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 UPS04M42912Structure · corrodedINSPECTION TYPE: C, HORIZONTAL STABILIZER NR 21 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, BEARING AND SIDEWALL SURFACE. CORROSION AT BARREL NUT HOLE S/W & BEARING SURFACE REAMED TO 1.067 INCH & BLENDED OUT TO 0.0200 INCH, FOUND OUT OF LIMIT. REPAIR SLEEVE May 29, 2004 · N276UP · Doug MD11SDR N150AW0009Skate Angle · wornFORWARD END OF LEFT SKATE ANGLE FOR VERTICAL DORSAL FIN IS WORN AT BS 1016. REPLACED SKATE ANGLE PER SRM 51-10-02.May 25, 2004 · N150AW · Boeing 7373G7SDR 04FDEA01159Structure · corrodedLEFT HORIZONTAL STABILIZER FIXED LEADING EDGE, ZONE 330 (FWD SPAR) UPPER LIP UPPER SECTION APPROX STA 158 RIB 5, 4 EA AREAS 1.0 INCH L ,(.200 INCH W AREA 2 & 3 AS MARKED), (.100 INCH W AREA 1 & 4 AS MARKED). UNABLE TO DETERMINE DEPTH WITHOUT BLENDOUT, CORROSIMay 7, 2004 · N428FE · Airbus A310203SDR CA040825003Bracket · cracked(CAN) TAIL REMOVED TO CHANGE BROKEN BRACKETS. PN 0712302-1 LT BRACKET AND 0732101-4 REINFORCEMENT REPLACED WITH NEW PARTS. ADJACENT RIVETS REPLACED. TAIL REASSEMBLED AND DUAL INSPECTED.May 6, 2004 · Cessna 180HSDR 2004UALA00441Skin · dentedFOUND DENT ON RIGHT STABILIZER LEADING EDGE. DENT IS LOCATED ELEVEN BAYS O/B OF STA 86.66 IN CENTER OF BAY. DIMENSIONS ARE 1.00 VERT LENGTH X 0.41 HORIZONTAL WIDTH X 0.047 DEEP. MAJOR REPAIR ACCOMPLISHED. INSTALLED INTERNAL DOUBLER AND FLUSH FILLER.May 4, 2004 · N399UA · Boeing 737322SDR 2004FA0000558Attach Bracket · misinstalledWHEN PN 1232041 ARE INSTALLED, INCORRECT FIT UNLESS SK210-125 ALSO INSTALLED ON STA 209.0 BULKHEAD. NO CORRELATING REFERENCE IN MFG PARTS OR SERVICE. TOOK 2 WEEKS WITH MFG TECH TO WORK OUT. IMPROPER FIT CAUSES STRESS AND BINDING ON PARTS THAT COULD LEAD TO May 3, 2004 · N4631C · Cessna T210NSDR 04FDEA01133Structure · corrodedHORIZONTAL STABILIZER, RIGHT UPPER CENTER PLANK NR 15R BARREL NUT BORE CORROSION BLEND-OUT EXCEEDED EO 1-5510-7-5000 LIMITATIONS. COMPLIED WITH FEDEX EA 1-5510-76025. HORIZONTAL STABILIZER BARREL NUT BORE REWORK/REPAIR A.D. 2003-22-08.May 3, 2004 · N590FE · Doug MD11SDR CA040427018Rib · cracked(CAN) DURING INSPECTION OF HORIZONTAL STABILIZER ATTACH BOLT HOLES INSPECTION IAW MFG SB04-55-01, FOUND RT AFTER ATTACHMENT HOLE ON THE RIB HAS TWO .0937 INCH LONG CRACKS. THE CRACKS ARE HIDDEN UNDER THE MOUNTING WASHER.Apr 27, 2004 · Cessna 172SSDR DLM88040378Stop Fitting · brokenDURING OP 5924 AD FOUND LOWER MECHANICAL STOP MADE CONTACT WITH JACKSCREW STOP. LOWER STOP BROKEN OFF. REPLACED JACKSCREW AND STOP ASSY. ADJUSTED STABILIZER JACKSCREW CONTROL AND INDICATION PER M/M. RIG CHECKED AND OPS CKS GOOD.Apr 25, 2004 · N916DL · Doug MD88SDR CALA0400395Clip · crackedLEFT ELEVATOR O/B SIDE HINGE PANEL SUPPORT CRACKED. INSTALLED CLIP PER SRM 55-20-02 FIG 1; 51-30-01 FIG 2.Apr 19, 2004 · N18350 · Boeing 7373T0SDR 04FDEA00974Panel · crackedON PANEL 7208-1 RT SIDE FOUND BY ULTRASONIC INSPECTION 1 HOLE WITH CRACK, L= .25 INCH AT 1 INCH FROM BOTTOM. REPLACED PANELS PER SB 55-16 FIG 3 GROUP 1 (EA -8-5510-70126) FEDEX P/N: SB10550016-17KIT, SB10550016-93KIT. THE P/N ITEM 5 IS A REPLACEMENT KIT. TApr 16, 2004 · N559FE · Doug DC1010SDR CALA0400382Pin · corrodedINSPECTION FOUND LEFT HORIZONTAL STABILIZER MIDDLE PIN CORRODED. THE PIN WAS REMOVED AND REPLACED IAW EA 5510-01696.Apr 16, 2004 · N23721 · Boeing 737724SDR CALA0400381Pin · corrodedINSPECTION FOUND RIGHT HORIZONTAL STABILIZER REAR SPAR MIDDLE AND LOWER PINS CORRODED. THE PINS WERE REMOVED AND REPLACED IAW EA 5510-01696.Apr 15, 2004 · N23721 · Boeing 737724SDR CALA0400380Pin · corrodedINSPECTION FOUND RIGHT HORIZONTAL STABILIZER REAR SPAR UPPER PIN CORRODED. THE PIN WAS REMOVED AND REPLACED IAW EA 5510-01696.Apr 15, 2004 · N23721 · Boeing 737724SDR CALA0400379Pin · corrodedINSPECTION FOUND THE LEFT HORIZONTAL STABILIZER REAR SPAR LOWER PIN CORRODED. THE PIN WAS REMOVED AND REPLACED IAW EA 5510-01696.Apr 15, 2004 · N23721 · Boeing 737724SDR CALA0400378Pin · corrodedINSPECTION FOUND LEFT HORIZONTAL STABILIZER REAR SPAR UPPER PIN CORRODED. THE PIN WAS REMOVED AND REPLACED IAW EA 5510-01696.Apr 15, 2004 · N23721 · Boeing 737724SDR CA040417001Fairing · lightning strike(CAN) FLYING THRU SHOWERS AT 10000 FT , ON ARRIVAL, LARGE FLASH WAS OBSERVED. NO AIRCRAFT SYSTEM AFFECTED. AFTER LANDING, 2 BLACK MARKS WERE FOUND ON THE LOWER RT HORIZONTAL STABILIZER. REPAIR EO 670-55-12-153 ALONG WITH NON DESTRUCTIVE TEST (NDT) CARRIED OApr 13, 2004 · Cndair CL6002B19SDR CALA0400365Pin · corrodedINSPECTION FOUND LEFT HORIZONTAL STABILIZER LOWER AND MIDDLE PINS CORRODED. THE PINS WERE REPLACED IAW EA 5510-01696.Apr 12, 2004 · N16713 · Boeing 737724SDR CALA0400366Pin · corrodedINSPECTION FOUND LEFT HORIZONTAL STABILIZER UPPER PIN CORRODED. THE PIN WAS REPLACED IAW EA 5510-01696.Apr 12, 2004 · N16713 · Boeing 737724SDR CALA0400348Pin · corrodedINSPECTION FOUND RIGHT HORIZONTAL STABILIZER AFT ATTACHMENT MID PIN AND LOWER PIN CORRODED. THE PINS WERE REMOVED AND REPLACED IAW EA 5510-01696.Apr 8, 2004 · N12238 · Boeing 737824SDR CALA0400347Pin · corrodedINSPECTION FOUND LEFT HORIZONTAL STABILIZER ATTACHMENT AFT PIN AND MIDDLE PIN CORRODED. THE PINS WERE REMOVED AND REPLACED IAW EA 5510-01696.Apr 8, 2004 · N12238 · Boeing 737824SDR CALA0400346Pin · corrodedINSPECTION FOUND RIGHT HORIZONTAL STABILIZER AFT ATTACHMENT UPPER PIN CORRODED. REMOVED AND REPLACED PIN IAW EA 5510-01696.Apr 8, 2004 · N12238 · Boeing 737824SDR CALA0400345Pin · corrodedINSPECTION FOUND LT HORIZONTAL STABILIZER UPPER AFT PIN CORRODED. REMOVED AND REPLACED PIN IAW EA 5510-01696.Apr 8, 2004 · N12238 · Boeing 737824SDR CALA0400334Pin · corrodedINSPECTION FOUND RIGHT HORIZONTAL STABILIZER UPPER PIN CORRODED. A NEW PIN WAS INSTALLED IAW EA 5510-01696.Apr 7, 2004 · N33714 · Boeing 737724SDR CALA0400333Pin · corrodedINSPECTION FOUND LEFT HORIZONTAL STABILIZER AFT SPAR UPPER PIN CORRODED. THE PIN WAS REPLACED IAW EA 5510-01696.Apr 7, 2004 · N33714 · Boeing 737724SDR CALA0400332Pin · corrodedINSPECTION FOUND LEFT HORIZONTAL STABILIZER AFT SPAR LOWER AND MIDDLE PINS CORRODED. THE PINS WERE REMOVED AND REPLACED IAW EA 5510-01696.Apr 7, 2004 · N33714 · Boeing 737724SDR UPS04242204Beam · corrodedINSPECTION TYPE: C, RT HORIZONTAL STABILIZER UPPER TRAILING EDGE BEAM HAS CORROSION AFT OF BALANCE PANEL BAYS. BEAM REPLACED IAW SRM 51-30-2 AND DRG NR 65-22987.Apr 6, 2004 · N926UP · Boeing 72731CSDR CALA0400322Pin · corrodedINSPECTION FOUND LEFT HORIZONTAL STABILIZER LOWER PIN CORRODED. A NEW PIN WAS INSTALLED IAW EA 5510-01696, REV C.Apr 5, 2004 · N18220 · Boeing 737824SDR CALA0400321Pin · corrodedINSPECTION FOUND LEFT HORIZONTAL STABILIZER UPPER PIN CORRODED. THE PIN WAS REMOVED AND REPLACED IAW EA 5510-01696, REV C.Apr 4, 2004 · N18220 · Boeing 737824SDR UPS04M42490Structure · corrodedINSPECTION TYPE: C, HORIZONTAL STAB, RT BARREL NUT HOLE NR 34 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.030 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-EApr 1, 2004 · N275UP · Doug MD11FSDR UPS04M42486Structure · corrodedINSPECTION TYPE: C, HORIZONTAL STAB, RT BARREL NUT HOLE NR 13 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.005 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-EApr 1, 2004 · N275UP · Doug MD11FSDR UPS04M42469Structure · corrodedINSPECTION TYPE: C, HORIZONTAL STAB, LT BARREL NUT HOLE NR 25 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.005 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-EApr 1, 2004 · N275UP · Doug MD11FSDR UPS04M42468Structure · corrodedINSPECTION TYPE: C, HORIZONTAL STAB, LT BARREL NUT HOLE NR 05 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.030 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-Apr 1, 2004 · N275UP · Doug MD11FSDR SWAA040960Fitting · corrodedDURING SCHEDULED D CHECK, FOUND HORIZONTAL STAB CENTER SECTION LT HINGE FITTING ON BOTH FACES CORRODED. REPAIRED FITTING PER ER.Apr 1, 2004 · N304SW · Boeing 7373H4SDR CALA0400297Pin · corrodedINSPECTION FOUND RIGHT HORIZONTAL STABILIZER UPPER MOUNT PIN CORRODED. THE PIN WAS REMOVED AND REPLACED IAW EA 5510-01696, STEP 6-9.Mar 30, 2004 · N14735 · Boeing 737724SDR CALA0400296Pin · corrodedINSPECTION FOUND RIGHT HORIZONTAL STABILIZER MID MOUNT PIN CORRODED. THE PIN WAS REMOVED AND REPLACED IAW EA 5510-01696, STEP 10-13.Mar 30, 2004 · N14735 · Boeing 737724SDR CA040401005Reinforcement · cracked(CAN) REPAIRED HORIZONTAL STABILIZER. AFT ATTACHMENT POINT REINFORCEMENT BRACKET PN 07321014 REPLACED WITH NEW. ADJACENT RIVETS REPLACED. TAIL REASSEMBLED. INDEPENDENT CONTROL CHECK CARRIED OUT.Mar 29, 2004 · Cessna 180ASDR UPS04M42518Structure · corrodedINSPECTION TYPE: C, HORIZONTAL STAB, BARREL NUT HOLE NR 28 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORR REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.048 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREMar 28, 2004 · N275UP · Doug MD11FSDR UPS04M42508Structure · corrodedINSPECTION TYPE: C, HORIZONTAL STAB, LT BARREL NUT HOLE NR 34 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF BARREL NUT HOLE REMOVED PER SRM 51-21-01 VOL 2 REV 34 MAT'L REMOVED 0.085 INCH DEEP FOUND WITHIN LIMITS PER EN1120-04Mar 28, 2004 · N275UP · Doug MD11FSDR UPS04M42507Structure · corrodedINSPECTION TYPE: C, HORIZONTAL STAB, LT BARREL NUT HOLE NR 31 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF BARREL NUT HOLE PER SRM 51-21-01 VOL 2 REV 34 MAT'L REMOVED 0.025 INCH FOUND WITHIN LIMITS PER EO MD11-5510-19409E. Mar 28, 2004 · N275UP · Doug MD11FSDR UPS04M42505Structure · corrodedINSPECTION TYPE: C, HORIZONTAL STAB, RT BARREL NUT HOLE NR 25 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF BARREL NUT HOLE REMOVED PER SRM 51-21-01 VOL 2 REV 34 MAT'L REMOVED 0.005 INCH FOUND WITHIN LIMTS PER EO MD11-5510-19Mar 28, 2004 · N275UP · Doug MD11FSDR UPS04M42514Barrel Nut · corrodedINSPECTION TYPE:C, HORIZONTAL STAB LT BARREL NUT HOLE NR 03 FOUND CORROSION AT BOTTOM SIDEWALL & BEARING SURFACE. CORR REMOVED PER SRM 51-21-01 V2R34, MAT REMOVED 0.030. SLEEVE BUSHING FAB & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE (LT NR 03) REPMar 27, 2004 · N275UP · Doug MD11FSDR UPS04M42506Structure · corrodedINSPECTION TYPE: C, HORIZONTAL STAB, RT BARREL NUT HOLE NR 03 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. MINOR SURFACE CORROSION AT BOTTOM OF HOLE REMOVED PER SRM 51-21-01 VOL 2 REV 34, MAT'L REMOVED 0.005 INCH FOUND WITHIN LIMITS PER EO MD11-55Mar 27, 2004 · N275UP · Doug MD11FSDR UPS04M42526Structure · corrodedINSPECTION TYPE: C, HORIZONTAL STAB, BARREL NUT HOLE NR 08 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF BARREL NUT HOLE REMOVED BOTTOM BORED DOWN 0.018 INCH PER EN 1124-04. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-Mar 26, 2004 · N275UP · Doug MD11FSDR UPS04M42509Structure · corrodedINSPECTION TYPE: C, HORIZONTAL STAB, LT BARREL NUT HOLE NR 19 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. MINOR CORROSION AT BOTTOM OF BARREL NUT HOLE REMOVED PER SRM 51-21- 01 VOL 2 REV 34 MAT'L REMOVED 0.005 INCH WITHIN LIMIT PER EO MD11-5510-1Mar 26, 2004 · N275UP · Doug MD11FSDR UPS04M42488Structure · corrodedINSPECTION TYPE: C, HORIZONTAL STAB, LT BARREL NUT HOLE NR 11 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.048 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-EMar 26, 2004 · N275UP · Doug MD11FSDR GAIA04067STFitting · crackedDURING C-CHECK, THE HORIZONTAL STABILIZER FRONT SPAR GIMBAL A FRAME RIGHT UPPER FORWARD AND AFT CLEVIS HOLES WERE FOUND CRACKED. REMOVED AND REPLACED A FRAME GIMBAL SUPPORT IAW BOEING 727 AMM. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Mar 26, 2004 · N856AA · Boeing 727223SDR SWAA040902Fitting · corrodedDURING SCHEDULED D CHECK, FOUND HORIZONTAL STAB CENTER SECTION RT UPPER THRUST FITTING, UPPER AND LOWER ATTACH LUGS CORRODED. REPAIRED HORIZONTAL STAB PER ER.Mar 26, 2004 · N304SW · Boeing 7373H4SDR UPS04M42491Structure · corrodedINSPECTION TYPE: C, HORIZONTAL STAB, BARREL NUT HOLE NR 10 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.035 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. Mar 25, 2004 · N275UP · Doug MD11FSDR UPS04M42489Structure · corrodedINSPECTION TYPE: C, HORIZONTAL STAB RT BARREL NUT HOLE NR 22 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORR REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED FOUND WITHIN LIMIT PER EO MD11-5510-19409-E. SLEEVE BUSHING FABRICATED & INSTALLMar 25, 2004 · N275UP · Doug MD11F
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