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 MALA010589Skin · chafedDURING 4K-HEAVY CHECK IN CWA, LT NACELLE I/B SKIN IS CHAFED WHERE FILLET PANEL SEAL CONTACTS SKIN.SDR MALA010588Skin · chafedDURING 4K-CHECK IN CWA, FOUND RT NACELLE I/B SIDE WHERE FILLET PANEL INTERSECTS IS CHAFED. MAINTENANCE INSTALLED REPAIR ON I/B SKIN OF RT NACELLE IN I/B WING FAIRING CHAFED AREA.SDR CALA0100639Access Panel · crackedINSPECTION FOUND A .5 INCH CRACK IN NR 1 ENGINE PYLON ACCESS PANEL 5727. A DOUBLER WAS INSTALLED IAW ECRA 5430-01230.SDR USAA010676Skin · crackedCLT - FOUND PYLON/STRUT SKIN CRACKED .75 INCH, NR 1 ENGINE STRUT, PANEL NR 5727 OPENING, OUTBOARD AFT RADIUS. STOP DRILLED CRACK, INSTALLED DOUBLER PER TR 54-30-07. (M)SDR 01FDEA00444Skin · wornSKIN FWD OF NR 2 ENG MATES TO FAN COWL WORN THRU NACELLE SKIN BS YTN138.977. REPAIRED PER IAW EA 8-5410-53241.SDR ASAA0110335Skin · dentedPAE - DURING SCHEDULED C-CHECK, FOUND FAIRING SKIN AT NACELLE STATION 113.79, NACELLE WATERLINE 126.14 DENTED. REPAIRED PER EA. (M)SDR 0102106307Skin · crackedDuring line check found crack in skin on the lower aft corner of cutout for number one pylon access panel 452ER . Repaired per EA 63-184047.SDR UPS01836147Skin · crackedINSPECTION TYPE:C1 NR 4 PYLON O/B WEB PNL FWD ACCESS HOLE HAS APPROX 1 INCH CRACK ON LWR SIDE. REMOVED FASTENER -22 & -28 IAW REO G08127 DC8 SRM 51-1-21 51-1-20D & 51 -3-0 MAT ID FOR -3 -5 DOUBLERS .125 7075-T6 PO 340779 IAW REO G08127. LOCATED AND DRILLED -SDR AWXA0001791Plate · crackedTOP LEFT PYLON LAND FOR ACCESS PANEL CRACKED NAC STA 214. REPAIRED IAW AWA ER 03-5433-00340-DL1.SDR 2001UALA00794Skin · crackedNR 1 ENG PYLON LT OUTBOARD SIDE, PANEL 436BL CUTOUT IS CRACKED AT FWD UPPER FASTENER HOLE. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REPAIRED SKIN PER SRM 54-53-97.SDR USAA010734Skin · crackedPIT - FOUND PYLON SKIN CRACKED 1 INCH, UPPER RIGHT CORNER OF PANEL 5724L OPENING. STOP DRILLED CRACK, INSTALLED DOUBLER PER TYPICAL REPAIR 54-50-07. (M)SDR CA010627012Panel · missing(CAN) DURING A MAINTENANCE CHECK, IT WAS OBSERVED THAT THE RT AFT NACELLE PANEL WAS MISSING. SERVICEABLE PANEL WAS INSTALLED. NO FURTHER INCIDENT DURING SUBSEQUENT FLIGHT.SDR ERKR200100125Skin · damagedREPAIR- ENGINE STRUT NR 4, RIGHT SKIN DAMAGE-NAC STA 236.5. THIS DAMAGE IS IN A PREVIOUSLY REPAIRED AREA AT NAC STA 236.5 AND COMMON AND TO THE LOWER EDGE OF THE SKIN. THE PREVIOUSLY INSTALLED REPAIR DOUBLER WAS DAMAGED. THIS REPAIR REPLACES THE DAMAGED REPSDR UIEA01050Skin · crackedDURING INSPECTION FOUND PYLON SKIN NR 4 POSITION CRACKED AT ACCESS DOOR R/S BETWEEN NAC 211.42 AND 222.50. TRIMMED OUT CRACKED AREA. HFEC AREA FOR ADDITIONAL CRACKING, NO CRACKS FOUND. FABRICATED FILLER AND REPAIR DOUBLER, INSTALLED SAME PER STANDARD PRACTISDR CALA0100402Access Panel · crackedLEFT ENGINE PYLON UPPER OUTBOARD ACCESS PANEL CRACKED AT CUTOUT (.75 INCH). STOP DRILLED CRACK AND INSTALLED A REPAIR DOUBLER PER EC/RA 5430C01230.SDR 0101596305Skin · crackedDURING H-CHECK FOUND CRACK ON NUMBER ONE PYLON SKIN AT NACELLE STATION 293. REPAIRED PER EA 63-183398.SDR 2001UALA00388Skin · crackedNR 2 PYLON INBOARD SKIN ACCESS CUTOUT CRACKED. MAJOR REPAIR ACCOMPLISHED.INSTALLED DOUBLER REPAIR PER SRM.SDR TWAA0105901Skin · delaminatedON THE NUMBER 2 PYLON, THE INBD SIDE PANEL JUST AFT OF THE HYD ACCESS PANEL HAD A HOT BOND REPAIR THAT WAS LOOSE. INSTALLED EXTERNAL DOUBLER 0.063 301 1/2 STAINLESS STEEL WET WITH PRC SECURED WITH HI-LOKS PER SRM 54-53-70, FIG 203 SHEET 1 TO 10. CHECK-C 3-10SDR QXEA0100866Panel · damagedPDX - INBOARD SIDE PANEL OF NR 1 NACELLE TO ACCESS RIGHT-HAND H MEMBER. REPAIRED IAW DHC-8 SRM 51-20-51.SDR QXEA0100411Rivet · loosePDX-RIGHT NACELLE HAS FOUR LOOSE RIVETS BOTTOM OUTBOARD OF OIL COOLER. REPAIRED IAW HORIZON AIR EA 9-54-290A AND DHC-8 RD-8-54-057.SDR MWEA010447Skin · crackedFOUND ONE INCH LONG CRACK AT ATTACH POINT FOR RIGHT ENGINE PYLON PANEL 8105, AFT OUTBOARD NUTPLATE AREA. INSTALLED CRACK REPAIR PER STRUCTURAL REPAIR MANUAL 54-01, FIGURE 2.SDR USAA010311Skin · crackedCLT - FOUND SKIN CRACKED .75 INCH BY .25 INCH, ACCESS PANEL NR 5828 CUTOUT NACELLE STATION 10 RBL OF 0. INSTALLED REPAIR DOUBLER PER TR 54-30-07. (M)SDR USAA010310Skin · crackedCLT - FOUND SKIN CRACKED 1 INCH, NR 1 ENGINE PYLON PANEL NR 5724L CUTOUT. INSTALLED REPAIR DOUBLER PER TR 54-50-07 FIG 2 STEP 4. (M)SDR QXEA0100408Skin · tornPDX-LEFT HAND NACELLE OUTBOARD LOWER CORNER S/M TORN WHERE MAIN LANDING GEAR FORWARD HINGE ATTACH POINT. REPAIRED IAW DHC-8 RD-8-54-729.SDR 0101256641Skin · crackedDURING H-CHECK, FOUND CRACK ON THE NUMBER 4 PYLON INBOARD STRUT SKIN. REPAIRED PER EA 66-181950.SDR ABXA010101Skin · crackedRIGHT PYLON ELECTRICAL BAY AFT UPPER SKIN TO VERTICAL WEB ANGLE WAS CRACKED AT THE OUTBOARD BOLT HOLE. MAINTENANCE INSPECTED AND REPAIRED THE PYLON IAW DC-9 SRM 54-01 FIG 2 SHEET 3.SDR 2001UALA00219Skin · crackedNR 2 ENGINE PYLON IB SKIN CRACKED AT FWD LIGHTING HOLE. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.REPAIRED SKIN PER MAINTENANCE MANUAL.SDR C2XA01IA153Skin · crackedYUL - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE LEFT HAND NACELLE LEFT HAND FORWARD EDGING WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EDGING IN ACCORDANCE WITH ATR42-320 SRM 51-25-03, AND THE AIRCRAFT WAS APPROVED FOR RETUSDR C2XA01IA151Skin · crackedYUL - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE RIGHT HAND NACELLE LEFT HAND FORWARD EDGING WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EDGING IN ACCORDANCE WITH ATR42-320 SRM 54-12-61, & 51-25-03, AND THE AIRCRAFT WAS APPRSDR QXEA01000256Skin · crackedPDX-CRACK PROPAGATING FROM 3RD RIVET HOLE FROM OUTBOARD SIDE OF RIGHT NACELLE AT STATION XN239. REPAIRED IAW HORIZON AIR EA 9-54-276.SDR AWXA0001462Skin · crackedNR 1 PYLON SKIN CRACKED AT AFT LWR CORNER OF PNL 5724L OPENING. STOP DRILLED CRACK, HFEC CONFIRMED CRACK CONTAINED W/I STOP DRILL; INSTALLED DOUBLER IAW AWA EO 54-33-01.SDR AWXA0001404Doubler · crackedNR 1 ENGINE PYLON SKIN DOUBLER CRACKED .5 INCH AT O/B SIDE OF PANEL 5727L ACCESS OPENING. REPAIRED IAW ER 03-5433-01037-DC1.SDR AWXA0001398Doubler · crackedNR 2 ENGINE PYLON SKIN DOUBLER CRACKED .4 AT OUTBOARD SIDE OF PANEL 5828R ACCESS OPENING. REPAIRED IAW BOEING SERVICE BULLETIN 737-54-1035; INSTALLED ACCESS DOOR MODIFICATION IAW ER 03-5433-01037-04.SDR 2001UALA00139Panel · crackedNR 1 NACELLE STRUT PLUME SUPPRESSOR AFT PANEL CRACKED. *S/D* FOUND PLUME PANEL CRACKED. REPAIRED PANEL.SDR 2001UALA00189Splice · corrodedNR 1 PYLON INBOARD SIDE BETWEEN 2 SIDE PANELS, ATTACH SPLICE IS CORRODED. REPLACED SPLICE PER SRM 51-40-02.SDR RRXA10841Panel · damagedDURING A MAINTENANCE VISIT FOUND HOLE ELONGATED DAMAGE TO NR 3 PYLON PANEL AT PANEL 392A, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PARTS AND INSTALLED IAW DC-8 SRM 51-1-21.SDR DHL2001712507Skin · crackedC-CHECK - NR 3 ENG UPPER COWLING SKIN, 0.125 INCH CRACKS. PERFORMED STOP DRILL IAW SRM 51-10-1, PAGE 6B. FABRICATED DOUBLER WITH ALCLAD 2024, T3, 0.050 INCH IAW SRM 54-10-3, FIG 5. INSTALLED DOUBLER IAW SRM 54-10-3, FIG 5. (NON-ROUTINE CARD 1177).SDR AALA20010150Panel · separatedBOS - FLT 1183 - EN ROUTE BOS-STT SHORTLY BEFORE TAKEOFF DETECTED NR 2 ENGINE SHUTDOWN DUE TO INGESTION FROM ACOUSTICAL PANEL AT NACELLE. RETURNED BOS GATE WITHOUT FURTHER INCIDENT. REPLCED NR 2 ENGINE DUE TO FOD FROM DETACHED PANEL. SYSTEM IS CURRENTLY UNDSDR GLBA2001011Cowling · separatedRETURN TO BLOCK, RIGHT SIDE UPPER COWLING DERARTED FROM NACELLE ON T/O. INSPECTED COWLING FOR DAMAGE, RE-INSTALLED COWLING. RETURNED TO SERVICE.SDR DL757010143Skin · crackedTHE LT SIDE SKIN ON THE NR 1 PYLON WAS FOUND EMANATING FROM THE FWD UPPER CORNER OF THE FWD ACCESS HOLE. ADDITIONAL TOOLING DAMAGE WAS INCURRED ON THE SIDE SKIN AFT OF THE CUTOUT ALONG THE UPPER CHORD ATTACH AREA. THE DAMAGE WAS ROUTED OUT OF THE SIDE SKIN ASDR USAA010060Skin · crackedCLT - FOUND PYLON SKIN CRACKED .5 INCH, TOP OF NR 1 PYLON LOWER AFT CORNER PYLON PANEL 5727L. INSTALLED DOUBLER PER TR 54-30-07. (M)SDR DL757010184Skin · crackedNR 1 PYLON CRACKED O/B FWD AT 433AL CUTOUT AFT UPPER CORNER. REPAIRED PER SRM 54-51-01-2-2.SDR DL757010183Skin · crackedPYLON SKIN CRACKED AT TORQUE BOX FWD I/B ACCESS CUTOUT FWD UPPER CORNER. REPAIRED PER SRM 54-51-01-2-2.SDR QXEA0100065Skin · dentedPDX- ENGINE NACELLE RIGHT HAND SIDE, BOTTOM INBOARD SIDE IS A DENT IN SKIN, INBOARD OF OIL COOLER. REPAIRED IAW DHC-854-30-21 AND HORIZON AIR EA 9-54-266.SDR MALA010389Skin · crackedDURING 4K INSPECTION IN CWA, LT AND RT NACELLE SKINS AND FRAMES WERE FOUND TO CRACKED AT NACELLE STA 203.0. REFER TO EO S54050. MAINTENANCE COMPLETED REPAIRS TO LT AND RT NACELLE AND FRAMES IAW SRS340 SDS001079.SDR EIA2001018Doubler · crackedHKG-HAECO - NR 2 PYLON RIGHT EXIT DOUBLER CRACKED AT NAC STATION 222. REMOVED CRACKED DOUBLER, FARRIED OUT NDT INSPECTION SKIN AREA. CONFIRMED CRACK FREE. FABRICTED AND INSTALLED NEW DOUBLER PER SRM 54-30-03 FIG 35 AND 36. (M)SDR COMA0110015Skin · crackedTHE LEFT HAND NACELLE AFT OUTBOARD SKIN IS CRACKED. A DOUBLER WAS INSTALLED IN ACCORDANCE WITH AERODESIGN REPORT NR 3860-1.SDR ERKR200100057Skin · damagedINSPECTION REVEALED DAMAGE TO THE RIGHT HAND PYLON TRAILING EDGE UPPER SURFACE SKIN, THIS DOCUMENT PROVIDES MATERIAL SUBSTITUTION INSTRUCTIONS TO USE DMS1592 IN LIEU OF DMS1536 PER ECRA 933-54-068-2 REV. A.SDR UPS01434924Doubler · damagedINSPECTION TYPE:C, NR 3 ENGINE INBOARD LOWER PYLON SKIRT AREA DAMAGED ON THE INSIDE AFT OF REAR ENGINE MOUNT. REPAIRED SKIRT IAW SRM 51-40-02.SDR AWXA0001145Skin · crackedLT PYLON SKIN CRACKED AT ACCESS PANEL 5727L. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER IAW SRM 54-50-01, S/B 737-54-1035
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