JASC 5414
Service difficulty reports · 4,357
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 DALA2025060904394Skin · dentedSHIP 3162 ENGINE N 2, O/B FAN COWL DOOR EXTERNAL SKIN WITH DENTS AT 5 O'CLOCK. CORRECTIVE ACTION: REPLACED #2 ENGINE O/B FAN COWL DOOR I.A.W A319 AMM TASK 71-13- 11-000-040-A AND AMM TASK 71-13-11-400-040-A. (1010947).SDR IXX2025F00010Skin · gouged#1 OB CORE COWL EXTERNAL SKIN IS GOUGED AT AFT LOWER EDGESDR IXXA2025060410Skin · corroded#2 PYLON I/B SIDE, SKIN HAS CORRROSION ON INTERIOR SIDE LOOKING THRU PNL 443JCSDR IXXA20250604009Doubler · damagedTHIS NR FOR DOC. OF MAJOR REPAIR FOR AMES DOC. 47651FAB28. DOUBLER WAS REMOVED ON NR 177268-0400-0133 AND LOST. PART WAS UNAVAILABLE FOR PURCHASE AND A SMAL WAS GRANTEDSDR IXXA20250604008Skin · corrodedCORROSION ON #1 PYLON O/B SIDE, ON INNER SKIN, SEEN THRU FORWARD 2 ACCESS PANEL (1 BEING D-DOOR)SDR CALA2025060305214Skin · cracked(SDR) (SUPPORT TASK) #1 ENG UPPER PYLON BULLNOSE FAIRING (GAP PA NEL) HAS CRACK. SFR REPORTING ONLY REPAIRED WING FIXED LE NOSE SKIN IAW B757-300 SRM 57-41-01. V950 914SDR UIEA2025042400567Skin · scratchedENGINE NO. 2 IN SKIN LEFT SIDE, BETWEEN ACCESS PANEL 446AL AND 447AL WITH THREE SCRATCHES.(<P>SCRATCHES WERE REWORKED, EVALUATED, INSPECTED I.A.W. TRE 6754214 ISSUED DATE 15APR25 AND FAA FORM 81009-9 ISSUED DATE 17APR25. NO FURTHER DEFECTS NOTED.</P>)SDR JR2R20250516542Skin · chafedRH PYLON PANEL 419NR HAS MULTIPLE CHAFES AT SCREW HOLES. REPAIRSDR JR2R20250516451Skin · chafedRH PYLON PANEL 419ML HAS MULTIPLE CHAFES AT SCREW HOLES. REPAIRSDR JR2R20250516449Skin · chafedRH PYLON PANEL 429NR HAS MULTIPLE CHAFES AT SCREW HOLES. REPAIRSDR JR2R20250516457Skin · chafedRH PYLON PANEL, 429ML, MULTIPLE CHAFES AT SCREW HOLES. REPAIRSDR SWAA2025062471502Skin · pulled#2 ENGINE OUTER LIP SKIN FASTENER PULLED THROUGH AT 2:00 POSITION.<[01] #2 ENGINE INLET COWL IS BEING REPLACED WITH A MODIFIED NEW INLET COWL ON CUSTOMER CARD 7111-E-17062-NG (TTG8Q00S71X1);[02] VERIFIED CORRECTIVE ACTIONSDR SWAA2025062473520Skin · out of position#2 ENGINE BARREL SKIN FASTENER AFT OF INLET SKIN NOT FLUSH AT 7:00 POSITION.<[01] #2 ENGINE INLET COWL IS BEING REPLACED WITH A MODIFIED NEW INLET COWL ON CUSTOMER CARD 7111-E-17062-NG (TTG8Q00S71X1);[02] VERIFIED CORRECTIVE ACTIONSDR IPXA2025053137890Skin · corrodedMAJOR REPAIR NR 2 ENGINE PYLON OUTBD INTERNAL SKIN, AFT OF THE MID SPAR FITTING HAS EXFOLIATION CORROSION. DOT 8-001. INSTALLED FITTING AFT HINGE REMOVED ON STEP 4 IAW SRM 51-40-02. AND REQUEST OK TO REINSTALL UPPER SILL ANGLE REMOVED ON STEP 27 FOR FOM. INSTASDR DALA2025060904406Skin · dentedSHIP 3132 FOUND DENT IN RH FAN COWL ON INBOARD SIDE. CORRECTIVE ACTION: COMPLIED WITH ER/A 626366-14. (7227498).SDR VNAA2025050800031Skin · gougedHN00194156 DISCREPANCY: LH PYLON SYSTEM PANEL LANDING HAS GOUGE DAMAGE. CORRECTIVE ACTION: REPAIRED IAW MHIRJ REO 670-53-61-2398 REV-- DATED 10-26-2024SDR DALA2025050803571Fitting · scratchedSHIP 692 A.D.//A.A. SCRATCHES ON OPEN HOLE #8 ON FITTING BTW 7-11 O CLOCK POSITION FROM LH ENG DRAG FTG CLAMP-UP (IN REF: CARD 5720-01100 -04A JOB # 000-0003 STEP 14.C.). CORRECTIVE ACTION: SUMMARY OF NRC 00198: SCRATCHES ON HOLE #8 WERE REPAIRED PER PRI 59060SDR IPXA2025050512703Skin · deformedNR 2 PYLON FWD FAIRING LH AND RH SIDE SUPPORT ANGLES (P/N A54612200200/201)DEFORMED FWD OF RIB J4. DOT# 110-99 JP-110SDR IPXA2025052523691Panel · cracked**SDR FILED OPEN** #1 PYLON LH UNDER SIDE PANEL#413CL CRACK ON LOWER SECTION SEE DOT#58/28 DARRYL FORD 91102506 VERIFIED STOP DRILLSDR CALA2025050104391Access Panel · corroded(SDR)-B757-54-3-0053 ENGINE # L/H NACELLE STRUT 433 FL ACCESS AR EA SHOWS LOWER NUT PLATE RIVETS LOOSE AND NUT PLATE SUPPORTY LIG HT CORROSION. DOT 75-029 HA-75. REF:123778 SDR/SFR REPORTING ONLY REMOVED PANEL 433FL AND SUPPORT PLATE IAW B757-200 SRM 51-40-02-SDR IXXA20250430005Skin · chafed#1 PYLON UNDER PANEL 431AT SKIN HAS CHAFFING MARK AT NAC STA 155 APPROX AS MARKEDSDR IPXA2025061910294Skin · wrinkledNR 1 ENGINE NACELLE FORWARD SKIN PANEL WRINKLED AT RIB J1 ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-93897-REQ1 AND VT-MAE EA 300-5452-27-A3925 REV. - . CAUTION: THE WORK INSTRUCTIONS CONTAINED WITHIN (OR APPROVED BY) THIS EO CONTAIN RII INSPECTION REQUSDR IPXA2025061810362Skin · wrinkledNUMBER 2 ENGINE NACELLE FORWARD SKIN PANEL WRINKLED THE CURRENT CONFIGURATION OF AIRCRAFT AND PYLON: ENGINE REMOVED, DAMAGED SKIN REMOVED,DAMAGED LH AND RH SIDE SUPPORT ANGLES REMOVED (ITEM 170 ON SRM 54-52-11 FIG 1)ACCOMPLISHED STEP 5 OF EA: 300-5452-27-A3926SDR IPXA2025051615335Access Panel · wornPANEL RACK ACCESS PANEL 435BR BRACKET HAVE EXESSIVE WEAR DOT 07-036. INSTALLED SEAL AND RETAINER AT NEW CHORD I.A.W A300-600 SRM 51-40-21.SDR IPXA2025050510362Skin · wrinkled#2 ENGINE NACELLE FORWARD SKIN PANEL WRINKLED VERIFIED ACCOMPLISHMENT OF STEP 17 PER EA: 300-5452-27-A3926 PRELIMINARY 3.<BR>VALIDATED DVI INSPECTION ON PYLON PRIMARY STRUCTURE, NO DAMAGE FOUND.SDR IPXA2025050510294Skin · wrinkled#1 ENGINE NACELLE FORWARD SKIN PANEL WRINKLED AT RIB J1 VERIFIED ACCOMPLISHMENT OF EA #300-5452-27-A3925 PRELIMINARY 3 STEPS 20, 21 AND 22<BR>NO DISCREPANCIES NOTED AT THIS TIME.SDR JR2R20250424270Panel · chafedRIGHT HAND PYLON PANEL, 429NR, CHAFED IN MULTIPLE PLACES AREAS OUT OF LIMITS.SDR JR2R20250423276Panel · chafedLEFT HAND PYLON PANEL, 419NR, CHAFED IN MULTIPLE PLACES AREAS OUT OF LIMITS.SDR JR2R20250423281Panel · chafedLEFT HAND PYLON PANEL, 419ML, CHAFED IN MULTIPLE PLACES AREAS OUT OF LIMITS.SDR EE4Y2025042222202Skin · damagedDURING THE ACCOMPLISHMENT OF SB190-57-0056 WING LOWER SKIN REINFORCEMENTS, THE PYLON WERE REMOVED FOR ACCESS. DURING THE INSPECTION BEFORE THE PYLON INSTALLATION, THE CUSTOMER FOUND THE RH PYLON SUPPORT LUGS (INBOARD AND OUTBOARD) WITH BUSHINGS FRETTING. AFTERSDR JR2R20250422284Panel · chafedRIGHT HAND PYLON PANEL, 429ML, CHAFED IN MULTIPLE PLACES AREAS OUT OF LIMITS.SDR IPXA2025050634634Skin · corrodedPYLON #2 INTERNAL AREA BETWEEN ACCESS PANEL 443CR AND 443BR HAVE CORROSION DOT 07-008 PERFORMED TRIM OUT CORROSION DAMAGE PER EA E.A# 757-5450-27-A3911 STEP 2 A, B, C, D. AND SRM 51-10-02. WORK ACCOMPLISHED PER UPS EO: EO-93643-REQ 1 AND VTMAE EA 757-5450-27-ASDR IPXA2025050324761Doubler · corrodedNR 1 ENG I/B PYLON PPS. 1.8317 AFT LOWER INSIDE PANEL 433HR HAS CORROSION. BLUE DOT TRIMMED OUT CORROSION DAMAGE FOR ACCOMPLISH STEP 2 OF E.A.# 757-5450-27-A3910 PRELIMINARY 1. COMPLETED THE REPAIR FOR ACCOMPLISH STEP 27 OF E.A.# 757-5450-27-A3910 PRELIMINARY SDR UIEA2025032500387Skin · worn#3 RH CORE COWL UPPER AFT AREA FND WORN OUT(<P>WORN OUT AREA REPAIRED AS PER SRM 54-41-01-2R-5 REPAIR 5 FIG 202 DETAIL III. NO FURTHER DEFECTS NOTED</P>)SDR JR2R20250415912Panel · chafedLH PYLON PANEL 419UR HAS CHAFE MARK ON INNER SURFACESDR DALA2025041402913Skin · crackedTHE #1 PYLON O/B ACCESS DOOR 432AL CUTOUT UPPER CRACK. A 2 INCH LONG CRACK WAS IDENTIFIED ON THE SKIN OF #1 PYLON. THE AFFECTED AREA HAS BEEN REMOVED AND REPAIRED PER PRI: 625594-14 REV 0. COMPARED AND COMPLIED WITH ER/A625594-14 REV ORIGINAL. NO DEVIATION. ASSDR SWIA2025082500411Skin · damagedNR 1 ENGINE FAN COWL BOTTOM. LOWER SURFACE 1.0" FORWARD OF PREVIOUS REPAIR 3.2"5 SPAN WISE X 2.5" X .065" DEEP. NO CREASES OR EVIDENCE OF CRACKS. W/D IS 38.46. SRM 54-14-00 SEE AEML 941117. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKEDSDR JR2R20250409915Panel · chafedRIGHT HAND PYLON PANEL, 429NR, INNER SURFACE, HAD MULTPLE AREAS OF CHAFING THAT ARE OUT OF LIMITS.SDR JR2R20250408914Panel · chafedLEFT HAND PYLON PANEL, 419NR, INNER SURFACE HAS MULTIPLE CHAFES OUT OF LIMITS.SDR 2025FA0000248Skin · unknownINTERIM REPAIR - OUTER SKIN, DOUBLERS,& FIRESHIELD, LH CORE COWL (PE4000), NAC STA 177.5 -180, P/N 314T4211-13, 314T4211-15, 314T3210-13, 314T3210-67.SDR 2025FA0000243Skin · unknownREPAIR / EVALUATION - 1ENGINE INLET COWL INNER SKIN EXISTING REPAIRS.SDR 2025FA0000237Skin · damagedREPAIR - ENG #1 LH CORE COWL INNER SKIN OUTER SURFACE, AFT OF THE PRECOOLER VENT. PANEL 314T3210.SDR VNAA20250525017Skin · dentedSEVERAL DENTS ON LOWER FAN COWL BTW 5 O'CLOCK TO 8 O'CLOCK POSITION AT LEFT ENGINE. DENT ON LOWER FAN COWL BTW 5 O´CLOCK AT LH ENGINE WAS REPAIRED PER REO 670-54-14-1314 REV. --SDR CALA2025040403540Panel · missingAIRCRAFT (EXTERNAL) INSPECT (ZONES 100, 200, 300, 500, 600,700,800). {B767-06-3-0217} - ON ARRIVAL, PANEL 436AR FOUND MISSING FROM RIGHT ENGINE PYLON REF IPC 54-53-01-17, PN 311T3065-160 IN TRANSIT FROM LHR HANGAR PANEL 436AR REPLACED, REQUEST EXT TO APPLY COMSDR IPXA2025042588024Access Panel · gougedFAULT - Z400, STR, #2 ENG STRUT ACCESS THROUGH PNL 443CR LOWER CORD HAS A GOUGE. DOT 95-23.ACCOMPLISHED STEP 1 OF EA # 757-5450-27-A3881 PRELIMINARY 1. REMOVED THE GOUGE DAMAGE BY BLENDING. MAINTAINED 1 INCH RADIUS AND 125 RA SMOOTHNESS. T90482.ACCOMPLISHED STSDR DALA2025033102342Skin · crackedFOUND RH PYLON I/B SKIN CRACK ON THE TOP OF PANEL 442AL. RH PYLON I/B SKIN ON TOP OF PANEL 442AL AT NAC STA 158-192 CRACK AREA (CRACK LENGTH 2") REPAIRED PER PRI 625198-14 REV O. THE PRI 625198-14 REV O COMPARED AND COMPLIED WITH ER/A 625198-14 REV ORIGINAL. NSDR IPXA2025041298764Skin · corroded# 2 PYLON OUTBD SIDE BETWEEN ACCESS PANELS SHOWS CORROSIONN AT INSIDE SKIN AREA. (RED DOT OUTSIDE). FABRICATED EXTERNAL REPAIR DOUBLER FOR ACCOMPLISHED STEP 19 OF EA # 757-5450-27-A3873 PRELIMINARY 3. VERIFIED FABRICATED EXTERNAL REPAIR DOUBLER FOR ACCOMPLISHSDR HNAA2025051200317Skin · chafedF0361458 RH PYLON EXTERNAL SKIN CHAFED UNDER ACCESS PANEL 424DB. REMOVED AND REPLACED DOUBLER ON RH PYLON UNDER ACCESS PANEL 424DB. IAW EMB 145 SRM 51-40-02SDR DXTA2025032602797Skin · dentedFOUND A SMALL DENT ON THE LH LOWER PYLON TRAILING EDGE SKIN. THE DENTS DEPTH IS MEASURED AT -.031. MAX ALLOWABLE LIMIT IS -.100.SDR SWAA2025032508545Skin · crackedCRACK FOUND ON RH ENGINE NACELLE SKIN IB SIDE NAC STA 303.8; NWL 117<[01] OK TO CONTINUE PER EA 25-154-00736. REF TTG8Q00ZESNM
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