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 03FDEA01111Skin · wornNR 2 ENGINE LT FWD COWL FWD FUSELAGE MATING SURFACE WORN THROUGH AT BS 1350. FOUND AREA ON 1350 RING CHORD TO HAVE 100 PERCENT MATERIAL LOSS AND CRACKED OUT OF LIMITS. REMOVED 1350 RING CHORD. DRILLED UP AND INSTALLED NEW 1350 CHORD IAW SRM 51-30-2, 51-30SDR AWXA200300824Skin · corrodedDURING C-04 CHECK CORROSION WAS FOUND ON AFT LOWER INNER SKIN OF THE NR 1 PYLON AFT FIXED FAIRING. MAINTENANCE CUT OUT DAMAGED AREA OF NR 1 PYLON AFT FIXED FAIRING SKIN BETWEEN RIBS 11-16A; FABRICATED A NEW REPLACEMENT SECTION OF SKIN; INSTALLED REPAIR PART ISDR QXEA200300801Panel · damagedPDX - NR 2 NACELLE TOP AFT PANEL 424AT HAS A SCREW HOLE WITH NO COUNTER SINK REMAINING ON OUTBOARD SIDE AT FLAP TRACK CUTOUT. REPAIRED IAW RD 8/4-54-133, PAGE 4, PARAGRAPH 4 AND HORIZON AIR EA 6-54-258.SDR 03FDEA00991Panel · crackedNR 1 ENGINE PYLON PRE-COOLER PANEL, CRACK REPAIR. FACT 27JUN03 03:15 BFM R COMPLIED WITH E.A. 6-5452-70948 NACELLES/PYLONS. NR 1 ENGINE PYLON PRE-COOLER PANEL PANEL CRACK REPAIR.SDR AWXA200300742Skin · corrodedMCN - MAJOR REPAIR - DURING B-02 CHECK PITTING CORROSION WAS FOUND ON INBOARD SIDE OF RT PYLON AFT FIXED FAIRING. MAINTENANCE REMOVED DAMAGED AREA SKIN ON INBOARD SIDE OF RT PYLON AFT FIXED FAIRING; FABRICATED A NEW REPLACEMENT SKIN PANEL PER DWG S4D54510054;SDR AWXA200300741Skin · corrodedMCN - MAJOR REPAIR - DURING B-02 CHECK PITTING CORROSION WAS FOUND ON INBOARD SIDE OF LT PYLON AFT FIXED FAIRING. MAINTENANCE REMOVED DAMAGED AREA SKIN ON INBOARD SIDE OF LT PYLON AFT FIXED FAIRING; FABRICATED A NEW REPLACEMENT SKIN PANEL PER DWG S4D54510054;SDR 03FDEA00947Skin · delaminatedNR 1 ENGINE RT TRANSLATING COWL IS DELAMINATED, FWD UPPER CORNER AT THE 2 O'CLOCK POSITION OF THE INNER BARREL 2 X 4 INCHES. REPAIRED BY T/R REPLACEMENT PER EA 6-7830-66985 WORK DOCUMENTED ON M-1805, S00029.SDR C2XA03SH184Skin · gougedDURING C-CHECK NUMBER ONE ENGINE LOWER COWLING SKIN WAS FOUND GOUGED BY FRAME 7. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED AREA IAW EMB 145 SRM 54-10-01. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR CALA0300311Skin · crackedINSPECTION FOUND A .25 INCH CRACK ON LIP OF HOLE CUT ON O/B SIDE OF ACCESS PANEL 5727L OF NR 1 PYLON. REPAIRED ACCESS PANEL IAW ECRA 5430-01230.SDR ABXA030194Panel · gougedDURING INSPECTION, TWO GOUGES WERE FOUND ON NR 1 ENGINE STRUT RIGHT SKIN PANEL NEAR AN ACCESS DOOR CUTOUT. MAXIMUM DEPTH OF BLEND OUT REQUIRED TO COMPLETELY REMOVE DAMAGE WAS 0.035 INCH. REPAIRED AREA IAW REA B654-46243MR.SDR UIEA200300031Skin · damagedDURING C-CHECK SERVICE IN SIAEC, NR 2 PYLON EXTERNAL SKIN FOUND WRINKLED AT INBOARD SIDE AREA OF PYLON VALVE FROM STATION 286 TO STATION 300, BETWEEN THE MID SPAR AND NR 5 STIFFENER. NDT AND CONDUCTIVITY CHECKS WERE ACCOMPLISHED AS PER CARDS A00043 AND A00044SDR CALA0300258Skin · crackedINSPECTION FOUND A .5 INCH CRACK IN NR 1 I/B PYLON SKIN AT FORWARD UPPER CORNER OF PANEL 5724. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5430-01204.SDR CALA0300257Skin · crackedINSPECTION FOUND A .5 INCH CRACK IN NR 1 ENGINE PYLON UPPER SURFACE PANEL 5727L CUTOUT. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5430-01230.SDR 0300956632Skin · crackedDURING H-CHECK FOUND CRACK IN NR 3 PYLON INBOARD SKIN AT CUTOUT OF SLOT SEAL AT NACELLE STATION 178. REPAIRED PER EA 66-164978.SDR QXEA0300538Skin · crackedPDX - LEFT HAND NACELLE LOWER COWL AFT CONE SUPPORT APPEARS TO HAVE CRACKS. REPAIRED IAW RD 8/4-71-016.SDR UPS03440617Skin · wornINSPECTION TYPE: P/S, NR 4 PYLON I/B SIDE HAS HOLE WORN IN PREVIOUS REPAIR. ***OPEN***SDR A6WA200360016Panel · chafedNR 4 PYLON PANEL 481 AT LOWER FORWARD RIGHT ATTACH HOLE CHAFED BADLY FROM LOOSE AND VIBRATING SCREW. HOLE WORN EXCESSIVELY. REPAIRED PANEL IAW BARA/AVR/6361/03-D. (M)SDR AWXA200300488Panel · crackedMCN - MAJOR REPAIR - DURING C-03 CHECK A 1.25 INCH CRACK WAS FOUND ON LT PYLON INBOARD SIDE AT FORWARD UPPER CORNER OF PANEL 414CR ATTACH POINT, STA 537. MAINTENANCE CUT OUT DAMAGED SECTION OF EXTRUSION PROFILE AT PYLON STA 537; FABRICATED A FILLER AND REPAIRSDR 03FDEA00529Skin · gougedNR 3 ENGINE UPPER NACELLE EXTERIOR SKIN HAS GOUGE NEXT TO NR 1 LATCH. REPAIRED NR 3 ENGINE NACELLE IAW BOEING 727-200 SRM 54-30-03.SDR USAA030042Skin · crackedFOUND SKIN CRACKED 1 INCH LONG, LEFT ENGINE PYLON AT ACCESS PANEL S724L CUTOUT. INSTALLED DOUBLER PER TYPICAL REPAIR 54-50-07. (M)SDR 03FDEA00496Skin · damagedNR 2 ENGINE RIGHT AFT NACELLE SKIN LOWER AFT CORNER BENT AND CHAFED. *S/D* REPAIRED BENT CORNER AND CHAFED EDGE IAW BOEING 727-200 SRM 54-10-03.SDR 03FDEA00495Skin · crackedNR 2 ENGINE LEFT AFT NACELLE LOWER FORWARD CORNER SKIN HAS A CRACK AND CHAFING. REPAIRED NR 2 ENGINE COWLING FWD LOWER CORNER IAW BOEING 727-200 SRM 54-10-03.SDR 03FDEA00494Skin · chafedNR 2 ENGINE FORWARD COWLING LOWER AFT CORNER INTERIOR SKIN CHAFED. *S/D* REPAIRED SKIN IAW BOEING 727-200 SRM 54-30-01.SDR 03FDEA00483Skin · damagedNR 1 ENGINE UPPER NACELLE FORWARD UPPER CORNER SKIN SEPARATED. REMOVED AND REPLACED REPAIR DOUBLER IAW BOEING 727 SRM 51-30-2.SDR 03FDEA00480Skin · dentedNR 3 ENGINE UPPER NACELLE EXTERIOR SKIN HAS 1 DENT APPROXIMATELY 24 INCHES FROM AFT EDGE. INSTALLED FLUSH REPAIR IAW BOEING 727 SRM 54-30-2.SDR 03FDEA00479Skin · damagedNR 3 ENGINE UPPER COWLING LOWER EDGE SKIN SEPARATED, BENT AND CHAFED AT NR 3 FRAME.SDR 03FDEA00476Skin · chafedNR 3 ENGINE LOWER COWLING UPPER FRAME NEXT TO OIL TANK ACCESS DOOR HINGE HAS CHAFING CONDITION.SDR 03FDEA00475Skin · dentedNR 3 ENGINE LOWER COWLING EXTERIOR SKIN FORWARD MID AND AFT HAS 7 DENTS.SDR 03FDEA00487Skin · damagedNR 1 ENGINE UPPER NACELLE EXTERIOR SKIN HAS A NICK AT BOTTOM OF AFT PIN LATCH CUTOUT.SDR 03FDEA00465Skin · gougedNR 3 ENGINE UPPER NACELLE EXTERIOR SKIN GOUGED NEXT TO NR 1 LATCH. *S/D* REPAIRED NR 3 ENGINE NACELLE IAW BOEING 727-200 SRM 54-30-03.SDR 03FDEA00464Skin · crackedNR 3 ENGINE NACELLE INBOARD SKIN CHAFED AND CRACKED 1 INCH LONG. *S/D* REMOVED AND REPLACED DAMAGED LONGERON IAW BOEING 727-200 51-30-02.SDR EIA2003064Skin · crackedNR 3 PYLON INBOARD SIDE SKIN CRACKED TO UPWARD ABOVE PLATE 473CL. PERMANENT REPAIR INSTALLED PER ECRA 480-54-158-1 PER 8110-3 FROM BOEING.SDR EIA2003058Skin · corrodedFRETTING CORROSION AT FWD EDGE OF NR 1 PYLON O/B SAILPLANE DOOR CUTOUT. TRIMMED DAMAGE, NDT AREA, FABRICATED AND INSTALLED REPAIR PER ECRA 486-54-017-2.SDR P5CA0300825Access Panel · crackedNR 3 PYLON STRUT ACCESS PANEL 453FL CUTOUT CRACKED. REPAIRED PER SRM 54-34-03 FIG 2.3.SDR P5CA0300826Access Panel · crackedNR 3 PYLON ACCESS PANEL CUTOUT LWR AFT CORNER CRACKED. REPAIRED PER SRM 54-34-03 FIG 23.SDR CGO2003F00007Panel · crackedFOUND CRACK/ DELAMINATED AREA IN PRODUCTION LAP JOINT BETWEEN MOLDED HALVES OF CLOSEOUT PANEL AT APPROX 6 OCLOCK POSITION BELOW SPINNER CUT-OUT AND ABOVE OIL COOLER EXIT DUCT. AREA USUALLY DIRTY/GREASY, HAVE TO CLEAN THOROUGHLY AND FLEX PARTS TO INSPECT ADEQUSDR UPS03440612Skin · crackedINSPECTION TYPE: C, NR 3 PYLON EXTERIOR SURFACE SKIN NAC STA 218.9 LHS 1EA RIVET HOLE UPPER AND LOWER EDGE SUSPECT CRACKS ARE FOUND AS MARKED. NR 3 PYLN EXTERIOR SKIN REPAIRED AT I/B SIDE AS PER RS R54-50-35005 AND UPS EO B747-5410-18686-A DVI THE REPAIRESDR UPS03440500Skin · crackedNR 3 PYLON ACCESS PANEL 473EL CUTOUT UPPER EDGE RIVET HOLE LOWER EDGE SUSPECT CRACK REVEALED AS MARKED. SKIN REPAIRED PER SRM 54-30-03 FIG 17B.SDR QXEA0300453Skin · crackedNR 1 NACELLE OUTBOARD NACELLE DOOR 412 BL HAS CRACKS AROUND TEN SPOT WELDS ON AFT EDGE OF DOOR, OUTER SKIN. REPAIRED IAW HORIZON AIR EA 6-71-85.SDR 0300756739Skin · crackedDURING H-CHECK, FOUND CRACK IN NR 1 PYLON SKIN AT NACELLE STA 174. REPAIRED PER EA 67-165061.SDR 0300766739Skin · crackedDURING H-CHECK, FOUND CRACK IN SKIN OF NR 3 PYLON AT ACCESS PANEL NR 473CL CUTOUT. REPAIRED PER EA 67-165062.SDR QXEA0300401Skin · scratchedPDX - NR 1 NACELLE INBOARD AT STATION X449.500 HAS SCRATCH AND DENT IN SKIN. REPAIRED IAW DHC-8 400 SRM 51-25-05 AND HORIZON AIR EA 6-54-216.SDR 0300635526Doubler · crackedDURING "L" CHECK FOUND CRACK IN RIGHT HAND STRUT SKIN AND INNER DOUBLER OF NR 2 PYLON. REPAIRED PER EA 55-194405.SDR ASAA0310084Doubler · crackedPAE - DURING C-CHECK, FOUND NR 2 ENGINE COWL LATCH PIN DOUBLER AT NACELLE STATION 181 CRACKED. REMOVED AND REPLACED DOUBLER PER SRM. (M)SDR UPS03440252Skin · crackedINSPECTION TYPE:ASV NR 4 ENGINE PYLON CRACKED ON I/B SIDE. CRACK IN NR 4 ENG PYLON INBD SIDE AFT OF SLOT SEAL COMING FROM TOP SIDE OF PREVIOUS DOUBLER. REMOVED EXISTING DOUBLER FROM A/C 75705 03/04/03, REPAIRED PER EO B747-5430-18401-A. NEW DOUBLER REPAIR ISDR BJNA030219Skin · corrodedDURING A SCHEDULED MAINTENANCE, LEVEL 2 CORROSION WAS DISCOVERED ON NR 2 ENGINE INBOARD COWLING. CORROSION WAS LOCATED UNDERNEATH THE FIRE SEAL AREA THROUGHOUT THE FORWARD AND AFT SECTION. REMOVED FIRE SEAL FOR ACCESS TO THE CORRODED SECTION OF SKIN. REMOVESDR UIEA200300009Skin · delaminatedDURING CURRENT C-CHECK AT SIAEC, FOUND NR 3 ENGINE LEFT FAN COWL DELAMINTED APPROXIMATELY 8 INCHES BY 8 INCHES IN GENERAL REWORK AREA NOTED BY SB 78-2150 DURING TRAS LOCK MODIFICATION. THE OUTER DELAMINTED SKIN AND FILLER WERE STAGGER CUT TO REMOVE DELAMINATESDR SIMA200305005Skin · chafedABI - DURING A MBV INSPECTION, THE LEFT NACELLE INBOARD FILLET AREA WAS FOUND TO BE CHAFED. BLENDED CHAFE. PERFORMED AN EDDY CURRENT INSPECTION OF BLENDED AREA AND FOUND NO REJECTABLE INDICATIONS. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW SAAB 340 SRM (SDR UPS03440187Skin · crackedINSPECTION TYPE:PFLT NR 3 ENG PYLON INBOARD SIDE AFT ENG MOUNT ACCESS CUT PANEL PREVIOUS DOUBLER HOLE CHAFED THROUGH, HOLE CHAFED APPROX 2 INCHES AFT OF CUTOUT. REMOVED PREVIOUS REPAIR TO INBOARD SIDE OF PYLON. REPAIRED ACCESS DOOR/TAB SPACER,REMOVED FASTENESDR UPS03840138Panel · crackedNR 4 PYLON SIDE HAS 3.5 INCH CRACK IN ACCESS PANEL 499E {FIBERGLASS PANEL} 8 INCHES AFT OF L/E OF PANEL VERTICAL CRACK FROM BOTTOM EDGE OF PANEL. PANEL REPAIRED PER REF SRM 51-1-19.
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