JASC 5521

Service difficulty reports · 520

Reports filed under 5521 · Elevator, Spar/Rib, 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 = '5521'
  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 DALA1127539871Spar · crackedLT ELEVATOR OTBD T/E SPAR CRACKED, OTBD HOLE IN SPAR ELONGATED. CUT OUT DAMAGED SECTION OF CHANNEL 7" LONG IAW SRM 51-70-5. NDT TO VERIFY DAMAGED CONTAINED. ORIG MAT 2024T3 .025 IAW SRM 51-70-5. FABBED 1EA CHANNEL MAT 2024T3, PO 1120031. MAT FOR SPLICE 20Apr 19, 2011 · N780NC · Doug DC951SDR CA110503007Spar · crackedLT OTBD ELEVATOR SPAR FOUND CRACKED AFTER INSP, COMPLETED REF AD2011-07-13.Apr 14, 2011 · Schler ASW19SDR 2011FA0000156Spar · crackedDURING THE ACCOMPLISHMENT OF SL-114-17 A SMALL HAIRLINE CRACK WAS DISCOVERED. THE CRACK IS APPROX. 2.35" IN LENGTH, ON THE RT ELEVATOR SPAR, BELOW THE OUTBOARD ELEVATOR HINGE ATTACH POINT. THE AREA OF CONCERN IS LOCATED ON THE RH ELEVATOR 69.35 FROM C/L & FS 2Mar 4, 2011 · N4732W · Gulstm 114SDR USAA2011022190838Rib · corrodedSAL - MAJOR REPAIR - S5 CHECK - CORROSION ON LEFT ELEVATOR OUTBOARD RIB. REPLACED LEFT ELEVATOR OUTBOARD RIB IAW EA 133353.Feb 20, 2011 · N621AW · Airbus A320231SDR HNAA2011022000032Rib · damagedDAMAGE ON T/E OF LT ELEVATOR BETWEEN AREA YH0, YH6.00 AND XH 28.200, XH33.950, INBD OF CAP. R & R INBD RIB ON OTBD CAP END OF LT ELEVATOR ASSY IAW DWG 85520002.Feb 10, 2011 · N806EX · Dhav DHC8102SDR CA110131009Spar · cracked(CAN) CRACK ON SPAR COMPLETE ACROSS LOCATED AT APPROX 4 INCHES IB OF OB HINGE AT THE INSPECTION HOLE THE SURFACE SKIN HAD A SMALL CRACK WHICH PROMPTED US TO LOOK FURTHER. THIS INSPECTION IS LONGER DONE AS PER AD 99-12-05. THIS VISUAL INSPECTION SHOULD BE DONEJan 28, 2011 · Piper PA31SDR FDEA201012064603Frame · corrodedLT ELEVATOR HAS CORROSION OTBD FWD EDGE OF LOWER SIDE OF CONDUCTIVE FRAME. CORRODED CONDUCTIVE FRAME ON LT ELEVATOR. R & R IAW SRM 51-40-02, REV 101. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.Dec 6, 2010 · N946FD · Boeing 757236SDR C2XA10TY166Rib · bentLT ELEVATOR CLOSING-RIB CAP IS BENT APPROX 10 INCHES FROM LEADING EDGE. MAINTENANCE INDUCED DAMAGE. PERFORMED DOUBLER AND FILLER REPAIR, FABRICATION, ALODINE, PRIME, PAINT AND INSTALL ALL IAW ETD2010-145/09760.Oct 21, 2010 · N17185 · Emb EMB145XRSDR CA100525019Doubler · crackedDURING ROUTINE MX WITH THE ELEVATOR OFF, A CRACK WAS NOTED ON THE BUTT RIB DOUBLER PN C2-TE-9ND. CF80-25 REQUIRES A INSP OF THE AREA EVERY 400 HOURS, THE CRACK WAS NOTICED WITH 278.2 HOURS SINCE THE LAST INSP.May 22, 2010 · Dhav DHC2MKISDR UIEA201000022Rib · crackedLT INBD ELEVATOR L/E MOST INBD RIB ANGLE CRACKED. INBD RIB UPPER MOST UPPER RIB ANGLE BRACKET REPLACED IAW SRM 51-00-02 AND 51-40-02.Mar 1, 2010 · N499MC · Boeing 74747UFSDR FOTR20006NR5222Spar · damagedC/W AD2008-17-14 SB 727-55-0089 ELEVATOR REAR SPAR AT THE TAB HINGE LOC. IAW PARA (A) REPLACEMENT OF THE ELEVATOR REAR SPAR AND SUPPORT FITTING IAW PART 2 OF S/B 727-55-0089 REV 1 (RT). REPAIRED ON FASI WO 20006. N/R 05222- R & R ELEVATOR REAR SPAR AND SUPPJan 29, 2010 · N286SC · Boeing 7272A1SDR C8GA20090295Spar · corrodedREMOVED AND REPLACED RT ELEVATOR SPAR AND SUPPORT FITTINGS. ACFT WAS RETURNED TO SERVICE.Jul 31, 2009 · N89427 · Boeing 727227SDR C8GA20090247Spar · defectiveREMOVED AND REPLACED LT ELEVATOR REAR SPAR AND SUPPORT FITTINGS TO COMPLY WITH SB 727-55-0089 NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVICE.Jul 31, 2009 · N89427 · Boeing 727227SDR 2009FA0000432Rib · crackedACFT EQUIPPED WITH STOL CANARDS. FOUND BOTH INBD CANARD ELEVATOR RIBS CRACKED AT ALL BOLT HOLES. BOTH ELEVATORS RETURNED TO MFG FOR MODIFICATIONS AND REPAIRS.May 27, 2009 · N769DB · Cessna 182QSDR TIMA20090003Rib · crackedINBOARD RIB WAS CRACKED AT LEADING EDGE. CRACKS BEGIN IN BOTH UPPER AND LOWER FLANGE RADIUS AND PROGRESSED THROUGH THE FIRST RIVET HOLE IN THE WEB. CRACKS EXTENDED ABOUT .5 INCH PAST THE RIVETS WHEN DISCOVERED. THE ELEVATOR BALANCE WEIGHT SUPPORT BOLTS TO TMay 18, 2009 · N955AA · Beech 99ASDR IPXA09555708Spar · damagedINSPECTION TYPE:C4 REMOVE & REPLACE RT ELEVATOR DUE TO SPAR DAMAGE AT ELEVATOR STA 117.5. REMOVED & REPLACED ELEVATOR, OPS TEST GOOD IAW MM 27-31-01-4.Apr 23, 2009 · N444UP · Boeing 75724APFSDR K11A2009022472002Spar · crackedREAR SPAR HAS CRACK, LT ELE STA 66.5.Feb 24, 2009 · N720CK · Boeing 7272B6SDR K11A2009022472001Spar · crackedREAR SPAR HAS CRACK, LT ELE STA 68.Feb 16, 2009 · N720CK · Boeing 7272B6SDR FDEA200901150203Rib · dentedLT ELEVATOR INBD UPPER SURFACE T/E RIB NR 1 HAS DENT MEASURES .50 INCH BY .50 IN BY .012 INCH DEEP. DENT REPAIRED AT LT ELEVATOR UPPER SURFACE RIB NR 1 WITH WET OVERLAY REPAIR IAW A310 SRM 55-21-11, FIG 204.Jan 15, 2009 · N435FE · Airbus A310203SDR C2XA08TY136AARib · burnedRT ELEVATOR TIP FAIRING SUPPORT NUT PLATE FASTENER HOLE WAS ELONGATED FROM A LIGHTNING STRIKE. THE DAMAGED TIP WAS CUT OUT AND A FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW EC5520-01162. THE ELEVATOR WAS REMOVED, BALANCED, AND INSTALLED IAW EMB AMM Dec 1, 2008 · N21154 · Emb EMB145XRSDR 08FDEA02416Rib · gougedRIGHT STABILIZER INBD ELEVATOR UPPER SURFACE IS GOUGED IN 2 PLACES. REPAIRED 2 EA GOUGES IAW DC/MD-10 SRM 55-10-00; VOL I; FIG 8 AND DC/MD-10 SRM 55-00-01; VOL I; FIG 3; SHEET 2. REPAIRED THE DAMAGED RIB CAP IAW DC/MD-10 SRM 55-00-01; VOL I; FIG 6. WEIGHT AJun 24, 2008 · N357FE · Doug MD1010FSDR ASAA0843063Spar · puncturedRIGHT ELEVATOR HAS PUNCTURE HOLE IN FORWARD SPAR. REMOVED DAMAGED ELEVATOR. INSTALLED REPLACEMENT ELEVATOR IAW B737 AMM 27 31 11 004 027 27 31 11 404 025.Jun 7, 2008 · N780AS · Boeing 7374Q8SDR K11A2008121672010Spar · crackedRT ELEVATOR REAR SPAR CRACKED FWD OF THE NR 4 TRIM TAB HINGE, ELEVATOR STA 99.79.Nov 21, 2007 · N720CK · Boeing 7272B6SDR 07FDEA04848Skin · crackedLT INBD ELEVATOR OUTER RIB UPPER SKIN WITH .25 INCH CRACK. REPAIRED SKIN IAW SRM 55-10-00 FIG 8 VOL I.Nov 19, 2007 · N306FE · Doug DC1030SDR 07FDEA03679Spar · corrodedCORROSION FOUND ON RT ELEVATOR FRONT SPAR WEB NEAR RIB 2A AROUND ONE BONDING POINT REPAIR PERFORMED BY BLENDOUT UNTIL CORROSION REMOVAL IAW EA 6-5520-79603 AND RAS/CASA/3692/2004 ISS A.Sep 13, 2007 · N432FE · Airbus A310203SDR ERH2007F00000Spar · crackedPILOT REPORTED A CRACK FOUND ON THE LT ELEVATOR WHILE PERFORMING A PREFLIGHT INSPECTION. THE ELEVATOR WAS REMOVED FROM THE AIRCRAFT FOR CLOSER INSPECTION. THE CRACK WAS IN THE FORWARD SPAR AND HAD ORIGINATED FROM UNDER THE OB ATTACH FITTING. FATIGUE. RECOMMSep 8, 2007 · N727KT · Dhav DHC3SDR 07FDEA03431Rib · damagedRT ELEVATOR TIP SKIN PLATE AND RIBS DEFORMED. FOUND CRACKS (20 AND 30 MM) IN LOWER SKIN AT T/E PROFILE. REAR UPPER ANCHOR NUT OF ELEVATOR RIB ER41 CRACKED. REPAIR PERFORMED BY TRIM OUT TO REMOVE THE CRACKED AND DENTED AREA. INSTALLATION OF REPAIR ANGLE ANDSep 7, 2007 · N808FD · Airbus A310324SDR SIMA200723219Hinge Fitting · corrodedLEFT ELEVATOR SERVO TAB INBOARD HINGE FITTING CORRODED. REMOVED AND REPLACED HINGE FITTING IAW EMB 55-22-01. AIRCRAFT WAS RETURNED TO SERVICE.Aug 17, 2007 · N725AE · Emb EMB135LRSDR 2007AP080901Spar · crackedRT ELEVATOR SPAR FOUND BROKEN/CRACKED AT OB ATTACH POINT. OB HINGE BRACKET PULLED AWAY FROM SPAR.Aug 9, 2007 · N48440 · Cessna 152SDR HNAA0700134Failsafe · corrodedRIGHT ELEV O/B HINGE FAIL SAFE CORRODED.Jun 6, 2007 · N912HA · Dhav DHC8102SDR K11A2008120372210Spar · corrodedELEVATOR REAR SPAR CORRODED.Jun 5, 2007 · N722CK · Boeing 7272H3SDR CA070426009Rib · cracked(CAN) THIS ELEVATOR LEADING EDGE RIB WAS FOUND CRACKED WHILE CARRYING OUT ANNUAL INSPECTION. IT WAS DETERMINED THAT THE CRACK WAS THE RESULT OF TOO SHARP OF A BEND RADIUS IN THE AREA WHERE THE PART GETS RIVETED TO THE ELEVATOR LEADING EDGE SKIN. THIS DEFECTApr 20, 2007 · Dhav DHC2MKISDR ABXA070121Spar · crackedX-RAY INSPECTION ON LEFT ELEVATOR REVEALED CRACKS AT STATIONS: XE 74(.750), XE 191(.600), XE 195(.750), XE 199 (.750), AND XE 219 (.400). REPAIRED CRACKS AT STATIONS: XE 191, XE 195, XE 199 AND XE 219. NO CRACKS DETECTED AT XE 74. REPAIRED IAW DC9 SRM 55-02Apr 9, 2007 · N785TW · Doug DC915FSDR DHL2007786513Rib · crackedRT ELEVATOR, FWD INBD RIB CRACKED AND MISSING RIVETS, ELEV STA 20. REMOVED ACCESS PANEL RT ELEVATOR LWR INBD IAW B727 SRM 51-30-2. REMOVED RIB IAW B727 SRM 51-30-2. FABRICATED NEW RIB FROM 7075T6, .040, 18.25 BY 2.50 IAW B727 SRM 55-20-2, FIG 2. TREATED ALMar 21, 2007 · N786AT · Boeing 727214SDR EIA2007032Spar · damagedRIGHT OUTBOARD FRONT SPAR LOWER CHORD FOUND DAMAGED. TRIMMED OUT DAMAGED PORTION OF LOWER CHORD PERFORMED HFEC ON TRIM EDGES AND FABRICATE FILLER AND REPAIR ANGLES. APPLIED ALODINE AND PRIMER ON PARTS AND INSTALL FASTENERS AND NUT PLATES WITH RIVETS AT NUT PFeb 22, 2007 · N471EV · Boeing 747273CSDR EIA2007027Spar · damagedDAMAGE FOUND COMMON TO FRONT SPAR, LOWER CHORD OF RT O/B ELEVATOR STA 227.65. TRIM OUT DAMAGED PORTION OF LOWER CHORD, CARRY OUT HFEC ON TRIM EDGES. FABRICATE FILLER AND REPAIR ANGLES. APPLY ALODINE COATING TO ALL REPAIR PARTS AND BASE METAL EDGES. INSTALLFeb 22, 2007 · N471EV · Boeing 747273CSDR 2007FA0000230Rib · broken1 INCH CRACK NOTED ON LOWER SKIN THRU RIVET. DRILLED OPEN SKIN AND FOUND 5 INCH OF RIB FLANGE BROKE OFF 2 INCHS FROM TRAILING EDGE. SKIN AND RIB HAVE TO BE REPLACED. (K)Feb 20, 2007 · N112ED · Piper PA31TSDR 2007FA0000059Attach Angle · crackedDURING INSPECTION, ANGLE PN 5102296-15 AND PN 5102296-16, WERE FOUND CRACKED IN THE BEND RADIUS OF THE UPPER END OF THE ANGLE AS INSTALLED. CAUSE OF CRACKING IS BELIEVED TO BE DUE TO HIGH STRESS LOADS IN THIS AREA. (K)Jan 10, 2007 · N4521A · Amrgen AA5BSDR 2007FA0000056Attach Angle · crackedDURING INSPECTION, ANGLE PN 5102296-15 AND PN 5102296-16, WERE FOUND CRACKED IN THE BEND RADIUS OF THE UPPER END OF THE ANGLE AS INSTALLED. CAUSE OF CRACKING IS BELIEVED TO BE DUE TO HIGH STRESS LOADS IN THIS AREA. (K)Jan 10, 2007 · N11966 · Amrgen AG5BSDR 2007FA0000050Attach Angle · crackedDURING INSPECTION, ANGLE PN 5102296-15 AND PN 5102296-16, WERE FOUND CRACKED IN THE UPPER END OF THE ANGLE AS INSTALLED. CAUSE OF CRACKING IS BELIEVED TO BE DUE TO HIGHT STRESS LOADS IN THIS AREA. (K)Jan 10, 2007 · N9962U · Amrgen AA5ASDR SROM200600020Spar · crackedDURING INSPECTION FOUND LT ELEVATOR TAB OUTBOARD HINGE FITTING TO HAVE CONSIDERABLE FLEX. UPON FURTHER EXAMINATION FOUND ELEVATOR REAR SPAR CRACKED IN THE AREA WHERE TAB HINGE FITTING ATTACHES. AD 2006-14-07/SB 737-55A1078 HAD NOT BEEN ACCOMPLISHED PRIOR TO Nov 30, 2006 · N736BP · Boeing 737205SDR 06FDEA03595Rib · corrodedFOUND LT NR 1 ELEVATOR THRUST HINGE RIB IB AND OB LUGS IB AND OB FACES CORRODED/WORN. REPARIED PER FED EX EA 7-5510-100595.Oct 6, 2006 · N285FE · Boeing 727233SDR CA060928003Stringer · failed(CAN) AFTER RECOVERING FROM AN AEROBATIC MANEUVER, THE PILOT FOUND THAT FULL DOWN ELEVATOR TRAVEL COULD NOT BE OBTAINED. A UNEVENTFUL RETURN TO THE AIRPORT AND LANDING WAS CARRIED OUT. ONCE THE ELEVATOR BELLCRANK COVER WAS REMOVED, THE LT GUSSET FROM THE AFT Sep 9, 2006 · Bbavia 7ECASDR UPS06247095Spar · crackedINSPECTION TYPE:C ON INSP CRACK DETECTED ON THE LEFT ELEVATOR REAR SPAR STA 138 APPROX. HFEC CARRIED OUT IAW B727 NDTM 51-00-00 PT 6 FIG 4, CRACK CONFIRMED, ENDS MARKED. ELEVATOR REMOVED IAW MM 27-30-01. NEW ELEVATOR INSTALLED IAW MM 27-30-01. ELEVATOR FRIMay 26, 2006 · N944UP · Boeing 72722CSDR UPS06247059Spar · crackedINSPECTION TYPE:C X-RAY INSPECTION HAS DETECTED 2 SUSPECT CRACKS ON INSPAR RIBS LOCATED BETWEEN ELEVATOR STATION 99.50-136.50 DISPLACED UPPER ELEVATOR SKIN FROM BS 99.5 TO BS 136.5 IAW SRM 51-30- 02 AND REMOVED REPAIR DOUBLER FROM LOWER SKIN. HFEC CARRIED May 23, 2006 · N944UP · Boeing 72722CSDR UPS06247053Rib · crackedINSPECTION TYPE:C X-RAY INSP DETECTED ONE SUSPECT CRACK ON THE LT ELEVATOR INTERNAL RIB LOCATED BETWEEN ELEV STA 179.50 - 205.50. ELEV BEYOND ECONOMIC REPAIR REF NRC 100783 FOR REPLACEMENT OF LT ELEVATOR.May 23, 2006 · N944UP · Boeing 72722CSDR 06FDEA1599Rib · damagedRIGHT HORIZONTAL STAB INBOARD ELEVATOR ASSY OUTER RIB FOUND DAMAGED.Apr 26, 2006 · N526FE · Doug MD11SDR LR7A06011Skin · crackedDURING 'A-1' CHECK PER HA1201, FOUND LT LOWER ELEVATOR SKIN CRACKED 5/8 IN AT HORIZONTAL STABILIZER STATION 76.5, FS 1151.5, WL 273. REPAIRED SKIN IAW SMP583 51-140-12, N/R M4.Mar 30, 2006 · N402LC · Lkheed 382GSDR DHL2006760524Spar · crackedRT ELEVATOR REAR SPAR HAS CRACK EXTENDING 0.125" FROM END OF SHEAR PLATE AT NR 4 HINGE BRACKET ELEV. STA 99.79 REMOVED AND REPLACED RT ELEVATOR REAR SPAR IAW S/B 727-55-0089 REV 1.Feb 19, 2006 · N760AT · Boeing 7272B7SDR DHL2006760523Spar · crackedRT ELEVATOR REAR SPAR HAS CRACK EXTENDING 0.125" FROM END OF SHEAR PLATE AT NR 4 HINGE BRACKET ELEV. STA 99.79 CORRECTIVE ACTION; REMOVED AND REPLACED RT ELEVATOR REAR SPAR IAW S/B 727-55-0089 REV 1 THIS REPAIR IS A CATEGORY AFeb 19, 2006 · N760AT · Boeing 7272B7
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