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 UPS01236300Skin · corrodedINSPECTION TYPE:C CORROSION OF RH STAB SKIN UPPER SURFACE & RIVET PULLED @ STAB STA 80 APPROX FWD OF REAR SPAR ***CPCP*** REPAIR CARRIED OUT IAW SRM 55-10-3Jul 2, 2001 · N909UP · Boeing 72727CSDR SWAA011944Skin · crackedDURING SCHEDULED D CHECK, FOUND RH HORIZ STAB LOWER SKIN CRACKED AT STA 124. REPAIRED SKIN PER SWA ACO.Jun 25, 2001 · N521SW · Boeing 7375H4SDR 01FDEA00544Stabilizer · corrodedN 409 L/H HORZ STAB UPR TRAILING EDGE BEAM HAS CORROSION 71" FROM O/B END. ** S/D ** R&R PER FEDEX EA 7-5510-57288.Jun 14, 2001 · N242FE · Boeing 727277SDR UPS01836133Fitting · crackedINSPECTION TYPE:C2,3 RIGHT HORIZONTAL STAB T-FITTING AT I/B LOWER SECTION FWD OF FRONT SPAR IS CRACKED AT APPROX 47.5. REMOVED AND REPLACED FITTING IAW DWG 3701427 AND SRM 51-1-20D, 51-1-21.Jun 7, 2001 · N705UP · Doug DC871FSDR 2001FA0000052Plate · corrodedDURING ANNUAL INSPECTION, UPPER AND MID RUDDER ATTACH FITTING PLATES (THESE CONTAIN THE BEARINGS) WERE FOUND TO BE SEVERELY EXFOLIATED. THE UPPER RUDDER ATTACH PLATE EXFOLIATED TO THE POINT THAT THE ATTACH POINT HAD FAILED. THE RUDDER COULD BE MOVED APPROXIMJun 6, 2001 · N19CR · Beech 65B80SDR ASAA0140086Attach Fitting · gougedSEA - DURING C-CHECK, FOUND RIGHT HORIZONTAL STABILIZER AFT SPAR ATTACH FITTING UPPER LUG ON FUSELAGE GOUGED. REPAIRED IAW ENGINEERING AUTHORIZATION. (M)Jun 4, 2001 · N755AS · Boeing 7374Q8SDR 01FDEA00426Cap · crackedLEFT HORZ STAB SSI CARD INSP FOUND BS XFS & 166, CTR I/B LEADING EDGE ON O/B TEE CAP. REMOVED AND REPLACED TEE CAP PER IAW DC10 SRM 51-30-01.Jun 1, 2001 · N301FE · Doug DC1030FSDR USAA010595Hinge Fitting · corrodedCLT - FOUND STAB HINGE FITTING CORRODED APPROXIMATELY 1 SQUARE INCH AREA, RIGHT CENTER SECTION, REAR SPAR, LOWER ATTACH POINT LUG. CORROSION REMOVED, LUG REWORKED PER EA 69577. (M)May 31, 2001 · N284AU · Boeing 7372B7SDR USAA010594Hinge Fitting · corrodedCLT - FOUND STAB HINGE FITTING CORRODED APPROXIMATELY 1.5 SQUARE INCH AREA, RT CENTER SECTION FORWARD LOWER ATTACH INBOARD CLEVIS, OUTBOARD FACE. CORROSION REMOVED, LUG REWORKED PER EA 69577. (M)May 31, 2001 · N284AU · Boeing 7372B7SDR QXEA0101024Structure · damagedYYC - STRUCTURE CRACKED AT RIVET ON RIGHT HAND SIDE. REPAIRED IAW FOKKER SRM 55-02-07, FIGURE 2 AND CHAPTER 51.May 31, 2001 · N481US · Fokker F28MK4000SDR USAA010589Hinge Fitting · corrodedCLT - FOUND STABILIZER HINGE FITTING CORRODED 1 SQUARE INCH, LEFT HORIZ STAB REAR SPAR, LOWER ATTACH POINT LUG. REWORKED PER EA 69633. (M)May 31, 2001 · N284AU · Boeing 7372B7SDR CA010627057Gusset · cracked(CAN) WHILE CARRYING OUT A ROUTINE INSPECTION (PHASE C6-1200HRS) ON THE HORIZONTAL STABILIZER "GUSSET" A CRACK WAS DISCOVERED IN THE GUSSET ERNINATING FROM THE EDGE OF THE LIGHTENING HOLE. THE INSPECTION SPECIFIES SCRUTINY OF THESEGUSSETS FOR CRACKS ON AIRCRAFMay 29, 2001 · Lear 35LEARSDR 2001F00090Hinge Bracket · corrodedDURING SCHEDULED MAINTENANCE, RIGHT CENTER ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANNULAR CORROSION. REMOVED AND REPLACED RIGHT ELEVATOR CENTER HINGE BRACKET. (M)May 25, 2001 · N1568W · Beech 1900CSDR CA010628022Channel · cracked(CAN) PREVIOUS FILED SDR FOR CRACKED STABILIZER- HINGE REINFORCMENT P/N 0732101-4 AFTER REMOVAL OF THE REINFORCEMENT CH-RT WAS FOUND CRACK IN P/N 0732602-2/1232114-1 CRACK IN 07323603-1. LOWER RADIUS LT SIDE STA 6 INCH. LENGTH OF COACH I".May 18, 2001 · Cessna A185FSDR AWXA0001728Hinge Fitting · damagedLEFT HORIZONTAL STABILIZER OUTBOARD RIB NR 6 HINGE MOUNT HAS 2 ELONGATED HOLES. REPAIRED HINGE FITTING IAW AWA ER 03-5510-01124-TB1.May 14, 2001 · N158AW · Boeing 7373G7SDR AALA20011027Beam · corrodedTUL - FOUND CORROSION ON HORIZONTAL STABILIZER UPPER T/E BEAM 2 PLACES, 4 INCHES BY 1 INCH AND 5 INCHES BY 1 INCH. BLENDED OUT CORROSION AND INSTALLED 2024T3.063 DOUBLER PER ESO 11697 DATED 5-10-01. (M)May 10, 2001 · N718AA · Boeing 727227SDR AUS20010425Hinge · misinstalled(AUS) LT AND RT HORIZONTAL STABILISER OUTBOARD HINGES FITTED WITH ONLYTWO RIVETS ON THE TOP AND BOTTOM WHEN THE PIPER MODIFICATION KITPNO 766-646 WHEN THE CORRECT NUMBER SHOULD BE FOUR RIVETS.PERSONNEL/MAINTENANCE ERROR.May 7, 2001 · Piper PA31350SDR AWXA0001672Bushing · wornPLATING WORN ON LT HORIZ STAB LOWER AFT ATTACH BUSHINGS (ON STAB) BS 1145. REMOVED BUSHINGS IAW CMM 55-10-06. CLEANED LUG AND SLEEVE, FOUND NO CORROSION OR DAMAGE. TREATED AND PRIMED IAW SRM 51-20-01; NDT VERIFIED NO CRACKS. INSTALLED FABBED BUSHINGS, SEALMay 1, 2001 · N309AW · Boeing 7373G7SDR AWXA0001671Bushing · wornPLATING WORN ON LT HORIZ STAB FWD UPPER ATTACH BUSHINGS (ON STAB) BS 1100. REMOVED BUSHINGS IAW CMM 55-10-06. CLEANED LUG AND SLEEVE, FOUND NO CORROSION OR DAMAGE. TREATED AND PRIMED IAW SRM 51-20-01; NDT VERIFIED NO CRACKS. INSTALLED FABBED BUSHINGS, SEALMay 1, 2001 · N309AW · Boeing 7373G7SDR AWXA0001670Bushing · wornPLATING WORN ON LT HORIZ STAB FWD LOWER ATTACH BUSHINGS (ON STAB) BS 1100. REMOVED BUSHINGS IAW CMM 55-10-06; CLEANED LUG AND SLEEVE, FOUND NO CORROSION OR DAMAGE. TREATED AND PRIMED IAW SRM 51-20-01; NDT VERIFIED NO CRACKS. INSTALLED FABBED BUSHINGS, SEALEMay 1, 2001 · N309AW · Boeing 7373G7SDR AWXA0001669Bushing · wornPLATING WORN ON LT HORIZ STAB CENTER AFT ATTACH BUSHINGS (ON STAB) BS 1145. REMOVED BUSHINGS IAW CMM 55-10-06. CLEANED SLEEVES - FOUND NO CORROSION OR DAMAGE; TREATED AND PRIMED IAW SRM 51-20-01; NDT VERIFIED NO CRACKS. INSTALLED FABBED BUSHINGS, SEALED ANDMay 1, 2001 · N309AW · Boeing 7373G7SDR AWXA0001665Bushing · wornPLATING WORN ON LT HORIZ STAB UPPER AFT ATTACH BUSHING (ON STAB) BS 1145. REMOVED BUSHING IAW CMM 55-10-06; CLEANED LUG AND SLEEVE; FOUND NO DAMAGE OR CORROSION. TREATED AND PRIMED AREA IAW SRM 51-20-01; NDT NOTED NO CRACKS. INSTALLED FABBED BUSHING, SEALEDMay 1, 2001 · N309AW · Boeing 7373G7SDR CALA0100425Bearing · wornRIGHT HORIZONTAL STAB SUPPORT BEARING HAS EXCESSIVE PLAY AND BOLT CORRODED. REMOVED HORIZONTAL STAB, REMOVED AND REPLACED STAB ATTACH PLATE BUSHINGS AND BEARINGS. REMOVED AND REPLACED HINGE PLATES PER 55-10-00 AND CARD 08-5530-1-0006.Apr 27, 2001 · N16806 · Doug DC982SDR USAA010467Gusset · crackedCLT - FOUND GUSSET/ANGLE CRACKED 6 INCHES, HORIZONTAL STABILIZER CENTER SECTION, INT SEC OF BEAMS INBOARD SIDE UP CHORD. INSTALLED REPAIR DOUBLER. (M)Apr 25, 2001 · N374US · Boeing 7373B7SDR USAA010466Gusset · crackedCLT - FOUND GUSSET/FITTING CRACKED .5 INCH, HORIZONTAL STABILIZER CENTER SECTION, AFT LEFT INT SECTION OF BEAMS. FABRICATED NEW ANGLE PER BOEING DRAWING 65-47598, INSTALLED PER SRM 51-40-02 AND 03. (M)Apr 25, 2001 · N374US · Boeing 7373B7SDR MALA010474Structure · damagedDURING C-CHECK, TOOL MARK AND/OR ELONGATED HOLE AT RT HORIZONTAL STABILIZER AT THE FORWARD SPAR. AINTENANCE COMPLIED WITH MESABA EO AD991921-03 HORIZONTAL STAB FWD SPAR COLDWORKING.Apr 25, 2001 · N427XJ · Saab 340BSDR RRXA11096Fairing · chafedDURING A MAINTENANCE VISIT FOUND CHAFING DAMAGE TO LT HORIZONTAL STAB LOWER FAIRING, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-0 FIG#6 AND DHSK 996-102.Apr 24, 2001 · N996CF · Doug DC862FSDR 2001F00089Hinge Bracket · corrodedDURING SCHEDULED MAINTENANCE, LEFT CENTER ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANNULAR CORROSION. REMOVED AND REPLACED LEFT ELEVATOR CENTER HINGE BRACKET. (M)Apr 24, 2001 · N199GA · Beech 1900SDR 2001F00088Hinge Bracket · corrodedDURING SCHEDULED MAINTENANCE, RIGHT OUTBOARD ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANNULAR CORROSION. REMOVED AND REPLACED RIGHT ELEVATOR OUTBOARD HINGE BRACKET. (M)Apr 24, 2001 · N199GA · Beech 1900SDR USAA010446Angle · crackedCLT - FOUND GUSSET/ANGLE CRACKED, HORIZ STAB CENTER SECTION, LEFT, THRUST BEAM INBOARD LOWER CHORD. INSTALLED DOUBLER PER SRM 51-10-2. (M)Apr 24, 2001 · N374US · Boeing 7373B7SDR HEEA072767Structure · crackedCRACKED.Apr 23, 2001 · N854PH · Snias AS350BSDR AALA20010845Beam · corrodedTUL - FOUND LEFT HORIZONTAL T/E BEAM CORRODED AT OUTBOARD END. REMOVED CORROSION AND INSTALLED DOUBLER PER ESO 11697 DATED 4/17/01. (M)Apr 18, 2001 · N890AA · Boeing 727223SDR 20010514CW004Stabilizer · bentDURING INSTALLATION OF RIGHT HAND ELEVATOR, IT WAS DISCOVERED THAT WHEN THE ELEVATOR WAS MOVED FROM FULL DOWN TO FULL UP, THE STABILIZER WOULD FLEX UPWARD .4375. INVESTIGATION DISCLOSED THAT THE STABILIZER WAS BENT DOWN 2 DEGREES AT THE CENTER HINGE( BOTH Apr 18, 2001 · N1848W · Beech 95B55SDR CA010510009Bracket · cracked(CAN) 2 CRACKS FOUND AT WELDED EDGE.2 CRACKS FOUND AT ANCHOR NUT HOLE.1 CRACK WELD CRACKED. 1 CORNER NOT WELDED.Apr 16, 2001 · Cessna 152SDR AALA20010931Casting · corrodedTUL - FOUND HORIZONTAL STABILIZER SPREADER CASTING IS CORRODED BEYOND LIMITS, YV 222.4321. REMOVED AND REPLACED HORIZONTAL STABILIZER SPREADER CASTING PER SRM 51-01. (M)Apr 11, 2001 · N7517A · Doug DC982SDR UPS01835643Skin · crackedINSPECTION TYPE:C2,3 LEFT HORIZONTAL STAB. L/E. SKIN IS CRACKED AND DENTED BEYOND LIMITS XFS 150. REPAIRED SKIN I.A.W. SRM. 55-2-1 FIG. 4Apr 11, 2001 · N797UP · Doug DC871FSDR ABXA010127Support Fitting · crackedTHE RIGHT HORIZONTAL STABILIZER SUPPORT FITTING WAS CRACKED ABOVE AND AFT OF THE ELEVATOR CONTROL VALVE ON THE ELEVATOR TRAILING EDGE. MAINTENANCE INSPECTED AND REPLACED THE FITTING IAW DC-9 SRM 51-30-2.Apr 11, 2001 · N968AX · Doug DC941SDR CA010424003Rib · cracked(CAN) DURING INSPECTION STABILIZER RIB 0432001-46 LT, CRACKED.Apr 9, 2001 · Cessna 152SDR 20010501CW004Bracket · corrodedDURING ANNUAL INSPECTION FOUND EXFOLIATION ON RIGHT HORIZONTAL STAB ATTACH BRACKET.Apr 5, 2001 · N59299 · Cessna 210LSDR USAA010365Beam · crackedCLT - FOUND THRUSTBEAM CRACKED 4 INCHES, HORIZONTAL STAB CENTER SECTION, RIGHT THRUST BEAMS. REPLACED THRUST BEAM SRM 51-10-02 AND 51-40-02. (M)Apr 5, 2001 · N374US · Boeing 7373B7SDR USAA010353Support · damagedCLT - FOUND WEB SUPPORT WITH .5 INCH BULGE, HORIZ STAB JACKSCREW LOWER WEB SUPPORT, STATION 1088, LBL 4. INSTALLED WEB DOUBLER AND FILLER PER EA 69281. (M)Apr 4, 2001 · N249US · Boeing 737201SDR 20010507CW013Cap · corrodedLOWER CAP LEFT STABILIZER OUTER 6 IS CORRODED.Apr 4, 2001 · N172GA · Beech 1900CSDR CA010409020Bracket · cracked(CAN) FOUND DURING INSPECTION FOR 80-11-04 NUTPLATES FOR CRACKS, ALSO TRANSPORT CANADA SDA AV-2000-06.Mar 26, 2001 · Cessna 152SDR CA010409018Bracket · cracked(CAN) FOUND DURING INSPECTION FOR 80-11-04 NUTPLATES FOR CRACKS, ALSO TRANSPORT CANADA SDA AV-2000-06.Mar 26, 2001 · Cessna 152SDR ERKR200100069Hinge · corrodedREPAIR - CORROSION, HORIZONTAL STABILIZER HINGE - SIDE LOAD FITTING. THIS DOCUMENT PROVIDES REPAIR INSTRUCTIONS FOR CORROSION FOUND AT THE HORIZONTAL STABILIZER HINGE SIDE LOAD FITTING. THE CORROSION IS IN THE AREA OF THE 2.0 INCHES DIAMETER COUNTERBORE. THMar 26, 2001 · N12FQ · Doug MD88SDR CALA0100244Support · crackedINSPECTION FOUND A 1.5 INCH CRACK IN LT HORIZONTAL STABILIZER SECONDARY PIVOT SUPPORT. THE PIVOT SUPPORT WAS REPLACED IAW EA 5310-03417 AND ECRA 5310-04118.Mar 22, 2001 · N14062 · Doug DC1030SDR CA010409019Bracket · cracked(CAN) FOUND DURING INSPECTION FOR 80-11-04 NUTPLATES FOR CRACKS. ALSO SDA AV-2000-06. AFFTER REMOVAL OF BRACKET ALSO FOUND REAR SPAR REINFORCEMENT P/N 0432001-15 CRACKED (HOLES ARE ALSO ELONGATED) ALONG TOPSIDE, AFTER REMOVAL OF REAR SPAR. REINFORCEMENT BOTH LMar 21, 2001 · Cessna 150FSDR UPS04M42458Structure · corrodedINSPECTION TYPE: C, HORIZONTAL STAB, LEFT BARREL NUT HOLE NR 26 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.006 INCH. SPLICE FITTING FABRICATED PER EN 1100-04. NEW SPLICE FITTINMar 19, 2001 · N275UP · Doug MD11FSDR DL73K010460Bearing · wornWHILE PERFORMING JIC5957 FOUND PIVOT BEARING PLAY TO BE OUT OF LIMITS. IN THE PROCCESS OF REMOVING BEARING HOUSING FOUND SAFETY WIRE BROKEN AND KEEPER BACKED OFF APROX 1/4 INCHMar 17, 2001 · N316DL · Boeing 737232SDR QXEA0100404Vortex Gen · unapproved partPDX-INBOARD VORTEX GENERATOR ON RIGHT HAND HORIZONTAL STABILIZER LOWER SKIN IS NOT APPROVED PART FOR THIS AIRCRAFT. REPAIRED IAW HORIZON AIR EA 9-55-144.Mar 17, 2001 · N816PH · Dhav DHC8102
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