JASC 5342
Service difficulty reports · 578
Reports filed under 5342 · Fuselage, Stabilizer Attach Fittings, 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 = '5342' 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 = '5342' 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 SIMA201032804Drag Angle · crackedDURING MAINTENANCE BASE VISIT FOUND THE RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACH DRAG ANGLE TO HAVE A POSSIBLE CRACK JUST AFT OF REAR SPAR DATUM 67.590. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW EO CR-53MR-164R1. THE AIRCRAFT WAS RETURNED TO SSDR DALA1029169874Attach Angle · damagedDURING L-CHECK FOUND SEVERAL ELONGATED FASTENER HOLES IN VERTICAL STABILIZER LT SIDE FUSELAGE TO STABILIZER ATTACH ANGLE. REPAIRED PER SRM 55-31-0 FIGURE 1 SHEET 2, SRM 51-60-0 FIGURE 1 SHEET 1, SRM 55-01 FIGURE 4 & SRM 51-30-01 PAGE 127,SDR DALA1028539874Attach Fitting · crackedDURING L-CHECK FOUND CRACK IN VERTICAL STABILIZER RIGHT ATTACH ANGLE APPROXIMATELY .25 INCH FROM TRAILING EDGE. REPAIRED 53-05 FIGURE 23 & SRM 51-10-3B.SDR DALA1157669229Attach Angle · crackedSTA 1542 CANT, DORSAL FIN ATTACH ANGLE REPAIRED IAW BAC TWX BNI-BNI-10-168-01C DWG SR09530296 S/B MD90-53-027 R2(TO 57).SDR DALA1157559229Angle · crackedSTA 1542 CANT, RT FUSELAGE TO VERTICAL STABILIZER DORSAL FIN REPAIRED IAW BAC TWX BNI-BNI-10-168-01C, DWG SR09530296 AND SERVICE BULLETIN MD90-53-027 R2__(TO 82).SDR AALA20101005TUL10Skate Angle · crackedVERTICAL STAB SKATE ANGLE DOUBLER HAS CRACK ON RIGHT SIDE. REMOVED OLD ANGLE, DYE CHECKED A/C ANGLE AND NO CRACKS FOUND. INSTALLED NEW ANGLE PER AARD 53-10-2.SDR SIMA201008104Attach Angle · crackedDURING MAINTENANCE BASE INSPECTION FOUND THE LEFT SIDE VERTICAL STABILIZER TO FUSELAGE FORWARD ATTACHED ANGLE TO BE CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED ATTACH ANGLE AND REPLACED WITH A NEW ANGLE IAW ENGINEERING ORDER EM-53MR-1281. THE ASDR SIMA201006706Attach Angle · crackedDURING MAINTENANCE BASE VISIT FOUND THE LEFT AND RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLES TO BE CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLETED REPAIRS TO ANGLES IAW ENGINEERING ORDER EM-53MR-1281. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR AALA20091222TUL09Angle · crackedTAIL VERTICAL STABILIZER SKATE ANGLE IS CRACKED AT FASTENER RIGHT SIDE STATION 1463. INSTALLED PREVENTIVE DOUBLER AND FILLER PER AARD 53-10-00-2.SDR AALA20091202TUL13Attach Angle · crackedFUSELAGE TO VERTICAL STABILIZER ATTACH ANGLE CRACKED. REMOVED DAMAGE AND INSTALLED REPAIR ANGLE PER AARD 53-10-00-2.SDR AALA20091029TUL03Skate Angle · crackedFUSELAGE TO VERTICAL STABILIZER LEFT SKATE ANGLE IS CRACKED BETWEEN FASTENER HOLES. INSTALLED DOUBLER.SDR C2XA09TY250Fitting · corrodedFRM 75 HAS AREAS OF FRETTING AT VERT STAB FITTING. REMOVED FITTING, REMOVED CORROSION FROM SKIN AND FITTING AROUND BOLTS. C/W NDI, ALODINED, PRIMED AND INSTALLED IAW SRM 51-40-02, AMM 51-20-01 AND EC 5310-01317.SDR C2XA09TY249Attach Bracket · corrodedFRETTING AT FRM 75 STR 1R AT FUSELAGE TO STAB ATTACH BRACKET AS MARKED. REMOVED FITTING AT FRM 75, BLENDED CORROSION, PERFORMED DYE-PEN, REPAIRED FITTING AND INSTALLED IAW EC5310-01480, EMB 145 SRM 51-40-02 AND EC5310-01317.SDR USAA2009052991349Hinge Pin · corrodedCLT - C5 - MAJOR REPAIR - NR 03-0555-8-0074/001 - CORROSION ON LEFT HAND HORIZONTAL INNER HINGE PIN NEAR TAPERED END. REPLACED INNER & OUTER HINGE PIN IAW US AIRWAYS TASK CARD 03-0555-8-0074.SDR USAA2009052991348Hinge Pin · corrodedCLT - C5 - MAJOR REPAIR NR 03-0555-8-0108/001 - CORROSION ON RIGHT HAND HORIZONTAL INNER HINGE PIN NEAR TAPERED END. REPLACED INNER & OUTER HINGE PIN IAW US AIRWAYS TASK CARD 03-0555-8-0108.SDR ZZDA2009098Attach Fitting · crackedFUSELAGE AFT SECTION FWD OF VERTICAL STABILIZER REAR SPAR ATTACH TANG STA Y=1178.225 AND LONG 2R TEAR STRAP IS CRACKED PASSING FASTENER HOLE. CUT OUT DAMAGED AREA OF TEAR STRAP ON AFT FUSELAGE SECTION FWD OF VERTICAL STAB REAR SPAR STA Y=1178.225 AND L2R, FABSDR 2009FA0000068Channel · crackedUPON REMOVAL OF THE HORIZONTAL STABILIZER, IT WAS NOTED THE FUSELAGE ATTACH FITTING CHANNEL APPARENTLY HAD BECOME FILLED WITH WATER, FROZE AND BURST. A (3) INCH CRACK ACROSS THE SPAN OF THE ATTACH FITTING SHOWED SIGNS OF BULGING OUTWARD. INSPECTION IN THIS ARESDR UPS09M54546Drag Angle · misrepairedINSPECTION TYPE:3C REPAIR SURVEY SEQ 255-F1-011 DRAG ANGLE FOR FUSELAGE TO VERTICAL STAB BETWEEN FS 2152-2164 LONGERON 2R HAS AN EXISTING REPAIR ANGLE INSTALLED NOT ON MRCSSR AND NO SRM REPAIR. REMOVED EXISTING REPAIR, FABRICATED AND INSTALLED REPLACEMENT REPSDR AALA2009020900055Plate · corrodedNUMBER SIX PLATE LUG BORE CORRODED AND OUT OF LIMITS. INSTALLED SERVICEABLE NUMBER SIX LUG PLATE PER CARD K2988AA.SDR AALA2009020900054Plate · corrodedNUMBER FIVE PLATE LUG BORE CORRODED AND OUT OF LIMITS. INSTALLED SERVICEABLE NUMBER FIVE LUG PLATE IN ACCORDANCE WITH WORK CARD K2988AA.SDR AALA200910560Attach Angle · crackedRIGHT ATTACH ANGLE, VERTICAL STABILIZER IS CRACKED. INSTALLED REPAIR ANGLE DOUBLER PER AARD 53-10-00-2, REFERENCE ECO K2221CC.SDR CA080715002Attach Fitting · cracked(CAN) LT ATTACH FITTING CRACKED AT LOWER OUTSIDE RADIUS ADJACENT TO AN 4-6A ATTACH BOLT.SDR TRAX200800435Attach Angle · crackedSUSPECTED CRACK AT RIGHT SIDE BASE OF VERTICAL STAB AT FS 1181. WORK COMPLETED IN ACCORDANCE WITH: PERFORMED EDDY CURRENT INSPECTION OF RIGHT SIDE BASE OF VERTICAL STAB AT FS 1181 IAW CRJ700 NDTM 51-20-006. AREA IS CONFIRMED CRACKED AND MARKED. 03/19/08 VSDR TRAX200800436Drag Angle · crackedSUSPECTED CRACK AT LEFT SIDE BASE OF VERTICAL STAB AT FS 1181. WORK COMPLETED IN ACCORDANCE WITH: PERFORMED EDDY CURRENT INSPECTION OF LEFT SIDE OF BASE OF VERTICAL STAB AT FS 1181 PER CRJ700 NDTM 51-20-006. AREA IS CONFIRMED CRACKED AND MARKED. 03/19/08 VSDR DHL2008805502Angle · corrodedCORROSION AT RT VERT STAB TO FUSELAGE JOINT LWR ANGLE, STA 1800.000 L-2R - L-3R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-5 FIG 16A SHEET 1, 2. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. CUT OUT DAMAGED SSDR UPS08851864Attach Angle · crackedINSPECTION TYPE:C2 VERT FIN TO FUSELAGE ATTACH ANGLE CRACKED AND CORRODED LT SIDE STA 1766. REPAIRED VERT FIN TO FUSELAGE ATTACH ANGLE IAW SRM 53-02-05-FIG 16A.SDR A6WA200740656Handle · crackedMAIN AVIONICS DOOR HANDLE CRACK MAIN AVIONIC DOOR HANDLE REPLACED IAW CRJ 200 SRM 51-42-06. (M)SDR TRAX200701501Drag Brace · crackedDRAG BRACE FOR FUSELAGE TO VERTICAL STAB, T/E CRACKED. 10-29-07 REPAIRED DRAG BRACE ANGLE IAW REO 670-55-31-018.SDR ABXA070281Angle · crackedDURING ROUTINE SERVICE BULLETIN INSPECTION OF LEFT DORSAL FIN ATTACH ANGLE, FOUND ANGLE CRACKED. REPLACED ANGLE IAW DC9 SRM 51-30-2 AND 51-30-5.SDR C2XA07TY044Attach Fitting · corrodedTYS - DURING A CURRENT C-CHECK INSPECTION, THE VERTICAL STAB ATTACH FITTING AT FRAME 75 WAS FOUND FRETTING. MAINTENANCE REMOVED AND REPLACED THE VERTICAL STAB FITTING AT FRAME 75 IAW EC5310-01317. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF SDR 2007UALA01334Fitting · corrodedVERTICAL STAB FUSELAGE FITTING AT BS 1088 RIGHT AFT PRIMARY FITTING FORWARD FACE CORRODED. [SUP 05-16-07] MAJOR REPAIR: REMOVED CORROSION AND SPOT FACED FORWARD FACE OF AFT RIGHT HAND SIDE PRIMARY FITTING.SDR DLM90070196Attach Angle · crackedTHE RT FUSELAGE TO VERTICAL STABILIZER ATTACH ANGLE WAS FOUND WITH A CRACK NEAR THE AFT END OF THE ANGLE. THE CRACK MEASURED 1" LONG AND IS TYPICAL OF CRACKS DOCUMENTED PER BAC S/B MD90-53-027. THE CRACK WAS TRIMMED OUT AND REPAIRED WITH A REPAIR ANGLE PER TSDR LR7A07012Angle · crackedDURING SCHEDULED A CHECK PER JOB CARD HA1200, FOUND DORSAL FIN ATTACH ANGLE CRACKED AT FS 848, WL285, RBL10. REPAIRED FRAME IAW LAC MEA 382-53-07-010.SDR ABXA070022Rivet · shearedLEFT VERTICAL STAB ATTACH ANGLE CHECKED AND HAD 2 SHEARED RIVETS. REPAIRED LEFT VERTICAL STAB ATTACH ANGLE IAW DC9 SRM 53-05, FIG 23.SDR ASAA0741348Attach Angle · crackedVERTICAL STABILIZER AT REAR SPAR AREA PANEL ATTACH ANGLE CRACKED AT APPROX FIN STA 140. VERTICAL STABILIZER REAR SPAR TO SKIN ATTACH ANGLE AT FIN STA 140 REPLACED IAW SRM 51-40-02.SDR TRAX200700001Attach Angle · crackedPOSSIBLE CRACK AT LEFT VERTICAL STAB TO FUSELAGE ATTACH ANGLE AFT END (MARKED). PERFORMED ET INSPECTION OF LT ATTACH ANGLE IAW CRJ 700 NDT MANUAL PART 1, CHAPTER 51-20-006. ANGLE IS CRACKED IN RADIUS. CUT OUT DAMAGED AREA PER REO 670-55-31-015. ALL WORK DOSDR DALA1154279258Attach Angle · damagedFUSELAGE TO VERTICAL STABILIZER ATTACH ANGLE REPAIR OD2006- SR-043 NRC B55-061119-328 BOEING APPROVAL 1-257893345-5.SDR PIDR2006043Fitting · corrodedCORROSION ON THE FORWARD FACE AND INSIDE DIAMETER OF THE RT FORWARD DRAG ANGLE FITTING AT THE VERTICAL STABILIZER AFT RT ATTACH FITTING. REPLACED FITTING IAW SRM 51-40-02, 51-40-03, AND DRAWING NR 65-53744.SDR 2006UALA01151Attach Fitting · corrodedFOUND VERTICAL STAB ATTACH FITTINGS, AFT PRIMARY FITTINGS, RT AFT, RT FWD, LT AFT FITTING DRAG ANGLES CORRODED.SDR 2006UALA01140Attach Fitting · corrodedFOUND VERTICAL STAB BS 1088 LT AND RT PRIMARY FUSELAGE ATTACH FITTINGS CORRODED ON FWD AND AFT FACES.SDR 2006FMAA02Reinforcement · crackedFOUND A .5 INCH LONG CRACK IN THE IB ANGLE-TAILCONE REINFORCEMENT LT FROM TOP OF ANGLE DOWN TO WITHIN .25 INCH OF IB HORIZONTAL MOUNTING BOLT HOLE. (K)SDR ASOA06188Attach Bracket · corrodedDURING A C-CHECK, THE FS 349 ATTACHMENT, LBL 36, WAS FOUND TO BE CORRODED. AFTER MAINTENANCE BLENDED, ALODINED, AND PRIMED THE FS 349 ATTACHMENT, LBL 36, IT WAS FOUND TO BE WITHIN ACCEPTABLE LIMITS IAW SRM. (K)SDR CA060321013Hinge Bracket · damagedBOTH THE FORWARD HORIZONTAL STABILIZER ATTACH HINGE BRACKETS (C3FS472-7 RT AND C3FS473-7 LT) WERE FOUND TO BE BUSHED BEYOND SERVICEABLE LIMITS. VIKING AIR HAD GIVEN A MAXIMUM OD OVERSIZE BUSHING OF .500. DURING INSPECTION THE BUSHINGS WERE MEASURED AT .650 +SDR CA051017008Fitting · unserviceableRT HORIZONTAL STABILIZER MOUNT FITTING FOUND CRACKED. THE STABILIZER SPAR WAS FOUND DAMAGED AS A RESULT OF THE FITTING DAMAGE AND WAS REPLACED ALONG WITH THE STABILIZER.SDR 2005FA0001134Fitting · brokenPILOT FOUND VERTICAL STABILIZER LOOSE ON PREFLIGHT. MAINTENANCE INSPECTED AND FOUND RT FWD ATTACHMENT FITTING BROKEN. REPLACED BOTH FWD FITTINGS WITH NEW PARTS. (K)SDR 2005FA0000972Bolt · looseAFTER USING AN ORBITAL WAXING BUFFER ON THE HORIZONTAL STABILIZER, THE OWNER NOTICED LOOSENESS AT THE HORIZONTAL STABILIZER LEADING EDGE AND THE OUTBOARD EDGE. INVESTIGATION REVEALED THAT BOTH FOWARD ATTACH BOLTS, P/N AN44-5A (IPC FIG 18A ITEM 1) WERE LOOSE. BSDR USAA050810Skate Angle · wornCLT - Q2 - SKATE ANGLE, 2 INCHES X 4 INCHES, WORN AREA, AFT END OF THE RT SKATE ANGLE AT THE BASE OF THE VERTICAL FIN TO FUSELAGE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS. (K)SDR USAA050780Channel · wornCLT - FOUND L-CHANNEL FRETTING WEAR .5 INCH BY 3 INCHES, FORWARD OF THE LEFT FORWARD VERTICAL FIN MOUNT AT BS 1016 NR 2412. FABRICATED NEW ANGLE AND INSTALLED IAW SRM 53-20-05. (M)SDR UPS05244732Fitting · crackedCLEAT CRACKED O/B OF S26R AT BS 600 LWR SECTION OF CLEAT ADJACENT TO S 26. REMOVED DAMAGED CLEAT IAW SRM 51-30-2. FABRICATED CLEAT IAW SRM 51-20-1. INSTALLED CLEAT IAW SRM 51-30-2.SDR IXXA05SMN11SFitting · crackedDURING ROUTINE C-CHECK INSPECTION, RT HORIZONTAL STABILIZER FITTING CRACKED 1 IN., XFS 47.000 - XFS 60.000 (LWR PART). REMOVED CRACKED FITTING IAW DC-8 SRM 51-1-20D PAGE 21. CLEANED, TREATED AND PRIMED IAW DC-8 SRM 51-1-8B. INSTALLED NEW FITTING IAW DC-8 SR
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