JASC 5412
Service difficulty reports · 1,087
Reports filed under 5412 · Nacelle/Pylon, Bulkhead/Firewall, 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 = '5412' 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 = '5412' 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 COEA2020101307805Firewall · crackedHATS WO 176998 NR00522, WO 211916 HEAVY CHECK HATS/MAJOR REPAIR. LEFT ENGINE UPPER FIREWALL HAS CRACK AT APPROXIMATELY AREA 3. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0120973_01 16585 ISSUE B, DATED 8/26/2020.SDR IPXA2020062256768Bulkhead · damagedINSPECTION TYPE:3C NR 1 PYLON INTERNAL BULKHEAD INSIDE ACCESS PANELS 438CR/DR HAS ELONGATED HOLE. REPAIRED ELONGATED HOLE ON NR 1 PYLON BULKHEAD WEB AT YWN 315.500 INSIDE ACCESS PANEL 438CR/DR IAW EA 011-5410-01-A8220 AND EO MD11-5410-76813-A. (MAJOR)SDR IPXA2020051555288Bulkhead · corrodedINSPECTION TYPE:2C#3 ENG. PYLON AFT BULKHEAD ASSY. HAS CORROSION COMMON TO THE INNER BORE LUG OF BULKHEAD P/N AUB7502-507 & AUB 7502-509.REPAIRED #3 ENG. PYLON AFT BULKHEAD ASSY. IAW VT-SAA EA 011-5410-01-A8166 REV. I/R AND UPS EO MD11-5410-76449-A. (MINOR).SDR 7C7A2020032600017Firewall · crackedLEFT NACELLE, INBOARD SIDE, LOWER SHEAR WEB (FIREWALL, P/N: 85410594-111) HAS A CRACK (0.550 INCHES LONG).SDR RAIA2020021131002Firewall · cracked#1 PYLON FIRE WALL HAS CRACK AT FRM 67......... REPAIRED #1 PYLON FIREWALL AT FRAME 67SDR ASOA202001217002Firewall · crackedTYS A/C WAS FOUND WITH THE #1 PYLON FIREWALL SKIN CRACKED, CRACKS CONFIRMED BY NDT AND MAINTENANCE REPAIRED THE CRACK SKIN IAW ECTC ETD 2019-145-16243. ALL WORK ACCOMPLISHED AND WAS RELEASED TO SERVICE.SDR IPXA2019103024456Bulkhead · crackedINSPECTION TYPE:SEG#2 ENG NOSE HAS CRACK ON AFT BULKHEAD OTBD SIDEREPAIRED IAW P&W SRM 54-10-00-00- REPAIR 14SDR 7C7A2019090400511Firewall · damaged#1 ENGINE FIREWALL CHAFED BY FIRE LOOP BRACKET. FIRE LOOP BRACKET MOUNTING HOLES IN FIREWALL ELONGATED.SDR 2019FA0000169Firewall · crackedLEFT ENGINE INLET AFT BULKHEAD/FIREWALL CRACK. ACCOMPLISHED TEXTRON AVIATION ENGINEERING LETTER. DQ21738M1REVA (CORRECTED DQ NUMBER, TT AND TL); 750-0203 (N999QS) LEFT ENGINE INLET AFT BULKHEAD/FIREWALL CRACK.SDR 7C7A2019052500505Firewall · crackedDURING ENGINE REMOVAL, A CRACK WAS NOTICED ON FORWARD SIDE OF RIGHT FIREWALL.SDR IPXA2019060342763Bulkhead Web · crackedINSPECTION TYPE:12YR#1 ENG INLET COWL INBD SIDE AT THE 3 O'CLOCK POSITION, THE INLET COWL AFT BULKHEAD IS CRACKED BELOW THE RIGID FITTINGREPAIRED PER P&W SRM 54-10-00 REPAIR #14SDR IPXA2019060342761Bulkhead Web · crackedINSPECTION TYPE:12YR#2 INBD INLET COWL AFT BLKHD WEB IS CRACKED AT SENSE LINEREPAIRED PER P&W SRM 54-10-00 REPAIR #14SDR IPXA2019032740534Bulkhead · crackedINSPECTION TYPE:12Y NR 2 ENGINE INLET REAR BULKHEAD CRACKED AROUND SENSE LINE. REPAIRED PER PW SRM 54-10-00 REPAIR #14.SDR CA190226004Fireshield · damaged(CAN) DURING A MAINTENANCE (A1) INSPECTION EVIDENCE OF ARCHING AND DAMAGE WAS DISCOVERED AT THE L/H ENGINE FIREWALL AT THE DC FEEDER CABLES. AN RD FOR A PERMANENT REPAIR WAS REQUESTED AND RECEIVED FROM BOMBARDIER. THE AIRCRAFT IS CURRENTLY UNDER REPAIR. P/N: 8SDR KCSA201902041023Bulkhead Web · corrodedNR 2 PYLON FWD TORQUE BOX WEB CUTOUT FOR HYDRAULIC LINE HAS CORROSION ON AFT SIDE OF HOLE.SDR A8ZR20181113003Firewall · crackedACCOMPLISHED DOUBLER INSTALLATION FOR CRACK ON UPPER FIREWALL WEB PN 85410554 OF #1 NACELLE RH IB SIDE AT XN 127.00 REF BOMBARDIER DEHAVILLAND RD 8-54-1565 ISSUE 3 DTD 18 FEB 04SDR A8ZR20181113002Structure · crackedACCOMPLISHED REPLACEMENT OF CRACKED CLOSING MEMBER PN 85410449 OF NR 1 NACELLE RT IB SIDE FIREWALL REF RD 8-54-611 ISSUE 4 DTD 12 APR, 2001.SDR A8ZR20181113001Firewall · crackedACCOMPLISHED DOUBLER INSTALLATION FOR CRACK ON UPPER FIREWALL WEB PN 85410554 OF NO 1 NACELLE RT IB SIDE REF RD 8-54-3940 ISSUE 1 DTD 24 MAY, 2017.SDR A8ZR20181106001Firewall · crackedACCOMPLISHED DOUBLER INSTALLATION FOR CRACK ON UPPER FIREWALL WEB PN 85410554 OF NR 2 NACELLE RT OB SIDE REF RD 8-54-3940 ISSUE 1 DTD 24 MAY, 2017.SDR A8ZR20181106002Structure · crackedACCOMPLISHED REPLACEMENT OF CRACKED CLOSING MEMBER PN 85410449 OF NR 2 NACELLE RT OB SIDE FIREWALL REF RD 8-54-611 ISSUE 4 DTD 12 APR, 2001.SDR ASOA2018092085221Firewall · crackedNR 1 PYLON FIREWALL WEB CRACKED IN SEVERAL PLACES AROUND HYDRAULIC FITTING. REPAIRED IAW EC/TC SNIEO MM670-37150 S03.SDR CVGA2018091805002Firewall · crackedINSPECTION REQUIREMENTS OF DOCUMENT 18, TASK 54-51-00-210 REVEALED RT ENGINE PYLON FIREWALL BOX ASSEMBLY IS CRACKED ON THE FORWARD PART OF THE BOX FROM THE OUTBOARD EDGE TO THE INBOARD RADIUS OF THE FIREWALL BOX APPROX .750" IN LENGTH, P/N 6312204-65. SERVICE SDR P5CA2018082700214Vapor Barrier · crackedRIGHT WING LE, INBD NR 3 NACELLE COVER, VAPOR BARRIER WAS FOUND CRACKED ON THE OTBD TAG. THE VAPOR BARRIER OTBD TAG WAS REPAIRED IAW RI-57-00-12982.SDR SRXR201808180020Bulkhead · crackedNR 1 PYLON CENTER STRUCTURE BULKHEAD, INBD SIDE WAS CRACKED AT YN 307. ACCOMPLISHED A REPAIR ON THE PYLON BULKHEAD IAW EA 011-5450-52-A7385, I/R.SDR COEA2018082213805Firewall · crackedRT ENGINE UPPER FIREWALL AFT OUTBOARD AREA WAS CRACKED. REPAIRED IAW ES-3628/18.13303.SDR UIEA2018061101100Bulkhead · damagedNR 1 PYLON BULKHEAD WEB DAMAGED INBD SIDE AT HYD BULKHEAD FITTING FDR PANEL 431 BT. FORMED NEW WEB IAW BDEW 313T3104 REV AP LEAK CHECK OF HYDRAULIC LINES IAW AMM 29-11-00-796 -053.SDR UIEA201806121111Bulkhead · crackedNR 1 PYLON BULKHEAD WEB DAMAGED INBD SIDE, AT THE HYD BULKHEAD FITTING FDR PANEL 431BT. FABRICATED A NEW WEB IAW BDEW 313T3104. REVAP LEAK CHECK OF HYDRAULIC LINES GOOD IAW AMM 29-11-00-796-053.SDR AALA201804099012Bulkhead · crackedNR 2 NACELLE OUTBOARD MID BULKHEAD IS CRACKED. REPAIRED THE BULKHEAD IAW EA 278458SDR HYIA20180403001Crossbeam · crackedA CRACK WAS DISCOVERED IN THE CROSSBEAM ON THE AFT LEFT SIDE, AROUND ONE OF THE TURBO BRACKET MOUNTING HOLES. THE CRACK MEASURED 1.304 INCHES IN LENGTH. THE TURBO BRACKET WAS INSTALLED TO CHECK FOR PRELOADING. NO PRELOADING WAS NOTED. BEAM WAS REPLACED.SDR A8ZR20180815001Firewall · crackedUPPER FIREWALL CRACKED, ON THE LT NACELLE STA 125.50.SDR IPXA2018030127010Bulkhead · crackedINSPECTION TYPE: 3C, NR 3 UPPER PYLON EWIS BULKHEAD WEB CRACKED FWD OF UPPER SPAR. ACCOMPLISHED A PERMANENT REPAIR IAW EA 011-5720-01-A7114, REV IR, AND EO MD11-5720-67613-A.SDR UIEA2017110902209Fireshield · tornNR 2 ENGINE LT CORE COWL INTERIOR SURFACE SEVERAL FIRESHEILD FOUND TORN. THE FIRESHIELD WAS REPAIRED IAW SRM 54-42-01-2R-6, REPAIR 6, REV 105.SDR DALA2017072505692Doubler · damagedNR 2 PYLON HYD SUPPLY HOSE FITTING LOOSE IN FIREWALL. REMOVED ORIGINAL REPAIR. FABRICATED REPAIR DOUBLER PER RI 560468-14. CLEANED UP HYD PRESSURE LINE HOLE IAW STEP 3 RI 560468-14, COMPLIED WITH HFEC SURFACE SCAN INSP PER MD88 NDT MANUAL MDC-93K0393 PARA 6.SDR 2017F00147Bulkhead · damagedBULKHEAD BOND ASSY. DAMAGED, DOUBLER CRACKED, NICKED AND DEBONDED.SDR DALA2017070505219Firewall · wornNR 2 ENGINE FIREWALL PASS THRU WORN AT PREVIOUS REPAIR LOCATED AT HYD PRESS LINE. SAME AREA HYD PRESS LINE LOOSE. FOUND DOUBLER AT PASS THRU FOR HYD LINES WORN. REMOVED OLD DOUBLER AND BAD HYD LINE. INSTALLED NEW DOUBLER IAW ERA 553921-14 REV ORIG. REINSTSDR DALA2017051503922Spar · corrodedNR 1 PYLON HEATSHIELD LOWER SPAR FOUND CORRODED. THE SPAR WAS REMOVED AND REPLACED IAW SRM 51-40-02, ER/A 558254-14 PRI, REV 0, ER/A 558254-14, PRI REV 0, AND COMPAIRED IAW ER/A 558254-14AD, REV 0. FOUND IN COMPLIANCE.SDR DALA2017051503918Spar · corrodedNR 1 PYLON HEATSHIELD LOWER SPAR FOUND CORRODED. THE SPAR WAS REMOVED AND REPLACED IAW SRM 51-40-02.SDR DALA2017051503915Spar · corrodedNR 2 PYLON HEATSHIELD LOWER SPAR FOUND CORRODED. THE SPAR WAS REMOVED AND REPLACED IAW SRM 51-40-02.SDR DALA2017051503914Spar · corrodedNR 2 PYLON HEATSHIELD LOWER SPAR FOUND CORRODED. THE SPAR WAS REMOVED AND REPLACED IAW SRM 51-40-02.SDR DALA2017051503913Spar · corrodedNR 1 PYLON HEATSHIELD LOWER SPAR FOUND CORRODED. THE SPAR WAS REMOVED AND REPLACED IAW SRM 51-40-02.SDR DALA2017051503921Spar · corrodedNR 1 PYLON HEATSHIELD LOWER SPAR FOUND CORRODED. THE SPAR WAS REMOVED AND REPLACED IAW SRM 51-40-02.SDR DALA2017051503920Spar · corrodedNR 1 PYLON HEATSHIELD LOWER SPAR FOUND CORRODED. THE SPAR WAS REMOVED AND REPLACED IAW SRM 51-40-02.SDR DALA2017051503919Spar · corrodedNR 2 ENGINE PYLON HEATSHIELD LOWER SPAR FOUND CORRODED. THE SPAR WAS REMOVED AND REPLACED IAW SRM 51-40-02.SDR DALA2017051503917Spar · corrodedNR 2 PYLON HEATSHIELD LOWER SPAR FOUND CORRODED. THE SPAR WAS REMOVED AND REPLACED IAW SRM 51-40-02.SDR DALA2017051503916Spar · corrodedNR 1 PYLON HEATSHIELD LOWER SPAR FOUND CORRODED. THE SPAR WAS REMOVED AND REPLACED IAW SRM 51-40-02.SDR QMLA2017041817040Firewall · crackedWHILE PERFORMING AN AIRWORTHINESS INSPECTION, MECHANIC DISCOVERED A CRACK ON THE LEFT AFT LOWER FIREWALL. THIS FIREWALL WAS REMOVED AND REPLACED. THE AIRCRAFT HAS SINCE BEEN RETURNED TO SERVICE.SDR UIEA2017040200490Fireshield · damagedRIGHT ENG, RT CORE COWL INTERIOR SURFACE FIRESHIELD FOUND WITH TWO HOLES. REPAIRED IAW SRM 54-42-01-2R-6, REPAIR 6, REV 103.SDR DALA2017040602792Fitting · wornNR 1 PYLON AFT BULKHEAD FITTING O/B LOWER SURFACE FOUND WORN. DAMAGE REMOVED, MATERIAL THICKNESS OUT OF LIMITS. AREA REPAIRED PER SRM.SDR FDEA201703150909Bulkhead · crackedNR 2 PYLON AFT BULKHEAD LOWER O/B SECTION AFT I/B HOLE HAS A CRACK INDICATION IN THE ALUMINUM BULKHEAD ONLY. COMPLIED WITH EA F-5450-T0331906 P1, DEVIATION TO EO F-5450-7-5006 DUE TO CRACK INDICATION IN BULKHEAD AT BRACE FITTING MOUNT HOLE ON NR 2.SDR CHIR201701122702Web · crackedINSPECTION REVEALED A CRACKED FORMER, PN 114S4104-13, AT STA 534, WL +72, BL 5 RIGHT. THIS AREA INCORPORATED A PREVIOUS REPAIR ONCE REMOVED, WEB WAS CRACKED AS WELL UNDER THE REPAIR DOUBLER. IN ADDITION IT WAS NOTED THAT THE T CAP 114S4104-13 WAS CRACKED. THE
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