JASC 5410
Service difficulty reports · 4,110
Reports filed under 5410 · Nacelle/Pylon, Main Frame, 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 = '5410' 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 = '5410' 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 UIEA2026083000826Fairing · damagedNR 2 PYLON AFT FAIRING FWD LWR FIXED FAIRING DRAIN INBD AND OTBD AREA FOUND SEVERAL RIVETS LOOSE. NR PYLON AFT FAIRING DRAIN REPAIRED IAW RI-54-50-18444, REV.A. NO FURTHER DEFECTS NOTED.SDR VNAA2026083145Hinge · bentLEFT ENGINE COWLING IS UNABLE TO BE OPENED DUE TO A DENTED HINGE LINE THAT WAS BENT UPON ARRIVAL . REPAIRED IAW REO 670-53--31-1226, REV-.SDR SWAA2026090180716Fairing · crackedNR 1 ENGINE AFT FAIRING HEAT SHIELD PLUME SUPPRESSOR HAS A FIVE INCH CRACK 28 INCHES FORWARD OF AFT TIP. PERFORMED TIME LIMITED REPAIR IAW EA 26-154-02358. AIRCRAFT OKAY FOR CONTINUED SERVICE.SDR SWIA2026082977229Frame · chafedCHAFING ON INBD OF FR 1 OF RT AFT PYLON FAIRING. REMOVED AND REPLACED RT AFT PYLON FR1 IAW SRM 51-40-02, & 51-40-08.SDR FDEA202608281248Strut · crackedNR 2 NACELLE STRUT, RIGHT SIDE SKIN, THROUGH ACCESS 443AR, SHOWS A CRACK WITH NO VISIBLE STOP HOLE. THIS ITEM HAS BEEN ACCOMPLISHED ON EA F-5430-T0388382 P1.SDR IXXA2026082800002Cowling · out of toleranceNR 1 ENGINE INBD CORE COWL GAPS ARE OUT OF LIMITS ON TRAILING EDGE IAW AMMSDR IXXA2026082800001Cowling · out of toleranceNR 1 ENGINE OTBD CORE COWL GAPS ARE OUT OF LIMITS ON TRAILING EDGE IAW AMM.SDR IXXA20260919NKJ01Cowling · crackedNUMBER 2 ENGINE OUTBOARD CORE COWL INTERNAL AREA #5 RIB/FRAME HAS CHAFING/WEAR MARKS (IS CRACKED)SDR IPXA2026090126837Bracket · chafedCHAFED BRACKET, NR 1 ENG RT CORE COWL INNER OPEN ROD STOW AREA. REMOVED THE DAMAGE BRACKET IAW SRM 51-40-02-0G, REV 96. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 96, & CMM IPL 71-13-24, REV 51.SDR IPXA2026090123388Bracket · chafedCHAFED BRACKET, NR 2 ENG LT CORE COWL OPEN HOLE ROD BRACKET. REMOVED DAMAGE BRACKET IAW SRM 51-40-02-0G, REV 96. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 96, & CMM IPL 71-13-23, REV 47.SDR IPXA2026090123395Bracket · chafedCHAFED BRACKET, NR 2 ENG RT CORE COWL OPEN HOLD ROD BRACKET. REMOVED THE DAMAGED BRACKETS IAW SRM 51-40-02-0G, REV 96. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 96, & CMM IPL 71-13-24, REV 51.SDR SWAA2026092490877Support Web · crackedCRACKED SUPPORT WEB INBD FAN COWL, LT ENGINE. REPLACED FASTENERS & SUPPORT WEB ON THE INBOARD FAN COWL IAW SRM 51-40-02, SRM 51-10-02, & 71-13-30, PAGE 10094.SDR FDEA202608211201Bulkhead · damagedNR 1 PYLON AFT SPHERICAL BEARING EXISTING BORE HOLE MEASURED DIAMETER = 2.9995. AND FOUND CORROSION. CORROSION AT NR 1 PYLON AFT BULKHEAD CARRIED OUT REPAIR IAW EA 1-5440-T0388481, PART1. THIS EA DEVIATES FROM EO 1-5440-E0385675, PART 1. REPAIR CLASSIFIED SDR SWAA2026092143257Cowling · pulledNR 2 ENGINE INLET COWLING OUTER LIP SKIN FASTENERS AT 2 OCLOCK AND 10 OCLOCK ARE PULLED THROUGH SKIN . REMOVED AND REPLACED #2 ENGINE INLET FAN COWL IAW AMM 71-11-01 AND COMPLIED WITH ACOUSTIC PANEL BLOCKAGE SURVEY IAW SRM 54-00-01. REMOVED AND REPLACED #2 ENSDR DALA2026082404780Cowling · damagedWITH THE PARKING BRAKE SET, THE JETWAY HIT THE AIRCRAFT. PERFORMED INSP IAW AMM 05-51-27-200-001-A FOUND INLET COWL DAMAGED. NO ADDITIONAL DAMAGE NOTED. W.I.P. R & R ENG #1 AIR INTAKE COWL PER AMM 71-11. NO LEAKS. OK FOR SERVICE. (LP: 7916802, AIRCRAFT WAS SDR IXXA20260820003Support Angle · crackedNUMBER 2 ENGINE PNEUMATIC DUCT SUPPORT ANGLE IS CRACKED AT 3 O'CLOCK POSITIONSDR FDEA202608191154Bearing · damagedNR 3 PYLON AFT SPHERICAL BEARING EXISTING BORE HOLE MEASURED DIAMETER=3.040" AND FOUND CORRODED. NR 3 PYLON AFT BULKHEAD CARRIED OUT REPAIR AS PER EA 1-5440-T0388374 PART1, PART 2 AND PART 3. CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR IPXA2026092805259Plate · out of limitsFAIRING 475AL, FWD UPPER I/B SIDE, 3EA FASTENER HOLES ELONGATED AND STRUCTURE BENT AND WITH CHAFFING. DOT 73-155. VERIFIED REMOVAL AND REPLACEMENT OF THE PLATE ON FAIRING 475AL, FWD UPPER I/B SIDE IAW A300-600 SRM 51-40-21.SDR IPXA2026092905418Support · crackedPANEL RACK, FAIRING 475AL, FWD WEB WITH CRACK. DOT 73-169. REMOVED AND REPLACED NEW SUPPORT P/N 221-0081-53 BATCH:0004506588 ON FAIRING 475AL, FWD WEB. IAW A300-600 SRM 51-40-21 REVIEWED.SDR CALA2026081718691Acoustic Panel · inflt separationNR 1 ENGINE ACOUSTIC PANEL NR 6 DEPARTED THE ACFT. MEASUREMENT 33 INCHES LONG & 21.5 INCHES WIDE. TOTAL 709 SQ INCHES. WORK ACCOMPLISHED REF LOG 9970963 & GMM 02-30-95 3C(1) NR 1 ENGINE INSPECTION, FOUND ACOUSTIC LINER PANEL 6 O'CLOCK MISSING & BROKEN OFF ATSDR SWAA2026081736240Frame · crackedLPT REAR FRAME CRACK AT STRUT #16 C1 HAS GROWN TO 1.00" AND NEW CRACK AT STRUT NR 1 C2 MEASURED 0.30" (ENG 01) ENGINE LPT REAR FRAME CRACK AT STRUT #16 C1 HAS GROWN TO 1.00" AND NEW CRACK AT STRUT NR 1 C2 MEASURED 0.30" STURT #16/C1 1.00" STRUT #1/ C2 0.30 COSDR IXXA20260813001Bushing · damagedLATCH RECIEVER BUSHINGS ON NR 1 PYLON INBD SIDE HAVE BEEN OVERSIZED.SDR IPXA2026090730575Mount · gougedSTR- DURING OK TO INSTALL FOUND #2 ENG PYLON AFT STRUT MOUNT I/B SIDE TO HAVE (3) GOUGES FROM BULGING SCREWS ON PNL 443ML ATA 54 ACCOMPLISHED THE REPAIR PER EO-98451-REQ1 AND STE-SAA EA 757-5724-01-B0812 REV IR. CASS FORM COMPLETED ON T3F18E009C5M2SDR IXXA20260811002Duct · crackedINBD CORE COWL EXHAUST DUCT IS CHAFED ON THE LEADING EDGESDR IPXA2026102312775Structure · crackedPYLON #1, TOP SECTION AT RIB 3A, EXTERNAL SURFACE IS CRACKED AND HAS TWO DAMAGED RIVETS.SDR IPXA2026102314263Fan Cowl · damagedLEFT ENG I/B FAN COWL AFT HINGE FWD LUG HAS DAMAGED.SDR HNAA2026092200883Skin · corrodedRT INLET HAS PITTING ON LIP SKIN. R/H INLET REMOVED AND REPLACED ON WO# H10452 S/N 00912 QUANTUM# 4600.SDR UIEA2026081000729Bearing · looseRIGHT PYLON SIDE LINK FITTING, ATTACHED ON RIGHT WING WS 400 FORWARD SPAR LOWER PANEL HAS 1EA LOOSE BEARING. REMOVED AND REPLACED FITTING ASSEMBLY ON RT WING FORWARD SPAR LOWER PANEL WS 400 PER DRAWING 112T7001-2 AND SERVICE BULLETIN 757-54-0081 REV 2 ON BOESDR IPXA2026100692769Plate · crackedNR 2 PYLON RH SIDE PANEL SUPPORT BETWEEN 422DR AND 424CR HAS CRACKED PLATE. NEW FISH PLATE INSTALLED IAW A300-600 SRM 51-40-21. REVIEWED.SDR SWAA2026090361660Support Web · crackedCRACKED SUPPORT WEB INBD FAN COWL, LT ENGINE. REPLACED THE SUPPORT WEB IAW SRM 51-40-02 0G-0, AND CMM 71-13-30, PAGE 1024, SHEET 5, AND PAGE 1112.SDR SWAA2026090232651Cowling · damagedELONGATED FASTENER HOLES ON NR 2 ENGINE INLET COWL LOWER ANTI-ICE OVERBOARD EXHAUST PANEL REF 26-171-01809-TLD [TTG8Q01D1YSU]. LOCATED AND DRILLED NEW PANEL ENGINE INLET NR 2 ENGINE INLET COWL LOWER IAW SRM 51-40-02-0G, AND IPC 71-11-01-02, ITEM 350, DETAISDR AALA202608103873Pin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT ENGINE AFT ENGINE MOUNT UPPER OUTBOARD MOUNT THRUST LINK INNER SHEAR PINS - MAINTENANCE REPLACED INNER SHEAR PINS PER AMM 71-22-11SDR DALA2026080704582Bushing · corrodedPITTING FOUND ON INNER RACE OF R3 INBOARD BUSHING. REPLACED BUSHING NR 436. (LP 1742279 - AIRCRAFT WAS GROUNDED)SDR FDEA202608051086Lug · corrodedNR 3 ENGINE PYLON AFT BULKHEAD LUG BORE HOLE FOUND WITH CORROSION AND DAMAGE AFTER SPHERICAL BEARING REMOVED. REPAIRED IAW EA 1- 5440 -T0388311, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6 -2-100.SDR HYIA20260811001Beam · crackedDURING SCHEDULED INSPECTION A CRACK WAS VISUALLY IDENTIFIED ON THE LEFT HAND CROSSOVER BEAM (OEM: 5654104-11) FORWARD FACE. THIS CRACK MEASURES APPROXIMATELY 1.375 INCHES LONG AND IS CONSISTENT WITH OTHER CRACKS VISUALLY IDENTIFIED ON THESE BEAMS IN THE PAST. SDR IPXA2026081387667Plate · wornNR 1 STRUT AFT FAIRING,INBOARD SUPPORT STIFFENER LINK PLATE BEARING WORN , BS 376.20. (REPLACE)1 ACCOMPLISHED JOB I.A.W UPS E0-98274-REQ1 REV.1 AND EGAT EI F2026A54M-1622 REV.1 AND SRM 51-40-02-0G REV.55 AND DWG 313T2303, SH.96, REV.C AND DWG 313T2303 SH.99 RSDR IPXA2026080987685Support · crackedNR 1 STRUT AFT FAIRING, INBD ZEE CRACK , BS 376.20. REMOVED DAMAGE ZEE INBD SEAL IAW SRM 51-40-02-0G, REV.55. INSTALLED NEW ZEE INBD SEAL IAW SRM 51-40-02-0G REV.55 AND DWG 313T2380, SH 48, REV -, DWG 313T2303, SH 92, REV: C, SH 93 REV: C, SH 98 REV B.SDR 2026FA0000616Cowling · detachedTHE FLIGHT ORIGINATED ON AUGUST 2, 2026, DEPARTING FROM KISM (VELOCITY FBO). BOTH PILOTS PERFORMED EXTERNAL PRE-FLIGHT INSPECTIONS OF THE AIRCRAFT AT SEPARATE TIMES, AND NO ABNORMALITIES WERE NOTED DURING EITHER INSPECTION.
AFTER LANDING AT KRYY, THE PILOT INSDR GRTA20260803003Support Bracket · crackedRH MLG ACTUATOR INBOARD SUPPORT BRACKET CRACKED. REMOVED CRACKED BRACKET AND REPLACED WITH NEW, PN 101-120122-16. REF BEECH SIRM CH 20-50-04.SDR GRTA20260803002Support Bracket · crackedLH MLG ACTUATOR INBOARD SUPPORT BRACKET CRACKED. REMOVED CRACKED BRACKET AND REPLACED WITH NEW, PN 101-120122-15. REF BEECH SIRM CH 20-50-04.SDR GRTA20260803001Support Bracket · crackedLEFT MLG ACTUATOR OUTBOARD SUPPORT BRACKET CRACKED. REMOVED CRACKED BRACKET AND REPLACED WITH NEW, PN 101-120122-13. REF BEECH SIRM CH 20-50-04.SDR SWAA2026080572858Strut · crackedRIGHT ENGINE TRF STRUT 1 WAS CRACKED AT C-1, 0.28 LONG. MERGED BOTH CRACKS TOGETHER ON ONE WRITE UP TTG8Q01DGQ1X.SDR SWAA2026080594116Strut · crackedRIGHT ENGINE TRF STRUT NR 1 IS CRACKED AT C-1 0.28 LONG AND C-2 0.49 LONG. COMPLIED WITH M-21-172-00810 TO TRIGGER EO-7256-I-11716-C THE REPETITIVE INSPECTION INTERVAL OF 1300 CYCLES FOR THE RIGHT ENGINE TRF.SDR IXXA20260731001Frame · chafedTHE UPPER CHORD IS DEEPLY CHAFED, ON THE BULKHEAD ON TOP OF THE RIGHT PYLON, LOCATED AT THE FWD O/B CORNER OF THE 441BT PANEL.SDR IXXA20260730001Pad · gougedNUMBER 1 ENGINE INBD FAN COWL HAS GOUGED RUB PADSDR UIEA2026061400481Frame · chafedNR 4L CORE COWL NR 2 FRAME PATCH FOUND CHAFING ( COUNT FROM FWD )(<P>FRAME REPAIRED AS PER SRM 54-41-02-2R-2 REPAIR 2 FIG 201. NO FURTHER DEFECT NOTED</P>)SDR WX0A2026072932904Bolt · corroded(AIRCRAFT NOT GROUNDED) (DEFECT DISCOVERED DURING AC HEAVY MX VISIT) RT PYLON LOWER AFT FAIRING BOLT (1X) CORRODED. RT PYLON LOWER AFT FAIRING BOLT (1X) REPLACED IAW AMM 54-56-00-400-001-A TW.SDR SWAA2026081746699Strut · damagedRIGHT AFT STRUT FAIRING FRAME HAS ELONGATED HOLES. REPAIRED THE STRUT FAIRING IAW EA 26-154-02060.SDR SWAA2026072938243Fairing · crackedNR 2 ENGINE PYLON AFT FAIRING PLUME SUPPRESSOR CRACK REPAIR REPAIRED NR 2 ENGINE PYLON AFT FAIRING PLUME SUPPRESSOR IAW SRM 54-50-70-2R-7 AFT FAIRING PLUME SUPPRESSOR-DVI EVERY 30 DAYS FOR 3 MONTHS THEN DVI EVERY 120 DAYS. VERIFIED FOLLOW ON -DVI EVERY 30 DAYSSDR UIEA2026072400649Pin · damagedFOUND NR 3 PYLON UPPER LINK FWD PIN AND BUSHING DAMAGE AND PYLON SIDE LUG BUSHING DAMAGE. IAW AMM 54-51-01-004-001 REV 116 AND AMM 54-51-02-004-001-005 REV 116, REMOVED NR 3 PYLON NACELLE STRUT AND ATTACH PIN BOLT. REPAIRED NR 3 PYLON UPPER SPAR LUG BUSHING
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