JASC 5410
Service difficulty reports · 4,110
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 UIEA2026072400650Link · damagedFOUND NR 1 PYLON LINK AFT SIDE BOLT, WASHER, NUT DAMAGE, AND WING LUG BUSHING DAMAGE. IAW AMM 54-51-01-004-001 REV 116 AND AMM 54-51-02-004-001-005 REV 116, REMOVED NR 1 PYLON NACELLE STRUT AND ATTACH PIN BOLT. REPAIRED WING FRONT SPAR LUG BUSHING. IAW AMM 5SDR UIEA2026072400651Bushing · gougedFOUND NR 2 PYLON UPPER LINK FWD AND AFT SIDE PIN AND BUSHING, BEARING GOUGE AND WING LUG, PYLON LUG BISHING GOUGE. IAW AMM 54-51-01-004-001 REV 116 AND AMM 54- 51-02-004-001-005 REV 116 AND REFER TO JOB CARD, REMOVED NR 2 PYLON NACELLE STRUT AND ATTACH PIN SDR SWAA2026082746627Mount Bracket · cracked#1 ENGINE HIGH STAGE REGULATOR MOUNT BRACKET IS CRACKED AT ATTACH POINT. REMOVED AND REPLACED #1 ENGINE HIGH STAGE REGULATOR MOUNT BRACKET PER AMM 70-20-02. INSPECTED WORK PERFORMEDSDR IPXA2026073183785Support Bracket · crackedNR 1 ENG COOLING AIR MANIFOLD INLET AT 3 OCLOCK POS. HAS A CRACKED SUPPORT BRACKET. INSTALLED NEW SUPPORT BRACKET AT NR 1 ENGINE COOLING AIR MANIFOLD INLET AT 3 OCLOCK POSITION IAW SRM 51-40-02-0G-0 PAR. 4 AND 9. AND AMM 70-51-00-912-001-R00, PAR.2SDR IPXA2026072469018Bracket · crackedNR 2 ENG AFT PYLON RT BOTTOM FWD BRACKET IS CRACKED. INSTALLED A NEW BRACKET AT NR 2 ENG AFT PYLON RT BOTTOM FWD IAW SRM 51-40-02.SDR VNAA202608310007Shim · wornWEAR ON SHIM IN SETTLEMENT AREA OF LATCH OF THE ACCESS PANEL 444CT AND 444CB AT RT ENGINE. WEAR ON SHIM IN SETTLEMENT AREA OF LATCH OF THE ACCESS PANEL 444CT AND 444CB AT RH ENG WERE BLEND OUT PER SRM 51-12-00-001-001-A01, ACCESS PANEL 444CT AT RH ENG WAS ESDR IPXA2026072835996Drain Mast · crackedCRACKED MAST, NR 1 ENG LWR DRAIN MAST. IAW AMM 71-71-01-024-001-H00, REV 148, AND AMM 71-71-01-424-005-H00, REV.148, REPLACED THE DRAIN MAST OF NR 1 ENGINE.SDR IPXA2026072223255Seal · crackedCRACKED ZEE SEAL, NR 1 PYLON LT AFT FAIRING DOOR CUTOUT LWR, AFT SEAL AREA. INSTALLED FABRICATED ZEE SEAL IAW SRM 51-40-02-0G, REV 55, AND DWG 313T2380, SHT 68, REV A, & DWG 313T2303, SH 90, REV C, & SB 767-54-0109, REV 2.SDR SWIA2026071577219Bracket · crackedLEFT PYLON BRACKET CRACKED AT PYLON FS 605 ON BOTTOM SIDE. COMPLIED WITH REO 601R-54-61-150. REPAIR TO LT PYLON LEADING EDGE RIB AT 605.SDR FDEA202607140922Skin · damagedWHEN PERFORM EA G-5730-T0384072 P2 STEP 2, REPORT THE CURRENT AIRCRAFT CONFIGURATION TO FEDEX SERVICE ENGINEERING TO REQUEST AIRPLANE JACKING REQUIREMENTS FROM BOEING TO PERFORM THE PERMANENT DOUBLER/TRIPLER REPAIR AS SHOWN IN FIGURE 1. NOTED: NO.1 ESDR IPXA2026091325488Web · crackedNR 2 ENGINE, INLET COWL, RH SIDE AT 3 O'CLOCK IS CRACKED. ACCOMPLISHED SPLICE REPAIR STEP 1 TO 10 IAW SRM 54-10-00 REPAIR NO. 14. ACCOMPLISHED SPLICE REPAIR IAW SRM 54-10-00 REPAIR NO. 14 STEP 11 TO 14 AND INSTALLED IAW SRM 51-40-21-001.SDR IPXA2026091426061Plate · crackedNR 2 PYLON, TOP SKIN RH SIDE AT RIB 3 IS CRACKED. REMOVED CRACKED FISHPLATE FROM NO. 2 PYLON, TOP SKIN RH SIDE AT RIB 3 IAW SRM 51-40-21. INSTALLED FISHPLATE BRACKET AT PYLON NR 2 TOP SKIN R/H O/B RIB 3 PER SRM 51-40-21-001.SDR IPXA2026091014150Bracket · crackedNR 1 ENG OTBD AFT PYLON, MOUNTING BRACKET COMMON TO FAIRING 475AL CRACKED, DOT 55-011. REMOVED EXTRUSION CRACKED P/N A54610811600 AT NR 1 ENG O/B AFT PYLON IAW P&W SRM 54-04-01. INSTALLED EXTRUSION P/N UP-A5461081160000 AND FAIRING ASSY P/N A54612280602 ON NR SDR IPXA2026091014252Seal · crackedNR 1 ENG, OTBD PYLON RAIN SEAL HAS 3EA CRACKS AT BASE PLATE, JUST FWD OF THE AFT ENG MOUNT. REMOVED EDGING EXTRUSION P/N A54610811500 AND SPRING P/N A54610811504 CRACKED AT ENG 1, O/B PYLON IAW P&W SRM 54-04-01. INSTALLED EDGING EXTRUSION P/N UP-A54610811500 ASDR IPXA2026082862693Seal · crackedNR 2 PYLON, LT SIDE, FR 5, LWR METALLIC SEAL CRACK. INSTALLED NEW EXTRUSION EDGING IN NR 2 PYLON, LT SIDE, FR 5, LWR. IAW SRM 51- 40- 21 AND AIPC 54-51-06-08 ITEM 10.SDR IPXA2026082662645Plate · crackedNR 2 PYLON, AT PRECOOLER AREA, UPPER, AFT RT PLATE CRACKED. REMOVED & REPLACED THE PLATE AT RIB 3A RT IAW SRM 51-40-21.SDR IPXA2026081962158Structure · crackedNR 2 PYLON, INSIDE PRECOOLER AREA, AT FR 4, L/H WALL WITH CRACK.SDR IPXA2026081462082Plate · crackedNR 2 PYLON, RT SIDE, FR 3A, CORNER BRACKET HAD 2 CRACKS. REMOVED AND REPLACED FISHPLATE P/N A5461237120140 BTCH: 0004501257. ON NR 2 PYLON R/H SIDE, FR3A, CORNER IAW A300-600 SRM 51-40-21.SDR FDEA202607080862Fitting · chafedLEFT ENGINE PYLON - AFT PYLON BULKHEAD LUG FITTING FOUND WITH CHAFE AT EXTERIOR UPPER AREA.YWN-418. CARRIED OUT REPAIR IN ACCORDANCE WITH EA #1-5440-T0387673 PART 1 AND 2 TITLE: NACELLES/PYLON - ATTACH/MOUNT/HINGE- NR 1 PYLON AFT BULKHEAD LUG INSPECTION ANDSDR DALA2026070904020Panel · missingON WALKAROUND, FOUND FAN DUCT PANEL SLIDE FROM 4 O'CLOCK POSITION. ALSO FOUND FAN DUCT PANEL FROM 4 O'CLOCK POSITION MISSING. NR1 ENG. REPLACED FAN DUCT PANEL SLIDE FROM 4 O'CLOCK POSITION IAW AMM 72-00-00-04, ACFT OK FOR SVC. (LP 8578478 - AIRCRAFT WAS GROUSDR IPXA2026070759188Cowling · dentedDENTED SKIN, NR 2 ENG NOSE COWL INLET AT 10 O'CLOCK POSITION. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.5", 12.8" FROM AFT EDGE, 51.7" FROM LWR EDGE, AT 10 O'CLOCK ON THE ACOUSTIC PNL OF NO.2 ENG INLET COWL ). FILL THE CUT OUT WITH ADHESIVE CSDR DALA2026070203881Receptacle · corrodedLEVEL 2 CORROSION, CORROSION SPIGOT FITTING RECEPTACLE ON LH PYLON. REPLACED SPIGOT FITTING RECEPTACLE ON LH PYLON AS PER A320 SRM 54-51-12-300-001. TOOK MEASURE INITIAL DIAMETER IS: 4.331 INCH. (LP: 1677696, AIRCRAFT WAS GROUNDED)SDR DALA2026070203880Receptacle · corrodedLEVEL 2 CORROSION, CORROSION SPIGOT FITTING RECEPTACLE ON RH PYLON. REPLACED SPIGOT FITTING RECEPTACLE ON RH PYLON AS PER A319 SRM 54-51-12-300-001. TOOK MEASURE INITIAL DIAMETER IS: 4.331 INCH.SEE INDIVIDUAL SIGN OFF ON ORNRC 68/400. RII INSPECTION COMPLETE.SDR 1Q2R2026070100003Structure · wornDURING INSPECTION OF THE L/H AFT CORE COWL, WEAR DAMAGED WAS FOUND ON THE FORWARD FLANGE BEHIND THE P-SEAL AT 9 O'CLOCK POSITION. PERFORMED REPAIR IN ACCORDANCE WITH EA 5413-2026-0653, REV-.SDR SWAA2026072246922Web · crackedCRACKED WEB OTBD FAN COWL ON RT ENGINE (1 EA). REPLACED THE WEB OTBD FAN COWL ON RT ENGINE IAW SRM 51-40-02 AND CMM 71-13-30.SDR IPXA2026070706484Panel · crackedNR 2 ENG OTBD SPRING PANEL IS CRACKED 115-072. INSTALLED NEW SPRING PANEL NR 2 ENG OTBD IAW SRM 51- 40-02.SDR CALA2026063017466Acoustic Liner · missingDURING ENGINE NR 1 WASH NOTED FAN BOOSTER ACOUSTICAL PANEL BETWEN POSITION 4 O'CLOCK MISSING. CONFIRMED MISSING PANEL LINER ACOUSTIC . REMOVED AND INSTALLED FAN BOOSTER ACOUSTIC PANEL REF AMM DMC-B787-A-G72-22-04-00A-520A-A AND DMC-B787-A-G72-22-04-00A-720A-A,SDR IPXA2026070694047Rub Strip · chafedCHAFED RUB STRIP, NR 2 ENG RT CORE COWL INNER FACE T/E UPPER SIDE. REMOVED DAMAGE RUB STRIP IAW SRM 51-40-02-0G, REV 95. INSTALLED A NEW RUB STRIP IAW SRM 51-40-02-0G, REV 95, AND CMM IPL 71-13-24, REV 50.SDR DALA2026070703953Bearing · corrodedCORROSION FOUND ON NR 1 ENGINE PYLON UPPER FORWARD SPHERICAL BEARINGS R7 AND R8. REMOVED AND REPLACED BEARINGS IAW DWG C01627010 -B. (LP# 1669886; AIRCRAFT WAS GROUNDED)SDR DALA2026070703952Bearing · damagedNR 1 ENGINE PYLON BOX BEAM R7. REMOVED AND REPLACED THE BEARINGS IAW DWG C01701332. (LP# 1669877; AIRCRAFT WAS GROUNDED)SDR IPXA2026070190225Cowling · crackedNR 1 ENG INLET COWL LIP CRACKED BETWEEN 11 AND 1 O'CLOCK POSITIONS. INSTALLED NR 1 ENGINE INLET COWL IAW AMM 71-11-01.SDR JR2R20260627079Fitting · chafedNR 1 ENGINE PYLON INBOARD AND OTBD UPPER LINK FITTINGS ARE CHAFED & GOUGED. REPAIRED PER ETD.SDR SWAA2026063016096Web · crackedNR 1 ENGINE INBD COWL WEB CRACKED AFT OF OIL SERVICE DOOR. REMOVED AND REPLACED NR 1 ENGINE INBD COWL WEB AFT OF OIL SERVICE DOOR PER SRM 51-40-02. REMOVED AND REPLACED NR 1 ENGINE INBD COWL WEB AFT OF OIL SERVICE DOOR IAW SRM 51-40-02.SDR IPXA2026070540146Seal · brokenBROKEN SEAL, NR 3 PYLON 472HR PANEL. REVIEWED TASK IAW GMM-MTX 09.05.01.09. INSTALLED A NEW SEAL IAW SRM 51-40-02-0G, REV.107, AND DWG 65B90466, SH 2, REV D.SDR CALA2026063017475Latch · damagedOPEN ENG LATCHES ON NR 2 ENGINE. CONTACTED ENGINEERING AND APPLYING ECRA 5452-01160. TERMINATING ACTION TO BE COMPLETED IN 5 DAYS.111 LATCH OF CONCERN IS INBD AFT LATCH, SECURED REF ECRA5452-01160. INTERIM REPAIR MADE TO #2 ENGINE PYLON THUMBNAIL FAIRING LATCHSDR SWAA2026072413423Plate · crackedCRACKED SEAL PLATE FOR ACCESS PANEL 431, LT PYLON. REPLACED THE SEAL PLATE FOR ACCESS PANEL 431 IAW SRM 51-40-02-0G, AND DWG 313A2110, SHEET 24, REV -. EVALUATED CRACK AND DID NOT FIND ALLOWABLE DAMAGE IN SRM.SDR IPXA2026072317101Frame · crackedRIGHT WING PYLON FAIRING 485AL FRAME NR 1 FWD OTBD SUPPORT ANGLE CRACKED AT UPPER INNER RADIUS AREA. INSTALLED A NEW ANGLE ON PYLON LOWER FAIRING 485AL FRAME NR 1 FWD OTBD SUPPORT IAW SRM 51-40-21-001.SDR SWAA2026072453602Seal Seat · crackedCRACKED SEAL BLADE ON ACCESS PANEL 441AL, AT RT PYLON. REPLACED SEAL BLADE ON ACCESS PANEL 441AL IAW SRM 51-10-02-0G-0, PARAGRAPH 9, AND SRM 51-40-02-0G-0.SDR VNAA20260623015Fitting · corrodedWHILE PERFORMING INSPECTION OF LT THRUST FITTING IAW AMM 71-22-01-400-801-A01 STEP 4.A.(1). FOUND FRETTING CORROSION ON LT PYLON OUTBD RIB THRUST FITTING HOUSING. REPAIRED LT PYLON OUTBOARD RIB REO 670-54-51-089, REV -.SDR IPXA2026090878639Seal · crackedRH PYLON, I/B SIDE, 2EA RAIN GUARD DAMAGED. REMOVE AND REMPLACE NEW METAL SEAL RH PYLON, I/B SIDE P\N: A5461081160200, IAW A300-600 SRM 51-40-21-001.SDR IPXA2026062754538Pad · corrodedNR 1 ENGINE O/B CORE COWL T/E RUB PAD, 3RD FROM BOTTOM, HAS AREA OF CORROSION. INSTALEED SERVICEABLE PART AT NR 1 ENGINE OTBD CORE COWL T/E STOP PAD, 3RD FROM BOTTOM IAW SRM 51-40-02-0G-0.SDR IPXA2026062204155Nose Cowl · dentedDENTED SKIN, NR 1 ENG NOSE COWL INNER BARREL NEAR 7:00 POS. (REPAIR) CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.3", 11" FROM AFT EDGE AND 27" FROM OUTBD EDGE, AT 7 O'CLOCK ON THE INNER BARREL OF NO.1 ENG INLET COWL ). BOND THE SPACER WITH FILSDR IPXA2026062204145Nose Cowl · dentedDENTED SKIN, NR 1 ENG NOSE COWL INNER BARREL NEAR 1:00 POS. (REPAIR) CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.5", 21" FROM FWD EDGE, 18" FROM UPPER EDGE, AT 1 O'CLOCK ON THE INNER BARREL OF NO.1 ENG INLET COWL ). FILL THE CUT OUT WITH ADHESSDR IPXA2026062204122Nose Cowl · dentedDENTED SKIN, NR 1 ENG NOSE COWL INNER BARREL NEAR 11:00 POS. (REPAIR) CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.3", 18.5" FROM AFT EDGE, 24" FROM UPPER EDGE, AT 11 O'CLOCK ON THE INNER BARREL OF NO.1 ENG INLET COWL ). FILL THE CUT OUT WITH SDR IPXA2026062204106Nose Cowl · dentedDENTED SKIN, NR 1 ENG NOSE COWL BARREL NEAR 4:00 POS. (REPAIR) CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.5", 20" FROM FWD EDGE, 4" FROM LOWER EDGE, AT 4 O'CLOCK ON THE INNER BARREL OF NO.1 ENG INLET COWL ). FILL THE CUT OUT WITH ADHESIVE CUSDR IPXA2026062203995Nose Cowl · dentedDENTED SKIN, NR 1 ENG NOSE COWL INNER BARRER NEAR 9:00 POS. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.5", 4.75" FROM AFT EDGE, 33" FROM LOWER EDGE, AT 9 O'CLOCK ON THE INNER BARREL OF NR 1 ENG INLET COWL). FILL THE CUT OUT WITH ADHESIVE CURESDR IPXA2026062203992Nose Cowl · dentedDENTED SKIN, NR 1 ENG NOSE COWL INNER BARREL NEAR 6:00 POS. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.3", 10.5" FROM AFT EDGE AND 45" FROM OUTBD EDGE, AT 6 O'CLOCK ON THE INNER BARREL OF NR 1 ENG INLET COWL). BOND THE SPACER WITH FILM ADHESISDR IPXA2026062203971Nose Cowl · dentedDENTED SKIN, NR 1 ENG NOSE COWL INNER BARRER NEAR 9:00 POS. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.3", 7" FROM AFT EDGE AND 24" FROM LOWER EDGE, AT 9 O'CLOCK ON THE INNER BARREL OF NO.1 ENG INLET COWL ). FILL THE CUT OUT WITH ADHESIVE CURSDR IPXA2026062203947Nose Cowl · dentedDENTED SKIN, NR 1 ENG NOSE COWL INNER BARREL NEAR 5:00 POS. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.3", 19.5" FROM UPPER EDGE AND 11.5" FROM AFT EDGE, AT 5 O'CLOCK ON THE INNER BARREL OF NR 1 ENG INLET COWL). BONDED THE SPACER WITH FILM ASDR IPXA2026062203822Nose Cowl · dentedDENT - SKIN, NR 1 ENG NOSE COWL INNER BARREL NEAR 4:00 POS. (REPAIR) CONFIRM THAT THE ENGINE NACELLE IS ACOUSTICALLY COMPLIANT IAW SRM 54-00-00-2R-0 REV. 95.
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