JASC 5420

Service difficulty reports · 3,949

Reports filed under 5420 · Nacelle/Pylon Miscellaneous Structure, 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 = '5420'
  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.

SDR QXEA200800268Panel · chafedPDX - C4 - PANEL 414AR UPPER AFT SECTION IS CHAFED. REPAIRED CHAFED AREA IAW RD8/4-54-012, Q400 NDTM PART 6 51-00-01.Feb 28, 2008 · N408QX · Bombdr DHC8402SDR KCSA081128Stiffener · crackedNR 2 PYLON INTERNAL O/B STIFFENER CRACKED .5 INCH AT ATTACH ANGLE NAC STA-130.Feb 28, 2008 · N715CK · Boeing 747209BSDR KCSA081127Angle · crackedNR 3 PYLON NAC STA-130 RT UPPER T-CHORD CRACKED .75 INCH.Feb 28, 2008 · N715CK · Boeing 747209BSDR 08FDEA00575Support Angle · corrodedNR 2 PYLON, ACCESS PANEL 484 BR CUTOUT, 2 AFT VERTICAL SUPPORT ANGLES HAVE CORROSION AROUND THE NUTPLATES AND FASTENER HOLES. REMOVED AND REPLACED GUSSET IN REF TO SRM 51-40-21; PG 7.Feb 22, 2008 · N803FD · Airbus A310324SDR 08FDEA00512Stiffener · crackedNR 1 ENG UPPER COWL STIFFENER CRACKED BETWEEN 2ND AN 3RD LOWER LATCH CUTOUTS. REMOVED SEAL AND SEAL RETAINER, REMOVED CRACKED COWL STIFFENER, VERIFIED MATERIAL ID. FABRICATED NEW COWL STIFFENER, TREATED AND PRIMED, INSTALLED NEW COWL STIFFENER. REINSTALLED Feb 19, 2008 · N486FE · Boeing 727227SDR KCSA081088Stiffener · crackedNR 3 PYLON LT UPPER STIFFENER CRACKED AT ATTACH POINT OF THE FWD ENG MOUNT BULKHEAD INTERNAL ANGLE. Feb 19, 2008 · N747CK · Boeing 747221FSDR KCSA081087Stiffener · crackedNR 3 PYLON RT UPPER STIFFENER CRACKED AT ATTACH ANGLE OF THE FWD ENG MOUNT BULKHEAD INTERNAL ANGLE.Feb 19, 2008 · N747CK · Boeing 747221FSDR USAA920080531Stiffener · crackedMCN - MAJOR REPAIR - C12 CHECK - CRACKED STIFFENER ON NR 1 PYLON STRUT, PYLON STATION 153.90. REPLACED STIFFENER ON NR 1 PYLON STRUT, PYLON STATION 153.90 IAW B757 SRM 51-40-02.Feb 18, 2008 · N901AW · Boeing 7572S7SDR HALA0800324Channel · corrodedLEVEL 1 CORROSION NR 1 ENGINE SEVEN PLACES ON LOWER COWL CHANNEL NEAR GUIDE PIN HOLES. REPAIR IN WORK.Feb 18, 2008 · N479HA · Boeing 717200SDR 08FDEA00507Fairing · damagedNR 1 PYLON LOWER FAIRING FWD LT ATTACH HOLES ARE ELONGATED. REMOVED SKIN PER SRM 51-40-21 PARA 6 & 7 DUE TO FASTENER HOLES ELONGATED BEYOND LIMITS PER SRM 54-55-51. FABRICATED UPPER LONGERON REPAIR SECTION & SPLICE PER SRM 54-55-51, FIG 207. ALODINED AFeb 18, 2008 · N684FE · Airbus A300F4605RSDR FDKA200802068Stiffener · damagedLEFT LOWER ENGINE COWLING HAS FRETTING DAMAGE TO THE AFT STIFFENER. THE DAMAGED STIFFENER HAS BEEN REMOVED AND REPLACED.Feb 17, 2008 · N836MJ · Emb EMB145LRSDR FDKA200802060Angle · chafedTHE O/B FRAME ANGLE, JUST AFT OF THE AFT HINGE, ON THE LT LOWER ENGINE COWLING IS CHAFED. THE DAMAGE HAS BEEN REPAIRED.Feb 14, 2008 · N836MJ · Emb EMB145LRSDR 08FDEA00428Intercostal · crackedNR 1 ENG LOWER COWL FWD END INTERCOSTAL CRACKED AND WORN MANUFACTURED AND INSTALLED NEW INTERCOSTAL FWD END OF NR 1 ENG COWL REF 65-19507 AND SRM 51-30-2.Feb 14, 2008 · N486FE · Boeing 727227SDR UIEA200800041Brace · wornNR 1 DIAGONAL BRACE FORWARD PORTION LOWER SURFACE PRIMER DISCOLORED. REPLACED DIAGONAL BRACE PER MM 54-10-03. Feb 12, 2008 · N526MC · Boeing 7472D7BSDR UIEA200800040Brace · wornNR 4 DIAGONAL BRACE FORWARD PORTION LOWER SURFACE PRIMER DISCOLORED. REPLACED DIAGONAL BRACE PER MM 54-10-03.Feb 12, 2008 · N526MC · Boeing 7472D7BSDR FDKA200801044Vent · chafedTHE LOWER VENT GRILL ON THE LT AND RT LOWER COWLING IS CHAFED OUT OF LIMITS. THE DAMAGED GRILL HAS BEEN REMOVED AND REPLACED.Jan 29, 2008 · N834MJ · Emb EMB145LRSDR UPS08M52108Fairing · damagedINSPECTION TYPE:C ENG NR 2 EXHAUST FAIRING RT SIDE WITH EXISTING PATCH REPAIR. FPI C/OUT ON EXISTING REPAIR IAW DACNDTSPM R.13 PART08 FOUND NO CRACK EVIDENT ON FAIRING SKIN & REPAIR DOUBLER. NEW REPAIR DOUBLER FAB USING 2219-0 0.071" PER EN 1123-08&MD11-54-2Jan 24, 2008 · N294UP · Doug MD11SDR 08FDEA00263Heat Shield · crackedPYLON NR 1 FWD ENG MOUNT, HEAT SHIELD CRACKED (MKD). REMOVED HEAT SHIELD NR 1 ENG PYLON IAW FEDEX A310-200 SRM 51-40-21 PAGE 1. RECEIVED NEW HEAT SHIELD P/N A2611501200200 S/N IC673554 PO 605041.1 FROM SUPPLY. INSTALLED NEW HEAT SHIELD IAW FEDEX A310-200 SJan 24, 2008 · N416FE · Airbus A310221SDR QXEA200800143Diaphragm · crackedPDX - C4 CHECK - RIGHT OUTBOARD DIAPHRAM HAS A SUSPECTED CRACK AT LOWER END NEAR LOCK FASTENER. REMOVED DIAPHRAM AND ASSOCIATED WEB IAW Q400 SRM 51-42-05. LOCATED AND DRILLED/DEBURRED AND INSTALLED FASTENERS COVERED BY AFT WEB AND INBOARD SOLID RIVETS IAW Q4Jan 19, 2008 · N405QX · Bombdr DHC8402SDR AA6WA200840030Separator · damagedQTY 1 SEPARATOR HAS FRETTING ON LT PYLON ACCESS PANEL 412DB. QTY (1) SEPARATOR REPLACED ON LT PYLON ACCESS PANEL 412DB IAW SRM 51-42-06. (K)Jan 18, 2008 · N428AW · Cndair CL6002B19SDR A6WA200840030Separator · corrodedQTY 1 SEPARATOR HAS FRETTING ON LT PYLON ACCESS PANEL 421DB. (K)Jan 18, 2008 · N428AW · Cndair CL6002B19SDR A6WA20084018ABracket · unknownRT ENGINE UPPER CORE COWL STA ROD PIN AND BRACKET (SPRING CLIP) FOUND. RT ENGINE UPPER CORE COWL STAY ROD PIN REPLACED AND BRACKET (SPRING CLIP) REPLACED IAW SRM 51-42-06. (K)Jan 17, 2008 · N428AW · Cndair CL6002B19SDR IXXA08SMN017SFlange · crackedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT COWLING AFT FLANGE CRACK STATION YN 181.000. REMOVED SPLICE CRACKED. FABRICATED SPLICE. CLEANED, TREATED AND PRIMED REPAIR PART INSTALLED REPAIR PART IAW DC8 SRM 51-1-21, DC8 SRM 54-3-2 FIGURE 33, BOEING MESSAGJan 15, 2008 · N41CX · Doug DC862FSDR A6WA200840042Angle · crackedONE ANGLE IS CRACKED ON LT PYLON ACCESS PANEL 412BT. ANGLE ON LT PYLON ACCESS PANEL 412BT, REPLACED IAW SRM 51-42-06. (K)Jan 14, 2008 · N428AW · Cndair CL6002B19SDR DL76L080015Angle · crackedNR 2 PYLON MIDSPAR CLOSEOUT ANGLES WER CRACKED AT THE MIDSPAR FITTINGS. THE ANGLE WAS REPLACED.Jan 8, 2008 · N191DN · Boeing 767332SDR 08FDEA00036Shim · misalignedNR 1 PYLON MID BULKHEAD O/B FWD LOWER SPAR HAS SHIM MIGRATION. REMOVED FWD O/B BOLT PER STEP 1.1 OF EA F-5450-110803 DATED 11/12/07. REMOVED AND REPLACED FWD O/B SHIM WITH NEW SHIM PER STEPS 1.2 THRU 1.6 OF EA F-5450-110803 DATED 11/12/07. REAMED FWD O/B Jan 4, 2008 · N903FD · Boeing 757200SDR 08FDEA00035Shim · misalignedNR 1 PYLON MID BULKHEAD INBOARD AFT AND FWD LOWER SPAR HAS SHIM MIGRATION. REMOVED FWD AND AFT I/B BOLTS PER STEP 2.1 OF EA F-5450-110803 DATED 11/12/07. REMOVED AND REPLACED FWD I/B SHIM WITH NEW SHIM. REMOVED AND REPLACED AFT I/B SHIM WITH NEW SHIM PER STJan 4, 2008 · N903FD · Boeing 7572B7SDR 2008UALA00065Brace · crackedNR 2 PYLON UPPER BRACE FUSE PIN SHOWS CRACK INDICATION IN SIDE INNER BORE. PERFORMED MAJOR REPAIR.Jan 3, 2008 · N532UA · Boeing 757222SDR 08FDEA00027Beam · corrodedNR 2 ENGINE PYLON AFT BEAM ATTACHMENT MOUNT HAS SEVERE RUST ON BOTTOM FACE OF MOUNT. CLEANED BEAM ASSY. IAW AMM 54-51-00-6.5 B-1. REMOVED CORROSION FROM BEAM SURFACE IAW 54-51-00-6.5 B-1 & SRM 51-74-10 ITEM 7 B-2, ITEM 5 A-5 & PMS 01-01-14-1. POLISHED REWORKJan 3, 2008 · N416FE · Airbus A310221SDR CA080102005Cover · cracked(CAN) FOUND EXHAUST SOOT IN COWLS. CLOSER INSPECTION FOUND THE BUTTERFIELD STC COVER PLATE LEAKING AND THE HEATED INLET CRACKED IN MULTIPLE LOCATIONS ON BOTH COWLS. (TC NR 20080102005)Dec 31, 2007 · Beech B200SDR 2007UALA05369Fitting · damagedNR 2 PYLON STRUT FITTING (DELTA FITTING) NEEDS TO BE FABRICATED.Dec 29, 2007 · N532UA · Boeing 757222SDR UPS08851466Drag Angle · crackedINSPECTION TYPE:C2 NR 1 PYLON INBOARD DRAG ANGLE CRACKED 1/4" PAST STOP DRILL. STOP DRILLED CRACK ON NR 1 PYLON DRAG ANGLE IAW EO DC8-5740-07164, CRACK DOES NOT EXCEED LIMITS OF 3" PER EO DC8-5740-07164.Dec 27, 2007 · N718UP · Doug DC871FSDR 07FDEA05144Bolt · shearedNR 3 PYLON, TOMBSTONE LOWER SPHERICAL BEARING ATTACH BOLT SHEARED AT 6 O'CLOCK POSITION, DOT NR 1. REMOVED AND REPLACED 6 BOLTS, P/N 77711-9-105, PLATE -P/N AUB7125-1, RETAINER P/N AUB7126-501 AND PLI WASHERS REF AMM 54-00-01-4.Dec 27, 2007 · N377FE · Doug MD1010FSDR DALA1145969202Fitting · damagedNR 1 AND NR 2 PYLON AFT TORQUE BOX BACK UP FITTING REPAIRED IAW ERA 465731-14.Dec 23, 2007 · N902DA · Doug MD9030SDR CALA0700777Splice Plate · crackedNR 2 PYLON LT SPLICE PLATE IS CRACKED AT NAC STA 345.28 AND NAC WL 118.95. REMOVED AND REPAIRED CRACKED SECTION ON NR 2 PYLON I/B SPLICE PLATE REF ECRA 5421-01016.Dec 21, 2007 · N12318 · Boeing 7373T0SDR MASA200700902Access Panel · departedASH FLT 7307 ORD - THE NR 2 ENG LOWER COWL DEPARTED THE AIRCRAFT AFTER LANDING. MX REMOVED AND REPLACED BLOCKER DOORS AND SUPPORT HINGES, OPS CHECK GOOD.Dec 18, 2007 · N75993 · Cndair CL6002B19SDR HNAA0800015Structure · crackedDURING INSPECTION, FOUND CRACKS IN THE NR 1 FORWARD RADIUS AT ABOUT 2 O’CLOCK AND NR 2 HORSE COLLAR FORWARD RADIUS AT THE 2 O’CLOCK AND 10 O’CLOCK POSITIONS. REPAIRED ALL THREE CRACKS PER RD8-54-2451 AND RD8-54-1736.Dec 7, 2007 · N914HA · Dhav DHC8102SDR USAA920071259Fitting · crackedCLT - MAJOR REPAIR-RON- NR 4214235/EO5407R146, CRACK AT NR 2 FASTENER HOLE (AFT INBD) OF NR 1 ENGINE DIAGONAL BRACE FITTING INSIDE PYLON EO 547R146. REPAIRED IAW EA100041.Dec 3, 2007 · N942UW · Boeing 7572B7SDR TRAX200701831Angle · crackedANGLE CRACKED UPPER PORT FIREWALL, RESOLVED ON W/O: 75891 TASKCARD: N/R-00584. ANGLE AT UPPER PART OF FIREWALL ON O/B SIDE OF RT ENGINE FABRICATED AS PER SRM 51-24-01 ANGLE AT UPPER PART OF FIREWALL ON O/B SIDE OF RT ENGINE REPLACED AS PER SRM 51-25-02.Nov 29, 2007 · N631AS · Aerosp ATR72212SDR 2007UALA04855Fitting · crackedNR 2 PYLON OUTBD MID SPAR FITTING AS SEEN FROM LWR INSIDE TORQUE BOX CRACKED AT 3 - 8INCHES BOLT I/B POSITION. MAJOR REPAIR ACCOMPLISHED: REMOVED FASTENER FROM CLOSEOUT ANGLE. VERIFIED CRACK BY HFEC. STOP DRILLED END OF CRACK. FABRICATED & INSTALLED A REPNov 27, 2007 · N662UA · Boeing 767322SDR 07FDEA04925Angle · chafedNR 1 PYLON THRUST LINK RUBBING AGAINST WING O/B THRUST ANGLE, STA YN348 CENTERED THRUST LINK, CLEANED AREA AROUND ATTACHMENT PIN & BUSHING, INSPECTED AREA OF BEARING & BUSHING IAW FEDEX WORK CARD 54X1201ALI-P1 LUBED THRUST LINK BEARING IAW FEDEX MM 12-21-02Nov 26, 2007 · N68054 · Doug MD1010FSDR MASA200700821Access Panel · departedASH 7160 - BHM-ORD, REPORTED AN UPPER FAN COWL ACCESS PANEL MISSING/DEPARTED ON THE RUNWAY. MX REPLACED THE COWL AND DID NOT FIND ANY SUBSEQUENT AIRCRAFT DAMAGE.Nov 23, 2007 · N37342 · Cndair CL6002B19SDR CALA0700695Fitting · crackedREF EA 5440-01234 REV B OP 11 FASTENER 20 HAS CRACK INDICATION, NR 1 PYLON AFT BULKHEAD FITTING. REPAIRED PER ECRA 5450-01724.Nov 23, 2007 · N12109 · Boeing 757224SDR 07FDEA04798Bolt · shearedDURING B CHECK, RT WING NR 3 ENGINE PYLON TOMBSTONE FITTING, FOUND 2(EA)3/8 DIAMETER BOLTS AT LOWER SPHERICAL BEARING SHEARED OFF. REMOVED AND REPLACED QTY (6) 77711-9-105 INCONEL BOLTS,AUB7125-1 PLATE ASSY AND AUB7126-501 RETAINER ASSY PER MM 54-00-01 AND Nov 15, 2007 · N68049 · Doug MD1010FSDR F3LA200700318Structure · crackedDURING C4/S1 CHECK, INSPECTION REPORTED CRACK EMANATING FROM RT PYLON (OTBD UPPER, ABOVE TR) SCREW HOLE. CUT OUT DAMAGED AREA, FABRICATED REPAIR FILLER AND SPLICE, AND INSTALLED REPAIR IAW SRM 54-52-11, REPAIR E, STEP 2C; 54-52-12, FIG. 205; AND EA A9-54R-122Nov 11, 2007 · N908FR · Airbus A319111SDR UALA2008111304633Structure · crackedNR 2 PYLON FUEL LINE CUTOUT FWD INBOARD ATTACH HOLE CRACKED. SUSPECT ENGINE VIBRATION CAUSE. INSTALLED NEW REPAIR DOUBLER PER REO-G12178 REV B. AC OK FOR SERVICE.Nov 9, 2007 · N653UA · Boeing 767322SDR HALA0700470Doubler · crackedNR 1 ENGINE NACELLE LOWER PAN DOUBLER AT NAC STA 352 CRACKED. REPLACED DOUBLER PER SRM 51-40-02 AND DRAWING 313T3355.Nov 6, 2007 · N583HA · Boeing 76733ASDR DL76L071407Angle · crackedCRACKED CLOSEOUT ANGLE FOUND DURING AD 2005-19-23 INSPECTIONS. INSPECTED AND REPLACED ANGLE PER B/P.Nov 4, 2007 · N175DN · Boeing 767332SDR ASAA0792207Rub Strip · wornNR 2 ENG INBOARD FAN COWL UPPER RUB STRIP WORN. NR 2 ENG INBOARD FAN COWL UPPER RUB STRIP REPLACED AND AREA REPAIRED IAW B737 900 SRM 54-20-01 FIG 202 REPAIR 7.Nov 3, 2007 · N307AS · Boeing 737990SDR HALA0700464Bracket · crackedCRACK ON "L" SECTION BRACKET LEFT ENGINE NACELLE STRUT HYDRAULIC COMPARTMENT FORWARD LOWER CORNER. REPLACED ANGLE BRACKET PER SRM 51-40-06.Nov 1, 2007 · N583HA · Boeing 76733A
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