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 IPXA09M55037Repair · damagedINSPECTION TYPE:N/A NR 2 ENG PYLON T/E FAIRING HAS PREVIOUS REPAIR ON RT DAMAGED. REMOVED PREVIOUS REPAIR, FABRICATED NEW DOUBLER AND INSTALLED IAW EO C-5430-32701-A.SDR ASAA0944771Panel · crackedLT PYLON PANEL 5727L CUTOUT CRACKED. REPAIRED PER ER 09-1861 AND ASA EA 400-54EA-00915.SDR ASAA0944768Skin Panel · gougedLT PYLON PANEL 5729L CUTOUT AFT EDGE HAS MECH DAMAGE. REPAIRED PER EA 400-54EA-00913.SDR DL757090749Skin · chafedCHAFING MARK (WORN) ON WING LOWER SKIN SURFACE AT WS321.5 DUE TO CONTACT WITH NR 2 PYLON ACCESS PANEL 445BR. REPAIRED PER ERA473679-14REVD DURING HMV AT SAA ON NRC127291.SDR WRLA2009064Panel · crackedDURING A-CHECK IN ATL INSPECTION FOUND NR 2 PYLON CAP PANEL CRACKED UNDER RUDDER PANEL 457BL. REMOVED CAP PANEL ASSY. REPLACED NR 2 ENGINE PYLON CAP PANEL UNDER RUDDER. REPAIR ACCOMPLISHED ON N/R CARD 154.SDR USAA2009031690606Skin · corrodedCLT - C1 - MAJOR REPAIR - CRACK IN NR 2 ENGINE NACELLE STRUT AT 7 O'CLOCK POSITION IN ALUMINUM CHORD IN OUTBOARD AFT HINGE FITTING UPPER AFT FASTENER HOLE. REPAIRED NR 2 ENGINE NACELLE STRUT OUTBOARD AFT HINGE FITTING UPPER AFT FASTENER HOLE IAW US AIRWAYS EASDR UALA2009031000618Panel · delaminatedPYLON FAIRING PANEL DELAMINATED. RTFL. REPLACED FILLET FAIRING.SDR UALA2009022300618Panel · delaminatedPYLON FAIRING PANEL DELAMINATED. RTFL.SDR IPXA09M54901Panel · puncturedINSPECTION TYPE:4C PNL 264HR HAS A APPROX 2 INCH SCRATCH AND SMALL PUNCTURE IN EXTERIOR SURFACE TRAILING EDGE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD-11 51-71-00 PARA 16B.SDR DU4R2009299Skin Panel · corrodedS/O 318002 N/R 34983 - DURING SCHEDULED INSPECTION, FOUND CORROSION ON NR 1 PYLON FWD O/B SKIN PSS 68 - 80.SDR DU4R2009298Skin Panel · corrodedS/O 318002 N/R 34848 - DURING SCHEDULED INSPECTION, FOUND CORROSION IN NR 2 ENGINE PYLON INBOARD SKIN PANEL BELOW FWD AND AFT OF MOST FWD ACCESS PANEL.SDR DU4R2009297Skin Panel · corrodedS/O 318002 N/R 34856 DURING SCHEDULED INSPECTION, FOUND CORROSION IN OUTBOARD PYLON SKIN PANEL FWD OF MOST FWD ACCESS PANEL NR 2 ENGINE.SDR DU4R2009296Skin Panel · corrodedS/O 318002 N/R 34856 DURING SCHEDULED INSPECTION, FOUND CORROSION IN OUTBOARD PYLON SKIN PANEL FWD OF MOST FWD ACCESS PANEL NR 2 ENGINE.SDR P5CA2008020601585Access Door · missingNR 1 RT OUTBOARD STRUT ACCESS DOOR 454DR WAS FOUND TO BE MISSING DURING WALK AROUND INSPECTION. EO 4454A072 WAS ISSUED WITH A TIME LIMITED REPAIR AND A PERMANENT REPAIR TO BE DONE PRIOR TO 25 FLIGHT CYCLES.SDR DU4R2009326Skin · corrodedS/O NR 318002 NR 35425, DURING SCHEDULED INSP AT, FOUND NR 1 PYLON RT AFT SIDE WEB HAS NUMEROUS AREAS OF CORROSION ON INNER AND OUTER SURFACES INCLUDING FASTENER HOLES FROM PPS 128-209.SDR DL757090120Strut · damagedDURING HMV, A FASTENER HOLE IN THE OUTBOARD PYLON SIDE STRUT WAS FOUND OVERSIZED AND ELONGATED. THE HOLE WAS CLEANED UP TO ROUND CONDITION AND BUSHED BACK TO THE NOMINAL SIZE PER BOEING INSTRUCTIONS.SDR DL757090119Strut · damagedDURING HMV, FIVE FASTENER HOLES WERE FOUND OVERSIZED IN THE PYLON INBOARD SIDE STRUT. THE HOLES WERE CLEANED AND INSPECTED AND FILLED WITH OVERSIZE BOLTS PER BOEING INSTRUCTIONS.SDR UPS09M54649Skin · misrepairedINSPECTION TYPE:1C REPAIR SURVEY 293-P2-01, EXISTING REPAIR DOUBLER ON NR 2 PYLON RT SIDE BETWEEN STA 537-549 IS NOT ON MRCSSR REPORT AND NOT PER SRM. REMOVED EXISTING REPAIR, FABRICATED, AND INSTALLED REPAIR DOUBLER IAW UPS EO MD11-5430-32170-A.SDR UPS09M54494Fairing · damagedINSPECTION TYPE:C TRANSFERRED FROM UPS LOG PG 062231/1, DMI D388059 - REPAIR OF DAMAGE TO LEFT SIDE TAIL PYLON AFT FAIRING. TAIL PYLON AFT FAIRING REMOVED. EXISTING REPAIR STRAP REMOVED. HFEC C/O IAW DAC NDT SPM REV 13 PART 06-10-01.001 ON EXISTING TRIMMED SDR UALA2009010500026Skin · crackedCRACK ON UPPER FWD RADIUS ON PANEL CUTOUT NR 2 PYLON INBOARD SIDE, PANEL 446BL. MAJOR REPAIR ACCOMPLISHED, STOP DRILLED 2 EA CRACKS. INSTALLED REPAIR DOUBLERS.SDR FDEA200812165175Skin · crackedNR 1 PYLON SKIN PNL. CRACKED AT FASTENER, AT RIB 8 O/B SIDE. REPAIRED CRACKED SKIN IAW AIRBUS REPAIR DWG R54610124.SDR UALA2008112506669Skin · crackedNR 1 PYLON INBOARD SIDE SKIN CRACKED AT UPPER AFT CORNER OF CUTOUT FOR PANEL 416BR. MAJOR REPAIR ACCOMPLISHED. REMOVED HINGE FITTING, STOP DRILLED THE CRACK AND PERFORMED HFEC TO VERIFY CRACK CONTAINMENT. FABRICATED AND INSTALLED A REPAIR DOUBLER-TRIPLER.SDR 08FDEA04942Skin · erodedNR 1 NOSE COWL L/E SKIN AT BOTTOM HAS AREAS OF EROSION AND 3 CRACKS. REMOVED ACCESS PANEL IAW B727 SRM 51-30-2, CUT OUT DAMAGE DIMS 9 3/4 BY 3/4 IAW B727 SRM 54-30-3 FIG 3. FAB DOUBLER MAT 2024T3 .050 PO NR 9007861 DIMS 19 3/8 BY 3 1/2 AND FILLER MATERIAL 2SDR KCSA081599Skin · wornNR 4 PYLON LOWER EDGE SKIN ON I/B AT NAC STA 180 TO 220 SIDE IS WORN.SDR KCSA081597Skin · chafedNR 1 PYLON HAS CHAFING ON O/B SKIN UPPER SURFACE AT NAC STA-215 TO 220.SDR KCSA081596Skin · crackedNR 2 PYLON UPPER SKIN AFT EDGE DOUBLER APPEARS TO BE CRACKED .5 INCH AT NAC STA 221 O/B SIDE.SDR KCSA081586Skin · crackedNR 3 PYLON O/B SKIN CRACKED AT LOWER EDGE NAC STA 221.9.SDR FDEA200811104839Skin · damagedWHILE DRILLING THE 311N5046-31 NR 1 PYLON OTBD SKIN 2 EA NUTPLATE ATTACH HOLES WERE OVERSIZED TO .250 DIA AT APPROX PPS 132 AND 1 EA HOLE WAS ELONGATED AT APPROX PPS 205.65 AND 2 EA HOLES DAMAGED IN LOWER CHORD AT PPS 174.30. COMPLIED WITH EA F-5450-124034 ANDSDR FDEA200811104838Skin · damagedWHILE REAMING THE -31 OTBD SKIN AND OTBD BATHTUB FITTING FOR THE NR1 PYLON SIP MOD F-5450-7-5003 A4 PT.5 1 EA. HOLE WAS OVERSIZED TO 0.390 DIA. AND COUNTERSUNK FOR A BACB30NW12K(*) X FASTENER. COMPLIED WITH EA F-5450-124034, 11/07/08 AND REPAIRED OVERSIZED HOSDR 2008FA0000843Cowling · brokenAFTER LIFTOFF, AT APPROX 250 TO 300 FEET AGL THE RT SIDE OF THE UPPER ENGINE COWLING CAME LOOSE AND BROKE OFF AT APPROX THE MIDDLE LT PORTION OF THE COWLING, FALLING TO THE GROUND. THE ACFT HAD UNDERGONE A 100 HOUR INSP ON THE ENGINE AT 6905.8 HRS. OWNER STASDR 08FDEA04839Skin · damagedWHILE DRILLING THE 311N5046-31 NR 1 PYLON OTBD SKIN 2 NUTPLATE ATTACH HOLES WERE OVERSIZED TO .250 DIAMETER AT APPROX PPS 132 AND 1 HOLE WAS ELONGATED AT APPROX PPS 205.65 AND 2 HOLES DAMAGED IN LOWER CHORD AT PPS 174.30. COMPLIED WITH FED EX EA NR F-5450-124SDR 08FDEA04838Skin · misrepairedWHILE REAMING THE -31 OTBD SKIN AND OTBD BATHTUB FITTING FOR THE NR 1 PYLON SIP MOD F- 5450-7-5003 A4 PT.5 1 HOLE WAS OVERSIZED TO 0.390 DIA AND COUNTERUNK FOR A BACB30NW12K(*) X FASTENER. COMPLIED WITH FEDEX EA NR F-5450-124034 11/07/08 AND REPAIRED OVERSIZSDR FDEA200811094822Skin · corrodedNR 2 NACELLE STRUT INTERNAL, INBD SKIN EXFOLIATED AT PP STA 166 APROX AND HAS CORROSION FROM PP STA 174-100 AT ACCESS DOORS CUT-OUTS. REMOVED AND REPLACED WITH A NEW SKIN PANEL PN 311N5046-33 "A" MAJOR REPAIR NO FOLLOW-UP INSP REQUIRED.SDR FDEA200811094821Skin · corrodedNR1 STRUT OTBD SIDE SKIN CORRODED INSIDE ACCES PANEL 433CL REMOVED AND REPLACED WITH NEW SKIN PN 311N5046-31 IAW SRM 51-40-02 AND DWG 311N5002, "A" MAJOR REPAIR NO FOLLOW-UP INSP REQUIRED.SDR FDEA200811094820Skin · corrodedNR 2 NACELLE STRUT, OTBD INTERNAL SKIN HAVE CORRODED SPOTS ALONG PYLON . REMOVED AND REPLACED NEW SKIN PN 311N5446-32 "A" MAJOR REPAIR NO FOLLOW-UP INSP REQUIRED.SDR DHLA2009743DG627Skin · crackedNR 1 ENG NOSE COWL AT NAC STA 68 OUTER SKIN WITH CRACK BETWEEN 5 AND 6 O`CLOCK POSITION. REPAIRED LIP SKIN OUTER SIDE BETWEEN 5 AND 6 O`CLOCK POSITION IAW COOPESA EO COO-2-54-452-08 DTD 12/08/08 DOCUMENTED ON FAA FORM 8110-3.SDR 08FDEA04822Skin · corrodedNR 2 NACELLE STRUT INTERNAL, INBD SKIN EXFOLIATED AT PP STA 166 APPROXIMATELY AND HAS CORROSION FROM PP STA 174-100 AT ACCESS DOORS CUT-OUTS. REMOVED AND REPLACED WITH A NEW SKIN PANEL P/N 311N5046-33 "A" MAJOR REPAIR. NO FOLLOW-UP INSPECTION REQUIRED.SDR 08FDEA04821Skin · corrodedNR 1 STRUT OTBD SIDE SKIN CORRODED INSIDE ACCESS PANEL 433CL. REMOVED AND REPLACED WITH NEW SKIN P/N 311N5046-31 IAW SRM 51-40-02 AND DWG 311N5002, "A" MAJOR REPAIR NO FOLLOW-UP INSPECTION REQUIRED.SDR 08FDEA04820Skin · corrodedNR 2 NACELLE STRUT, OTBD INTERNAL SKIN HAVE CORRODED SPOTS ALONG PYLON. REMOVED AND REPLACED NEW SKIN P/N 311N5446-32 "A" MAJOR REPAIR NO FOLLOW-UP INSPECTION REQUIRED.SDR FDEA200811084814Skin · corrodedNR1 STRUT CORROSION ON INNER AFT SKIN INBD SIDE. R & R INBD SIDE SKIN PANEL ASSY. IAW DWG N311N5002 AND SRM 51-40-02. OLD CONTROL NR: 08FDEA04814SDR 08FDEA04814Skin · corrodedNR 1 STRUT CORROSION ON INNER AFT SKIN INBD SIDE. REMOVED AND REPLACED INBD SIDE SKIN PANEL ASS'Y IAW DRAWING N311N5002 AND SRM 51-40-02.SDR 08FDEA04760Skin · corrodedNR 1 PYLON INBD AFT 311N5046-34 SKIN PANEL ASSY HAS CORROSION ON INNER SURFACE. REMOVED AND INSTALLED REPAIRED NR 1 PYLON INBD AFT SKIN PANEL ASSY IAW DWG 311N5002 AND SRM 51-40-02. THIS REPAIR IS CLASSIFIED AS A CAT "A" MAJOR REPAIR WITH NO FOLLOW UP TRACKISDR 08FDEA04756Skin · crackedNR 2 PYLON LOWER SPAR, LOWER SIDE; 12 INCHES FWD OF THE AFT ATTACH BEAM, SKIN IS CRACKED. COMPLIED WITH EA E 6-5410-7-3000 A5 PTPT 4.SDR FDEA200811044709Skin · wornAFT NACELLE, FIREWALL SEAL PLANE AT FS Y2166 AND LEFT SIDE OF THE TRAILING EDGE OF THE DIVERTER, HAS WORN SKIN. REPAIR WORN SKIN AREA IAW SRM 51-31-01; VOL II; PG 1; SRM 55-35-04; VOL III AND DWG AJC7415, REV "BK". ALODINED AND PRIMED IAW SRM 51-21-01; VOLSDR 08FDEA04708Skin · wornAFT NACELLE, FIREWALL SEAL PLANE AT FS Y2166 AND RIGHT SIDE OF THE TRAILING EDGE OF THE DIVERTER; HAS WORN SKIN AND IS CRACKED. REMOVED AND FABRICATED NEW SKIN SECTION IAW SRM 51-35-01 VOL II AND DWG AJC7415 REV BK, ALODINED AND PRIMED IAW SRM 51-21-01 VOL I SDR 08FDEA04696Panel · wornNR 3 PYLON PANEL 487 ER IS WORN. NR 3 PYLON PANEL 487ER WAS WORN BEYOND ALLOWABLE LIMITS IAW SRM 54-00-01 VOL I PG 5. FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 54-00-01 VOL I PG 11. ALODINED AND PRIMED DOUBLER AND FILLER IAW SRM 51-21-01 VOL II. INSTALLSDR 08FDEA04709Skin · wornAFT NACELLE, FIREWALL SEAL PLANE AT FS Y2166 AND LEFT SIDE OF THE TRAILING EDGE OF THE DIVERTER, HAS WORN SKIN.SDR 08FDEA04688Skin · dentedNR 2 ENGINE FAN COWL EXTERIOR SURFACE DENTED APPROX 10 INCH FROM THE L/E; 3' FROM THE TOP. EVAULATED THE DENT AND FOUND TO BE OUT OF LIMITS IAW SRM 51-80-01. DENTED AREA IS DELAMINATED. REPAIRED DELAMINATED AREA BY REMOVING DAMAGE, FABRICATED DETAILS, PREPPSDR 08FDEA04687Panel · chafedNR 3 PYLON PANEL 487 EL IS CHAFED AT THE FWD END. BLENDED CHAFED AREA. FOUND TO BE OUT OF LIMITS IAW SRM 54-00-01. FABRICATED IAW SRM 51-21-01. ALODINED & PRIMED IAW SRM 51-21-01. INSTALLED IAW SRM 51-35-01.SDR USAA920081988Skin · crackedCLT MAJOR REPAIR Q3 CHECK NR 03975480042, CRACKED NR 1 ENGINE PYLON SKIN AT ACCESS OPENING 5727L. REPAIRED NR 1 ENGINE PYLON SKIN AT ACCESS OPENING 5727L. IAW US AIRWAYS TYPICAL REPAIR 54-30-07.
Back to JASC 5414