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.

SDR P5CA9800454Bracket · crackedCRACKED INBOARD AND OUTBOARD SUPPORT BRACKETS ON NR 4 PYLON LOWER FIREWALL RIB. REPLACED SUPPORT BRACKETS PER BAC SRM 51-30-02.Mar 2, 1998 · N854FT · Boeing 747122SDR DHL98726123S-Duct · crackedAT D CHECK, NR 2 ENGINE INLET S DUCT FWD EDGE CRACKED AT 9 O'CLOCK. REMOVED FASTENERS AND TRIMMED OUT DAMAGED AREA. INSTALLED DOUBLER REPAIR PER SRM 54-10-3, 11 BY 2.5. N/R 6280.Feb 28, 1998 · N726DH · Boeing 727228SDR DHL98726118S-Duct · crackedAT D CHECK, NR 2 ENGINE INLET DUCT FWD EDGE CRACKED AND SEVERAL GOUGES BETWEEN 4-6 O'CLOCK. CUT OUT DAMAGED AREA, INSTALLED DOUBLER REPAIR PER SRM 54-10-3, 14 BY 5. CUT OUT DAMAGED AREA FROM 4-6 O'CLOCK AND INSTALLED DOUBLER REPAIR PER SRM 54-10-3, 19 BY 3. Feb 28, 1998 · N726DH · Boeing 727228SDR CALA9800355Stiffener · galledINSPECTION FOUND VERTICAL STIFFENERS AT LEFT AND RIGHT SIDE OF NR 3 PYLON HAD ELONGATED HOLES AND WERE GALLED AT PAN SUPPORT RIB. THE STIFFENERS WERE REMOVED IAW SRM 51-10-1. NEW STIFFENERS WERE FABRICATED AND INSTALLED IAW SRM 51-10-00, 51-21-01, AND 51-10-Feb 28, 1998 · N68044 · Doug DC1010SDR CALA9800337Stiffener · crackedINSPECTION FOUND A 1 INCH CRACK IN VERTICAL STIFFENER AT TOP OF NR 1 PYLON ON AFT SIDE OF YN 342.0 FORGING AT INBOARD SIDE. REPAIR WAS ACCOMPLISHED IAW SRM 54-00-01.Feb 26, 1998 · N68044 · Doug DC1010SDR DHL98726119Inlet · crackedAT D CHECK, NR 2 ENGINE INLET INNER SKIN HAS CRACKS END AT RIVETS AT 2 O'CLOCK POSITION. INSTALLED DOUBLER REPAIR PER SRM 54-10-3, 13 BY 6. N/R 6364.Feb 24, 1998 · N726DH · Boeing 727228SDR CALA9800308Angle · crackedINSPECTION FOUND A .25 INCH CRACK IN L-ANGLE ON TOP OF NR 3 PYLON AT AFT END OF HEAT EXCHANGER. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-01 AND 54-11-02.Feb 23, 1998 · N17087 · Doug DC1030SDR CALA9800294Spar Web · crackedINSPECTION FOUND A 6 INCH CRACK IN NR 3 PYLON UPPER SPAR WEB AT STA YN 200. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 54-20-0.Feb 21, 1998 · N68044 · Doug DC1010SDR RAAA98E9007Shear Tie · crackedDURING SCHEDULED NR 1 CHECK, FOUND NR 2 NACELLE SHEAR TIE CRACKED (APPROX .25 IN) AT NAC STA -31, 13 INCHES ABOVE LOWER LONGERON. REPLACED SHEAR TIE PER SRM 51-2-9, M-54 NR 101.Feb 19, 1998 · N1968R · Lkheed 188CSDR EIAA980138Fitting · crackedHKG - DURING 'C5/D' CHECK INSPECTION, RT WS 669.5 BULKHEAD PYLON SUPPORT FORWARD INBOARD BACK-UP FITTING CRACKED AT STR 24. BACK-UP FITTING REPLACED IAW SB 54A2159. (X)Feb 19, 1998 · N471EV · Boeing 747273CSDR ASAA9840034Fairings · wornSEA - DURING C-CHECK, WEAR WAS FOUND AT VARIOUS LOCATINS ON ALL FOUR BULLNOSE FAIRINGS ON NR 1 AND NR 2 ENGINES AS A RESULT OF THE BLOCKER DOOR HINGE FITTINGS RUBBING AGAINST THE FAIRING SURFACES. REPAIRED PER EA 5430-01029 AND BOEING TELEX ASA-SEA-98-0049RR.Feb 19, 1998 · N763AS · Boeing 7374Q8SDR P5CA9800322Brace · wornNR 2 ENG DIAGONAL BRACE WORN ON AFT END ON LT SIDE. AREA SMOOTHED OUT AND SHOT PEENED. NO CRACKS NOTED PER SRM 51-10-02, OHM 20-10-03, NDT PT 6 51-00-00 FIG 4.Feb 18, 1998 · N3203Y · Boeing 747128SDR ABXA9800092Web · crackedDURING C-CHECK, FOUND RIGHT PYLON VERTICAL WEB CRACKED FORWARD AND INBOARD OF THE AFT ENGINE MOUNT. REPLACED WEB IAW DC9 SRM 54-10-00 AND 51-10-5.Feb 18, 1998 · N938AX · Doug DC931SDR ABXA9800091Angle · crackedDURING C-CHECK, FOUND RIGHT PYLON TO FUSELAGE UPPER ATTACH ANGLE CRACKED AT STA 980. REPLACED ANGLE IAW DC9 SRM 54-04.Feb 18, 1998 · N938AX · Doug DC931SDR ABXA9800090Angle · crackedDURING C-CHECK, FOUND ANGLE JUST INBD OF AFT ENGINE MOUNT IN NR 1 PYLON CRACKED AT LOWER FASTENER. REPLACED ANGLE IAW DC9 SRM 51-30-1.Feb 18, 1998 · N938AX · Doug DC931SDR EIAA980125Web · misinstalledHKG - DURING 'C5/D' CHECK INSPECTION, NR 1 PYLON MID-SPAR WEB CUT-OUT AREA ON REWORK HAS AS EXTRA ROW OF FASTENERS. REPAIRED IAW HAECO RS R54-53-33608. (X)Feb 17, 1998 · N471EV · Boeing 747273CSDR MWEA98166Bracket · crackedCORNER BRACKET JUST FORWARD OF THE NR 2 PYLON AFT UPPER SPAR STRAP WAS FOUND CRACKED. INSTALLED REPLACEMENT PART IAW SRM 51-30.Feb 16, 1998 · N212ME · Doug DC932SDR CALA9800244Web · cannedINSPECTION FOUND UPPER SPAR WEB OF NR 1 PYLON OIL CANNED FORWARD OF HEAT EXCHANGER. A NEW WEB WAS FABRICATED AND INSTALLED IAW SRM 54-11-2 AND 51-31-01.Feb 13, 1998 · N68044 · Doug DC1010SDR CALA9800243Stiffener · crackedINSPECTION FOUND A 2 CRACK ON INBOARD SIDE OF LT UPPER SPAR WHERE CENTER HINGE OF LT REV COWL ATTACHES, NR 1 PYLON. THE STIFFENER WAS REMOVED AND REPLACED IAW SRM 51-33-01.Feb 13, 1998 · N68044 · Doug DC1010SDR QXEA9800231Bracket · chafedNACELLE AFT WALL GRAVEL GUARD MOUNT BRACKETS CHAFED. REPAIRED IAW HORIZON EA 9-54-154.Feb 12, 1998 · N821PH · Dhav DHC8102SDR UPS98225728Web · crackedINSPECTION TYPE:C, CRACK ON WEB ABOVE NR 2 ENGINE HORIZONTAL FIREWALL, RT SIDE AT STATION 1381.5. WEB FABRICATED AND FITTED IAW DRAWING 65-17555.Feb 11, 1998 · N941UP · Boeing 72722CSDR EIAA980124Brace · wornHKG - DRUING 'C5/D' CHECK INSPECTION, NR 4 PYLON FORWARD DIAGONAL BRACE FITTING HAS THREE SLOTTED HOLES. REPAIRED IAW HAECO RS R54-54-33605. (X)Feb 10, 1998 · N471EV · Boeing 747273CSDR EIAA980123Brace · wornHKG - DURING 'C5/D' CHECK INSPECTION, NR 1 PYLON FORWARD DIAGONAL BRACE FITTING HAS THREE SLOTTED HOLES. REPAIRED IAW HAECO RS R54-54-33605. (X)Feb 10, 1998 · N471EV · Boeing 747273CSDR EISA98037S-Duct · tornDURING C-CHECK, FOUND NR 2 ENGINE INTAKE 12 O'CLOCK POSITION HAS A TEAR IN SKIN AT OPENING NEXT TO ENGINE RING FLANGE. REMOVED DAMAGED AREA, FABRICATED REPAIR FILLER AND DOUBLER PER SRM 54-10-03. INSTALLED REPAIR PER SRM 54-10-03. (M)Feb 9, 1998 · N6826 · Boeing 727223SDR ABXA9800066Angle · crackedDURING C-CHECK, FOUND LOWER PYLON TO FUSELAGE ATTACK ANGLE AT LEFT PYLON LEADING EDGE CRACKED. REPAIRED ANGLE IAW DC9 SRM 54-04.Feb 9, 1998 · N945AX · Doug DC931SDR MWEA98146Angle · crackedDURING C-CHECK, FOUND A CRACKED ANGLE ON LT PYLON STATION 1019. MTC REPAIRED IAW SRM 54-01 FIG 2 AND 51-30-05.Feb 4, 1998 · N203ME · Doug DC932SDR EIAA98035Brace · corrosionHKG - DURING 'C5/D' CHECK INSPECTION, NR 1 PYLON DIAGONAL BRACE UNDER WING FITTING HAS CORROSION UNDER BUSHING. REPAIRED IAW SB 57-2246. LUG BORE AFTER INSURANCE CUT 2.457 INCH. (M)Feb 4, 1998 · N471EV · Boeing 747273CSDR EIAA980139Fitting · misalignedDURING 'C5/D' CHECK INSPECTION, NR 1, 2, 3 AND 4 PYLON DSB AND BACKUP FITTING HOLES DO NOT ALIGN. ALTERNATE HOLE LOCATIONS IAW SB AND HAECO RS R57-04-33642, R57-04-33631, R57-04-33632, AND R57-04-33633. (M)Feb 4, 1998 · N471EV · Boeing 747273CSDR CALA9800168Web · crackedINSPECTION FOUND A 1 INCH CRACK IN HORIZONTAL WEB UNDER REV INTERLOCK VALVE/CYLINDER ON TOP OF NR 1 PYLON. THE WEB WAS REMOVED IAW SRM 51-31-01. A NEW WEB WAS FABRICATED AND INSTALLED IAW SRM 51-20-01 AND 51-31-01.Feb 2, 1998 · N68044 · Doug DC1010SDR P5CA9800054Angle · brokenNR 2 PYLON, LEFT SIDE ATTACH ANGLE BROKEN SLOT SEAL AREA. REMOVED AND REPLACED PER SRM 51-30-02.Jan 29, 1998 · N858FT · Boeing 747123SDR UPS98225629Tee · crackedINSPECTION TYPE-D, CRACK ON VERTICAL ANGLE ABOVE NR 2 ENGINE HORIZONTAL FIREWALL, LT SIDE AT STATION 1409 NR 2 ENGINE AFT MOUNT SUPPORT RIB CHORD. REPAIR CARRIED OUT IAW SRS ENGINEERING ORDER 98-01-012R1.Jan 28, 1998 · N943UP · Boeing 72722CSDR LR7A9820Angle · crackedDURING C-CHECK/BRIDGING INSPECTION, FOUND ANGLE AT LOWER AFT NACELLE ASSY CRACKED NEAR FORWARD MOST SPOT WELD NR 1, 2, 3, 4 ENGINES FS 517, PPBL 5.0.Jan 27, 1998 · N903SJ · Lkheed 382GSDR LR7A9813Bulkhead · wornDURING C-CHECK/BRIDGING INSPECTION, NR 4 ENGINE QEC FRONT BULKHEAD ASSEMBLY WORN ON BOTH SIDES OF FILLER, TOP CENTER. REPLACED EXISTING FILLER, INSTALLED WEAR STRIP.Jan 27, 1998 · N903SJ · Lkheed 382GSDR LR7A9812Extrusion · wornDURING C-CHECK/BRIDGING INSPECTION, FOUND TEE EXTRUSION WORN 0.025 THICKNESS AND GOUGED TO DEPTH OF 0.045 AT NR 4 ENGINE, LHS, FS 410, 11.0. WORN AREA BLENDED SMOOTH, EPOXY FILLER APPLIED, STAINLESS STEEL WEAR STRIP INSTALLED.Jan 27, 1998 · N903SJ · Lkheed 382GSDR LR7A9809Tee · wornDURING C-CHECK/BRIDGING INSPECTION, TEE EXTRUSION IS WORN, NR 3 ENGINE, FS 410, PPBL 0.0 AND PPWL 11.0, AT THE TOP OF THE BULKHEAD. THE WORN AREA WAS BLENDED SMOOTH, EPOXY FILLER APPLIED, STAINLESS STEEL WEAR STRIP INSTALLED.Jan 27, 1998 · N903SJ · Lkheed 382GSDR DL72K980316Lip · gougedAT MV2, FOUND DEEP GOUGE IN NR 2 PYLON LIP 5 O'CLOCK POSITION. FABRICATED REPAIR DOUBLER/FILLER PER MM 53-11-00 PG 801.Jan 27, 1998 · N472DA · Boeing 727232SDR EIAA98020Fitting · corrosionHKG - DURING 'C5/D' CHECK INSPECTION, NR 4 PYLON UPPER SPAR FITTING CORROSION FOUND IN LUG BORE. REMOVED CORROSION IAW SB 54.2164 FIG 2. (M)Jan 23, 1998 · N471EV · Boeing 747273CSDR EIAA98019Fitting · corrosionHKG - DURING C5/D CHECK INSPECTION, NR 3 PYLON UPPER SPAR FITTING CORROSION FOUND IN LUG BORE. REMOVED CORROSION IAW SB 54.2164 FIG 2. (M)Jan 23, 1998 · N471EV · Boeing 747273CSDR EIAA98018Fitting · corrosionHKG - DURING C5/D CHECK INSPECTION, NR 2 PYLON UPPER SPAR FITTING CORROSION FOUND IN LUG BORE. REMOVED CORROSION IAW SB 54.2164 FIG 2. (M)Jan 23, 1998 · N471EV · Boeing 747273CSDR EIAA98017Fitting · corrosionHKG - DURING C5/D CHECK INSPECTION, NR 1 PYLON UPPER SPAR FITTING CORROSION FOUND IN LUG BORE. REMOVED CORROSION IAW SB 54.2164 FIG 2. (M)Jan 23, 1998 · N471EV · Boeing 747273CSDR P5CA9800158Channel · crackedNR 3 PYLON THROTTLE PUSH PULL CABLE ATTACH CHANNEL ADJACENT TO ANTI-ICE DUCT IS CRACKED. REPAIRED PER SRM 51-40-03 FIG 3.Jan 21, 1998 · N856FT · Boeing 747132SDR P5CA9800121Channel · crackedNR 4 PYLON SKIRT BEAM AREA HYD PRESS FILTER SUPPORT CHANNELS CRACKED. REPLACED CHANNELS PER SRM 51-10-01.Jan 21, 1998 · N856FT · Boeing 747132SDR P5CA9800120Channel · crackedNR 3 PYLON SKIRT BEAM AREA HYD PRESS FILTER MODULE UPPER SUPPORT CHANEL CRACKED. REPLACED CHANNEL PER SRM 51-10-01.Jan 21, 1998 · N856FT · Boeing 747132SDR P5CA9800023Brace · chafedLT SIDE OF DIAGONAL BRACE CHAFED FWD END OF NR 1 ENGINE PYLON. BLENDED OUT CHAFED AREA PER SRM 54-40-01.Jan 18, 1998 · N851FT · Boeing 747122SDR MWEA98028Angle · crackedDURING C-CHECK, FOUND 2 SMALL CRACKS THROUGH 2 RIVET HOLES ON RIGHT UPPER PYLON TO FUSELAGE ATTACH ANGLE AT FS 1019. MTC REPAIRED IAW 54-04 FIG 10.Jan 18, 1998 · N502ME · Doug DC932SDR P5CA9800026Brace · chafedNR 4 ENGINE PYLON SAIL AREA DIAGONAL BRACED CHAFED FWD END LT SIDE. CHAFE OF DIAGONAL BRACE WITHIN LIMITS PER 54-40-01 ZONE 3. EDDY CURRENT C/W, NO CRACKS NOTED PER NDT 54-40-08 PART 6. BLENDED OUT CHAFED AREA, SHOT PEENED AND TREATED PER SRM 54-40-01.Jan 16, 1998 · N921FT · Boeing 747238BSDR P5CA9800025Brace · chafedNR 1 ENGINE PYLON SAIL PLANE AREA DIAGONAL BRACE CHAFED 2 PLACES LT SIDE. CHAFE WITHIN LIMITS ZONE 3 PER SRM 54-40-01. EDDY CURRENT C/W PER NDT 54-40-08 PART 6. BLENDED OVER CHAFE AREA SHOT PEENED AND TREATED PER SRM 54-40-01.Jan 16, 1998 · N921FT · Boeing 747238BSDR P5CA9800024Brace · chafedNR 1 ENGINE PYLON SAIL PLANE AREA DIAGONAL BRACE CHAFED FWD RT SIDE. CHAFE OF DIAGONAL BRACE WITHIN LIMITS PER ZONE 3 SRM 54-40-01. EDDY CURRENT C/W PER NDT 54-40-08 PART 6, NO CRACKS FOUND. BLENDED OUT CHAFED AREA AND TREATED AREA PER SRM 54-40-01.Jan 16, 1998 · N921FT · Boeing 747283BSDR ABXA9800019Angle · crackedDURING C-CHECK, FOUND UPPER PYLON ATTACH ANGLE CRACKED AT STA 980. REPAIRED ANGLE IAW DC9 SRM 54-04.Jan 16, 1998 · N932AX · Doug DC933FSDR ABXA9800018Angle · crackedDURING C-CHECK, FOUND ANGLE IN NR 2 ENGINE PYLON CRACKED AT AFT LOWER SPAR STRAP ABOVE PANEL 8212. REPLACED ANGLE IAW DC9 SRM 51-30-1.Jan 16, 1998 · N932AX · Doug DC933F
Back to JASC 5400