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 DL72S953081Skin · crackedDURING HMV, FOUND CRACK IN SKIN INSIDE NR 2 ENG INLET S-DUCT. REPAIRED PER SRM 54-10-3 FIG 13.Jun 26, 1995 · N489DA · Boeing 727232SDR 95ZZZX4121Bolt · crackedNR 3 PYLON - LOWER RT BOLT, P/N HC574H0036-20D, REQUIRES REMOVAL FOR VERIFICATION OF CRACK INDICATIONS, REF SSI 57-20-174. REMOVED AND REPLACED RT LOWER NR 3 PYLON BOLT, P/N HC574H0036-200, IAW A.M.M.Jun 20, 1995 · N463AP · Bag BAE146100ASDR 95ZZZX4120Bolt · crackedNR 2 ENGINE YOKE TO PYLON BOLT, LEFT TOP TO BE REMOVED FOR MAINTENANCE INSPECTION OF CRACK INDICATION ON THREAD RUN-OUT AREA. REF: P/N HC712H0041-000. SSI 54-00-123. CARD NR 268. REPLACED NR 2 ENGINE YOKE TO PYLON BOLT AT LEFT TOP POSITION.Jun 20, 1995 · N463AP · Bag BAE146100ASDR 95ZZZX3274Gusset · corrodedANNUAL INSPECTION FOUND GUSSET LOCATED BELOW AUGMENTOR IN LT ENG NACELLE COMPLETELY CORRODED THROUGH. NUMEROUS RIVETS IN AREA WERE GONE ALSO DUE TO CORROSION FROM EXHAUST GASSES AND HEAT OVER THE YEARS. PART IS LOCATED IN NACELLE ON TOP OF WING SKIN AND CONNJun 17, 1995 · N1719H · Cessna 310CSDR RAIA950616Latch · unlatchedSTL - FLT 7460 - LEFT ENGINE INBOARD FORWARD COWL LATCH NOT SECURED. CREW LANDED IN PAH AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED ENGINE COWL NO DEFECTS WERE NOTED. MAINTENANCE SECURED LATCH. LATCH REINSPECTED NEXT STATION FOR SECURITY, CHECK OK. Jun 13, 1995 · N124AM · Emb EMB120RTSDR 95ZZZX6190Pulley Drum · failedDURING ENGINE REMOVAL, NR 2 CENTER POSITION USING THE MFR INSTALLED AVIAC HOISTING WINCH, HOIST FAILED ALLOWING ENG TO RAPIDLY DROP BREAKING CABLE AND HITTING FLOOR. CABLE STOW TORQUE WAS CHECKED USING HOIST WINCH TORQUE TOOL. AFTER PROPER STOW, TORQUE WAS EJun 12, 1995 · N86AK · Amd FALCON50MYSTSDR MALA954500Angle · crackedMSP - DURING SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED THE RT LOWER WING TO NACELLE TRANSIT ANGLE WAS CRACKED AT THE LEADING EDGE. MAINTENANCE REPLACED THE FORWARD 8 INCH SEGMENT AND APPLIED A DOUBLER IAW FAIRCHILD ARP 54-20-9101. (X)Jun 8, 1995 · N60NE · Swrngn SA227ACSDR UPS803472Fitting · crackedWHILE IN C-CHECK, MAINTENANCE FOUND CRACK ON NR 3 PYLON SUPPORT FITTING. REPLACED FITTING IAW SRM 51-1-20D.Jun 7, 1995 · N867UP · Doug DC873FSDR TWRA954493Structure · damagedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND RT NACELLE INBOARD LOWER FORMER, NS 99.79, CRACKED AT LOWER KEELSON ATTACH FLANGE. COMPLETED REPAIRS TO RT NACELLE. REPLACED SKIN P/N 27-35112-2-03, ANGLE 27-31128-016, FORMER 27-35025-968. REPAIRED FOJun 7, 1995 · N446MA · Swrngn SA227ACSDR DLM88952488Angle · cracked.50 INCH CRACK IN UPPER PYLON ATTACH ANGLE 18 INCHES FROM AFT WEDGE. FOUND DURING E-1 LTR CK. REPAIRED PER SRM 54-04A PG 17-18.Jun 6, 1995 · N970DL · Doug MD88SDR PLGA64951Keel Web · crackedDURING PERFORMANCE OF A NR 1 DETAIL WING INSPECTION THE LEFT NACELLE OUTBOARD KEEL WEB (P/N 114-980022-1) WAS FOUND TO HAVE A CRACK APPROXIMATELY 3 INCHES IN LENGTH. THE CRACK WAS ON THE FORWARD FLANGE THAT RIVETS TO THE ENGINE BAY AFT FIREWALL, ON THE LOWER Jun 4, 1995 · N807BE · Beech 1900CSDR USAA950668Angle · crackedPIT - DURING Q-3 CHECK INSPECTION, FOUND .1250 INCH CRACK IN LEFT PYLON TOP ATTACH ANGLE AT STA 980. CUT OUT DAMAGED AREA AND INSTALLED FILLER AND DOUBLER REPAIR PER SRM 54-04, FIGURE 10. (X)Jun 1, 1995 · N983VJ · Doug DC931SDR DLM88952360Angle · crackedFOUND DURING D-1 LETTER CHECK - .25 INCH CRACK IN RT UPPER ENG PYLON TO FUSELAGE ANGLE 12 INCHES FROM AFTM EDGE. REPAIRED PER SRM 54-04A PG17 FIG 4.May 31, 1995 · N992DL · Doug MD88SDR DL72S952343S Duct · bentAT HMV FOUND S-DUCT LE RIM BENT AND WORN. REPAIRED PER SRM 54-10-3 FIG 13.May 31, 1995 · N497DA · Boeing 727232SDR P5CA9500190Bracket · brokenBROKEN BRACKET THAT ATTACHES FUEL FEED LINE ON NR 3 PYLON CLOSURE SPAR APPROXIMATELY NS 236. FABRICATED NEW BRACKET PER SRM 54-30-02.May 28, 1995 · N831FT · Boeing 747121SDR P5CA9500189Angle · crackedCRACK ON ANGLE ON NR 3 PYLON CLOSURE SPAR RIGHT INSIDE, APPROXIMATELY NS 215 TO 290. FABRICATED NEW ANGLE AS PER SRM 54-10-02, INSTALLED PER SRM 51-30-02.May 28, 1995 · N831FT · Boeing 747121SDR P5CA9500188Angle · crackedCRACK AND DAMAGE ON ANGLE THAT ATTACHES FAIRING TO WING RIGHT ADJACENT TO UPPER LINK FITTING NS 222 NR 3 PYLON. REPLACED ANGLE PER BOEING SRM 54-10-02.May 28, 1995 · N831FT · Boeing 747121SDR P5CA9500187Rib · crackedCRACK WITH STOP HOLE ON INNER RIB SIDE AT NS 222 NR 3 PYLON. REPAIRED PER BOEING SRM 54-10-03.May 28, 1995 · N831FT · Boeing 747121SDR P5CA9500186Spar · chafedCHAFING ON INSIDE OF LOWER SPAR FROM NS 180 TO NS 236, NR 3 PYLON. REPLACED WEAR STRAPS PER BOEING SRM 51-30-02.May 28, 1995 · N831FT · Boeing 747121SDR 9509115528Bracket · crackedDURING PERIODIC CHECK, FOUND A 3.75 INCH CRACK IN THE NR 1 ENGINE FAN COWL SUPPORT BEAM ANGLE STA 105. REPAIRED ANGLE PER EA 55-98490.May 28, 1995 · N528US · Boeing 757251SDR P5CA9500133Sail Boat · damagedDAMAGE ON LOWER SAIL BOAT NS 301 NR 3 PYLON. REPAIRED PER BOEING SRM 51-30-02.May 27, 1995 · N831FT · Boeing 747121SDR P5CA9500130Spar · damagedDAMAGE ON LOWER SPAR STRAP NS 222 FIREWALL NR 3 PYLON. REPAIRED PER BOEING SRM 54-30-03 FIG 35.May 27, 1995 · N831FT · Boeing 747121SDR P5CA9500097Spar · chafingCHAFING ON BOTH SIDES LOWER SPAR FROM INSIDE NS. 180 TO NS. 236. FABRICATED NE STRAPS AS PER BOEING SRM 54-10-02, INSTALLED PER SRM 51-30-02.May 27, 1995 · N831FT · Boeing 747121SDR P5CA9500096Blow Out Panel · damagedNR 2 PYLON DAMAGE ON CUT-OUT ON BLOW OUT PANEL AT NS. 180. INSTALLED DOUBLER PER BOEING SRM 54-10-02 AND 51-30-02.May 27, 1995 · N831FT · Boeing 747121SDR P5CA9500095Fairing · crackedNR 2 PYLON HAS CRACK WITH STOP HOLE ON LOWER SAIL BOAT AT NS. 286. DAMAGED SECTION REMOVED FROM SAIL BOAT, FOUND WITHIN LIMITS PER SRM 54-10-01.May 27, 1995 · N831FT · Boeing 747121SDR P5CA9500092Strap · bentNR 2 PYLON STRAP VENT ON LOWER SPAR AT NS. 180. NEW STRAP FABRICATED PER SRM 54-30-03, INSTALLED PER SRM 51-30-02.May 27, 1995 · N831FT · Boeing 747121SDR P5CA9500091Strap · damagedNR 2 PYLON RIGHT SIDE FORWARD LOWER STRAP IS DAMAGED AT NS. 128. NEW STRAP FABRICATED AS PER SRM 54-10-02 AND INSTALLED AS PER SRM 51-30-02.May 27, 1995 · N831FT · Boeing 747121SDR DLL10952437Web · crackedAT HMV, WEB CRACKED 1 INCH LONG JUST AFT NR 2 ENG INLET RING INTERIOR TO PNL 311RL. REPAIRED PER SRM 54-34-00 FIG 804.May 27, 1995 · N721DA · Lkheed 10113851SDR DLL10952410Web · crackedAT HMV, WEB CRACKED 1.5 INCH LONG JUST AFT OF NR 2 ENG INLET RING INTERIOR TO PNL 311NL. REPAIRED PER SRM 54-34-00 FIG 804.May 27, 1995 · N721DA · Lkheed 10113851SDR DLL10952409Web · crackedAT HMV, WEB CRACKED 3 EACH THE RIVET BUCKTAIL, EACH APPROX 1 INCH LONG JUST AFT NR 2 ENG INLET RING INTERIOR TO PNL 311DR, 3 O'CLOCK. REPAIRED PER SRM 54-34-00 FIG 804.May 27, 1995 · N721DA · Lkheed 10113851SDR DLL10952408Intercostal · crackedAT HMV, WEB CRACKED 2 INCHES LONG JUST AFT NR 2 ENG INLET RING INTERCOSTAL PNL 311DR, 4 O'CLOCK. REPAIARED PER SRM 54-34-00 FIG 804.May 27, 1995 · N721DA · Lkheed 10113851SDR DLL10952407Intercostal · crackedAT HMV, WEB CRACKED 2 INCHES LONG JUST AFT OF NR 2 ENG INLET RING INTERCOSTAL PNL 311AR, 11 O'CLOCK. REPAIRED PER SRM 54-34-00 FIG 804.May 27, 1995 · N721DA · Lkheed 10113851SDR UPS203335Web · crackedWHILE IN SI CHECK, MAINTENANCE FOUND LT PYLON WEB CRACKED ON UPPER VERTICAL STAB. REMOVED AND REPLACED WEB IAW SRM 51-30-2.May 26, 1995 · N919 · Boeing 72730CSDR 95ZZZW771Doubler · crackedON B-CHECK INSPECTION, FOUND CRACK IN DOUBLER PLATE NACELLE STATION 180, ON 4 PYLON INBOARD. INSTALLED REPAIR DOUBLER IAW SERVICE BULLETIN 54-2034 REV 4. TOTAL CYCLES 18,040.May 26, 1995 · N853FT · Boeing 747122SDR USAA950695Angle · crackedPIT - DURING Q-5 CHECK INSPECTION, FOUND 1 INCH CRACK IN THE STA 1480 UPPER PYLON ATTACH ANGLE RT SIDE. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER TO ANGLE PER SRM 54-04 FIG 10 SHT 3. (W)May 25, 1995 · N809US · Doug DC981SDR MALA954474Angle · crackedMSP - DURING PHASE INSPECTION IN MSP, MAINTENANCE FOUND LT INBOARD UPPER WING TO NACELLE ANGLE PN 27-335112 FORWARD END AT STA 115.00 CRACKED APPROXIMATELY 1 INCH IN RADIUS. FABRICATED AND INSTALLED NEW ANGLE IAW FAIRCHILD SRM 51-00-00, PAGE 4, 51-30-00, AND May 25, 1995 · N60NE · Swrngn SA227ACSDR MALA954473Angle · crackedMSP - DURING PHASE INSPECTION IN MSP, MAINTENANCE FOUND LEFT INBOARD LOWER WING TO NACELLE ANGLE PN 27-35112 FORWARD END, AT APPROXIMATE STA 115.00 CRACKED APPROXIMATELY 1 INCH IN RADIUS AND HAS AN ELONGATED RIVET HOLE. FABRICATED AND INSTALLED NEW ANGLE PN 2May 25, 1995 · N60NE · Swrngn SA227ACSDR UPS803301Angle · crackedWHILE IN C CHECK, MAINTENANCE FOUND CRACK AT THE NR 1 PYLON FORWARD HOLE OF THE INBD. SKATE ANGLE LOWER FRONT SPAR.May 24, 1995 · N802UP · Doug DC873FSDR PLGA523951Keel · crackedDURING NR 1 DETAIL (WING) INSPECTION, THE LEFT NACELLE UPPER FORWARD KEEL (OUTBOARD) WAS FOUND TO HAVE 4 CRACKS ON FORWARD EDGE FLANGE. THESE CRACKS WERE FROM .375 INCH TO 1 INCH IN LENGTH BETWEEN RIVETS ON FORWARD EDGE FLANGE. AN APPROVED REPAIR IS BEING DEMay 23, 1995 · N817BE · Beech 1900CSDR DLM88952199Angle · crackedNR 2 ENG PYLON TO FUSELAGE UPPER ATTACH ANGLE CRACKED 1 INCH. FOUND DURING D-1 LTR CK TPAMM. REPAIRED PER SRM 54-04A FIG 4.May 19, 1995 · N986DL · Doug MD88SDR 95ZZZZ240Angle · crackedLT PYLON ANGLE HAS 1 INCH LONG CRACK ON LOWER SIDE, 6 INCHES OF AFT CONE BOLT. REPLACED ANGLE PER SRM 51-40-12.May 18, 1995 · N2FOR · Boeing 737317SDR MALA954463Former · crackedDURING A PHASE INSPECTION IN MSP, FOUND A CRACK IN LEFT INBOARD NACELLE FORMER AT NS 120.00. THE REPAIRS WERE COMPLETED BY REPLACING THE FORMER P/N 27-35025-967 AND A SKIN PANEL, P/N 27-35001-178. ALL WORK WAS PERFORMED IAW FAC SRM 51-00-00 PAGE 4, 51-30-00,May 17, 1995 · N442MA · Swrngn SA227ACSDR MALA954462Former · crackedDURING PHASE INSPECTION IN MSP, FOUND SMALL CRACK IN RT INBOARD NACELLE FORMER P/N 27-35025-968. THE REPAIRS WERE COMPLETED BY REPLACING THE FORMER, P/N 27-35025-968 AND SKIN PANEL, P/N 27-35001-180, IAW FAC SRM 51-00-00 PAGE 4, 51-40-00, 51-30-00 AND 54-90-1May 17, 1995 · N442MA · Swrngn SA227ACSDR DL757952201Doubler · crackedNR 2 ENG PYLON CRACKED IN LWR AFT RADIUS OF FWD LIGHTNING HOLE INBD SIDE OF PYLON. REPAIRED PER SRM 54-51-01 PG 206 TO 211.May 14, 1995 · N615DL · Boeing 757232SDR 95ZZZM107Keel · crackedDURING LT ENG & TRUSS REPLACEMENT, LT NACELLE INBD & OTBD UPPER KEEL WEBS FND CRACKED. TWO CRACKS FND ON OTBD KEEL, P/N 114-98002201. ONE CRACK, APPROX 1.25 INCH LONG, LOCATED BETWEEN UPPER 2 RIVETS ON FWD SIDE OF KEEL WEB JUST BELOW UPPER OTBD TRUSS ATTACH May 13, 1995 · N812BE · Beech 1900CSDR 95ZZZM106Keel · crackedDURING LEFT ENGINE AND TRUSS REPLACEMENT THE LEFT NACELLE INBOARD AND OUTBOARD UPPER KEEL WEBS WERE FOUND TO BE CRACKED. TWO CRACKS WERE FOUND ON THE OUTBOARD KEEL, P/N 114-98002201. ONE CRACK, APPROXIMATELY 1.25 INCH LONG, WAS LOCATED BETWEEN THE UPPER 2 RIMay 13, 1995 · N812BE · Beech 1900CSDR DLL13952286Angle · crackedAT HMV, INSPECTION FOUND AN ANGLE CRACKED 6 FEET AFT OF NR 2 INLET, LT SIDE, 9 O'CLOCK POSITION, ON FWD SIDE OF BULKHEAD RING. REMOVED ANGLE, FABRICATED T-ANGLE AND FILLER PER SRM 54-12-00.May 11, 1995 · N784DA · Lkheed 10113851SDR DLL13952285Angle · crackedAT HMV, INSPECTION FOUND AN ANGLE CRACKED 6 FT AFT OF THE NR 2 INLET FS 1705, 3 0'CLOCK POSITION, INSIDE OVAL ACCESS OPENING. REMOVED CRACKED ANGLE, FABRICATED T-ANGLE AND FILLER PER SRM 54-12-00 PG 805.May 11, 1995 · N784DA · Lkheed 10113851SDR ABXA9500812Angle · crackedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE OUTBOARD LEFT PYLON WEB UPPER ATTACH ANGLE CRACKED. REPLACED UPPER WEB ATTACH ANGLE IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.May 11, 1995 · N979AX · Doug DC941SDR UPS803198Fitting · crackedWHILE IN C-CHECK, MAINTENANCE FOUND CRACK ON NR 2 PYLON FOOT STOOL FITTING AT LWR I/B CORNER. REPLACED FITTING PER UPS EO FILE NR DC8-57-0551.May 10, 1995 · N874UP · Doug DC873F
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