JASC 5410
Service difficulty reports · 4,119
Reports filed under 5410 · Nacelle/Pylon, Main Frame, 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 = '5410' 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 = '5410' 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 DHL2007793023Duct · crackedCRACK AT "S" INSIDE DUCT INLET 7 O'CLOCK POSITION BS 1130. REMOVED PREVIOUS REPAIR AND FILLER ON "S" DUCT AT 7 O'CLOCK POSITION BS 1130 IAW SRM 51-30-2 FIGURE 1. REMOVED FRAME IAW SRM 51-30-2 FIGURE 1. FABRICATED NEW FILLER FRAME. FABRICATED REPAIR DOUBLERSDR DHL2007793004Duct · crackedCRACK AT "S" INSIDE DUCT INLET, 6 O'CLOCK POSITION BS 1130. REMOVED FASTENERS FOR ACCESS IAW SRM 51-30-2 FIGURE 1. CUT OUT DAMAGE AREA 1" BY .75" ON "S" DUCT SKIN. CUT DAMAGE AREA ON STRAP 1" BY 15.25" IAW SRM 54-10-2 FIGURE 10. FABRICATED FILLER AND FABRISDR UIEA200700478Cowling · crackedNR 3 ENG I/B CORE COWL UPPER AFT EDGE WHERE COWL SITS AGAINST FIRE SEAL FINGERS, 5 INCHES LONG CRACK WITH 4 PULLED FASTENERS. UNDERSIDE GOUGED.SDR QXEA200701799Diaphragm · crackedPDX - C4 CHECK - RIGHT NACELLE OUTBOARD DIAPHRAM CRACKED. FABRICATED NEW SUPPORT ANGLES AND INSTALLED NEW SUPPORT ANGLE. PRIMED AND PAINTED AREA.SDR P5CA0701540Access Door · inflt separationNR 4 ENGINE STRUT I/B ACCESS DOOR PARTIALLY LOST IN FLIGHT AND NR 4 ENGINE STRUT O/B ACCESS DOOR PEELED BACK IN FLIGHT. MAJOR REPAIR AND PARTS REPLACEMENT ACCOMPLISHED PER XEO-51-120607, P/N: 323U2304-84, 323U2303-72.SDR UIEA200700473Acoustic Panel · crackedDURING A CHECK INSPECTION, NR 2 ENGINE NOSE COWL, VISUALLY FOUND AFT INNER SKIN OF ACOUSTIC PANEL CRACKED THREE PLACES (AS VIEWED WITH COWL OPEN): 6 O'CLOCK/8 INCHES LONG; 06:45 O'CLOCK/11 INCHES LONG; 7 O'CLOCK/15 INCHES LONG. APPLIED INTERIM REPAIR IAW SRM SDR 07FDEA04785Flange · delaminatedNR 1 ENGINE UPPER COWL T/E FLANGE IS CHIPPED AND DISBONDED REMOVED NR 1 ENGINE UPPER COWL T/E FLANGE, LOCATED AND DRILLED NEW FLANGE. INSTALLED NEW FLANGE, REF SRM 51-30-2 PG 1-4 REF DWG 65-19508.SDR 07FDEA04779Bushing · misalignedNR 1 PYLON LOWER SPAR FITTING 311N5024-3 ASSY HAS 2, 311N5058-22 BUSHINGS WITH THE INTERNAL BORE NOT PERPENDICULAR TO THE FITTING. REMOVED BUSHINGS 2 PER SRM 54-50-90. CHECKED LUG PER NTM 51-00-13, NO DAMAGE FOUND. LUG HOLE DIAMETER 1.531". FABRICATED 2 NESDR UIEA200700468Structure · erodedNR 2 ENGINE LT FAN COWL L/E HAS 78.0 INCH AREA OF EROSION AT L/E. PERMANENT REPAIR ACCOMPLISHED AS PER B747-400 SRM 54-21-01, REPAIR 6. REFERENCE ATLAS EO NR 4471A009.SDR 2007UALA04633Structure · crackedNR 2 PYLON FUEL LINE CUTOUT FWD INBOARD ATTACH HOLE CRACKED.SDR CO1Y200700008Hinge · out of limitsON FWD AND AFT CORE COWLS HINGES HAVE BEEN FOUND HOLES OUT OF DWG LIMITS.SDR CA071025011Cowling · loose(CAN) ACTUALLY WE HAVE A AOG A/C AT PRG. DURING THRUST REVERSER OPERATING AFTER TOUCHDOWN AT PRG WE’RE LOSING THE UPPER AND LOWER RT ENGINE COWLINGS. ONE OF THE COWLINGS HIT THE A/C AT FS 700 IN BETWEEN STR 5 TO 7 AND DAMAGED THE FUSELAGE AND ALSO THE FRAME FSSDR F3LA200700267Fairing · crackedDURING C-3 CHECK, INSPECTION REPORTED APPROX A 2 1/2 INCH CRACK ALONG BOTTOM SECTION OF LT ENGINE INBD PYLON PANEL (ABOVE PANEL NR 473AR). REMOVED LATERAL FAIRING ASSY FROM LT ENG I/B SIDE IAW A319 MM 54-57-22-010-050. TRANSFERRED FASTENER HOLES AND NUT PLATSDR SWIA200718728Rod · unsecureFLT 3923 - LEFT THRUST LEVER WOULD NOT PULL BACK. SECURED UPPER CORE COWL SUPPORT ROD INTO STOWED POSITION. PERFORMED ENGINE RUNS WITH NO BINDING NOTED.
SDR UPS07M51231Web · scratchedINSPECTION TYPE:C PYLON NR 3 WIRING SUPPORT WEB WITH SCRATCHES ABOVE PRECOOLER. REMOVAL C/OUT TO ACCESS SCRATCHES MARK MENTIONED ABOVE, FOUND EXCEEDED LIMIT PER SRM 54-00-01,F1A, V1, .ORI THK 0.032", REMAIN THK 0.012". NEW WEB AT NR 3 PYLON FAB PER P/N AUB7SDR KCSA071408Stiffener · dentedNR 2 PYLON NAC STA 219 LOWER SPAR STIFFENER DENTED AND GOUGED.SDR 07FDEA04269Angle · crackedNR 2 ENG INLET DUCT HOUSING FRAME-TO-LEADING EDGE OF VERTICAL STAB ATTACH CLIP ON RT SIDE IS CRACKED LOCATED AT STA 1233 REMOVED CRACKED ATTACH CLIP, FABRICATED NEW CLIP AND INSTALLED. REF BOEING DOCUMENT NR 69-14476/ID NR 0001/ITEM NR 14/FRAME 1 OF 2 AND SRMSDR A6WA200740516Attach Fitting · damagedRIGHT ELEVATOR NR 3 HYD SYSTEM PCU ATTACHMENT FITTING ASSY ON ELEVATOR, P/N 601R24056-41, HAS SHEARED LOCK FASTENER AT BOTTOM OF LINK. 10-25-07 MAINTENANCE REPLACED LOCK FASTENER IAW SRM 51-42-21. (M)SDR QXEA200701462Support Bracket · chafedC5 PDX - RIGHT NACELLE INBOARD FRAME SUPPORT BRACKET CHAFED. REPAIRED IAW SRM 51-20-51, RD8-54-2397.SDR 07FDEA03889Spar · corrodedCORROSION FOUND ON THE UPPER SURFACE OF THE LT PYLON LOWER SPAR BETWEEN RIBS 4-8, FURTHER TO HYDRAULIC FLUID CONTAMINATION. REPAIR PERFORMED BY BLENDING OUT CORROSION, CUTTING OUT THE MOST DAMAGED AREAS AND INSTALLING A DOUBLER TO REINFORCE THE AREA IAW EA SDR DU4R2007167Fitting · wornFOUND DEEPLY WORN CORNER FITTING OF NR 1 PYLON LT AFT LOWER CORNER AT AFT ENGINE MOUNTS. REPAIRED BY BLENDING, HFEC NO RELEVANT INDICATIONS, FABRICATING AND INSTALLING REPAIR GUSSET 4.34" BY 2.88" BY 1.2" FROM 7050-T7451 IAW DELTA EA NR 463490-14AD DATED 9/12SDR 07FDEA03497Structure · crackedFOUND CRACKED PICK UP MEMBER ON PYLON NR 2. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 54-54-11.SDR DL76P071178Door · missingFOUND BY MTC ON PDC WALK AROUND FOUND NUMBER 2 ENGINE PYLON INBOARD NACELLE STRUT ACCESS DOOR MISSING FWD TO CDL PER 54-53-03 NEEDS DOOR MFG 311T3065-127. REPLACED ACCESS DOOR, MCO/PLACARD REMOVED.SDR 07FDEA03269Plate · damagedDAMAGED CORNER SECTION AT RT PYLON AFT MOUNT FITTING REPAIR PERFORMED BY BLEND OUT TO SMOOTH PROFILE AND NDT INSPECTION FOR CRACK FREE IAW EA 6-5720-99222 AND RAS/BAE/1002436/2006 ISSUE A.SDR TAMF20070023SCowling · damagedDURING C CHECK INSPECTION WAS FOUND CORE COWL P/N: 224-2301-513 S/N: 0130 WITH ELONGATED HOLE AT FRAME STA NAC 294 - CF6-80C2. DAMAGED AREA WAS REPAIRED IAW CV07-1781-01 AND EWO 767-54-020. THIS REPAIR CONSTITUTES A MAJOR REPAIR.SDR UIEA200700320Door · puncturedNR 1 PYLON OUTBOARD TRAILING EDGE DOOR INNER FACE PUNCTURED BY HOLD OPEN ROD WHEN DOORS ARE CLOSED 1.5 BY 1.5. PERM REPAIR CARRIED OUT IAW SRM 51-40-20 PAGE 1 250 DEGREES F.SDR QXEA200701249Support Angle · crackedC5 PDX - LEFT NACELLE AT STATION YW139.200 AND XN209.00 AND ZN8.00. THERE IS A CRACK THROUGH THE LOWER AFT FASTENER HOLE IN THE VERTICAL SUPPORT ANGLE FOR LEFT NACELLE SKIN. REPAIRED IAW RD8-54-1726.SDR TAMF20070014SFairing · crackedDURING C-CHECK INSPECTION WAS FOUND NR 2 NACELLE STRUT NR 446CL ACCESS PANEL DELAMINATED AND CRACKED. ACCESS PANEL WAS FABRICATED AND INSTALLED IAW MFG SERVICE REQUEST 1-50853397 AND DRAWING 015T0563-8.SDR DHL2007746510Cowling · damagedDURING AN "C" CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED, REF NR 098958 NR 1 ENG NOSE COWL EXTERIOR SKIN AT 9 O'CLOCK POSITION HAS 3 INCH CRACK FROM RIVET HEAD FWD. CUT OUT DAMAGED AREA ON NR 1 ENG NOSE COWL EXTERIOR SKIN 9 O`CLOCK POSITION 3" BY 2" IAW B7SDR DL757071002Bushing · migratedTHE DIAGONAL BRACE WING END FITTINGS OF BOTH THE NR 1 AND NR 2 PYLONS WERE FOUND WITH MIGRATED BUSHINGS DURING ACCOMPLISHMENT OF 6-75079-3. NEW BUSHINGS WERE INSTALLED AS AN AMOC TO AD 2003-18-05.SDR AMWA06032BStructure · chafedFRICTION CHAFING DURING OPERATION HAS CREATED WORN SEGMENTS ON THE RT ENGINE NACELLE. DAMAGE WAS ALONG THE ENTIRE LENGTH OF THE NACELLE SHAPE: DEPTH VARIED AS INDICATED ON THE REPAIR AUTHENTICATION. REPAIRED IAW ACFT ENGINEERING REPORT 6799-2 REV 1R.SDR AMWA06032AStructure · chafedFRICTION CHAFING DURING OPERATION HAS CREATED WORN SEGMENTS ON THE LT ENGINE NACELLE. DAMAGE WAS ALONG THE ENTIRE LENGTH OF THE NACELLE SHAPE: DEPTH VARIED AS INDICATED ON THE REPAIR AUTHENTICATION. REPAIRED IAW ACFT ENGINEERING REPORT 6799-2 REV 1R.SDR WRNA200700053Support · crackedDURING M-96 CHECK, A 3 INCH CRACK WAS FOUND IN THE NR 2 ENGINE OUTBOARD CORE COWL SUPPORT. ACCOMPLISHED WELD REPAIR IAW ENGINEERING ORDER 2-54907-800 FROM EMTEQ.SDR 07FDEA02519Stiffener · crackedNR 1 PYLON HAS 6" CRACK VERTICAL STRUCTURE SUPPORT ON OUTBOARD BULKHEAD. VIEWED THROUGH ACCESS PANEL AUB7025-3 APPROXIMATE 4 FEET FWD PYLON STATION YN=358. [08-24-07] REMOVED AND REPLACED STIFFENER BRACKET AS REQUIRED, REF. DAC DRAWING AUB 7087. 09-04-07 SDR UIEA200700265Door · delaminatedNR 1 ENGINE RT STRUT TRAILING EDGE FAIRING DOOR, PANEL NR 454AR, FORWARD LOWER CORNER HAS AN AREA OF 7.0 INCH BY 10.0 INCH AREA OF DELAMINATION. ACCOMPLISHED PERMANENT REPAIR AS PER 747-200 SRM 51-40-06 FIG 4, SHEET 1 AND 747-200 SRM 51-40-20. ALSO, REF: ATLSDR DHL2007784521Nose Cowl · crackedNR 3 ENGINE NOSE COWL INTERNAL TAI DUCT SUPPORT BRACKET BROKEN AT APPROX 8 O`CLOCK POSITION, NAC STA 77.5, NAC LBL 28, NAC WL 180. CUT ACCESS HOLE IN NOSE COWL AT 9 O`CLOCK POSITION TO FOM 6 IN DIA IAW B727 SRM 54-30-3, FIG 3. REMOVED BROKEN SUPPORT BRACKET SDR AC2A116357Cowling · burnedCOWLING WAS FOUND BURNED DURING EXHAUST BRACKET REPLACEMENT. BURNED AREA WAS APPROXIMATELY (2) INCHES BY (3) INCHES. COWLING WAS REPAIRED AND RETURNED TO SERVICE. ALL OTHER AIRCRAFT IN FLEET WERE INSPECTED AND FOUND OK PHOTO OF COWLING HAS BEEN SENT TO FSDOSDR QXEA200701111Frame · crackedC3 OKC - RIGHT LOWER TRANS COWL CENTER FRAME CRACKED ON OUTBOARD SIDE. REPAIRED IAW REO670-54-21-814.SDR QXEA200701049Cowl Door · crackedC4 - PDX NR 2 RIGHT SIDE ENGINE FORWARD INBOARD SIDE COWL DOOR 423AL HAS A CRACK ON THE UPPER STIFFENER FOR THE OIL ACCESS DOOR. REPLACED IAW DHC-8-200 SRM 51-40-11.SDR AMWA31034BStructure · damagedFRICTION CHAFING DURING OPERATION HAS CREATED WORN SEGMENTS ON THE LT AND RT ENGINE NACELLES. DAMAGE WAS ALONG THE ENTIRE LENGTH OF THE NACELLE SHAPE, DEPTH VARIED AS INDICATED ON THE REPAIR AUTHORIZATION. REPAIRED IAW AIRCRAFT ENGINEERING REPORT NR 6732-1 SDR DHL2007740011Nose Cowl · damagedNR 1 ENG NOSE COWL AT O/B SIDE 9 O`CLOCK POSITION HAS EXISTING REPAIR PULLING LOOSE AND CHAFF MARK. REMOVED PREVIOUS REPAIR IAW B727 SRM 51-30-2 FABRICATED NEW REPAIR USING 2024-T3 .040 PO#9005138 DIM 9" BY 4" AND FILLER USING 2024T3 .032 PO NR 9005049 DIM 5"SDR HNAA0700204Heat Shield · corrodedHEAT SHIELD PANEL AND STRAP AFT NACELLE STRUCTURE CORRODED. LEFT NACELLE FABRICATED PER DRAWING 85410741, 85411027 INSTALLED PER SRM 51-40-00.SDR QXEA200700946Diaphragm · crackedC4 PDX - LEFT NACELLE OUTBOARD DIAPHRAGM CRACKED. REPAIRED IAW SRM 51-42-05 AND 51-40-15.SDR 07FDEA02021Stiffener · crackedENG NR 1 AFT LOWER PYLON INNER COMPARTMENT AT FLOOR AREA,RIB NR 14 "C"-CHANNEL SUPPORT HAS A CRACK VISIBLE THRU OPEN ACCESS NR 473 AL. REMOVED AND REPLACED STIFFENER IAW SRM 51-40-21 AND 51-40-00.SDR QXEA200700882Diaphragm · damagedC4 PDX - THE NR 1 NACELLE HAS SMOKING FASTENERS ON THE OUTBOARD AFT DIAPHRAGM. REPAIRED IAW RD8/4-54-154, EO 6-54-441, AND SRM 51-42-05.SDR QXEA200700885Diaphragm · crackedC4 PDX - NR 1 ENGINE NACELLE DIAPHRAGM CRACKED. REPAIRED IAW SRM 51-42-05, 51-40-10.SDR TRAX200700723Cowling · departedNR 2 ENG FAILURE AT 32,000 FT, LOUD BAM WAS HEARD NR 2 THRUST LEVER SLAMMED TO IDLE. A/C YAWED TO THE LT, SEVER VIBRATION BEGAN IMMEDIATELY, UNABLE TO SECURE ENGINE, EMERGENCY DECLARED. EN ROUTE TO ATL A/C DIVERTED TO TRI DUE TO MTC. UPON GROUND INSPECTION SDR 07FDEA01865Fairing · crackedNR 1 PYLON TO NACELLE FILLET FAIRING IS CRACKED LENGTH 2.5 IN LT SIDE STA 683/RIB6. INSTALLED NEW FILLET FAIRING IAW SRM 51-40-21.SDR QXEA200700857Support Angle · crackedC4 OKC - 2 ENGINE TRANS COWL SUPPORT ANGLE BEHIND 2ND FROM END LATCH IS CRACKED. REPAIRED IAW REO670-78-800, AND SRM 51-42-13.SDR DHL2007788526Nose Cowl · wornWHILE IN C CHECK AT FLIGHT STAR, NR 1 ENG NOSE COWLING 9:00 POS AFT END COWLING FAYING SURFACE IS WORN AWAY AND KNIFE EDGED. CUT OUT DAMAGED AREA ON NR 1 ENGINE NOSE COWLING AFT END 9:00 POSITION IAW B727 SRM 54-10-03 FIG3. CUTOUT AREA 5" BY 75", FABRICATED
Back to JASC 5410