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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR UPS07M49922Structure · corrodedINSPECTION TYPE:C HORZ STAB BARREL NUT BORE LEFT NR 15 FOUND WITH CORROSION. CORROSION REMOVED SRM 51-21-01 VII R38. BOTTOM REMAIN BLENDOUT 0.100" DEEP. BORE REAMED TO 1.067" DIA REMAIN BLENDOUT 0.035" DEEP EXCEED EO LIMITS. 10X MAG DVI C/O NO CORROSION. SDR UPS07M49895Structure · corrodedINSPECTION TYPE:C HORZ STAB BARREL NUT BORE NR 15 RIGHT FOUND CORROSION. CORROSION REMOVED SRM 51-21-01 VII R38. BOTTOM REMAIN BLENDOUT 0.050" DEEP. BORE REAMED TO 1.067" DIA REMAIN BLENDOUT 0.030" EXCEED EO LIMITS. 10X MAG DVI C/O NO CORROSION. BORE BOTTSDR 07FDEA01179Beam · crackedLT HORIZONTAL STAB T/E LWR BEAM BESIDE NR 5 RIB FROM I/B HAS CRACK. REPAIRED LT HORIZONTAL STAB LWR BEAM IAW SRM 55-10-6 FIG 1. PREPPED AND PAINTED. REPAIRED AREA IAW AMM 51-20-151-7.SDR UPS07M49923Structure · corrodedINSPECTION TYPE:C HORIZONTAL STAB BARREL NUT BORE NR 2 LEFT FOUND WITH CORROSION. CORROSION REMOVED SRM 51-21-01VII R 38. BOTTOM SURF REMAIN BLENDOUT 0.035" DEEP X 0 .150" DIA BORE REAMED TO 1.067" DIA REMAIN BLENDOUT 0.020" DEEP EXCEED EO LIMITS. 10X MAG DSDR 07FDEA01059Attach Fitting · crackedNR 2 ENGINE INLET DOGHOUSE AT BASE OF VERTICAL LEADING EDGE VERTICAL WEB ATTACH CLIP CRACKED RT SIDE INTERIOR AT STA 1274. REMOVED AND REPLACED VERTICAL WEB ATTACH CLIP AT STA 1274 INSIDE VERTICAL STABILIZER ABOVE S DUCT ON RT SIDE, REF B727 SRM 51-30-2 PAGE SDR GUUA03180701Hinge Bracket · corrodedAT SCHEDULED ROUTINE MAINTENANCE LT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REPLACED LT OB ELEVATOR HINGE BRACKET.SDR 2007FA0000266Hinge Bracket · crackedUPON REMOVAL OF THE HORIZONTAL STABILATOR FOR BEARING REPLACEMENT, A CRACK WAS NOTED COMING OUT FROM UNDER THE LEFT HINGE BRACKET THAT IS RIVETED TO THE SPAR OF THE HORIZONTAL STABILATOR. (K)SDR 07FDEA00838Support · damagedDURING ACF MODIFICATION , FOUND ON HORIZ STAB ON SUPPORT NOTED 1 HOLE OVALIZATION DIA, 0.2720" HOLE NOMINAL: 0.1870". REPAIRED FOR EA FEDEX 8-5340-97792 REV A DATE 02-02-07.SDR 07FDEA00703Bearing · damagedRUDDER HINGE ARM NR 4 WITH FWD BEARING DAMAGED. BEARING REPLACED PER SB NO A310-55-2025 PG 27/28 DATE OCT 12/98 REVISION NO 3 APR 08/04 FEDEX EA 6-5510-106687. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".SDR COEA0701908Frame · gougedGOUGE LOCATED ON THE INBOARD AFT RADIUS OF FR 13 LOCATED 3 INCHES UP FROM FLOOR. DAMAGE BLENDED OUT AND REINFORCING DOUBLER INSTALLED PER DO/TS-2986-06-7405 REPAIR INSTRUCTIONS. REF SRAS DO/TS-2986/06..3782. (M)SDR UPS07M49904Structure · corrodedINSPECTION TYPE:C HORZ STAB BARREL NUT BORE NR 21 LEFT FOUND WITH CORROSION. CORROSION REMOVED SRM 51-21-01 VII R38. BOTTOM SURF CLEANED. BORE REAMED TO 1.067 "DIA. REMAIN BLENDOUT 0.020" DEEP EXCEED EO LIMITS. 10X MAG DVI C/O NO CORROSION. BORE REAMED FSDR 2007UALA00640Structure · damagedRUDDER S/N -099 LEFT SIDE JUST ABOVE COUNTER BALANCE AREA HAS GROOVE WEAR DAMAGE. *S/D* MAJOR REPAIR: ACCOMPLISHED COMPOSITE REPAIR PER AAR EA-I070152 & SRM 51-70-17.SDR WRNA200700010Ball Screw · failedDURING C-CHECK, HORIZONTAL STABILIZER BALL SCREW AND BALL NUT FAILED FREE PLAY CHECK. REMOVED STABILIZER DRIVE MECHANISM, CHECKED WEAR OF PINS AND FITTINGS, FOUND IN TOLERANCE IAW 747 MM 27-41-06. REINSTALLED DRIVE MECHANISM PER 747 MM 27-41-06 AND PERFORMED BSDR QXEA200700178Frame · crackedC4 PDX - FOUND FRAME CRACKED. LOCATED IN REAR FUSELAGE AT STRINGER NR 4 PORT. REPAIRED IAW SRM 51-20-16 AND 51-20-36, RD/8-55-199.SDR DLM90070123Bolt · brokenRT MANUAL REVERSION CYLINDER HOUSING BOLTS BROKE AND THE HOUSING BODY CAME APART CAUSING BOTH HYDRAULIC SYSTEMS TO LOSE QUANTITY. THIS RESULTED IN LOSS OF STEERING AND BRAKING DURING TAXI TO GATE AFTER LANDING. AIRCRAFT WAS MET ON THE TAXIWAY AND TOWED TO THSDR 2007UALA00220Clevis · corrodedLEFT HORIZONTAL STAB CENTER SECTION FWD CLEVIS LOWER AFT LUG CORRODED. MAJOR REPAIR: REMOVED BUSHING AND REMOVED CORROSION. SPOT FACED PER EA I070072 REV IR AND INSTALLED THE BUSHING.SDR AMTA200700033Pivot · gougedRIGHT STABILIZER OUTBOARD PIVOT PITTING WITH DEEP GOUGE AT LOWER END. REPAIRED IAW EER12968 WORKORDER 316063. (M)SDR AWXA200700116Structure · corrodedPHX - MAJOR REPAIR - CORROSIONS FOUND OUT OF LIMIT ON UPPER CHORD OF LEFT HORIZONTAL STAB TRAILING EDGE REAR SPAR FROM STAB STA 69.0 TO STAB STA 204.0 IAW B757 SRM 55-10-10-1A AND BOEING MESSAGE 1-27638147-3, CORROSIONS ARE WITHIN LIMITS FOR ACCEPTABLE FERRY FSDR AWXA200700115Beam · corrodedPHX - CORROSIONS FOUND OUT OF LIMIT ON UPPER BEAM OF LEFT HORIZONTAL STAB TRAILING EDGE BEAM FROM ELEVATOR STA 70 TO ELEV STA 172 IAW B757 SRM 55-10-13-1A AND BOEING MESSAGE 1-276738147-3. CORROSIONS ARE WITHIN LIMITS FOR ACCEPTABLE FERRY FLT. REPAIRED LT STSDR AC2A113661Bolt · shearedEND OF BOLT SHEARED OFF WITH NUT.SDR GUUA01140703Hinge Bracket · corrodedAT SCHEDULED ROUTINE MAINTENANCE LT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REPLACED LT OB ELEVATOR HINGE BRACKET.SDR WRLA2007025Rib · brokenITEM:DURING 2C+12A+150M CHECK, MECHANIC FOUND RT HORI STAB UPPER TO BODY FAIRING PANEL SUPPORT RIB BROKEN AT INTERSECTION STA 2025.00. FABRICATE FAIRING PANEL SUPPORT RIB IAW EGAT E1 NO.W2007P55B-075 REV.01. AND APPROVED DOCUMENT MFG CONTROL NR PO209380. INSSDR USAA070022Stiffener · crackedSTATION 175.5 RT HORIZONTAL STAB CRACKED. REPLACED STIFFENER IAW DRAWING NUMBER 65-47513, DEFECT SIZE: 1 INCH.SDR 06FDEA04345Structure · misrepairedPREVIOUS FLUSH REPAIR FOUND LOCATED ON THE LT HORIZONTAL STABILIZER L/E EDGE SECTION 341CB. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR EVALUATED AND FOUND NOT CONFORM TSDR DJFA2006366Support Bracket · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION THE LEFT INBOARD HORIZONTAL STABILIZER ROLLER BRACKET WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN BEECHJET COMMUNIQUE' NUMBER SDR A6WA200640421Angle · crackedRUDDER SYSTEM (MID SPAR) ANGLE P/N 600-92638-1 AT LEFT AFT SIDE OF VS 67.5 PERCENT FRAME CRACKED APPROX .5 INCH LENGTH AT TOP INBOARD ATTACH RIVET. MAINTENANCE FABRICATED NEW ANGLE FROM 7075T6511 PO NR 74697/1 PER DRAWING 600-92638 AND INSTALLED IAW CRJ SRM 5SDR AMTA200600729Pin · corrodedRIGHT HORIZ STAB AFT LOWER ATTACH PIN HAS CORROSION PITTING. REMOVED AND REPLACED PIN PER OE 737-55AD-2935. (M)SDR AMTA200600728Pin · corrodedRIGHT HORIZ STAB AFT CENTER PIN HAS CORROSION PITTING FUSE 1138 STRINGER 11R. REMOVED AND REPLACED PIN PER EO 737-55AD-2935 MM 27-41-11. (M)SDR AMTA200600727Pin · corrodedRIGHT HORIZ STAB AFT UPPER ATTACH PIN HAS CORROSION PITTING AT STS 1138 STRINGER 11R. REMOVED AND REPLACED PIN PER EO 737-55AD-2935 MM 27-41-11. (M)SDR AMTA200600725Pin · corrodedLEFT HORIZ STAB AFT UPPER ATTACH PIN HAS CORROSION PITTING. REMOVED AND REPLACED PIN PER EO 737-55AD-2935 MM 22-41-11. (M)SDR AMTA200600722Pin · corrodedLEFT HORIZ STAB LOWER AFT ATTACH PIN HAS CORROSION PITTING AT FS 1138 AT STRINGER 11L. REMOVED AND REPLACED PIN PER EO 737-55AD-2935. (M)SDR 2006UALA02328Bushing · corrodedRT STAB FWD AND AFT BUSHINGS ARE CORRODED. MAJOR REPAIR: REMOVED BUSHINGS AND CORROSION. INSTALLED BUSHINGS PER AAR EA REV. IR EAI060510.SDR 2006UALA02245Gusset · crackedHORIZONTAL STAB CENTER SECTION - TRUSS GUSSET CRACKED, BS 1108 LBL 16. MAJOR REPAIR: INSTALLED NEW TRUSS GUSSET PER SRM 51-40-02.SDR IXXA06SMN417SAngle · crackedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER LOWER TRAILING EDGE ANGLE CRACKED AT STATION XE29.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. STOP DRILLED CRACKED ENDS AND FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED ARESDR CA061104001Plate · corroded(CAN) UPON VISUAL INSPECTION AND CLEANING OF ATTACHMENT LUG AREA OF VERTICAL FIN TO HORIZONTAL STABILIZER, MECHANIC NOTICED MATERIAL FLAKING OFF OF ONE BOLT HOLE. FURTHER INSPECTION REVEALED EXFOLIATION CORROSION. SINCE THIS TYPE OF CORROSION IS DIFFICULT TO DSDR 2006UALA02117Bushing · corrodedRT STAB AFT UPPER LUG, FWD BUSHING FACE PITTED, MATERIAL LOSS OUT OF LIMITS. MAJOR REPAIR: REWORKED LUG IAW EA-1060488.SDR 06FDEA03772Bulkhead · crackedCLG W/W FOUND 1 CRACK 1" LONG ON HORIZONTAL BLKHD BTWN STA 1441 AND STA 1431 X = 30 RT. TRIMMED OUT DAMAGED PORTION WEB AND INSTALLED FILLER AND RETAINER DOUBLER IAW SRM 53-00-01 FIG 4 SHT 2 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I026748/ N01748 ISDR UPS06848445Angle · crackedINSPECTION TYPE:C2 RT HORIZ STAB UPPER BULLNOSE "L" ANGLE IS CRACKED, INBD END OF STAB NEXT TO FUSELAGE FWD OF FRONT SPAR. REMOVED AND REPLACED "L" ANGLE AND CAP ON RT HORIZ STAB UPPER BULL NOSE FWD OF FRONT SPAR IAW DWG 5654549, AND SRM 51-01-21, 51-03-00, 5SDR UPS06848320Intercostal · crackedINSPECTION TYPE:C2 LT HORIZ STAB 2 CRACKS INBD END ON TEE ANGLE, FWD OF FRONT SPAR (PNL 64J). REMOVED AND REPLACED T-ANGLE FITTING, LWR HORIZ STAB L/E INTERCOSTAL FWD OF FRONT SPAR INSIDE PNL 64J IAW SRM 51-03-02-0, 51-1-21, AND SRM 51-1-20D.SDR HALA0600817Channel · damagedDURING REMOVAL OF RT HORIZONTAL STAB OB TE WEDGE, FOUND U-COMMON TO WEDGE AND STAB WITH LIGHTING STRIKE DAMAGE. REMOVED AND REPLACED RT HORIZONTAL STAB OB T/E WEDGE U-CHANNEL IAW SRM 51-40-02 AND DWG 183T1140.SDR UPS06M48415Structure · corrodedINSPECTION TYPE:C RT HORIZ STAB FOUND NR 27 BARREL NUT BORE CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOL II R38. BORE REAMED TO 1.178 DIA REMAINING BLEND OUT 0.070 DEEP, BOTTOM SURF CLEANED FOUND EXCEED EO LIMITS. B/N BORE BLEND OUT AND BOTTOM PERI RADISDR UPS06M48427Structure · corrodedINSPECTION TYPE:C RT HORIZ STAB FOUND NR 30 BARREL NUT BORE CORRODED CORROSION AT B/N BORE REMOVED PER SRM51-21-01 V.II R.38. BORE REAMED TO 1.178"DIA. REMAINING BLEND OUT FOUND EXCEEDED LIMITS PER EO MD11-551 -19409K. REPAIR SLEEVE BUSHING FAB AND PROTSDR UPS06M48435Structure · corrodedINSPECTION TYPE:C LT HORIZ STAB FOUND NR 28 BARREL NUT BORE CORRODED CORROSION REMOVED AT B/N BORE AS PER SRM 51-21-01 V.II R.38. BORE REAMED TO 1.178" DIA REMAINING BLEND OUT 0.015" DEEP, BOTTOM SURFACE CLEANED, REMAINING BLEND OUT 0.045" DIA DEEP FOUND SDR UPS06M48425Structure · corrodedINSPECTION TYPE:C RT HORIZ STAB FOUND NR 28 BARREL NUT BORE CORRODED CORROSION AT B/N BORE REMOVED PER SRM51-21-01 V.II R.38. BORE REAMED TO 1.178" DIA REMAINING BLEND OUT 0.050" DEEP BOTTOM THRU, EXCEEDED PER B/N EO 5510-19409K. REPAIR BUCKET BUSHING FASDR UPS06M48416Structure · corrodedINSPECTION TYPE:C RT HORIZ STAB FOUND NR 34 BARREL NUT BORE CORRODED. CORROSION AT B/N BORE REMOVED PER SRM 51-21-01VOL IIR 38. BORE REAMED TO 1.178D IA REMAINING BLEND OUT 0.040 BOTTOM SURFACE CLN AND REMAINING BLEND OUT 0.035 DEEP EXCEED EO LIMITS. B/N BOSDR QXEA200602679Bolt · looseC4 YYC - HORIZONTAL STAB GUST LOCK ASSEMBLY HAS LOOSE JO BOLTS ON LEFT SIDE AND RIGHT SIDE PLATE ASSEMBLY. REPAIRED IAW RD8-55-112.SDR WRLA2006095Structure · corrodedDURING 2C+12A+150M CHECK WHILE COMPLYING WITH EO 02-5510-098 REV 4, FOUND CORROSION ON HST LH BARREL NUT HOLE NR 4. ACCOMPLISHED BARREL NUT REMOVAL AND INSPECTION IAW EO 02-5510-098 SEC06, REMOVED CORROSION AND OVERSIZED BARREL NUT HOLE, FABRICATED REPAIR BUSSDR WRLA2006094Structure · corrodedITEM: DURING 2C+12A+150M CHECK WHILE COMPLYING WITH EO 02-5510-098 REV 4, FOUND CORROSION ON HST LT BARREL NUT HOLE NR 7. ACCOMPLISHED BARREL NUT REMOVAL AND INSPECTION IAW EO 02-5510-098 SEC06, REMOVED CORROSION AND OVERSIZED BARREL NUT HOLE, FABRICATED REPASDR UPS06M48430Structure · corrodedINSPECTION TYPE:C RT HORIZ STAB FOUND NR 22 BARREL NUT BORE CORRODED CORROSION AT B/N BORE REMOVED PER SRM 51-21-01 V.II R.38. BORE REAMED TO 1.067" DIA, REMAINING BLEND OUT 0.055"DEEP FOUND EXCEEDED LIMITS PER EO MD11-5510-19409K. B/N BORE REWORKED TO 1SDR UPS06M48437Structure · corrodedINSPECTION TYPE:C RT HORIZ STAB FOUND NR 18 BARREL NUT BORE CORRODED CORROSION AT B/N BORE REMOVED PER SRM 51-21-01 VII R.38. BORE REAMED TO 1.067" DIA BOTTOM BORED THRU, REMAINING SIDEWALL BLEND OUT IS 0.040" DEEP , EXCEEDED LIMITS PER B/N EO. REPAIR BU
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