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 08FDEA04618Skin · corrodedNR 1 PYLON INBD AFT 311N5046-34 SKIN PANEL ASSY HAS CORROSION ON INNER SURFACE. FOUND SKIN ASSY CORRODED OUT OF LIMITS IAW SRM 54-50-01 (L= 1.5 INCH, W= 2.0 INCH, D= .028 INCH). ROUTED SKIN PANEL ASSY FOR REPAIR ON AMII WORK ORDER NR 7434, DATED 07/14/08 AGASDR 08FDEA04612Panel · chafedNR 1 PYLON PANEL 437 FR IS CHAFED. BLENDED AREA IAW SRM 54-00-01. BOTH FOUND TO BE OUT OF LIMITS IAW 54-00-01 & DWG 7108. ALODINED & PRIMED IAW SRM 51-21-01. INSTALLED IAW SRM 51-35-01 & 51-41-01.SDR 08FDEA04598Panel · chafedNR 3 PYLON PANEL 488 GL IS CHAFED IN SEVERAL AREAS. BLENDED AND FOUND TO BE OUT OF LIMITS IAW SRM 54-00-01. FABRICATED REPAIR DOUBLERS IAW SRM 54-00-01. TREATED & PRIMED REPAIR DOUBLERS IAW SRM 51-21-01. INSTALLED REPAIR DOUBLERS IAW SRM 51-31-01.SDR USAA920081953Skin · crackedCLT MAJOR REPAIR Q5 CHECK NR 03C50754003/011 LT PYLON STRUT SKIN CRACKED AT ACCESS PANEL OPENING 5724. REPAIRED THE LT PYLON STRUT SKIN AT ACCESS PANEL OPENING 5724 IAW US AIRWAYS TYPICAL REPAIR 54-50-07 PART 2 FIGURE 3.SDR QXEA2008110501131Skin · crackedPDX - C1 - UPPER OUTBOARD SKIN OF THE NR 1 NACELLE IS CRACKED. ROUTED OUT CRACK AND RESTORED FINISH REF RD 8/4-54-157.SDR 08FDEA04369Fairing · crackedNR 1 PYLON PANEL 438 CR IS CRACKED AT THE WELD. FABRICATED REPAIR DOUBLER IAW SRM 54-00-01. INSTALLED REPAIR DOUBLER IAW SRM 54-00-01 & SRM 51-35-01.SDR 08FDEA04325Skin Panel · corrodedNR 2 PYLON I/B AFT SKIN PANEL ASSY HAS CORROSION ON INNER SURFACE. REMOVED AND REPLACED SKIN PANEL ASSY PER DWG 311N5002 AND SRM 51-40-02. CORROSION ON SKIN WAS APPROXIMATELY 80% THROUGH MATERIAL. REPAIRED SKIN WAS RECEIVED ON TAG 031B66. THIS REPAIR IS CLASSDR 08FDEA04250Skin · corrodedNR 2 PYLON O/B FWD. 311N5193-3 SKIN PANEL HAS CORROSION ON INNER SURFACE. REMOVED HINGE TO GAIN ACCESS TO REMOVED SKIN PER SRM 51-40-02, INSTALLED AFT T/R HINGE PER SRM 51-401-02. REMOVED FWD SKIN P/N 311N5193-2 PER SRM 51-40-02, REMOVED CORROSION PER SRM 54-SDR 08FDEA04234Skin Panel · corrodedNR 2 PYLON I/B FWD SKIN PANEL ASSY, HAS CORROSION ON INNER AND OUTER SURFACE. REMOVED AND REPLACED NR 2 PYLON I/B FWD SKIN PANEL ASSY IAW SRM 51-40-02 AND DRAWING 311N5002. CORROSION DETERMINED TO BE OUT OF LIMITS IAW SRM 54-50-01. THIS REPAIR IS CLASSIFIEDSDR 08FDEA04233Skin Panel · corrodedNR 2 PYLON I/B AFT SKIN PANEL, 311N5046-33, HAS CORROSION ON INNER SURFACE. REMOVED AND REPLACED NR 2 PYLON I/B AFT SKIN PANEL IAW SRM 51-40-02 AND DRAWING 311N5002. CORROSION WAS DETERMINED TO BE OUT OF LIMITS IAW SRM 54-50-01. THIS REPAIR IS CLASSIFIED ASDR 08FDEA04232Skin Panel · corrodedNR 1 PYLON LT SKIN, INNERWALL IS CORRODED JUST FWD OF PRE-COOLER. REMOVED AND REPLACED LT SKIN PANEL ASSY IAW SRM 51-40-02 AND DRAWING 311N5002 AND EA F-5450-121408. CORROSION WAS DETERMINED TO BE OUT OF LIMITS IAW SRM 54-50-01. THIS REPAIR IS CLASSIFIED AS SDR FDEA200810034185Panel · corrodedNR 2 PYLON PNL 443 FR CUT OUT HAS SURFACE CORROSION. BLENDED AREA IAW 54-50-71 CHECKED LIMITS, FOUND TO BE OUT OF LIMITS IAW SRM 54-50-71 FIG 101 DETAIL IV. REMOVED MACHINE DOUBLER IAW SRM 51-40-02. REPLACED MACHINE DOUBLER IAW SRM 51-10-02. FABRICATED DOUSDR DL757081288Skin · damagedDURING A SKIN REPAIR PER THE SRM, SEVERAL FASTENER HOLES WERE MISDRILLED IN VARIOUS LOCATIONS AS NOTED IN ER/A 06-362852-14. THE ER/A PROVIDED REPAIR INSTRUCTIONS. NOTE: AT THE TIME OF ER/A ISSUE, AN MRR WAS NOT SUBMITTED. THIS SUBMITTAL CORRECTS THIS SITUSDR 08FDEA04185Doubler · corrodedNR 2 PYLON PANEL 443 FRAME CUT OUT HAS SURFACE CORROSION. BLENDED AREA IAW 54-50-71 FOUND TO BE OUT OF LIMITS IAW SRM 54-50-71. REMOVED MACHINE DOUBLER IAW SRM 51-40-02 REPLACED DOULBER IAW SRM 51-10-02.SDR 08FDEA04177Skin Panel · corrodedNR 2 PYLON TORQUE BOX INTERNAL SKIN HAS CORROSION AT LWR CHORD ATTACHMENT ON SEVERAL LOCATIONS. REMOVED AND INSTALLED HINGE BRACKET PER SRM 51-40-02. REMOVED AND INSTALLED HEATSHIELD PER SRM 51-40-02. REMOVED AND INSTALLED FWD. FAIRING PER SRM 51-40-02. REMOSDR KCSA081500Skin · damagedNR 2 PYLON INBD LOWER SKIN DAMAGED AT NAC STA 194. (K)SDR KCSA081499Skin · damagedNR PYLON OTBD SKIN LOWER FASTERNER HOLES DAMAGED AT NAC 221.9. (K)SDR ASOA200801318Skin · corrodedRT ENG LIPSKIN HAS CORROSION ON L/E IN SEVERAL AREAS. COMPLIED WITH CMM 71-61-01-200-802-A01. PERFORMED ULTRASONIC INSPECTION OF RT NOSE INLET LIPSKIN IAW WVAC. FOUND RT NOSE INLET LIPSKIN TO BE WITHIN LIMITS. REQUIRES BLEND IN PITTING AREAS. BLENDED RT SDR 2008UALA05896Skin · crackedNR 2 STRUT, ONBOARD AFT SKIN CRACKED AT PANEL CUTOUT RADIUS, FORWARD OF AFT BULKHEAD. MAJOR REPAIR ACCOMPLISHED. STOP-DRILLED CRACK. VERIFIED HFEC. INSTALLED -1 & -3 DOUBLERS.SDR FDEA200809234006Skin · corrodedNR 1 PYLON OTBD AFT 311N5046-31 SKIN PANEL ASSY HAS CORROSION ON INNER SURFACE. REMOVED AND INSTALLED STRIKER PLATE AND MOUNT FITTING IAW SRM 51-40-02 AND DWG 311N5108. REMOVED AND INSTALLED HEAT SHIELD IAW SRM 51-40-02. REMOVED AND INSTALLED FWD FAIRING IASDR 08FDEA04006Skin · corrodedNR 1 PYLON O/B AFT 311N5046-31 SKIN PANEL ASSY HAS CORROSION ON INNER SURFACE. REMOVED AND INSTALLED STRIKER PLATE AND MOUNT FITTING PER SRM 51-40-02 AND DRAWING 311N5108. REMOVED AND INSTALLED HEAT SHIELD PER SRM 51-40-02. REMOVED AND INSTALLED FWD FAIRINGSDR UIE2008F00032Skin · crackedFOUND NR 3 ENGINE RT CORE COWL LOWER FACE CRACKED. 0.3 INCH AT NAC STA 288. REPAIRED IAW FORM NR E8207.4. (K)SDR 08FDEA03882Panel · chafedNR 3 PYLON PANEL 487 HR IS CHAFED AND HAS BARE METAL. BLENDED AREA IAW SRM 54-00-01; VOL I. ORIGINAL MATERIAL THICKNESS, 0.071 IAW SRM 54-51-01; VOL III. MATERIAL LOSS 0.020. REMAINING THICKNESS 0.051. FOUND TO BE OUT OF LIMITS IAW SRM 54-00-01;VOL I. FASDR 08FDEA03842Panel · chafedNR 1 PYLON PANEL 738 GL IS CHAFED AT THE MATING SURFACE. FABBED REPAIR PARTS IAW EA 8-5480-123637 & SRM 54-00-01. ALODINED & PRIMED FILLERS IAW SRM 51-21-01. INSTALLED REPAIR PARTS PER EA 8-5480-123637 & SRM 54-00-01.SDR DL764081161Panel · missingNR 1 ENGINE NACELLE STRUT ACCESS DOOR MISSING.SDR 08FDEA03749Skin · tornTORN SKIN NR 1 ENGINE INLET COWL 4 O`CLOCK POS INBD SIDE AT COWL ATTACH LIP. CUT OUT DAMAGED AREA DIMS 1 1/2" BY 1" IAW SRM 51-10-1. FABRICATED DOUBLER REPAIR AND FILLER IAW SRM 54-30-3 FIG 3A. INSTALLED REPAIR PARTS IAW SRM 51-30-2 AND 54-30-3 FIG 3A.SDR C8GA20080034Nose Cowl · dentedWHILE IN HEAVY MAINTENANCE PERFORMING VISUAL INSPECTION ON THE NR 1 ENGINE NOSE COWL A DENT WAS NOTED AT THE 1 O'CLOCK POSITION. EVALUATED DENT AND FOUND A/Y RATIO OUT OF LIMITS. CUT OUT DAMAGED AREA AND FABRICATED INTERNAL DOUBLER OF 2024 T3 .040, FABRACATED SDR 08FDEA03715Panel · damagedNR 2 PYLON APRON HAS EDGE DAMAGE AT THE FWD END WHERE THE LT FAN COWL MATES. REPAIRED NR 2 FAN COWL LT APRON IAW E.A. 8-5480-123629.SDR 08FDEA03700Panel · crackedNR 3 PYLON PANEL 488 DL IS CRACKED. FABRICATED THE REPAIR DOUBLER IAW SRM 54-00-1 VOL I. INSTALLED DOUBLER IAW SRM 51-31-01 VOL II & SRM 54-00-01 VOL I.SDR 08FDEA03699Panel · chafedNR 3 PYLON PANEL 488 GL IS CHAFED AT & AROUND THE FASTENER HOLES. BLENDED CHAFED AREAS, FOUND TO BE OUT OF LIMITS IAW SRM 54-00-01. FABRICATED IAW EA 8-5480-123637 & DWG AUB 7036 EV W.SDR 08FDEA03698Panel · crackedNR 1 PYLON PANEL 438 CL IS CRACKED. FABBED A REPAIR DOUBLER & INSTALLED DOUBLER REF SRM 54-00-01 VOL I.SDR 08FDEA03697Fairing · chafedNR 1 PYLON PANEL 438 FL IS CHAFED AT THE FWD END. REMOVED DAMAGE IAW SRM 54-00-01; VOL I.SDR FDEA200808253579Skin · corrodedNR 2 PYLON INTERIOR SURFACE BETWEEN PANELS 443 AR AND 443 BR HAS LIGHT CORROSION. REMOVED AND REPLACED NR 2 PYLON OTBD SKIN PANEL PN 311N5046-32 IAW DWG 311N5002 AND SRM 51-40-02, CATEGORY A MAJOR REPAIR NO FOLLOW-UP TRACKING REQUIRED .SDR FDEA200808253578Skin · corrodedNR 1 PYLON OTBD FWD 311N5193-1 SKIN PANEL HAS CORROSION ON INNER SURFACE. REMOVED AND REPLACED SKIN PAANEL IAW SRM 51-40-02, AND DWG 311N5002, 311N5108. (CATEGORY A MAJOR REPAIR, NO FOLLOW-UP TRACKING REQUIRED)SDR CA080826006Skin · cracked(CAN) DURING A WALKAROUND, THE LT NACELLE SKIN PANEL 85410587 DISPLAYS A SMALL CRACK FROM ONE OF THE UPPER AFT FASTENERS TO THE SKIN EDGE, AND A LARGE 4 INCH+ CRACK RUNNING ALONG THE LENGTH OF THE SKIN PANEL. AS THE SKIN PANEL IS NOTED AS BEING BULGED OVER APPSDR DL757081265Skin · damagedONE EACH HOLE IS OVERSIZED TO .437 ON NR 1 PYLON I/B SIDE. REPAIR C/W PER ERA 469688-14 DATED 9/10/08.SDR 08FDEA03579Skin Panel · corrodedNR 2 PYLON INTERIOR SURFACE BETWEEN PANELS 443 AR AND 443 BR HAS LIGHT CORROSION. REMOVED AND REPLACED NR 2 PYLON O/B SKIN PANEL P/N 311N5046-32 IAW DWG 311N5002 AND SRM 51-40-02, CATEGORY A MAJOR REPAIR NO FOLLOW-UP TRACKING REQUIRED .SDR 08FDEA03578Skin Panel · corrodedNR 1 PYLON O/B FWD 311N5193-1 SKIN PANEL HAS CORROSION ON INNER SURFACE. REMOVED AND REPLACED SKIN PANEL IAW SRM 51-40-02,AND DWG. 311N5002, 311N5108, CATEGORY A MAJOR REPAIR, NO FOLLOW-UP TRACKING REQUIRED.SDR 08FDEA03550Panel · crackedTHE NR 1 ENGINE PYLON PANEL NR 475 AL HAS A 3/8 INCH CRACK AT THE RADIUS. COMPLIED WITH FEDEX EA 6-5480-123386 "NACELLES/PYLON, NR 1 ENGINE PYLON 475 AL EQUIPMENT ACCESS PANEL ASSY, CRACK WELD REPAIR".SDR 2008UALA05410Skin · gouged21AUG ORD CF -T : NR 2 ENG RIGHT SIDE FAN COWL GOUGED APPROX 3 INCHES FROM REAR ABOUT 3 O'CLOCK POSITION. ACCOMPLISHED INTERIM REPAIR PER UA-EVA-71852, NO DELAMINATION PRESENT & APPLIED SPEED TAPE. RECHECK REPAIR AT NEXT A01 CHECK, REPAIR WITHIN 500 FLIGHT HSDR ASAA0843417Skin · damagedRT ENGINE INLET COWL LIP SKIN AT 6 O'CLOCK POSITION MULTIPLE SCRATCHES. REPAIRED IAW GRO8617 AND EA.SDR NWAA083725502Skin · crackedDURING NR1 ENG CHANGE FOUND CRACK IN PYLON SKIN AT NAC STA 132. REPAIRED PER IA 55-213789 SECT I. SECT II REQUIRES PERMANENT REPAIR TO BE ACCOMPLISHED WITHIN 24 MONTHS OR 3000 CYCLES AFTER SECTION 1. (S)SDR 2010FA0000360Skin · worn(KADY) WEAR DAMAGE WAS FOUND ON THE CAP SKIN OF THE NR 4 PYLON AT NAC STA 210.00-221.90 NAC WL 187.63-190.68.SDR 2010FA0000359Skin · worn(KADY) WEAR DAMAGE WAS FOUND ON THE CAP SKIN OF THE NR 1 PYLON AT NAC STA 210.00-221.90 WL 187.63-190.60.SDR CNMA20090033Panel · damagedPYLON NR 2 PANEL, 457BT DAMAGED. REPAIRED IAW SRM 54-00-01, FIG 1A SHEET 1 REV 94 VOL J.SDR KCSA081367Skin · damagedNR 4 PYLON INBOARD LOWER SKIN DAMAGED AT NAC STA 215. (S)SDR KCSA081365Skin · crackedNR 3 PYLON SKIN OUTBOARD SIDE EXTENDING FROM DOUBLER CRACKED 3 INCHES. (A)SDR 08FDEA03080Panel · wornNR 3 PYLON PANEL 437 DL HAS ELONGATED HOLES. REPAIRED PANEL 437 DL IN REF TO EA 8-5480-116998 P/N AUB 7038-7.SDR 08FDEA03031Panel · crackedNR 1 PYLON PANEL 437 DR INNER SKIN IS CRACKED. RECEIVED NEW PRECOOLER VENTILATOR ASSEMBLY P/N AUB 7054-501, PO 626793.1. LOCATED AND DRILLED IN REF TO DC/MD-10 SRM 51-31-01; VOL II AND DAC DWG AUB 7054; REF "J".SDR 08FDEA03030Skin · crackedNR 1 PYLON PANEL 437 DOOR SKIN IS CRACKED AT A FASTENER HOLE. 3 1 PYLON PANEL 437 DOOR WAS REPLACED ON N/R N00808. SEE SDR TRACKING NR 08-3031 FOR THE DETAILED INFORMATION.
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