JASC 5511

Service difficulty reports · 6,462

Reports filed under 5511 · Horizontal Stabilizer, 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 = '5511'
  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 JEM2004F00007Rib · crackedDURING A SCHEDULED INSPECTION OF THE HORIZ STAB ROLLER BRACKET ASSY AND AREA, IT WAS DISCOVERED THAT THE RIB AS WELL THE TWO SUPPORTING BRACKETS BEHIND THE RIB WHERE CRACKED. THE INSPECTION WAS ACCOMPLISHED BY USING A BORESCOPE AND INSERTING INTO THE HORIZ STAug 28, 2003 · N400FT · Beech 400ASDR UPS03841157Rib · crackedINSPECTION TYPE: C2, LEFT HORIZONTAL STAB. LE. RIB IS CRACKED AT XFS 47.5 STOPDRILLED CRACK,NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLES I.A.W. SRM. 55-2-0 FIG. 2Aug 25, 2003 · N809UP · Doug DC873FSDR UPS03841163Rib · crackedINSPECTION TYPE: C2, RT HORIZONTAL STAB. LEADING EDGE RIB IS CRACKED AT XFS 116.25 STOPDRILLED CRACK,NDT VERIFIED STOPDRILL TERMINATED CRACK,FABRICATED AND INSTALLED REPAIR ANGLES I.A.W. SRM. 55-2-0 FIG. 2Aug 25, 2003 · N809UP · Doug DC873FSDR 03FDEA01200Spar Cap · corrodedHORIZONTAL STAB RT AFT SPAR CAP NR 36R BARREL NUT BORE FOUND CORROSION BEYOND EO 1-5510-7-5000 LIMITATIONS. RT HORIZONTAL STABILIZER AFT SPAR CAP NR 36R BARREL NUT BORE REPAIR CARRIED-OUT AS PER FEDEX EA 1-5510-69404 - STABILIZERS - HORIZONTAL STABILIZERJul 30, 2003 · N605FE · Doug MD11SDR 2003F00550Spar · crackedAT SCHEDULED EMPANNAGE ZONAL INSPECTION, FOUR CRACKS FOUND RADIATING FROM PASSAGE HOLE IN FORWARD WEB OF THE HORIZONTAL STABILIZER FORWARD SPAR. REMOVED SECTION OF CRACKED SKIN. FABRICATED AND INSTALLED SHIM AND DOUBLER IAW FAA APPROVED DATA CONTAINED IN DERJul 16, 2003 · N69547 · Beech 1900DSDR AUS20030745Spar · cracked(AUS) HORIZONTAL STABILISER FRONT SPAR CENTRE LAMINATE CRACKED. FOUND DURING INSPECTION IAW AD C21069.Jul 16, 2003 · Cessna 210NSDR 03FDEA00965Spar Cap · corrodedHORIZONTAL STAB RIGHT UPPER AFT SPAR CAP BARREL NUT BORE NR 36R FOUND CORROSION BEYOND EO 1-5510-7-5000 LIMITATION. RIGHT HORIZONTAL STAB UPPER AFT SPAR CAP BARREL NUT BORE NR 36R REPAIR CARRIED OUT AS PER FEDEX EA 1-5510-71721, STABILIZERS- HORIZONTAL STABILJun 24, 2003 · N588FE · Doug MD11SDR AUS20030653Spar · cracked(AUS) STABILIZER SPAR CRACKED IN AREA AROUND ATTACHMENT BRACKET NUT PLATE. CRACK LENGTH 12.7MM (0.5 IN).Jun 19, 2003 · Cessna A150KSDR CALA0300433Spar · damagedAN EXISTING REPAIR ON THE RT HORIZONTAL STABILIZER FRONT SPAR NEEDED TO BE REPLACED. THE EXISTING REPAIR WAS LOCATED AT STAB STA 245 ON THE FORWARD FLANGES OF THE UPPER AND LOWER CHORDS. THE SPAR CHORDS WERE REPAIRED IAW ECRA 5510-01682.Jun 19, 2003 · N18350 · Boeing 7373T0SDR 03FDEA00941Spar Cap · corrodedSNRM N0824 - HOR STAB LT UPPER SPAR CAP NR 36L BARREL NUT BORE CORROSION FOUND BEYOND EO 1-5510-7-5000 B PT1 LIMITATION. CORRECTIVE ACTION: SNRM N0824 - HOR STAB LH UPPER SPAR CAP NR 36L BARREL NUT BORE REPAIR CARRIED OUT EA 1-5510-71721, STABILIZERS- HORIZOJun 19, 2003 · N588FE · Doug MD11SDR 03FDEA00928Spar Cap · corrodedHORIZONTAL STAB LT UPPER SPAR CAP 36L BARREL NUT BORE CORROSION FOUND BEYOND EO 1-5510-7-5000 B PT1 LIMITATION. HORIZONTAL STAB LT UPPER SPAR CAP 36L BARREL NUT BORE REPAIR CARRIED OUT AS PER FEDEX EA 1-5510-71721, STABILIZERS- HORIZONTAL STABILIZER- BARREL NJun 19, 2003 · N588FE · Doug MD11SDR CALA0300375Spar · damagedAN EXISTING REPAIR ON THE RT HORIZONTAL STABILIZER FRONT SPAR NEEDED TO BE REPLACED. THE EXISTING REPAIR WAS LOCATED AT STAB STA 245 ON THE FORWARD FLANGES OF THE UPPER AND LOWER CHORDS. A PERMANENT REPAIR WAS INSTALLED IAW ECRA 5510-01682.Jun 19, 2003 · N18350 · Boeing 7373T0SDR CA030618007Spar · cracked(CAN) DURING 100 HR INSPECTION SMOKING RIVETS WERE OBSERVED ON THE BOTTOM CENTER DOUBLER OF THE HORIZONTAL STABILIZER. INVESTIGATION REVEALED SPAR CRACK IN WEB AND LOWER FLANGE. HORIZONTAL STAB WAS REMOVED AND SENT OUT FOR SPAR REPLACEMENT.Jun 18, 2003 · Hughes 369DSDR DHL2003873516Frame · crackedLT HORIZ STAB L/E INNER FORMER HAS 0.500 CRACK IN UPPER AND LOWER PART (XFS. 53.750). REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK AND FABRICATED REINFORCING ANGLES IAW SRM 55-2-0 PG 7-8. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B INSTALLED REINJun 17, 2003 · N873SJ · Doug DC873FSDR 2003FA0000627Spar · crackedFOUND HORIZIONAL STABILIZER SPAR CRACKED AROUND CENTER LIGHTING HOLEJun 16, 2003 · N52250 · Cessna 172PSDR 2003FA0000642Spar · crackedFOUND HORIZONTAL STABILIZER SPAR CRACKED AROUND CENTER LIGHTING HOLE.Jun 16, 2003 · N100SU · Cessna 172PSDR DHL2003873505Frame · crackedLT HORIZONTAL STAB L/E INNER FORMER CRACKED 0.500 AT XFS 60.000 (UPPER/LOWER PART). REMOVED FASTENERS IAW SRM 51-1-20D PG 21. STOP DRILLED CRACK IAW SRM 55-2-0 PG 7,8. FABRICATED REINFORCING ANGLE IAW SRM 55-2-0 PG 7,8. CLEANED,TREATED AND PRIMED IAW SRM 51-1Jun 14, 2003 · N873SJ · Doug DC873FSDR ABXA030196Stringer · corrodedRIGHT HORIZONTAL STAB. LOWER STRINGER NO. 10 LOWER HORZ. FLANGE RBL 56, P/N 181T4110-4, FOUND CORROSION DURING INSPECTION ON STRINGER P/N 181T4110-4 COMMON TO SKIN PANEL REMAIN THICKNESS MATERIAL OF 0.135 INCH ORIGINAL THICKNESS WAS 0.165 INCH. THE TOTAL BLEJun 10, 2003 · N796AX · Boeing 767281SDR CA030613007Spar · cracked(CAN) COMPLETED CF-91-42, SB 2/47 REV.C ON POST MOD 2/758 STABILIZER. NO CRACK WAS INITIALLY DETECTED. ALTHOUGH IT IS NOT REQUIRED BY THE AD, BRACKETS C2TP159A AND C2TP160A WERE REMOVED FOR DETAILED VISUAL INSPECTION OF THE SPAR. THE SPAR WAS FOUND CRACKED UNDJun 9, 2003 · Dhav DHC2MK1SDR CA031021005Spar · broken(CAN) DISCOVERED A BREAK IN THE STABILIZER SPAR DURING AN ANNUAL INSPECTION.May 16, 2003 · Cessna 175SDR DHL2003604558Frame · crackedRT. HORIZONTAL STABILIZER L/E INNER FRAME CRACKED 0.500 AT XFS. 47.500. (INNER PART). REMOVED FASTENERS IAW SRM 51-1-21 PG.1. STOP DRILLED CRACK AT XFS.47.500 AND FABRICATED ANGLE DOUBLER (2024-T3 0.032) IAW SRM 55-2-0 PG.7,8. CLEANED, TREATED AND PRIMED AREA May 16, 2003 · N604AL · Doug DC873FSDR SWAA031082Skin · crackedDURING SCHEDULED C3 CHECK, FOUND RT HORIZ STAB SKIN CRACKED (3 EA) ON LOWER SURFACE RADIATING FWD OUT OF FWD RIVET ROW. REPAIRED SKIN PER SRM.May 13, 2003 · Boeing 7372H4SDR SWAA031081Skin · crackedDURING SCHEDULED C3 CHECK, FOUND LT HORIZ STAB SKIN CRACKED (11 EA) ON LOWER SURFACE RADIATING FWD OUT OF FWD RIVET ROW. REPAIRED SKIN PER SRM.May 13, 2003 · Boeing 7372H4SDR CA030526011Spar · cracked(CAN) CRACK FOUND ON INBOARD PORTION OF SPAR RUNNING LONGITUDINALLY.May 5, 2003 · Bell 206BSDR MALA030259Spar · damagedDURING C1 INSPECTION IN CWA, LT HORIZONTAL STABILIZER UPPER FWD SPAR CUP FWD WEB WAS DAMAGED. MAINTENANCE COMPLETED REPAIR IAW EO 55034.May 2, 2003 · N361PX · Saab 340BSDR AUS20030435Spar · cracked(AUS) LT TAILPLANE OUTBOARD SPAR CRACKED AT HINGE POINT. FOUND DURING INSPECTION IAW AD.Apr 24, 2003 · Piper PA31325SDR CA030423006Rib · cracked(CAN) LEADING EDGE RIB ASSEMBLIES ARE VERY DIFFICULT TO SEE.THE USE OF A MIRROR THROUGH THE HORIZONTAL SPAR AND RIB LIGHTNING HOLES IS THE ONLY WAY TO SEE THE CRACKS ALONG THE TABS.WE BELIEVE THE RIBS ARE CRACKING DUE TO IMPROPER GROUND HANDLING.THE PRACTICE OApr 23, 2003 · Cessna 150LSDR CA030526007Spar · cracked(CAN) INSPECTED STABILIZER FRONT SPAR AS PER 2 YEAR INSPECTION REQUIREMENTS OF A/D CF91-42. SPAR WAS FOUND CRACKED UNDER ATTACH BRACKET. CRACK STARTED AT UPPER BOLT HOLE FOR RIGHT ATTACH BRACKET. SPAR REPLACED WITH NEW PART AND AIRCRAFT RETURNED TO SERVICEApr 15, 2003 · Dhav DHC2MK1SDR ABXA030164Spar Cap · corrodedLEFT HORIZONTAL STABILIZER REAR UPPER SPAR CORRODED JUST INBOARD OF XHS 68. REPAIRED AREA IAW REA D955-47165 AND DC-9 SRM.Apr 15, 2003 · N942AX · Doug DC931SDR CA030401004Spar · cracked(CAN) ON INSPECTION 0432001-15 SPAR REINFORCEMENT FOUND CRACKED AFTER DISASSEMBLEY LT & RT SPARS ALSO FOUND CRACKED. REASSEMBLED WITH NEW PARTS INCLUDING NEW STYLE BRACKET. AIRCRAFT RETURNED TO SERVICE.Apr 1, 2003 · Cessna 150LSDR DL757030289Structure · dentedTHE LOWER STRUCTURE OF THE RT HORIZONTAL STABILIZER AUXILIARY SPAR WAS FOUND DENTED AT SPAR STA 330. THE STRUCTURE WAS CUT AND THE DAMAGED SECTION REMOVED. A NEW SECTION OF STRUCTURE WAS INSTALLED WITH 2 STEEL REPAIR ANGLES AND A STRAP PER ER/A 384563-14, REMar 24, 2003 · N612DL · Boeing 757232SDR CA030423004Rib · cracked(CAN) LEADING EDGE RIB ASSEMBLIES ARE VERY DIFFICULT TO SEE.THE USE OF A MIRROR THROUGH THE HORIZONTAL SPAR AND RIB LIGHTNING HOLES IS THE ONLY WAY TO SEE THE CRACKS ALONG THE TABS.I HAVE INCLUDED TWO PHOTOS. ONE OF THE PHOTOS SHOWS A NEW PART AND WERE THE LOCMar 20, 2003 · Cessna 150MSDR DL738030264Structure · damagedWHILE ACCOMPLISHING THE REQUIRED ELEVATOR MODS PER AD 2003-03-22, A CLEVIS FITTING ATTACH HOLE WAS COUNTERSUNK ON THE WRONG SURFACE OF THE MATING STRUCTURE. THE HOLE WAS OVERSIZED TO REMOVE THE MAJORITY OF THE COUNTERSINK AND AN OVERSIZE FASTENER INSTALLED WIMar 20, 2003 · N3748Y · Boeing 737832SDR 2003UALA00296Rib · crackedLT O/B HORIZONTAL STABILIZER CLOSE-OUT RIB POST IS DAMAGED/CRACKED. MAJOR REPAIR ACCOMPLISHED. CRACKED RIB POST WAS REPLACED.Feb 10, 2003 · N767UA · Boeing 777222SDR 03FDEA00112Rib · crackedRT HORIZONTAL STAB AT STA XE 122.594, FWD RIB, ONE HORIZONTAL MACHINED ANGLE FOUND A CRACKED, LINE MEASURED APPROX. 1 INCH IN LENGTH. HORIZONTAL STABILIZER UPPER FORWARD RIB XE 122.594 REPAIRED AS PER FEDEX EA 1-5510-63146 - STABILIZERS - HORIZONTAL STABFeb 6, 2003 · N578FE · Doug MD11FSDR CA030211011Rib · cracked(CAN) THE HORIZONTAL STABILIZER WAS REMOVED FOR ROUTINE MAINTENANCE. UPON INSPECTION OF THE LT AND RT NR 1 LEADING EDGE RIBS IT WAS NOTED THAT THE LT RIB WAS CRACKED ALONG LOWER FORWARD RADIUS FOR APPROXIMATELY TWO INCHES. THIS AREA IS DIFFICULT TO INSPECT WITFeb 4, 2003 · Beech 100BEECHSDR CA030211007Spar · cracked(CAN) DURING SCHEDULED 100 HOUR EVENT NR 2 INSPECTION, CRACKS FOUND ON LEFT SIDE STABILIZER SPAR ASSEMBLY AFT BETWEEN RIB STABILIZER LEADING EDGE BL102 AND BL114.Feb 3, 2003 · Piper PA31T2SDR 03FDEA00075Spar Cap · corrodedCOMPLY WITH EA 1-5510-67532, HORIZONTAL STABILIZER, RT SPAR CAP, REPLACEMENT IAW SR DRAWING REPLACES EA 1-5510-64246 PART 3 AND IS TERMINATING ACTION. HORIZONTAL STABLIZER, RT SPAR CAP REMOVED AND REPLACED IAW EA 1-5510-67532. HORIZONTAL STABILIZER, RT SPJan 23, 2003 · N578FE · Doug MD11SDR UIEA200300001Spar · corrodedDURING CURRENT C CHECK, FOUND LT STABILIZER REAR SPAR CORRODED AT STABILIZER B/L 372, STA 550. NO ESTABILISHED LEVEL OF CORROSION DECLARED SINCE ITEM DISCOVERED DURING ROUTINE INSPECTION. REMOVED EXISTING SPAR SPLICES LOCATED AT STAB STA. 525 AND 570. REMOVJan 22, 2003 · N516MC · Boeing 747243BSDR GTIA021397Rib · crackedFTW - FOUND LT INBOARD HORIZONTAL STABILIZER INBOARD RIB FLANGE WAS A 3 INCH CRACK. REMOVED DAMAGED AREA AT RIB FLANGE. FABRICATED REPAIR ANGLES AND FILLER. INSTALLED REPAIR. (M)Jan 21, 2003 · N803NK · Doug DC982SDR 2003UALA00295Rib · crackedLT O/B HORIZONTAL STABILIZER CLOSE-OUT RIB POST IS DAMAGED/CRACKED. MAJOR REPAIR ACCOMPLISHED. CRACKED RIB POST WAS REPLACED.Jan 20, 2003 · N766UA · Boeing 777222SDR CA030127006Rib · cracked(CAN) DURING INSPECTION OF THE HORIZONTAL STABILIZER TRAILING EDGE RIBS, IN ACCORDANCE WITH AD 2002-12-13 AND BOEING SB 727-55A0091 A CRACK WAS FOUND ON THE UPPER OUTBOARD FLANGE OF THE FITTING AT ELEVATOR STATION 66.50 RT. THE CRACK WAS REPORTED TO BOEING SERJan 17, 2003 · Boeing 727171CSDR 03FDEA00059Spar Cap · damagedLEFT HORIZONTAL STABILIZER UPPER SPAR CAP AFT PLANK NR 33L BORE REAMED TO ALLOWABLE OVERSIZE DIA 1.178 INCHES IAW SB FOUND WITH 02 EA.Jan 16, 2003 · N578FE · Doug MD11SDR UPS03240064Frame · crackedINSPECTION TYPE: C, SUSPECT CRACK ON LT HORIZONTAL STAB UPPER FRAME JUST I/B OF ELEVATOR RIB STA 173.21. REPAIR CARRIED OUT IAW SMRO EO 2003-001-004 UPS ENGINEERING FILE 727-55-20029.Jan 4, 2003 · N934UP · Boeing 72721CSDR CA030107012Rib · cracked(CAN) RT HORIZONTAL STAB RIB WAS FOUND CRACKED.Dec 6, 2002 · Cessna 152SDR CA021119010Rib · cracked(CAN) THE RT INBOARD LEADING EDGE RIB CRACKED AT TOP REAR CORNER.Nov 8, 2002 · Cessna 152SDR CA021119009Rib · cracked(CAN) THE LT INBOARD LEADING EDGE RIB CRACKED AT TOP REAR CORNER.Nov 8, 2002 · Cessna 152SDR CA021105009Rib · cracked(CAN) L/H INBOARD LEADING EDGE RIB WAS FOUND CRACKED AT THE TOP REAR CORNER OF THE HORIZONTAL STABILIZER.Nov 1, 2002 · Cessna A152SDR 02FDEA00777Spar · corrodedRIGHT HORIZ STAB REAR SPAR TOP T-CHORD CORRODED BETWEEN RIB 3 TO 5. R&R T CHORD PER EA 6-5100-66468.Oct 29, 2002 · N419FE · Airbus A310SDR 02FDEA00775Spar · corrodedLEFT HORIZ STAB REAR SPAR TOP T-CHORD CORRODED APPROX 280 MM FROM RIB 3 TO 5. R&R T CHORD PER EA 6-5100-66468.Oct 29, 2002 · N419FE · Airbus A310
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