JASC 5342

Service difficulty reports · 578

Reports filed under 5342 · Fuselage, Stabilizer Attach Fittings, newest first.

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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 = '5342'
  ORDER BY difficulty_date DESC"

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SDR CALA0101001Fitting · corrodedINSPECTION FOUND VERTICAL STABILIZER ATTACH FITTING IN FUSELAGE CORRODED AT R/H AFT O/B FORWARD LUG AND AT L/H AFT O/B FORWARD LUG. THE CORROSION WAS REMOVED AND AN OVERSIZE BUSHING WAS INSTALLED AT EACH LOCATION IAW ECRA 5340-01356.Nov 13, 2001 · N59338 · Boeing 7373T0SDR SWAA012987Angle · crackedDURING SCHEDULED 1/4D CHECK, FOUND VERTICAL STAB AFT RH ATTACH FITTING FWD DRAG ANGLE CRACKED. REPAIRED DRAG ANGLE PER SRM.Oct 26, 2001 · N302SW · Boeing 7373H4SDR ZW0A0109702Attach Angle · crackedDURING CHECK-C MAINT FOUND CRACK BETWEEN 2 FASTENERS AT ATTACH ANGLE FROM FUSELAGE TO VERTICAL STABILIZER, 7 INCHES FROM AFT END OF THE STABILIZER AT RT SIDE. STOP DRILLED SMALL CRACK PER SRM 53-05, FIG 23. ACCOMP HIGH FREQ EDDY CURRENT PER NDT 51-00-03. CHOct 11, 2001 · N9620D · Doug DC983SDR ZW0A0109102Attach Angle · crackedDURING CHECK-C MAINT ON THE AFT FUSELAGE EXTERIOR, LT SIDE 3 INCHES FWD OF VERTICAL FIN REAR SPAR, A CRACK WAS FOUND BETWEEN FASTENERS IN THE ATTACH ANGLE. CONFIRMED BY EDDY CURRENT. ACCOMP HIGH FREQ EDDY CURRENT AND FOUND CRACK CONTAINMENT PER NDT MANUAL 51Sep 21, 2001 · N9617R · Doug DC983SDR SWIA200110248Angle · crackedCRACK AND PULLED RIVET IN VERTICAL STABILIZER TO EMPENNAGE SUPPORT ANGLE LEFT SIDE. REPLACED LEFT L-FORWARD PROFILE PER PART II OF SB 120-053-0074 AND EMBRAER AUTHORIZATION GST-3216/01. P/N: SB120-53-0074 KIT 1.Sep 6, 2001 · N137H · Emb EMB120RTSDR CA010912017Stiffener · cracked(CAN) COMMON PROBLEM ON OLDER CESSNA 150 SERIES, MANUFACTURER HAS BEEN REPLACED THIS PART WITH A NEW IMPROVE PART P/N 0432169-1 ALSO INCLUDING NEW IMPROVE BULKHEAD ASSY P/N 0412177-2.Sep 4, 2001 · Cessna 150JSDR CALA0100747Attach Angle · crackedINSPECTION FOUND A 3/4" CRACK COMING FROM RIVET HOLE IN R/H SIDE VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE AT STA 1463. THE CRACKED AREA WAS CUT OUT AND A REPAIR ANGLE WAS INSTALLED IAW SRM 53-05, FIGURE 23.Aug 8, 2001 · N72821 · Doug DC982SDR DL73K011194Fitting · corrodedCORROSION WAS FOUND ON THE LUG BORES AND FACES OF THE RH ANDLH HORIZONTAL STABILIZER CLEVIS ATTACH FITTINGS. THE CORROSION WAS REMOVED AND OVERSIZED BUSHINGS INSTALLED.Jul 19, 2001 · N317DL · Boeing 737232SDR DL73K011180Attach Fitting · corrodedTHE FUSELAGE CLEVIS LUGS AND THE VERTICAL FIN ATTACHMENT LUGS WERE FOUND CORRODED IN THE BORES AND THE FACES. THE CORROSION WAS REMOVED AND OVERSIZED BUSHINGS INSTALLED. THE DAMAGE WAS FOUND DURING HMV.Jul 17, 2001 · N317DL · Boeing 737232SDR DL73K010951Attach Fitting · corrodedCORROSION WAS FOUND ON THE RT FUSELAGE CLEVIS LUGS FOR THE HORIZONTAL STABILIZER. CORROSION WAS REMOVED FROM SOME OF THE FACES, BORES AND OVERSIZED BUSHINGS WERE INSTALLED. THE DAMAGE WAS FOUND AT HMV.Jun 12, 2001 · N320DL · Boeing 737232SDR CALA0100495Attach Angle · crackedINSPECTION FOUND A 1.5 INCH CRACK IN RT VERTICAL STABILIZER LOWER ATTACH ANGLE, 6 INCHES FROM TRAILING EDGE. REPAIRED IAW SRM 53-05.May 23, 2001 · N72825 · Doug DC982SDR CALA0100494Attach Angle · crackedINSPECTION FOUND A 2 INCH CRACK IN LT VERTICAL STABILIZER LOWER ATTACH ANGLE, 7 INCHES FROM TRAILING EDGE. REPAIRED IAW SRM 53-05.May 23, 2001 · N72825 · Doug DC982SDR CALA0100444Attach Angle · crackedINSPECTION FOUND A .5 INCH CRACK AT RIVET IN LOWER FLANGE OF RT VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE AT STA 1463 JUST FORWARD OF VERTICAL STABILIZER REAR SPAR PLANE. A REPAIR DOUBLER AND SPLICE WERE INSTALLED IAW SRM 53-05, FIGURE 23 AND 23A.May 5, 2001 · N16894 · Doug DC982SDR 2001UALA00615Skin · dentedRT HORIZONTAL STAB DENTED 6 FT FROM INBD AND 6 INCHES FWD REAR SPAR. ACCOMPLISHED FLUSH REPAIR.May 1, 2001 · N313UA · Boeing 737322SDR ZW0A0100706Attach Angle · crackedDURING CHECK-C MAINT FOUND VERTICAL STABILIZER RT SIDE OF DORSAL FIN, AFT END OF VERTICAL STAB TO FUSELAGE ATTACH ANGLE, AFT OF PREVIOUS REPAIR HAD ANGLE WITH A 2 INCH CRACK. TRIMMED OFF BROKEN PART. MADE FILLER AND DOUBLER PER SRM 53-05, FIG 23A, AND INSTALApr 19, 2001 · N904TW · Doug DC982SDR AT0100159Attach Angle · crackedFOUND DORSAL FIN ATTACH ANGLES CRACKED BEYOND LIMITS. REPLACED ATTACH ANGLES IAW EO 09-5350-29-E1645.Apr 15, 2001 · N803AT · Doug DC932SDR DL73K010535Strap · crackedCRACKS WERE FOUND AT THE CUTOUT IN THE FUSELAGE FOR THE HORIZONTAL STABILIZER SIMILIAR TO THE TYPICAL CRACKS OF S/B 737-53-1134. CRACKS WERE FOUND IN THE LT & RT STINGER 12 STRAP, FS 1140, AND THE LT & RT FS 1138 FRAME STRAPS. THE DAMAGE WAS REPAIRED PER SRApr 2, 2001 · N316DL · Boeing 737232SDR DL73K010533Fitting · corrodedCORROSION WAS FOUND IN THE BORE AND FACES OF THE LT AND RT FUSELAGE CLEVIS LUGS FOR THE HORIZONTAL STABILIZER. THE CORROSION WAS REMOVED AND NEW BUSHINGS WERE INSTALLED PER ERA 397371-14AD AT HMV.Apr 2, 2001 · N316DL · Boeing 737232SDR CALA0100250Angle · crackedINSPECTION FOUND A CRACK IN AFT FUSELAGE TO VERTICAL STABILIZER ANGLE AT AFT END LT SIDE. THE CRACKED AREA WAS REMOVED IAW SRM 53-05, FIGURE 23. DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-05, FIGURE 23, 51-10-3, 51-20-0, AND 51-30-5.Mar 24, 2001 · N72822 · Doug DC982SDR CALA0100249Angle · crackedINSPECTION FOUND A CRACK IN AFT FUSELAGE TO VERTICAL STABILIZER ANGLE AT AFT END RT SIDE. THE CRACKED AREA WAS REMOVED IAW SRM 53-05, FIGURE 23. DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-10-3, 53-05, FIGURE 23, AND 51-20-0.Mar 24, 2001 · N72822 · Doug DC982SDR DL73K010346Fitting · corrodedCORROSION WAS FOUND ON THE VERTICAL STABILIZER ATTACH LUGS AND FUSELAGE CLEVIS LUGS. CORROSION WAS FOUND ON VARIOUS LUG BORES AND FACES. THE CORROSION WAS REMOVED AND THE BUSHINGS AND SLEEVES REMANUFACTURED PER ERA 397239-14 AT HMV.Mar 1, 2001 · N315DL · Boeing 737232SDR DL73K010343Fitting · corrodedCORROSION WAS FOUND ON THE LT AND RT FUSELAGE CLEVIS ATTACH LUGS FOR THE HORIZONTAL STABILIZER. THE CORROSION WAS FOUND ON SEVERAL LUG BORES AND FACES. THE CORROSION WAS REMOVED AND NEW BUSHINGS WERE INSTALLED. THE DAMAGE WAS FOUND AT HMV.Mar 1, 2001 · N315DL · Boeing 737232SDR AWXA0001393Bolt · corrodedRIGHT O/B AFT VERT STAB ATTACH BOLT CORRODED AND REQUIRED REPLACEMENT STA 1088 WL 301.11. BOLT REPLACED ON C-12 CHECK IAW AWA W/C 1GB55002.Feb 20, 2001 · N302AW · Boeing 7373G7SDR CALA0100103Angle · gougedINSPECTION FOUND RT SIDE VERTICAL STABILIZER TO FUSELAGE ANGLE GOUGED AT STA 1088 - 1156. THE LT ANGLE AT STA 1121 - 1138 WAS ALSO GOUGED. THE GOUGED SECTIONS WERE REMOVED AND REPLACED IAW ECRA 5380-01013.Feb 4, 2001 · N14383 · Boeing 7373Q8SDR DL73K010110Fitting · corrodedCORROSION WAS FOUND ON THE LT AND RT FUSELAGE CLEVIS LUGS THAT ATTACH THE HORIZONTAL STABILIZER. CORROSION WAS REMOVED FROM THE LUG BORES AND FACES PER ERA 396637-14 AT HMV.Jan 22, 2001 · N313DL · Boeing 737232SDR 0103419616Attach Angle · corrodedDURING H-CHECK FOUND CORROSION ON THE HORIZONTAL FLANGE OF THE VERTICAL STABILIZER-FUSELAGE ATTACH ANGLE. REPAIRED PER EA 99-177558.Jan 5, 2001 · N616NW · Doug DC932SDR ERKR200000006Spar · corrodedHORIZONTAL STABILIZER CENTER SECTION REAR SPAR FITTING RIGHT HAND SIDE INNER BORE HAS CORROSION. REPAIRED PER ECRA N703S-55-B737-005-EAC. (X)Dec 29, 2000 · N703S · Boeing 7372T4SDR DL73K002488Fitting · corrodedTHE RT FUSELAGE CLEVIS LUGS ATTACHING THE HORIZONTAL STABILIZER WERE FOUND CORRODED ON THE FACES AND BORES. THE CORROSION WAS REMOVED AND NEW BUSHINGS WERE INSTALLED PER ERA 396532-14AD AT HMV.Dec 21, 2000 · N314DA · Boeing 737232SDR AU001197Bracket · corroded(AUS) STABILISER ATTACHMENT BRACKET CONTAINED EXFOLIATION CORROSION INTHE OUTBOARD VERTICAL FACE.Dec 15, 2000 · Socata TB10TOBAGOSDR AALA20004088Mount · out of toleranceAFW - FOUND BORE IN MLG BEAM HOLE AT AFT TRUNNION BEARING MOUNT, INBOARD AFT HOLE IS OUT OF DESIGN LIMITS. HOLE MEASURES 1.064 SHOULD BE 1.0625-1.0632. VERIFY HOLE IS CRACK FREE. FABRICATED 0S BUSHING TO HAVE INTERFERENCE FIT OF .0006-.0013. REFER TO BOEINNov 30, 2000 · N687AA · Boeing 757223SDR AWXA0000985Spar · gougedLT HORIZ STAB AFT SPAR TO CENTER SEC ATTACH FITTING HAS GOUGE FROM SCREW ON CENTER UPPER LUG. BLENDED GOUGE MAT LOSS .035 MAX ALLOWED .050; FLAT PEENED IAW SRM 55-10-10 AND 51-20-06.Nov 27, 2000 · N330AW · Boeing 7373Y0SDR DL73K002259Fitting · corrodedCORROSION WAS FOUND ON THE HORIZONTAL STABILIZER CLEVIS LUGS IN THE BORES AND FACES. THE DAMAGE WAS REMOVED AND REPAIRED PER ERA 396374-14 AT HMV.Nov 20, 2000 · N310DA · Boeing 737232SDR COMA0060827Frame · crackedFRAME FLANGE AT FS 718.0 RHS CRACKED. PERFORMED A MAJOR REPAIR TO CRACKED FRAME FLANGE AT FS 718.0 RHS IAW CRJ REO 601R-53-61-193 REV A.Oct 14, 2000 · N969CA · Cndair CL6002B19SDR DL73K001686Fitting · corrodedTHE RT AND LT FUSELAGE CLEVIS LUGS THAT ATTACH THE HORIZ STABILIZER WERE FOUND CORRODED. SEVERAL BORES WERE OVERSIZED AND SOME OF THE FACES WERE BLENDED. THE REPAIR WAS ACCOMPLISHED AT HMV PER ERA 334873-14.Sep 1, 2000 · N309DL · Boeing 737232SDR TWAA0013317Attach Angle · crackedDURING CHECK-C MAINT, THE DORSAL FIN ATTACH ANGLE WAS CRACKED ON LT SIDE OF ACFT, O/B OF VERT STAB REAR SPAR. ACCOMP NDT HIGH FREQ EDDY CURRENT PER 51-00-03 PART 6. CRACKS FOUND WERE STOP DRILLED. ONE INCH CRACK REPAIRED PER SRM 53-05 FIG B.Aug 22, 2000 · N901TW · Doug DC982SDR DL73K001575Attach Fitting · corrodedTHE HORIZONTAL STABILIZER RT AND LT CLEVIS LUGS WERE FOUND CORRODED. THE LUG DIAMETER WAS ENLARGED AND NEW BUSHINGS WERE INSTALLED PER ERA 334719-14 AT HMV.Aug 14, 2000 · N308DL · Boeing 737232SDR AU000540Bracket · cracked(AUS) FIN ATTACHMENT BRACKET CRACKED. (X)Jul 11, 2000 · Cessna 152SDR LR7A00156Attach Angle · crackedDURING SCHEDULED B1 CHECK PER JOB CARD HB0502, FOUND RT FS 902 DORSAL FIN ATTACH ANGLE CRACKED IN RADIUS AT RBL 13, WL 285. REPAIRED PER LAC MEA 382-53-00-089. NR 44276.Jun 23, 2000 · N404LC · Lkheed 382GSDR LR7A00153Attach Angle · crackedDURING SCHEDULED B1 CHECK PER JOB CARD HB0502, FOUND LT FS 840 DORSAL FIN ATTACH ANGLE CRACKED APPROX 1 INCH IN RADIUS, RBL 15, WL 280. REPAIRED PER LAC MEA 382-53-00-088. NR 39925.Jun 23, 2000 · N404LC · Lkheed 382GSDR LR7A00151Attach Angle · crackedDURING SCHEDULED B1 CHECK PER JOB CARD HB0502, FOUND RT FS 840 DORSAL FIN ATTACH ANGLE CRACKED APPROX 2 INCHES IN RADIUS, RBL 15, WL 280. REPAIRED PER LAC MEA 382-53-00-087. NR 39912.Jun 23, 2000 · N404LC · Lkheed 382GSDR COMA0060517Fitting · misdrilledHORIZONTAL STABILIZER SPLIT VISOR FITTING PRE-DRILLED HYD LINES AND PILOT HOLES DO NOT ALIGN. PERFORMED HORIZ STABILIZER RIB REPAIR ON SPLIT VISOR FITTING IAW WEST VIRGINIA AIR CENTER EO 601R-55-1426.Jun 16, 2000 · N941CA · Cndair CL6002B19SDR LR7A0090Attach Angle · crackedDURING SCHEDULED C2 INSPECTION PER HSP57110, FOUND LT FS 844 DORSAL FIN ATTACH ANGLE CRACKED IN RADIUS AT LBL 13, WL 285. REPAIRED PER LAC MEA 382-53-00-066.Jun 3, 2000 · N402LC · Lkheed 382GSDR QXEA0001625Fitting · corrodedYYC- STAB JUNCTION DRIVE FITTING AND STAB JUNCTION FITTING HAS FRETTING/PITTING CORROSION. REPAIRED IAW FOKKER SRM 55-01-01, 51-10-04 AND HORIZON AIR EA 4-55-222.May 31, 2000 · N480AU · Fokker F28MK4000SDR CALA0000784Attach Angle · crackedINSPECTION FOUND A 2 INCH CRACK IN LT DORSAL FIN INNER ATTACH ANGLE. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-02, 51-10-04, 51-10-03, AND 51-30-04.May 31, 2000 · N819NY · Doug DC982SDR CALA0000656Attach Angle · crackedINSPECTION FOUND DORSAL FIN LT INNER ATTACH ANGLE CRACKED. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-4 AND 51-30-2.May 10, 2000 · N72830 · Doug DC982SDR CALA0000643Angle · crackedINSPECTION FOUND A .5 INCH CRACK IN LT SIDE DORSAL FIN TO FUSELAGE ANGLE. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-4 AND 51-10-4.May 8, 2000 · N71828 · Doug DC982SDR GAIA00131Frame · corrodedDURING HEAVY C-CHECK AT TIMCO/OSC, FOUND E/E FORWARD JAMB LOWE CHORD HAS PULLED FASTENER AT STATION 422, LBL 8. REPAIRED IAW SRM 51-20-1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Mar 30, 2000 · N6808 · Boeing 727223SDR 99ZZZX1782Seat Track · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON SEAT TRACK STA 1050 - STA 1070 BL 45.5 R.Apr 12, 1999 · N79754 · Boeing 727227SDR CA990323031Fitting · corroded(CAN) THE DEFECT WAS DETECTED DURING AN ANNUAL INSPECTION. CORROSION WAS EXTENSIVE ENOUGH TO REQUIRE REPLACEMENT OF THE FIN ATTACH FITTING. ALL AIRCRAFT IN FLEET TO BE SUBJECTED TO SPECIAL INSPECTION IN THE AFFECTED AREA.Mar 1, 1999 · Grumav TBM3EAIRTRDSDR DLM90982594Angle · crackedFUSELAGE ATTACH FITTING, VERTICAL STAB TO FUSE ANGLE, REPAIR FOR CRACK. THE VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE WAS FOUND WITH A .75 CRACK BETWEEN FASTENERS AT FS 940 ON THE LT SIDE OF THE FUSELAGE. THE CRACKED AREA WAS ROUTED OUT OF THE ANGLE ADec 17, 1998 · N914DN · Doug MD9030
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