA202608010003Diaphragm · corrodedSEVERAL AREAS OF CORROSION ON SETTLEMENT AREA OF FAIRING ACCESS PANEL 194AB (AFT SIDE), ON SETTLEMENT AREA OF ACCESS PANELS 174BZ, 174DZ 173BZ AND 173DZ ALSO IN ANGLE OF KEEL BEAM NEAR FS 669.40 AT MLG WHEEL AREA. CORROSION WERE REMOVED ON SETTLEMENT AREA OF SDR VNAA202608010002Angle · corrodedSEVERAL CORRSION ON SETTLEMENT AREA OF FAIRING ACCESS PANEL 194AB (AFT SIDE), ON SETTLEMENT AREA OF ACCESS PANELS 174BZ, 174DZ 173BZ AND 173DZ ALSO IN ANGLE OF KEEL BEAM NEAR FS 669.40 AT MLG WHEEL AREA. CORROSION WERE REMOVED ON SETTLEMENT AREA OF FAIRING ACSDR SWAA2026061505138Panel · crackedPANEL 194AR INNER SKIN IS CRACKED. REPAIRED IAW SRM 51-70-05-2R-2-A00733, REPAIR 2.SDR JJBA20260526025Radome · damagedLIGHTNING STRIKE HIT AIRCRAFT. PERFORMED LIGHTNING STRIKE INSPECTION. FOUND DAMAGE TO RADOME, LH & RH SPRING TABS & RH WINGLET. REMOVED AND REPLACED RADOME.SDR SWAA2026062204297Access Panel · debondedACCESS PANEL 191FL L/E IS DISBONDED. REPAIRED DISBONDED L/E ON ACCESS PANEL 191FL IAW SRM 53-30-70-2R-1 AND SRM 51-70-05-2R-6.SDR SWAA2026061003734Fairing · corrodedCORROSION FOUND ON LOWER FUSELAGE AT BS 440+14, STRINGER 26L; NEAR LOW RANGE RADIO ALTIMETER ANTENNA AREA. REPLACED (FAIRING ASSY; NUT PLATE ASSEMBLIES; COVER PLATE) IAW AMM 34-33-11 AND DWG 143A3230, REV A.SDR SWAA2026061003735Fairing · corrodedCORROSION FOUND ON LOWER FUSELAGE AT STA 400+7, STRINGER 26L; NEAR LOW RANGE RADIO ALTIMETER ANTENNA AREA. REPLACED THE FAIRING ASSY; NUT PLATE ASSEMBLIES; COVER PLATE IAW AMM 34-33-11 AND DWG 143A3230, REV A.SDR SWIA2026051677295Support Angle · crackedPANEL 161DL SUPPORT ANGLE CRACKED AT APPROXIMATELY BS 476. REMOVED AND INSTALLED A NEW PANEL 161DL SUPPORT ANGLE, BRACKET (PN 601R31037-33) IAW DWG 601R31037, REV F, SRM 51-41-02, SRM 51-42-06, SRM 51-42-10, AND AMM 20-21-00-910-801.SDR IPXA2026060906876Tee Angle · corrodedRH WING TO BODY T-CHORD AT STA 1060 IS CORRODED. INSTALLED NEW T-CHORD IAW SRM B757-200 TASK: 51-40-02SDR IPXA2026052305463Tee Fitting · corrodedRH LOWER W TO B PANEL#198AR STRUCTURAL T-CHORD CORROSION PRESENT INSTALLED T-CHORD LOCATED RBL65 AND BTW STA 1037 TO 1060 WTB. IAW B757-200 SRM 51-40-02. REVIEWEDSDR CALA2026051716305Support Frame · gougedLEFT SIDE FUSELAGE WING-TO-BODY FAIRING SUPPORT AT APPROXIMATELY STA 727 JUST ABOVE FLAP TRACK #4 GOUGED. ACCOMPLISHED REPAIR AT LEFT SIDE FUSELAGE WING-TO-BODY FAIRING SUPPORT FRAME AT STA 727 JUST ABOVE FLAP TRACK #4 AS REQUIRED PER ECRA # 5360-02141, COMP
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