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 AU991015Rod · worn(AUS) FOLLOWING REMOVAL OF THE RT PYLON BOAT FAIRING FOR REPAIR THE FOLLOWING DEFECTS WERE FOUND: 1. RT ENGINE DRIVEN HYDRAULIC PUMP PRESSURE AND SUPPLY LINE ELBOW JAM NUTS BACKED OFF AND ELBOW FRETTING IN PYLON RECEPTACLES2S. 2. INBOARD VERTICAL STRAKESep 30, 1999 · Boeing 76733ASDR UF6A990945Modular · crackedSBN - LEFT MODULAR 7 AFT INBOARD DIAPHRAGM IS CRACKED. MAINTENANCE STOP DRILLED CRACK AND REPAIRED. ALL WORK WAS DONE IAW BAE ATP SRM 53-10-02 AND 51-30-01. (M)Sep 28, 1999 · N858AW · Bag ATPSDR DL72S992116Skin · crackedTPA LTR CHK D-2 9/21/99, 1 CRACK ON S-DUCT HOUSING RT SIDE AT UPPER END OF PANEL 9524. REPAIRED PER MM 54-30-0.Sep 21, 1999 · N492DA · Boeing 727232SDR TWAA9917404Clip · brokenDURING OP 16 MAINT CHECK AT STA 944, THE LOWER SIDE OF NUMBER 2 PYLON DOUBLER ANGLE CLIP WAS BROKEN. REPLACED DOUBLER PER SPM 6-70-01.Sep 19, 1999 · N925L · Doug DC932SDR DL767992171Brace · corrodedMIGRATED/ROTATED BUSHINGS WERE FOUND IN THE FORWARD LUGS OF THE NR 1 AND NR 2 PYLON DIAGONAL BRACES DURING PYLON INSTALLATION. MINOR CORROSION DAMAGE AND FRETTING DAMAGE WAS FOUND IN THE BORES UPON BUSHING REMOVAL.Sep 17, 1999 · N108DL · Boeing 767232SDR COMA9960507Angle · chafedPANEL 411AL CHAFED BY FASTENER MID FRAME OUTBOARD EDGE LEFT HAND ENGINE PYLON. PERFORMED MAJOR REPAIR SMOOTHED CHAFE ON (P/N 601-37004-133) AND FABED NEW SUPPORT ANGLE 601-37004-57 AS PER SAMPLE USING 2024-T3.040 PO NR 4206/1 AND INSTALLED IAW WVAC EO NR 601RSep 12, 1999 · N943CA · Cndair CL6002B19SDR DL72S992010Skin · cracked.5 INCH CRACK ON DUCT HOUSING SKIN AT PANEL 9524 RT SIDE. REPAIR PER MM 54-30-0.Sep 10, 1999 · N416DA · Boeing 727232SDR ABXA9900699Angle · crackedDURING C-CHECK, FOUND RIGHT PYLON LEADING EDGE INBOARD LOWER ATTACH ANGLE CRACKED. REPLACED ANGLE IAW DC9 SRM 54-04.Sep 10, 1999 · N938AX · Doug DC931SDR ABXA9900696Angle · crackedDURING C-CHECK, FOUND RIGHT PYLON HAD CRACKED WEB AT LOWER ATTACH ANGLE. REPLACED ANGLE IAW DC9 SRM 51-30-2 AND 51-30-5.Sep 10, 1999 · N938AX · Doug DC931SDR DL76S992061Fitting · corrosionI/B LUG OF THE NR 1 ENGINE PYLON MIDSPAR O/B FITTING FOUND WITH CORROSION AND WEAR DAMAGE. DAMAGE FOUND ON FACE OF LUG AND IN BORE, ERA 333570-14 REV A.Sep 9, 1999 · N116DL · Boeing 767332SDR DL72W992014Angle · corrodedDURING HUSH-KIT MOD, FOUND NR 2 AFT MOUNT SUPPORT CHORD ANGLE CORRODED BEYOND MFG SPECS. REPLACED OLD ANGLE WITH ONE OF NEW MFG.Sep 9, 1999 · N2812W · Boeing 727247SDR ABXA9900711Angle · crackedDURING C-CHECK, FOUND THE NR 2 PYLON UPPER ATTACH ANGLE CRACKED AT FORWARD END. REPAIRED ANGLE IAW DC9 SRM 54-04.Sep 3, 1999 · N959AX · Doug DC941SDR CALA9901117Web · crackedINSPECTION FOUND A 5 INCH CRACK AT FORWARD WEB OF NR 2 PYLON AFTER REMOVING VERTICAL FIN. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-31-01.Sep 1, 1999 · N76073 · Doug DC1030SDR UIEA99071Strap · crackedNR 1, 2, 3, 4, PYLONS EXTERIOR RIGHT PRE-COOLER EXHAUST CUTOUT FOUND WITH CRACK,AND NR 3 STIFFENER CRACK. REPAIRS CARRIED OUT IAW BOEING TELEXS AND SB 747-54-2163 R1 AND SB 747-54A2158 R2. THE SB REVS HAVE BEEN APPROVED ALTERNATE METHOD OF COMPLIANCE. (M)Aug 31, 1999 · N509MC · Boeing 747230BSDR UIEA99070Strap · cracksNR 4 PYLON INTERIOR, LEFT BULKHEAD STRAP AT NAC STATION 286 FOUND CRACKED. REPAIRED IAW BOEING TELEXS, TO BE RE-INSPECTED EVERY C-CHECK NOT TO EXCEED 18 MONTHS OR 1000 FLTS. (M)Aug 31, 1999 · N509MC · Boeing 747230BSDR UIEA99069Fitting · oversizeNR 1 AND NR 4 PYLONS FOUND FASTENER HOLE SIZE TO EXCEED TOLERANCE PER SB 747-54A2152 IN SPRINGBEAM SUPPORT FITTINGS IN 3 HOLE LOCATIONS. HOLES WERE OVERSIZED, NDT PERFORMED TO VERIFY NO CRACKS. NO INSURANCE CUT WAS PERFORMED AND FASTENERS INSTALLED. THIS ISAug 31, 1999 · N509MC · Boeing 747230BSDR UIEA99065Doubler · crackedNR 1 PYLON CAP SKIN MOD MO 54-0074 AREA FOUND WITH EXISTING DOUBLER, BULKHEAD FRAME CRACK AT STATION 270. THE CRACKED FRAME FLANGE WAS TRIMMED TO REMOVED DAMAGE, NDT PERFORMED TO VERIFY NO OTHER CRACKS. NEW REPAIR ANGLES AND NEW DOUBLER INSTALLED IAW BOEING Aug 31, 1999 · N509MC · Boeing 747230BSDR MWEA99550Web · crackedCRACK AT RIGHT PYLON VERTICAL WEB U-CHANNEL OUTBOARD OF STATION 859. MTC FABRICATED AND INSTALLED DOUBLERS.Aug 27, 1999 · N600ME · Doug DC914SDR MWEA99544Stiffener · crackedLEFT PYLON 2 CHANNEL STIFFENER HAS A CRACK ON OUTBOARD END. MTC FABRICATED AND INSTALLED DOUBLER AND TRIPLER.Aug 25, 1999 · N500ME · Doug DC914SDR DHL9972743CS Duct · crackedAT C CHECK, NR 2 ENGINE S DUCT HOUSING LT OUTER SKIN AT BS 1216 HAD 2 INCH CRACK JUST RIGHT UP OF ACCESS PANEL 9523. REMOVED ACCESS PANEL 9523 TO GAIN ENTRY REMOVED ATTACH RING PER SRM 51-30-2 AND REMOVED PREVIOUS REPAIR. STOP DRILLED CRACK IAW SRM 51-10-1. Aug 21, 1999 · N727DH · Boeing 727228SDR DHL9972757CBracket · crackedAT C-CHECK, NR 1 PYLON FWD IND END VERTICAL BRACKET CRACKED AT UPPER I/B END ACCESS PANEL 5407. REMOVED AND REPLACED BRACKET PER SRM 51-30-2, 9 X 4 N/R 6338.Aug 20, 1999 · N727DH · Boeing 727228SDR DHL9972752CBracket · crackedAT C CHECK, NR 1 ENG PYLON FWD I/B END VERTICAL BRACKET CRACKED AT UPPER I/B END ACCESS PANEL 5407. REMOVED THRUST REV SHUTOFF VALVE. REMOVED 6 BOLTS FROM QUADRANT DISCONNECTED THRUST REV QUADRANT DRUM FOR SM ACCESS PER MM 71-11-21. REMOVED AND REPLACED BRAAug 20, 1999 · N727DH · Boeing 727228SDR UF6A990815Modular 5 · damagedSBN - RIGHT MODULAR 5 IS PUNCTURED ON TOP AND DELAMINATING. MAINTENANCE REPAIRED DAMAGE. ALL WORK WAS DONE IAW BAE ATP SRM 54-10-01. (M)Aug 18, 1999 · N851AW · Bag ATPSDR UF6A990609Modular 6 · crackedSBN - LEFT MODULAR 6 IS CRACKED AT THE AFT FAIRING. MAINTENANCE REPAIRED CRACK. ALL WORK WAS DONE IAW BAE ATP SRM. (M)Aug 12, 1999 · N853AW · Bag ATPSDR 99FDEA00328Bolt · crackedNR 190 NR 3 PYLON AFT SPHERICAL BEARING, THROUGH BOLT FOUND WITH CRACK IND DURING MAGNAFLUX INSP. INSTALL NEW NR 3 PYLON AFT BEAR THROUGH BOLT PER EO 8-5410-7-430734 PART 4 STEP 12 AND 13.Aug 9, 1999 · Doug DC1010FSDR UPS99830448Doubler · crackedINSPECTION TYPE:C3, NR 1 PYLON LWR FWD EXTERNAL HORSE SHOE DOUBLER IS CRACKED. FABRICATED AND INSTALLED DOUBLER, MATERIAL ID PO NR 22463 7075-T6.080 IAW DC8 SRM 57-2-1A.Aug 6, 1999 · N801UP · Doug DC873FSDR 99ZZZX3196Stiffener · crackedDURING CONTINENTAL EXPRESS C-CHECK, FOUND LT MLG WHEELWELL AFT BULKHEAD, OUTBOARD STIFFENER CRACKED. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 54-20-04. AIRCRAFT APPROVED FOR RETURN TO SERVICE. TAT: 20,512.5 HOURS. TAC: 27,506. (X)Aug 5, 1999 · N59708 · Emb EMB120RTSDR UPS99830459Fairing · crackedINSPECTION TYPE:C3, NR 4 PYLON NOZZLE FAIRING HAS CRACKED FORMER. FABRICATED AND INSTALLED REPAIR IAW TIMCO REO NR 06674, HEAT TREATED REPAIR ANGLE AND CLIP IAW DAC DWG 9756774 GEN NOTE 23 AND TIMCO REO NR 0667 4, DC8 SRM 51-1-21.Aug 1, 1999 · N801UP · Doug DC873FSDR UF6A990777Module · wornSBN - THE MODULAR 6 TITANIUM TUBE HAS A HOLE IN IT AND IS WORN DEEPLY ON BOTH SIDES. MAINTENANCE ROUTED OUT THE HOLE AND SMOOTHED THE EDGES. THE CHAFFED AREAS WRE BLENDED OUT SMOOTH. ALL WORK WAS DONE IAW WITH ENGINEERING REPORT NR 99-131. (M)Jul 30, 1999 · N859AW · Bag ATPSDR AU990808Nacelle · fod(AUS) RIGHT ENGINE FIRE DECK FOD. A SCREWDRIVER WAS FOUND DURING THE PRE-FLIGHT INSPECTION.Jul 29, 1999 · Saab 340BSDR MWEA99456Angle · crackedUPPER AND LOWER RIB ANGLES AT STATION XN 61-410 IN LEFT PYLON IS CRACKED. MAINTENANCE FABRICATED AND INSTALLED REPAIR ANGLES.Jul 28, 1999 · N209ME · Doug DC932SDR UIEA99059Tee Chord · crackedDURING ROUTINE INSPECTION OF NR 1 AND NR 4 PYLONS, CRACKS WERE DISCOVERED IN THE RT UPPER TEE CHORD, FORWARD HORIZONTAL FLANGE, NACELLE STA 270. CRACK LENGTH IN NR 1 PYLON WAS 2.25 INCHES, NR 4 PYLON WAS 1.25 INCHES. REPAIRS ACCOMPLISHED IAW KLM DATA FAX 99-Jul 23, 1999 · N508MC · Boeing 747230BSDR 99ZZZX3052Tee Chord · crackedDURING ROUTINE INSPECTION OF NR 1 AND NR 4 PYLONS, CRACKS WERE DISCOVERED IN THE RT UPPER TEE CHORD, FORWARD HORIZONTAL FLANGE, NACELLE STA 270. CRACK LENGTH IN NR 1 PYLON WAS 2.25 INCHES, NR 4 PYLON WAS 1.25 INCHES. REPAIRS ACCOMPLISHED IAW KLM DATA FAX 99-Jul 23, 1999 · N508MC · Boeing 747230BSDR USAA990710Channel · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK FORWARD OUTBOARD ACCESS CUTOUT PYLON CHANNEL. INSTALLED DOUBLER PER TR 54-30-07. (M)Jul 17, 1999 · N405US · Boeing 737401SDR F3LA99102Fairing · crackedDEN - DURING C-CHECK INSPECTION, REPORTED CRACK IN NR 1 ENGINE NACELLE TAILCONE FAIRING AT AFT INBOARD ATTACH POINT. MAINTENANCE FABRICATED AND REPLACED RIB PER SRM 51-40-3 AND EA 51-737-003. (M)Jul 10, 1999 · N207AU · Boeing 737201SDR F3LA99101Fairing · crackedDEN - DURING C-CHECK INSPECTION, REPORTED CRACK IN NR 1 ENGINE NACELLE TAILCONE FAIRING AT FORWARD OUTBOARD ATTACH POINT. MAINTENANCE FABRICATED AND REPLACED RIB PER SRM 51-40-3 AND EA 51-737-003. (M)Jul 10, 1999 · N207AU · Boeing 737201SDR CA990719038Heat Shield · damaged(CAN) REFERENCE: IPC FIG 82 ITEMS 23, 29, AND 57. DURING 50 HR INSPECTION FOUND SHIELD P/N 41604-01 WITH 6 CHERRY MAX RIVETS PULLED OUT WHICH SECURES HEAT SHIELD TO SKIN P/N 41667-08 AND ANGLE P/N 40667-1 ON RT NACELLE. HEAT SHIELD SHOWS TO HAVE BEEN EITHEJul 10, 1999 · Piper PA31SDR UPS99230107Clevis · crackedINSPECTION TYPE:C, ENGINE NR 2 STRUTS ABOVE NR 2 HORIZONTAL FIRE WALL, CLEVIS CRACKED ON LOWER END OF LOWER STRUT. CLEVIS REPLACED IAW DWG 65-17553.Jul 9, 1999 · N928UP · Boeing 72722CSDR EIA990248Pan · wornHKG - DURING C/D CHECK, NR 3 PYLON FORWARD STRUT CLOSURE PAN, RT REAR CORNER SKIN WORN. CLOSURE PAN TRIMMED AND REPAIRED PER RS-R-71-90-34115. (M)Jul 9, 1999 · N481EV · Boeing 747132SDR EIA990243Spar · crackedHKG - DURING C/D CHECK, NR 1 PYLON LOWER SPAR WEB CRACKED AT NAC 221.5 BL 0, DURING EO ACCOMPLISHMENT. REPAIRED PER SRM 54-10-03 FIG 2. (M)Jul 9, 1999 · N481EV · Boeing 747132SDR EIA990235Fitting · nickedHKG - DURING C/D CHECK, NR 4 PYLON UPPER FRONT SPAR FITTING AT STATION 225 HAS SEVERAL BAD NICKS. REPAIRED PER RS-R-54-54-34111 AND SRM 54-40-01 FIG 1, 8110-3. (M)Jul 9, 1999 · N481EV · Boeing 747132SDR EIA990234Fitting · corrodedHKG - DURING C/D CHECK, NR 4 PYLON UPPER FRONT SPAR FITTING AT STATION 225, CORROSION FOUND IN BUSHING BORE. REPAIRED BUSHING BORE IAW SB 747-54-2164 FIG 2, INSURANCE CUT TO FINAL SIZE 2.360 INCH AND RS-R-54-34085, 8110-3. (M)Jul 9, 1999 · N481EV · Boeing 747132SDR HNAA9900092Angle · chafedNR 1 ENG HORSE COLLAR CHAFED ON INBOARD SIDE, FWD ANGLE DOUBLER. PART OF MONOCOQUE STRUCTURE OF NAC CAUSE BY BONDING STRAP DEPTH= .016. BLENDED AREA IAW EO8-54-99-727.Jul 4, 1999 · N938HA · Dhav DHC8102SDR A6WA9900084Bolt · failedNR 2 ENGINE PYLON TO WING, OUTBOARD LOWER BOLT HAD IS SHEARED OFF. REPLACED LOWER OUTBOARD WING TO PYLON BOLT IAW MM 54-52-00. (X)Jul 2, 1999 · N614AW · Bag BAE146300ASDR EIA990215Block · scratchedHKG - DURING C/D CHECK, NR 3 NACELLE STRUT FORWARD UNIVERSAL BLOCK FOUND DEEP SCRATCH MARKS IN BUSHING BORE AREA. REPLACED FORWARD MOUNT UNIVERSAL BLOCK ASSEMBLY PER MM 71-21-02. (M)Jun 29, 1999 · N481EV · Boeing 747132SDR ABXA9900555Angle · crackedDURING C-CHECK, FOUND NR 1 PYLON LEFT LOWER ATTACH ANGLE CRACKED AT STATION 990. REPAIRED ANGLE IAW DC9 SRM 54-04.Jun 28, 1999 · N987AX · Doug DC932SDR EIA990201Fitting · corrodedHKG - DURING C/D CHECK, NR 2 PYLON DIAGONAL BRACE AFT WING FITTING HAS 2 BOLT HOLES WITH CORROSION IN BORES. NR 2 PYLON DIAGONAL BRACE AFT WING FITTING BOLT HOLE CORROSION REMOVED BY OVERSIZING. HOLE SIZES TO MAX LIMIT PER SB 54-2159. (M)Jun 26, 1999 · N481EV · Boeing 747132SDR EIA990199Pan · wornHKG - DURING C/D CHECK, NR 1 PYLON FORWARD STRUT CLOSURE PAN LEFT AND RIGHT SKIN WORN. STRUT CLOSURE PAN REPAIRED PER RS-R-71-90-34116, 8110-3. (M)Jun 26, 1999 · N481EV · Boeing 747132SDR DL72L991467Angle · corrodedON HUSH-KIT MOD, FOUND RT NR 2 AFT MOUNT CHORD ANGLE CORRODED BEYOND MFG SPECS. REPLACED RT CHORD ANGLE WITH ONE OF NEW MFG.Jun 26, 1999 · N509DA · Boeing 727232SDR CALA9900729Support · crackedINSPECTION FOUND A 3 INCH CRACK IN NR 1 ENGINE DIAGONAL FRAME SUPPORT AT NACELLE STA 315 ON RT SIDE. THE DIAGONAL FRAME SUPPORT WAS REPLACED IAW SRM 51-40-02.Jun 26, 1999 · N60312 · Boeing 7373T0
Back to JASC 5400