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 03FDEA00243Nut · corrodedRT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 1R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.Mar 3, 2003 · N585FE · Doug MD11FSDR 048329Structure · bird strikeON FLIGHT 5437 FROM KANSAS CITY MISSOURI, THE CREW THOUGHT THEY HAD A BIRD STRIKE AND DIVERTED TO SALINA KANSAS DUE TO WEATHER CONDITIONS. THE AIRCRAFT LANDED WITH NO FURTHER INCIDENT. UPON POSTFLIGHT INSPECTION, THE CREW REPORTED DAMAGE TO THE VERITCAL AND Mar 1, 2003 · N133YV · Beech 1900DSDR CA030306004Spar · cracked(CAN) INSPECTION CARRIED OUT AS PER SB 2/47 REV 'D' AD CR-91-42.TAILPLANE SPAR FOUND CRACKED LT SIDE TOP UNDER LT PICK-UP BRACKET C2TP159. MODS 2/436, 2/466, 2/758 HAD ALREADY BEEN INCORPORATED.AIRCRAFTTTSN 10127.3 HOURS.Feb 28, 2003 · Dhav DHC2MK1SDR CA030228001Hinge · cracked(CAN) DURING ROUTINE SCHEDULED MAINTENANCE, IT WAS DISCOVERED THAT THE REINFORCEMENTS - STABILIZER HINGE WERE CRACKED. P/N 0732101-4 REPLACED WITH NEW PARTS.Feb 28, 2003 · Cessna A185FSDR HEEA085030Bearing · wornHORIZONTAL STAB HORN HAS A WORN BEARING. REPAIRED.Feb 28, 2003 · N205FC · Bell 206L3SDR CA030305007Spar · cracked(CAN) REMOVED STABILIZER P/N C2-TP-1A AND LT AND RT ATTACH BRACKETS P/N C2-TP-159 AND -160 FOR INSPECTION AS PER AD CF-91-42 AND SB 2/47. - FOUND CRACK IN SPAR ABOVE LT BRACKET ATTACH POINT.Feb 19, 2003 · Dhav DHC2MK1SDR CA030221006Channel · chafed(CAN) UPPER ELEVATOR CABLE P/N NAS304-34-0753 FOUND INCORRECTLY ROUTED. INSTEAD OF PASSING THROUGH THE LIGHTNING HOLES IN AFT BOX STRUCTURE P/N50-440031-7, THE CABLE WAS ROUTED ABOVE THE STRUCTURE. THIS CAUSED THE ELEVATOR CABLE TO CUT INTO THE CHANNEL ASSY. WFeb 18, 2003 · Beech C90ASDR 2003FA0000192Bracket · crackedUNIT WAS MANUFACTURED BY COMBINING TWO SHEETMETAL BRACKETS RIVETED TO A CASTING THAT HOLDS THE OUTBOARD ELEVATOR HINGE BEARING. CRACKING WAS FOUND IN BOTH THE RIGHT AND LEFT HAND ASSEMBLIES ON THE UPPER, INBOARD BEND RADIUS. THIS CAN BE SEEN FROM UNDERNEATH Feb 17, 2003 · N721X · Cessna 310NSDR CA030217001Fitting · cracked(CAN) CRACKS FROM RIVIT HOLE IN 0.125 INCH STAMPED ATTACHMENT FLANGE COMPLETELY ACROSS FLANGE SEPARATING IT INTO TWO PIECES. (NOTE) THERE IS NO DANGER OF STABILIZER SEPARATION FROM THE AIRCRAFT AS THE FLANGE ISSTILL RIVITED TO THE INBOARD RIB IN 5 OTHER PLACESFeb 14, 2003 · Bell 206BSDR OEZ2003F00000Hinge Bracket · brokenDURING SCHEDULED INSPECTION MAINTENANCE PERSONNEL FOUND RIGHT ELEVATOR OUTBOARD HINGE PLATE LOOSE WITH RIVETS (WORKING) AT ATTACHMENT TO OUTBOARD STABILIZER RIB. UPON DISASSEMBLY FOR REPAIR. HINGE PLATE BRACKET WAS FOUND CRACKED AND BROKEN AWAY FROM FORWARD Feb 12, 2003 · N227SA · Dhav DHC6SDR SWAA030339Skin · crackedDURING SCHEDULED 1/2D CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN CRACKED AT REAR SPAR FWD OF INBD BALANCE BAY. REPAIRED SKIN PER SRM.Feb 9, 2003 · N691WN · Boeing 7373G7SDR 2003FA0000208Nut · failedON BOTH STABILATOR HINGE BOLTS THE NYLON LOCKNUTS BACKED OFF DUE TO THE NYLON PART OF THE NUT BECOMING DETACHED FROM THE NUT ITSELF. THIS HAPPENED IN APPROXIMATELY 100 HOURS TSN.Feb 7, 2003 · N668AM · Zinair CH2000SDR 2003FA0000209Nut · failedON BOTH STABILATOR HNGE BOLTS THE NYLON LOCKNUTS BACKED OFF DUE TO THE NYLON PART OF THE NUT BECOMING DETACHED FROM THE NUT ITSELF. THIS HAPPENED IN APPROXIMATELY 100 HOURS TSNFeb 1, 2003 · N649AM · Zinair CH2000SDR AMTA200300206Shim · dislodgedHORIZONTAL STABILIZER LEFT AFT SPAR INBOARD END HAS MIGRATING SHIM. COMPLIED WITH ER/A 737-55N-5076 SECTION 1. (M)Jan 30, 2003 · N314TZ · Boeing 73783NSDR 2003FA0000110Hinge · crackedDURING THE PERFORMANCE OF AD-89-12-08 THE LT OUTBOARD HINGE LUG WAS FOUND CRACKED. CRACK WAS VISUAL TO THE NAKED EYE, MICRO FRACTURES WERE NOTED LAST 200 HOUR INSPECTION BUT WERE NOT DEFINED. SUGGEST THAT CAUSE COULD BE DUE TO EXCESSIVE RADIAL AND AXIAL LOADJan 29, 2003 · N400TF · Israel 1124SDR 2003FA0000111Hinge · crackedDURING THE PERFORMING OF AD 89-12-08, THE LT OUTBOARD HINGE LUG WAS FOUND CRACKED. CRACK WAS VISUAL TO THE NAKED EYE. SUGGEST THAT CRACK CAUSE DUE TO EXCESSIVE RADIAL AND AXIAL LOADS TRANSMITTED TO THE HINGE DURING THRUST REVERSE APPLICATIONS AND FLIGHT INTOJan 28, 2003 · N59PT · Israel 1124SDR 03FDEA00080Fitting · crackedRT HORIZONTAL STAB NR 26 BARREL NUT HOLE FOUND FITTING WITH CRACK. COMPLIED WITH FEDEX EA 1-5510-67565, STABILIZERS, HORIZONTAL STABILIZER, BARREL NUT BORE 26 RT FITTING FABRICATION.Jan 27, 2003 · N607FE · Doug MD11SDR SWAA030196Skin · crackedDURING SCHEDULED C4 CHECK, FOUND LT HORIZ STAB LOWER SKIN CRACKED AT AFT SPAR RIVET ROW, CENTER BALANCE BAY. REPAIRED SKIN PER SRM.Jan 25, 2003 · N344SW · Boeing 7373H4SDR 2003F00266Bearing · crackedAT C-CHECK, FOUND CRACK ON VERTICAL STAB, RIGHT HORIZONTAL STAB HINGE BEARING. REMOVED AND REPLACED VERTICAL STAB, RIGHT HORIZ STABILIZER HINGE BEARING. (M)Jan 24, 2003 · N7643U · Boeing 727222SDR UPS03240121Beam · corrodedINSPECTION TYPE: C&SI, RT HORIZ STAB UPPER T/E BEAM BETWEEN RIB AT STR 66.50 & STR 99.76 IS CORRODED UNDER RUBSTRIP. BEAM REPLACED IAW DRAWINGS 65-20657, 65-20658, 65-20659, 65-20660-65 22402 & 65-22987Jan 21, 2003 · N945UP · Boeing 72722CSDR TSAA0355034Fitting · corrodedTHE LEFT HORIZONTAL STABILIZER CENTER SECTION REAR SPAR LOWER FITTING ASSEMBLY FAIL/SAFE AND LOWER CLEVIS LUG REQUIRED REWORK BEYOND THE LIMITS PROVIDED IN SB 737-55-1055. REFINISHED THE LUG BORE AND FABRICATED A NEW SLEEVE BUSHING AND FLANGE BUSHING PER DRAWJan 15, 2003 · N808AL · Boeing 7372T4SDR TSAA0355032Fitting · crackedTHE LEFT HORIZONTAL STABILIZER CENTER SECTION REAR SPAR ATTACHMENT FITTING CLEVIS LUGS BUSHINGS REMOVED. EDDY CURRENT INSPECTED LUGS FOR CRACKS BEFORE AND AFTER OVERSIZING AND SHOT PEENING. MACHINED, SHOT PEENED, AND FINISHED THE LUG/CLEVIS. INSTALLED BUSHIJan 15, 2003 · N808AL · Boeing 7372T4SDR GTIA030030Doubler · crackedFTW - FOUND RIGHT ELEVATOR STATION 1417 DOUBLER BENT CRACKED. REMOVED DOUBLER. FABRICATED NEW DOUBLER. INSTLALED NEW DOUBLER. (M)Jan 15, 2003 · N825NK · Doug DC983SDR TSAA0355033Fitting · corrodedTHE LEFT HORIZONTAL STABILIZER CENTER CENTER SECTION REAR SPAR UPPER FITTING ASSEMBLY UPPER CLEVIS LUG REQUIRED REWORK BEYOND THE LIMITS PROVIDED IN SB 737-55-1055. REFINISHED THE LUG BORE AND FABRICATED A NEW OVERSIZED BUSHING PER DRAWING. SHOT PEENED, REFIJan 14, 2003 · N808AL · Boeing 7372T4SDR UPS03240105Bracket · crackedINSPECTION TYPE:C+SI R/H HOR-STAB,REAR SPAR,T-BRACKET ON REAR SPAR AT ELEV.RIB ST.66.50 I S CRACKED. BRACKET REMOVED IAW SRM 51-30-2 AND DRG.NO.65-16876. NEW BRACKET FITTED IAW SRM 51-30-2 AND DRG. NO.65-16876.Jan 6, 2003 · N945UP · Boeing 72722CSDR UPS03840031Fitting · crackedINSPECTION TYPE: C2, RT HORIZONTAL STAB L/E LOWER T-ANGLE IS CRACKED AT XFS 47. REMOVED AND REPLACED FITTING IAW DWG SE08550009, AND SRM 51-1-20D.Jan 3, 2003 · N701UP · Doug DC871FSDR 010203Rib · misrepairedHORIZONTAL STABILIZER WAS REPAIRED AT AIRCRAFT TOTAL TIME OF 6658.5. 6 EACH NEW AND IMPROVED NOSE RIBS WERE INSTALLED AND NUMEROUS RIVETS WERE NOT INSTALLED IN THE REPLACED RIBS. REFERENCE SERVICE NEWSLETTER NR 87-18R1. RIBS THAT WERE DETERMINED TO BE REPLAJan 3, 2003 · N6506R · Cessna U206CSDR 2003F00340Support · corrodedLEFT HORIZONTAL STABILIZER, INTERGRANULAR CORROSION ON AFT LOWER SUPPORT BEAM, AFT LOWER FLANGE, AT 21 INCHES AND 30 INCHES FROM INBOARD END. ELEVATOR STATION 17.20 TO 47.20, CUTOUT CORRODED AREA PER SRM 51-10-1. REPAIRED PER SRM 55-10-06. (M)Jan 2, 2003 · N727PX · Boeing 72721SDR SWAA030004Skin · crackedDURING SCHEDULED D CHECK, FOUND LT HORIZONTAL STAB CRACKED ON LOWER SKIN AT STA 125 JUST FWD OF REAR SPAR. REPAIRED SKIN PER BFG ER.Jan 2, 2003 · N370SW · Boeing 7373H4SDR 2003F00338Support · corrodedLEFT HORIZONTAL STABILIZER, INTERGRANULAR CORROSION ON AFT LOWER SUPPORT BEAM UPPER FORWARD FLANGE, 27 INCHES FROM INBOARD END AT ELEVATOR STATION 17.20 TO 44.20 CUTOUT CORRODED AREA PER SRM 51-10-1. REPAIRED PER SRM 55-10-6. (M)Dec 30, 2002 · N727PX · Boeing 72721SDR EVAS091025Structure · corrodedTWO DEEP SITES CORROSION WERE FOUND WITH LT HORIZONTAL STAB, CUTOUT THE DAMAGE PORTION & PERFORM EXTERNAL REPAIR BY USING TWO DOUBLER. TWO DEEP SITES CORROSION WERE FOUND WITH INBOARD MAIN FLAP LOWER. CUTOUT THE DAMAGE PORTION & PERFORM SPLICE REPAIR BY USINDec 26, 2002 · N16605 · Boeing 767300SDR SWIA200211721Fitting · corrodedANTI-ROTATION FITTING HAS CORROSION. FOUND DURING C-CHECK INSPECTION. ANTI-ROTATION FITTING REPLACED IAW SB 601R-55-007. P/N: 600-21073-7.Dec 12, 2002 · N407SW · Cndair CL6002B19SDR USAA020472Frame · crackedHORIZONTAL STABILIZER, LOWER CHORD, 1.5 INCH CRACKED. TRIM OUT AFT SECTION LOWER CHORD AND SPLICE IN NEW SECTION.Nov 30, 2002 · N504AU · Boeing 7373B7SDR ZW0A021194Bracket · crackedBRACKET CRACKED INSIDE HORIZONTAL STABILIZER AT STA 1429 AND RBL 6. REPLACED ANGLE PER SPM 6-70-01 AND DOUGLAS DRAWING 5912188. LAST CHECK C PERFORMED IN STL 01/07/02 --CLOSED--Nov 22, 2002 · N939AS · Doug DC983SDR DLM11021325Spar Cap · crackedHORIZ STABILIZER / RH / REAR SPAR / LOWER CAP : GROUND DAMAGE REPAIR THE RH HORIZONTAL STABILIZER REAR SPAR LOWER CAP STRUCK A WORK PLATFORM DURING A TOWING OPERATION. THE AFT FLANGE OF THE LOWER CAP WASNov 14, 2002 · N813DE · Doug MD11SDR DLM90021316Bearing · crackedHORIZONTAL STAB PIVOT BEARINGS CRACKED. FOUND DURING HORIZONTAL STAB PIVOT BEARING FREE PLAY. REPLACED.Nov 13, 2002 · N915DN · Doug MD9030SDR 2002FA0001244Clip · crackedCRACKS AT TWO FASTENER HOLES ATTACHING NOTED CLIP TO THE VERTICAL STABILIZER AFT SPAR.Oct 31, 2002 · Cessna 560XLSDR ASAA020510Strake · damagedOKC - FOUND DURING 30K CHECK, RIGHT STRAKE AFT EDGE IS FLATTENED. REPAIRED IAW EA. (M)Oct 29, 2002 · N976AS · Doug DC983SDR AWXA200201091Angle · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A 1/4" CRACK WAS FOUND ON THE FORWARD UPPER SIDE OF THE L/H HORIZONTAL STABILIZER ATTACH BRACKET, BS 1156. MAINTENANCE REMOVED THE DAMAGED L/H HORIZONTAL STABILIZER ATTACH BRACKET AT BS 1156; FABRICATED A NEW REPLACEMENT Oct 29, 2002 · N150AW · Boeing 7373G7SDR 0203659981Stabilizer · crackedDuting Hck in ATL, a .25" crack was found in the upper plate of the horizontal stabilizer center section. Repaired per EA 98-190787.Oct 22, 2002 · N676MC · Doug DC951SDR C2XA02TY153Support · gougedTYS DURING A SCHEDULED 2-C INSPECTION THE R/H HORIZ. STAB HINGE SUPPORTS WERE FOUND GOUGED INSIDE THE PIVET BUSHING MOUNTS. MAINT. MEASURED INBD/OTBD PIVOT BUSHING HOLES,REAMED BOTH TO 1.640" ALLODINED BOTH HOLES AND INSTALL BUSHINGS IAW EMB 135/145 CPM 51-21Oct 21, 2002 · N16976 · Emb EMB145LRSDR QXEA0201720Support · gougedPDX - HORIZONTAL STAB, LT FORWARD SPAR, LT FORWARD SUPPORT HAS MULITPLE GOUGES ACROSS FACE OF LEG. REPAIRED IAW DHC-8200 SRM 51-20-26, PAGE 7.Oct 15, 2002 · N364PH · Dhav DHC8202SDR C2XA02SH083Bushing · damagedDURING C CHECK, ALL HAT BUSHINGS ON THE RUDDER ATTACHING BRACKETS WERE FOUND DAMAGED. MAINTENANCE REMOVED AND REPLACED ALL HAT BUSHINGS ON RUDDEDR ATTACHING BRACKETS IAW EMB AMM 20-10-08. THE AURCRAFT WAS APPROVED TO RETURN TO SERVICE.Oct 4, 2002 · N14937 · Emb EMB145ERSDR DF22002F00002Nut Plate · brokenDURING 100 HOUR INSPECTION, TECHNICIAN FOUND LOWER ELEVATOR STOP NUTPLATE BROKEN AND FIBER LOCK PORTION OF PART SEPARATED FROM THE REST OF NUTPLATE. STOP BOLT COULD MOVE FREELY.Sep 27, 2002 · N23675 · Cessna 172RSDR UPS02239557Pin · corrodedINSPECTION TYPE:C&SI HORIZ. STAB. HINGE R/H OUTER PIN HAS EVIDENCE OF PITTING CORROSION A DJACENT TO RELIEF RADIUS HORIZ. STAB HINGE R/H O/B PIN REPLACED IAW MM 55-10-01Sep 24, 2002 · N930UP · Boeing 72722CSDR C2XA02TY143Fitting · gougedTYS DURING A SCHEDULED 2-C INSPECTION, MAINTENANCE FOUND A GOUGE IN THE RT HORIZONTAL STAB HINGE PIN SAFETY PIN WHICH REQUIRED A GST, ALL WORK WAS ACCOMPLISHED IAW GST WHICH STATED BLEND, ALODINE, PRIME AND PAINT SRM 51-70-03, CPM 51-21-04, 05, 06. A/C WILL Sep 18, 2002 · N14974 · Emb EMB145SDR C2XA02TY142Fitting · gougedTYS DURING A SCHEDULED 2-C INSPECTION MAINTENANCE FOUND A GOUGED IN THE HORIZONTAL STAB LT HINGE PIN, A GST 2827/02 WAS ISSUED, WHICH STATED ALODINE, PRIME AND PAINT IAW WITH THE GST-2827-02, EMB 145 SRM 51-71-03, CPM 51-21-04-05 AND 51-21-06. ALL WORK WAS ASep 18, 2002 · N14974 · Emb EMB145SDR AAL2003F00016Plate · corrodedLEFT INBOARD HORIZONTAL STABILIZER PIVOT BEARING LUG PLATES ARE CORRODED. 1.5 INCH X 1.5 INCH AREA, BEYOND LIMITS. REPLACED LEFT INBOARD HORIZONTAL STABILIZER LUG PLATES AND MACHINED PIVOT BORE IAW FCO 0488A, 9, D AND E.Sep 17, 2002 · N596AA · Doug DC983SDR AALA20021330Plate · corrodedTUL - FOUND RIGHT INBOARD HORIZONTAL STAB PIVOT BEARING LUG PLATES ARE CORRODED. REPLACED RIGHT INBOARD HORIZ STAB LUG PLATES AND MACHINED PIVOT BORE PER FCDKF0488A, 9, D/E. (M)Sep 17, 2002 · N596AA · Doug DC983SDR AALA20021329Plate · corrodedTUL - FOUND LEFT OUTBOARD HORIZONTAL STAB PIVOT BEARING LUG PLATES ARE CORRODED. REPLACED LEFT OUTBOARD LUG PLATES AND MACHINED PIVOT BORE PER FCD0488A, 9, D/E. (M)Sep 17, 2002 · N596AA · Doug DC983
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