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 QXEA9700862Skin · damagedPDX - IMPACT DAMAGE AFT OF REFUEL DOOR ON OUTBOARD SIDE OF RIGHT NACELLE. REPAIRED DAMAGE IAW DEHAVILLAND SRM 51-70-00 PAGE 401 REPAIR 4.SDR P5CA9701577Panel · delaminatedDELAMINATION ON PANEL NR 474AR ON NR 3 PYLON. REPAIRED DELAMINATION PER BAC SRM 51-40-06.SDR P5CA9701576Panel · delaminatedDELAMINATION ON PANEL NR 484AR ON NR 4 PYLON. REPAIRED DELAMINATION PER BAC SRM 51-40-06.SDR P5CA9701575Panel · puncturedPUNCTURE ON PANEL NR 474AL ON NR 3 PYLON. POTTED CORE AND APPLIED A DOUBLER PER BAC SRM 51-40-06.SDR P5CA9701574Panel · puncturedPUNCTURE ON PANEL NR 484 ON NR 4 PYLON. REPAIRED PUNCTURE PER BAC SRM 51-40-06.SDR P5CA9701573Panel · puncturedTWO PUNCTURES ON NR 3 PYLON PANEL NR 474AR. POTTED CORE AND APPLIED DOUBLER PER BAC SRM 51-40-06.SDR P5CA9701564Panel · delaminatedDELAMINATED PANEL NR 464AR ON NR 2 PYLON. POTTED AND SEALED DAMAGED AREA PER BAC SRM 51-40-06.SDR P5CA9701561Panel · delaminationDELAMINATION OF INNER SKIN ON ACCESS PANEL NR 462AL ON NR 2 PYLON. REPLACED INNER SKIN AND PANEL CORE PER BAC SRM 51-40-06.SDR 97UAL900705Skin · crackedNR 1 ENGINE NACELLE STRUT LEFT HAND SIDE SKIN, (P/N 311N345017), WAS FOUND WITH A CRACK EMANATING FROM THE FORWARD MOST ACCESS HOLE, NAC STA 112.92 WL 137, AT APPROXIMATELY THE ONE O'CLOCK POSITION. CRACK LENGTH IS APPROXIMATELY 1.625 INCHES. UAL FEELS THIS SDR SRAA970994Fireshield · delaminatedDURING POST FLIGHT WALKAROUND, NR 2 AND NR 3 PYLON'S HAVE SKIN DELAMINATED, APPROX 12 BY 3. TRIMMED OUT THE DELAM PORTION OF FIRESHIELDS AND INSTALLED NEW FIRESHIELD PIECES AS PER SRM 54-30-03.SDR AU971383Skin · cracked(AUS) NO1 AND NO4 ENGINE NACELLE STRUT OUTBOARD SKIN AND DOUBLER CRACKED BEYOND LIMITS.SDR QXEA9700832Skin · crackedPDX - LEFT STUBWING LOWER SKIN AFT EDGE HAS CRACK FROM A RIVET JUST OUTBOARD OF A PREVIOUS REPAIR PATCH. REPAIRED IAW EA 4-54-17.SDR USAA970266Skin · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1.2 INCH CRACK NR 1 PYLON INBOARD SKIN AT ACCESS PANEL 5724L. INSTALLED DOUBLER PER REPAIR DOCUMENT TRM 54-40-04L. (M)SDR P5CA9701438Panel Door · delaminatedNR 3 PYLON 473 CL PANEL DOOR DELAMINATED. REPAIRED PER BOEING SRM 51-40-06.SDR ABXA9701447Skin · gappedA GAP WAS DISCOVERED BETWEEN NR 2 PYLON APRON AND COWLING AT FWD LEADING EDGE. REPAIRED IAW ABX REA D854-20688.SDR CA970904037Gusset · chafed(CAN) IN COMPLYING WITH WILDENESS TIRE MODIFICATION SA00185LA, IT WAS FOUND THAT ON RETRACTION TESTS THE TIRE RUBBED ON THE WHEELWELL GUSSET THAT EXTENDS AFT, LOWER INNER/OUTBOARD WALL ACROSS BOX CHANNEL NEAR NACELLE TANK LINER. WILDERNESS TIRE MODIFICATION RSDR ABXA9701408Skin · excessive gapDURING PREFLIGHT, FOUND EXCESSIVE GAP AT LEADING EDGE OF NR 3 PYLON. INSTALLED SEAL AND STAINLESS STEEL STRIP IAW ABX REA D854-20655.SDR CKSA97521Skin · crackedDURING ROUTINE C-4 CHECK INSPECTION, FOUND LT WING NR 2 PYLON AFT SIDE STA YOP320 TO YOP420 CRACKED 8. REPAIRED AFFECTED AREA AS PER SRM 54-2-1. NON-ROUTINE TASK CARD NUMBER 098726.SDR AALA971359S Duct Skin · corrodedTUL - SKIN BULGING AND SEVERAL RIVET HEADS POPPED IN 1.50 INCH BY 8 INCH AREA OF LOWER S-DUCT SKIN, LEFT SIDE FORWARD OF VORTEX GENERATORS. REMOVED CORROSION AND INSTALLED DOUBLER REPAIR PER SRM 54-10-3, PAGE 41B. TST: 66,905 HOURS. CYCLES, 43,822. (X)SDR P5CA9701345Skin · crackedNR 3 PYLON SKIN IS CRACKED ON INBD SIDE UNDER SKIN DOUBLER AT NAC ST 180 NAC WL 140.2-142.2, REPAIRED IAW SB 54-2034. NON ROUTINE CARD S/N 6144.SDR P5CA9701328Skin · crackedNR 1 PYLON OUTBD SKIN CRACKED UNDER DOUBLER AT NAC ST 180 NAC WL 140.2. STOP HOLE DRILLED IAW BOEING SRM 51-10-01 SKIN REPAIRED IAW SB 54-2034 FIG 5.SDR CKSA97342Skin · crackedDURING C1-12 CHECK INSPECTION, FOUND NR 1 PYLON I/B SKIN APPEARS CRACKED PS 180 LWR. REPAIRED NR 1 PYLON I/B SKIN PS 180 LWR IAW B747 SB 54-2034, 15-5PH (H-1100). C-CHECK WORK CARD NUMBER 7CI4509. NON-ROUTINE TASK CARD NUMBER 107973.SDR CKSA97341Skin · crackedDURING C1-12 CHECK INSPECTION, FOUND NR 3 PYLON NS 175 I/B SKIN CRACKED. REPAIRED NR 3 PYLON NS 175 I/B SKIN IAW B747 SB 54-2034, WHICH ALSO INCORPORATES PREVIOUS REPAIR IAW SRM 54-30-03 FIG 17, 15-5PH (H-1100). C-CHECK WORK CARD NUMBER 7CI4709. NON-ROUTINESDR CKSA97340Skin · crackedDURING C1-12 CHECK INSPECTION, FOUND NR 4 PYLON I/B EXT SKIN CRACKED AND FASTNERS LOOSE. REPAIRED NR 4 PYLON I/B EXT SKIN IAW B747 SB 54-2034, (155PH-H 1100). C-CHECK WORK CARD NUMBER 7CI4809. NON-ROUTINE TASK CARD NUMBER 107880.SDR CKSA97336Skin · damagedDURING C1-12 CHECK INSPECTION, FOUND NR 1 PYLON I/B LWR INNER SKIN DAMAGED FWD OF AFT MOUNT. REMOVED DAMAGED SKIN AND REPAIRED IAW SRM 54-30-03 FIG 36, (2024-T3). C-CHECK WORK CARD NUMBER 7CI4509. NON-ROUTINE TASK CARD NUMBER 107977.SDR CKSA97335Skin · damagedDURING C1-12 CHECK INSPECTION, FOUND NR 1 PYLON O/B LWR SKIN AND AFT MOUNT PNL DAMAGED. REPAIRED CRACKED AREA IAW B747 SRM 54-30-03 FIG 35, (2024-T3). C-CHECK WORK CARD NUMBER 7CI4506. NON-ROUTINE TASK CARD NUMBER 107975.SDR CKSA97334Skin · crackedDURING C1-12 CHECK INSPECTION, FOUND NR 1 PYLON I/B SKIN CRACKED NEAR AFT MOUNT PS221. REPAIRED CRACKED AREA IAW B747 SRM 54-30-03 FIG 35, (2024-T3). C-CHECK WORK CARD NUMBER 7CI4506. NON-ROUTINE TASK CARD NUMBER 107974.SDR CKSA97326Skin · crackedDURING C1-12 CHECK INSPECTION, FOUND NR 3 PYLON SKIN CRACKED AT PNL 473EL CUTOUT. REPAIRED CRACKED SKIN IAW B747 SRM 54-30-03, (2024-T3). C CHECK WORK CARD NUMBER 7CI4709. NON-ROUTINE TASK CARD NUMBER 107894.SDR CKSA97325Skin · crackedDURING C1-12 CHECK INSPECTION, FOUND NR 3 PYLON SKIN CRACKED AT PNL 473GL CUTOUT. REPAIRED CRACK IN SKIN IAW B747 SRM 54-30-03, (2024-T3). C CHECK WORK CARD NUMBER 7CI4709. NON-ROUTINE TASK CARD NUMBER 107893.SDR 97FDEA00405Skin · gougedB-CK B36 LT NR 3 PYLON, DIAGONAL BRACE BOX SECTION. TITANIUM SKIN HAS SEVERAL DEEP GOUGES. 9 EA FROM HUCK FASTENERS OF INBOARD THRUST REVERSER. NDT MEASURED DEPTH OF ACH GOUGE 9 PLCS, DEPTH RANGED FROM .018 IN DEEP TO .060 INCH DEEP INTO PYLON SKIN. *S/D* SDR P5CA9701329Skin · crackedLEVEL 2 CORROSION, NR 1 PYLON INBD SKIN UNDER DOUBLER HAS CRACK AND CORROSION AT NAC STA 180 WATER LINE 140.2. REPAIRED IAW SB 747-54-2034 FIG 5.SDR CALA9701090Skin · crackedINSPECTION FOUND A 2 INCH CRACK IN LEFT ENGINE PYLON SKIN AT PANEL NR 5724. REPAIRED IAW ECRA 5430-01204.SDR CKSA97434Skin · crackedDURING ROUTINE C-3 CHECK INSPECTION, FOUND NR 4 PYLON LT SIDE UPPER PART YOP280.0 PANEL SKIN HAS A CRACK (.5 INCH). REPAIRED AFFECTED AREA PER SRM 54-2-0. NON-ROUTINE TASK CARD NUMBER 108834.SDR P5CA9701338Skin · corrodedLEVEL 1 CORROSION, NR 2 PYLON CAP SKIN IS CORRODED AT NAC ST 221-222 LWBL 463. REMOVED CORROSION IAW BOEING SRM 51-10-01 AND IS WITHIN LIMITS PER BOEING SRM 54-10-01 NON ROUTINE CARD S/N 6274.SDR P5CA9701337Skin · crackedNR 2 PYLON SKIN CRACKED UNDER SKIN DOUBLER. REPAIRED CARRIED OUT IAW SB 54-2034. NON ROUTINE CARD S/N 6270.SDR P5CA9701240Skin · corrodedLEVEL 1 CORROSION NR 2 PYLON CAP SKIN AT NAC ST 221-222 LWBL 463. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02. AD: NR 94-15-18.SDR P5CA9701239Skin · corrodedLEVEL 1 CORROSION NR 1 PYLON CAP SKIN UNDER SADDLE FAIRING HAS LIGHT SURFACE AT FAIRING ATTACHMENT FASTENER HOLES AND REQUIRES PAINT TOUCH UP. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02. AD: NR 94-15-18.SDR P5CA9701204Skin · crackedCRACKS FOUND AT NR 4 DOGHOUSE, AFT R/S SKIN. REPAIRED PER BOEING SRM 54-32-03.SDR P5CA9701336Skin · corrodedLEVEL 1 CORROSION, NR 3 PYLON CAP SKIN IS CORRODED JUST FORWARD OF UPPER LINK FORWARD FITTING NAC ST 221-217 RWBL 473-467. REMOVED CORROSION IAW BOEING SRM 51-10-01 AND REPROTECTED CUT OUT SRM 51-24-11. NON ROUTINE CARD S/N 6143.SDR P5CA9701238Skin · corrodedLEVEL 1 CORROSION NR 3 PYLON SKIN JUST FWD OF UPPER LINK FWD FITTING (PYLON CAP SKIN) NAC ST 221-217. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02. SB/EO: NR 747-54-2159.SDR P5CA9701353Skin · crackedLEVEL 2 CORROSION, NR 1 PYLON INBD SIDE SKIN IS CRACKED AND CORRODED UNDER SKIN DOUBLER AT NAC ST 186-174, NAC WL 140.2. REPAIRED CARRIED OUT IAW SB 747-54-2034. NON ROUTINE CARD S/N 5999.SDR P5CA9701352Skin · crackedLEVEL 2 CORROSION, NR 4 PYLON OUTBD SIDE SKIN IS CRACKED AND CORRODED AT NAC ST 186-174, NAC WL 142.2 - 140.2. REPAIRED CARRIED OUT PER SB 747-54-2034. NON ROUTINE CARD S/N 6000.SDR COMA9710310Skin · crackedWHILE AIRCRAFT WAS IN THE HANGAR FOR SCHEDULED MAINTENANCE, MECHANIC NOTICED A CRACK IN THE LEFT NACELLE OUTBOARD AFT SKIN, JUST BELOW THE ROLLER SUPPORT FOR THE OUTBOARD FLAP. THE SKIN WAS REPAIRED PER AERODESIGN REPORT NR 2331-1 REV IR, 6-12-97.SDR USAA970238Skin · crackedCLT - DURING Q-1 CHECK VISUAL, INSPECTION FOUND A 1 INCH CRACK IN THE UPPER FORWARD AND LOWER AFT CORNERS AT ACCESS PANEL NR 572LL OPENING ON SKIN. TRIMMED OUT DAMAGE AND INSTALLED DOUBLER PER REPAIR DOCUMENT 54-50-04C AND EA 60072. (M)SDR USAA970236Skin · crackCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT INNER AND OUTER SKINS AT ACCESS PANEL NR 5824R OPENING. INSTALLED DOUBLERS PER TYPICAL REPAIR 54-50-04C. (M)SDR EIAA970175Skin · crackedSYZ - LOG PAGE: E04744 - ON W.A.C., FOUND CRACK IN NR 1 ENGINE PYLON OUTBOARD SKIN AT NACELLE STA 180, 2.6250 INCHES LONG. REPAIR CARRIED OUT PER B747 SRM 54-30-03 FIG 17A. (X)SDR DL72S971098Skin · crackedA .5 INCH CRACK EMPENNAGE SKIN LT SIDE FWD OF SADDLE PLATE 9501. REPAIRED PER M/M 54-30-0 FIG 801, TIME LIMITED REPAIR.SDR ABXA9701041Skin · crackedDURING C/P3 CHECK, FOUND LOOSE FASTENERS IN REMOVABLE PLANK ON NR 1 PYLON. REPAIRED IAW ABX EA SB 54-04020MR.SDR P5CA9701013Panel · delaminatedNR 3 PYLON ACCESS PANEL 472BL IS DEBONDED. REBONDED IAW BOEING SRM 51-40-06 REF TO CWS NR 834288.SDR P5CA9700827Skin · delaminatedNR 3 PYLON LWR SPAR SKIRT FAIRINGS I/B AND O/B HAVE LOOSE FASTENERS DEBONDED INNER SKIN AND INTERLINKING RIBS WITH LOOSE FAST FROM AFT MOUNT TO NAC STA 260. REPAIRED IAW BOEING SRM 54-30-03, REF NR 854328.
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