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 FDEA201008022784Support · crackedNR1 PYLON LT FWD L/E NACELLE FAIRING STRUCTURE IS CRACKED AT A FASTENER. R & R CRACKED A5461221600040 SUPPORT WITH A NEW A5461221600040 SUPPORT, PO 688444.2 IAW SRM 51-40-21, PG 7.SDR FDEA201007292719Beam · chafedFOUND A CHAFED AREA ON THE EDGE OF LIGHTING HOLE ON CANTILEVER BEAM ON NR 1 PYLON, 5" LT OF CTR LINE AT RIB J4. REPAIRED NR1 PYLON CANTILEVER BEAM AT RIB J4 BY REMOVING SHARP EDGES AND ADDING A DOUBLER IAW EA 6-5450-135245. ALL WORK WAS DOCUMENTED ON N00729 SDR MALA100101Beam · chafedOTBD FACE OF INBD UPPER BEAM ON LT NACELLE HAS HOLE CHAFED THRU FROM BLEED TUBE LOCATED 2.5" FROM AFT EDGE, MEASURING 0.522 X 0.140 INCH. WEB MATERIAL IS 0.020 INCH 6AL4V TITANIUM SHEET. COMPLETED REPAIR OF OTBD FACE OF INBD UPPER BEAM ON LT NACELLE IAW EOS542SDR IPXA10561442Bracket · crackedINSPECTION TYPE:C2, NR 1 ENGINE PYLON ACCESS PANEL 835AL FWD HINGE POINT, AFT HINGE BRACKET IS CRACKED. REPLACED BRACKET.SDR FDEA201007192590Structure · corrodedNR 1 PYLON SPIGOT FITTING BORE HAS CORROSION. CLEANED NR 1 PYLON SPIGOT FITTING BORE IAW SB A310-54-2019, REV 3. MEASURED HOLE WITH MIC T8723B AND FOUND TO BE LESS THAN 4.728 IAW S/B A310-54-2019, REV 3. CAD PLATED BORE IAW SRM 51-21-10.SDR FDEA201007192588Fitting · corrodedNR 2 PYLON INTERNAL, SPIGOT BEARING IS COVERED WITH A BROWN LAYER AND THE CUTOUT CIRCUMFERENCE IS PACKED WITH RUST DUST. ACCESS 483 AL. CLEANED NR 2 PYLON SPIGOT FITTING BORE IAW SB A310-54-2019, REV 3. MEASURED HOLE WITH MIC T8723B AND FOUND TO BE LESS THSDR IPXA10561156Bracket · crackedINSPECTION TYPE:C4, NR1 ENG PYLON SUPPORT CLIP CRACKED AT FASTENER LOCATION AT NAC STA 205 UNDER FWD SIDE OF PANEL 435AR (MARKED, REPLACED CLIP IAW SRM 51-40-02-0G, SRM 51-40-05-0G, SRM 51-10-02-OG, STEP 8C.SDR QXEA2010071500413Cowling · chafedC CHECK - RT ENGINE UPPER FAN COWL CHAFE UNDER T/R TRANSMISSION FLEX LINE. BLENDED CHAFED AREAS ON FAN COWL SKIN AND REINFORCING ANGLE. SENT TO MFG FOR ENGINEERING. PERFORMED ECI ON RT ENGINE UPPER FAN COWL REINFORCING ANGLE WHERE AREA WAS BLENDED. NO CRACKSDR USAA2010081691685Fuse Pin · corrodedMAJOR REPAIR, NR 1 PYLON OUTBOARD MID SPAR FUSE PIN FLANGE HAS CORROSION AT NAC STA 283. REPLACED NR 1 PYLON OUTBOARD MID SPAR FUSE PIN IAW B737 AMM 54-10-00.SDR USAA2010081691684Fuse Pin · corrodedMAJOR REPAIR, RIGHT PYLON INBOARD MID SPAR FUSE PIN HAS CORROSION AT NAC 283. REPLACED RIGHT PYLON INBOARD MID SPAR FUSE PIN IAW B737 AMM 54-10-00.SDR USAA2010081691683Pin · corrodedRIGHT PYLON OUTBOARD MID SPAR FUSE PIN HAS CORROSION. REPLACED RIGHT PYLON OUTBOARD MID SPAR FUSE PIN IAW B737 AMM 54-10-00. NOTE: A SUPPLEMENT WILL BE SUBMITTED UPON RECEIVAL OF THE MAJOR REPAIR REPORTING FORM.SDR USAA2010081691682Fuse Pin · corrodedLEFT PYLON INBOARD MID SPAR FUSE PIN HAS CORROSION. REPLACED LEFT PYLON INBOARD MID SPAR FUSE PIN IAW AMM 54-10-00.SDR USAA2010081691681Pin · corrodedNR 1 PYLON INBOARD MID SPAR ATTACH FUSE PIN HAS CRACKED SEALANT & RUSTY. REPLACED NR 1 PYLON INBOARD MID SPAR ATTACH FUSE PIN IAW AMM 54-10-00.SDR V0XR201007120001Angle · cracked(V0XR)RT EXHAUST FINGERNAIL HAS DAMAGE TO FWD INBD BOTTOM CORNER OF FRAME ANGLE. R & R RT EXHAUST FINGERNAIL CORNER FRAME ANGLESDR UIEA2010070700095Strut · gougedDURING THE LCF MODIFICATION IN TPE AND INSP IAW SB 747-54A2218 (AD 2005-19-09), A GOUGE WAS FOUND IN THE NR 4 STRUT LT SIDE & NBSP; LINK & NBSP; DO NOT SCHEDULE; THIS EO DOCUMENTS AN INTERIM REPAIR ACCOMPLISHED AT TPE DURING THE SEPTEMBER 2008 LCF MODIFICATIONSDR V0XR20100701003Intercostal · damaged(V0XR) CHANNEL BEHIND SKIN ON LOWER FWD INBD CORNER OF NR1 NACELLE HAS BLOWN OUT HOLES. (APPROX .25) R & R DAMAGED INTERCOSTAL. W/C 4077SDR WGFY2010FA0000494Stiffener · crackedPYLON NR1 STIFFENER NR3 BETWEEN NAC STA 234-259 WAS CRACK +/- 25MM. PERFORMED A DETAIL VISUAL REPEAT INSPECTION OF SUBJECT REPAIR AREA AT THE INSPECTION INTERVAL SPECIFICATION IN THE SB 747-54-2223 TO ENSURE ABSENCE OF ANY ADDITIONAL HEAT DAMAGE, LOOSE FASTSDR ASOA201000946Angle · chafed2 EACH ANGLES CHAFED THROUGH AND CRACKED ON RT ENGINE UPPER FIREWALL DOOR 422BT. R & R (2 EA) ANGLES ON RT ENGINE UPPER FIREWALL DOOR PANEL 422BT AND INSTALLED NEW NO STEP DECAL ON PANEL 422BT ALSO IAW SRM 51-42-06 AND AMM 11-20-04.SDR UALA2010062402237Sleeve · crackedNR1 PYLON FWD ATTACHMENT INBD UPR SLEEVE CRACKED. INSTALLED NEW NR1 PYLON FWD INBD UPR SLEEVE.SDR UALA2010062402236Bearing · corrodedNR 1 PYLON SPIGOT BEARING CORRODED. INSTALLED NEW NR1 PYLON SPIGOT BEARING.SDR R61A20100271Heat Shield · corrodedWHILE AC WAS IN FOR HEAVY CHECK, LEVEL TWO CORROSION WAS FOUND ON LT ENGINE NUMBER FOUR HEAT SHIELD AND INTERNAL STIFFENERS ON BOTTOM. MAINTENANCE REMOVED AND REPLACED THE HEAT SHIELD (P/N 170-39554-001) AND INTERNAL STIFFENERS (P/N 170-34584-001) PER THE EMBSDR UALA2010062302223Sleeve · crackedRIGHT PYLON OUTBOARD UPPER SLEEVE CRACKED. REMOVED CRACK SLEEVE. INSTALLED NEW NR 2 PYLON FWD OUTBOARD UPPER SLEEVE.SDR UALA2010062302222Bearing · corrodedNR2 PYLON SPIGOT BALL JOINT SPHERICAL BEARING HAS PITTING CORROSION. INSTALLED NEW NR 2 PYLON SPIGOT BALL JOINT BEARING.SDR UALA2010062302219Sleeve · crackedNR 1 PYLON AFT ATTACHMENT OTBD FITTING SLEEVE CRACKED. REMOVED CRACKED SLEEVE. INSTALLED NEW NR 1 ENG PYLON AFT SHACKLE OTBD PIN ASSY.SDR UALA2010062302217Sleeve · crackedNR 2 PYLON FWD MOUNT LWR INBD SHACKLE SLEEVE HAS A CRACK AROUND SHANK HEAD AREA. INSTALLED NEW FWD LWR INBD SLEEVE.SDR UALA2010062302215Sleeve · crackedNR 2 PYLON FWD MOUNT UPPER INBD SHACKLE SLEEVE HAS A CRACK AROUND THE SHANK HEAD AREA. INSTALLED NEW SHACKLE SLEEVE.SDR DALA1405979218Fastener · damagedPYLON AFT FITTING UPPER FASTENERS DAMAGED. REPLACED IAW AA 5440-01069.SDR FDEA201006212094Latch · wornNR 2 ENGINE PYLON ACCESS PANEL, 457 CL ON LT SIDE HAS WORN LATCHES. LATCH LANDS FOUND TO BE OUT OF LIMITS IAW SRM 54-00-01, VOL I. FABRICATED NEW DOUBLER AND INSTALLED IAW DAC DWG AVB7332 AND SRM 51-33-01, VOL II.SDR P5CA2010062101643Door · damagedNR 4 LEFT PYLON FAIRING DOOR WAS DAMAGED DURING MAINTENANCE BY A WORK STAND. ACCOMPLISHED TIME LIMITED REPAIR PER ENGINEERING ORDER 4454A098, WITH FAA 8110-3 DATED 15 JUNE 2010. DVI EVERY 25 FLIGHT CYCLES WITH PERMANENT REPAIR PRIOR TO 2000 FLIGHT HOURS.SDR P5CA2010062101642Structure · damagedNR 4 ENGINE & NBSP; RIGHT CORE COWL DAMAGED DURING MAINTENANCE BY STAND. ACCOMPLISHED TIME LIMITED REPAIR PER ENGINEERING ORDER 4471A058, WITH FAA 8110-3 DATED 15 JUN 2010. DVI EVERY 2 FLIGHT CYCLES WITH PERMANENT REPAIR PRIOR TO 25 FLIGHT CYCLES.SDR QXEA2010062100358Structure · crackedFRONT OTBD CLIP ON RT NACELLE SPINE COWL IS CRACKED UNDER WASHER. REMOVED AND REPLACED DAMAGED CLIP REF RD 8/4-71-032.SDR USAA2010062491260Ball Joint · corrodedSAL - S4 - MAJOR REPAIR - CORROSION ON BALL JOINT OF SPIGOT LEFT PYLON. REPLACED THE BALL JOINT OF SPIGOT LEFT PYLON IAW A319 AMM 54-51-41.SDR A6WA201040432Strip · chafedLT ENGINE LOWER NOSE COWL AFT EDGE STRIP IS CHAFED. R & R UNSERVICEABLE LT ENGINE LOWER NOSE COWL AFT EDGE STRIP AND INSTALLED SERVICEABLE AFT EDGE STRIP IAW CMM 71-14-10.SDR UALA2010061502104Nacelle · damagedGROUND OPS REPORTING DAMAGE TO CNA FOR THE NR 1 ENG STRUCK BY TUG AND OR CART. DETERMINE DIMENSIONS, LENGTH- WIDTH - AND AMOUNT OF DEFLECTION. CNA DAMAGED BEYOND ANY LIMITS. REPLACED CNA.SDR A6WA201040418Structure · chafedRT UPPER NOSE COWL AFT EDGE STRIP IS CHAFED. REPAIR CHAFED DAMAGE ON RT UPPER NOSE COWL AFT AND EDGES STRIP IAW CMM 71-14-01.SDR FDEA201006091916Bearing Race · corrodedLT PYLON SPIGOT RECEPTACLE FITTING HAS CORROSION AROUND ENTIRE CIRCUMFERANCE OF BEARING RACE AND INSIDE RACE ACCOMPLISHED S/B IAW EA 6-5450-135184 NACELLES/PYLONS NR 1 PYLON SPIGOT FITTING.SDR P5CA2010060801640Structure · damagedNUMBER 4 ENGINE LT & RT CORE COWLS DAMAGED AT FORWARD EDGE AT 6 O'CLOCK POSITION. TIME LIMITED REPAIR PART ONE ACCOMPLISHED PER ENGINEERING ORDER 4471A057, WITH FAA 8110-3 DATED 08 JUN 2010. DVI EVERY 15 FLIGHT CYCLES AND PERMANENT REPAIR PRIOR TO 50 FLIGHT CSDR QXEA2010060100330Diaphragm · crackedLT NACELLE UPPER OTBD WING TO NACELLE SUPPORT DIAPHRAGM IS CRACKED. REPLACED DIAPHRAGM IAW SRM 51-42-05SDR A6WA201040492Strip · chafedRT ENGINE UPPER NOSE COWL AFT EDGE STRIP IS CHAFED. R & R WITH SERVICEABLE AFT EDGE STRIP PN 228-50080-108 IAW CMM 71-14-01.SDR CA100604001Cowl Door · damagedAIRCRAFT FLEW AND ARRIVED 14:18 Z DURATION 1:17. CREW REPORTED ON JLS 525995 DEFECT DESCRIPTION RT FRONT COWL SEPARATED FROM NACELLE UPON LANDING 21-MAY-2010 LINE MAINTENANCE WAS DISPATCHED FOR REPLACEMENT OF DAMAGED COWL. NEW COWL WOULDN’T FIT CORRECTLY ANDSDR A6WA201040496Retainer · crackedPANEL 412DB HAS CRACKED SEAL RETAINER. REMOVED DAMAGED SEAL RETAINER AND INSTALLED NEW SERVICEABLE SEAL RETAINER AND SEAL IAW AMM 54-63-01.SDR QXEA2010051700302Bearing · migratedMOD - BEARING ON NR 1 NACELLE FOR TOP ALTERNATE EXTENSION ACTUATOR ROD END HAS MIGRATED OUT. REPAIRED THE ALTERNATE EXTENSION ACTUATOR ATTACHMENT HOLE ON LT NACELLE TO WING SPAR ATTACHMENT FITTING IAW -8 400 RD 8/4-54-667 STEPS 1 THRU 3. PERFORMED HFEC OF RESDR FDEA201005151544Structure · crackedNR 1 PYLON LT FWD SIDE SKIRT HAS 0.125" CRACK AFT EDGE UPPER CORNER OF LT FAN COWL. STOP DRILLED CRACK IAW SRM 54-56-10 FIG 201, NDT VERIFIED NO CRACK INDICATIONS IAW NTM 51-60-00 BEYOND STOP DRILL. FABRICATED, LOCATED, AND DRILLED DOUBLER IAW SRM 54-56-SDR FDEA201005151542Structure · crackedNR 1 PYLON LOWER AFT AREA SECTION MEMBER HAS 1.5 IN LONG CRACK. R & R MEMBER ON NR 1 PYLON LOWER AFT AREA AT RIB 19 IAW SRM 51-72-10, PARAGRAPH 3A.SDR A6WA201040361Strip · chafedRT ENGINE UPPER NOSE COWL AFT EDGE STRIP IS CHAFED, SHORTS IPS 71-14-01, FIG 1, ITEM 45. R & R WITH SERVICEABLE AFT EDGE STRIP PN 228-50080-108 AT RT ENGINE UPPER NOSE COWL ALL WORK DONE IAW CMM 71-14-01, SRM 51-21-11, 51-25-06, 51-25-16.SDR A6WA201040359Strip · chafedRT ENGINE LOWER NOSE COWL AFT EDGE STRAP IS CHAFED, SHORTS IPC 71-14-01, FIG 2, ITEM 105. R & R WITH SERVICEABLE AFT EDGE STRIP PN 228-50081-108 AT RT ENGINE LOWER NOSE COWL WORN DOWN IAW SRM 51-21-11, 51-25-06, 57-25-18.SDR A6WA201040360Splice · chafedUPPER NOSE COWL AFT EDGE STRIP IS CHAFED, SHORTS IPC 71-14-01, FIG 1, ITEM 40. R & R WITH SERVICEABLE AFT EDGE STRIP PN 228-50080-107 ALL WORN DOWN IAW CMM 71-14-01 AND SRM 51-21-11, 51-25-06, 51-25-16.SDR A6WA201040396Fairing · crackedLT UPPER STANG FAIRING CRCKED PN 228-50253-805 LT ENG R & R LT UPPER STANG FAIRING IAW SRM 51-41-02.SDR IPXA10659961Support · crackedINSPECTION TYPE:8C, NR 1 PYLON MID SPAR WEB RT SUPPORT CLIP FOUND CRACKED JUST AT NAC STA 285.45 CRACK LENGTH 1" NR 1 PYLON MID SPAR WEB RT SUPPORT CLIP REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02, REV 46.SDR ASOA201000665Fairing · brokenNR 1 ENGINE TOP STANG FAIRING BROKEN. RECEIVED NEW NR1 ENGINE TOP STANG FAIRING PN 228-50253-805, TAG AB0166 TO BE INSTALLED ON W/O 1005869 CN 9000-0001.
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