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 UPS08M53017Structure · corrodedINSPECTION TYPE-1C, CORROSION FOUND IN NR 17 RT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED BUSHING, AND INSTALLED BUSHING IAW E.O. MD1-5510-19409-N AND SAA TRAVELER 80538320001.Jul 11, 2008 · N257UP · Doug MD11FSDR 2008FA0000498Bracket · crackedWHILE CONDUCTING A 100 HOUR INSPECTION ON THE AIRCRAFT, COMPLYING WITH AD80-11-04 (NUTPLATE INSPECTION). UPON INSPECTION, IT WAS FOUND THAT NOT ONLY WAS THERE A CRACKED NUTPLATE, BUT THERE IS ALSO A (1 INCH) CRACK IN THE WELDED BRACKET- THE PART THAT THE NUTPJul 11, 2008 · N66970 · Cessna 152SDR UPS08M53040Structure · corrodedINSPECTION TYPE-1C, CORROSION FOUND IN NR 8 RT BARREL NUT BORE HOLE, REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING IAW E.O. MD11-5510-19409-N.Jul 10, 2008 · N257UP · Doug MD11FSDR UPS08M53039Structure · corrodedINSPECTION TYPE-1C, CORROSION FOUND IN NR 2 RT BARREL NUT BORE HOLE, REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING IAW E.O. MD11-5510-19409-N.Jul 10, 2008 · N257UP · Doug MD11FSDR UPS08M53019Structure · corrodedINSPECTION TYPE-1C, CORROSION FOUND IN NR 11 LT BARREL NUT BORE HOLE REMOVED CORROSION, FABRICATED BUSHING AND INSTALLED BUSHING IAW E.O. MD11-5510-19409-N AND SAA TRAVELER 80538350001.Jul 10, 2008 · N257UP · Doug MD11FSDR UPS08M53018Structure · corrodedINSPECTION TYPE-1C, CORROSION FOUND IN NR 29 RT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED BUSHING, AND INSTALLED BUSHING IAW E.O. MD11-5510-19409-N AND SAA TRAVELER 80538330001.Jul 10, 2008 · N257UP · Doug MD11FSDR UPS08M53015Structure · corrodedINSPECTION TYPE-1C, CORROSION FOUND IN NR 11 RT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED BUSHING AND INSTALLED BUSHING IAW EO MD11-5510-19409-N AND SAA TRAVELER 80538310001.Jul 10, 2008 · N257UP · Doug MD11FSDR UPS08M52927Structure · corrodedINSPECTION TYPE-1C, CORROSION FOUND IN NR 8 LT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED BUSHING AND INSTALLED BUSHING IAW EO, MD11-5510-19409-N AND SAA TRAVELER 80538360001.Jul 10, 2008 · N257UP · Doug MD11FSDR UPS08M52925Structure · corrodedINSPECTION TYPE-1C, CORROSION FOUND IN NR 5 RT BARREL NUT BORE HOLE, REMOVED CORROSION, FABRICATED BUSHING, AND INSTALLED BUSHING IAW EO MD11-5510-19409-N AND SAA TRAVELER 80538290001.Jul 10, 2008 · N257UP · Doug MD11FSDR UPS08M52959Structure · corrodedINSPECTION TYPE-1C, CORROSION FOUND IN NR 36 RT BARREL NUT BORE HOLE AND BOTTOM SURFACE. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING IAW EA 011-5510-01-A1472, EO 5510-30129-A, AND EO 5510-19409-N.Jul 8, 2008 · N257UP · Doug MD11FSDR 2008FA0000454Bracket · crackedHORIZ STAB IB RIBS LT AND RT ROLLER BRACKETS FOUND CRACKED. REPLACED PN 45A21085-003 LT FWD BRACKET. PN 45A21086-003 LT AFT BRACKET, PN 45A21085-004 RT FWD. BRACKET PN 45A21086-004 RT AFT BRACKET WITH IMPROVED PN 128-620021-0001 (LT) AND PN 128-620021-0002 (Jun 30, 2008 · N184AR · Beech 400ASDR UPS08M52861Structure · corrodedINSPECTION TYPE-C, RT HORIZ STAB BARREL NUT BORE NR 35 FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED IAW SRM 51-21-01 VII REV 35. BORE REAM TO 1.178"DIA, REMAINING BLEND OUT 0.095" DEEP, BOTTOM REMAINING BLEND OUT 0.068"DEEP, FOUND EXCEEDING LIMITS Jun 3, 2008 · N296UP · Doug MD11FSDR UPS08M52852Structure · corrodedINSPECTION TYPE-C, RT HORZ STAB BARREL NUT BORE NR 19 FOUND CORRODED EXISTING REPAIR SLEEVE BUSHING REMOVED. BORE SURFACE CLEANED & MEASURE 1.126" DIA, BOTTOM SURFACE CLEANED & MAT'L THK REMAINING 0.082" MIN, FOUND BORE CLEAN HOLE COND * BORE SIZE EXCEEDJun 3, 2008 · N296UP · Doug MD11FSDR UPS08M52858Structure · corrodedINSPECTION TYPE-C, RT HORIZ STAB BARREL NUT BORE NR 22 FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED IAW SRM 51-21-01 VII REV 35. BORE REAM TO 1.067" DIA, REMAINING BLEND OUT 0.040" DEEP, BOTTOM SURFACE REMAINING BLEND OUT 0.055" DEEP, BORE BLEND OUT Jun 2, 2008 · N296UP · Doug MD11FSDR UPS08M52856Structure · corrodedINSPECTION TYPE-C, RT HORIZ STAB BARREL NUT BORE NR 16 FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED IAW SRM 51-21-01 VII REV 35. BORE REAM TO 1.067"DIA, REMAINING BLEND OUT 0.068" DEEP, BOTTOM SURFACE CLEAN & BORE BLEND OUT, EXCEEDED LIMITS IAW EOJun 2, 2008 · N296UP · Doug MD11FSDR UPS08M52851Structure · corrodedINSPECTION TYPE-C, LT HORIZ STAB BARREL NUT BORE NR 22 FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED IAW SRM 51-21-01 VII REV 35. BORE REAM TO 1.067" DIA, REMAINING BLEND OUT 0.015" DEEP, BOTTOM SURFACE CLEANED, BLEND OUT AT SIDEWALL FOUND OUT OF LIMIJun 2, 2008 · N296UP · Doug MD11FSDR UPS08M52855Structure · corrodedINSPECTION TYPE-C, RT HORIZ STAB BARREL NUT BORE NR 31 FOUND CORRODED CORROSION AT BARREL NUT BORE REMOVED IAW SRM 51-21-01 VII REV35.BORE REAM TO 1.162"DIA, REMAINING BLEND OUT AT BOTTOM RADIUS 0.130" DEEP FOUND EXCEEDING EO LIMIT IAW EO MD11-5510-19409M.May 31, 2008 · N296UP · Doug MD11FSDR UPS08M52853Structure · corrodedINSPECTION TYPE-C, RT HORIZ STAB BARREL NUT BORE NR34 FOUND CORRODED EXISTING SLEEVE BUSHING REMOVED & CORROSION AT BARREL NUT BORE REMOVED IAW SRM 51-21-01 VII REV 35. BORE REMAINING BLEND OUT 0.030" DEEP, BOTTOM SURFACE CLEANED, BORE BLEND OUT EXCEEDED May 31, 2008 · N296UP · Doug MD11FSDR UPS08M52850Structure · corrodedINSPECTION TYPE-C, RT HORIZ STAB BARREL NUT BORE NR 28 FOUND CORRODED, CORROSION AT BARREL NUT BORE REMOVED IAW SRM 51-21-01 VII REV35. BORE REAMED TO 1.178" DIA, REMAINING BLEND OUT 0.060", BOTTOM REMAINING 0.070" DEEP. BORE BLEND OUT FOUND EXCEEDING LIMIMay 30, 2008 · N296UP · Doug MD11FSDR UPS08M52844Structure · corrodedINSPECTION TYPE-C, RT HORIZ STAB BARREL NUT BORE NR 8 FOUND CORRODED CORROSION REMOVED AT BARREL NUT BORE IAW SRM 51-21-01 VII REV 35. BORE REAM TO 0.988" DIA REMAINING BLEND OUT 0.095" DEEP, BOTTOM SURFACE CLEANED. BORE BLEND OUT FOUND EXCEEDING LIMITS May 27, 2008 · N296UP · Doug MD11FSDR UPS08M52854Structure · corrodedINSPECTION TYPE-C, RT HORIZ STAB BARREL NUT BORE NR17 FOUND CORRODED. CORROSION REMOVED AT BARREL NUT BORE IAW SRM 51-21-01 VII REV35. BORE REAM TO 1.067"DIA, REMAINING BLEND OUT 0.050", BOTTOM REMAINING, BLEND OUT 0.045" DEEP, FOUND EXCEEDING LIMIT IAW May 26, 2008 · N296UP · Doug MD11FSDR UPS08M52845Structure · corrodedINSPECTION TYPE-C, LT HORIZ STAB BARREL NUT BORE NR33 FOUND CORRODED CORROSION AT BARREL NUT BORE REMOVED IAW SRM 51-21-01 VII REV 35. BORE REAM TO 1.178" DIA, REMAINING SIDEWALL BLEND OUT 0.020" DEEP, BOTTOM SURFACE REMAINING BLEND OUT 0.065" DEEP, BLENMay 24, 2008 · N296UP · Doug MD11FSDR UPS08M52842Structure · corrodedINSPECTION TYPE-C, LT HORIZ STAB BARREL NUT BORE NR17 FOUND CORRODED. CORROSION AT BARREL BORE REMOVED IAW SRM 51-21-01 VII REV 35. BORE REAM TO 1.067" DIA REMAINING BLEND OUT 0.035", BOTTOM SURFACE CLEANED & BORE FOUND OUT OF LIMIT IAW EO MD11-5510-194May 24, 2008 · N296UP · Doug MD11FSDR UPS08M52848Structure · corrodedINSPECTION TYPE-C, RT HORIZ STAB BARREL NUT BORE NR 36 FOUND CORRODED CORROSION AT BORE NR36 RT REMOVED IAW SRM 51-21-01 VII REV 35. BORE REAM TO 2.538" DIA, REMAINING BLEND OUT 0.098" DEEP, BOTTOM REMAINING BLEND OUT 0.150" DEEP, BORE EXCEEDED LIMITS IAMay 23, 2008 · N296UP · Doug MD11FSDR UPS08M52857Structure · corrodedINSPECTION TYPE-C, LT HORIZ STAB BARREL NUT BORE NR30 FOUND CORRODED. EXISTING REPAIR BUCKET BUSHING REMOVED IAW EO MD11-5510-19409M. MINOR CORROSION AT BORE REMOVED IAW SRM 51-21-01 VII REV 35. BOTTOM WAS BORED THRU & BORE MEASURED TO 1.255"DIA, REMAINMay 18, 2008 · N296UP · Doug MD11FSDR UPS08M52849Structure · corrodedINSPECTION TYPE-C, RT HORIZONTAL STABILIZER BARREL NUT BORE NR30 FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED IAW SRM 51-21-01 VII REV 35. BORE REAM TO 1.178" DIA REMAINING BLEND OUT 0.040" DEEP, BORE BLEND OUT FOUND EXCEEDING LIMITS IAW EO MD11-5510May 18, 2008 · N296UP · Doug MD11FSDR UPS08M52847Structure · corrodedINSPECTION TYPE-C, RT HORIZONTAL STABILIZER BARREL NUT BORE NR27 FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED IAW SRM 51-21-01 VII REV 35.BORE REAM TO 1.178" DIA,REMAINING BLEND OUT 0.025" DEEP, BOTTOM REMAINING BLEND OUT 0.055" DEEP. BORE BLEND OUTMay 18, 2008 · N296UP · Doug MD11FSDR UPS08M52860Structure · corrodedINSPECTION TYPE-C, RT HORIZ STAB BARREL NUT BORE NR 21 FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED IAW SRM 51-21-01 REV 35. BORE REAM TO 1.067"DIA, REMAINING BLEND OUT 0.083" DEEP, BOTTOM REMAINING BLEND OUT 0.045", BORE BLEND OUT FOUND EXCEEDINGMay 17, 2008 · N296UP · Doug MD11FSDR UPS08M52859Structure · corrodedINSPECTION TYPE-C, RT HORZ STAB BARREL NUT BORE NR 24 FOUND CORRODED CORROSION AT BARREL NUT BORE REMOVED IAW SRM 51-21-01 VII REV 35. BORE REAM TO 1.067"DIA, REMAINING BLEND OUT 0.040" DIA, BOTTOM REMAINING BLEND OUT 0.060" DEEP, BORE FOUND BLEND OUT EXCEMay 17, 2008 · N296UP · Doug MD11FSDR UPS08M52846Structure · corrodedINSPECTION TYPE-C, RT HORIZ STAB BARREL NUT BORE NR1 FOUND CORRODED EXISTING SLEEVE BUSHING REMOVED IAW EO MD11-5510-19409M. CORROSION AT BORE REMOVED IAW SRM 51-21-01 VII REV 35. BORE REAM TO 1.549" DIA, REMAINING BLEND OUT 0.050" DEEP, BOTTOM SURFACE CLMay 17, 2008 · N296UP · Doug MD11FSDR MALA080103Counterweight · looseRT HORIZONTAL STAB FOUND ANTI-OSCILLATION FIXTURE LOOSE AND END RIB MOUNTING HOLE FIXTURE DAMAGED. THE RT HORIZONTAL STAB OUTBD RIB AT HS 174.95 WAS FOUND TO HAVE FRETTING DAMAGE ON THE INBD AND OUTBD FACES DUE TO THE COUNTERWEIGHT BOX WORKING LOOSE. THE COUMay 16, 2008 · N442XJ · Saab 340BSDR UPS08M52843Structure · corrodedINSPECTION TYPE-C, RT HORIZ STAB BARREL NUT BORE NR 09 FOUND CORRODED EXISTING REPAIR SLEEVE BUSHING REMOVED IAW EO MD11-5510-19409M. BARREL NUT BORE SURFACE CLEANED & MEASURED 1.065" DIA,BOTTOM SURFACE CLEANED & MINIMUM THK MEASURED 0.122" THICK, BORE SIMay 15, 2008 · N296UP · Doug MD11FSDR 08FDEA01581Panel · delaminatedPANEL 344 EP DELAMINATED. REPAIRED PANEL 344 EP BY REMOVING THE DAMAGE; CLEANING; CLEANING THE AREA, POTTING REPAIR AND APPLYING A FIBERGLASS WET LAY UP REPAIR IAW SRM 51-77-12 PARA 2-A (2) FIG 202 AND SRM 51-77-10 PARA 3. RESTORED SURFACE REPAIR IAW SRM Apr 25, 2008 · N661FE · Airbus A300F4605RSDR A6WA200840327Diaphragm · missingSTABILIZER DRAG ANGLE DIAPHRAGM CLOTH MISSING. (M) REPAIRED IAW REO 601R-55-32-075 REV E.Apr 10, 2008 · N404AW · Cndair CL6002B19SDR HALA0800505Structure · damagedLIGHTNING STRIKE ON LT HORIZ STAB O/B TIP T/E BY STATIC WICK. OK TO CONTINUE PER M105-596086.Apr 5, 2008 · N596HA · Boeing 767332SDR CO1Y200800002Structure · corrodedAT HORIZONTAL STABILIZER CTR SECTION, FOUND CORROSION INSIDE BARREL NUT HOLE NR 36 LT HORIZ STAB.Mar 27, 2008 · N725BC · Doug MD11FSDR 08FDEA01104Fairing · delaminatedLT HORIZONTAL STABILIZER FWD APRON IS TORN. REPLACED NEW APRON FAIRING ON N00181.Mar 21, 2008 · N425FE · Airbus A310203SDR 08FDEA01701Structure · damagedHORIZONTAL STAB, UPPER APRON RT SIDE DAMAGED RT UPPER RT SIDE WAS REPAIRED IAW FEDEX EA 6-5510-117324.Mar 18, 2008 · N724FD · Airbus A300B4622RSDR 08FDEA01010Access Panel · dentedEMPENNAGE, LT INLET DUCT ACCESS PANEL 363 GL IS DENTED REPAIRED DENT DAMAGES ON LT LOWER VERT STAB FAIRING PNL 363 GL BY REMOVING DAMAGED AREAS, HOT BONDING SKIN PLUGS, DOUBLERS, AND FILL AND FAIR, AND REFINISHING IAW DC/MD-10 SRMS 55-33-01 VOL III, 51-71- 00Mar 18, 2008 · N384FE · Doug MD1010FSDR 08FDEA00819Attach Angle · cracked2ND INBD LEADING EDGE SECTION ON THE RT HORIZONTAL STABILIZER; "UPPER OUTBD ATTACH ANGLE" IS CRACKED. REMOVED CRACKED ANGLE IAW SRM 51-31-01 VOL II PG 1. FORMED NEW ANGEL IAW DWG ALC 07052 REV G. LOCATED; DRILLED & DEBURRED NEW ANGLE IAW SRM 51-31-01 VOL II PMar 10, 2008 · N684FE · Airbus A300F4605RSDR 08FDEA00818Tee Fitting · cracked2ND FROM INBD LEADING EDGE SECTION AT THE RT HORIZONTAL STABILIZER; "UPPER OUTBD ATTACH ANGLE" IS CRACKED. REMOVED RACKED TEE ANGLE IAW SRM 51-31-01 VOL II PG 1. FORMED NEW TEE CAP IAW DWG ALC 07052 REV G. LOCATED, DRILLED & DEBURRED NEW TEE CAP IAW SRM 51-Mar 10, 2008 · N384FE · Doug MD1010FSDR 08FDEA00784Tip Cap · erodedLT HORIZONTAL STABILIZER TIP IS ERODED AT THE LOWER L/E. REPAIRED LT HORIZONTAL STAB TIP BY REMOVING PREVIOUS REPAIR AND APPLING A WET LAY-UP FIBERGLASS REPAIR AND REFINISHING AREA IAW SRM 55-14-11.Mar 7, 2008 · N425FE · Airbus A310203SDR 08FDEA00780Tip Cap · damagedRT HORIZONTAL STABILIZER TIP LOWER L/E IS ERODING BEHIND THE ANTI-EROSION STRIP. REMOVED DAMAGE, VERIFIED MAT I.D. APPLIED LAYUP & CURED, RESTORED FINISH IAW 55-14-11.Mar 7, 2008 · N425FE · Airbus A310203SDR 08FDEA00755Bridge · corrodedLT HORZIONTAL STABILIZER TIP BRIDGING STRIP CORRODED UNDER THE NUTPLATES. REMOVED THE CORROSION REF SRM 51-74-10; PARA 5. FOUND TO BE WITHIN LIMITS IAW SRM 55-10-00 TABLE 101. ALODINED REF SRM 51-21-10, PARA 5. PRIMED REF SRM 51-23-10; PG 1. INSTALLED NMar 6, 2008 · N425FE · Airbus A310203SDR 08FDEA00717Fairing · crackedRT HORIZONTAL STABILIZER UPPER APRON FAIRING IS CRACKED AND DELAMINATED IN SEVERAL PLACES. FABRICATED DOUBLER IAW SRM 55-15-11. REMOVED DAMAGED SECTION IAW SRM 55-15-11 FIG 201. INSTALLED DOUBLER IAW SRM 55-15-11 PGS 219/220. INSTALL SILICONE DOUBLER AND REMar 5, 2008 · N425FE · Airbus A310203SDR 08FDEA00715Fairing · debondedLT HORIZONTAL STABILIZER LOWER APRON FAIRING IS DISBONDED. RE-APPLIED ADHESIVE PER SRM 55-15-11 PARAGRAPH 5 SECTIONS H & I TO DISBONDED SILICONE MATERIAL.Mar 5, 2008 · N425FE · Airbus A310203SDR 08FDEA00714Fairing · delaminatedLT HORIZONTAL STABILIZER FWD APRON FAIRING IS DELAMINATED. INSTALLED NEW APRON FAIRING. MINOR REPAIR.Mar 5, 2008 · N425FE · Airbus A310203SDR 08FDEA00713Fairing · crackedRT HORIZONTAL STABILIZER FWD APRON FAIRING BLADES ARE CRACKED. REMOVED THE DAMAGED SECTION IAW SRM 15-15-11 PGS 219 & 220. FABRICATED DOUBLER PLATE IAW SRM 15-15-11 PG 225. INSTALLED DOUBLER IAW SRM 15-15-11 PARA 5-B (4).Mar 5, 2008 · N425FE · Airbus A310203SDR DJFA2008022Support Bracket · crackedDURING A SCHEDULED MAINT VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSP OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE RT ROLLER BRACKET WAS FOUND CRACKED. DETAILED INSP INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COMMUNIQUE' NR 70.Mar 2, 2008 · N751TA · Beech 400ASDR DJFA2008021Support Bracket · crackedDURING A SCHEDULED MAINT VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSP OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE RT ROLLER BRACKETS WERE FOUND CRACKED. DETAILED INSP INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COMMUNIQUE' NR 7Mar 1, 2008 · N449LX · Beech 400A
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