JASC 5500

Service difficulty reports · 490

Reports filed under 5500 · Empennage 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 = '5500'
  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 DALA1502670982Lug · unknownHS HINGE RIB PIVOT BEARING LUG REPAIRED IAW AA 5500-01011.Jun 26, 2012 · N982DL · Doug MD88SDR DALA1224960927Plate · corrodedIRR: RT OUTER INBOARD HINGE PLATE CORRODED BEYOND LIMITS. REPLACED RT OUTER INBOARD HINGE PLATE IAW ERA 502265-14.Apr 14, 2012 · N927DA · Doug MD88SDR DALA1224950927Plate · corrodedIRR: RT INNER INBOARD HINGE PLATE CORRODED BEYOND LIMITS. REPLACED RT INNER INBOARD HINGE PLATE IAW ERA 502265-14.Apr 13, 2012 · N927DA · Doug MD88SDR DALA1224940927Plate · corrodedIRR: RT INNER OUTBOARD HINGE PLATE CORRODED BEYOND LIMITS. REPLACED RT INNER OUTBOARD HINGE PLATE IAW ERA 502265-14.Apr 12, 2012 · N927DA · Doug MD88SDR DALA1224920927Plate · corrodedIRR: RT OUTER OUTBOARD HINGE PLATE CORRODED BEYOND LIMITS. REPLACED RT OUTER OUTBOARD HINGE PLATE IAW ERA 502265-14.Apr 11, 2012 · N927DA · Doug MD88SDR DALA1224910927Plate · corrodedIRR: LT OUTER INBOARD HINGE PLATE CORRODED BEYOND LIMITS. REPLACED LT OUTER INBOARD HINGE PLATE IAW ERA 502265-14.Apr 10, 2012 · N927DA · Doug MD88SDR DALA1224900927Plate · corrodedIRR: LT INNER INBOARD HINGE PLATE CORRODED BEYOND LIMITS. REPLACED INNER INBOARD HINGE PLATE IAW ERA 502265-14.Apr 9, 2012 · N927DA · Doug MD88SDR DALA1224880927Plate · corrodedIRR: LT INNER OUTBOARD HINGE PLATE CORRODED BEYOND LIMITS. REPLACED INNER OUTBOARD HINGE PLATE IAW ERA 502265-14.Apr 8, 2012 · N927DA · Doug MD88SDR DALA1224840927Plate · corrodedIRR: LT OUTER OUTBOARD HINGE PLATE CORRODED BEYOND LIMITS. CORR: REPLACED LT OUTER OUTBOARD HINGE PLATE IAW ERA 502264-14.Apr 7, 2012 · N927DA · Doug MD88SDR AALA20120325008Angle · crackedFIXED LEADING EDGE EXPANSION JOINT J-ANGLE CRACKED ON RIGHT SIDE. REPLACED ANGLE.Mar 7, 2012 · N933AN · Boeing 737823SDR AALA20120307003Structure · crackedCRACK AT RIGHT FORWARD OUTER CHORD STATION 1809.5. REPAIR PIECE INSTALLED PER ECO C1945DN.Mar 6, 2012 · N370AA · Boeing 767323SDR ERAA201200025Fastener · looseREPLACED 8 LOOSE FASTENERS WITH JOBOLTS IAW RD8-55-032.Feb 11, 2012 · N881EA · Dhav DHC8106SDR CA111213008Tube · cracked(CAN) DURING ANNUAL INSPECTION, A CRACK WAS DISCOVERED AT THE UPPER DIAGONAL TUBE IN THE AFT EMPENNAGE AREA. SL 266 CALLS FOR AN INSPECTION OF THIS AREA EVERY 100HRS WITH REPAIR PROVISIONS IF DAMAGE IS FOUND. THIS SL APPLICABILITY IS FOR ACFT PRIOR TO SN 0259Dec 9, 2011 · Airtrc AT802ASDR AALA20110922TUL04Spar Cap · crackedCRACK INDICATION WITH A HFEC HOLE PROBE, LEFT SIDE SIXTH HOLE DOWN FROM UPPER EDGE OF LOWER SKIN. DOUBLER AND TRIPLER INSTALLATION ON SPAR CAP PER EA MD80-55-019313.Sep 22, 2011 · N9615W · Doug DC983SDR GLBA20110803HCap · damagedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP, MX FOUND THE RT STABILON END CAP DAMAGED FROM TE FWD 10.7" AND FROM T/E OTBD TIP 7" GOING 2.5" PAST SPLICE. MX REPLACED, REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW. EO 11-1900-55Aug 3, 2011 · N231YV · Beech 1900DSDR GLBA20110428FStructure · damagedMAJOR REPAIR - MX REPORT THAT DURING REFUELING, THE FUEL TRUCK STRUCK THE RT STABILON, THE RT STABILON WAS REPLACED ON 192GL. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-55-007. MATERIALS UTILIZED ARE INCLUDED IN THApr 27, 2011 · N192GL · Beech 1900DSDR UIEA2011031000186Rib · crackedCRACK ON 65B23604-27 RIB OF LT GST L/E FAIRING UPPER SIDE AT 51A 527.190. (REPAIR - IAW EI T2011A55B-618 REV 00, AMP; REV 01)Mar 10, 2011 · N499MC · Boeing 74747UFSDR VNAA2010110500005Rivet · damagedCREW REPORTED A POSSIBLE LIGHTNING STRIKE. MAINTENANCE INSPECTED AND REPAIRED RIVETS ON STABILIZER. INSPECTION AND REPAIRS WERE DONE USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.Nov 5, 2010 · N229PS · Cndair CL6002B19SDR AALA20100118AFW01Structure · crackedFOUND CRACK INDICATION AT STATION 1809.5 LEFT FORWARD CHORD FASTENER HOLE. THE HOLE WAS OVERSIZED TO 0.2636 INCH IN ORDER TO REMOVE ANY CRACK INDICATIONS. BOEING REQUIRED AN INSURANCE CUT OF AT LEAST 0.030 INCH. THE INSURANCE CUT RESULTED IN A FINAL HOLE SIJan 18, 2010 · N371AA · Boeing 767323SDR AALA20091104TUL09Attach Angle · brokenLEFT ANTI FLOAT GEAR TAB CONTROL ROD FAIRING UPPER ATTACH ANGLE BROKEN. INSTALLED DOUBLER PER ENGINEERING AUTHORIZATION MD80-55-007984.Nov 4, 2009 · N7525A · Doug DC982SDR AALA20090811TUL11Plate · corrodedRIGHT OUTBOARD LUG PLATE G AT STATION 1630 HAS CORROSION. INSTALLED NEW RIGHT OUTBOARD LUG PLATE G UNDER AARD 55-94-05.Aug 8, 2009 · N9628W · Doug DC983SDR AALA20090821TUL07Plate · corrodedRIGHT OUTBOARD LUG PLATE H AT STATION 1630 HAS CORROSION. INSTALLED BE RIGHT OUTBOARD LUG PLATE H AT STATION 1630 UNDER AARD 55-94-05.Aug 7, 2009 · N9628W · Doug DC983SDR AALA20090521TUL28Tab · burnedTAIL, GEARED TAB TRAILING EDGE HAS STATIC DISCHARGE BURN MARKS. INSTALLED DOUBLER WITH HOT BOND PER SRM 51-70-2.May 5, 2009 · N446AA · Doug DC982SDR AALA200910626Lug · corrodedTAIL, NUMBER 1 LUG PLATE HAS CORROSION. INSTALLED A SERVICEABLE NUMBER 1 LUG.Jan 7, 2009 · N434AA · Doug DC983SDR AALA200910625Lug · corrodedTAIL, NUMBER 2 LUG PLATE HAS CORROSION. INSTALLED A SERVICABLE NUMBER 2 LUG.Jan 7, 2009 · N434AA · Doug DC983SDR AALA200910624Fitting · corrodedTAIL, NUMBER 3 LUG PLATE HAS CORROSION. INSTALLED A SERVICEABLE NUMBER 3 LUG.Jan 7, 2009 · N434AA · Doug DC983SDR AALA200910623Lug · corrodedTAIL, NUMBER 4 LUG PLATE HAS CORROSION. INSTALLED A SERVICEABLE NUMBER 4 LUG.Jan 7, 2009 · N434AA · Doug DC983SDR UPS08853731Rib · crackedINSPECTION TYPE:SV EVALUATION OF N/R288527 RIB CRACKED AT TOP AFT END AT XFS 185. REPAIRED 55-02-00 FIG 2.Oct 2, 2008 · N702UP · Doug DC871FSDR HNAA2009020100042Tab · dentedDENT ON TRAILING ARM OF LT STRING TAB 3.3" FROM INBD EDGE. REPAIR DAMAGE IAW WITH RD8-55-037.Jun 13, 2008 · N980HA · Dhav DHC8102SDR S9BA200800016Attach Bracket · corrodedDURING CAMP INSPECTION, FOUND CORROSION ON LT AFT (SEA FIN) ATTACHMENT BRACKET. REMOVED AND REPLACED SEA FIN ATTACHMENT BRACKET. EMERGENCY DECLARED? NO, AIRCRAFT GROUNDED, REPAIRED DURING INSPECTION NO.Apr 10, 2008 · N573SA · Dhav DHC6SDR FDKA200801034Bonding Strap · corrodedTHE BONDING STRAPS ON PANEL NR 337DL, NR 321EL AND NR 321DR ARE CORRODED. THE STRAPS HAVE BEEN REMOVED AND REPLACED.Jan 17, 2008 · N834MJ · Emb EMB145LRSDR AWXA200601559Structure · vibrationCMH - CREW WAS EXPERIENCING SEVERE TAIL VIBRATIONS AND DIVERTED TO IND. THE AIRCRAFT WAS MAINTENANCE FERRIED BACK TO PHX AND EXPERIENCED NO VIBRATION ISSUES.Aug 20, 2006 · N804AW · Airbus A319132SDR KCSA061233Fastener · looseLOOSE FASTENERS ON L/H SIDE OF EMPENNAGE BETWEEN STA 2680 TO 2701 12 TO 40 INCHES ABOVE APU DOOR HINGE.Jul 21, 2006 · N706CK · Boeing 747249FSDR 2006FA0000523Skin · corrodedAFTER A PHASE 1,2,3,4,49&59 CORROSION AND DELAMINATION WAS FOUND ON TOP AND BOTTOM SKINS LT AND RT SIDES OF THE HORIZONTAL STABILIZER, LT SKIN OF THE VERTICAL STABILIZER. TAIL SKINS 5512010-9 AND 6512010-20 (SKINS UNDER VERT. STAB.) AS WELL AS THE AFT BULKHEADMay 20, 2006 · N1255K · Cessna 550SDR 2006FA0000869Fitting · crackedSTABILIZER FITTING REMOVED FROM AC TO BE CHECKED IAW AD76-05-04. DYE PENETRANT INSPECTION REVEALED (2) CRACKS RADIATING FROM THE LOWER BOLT HOLE ATTACHMENT POINTS AS DEPICTED IN DWG. PROBABLE CAUSE COULD BE FROM IMPROPER TORQUE OF ATTACHMENT BOLTS AT PREVIOUMar 15, 2006 · N4473V · Beech 35BEECHSDR 2006UALA00456Skin · dentedRIGHT STAB DENTED APPROXIMATELY 4 FT FROM INBOARD EDGE. DENT WAS REMOVED AND REPAIRED WITH A DOUBLER AND FILLER PER THE SRM 55-10-01, REPAIR 2.Mar 11, 2006 · N929UA · Boeing 737522SDR USAA060412Repair · unknownRIGHT ELEVATOR LOWER SURFACE 59 INCHES I/B OF O/B END AND 10 INCHES AFT OF FRONT SPAR DAMAGED. PREVIOUS REPAIR IAW SRM 55-20-01-2, DEFECT SIZE: 6 INCHES.Mar 6, 2006 · N527AU · Boeing 7373B7SDR S9B2006F00000Structure · corroded(REF NR: 888-07)LT LWR FINLET REQUIRES CHANGE DUE TO CORROSION. REMOVED AND REPLACED LT LWR FINLET ASSY IAW MM.(K)Mar 5, 2006 · N888PV · Dhav DHC6300SDR 06FDEA0871Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED ON UPPER RUDDER TRAILING EDGE WAS ACCOMPLISHED IAW SRM 51-40-9, FIG 1 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SIZE, SHAPE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBERS, GENERAL WORKMANSHIP, REFeb 28, 2006 · N275FE · Boeing 727200SDR QXEA200600614Attach Fitting · crackedPDX C4 CHECK, EMPENNAGE HALF OBLIQUE FRAME NR 4 HAS CRACKED ATTACH CLIP AT AFT SIDE OF FRAME AND STRINGER NR 4 RIGHT HAND. REPAIRED IAW RD 8-55-199 AMD SRM 51-10-21.Feb 22, 2006 · N349PH · Dhav DHC8202SDR 2006F00009Lug · crackedWILL PERFORMING ASB-328-27-036, FOUND SPRING TAB LEVER LUG CRACKED/BROKEN.Jan 26, 2006 · N462PS · Dorner DO328100SDR 2006F00008Lug · crackedWHILE PERFORMING ASB-328-27-036, FOUND SPRING TAB LEVER LUG CRACKED/BROKEN.Jan 26, 2006 · N462PS · Dorner DO328100SDR WX0600011Fairing · departedSFB - SFG, AIR RETURN TO SFB PER DISPATCHES INSTRUCTIONS. BANANA FAIRING FELL OFF AIRCRAFT AS REPORTED BY DISPATCH. MAINTENANCE INSTALLED LEFT UPPER BANANA FAIRING IAW BOEING MD-80 MM 55-10-03 PAGE 501 THRU 507. AIRCRAFT RETURNED TO SERVICE.Jan 11, 2006 · N861GA · Doug MD83SDR 06FDEA0153Unknown · unknownEMPENNAGE, TO CARRY OUT FEDEX EA 1-5510-80336 HORIZONTAL STABILIZER AFT STRINGER PANEL ASSEMBLY SPLICE REPAIR. COMPLIED WITH FEDEX EA 1-5510-80336, TITLE: STABILIZERS - HORIZONTAL STABILIZER - AFT STRINGER PANEL ASSEMBLY (P/N: ALC8103-504) SPLICE REPAIR, AIRWJan 11, 2006 · N613FE · Doug MD11SDR 05FDEA04301Repair · noneVERTICAL STABILIZER LT SIDE FOUND A FITTING AND DOUBLER REPAIR ON NR 4 BANJO FITTING. PERFORMED INSPECTION FITTING AND DOUBLER REPAIR IAW ESO7349-ACF1275501. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2.Dec 14, 2005 · N563FE · Doug DC1010SDR SIMA200531505Bushing · migratedFOUND HORIZONTAL STABILIZER NR 3 BUSHING HAS EVIDENCE OF MIGRATING. REMOVED AND REPLACED HORIZONTAL STABILIZER NR 3 BUSHING IAW EMB SRM 55-10-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)Nov 1, 2005 · N822AE · Emb EMB135KLSDR 2005FA0001340Tip Cap · damagedOWNER REMOVED ORIGINAL HORIZONTAL STABILATOR TIPS AND INSTALLED AMR, D, STC SA520CH. OWNER COMPLAINED THAT THE CONTROL FORCES HAD CHANGED CONSIDERABLY. THE CONTROL FORCES WERE HEAVY ON TAKEOFF CAUSING THE OWNER TO OVER ROTATE. OWNER REVERTED BACK TO ORIGINASep 22, 2005 · N9467J · Piper PA28180SDR IXXA05RNG081SSkin · deformedDURING INSPECTION CHECK WAS FOUND A OIL CAN ON LOWER SURFACE SKIN STA XE 89.718 TO 108.843-LT. REPAIR DOUBLER WAS INSTALLED IAW EWO ATI 55-013 AND SRM 55-2-1 FIG 2A.Sep 16, 2005 · N721CX · Doug DC872SDR IXXA05RNG080SSkin · deformedDURING INSPECTION CHECK WAS FOUND A OIL CAN ON LOWER SURFACE SKIN STA XE 279.125 TO 288.957 - LT. SKIN WAS REPLACED IAW DRAWING 5654970 ZONE 17 TO 21, RIVETS WERE INSTALLED IAW SRM 51-1-21 PAGE 1-7 AND PROTECTIVE TREATMENT WAS APPLIED IAW SRM 51-1-8 PAGE 13-16Sep 16, 2005 · N721CX · Doug DC872SDR IXXA05RNG079SSkin · deformedDURING INSPECTION CHECK WAS FOUND A OIL CAN ON LOWER SURFACE SKIN STA XE 104.051 TO 108.815 - LT. REPAIR SKIN AND REPAIR SPLICE WERE FABRICATED AND INSTALLED IAW SRM 55-2-1 FIG 2A AND EWO ATI 55-011.Sep 7, 2005 · N721CX · Doug DC872
Back to JASC 5500