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 03FDEA00931Structure · corrodedLEFT HORIZONTAL STAB UPPER CENTER PLANK 16L BORE FOUND CORROSION BEYOND EO 1-5510-7-5000 LIMITATIONS. LEFT HORIZONTAL STAB UPPER CENTER PLANK 16L BORE REPAIR CARRIED OUT AS PER FEDEX EA 1-5510-71721, STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK/Jun 20, 2003 · N588FE · Doug MD11SDR 2003FA0000690Fitting · brokenRIGHT HAND AFT (T) FITTING BROKEN. THIS FITTING IS ONE OF FOUR THAT ATTACHES THE HORIZONTAL STABILIZER TO THE TAILBOOM. NO ABNORMAL VIBRATIONS. CAUSE UNKNOWN, NEW UNPROVEN MODIFICATIONS. AT 448 HOURS TT THIS STABILIZER HAS THE HIGHEST TIME ON THIS STC. SUJun 20, 2003 · N58000 · Aerosp SA315BSDR 03FDEA00933Structure · corrodedLEFT HORIZONTAL STAB UPPER CENTER PLANK 24L BORE FOUND CORROSION BEYOND EO 1-5510-7-5000 LIMITATIONS.Jun 20, 2003 · N588FE · Doug MD11SDR 03FDEA00935Structure · corrodedLEFT HORIZONTAL STAB UPPER AFT PLANK 30L BORE FOUND CORROSION BEYOND EO 1- 5510-7-5000 LIMITATIONS.Jun 20, 2003 · N588FE · Doug MD11SDR 2003FA0000803Brace · shearedPREFLT INSPECTION FOUND THE TERMINAL HOLDING THE LT FORWARD TAIL BRACE TO THE HORIZONTAL STABILIZER TO BE SHEARED OFF.Jun 15, 2003 · N190BA · Aviat A1ASDR 03FDEA00930Structure · corrodedHORIZONTAL STAB UPPER CENTER PLANK 26L BARREL NUT BORE FOUND CORROSION BEYOND EO 1-5510-7-5000 B PT1 LIMITATIONS. HORIZONTAL STAB CENTER PLANK 26L FITTING REMOVED AND REPLACED AS PER FEDEX EA 1-5510-71721, STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BOREJun 12, 2003 · N588FE · Doug MD11SDR QXEA200300746Shim · damagedPDX - SHIMS UNDER FORWARD RIGHT HAND MOUNT FOR HORIZONTAL STABILIZER HAVE EXTRUDED OUT. REPAIRED IAW TR 55-011, TASK 55-10-00-400-801, PAGE 6.Jun 11, 2003 · N408QX · Bombdr DHC8401SDR HEEA087134Panel · delaminatedFIBERGLASS CLOSE OUT BEHIND FITTING ASSEMBLY DELAMINATED FROM SPAR. REPAIRED.Jun 10, 2003 · N4253S · Skrsky S76ASDR CALA0300301Fitting · crackedINSPECTION FOUND A 4 INCH CRACK IN HORIZONTAL STABILIZER CENTER SECTION UPPER CROSS BEAM FITTING AT STA 1121, LBL 10. THE FITTING WAS REMOVED AND REPLACED IAW BOEING DRAWING 65-47598 AND SRM 51-40-2.Jun 9, 2003 · N70352 · Boeing 7373T0SDR CALA0300298Fitting · crackedINSPECTION FOUND A 1 INCH CRACK IN HORIZONTAL STABILIZER CENTER SECTION UPPER CROSS BEAM FITTING AT STA 1121, RBL 10. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-40-02, FIGURE 12, SHEET 2.Jun 8, 2003 · N70352 · Boeing 7373T0SDR QXEA200300744Shim · damagedPDX - SHIMS UNDER FORWARD RIGHT HAND MOUNT FOR HORIZONTAL STABILIZER HAVE EXTRUDED OUT. REPAIRED IAW RD 8/4-55-089.Jun 7, 2003 · N408QX · Bombdr DHC8401SDR DHL2003604671Attach Fitting · crackedLT HORIZONTAL STAB. FITTING WITH 1.000 CRACK IN IT AT FWD. LWR. SECTION STA. XFS.60.000. PERFORMED MAJOR REPAIR IAW SRM 55-1-0 PG.1, SRM 51-1-20D PG.9,21, SRM 51-1-21 PG.1. REMOVED CRACKED FITTING IAW SRM 51-1-21 PG.1. SRM 1-1-20D PG.21. CLEANED, TREATED, AND May 27, 2003 · N604AL · Doug DC873FSDR UPS03840745Cap · crackedINSPECTION TYPE:C-2 LT HORIZ STAB INBOARD LOWER CAP CRACKED. REMOVED LT HORIZ L/E CAP, PERFORMED HEFC IAW NDT SPM 06-10-001.01. LOCATED & DRILLED IAW DC8 SRM 51-1-24. INSTALLED NEW FITTING IAW DC8 SRM 51-1-21/51-1-20D.May 14, 2003 · N840UP · Doug DC873FSDR UPS03840744Cap · crackedINSPECTION TYPE: C-2, RT HORZ STAB INBOARD BOX LOWER CAP CRACKED. REMOVED RT HORZ LEADING EDGE CAP LOCATED & DRILLED NEW FITTING IAW DC8 SRM 51-1-21 & 51-1-20D.May 13, 2003 · N840UP · Doug DC873FSDR UPS03440774Web · crackedINSPECTION TYPE: C, EMP - LT HORIZONTAL STAB TIP FAIRING SUPPORT STRUCTURE VERTICAL WEB IS FOUND CRACKED AT APPROX 10 INCHES AFT OF HS REAR SPAR AT HSBL 421.5. EMP - LT HORIZONATAL STAB TIP FAIRING SUPPORT STRUCTURE VERTICAL WEB REPAIRED AS PER HX RS R55-13-May 13, 2003 · N521UP · Boeing 747200SDR 03FDEA00690Structure · corrodedHORIZONTAL STAB CENTER BOX RT 31R BORE EXISTING BUSHING REMOVED FOUND SIDEWALL AND BEARING SURFACE WITH CORROSION. REAM BORE TO 1.181 INCH MAX CORROSION STILL PRESENT ON SIDEWALL SURFACE. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5510-69213 - STABILIZERS - HORIMay 7, 2003 · N602FE · Doug MD11SDR 03FDEA00689Structure · corrodedHORIZONTAL STAB CENTER BOX LT 31L BORE EXISTING BUSHING REMOVED FOUND BORE SIDEWALL AND BEARING SURFACE WITH CORROSION. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5510-69213 - STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE REWORK/REPAIR.May 7, 2003 · N602FE · Doug MD11SDR UPS03840739Cap · crackedINSPECTION TYPE: C-2, LT HORZ STAB INBOARD BOX INSTALLATION FWD LOWER TEE CAP CRACKED AT OUTBOARD END STA XFS 47. REMOVED LT HORZ STAB INBOARD BOX T-CAP, REC'D NEW FITTING LOCATED, DRILLED NEW FITTING IAW DC8 SRM 51-1-24. INSTALLED NEW FITTING IAW DC8 SRM 5May 5, 2003 · N840UP · Doug DC873FSDR UPS03840738Cap · crackedINSPECTION TYPE: C-2, RT HORIZONTAL STAB INBD BOX INSTALLATION FWD LOWER TEE CAP CRACKED AT OUTBOARD END STA XFS 47. PERFORMED E/C INSP OF LOWER TEE CAP IAW NDT SPM 06-10-01.001 CRACKED AT RADIUS. REMOVED ANGLE LOCATED AND DRILLED NEW ANGLE IAW DC8 SRM 5 1-May 5, 2003 · N840UP · Doug DC873FSDR 03FDEA00659Structure · corrodedHORZ STABILIZER CENTER BOX LT NR 1 BARREL NUT HOLE FOUND WITH CORROSION. REAM BORE UP TO 1.549 INCH CORROSION STILL PRESENT ON THE SIDE OF BEARING SURFACE. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5510-69213 - STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BOApr 29, 2003 · N602FE · Doug MD11SDR USAA030059Fitting · crackedFOUND FITTING CRACKED 1.5 INCHES LONG, FITTING IN HORIZONTAL STABILIZER CENTER SECTION OF RIGHT THRUST BEAM. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR. (M)Apr 25, 2003 · N560AU · Boeing 737301SDR 03FDEA00620Fitting · corrodedHORIZONTAL STABILIZER CENTER BOX LT SIDE BARREL NUT HOLE NR 26 FOUND FITTING WITH CORROSION (BOTTOM & BEARING SURFACE). HORIZONTAL STABILIZER CENTER BOX LT SIDE BARREL NUT HOLE NR 26L FITTING REMOVED AND REPLACED AS PER FEDEX EA 1-5510-69219 - STABILIZERS -Apr 25, 2003 · N602FE · Doug MD11SDR QXEA0300503Shim · looseSHIM AT FORWARD RIGHT HAND HORIZONTAL STAB ATTACH FITTING IS MIGRATING. REPAIRED IAW DHC-8 400 AMM 55-10-00-400-801.Apr 21, 2003 · N407QX · Bombdr DHC8401SDR QXEA0300502Shim · looseSHIM AT FORWARD RT HORIZONTAL STAB ATTACH FITTING IS MIGRATING. REPAIRED IAW DHC-8 400 AMM TEMPORARY REVISION 55-10-00, PAGES 1-3.Apr 21, 2003 · N407QX · Bombdr DHC8401SDR QXEA0300511Shim · loosePDX - SHIM AT FORWARD RIGHT HAND HORIZONTAL STAB ATTACH FITTING IS MIGRATING. REPAIRED IAW DHC-8 400 AMM TEMPORARY REVISION 55-10-00, PAGE 3-5.Apr 21, 2003 · N407QX · Bombdr DHC8401SDR ASAA0380361Fairing · crackedOAK - DURING 15K CHECK, FOUND LEFT HORIZONTAL STAB FAIRING CRACKED AT ATTACH POINT. INSTALLED DOUBLER PER EA 5520-01156 AND SRM'S 51-10-3 AND 55-03. (M)Apr 18, 2003 · N947AS · Doug DC983SDR QXEA0300516Rib · bentRT HORIZONTAL STAB TIP FOR LEADING EDGE HAS A BENT RIB INSIDE TIP FAIRING. REPAIRED IAW HORIZON AIR EA 6-55-29.Apr 18, 2003 · N407QX · Bombdr DHC8401SDR CA030414002Insert · stripped(CAN) DURING SCHEDULED INSPECTION, REPLACING THE HORIZONTAL STAB AFT ATTACHMENT POINTS. WE REMOVED THE BOLTS THAT ATTACH TO THE CASTING TO GAIN ACCESS, THREE OF THE 12 BOLTS WOULD JUST SPIN IN PLACE.AFTER REMOVING THESE BOLTS WE FOUND THAT THE NUTS (INSERTS) Apr 14, 2003 · Beech B100SDR PCAA0304072Structure · separatedCREW REPORTED AIRFRAME VIBRATION OCCURED 3 TIMES ON APPROACH. FLIGHT ATTENDANT REPORTED A VERY LOUD VIBRATION IN FORWARD PART OF CABIN, AND NR 2 ENGINE NH INCREASED 1.5 PERCENT DURING VIBRATION PERIOD. EMERGENCY WAS DECLARED AND AIRCRAFT LANDED WITHOUT INCIDENApr 8, 2003 · N804EX · Dhav DHC8102SDR ABXA030161Cap · crackedHORIZONTAL STABILIZER LEFT LOWER T-CAP CRACKED AT OUTER TIP. REPAIRED AREA IAW DC-9 SRM 55-02.Apr 3, 2003 · N944AX · Doug DC931SDR SIMA200309603Housing · wornABI - DURING A IMBV INSPECTION, THE HORIZONTAL STABILIZER LEFT AND RIGHT SPHERICAL BEARING HOUSING WORN BEYOND LIMITS. REMOVED THE EXISTING BEARING FROM THE HOUSING. REAMED THE LEFT AND RIGHT HOUSING TO 2.2834 INCH. TREATED THE REWORK HOUSING AND INSTALLED Apr 2, 2003 · N643AE · Emb EMB145LRSDR SWAA030721Skin · crackedDURING SCHEDULED C2 CHECK, FOUND LT HORIZ STAB LOWER SKIN CRACKED AT FWD EDGE OF AFT SPAR. REPAIRED SKIN PER SRM.Mar 31, 2003 · N515SW · Boeing 7375H4SDR CALA0300160Skin · damagedWHILE PERFORMING A PERMANENT REPAIR OF THE LT HORIZONTAL STABILIZER LE SKIN AT LE STA 69.93 IN IAH PER SRM 55-10-01, FIGURE 203, MAINTENANCE NOTED THE REQUIRED FLUSH REPAIR WAS NOT APPLICABLE TO THIS AREA BECAUSE THE DAMAGED AREA WAS CLOSE TO A RIB. THE REPAIRMar 28, 2003 · N10323 · Boeing 7373T0SDR 03FDEA00354Rib · crackedLT HORIZONTAL STAB. INTERIOR RIB 5 UPPER CHORD AT REAR SPAR IS CRACKED AT HOISTING POINT WRITTEN ON FEDEX N/R N00494 UNDER MAE W/O NR 13350 CUT OUT DAMAGED SECTION IAW/SRM 51-71-50 FABRICATED REPAIR ANGLE OF 7075T6 BATCH NR 7R00115001 IAW/SRM 51-71-50 Mar 28, 2003 · N443FE · Airbus A310SDR JGV2003F00001Scissors · damagedWHILE PERFORMING, PHASE 5 INSPECTION, ITEM CODE: D274000, TASK: HORIZONTAL STABILIZER SCISSORS FREE PLAY CHECK, THE FREE PLAY WAS FOUND OUT OF LIMITS. THE UPPER AND LOWER SCISSORS( PN 62321809 & 10) WERE REMOVED TO REPLACE THE BUSHINGS IN EACH ASSEMBLY. THMar 27, 2003 · N77LX · Cessna 650SDR DHL2003741540Structure · crackedDURING C-CHECK DISCREPANCY AS FOLLOWS, EMPENNAGE INT'R STRUCTURE VERTICAL FIN HAS CRACK AT STR 8L FIN STA 133.8 AT THRU BOLT ATTACH ANGLE TO CHORD ANGLE. CUT OUT DAMAGED AREA DIM 7.75 INCH AND FABRICATED FILLER AND 2 EACH REPAIR ANGLES FROM BAC 1517-1367 PO 3Mar 25, 2003 · N741DH · Boeing 727200SDR DHL2003741536Structure · crackedDURING C-CHECK DISCREPANCY AS FOLLOWS, EMPENNAGE INT'R STRUCTURE VERTICAL FIN HAS CRACK AT STR 9L FIN STA 133.8 AT THRU BOLT ATTACH ANGLE TO CHORD ANGLE. CUT OUT DAMAGED AREA DIM 7.75 INCH AND FABRICATED FILLER AND 2 EACH REPAIR ANGLES FROM BAC1517-1367 PO 30Mar 25, 2003 · N741DH · Boeing 727200SDR 03FDEA00357Spar Cap · corrodedLT HORIZONTAL UPPER AFT SPAR CAP CORRODED APPROX. 4FT. FROM FUSELAGE. UNDER MAE W/O NO. 13350. REPAIRED AFT SPAR CAP IAW SRM 55-13-11 AND SRM 51-41-01. Mar 21, 2003 · N443FE · Airbus A310SDR 03FDEA00312Bracket · corrodedLT HORZONTAL STABILIZER LEADING EDGE ATTACH APRON IS HEAVILY CORRODED AT AFT UPPER "L" ANGLE. REMOVED AND REPLACED WITH ON SITE FABBRICATED PARTS.Mar 13, 2003 · N445FE · Airbus A310SDR ASAA0380237Channel · puncturedOKC - DURING 30K CHECK, FOUND RIGHT HORIZONTAL STABILIZER AFT SPAR HINGE CHANNEL SUPPORT PUNCTURED. REPLACED DAMAGED CHANNEL PER SRM. (M)Mar 7, 2003 · N935AS · Doug DC982SDR UPS03840317Fitting · crackedINSPECTION TYPE: C2, RT STAB I/B LEADING EDGE ANGLE FITTING IS CRACKED AT XRS 0. REMOVED AND REPLACED FITTING IAW DWG 3701427 AND SRM 51-1-20D, 51-1-21.Mar 4, 2003 · N880UP · Doug DC873FSDR 03FDEA00263Nut · corrodedRT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 23R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579Mar 4, 2003 · N585FE · Doug MD11SDR 03FDEA00244Nut · corrodedRT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 2R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.Mar 4, 2003 · N585FE · Doug MD11FSDR 03FDEA00245Nut · corrodedRT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 3R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.Mar 4, 2003 · N585FE · Doug MD11FSDR 03FDEA00246Nut · corrodedRT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 4R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.Mar 4, 2003 · N585FE · Doug MD11FSDR 03FDEA00247Nut · corrodedRT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 6R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.Mar 4, 2003 · N585FE · Doug MD11FSDR 03FDEA00248Nut · corrodedRT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 7R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.Mar 4, 2003 · N585FE · Doug MD11FSDR 03FDEA00249Nut · corrodedRT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 8R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.Mar 4, 2003 · N585FE · Doug MD11FSDR 03FDEA00250Nut · corrodedRT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 9R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.Mar 4, 2003 · N585FE · Doug MD11FSDR 03FDEA00251Nut · corrodedRT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 10R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.Mar 4, 2003 · N585FE · Doug MD11F
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