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 FDEA200909123291Skin · corrodedLT PYLON EXT LWR OTBD SKIN JUST BELOW MID SPAR FUSE PIN (APROX PP-185 TO PPS-196 ) HAS CORROSION. REMOVED CORROSION IAW SRM 54-50-01, DETAIL 1 AND FIG 101. ORIGINAL MAT 0.090 INCH, REMAINING MAT. 0.074 INCH, L=12.0 INCH, W=1.75 INCH, D=0.016 INCH FOUND TO BESDR FDEA200909123290Skin · corrodedNR 1 PYLON OTBD AFT 311N5046-31 SKIN ASSY HAS CORROSION ON INTERIOR SURFACE BETWEEN FWD ACCESS DOOR OPENING AND PRECOOLER OPENING. REMOVED CORROSION FROM INTERIOR SURFACE IAW SRM 54-50-01 ORIGINAL MATERIAL 0.90 INCH, MATERIAL LOSS 0.013", MAT REMAINING 0.077 SDR USAA2009091692543Skin · crackedCLT - Q4 - MAJOR REPAIR - CRACK IN NR 1 ENGINE PYLON SKIN UNDER ACCESS PANEL 5724L. REPAIRED NR 1 ENGINE PYLON SKIN UNDER ACCESS PANEL 5724L IAW EA 101396 & TYPICAL REPAIR 54-50-07.SDR DL757091465Skin · damagedFOUND TWO (2) EA HOLES TO BE .500 AT RT STA 116.05. C/W ERA 476265-14 REV O.SDR Q2S2010F00004Skin · crackedPYLON NR 4 SKIN BELOW ACCESS PANEL 483AL CUTOUT FOUND CRACKED. REPAIR CARRIED OUT IAW EN NR 1370-09.SDR JAF2009F00000Skin · crackedUPON REMOVING THE LT NACELLE FUEL TANK, WE NOTED A TOP WING SKIN CRACK ABOUT 3.5 INCHES LONG. FROM LOOKING UNDERNEATH IN THE GEAR WELL, JUST ABOVE THE MLG SIDE BRACE, YOU COULD SEE THE CRACK RUNNIING PARRALLEL WITH THE ANGLE STIFFENER. INSPECTED THE RIGHT GESDR USAA2009082492235Skin · crackedCLT - Q3 - MAJOR REPAIR - CRACK ON PYLON SKIN AT NAC STA 200. REPAIRED PYLON SKIN AT NAC STA 200 IAW TYPICAL REPAIR 54-30-07.SDR DL76G091357Skin · crackedNR 1 ENG PYLON STRUT SKIN REPAIR, PERMANENT REPAIR COMPLIED WITH PER ERA 476516-14.SDR ASAA0946411Skin · gougedNR 1 PYLON PANEL 5727L CUTOUT SKIN FWD EDGE IS GOUGED FROM PANEL. BLENDED AREA, FOUND OUT OF LIMITS. ACCOMPLISHED REPAIR TO THE NR 1 ENG PYLON PANEL CUTOUT.SDR UIEA200900050Skin · crackedRT NR3 CORE COWL UPPER AFT AREA FAIRING OUTER SKIN AT NAC STATION 296.25 TO 304.5 HAS A 8.250 INCH CRACK. TIME LIMITED REPAIR WAS ACCOMPLISHED IAW SRM 51-40-02-06-0 AND EO 4471A043. TO INSPECT OR ACCOMPLISH PERMANENT REPAIR NEXT A-CHECK.SDR FDEA200908072948Skin · corrodedRT NAC- I/B FWD PANEL 443GL CUT OUT EXTERNAL SURFACE CORRODED. REMOVED SKIN, FABRICATED NEW SKIN P/N 311N5193-1, INSTALLED NEW SKIN ASSY I/B PYLON SURFACE, IAW SRM 54-50-01, 51-20-01, 51-40-02. MAJOR REPAIR.SDR UALA2009073102289Skin · crackedNR 4 PYLON RT SIDE SKIN CRACKED AT ACCESS PLATE 482 ER CUTOUT. INSTALLED REPAIR. ACPD ON JOCR 540089.SDR EIAA200900102Panel · crackedNR 2 PYLON EXTERIOR SKIN CRACK O/B SIDE AT ACCESS PANEL 463 BL CUT OUT APPROX NAC STA 318. FABBED AND INSTALLED REPAIR PER ECRA 488-54-033-2.SDR EIAA200900101Skin · deformedNR 2 PYLON ESTERIOR SKIN I/B SIDE AT ACCESS PANEL 463 AR CUTOUT AREA HAS CHIPPED AND DEFORMED EDGES. FABRICATED AND INSTALLED REPAIR PER ECRA 488-54-031-2 REV A.SDR MALA090099Skin · chafedINSIDE OF RT NACELLE CHAFED AT INSIDE OF LOWER FWD INTAKE BAY, ON INBD LOWER STIFFENER AND SKIN AT NS 92. FABRICATED AND INSTALLED NEW SKIN, STRAP, AND STRAP SUPPORT IAW EO S54224.SDR USAA2009071691850Skin · crackedCLT - Q-2 - MAJOR REPAIR - NR 03C60754003/003 - CRACK IN RIGHT HAND PYLON SKIN AT FORWARD OUTBOARD CORNER UNDER PANEL 5827. REPAIRED RIGHT HAND PYLON SKIN AT FORWARD OUTBOARD CORNER UNDER PANEL 5827 IAW US AIRWAY TYPICAL REPAIR 54-70-07.SDR IPXA09556733Panel · chafedINSP TYPE: C2 PANEL 434BL HAS CHAFING ON INNER SURFACE. REMOVE AND REPLACE WITH FABRICATED REPLACEMENT PART.SDR IPXA09556732Panel · chafedINSPECTION TYPE: C2 PANEL 444BL HAS CHAFING ON INNER SURFACE. REMOVED AND REPLACED WITH FABRICATED REPLACEMENT.SDR IPXA09656684Skin · crackedINSPECTION TYPE:7C NR 2 PYLON - ACCESS PANEL 442AL CUTOUT SKIN CRACKED. NR 2 PYLON I/B ACCESS FWD HOLE CUTOUT SKIN REPAIRED AS PER HX RS R54-51-36368 REV A AND UPS EO B767-5430-34212-A. THIS REPAIR IS CLASSIFIED AS MAJOR REPAIR WITH MATERIAL AMS4911-0090IN ASDR 2009FA0000549Skin · delaminatedLT NACELLE HAS SEVERAL AREAS OF DELAMINATION AND CORROSION OF OUTER SKIN. OBTAINED DER APPROVAL FOR REPAIRS OF AFFECTED AREAS.SDR 2009FA0000548Skin · delaminatedRT NACELLE HAS SEVERAL AREAS OF DELAMINATION AND CORROSION OF OUTER SKIN. OBTAINED DER APPROVAL FOR REPAIRS OF DELAMINATED AND CORRODED AREAS.SDR IPXA09556539Panel · chafedINSPECTION TYPE:C2, NR 2 ENG NACELLE STRUT HAS CHAFING COMMON TO PANEL 443FR CUTOUT. REMOVED DAMAGE, FOUND OUT OF LIMITS. FABRICATED NEW DOUBLER, INSTALLED AND COMPLETED REPAIR PER SRM 51-10-02-0G, SRM 51-40-05 OHM 20-50-01.SDR IPXA09M56466Skin · misrepairedINSPECTION TYPE:1C REPAIR SURVEY SEQ 273-P2-01 EXTERNAL REPAIR DOUBLER ON NR 2 ENGINE PYLON RT SIDE BETWEEN STA YID558-913 AND 562-913 NOT CORRELATED TO SRM REPAIR. REMOVED EXISTING REPAIR FROM NR 2 PYLON LOWER AFT SECTION SKIN AT STA ZPTN2 36.270, FABRICATEDSDR IPXA09M56350Skin · crackedINSPECTION TYPE:N/A PYLON FAIRING SKIN CRACKED. REPAIRED PER EO MD11-5450-33884.SDR USAA2009061691489Flange · crackedCLT - C5 - MAJOR REPAIR - FLANGE CRACKED ON NR 1 ENGINE PYLON PANEL 5727L CUTOUT. REPAIRED CRACKED FLANGE ON NR 1 ENGINE PYLON PANEL 5727L CUTOUT IAW US AIRWAYS TYPICAL REPAIR 54-30-07.SDR KCSA091048Skin · wornNR 2 PYLON O/B SKIN LOWER EDGE WORN BETWEEN NAC STA 210 AND 217.SDR IPXA09M56185Doubler · crackedINSPECTION TYPE:2C REPAIR SURVEY SEQ 250-P2-01, EXISTING REPAIR DOUBLER ON NR 2 ENG RT CORE COWL FWD LATCH AREA SKIN CRACKED, COULD NOT CORRELATE WITH AN APPROPRIATE MD-11 SRM REPAIR. REMOVED DOUBLER, CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER ANDSDR IPXA09656146Skin · crackedINSPECTION TYPE:7C NR 2 PYLON STRUT LT EXT SKIN 425DL CUTOUT CRACKED. NR 2 PYLON STRUT LT EXT SKIN 425DL CUTOUT REPAIRED AS PER HX RS R-54-51-36328 REV A. THIS IS CLASSIFIED AS A MAJOR REPAIR WITH MATERIAL AMS4911-00901IN AND AIS1-301-00161INFH, REPAIR SIZE SDR UALA2009051801408Skin · damagedNR 2 PYLON INBOARD SAILTAIL AT AFT LOWER STRUT FAIRING, 3 -8TH HUCK BOLT INSTALLED. MAJOR REPAIR ACCOMPLISHED, REMOVED DAMAGED SKIN SECTION. FABRICATED NEW SKIN FROM .05 INCH INCONEL AND INSTALLED.SDR USAA2009060291377Access Panel · crackedSAL - C19 - MAJOR REPAIR - CRACK ON LEFT PYLON UPPER SKIN AT ACCESS PANEL 5728L CUTOUT. REPAIRED LEFT PYLON UPPER SKIN AT ACCESS PANEL 5728L CUTOUT IAW US AIRWAYS TYPICAL REPAIR 54-30-07.SDR USAA2009060191363Skin · crackedSAL - C19 - MAJOR REPAIR - NR 6176110 - 2 CRACKS ON RIGHT HAND PYLON OUTBOARD SIDE AT ACCESS PANEL CUTOUT 5824R. REPAIRED RIGHT HAND PYLON OUTBOARD SIDE AT ACCESS PANEL CUTOUT 5824R IAW US AIRWAYS TYPICAL REPAIR 54-10-07.SDR FDEA200905121929Skin · crackedNR 3 ENGINE NOSE COWL EXTERIOR SKIN CRACKED AND CHAFED AT T/E, APPX 4 O'CLOCK. CUT-OUT DAMAGE AREA IAW SRM 51-10-1 AND FABRICATED DOUBLER REPAIR AND FILLER IAW SRM 54-30-3 FIG 3A. TREATED AND PRIMED NEW PARTS IAW SRM 51-10-2. INSTALLED NEW PARTS IAW SRM 5SDR FDEA200905121928Skin · crackedNR 1 ENGINE NOSE COWL AFT EXTERIOR SKIN OTBD SIDE AT 9 O'CLOCK POSITION. AFT T/E SKIN EDGE IS BENT OUT AND CRACKED. CUT OUT DAMAGED AREA, FABRICATED DOUBLER REPAIR AND FILLER AND INSTALLED REPAIR IAW SRM 54-30-3, 51-30-2, 51-10-1 AND 51-10-2.SDR NWAA091615503Skin Panel · crackedDURING "L" CHECK FOUND CRACK THE NR 2 PYLON NACELLE STRUT RT SKIN PANEL AT NAC STA 107.7-116.09. REPAIRED PER EA 55-215154 SECT I, SECTION II PERMANENT REPAIR TO BE ACCOMPLISHED NO LATER THAN MAY 08, 2011.SDR NWAASkin · crackedDURING "L" CHECK FOUND CRACK IN NR 2 PYLON NACELLE STRUT RT SKIN PANEL AT NAC STA 107.7-116.09. REPAIRED PER EA 55-215154 SECT I, SECTION II PERMANENT REPAIR TO BE ACCOMPLISHED NO LATER THAN MAY 10, 2009.SDR IPXA09M55897Skin · damagedINSPECTION TYPE:2C REPAIR SURVEY SEQ NR 286-P2-01 EXISTING REPAIR ON RT NR 2 PYLON BETWEEN STA YID 524.303 - YID 546.559 NOT PER SRM. REMOVED EXISTING REPAIR, FABRICATED AND INSTALLED REPLACEMENT REPAIR IAW IPXA EO MD11-5430-33491-A AND SAA EA 011-5430-01-A17SDR UALA2009041701124Panel · crackedFOUND CRACKS IN 2 DIFFERENT PYLON PANELS, 1 PANEL HAS 15 INCH CRACK AND OTHER PANEL HAS 2 CRACKS 4 INCHES LONG. OLD PANELS ARE OFF. WILL REPAIR PANEL WITH SMALL CRACKS. P/N 311U4536-3. REPLACED PANEL.SDR WRLA2009094Panel · damagedDURING C2-CHK IN TPE INSPECTION FOUND NR 2 ENG PYLON UPPER PANEL 457BR AND 457FR RIVET HOLES DAMAGED 20EA. REPAIRED NR 2 ENG PYLON UPPER IAW EGAT EI W2009A54B-498 REV 00. CONDITION CHECK NORMAL & JOB COMPLETE.SDR USAA2009042490977Skin · crackedMCN - C2 - MAJOR REPAIR - NR 1 PYLON SKIN CRACKED AT AFT OUTBOARD & INBOARD THRUST REVERSER FITTING UPPER AFT HOLE. REPAIRED NR 1 PYLON SKIN AT AFT OUTBOARD & INBOARD THRUST REVERSER FITTING UPPER AFT HOLE IAW US AIRWAYS EA 130245.SDR FDEA200904061205Skin · delaminatedNR 1 PYLON PANEL 474 BR INNER SKIN IS DELAMINATED. REPAIRED NR 1 PYLON PANEL 474 BR BY REMOVING DAMAGE; CLEANING; PREPARING AREA AND APPLYING FIBERGLASS WET LAY-UP REPAIRED IAW 54-50-00 AND 51-77-10. INSTALLED SEAL IAW DWG A54515353 CURED REPAIR IAW SRM 51SDR FDEA200904021153Skin · corrodedNR 2 PYLON FORWARD SKIN LEFT SIDE CORRODED 3 INCH ABOVE LOWER EDGE OF PYLON PP STA 120 APPROX. FOUND EXCEEDED SRM LIMITS. REMOVED AND REPLACED INBD SKIN IAW SRM 51-10-02 AND SRM 51-40-02 REV.96. REPAIR IS CLASSIFIED AS MJOR IAW GMM 6-2-100 CRITERIA.SDR FDEA200904021136Panel · crackedFOUND 2 CRACKS ON PYLON NR 2 OUTBOARD SIDE PANEL AT RIB 8 DOUBLER REPAIR PERFORMED IAW DRAWING R546-10124, COVERED BY EO 6-5450-7-5003 PT 2.SDR FDEA200903311112Skin · corrodedNR 2 PYLON LT SIDE SKIN EXFOLIATED AROUND FASTENERS APPROX BETWEEN P/P STA 136 AND 140, AND 1 INCH ABOVE LWR SPAR. CORROSION ON NR 2 PYLON SKIN FOUND EXCEEDED ALLOWABLE DAMAGE LIMITS. PYLON SKIN REMOVED AND REPLACED IAW SRM 51-40-02 REV 97. REPAIR IS CLASSISDR FDEA200903311113Panel · crackedNR 1 PYLON PANEL 413 BL IS CRACKED IN THE CORNER UNDER THE SEAL. REMOVED SEAL RETAINERS AND SEALS IAW SRM 51-40-21; PG 5. STOP DRILLED CRACKS IAW SRM 54-52-51; PG 225; STEP E. FABRICATED DOUBLER AND INSTALLED IAW SRM 54-52-51; PGS 229 / 230. REINSTALLED SDR FDEA200903311111Skin Panel · corrodedNR 1 PYLON HAS LIGHT CORROSION ON INNER SKIN FWD OF PANEL 433BL. REPAIR AS REQUIRED. NR 1 PYLON OTBD SKIN FROM PP STA 120.50 TO PP STA 209.50 REMOVED AND REPLACED IAW SRM 51-40-02 REV 96, AND DWG 311N5002 SHT 13, REV E. REPAIR IS CLASSIFIED AS MAJOR IAW GMMSDR FDEA200903311110Skin Panel · corrodedNR 1 PYLON HAS CORROSION AROUND VERTICAL FRAME ON INNER SKIN FWD AND AFT OF ACCESS HOLE PANEL 433HR. FOUND EXCEEDED SRM DAMAGE LIMITS. REMOVED AND REPLACED PYLON SKIN IAW SRM 51-40-02 REV 96. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.SDR FDEA200903311109Skin Panel · corrodedINSIDE PYLON NR 2 RT SIDE HAS CORROSION APPROX 8 INCHES FWD OF PANEL 443BR TO APPROX. 10 INCHES AFT OF PANEL 443BR. REPAIR AS REQUIRED. NR 2 PYLON OTBD SKIN REMOVED AND REPLACED IAW SRM 51-10-02 REV 96, SRM 51-40-02 REV 96, AND DWG 311N5002 SHT 13, REV E. RESDR IPXA09555298Panel · damagedINSPECTION TYPE:C2 NR 2 ENG NACELLE PANEL 444BL HAS WORN FASTENER HOLE. FABRICATED REPLACEMENT PANEL IAW EO 757-5450-22203-B.SDR C8GA20090124Skin · damagedWHILE IN HEAVY MX IT WAS NOTED THAT NR 1 AND NR 3 PYLON UPPER SURFACE FASTENERS G AND H ARE PULLED THRU THE PANEL AT ENGINE STA 146 BBL 68. REMOVED PANELS AND FABRICATED NEW PANELS. INSTALLED NEW PANELS. NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SESDR ASAA0944860Skin Panel · gougedRT ENGINE PYLON PANEL 5827B CUTOUT INNER SURFACE ON MOUNTING FLANGE GOUGED. REPAIRED PER EA 400 54EA 00912.
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