JASC 5410
Service difficulty reports · 4,119
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 CA190603005Seal · damaged(CAN) DURING MAINTENANCE INSPECTING, #2 NACELLE HAD OBSERVE SIGN OF OVERHEAT. EXHAUST SEAL DAMAGE OBSERVED, BUT UNABLE TO DETERMINE IF THE HEAT DAMAGE IS DUE TO THE EXHAUST SEAL OR RELATED TO EARLIER EVENT. REPAIR DRAWING PROVIDED TO THE EXHAUST SEAL AND FOR SDR CALA2019042200632Nut Plate · missing#2 ENG INBD PYLON PANEL 446CL HAS 1 MISSING NUTPLATE. REPLACED NUTPLATE REF SRM 51-40-02SDR REXA2019042250490Retainer · crackedDURING SEAL REPLACEMENT ON PANEL 412AB, FOUND RETAINER TO BE CRACKED AND BROKEN. REMOVED OLD SEAL RETAINER/REPLACED WITH NEW SEAL ON PNL 412AB IAW 51-42-06.SDR P5CA2019041600056Spar · crackedNO.2 PYLON CAVITY REAR SPAR BOTTOM AREA WING FIXED LEADING EDGE VAPOR BARRIER CRACK AT I/B NACELLE AREA. (<P>NO.2 PYLON CAVITY REAR SPAR BOTTOM AREA WING FIXED LEADING EDGE VAPOR BARRIER CRACK AT I/B NACELLE AREA REPAIRED IAW SRM 57-41-01-2R-6 REPAIR 6, TEMPORSDR DALA2019041732485Fitting · crackedR/H ENGINE DRAG FITTING #9 BOLT HOLE HAS A CRACK INDICATION, VERIFIED BY HFEC. (PAGES 19 & 20, STEP 26 OF JOB CARD). REPAIRED RH ENGINE DRAG FITTING #9 BOLT HOLE PER DELTA ER/A 576632-14AD REV. ORIGINAL ASSOCIATED ER/A 14-576632 ADDED FOR AC 6702. (LP# 1027760SDR DALA2019041732484Fitting · crackedRT ENGINE DRAG FITTING #2 BOLT HOLE HAS A CRACK INDICATION, VERIFIED BY HFEC. (PAGES 19 & 20, STEP 26 OF JOB CARD). REPAIRED RH ENGINE DRAG FITTING #2 BOLT HOLE PER DELTA ER/A 576632-14AD REV ORIGINAL. ASSOCIATED ER/A 14-576632 ADDED FOR AC 6702. (LP 1027747)SDR REXA2019043040546Access Panel · chafedL/H NOSE ACCESS COWL 432AB HAS AFT TRAILING EDGE CHAFED. REMOVED AND REPLACED WITH NEW TRAILING EDGE AFT OF L/H NOSE ACCESS COWL 432AB IAW CMM 71-14-01.SDR IPXA2019040440760Structure · puncturedR. ENGINE COWL EXTERIOR HAS LG PUNCTURE HOLE WITH FIBERGLASS PROTRUDING FROM ENTRY HOLE. NOTICED ON PREFLIGHT WALK AROUND DAMAGE IS PROB. 4-6 INCHES LONG. 3 INCHES IN DIAMETER. ACCOMPLISHED INTERIM INSPECTION & REPAIR IAW EO. B767-7110-72129-A. DEFERRED PER SDR EE4Y2019040108585Inlet · crackedNR 1 ENGINE INLET COWL LIP SKIN AT 4 AND 12 O’CLOCK POSITION WITH TOOL MARKS AROUND FASTENERS HEAD.FOR CORRECTIVE ACTION SEE COOPESA NRI 4-86,ACTION TAKEN,PERFORMED PERMANENT REPAIR IAW COO-EO-2019-8117 R01 AND COLLINS AEROSPACE MESSAGE # CV19-01268 REV D.SDR CA190319019Structure · misrepaired(CAN) NUMBER OF FASTENERS AND COLLARS ON THE PYLON ASSEMBLY WERE FOUND NOT CORRESPOND TO THE DRAWING. THESE WRONG FASTENERS AND COLLARS ARE INSTALLED ON PYLON ASSEMBLY RH & LH AT FS 929 (A), 945 (B), 982 (C), 999 (D), 1017 (E), 1046 (F) AND 1072 (G), WHICH AFFSDR DALA2019031101740Beam · crackedNR 2 PYLON OUTBD HYD BAY LOWER BEAM IS CRACKED @ FORWARD END C/W EAR 524549-14. (LP 0975491)SDR IPXA2019060742936Retainer · corrodedNUMBER 1 PYLON SPIGOT RETAINER IS CORRODED. REMOVED AND REPLACED FLANGE IAW A300-600 AMM 54-51-78-0401SDR CA190226002Clamp · deteriorated(CAN) DIVERTED TO DUE TO #2 HYD FLUID LOSE. #2 HYD ISO VALVE AND #2 EDP CAUTION LIGHT ON. EMERGENCY LANDING. ALTERNATE GEAR EXTENSION. MAINTENANCE FOUND LEAK IN NACELLE CAUSED BY ADEL CLAMP CUSHION MISSING/DETERIORATED BETWEEN EDP PRESSURE LINE AND CASE DRAIN SDR IPXA2019022549347Fairing · crackedINSPECTION TYPE:5YR#2 PYLON AFT LOWER FAIRING AFT LH SIDE OF SKIN IS CRACKED AT FASTENER HOLEACCOMPLISHED REPAIR ON #2 PYLON AFT LOWER FAIRING SKIN LH SIDE PER VT SAA EA#300-5450-01-A7613 I/R AND UPS EO A300-5430-71693-ASDR DALA2019022761271Doubler · detachedON ARRIVAL FOUND NR 1 ENGINE PYLON THUMBNAIL FAIRING DETACHED. CORR BY FANTA 00608873 SEA 19FEB19 ATA 5433. INSTALLED THUMBNAIL PANEL PER A319 AMM 54-22 AND COMPLETED PHASE 1 INSPECTION PER A319 AMM 05-51. NO DAMAGE NOTED.SDR IPXA2019022039244Inlet · crackedINSPECTION TYPE:1C#2 ENGINE NOSE COWL OB TEMP SENSOR AREA IS CRACKEDREMOVED AND REPLACED WEB PER P&W SRM 54-10-00 REPAIR 14.SDR UIEA2019021103181Rod · damaged#2 ENGINE I/B COWL HOLD OOPEN ROD DAMAGED.(<P>REMOVED AND REPLACED #2 ENGINE I/B CORE COWL HOLD OPEN ROD IAW B767 AMM 20-11-00,ASSET #0019776.</P>)SDR IPXA2019022539409Rib · gougedINSPECTION TYPE:3C#1 ENG. PYLON ACCESS PANEL 439AL HAS GOUGED RIB.REMOVED AND REPLACED #1 PYLON ACCESS PANEL #439AL RIB IAW SRM 54-01-42. (MINOR)SDR ASOA2019020865037Riser · corrodedREF BOMBARDIER TUCSON AIR CENTER JOB 2744561 L/H PRODUCTION RISER HAS EVIDENCE OF FRETTING CORROSION. REPAIRED IN ACCORDANCE BOMBARDIER REO 601R-54-50-036 REV-C DATED 2004-10-05.SDR ASOA2019020765036Riser · corrodedR/H PRODUCTION RISER HAS EVIDENCE OF FRETTING CORROSION. REPAIRED IN ACCORDANCE BOMBARDIER REO 601R-54-50-036 REV-C DATED 2004-10-05.SDR UIEA2019020503118Acoustic Liner · corrodedBULGE ON ACOUSTIC PANEL AFT EDGE OF NO.1 ENG INLET COWL NEAR 7 O'CLOCK POSITION.(<P>1.REPAIR DAMAGE AREA I.A.W. EI NO=T2019A71M-365 REV.1 2.JOB COMPLETED AND COND. CHK NML.</P>)SDR DALA2019020540754Seal · missingLEFT UPPER FWD PYLON APRON SEAL ON LT ENGINE COWLING IS MISSING. REMOVED PANEL & SEPARATED APRON SEAL PER AMM 71-14 -01. INSTALLED NEW APRON SEAL FWD POS, LT ENG. IAW MD 90 AMM 71-14 OK FOR SVC. (LP# 5318774)SDR IPXA2019022039259Precooler · crackedINSPECTION TYPE:5Y#1 PYLON AFT L/H SIDE OF PRECOOLER BOX STRIP SKIN UPPER EDGE IS CRACKED AT RIB 8A.REPAIRED #1 PYLON L/H STRIP SKIN CRACK AT RIB 8A IAW UPS EO A300-54-50-51643-A. (MINOR)SDR HYIA20190117001Beam · crackedDURING MAINTENANCE A CRACK WAS DISCOVERED ON THE RIGHT NACELLE INBOARD CROSSOVER BEAM SUPPORT CHANNEL P/N: 5654102-15. AFTER REMOVING THIS CHANNEL IT WAS DISCOVERED THAT THE RIGHT HAND INBOARD BEAM, P/N: 5654109-7 WAS CRACKED UNDERNEATH THE SUPPORT CHANNEL. THSDR HYIA201812180001Fitting · crackedTHE RT NACELLE IB FITTING WAS FOUND TO BE CRACKED AT THE LWR PORTION OF THE OB LEG WHILE PERFORMING BORESCOPE INSPECTION (TEXTRON MEL54-02R2) TO SATIDFY THE REQUIREMENT OF AD2017-10-09. THE FITTING DOES NOT APPEAR CORRODED OR OTHERWISE DAMAGED AND THERE DO NOSDR DXTR2018121901Fairing · brokenRIGHT ENGINE LOWER FAIRING LEADING EDGE IS MISSING. MISSING PIECE HAD DEPARTED AIRCRAFT AND COULD NOT BE FOUND. DISASSEMBLED R/H ENGINE TO EXTENT NECESSARY TO GAIN ACCESS TO THE BYPASS DUCT LOWER FAIRINGS TO REMOVE REMAINING PIECE OF FAIRING AND ADJOINING CRACSDR REXA201812281335Guide · chafedL/H LWR TRANS COWL HAS 4EA. CHAFED GUIDES.
REMOVED GUIDE RETAINER CHAFED 3 EA FOUND TO BE IN LIMITS
IAW CRJ 900 SRM 54-21-00. REMOVED AND REPLACED 1 EA GUIDE RETAINER
TRANS COWL IAW CRJ 900 SRM 51-42-21.
SDR REXA2018122871355Pad · chafedL/H LWR TRANS COWL HAS 2EA. CHAFED WEAR PADS FOR ACCESS DOOR.
REMOVED AND REPLACED WEAR PADS IAW CRJ 900 SRM 51-42-06SDR DALA2018121407211Bushing · corroded(AIRCRAFT 6703, L/P 0863620) RII: CORROSION ON RH PYLON UPPER LINK BUSHING AMDS 2021-2718-2 (MOT2). REPLACED PER B757-200 AMM 54-51-01.SDR AALA2018121329020Acoustic Panel · delaminatedTHE AFT ACOUSTICAL PANEL ON THE NR 2 ENGINE AT THE 8:30 O`CLOCK POSITION WAS DELAMINATED. THE AIRCRAFT WAS GROUNDED. REPLACED THE ACOUSTICAL PANEL IAW AMM 72-23-02.SDR AALA201812129029Acoustic Panel · delaminatedNR 2 ENGINE AFT ACOUSTICAL PANEL DELAMINATED. THE AIRCRAFT WAS GROUNDED. THE ACOUSTICAL PANEL WAS REPLACED IAW AMM 72-23-02.SDR DALA2018120507068Strut · chafed(AIRCRAFT 6703, L/P 0852106) RII: CORROSION ON RH PYLON NACELLE STRUT BUSHING AMDS 2021-2718-2 (MOT2). SUMMARY: IN ACCORDANCE OF NRC # 368 RH PYLON STRUT WAS REPAIRED PER B757-200 SRM 54-51-90 REPAIR 3 PAG.201 AND NEW BUSHINGS WERE REPLACED ON RH PYLON STRUT PSDR DALA2018120657067Bushing · worn(AIRCRAFT 6703, L/P 0852103) AWR. DUE TO THE REMOVAL OF LH ENGINE PYLON STRUT. WORN BUSHINGS INBD/OUTBD ON UPPER LUGS NAC STA: 162 AT LH ENGINE PYLON STRUT. (IN REF. CARD 2021-2718-1). SUMMARY: IN ACCORDANCE OF NRC # 546 LH PYLON STRUT WAS REPAIRED PER B757-20SDR DALA2018120647061Spar · crackedCRACKED ON LH PYLON AFT FIXED FAIRING - UPPER SPAR WEB IB AND OB SIDES BETWEEN RIB 14 AND 15, REPAIRED #1 PYLON AFT FIXED FAIRING PER AA5450-01052-10ASDR DALA2018120647060Rib · crackedCRACK #2 ENG PYLON AFT FIXED FAIRING UPPER CLOSURE RIB, REPAIRED #2 RH PYLON AFT FIXED FAIRING PER AA5450-01052-10BSDR FDEA201811303398Door · departedON ARRIVAL FOUND PANEL BROKEN OFF AND GONE FROM THE INSIDE OF THE LEFT ENGINE PYLON. ONLY SMALL PIECES OF DOOR REMAIN. ITEM PREVIOUSLY ON O.I.L. INSTALLED NEW STRUT PRESSURE RELIEF AND ACCESS DOOR SDR DALA2018112976895Structure · erodedCRACKING THROUGHOUT #1 ENGINE OUTBOARD FAN COWLING LEADING EDGE ERODED. REPLACED SAME SYSTEM OPERATION IS NORMAL.SDR DALA20181126802Bushing · damagedSHIP 5650 #1 PYLON UPPER BRACE ATTACH POINT, BOTH BUSHINGS DAMAGED. CORRECTIVE ACTION: REMOVED AND REPLACED BUSHINGS ON #1 PYLON UPPER BRACE ATTATCH POINT. I.A.W. B757-SRM. (0835092)SDR DALA2018112186740Fairing · cracked#1 PYLON AFT. FIXED FAIRING CRACKED AT #15 RIB, SEE NR FOR ADDITIONAL INFORMATION 069-0001:5450-01052-01A/001 00043 REPAIR OF AFT FIXED FAIRING WAS ACCOMPLISHED PER AA5450-01052-06ASDR REXA2018112831136Landing · crackedRH ENGINE LOWER T/R COWL PANEL 443AB LATCH DOOR LANDING IS CRACKED. REMOVED DAMAGED COAMING AND DOUBLER AND INSTALLED NEW COAMING AND DOUBLER IAW CRJ 900 SRM 51-42-13 AND 51-42-06. AAR SM-39SDR T17A201811134054Inlet · crackedRH ENGINE INLET FOUND CRACKED AT THE 6 O'CLOCK POSITION. INSPECTED CRACK IN R/H ENGINE INLET FINDING IT TO BE WITHIN LIMITS IAW SERVICE ALERT SA-2015-18 REV. A CRACK DUE REINSPECT IN 10 FLIGHT CYCLES.SDR DALA2018110606454Rib · cracked#2 ENG NOSE COWL HAS A CRACKED SUPPORT RIB @ 6 O'CLOCK POS. R & R NBR 2 ENG NOSE COWL, REF CARD 7100-4680. (LP0814998)SDR DALA2018110206415Hinge Fitting · gougedNR 2 ENGINE, OTBD CORE COWL, CENTER HINGE FITTING WAS GOUGED ON THE FORWARD SIDE. FOUND TO BE OUT OF LIMITS IAW SRM 54-53-90, COMPLIED WITH ER/A 572646-14.SDR DALA2018102806460Frame · crackedLT PYLON AFT FAIRING O/B AREA FRAME AFT OF PANEL 434BL FOUND CRACKED AS MARKED. LT PYLON AFT FAIRING O/B AREA NR 5 FRAME CARRIED OUT REPAIR AS PER PRI ER/A 572027-14 REV 0 AND REV 1. AWAITING FOR FINAL ER/A. COMPARED WITH PRI ER/A 572027-14 REV 0 AND REV 1, FISDR SWIA2018120745334Panel · chafedLH ENGINE PANEL 433AL HAS CHAFING ON THE TOPHAT. (C-CHECK) RO: 12/06/2018 REMOVED AND REPLACED P/N CN624-2025-201 IAW SRM.SDR 2018FA0000486Keelbeam · crackedINSPECTION DETECTED CRACKS IN THE LEFT AND RIGHT NACELLES AT N.S 136-137 IN THE KEELSON WEBS ADJACENT TO THE BATTERY BOX AREA. NUMEROUS MILITARY SA227-DC HAVE BEEN IDENTIFIED WITH CRACKING. EO NUMBER SA227-0147 IS ESTABLISH TO PROVIDED THE MAJOR REPAIR PROCEDUSDR IPXA2018102435322Heat Shield · crackedNR 3 PYLON HEAT SHIELD WAS CRACKED AT YWN 332. REPAIRED THE HEAT SHIELD IAW EA 011-5400-01-A7512, REV I/R, AND EO MD11-5420-70325-A. MINOR.SDR DALA2018101506054Frame · cracked(AIRCRAFT 684, L/P 0781588) INITIAL INSPECTION: CRACKED OUTBD FRAME ON STA NAC 136 AT RT PYLON UPPER SURFACE. SUMMARY: IN REFERENCE NRC 00466 FRAME WAS REPLACED PER. SRM 51-40-02 PAR 7 AND DWG. 313N3100 REV. AY.SDR FDEA201810042788Beam · damagedDURING L/H ENGINE CHANGE, FOUND DAMAGE TO OUTBOARD LATCHBEAM AT FORWARD NUTPLATE. REPAIRED OTBD BEAM REF EA #: H-5450-T0342766 PT 1SDR FDEA2018100542788Beam · damagedMDIS 120 54-50 3684 04OCT18 MEM OPEN U DURING LT ENGINE CHANGE, FOUND DAMAGE TO OUTBOARD LATCH BEAM AT FORWARD NUTPLATE. PART 04OCT18 10:01 MEM U IDENTIFIED PARTS MPN: BACN11P3B16C QTY: 10 MPN: BACN11P3B14C QTY: 10 PART 04OCT18 10:01 MEM U ORDER PART MPN: BACN
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