JASC 5514

Service difficulty reports · 2,805

Reports filed under 5514 · Horizontal Stabilizer Miscellaneous 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 = '5514'
  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 05FDEA00898Structure · corrodedRT HORIZONTAL STABILIZER UPPER BARREL NUT NR 13 HAS BORE CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-78133.Apr 8, 2005 · N576FE · Doug MD11SDR 05FDEA00897Structure · corrodedRT HORIZONTAL STABILIZER UPPER BARREL NUT NR 11 HAS BORE CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-78133.Apr 8, 2005 · N576FE · Doug MD11SDR 05FDEA00892Structure · corrodedSTABILIZERS - HORIZONTAL STABILIZER BARREL NUT BORES, CORROSION REMOVAL, COMPLY WITH EA 1-5510-71839. COMPLIED WITH EA 1-5510-71839.Apr 7, 2005 · N582FE · Doug MD11SDR 05FDEA00891Structure · corrodedSTABILIZERS - HORIZONTAL STABILIZER BARREL NUT BORES, CORROSION REMOVAL COMPLY WITH EA 1-5510-71838. COMPLIED WITH EA 1-5510-71838.Apr 7, 2005 · N582FE · Doug MD11SDR 05FDEA00890Structure · corrodedRT HORIZONTAL STABILIZER UPPER BARREL NUT NR 23 HAS BORE CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-78133.Apr 7, 2005 · N576FE · Doug MD11SDR 05FDEA00860Structure · corrodedCORROSION REMOVED ON HORIZONTAL STABILIZER LEFT UPPER FORWARD SKIN PLANK NR 5L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-82991.Apr 6, 2005 · N617FE · Doug MD11SDR 05FDEA00853Structure · corrodedCORROSION REMOVED ON HORIZONTAL STABILIZER LEFT UPPER FORWARD SKIN PLANK NR 2L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-82939.Apr 5, 2005 · N616FE · Doug MD11SDR 05FDEA00852Structure · corrodedCORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT UPPER AFT SKIN PLANK NR29R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-82942.Apr 5, 2005 · N616FE · Doug MD11SDR DXTA200500661Structure · bird strikeBIRD STRIKE ON TAKEOFF. DAMAGE TO RIGHT HORIZONTAL STAB APPROX 8 INCHES WIDE & 2 INCHES DEEP.Apr 4, 2005 · N340QS · Cessna 560CESSNASDR 05FDEA00788Structure · corrodedCORROSION REMOVED ON HORIZONTAL STAB RT UPPER CENTER SKIN PLANK NR 16R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82953.Apr 1, 2005 · N616FE · Doug MD11SDR 05FDEA00771Skin · corrodedRT HORIZONTAL STABILIZER UPPER BARREL NUT NR 28 HAS BORE CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-78133.Mar 31, 2005 · N576FE · Doug MD11SDR GTIA050098Doubler · crackedHORIZONTAL STABILIZER, RT SIDE IB UPPER BRACKET SUPPORT HAS CRACK ON DOUBLER. REMOVED CRACKED DOUBLER. FABRICATED NEW DOUBLER. TREATED AND PRIMED, INSTALLED DOUBLER IAW SRM. (K)Mar 10, 2005 · N821NK · Doug DC982SDR 2005UALA00236Skin · dentedFOUND DENT IN HORIZONTAL STAB RT SIDE ABOUT 2 FEET IN FROM TIP. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER REPAIR.Mar 10, 2005 · N332UA · Boeing 737322SDR SIMA200507521Bushing · wornSAW - BUSHING AT HORIZONTAL STABILIZER HINGE POINTS HAVE PLAY. COMPLIED WITH EMB 135 SRM 55-10-02 FOR HORIZONTAL STABILIZER BUSHING RAI. AIRCRAFT WAS RETURNED TO SERVICE. (M)Mar 8, 2005 · N705AE · Emb EMB135LRSDR CA050224006Torque Link · misinstalled(CAN) DURING COMPLIANCE OF SB 45-27-13, REPLACEMENT OF HORIZONTAL STAB. UPPER AND LOWER TORQUE LINK ASSYS, THE LOWER TORQUE LINK WAS FOUND INSTALLED UPSIDE DOWN AND WAS MAKING CONTACT WITH THE UPPER TORQUE LINK WHEN HORIZONTAL STAB. TRAVELS TO FULL DOWN POSITIFeb 22, 2005 · Lear 45LEARSDR CA050225003Reinforcement · cracked(CAN) BOTH STABILIZER HINGE REINFORCEMENT FOUND CRACKED WHILE PERFORMING ANNUAL INSPECTION. REPLACEMENT PARTS ORDERED FROM MFG. THIS IS NOT UNCOMMON TO FIND CRACKS IN THIS AREA. PROBABLE GROUND HANDLING LOADS OR MISFIT ON INSTALLATION. NOTE THAT STABILIZER HFeb 21, 2005 · Cessna A185ESDR 2005FA0000258Tab · crackedPILOT NOTED IN FLIGHT WITH MAX NOSE DOWN TRIM AND AIRCRAFT STILL WANTED TO CLIMB. INSP REALIZED THAT STABILATOR TAB HORN BEGAN TO TEAR AWAY FROM TAB SKINS. THIS DECREASED OVERALL TAB EFFECTIVENESS. STAB TRIM TAB SKIN AND RIBS WERE CRACKED AT THE IB JACK SCRFeb 19, 2005 · N41343 · Piper PA28R200SDR LCQ36Fitting · corrodedHORIZONTAL STABILIZER LT MOUNT LUG FITTING FOR PIVOT BEARING O/B FACE HAS CORROSION. S/O 152051, OPS 29688, ZONE 2A-24.Jan 19, 2005 · N867AT · Doug DC932SDR SWAA050027Fitting · crackedDURING SCHEDULED 1/2D CHECK, FOUND HORIZONTAL STAB CENTER SECTION UPPER FITTING AND THRUST BEAM, CRACKED. REMOVED AND REPLACED FITTING PER MM.Jan 4, 2005 · N345SA · Boeing 7373K2SDR 04FDEA03409Structure · corrodedEMPENNAGE, HORIZONTAL STAB LEFT HAND UPPER FORWARD PLANK NR 5L, BARREL NUT BORE CORROSION REWORKED. FOUND EXCEEDED LIMIT. REPAIRED AS PER FEDEX EA 1-5510-78096.Dec 14, 2004 · N577FE · Doug MD11SDR ASA0440290Skin · crackedPAE - FOUND RIGHT HORIZONTAL STAB LOWER SKIN IS CRACKED. CUT OUT DAMAGED SKIN, FABRICATED REPAIR FILLER AND DOUBLER PER SRM AND EA, INSTALLED REPAIR DOUBLER TO LOWER SKIN OF RIGHT HORIZONTAL STABILIZER. (M)Dec 12, 2004 · N769AS · Boeing 7374Q8SDR CA041118004Fairing · mislocated(CAN) DURING ANNUAL INSPECTION THE HORIZONTAL STAB FAIRING SCREW HOLES FOUND TO BE DRILLED THROUGH THE RIVETS ATTCHING THE SKIN TO THE CLOSING RIBS OF BOTH HORIZONTALSTABS. HOLES WERE LOCATED ON THE LOWER SURFACES ONLY. 7 OF 19 RIVETS WERE DRILL ED ON THE PORTNov 18, 2004 · Airtrc AT802ASDR SWIA200414193Web · crackedLEFT HORIZONTAL STAB WEB CRACKED FROM LIGHTNING HOLE AT LBL 58.92 AND STRINGER NR 2, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED LT HORIZONTAL STAB, WEB AT LBL 58.92 AND STRINGER NR 2, IAW CRJ REO 601R-55-11-136.Nov 18, 2004 · N410SW · Cndair CL6002B19SDR SWIA200414192Fitting · corrodedHORIZONTAL STAB ANTI-ROTATION FITTING CORRODED, ITEM FOUND AT C-CHECK INSPECTION. HORIZONTAL STAB ANTI-ROTATION FITTING REPLACED IAW SB 601R-55-007.Nov 18, 2004 · N410SW · Cndair CL6002B19SDR 04FDEA03152Fitting · corrodedCORROSION REMOVED ON BARREL NUT BORE NR 21R EXCEEDED LIMITS. REF TO EO 1-5510-7-5000 C4 PT1, BARREL NUT BORE NR 21R. REPAIRED PER FEDEX EA NR 1-5510-79789, STABILIZERS, HORIZONTAL STABILIZERS, BARREL NUT BORE, REWORK/REPAIR, 1-5510-7-5000.Nov 17, 2004 · N618FE · Doug MD11SDR 04FDEA03150Fitting · corrodedCORROSION REMOVED ON BARREL NUT BORE NR 15R EXCEEDED LIMITS. REFERENCE TO EO 1-5510-7-5000 C4 PT1, BARREL NUT NR 15R REPAIRED PER FEDEX EA NR 1-5510-79789, STABILIZERS, HORIZONTAL STABILIZERS, BARREL NUT BORE REWORK/REPAIR - 1-5510-7-5000.Nov 17, 2004 · N618FE · Doug MD11SDR GLBA20030753Web · crackedIN PANEL 332 ATC WHERE DE-ICE LINE GOES THROUGH METAL CRACKED AROUND GROMMET ( FWD WEB). REPAIRED HORIZ MAIN SPAR WEB.Nov 5, 2004 · N122UX · Beech 1900DSDR IXXA060053SAngle · crackedDURING ROUTINE C CHECK, FOUND LEFT HORIZONTAL STABILIZER INBOARD TRAILING EDGE LOWER ANGLE CRACKED AT STATION XE 29.77. REMOVED DAMAGE, FABRICATED REPAIR PART, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR PART AND FASTENERS IN LEFT HORIZONTAL Oct 7, 2004 · N825BX · Doug DC871FSDR UPS04M43189Structure · corrodedINSPECTION TYPE:C, HORIZONTAL STAB NR 32 RT BARREL NUT HOLE FOUND CORRODED ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED, BLEND & REAMED TO 1.178 INCH FOUND OUT OF LIMIT AT BARREL NUT HOLE NR 32 RT. FAB SLEEVE & BUSHING PER EO MD11-5510-19409-H.Aug 4, 2004 · N277UP · Doug MD11FSDR UPS04M43188Structure · corrodedINSPECTION TYPE:C, HORIZONTAL STAB NR 14 RT BARREL NUT HOLE FOUND CORRODED ON BOTTOM SIDEWALL & BEARING SURFACE. CORROSION REMOVED, BLEND & REAMED TO 0.988 INCH AT BARREL NUT HOLE NR 14 RT, FOUND OUT OF LIMIT. FAB SLEEVE & BUSHING PER EO MD11-5510-19409-H. Aug 1, 2004 · N277UP · Doug MD11FSDR IXXA060385SBushing · corrodedDURING ROUTINE C CHECK, FOUND LEFT HORIZONTAL STABILIZER ELEVATOR SUPPORT BUSHING CORRODED AT STATION XE 140. REPAIRED PER ALL APPLICABLE DATA.Jun 22, 2004 · N41CX · Doug DC862FSDR IXXA060384SFitting · crackedDURING ROUTINE C CHECK, FOUND LEFT HORIZONTAL STABILIZER SUPPORT FITTING CRACKED AT STATION XFS72 BETWEEN STRINGER 2 AND FRONT SPAR. REPLACED PER ALL APPLICABLE DATA.Jun 21, 2004 · N41CX · Doug DC862FSDR IXXA060376SSupport Fitting · crackedDURING ROUTINE C CHECK FOUND LEFT HAND HORIZONTAL STABILIZER SUPPORT FITTING CRACKED AT STATION XFS72 BETWEEN STRINGERS 6 AND 7. REPLACED PER ALL APPLICABLE DATA.Jun 17, 2004 · N41CX · Doug DC862FSDR IXXA060373SHousing · crackedDURING ROUTINE C CHECK FOUND LEFT HAND HORIZONTAL STABILIZER LINKAGE HOUSING CRACKED AT STATION XRS218. REPAIRED PER ALL APPLICABLE DATA.Jun 17, 2004 · N41CX · Doug DC862FSDR IXXA060371SSupport · crackedDURING ROUTINE C CHECK FOUND RIGHT HAND HORIZONTAL STABILIZER LOWER SECTION SUPPORT CRACKED AT STATION XFS47. REPAIRED PER ALL APPLICABLE DATA.Jun 17, 2004 · N41CX · Doug DC862FSDR IXXA060366SHousing · crackedDURING ROUTINE C CHECK FOUND LINKAGE HOUSING CRACKED ON LEFT HAND HORIZONTAL STABILIZER AT STATION XRS136. REPLACED PER ALL APPLICABLE DATA.Jun 17, 2004 · N41CX · Doug DC862FSDR IXXA060367SDoubler · bulgedDURING ROUTINE C CHECK FOUND DOUBLER BULGING AND CRACKED ON LEFT HAND HORIZONTAL STABILIZER AT STATION XRS250. REPAIRED PER ALL APPLICABLE DATA.Jun 16, 2004 · N41CX · Doug DC862FSDR IXXA060364SCap · crackedDURING ROUTINE C CHECK FOUND LEFT HAND HORIZONTAL STABILIZER STATION XRS54 TEE CAP CRACKED. REPAIRED PER ALL APPLICABLE DATA.Jun 16, 2004 · N41CX · Doug DC862FSDR IXXA060361SPanel · bulgedDURING ROUTINE C CHECK FOUND LEFT HAND HORIZONTAL STABILIZER TRAILING EDGE LOWER PANEL BETWEEN STATION XE77 TO XE149 BULGED. REPAIRED PER ALL APPLICABLE DATA.Jun 5, 2004 · N41CX · Doug DC862FSDR IXXA060360SPanel · bulgedDURING ROUTINE C CHECK FOUND LEFT HAND HORIZONTAL STABILIZER TRAILING EDGE UPPER PANEL BETWEEN STATION XE221 TO XE272 BULGED AND RIVET SHEARED. REPAIRED PER ALL APPLICABLE DATA.Jun 5, 2004 · N41CX · Doug DC862FSDR 04FDEA01279Structure · corrodedTAIL TANK - NR 28L BARREL NUT BORE CORROSION REMOVAL EXCEEDED LIMIT. COMPLIED AS PER FEDEX EA 1-5510-76711 - STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE REWORK / REPAIR - AD 2003-22-08.May 17, 2004 · N597FE · Doug MD11SDR WVE2004F00004Bushing · lack of lubeLT VERTICAL STABILIZER PIVOT FITTING FOR THE HORIZONTAL STABILIZER HAS BUSHING (PN 601R55310025) MIGRATED AT WL 235.00, LBL 4.10. PROBABLE CAUSE: PIVOT PIN LUBRICATION NOT ADEQUATE. (EA09200401997)Apr 20, 2004 · N408SW · Cndair CL6002B19SDR MALA040333Structure · damagedDURING 4Y/2Y INSPECTION, RIGHT I/B UPPER STAB SPAR FASTENER HOLES FOUND TO BE IRREGULARLY SHAPED. COMPLIED WITH EO AD991921-03 PROCEDURE, FINAL REAMING OF HOLES, STEP 2 E-(1)-(2) 246 IAW MESABA EO AD991921-03. AIRCRAFT RELEASE DATE 4/16/2004.Apr 8, 2004 · N369PX · Saab 340BSDR SWAA040941Fitting · corrodedDURING SCHEDULED D CHECK, FOUND HORIZONTAL STAB RT AND LT, AFT SPAR CLEVIS FWD AND AFT LUGS CORRODED. REPAIRED HORIZONTAL STAB AFT SPAR CLEVIS PER ER.Mar 30, 2004 · N304SW · Boeing 7373H4SDR AUS20040207Bracket · cracked(AUS) HORIZONTAL STABILIZER STEEL BRACKET CRACKED. CRACK LENGTH 10MM(0.393IN).Mar 17, 2004 · Cessna A152SDR 04061303Panel · crackedDURING AIRCRAFT OPERATION THE CREW REPORTED A LOUD THUMPING ON THE RIGHT SIDE NOSE OF THE AIRCRAFT. FLIGHT LANDED UNEVENTFULLY AND PASSENGERS DEPLANED NORMALLY. THE LEFT HAND VERTICAL STABILIZER TO HORIZONTAL STABILIZER FILLET PANEL WAS FOUND CRACKED AND WASMar 1, 2004 · N303UE · Jetair JETSTM4101SDR UPS04M42093Structure · corrodedINSPECTION TYPE:C HORIZONTAL STABILIZER RIGHT NR 24 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF HOLE NR 24 RIGHT REMOVED PER SRM 51-21-01 VOL 2 REV 34. MATERIAL REMOVED 0.060 INCH. BARREL NUT HOLE REPAIREDFeb 21, 2004 · N274UP · Doug MD11FSDR UPS04M42095Structure · corrodedINSPECTION TYPE:C HORIZONTAL STABILIZER RIGHT NR 15 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF HOLE NR 15 RIGHT REMOVED PER SRM 51-21-01 VOL 2 REV 34. MATERIAL REMOVED 0.060 INCH. BARREL NUT HOLE REPAIREDFeb 20, 2004 · N274UP · Doug MD11FSDR UPS04M42094Structure · corrodedINSPECTION TYPE:C HORIZONTAL STABILIZER RIGHT NR 21 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF HOLE NR 21 RIGHT REMOVED PER SRM 51-21-01 VOL 2 REV 34. MATERIAL REMOVED 0.039 INCH. BARREL NUT HOLE REPAIREDFeb 19, 2004 · N274UP · Doug MD11FSDR UPS04M42247Structure · corrodedINSPECTION TYPE:C HORIZONTAL STABILIZER RT NR 25 BARREL NUT HOLE FOUND CORROSION ON BOTTOM , SIDEWALL AND BEARING SURFACE. CORR AT BOTTOM OF NR 25 RT HOLE REMOVED PER SRM51-21-01 VOL II REV 3 4, MATERIAL REMOVED 0.044 INCH WITHIN LIMITS PER EO MD11-5510-19409Feb 17, 2004 · N274UP · Doug MD11F
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