JASC 5420
Service difficulty reports · 3,949
Reports filed under 5420 · Nacelle/Pylon Miscellaneous Structure, 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 = '5420' 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 = '5420' 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 IPXA11567310Channel · gougedINSPECTION TYPE:C1, RT AFT FAIRING STRUCTURE LOWER AFT PAN ASSY FROM PPS 278-301.6 IS GOUGED AND DAMAGED. R & R CHANNEL IAW SRM 51-40-02.SDR IPXA11567279Pan · gougedLEFT AFT FAIRING STRUCTURE LOWER PAN ASSY. FROM PPS 278-301.6 IS GOUGED AND DAMAGED. REPLACED IAW SRM 51-40-02-0G.SDR IPXA11567278Attach Bracket · wornLT AFT FAIRING STRUCTURE AFT UPPER DRAIN TUBE IS LOOSE, ATTACHING BRACKET WORN. R & R BRACKET IAW SRM 51-40-02-0G; SRM 51-40-05-0G.SDR IPXA11567281Support Angle · crackedINSPECTION TYPE: MOD, LT AFT FAIRING STRUCTURE LOWER AFT INBD SUPPORT ANGLE IS CRACKED AT PPS 291. REPLACED ANGLE IAW SRM 51-40-02-0G.SDR IPXA11567280Angle · crackedLEFT AFT FAIRING STRUCTURE LOWER AFT OTBD SUPPORT ANGLE IS CRACKED AT PPS 291. REPLACED IAW SRM 51-40-02-0G.SDR IPXA11567249Seal · bentRT PYLON FWD CHANNEL ON OTBD SIDE IS BENT PN 311N5175-2. R & R SEAL LAND IAW SRM 51-40-02.SDR K11A2011080491502Web · crackedNR 2 PYLON AFT PYLON WEB CRACK, 2 INCH CRACK.SDR EE4Y20110326Fitting · crackedENGINE NR 1, PYLON AFT FIXED FAIRING, PYLON STA 837 FWD LOWER SECTION INTERNAL FITTING CRACKED. NOTE: THE FITTING CRACK REQUIRES A MAJOR REPAIR IAW SRM GUIDELINES.SDR IPXA11567230Fairing · chafedINSPECTION TYPE:MOD, RT AFT FAIRING STRUCTURE, FWD RT UPR NUTPLATE MACHINED DOUBLER IS WORN, CHAFED AND DAMAGED ON BOTH SIDES. R & R IAW SRM 54-50-71-1A1; SRM 51-40-02; SRM 51-40-05; SRM 51-21-11-7.SDR IPXA1567012Support Bracket · crackedINSPECTION TYPE: MOD LT AFT FAIRING STRUCTURE. RT UPPER AFT WIRE SUPPORT BRACKET IS CRACKED. REMOVED, FABRICATED AND INSTALLED NEW RT UPPER AFT WIRE SUPPORT BRACKET IAW SRM 54-50-71-1A1, SRM 51-10-02-0G, SRM 51-40-05-0G, SRM 51-20-01-0G.SDR DHLA201100528Angle · crackedNR 2 ENG TO PYLON ANGLE CRACK 10" STA YN 183.000 AT 12 O'CLOCK POS, LT SIDE. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3, DATE 07-02-11, EVA D854-00407, REV IR DATED 06-14-11, DWG ASTAR ES D85400407-001-D. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-20D, SRM 5SDR IPXA1567645Cover · gougedINSPECTION TYPE:MOD, LT DIAGONAL BRACE COVER ASSY IS GOUGED AND WORN IN 2 AREAS ON THE BOTTOM SIDE. PN 313N5047-1, REPAIRED IAW ER 11-02979, DATED 07-02-2011.SDR UALA2011053102663Tube · damagedNR 2 ENG PYLON INBD DRAIN TUBE BROKEN OFF. REPLACED BROKEN DRAIN TUBE WITH A TIME LIMITED REPAIR TUBE PER MT 54-UA3. A CF ITEM WAS CREATED FOR A PERMANENT REPAIR.SDR ABXR2011052800025Gusset · chafedNR 2 PYLON UPPER SKIN LT AND RT FWD GUSSETS CHAFED. REPAIRED IAW B767 SRM.SDR ABXR2011052700014Stiffener · crackedINBOARD HYD BAY INSIDE STIFFENER CRACKED ON INBOARD AFT END. REPAIRED IAW B767 SRM.SDR NSVA2011121Strap · damagedRIGHT O/B NACELLE OVERSIZED HOLES FROM PREVIOUS FIGURE 8 STRAP LUG REPAIR IAW SB-340-54-022. COMPLETED REPAIR BY REPLACING STRAP IAW SF340 SRM 51-70-10 AND COLGAN AIR TD 340-54-11-17.SDR KCSA111137Fitting · crackedNR 1 PYLON O/B VERT FRAME NAC STA 235 HAS A CRACKED CLIP - TOP SIDE.SDR EIAA2011043Fitting · corrodedNR 4 PYLON BOTH UPPER AND LOWER DUAL SIDE BRACE FITTINGS HAVE CORROSION IN THE BEARING MOUNT RACES. REPLACED DSB FITTINGS BEARING RACES PER EO 747-54-1804-05.SDR NSVA2011116Structure · damagedVERIFY PERMANENT REPAIR WAS ACCOMPLISHED IAW SAAB SDS-1661 FOUND PREVIOUSLY INSTALLED DOUBLER ON RT NACELLE I/B SIDE NS 248 REF CONTROL NUMBER 196-44. VERIFY PERMANENT REPAIR WAS ACCOMPLISHED IAW SAAB SDS-2331 FOUND PREVIOUSLY INSTALLED DOUBLER/TRIPLERS ON RTSDR JR2R2011052400225Structure · chafedRT NACELLE OUTBOARD WHEEL HUMP CHAFED THRU 100 PERCENT. REMOVED AND REPLACED RT OUTBOARD WHEEL HUMP IAW DASH 8 SRM 51-42-05.SDR JR2R2011052400221Bracket · damagedTOP BRACKET IS CRACKED AND HALF MISSING THAT IS CONNECTED TO THE SOFT BUSHING TIE BAR ON THE I/B SIDE OF THE LT ENGINE. REMOVED AND REPLACED BRACKET IAW CRJ 900 SRM 51-42-06, 51-32-06, 54-12-10.SDR FDEA201105201894Shim · looseNR2 PYLON MID BULKHEAD RT FWD SIDE LOWER FLANGE AT PP STA 174.30 FOUND WITH SHIMS MIGRATION. REPAIRED IAW SRM 54-50-90, REV 102, REPAIR 7. REPAIR IS CLASSIFIED AS MAJOR.SDR FDEA201105201893Shim · looseNR1 PYLON MID BULKHEAD LT AFT SIDE LOWER FLANGE AT PP STA 174.30 FOUND WITH SHIMS MIGRAGTION. RECTIFIED IAW SRM 54-50-90, REV 102. REPAIR 7. REPAIR IS CLASSIFIED AS MAJOR.SDR FDEA201105201892Shim · looseNR1 PYLON MID BULKHEAD RT FWD SIDE LOWER FLANGE AT PP STA 174.30 FOUND WITH SHIMS MIGRATION. RECTIFIED IAW SRM 54-50-90, REV 102. REPAIR IS CLASSIFIED AS MAJOR.SDR FDEA201105201891Shim · looseNR2 PYLON MID BULKHEAD UPPER LINK FITTING AT PP STA 174.30 FOUND WITH SHIMS MIGRATION. RECTIFIED IAW SRM 54-50-90, REV 102. REPAIR 6. REPAIR IS CLASSIFIED AS MAJOR.SDR FDEA201105201890Bushing · looseNR 2 PYLON STRUT TO DIAGONAL BRACE LOWER SPAR FITTING BUSHING FOUND WITH MIGRATION. REPAIR CARRIED OUT IAW SRM 54-50-90, REPAIR 5, REV 102. REPAIR IS CLASSIFIED AS MAJOR.SDR DALA1135521318Angle · crackedWHILE AT PSV IN ATL, MTC FOUND A 2.25 INCH CRACK IN THE RADIUS OF THE INBOARD SKATE ANGLE OF THE NR 2 AFT STRUT FAIRING. THE CRACK EXTENDS FORWARD FROM THE AFT EDGE OF THE PART. THE SKATE ANGLE IS MANUFACTURED FROM 0.125 INCH BARE 7075-T6 SHEET. CRACK REPAISDR UALA2011051702428Strip · damagedNR 1 ENG NR 2 GAP STRIP DAMAGED. REPAIRED PER MT 54-UA2 2.375 INCH LONG .150 INCH DEEP SECOND CRACK FOUND EXCEEDS 4.0 INCHES. SECOND REPAIR EXCEEDS MT 54-UA1 LIMITS 3.875 INCH LONG .180 DEEP. ACCOMPLISHED HFEC PER 777 NDT MANUAL PART 6 CHAPTER 51-00-06, NO SDR KCSA111130Structure · chafedNR 1 PYLON, PNEUMATIC DUCT - TO ENGINE CONNECTION - ANTI ROTATION STRAPS CHAFING STRUCTURE - BOTH SIDES- NAC STA 200 APPROX.SDR KCSA111129Structure · chafedNR 2 PYLON, PNEUMATIC DUCT- TO ENGINE CONNECTION - ANTI ROTATION CHAFING STRUCTURE - BOTH SIDES - NAC STA 200 APPROX.SDR KCSA111128Structure · chafedNR 3 PYLON, PNEUMATIC DUCT - TO ENGINE CONNECTION - ANTI ROTATION STRAPS CHAFING STRUCTURE - BOTH SIDES, NAC STA 200 APPROX.SDR KCSA111127Structure · chafedNR 4 PYLON, PNEUMATIC DUCT - TO ENGINE CONNECTION - ANTI ROTATION STRAP CHAFING STRUCTURE INBOARD NACELLE STA 200 APPROX.SDR EE4Y20110289Fairing · crackedENGINE NR 1, AFT PYLON SECTION LOWER AFT FIXED FAIRING WITH CRACK. MAJOR REPAIR.SDR EE4Y20110288Support Angle · crackedENGINE NR 2, PYLON UPPER SIDE (AT PRECOOLER AREA LT SIDE) BETWEEN PYLON STA 537 AND STA 608, SUPPORT ANGLE WITH CRACK. NOTE: THE SUPPORT ANGLE CRACK REQUIRES A MAJOR REPAIR.SDR EE4Y20110287Support Angle · crackedENGINE NR 1, PYLON UPPER SIDE (AT PRECOOLER AREA RT SIDE) BETWEEN PYLON STA 537/RIB07 AND STA 608/RIB08, SUPPORT ANGLE WITH CRACK. NOTE: THE SUPPORT ANGLE CRACK REQUIRES A MAJOR REPAIR.SDR P5CA2011051200054Acoustic Panel · dentedNUMBER 2 ENGINE NOSE COWL INLET HAS DENTS TO THE ACOUSTIC PANELS AT THE 3 AND 6 O'CLOCK POSITIONS. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A54B-1136 AND SRM 54-15-01.SDR P5CA2011051200053Acoustic Panel · dentedNUMBER 4 ENGINE NOSE COWL INLET & NBSP; HAS DENTS TO THE ACOUSTIC PANELS AT THE 3, 6 AND 11 O'CLOCK POSITIONS. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A54B-1137, SRM 54-15-01.SDR USAA2011051891904Sleeve · corrodedSAL - S5 - LEVEL 2 GALVANIC CORROSION ON LEFT PYLON SPIGOT FITTING SLEEVE BETWEEN PYLON STA 6465 TO 7063 & BETWEEN RIB 3 TO RIB 5. REPLACED LEFT PYLON SPIGOT FITTING SLEEVE IAW JOB CARD 26C40054034.SDR USAA2011051891906Bearing · corrodedSAL - S5 - LEVEL 2 GALVANIC CORROSION ON RIGHT PYLON SPIGOT BEARING BETWEEN PYLON STA 6465 TO 7063 & BETWEEN RIB 3 TO RIB 5. REPLACED RIGHT PYLON SPIGOT BEARING IAW JOB CARD 26C40054035.SDR USAA2011051891905Sleeve · corrodedSAL - S5 - LEVEL 2 GALVANIC CORROSION ON RIGHT PYLON SPIGOT FITTING SLEEVE BETWEEN PYLON STA 6465 TO 7063 & BETWEEN RIB 3 TO RIB 5. REPLACED RIGHT PYLON SPIGOT FITTING SLEEVE IAW JOB CARD 26C40054035.SDR KCSA111101Structure · crackedNR 2 PYLON STRUT CHORD CRACKED, NAC STA 221.9. HFEC INDICATED CRACK IN AFT LT I/B HOLE.SDR KCSA11101Structure · crackedNR 2 PYLON STRUT CHORD CRACKED, NAC STA 221.9, AFT LT I/B HOLE - CRACK INDICATED HFEC.SDR DALA1130909875Support · crackedNR 2 PYLON AFT MOUNT LWR BEAM SUPPORT STRUCTURE CORNER ANGLE CLIP CRACKED, VIEWED THRU ACCESS DOOR PNL 8212. REMOVED ANGLE CLIP PER SRM DC9 51-30-1, FABBED ANGLE CLIP DWG 9915500 TRAVELER 8736011001 LOCATED & DRILLED HOLES PER SRM DC -9 51-10-4 INSTALLED ANGSDR DALA1129711201Skate Angle · crackedNR 1 PYLON I/B AFT SKATE ANGLE AFT END CRACKED & REPAIRED PER ERA 489730-14 REV ORG.SDR CALA2011042600307Stiffener · crackedNR 1 PYLON STA 285 FOUND O/B STIFFENER CRACKED NR1 PYLON STA 285 O/B CRACKED STIFFENER. REPLACED AS PER SRM 51-10-02 AND NEW STIFFENER INSTALLED AS PER SRM 51-40-02 AND FORM 44.0008 ITEM 1-2 ACCOMPLISHED.SDR DALA1126835501Skate Angle · crackedRT WING OUTBD OF RT PYLON T/E SKATE ANGLE CRACKED. PERFORMED HFEC INSP IAW NTM 51-00-19 PT 6. STOP DRILLED CRACK IAW SRM 54-52-01-801. REMOVED PNL 455BR IAW SRM 51-40-02. REMOVED SKATE ANGLE IAW SRM 51-40-02. RECEIVED FABBED SKATE ANGLE WITH TRAVELER T11/SDR FDEA201104131464Stiffener · crackedPYLON NR 2, STIFFENER END BETWEEN RIB 6 AND RIB 7 FOUND CRACKED INDICATION APPROX 0.1 INCH DURING HIGH FREQUENCY EDDY CURRENT INSP. REPAIRED AS PER E.A. 6-5450-150310 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 112.SDR KCSA111096Stiffener · chafedNR 3 PYLON STIFFENER CHAFED AT NCA STA 249, CUTOUT PANEL 473EL.SDR ABXA2011051048Angle · crackedNR 2 PYLON RT SIDE ANGLE LOCATED BETWEEN AFT STRUT FAIRING AND CORE COWL HINGE HAS 2 INCH CRACK. REMOVED NR 2 PYLON RT SIDE, ANGLE AND WELD REPAIRED IAW ABX PROCESS STANDARD MANUAL 900-7-2-1. RE-INSTALLED BRACKET IAW B767-200 SRM 51-40-02.SDR ASAA1149442Panel · chafedNR 2 STRUT OUTBOARD FUSE PIN PANEL CHAFED. FABRICATED REPLACEMENT PANEL AND INSTALLED IAW BOEING DWG 313A1200 AND B737 400 SRM 51 30 01.
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