JASC 5550

Service difficulty reports · 66

Reports filed under 5550 · Empennage Flight Control Surfaces, Attach Fittings, newest first.

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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 = '5550'
  ORDER BY difficulty_date DESC"

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SDR DALA2024120411445Bushing · corrodedSHIP 3136 CORROSION ON BUSH LOCATED AT ELEVATOR HINGE FITTING #3 I/B AND O/B LUG LH HORIZONTAL STABILIZER (2 EA). CORRECTIVE ACTION: REPLACED BUSHINGS (2 EA) ON HINGE #3 AT L/H ELEVATOR AS PER A319 SRM 55-26-41-300-004. (0681477)Nov 27, 2024 · N336NB · Airbus A319114SDR DALA2024120411444Bushing · corrodedSHIP 3136 CORROSION ON BUSH LOCATED AT ELEVATOR HINGE FITTING #1 I/B AND O/B LUG LH HORIZONTAL STABILIZER (2 EA). CORRECTIVE ACTION: REPLACED BUSHINGS (2 EA) ON HINGE #1 AT L/H ELEVATOR AS PER A319 SRM 55-26-41-300-004. (0681458)Nov 27, 2024 · N336NB · Airbus A319114SDR VNAA202304270015Hinge Fitting · corrodedCORROSION ON LOWER RUDDER HINGE AT REAR SPAR OF VERTICAL STABILIZERMar 16, 2023 · N619NN · Cndair CL6002D24SDR IPXA2022030479714Fitting · noneINSPECTION TYPE:1CLH HORIZONTAL STAB ELEVATOR #3 ACTUATOR HINGE SUPPORT FITTING IS CHAFE AT STA XE=122.REPAIRED CHAFED HINGE SUPPORT FITTING IAW VT-SAA EA 011-5510-01-A9501 REV I/R AND UPS EO MD11-5550-83032-A (MINOR).Feb 23, 2022 · N278UP · Doug MD11FSDR DALA2021121607800None · noneSHIP 3257 CORROSION ON BUSHING (1EA) ON OUTBOARD ACTUATOR FITTING INBOARD LUG RH ELEVATOR. CORRECTIVE ACTION: REPAIRED BORE AND REPLACED BUSHING (1EA) OF IB LUG ON OB ACTUATOR FITTING ON RH ELEVATOR AS PER A320 SRM 55-26-47. (2050657)Dec 13, 2021 · N357NW · Airbus A320212SDR DALA2021121607799None · noneSHIP 3257 CORROSION ATTACH FITTING ELEVATOR ACTUATOR INBOARD SIDE INBOARD ACTUATOR ON RH HORIZONTAL STABILIZER. CORRECTIVE ACTION: REPAIRED BORE AND REPLACED BUSHING (1EA) OF IB LUG ON IB ACTUATOR FITTING OF RH ELEVATOR AS PER A320 SRM 55-26-47. (2050646)Dec 13, 2021 · N357NW · Airbus A320212SDR DALA2021121607798None · noneSHIP 3257 CORROSION ATTACH FITTING ELEVATOR ACTUATOR OUTBOARD ACTUATOR INBOARD SIDE ON LH HORIZONTAL STABILIZER. CORRECTIVE ACTION: REPAIRED BORE AND REPLACED BUSHING (1EA) OF I/B LUG ON OB ACTUATOR FITTING OF LH ELEVATOR AS PER A320 SRM 55-26-47. (2050630)Dec 13, 2021 · N357NW · Airbus A320212SDR FDEA201205181858Intercostal · crackedNR 2 ENGINE AIR INTAKE INSIDE PANEL 363PL FOUND WIRE CUT-OUT INTERCOSTAL CRACKED. CARRIED OUT REPAIR IAW SRM 55-30-02, FIG 201. REPAIR 2 REV 49. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.May 18, 2012 · N612FE · Doug MD11FSDR IPXA2M73978Fitting · wornINSPECTION TYPE: 4C, ONE SHEARED FASTENER ON FWD SIDE LOWER FASTENER OF THE NR 4 BANJO FITTING LT SIDE. REPAIRED VERT STAB AFT SPAR NR 4 BANJO FITTING LT SIDE REF EO MD11-5530-46641-A APPX C AND E.May 10, 2012 · N290UP · Doug MD11FSDR IPXA2M73977Fitting · wornINSPECTION TYPE: 4C, ONE LOOSE FASTENER ON FWD SIDE LOWER FASTENER OF THE NR 4 BANJO FITTING RT SIDE. REPAIRED VERTICAL STAB AFT SPAR NR 4 BANJO FITTING RT SIDE, REF EO MD11-5530-46641-A APPX B AND D.May 10, 2012 · N290UP · Doug MD11FSDR C2XA09SH177Bracket · damagedSHV - DURING C-CHECK, RUDDER 2 UPPER ATTACHMENT BRACKET HAS MIGRATED HAT BUSHING. REMOVED AND REPLACED RUDDER 2 UPPER HINGE BRACKET IAW SRM 55-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Jun 29, 2009 · N12540 · Emb EMB145LRSDR 08FDEA04781Support Fitting · crackedEMPENNAGE, AFT FUSELAGE COMPARTMENT PRESSURE BULKHEAD UPPER AFT SURFACE QUANTITY 01 SUPPORT FITTING AT STATION 2007, X=-31.930 FOUND CRACKED.Nov 7, 2008 · N593FE · Doug MD11FSDR DLM90080204Plate · corrodedDURING HMV THE RT VERTICAL-TO-HORIZONTAL STABILIZER INBOARD AND OUTBOARD HINGE PLATES WERE FOUND WITH CORROSION IN THE BORES. A REPAIR WAS MADE AND APPROVED VIA FAA FORM 8100-9.Feb 12, 2008 · N911DA · Doug MD9030SDR IXXA07SMN271SAttach Angle · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND FUSELAGE TO STABILIZER LEFT ATTACH ANGLE SHOWS CORROSION AT STATION 1754.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGES AREA. FABRICATED ANGLE. PERFORMED HEAT TREATMENT TO ANGLE. CLEANED, TREATED ANDNov 16, 2007 · N604BX · Doug DC873FSDR AMTA200600268Bearing · corrodedDURING THE INSPECTION OF THE LT HORIZONTAL STABILIZER PIVOT BEARING INSPECTION, FOUND THE FOLLOWING ITEMS CORRODED, PIVOT BEARING, OUTER PIN, BEARING RETAINER NUT AND FITTING HOUSING. REPLACED THE PIVOT BEARING, OUTER PIN, BEARING RETAINER NUT AND FITTING HOUApr 3, 2006 · N163AT · Lkheed 10113853SDR AMTA200600267Bearing · corrodedDURING RT HORIZONTAL STAB PIVOT BEARING INSPECTION FOUND THE FOLLOWING ITEMS CORRODED. PIVOT BEARING, OUTER PIN, BEARING RETAINER NUT AND FITTING HOUSING. REPLACED PIVOT BEARING, OUTER PIN, BEARING RETAINER NUT AND FITTING HOUSING IAW AMM. FREEPLAY INSPECTIApr 3, 2006 · N163AT · Lkheed 10113853SDR 06FDEA0807Fitting · crackedEMPENNAGE, FORWARD UPPER DOG HOUSE ENTRANCE, CUT OUT EDGE FOUND CRACKED CORRECTIVE ACTION: SNRM NO.: N00958 - EMPENNAGE, FORWARD UPPER DOG HOUSE ENTRANCE, CUT OUT EDGE CRACKED AREA REPAIRED AS PER SRM 53-00-01 VOLUME I, FIGURE 5. REPAIR CLASSIFIED AS Feb 22, 2006 · N585FE · Doug MD11SDR 06FDEA0370Support Fitting · unknownCOMPLY WITH EO 7-5550-7-2302E SECTION 4B - RUDDER CENTER HINGE SUPPORT FITTING REPLACEMENT ON LOWER RUDDER. REPLACED HINGE SUPPORT FITTING PER E.O. 7-5550-7-2302E.Jan 24, 2006 · N490FE · Boeing 727200SDR MALA040625Skin · dentedDURING 4Y/2Y INSPECTION IN BNA, NOTED 7 DENTS IN LT UPPER STAB SKIN. FIVE ARE WITHIN LIMITS PER THE SRM & 2 WERE DELAMINATED AND REPAIRED PER EO S55017.Oct 27, 2004 · N27XJ · Saab SF340ASDR 2004FA0000230Sleeve · looseTHE SLEEVE ON THE RUDDER HINGE PIN CAME LOOSE FROM ITS LOCTITED POSITION ON THE PIN AND WORKED UP INTO THE CAVITY ABOVE THE BEARING ON THE FIN. RUDDER HAD CONSIDERABLE PLAY AT THE TOP.Feb 20, 2004 · N922AF · Diamon DA20C1SDR DL73S040175Attach Fitting · corrodedCORROSION WAS NOTED ON THE VERT STAB ATTACH LUGS, ON THE AFT FACE OF THE NR 6 FIN LUG. CORROSION REMOVED AND LUG REWORKED PER ERA 386225-14.Feb 19, 2004 · N239WA · Boeing 737247SDR DL73S040104Attach Fitting · corrodedNUMEROUS ATTACHMENT FITTING LUGS ON THE HORIZ STAB TO FUSELAGE JOINT REQUIRED MACHINING BEYOND PUBLISHED LIMITS IN ORDER TO REMOVE CORROSION. CORROSION WAS REMOVED AND LUGS REWORKED IAW ERA 386108-14AD.Jan 28, 2004 · N319DL · Boeing 737232SDR DL73S040103Fitting · corrodedDURING ACCOMPLISHMENT OF 03-085220-03 CORROSION WAS NOTED ON THE TWO VERT STAB FIN LUGS. ADDITIONALLY, TWO FUSELAGE CLEVIS LUGS WERE NOTED AS HAVING LUG THICKNESSES BELOW THAT ALLOWED BY 03-085220-03. CORROSION REMOVED AND LUGS/CLEVISES REWORKED PER ERA 3860Jan 28, 2004 · N242WA · Boeing 737247SDR N136FE0401Hinge · crackedDURING SERVICE CHECK, FOUR CRACKS WERE FOUND ON THE NR 7 GROUND SPOILER SUPPORT HINGE. HINGE REPLACED WITH NEW PART. ALL HINGES INSPECTED FOR CRACKS, NO FAULTS FOUND.Jan 13, 2004 · N136 · Boeing 72725CSDR C2XA02TY191Bracket · gougedTYS, During a scheduled inspection the left hand horizontal stab. actuator mounting bracket was found gouged. Maintenance removed and replaced the fitting I/A/W-EMB-135/145-SRM-51-40-02, CMP-51-21-04, 05 and 06. The repair was satisfactory and the aircraft wilDec 29, 2002 · N17521 · Emb EMB135LRSDR CSA2002F00001Pivot Assy · crackedUSING VISABLE DYE PENTRANT INSPECTION, FOUND CRACKS IN STRUCTURAL WEBBING OF PIVOT POINT EXTENSIONS OF BOTH LEFT AND RIGHT HAND BRACKETS. CRACK ON LEFT BRACKET MEASURED APPROXIMATELY .5 INCHES. CRACK IN RIGHT BRACKET EXTENDED ENTIRE LENGTH OF WEB. TOTAL TIMAug 27, 2002 · N995SB · Beech C99SDR USAA020206Angle · crackedPIT - FOUND DRAG ANGLE CRACKED .25 INCH, SECT 48 DRAG ANGLE LIGHT SIDE 10 INCH BEHIND ATTACH LUG. REPAIRED FILLER AND STRAPS ON OUTSIDE AND INSIDE OF DRAG ANGLE PER TYPICAL REPAIR 53-80-03. (M)Apr 17, 2002 · N373US · Boeing 7373B7SDR 2002FA0000377Fitting · malfunctionedLOOKED AT RUDDERVATORS MOVEMENT, THIS FITTING WAS MOVING, CALLED MANUFACTURER FOR INFORMATION ON THIS FITTING.Mar 2, 2002 · N5208C · Beech B35SDR CA011029008Hinge · corroded(CAN) WHILE PERFORMING AN ANNUAL INSPECTION ON THIS AIRCRAFT, EXCESSIVE MOVEMENT WAS NOTED FROM THE OUTBOARD AND CENTRE HINGE BEARINGS FOR THE R/H ELEVATOR. WHEN THE HINGE SUPPORTS WERE DISMANTLED TO REPLACE THE BEARINGS, CORROSION WAS FOUND ON BOTH HALVES OF Sep 15, 2001 · Cessna 208SDR USAASB01234Bolt · wornDCA - FLT 360 - ON CLIMB-OUT FROM DCA, EN ROUTE TO ROC, CREW FELT A RUMBLE/AIRFRAME VIBRATION THROUGHOUT THE CABIN. DUE TO PREVIOUS FILGHT SEGMENT EXPERIENCING THE SAME PROBLEM, FLIGHT RETURNED TO FIELD AT DCA. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMEAug 18, 2001 · N351US · Boeing 737301SDR CA011029012Hinge · cracked(CAN) DURING 100 HOUR INSPECTION FOUND LT OUTBOARD ELEVATOR BEARING LOOSE. REMOVED LT ELEVATOR TO CHANGE BEARING. WITH ELEVATOR REMOVED, FOUND LT OUTBOARD HINGE ASSEMBLY TO BE CORRODED AND CRACKED WHERE BEARING IS INSTALLED.Aug 2, 2001 · Cessna 180JSDR C2XA011A007Bushing · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT AND LEFT HORIZONTAL STABILIZER PLAIN BUSHINGS WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PLAIN BUSHINGS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Dec 30, 2000 · N15941 · Emb EMB145SDR C2XA011A006Bushing · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT AND LEFT HORIZONTAL STABILIZER FLANGED BUSHINGS WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLANGED BUSHINGS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Dec 30, 2000 · N15941 · Emb EMB145SDR AALA20010062Hinge · corrodedTUL - FOUND VERTICAL STABILIZER HINGE LUGS AND SPREADER HAVE PITTING, CORROSION IN AND AROUND BORES. INSTALLED NEW LUG PLATES AND SPREADER PER SRM 55-02 PAGE 68. (M)Dec 19, 2000 · N3507A · Doug DC982SDR DL73K002264Fitting · corrodedTHE VERTICAL STABILIZER ATTACHMENT LUGS WERE FOUND CORRODED AT HMV. ERA 396368-14 REMOVES CORROSION FROM THE BORES AND FACES OF THE LUGS AND REINSTALLS THE BUSHING AND SLEEVES.Nov 20, 2000 · N310DA · Boeing 737232SDR DL73K002258Fitting · corrodedCORROSION WAS REMOVED FROM THE HORIZONTAL STABILIZER ATTACH LUGS FROM THE BORE AND FACE. ERA 396375-14 REPAIRED THE AREA AT HMV.Nov 20, 2000 · N310DA · Boeing 737232SDR USAA002115Clevis · corrodedPIT - FOUND CLEVIS LUG CORRODED .014 INCH DEEPEST AREA, RIGHT HORIZ STAB CENTER SECTION BOTTOM FORWARD CLEVIS BORE. REAMED, SPOTFACED AND CHAMFERED CLEVIS LUGS WITHIN LIMITS IN SRM 55-10-10. OVERSIZE BUSHINGS MANUFACTURED. (M)Oct 24, 2000 · N518AU · Boeing 7373B7SDR USAA002116Clevis · corrodedPIT - FOUND CLEVIS LUG CORRODED .018 DEEPEST AREA, RIGHT HORIZONTAL STAB CENTER SECTION TOP FORWARD CLEVIS BORE. REAMED, SPOTFACED AND CHAMFERED CLEVIS LUGS WITHIN LIMITS IN SRM 55-10-10. OVERSIZE BUSHINGS MANUF. (M)Oct 24, 2000 · N518AU · Boeing 7373B7SDR USAA002117Clevis · corrodedPIT - FOUND CLEVIS LUG CORRODED .004 INCH DEEPEST AREA, RIGHT HORIZ STAB CENTER SECTION TOP AFT CLEVIS BORE. REAMED, SPOTFACED AND CHAMFERED CLEVIS LUG WITHIN LIMITS IN SRM 55-10-10. OVERSIZE BUSHINGS MANUFACTURE. (M)Oct 24, 2000 · N518AU · Boeing 7373B7SDR DL73K002055Fitting · corrodedCORROSION WAS FOUND ON MULTIPLE LUGS ON THE VERTICAL STABILIZER ATTACHMENT LUGS AND FUSELAGE ATTACH LUGS. ALL CORROSION WAS REMOVED AND REPAIRED PER ERA 396259-14 AT HMV.Oct 19, 2000 · N311DL · Boeing 737232SDR C2XA00IA364Bushing · corrodedIAH-DURING C-CHECK INSPECTION, THE RIGHT HAND HORIZONTAL STABILIZER AFT ATTACHMENT INBOARD BUSHING WAS FOUND TO BE CORRODED AND PITTED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUSHING IN ACCORDANCE WITH EMB145 M/M 20-10-08, AND THE AIRCRAFT WAS APPROVED Oct 4, 2000 · N15932 · Emb EMB145SDR C2XA00IA363Bushing · groovedIAH-DURING C-CHECK INSPECTION, THE RIGHT HAND HORIZONTAL STABILIZER AFT ATTACHMENT OUTBOARD BUSHING WAS FOUND TO BE PITTED AND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUSHING IN ACCORDANCE WITH EMB145 M/M 20-10-08, AND THE AIRCRAFT WAS APPROVEDOct 4, 2000 · N15932 · Emb EMB145SDR C2XA00IA362Bushing · groovedIAH-DURING C-CHECK INSPECTION, THE LEFT HAND HORIZONTAL STABILIZER AFT ATTACHMENT OUTBOARD BUSHING WAS FOUND TO BE HEAVILY GROOVED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUSHING IN ACCORDANCE WITH EMB145 M/M 20-10-08, AND THE AIRCRAFT WAS APPROVED FOR Oct 4, 2000 · N15932 · Emb EMB145SDR C2XA00IA361Bushing · groovedIAH-DURING C-CHECK INSPECTION, THE LEFT HAND HORIZONTAL STABILIZER AFT ATTACHMENT INBOARD BUSHING WAS FOUND TO BE HEAVILY GROOVED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUSHING IN ACCORDANCE WITH EMB145 M/M 20-10-08, AND THE AIRCRAFT WAS APPROVED FOR ROct 4, 2000 · N15932 · Emb EMB145SDR C2XA00IA360Bearing · corrodedIAH-DURING C-CHECK INSPECTION, THE VERTICAL STABILIZER TO HORIZONTAL STABILIZER LEFT HAND AND RIGHT HAND SPHERICAL BEARINGS WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEARINGS IN ACCORDANACE WITH EMB145 M/M 55-37-00-400-801-A, ANDOct 4, 2000 · N15932 · Emb EMB145SDR AALA20001671Bearing · scoredTUL - FOUND LEFT BEARING BORE SCORED, STATION XH 6.625, YH 70.95, ZH 7.25. HONED BORE TO 3.008 INCH AND INSTALLED NEW BUSHING PER CARD 3702 SRM 5502 FIG 12A. (M)Sep 27, 2000 · N7508 · Doug DC982SDR C2XAOOIA378Pin · corrodedREFERENCE OPEN SDR C2XAOOIA338-IAH-DURING C-CHECK INSPECTION, THE RIGHT HAND HORIZONTAL STABILIZER HINGE PIN WAS FOUND TO BE CORRODED. MX REMOVED/REPLACED THE AFFECTED PIN, AND A/C WAS APPROVED FOR RETURN TO SERVICE.Sep 26, 2000 · N15932 · Emb EMB145SDR C2XAOOIA379Pin · corrodedREFERENCE OPEN SDR C2XAOOIA337-IAH-DURING C-CHECK INSPECTION, THE LEFT HAND HORIZONTAL STABILIZER HINGE PIN WAS FOUND TO BE CORRODED. MX REMOVED/REPLACED AFFECTED PIN AND A/C WAS APPROVCED FOR RETURN TO SERVICE.Sep 26, 2000 · N15932 · Emb EMB145SDR C2XA00IA378Pin · corrodedREFERENCE OPEN SDR C2XAOOIA338 DURING C-CHECK INSPECTION RT HORIZONTAL STABILIZER HINGE PIN WAS FOUND TO BE CORRODED. MX REMOVED/REPLACED AFFECTED PIN, AND A/C WAS APPROVED FOR RETURN TO SERVICE.Sep 26, 2000 · N15932 · Emb EMB145SDR C2XA00IA338Pin · corrodedDURING C-CHECK INSPECTION R/H HORIZONTAL STABILIZER HINGE PIN WAS FOUND TO BE CORRODED. THIS SDR IS BEING FILED OPEN AWAITING FINAL CORRECTIVE ACTION.Sep 26, 2000 · N15932 · Emb EMB145
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