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 2003F00438Hinge Pin · corrodedAT C-CHECK, FOUND HORIZONTAL STAB, RIGHT INNER HINGE PIN, HAS CORROSION ON THREADED END. REMOVED AND ERPLACED RIGHT INNER HINGE PIN. (M)Jan 24, 2003 · N7643U · Boeing 727222SDR 2003F00437Hinge Pin · corrodedAT C-CHECK, FOUND HORIZONTAL STAB, LEFT OUTER HINGE PIN, IS CRACKED AND CORRODED. REMOVED AND REPLACED HORIZONTAL STAB RIGHT OUTER HINGE PIN. (M)Jan 24, 2003 · N7643U · Boeing 727222SDR CA030131005Bracket · cracked(CAN) HORIZONTAL STABILILZER REAR RT REINFORCEMENT ATTACH BRACKET WAS FOUND CRACKED .250 INCH LONG.Jan 24, 2003 · Cessna U206CSDR 03FDEA00019Structure · corrodedLEFT HORIZONTAL STABILIZER UPPER BARREL NUT BORE NR 26L FOUND CORROSION ON BEARING SURFACE AND BORE REAMED BEYOND MAXIMUM OVERSIZE LIMIT IAW EO 1-5510-7-5000 AND SB MD11-55-023.Jan 13, 2003 · N578FE · Doug MD11SDR AALA20021718Attach Angle · corrodedTUL - FOUND RIGHT HORIZ STAB L/E ATTACH ANGLE, UPPER, AFT ANGLE CORROSION AROUND NUTPLATES FOR L/E ATTACH FASTENERS. REMOVED AND REPLACED SUPPORT ASSEMBLY. (M)Dec 2, 2002 · N7083A · Airbus A300B4605RSDR UPS02239938Pin · corrodedINSPECTION TYPE:C PITTING FOUND ON RT STAB INNER PINS. RT STAB INNER PIN REPLACED IAW MM 55-10-01.Nov 16, 2002 · N905UP · Boeing 72751CSDR C2XA02TY162Fitting · chafedDURING A SCHEDULED INSPECTION THE RIGHT HAND HORIZONTAL STAB FAIL SAFE PIN FITTING WAS FOUND TO BE CHAFED. MAINTENANCE ACCOMPLISHED A BLEND-OUT REPAIR IAW EMB GST 3201/02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTINov 2, 2002 · N13975 · Emb EMB145LRSDR C2XA02TY161Fitting · chafedDURING A SCHEDULED INSPECTION THE LEFT HAND HORIZONTAL STAB FAIL SAFE PIN FITTING WAS FOUND TO BE CHAFED. MAINTENANCE ACCOMPLISHED A BLEND-OUT REPAIR IAW EMB GST 3201/02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTIONov 2, 2002 · N13975 · Emb EMB145LRSDR ASAA0210268Retainer · crackedPAE - DURING SCHEDULED C-CHECK, FOUND VERTICAL STABILIZER ACCESS PANEL SEAL DEPRESSOR AT VERTICAL STABILIZER STATION 56.57 CRACKED. REMOVED AND REPLACED SEAL DEPRESSOR PER SRM AND MANUFACTURER DRAWING. (M)Oct 30, 2002 · N743AS · Boeing 737210CSDR C2XA02TY156Fitting · gougedDURING A SCHEDULED INSPECTION THE HORIZONTAL STAB LEFT INBOARD LUG FOR THE MOUNT PIN WAS FOUND TO BE GOUGED. MAINTENANCE POLISHED OUT THE DAMAGED AREA IAW EMBRAER GST 3175/02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPOct 25, 2002 · N13975 · Emb EMB145LRSDR TSAA0253234Structure · corrodedBLENDED THE DAMAGE ON THE LUG. SPOTFACED THE INBOARD AND OUTBOARD SURFACES. OVERSIZED THE TAPERED/ELONGATED HOLE OF THE INBOARD LUG ON THE ORIGINAL CENTERLINE TO OBTAIN A ROUND AND TRUE CONDITION. FABRICATED NEW REPAIR SLEEVE BUSHING TO FIT THE OVERSIZED INOct 18, 2002 · N824AL · Boeing 737282SDR 02FDEA00746Structure · corrodedHORIZ STAB INTERIOR , FOUND BARREL 27TH NUT HOLE AFTER CORROSION BLEND OUT, EXCEEDED SB LIMIT. R&R HORIZ STABILIZER PER EA 1-5510-66415.Oct 18, 2002 · N601FE · Doug MD11SDR 02FDEA00748Structure · corrodedHORIZ STAB INTERIOR, NR 16 RT BARREL NUT HOLE CORRODED. R&R HORIZ STABILIZER PER EA 1-5510-66415.Oct 18, 2002 · N601FE · Doug MD11SDR DL73K021206Web · chafedFOUND ON Q1 LETTER CK RT AND LT INBD BALANCE BOARD PANELS CHAFING THROUGH THE INBD WEBS. REPAIRED PER SRM 51-40-20 AND OPERATION 1000Oct 17, 2002 · N376DL · Boeing 737247SDR ASAA0280375Bracket · crackedOKC - FOUND DURING 30K-CHECK, LEFT HORIZONTAL STABILIZER REAR SPAR CAP COVER INTERNAL BRACKET IS CRACKED. REPLACED BRACKET PER SRM 51-10-2, AND DOUGLAS DWG 9917401. (M)Oct 16, 2002 · N976AS · Doug DC983SDR BJNA021008Angle · crackedLEFT CENTER HORIZONTAL STABILIZER REAR STABILIZER FITTING HAS CRACKED ANGLE STATION 1170, BELOW LEFT HORIZONTAL STABILIZER PIN/AFT. REMOVED CRACKED ANGLE IAW B737 SRM 51-30-2. TRIMMED TO FIT NEW SUPPORT ANGLE IAW B737 SRM 51-30-5, 51-10-1, 51-20-1 FIG 1/2. Oct 15, 2002 · N233TM · Boeing 737282SDR UPS02839829Fitting · crackedINSPECTION TYPE:C2 RIGHT HORIZONTAL STAB LOWER PLANK FITTING IS CRACKED AT XFS 46. REMOVED AND REPLACED FITTING IAW DWG 3701427, AND SRM 51-1-21.Oct 15, 2002 · N779UP · Doug DC871FSDR 02FDEA00743Structure · corrodedHORIZ STAB INTERIOR, FOUND BARREL NUT HOLE NR 35 AFTER CORROSION BLEND OUT, EXCEEDED SB LIMIT. R&R HORIZ STABILIZER PER EA 1-5510-66415.Oct 12, 2002 · N601FE · Doug MD11SDR 02FDEA00710Structure · corrodedHORIZ STAB INT, BARREL NUT HOLE 32R AFTER CORROSION BLEND OUT, EXCEEDED SB LIMIT. R&R HORIZ STAB PER EA 1-5510-66415.Oct 8, 2002 · N601FE · Doug MD11SDR 02FDEA00711Structure · corrodedHORIZ STAB INT, BARREL NUT HOLE NR 26R AFTER CORROSION BLEND OUT, EXCEEDED SB LIMIT. R&R HORIZ STABILIZER PER EA 1-5510-66415.Oct 8, 2002 · N601FE · Doug MD11SDR 02FDEA00713Structure · corrodedHORIZ STAB INT, BARREL NUT HOLE NR 23L AFTER CORROSION BLEND OUT, OUT OF SB LIMIT. R&R HORIZ STABILIZER PER EA 1-5510-66415.Oct 8, 2002 · N601FE · Doug MD11SDR 02FDEA00714Structure · corrodedHORIZ STAB INT BARREL NUT HOLE NR 24R AFTER CORROSION BLEND OUT, EXCEEDED SB LIMIT. R&R HORIZ STABILIZER PER EA 1-5510-66415.Oct 8, 2002 · N601FE · Doug MD11SDR 02FDEA00712Structure · corrodedHORIZ STAB INT, BARREL NUT HOLE NR 20R EXCEEDED SB LIMIT. R&R HORIZ STABILIZER PER 1-5510-66415.Oct 4, 2002 · N601FE · Doug MD11SDR 02FDEA00704Structure · damagedHORIZ STAB INTERIOR, FOUND BARREL NUT HOLE NR 19R BOTTOM SURFACE EXCEEDED LIMIT AS PER SB. R&R HORIZ STAB PER EA 1-5510-66415.Oct 2, 2002 · N601FE · Doug MD11SDR 02FDEA00705Structure · damagedHORIZ STAB INTERIOR, FOUND BARREL NUT HOLE NR 9R BOTTOM SURFACE EXCEEDED LIMIT AS PER SB. R&R HORIZ STAB PER EA 1-5510-66415.Oct 2, 2002 · N601FE · Doug MD11SDR 02FDEA00706Structure · damagedHORIZ STAB EXTERIOR, FOUND BARREL NUT HOLE NR 14R ELONGATED. R&R STAB HORIZ PER EA 1-5510-66415.Oct 2, 2002 · N601FE · Doug MD11SDR 02FDEA00707Structure · damagedHORIZ STAB INTERIOR, FOUND BARREL NUT HOLE NR 14L OUT OF SB LIMIT. R&R HORIZ STAB PER EA 1-5510-66415.Oct 2, 2002 · N601FE · Doug MD11SDR 02FDEA00708Structure · corrodedHORIZ STAB INTERIOR FOUND BARREL NUT HOLE NR 21 L BOTTOM SURFACE LOCAL BLENDOUT CORROSION EXCEEDED LIMIT AS PER SB. R&R HORIZ STAB PER EA 1-5510-66415.Oct 2, 2002 · N601FE · Doug MD11SDR UPS02239773Hinge Pin · corrodedHORIZONTAL STAB HINGE LEFT OUTER PIN HAS EVIDENCE OF PITTING CORROSION ADJACENT TO RELIEF RADIUS. HORIZONTAL STABILIZER HINGE PIN LEFT OUTER REPLACED IAW MM 55-10-01 STEPS 3 AND 4.Sep 24, 2002 · N930UP · Boeing 72722CSDR 02FDEA00672Structure · corrodedAFTER CORROSION REMOVAL ON BARREL NUT HOLE NR 36 RT, BOTTOM SURFACE AND SIDEWALL BLEND OUT EXCEEDED LIMIT AS PER SB MD11-55-023. R&R HORIZ STAB PER EA 1-5510-66415.Sep 23, 2002 · N601FE · Doug MD11SDR 02FDEA00671Structure · corrodedAFTER CORROSION REMOVAL ON BARREL NUT HOLE NR 36 LT, BOTTOM SURFACE BLENDOUT EXCEEDED LIMIT AS PER SB MD11-55-023. R&R HORIZ STABILIZER PER EA 1-5510-66415.Sep 23, 2002 · N601FE · Doug MD11SDR 02FDEA00769Structure · corrodedCORROSION ON HORIZONTAL STABILIZER. R&R HORIZONTAL STABILIZER PER ME 11-55-023.Sep 6, 2002 · N601FE · Doug MD11SDR QXEA0201250Support Fitting · gougedPDX - LEFT HAND FORWARD HORIZONTAL STABILIZER SUPPORT FITTING IS GOUGED BETWEEN HORIZONTAL AND VERTICAL STABILIZERS. REPAIRED IAW RD 8-55-847.Aug 20, 2002 · N363PH · Dhav DHC8202SDR 02FDEA00596Structure · corrodedRUST EMITTING FROM 40 EACH BARREL NUT HOLES ON RT AND LT HORIZ STAB LWR PLANK ATTACHMENT TO CENTER TORQUE BOX. R&R RUSTY BARREL NUTS & CLEANED HOLES MID PLANK AND BOLTS WITH PLI WASHERS PER MM 52-22-02-1.Aug 17, 2002 · N550FE · Doug DC1010SDR COMA0260425Bushing · damagedTHE RIGHT VERTICAL STABILIZER HINGE BUSHING WAS DAMAGED AND REQUIRES REPLACEMENT. REMOVED AND REPLACED BUSHING IAW WVAC EO 601R-55-3359 CRJ AMM 20-26-00-910-803.Jul 15, 2002 · N960CA · Cndair CL6002B19SDR ASAA0280220Fairing · damagedOAK - RIGHT HORIZONTAL STABILIZER UPPER FAIRING WAS DAMAGED DURING LINE MAINTENANCE. TEMP REPAIRED FAIRING WITH CUT OUT PIECE FROM ANOTHER FAIRING AND SPEED TAPE PER EA 5510-01157. (M)Jul 10, 2002 · N972AS · Doug DC983SDR CA020723005Bearing · corroded(CAN) WHEN INSPECTING CONTROL SURFACES, IT WAS NOTICED THAT THE HORIZONTAL STABILATOR HAD AN ABNORMAL FORE / AFT MOVEMENT. UPON DISINSTALLATION, THE HORIZONTAL STAB BUSHINGS AND BEARINGS WERE FOUND TO BE WORN AND THE BOLTS WERE FOUND TO BE CORRODED.Jun 26, 2002 · Beech A24RSDR USAA020243Stiffener · crackedPIT - FOUND STIFFENER ANGLE CRACKED 1.5 INCHES LONG, LEFT HORIZONTAL STAB REAR SPAR ELEVATOR STATION 221.50. NEW STIFFENER REPLACED AND DOUBLER PER SRM 55-10-10 AND EA 74155. (M)Jun 13, 2002 · N406US · Boeing 737401SDR COOSDR02138Beam · corrodedRIGHT AND LEFT HORIZONTAL STABILIZER, TRAILING EDGE, LOWER BEAM CORRODED.Jun 1, 2002 · N1910 · Boeing 72723SDR COOSDR02137Beam · corrodedRIGHT AND LEFT HORIZONTAL STABILIZER, TRAILING EDGE, UPPER BEAM CORRODED.Jun 1, 2002 · N1910 · Boeing 72723SDR COOSDR02110Beam · corrodedLEFT HORIZONTAL STAB TRAILING EDGE BEAM LOWER CHORD AT STAB STA 105 INCHES WITH CORROSION.Jun 1, 2002 · N994AJ · Boeing 727233SDR COOSDR02109Beam · corrodedLEFT HORIZONTAL STAB, TRAILING EDGE BEAM UPPER CHORD AT STAB STA 198 INCHES WITH CORROSION.Jun 1, 2002 · N994AJ · Boeing 727233SDR USAA020188Fitting · corrodedTPA - FOUND FITTING CORRODED .625 INCH, LEFT SIDE HORIZONTAL STAB CENTER SECTION, FRONT SPAR. CORROSION LEVEL 2. REMOVED CORROSION, BLENDED, SPOT FACE, REPAIRED PER SRM 55-10-10, FIG 103 AND EA 94305. (M)May 15, 2002 · N412US · Boeing 737401SDR AUS20020473Fitting · worn(AUS) RT HORIZONTAL STABILISER ATTACHMENT HOLES WORN. HOLES IN STUB SPAR ALSO WORN.May 6, 2002 · Beech 58SDR UPS02238292Beam · corrodedINSPECTION TYPE:C, CORROSION ON LT STAB T/E UPPER BEAM AT STAB STA 155. CORROSION REMOVED IAW SRM 51-10-06 FOUND TO BE OUTSIDE LIMITS HFEC C/O IAW B727 NDTM PT 6 51-00-00 - NDF. REPAIR CARRIED OUT IAW SMRO EO 2002-027-008 UPS ENGINEERING FILE 727-55-20006.May 4, 2002 · N943UP · Boeing 72722CSDR UPS02238291Beam · corrodedINSPECTION TYPE:C CORROSION ON LT STAB T/E UPPER BEAM AT STAB STA 215. CORROSION REMOVED IAW SRM 51-10-06 FOUND TO BE OUTSIDE LIMITS HFEC C/O IAW B727 NDTM PT 6 51-00-00 - NDF. REPAIRED BEAM IAW EO 2002-027-006.May 4, 2002 · N943UP · Boeing 72722CSDR UPS02238290Beam · corrodedINSPECTION TYPE:C CORROSION ON RT STAB T/E BEAM (UPPER) AT STAB STA 205 AND STA 209. CORROSION REMOVED IAW SRM 51-10-06 & FOUND TO BE OUTSIDE LIMITS AFTER CORROSION REMOVAL HFEC CARRIED OUT IAW B727 NDT MANUAL PART 6, 51-00-00 - NDF. AREA ON RT STAB T/E BEAMay 4, 2002 · N943UP · Boeing 72722CSDR USAA020155Fitting · corrodedTPA - FOUND FITTING CORRODED .5 INCH AREA, FORWARD FACE, FORWARD UPPER JOINT CLEVIS, LT SIDE HORIZ STAB. CORROSION LEVEL 2. REMOVED CORROSION, TREATED, PRIMED, INSTALLED FILLER PER SRM 55-10-10 AND EA 94300. (M)Apr 30, 2002 · N418US · Boeing 737401SDR AUS20020316Beam · corroded(AUS) LT HORIZONTAL STABILIZER UPPER TRAILING EDGE BEAM CORRODED IN AREA OF ELEVATOR STA 111.Mar 28, 2002 · Boeing 73733ASDR AUS20020391Fitting · corroded(AUS) HORIZONTAL STABLISER BEARING ATTACHMENT FITTINGS CORRODED. CPCP - LEVEL 2 CORROSION.Mar 23, 2002 · Boeing 727281
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