JASC 5514

Service difficulty reports · 2,805

Reports filed under 5514 · Horizontal Stabilizer Miscellaneous 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 = '5514'
  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 UPS04M42096Structure · corrodedINSPECTION TYPE:C HORIZONTAL STABILIZER RT NR 14 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, BEARING & SIDEWALL SURFACE. CORROSION ON BOTTOM REMOVED PER SRM 51-21-01 VOL 2 REV 34. MATERIAL REMOVED 0.010 INCH. BARREL NUT HOLE REPAIRED PER EN1025-04. BUSHING Feb 5, 2004 · N274UP · Doug MD11FSDR 373PA0024Pin · damagedDURING ACCOMPLISHMENT OF BOEING SB 737-55A1077 PART 2, FOUND CORROSION AROUND THREADS AND THREAD RELIEF ON RIGHT HORIZONTAL STABILIZER OUTER HINGE PIN. REPLACED INNER AND OUTER PINS PER SB737-55A1077 AND MM 27-41-31.Feb 2, 2004 · N373PA · Boeing 7373Y0SDR UPS04M42097Structure · corrodedINSPECTION TYPE:C HORIZONTAL STABILIZER BARREL NUT LEFT NR 36 HOLE FOUND CORROSION ON FWD & AFT WALL & GOUGE MARK ON O/B WALL DURING INSPECTION. HOLE BOTTOM SURFACE CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34. MATERIAL REMOVED 0.125 INCH. BARREL NUT HOLJan 29, 2004 · N274UP · Doug MD11FSDR AWXA200400176Clevis · corrodedDURING C-18 CHECK INTERGRANULAR CORROSION WAS FOUND ON RT HORIZONTAL STABILIZER FORWARD CLEVIS, AT FORWARD LOWER FACE BS 1088, WL 256, RBL 30. MAINTENANCE REMOVED BUSHING FROM RT HORIZONTAL STABILIZER FORWARD CLEVIS; OVERSIZED CENTER SECTION CLEVIS FORWARD LOWJan 20, 2004 · N324AW · Boeing 737301SDR AWXA200400177Clevis · corrodedDURING C-18 CHECK INTERGRANULAR CORROSION WAS FOUND ON RT HORIZONTAL STABILIZER FORWARD LOWER ATTACH POINT AT CENTER SECTION FITTING AFT CLEVIS, AFT FACE BS 1088, WL 256, RBL 30. MAINTENANCE REMOVED BUSHING FROM RT HORIZONTAL STABILIZER FORWARD LOWER ATTACH POJan 6, 2004 · N324AW · Boeing 737301SDR COOSDR030032Attach Fitting · corrodedLT HORIZONTAL STABILIZER FRONT SPAR, LOWER ATTACH LUG SURFACE CORRODED.Jan 1, 2004 · N318FL · Boeing 737300SDR CALA0300718Fitting · corrodedINSPECTION FOUND RT HORIZONTAL STABILIZER AFT UPPER ATTACH, FWD ATTACH LUG CORRODED AROUND BUSHING AND FACE OF LUG. REMOVED BUSHING AND FOUND CORROSION ON ID AND BOTH FACES. SPOT FACED 0.012 INCH AND REAMED BORE ID TO 1.530 INCH. FABRICATED AND INSTALLED OVDec 22, 2003 · N76354 · Boeing 7373T0SDR CALA0300717Fitting · corrodedINSPECTION FOUND LT HORIZONTAL STABILIZER ATTACH LUG FWD UPPER BUSHING FACE PITTED. REMOVED BUSHING AND FOUND CORROSION ON AFT FACE. SPOT FACED 0.023 INCH AND INSTALLED NEW BUSHING PER SRM 55-10-10.Dec 22, 2003 · N76354 · Boeing 7373T0SDR CALA0300716Fitting · corrodedINSPECTION FOUND LT HORIZONTAL STABILIZER AFT UPPER ATTACH FWD LUG CORRODED AROUND BUSHING AND FACE OF LUG. REMOVED BUSHING, FOUND CORROSION ON ID AND BOTH FACES. SPOT FACE 0.013 INCH DEEP AND REAMED BORE ID TO 1.5795 INCH. FABRICATED AND INSTALLED OVERSIZEDec 22, 2003 · N76354 · Boeing 7373T0SDR C2XA03TY205Bearing · wornDURING A SCHEDULED INSPECTION BOTH HORIZONTAL STABILIZER SPHERICAL BEARING WERE FOUND TO BE WORN BEYOND SERVICE LIMITS. MAINTENANCE REMOVED AND REPLACED THE SPHERICAL BEARINGS IAW EMB MM 55-37-00 AND EC 5510-01070. AIRCRAFT RELEASED FOR SERVICE.Dec 7, 2003 · N22971 · Emb EMB145SDR CALA0300684Bushing · corrodedFORWARD LEFT LOWER HORIZONTAL STAB CENTER SECTION FORWARD CLEVIS HAS PITTING CORROSION AT BUSHING ON FORWARD FACE. REPAIRED AND REPLACED OVERSIZE BUSHING PER SRM 55-10-10.Dec 2, 2003 · N16649 · Boeing 737524SDR CALA0300683Bushing · corrodedFORWARD LEFT UPPER STAB CENTER SECTION FORWARD CLEVIS HAS PITTING CORROSION AT THE BUSHING ON FORWARD EDGE. REPAIRED AND REPLACED OVERSIZE BUSHING PER SRM 55-10-10.Dec 2, 2003 · N16649 · Boeing 737524SDR CALA0300682Bushing · corrodedCORROSION ON FORWARD UPPER HORIZONTAL STAB CENTER SECTION LUG AFT CLEVIS ON AFT FACE AT BUSHING. REPAIRED AND REPLACED OVERSIZE BUSHING PER SRM 55-10-10.Dec 2, 2003 · N16649 · Boeing 737524SDR 03FDEA01957Structure · corrodedHORIZONTAL STAB LEFT UPPER CENTER PLANK NR 26L BARREL NUT BORE FITTING FOUND CORROSION ON BEARING SIDEWALL SURFACES BEYOND EO 1-5510-7-5000 LIMITATIONS. NEW 26L FITTING FABRICATED AS PER DWG ALC8107 AND EA 1-5510-74245, STABILIZERS - HORIZONTAL STABILIZER -Nov 19, 2003 · N583FE · Doug MD11SDR 03FDEA01928Structure · corrodedHORIZONTAL STAB RIGHT UPPER FWD PLANK NR 2R BARREL NUT BORE FOUND CORROSION ON BOTTOM & SIDEWALL SURFACE BEYOND EO 1-5510-7-5000 LIMITATIONS. COMPLIED WITH FEDEX EA 1-5510-74245, STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE REWORK/ REPAIR - 1-5510-7-Nov 17, 2003 · N583FE · Doug MD11SDR QXEA200301460Skin · damagedLEFT HAND AILERON OUTBOARD TIP HAS HOLE IN FIBER. REPAIRED IAW DHC-8 SRM 51-20-61, 51-30-70, 51-20-26 AND 57-60-71.Nov 4, 2003 · N349PH · Dhav DHC8202SDR UPS03841514Fitting · crackedINSPECTION TYPE:C2 T-CHORD CRACKED, RT HORIZONTAL STAB INBOARD FRONT SPAR LOWER OUTBOARD CORNER AT XFS 60. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D, 51-1-21, 51-3-0 AND DWG 3701427.Oct 22, 2003 · N867UP · Doug DC873FSDR DL73S030927Web · wornFOUND ON R1 LETTER CK,OUTBOARD BALANCE BAY I/B WEB CHAFED THRU AT LT HORIZ STAB. REPAIRED PER SRM 51-40-20 FIG 11.Oct 14, 2003 · N377DL · Boeing 737247SDR AUS20031034Bolt · corroded(AUS) STABILATOR BALANCE WEIGHT ATTACHMENT BOLTS AND ACTUATOR COLLAR ATTACHMENT BOLTS CORRODED (RUSTED). BOLT PART NUMBERS PN AN175-32A AND PN AN175-33A.Oct 13, 2003 · Piper PA23250SDR AWXA200301221Shield · crackedDURING C-17 CHECK A 1 INCH CRACK WAS FOUND ON LT HORIZONTAL STABILIZER PANEL (9123) METAL SHIELD (BLADE), AT STAB STA 67.54, STAB LBL 21.75. MAINTENANCE REMOVED CRACKED LT HORIZONTAL STAB BLADE, AT STAB STA 67.54, STAB LBL 21.75; FABRICATED A NEW REPLACEMENT Sep 20, 2003 · N326AW · Boeing 737301SDR AUS20030883Fitting · cracked(AUS) HORIZONTAL STABILIZER PITCH TRIM ACTUATOR UPPER ATTACHMENT BRACKETS CRACKED ALONG LUG. FURTHER INVESTIGATION REVEALED THAT THERE WAS CONSIDERABLE CLEARANCE BETWEEN THE BUSHINGS AND ACTUATOR ROD ENDS WHICH RESULTED IN THE LUGS BEING STRESSED WHEN THE ATTAAug 30, 2003 · Swrngn SA227ACSDR CALA0300481Bushing · corrodedINSPECTION FOUND RT HORIZONTAL STABILIZER CENTER SECTION FRONT SPAR LOWER FORWARD LUG PITTED AT BUSHING. THE BUSHING WAS REMOVED AND REPLACED IAW CMM 55-10-06.Aug 22, 2003 · N14645 · Boeing 737524SDR CALA0300480Bushing · corrodedINSPECTION FOUND LT HORIZONTAL STABILIZER CENTER FORWARD SPAR LOWER AFT LUG PITTED AT BUSHING. A NEW BUSHING WAS INSTALLED IAW CMM 55-10-06.Aug 22, 2003 · N14645 · Boeing 737524SDR CALA0300459Attach Angle · crackedINSPECTION FOUND A 6 INCH CRACK IN ATTACH ANGLE ON HORIZONTAL STABILIZER CENTER SECTION AT UPPER BEAM. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02.Aug 10, 2003 · N70330 · Boeing 7373T0SDR CALA0300440Bushing · corrodedINSPECTION FOUND LT HORIZONTAL STABILIZER UPPER FORWARD LUG CORRODED AROUND BUSHING. THE BUSHING WAS REMOVED AND REPLACED IAW SRM 55-10-10.Aug 6, 2003 · N17640 · Boeing 737524SDR CALA0300438Bushing · corrodedINSPECTION FOUND RT HORIZONTAL STABILIZER UPPER FORWARD LUG CORRODED AROUND BUSHING. THE BUSHING WAS REMOVED AND REPLACED IAW SRM 55-10-10.Aug 5, 2003 · N17640 · Boeing 737524SDR 03FDEA01191Structure · corrodedRIGHT HORIZONTAL STABILIZER UPPER AFT PLANK NR 35R BARREL NUT BORE FOUND CORROSION BEYOND EO 1-5510-1-5000 LIMITATIONS. RIGHT HORIZONTAL STABILIZER UPPER AFT PLANK NR 35R BARREL NUT BORE REPAIR CARRIED-OUT AS PER FEDEX EA 1-5510-69402 - STABILIZERS - HORIZONTJul 28, 2003 · N605FE · Doug MD11SDR UPS03841096Attach Angle · crackedINSPECTION TYPE:C2 RT HORIZONTAL STAB. FRONT SPAR AT STA. XFS322. RIB ATTACH ANGLE IS CRACKED REMOVED, FABRICATED AND REPLACED ATTACH ANGLE I.A.W. DWG.4653025 AND SRM. 51-1-20D.Jul 24, 2003 · N874UP · Doug DC873FSDR UPS03841022Angle · crackedINSPECTION TYPE:C2 LEFT HORIZONTAL STAB AT XFS 32 L-ANGLE IS CRACKED. REMOVED AND REPLACED ANGLE IAW DWG 5654501 AND SRM 51-1-20D, 51-1-21.Jul 23, 2003 · N874UP · Doug DC873FSDR QXEA200300817Shim · missingPDX - HORIZONTAL STABILIZER TO VERTICAL STABILIZER FORWARD LEFT CONNECTION POINT SHIMS/SPACERS COMPLETELY EXTRUDED/MISSING. REPAIRED IAW SRM 51-23-00 AND RD 8/4-55-094.Jul 9, 2003 · N410QX · Bombdr DHC8401SDR QXEA200300818Shim · damagedPDX - H-STAB TO V-STAB FORWARD RIGHT HAND CONNECTION POINT SHIMS/SPACERS IS EXTRUDED. REPAIRED IAW DHC-8-S00 T/R 55-011, TASK 55-10-00-400-801 AND RD 8/4-55-094.Jul 9, 2003 · N410QX · Bombdr DHC8401SDR QXEA200300833Shim · damagedPDX - H-STAB TO V-STAB FORWARD RIGHT HAND CONNECTION POINT SHIMS/SPACER IS EXTRUDING. REPAIRED IAW Q400 AMM 55-10-010, TASK 55-10-00-000-801 AND RD 8/4-55-094.Jul 7, 2003 · N410QX · Bombdr DHC8401SDR 03FDEA01071Structure · corrodedRT HORIZONTAL STABILIZER NR 2 BORE CORROSION EXCEEDED CONDITION 3. CORROSION ON RT HORIZONTAL STABILIZER NR 2 BORE REMOVED AND REPAIR CARRIED OUT IAW EA NR 1-5510-71832.Jul 7, 2003 · N582FE · Doug MD11SDR CALA0300365Hinge Pin · corrodedINSPECTION FOUND EXTERIOR OF INNER PIN AND BORE OF OUTER HINGE PIN FOR HORIZONTAL STABILIZER CORRODED. THE INNER PIN AND OUTER HINGE PIN ASSEMBLY WERE REMOVED AND REPLACED IAW EA 5550-01315 AND MM 27-41-31.Jul 7, 2003 · N17644 · Boeing 737524SDR 03FDEA01044Fitting · corrodedLEFT HORIZONTAL STABILIZER NR 26 BORE CORROSION EXCEEDED LIMIT. LEFT HORIZONTAL STABILIZER NR 26 FITTING FABRICATED IAW FEDEX EA 1-5510- 71836, STABILIZERS- HORIZONTAL STABILIZER BARREL NUT BORES- CORROSION REMOVAL- BORE 26 LEFT- FITTING ALC8107-1- FABRICATJul 5, 2003 · N582FE · Doug MD11SDR 03FDEA01042Structure · corrodedLEFT HORIZONTAL STABILIZER NR 4 BORE CORROSION EXCEEDED LIMIT AFTER REWORKED. CORROSION ON LEFT HORIZONTAL STABILIZER NR 4 BORE REMOVED AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5510-69395, TITLE: STABILIZERS- HORIZONTAL STABILIZER BARREL NUT BORES- CORROSIONJul 4, 2003 · N582FE · Doug MD11SDR 03FDEA01041Structure · corrodedLEFT HORIZONTAL STABILIZER NR 2 BORE CORROSION EXCEEDED LIMIT AFTER REWORKED. CORROSION ON LEFT HORIZONTAL STABILIZER NR 2 BORE REMOVED AND REPAIRED CARRIED OUT AS PER EA 1-5510-69394 (TITLE : STABILIZERS - HORIZONTAL STABILIZER BARREL NUT BORES - CORROSIONJul 4, 2003 · N582FE · Doug MD11SDR DHL2003873534Angle · crackedRT HORIZONTAL STABILIZER INNER ANGLE CRACKED AT XFS.47.500. REMOVED CRACKED ANGLE IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED NEW ANGLE IAW SRM 55-2-0 PG 7-8. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW ANGJun 27, 2003 · N873SJ · Doug DC873FSDR QXEA200300804Shim · damagedPDX - PEEL SHIMS EXTRUDING AT RIGHT HAND FORWAD V-STAB TO H-STAB CONNECTION POINTS. REPAIRED IAW Q400 AMM TASK 55-10-60-000-801, PAGE 3, PARAGRAPH 3.Jun 24, 2003 · N411QX · Bombdr DHC8401SDR EIA2003083Attach Fitting · corrodedCORRSION ON UPPER SKIN TO STR ATTACH AREA IN RT HAND HORIZONTAL INTERIOR MAIN BOX 5 INCHES INBOARD OF RIB AT STAB STATION 235 ON 5TH STR AFT OF FWD SPAR ON FWD END. REMOVED DAMAGE, NDT AREA, FABRICATED AND INSTALLED REPAIR PER ECRA478-55-1582.Jun 14, 2003 · N478EV · Boeing 747SR46SDR 03FDEA00853Structure · corrodedSNRM N0938 - RT HORZ STAB BARREL NUT BORE NR 35 CORROSION BLEND OUT, OUT OF LIMIT. CORRECTIVE ACTION: SNRM N0938: RH HORIZONTAL STABILIZER BARREL NUT BORE NR 35 CORROSION BLEND OUT AREA CARRIED-OUT REPAIR AS IAW EA 1-5510-71716 - STABILIZER - HORIZONTAL STABJun 2, 2003 · N595FE · Doug MD11SDR DHL2003604568Angle · crackedLT HORIZ STAB INNER ANGLE CRACKED 1.000 AT XFS.30.500. REMOVED CRACKED ANGLE IAW SRM 51-1-21 PG 1. FABRICATED NEW ANGLE IAW SRM 55-1-0 PG 1. PERFORMED HEAT TREATMENT TO NEW ANGLE IAW SRM 51-1-1 PG 11,13. CLEANED, TREATED AND PRIMED AREA AND NEW ANGLE IAW SRM May 23, 2003 · N604AL · Doug DC873FSDR QXEA200300613Shim · damagedPDX - SHIMS BETWEEN FORWARD, LEFT HAND, H-STAB TO V-STAB ATTACH POINT ARE EXTRUDING. REPAIRED IAW Q400 AMM TASK 55-10-00-400-801.May 8, 2003 · N409QX · Bombdr DHC8401SDR QXEA200300612Shim · damagedPDX - SHIMS BETWEEN FORWARD, RT HAND H-STAB TO V-STAB ATTACH POINT HAVE COMPLETELY EXTRUDED. REPAIRED IAW Q400 AMM TASK 55-10-00-400-801.May 8, 2003 · N409QX · Bombdr DHC8401SDR QXEA200300588Shim · damagedPDX - SHIMS BETWEEN FORWARD LEFT HAND H-STAB TO V-STAB ATTACH POINTS ARE EXTRUDING. REPAIRED IAW HORIZON AIR EA 6-55-31.May 8, 2003 · N409QX · Bombdr DHC8401SDR QXEA200300587Shim · damagedPDX - SHIMS BETWEEN FORWARD RIGHT HAND H-STAB TO V-STAB ATTACH POINTS HAVE COMPLETELY EXTRUDED. REPAIRED IAW HORIZON AIR EA 6-55-31.May 8, 2003 · N409QX · Bombdr DHC8401SDR DHL2003804536Rib · crackedITEM REF. N/R 1430 PERFORMED MAJOR REPAIR IAW SRM 55-1-0 PG.1 . REMOVED UPPER CAP-AFT DAMAGED RIB IAW SRM51-1-21 PG. 1 , FABRICATED UPPER CAP-AFT RIB (7075-T6)IAW ATM 5-19-00 , DWG. 5654192-1. CLEANED, TREATED AND PRIMED IAW SRM51-1-8B. INSTALLED NEW UPPER CAFeb 12, 2003 · N804DH · Doug DC873FSDR 2003F00464Bearing · crackedAT C-CHECK, FOUND CRACK ON VERTICAL STAB, LEFT HORIZONTAL STAB HINGE BEARING. REMOVED AND REPLACED VERTICAL STAB, LEFT HORIZONTAL STAB HINGE BEARING. (M)Jan 24, 2003 · N7643U · Boeing 727222SDR 2003F00452Hinge Pin · corrodedAT C-CHECK, FOUND HORIZONTAL STAB, RIGHT OUTER HINGE PIN IS GALLED AND PITTED. REMOVED AND REPLACED HORIZONTAL STAB RIGHT OUTER HINGE PIN. (M)Jan 24, 2003 · N7643U · Boeing 727222SDR 2003F00450Hinge Pin · corrodedAT C-CHECK, FOUND HORIZONTAL STAB, LEFT INNER HINGE PIN, HAS CORROSION ON THREADED END. REMOVED AND REPLACED HORIZONTAL STAB LEFT INNER HINGE PIN. (M)Jan 24, 2003 · N7643U · Boeing 727222
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