JASC 5340

Service difficulty reports · 22,411

Reports filed under 5340 · Fuselage Main, Attach Fittings, 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 = '5340'
  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 DHL200080319CAttach Fitting · wornAT C-CHECK, FUSELAGE SURFACE SKIN RT SIDE FILLET WORN OUT OF LIMITS FS 480.000 XWC 0.000 NEAR L-23 RT. REMOVED WORN FILLET IAW SRM 51-1-21 PG 1, FABRICATED FILLET IAW SRM 53-2-0, TREATED AND PRIMED IAW SRM 51-1-8, INSTALLED FILLET IAW 53-2-0 PG 10 TO 12.Jan 20, 2000 · N803DH · Doug DC873FSDR ASAA0080020Attach Fitting · corrodedPHX - DURING 30K CHECK, FOUND CORROSION ON FUSELAGE FRAME ATTACH FITTING AT FS 1250, LONGERON 18L. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 51-30-00. (M)Jan 18, 2000 · N951AS · Doug DC982SDR RRXA000025Intercostal · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FWD LWR CARGO BILGE AT STA 500 TO STA 520, LONGERON 31 RIGHT, INTERCOSTAL. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-21Jan 17, 2000 · N792FT · Doug DC873FSDR RRXA000157Intercostal · damagedDURING A MAINTENANCE VISIT FOUND DAMAGE, FUSELAGE, CABIN AT STA 620, LONGERON 11 RIGHT, INTERCOSTAL TIE HAS A SAW CUT IN IT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8.Jan 13, 2000 · N994CF · Doug DC862SDR RRXA002970Attach Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE ATTACH ANGLE AT STA 1240, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 51-1-0. (CORROSION DAMAGE RECORDED INJan 11, 2000 · N792FT · Doug DC873FSDR RRXA002969Attach Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE ATTACH ANGLE AT STA 1220, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-0. (CORROSION DAMAGE RECORDED INJan 11, 2000 · N792FT · Doug DC873FSDR RRXA003358Support · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE GILINER SUPPORT AROUND NUT PLATE AT STA 75 X=18 TO 48L AND -24, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PART IAW DOUGLAS DWJan 9, 2000 · N831AL · Doug DC873FSDR UPS00231337Fitting · crackedINSPECTION TYPE:C, BS 740 FITTING RT, CRACK ON LWR FLANGE OF FITTING. FITTING REPLACED IAW EO B727-5310-7477-E AND SMRO EO 2000-001-02 UPS ENGINEERING FILE NR 727-53-2215.Jan 4, 2000 · N945UP · Boeing 72722CSDR RRXA000317Attach Fitting · crackedDURING A MAINTENANCE VISIT FOUND FITTING CRACKED AT STA 1200 AND LONGERON 21 RIGHT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-20D.Nov 25, 1999 · N605AL · Doug DC873FSDR RRXA000282Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON 27 RIGHT SPLICE FITTING AT STA 450, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED NEW FITTING AND INSTALLED IAW DC-8 SRM 51-1-4.Nov 16, 1999 · N605AL · Doug DC873FSDR RRXA000279Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FITTING AT STA 70 AND LONGERON 31 LEFT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW FITTING AND INSTALLED IAW DC-8 SRM 53-4-1.Nov 12, 1999 · N605AL · Doug DC873FSDR RRXA000310Attach Fitting · crackedDURING A MAINTENANCE VISIT FOUND UPPER CARGO DOOR JAMB FRAME ATTACHMENT FITTING CRACKED AT STA 120 AND LONGERON 21 RIGHT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED NEW FRAME ATTACHMENT FITTING IAW Nov 2, 1999 · N605AL · Doug DC873FSDR RRXA000316Attach Fitting · crackedDURING A MAINTENANCE VISIT FOUND CUSP ATTACHMENT FITTING CRACKED AT STA 1160 AND LONGERON 21 LEFT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED NEW CUSP ATTACHMENT FITTING IAW DC-8 SRM 51-1-20D.Oct 28, 1999 · N605AL · Doug DC873FSDR RRXA000266Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FITTING BETWEEN STA 80 TO STA 100 AND LONGERON 13 RIGHT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW FITTING AND INSTALLED IAW DC-8 SRM 51-1-2Oct 25, 1999 · N605AL · Doug DC873FSDR CALA9901344Pan · corrodedFORWARD CARGO DOOR LOWER JAMB SUPPORT HAS CORROSION FS 370 - 427 STR 28 O/B SIDE. CUT OUT DAMAGED AREA FABRICATED SPLICES INSTALLED PAN, SPLICES AND SCUFF PLATED PER SRM 53-0151-10-2, 53-05 AND 51-30-5.Oct 8, 1999 · N16802 · Doug DC982SDR RRXA000275Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO ATTACHMENT ANGLE AT STA 680 AND BETWEEN LONGERONS 22 RIGHT TO 23 RIGHT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ATTACHMENT Oct 5, 1999 · N605AL · Doug DC873FSDR RRXA000284Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FITTING AT STA 400 BETWEEN LONGERON 22 LEFT TO 23 LEFT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RETURN TO SERVICE, LIMITS ACCEPTABLE IAW FAA DER APPROVESep 30, 1999 · N605AL · Doug DC873FSDR RRXA000270Bracket · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO 2 EACH BRACKETS AT STA -131 AND LONGERON 23 LEFT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-0.Sep 27, 1999 · N605AL · Doug DC873FSDR RRXA000268Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FITTING AT STA 879 AND LONGERON 24 RIGHT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW FITTING AND INSTALLED IAW DC-8 SRM 51-1-20D.Sep 24, 1999 · N605AL · Doug DC873FSDR HEEA063169Fitting · corrodedCORROSION ON BOTTOM SIDE OF FITTING.Aug 3, 1999 · Bell 212SDR 99ZZZX2152Fitting · crackedTHERE ARE 2 OF THESE FITTINGS USED TO SECURE VERTICAL FIN TO FUSELAGE. THE RIGHT FITTING WAS CRACKED AT THE BASE IN THE RADIUS. THIS CRACK WAS FOUND DURING A 100-HOUR INSPECTION. BOTH FITINGS WERE CHANGED AS PRECAUTION. CAUSE UNKNOWN.May 10, 1999 · N49848 · Cessna 152SDR DLM88990727Scuff Plate · crackedIN CLIMB PASSING THRU FL 360, A LOUD NOISE AND VIBRATION STARTED. F/C GALLEY AREA WAS MOST EXCESSIVE. VIBRATION STOPPED IN DESCENT THRU FL 185. FOUND R1 DOOR SCUFF PLATE BENT AND CRACKED. REPLACED SAME.Apr 2, 1999 · N932DL · Doug MD88SDR UPS99829018Fitting · crackedINSPECTION TYPE:C2 BATHTUB FITTING AT FS 920 LEFT LONGERON 24 IS CRACKED AND CORRODED. DRILLED AND DEBURRED NEW FITTING IAW DC8 SRM 51-1-20D. FINAL INSTALLATION ON UPS N/R 875504.Feb 23, 1999 · N810UP · Doug DC873FSDR UPS99228622Fitting · corrodedINSPECTION TYPE:C SEAT TRACK ATTACH FITTING CORRODED AT BS 740 RBL 45. FITTING AT BS 740 RBL 45 REPLACED PER DWR NR 65C13724.Jan 29, 1999 · N917UP · Boeing 72730CSDR ABXA9800776Fitting · corrodedEXFOLIATED FITTING INSIDE LOWER AFT TORQUE BOX WEB AT RIGHT AFT SERVICE DOOR. REPAIRED IAW DC8 SRM 51-1-20D AND DWG 4773146.Aug 5, 1998 · N803AX · Doug DC862SDR CA980303001Fitting · sheared(CAN) STBD MAIN SPAR-TO-FUSE FITTING 2 MOST INNER JO-BOLTS FASTENERS SHEARED 5/16INCH BELOW HEAD. REPLACED.Feb 24, 1998 · Piper PA60600SDR 97ZZZX4251Channel · crackedDURING ROUTINE INSPECTION, TWO CHANNELS THAT SUPPORT THE NOSE LANDING GEAR ACTUATOR WERE FOUND CRACKED. AFTER REMOVING CHANNELS FOR REPLACEMENT, FORWARD SUPPORT ZEE P/N 5813045-1 WAS DISCOVERED CRACKED AND DAMAGED. AIRCRAFT HAD NO HISTORY OF PROBLEMS ASSOCIASep 16, 1997 · N2610Z · Cessna 402CSDR ABXA9700743Fitting · corrodedDURING C-CHECK, FOUND ATTACH FITTING OUTBOARD OF THE TRAPEDZOIDAL PANEL MOST FORWARD HOLE COMMON TO TRAP PANEL CORRODED INSIDE. REPLACED FITTING IAW DC9 SRM 51-30-5 AND 51-30-1.Apr 11, 1997 · N925AX · Doug DC915SDR 97ZZZX2800Attach Angle · excess wornLOWER RT TAILCONE TO STEEL TUBE FUSELAGE ATTACH BOLTS WORN SEVERELY IN ALUM ATTACH ANGLES. INSTALLED AN5 BOLTS GROOVED. WASHER NEXT TO NUT CHAFED AROUND COUNTERBORE APPROXIMATELY .060 INCH INTO A .090 INCH THICK ALUM ANGLE. .3125 INCH BOLT HOLES ELONGATED AApr 2, 1997 · N417AS · Namer AT6CSDR 9624396622Fitting · corrodedDURING P-CHECK, FOUND CORROSION ON THE U-CHANNEL SUPPORT FITTING IN THE LEFT BODY MAIN LANDING GEAR WHEEL WELL FS 1476 ON THE KEEL BEAM TOP PLATE 8 OUTBOARD OF THE INBOARD WALL. REPLACED FITTING PER SRM 51-10-01.Nov 13, 1996 · N622US · Boeing 747251BSDR ARWA9610021Fitting · crackedDURING C-CHECK, FOUND CRACKED FITTING AT MAIN CARGO COMPARTMENT STA 1690 L26L. REMOVED AND REPLACED CRACKED FITTING AT MAIN CARGO IAW DC-8 SRM 51-1-20D.Oct 25, 1996 · N661AV · Doug DC863FSDR P5CA9600361Stop Fitting · crackedAFT CARGO DOOR FRAME STRUCK BY PALLET AND DAMAGED DURING LOADING. FOUND WEB DAMAGE AT BS 1820 AT LOWER STOP FITTING, FITTING CRACKED. REPAIRED WEB AND FITTING IAW SRM 53-10-04.Jun 22, 1996 · N853FT · Boeing 747122SDR AU961173Fitting · corroded(AUS) STABILATOR ATTACHMENT FITTINGS, FUSELAGE STRINGERS AND SKIN CORRODED - FOUND DURING INSPECTION IAW AD/PA32/75May 30, 1996 · Piper PA32300SDR AU960783Block · corroded(AUS) CENTRE WING SPAR BEARING BLOCK CONTAINS SEVERE INTERGRANNULAR EXFOLIATION CORROSIONMay 13, 1996 · Cessna 172DSDR 96ZZZM1001Trapezoidal Ftg · corrosionDURING CHECK, LEFT MLG FIXED SIDE BRACE ATTACH FITTING INBOARD ATTCH BOLT HOLE SHOW EVIDENCE OF CORROSION IN TRAP FITTING. REPAIRED BOLT HOLE ON LEFT MLG FIXED SIDE BRACE ATTACH FITTING IAW SRM 57-20-00 FIG 20. (M)Apr 16, 1996 · N229NW · Doug DC1030SDR 96ZZZM1000Trapezoidal Ftg · corrosionDURING CHECK, RIGHT MLG FIXED SIDE BRACE ATTACH FITTING INBOARD ATTACH BOLT HOLE SHOWS EVIDENCE OF CORROSION IN TRAP FITTING. REMOVED CORROSION AND REPAIRED INBOARD ATTACH HOLES IAW SRM 57-20-00 FIG 20.Apr 16, 1996 · N229NW · Doug DC1030SDR AU960501Fitting · damaged(AUS) LH FRONT WING ATTACHMENT FITTING AT FUSELAGE DAMAGED - FUSELAGE PANELS LH AND RH SIDE ABOVE MAIN SPARS DISTORTEDMar 10, 1996 · Socata TB10TOBAGOSDR 96016122811Trunnion Ftg · wornLEFT MLG TRUNNION FITTING ATTACHING BORES (AFT TOP AND BOTTOM) (RETRACT ACTUATOR A-FRAME) ARE RE-WORKED BEYOND MAXIMUM LIMITS PER NWA SA5743-01026-5, NOTE 2. OVERSIZED BORES TO 1.0075 INCHES PER STEP 1 NWA SA5743-01026-5. FABRICATED AND INSTALLED BUSHINGS. Mar 5, 1996 · N228NW · Doug DC1030SDR CA960319101Chord Angle · cracked(CAN)CHORD ANGLE AT STA 178 CRACKED IN TWO PLACES WL 196 AND STRINGER 17. REPAIRED.Mar 3, 1996 · Boeing 737275SDR AU960683Bracket · cracked(AUS) LH WING ROOT BRACKETS PNO 5170036-5-165 AND PNO 5170036-7-165 CRACKED - FOUND DURING INSPECTION IAW AD/AC/93Feb 9, 1996 · Gulstm 500SSDR AU960682Bracket · cracked(AUS) LH WING ROOT BRACKETS PNO 5170036-5-165 AND PNO 5170036-7-165 CRACKED - FOUND DURING INSPECTION IAW AD/AC/93Feb 8, 1996 · Gulstm 500SSDR AU960561Rivet · sheared(AUS) HORIZONTAL STABILISER RH ATTACHMENT BRACKET RIVETS (8OFF) SHEAREDJan 31, 1996 · Mooney M20FSDR AU960115Hinge · cracked(AUS) TOP DOOR HINGE CRACKED IN AFT SECTION - DOOR HINGE PIN ALSO SHEAREDJan 31, 1996 · Cessna 152SDR DLL15954160Latch Fittings · corrodedDURING ACCOMPLISHMENT OF S.I. 7-58181-12AD, THE NR 7 C-1A CARGO DOOR LATCH FITTING HAD SURFACE CORROSION IN THE UPPER WELL. DRAIN HOLES HAVE BEEN ADDED IN THE CENTER OF THE LOWER WEB FOR FITTINGS NR 1, NR 2, NR 5, NR 6, NR 7, NR 8. THE SURFACE CORROSION ON TOct 27, 1995 · N753DA · Lkheed 10113853SDR CAL950844Jamb Door · dentedHOU - INSPECTION FOUND A DENT IN THE FORWARD SERVICE DOOR AFT JAMB. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-05, FIGURE 42. (M)Sep 20, 1995 · N15525 · Doug DC932SDR 95FDEA01364Fitting · crackedRT I/B FLAP I/B ACTUATOR ATTACHMENT TO FUSELAGE BOLTS NOT SECURED. CHECKED BARREL NUTS FOR WEAR, FOUND ACT LOWER ATTACH FITTING CRACKED AT LOWER BOLT HOLES.Sep 17, 1995 · N301FE · Doug DC1030FSDR ABXA9500874Fitting · corrodedDURING C-CHECK INSPECTION, FOUND FITTING ON LEFT FUSELAGE SKIN THAT TIES INTO THE MAIN FRAME AND INTO LEFT TRAPEZOID PANEL HAD CORROSION IN THE BOLT HOLE. REPAIRED IAW ABX REA D953-12649-MR.Aug 30, 1995 · N905AX · Doug DC932SDR UPS803765Bathtub Fitting · corrodedWHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON BATHTUB FITTING F.S. 280, LONGERON 33A RT. REPLACED IAW SRM 51-1-20D.Jul 6, 1995 · N772UP · Doug DC871FSDR P5CA9500463Web · corrodedCORROSION ON THE WEB BETWEEN BS 1300 AND 1310 LBL 33. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02.Jun 30, 1995 · N831FT · Boeing 747121SDR P5CA9500351Angle · crackedCRACK IN SUPPORT ANGLE FOR FLOOR PANEL BS 2040 BL 0. REPAIRED PER BOEING SRM 51-40-03.Jun 30, 1995 · N831FT · Boeing 747121
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