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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR 05FDEA00898Structure · corrodedRT HORIZONTAL STABILIZER UPPER BARREL NUT NR 13 HAS BORE CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-78133.SDR 05FDEA00897Structure · corrodedRT HORIZONTAL STABILIZER UPPER BARREL NUT NR 11 HAS BORE CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-78133.SDR 05FDEA00892Structure · corrodedSTABILIZERS - HORIZONTAL STABILIZER BARREL NUT BORES, CORROSION REMOVAL, COMPLY WITH EA 1-5510-71839. COMPLIED WITH EA 1-5510-71839.SDR 05FDEA00891Structure · corrodedSTABILIZERS - HORIZONTAL STABILIZER BARREL NUT BORES, CORROSION REMOVAL COMPLY WITH EA 1-5510-71838. COMPLIED WITH EA 1-5510-71838.SDR 05FDEA00890Structure · corrodedRT HORIZONTAL STABILIZER UPPER BARREL NUT NR 23 HAS BORE CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-78133.SDR 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.SDR 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.SDR 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.SDR DXTA200500661Structure · bird strikeBIRD STRIKE ON TAKEOFF. DAMAGE TO RIGHT HORIZONTAL STAB APPROX 8 INCHES WIDE & 2 INCHES DEEP.SDR 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.SDR 05FDEA00771Skin · corrodedRT HORIZONTAL STABILIZER UPPER BARREL NUT NR 28 HAS BORE CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-78133.SDR 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)SDR 2005UALA00236Skin · dentedFOUND DENT IN HORIZONTAL STAB RT SIDE ABOUT 2 FEET IN FROM TIP. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER REPAIR.SDR 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)SDR 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 POSITISDR 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 HSDR 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 SCRSDR LCQ36Fitting · corrodedHORIZONTAL STABILIZER LT MOUNT LUG FITTING FOR PIVOT BEARING O/B FACE HAS CORROSION. S/O 152051, OPS 29688, ZONE 2A-24.SDR SWAA050027Fitting · crackedDURING SCHEDULED 1/2D CHECK, FOUND HORIZONTAL STAB CENTER SECTION UPPER FITTING AND THRUST BEAM, CRACKED. REMOVED AND REPLACED FITTING PER MM.SDR 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.SDR 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)SDR 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 PORTSDR 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.SDR SWIA200414192Fitting · corrodedHORIZONTAL STAB ANTI-ROTATION FITTING CORRODED, ITEM FOUND AT C-CHECK INSPECTION. HORIZONTAL STAB ANTI-ROTATION FITTING REPLACED IAW SB 601R-55-007.SDR 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.SDR 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.SDR GLBA20030753Web · crackedIN PANEL 332 ATC WHERE DE-ICE LINE GOES THROUGH METAL CRACKED AROUND GROMMET ( FWD WEB). REPAIRED HORIZ MAIN SPAR WEB.SDR 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 SDR 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.SDR 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. SDR IXXA060385SBushing · corrodedDURING ROUTINE C CHECK, FOUND LEFT HORIZONTAL STABILIZER ELEVATOR SUPPORT BUSHING CORRODED AT STATION XE 140. REPAIRED PER ALL APPLICABLE DATA.SDR 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.SDR 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.SDR IXXA060373SHousing · crackedDURING ROUTINE C CHECK FOUND LEFT HAND HORIZONTAL STABILIZER LINKAGE HOUSING CRACKED AT STATION XRS218. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060371SSupport · crackedDURING ROUTINE C CHECK FOUND RIGHT HAND HORIZONTAL STABILIZER LOWER SECTION SUPPORT CRACKED AT STATION XFS47. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060366SHousing · crackedDURING ROUTINE C CHECK FOUND LINKAGE HOUSING CRACKED ON LEFT HAND HORIZONTAL STABILIZER AT STATION XRS136. REPLACED PER ALL APPLICABLE DATA.SDR IXXA060367SDoubler · bulgedDURING ROUTINE C CHECK FOUND DOUBLER BULGING AND CRACKED ON LEFT HAND HORIZONTAL STABILIZER AT STATION XRS250. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060364SCap · crackedDURING ROUTINE C CHECK FOUND LEFT HAND HORIZONTAL STABILIZER STATION XRS54 TEE CAP CRACKED. REPAIRED PER ALL APPLICABLE DATA.SDR 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.SDR 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.SDR 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.SDR 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)SDR 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.SDR 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.SDR AUS20040207Bracket · cracked(AUS) HORIZONTAL STABILIZER STEEL BRACKET CRACKED. CRACK LENGTH 10MM(0.393IN).SDR 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 WASSDR 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 REPAIREDSDR 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 REPAIREDSDR 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 REPAIREDSDR 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 MD11-5510-19409
Back to JASC 5514