JASC 5510

Service difficulty reports · 5,966

Reports filed under 5510 · Horizontal Stabilizer 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 = '5510'
  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 IXXA0100031Doubler · crackedDURING ROUTINE C CHECK INSPECTION, A CRACK WAS DETECTED ON THE RIGHT HORIZONTAL STABILIZER AFT SPAR WEB INTERNAL DOUBLER AT STATION XE 105. REPAIR ACCOMPLISHED REMOVAL OF DAMAGE AREA, FABRICATION AND INSTALLATION A NEW INTERNAL DOUBLER IN ACCORDANCE WITH DOUGLMar 15, 2001 · N820BX · Doug DC871FSDR DHL2001806503Fitting · crackedRT HORIZONTAL STABILIZER, LE INTERIOR LWR FITTING CRACKED 1 IN AT STA XFS 60.REMOVED CRACKED FITTING AT STA. XFS.60 OF RT HORIZONTAL STAB LE INTERIOR IAW SRM 51-1-20D PAGE 21. CLEANED, TREATED, & PRIMED AREA IAW SRM 51-1-8 PAGE 12-13. INSTALLED NEW FITTING IMar 13, 2001 · N806DH · Doug DC873FSDR UPS01435443Bracket · crackedINSPECTION TYPE:C TAIL. CRACK IN ANGLE BRACKET ON RT HORIZONTAL STAB REAR SPAR AT STAB STA . 580 NEW BRACKET FABRICATED AND FITTED IAW SRM 51-30-02Mar 13, 2001 · N672UP · Boeing 747123FSDR 01FDEA00283Angle · crackedNR 3 RT LEAD EDGE ASSY FOR HORIZONTAL HAS 7 INCH STRESS CRACK, RUNNING THRU HOLES ON UPPER FLANGE. *S/D* REMOVED AND REPLACED T-ANGLE REF SRM 55-10-00. RE-INSTALLED NR 3 RT LEADING EDGE ASSY.Feb 23, 2001 · N315FE · Doug DC1030FSDR UPS01235215Pin · crackedINSPECTION TYPE:C+SI, LT OUTER HORIZ STAB HINGE PIN CRACKED. REPLACED PIN IAW MM 55-10-01.Feb 18, 2001 · N941UP · Boeing 72722CSDR COMA0160268Bushing · scoredHORIZONTAL STABILIZER LEFT O/B BUSHING (P/N 600-23068-1) WAS FOUND SCORED DURING INCORPORATION OF COMAIR EO 55-007. REPLACED BUSHING IN LT ORIZ STAB WITH 1ST OVERSIZE BUSHING (P/N 601R-55-11-022-1) IAW CRJ REO 601R-55-11-022A CRJ DRWG 600-23068 AND CRJ AMM 20Feb 18, 2001 · N912CA · Cndair CL6002B19SDR USAA010206Fitting · crackedPIT - FOUND FITTING CRACKED AND CORRODED .25 INCH BY .075 INCH PLUS DEEP, RIGHT HORIZONTAL STABILIZER FITTING FORWARD TOP SPAR LUG HORIZ SIDE. CORROSION LEVEL 1. MACHINED FITTING AND INSTALLED NEW BUSHINGS PER SRM 55-10-10, J3-90-09000-173. (M)Feb 15, 2001 · N352US · Boeing 737301SDR USAA010205Fitting · corrodedPIT - FOUND FITTING BUSHING DAMAGE, RIGHT HORIZONTAL STAB FORWARD CENTER SECTION, TOP AFT CLEVIS FITTING. CORROSION LEVEL 1. MACHINED FORWARD FACE OF LUG REMOVED .014 INCH PER SRM 55-10-10, MFG NEW BUSHING PER SRM 55-10-10. (M)Feb 15, 2001 · N352US · Boeing 737301SDR 20010322CW005Bracket · crackedTHE LT ATTACH BRACKET THAT SECURES THE HORIZONTAL STABILIZER TO THE VERTICAL FIN HAD A CRACK AT THE LOWER HUCKBOLT HOLE ATTACHING IT TO THE VERTICAL FIN. REPLACEMENT OF THE BRACKET WAS REQUIRED DUE TO THIS CRACK. AREA IS HARD TO SEE, LOCATED ON THE FORWARD LFeb 15, 2001 · N333RD · Beech B200SDR CA010308013Boot · detached(CAN) AIRCRAFT WAS IN CLIMBOUT FROM ST.JOHNS AIRPORT, AT 22,000 FEET, AIRSPEED 140 KNOTS, RATE OF CLIMB 1,800 F.P.M., PILOT EXPERIENCED SEVERE BUFFETING TO THE POINT THAT A/C WAS ABOUT TO STALL. STALL WARNING DID NOT ACTIVATE, A/C WAS PLACED IN LEVEL FLIGHT ANFeb 12, 2001 · Beech B300SDR 20010322CW004Fitting · crackedDURING ANNUAL INSPECTION THE HORIZONTAL STABILIZER ATTACHMENT POINT REINFORCEMENT ON THE LEFT SIDE WAS FOUND CRACKED. THIS REINFORCEMENT WAS THE NEW STYLE STEEL PN 12326241 THAT WAS CRACKED. THIS AC IS USED FOR LOW LEVEL OVERLAND SURVEY AND THESE REINFORCEMEFeb 5, 2001 · N967CC · Cessna T210NSDR AU010088Hinge · loose(AUS) ELEVATOR CENTER BEARING SUPPORT BLOCK MOVING IN CLAMPING FLANGES DUE TO APPROXIMATELY 0.127MM TO 0.254MM (0.005IN TO 0.010IN) ELONGATION OF THE RIVET HOLES.Feb 2, 2001 · Beech 76SDR MWEA010142Web · crackedLEFT HORIZONTAL STABILIZER LEADING EDGE SIDE ROLLER SUPPORT WEB IS CRACKED. REMOVED CRACKED SUPPORT WEB AND INSTALLED NEW SUPPORT WEB.Feb 1, 2001 · N805ME · Doug DC981SDR 20010509CW007Hinge Bracket · corrodedUPON INSPECTION OF RIGHT HAND OUTBOARD HORIZONTAL STABILATOR ELEVATOR HINGE BRACKET, A BADLY EXFOLIATED BRACKET WAS FOUND.Jan 30, 2001 · N154GA · Beech 1900CSDR COMA0160179Bushing · wornHORIZONTAL STABILIZER RIGHT OUTBOARD BUSHING IS WORN. REMOVED AND REPLACED BUSHING (P/N 600-23068-1) AND REAMED BUSHING TO 1.5004 IAW CRJ AMM 20-26-00-910-803 AND DRAWING 600-23068.Jan 29, 2001 · N937CA · Cndair CL6002B19SDR UPS01835135Bulkhead · crackedINSPECTION TYPE:C1/3, RT HORIZ STAB JACKSCREW FWD MOUNTING BULKHEAD HAS CRACKS THAT HAVE GONE THROUGH STOP DRILLS 2 EACH. REPAIRED IAW DC8 SRM 53-2-0 FIG 23.Jan 26, 2001 · N810UP · Doug DC873FSDR CALA0100032Strap · gougedINSPECTION FOUND BOWTIE STRAP GOUGED AT TAIL CONE ATTACH POINT AFT OF RT HORIZONTAL STABILIZER ATTACH FITTING. REPLACED WITH NEW STRAP IAW SRM 51-10-2.Jan 16, 2001 · N14381 · Boeing 7373Q8SDR COMA0160122Bushing · wornHORIZONTAL STABILIZER LEFT O/B PIVOT POINT BUSHING WAS FOUND TO BE WORN. PERFORMED A MAJOR REPAIR BY REPLACING HORIZONTAL STABILIZER LEFT O/B PIVOT POINT BUSHING (P/N 601R55-11-022-1) IAW CRJ REO 601R-55-11-2=022 REV A.Jan 12, 2001 · N915CA · Cndair CL6002B19SDR CA010130009Bushing · failed(CAN) HORIZONTAL STABILIZER HAS MOVEMENT OF .003 AT ATTACHMENT POINTS, WHEN TIP OF STAB IS MOVED IN A UP AND DOWN MOTION. THIS AIRCRAFT HAS BEEN LIKE THIS SINCE NEW. AS PER PILATUS, 0 TOLERANCE ALLOWED AT ATTACHMENT POINT. BUSHINGS WERE REPLACED WITH NO IMPROVJan 3, 2001 · Pilats PC1245SDR C2XA011A005Bearing · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT AND LEFT HORIZONTAL STABILIZER SPHERICAL BEARINGS WERE FOUND TO BE WORN AND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SPHERICAL BEARINGS IAW EMB145 MM 55-37-00-400-801A, AND THE AIRCRAFT WAS APPROVED FODec 30, 2000 · N15941 · Emb EMB145SDR SWAA002766Housing · corrodedDURING SCHEDULED D-CHECK, FOUND HORIZONTAL STAB CENTER SECTION CORRODED AT UPPER ATTACH LUG FOR HINGE HOUSING. REPAIRED HINGE HOUSING FITTING PER ERO.Dec 28, 2000 · Boeing 7372H4SDR SWAA002765Fitting · corrodedDURING SCHEDULED D-CHECK, FOUND HORIZONTAL STAB CENTER SECTION CORRODED AT ATTACH FITTING LUGS, LT UPPER AFT, LT LOWER AFT, LT LOWER FWD, RT UPPER AFT AND LOWER CLEVIS. REPAIRED FITTING AND LUGS PER ACO.Dec 28, 2000 · Boeing 7372H4SDR CALA0001991Bracket · crackedINSPECTION FOUND A 1 INCH CRACK IN RT HORIZONTAL STABILIZER BRACKET AFT OF AFT UPPER ATTACH LUG. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-10-02.Dec 24, 2000 · N19382 · Boeing 7373Q8SDR CALA0001990Bracket · crackedINSPECTION FOUND A 1 INCH CRACK IN RT HORIZONTAL STABILIZER BRACKET AFT OF AFT UPPER ATTACH LUG. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-10-02.Dec 24, 2000 · N19382 · Boeing 7373Q8SDR CALA0001989Strap · gougedINSPECTION FOUND BOWTIE STRAP JUST AFT OF LT HORIZONTAL STABILIZER ATTACH LUG GOUGED. THE STRAP WAS REMOVED AND REPLACED IAW SRM 51-10-02.Dec 23, 2000 · N19382 · Boeing 7373Q8SDR CALA0001984Fitting · corrodedINSPECTION FOUND CORROSION ON LUG RT UPPER FORWARD BOSS AT RT HORIZONTAL STABILIZER CENTER SECTION. INSTALLED NEW BUSHING AND VERIFIED DIMENSIONS IAW CMM 55-10-06.Dec 22, 2000 · N19382 · Boeing 7373Q8SDR AALA20010068Beam · corrodedTUL - FOUND CORROSION ON UPPER LEFT HORIZONTAL TIE (BEAM) 8 INCHES FROM INBOARD END. REMOVED CORROSION, TREATED AND PRIMED AND INSTALLED DOUBLER PER SRM 55-10-6. (M)Dec 21, 2000 · N875AA · Boeing 727223SDR AALA20010067Beam · corrodedTUL - FOUND CORROSION ON TIE OF LEFT HORIZ STABILIZER OUTBOARD END 6 INCHES INBOARD OF OUTBOARD END, T/E BEAM. REMOVED CORROSION, TREATED AND PRIMED AND INSTALLED DOUBLER OF T3 2024.063 PER SRM 55-10-6. (M)Dec 21, 2000 · N875AA · Boeing 727223SDR SPAA0000040Spar · damagedDURING ACCOMPLISHMENT OF SB 737-55-1055 FOUND UNEVEN PREVIOUSLY BLENDED AREA AT LEFT SIDE HORIZONTAL STABILIZER CENTER SECTION REAR SPAR FITTING LOWER CLEVIS AFT LUG, AFT FACE. REPAIRED BY SPOT FACING/MACHINING SURFACE TO OBTAIN A FLAT SURFACE. APPROVAL FOR REDec 20, 2000 · N703S · Boeing 7372T4SDR SPAA0000039Fitting · damagedDURING ACCOMLISHMENT OF SB 737-55-1055 FOUND TOOLING MARK ON THE LT HORIZONTAL STAB CENTER SECTION FRONT SPAR LOWER CLEVIS FORWARD LUG, FORWARD FACE. BLENDED AND SPOT FACED EXISTING DAMAGE. APPROVAL OF REPAIR PROVIDED BY FAA FORM 8110-3 DATED DECEMBER 13, 2000Dec 20, 2000 · N703S · Boeing 7372T4SDR SPAA0000037Spar · corrodedDURING ACCOMPLISHMENT OF SB 737-55-1055, RT SIDE OF HORIZONTAL STABILIZER CENTER SECTION LOWER AFT CLEVIS LUG, FWD EAR BUSHING HOLE WAS FOUND TO HAVE CORROSION AND WAS ABOVE ALLOWABLE DIMENSIONS PER DRAWING 65C22125. REPAIRED BY REMOVING CORROSION AND INCREASIDec 20, 2000 · N703S · Boeing 7372T4SDR SPAA0000036Fitting · corrodedDURING ACCOMPLISHMENT OF SB 737-55-1055, CORROSION WAS FOUND AT THE LOWER AFT LUG BUSHING HOLE COMMON TO THE HORIZONTAL STABILIZER CENTER SECTION REAR SPAR FITTING RIGHT HAND SIDE. REPAIRED BY INCREASING THE DIAMETER OF THE BUSHING HOLE TO 1.540 DIAMETER. REPADec 20, 2000 · N703S · Boeing 7372T4SDR 20010208CW001Fitting · damagedWHILE INSPECTING AC AFTER A TAIL STRIKE REPORT, HEARD LOUD NOISES OCCURING WHILE LIFTING AND PUSHING ON HORZ STAB TIPS. UPON FURTHER DISASSEMBLY AND INSPECTION, MECHANIC FOUND HOLES IN THE AFT HORZ STAB. FITTINGS ELONGATED, ALL FITTINGS AND HARDWARE WERE REPDec 18, 2000 · N10849 · Cessna 150LSDR AU001196Skin · delaminated(AUS) RT HORIZONTAL STABILISER LEADING EDGE (LAMINATED TIMBER CONSTRUCTION) BADLY DELAMINATED , THE TIMBER SECTION ROTTED AND THE BONDED SECTION FULL OF WATER. RUBBER BOOT DISBONDED AND INFLATION CELLS PERISHED ON THE TOP SURFACE.Dec 17, 2000 · Fokker F27MK500SDR SPAA0000038Fitting · damagedDURING ACCOMPLISHMENT OF SB 737-55-1055 DAMAGE WAS FOUND TO THE LEFT HAND HORIZONTAL STABILIZER REAR SPAR UPPER TERMINAL FITTING. BLENDED DAMAGED AREA, FLAP PEENED, AND FINISHED REWORK PER SB 737-55-1055. APPROVAL PROVIDED BY FAA FORM 8110-3 DATED DECEMBER 8,2Dec 13, 2000 · N703S · Boeing 7372T4SDR CA001214016Bracket · cracked(CAN) THE HORIZONTAL STABILIZER UPPER AND LOWER SKIN AT THE RIGHT HAND ELEVATOR ATTACH BRACKET WERE FOUND DENTED AND CRACKED. THE DAMAGED AREA WAS OUT AWAY AND REPAIRED BY INSTALLING AN INNER SPLICE PLATE AND AN EXTERNAL DOUBLERS PLATE PATCH OF 2024T3 ALUMINUMDec 4, 2000 · Emb EMB110P1SDR DHL200180257CStructure · crackedVERTICAL STAB L/E INTERIOR 1/2 INCH CRACK AT STA ZFS 123.000. STOP DRILLED CRACK PER SRM 55-2-0. FABRICATED DOUBLER PER SRM 55-2-0. CLEANED,TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED DOUBLER PER SRM 55-2-0Dec 3, 2000 · N802DH · Doug DC873FSDR RRXA003548Plate · gougedDURING A MAINTENANCE VISIT FOUND GOUGES IN TWO PLACES ON THE R/H HORIZ STAB RUB PLATE AFT SECTION, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////OPEN/////Dec 1, 2000 · N795FT · Doug DC873FSDR CA001218013Fitting · broken(CAN) UPON SCHEDULED INSPECTION THE RT HORIZONTAL STABILIZER WAS FOUND TO HAVE SOME PLAY. FURTHER INVESTIGATION REVEALED THE FITTING WHICH ATTACHES THE STABILIZER TO THE TAIL BOOM WAS CRACKED. WHEN THE STAB WAS REMOVED, THE FITTING CAME OFF IN 2 PIECES. IT WASNov 28, 2000 · Bell 206BSDR 20001214SH025Bracket · crackedDURING ANNUAL INSPECTION, MECHANIC FOUND REINFORCEMENT BRACKET LOCATED CENTER AFT ON HORIZONTAL STABILIZER WAS CRACKED. POSSIBLE CAUSE, MOVING AIRCRAFT VIA HORIZONTAL STABILIZER AND NOT WITH TOW POINTS. INSTALLED NEW AND IMPROVED BRACKETS PER SEB00-10. (X)Nov 20, 2000 · N6509N · Cessna T210NSDR 20001120SH014Structure · corrodedHORIZONTAL STABILIZERS - CENTER SECTION REAR SPAR UPPER FAILSAFE STRAP, CORROSION BLEND-OUT NEAR LEFT AND RIGHT STABILIZER STA 32.08 TOP SURFACE EXCEEDED CORROSION REMOVAL LIMITS. SERVICE ORDER NR 109003 OPS NR 20932 AND 20864 TIMCO RED NR S00330. FOUND DUNov 20, 2000 · N129NA · Boeing 7272J7SDR SWAA002363Stiffener · crackedDURING SCHEDULED 1/4D CHECK, FOUND RT HORIZ STAB STIFFENER CRACKED AT STA 83.50. REPLACED STIFFENER PER SRM.Nov 14, 2000 · N658SW · Boeing 7373L9SDR L1GA200000386Fairing · chafedLT HORIZONTAL STAB UPPER FAIRING CHAFED AFT END. REPAIRED PER DRAWING FVT DWG 55-00536-4.Nov 14, 2000 · N12510 · Doug DC932SDR L1GA200000379Fairing · corrodedCORRODED AND GOUGED FAIRING LT HORIZONTAL STAB I/B LEADING EDGE FAIRING. FABBED NEW FAIRING.Nov 14, 2000 · N12510 · Doug DC932SDR RRXA003648Fitting · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE L/HORIZ STAB BATH TUB AREA OF AFT UPPER RIB CAP AT ELEVATOR HINGE SUPPORT AT STA XE 147.9, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8S RM 51-1-8.Nov 9, 2000 · N603AL · Doug DC873FSDR RRXA003647Fitting · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE BATH TUB FITTING OF AFT LWR RIB CAP AT ELEVATOR HINGE SUPPORT AT STA XE 147.9, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NNov 9, 2000 · N603AL · Doug DC873FSDR CA001110041Bushing · damaged(CAN) SHORTLY AFTER TAKEOFF, THREE MINUTES AFTER AUTOPILOT WAS ENGAGED PILOT RECEIVED AP PITCH TRIM MESSAGE. SECOND FAILURE OF AUOPILOT OCCURRED 1 MINUTE AFTER RE-ENGAGEMENT MESSAGES POSTED ON EICAS DURING EVENT WERE AP TRIM IS ND AND NU. ELECTRIC STAB TRIM OPNov 9, 2000 · Cndair CL6002B19SDR COMA0060882Bushing · out of positionLEFT HAND VERTICAL STAB BUSHING IS MIGRATED AT HORIZONTAL STAB PIVOT POINT. REMOVED MIGRATED BUSHING. FOUND VERT STAB FITTING LUG BORE TO BE OUT OF TOLERANCE AT 1.7020 INCH. TOOK 1ST OVERSIZE BUSHING (P/N 601R55-31-002-5) AND MACHINED AND CAD PLATED IAW CRJNov 6, 2000 · N951CA · Cndair CL6002B19SDR 20001128SH001Hinge · corrodedTHE PAINT WAS CRACKED AROUND THE HINGE PLATE ON THE RT SIDE. A FINGERNAIL WOULD GO UNDER A COUPLE OF THE RIVETS. WHEN THE RIVETS WERE DRILLED OUT, SEVERAL SPUN AND BROKE BEFORE THE BIT WENT THROUGH. THE BACK SIDE OF THE HINGE PLATES WAS RUSTED AND BLACK GANov 2, 2000 · N8022R · Beech A24RSDR CA001122028Plate · cracked(CAN) AT 8,724.9 AIRFRAME HOURS, WHILE CONDUCTING A 100-HOUR INSPECTION, A CRACK WAS DETECTED ON THE LT UPPER HORIZONTAL STABILIZER ATTACHMENT DOUBLER. THIS IS A KNOWN STRESS AREA AND REPLACEMENT PARTS ARE NOW UPGRADED. EUROCOPTER SERVICE LETTER 400-53-82 SHONov 2, 2000 · Snias AS350B
Back to JASC 5510