JASC 5400
Service difficulty reports · 1,907
Reports filed under 5400 · Nacelle/Pylon 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 = '5400' 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 = '5400' 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 ASAA9740057Rivets · looseSEA - DURING STRUCTURAL INSPECTION, THE NR 1 ENGINE NACELLE AFT FAIRING END CAP WAS FOUND TO HAVE LOOSE RIVETS. REPAIRED PER EA 5750-01212 AND BOEING TELEX ASA-SEA-96-0203RR. TT: 16,604 HOURS. TC: 8,816. (X)SDR P5CA9701512Brace · chafedDIAGONAL BRACE CHAFFED FWD ENG RIGHT SIDE NR 4 ENGINE PYLON. REWORKED AREA PER BOEING SRM 54-40-01.SDR P5CA9701511Brace · chafedDIAGONAL BRACE CHAFFED FWD END RT SIDE NR 1 ENGINE PYLON. REWORKED AREA PER BOEING SRM 54-40-01.SDR P5CA9701510Brace · chafedDIAGONAL BRACE CHAFED 2 PLACED LEFT SIDE NR 1 ENGINE PYLON. REWORKED PER BOEING SRM 54-40-01.SDR P5CA9701509Brace · chafedDIAGONAL BRACE CHAFFED FWD END RIGHT SIDE NR 2 ENGINE PYLON. REWORKED AREA PER BOEING SRM 54-40-01.SDR P5CA9701516Fitting · damagedNR 4 PYLON FORWARD DIAGONAL BRACE FITTING HAS 3 EACH DRILL STARTS. REPAIRED PER HAECO RS R54-33472.SDR QXEA9700607Angle · crackedPDX - CRACK FLANGE OF THE NACELLE DRAG ANGLE, (P/N 85710323). REPAIRED IAW EA 9-57-291.SDR QXEA9700608Web · chafedPDX - RIGHT HAND NACELLE FINGERNAIL UPPER DECK CHAFE HOLE IN WEB. DAMAGE IS JUST OUTBOARD OF YN=0.00 AND JUST AFT OX XN=245. REPAIRED IAW 9-54-139.SDR DLL10971685Drag Strut · corrosionTHE FWD O/B LUG OF THE NUMBER 3 ENGINE PYLON DRAG STRUT WAS FOUND WITH CORROSION DAMAGE ON THE INNER AND OUTER FACES. THE INNER FACE OF THE OUTBOARD LUG WAS MACHINED 0.041. THE OUTER FACE OF THE OUTBOARD LUG WAS MACHINED 0.023. A LOCAL BLEND OF 0.013 BY .375SDR DLL10971684Drag Strut · corrosionTHE FORWARD O/B LUG OF THE NR 1 ENGINE PYLON DRAG STRUT WAS FOUND WITH CORROSION DAMAGE ON THE OUTER SURFACE OF THE LUG. THE LUG HAS BEEN SPOTFACED 0.050 TO REMOVE CORROSION. THE NR 1 PYLON DRAG STRUT O/B LUG THICKNESS REMAINING IS 1.353. THE LUG WAS REWORKSDR ABXA9701431Angle · crackedDURING D-CHECK, FOUND NR 2 ENGINE PYLON UPPER ATTACH ANGLE CRACKED AND RIVET HEADS ARE POPPED. *S/D* REPAIRED CRACKED ANGLE IAW DC9 SRM 54-04.SDR P5CA9701426Brace · chafedNR 4 PYLON DIAGONAL BRACE FWD END CHAFED. BLENDED OUT PER BOEING SRM 51-10-01.SDR P5CA9701425Brace · chafedNR 2 PYLON DIAGONAL BRACE FWD END CHAFED. BLENDED OUT PER BOEING SRM 51-10-06.SDR P5CA9701424Brace · chafedNR 1 PYLON DIAGONAL BRACE CHAFED BY AFT FUSELAGE PIN FAIL-SAFE BRACKET. BLENDED OUT PER BOEING SRM 51-10-06.SDR P5CA9701422Brace · chafedNR 4 ENGINE DIAGONAL BRACE CHAFED BY AFT FUSELAGE PIN FAIL-SAFE BRACKET. BLENDED OUT CHAFED AREA IAW BOEING SRM 51-10-01.SDR P5CA9701421Stiffener · wornNR 4 ENGINE PYLON FUEL FAIRING (DOGHOUSE) INBD HORIZONTAL STIFFENER IS WORN THROUGH AT 1ST RIB. REMOVED AND REPLACED ANGLE PER BOEING SRM 51-10-01, TREATED AND PRIMED PER SRM 51-10-06.SDR P5CA9701415Fasteners · looseNR 2 PYLON DOUBLER ABOVE AFT MOUNT ASSY LOOSE FASTENERS. REMOVED AND REPLACED FASTENERS PER BOEING SRM 51-30-02.SDR P5CA9701408Bracket · wornNR 4 PYLON (DOGHOUSE) ASSY FWD MOUNT BRACKET WORN. REMOVED AND REPLACED BRACKET PER BOEING SRM 51-10-01.SDR P5CA9701405Fasteners · missingNR 4 PYLON FAIRING MISSING FASTENERS. REPLACED PER BOEING SRM 51-30-02, MM 78-11-03.SDR ABXA9701341Angle · crackedNR 3 PYLON LOWER FORWARD SUPPORT ANGLE AT TOMBESTONE IS CRACKED AT OUTBOARD FASTENER. INSTALLED NEW ANGLE IAW DC-8 SRM 51-3-0 AND DAC DWG NR 9753018.SDR MWEA97699Angle · crackedDURING C-CHK, FOUND CRACK ON LT ENG PYLON ANGLE FLANGE. REPAIRED IAW SRM 54-01 FIG 2 SHT 3 AND 51-30.SDR 97UAL900581Angle · crackedWHILE ACCOMPLISHING AD97-12-03, CRACKS WERE FOUND ON THE 65B91333-1 AND -2 ANGLES WHICH ATTACH TO THE CANTED WEB COMMON TO THE AFT VERTICAL AND THE UPPER HORIZONTAL WEBS. THESE ANGLES ARE NOT PART OF THE FITTING INSPECTION REQUIREMENTS BUT ARE ADJACENT TO THESDR MWEA97694Angle · crackedDURING B-CHK, FOUND 3 INCH CRACK BETWEEN RIVETS ON RT PYLON ATTACH ANGLE FS 1019. MTC REPAIRED IAW SRM 54-04 FIG 10.SDR HALA9700167Rib · corrosionSBA - IN C-CHECK, FOUND PITTING CORROSION, LEVEL 2 ON NR 4 RIB OF RT TRAILING EDGE ENGINE PYLON. FABRICATED REPAIR DOUBLER AND INSTALLED PER DACO DC-9 SRM 51-60-0. (M)SDR MWEA97668Doubler · crackedDURING C-CHK, FOUND CRACK IN STIFF MEMBER BELOW UP RT PYLON SKIN. MTC REPAIRED IAW SRM 51-30-2.SDR GAIA9740S Duct Skin · corrodedDURING INITIAL APPLICATION OF THE CPC BASIC TASK PER AD 90-25-03, THE FOLLOWING FIVE LEVEL 2 CORROSION FINDINGS REQUIRED REPAIR: C54-451-02, 'S' DUCT UPPER FORWARD INNER SKIN AT BS 1151.68 APPLIED DOUBLER PER SRM. (X)SDR CALA9701206Angle · crackedINSPECTION FOUND A 1 INCH CRACK IN LT PYLON TOP SKIN TO FUSELAGE L-ANGLE AT STA 1019. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 54-04.SDR ABXA9701263Angle · crackedDURING C-CHECK, FOUND THE TOP ANGLE FOR THE 4TH WEB FORWARD FROM THE END OF THE LT PYLON TRAILING EDGE CRACKED. *S/D* REPAIRED IAW DC9 SRM 54-50.SDR MWEA97648Angle · crackedDURING C-CHK, FOUND 1 INCH CRACK ON PAX DOOR HAND HOUSING. MAINT REMOVED AND REPLACED PAN.SDR MWEA97644Angle · crackedDURING C-CHK, FOUND FS 980 RT FUSE UP PYL ATTACH ANGLE CRACKED. MAINT REPAIRED IAW SRM 54-04 FIG 10.SDR CALA9701111Brace · crackedINSPECTION FOUND NR 2 ENGINE PYLON STRUT TO WING DIAGONAL BRACE CRACKED THROUGH THE LOWER LUG RADIUS(1 INCH LONG BY .75 INCH DEEP). THE BRACE WAS REMOVED AND REPLACED IAW MM 54-10-01.SDR VTZA97383Camlock · looseHVN/IAD - FLT 6441 - DURING TAKEOFF AT 1940 HOURS ON 7-11-97, THE FLIGHT CREW WAS INFORMED BY A PASSENGER THAT THERE WAS A LOOSE COWLING ON LT ENGINE. THE CAMLOCK WAS PROPERLY SECURED AND THE DISCREPANCY WAS PROPERLY SIGNED OFF. THE AIRCRAFT WAS THEN RELEASEDSDR DLM88971387Bolt · wornTHE NR 1 PYLON APRON SUPPORT BOLT HAS WORN SURFACES ON BOTH ENDS. THIS ER/A AUTHORIZES THE MANUFACTURE OF THE BOLT (DAC P/N 4938184-3) PER DRAWING 4938184, USING SUBSTITUTE MATERIAL 17-4PH HT TR 180-200 KSI.SDR CKSA97337Angle · crackedDURING C1-12 CHECK INSPECTION, FOUND NR 4 PYLON STA 211 WEB SUPPORT ANGLE CRACKED. REPAIRED WEB SUPPORT ANGLE IAW B747 SRM 51-40-3, (7075-T6). C-CHECK WORK CARD NUMBER 7CI4806. NON-ROUTINE TASK CARD NUMBER 109832.SDR CKSA97324Chafe Strip · damagedDURING C1-12 CHECK INSPECTION, FOUND NR 4 PYLON I/B LWR SKIN AND INNER CHAFE STRIP DAMAGED FWD AND AFT OF AFT ENG MOUNT. REPAIRED DAMAGE SKIN AREA IAW B747 SRM 54-30-03. REPLACED CHAFE STRIP IAW SRM 51-10-01, 54-30-02 AND 51-30-02, (2024-T3). C CHECK WORK CSDR CKSA97323Fitting · crackedDURING C1-12 CHECK INSPECTION, FOUND NR 4 PYLON ADP O/B MOUNTING LUG FITTING CRACKED. REMOVED AND REPLACED PART IAW B747 SRM 51-10-1 AND 51-30-02 (7075-T6). C CHECK WORK CARD NUMBER 7CI4809. NON-ROUTINE TASK CARD NUMBER 107883.SDR ABXA9701244Angle · crackedDURING C-CHECK, FOUND THE LT PYLON STIFFENER ANGLE CRACKED AT STA 980. REPAIRED IAW DC-9 SRM 51-30-2 AND 51-30-5.SDR P5CA9701290Bracket · brokenNR 2 PYLON ATTACH BRACKET BROKEN, I/B INTERNAL RIB, BY ACCESS PANEL 462BL. REMOVED AND REPLACED BRACKET PER BOEING SRM 51-30-02 AND FABRICATED PER SRM 51-10-01.SDR CKSA97392Bearing · corrodedDURING ACCOMPLISHMENT OF AD 93-20-03 FOUND LEVEL 2 CORROSION: BEARING IN FITTING FOR AFT MOUNT OF DRAG STRUT INNER SURFACE CORRODED/FLAKING. REMOVED AND REPLACED NR 1 PYLON AFT DRAG STRUT MOUNT BEARING IAW L1011 MM 57-43-01. NON-ROUTINE TASK CARD NUMBER 107SDR CKSA97373Drag Strut · corrodedDURING ACCOMPLISHMENT OF AD 93-20-03 FOUND LEVEL 2 CORROSION: NR 3 ENGINE DRAG STRUT CORRODED AT AFT O/B HOLE. REMOVED CORROSION IAW L1011 SRM 54-11-00 FIG 807. REPLACED BUSHINGS AFT END IAW SRM 54-11-00 FIG 802. NON-ROUTINE TASK CARD NUMBER 098412.SDR P5CA9701288Brace · damagedDAMAGE ON NR 2 PYLON DIAGONAL BRACE DUE TO RUBBING SAILBOAT DOOR LATCH. FOUND DAMAGE IN LIMITS, INSPECTED PER BAC NDT MANUAL PART 6 54-40-03, FOUND OK, AND BLENDED DAMAGED AREA TREATED PER BAC SRM 51-40-01 AND 51-10-01.SDR P5CA9701287Brace · damagedDAMAGE ON NR 1 PYLON DIAGONAL BRACE DUE TO RUBBING SAILBOAT DOOR LATCH. FOUND DAMAGE IN LIMITS, INSPECTED PER BAC NDT MANUAL PART 6 54-40-03, FOUND OK, AND BLENDED DAMAGED AREA TREATED PER BAC SRM 51-40-01 AND 51-10-01.SDR ASAA9710054Rib · gougedSEA - DURING 'C' CHECK, SEVERAL GOUGES WERE FOUND ON NR 2 ENGINE INBOARD FIXED COWL FOURTH RIB. REPAIRED PER EA 5420-01003 AND BOEING SRM. (M)SDR 97ZZZM779Rib · gougedSEA - DURING 'C' CHECK, SEVERAL GOUGES WERE FOUND ON NR 2 ENGINE INBOARD FIXED COWL FOURTH RIB. REPAIRED PER EA 5420-01003 AND BOEING SRM. REFERENCE ASAA9710054.SDR P5CA9701339Spar Chord · corrodedLEVEL 1 CORROSION, NR 2 PYLON INBD AND OUTBD MID SPAR CHORDS HAVE LIGHT SURFACE CORROSION AT NAC ST 296-286 NAC WL 181. REMOVED CORROSION IAW BOEING SRM 51-10-01 WITHIN SRM LIMITS 54-10-01 NON ROUTINE CARD S/N 6275.SDR P5CA9701241Spar Chord · corrodedLEVEL 1 CORROSION NR 2 PYLON I/B AND O/B MID SPAR CHORDS HAVE LIGHT SURFACE AT UPPER AND LOWER SURFACE AT NAC ST 296-286 NAC WL 181. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02. AD: NR 94-15-18.SDR P5CA9701205Angle · crackedCRACK FOUND #4 DOGHOUSE - AFT R/H INNER ATTACH ANGLE. REPAIRED PER BOEING SRM 54-12-03.SDR MWEA97591Angle · crackedDURING SERV CHK, FOUND 1 INCH CRACK IN FWD END LT PYLON FUSE ATTACH ANGLE. MAINT REPAIRED IAW SRM 54-04 FIG 10.SDR ABXA9701361Fitting · corrodedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE RIGHT PYLON UPPER BEAVERTAIL EXCESSIVELY CORRODED. REPAIRED RIGHT UPPER BEAVERTAIL IAW ABX REA D954-19607-MR.SDR P5CA9701333Spar Chord · corrodedLEVEL 1 CORROSION, NR 4 PYLON INBD AND OUTBD MID SPAR CHORDS HAVE LIGHT SURFACE CORROSION AT NAC ST 267-257 NAC WL 180. REMOVED CORROSION AND CHORDS REPROTECTED PER BOEING SRM 51-10-01, 54-10-01 AND SB 747-54-2159 R2, NON ROUTINE CARD S/N 6003.
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