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 ABXA000124Fitting · crackedRIGHT HORIZONTAL STAB OUTBOARD END FITTING WAS CRACKED AT THE UPPER FORWARD FLANGE. REPLACED FITTING IAW DC9 SRM 51-30-1, 51-30-2, 51-30-5.Feb 22, 2000 · N933AX · Doug DC933FSDR RRXA000659Angle · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE LT HORIZONTAL STAB L/E FORMER ANGLE AT STA XFS 47, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW ANGLE AND INSTALLED IAW DC-8 SRM 53-2-0, 51-2-20D ANDFeb 21, 2000 · N831AL · Doug DC873FSDR CA000224032Bracket · cracked(CAN) ON INSPECTION, RIGHT HORIZONTAL STABILIZER ATTACH BRACKET WAS FOUND CRACKED IN THE MAIN PART OF THE CASTING.Feb 21, 2000 · Beech B99SDR UPS00231976Lug · damagedINSPECTION TYPE:C&SI, ULTRASONIC INSPECTION OF HORIZ STAB HINGE LUGS (ON VERT STAB) LT AND RT, I/B AND O/B DUE SUSPECT INDICATION FROM HFEC INSPECTION. ULTRASONIC INSPECTION CARRIED OUT BOTH LEFT AND RIGHT BORES REPAIRED IAW UPS EO B727-5510-2284.Feb 17, 2000 · N908UP · Boeing 72727CSDR 2000ZZZX720Nut · splitDURING A PHASE INSPECTION, THE LEFT NUT THAT RETAINS THE HORIZONTAL STABILIZER WAS FOUND SPLIT FROM TOP TO BOTTOM. RECORDS SHOW THAT SB CQB 85-25 AND AD 85-25-11 WERE C/W IN 1986. THE SB AND AD ADDRESS THIS PROBLEM. THE NUT THAT SPLIT APPEARS TO HAVE BEEN TFeb 16, 2000 · N8FR · Cessna 425SDR 20000407SH003Support Fitting · wornROUTINE INSPECTION REVEALED HORIZONTAL STABILIZER LOOSE AT PIVOT SUPPORTS. REPLACED BOTH LEFT AND RIGHT PIVOT SUPPORT BRACKETS AND BEARINGS AND HARDWARE. PROBLEM DETERMINED TO BE DUE TO NORMAL WEAR AND POSSIBLE LACK OF LUBRICATION. (X)Feb 15, 2000 · N950AA · Beech B99SDR AALA2000360Beam · corrodedTUL - FOUND CORROSION ON TOP OF T/E BEAM RIGHT HORIZ STAB 2ND FROM OUTBOARD ELEV HINGE. INSTALLED DOUBLER REPAIR PER ESO 11697, DATED 2-14-00. (M)Feb 15, 2000 · N868AA · Boeing 727223SDR 20000405SH003Slat · damagedSLATS REPLACED WITH NEW. C/W BELL ASB 407-99-32. (X)Feb 11, 2000 · N175P · Bell 407SDR 20000405SH002Slat · damagedSLATS REPLACED WITH NEW. C/W BELL ASB 407-99-32. (X)Feb 11, 2000 · N10EW · Bell 407SDR HNAA0000017Skin · damagedHORIZONTAL STABILIZER FAILED BOND TEST PER AD2000-01-07. REPLACED HORIZONTAL STABILIZER.Feb 11, 2000 · N909HA · Dhav DHC8102SDR 20000622SH021Slat · damagedREPLACED WITH NEW SLATS FROM BELL HELICOPTER. C/W BELL ASJ 407-99-32. (X)Feb 9, 2000 · N407WH · Bell 407SDR TSAA200055059Attach Fitting · crackedLEFT AND RIGHT HORIZONTAL STABILIZER UPPER ATTACH FITTINGS FOUND CRACKED. BOEING AOG TEAM REPLACED THE HORIZONTAL STABILIZER UPPER ATTACH CHORD. AIRCRAFT RETURNED TO SERVICE. (M)Feb 9, 2000 · N802AL · Boeing 7372S5CSDR QXEA0000201Fitting · corrodedPDX - LEFT UPPER INBOARD LUG OF HORIZONTAL STABILIZER DIRVE FITTING HAS PITTING/CORROSION ON INSIDE FACE. REPAIRED IAW FOKKER SRM 51-10-01.Feb 1, 2000 · N477AU · Fokker F28MK4000SDR QXEA0000200Fitting · corrodedPDX - BOTH RIGHT UPPER LUGS ON HORIZONTAL STABILIZER DRIVE FITTING HAS PITTING/CORROSION ON INSIDE FACES. REPAIRED IAW FOKKER SRM 51-11-01.Feb 1, 2000 · N477AU · Fokker F28MK4000SDR QXEA0000199Fitting · corrodedPDX - HORIZONTAL STABILIZER DRIVE FITTING RIGHT LOWER INBOARD LUG HAS PITTING/CORROSION. REPAIRED IAW FOKKER SRM 51-10-4.Feb 1, 2000 · N477AU · Fokker F28MK4000SDR QXEA0000197Fitting · gougedPDX - THERE ARE SEVERAL GOUGES ON THE FORWARD LEFT AND RIGHT LUGS OF THE HORIZONTAL STABILIZER DRIVE FITTING. REPAIRED IAW FOKKER SRM 51-10-4.Feb 1, 2000 · N477AU · Fokker F28MK4000SDR QXEA0000198Fitting · corrodedPDX - HORIZONTAL STABILIZER DRIVE FITTING LEFT-HAND LOWER INBOARD LUG HAS PITTING/CORROSION. REPAIRED IAW FOKKER SRM 51-10-01.Feb 1, 2000 · N477AU · Fokker F28MK4000SDR CA000209010Attach Angle · damaged(CAN) FLIGHT LOADS AND FREE PLAY HAD ELONGATED THE BOLT HOLES FOR THE HORIZONTAL PITCH TRIM ACTUATOR ATTACHMENT, IN THE BUILD UP STEEL AND ALUMINUM STABILIZER RIB ASSY. IT IS SUSPECTED THAT THE LOW TORQUE APPLICATION AT PREVIOUS INSTALLATION HAD ALLOWED THE BOJan 29, 2000 · Lear 35ASDR QXEA0000205Fitting · corrodedPDX - LEFT UPPER HORIZONTAL STABILIZER JUNCTION FITTING HAS CORROSION/PITTING ON INBOARD SURFACE. REPAIRED IAW HORIZON AIR EA 4-55-183.Jan 28, 2000 · N477AU · Fokker F28MK4000SDR QXEA0000204Fitting · corrodedPDX - LEFT LOWER HORIZONTAL STABILIZER JUNCTION FITTING HAS PITTING/CORROSION ON INBOARD SURFACE. REPAIRED IAW HORIZON AIR EA 4-55-183.Jan 28, 2000 · N477AU · Fokker F28MK4000SDR QXEA0000203Fitting · corrodedPDX - RIGHT UPPER HORIZONTAL STABILIZER JUNCTION FITTING HAS PITTING/CORROSION ON INBOARD AND OUTBOARD SURFACES. REPAIRED IAW HORIZON AIR EA 4-55-183.Jan 28, 2000 · N477AU · Fokker F28MK4000SDR QXEA0000202Fitting · corrodedPDX - RIGHT LOWER HORIZONTAL STABILIZER JUNCTION FITTING HAS PITTING/CORROSION INBOARD SURFACE. REPAIRED IAW HORIZON AIR EA 4-55-183.Jan 28, 2000 · N477AU · Fokker F28MK4000SDR TWAA0001906Hinge Plate · corrodedDURING CHECK-C MAINT, THE HORIZONTAL STABILIZER RT I/B PIVOT BEARING HINGE PLATES WERE CORRODED/PITTED IN BORE. REAMED, BUSHED AND FINAL HONED TO DIMENSION PER SRM 55-02.Jan 27, 2000 · N952U · Doug DC982SDR TWAA0001905Hinge Plate · corrodedDURING CHECK-C MAINT, THE HORIZONTAL STABILIZER LT O/B PIVOT BEARING HINGE PLATES WERE CORRODED AND PITTED IN BORE. REAMED HOLE, BUSHED AND FINAL HONED PER SRM 55-02.Jan 27, 2000 · N952U · Doug DC982SDR TWAA0001904Hinge Plate · corrodedDURING CHECK-C MAINT, THE HORIZONTAL STABILIZER LT I/B PIVOT BEARING HINGE PLATES HAD CORROSION AND PITTING IN THE BORE. REAMED HOLE TO REMOVED CORROSION. HOLE DIMENSION 1.435 PER SRM 55-02. INSTALLED BUSHINGS AND FINAL HOLE DIM PER SRM 55-02.Jan 27, 2000 · N952U · Doug DC982SDR 20000404SH023Structure · damagedOBTAINED ONE RT HORIZ STAB L/E RT ASSY FROM CESSNA FOR REPAIR OF A DAMAGED STAB. THE NUTPLATE ON THE RIB MUST BE USED TO PROPERLY ORIENT THE RIB TO THE FUSELAGE STRUCTURE BEFORE RIVET HOLES ARE DRILLED TO ATTACH THE RIB TO THE STAB SPAR AND LEADING EDGE SKID.Jan 21, 2000 · Cessna 152SDR TWAA0001611Bearing · corrodedDURING CHECK-C MAINT THE HORIZONTAL STABILIZER O/B PIVOT BEARING, RT SIDE, INNER AND OUTER PLATES WERE RUSTY AND PITTED. REMOVED RT O/B, INNER AND OUTER PLATES AND INSTALLED NEW PLATES PER MO 72N10.Jan 21, 2000 · N952U · Doug DC982SDR SWAA000091Lug · crackedDURING SCHEDULED D CHECK, FOUND LT HORIZONTAL STAB REAR SPAR UPPER LUG BORE CORRODED AND CRACKED AT 1 AND 9 O'CLOCK POSITIONS. REPAIRED LUG PER ER NR 99-6540.Jan 14, 2000 · N129SW · Boeing 7372T4SDR RRXA000660Fitting · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE RT HORIZONTAL STAB LOWER FWD SUPPORT BRACKET (O/B END) AT STA XFS 47, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW SUPPORT BRACKET AND INSTALLED IAW Jan 10, 2000 · N831AL · Doug DC873FSDR RRXA003360Jackscrew · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE R/H HORIZONTAL STABILIZER JACK SCREW AT STA 1800 AND X=-24, Z=35, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW MM 27-Jan 8, 2000 · N831AL · Doug DC873FSDR RRXA003359Jackscrew · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE L/H HORIZONTAL STABILIZER JACK SCREW AT STA 1800 X=24 Z=35, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 MM 27-41-1.Jan 8, 2000 · N831AL · Doug DC873FSDR 2000ZZZX136Fairing · mismanufacturedPART INDICATED CAME FROM FACTORY INSTALLATION ON BRAND NEW AIRCRAFT WITHOUT 2 FORWARD HOLES DRILLED AND FITTED.Dec 16, 1999 · N213CM · Cessna 182SSDR AALA991926Casting · crackedTUL - RIGHT STABILIZER HINGE CASTING CRACKED. ABOUT 1.50 INCHES LONG. REMOVED CRACKED AREA PER SRM 55-10-4. INSTALLED DOUBLER PLATE PER SRM 55-10-4. TST: 62,106 HOURS. CYCLES: 37,887. (X)Dec 14, 1999 · N865AA · Boeing 727223SDR 2000ZZZX110Structure · misdrilledDURING COURSE OF 10,000-HOUR INSPECTION, THE HORIZONTAL STABILIZER WAS FOUND TO HAVE NUMEROUS DOUBLE HOLES, HOLES DRILLED OFF-CENTER, HOLES DRILLED ON AN ANGLE AFTER REMOVAL OF THE HYLOCKS IN THE CENTER SECTION THROUGH ALL SPARS AND FITTINGS. SUBMITTER STATEDDec 14, 1999 · N87SF · Cessna 550SDR CALA9901582Skin · puncturedINSPECTION FOUND A PUNCTURE IN LT I/B HORIZONTAL STABILIZER LEADING EDGE AT STA 70. A FLUSH DOUBLER REPAIR WAS INSTALLED IAW SRM 55-10-01.Dec 9, 1999 · N16650 · Boeing 737524SDR RRXA000319Fitting · crackedDURING A MAINTENANCE VISIT FOUND HORIZONAL STABILIZER FITTING RIGHT SIDE AT STA 1798 AND XCW 47.5. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-20D.Dec 7, 1999 · N605AL · Doug DC873FSDR 2000ZZZX380Rivet · missingDURING AN EXTERNAL VISUAL INSPECTION OF THE HORIZONTAL STABILIZER, FOUND TWO RIVET HEADS FROM LOWER RT SKIN TO BE MISSING. REMAINING RIVET STEMS/SHANKS FOUND, ALSO PREVIOUSLY PAINTED OVER WHEN AIRCRAFT WAS PAINTED. UPON REPLACING THESE RIVETS WITH NEW SOLID Dec 6, 1999 · N24YS · Gulstm G1159BSDR CA991229072Spar · cracked(CAN) ROUTINE INSPECTION REVEALED SPAR WEB CRACKING AT STATION 110 OF L/H HORIZONTAL STABILIZER.CRACK JUST VISISBLE FRON AFT VIEW.STABILIZER SKINS LIFTED TO GAIN ACCESS TO INTERNAL AREA.CRACKED DETERMINED TO BE APPROX. 0.750 IN LENGTH AND ORIGINATING FROM RIVEDec 3, 1999 · Piper PA31TSDR AALA991784Casting · corrodedTUL - VERTICAL FIN - HORIZONTAL STABILIZER ATTACH LUGS HAD CORROSION IN BORE, BOTH LEFT AND RIGHT. REMOVED CORROSION ON RIGHT LUG PER SB 727-55-7 AND SRM 55-30-6. REMOVED CORROSION ON LEFT LUG PER ESO 11697 DATED 11-22-99. (X)Nov 23, 1999 · N722AA · Boeing 727227SDR AALA991783Casting · corrodedTUL - HORIZONTAL STABILROSION ON BORES, LEFT SIDE. REMOVED CORROSION ER SRM 55-10-2 AND FABRICATED NEW BUSHING PER 55-10-2. TST: 72,812.33 HOURS. CYCLES: 47,830. (X)Nov 23, 1999 · N722AA · Boeing 727227SDR AALA991782Casting · corrodedTUL - HORIZONTAL STABILIZER HINGE LUGS RIGHT SIDE, BOTH INBOARD AND OUTBOARD HAS CORROSION. REMOVED CORROSION PER SRM 55-10-2. FABRICATED NEW BUSHING PER 55-10-2. TST: 72,812.33 HOURS. CYCLES: 47,830. (X)Nov 23, 1999 · N722AA · Boeing 727227SDR AALA991779Beam · corrodedTUL - HEAVY CORROSION ON TOP OF LEFT HORIZONTAL STABILIZER UPPER REAR T/E BEAM. INSTALLED DOUBLER OVER DAMAGED AREA PER 55-10-6. TST: 72,812 HOURS. CYCLES: 47,830. (X)Nov 21, 1999 · N722AA · Boeing 727227SDR QXEA9902366Fitting · corrodedPDX - HORIZONTAL STAB DRIVE FITTING AFT RIGHT-HAND LOWER LUG HAD CORROSION. REPAIRED IAW HORIZON AIR EA 4-55-169.Nov 17, 1999 · N482US · Fokker F28MK4000SDR QXEA9902365Fitting · corrodedPDX - HORIZONTAL STAB DRIVE FITTING AFT RIGHT-HAND UPPER LUG HAD CORROSION. REPAIRED IAW HORIZON AIR EA 4-55-169.Nov 17, 1999 · N482US · Fokker F28MK4000SDR QXEA9902364Fitting · corrodedPDX - HORIZONTAL STAB DRIVE FITTING AFT LEFT-HAND LOWER LUG HAD CORROSION. REPAIRED IAW HORIZON AIR EA 4-55-169.Nov 17, 1999 · N482US · Fokker F28MK4000SDR QXEA9902363Fitting · corrodedPDX - HORIZONTAL STAB DRIVE FITTING LEFT-HAND UPPER AFT LUG CORRODED. REPAIRED IAW HORIZON AIR EA 4-55-169.Nov 17, 1999 · N482US · Fokker F28MK4000SDR QXEA9902362Fitting · corrodedPDX - HORIZONTAL STAB JUNCTION FITTING UPPER RIGHT-HAND LUG HAD PITTING/CORROSION. REPAIRED IAW HORIZON AIR EA 4-55-169.Nov 17, 1999 · N482US · Fokker F28MK4000SDR QXEA9902361Fitting · corrodedPDX - HORIZONTAL STAB JUNCTION FITTING LOWER RIGHT-HAND LUG HAD PITTING/CORROSION. REPAIRED IAW HORIZON AIR EA 4-55-169.Nov 17, 1999 · N482US · Fokker F28MK4000SDR QXEA9902360Fitting · corrodedPDX - HORIZONTAL STAB JUNCTION FITTING LOWER LEFT-HAND LUG HAD PITTING/CORROSION. REPAIRED IAW HORIZON AIR EA 4-55-169.Nov 17, 1999 · N482US · Fokker F28MK4000SDR QXEA9902359Fitting · corrodedPDX - HORIZONTAL STAB JUNCTION FITTING UPPER LEFT-HAND LUG HAD PITTING/CORROSION. REPAIRED IAW HORIZON AIR EA 4-55-169.Nov 17, 1999 · N482US · Fokker F28MK4000
Back to JASC 5510