JASC 5510

Service difficulty reports · 5,966

Reports filed under 5510 · Horizontal Stabilizer Structure, 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 = '5510'
  ORDER BY difficulty_date DESC"

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SDR P2EA97045Brace · corrodedPAE - FOUND C-CHECK MAINTENANCE VISIT, HORIZONTAL STABILIZER HINGE HOUSING RIGHT UPPER THRUST BRACE IS CORRODED. REMOVED, REPLACED HORIZONTAL STABILIZER HINGE HOUSING RIGHT UPPER THRUST BRACE IAW MM 55-10-10. INSTALLED BUSHINGS IAW OHM 55-10-5. THIS HAS BEEMay 14, 1997 · N204AU · Boeing 737247SDR P2EA97044Brace · corrodedFOUND C-CHECK MAINTENANCE VISIT, HORIZONTAL STABILIZER HINGE HOUSING RIGHT LOWER THRUST BRACE IS CORRODED. REMOVED, REPLACED HORIZONTAL STABILIZER HINGE HOUSING RIGHT LOWER THRUST BRACE IAW MM 55-10-10. INSTALLED BUSHINGS IAW OHM 55-10-5. THIS HAS BEEN CLASMay 14, 1997 · N204AU · Boeing 737247SDR DL72S970909Hinge · wornHORIZON STAB ELEV INBOARD HINGE WORN, ALSO FRETTING CORROSION ON FITTING OUTBOARD SIDE. REMOVED CORROSION PER SRM 51-10-6 SPOT FACED INSIDE FACED TO REMOVE WEAR WITHIN M/M 55-50-0 LIMITS. ROTO PEENED AREA. TREATED AND PAINTED AREA. INSTALLED SPACERS PER M/May 13, 1997 · N8873Z · Boeing 727225SDR SCNA97268Fitting · corrodedDURING HEAVY MAINTENANCE VISIT THE LEFT PORTION OF THE HORIZONTAL STABILIZER WAS FOUND TO HAVE PITTING CORROSION IN TWO OF THE TENSION TIE ATTACH FITTING HOLES AND DEEP GOUGE IN ONE OF THE HOLES. REAMED HOLES TO REMOVE CORROSION AND GOUGE PER B727 SERVICE BULMay 12, 1997 · N285SC · Boeing 7272J4SDR CA970523012Vortex Gen · missing(CAN) VORTEX GEN MISSING ON TOP OF WING STN 174.5 AND BOTTOM OF RT STAB AT STN BL 9 8.25. SUBMITTER STATED POSSIBLY LOOSENED DURING WASHING AND FELL OFF DURING TAXI OR FLIGHT. VG ON STAB IS PARTLY ON CORNER OF TRIM PANEL. AIRCRAFT TT: 10,273 HOURS.May 12, 1997 · Piper PA31350SDR 97FDEA00322Beam · corrosionNR 0542 026, CORROSION (C55-391-20, 2) RT HORIZONTAL STAB UPPER TIE BEAM HAS AN AREA OF CORROSION 138 FROM INBOARD END LWR FWD SIDE. * S/D* REMOVED AND REPLACED RT HORIZONTAL STAB UPPER TRAILING EDGE BEAM IAW FED-EX SRM 51-30-5.May 10, 1997 · N153FE · Boeing 72725SDR MWEA97346Stringer · crackedDURING INSPECT, LT HORIZ STAB UP PLATE STRINGER 4 STA XHS 15 CRACKED. MAINT REPAIRED IAW DAC TELEX SVC-MSP-0079/DLP 24-JAN-97.Apr 28, 1997 · N205ME · Doug DC932SDR 97ZZZX2023Bearing · wornANNUAL INSP FOUND STAB BEARING WAS WORN. INSP IN AREA COVERED IN AD 97-13-10 NOTE 1 PARA (A2) AND SB 411A INST PARA (1-4).Apr 28, 1997 · N8200P · Piper PA24250SDR UPS97822898Doubler · crackedINSPECTION TYPE-D, RT INBD HORIZONTAL L/E INBD SECTION DOUBLER CRACKED. REMOVED FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1-21 AND 55-3-1.Apr 23, 1997 · N894UP · Doug DC873FSDR ABXA9700456Fitting · crackedDURING C-CHECK, FOUND THE FITTING AT THE AFT END OF THE HORIZONTAL STABILIZER CENTER SPAR BOX CRACKED AT THE UPPER FLANGE FOR PANEL NUMBER 3902. REPLACED FITTING IAW DACO DRAWING 5912981 AND DC9 S/B 55-32.Apr 2, 1997 · N979AX · Doug DC941SDR MWEA97241Doubler · crackedFOUND UPPER STRINGER NR 6 AND LOWER STRINGER NR 6 CRACKED, AT STA XHS-15 LEFT HORIZ STAB. MAINTENANCE REPAIRED THE UPPER AND LOWER STRINGER CRACKS IAW SRM 55-02 FIG 16.Apr 1, 1997 · N205ME · Doug DC932SDR MWEA97240Doubler · crackedFOUND BOTTOM STRINGER NR 2 CRACKED, AT STA XHS-50 IN THE LEFT HORIZ STAB. MAINTENANCE REPAIRED THE CRACK IAW SRM 55-02 FIG 16.Apr 1, 1997 · N205ME · Doug DC932SDR MWEA97239Doubler · crackedFOUND LEFT HORIZ STAB UPPER STRINGER NR 4 CRACKED, AT STA XHS-15. MAINTENANCE REPAIRED THE CRACK IAW RM 55-02 FIG 16 AND DOUGLAS TELEX SVC MSP 0079 DLP.Apr 1, 1997 · N205ME · Doug DC932SDR MWEA97238Doubler · crackedFOUND LEFT HORIZ STAB LOWER STRINGER NR 5 CRACKED, AT STA XHS-15. MAINTENANCE REPAIRED THE CRACK IAW SRM 55-02 FIG 16.Apr 1, 1997 · N205ME · Doug DC932SDR MWEA97237Stringer · crackedFOUND UPPER STRINGER NR 2 CRACKED AT STA XHS 204 IN THE LEFT HORIZ STAB. MAINTENANCE REPAIRED THE CRACK IAW SRM 55-02 FIG 16.Apr 1, 1997 · N205ME · Doug DC932SDR MWEA97236Stringer · crackedFOUND THE LEFT HORIZ STAB UPPER STRINGER NR 1, CRACKED AT STA XHS 204. MAINTENANCE REPAIRED THE CRACK IAW SRM 55-02 FIG 16.Apr 1, 1997 · N205 · Doug DC932SDR UPS97822532Angle · crackedINSPECTION TYPE-D, LT HORZ STAB L/E REPAIR ANGLE CRACKED AT STA FXS53.7. REMOVED, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 55-2-0 AND 51-1-20D.Mar 31, 1997 · N894UP · Doug DC873FSDR SWAA970314Fitting · crackedDURING SCHEDULED D-CHECK, FOUND A 2 INCH CRACK IN RADIUS OF SUPPORT FITTING MEMBER AT HORZ STAB CENTER SECTION UPPER SUPPORT, O/B SIDE OF BEAM, 25 AFT OF FWD SPAR, 20 I/B OF RT SIDE INTERNAL FUSE SKIN. REPAIRED PER BOEING SRM.Mar 18, 1997 · N693SW · Boeing 737317SDR AU970355Bracket · cracked(AUS) STABILATOR WEIGHT ARM REAR MOUNTING BRACKETS PNO 1732031-1 ANDPNO 1732031-2 CRACKED ON VERTICAL BENDSMar 18, 1997 · Cessna 177RGSDR CALA9700371Angle · crackedINSPECTION FOUND A 1.5 INCH CRACK IN LT HORIZONTAL STABILIZER ATTACH ANGLE AT STA 142 CENTER SPAR LEADING EDGE. THE CRACK WAS STOP DRILLED IAW SRM 55-10-4. REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 55-10-4 AND 51-30-2.Mar 7, 1997 · N10251 · Boeing 737291SDR AALA970527Beam · corrodedTUL - TOP CHORD OF RT HORIZ T/E BEAM HAS LARGE AREA ON OUTBOARD END REWORKED, APPEARED TO HAVE EXCESSIVE MATERIAL REMOVED. INSTALLED DOUBLER PER ESO 11697, DATED 3-5-97. (M)Mar 7, 1997 · N712AA · Boeing 727223SDR AALA970525Beam · corrodedTUL - TOP T/E CHORD OF RT HORIZONTAL CHORD ANGLE HAS AREA OF CORROSION 1 INCH TO THE RIGHT OF SECOND DOUBLER OUTBOARD. INSTALLED DOUBLER PER SRM 51-10-6 AND ESO 11697, DATED 3/3/97. (M)Mar 7, 1997 · N712AA · Boeing 727223SDR 97ZZZX1317Bearing · wornPIVOT BEARINGS WERE WORN TO POINT WHERE OUTBOARD END OF STABILATOR HAD 2 INCHES PLAY UP AND DOWN.Mar 7, 1997 · Piper PA28161SDR AALA970477Upper Beam · corrodedTUL - FOUND RIGHT HORIZONTAL TOP T/E CHORD ANGLE HAS CORROSION IN AREA OF NR 3 ELEVATOR HINGE, 2 AREAS. INSTALLED DOUBLER PER SRM 55-10-6 FIG 1 AND PER ESO 11697, DATED 3-3-97. (M)Mar 6, 1997 · N712AA · Boeing 727223SDR AALA970476Upper Beam · corrodedTUL - RIGHT HORIZONTAL TOP T/E TOP CHORD HAS CORROSION IN AREA OF NR 4 ELEVATOR HINGE, 2 AREAS. INSTALLED DOUBLER PER SRM 55-10-6 FIG 1 AND ESO 11697, DATED 3-3-97. (M)Mar 6, 1997 · N712AA · Boeing 727223SDR AALA970475Upper Beam · corrodedTUL - RIGHT HORIZONTAL T/E TOP CHORD HAS CORROSION IN AREA OF NR 5 ELEVATOR HINGE, 2 AREAS. INSTALLED DOUBLER PER SRM 55-10-6 FIG 1 AND PER ESO 11697, DATED 3-3-97. (M)Mar 6, 1997 · N712AA · Boeing 727223SDR AALA970474Upper Beam · corrodedTUL - LEFT HORIZONTAL T/E TOP CHORD HAS CORROSION IN AREA OF NR 1 ELEVATOR HINGE. INSTALLED DOUBLER PER SRM 55-10-6 FIG 1 AND ESO 11697, DATED 3-3-97. (M)Mar 6, 1997 · N712AA · Boeing 727223SDR AALA970473Upper Beam · corrodedTUL - FOUND LEFT TOP HORIZONTAL T/E CHORD HAS CORROSION IN AREA OF NR 2 ELEVATOR HINGE. INSTALLED DOUBLER PER SRM 55-10-6 FIG 1 AND ESO 11697, DATED 3-3-97. (M)Mar 6, 1997 · N712AA · Boeing 727223SDR 97FDEA00127Banjo Fitting · crackedN 00192, RT NR 4 BANJO FITTING FWD MID HOLE HAS A CRACK INDICATION FWD FLANGE, FWD DIRECTION. REF EO 8-5510-7-3314, COMPLIED WITH EA 8-5530-32533 OVERSIZE HOLE REPAIR RT NR 4 BANJO FITTING AND PYLON CARRY THROUGH CAP SEQ NR SNRM N00192. COMPLETED 3/1/97.Mar 1, 1997 · N312FE · Doug DC1030SDR CALA9700522Stiffener · crackedINSPECTION FOUND A 12.5 INCH CRACK IN LT HORIZONTAL STABILIZER LEADING EDGE OUTBOARD RIB UPPER STIFFENER. THE STIFFENER WAS REMOVED AND A NEW STIFFENER WAS INSTALLED IAW SRM 51-31-01.Feb 28, 1997 · N68041 · Doug DC1010SDR P5CA9700376Mounting Frame · corrodedLEVEL 1 CORROSION ON A PANEL MOUNTING FRAME STAB STA 231 ON THE RIGHT SIDE OF THE HORIZONAL STABLIZER. REMOVED CORROSION AND TREATED FRAME PER BAC SRM 51-10-01 AND 51-10-02.Feb 27, 1997 · N859FT · Boeing 747123SDR ABXA9700498Fitting · crackedDURING C-INSPECTION, FOUND THE RIGHT HORIZONTAL STAB SIDE ROLLER ATTACH FITTING CRACKED. REPLACED RIGHT SIDE ROLLER ATTACH FITTING IAW DC9 MAINTANCE MANUAL CHAPTERS 55-10-0 AND 20-16-0.Feb 27, 1997 · N985AX · Doug DC932SDR DL72W970354Fitting · crackedFOUND A 1 INCH CRACK IN RT ELEVATOR HINGE SUPPORT CASTING 4TH HINGE FROM O/B END. REPAIRED PER M/M 55-10-31.Feb 25, 1997 · N2817W · Boeing 727247SDR 97ZZZM951Panel · looseDURING INSPECTION, THE LEFT OUTBOARD CLOSING PANEL COMMON TO THE HORIZONTAL STABILIZER WAS FOUND LOOSE. THE ATTACH BOLTS WERE FOUND LOOSE. THE BOLTS WERE TIGHTENED AND NO OTHER DISCREPANCIES NOTED.Feb 22, 1997 · N445YV · Dhav DHC8202SDR GTIA9700199Fairing · corrodedYIP - LEFT HORIZONTAL STABILIZER LOWER SCRAPPER FAIRING: INTERIOR BOX CHANNEL HAS SURFACE CORROSION ALONG ATTACH EDGES. REMOVED MINOR SURFACE CORROSION IAW DC-9 SRM 51-10-3. (X)Feb 17, 1997 · N947ML · Doug DC932SDR GTIA9700195Rivet · failedYIP - LEFT UPPER HORIZONTAL STABILIZER FAIRING - POPPED RIVET AT AFT ATTACH AND AFT CDCC AREA CRACKED. REPAIRED CRACK AND INSTALLED EXTERNAL DOUBLER AND FILLER PER DC-9 SRM 55-01 PAGE 7, 51-30-2 AND USING MATERIAL AS PRESCRIBED IN DC-9 SRM 55-10-0, PAGE 11, FFeb 14, 1997 · N947ML · Doug DC932SDR P5CA9700278Torque Box · crackedHORIZONTAL STABILIZER TORQUE - BOX RT L/E CHAFE BUMPER SUPPORT TUBE CRACKED. REMOVED AND REPLACED HORIZ STAB TORQUE BOX RT SUPPORT TUBE I/A/W M.M. 55-10-00.Feb 10, 1997 · N858FT · Boeing 747123SDR CALA9700220Fitting · crackedINSPECTION FOUND A 3 INCH CRACK ON FITTING ATTACHED TO THE HORIZONTAL STABILIZER CENTER SECTION BOX. THE FITTING WAS REPLACED IAW SRM 51-40-02.Jan 31, 1997 · N19357 · Boeing 7373T0SDR P5CA9700177Angle · crackedCRACKED UPPER CHORD ANGLE LEFT HORIZONTAL STABILIZER TRAILING EDGE REAR SPAR AREA STA 331.8. REMOVED FABRICATED AND INSTALLED A NEW CHORD ANGLE PER BOEING SRM 51-10-01, 53-30-02 AND 51-24-11.Jan 20, 1997 · N858FT · Boeing 747123SDR P5CA9700170Angle · crackedCRACKED UPPER CHORD ANGLE RIGHT HORIZONTAL STABILIZER TRAILING EDGE REAR SPAR AREA STA 406.8. REMOVED FABRICATED AND INSTALLED A NEW CHORD ANGLE PER BOEING SRM 51-10-01, 53-30-02 AND 51-24-11.Jan 20, 1997 · N858FT · Boeing 747123SDR 97ZZZM616Beam · corrodedAFT UPPER RIGHT HORIZONTAL STAB T/E BEAM HAS EXFOLIATION CORROISON AT ES 1763149 AND SURFACE CORROISON AT ES 44. MATERIAL REMOVAL BEYOND LIMITS IAW SRM 55-20-6. FABRICATED SPLICE CAP FROM 100 INCH 7075 T6 46 INCH BY 1.7 INCH. FABRICATED SPLICE PLATE FROM .0Jan 13, 1997 · N467AT · Boeing 7372T4SDR 9627641153Support · crackedDURING PERIODIC CHECK, A CRACK WAS FOUND ON THE LEFT HORIZONTAL STABILIZER SECONDARY PIVOT SUPPORT. REMOVED AND REPLACED PIVOT SUPPORT PER EA 11-120135 (P/N AJC7230-1).Dec 20, 1996 · N153US · Doug DC1040SDR HEEA968703Stabilizer Assy · mis mfgBOTH ENDS OF STABILIZER ARE TOO THICK AND WON'T ALLOW WINGLET WITH ANGLES TO BE INSTALLED.Dec 11, 1996 · Bell 206L1SDR HEEA968699Stabilizer Assy · mis mfg2 INSERTS ON R/H FORWARD BOTTOM SIDE MISLOCATED. 4 INSERTS ON L/H AFT BOTTOM SIDE MISLOCATED.Dec 11, 1996 · Bell 206L1SDR HEEA968697Stabilizer Assy · mis mfgSTABILIZER INSERTS FOR L/H AND R/H TAILBOOM ATTACHMENT SUPPORTS MISLOCATED. INSTALLED TOO FAR OFF.Dec 11, 1996 · Bell 206L1SDR HEEA968696Stabilizer Assy · damagedDURING PAINT PREPARATION FOUND THAT EXISTING PRIMER COAT WAS PEELING OFF STABILIZER AND THAT PRIMER COAT WOULD NOT ADHERE TO EXISTING PRIMER COAT. BLASTED ASSEMBLY TO REMOVE EXISTING PRIMER COAT. FOUND THAT STABILIZER SKIN HAD SEVERAL SMALLDENTS IN AREA WHDec 11, 1996 · Bell 206L1SDR HEEA968695Stabilizer Assy · mis fitSTABILIZER TOO THICK; WILL NOT ALIGN TO STABILIZER SUPPORTS THAT ATTACH TO TAILBOOM. REPAIRED BY DODS.Dec 11, 1996 · Bell 206L1SDR N3VR96153Retainer · crackedLEFT HORIZ STABILIZER LOWR T/E SEAL RETAINER HAS SEAL RIVETS LOOSE AND LIGHT SURFACE CORROSION BETWEEN ELEVATOR HINGES NR 3 THROUGH NR 6 POSITION. CRACKS FOUND RUNNING FROM LOOSE RIVET HOLES. BLENDED OUT DAMAGED AREA, REMOVED CORROSION, RELOCATED FASTENERS IDec 4, 1996 · N590CA · Boeing 727231SDR CKSA96224Doubler · corrodedDURING C-4 CHECK INSPECTION, FOUND LEFT HORIZONTAL STABILIZER LEADING EDGE AT STA XFS185 CORRODED. REPAIRED CORROSION DAMAGE IAW SKETCH AIA/E/2404 AND EA 96-326 AND 8110-3. C-4 CHECK WORK CARD NR 4001 1OF1, NON-ROUTINE TASK CARD NR 87530.Nov 24, 1996 · N811CK · Doug DC863FSDR 96ZZZX6018Nutplate · crackedDURING REPAIR OF HORIZ STAB, FOUND STRUCTURAL NUTPLATES CRACKED THROUGH THREADS. NUTPLATES ARE USED TO ATTACH ELEVATOR HINGE BRACKETS AND FORWARD STAB SPAR TO FUSELAGE. THESE PARTS CANNOT BE SEEN DURING ROUTINE INSPECTIONS. ATTEMPTED TO REUSE ONE PREVIOUSLYNov 15, 1996 · N74420 · Gulstm AA5B
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