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 EIAA2011088Skin · damagedNR 3 PYLON HAS 286 UPPER SKIN CAP 1 EACH HOLE EXCEEDS SB 747-54A2230 HOLE SIZE. REMOVED DAMAGE HOLE AREA, FABBED AND INSTALLED REPAIR PER ECRA 488-54-052-2.SDR FDEA201107052572Skin · corrodedNR 1 PYLON NAC STRUT INBD INNER SIDE SKIN AT PPSTA 144.4 - PPSTA 174.30 FOUND WITH CORROSION. SKIN R & R IAW EA 5450-152562. REPAIR IS CLASSIFIED AS MAJOR.SDR FDEA201107052571Skin · corrodedNR 2 PYLON NAC STRUT INBD INNER SIDE SKIN AT PP STA 136.7 - PP STA 174.30 FOUND WITH CORROSION. SKIN R & R IAW SRM 51-40-02, REV 103 AND DWG 311N5002, REV E. REPAIR IS CLASSIFIED AS MAJOR.SDR FDEA201107052570Skin · corrodedNR 2 PYLON NAC STRUT STRUCTURE INBD ACCESS HOLE FOR PANEL NR 443GL CUT-OUT INNER EDGES FOUND WITH CORROSION. SKIN R & R IAW SRM 51-40-02 REV.103 AND DWG 311N5002, REV E. REPAIR IS CLASSIFIED AS MAJOR.SDR FDEA201107052569Skin · corrodedNR 2 PYLON NAC STRUT STRUCTURE OTBD ACCESS HOLE FOR PANEL NR 443AR CUT-OUT INNER EDGES FOUND WITH CORROSION. PANEL R & R IAW EA F-5450-152563. REPAIR IS CLASSIFIED AS MAJOR.SDR FDEA201107052568Skin · corrodedNR 1 PYLON NAC STRUT STRUCTURE INBD ACCESS HOLE FOR PANEL NR 433GR CUT-OUT INNER EDGES FOUND WITH CORROSION. SKIN PANEL R & R IAW SRM 51-40-02 REV 103 AND EA F-5450-145386. REPAIR IS CLASSIFIED AS MAJOR.SDR FDEA201107052567Skin · corrodedNR 1 PYLON NAC STRUT STRUCTURE OTBD ACCESS HOLE FOR PANEL NR 433AL CUT-OUT INNER EDGES FOUND WITH CORROSION. R & R IAW E.A. F-5450-152562. REPAIR IS CLASSIFIED AS MAJOR.SDR EIAA2011077Doubler · gougedGOUGE IN AFT EDGE OF OPENING FOR NR 2 PYLON I/B AFT ACCESS PANEL 463AR. REMOVED AND REPLACED ACCESS PANEL 463AR DOUBLER PER ECRA 488-54-031-2 REV A.SDR FDEA201107012530Skin · damagedUPON REMOVAL OF SKIRT ANGLE ON NR 2 PYLON INBD SIDE, 2 EA DOUBLE DRILLED HOLES, 1 HOLE WITHIN .1 OF ANOTHER HOLE. REPAIRED HOLES IAW TD 70548824/012/2011, ISSUE A.SDR USAA2011070700005Skin · crackedC23 CHECK - CRACK ON NR 1 PYLON SKIN AND PANEL DOUBLER CRACKED PAST STOP DRILL AT PANEL 5727L. REPAIRED NR 1 PYLON SKIN AND PANEL DOUBLER CRACKED PAST STOP DRILL AT PANEL 5727L IAW TYPICAL REPAIR 737-5430-10-0054.SDR A6WA201140708Skin · chafedRT LOWER CORE COWL T/E CHAFED. REPAIRED IAW REO 601R-71-12-3276.SDR USAA2011070600017Skin · crackedQ6 CHECK - CRACK ON NR 2 PYLON SKIN AT PANEL 5828R, BETWEEN NAC STA 220 TO NAC STA 226, RBL 12. REPAIRED NR 2 PYLON SKIN AT PANEL 5828R, BETWEEN NAC STA 220 TO NAC STA 226, RBL 12 IAW TR 737-5430-10-0054.SDR NSVA2011142Skin · damagedAIRCRAFT RETURNED TO FIELD DUE TO MULTIPLE BIRD STRIKES AT APPROX 200-300 FT. MX INSPECTED AIRCRAFT AND FOUND BIRD STRIKES ON LT OUTBOARD NACELLE LOWER WING, RT INBOARDD WING AND NOSE GEAR DOORS. NO DAMAGE NOTED OK FOR SERVICE.SDR EE4Y20110441Skin Panel · corrodedENGINE NR 2, PYLON AFT FIXED FAIRING, OTBD AND INBD LATERAL SKIN PANEL WITH CORROSION. NOTE: THE FAIRING SKIN PANEL REQUIRES A MAJOR REPAIR IAW SRM GUIDELINES.SDR EE4Y20110440Skin Panel · corrodedENGINE NR 1, PYLON AFT FIXED FAIRING, OTBD AND INBD LATERAL SKIN PANEL WITH CORROSION. NOTE: THE FAIRING SKIN PANEL REQUIRES A MAJOR REPAIR IAW SRM GUIDELINES.SDR EE4Y20110383Skin · crackedENGINE NR 2, PLYLON PRECOOLER PANEL (423DL) SKIN VENT GRILL WITH CRACK. NOTE: THE SKIN PANEL CRACKS REQUIRE A MAJOR REPAIR IAW SRM GUIDELINES.SDR HNAA2011062100178Panel · missingNR 1 HORSE COLLAR PANEL MISSING. INSPECTED SURFACE AREA OF ACFT FOR POTENTIAL DAMAGE RESULTING FROM NR 1 HORSE COLLAR LOSS. NONE FOUND.SDR WX0A070881Cowling · gougedRIGHT UPPER ENGINE COWLING HAS GOUGE DAMAGE AT 3 LATCH CUTOUTS. REPAIRED IAW EA 14424 IAW IR DATED 6/13/2011 AND SRM 54-06, PARA 15, FIG 3.SDR EE4Y20110372Skin Panel · corrodedENGINE NR 2, PYLON AFT FIXED FAIRING, OTBD AND INBD LATERAL SKIN PANEL WITH CORROSION. MAJOR REPAIR.SDR EE4Y20110371Skin Panel · corrodedENGINE NR 1, PYLON AFT FIXED FAIRING, OTBD AND INBD LATERAL SKIN PANEL WITH CORROSION. MAJOR REPAIR.SDR A6WA201140707Skin · chafedRT UPPER CORE COWL T/E CHAFED. REPAIRED UPPER CORE COWL T/E IAW REO 61R-71-12-3276.SDR USAA2011062000006Skin · crackedCLT - C1 - CRACK ON NR 1 ENGINE PYLON PANEL 5727L CUTOUT AT PYLON STA 206.50. REPAIRED NR 1 ENGINE PYLON PANEL 5727L CUTOUT AT PYLON STA 206.50 IAW TYPICAL REPAIR 737-5430-10-0054.SDR USAA2011070600020Skin · crackedQ6 - CRACK ON FORWARD UPPER CORNER OF PYLON ACCESS (5724L) CUTOUT. REPAIRED FORWARD UPPER CORNER OF PYLON ACCESS (5724L) CUTOUT IAW EA 103051.SDR A6WA201140661Panel · chafedPANEL 422DB HAS KNIFE EDGE (QTY 2). R & R SEPARATOR PANELS IAW SRM 51-42-06.SDR A6WA201140658Skin · chafedLT ENG LOWER CORE COWL HAS 3 CHAFE MARKS THRU SKIN CUT OUT DAMAGE SECTION IAW REO 601R-71-12-4059 AND APPLY EA934NO ADHESIVE TO AREA.SDR USAA2011070600018Skin · crackedQ6 CHECK - CRACK ON NR 2 PYLON SKIN AT RIGHT ACCESS PANEL, NAC STA 240. REPAIRED NR 2 PYLON SKIN AT RIGHT ACCESS PANEL, NAC STA 240 IAW EA 103063.SDR KCSA111141Skin · wornNR 4 PYLON O/B LOWER SKIN EDGE AND FIREWALL WORN NAC STA 221 TO 230.SDR KCSA111140Skin · wornNR 4 PYLON O/B LOWER SKIN EDGE AND FIREWALL WORN AWAY NAC STA 180 TO 221.SDR A6WA201140655Skin · chafedRT ENG TOWER CORE COWL TIE CHAFED, KNIFE EDGE. REPAIRED CHAFED/KNIFE DAMAGE ON EDGE T/E RT ENG LOWER CORE COWL IAW REO 601R-71-12-3276, REV NC.SDR A6WA201140657Skin · chafedRT ENGINE UPPER CORE COWL T/E IS CHAFED KNIFE EDGED. REPAIRED CHAFED/KNIFE DAMAGE ON EDGE AFT T/E RT ENGINE UPPER CORE COWL IAW REO 601R-71-12-3276, REV. NC.SDR IPXA11567494Skin · wornINSPECTION TYPE:MOD, LT AFT FAIRING STRUCTURE OTBD FWD LWR SIDE SKIN WORN AND DAMAGED ON THE FWD END REQUIRES REPLACEMENT OF ENTIRE SIDE SKIN. R & R SIDE SKIN IAW SRM 51-40-02-0G, 51-40-08-0G, 51-21-00-7. AND AMM 57-21-10-7.SDR IPXA11567309Panel · crackedINSPECTION TYPE:MOD, RT AFT FAIRING STRUCTURE LOWER AFT T/E PANEL IS CRACKED JUST ABOVE THE AFT DRAIN TUBES. R & R PANEL IAW SRM 51-40-02.SDR FDEA201106012076Skin · damagedLEFT PYLON, LT SIDE SKIN AT P/P STA 204 HAS ELONGATED HOLE. NACELLE/PYLON - SKIN GOUGE ADJACENT TO TOOLING HOLE, COMPLIED WITH/ REPAIR IAW EA F-5450-146516. THIS IS A CAT "A" MAJOR REPAIR.SDR IPXA11567523Skin · gougedINSPECTION TYPE:C1, NR1 PYLON AFT STRUT FAIRING LWR SKIN LWR SURFACE IS GOUGED AND HILOCK HEAD IS CHAFED 11.5" AFT OF CNA 12 O'CLOCK. REPAIRED IAW SRM 54-50-70-1A 1, 51-30-01, 51-40-02-0G, 51-70-11-0G, 51-40-05-0G.SDR EE4Y20110305Skin · crackedENGINE NR 2 PYLON PRECOOLER PANEL (423DL) SKIN VENT GRILL WITH CRACKS. MAJOR REPAIR.SDR EE4Y20110304Skin · crackedENGINE NR 1, PYLON PRECOOLER PANEL (413DL) SKIN VENT GRILL WITH CRACKS. MAJOR REPAIR.SDR MALA110147Skin · chafedLOWER FWD COR COWL (RT) IS HEAVILY CHAFED ON INNER SIDE 4" FWD OF SUPPER DRAIN. COMPLIED WITH EO R54071 AND REO 690-54-23-137 FOR REPAIR OF RT LOWER CORE COWL CHAFE ON FWD SIDE OF SCUPPER DRAIN.SDR EE4Y20110308Skin · corrodedENGINE NR 2, PYLON AFT FIXED FAIRING, OTBD AND INBD LATERAL SKIN PANEL WITH CORROSION. MAJOR REPAIR.SDR EE4Y20110307Skin · corrodedENGINE NR 1, PYLON AFT FIXED FAIRING, OTBD AND INBD LATERAL SKIN PANEL WITH CORROSION. MAJOR REPAIR.SDR ABXR2011052800026Skin · crackedNR 2 PYLON UPPER FWD SKIN CRACKED. REPAIRED IAW B767 SRM.SDR ABXR2011052700015Skin · chafedNR 2 PYLON L/E CHAFED. REPAIRED IAW B767 SRM.SDR DALA1136300121Skin · crackedNR 1 PYLON OTBD CORE COWL UPP AFT EXTERIOR CRACKED SKIN REPAIRED PER PRI490780-14 REV.0 TO REV.2 DATED 25APR2011 1117HRS. PRI490890-14 REV.0 TO REV.2 COMPARED WITH ER/A490890-14 REV.0 DATED 20MAY2011 1228 HRS FOUND IN COMPLIANCE.SDR DALA1136250121Access Panel · damagedNR 1 PYLON ACCESS PANEL NR 436AR CUTOUT REPAIRED PER PRI490910-14 REV.0 AND REV.1 DATED 28APR2011 1714HRS. PRI490910-14 REV.0 AND REV.1 COMPARED WITH ER/A490910-14 REV.0 DATED 20MAY2011 1327HRS FOUND IN COMPLIANCE.SDR USAA2011061000002Skin · crackedCLT - Q4 - CRACK IN RIGHT PYLON STRUT SKIN AT PANEL 5827R AT WBL 191. REPAIRED RIGHT PYLON STRUT SKIN AT PANEL 5827R AT WBL 191 IAW TYPICAL REPAIR 737-5430-10-0054.SDR UIEA2011051900262Skin · dentedMX FOUND THE NR1 ENGINE INLET NOSE COWL - OUTER BARREL SKIN DENT, MEASURING: 12.0" X 9.0" AND THE DEPTH 0.250 (REF FIG 1), LOCATED APPROX AT 3 O'CLOCK POSITION. THE DAMAGE IS BEYOND THE ALLOWABLE DAMAGE LIMITS IAW SRM 54-31-01, FIG 1, IAW SRM 51-40-06, FIG 2. SDR AALA20110517AFW01Panel · dentedTHE RIGHT PYLON AFT OUTBOARD FAIRING PANEL HAS 3 EACH EXISTING SMALL DENTS. EXAMINATION OF THE DISCREPANT AREA CONFIRMS THAT THIS DAMAGE IS LIMITED TO THE SKIN PANEL ONLY. ACCOMPLISHED REPAIR PER EA 767-54-016759.SDR KCSA111117Skin · crackedNR 3 PYLON UPPER SKIN HAS A CRACK AT NAC STA 221 - .5 INCH.SDR P5CA2011051200050Access Panel · damagedNUMBER 3 ENGINE STRUT FAIRING ACCESS PANEL 472ER HAS ELONGATED FASTENER HOLES. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A54B-1002.SDR DALA1133519866Panel · crackedNR 1 ENG PYLON T/E PNL LANDING HAS A CRACK FWD OTBD END COMING PAST PREVIOUSLY REPAIRED STOP DRILL HOLE AT UPPERSIDE. REMOVED PREVIOUS REPAIR DOUBLER PER DC9 SRM 51-30-2. DRILLED STOP HOLE, FABRICATED NEW REPAIR DOUBLER PER DC-9 SRM 54-01 FIG 2 SHEET 3. MATSDR EE4Y20110279Skin · corrodedENG NR 2, PYLON AFT FIXED FAIRING , INBD AND OTD LATERAL SKIN PANEL WITH CORROSION. NOTE: THE PANELS' CORROSION REQUIRES A MAJOR REPAIR.
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