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 QXEA9900527Skin · damagedYXX - NR 1 NACELLE INBOARD AND OUTBOARD SIDE RIVETS PULLED THROUGH SKIN AT STA 134.55 AND ZN15. REPAIRED IAW CONAIR EO 2224, HORIZON AIR EA 9-54-188 AND DHC-8 RD 8-54-953.SDR QXEA9900524Skin · damagedYXX - NR 2 NACELLE INBOARD AND OUTBOARD AT STA 130.60, RIVETS ARE PULLED THROUGH SKIN. REPAIRED IAW DHC-8 RD 8-54-953.SDR COMA9910036Plate · dentedDURING ENGINE REPLACEMENT, THE LEFT NACELLE CENTER PLATE SECTION WAS FOUND TO HAVE A DENT AND CHAFING DAMAGE ON THE AFT OUTBOARD SIDE. BOTH THE DENT AND CHAFING DAMAGE WERE REPAIRED PER AERODESIGN REPORT NR 3133-1, REV IR, 2-12-99.SDR SIMA990442Skin · chafedABI - DURING AN MBV INSPECTION, FOUND A CHAFE ON LT NACELLE INNER SKIN. BLENDED CHAFE AREA AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO INDICATIONS OF CRACKS. FABRICATED A DOUBLER FROM CRES 301 1/4 HARD .025 INCH THICK. APPLIED SEALANT TO THE CONTACT SUSDR SIMA990432Skin · chafedABI - DURING AN MBV INSPECTION, FOUND A CHAFE ON RT NACELLE OUTBOARD INNER SKIN. CUT OFF AND REMOVED THE CHAFED CORNER ANGLE BETWEEN THE FIRE FLOOR AND THE CHAFED INNER WALL. CUT OFF AND REMOVED THE FORWARD SECTION OF THE CHAFED SIDE WALL. FABRICATED A NEW SDR 99ZZZX1478Skin · damagedDURING STRUT MODIFICATION, THE SKIN BELOW MID-SPAR CHORD BETWEEN NAC STA 286 AND NAC STA 300 ON THE RIGHT SIDE OF NR 2 ENGINE PYLON WAS FOUND WITH HEAT DAMAGE WRINKLES. THE DAMAGED AREA WAS REPAIRED AS FOLLOWS: HEAT DAMAGED SKIN AREA WAS TRIMMED AND REMOVED. RSDR QXEA9900525Skin · damagedYXX - NR 2 NACELLE OUTBOARD SKIN AT STA 179.10 HAS RIVETS PULLED THROUGH STRAP. REPAIRED IAW DHC-8 SRM 51-20-36, 51-20-16 AND RD 8-54-215.SDR EIA990081Skin · crackedHKG - DURING C-CHECK, NR 3 PYLON VALVE ACCESS HOLE AFT LOWER AREA INNER AND OUTER SKIN CRACKED. REPAIRED IAW SRM 54-30-03. (M)SDR EIA990053Skin · chafedHKG - DURING C-CHECK, NR 3 PYLON LEFT SKIN AT NAC STATION 235 INTERNAL AREA CHAFED AND EXTERNAL DOUBLER CRACKED, NRC 6169. REPAIRED IAW SRM 54-30-03 FIG 35 AND 36. (M)SDR EIA990052Skin · disbondedHKG - DURING C-CHECK, NR 2 PYLON LEFT SKIN DISBONDED NEAR MIDSPAR FITTING NRC 6678. REPAIRED IAW SRM 54-30-03. (M)SDR P5CA9900170Skin · crackedNR 2 PYLON LEFT EXTERNAL SKIN CRACKED AT LOWER CUTOUT AREA. REPAIRED PER SRM 54-30-03.SDR P5CA9900163Skin · damagedNR 1 PYLON OUTBOARD LOWER SPAR SKIRT PATCH INNER AND OUTER SKIN DAMAGED. REPAIRED PER SRM 54-30-03.SDR 9900349608Skin · crackedDURING PERIODIC CHECK, FOUND PYLON AREA SKIN CRACKED AT FS 1038, LONGERON 15R. REPAIRED PER EA 99-163248.SDR SIMA9900332Skin · chafedABI - DURING MBV INSPECTION, CHAFE WAS DISCOVERED IN THE RIGHT NACELLE INBOARD SKIN AT FILLET FAIRING. BLENDED OUT DAMAGE FROM CHAFING TO VERY FINE SURFACE FINISH. PERFORMED EDDY CURRENT INSPECTION OF AREA WITH NO DEFECTS NOTED. FABRICATED DOUBLER .050 THICSDR SIMA990253Skin · chafedABI - DURING MBV INSPECTION, A CHAFE WAS FOUND ON THE RT NACELLE FIRE FLOOR ATTACHMENT ANGLE TO INNER SKINS. REMOVED AND REPLACED CHAFED FASTENER. FABRICATED AND ANGLE .040 THICK. NESTED THE ANGLE INTO THE EXISTING ANGLE. INSTALLED ANGLES USING CR3523-6 FOSDR ABXA9900122Skin · crackedLEFT WING INBOARD NR 2 PYLON LOWER AFT SKIN CRACKED AT LOWER TRAILING EDGE. REPAIRED IAW DC8 SRM 57-2-1.SDR QXEA9900279Skin · crackedPDX - INSIDE PANEL 02C, AT THE OUTBOARD SIDE THE 7TH STAGE BLEED AIR NACELLE FLANGE AREA IS CRACKED FROM SEVERAL RIVET HEADS ALONG THE FORWARD EDGE. REPAIRED IAW FOKKER SRM 54-14-01, PAGE 405 AND SRM 54-02-01, PAGE 4, FIGURE 3.SDR P2EA99065Fairing · wornSJO - NR 1 ENGINE LEADING EDGE WORN. REPAIRED NR 1 ENGINE PYLON LEADING EDGE FAIRING PER COOPESA EO C00-3-54-031-99 DATED 1-23-99, BOEING FAXES COO-SJO-99-0075RR DATED JAN 1-22-99 AND COO-SJO-99-0083RR DATED 1-2-99. (M)SDR SIMA990081Skin · chafedABI - DURING ABV INSPECTION A CHAFE WAS FOUND ON THE INNER WALL OF THE RIGHT NACELLE, INBOARD BEAM AFT OF NS 212. PERFORMED DYE PENETRANT INSPECTION, NO CRACKS FOUND. FABRICATED AND INSTALLED DOUBLER .025 THICK TO NACELLE. APPLIED FIRE SEAL AROUND DOUBLER WSDR DHL9971229CPanel · corrodedAT C-CHECK, AFT UPPER PANEL ON NR 3 STUB WING HAS A LARGE DOUBLER AT WHICH 90 PERCENT OF FASTENERS HAVE SKIN BULGED AND ARE PULLING THROUGH. REMOVED DOUBLER, PANEL DELAMINATED, REMOVED PANEL, INSTALLED NEW PANEL PER SRM 51-30-2.SDR DL72S990029Skin · crackedFOUR CRACKS AT FASTENER HOLES FWD OF PNL 9501 RT SIDE. REPAIRED PER MM 54-30-0.SDR C2XA99IA022Skin · chafedDURING C-CHECK INSPECTION, FOUND RIGHT ENGINE VENT TUBE WAS CHAFED INTO NACELLE FIREWALL DECK AT TAIL PIPE/ENGINE JUNCTION. WELDED IN REPAIR DOUBLER. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA99IA021Skin · chafedDURING C-CHECK INSPECTION, FOUND RIGHT ENGINE FUEL INLET TO NOZZLES LINE CHAFING INTO NACELLE DECK. INSTALLED REPAIR DOUBLER. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR EIA990104Skin · crackedDURING C-CHECK, LEFT PYLON SKIN AND STIFFENER WAS FOUND CRACKED AT STATION 965 ABOVE PANEL NR 8101A, NRC NR P062. REPAIRED IAW SRM 54-04 FIG 17A AND EO 9AV 981123) AND ECRA. (M)SDR UF6A981217Skin · crackedSBN - LEFT HAND INBOARD LEADING EDGE HAS CRACK ON UPPER LEFT HAND CORNER. MAINTENANCE REPAIRED BY INSTALLATION OF FABRICATED L-SHAPED PATCH DOUBLER MADE OF 2024-T3 .063 INCH. ALL WORK DONE IAW DER REPORT NR 98-199. (X)SDR C2XA98IA533Panel · chafedDURING C-CHECK INSPECTION, FOUND THE NACELLE ACCESS PANEL 432BB HAD SMALL CHAFE MARKS TO INNER SURFACE. LOCATED AND DRILLED NEW PANEL. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA532Panel · brokenDURING C-CHECK INSPECTION, FOUND ACCESS PANEL 442BB HAD SEVERAL FASTENER HOLES CRACKED AND BROKEN OUT. LOCATED AND DRILLED PANEL. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA528Skin · crackedDURING C-CHECK INSPECTION, FOUND THE RIGHT MLG AFT INBOARD DOOR FORWARD HINGE ATTACH POINT NACELLE SKIN CRACKED AT RIVET. STOP DRILLED AND FABRICATED DOUBLER REPAIR. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR QXEA9900006Skin · dentedDENTS FOUND IN OUTER SKIN OF INBOARD NR 2 ENGINE PANEL 425AL. REPAIRED IAW DHC-8 RD 8-71-139.SDR AU981653Panel · missing(AUS) DURING PRE-FLIGHT INSPECTION, TWO PANELS FOUND MISSING FROM NR 1 PYLON: PANEL NR 5728L, PN 311A1065-77, AND PANEL NR 5729L, PN 311A1065-78.SDR SIMA983442Skin · chafedABI - DURING MBV INSPECTION, FOUND A CHAFE ON LEFT NACELLE INBOARD FILLET FAIRING SEAL CONTACT AREA. BLENDED CHAFED AREA AND PERFORMED AND EDDY CURRENT INSPECTION WITH NO CRACKS INDICATED. FABRICATED AND INSTALLED A DOUBLER .050 THICK. AIRCRAFT RETURNED TO SDR EIAA980364Skin · crackedHKG - DURING C5 CHECK, NR 3 PYLON SKIN AT PANEL 473EL CUTOUT IS CRACKED, AND STIFFENER BEHIND IS CRACKED. REPAIRED PER RS R54-51-33962 AND ECRA 482-99-125-1. (M)SDR SIMA983353Skin · chafedABI - DURING MBV INSPECTION, RIGHT NACELLE INBOARD PANEL AFT OF PGB AS FOUND CHAFED. BLENDED CHAFED AREA AND PERFORMED A DYE PENETRANT INSPECTION WITH NO CRACKS FOUND. FABRICATED AND INSTALLED DOUBLER .025 THICK. AIRCRAFT RETURNED TO SERVICE. (M)SDR C2XA98IA474Skin · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT THRUST REVERSER MODULE UPPER SKIN WAS FOUND TO BE CRACKED WITH SHEARED RIVETS ABOVE FORWARD OF PANEL 426SL. MAINTENANCE STOP DRILLED THE CRACK, INSTALLED A REPAIR DOUBLER, AND REPLACED THE SHEARED FASTENERS IAW EMB14SDR HNAA9893685Skin · crackedORF - NR 1 NACELLE EXHAUST FINGERNAIL IS CRACKED AT THE OUTBOARD FORWARD SIDE SKIN AND HAS SEVERAL LOOSE RIVETS AND MISSING RIVETS AT THE TOP FORWARD SKIN. REPAIRED CRACKED SKIN AND REPLACED RIVETS. (M)SDR QXEA01769Skin · damagedNR 2 NACELLE INBOARD SIDE LOOSE RIVETS AND RIVETS WORN THROUGH SKIN AT STATION XN 134.68. REPAIRED IAW DHC - RD 8-54-983.SDR QXEA01767Skin · damagedNR 2 NACELLE OUTBOARD SIDE LOOSE RIVETS AND RIVETS PULLED THROUGH SKIN AT STATION 134.68 AND 24.25. REPAIRED IAW DHC-8 RD 8-54-983.SDR USAA980592Skin · crackedCLT - DURING C-1 CHECK VISUAL INSPECTION, FOUND A 1.5 INCH CRACK RIGHT ENGINE PYLON RIGHT SIDE CUTOUT FOR PANEL 443 BR SKIN. INSTALL EXTERNAL DOUBLER PER EA 62939. (M)SDR SIMA9830616Skin · chafedABI - LEFT NACELLE OUTBOARD UPPER SKIN CHAFING. CUT OUT DAMAGED AREA, PERFORMED EDDY CURRENT INSPECTION. NO INDICATIONS OF CRACKS. FABRICATED AND INSTALLED REINFORCEMENT DOUBLER .025 INCH. AIRCRAFT OK FOR SERVICE. (M)SDR SIMA982947Skin · chafedABI - CHAFED LEFT NACELLE OUTBOARD BEAM INNER SKIN PANEL AT NS 212. BLENDED CHAFE, PERFORMED EDDY CURRENT INSPECTION. FABRICATED AND INSTALLED DOUBLER. AIRCRAFT RETURNED TO SERVICE. (M)SDR SIMA982945Skin · chafedABI - FOUND CHAFE ON THE LEFT INBOARD NACELLE FILLET FAIRING SEAL CONTRACT AREA. PERFORMED EDDY CURRENT INSPECTION, FABRICATED AND INSTALLED DOUBLER. AIRCRAFT RETURNED TO SERVICE. (M)SDR QXEA01768Skin · damagedNR 2 NACELLE INBOARD SIDE LOOSE RIVETS AND RIVET HEADS WORN THROUGH ON STRAP AT STATION XN 182.70. REPAIRED IAW DHC-8 RD 8-54-215, PAGE 5.SDR VJ9800592Skin · corrodedNR 1 ENGINE I/B TAIL DOOR SKIN CORRODED. LOSS ON SKIN AT 3RD RIB FROM FWD PART OF COWL OUT OF LIMIT IAW B737 SRM 54-30-1. CUT OUT AND FABRICATED REPAIR DOUBLER, DRILLED, DEBURRED AND INSTALLED IAW B737 SRM 54-10-3. TREATED ALL BLENDED AREAS IAW B737 SRM 51-SDR DL757982052Skin · crackedNR 2 NACELLE STRUT SKINS, IB AND OB WERE FOUND CRACKED BEYOND PREV STOP DRILLS, ON REPETITIVE INSP BOTH WERE REPAIRED ON SRM 54-51-01-2-203 MIF ERA 259383-14. LOCATION IS NAC STA 107.7 REPAIR IS CLASSIFIED MAJOR.SDR P5CA9801479Skin · chafedNUMBER FOUR PYLON OUTBOARD SKIRT FOUND CHAFED ON INSIDE SURFACE. REPAIRED PER SRM 54-30-03 FIGURE 35 AND 36.SDR DL757981952Skin · crackedTHE NR 2 PYLON OUTBD STRUT SKIN WAS FOUND WITH A CRACK IN THE UPPER FWD CORNER OF THE STRUT SKIN CUTOUT. THE CRACK WAS ROUTED OUT AND REPAIRED WITH A DOUBLER AND TRIPLER PER SRM 54-51-01-2, FIG 203. OVERSIZED FASTENERS WERE AUTHORIZED PER ER/A 365652-14, REVSDR DHL9880402CSkin · crackedAT C-CHECK, I/B SIDE FROM PYLON NR 4 STUB WING LEADING EDGE HAS 2 INCH CRACK PROGRESSING FROM PREVIOUS REPAIR. REMOVED, REPAIRED, FABRICATED NEW DOUBLER PER SRM 51-1-4. N/R 530SDR 98FDEA00538Access Panel · torn98-213 - NR 3 ENG PYLON PNL 400GL TORN OFF ON INBD SIDE. AIRCRAFT LANDED EWR WITHOUT INCIDENT. REPLACED ACCESS PANEL. ALL NUTPLATES APPEAR TO BE IN GOOD WORKING ORDER.SDR VJ9800384Skin · corrodedRT PYLON LOWER TRAILING EDGE SKIN CORRODED ON INBOARD SIDE. REMOVED CORRODED SKIN FROM RT PYLON LOWER TRAILING EDGE IAW DC9 SRM 51-10-2, 51-10-4. INSTALLED NEW SKIN IAW DC9 SRM 51-30-2 AND RES 981313, REINSTALLED TRAILING EDGE ON PYLON IAW DC9 SRM 51-30-1.SDR RAAA98E9025Skin · crackedDURING SCHEDULED NR 3 CHECK PER CARD 42.03.78, FOUND NR 3 NACELLE I/B SKIN CRACKED, APPROX .75 IN, AT NAC STA -30, NAC WL -8. REPAIRED PER SRM 54-2-1. M-54 NR 215.
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