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 20000501SH006Support Bracket · crackedTHE SUPPORT ASSY (MOUNTING BRACKET) FOR BOTH THE LEFT AND RIGHT ENGINE FIRE EXTINGUISHER BOTTLES WAS FOUND CRACKED. THIS MOUNTING BRACKET HAS BEEN FOUND CRACKED ON SEVERAL OTHER MODEL 2000 AIRCRAFT. SUBMITTER STATED THEIR EXPERIENCE HAS BEEN THAT A REPLACEMEApr 4, 2000 · N638LD · Beech 2000SDR RRXA001748Angle · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK ON THE INBD DRAG ANGLE ON FOR NR 3 PYLON 1 INCH AFT WING SPAR AT XRS 198, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW DRAG ANGLE IAW DC-8 SApr 3, 2000 · N2674U · Doug DC873FSDR TWAA0004703Angle · crackedDURING OP 16 MAINT CHECK, THE RT PYLON UPPER ATTACH ANGLE WAS CRACKED, RT SIDE APPROX STA 980. CRACK RUNS FWD .25 INCH. STOP DRILLED CRACK PER SRM 34-04, FIG 10. MANUFACTURED REPAIR ANGLE PER SRM 54-04 FIG 10 SHEET 4. INSTALLED REPAIR ANGLE WET AND WITH APMar 20, 2000 · N989Z · Doug DC931SDR AU000975Connector · damaged(AUS) NR 2 PYLON HARNESS FIREWALL CONNECTOR DAMAGED DUE TO ARCING.Mar 6, 2000 · Boeing 737377SDR P5CA0000092Fairing · errodedNR 4 ENGINE PYLON STRUT TO WING FAIRING EROSION. REPAIRED PER SRM 51-40-09.Feb 22, 2000 · N859FT · Boeing 747123SDR UPS00231879Bracket · crackedINSPECTION TYPE:C&SI, ENGINE NR 1 THROTTLE SHUT OFF CONTROL BRACKET ASSY IN FWD END OF PYLON IS CRACKED. BRACKET REPLACED IAW MM 76-11-21.Feb 18, 2000 · N908UP · Boeing 72727CSDR KPVA200008Angle · crackedRIGHT NACELLE TO WING INBOARD AND OUTBOARD DRAG ANGLES CRACKED AT STATION YW171 AND YW139 XN 169. REPAIRED DRAG ANGLES AT STATIN YW171 AND YW139 XN 169 IAW RD8-54-1053. (M)Feb 17, 2000 · N803WP · Dhav DHC8103SDR KPVA200009Angle · crackedLEFT NACELLE TO WING INBOARD DRAG ANGLE AT STATION YW139XN127 TO DN169 CRACKED. REPLACED NACELLE TO WING INBOARD DRAG ANGLE AT STATION YW139 XN127 TO XN169 IAW DHC-8 SRM 1-8-3 CHAPTER 51 AND DEHAVILLAND DRAWING (CARD 54-10-4023). (M)Feb 17, 2000 · N803WP · Dhav DHC8103SDR KPVA200020Fairing · debondedRIGHT NACELLE TAIL INBOARD FAIRING DISBONDED ON EXTERNAL SURFACE AT STATION XN250. REPAIRED DISBONDING IAW DHC-8 RD 8-54-0153. (M)Feb 17, 2000 · N803WP · Dhav DHC8103SDR KPVA200021Fairing · debondedRIGHT NACELLE INBOARD FAIRING INTERNAL SURFACE DISBONDING AT STATION XN245. REPAIRED FAIRING AT STATION XN245 IAW DHC8- RD8-54-1195. (M)Feb 17, 2000 · N803WP · Dhav DHC8103SDR DL72K000291Housing · crackedA 2 INCH CRACK AT NR 2 ENGINE INLET HOUSING BELOW ACCESS PANEL 9523. REPAIRED PER M/M 54-30-0 PG 803 - 804.Feb 11, 2000 · N414DA · Boeing 727232SDR MWEA00050Bracket · crackedFOUND ANGLE BRACKET ON LEFT ENGINE PYLON LOWER SIDE AT ACCESS PANEL 8105A CRACKED. MAINTENANCE FABRICATED AND INSTALLED BRACKET REPAIR.Feb 6, 2000 · N215ME · Doug DC932SDR MWEA00049Web · crackedFOUND WEB ON LEFT ENGINE PYLON LOWER SIDE AT ACCESS PANEL 8105A CRACKED. MAINTENANCE FABRICATED AND INSTALLED WEB REPAIR.Feb 6, 2000 · N215ME · Doug DC932SDR TWAA0002315Structure · corrodedDURING OP 16 MAINTENANCE CHECK, ON NUMBER 1 PYLON TOP AND BOTTOM OF PYLON FOR ENG MOUNT YOKE STRUCTURE HAD RUSTY SURFACES AT LE ATTACH. CHECKED MATERIAL THICKNESS PER SPM 04-00. REPAIRED PER ARA 16530 AND SRM 54-04 PAGE 77. SHOT PEENED PER DRS 4999.Feb 2, 2000 · N925L · Doug DC932SDR DL757000241Bushing · corrodedNR 1 PYLON UPPER LINK (P/N 311N3710-901) FOUND CORROSION IN LOWER BUSHING. AFTER REMOVAL OF DAMAGE, BUSHING WAS WORN BEYOND LIMITS. NEW BUSHING INSTALLED (P/N 310N3026-15). NO DAMAGE FOUND IN BORE OR UPPER LINK. DAMAGE WAS ISOLATED TO BUSHING ONLY.Jan 31, 2000 · N635DL · Boeing 757232SDR RRXA000644Fitting · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE FOOTSTOOL SUPPORT FITTING UPPER END NR 4 PYLON I/B SIDE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED IAW DC-8 SRM 51-3-0 AND DAC DWG 357Jan 30, 2000 · N831AL · Doug DC873FSDR QXEA9902718Web · corrodedPDX - RIGHT NACELLE TOP DECK AFT PORTION HAS CORROSION WHERE EXHAUST FINGERNAIL MOUNTS BETWEEN STATION XN255 AND XN286.0. REPAIRED IAW DHC-8 SRM 51-40-4.Dec 23, 1999 · N825PH · Dhav DHC8102SDR QXEA9902699Web · corrodedPDX - RIGHT NACELLE TOP DECK AFT PORTION HAS CORROSION WHERE EXHAUST FINGERNAIL MOUNTS BETWEEN STATION XN255 AND XN280.00. REPAIRED IAW DHC-8 SRM 51-40-00 AND SRM 51-40-11.Dec 23, 1999 · N825PH · Dhav DHC8102SDR AALA991984Web · corrodedTUL - NR 3 PYLON AFT UPPER WEB HAS FRETTING CORROSION ON BOTH INBOARD AND OUTBOARD EDGES IN 2 AREAS OF LAST 12 INCHES OF ONE AREA INBOARD SIDE OF AFT LIGHTENING HOLE. TREATED AND REPAIRED PER SRM 54-20-00 FIG 34 (VOL I). INSTALLED DOUBLER PER SRM 54-20-00 FIDec 21, 1999 · N163AA · Doug DC1030SDR QXEA9902695Web · chafedPDX - TOP EXHAUST DECK HAS CHAFE HOLE CENTER OF DECK AT RIVET LINE. REPAIRED IAW RD8-54-866.Dec 20, 1999 · N285PH · Dhav DHC8102SDR QXEA9902698Web · puncturedPDX - AFT NACELLE TOP DECK HAS A PUNCTURE HOLE AT APPROXIMATELY STATION X236.00 AND YW139.900. REPAIRED IAW HORIZON AIR EA 9-54-237.Dec 19, 1999 · N825PH · Dhav DHC8102SDR TWAA0005809Angle · crackedDURING OP 16 MAINT CHECK, NUMBER 2 PYLON FWD END OF CANNON PLUG CONNECTOR HOOK UP, IN PYLON FWD I/B ANGLE WAS CRACKED OUT BEYOND STOP DRILL. ADDITIONAL DAMAGE FOUND ON ANGLE. REMOVED AND REPLACED PER DRAWING 9958193. CANCELLED ARA 16323 WITH 16323A. REPLACDec 13, 1999 · N925L · Doug DC932SDR QXEA9902633Heat Shield · chafedYXX - LEFT NACELLE DISHED HEAT SHIELDS HAVE CHAFE DAMAGE. REPAIRED IAW DHC-8 SRM 51-20-16, SRM 51-20-36 AND RD8-54-1442.Dec 12, 1999 · N355PH · Dhav DHC8202SDR QXEA9902634Heat Sheild · crackedYXX - LEFT HEATSHIELD TO FINGERNAIL ATTACH TABS AT XN280 IS CRACKED ON OUTBOARD TAB. REPAIRED IAW RD8-54-163 AND DHC-8 SRM 51-40-11.Dec 9, 1999 · N355PH · Dhav DHC8202SDR QXEA9902635Heat Shiled · chafedYXX - RIGHT OUTBOARD DISHED HEAT PANEL HAS CHAFE DAMAGE ON INBOARD SIDE AT XN223. REPAIRED IAW RD8-54-194.Dec 8, 1999 · N355PH · Dhav DHC8202SDR QXEA9902628Heat Shield · chafedYXX - RIGHTHEATSHIELD HAS CHAFE DAMAGE AT XN245.0. REPAIRED IAW DHC-8 RD8-54-866.Dec 8, 1999 · N355PH · Dhav DHC8202SDR 20000609AP010Angle · crackedDURING C-CHECK, FOUND NR 1 ENGINE PYLON T/E RIB ATTACH ANGLE CRACKED AND RIB HOLES ELONGATED. REMOVED CRACKED ANGLE, FABRICATED NEW REPAIR PARTS PER SRM 51-40-2. INSTALLED NEW REPAIR PARTS AND SEALED AREA PER SRM 51-10-1 AND SRM 51-40-2. (M)Nov 30, 1999 · N802EA · Boeing 727225SDR TWAA0005808Angle · crackedDURING OP 16 MAINT CHECK, NUMBER 2 PYLON INTERIOR, O/B VERTICAL ANGLE WAS CRACKED AT BOTTOM, JUST AFT OF 13TH STAGE PNEUMATIC DUCT. DIRECTLY BELOW FIRE SPRAY TUBE. REPAIRED FLANGE USING 2 FABRICATED DOUBLERS OF 0.012 ALUMINUM PER SRM 53-01, PAGE 10 FIG 2, SHNov 29, 1999 · N925L · Doug DC932SDR QXEA9902616Heat Shield · chafedYXX - LEFT NACELLE HEAT SHIELD HAS CHAFFING DAMAGE ON TOP SIDE AT STATION XN255.00. REPAIRED IAW RD8-54-177.Nov 29, 1999 · N356PH · Dhav DHC8202SDR MZZA99231Flange · crackedTNN - DURING HALF D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 1 INCH LONG CRACK WAS FOUND ON NR 2 ENGNE S-DUCT MOUNTING FLANGE AT BS 1342. THE CRACKED FLANGE WAS REMOVED AND REPLACED WITH A NEW ONE PER B727SB 727-54-15R2 AND CMI ECRA 5410-01525. (M)Nov 21, 1999 · N622DH · Boeing 727264SDR 20000613AP010Rib · crackedDURING C-CHECK, FOUND NR 3 ENGINE PYLON T/E INNER COMPARTMENT, AFT OF AFT ENGINE MOUNT SUPPORT RIB CRACKED. FABRICATED NEW MOUNT SUPPORT RIB PER SRM 51-10-2 PAGE 1 AND INSTALLED PER SRM 51-30-2 PAGE 1. (M)Nov 13, 1999 · N802EA · Boeing 727225SDR DL72L992508Angle · corrodedON HEAVY WEIGHT HUSH-KIT MOD, FOUND RT AFT MOUNT CHORD ANGLE CORRODED BEYOND MFG SPECS. REPLACED RT CHORD ANGLE WITH ONE OF NEW MFG.Nov 13, 1999 · N507DA · Boeing 727232SDR DL72L992507Angle · corrodedON HEAVY WEIGHT HUSH-KIT MOD, FOUND NR 2 ENG AFT MOUNT SUPPORT LT CHORD ANGLE CORRODED BEYOND MFG SPECS. REPLACED LT CHORD ANGLE WITH ONE OF NEW MFG.Nov 12, 1999 · N507DA · Boeing 727232SDR 2000T74R547EWMetal Strip · crackedDURING C-CHECK. NR 2 ENGINE LT SIDE METAL STRIP ABOVE REVERSER COWL HAS .75 INCH CRACK. NDT TO DETERMINE LENGTH OF CRACK. STOP DRILLED AND NDT TO CONFIRM CRACK. STOP DRILLED - BROKEN SHARP EDGES. TREATED, PRIMED AND FILLED STOP DRILL HOLES WITH SEALER PERNov 12, 1999 · N8079U · Doug DC871SDR TWAA9917409Stiffener · wornDURING OP 16 MAINT CHECK ON NUMBER 2 PYLON, THE SIDE COWL PANEL VERTICAL STIFFENER HAD WORN THROUGH AT REPAIR AND METAL HAD NOT BEEN ROUTED OUT TO PREVENT FURTHER CRACKING. ACCOMP EDDY CURRENT INSPECTION PER NDT 51-00-03 AND FOUND CRACK CONTAINED. REPAIRED PNov 10, 1999 · N925L · Doug DC932SDR QXEA9902234Angle · damagedPDX - ANGLE ATTACHMENT FOR OUTBOARD NACELLE SKIN TO WIG BOX, TO FROM MAIN LANDING GEAR FRAME. REPAIRED IAW HORIZON AIR EA 9-53-485.Oct 30, 1999 · N827PH · Dhav DHC8102SDR ABXA9900783Stiffner · crackedDURING C-CHECK, FOUND NR 1 PYLON INTERIOR WEB STIFFENER BETWEEN 8TH AND 13TH DUCT CRACKED AT END. REPLACED STIFFENER IAW DC9 SRM 54-10-0.Oct 27, 1999 · N904AX · Doug DC932FSDR ASOA99130Stiffener · crackedDURING INSPECTION, FOUND LEFT NACELLE FLAP TOP SKIN STIFFENER HAS A CRACK. MAINTENANCE REPAIRED STIFFENER IAW EMB 120 SRM 54-20-02. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE (M)Oct 18, 1999 · N269AS · Emb EMB120RTSDR WXOA99019Angle · crackedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, NDT HFEC DETECTED A CRACK ON ANGLE P/N 9912243-10 AT THE RIGHT PYLON BULKHEAD LOWER FRONT SPAR (F/S 786) EXTENDING FROM FASTENER HOLE APPROX .400 INCH LONG. REMOVED AND REPLACED ANGLE IAW DC-9 SRM Oct 15, 1999 · N127NK · Doug DC921SDR WXOA99017Fitting · crackedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, NDT HFEC INSPECTIN PERFORMED PER OPS 4.751 OF LEFT PYLON 'BATH TUB' FITTING. INDICATION OF CRACK NOTED AT FAIL/SAFE STRAP INBOARD UPPER RIVET. DIMENSION OF CRACK APPROXIMATELY 2.5 INCH IN LENGTH. Oct 15, 1999 · N127NK · Doug DC921SDR SIMA992881Mount · chafedSAW - DURING PS-2 INSPECTION, FOUND THE LEFT ENGINE BLEED AIR SHUTOFF VALVE HAD CHAFED THROUGH THE AFT OUTBOARD ZEE MOUNT. REMOVED AND REPLACED THE ZEE MOUNT IAW JIC 542161-RAI-1000-007. AIRCRAFT RETURNED TO SERVICE. (M)Oct 15, 1999 · N971NA · Aerosp ATR42300SDR QXEA9902254Web · chafedPDX - RIGHT NACELLE AFT WALL OF WHEEL WELL IS CHAFED WHERE LOWER PORTION OF GRAVEL GUARD ATTACHES. REPAIRED IAW RD 8-54-041.Oct 14, 1999 · N827PH · Dhav DHC8102SDR ABXA9900753Angle · crackedDURING C-CHECK, FOUND NR 2 ENGINE PYLON UPPER ATTACH ANGLE CRACKED AT STATION 950. REPAIRED ANGLE IAW DC9 SRM 54-04.Oct 14, 1999 · N928AX · Doug DC932SDR ASOA99116Stiffener · crackedDURING C-CHECK, FOUND RIGHT NACELLE AFT OUTBOARD STIFFENER IS CRACKED. MAINTENANCE REMOVED AND REPLACED RIGHT NACELLE STIFFENER IAW EMB120 SRM 51-40-02. (M)Oct 13, 1999 · N227AS · Emb EMB120RTSDR WXOA99008Clips · crackedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, CRACKS DETECTED IN TWO CLIPS ON RIGHT ENGINE LOWER APRON. REMOVED CRACKED CLIPS, FABRICATED REPAIR CLIPS PER DC-9 SRM 51-10-2 AND SAMPLE, ALODINE AND PRIMED CLIPS PER DC-9 SRM 51-10-3, AND INSTALLEOct 12, 1999 · N127NK · Doug DC921SDR WXOA99007Angle · crackedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, PERFORMED NDT HFEC INSPECTION PER OPS 4.735. RESULTS OF INSPECTION DETECTED CRACK ON ANGLE P/N 9912243-9 AT THE LEFT PYLON LOWER FRONT SPAR STATION Y781/Z20. REMOVED CRACKED ATTACH ANGLE AND INSTAOct 11, 1999 · N127NK · Doug DC921SDR CALA9901363Support · crackedPYLON NUMBER ONE SUPPORT PANELS 437DR/437ML CRACKED (0.5). REPLACED SUPPORT PER SRM 51-31-01.Oct 8, 1999 · N19072 · Doug DC1030SDR AT9900713Angle · crackedFOUND RIGHT PYLON WEB LOWER SUPORT ANGLE FOUND 3 CRACK, PYLON STATION 105 3 BELOW PYLON REFERANCE PLANE, 5 OUTBOARD FUSELAGE SKIN. REMOVED SUPPORT ANGLE, FABRICATED AND INSTALLED NEW SUPPORT ANGLE IAW DC9 SRM 51-10-2, 51-10-3, 51-30-2, 51-30-4.Oct 6, 1999 · N812AT · Doug DC932SDR 99FDEA00418Hardware · loose12 OFF MOUNTING BOLTS LOOSE AND 3 OFF NUTS MISSING FROM SHEAR WEB FORGINGS ON AFT NR 1 PYLON FRAME, ADJACENT TO SPHERICAL BEARING FITTING. REMOVED AND REPLACED PER MM 70-00-00-2.Oct 6, 1999 · N317FE · Doug DC1030FSDR UF6A990958Angle · damagedSBN - THE RIGHT MODULAR 7 AFT SUPPORT ANGLE BRACKET IS BROKEN. MAINTENANCE REMOVED AND REPLACED BRACKET. (M)Sep 30, 1999 · N856AW · Bag ATP
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