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 DALA1231179255Fastener · wornFASTENERS ON LT PYLON WORN, REMOVED AND REPLACED FASTENERS PER EA 02-476701-12AD REV E OPN 0101.SDR C77A20120502023Heat Shield · erodedLT ENGINE FAIRING NR 2 HEAT SHIELD LOWER INBD. SCREW HOLE ELONGATED. REAM THE HOLE TO SPECIFIED DIA OF ETD, INSTALL COUNTERSUNK WASHER NAS1169 BONDED TO HEAT SHIELD ON WO 485382-422 IAW ETD ETD 2012-170-006111 AND EA E175-54-096 REV.SDR C77A20120502022Shear Pin · looseRT PYLON DRAG BRACE-AFT SHEAR PIN OTBD WASHER PN NAS1149C1432R & 170-16192-405 ROTATES. REMOVE CASTELLATED NUT, PN PE22072L14, CHECK RUN-ON TORQUE AND REINSTALL AND TORQUED NUT TO SPECIFIED TORQUE VALUE LISTED IN ETD AND RESAFTIED ON WO 485382-421 IAW ETD 201SDR DALA1227310181Fitting · damagedLEFT WING PYLON AFT PITCH LOAD BACKUP FITTING O/B BOLT HOLE HAS SHORT EDGE MARGIN. WORKING FROM PRI.SDR AALA20120428005Hinge Fitting · crackedNUMBER 2 PYLON OUTBOARD HINGE FITTING UPPER AFT HOLE HAS TWO CRACK INDICATIONS. INSTALLED DOUBLER PER EA B757-54-023384.SDR FDEA201204271660Plate · crackedNR 2 PYLON STRUCTURE, JUST ABOVE PANEL 423CL CUT OUT HAS LOOSE FASTENER. FOUND FISHPLATE CRACKED. R & R FISHPLATE IAW SRM 51-72-10.SDR UALA2012042402481Rub Strip · damagedNR 3 ENGINE INBOARD CORE COWL FWD RUB STRIP IS DAMAGED. REPLACED DAMAGED SECTION OF RUBSTRIP ON NR 3 ENG INBOARD CORE COWL LEADING EDGE.SDR UALA2012042402471Seal · damagedFOUND HEAT SHIELD SEAL DAMAGED. REPLACED SEAL PER AMM.SDR UALA2012042002360Seal · missingLEFT WING PYLON FIRE SEAL APPEARS TO BE MISSING. REPLACED MISSING SEAL PER SERVICE TIP AMM. PANEL 437AR.SDR DALA1223030185Angle · crackedDURING OPN 5181 OF TRANS 1T203 NACELLE/PYLON ATTACH FITTING INSPECTION. FOUND CRACK ON THE CLOSEOUT ANGLE NEAR THE INBD END, OUTBD OF THE MIDSPAR. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPSSDR DALA1223001501Web · chafedNR 2 PYLON AFT FAIRING, LOWER HORIZONTAL WEB, LT FWD UPPER SURFACE HAS DAMAGE FROM DEEP CHAFING.SDR FDEA201204121379Fairing · crackedNR 1 ENGINE PYLON LOWER AFT FAIRING ASSY, LT AFT ATTACH LUG AT RIB 18 CRACKED. REPAIRED IAW DWG R54610384 ISSUE A COMPLIED WITH EA 6-5450-160114, PT1.SDR UALA2012040902169Heat Shield · crackedNR 2 PYLON HEAT SHIELD GAP COVER STRIP (2ND STRIP COUNTING FROM FWD TO AFT) IS CRACKED AT TWO PLACES (ONE CRACK IS LOCATED AT A PREVIOUS REPAIR). REMOVED DAMAGE & ACP HFEC INSPECTION REF 777MT 54-UA2 DAMAGE 1.28-32L BY 1-4 DEEP.SDR UALA2012040902167Heat Shield · looseFOUND FWD SEGMENTS ON LT AND RT ENGS WITH LOOSE FASTENERS. SUPPLEMENTAL DATA UPDATE, ALSO FOUND BAD BULB SEALS. SEALS ON HAND NEED REMOVED AND REPLACED THEN RE-INSTALL SEGMENTS. NR 2 ENGINE STRUT AFT FAIRING HEAT SHIELD SEAL FASTENERS ARE LOOSE (FASTENERS NSDR LR7A2012040500370Duct · damagedDURING SCHEDULED C-10 CHECK, FOUND NR 4 QEC, SN LMG-1869-14 OIL COOLER DUCT FWD CHIN SCOOP ASSY WITH ELONGATED FASTENER HOLES AND CRACKS. REPAIRED IAW LAC MEA 382-54-12-018.SDR LR7A2012040500369Structure · crackedDURING SCHEDULED C-10 CHECK, FOUND NR 4 POSITION QEC SN LMG-1869-14 FWD BULKHEAD RT OUTER CAP TEE CRACKED AT FS 410.70. REPAIRED IAW MEA 382-54-07-081.SDR ABXA20120404340Beam · crackedNAC STA 295 NR 2, INBD ANGLE AT BOTTOM MOUNTING HOLES FOR PANEL 447ERX IS CRACK AND WORN. REMOVED AND REPLACED NR 2 O/B PYLON BEAM IAW B767-200 SRM 51-40-02, ACFT WAS GROUNDED.SDR USAA2012042400013Fitting · cracked2S CHECK - CRACK ON FITTING ON LEFT PYLON AT XM9528, RIB 1. REPLACED FITTING AT LEFT PYLON AT XM9528, RIB 1 IAW A319 SRM 54-55-12; PARAGRAPH 5B; FIGURE 202.SDR USAA2012041900012Fitting · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LEFT PYLON SPIGOT FITTING RECEPTICAL BETWEEN PYLON RIB 4 & RIB 5. REPLACED LEFT PYLON SPIGOT FITTING IAW A319 SRM 54-51-12.SDR USAA2012040300010Structure · corrodedBC7 CHECK, LT PYLON SPIGOT PIN OUTER RACE APPROXIMATELY 75% DAMAGED DUE TO CORROSION, EXCEEDS THE .002 LIMIT. REPLACED LT PYLON SPIGOT PIN OUTER RACE IAW A320 SRM 54-51-12, FIG 201.SDR USAA2012040200010Plate · corrodedBC7 CHECK CORROSION ON SPIGOT PIN RT PYLON UPPER PANEL INNER RACE. REPLACED RT PYLON UPPER PANEL INNER RACE IAW A320 AMM 54-51-12 & REPLACED RT PYLON UPPER SPIGOT PLATE IAW A320 SRM 54-51-12 FIG 201.SDR UALA2012033002000Heat Shield · wornRIGHT HEAT SHIELDS WORN. REMOVED PYLON HEAT SHIELDS NR 2 ENG, PER MT 54-UA2. OUT OF LIMITS. REPAIRED HEATSHIELD. INSTALLEDSDR EIAA20120330026Structure · crackedNR 4 PYLON O/B SIDE FWD ACCESS CUT OUT HAS CRACK IN UPPER FWD SIDE. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER ECRA 489-54-019-2SDR DALA1218390678Bushing · migratedNR 1 PYLON DIAGONAL BRACE WING SIDE I/B BUSHING MIGRATED. REMOVED AND INSTALLED NEW 2 EA BUSHINGS IAW BAC DWG 112N2011 REV B AND ERA 499397-14AD REV ORIG.SDR CA120327003Angle · cracked(CAN) WHILE CONDUCTING A CORROSION INSPECTION, CRACKS WERE FOUND ON THE NR 1 NACELLE, OTBD LONGERON CHANNEL, PN 75410103-105, AND LONGERON ANGLE, PN 75410104-103, AND NR 4 NACELLE, INBD LONGERON CHANNEL, P/N 75410119-106, LONGERON ANGLE P/N 75410104-104, NR 4 SDR ABXA20120322318Angle · chafedRIGHT PYLON STRUCTURE JUST AFT OF NOSE COWL CHAFE PAD ON PYLON CHAFED. FABRICATED - 134 ANGLE IAW DWG 311T1510 USING .050 2024-0 PO#0011149. FABRICATED 133 ANGLE IAW DWG 311T1510 USING .050 2024-0 PO# 0011149, ACFT WAS GROUNDED.SDR FDEA201203211046Fastener · damagedLEFT PYLON, RT SIDE ACCESS THRU PANEL NR 433LR MID BULKHEAD UPPER SIDE WITH DAMAGED FASTENER. BLENDED IAW EA F-5450-159926.SDR DALA1217230180Angle · crackedNR 2 PYLON MIDSPAR FITTING CLOSE OUT ANGLE WAS CRACKED AND REPAIR WAS C/W BY ERA 461004-14AD REV A AND EO 01-074965-03AD REV ORG.SDR UALA2012032001806Fastener · missingRT ENG PYLON MISSING FASTENER ON INSIDE SMALL ALT PANEL. REPLACED SCREWS.SDR UALA2012032001805Fastener · missingLT ENG PYLON MISSING FASTENER INBD SIDE AFT EDGE OF PANEL. REPLACED SCREWS.SDR AALA20120319007Stiffener · crackedRIGHT PYLON HORIZONTAL STIFFENER CRACKED JUST OUTBOARD OF FRAME CHORD AT STATION 285. REPLACED STIFFENER PER SRM 51-40-02.SDR KCSA201203171034Strap · crackedNR 1 PYLON STRAP AT NAC STA 221 HAS A CRACK INDICATION .1 LONG IN THE AFT CENTER HOLE.SDR AALA20120316005Torque Box · crackedCRACK IN UPPER TORQUE BOX ON LEFT PYLON AT NUT PLATE HOLE. INSTALLED DOUBLER PER AARD 54-52-01-1.SDR ABXA20120314317Support Bracket · crackedRIGHT PYLON RT SIDE, AFT CORE COWL FAIRING SUPPORT BRACKET CRACKED. LOCATED JUST FORWARD OF EXHAUST CONE SEAL. WELDED IAW ABX PROCESS STANDARDS MANUAL CHAPTER 900-7, ACFT WAS GROUNDED.SDR ABXA20120313316Fitting · chafedRIGHT PYLON WING SIDE FITTING CHAFED ACCESS PNL 447AL. REPAIRED ON REA B654-59729-MR, ACFT WAS GROUNDED.SDR UALA2012031301656Bearing · damagedNR 2 PYLON CROWN BEARING ROTATED AND RUSTY. REMOVED & REPLACED BEARING USING ALTERNATE TOOLING. REF SRM54-50-90 & AAR EA 080367. THIS REPAIR IS APPROVED BY FAA FORM 8100-9.SDR UALA2012031301643Clamp · broken2EA CONDUITS ASSY WORN THROUGH AND CLAMPS BROKEN. REF IPC-54-51-70-002A, REMOVED 6EA CLAMPS, 2EA BROKEN ALSO REMOVED CONDUIT TEES. ALSO SEE IPC-54-51-70-011. NR 4 PYLON SAILTAIL. RPL REPAIRED WIRE BUNDLE. REF:WDM29-33-12 & WDM29-34-11 & WDM73-21-84 FROM WISDR ABXA20120310314Channel · crackedLEFT PYLON PNL 447 ELX ACCESS CUTOUT LWR FWD "U" CHANNEL CRACKED. REMOVED AND REPLACED BEAM UNDER NR 2 PYLON PANEL 447ELX IAW B767 SRM 51-40-02, ACFT WAS GROUNDED.SDR UIEA2012042000157Fairing · distortedNR 4 ENGINE RT CORE COWL AFT UPPER TITANIUM FAIRING FOUND DISTORTED AND CHAFED. (NR 4 ENG RT CORE COWL AFT UPPER TITANIUM FAIRING DAMAGED AREA REPAIRED IAW SRM 54-41-01, FIG 201, REPAIR 5.)SDR ABXA20120307315Beam · crackedLEFT INBD PYLON BEAM BELOW HYD BAY DOOR IS CRACKED AT FWD LATCH FITTING INSIDE. REMOVED & REPLACED BEAM IAW B767-200 SRM 51-40-02, ACFT WAS GROUNDED.SDR HNAA2012030700661Angle · crackedOTBD NACELLE TO FRONT SPAR CLOSING ANGLE IS CRACKED ON NR 1 NACELLE. REMOVED SIDWALL ANGLE. FABRICATED NEW ANGLE IAW DWG 85710407. INSTALLED NEW ANGLE IAW EO 8-57-12-0082.SDR UALA2012030601415Panel · damagedPANEL ABOVE HEAT SHIELD ON ENG 1 OTBD SIDE PNL PART 313W3701-3 REMOVED FOR HEAT DAMAGE AND ROUTED TO THE SHOP FOR REPAIR IR TAG 313W3801-3. REMOVED AND REPLACED R57041. REMOVED AND REPAIRED PNL.SDR UALA2012030501408Seal · deterioratedLT ENGINE PYLON FAIRING HEATSHIELD FWD SEAL HEAVILY DETERIORATED & SPLIT, REF EQ4498. REMOVED HEATSHIELD SEGMENTS NR 1, 2, 3, & 4 PER MM. REPLACED FWD SEALSDR AALA20120303002Torque Box · crackedUPPER TORQUE BOX WEB CRACK. REPAIRED PER AARD 54-52-01-1.SDR UALA2012030201307Fireseal · missingPANEL 437AR AFT FIRE SEAL MISSING. REPAIRED FIRE SEAL SECTION.SDR USAA2012032000005Fitting · corroded2S CHECK - CORROSION ON PYLON SPIGOT RECEPTACLE FITTING BETWEEN STA 679 & STA 829 & BETWEEN RIB 4 & RIB 5. REPLACED PYLON SPIGOT RECEPTACLE FITTING IAW A319 SRM 54-51-12.SDR HNAA2012030200641Structure · corrodedLEFT NACELLE AFT SECTION OF NACELLE UNDER THE FINGERNAIL IS CORRODED. REMOVED CORROSION UNDER LT NACELLE FINGERNAIL AFT SECTION IAW SRM 51-20-11.SDR UALA2012022701190Fastener · looseAFTER FURTHER VISUAL INSPECTION FOUND 2 BLIND HUCKS SECURE BUT WITH WASHERS UNDER HEAD LOOSE AT THE 11 O' CLOCK AND 12:30 POSITION. THERE IS ONE ORIGINAL FASTENER LOOSE AT THE 1 O'CLOCK POSITION. REPLACED TWO LOOSE INTERIM REPAIR FASTENERS, WILL CF OTHER LOOSDR HALA2012022700086Attach Bracket · crackedLEFT PYLON INBD SIDE PYLON TO CORE COWL FAIRING ATTACH BRACKETS 3 EA CRACKED. BRACKETS LOCATED BETWEEN 1ST & 3RD CORE COWL HINGES. REMOVED 3 EA CRACKED BRACKETS. FABRICATED 3 EA BRACKETS IAW HAL M105 597140. INSTALLED BRACKETS AND PANEL.SDR P5CA2012030500021Skate Angle · crackedCRACK ON SKATE ANGLE OF NR 3 PYLON INBOARD FAIRING AT NACELLE STATION 457. (ACCOMPLISHED TIME LIMITED REPAIR PER EO 4454A142 AND BOEING SR 2112722461 AND REPAIR AND DEVIATION RECORD. PERMANENT REPAIR TO BE ACCOMPLISHED PRIOR TO 24 MONTHS).
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