JASC 5414
Service difficulty reports · 4,361
Reports filed under 5414 · Nacelle/Pylon, Plate/Skin, 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 = '5414' 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 = '5414' 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 FDEA201303060504Skin · corrodedNR 2 PYLON LEFT SKIN PANEL 443GL CUTOUT, EDGE CORRODED. REPAIRED IAW EA F-5450-T0300094. MAJOR REPAIRSDR SWAA2013030613390Rub Strip · crackedRUBSTRIP'S ON PANEL'S 431AL & 431AR ARE CRACKED. REMOVED AND REPLACED RUBSTRIPS PER SRM.SDR KCSA201302280034Skin · crackedNR 3 PYLON CAP SKIN HAS A 1 INCH CRACK AT NAC STA 221 COMING FROM A FASTENER HOLE.SDR FDEA201302270464Skin · corrodedNR 1 NAC STRUT PYLON STRUCTURE INBD SKIN AT PP STA 185.0 FOUND WITH BULGING. SKIN REMOVED AND REPLACED IAW DWG 311N5002 SHT.14 REV.E, WITH ALTERNATE SKIN IAW REF EA F-5410-155964. MAJORREPAIR.SDR FDEA201302210400Skin · corrodedNR 1 ENG STRUT HAS CORROSION ON SKIN INSIDE STRUT AT ACCESS 433CL ACCOMPLISHED EA F-5450-165133. NACELLES/OYLONS- NR 1 PYLON OUTBD SKIN CORROSION. MAJOR REPAIR.SDR UALA2013021800936Panel · crackedCRACK ON 4 ENGINE PYLON. CRACK IS 2.5 INCHES LONG. REPLACED WITH NEW PANEL PER AMM 54-50-99P801.SDR FDEA201302130341Skin · corrodedNR 1 PYLON NAC STRUT STRUCTURE INBD ACCESS HOLE CUT-OUT INNER EDGES SKIN FOR PANEL NR 433LR AT PPSTA.181.0 FOUND WITH CORROSION. CORRODED SKIN PANEL R & R IAW DWG 311N5002, SHT 14, REV E WITH ALTERNATE SKIN IAW EA F-5410-155964. REPAIR IS MAJOR.SDR KCSA201302100030Skin · chafedNR 4 PYLON I/B SKIN CHAFED THROUGH AT APPROX NAC STA 205 TO 220.SDR KCSA201302050028Skin · damagedNR 2 PYLON O/B SKIN DAMAGED AT NAC STA 180 TO 192.SDR KCSA201302050022Skin · damagedNR 2 PYLON O/B SIDE, OUTER AND INNER SKIN DAMAGED, NAC STA 225 TO 234.SDR UALA2013020400681Skin · crackedON WALKAROUND FOUND 3 INCH CRACK ON NR 3 ENGINE PYLON PANEL. FOUND CRACKED FROM SCREW HOLE TO EDGE ABOUT 1.5 INCH. MM 06-09-99,PG 215 PANEL 472WR. INTERIM REPAIRED PER ECRA 5450-02013.SDR FXGA2013020101Skin · crackedTHE NR 3 NACELLE LONGERON 11 Z ANGLE WAS FOUND CRACKED. THE STRINGER F WAS FOUND WORN THROUGH & THE NACELLE SKIN WAS FOUND CRACKED AT STATION 408, LONGERON 11. THE Z ANGLE & STRINGER WILL BE REPLACED WITH NEW PARTS MADE FROM THE SAME MATERIAL & THE SKIN WILLSDR UALA2013020400675Screw · missingFOUR SCREWS MISSING FROMM ONE PANEL ON LEFT ENGINE PYLON INBD SIDE ABOVE ENGINE. INSTALLED MISSING SCREWS ON PANEL OK TO CONTINUE.SDR DALA1303050172Access Panel · damagedNR 2 PYLON AT NR 446BL ACCESS PANEL CUTOUT, CRES RUB STRIPS WERE FOUND DAMAGED AND DOUBLER SKIN CHIPPED. RUB STRIPS REPLACED AND DOUBLER SKIN REPAIRED IAW ERA 510079-14.SDR A6WA2013021804664Skin · dentedRIGHT UPPER CORE COWL SKIN DENT ON O/B SIDE ON POLISHED AREA. REPAIRED DENT PER CMM 71-12-01 REPAIR SRS021.SDR UALA2013013000570Fastener · looseNR 1 ENGINE FOUND FASTENERS LOOSE. REPLACED FASTENERS IAW ECRA 5454-01062. ACCOMPLISHED INSPECTION.SDR 7AHR20130129014Skin · wornRT ENGINE COWL WORN. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2. FABRICATED AND INSTALLED NEW REPAIR DOUBLER ON THE RT ENGINE COWL IAW SRM 51-40-3.SDR SIMA20130128001Skin · dentedDURING MAINTENANCE INSPECTION FOUND A DENT ON THE RIGHT UPPER PYLON EXTERNAL SKIN JUST AFT OF 424GT. THE AIRCRAFT WAS REMOVED FROM SERVICE. CUT OUT DAMAGE, PERFORMED NDT-NO CRACKS, FABRICATED & INSTALLED FILLER FROM AL2024-T3 SAME THICKNESS AS SKIN AND DOUBSDR UALA2013012900518Skin · wornNR 2 PYLON LT SIDE INSIDE PANEL 423AL BETWEEN RIBS 7 AND 8 PILLAR IS WORN. REPLACED NR 2 PYLON LT SIDE PILLAR BETWEEN RIBS 7/8 PER SRM 51-42-11.SDR DALA2014011306966Skin · chippedCHIP OFF SKIN FOUND ON NR 2 NACELLE STRUT LT SKIN PANEL ASSY 311T3450-39 AT NR 446BL ACCESS PANEL. ER/A 510079-14 REV A IS CURRENT. DTA RESTRICTION REMOVED AND LOGPAGE TERMINATED.SDR USAA2013012200008Access Panel · crackedRON VISIT - CRACK ON INBOARD SIDE OF NR 1 PYLON AT ACCESS PANEL 5724 AT NAC STA 254, WL121. REPAIRED INBOARD SIDE OF NR 1 PYLON AT ACCESS PANEL 5724 IAW TR 54-50-07.SDR UALA2013012400439Screw · missingSCREW MISSING AT FWD CORNER OF PANEL 424CR ON OTBD SIDE NR 2 ENGINE PYLON. REPLACED MISSING SCREW.SDR DALA1301956711Skin · puncturedNR 1 ENGINE HAS A PUNCTURE IN LOWER PORTION OF THE NOSE COWL APROX 6 O`CLOCK POSITION REMOVED PANEL AND SENT TO COMPOSITE SHOP REMOVED DAMAGE SANDED AREA BONDED IN CORE APPLIED 350 DEGREES REPAIRS TO INSIDE AND OUTSIDE OF PANEL IAW 51-70-04 INSTALLED PANEL.SDR DALA1301946711Skin · puncturedNR 2 ENGINE HAS A PUNCTURE IN LOWER PORTION OF THE NOSE COWL APPROX 6 O`CLOCK POSITION INSTALLED PERMANENT REPAIR 200 DEGREE WET LAY UP IAW SRM 54-11-01, TABLE 1.SDR ASOA20130121242Skin · chafedACFT WAS FOUND WITH THE NR 1 ENGINE PYLON SKIN PANEL, CHAFED. MX REPAIRED THE PANEL IAW EC5330-02681. WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF ALL WORK.SDR SWAA2013011411401Skin Panel · crackedNR 1 ENGNIE PYLON I/B PANEL 5753L HAS CRACKED AND DELAMINATED SKIN AT UPPER FASTENER ROW. REPAIRED CRACKED AND DELAMINATED SKIN AT UPPER FASTENER ROW OF NR 1 ENGINE PYLON I/B IAW SRM 54-50-70-01-1, SRM 54-50-70-1A-1 AND SRM 51-70-10-2R-0.SDR SWAA1944020112343Skin · crackedLTW MDDR 215893 LEFT APRON CRACKED AT FORWARD END AFT LOWER COWLING ATTACH POINT (REF EA 17-54-03471 R1). CUT OUT DAMAGE AT LT APRON FWD END AFT LOWER COWL ATTACH POINT, C/W HFEC, FABRICATED REPAIR DOUBLER FROM 2024T30.071. R&R SKIN IAW SRM.SDR DALA1303820125Skin · misrepairedHMV2, DURING ACCOMPLISHMENT OF EA 01-487658, REV A MEO1. FOUND NR 1 PYLON NS 150-180 RT SIDE ACCESS DOOR CUT OUT EXISTING REPAIR NOT IAW THE SRM EXISTING REPAIR DOUBLER AT NR 1 PYLON NACELLE STRUT SKIN ASSY RT SIDE ACCESS DOOR CUT OUT EXTERIOR. REMOVED AND NESDR R61A20130104016Panel · separatedCREW REPORTED A PYLON PANEL ON THE NR 2 ENGINE HAD COME OF ON TAKEOFF. CREW LANDED WITHOUT DECLARING AN EMERGENCY OR FURTHER INCIDENT. MAINTENANCE INSPECTED FOR FURTHER DAMAGE AND REPLACED THE PANEL PER BOBMA AMM.SDR SWAA2012122710903Plate · crackedCRACK ON PLATE LOCATED LOWER SURFACE OF WING RIGHT AT LEVEL WBL 198 AND 5.10 OF STRUT AREA MOD. PERFORMED REPAIR ON PLATE PER EA.SDR DALA12017035521Skin · crackedCRACK INDICATED ON INBD SKIN . CRACK APPROX .250" LONG AT FWD TOP AREA OF CUTOUT. ACCOMPLISHED DETAILED INSPECTION OF THE INBD SKIN IAW PRI 488100-14, REV B, PEV ORIG. NO FURTHER DAMAGE TRIMMED OUT DAMAGE IAW STEP 2 OF PRI 488100-14, REV B, REV ORIG HIGH FREQSDR FDEA201212184317Skin · corrodedNR 1 ENG SKIN HAS CORROSION AT SPIGOT HOLE AND LIGHT SURFACE CORROSION ON SKIN LOWER SURFACE. DEFECT MEASURES 6". REMOVED CORROSION, MEASURED REMAINING THICKNESS AND CHECKED LIMITS IAW 51-74-10 AND 54-51-81. NDT OK, PREPPED AND REPROTECTED AREAS IAW SRM 54-5SDR DXTR20121217001Skin · crackedLT PYLON AFT UNDERSIDE SKIN IS CRACKED AT TOW RIVET LOCATIONS. COMPLIED WITH THE REMOVAL AND REPLACEMENT OF THE LT PYLON SKIN, PN 45A34420-049. PN OF THE RIVETS USED FOR THE R & R IS CR3242-4-02 BLIND RIVETS. WORK WAS PERFORMED IAW THE MODEL 400XP, SRM CHAPSDR SWAA2012121710723Rub Strip · crackedCRACK ON RUBSTRIP LOCATED NACELLE STRUT ACCESS PANEL 57700L ENGINE NR 1 (2EA). REPLACED RUBSTRIP LOCATED NACELLE STRUT ACCESS PANEL 57700L ENGINE NR 1 (2EA) IAW B737-300 51-10-02 ITEM 8 51-40-02 AND DWG 65C26720.SDR USAA2012121100001Panel · crackedC1 CHECK - RIGHT PYLON PANEL ABOVE 483AL HAS CRACK APPROX 2.5 INCHES. REPLACED RIGHT PYLON PANEL ABOVE 483AL IAW A319 AMM 54-56-11.SDR UALA2012120407043Skin · crackedNR 1 PYLON RIGHT SKIN CRACK AT NAC STA 225.27. PERFORMED REPAIR IAW ECRA 5430-01941SDR UALA2012120406992Panel · missingDURING ARRIVAL WAC FOUND NR 1 ENGINE OUTBD PANEL 452DL MISSING. IAW EC-RA AREA INSPECTED NO DAMAGED AND INTERIM REPAIR PERFORMED PANEL FABRICATED ECRA 5462-01002 REV A. REMOVED INTERIM REPAIR AND INSTALLED NEW PANEL.SDR UALA2012120406950Skin · tornNR 2 ENGINE OUTBOARD PYLON FAIRING SKIN TORN 45 DEG APPROX 2.5" X 2.5" AT STN 237 BELOW PANEL 447ERX. ACCOMPLISHED INTERIM REPAIR AS PER ECRA 5453-01057. REMOVED DAMAGED AREA AND PERFORMED COMPOSITE REPAIR TO PANEL REF. ECRA 5453-01057 AND SRM 51-70-10.SDR SWAA2012120410215Skin · crackedNR 1 PYLON - INNER & OUTER SKINS CRACKED AT ACCESS PANEL 5727L (O/B AFT CORNER). VERIFIED WITH HFEC. INSPECTED AND STOP DRILLED CRACK PER EA 1-354-1518.SDR WRLA20121117563Skin · crackedCRACK - DURING C04 CHECK, EGAT MECHANIC FOUND CRACKS ON RIGHT FAIRING SKIN OF TAIL PYLON LWR AFT SECTION. REPAIRED PER EGAT EI: W2012A54B-2664,R01. CONDITION CHECK NORMAL AND JOB COMPLETED.SDR FDEA201211164057Skin · corrodedNR 1 PYLON RT FWD SKIN INTERNAL SURFACE AT 433GR DOOR CUT-OUT LOWER SIDE HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 54-50-01, FIG 101 DET III. R & R NR 1 PYLON RT FWD SKIN, IAW DWG 311N5002, SRM 51-40-02. MAJOR REPAIR.SDR FDEA201211164056Skin · corrodedNR 1 PYLON RT AFT SKIN INTERNAL SURFACE PP STA 153 TO 174 HAS SIGNS OF CORROSION BETWEEN THE SKIN AND LOWER CHORD. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 54-50-01, FIG 101, DET III, PYLON. RT AFT INTERNAL STRUT FAIRING SKIN CORROSION REPAIRSDR DALA1256250183Skin · crackedNR 2 PYLON PANEL 442AL ACCESS CUTOUT SKIN AND DOUBLER CRACKED. AREA TRIMMED OFF AND REPAIRED IAW ERA 507546-14, REV ORIG.SDR U2RA201211140001Doubler · corrodedNR 2 PYLON ACCESS PANEL 443LL CUT OUT SKIN DOUBLER HAS CORROSION LENGTH 2.5", WIDTH 1.1", DEPTH .065", ORIGINAL MATERIAL THICKNESS .090", REMAINING MATERIAL THICKNESS .065".SDR SWAA2012111409323Panel · crackedRIGHT WING UPPER SURFACE AFT PYLON PANEL 58710R AFT LANDING, OUTBOARD PLASTIC NUT PLATE STRIP CRACKED. ACCOMPLISHED TIME-LIMITED REPAIR PER EA 1-354-1508.SDR UALA2012102906195Skin · misrepairedNR 1 PYLON RIGHT SIDE SKIN AT NAC STA 228 NOT IAW SRM. NO REPAIR RECORD FOUND. REPAIRED ACP IAW ECRA 5431-01064.SDR UALA2012102906193Skin · misrepairedNR 2 PYLON LEFT SIDE SKIN AT NAC STA 350 NOT IAW SRM. NO REPAIR RECORD FOUND. REPAIRED ACP IAW ECRA 5430-01935.SDR EIAA20121026091Skin · crackedNR 2 STRUT CAP SKIN 2 EA FASTENER HOLES FOUND CRACKED. NR 2 STRUT CAP SKIN CRACKED FASTENER HOLE REPAIRED AS PER ENGINEERING DOCUMENT # TEC-EVR-12-0010-10B.SDR ERAA20120094Skin Panel · crackedRIGHT FINGERNAIL SHROUD SKIN CRACKED ON INBOARD SIDE FORWARD SECTION AT STA XN215.SDR ERAA20120092Skin Panel · chafedRIGHT NACELLE DISHED PANEL HAS SHEET METAL REPAIR CHAFED.
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