JASC 5534

Service difficulty reports · 820

Reports filed under 5534 · Vertical Stabilizer Miscellaneous 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 = '5534'
  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 SWIA2020061851088Shim · migratedFORWARD STEADY FITTING MOUNTED TO THE TOP OF THE VERTICAL STAB HAS MIGRATED SHIMS ON THE LT SIDE OUTBD BOLTS. REPLACED WITH NEW LT SIDE OUTBOARD SHIM AND NUTS(2(EA) ON FORWARD STEADY FITTING REF RIL AND REF AMM. THIS SDR FOR T/STEADY FITTING IS BEING SUBMITTJan 30, 2020 · N461SW · Cndair CL6002B19SDR SWIA2020031049240Attach Angle · chafed*THE VERITCAL STABILIZER LEADING EDGE PANEL LOWER FAIRING SUPPORT RIB'S RH UPPER ATTACH ANGLE IS CHAFED. (C CHECK) RO 3/7/2020 REMOVED AND INSTALLED A NEW ANGLE, ON THE VERTICAL STABILIZER LEADING EDGE, THE LOWER FAIRING SUPPORT RIB R-H UPPER ATTACH ANGLE Jan 17, 2020 · N905EV · Cndair CL6002B19SDR SWIA2020031049239Attach Angle · chafed*THE VERITCAL STABILIZER LEADING EDGE PANEL LOWER FAIRING SUPPORT RIB'S LH UPPER ATTACH ANGLE IS CHAFED. (C CHECK) RO 3/7/2020 REMOVED AND INSTALLED A NEW ANGLE, ON THE VERTICAL STABILIZER LEADING EDGE, THE LOWER FAIRING SUPPORT RIB L-H UPPER ATTACH ANGLE Jan 17, 2020 · N905EV · Cndair CL6002B19SDR VNAA2020010899902Drag Angle · crackedRH AFT VERTICAL DRAG ANGLE IS CRACKED FS 1200. 12/14/19 (PCC) M/A: 1. N/A C/A: 1. COMPLIED WITH BOMBARDIER REO 670-55-31-018 REV A DATED 2016-11-10. 12/19/19 M/A: 2. REPAIR REQUIRES TOPCOAT UP PAINT. 12/19/19 C/A: 2. APPLIED TOPCOAT IAW CRJ 900 SRM 51-25-01-00Jan 8, 2020 · N557NN · Cndair CL6002D24SDR SWAA2021051326028Skate Angle · chafedVERTICAL FIN L/H SKATE ANGLE HAS MULTIPLE SPOTS OF CHAFING DAMAGE BS1016 - BS1121. / REPAIRED VERTICAL FIN L/H SKATE ANGLE BTW. BS1016. TO BS1022 AS PER B737-700 SRM 53-80-71-2R-6 AND CHAFING DAMAGE LOCATED BS1022 TO BS1127 IS LIMITED TO EXTERIOR FINISH ONLY; Jan 3, 2020 · N7873A · Boeing 7377Q8SDR SWIA2020061851087Fitting · damagedSTEADY FITTING HAS 6 LOOSE BOLTS, WASHERS ON RIGHT HAND OUTBOARD BOLT CAN BE TURNED BY HAND. REPAIRED V/STAB STEADY FITTING ELONGATED HOLES AND LOOSE HDWR IAW REO. THIS SDR FOR T/STEADY FITTING IS BEING SUBMITTED AS A PART OF VDR_2020NM064006.Dec 23, 2019 · N900EV · Cndair CL6002B19SDR V0XD202001030003Drag Angle · crackedLH FWD VERTICAL STABILIZER DRAG ANGLE CRACKED. RECTIFICATION REPAIRED LH FWD STABILIZER FWD DRAG ANGLE IAW REO 670-55-31-018 REV. A 2016-11-10.Dec 12, 2019 · N613QX · Cndair CL6002C10SDR SWAA2022032544596Retainer · crackedL/H SIDE OF VERTICAL STAB. PANEL #323CL RETAINER IS CRACKED / REMOVED AND REPLACED L/H VERTICAL STAB PANEL #323CL RETAINER PER SRM 51-40-02Nov 28, 2019 · N431WN · Boeing 7377H4SDR FDEA2019120183141Intercostal · crackedUPON REMOVEL BANJO ACCESS, VERTICAL STABILIZER REAR CENTER SPAR TO REAR SPAR LEFT HAND LOWER PANEL INTERCOSTAL FOUND CRACK STATION 2164. VERTICAL STABILIZER REAR CENTER SPAR TO REAR SPAR LEFT HAND LOWER PANEL INTERCOSTAL STATION 2164 CARRIED OUT REPAIR AS PERNov 28, 2019 · N610FE · Doug MD11FSDR FDEA2019120183142Intercostal · crackedUPON REMOVAL BANJO ACCESS, VERTICAL STABILIZER REAR CENTER SPAR TO REAR SPAR, RIGHT HAND LOWER PANEL INTERCOSTAL FOUND CRACK STATION 2164. VERTICAL STABILIZER REAR CENTER SPAR TO REAR SPAR RIGHT HAND LOWER PANEL INTERCOSTAL AT STATION 2164 CARRIED OUT REPAIR Nov 28, 2019 · N610FE · Doug MD11FSDR SWAA2022032511330Angle · crackedVERTICAL STAB PANEL SUPPORT ANGLE ABOVE R/H FWD MOUNT LUG IS CRACKED (MARKED) / REMOVED AND REPLACED ANGLE PER SRM 51-10-02 AND SRM 51-40-02Nov 27, 2019 · N234WN · Boeing 7377H4SDR SWAA2022032428791Angle · corroded***CORROSION*** VERTICAL FIN CORROSION UNDER PANEL 324WL; AT LOWER O/B SUPPORT ANGLE; BODY STA. 1198; RUDDER STA. 151 APPROX. / REMOVED SUPPORT ANGLE FROM BODY STA 1198 RUDDER STA 151 APROX UNDER PANEL 324WL LOWER O/B RIB. AND INSTALLED REPLACEMENT SUPPORT ANGNov 22, 2019 · N7888A · Boeing 737752SDR V0XD2019110300004Drag Angle · crackedVERTICAL STABILIZER, RH AFT DRAG ANGLE CRACKED, CORRECTIVE ACTION: REPAIRED VERTICAL STABILIZER RH AFT DRAG ANGLE IAW BOMBARDIER REO#670-55-31-018 DATED 2016-11-10, BOMBARDIER REO#670-55-31-124 DATED 201910-26, AND GOJET ENGINEERING ORDER C700-55MR-001-REV O DOct 31, 2019 · N669CA · Cndair CL6002C10SDR SWAA2022032386994Panel · cracked324QL VERT STAB T/E LH PANEL CRACKED. (200-034) / REMOVED AND REPLACED VERTICAL STAB T/E L/H PANEL 324QL IAW B737 SRM 51-40-02-0G-0Oct 21, 2019 · N765SW · Boeing 7377H4SDR SWAA2022032365519Expansion Joint · crackedCRACK IN 'JOINT ASSY - EXPANSION VERT. FIN ' STA 1021.27 WL 308 (P/N 176A3101-26) (MARKED) / REMOVED & REPLACED JOINT ASSY - EXPANSION VERT. FIN STA. 1021.27 WL 308 IAW SRM 51-40-02-0G-0 PARA 4 & FIG 8Oct 20, 2019 · N562WN · Boeing 737790SDR AALA201909069022Splice Strap · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON VERTICAL STABILIZER TIP UPPER AND LOWER SPLICE STRAPS. REPLACED SPLICE STRAPS PER SRM 51-40-02-0G.Sep 4, 2019 · N199AN · Boeing 757223SDR V0XD201909090005Drag Angle · crackedVERTICAL STAB LT DRAG ANGLE CRACKED. CORRECTIVE ACTION: REPAIRED VERT STAB DRAG ANDLGE IAW REO670-55-31-018 REVA, 2016-11-10 BY COMPLYING WITH EO-C700-55MR-001-0.Aug 31, 2019 · N374CA · Cndair CL6002C10SDR SWAA2022031585727Channel · crackedVERTICAL STAB PANEL 324AR; SUPPORT CHANNEL ON BACK OF PANEL IS BROKEN. / EVALUATED DAMAGE. OUT OF LIMITS; REPLACED W/NEW SUPPORT CHANNEL P/N 172A6124U6 IAW BOIENG DWG 172A6124803 REV F AND SRM 51-40-02-0G-0 ATAG A20165.Aug 19, 2019 · N758SW · Boeing 7377H4SDR SWAA2022031585728Strap · crackedVERTICAL STAB PANEL 324AR; SUPPORT STRAP ON BACK OF PANEL IS CRACKED/BROKEN. / REMOVED AND INSTALLED NEW SUPPORT STRAP P/N 172A6124U10 ON THE PANEL # 324AR IAW B737-700 SRM 51-40-02-0G-0 AND DWG # 172A 6123 REV:A.Aug 19, 2019 · N758SW · Boeing 7377H4SDR SWAA2022031585729Strap · crackedVERTICAL STAB PANEL 323CR; SUPPORT STRAP ON BACK OF PANEL IS CRACKED/BROKEN. / REMOVED AND INSTALLED NEW SUPPORT STRAP P/N 172A6124Y8 ON THE PANEL # 323CR IAW B737-700 SRM 51-40-02-0G-0 AND DWG #172A6124 REV: 'F'Aug 19, 2019 · N758SW · Boeing 7377H4SDR 2019FA0000228Rivet · looseTHE AIRCRAFT CAME IN FOR AN INSPECTION AND WE NOTICED THE BOTTOM ROW OF RIVETS NEXT TO THE FUSELAGE ON BOTH SIDES OF THE VERTICAL STABILIZER HAVE BEEN WORKING. WE CONTACTED GULFSTREAM AND ARE WORKING TO GET A FIX FOR THE ISSUE.Jul 22, 2019 · N30DJ · Gulstm GIVSDR SWAA2022031183033Bracket · crackedVERTICAL STAB ACCESS PANEL 323CL LOWER RETAINING BRACKET CRACKED. / REMOVED AND REPLACED CRACKED RETAINER ON VERTICAL STAB PANEL 323CL IAW SRM 51-40-02-0G-0; SRM 51-40-05-0G-0 AND BOEING DWG 172A6124 REV E. ATAG A95924Jul 17, 2019 · N750SA · Boeing 7377H4SDR IPXA2019071944620Intercostal · crackedINSPECTION TYPE:4CLOWER PYLON CARRY THRU REAR SPAR INTERCOSTAL AT CRACKED AT STA. YID=375, XID=-7.1 AND ZID=65.REPAIRED CRACKED LOWER PYLON CARRY THRU REAR SPAR INTERCOSTAL AT STA. YID=375, XID=-7.1 AND ZID=65 IAW SRM 55-30-02 REPAIR 7 FIG. 204. (MAJOR)Jul 11, 2019 · N273UP · Doug MD11FSDR V0XR20190705009Drag Angle · crackedLT FWD VERTICAL DRAG ANGLE AT FS 1200 CRACKED. CORRECTIVE ACTION: REPAIRED LT FWD VERTICAL DRAG ANGLE BY CUTTING DAMAGED AREA, FABRICATING AND INSTALLED REPAIR PARTS IAW REO 670-55-31-018 REV.A DATED 2016-11-10, SRM 51-25-16, 51-42-06, 51-42-21, 51-21-11, 51-2Jul 9, 2019 · N379CA · Cndair CL6002C10SDR SWAA2022031100646Retainer · crackedLEFT VERTICAL FIN PANEL 323AL HORIZONTAL RETAINER CRACKED / R&R LEFT VERTICAL FIN PANEL 323AL HORIZONTAL RETAINER PER SRM 51-40-02.Jun 25, 2019 · N778SW · Boeing 7377H4SDR SWAA2019071935032Skate Angle · damagedLT VERTICAL STABILIZER SKATE ANGLE DAMAGED BETWEEN BS. 1005 TO BS. 1131. R&R SKATE ANGLE IAW DWG.Jun 25, 2019 · N417WN · Boeing 7377H4SDR LR7A2019062401733Attach Angle · corrodedDURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5511, FOUND VERT STAB LT / RT LOWER ATTACH ANGLE CORRODED AT FWD AND REAR LOCATED AT FS946-1128, VSS0, WL285, LBL20, AND RBL20. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# XXXX.Jun 24, 2019 · N409LC · Lkheed 382GSDR LR7A2019062401732Cap · crackedDURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5511, FOUND VERT STABILIZER LT FRONT BEAM CAP WITH 6" CRACK. REPAIRED IAW SMP583 SRM FIG. 55-040-12. NR# 2336.Jun 24, 2019 · N409LC · Lkheed 382GSDR SWAA2019070334382Drag Brace · corrodedRT VERTICAL STABILIZER REAR SPAR ATTACH FITTING AFT OUTBOARD FAIL SAFE DRAG BRACE CORRODED AT BS. 1016, RBL 2. R&R DRAG BRACE IAW DWG & SRM.Jun 8, 2019 · N737JW · Boeing 7377H4SDR SWAA2022030979605Channel · brokenRH VERTICAL FIN TO BODY PANEL 324AR U-CHANNEL LOWER EDGE BROKEN OFF / REPLACED DAMAGE U-CHANNEL ON PANEL 324AR LWR EDGE I.A.W EDGE I.A.W B737-700 SRM 51-40-02-0G & BOEING DWG # 172A6134. TY:DWG; ID:0001; REV:4EMay 29, 2019 · N738CB · Boeing 7377H4SDR SWAA2022030979606Retainer · crackedRH VERTICAL FIN TO BODY PANEL 324AR PANEL RETAINING CLIP CRACKED / REPLACED DAMAGE RETAINER ON PANNEL 324AR I.A.W SRM 51-40-02-0G & BOEING DWG # 172A6123 TY:DWG ID:0001 REV:A. A-TAG # SI1255.May 29, 2019 · N738CB · Boeing 7377H4SDR SWAA2022030979607Panel · crackedRH VERTICAL FIN CLOSEOUT PANEL 323AR CRACKED UNDER RETAINER TAB / REPLACED CRACKED R/H VERTICAL FIN CLOSED OUT PANEL 323AR LOCATED + DRILLED NEW PANEL IAW DWG #172A6122 TRETAED + PRIMED + APPLIED EXTERIOR FINISH IAW SRM 51-20-01-0G-0 + AMM 51-21-99-300 ATAG WNMay 29, 2019 · N738CB · Boeing 7377H4SDR SWAA2022030881797Panel · elongatedVERTICAL FIN L/E PANEL 322B HAS ELONGATED FASTENER HOLE ON L/H SIDE AT L/E STA 314.2 / VERTICAL FIN L/E PANEL FASTENER HOLE ON L/H SIDE AT L/E STA 314.2 WAS REPAIRED ON ATS COMPONENTS JOB#523817; CUSTOMER RO# 0550028-D8R.May 21, 2019 · N747SA · Boeing 7377H4SDR IPXA2019051742221Intercostal · crackedINSPECTION TYPE:4C LOWER PYLON CARRY THRU INTERCOSTAL IS CRACKED AT STA. YID=375, XID=-7.1 AND ZID=65. REPAIRED CRACKED LOWER PYLON CARRY THRU INTERCOSTAL AT STA. YID=375, XID=7.1 AND ZID=65 IAW EA 011-5530-01-A7765 REV. I/R AND UPS EO MD11-5330-72605-A. (MAJOMay 8, 2019 · N291UP · Doug MD11FSDR SWAA2022030878187Angle · brokenR/H VERTICAL STABILIZER; ACCESS PNL 324AR WITH SUPPORT ANGLE BROKEN / REMOVED AND REPLACED ANGLES (CHANNEL AND RETAINER) AT R/H VERTICAL STABILIZER; ACCESS PANEL 324 AR AS PER REF B737-700 SRM SRM 51-40-02-06-0Apr 25, 2019 · N735SA · Boeing 7377H4SDR FDEA201904231017Not Reported · cracked2IN CRACK ON LT LOWER CENTER VERTICAL ON NR 2 ENG. COMPLIED WITH FINAL EA# 1-5530-T0346813 A.Apr 23, 2019 · N587FE · Doug MD11FSDR SWAA2022030476344Panel · elongatedVERT STAB PNL 323CR HAS OVERSIZED AND ELONGATED FASTENER HOLE AT LWR AFT CORNER. / REMOVED CHANNEL ON VERTICAL STAB PANEL 323CR. FABRICATED NEW PANEL; TREATED; PRIMED AND APPLIED TOP COAT. REINSTALL CHANNEL TO NEW PANEL IAW EA 190252 REV IR; AND S/W EA 1-755-4Mar 27, 2019 · N731SA · Boeing 7377H4SDR SWAA2022030476340Strip · crackedVERT STAB PNL 323CL RETAINER STRIP CRACKED AND WORN THRU. / REMOVED AND INSTALLED NEW RETAINER AT VERT. STAB. PANEL #323CL IAW SRM 51-40-02-0G-0; VERIFED NEW RETAINER IAW DWG 172A6124 P/N 172A6124Y7; LOCATED AND DRILLED NEW RETAINER IAW SRM 51-40-05-0G-0 TAG#AMar 26, 2019 · N731SA · Boeing 7377H4SDR DALA2019031501703Web · crackedSUMMARY OF NRC 00043: SUPPORT WEB (RT AREA) IN VERTICAL STABILIZER INNER STRUCTURE STA ZRS 134 WAS REPAIRED PER ETI-90-19-012 REV. 3 AND ER/A. 576366-14 REV.ORIGINAL CRACK LENGTH 2.500IN. (LP# 0985085)Mar 14, 2019 · N906DA · Doug MD9030SDR HALA2019031201617Structure · corrodedVERTICAL STABILIZER TRAILING EDGE LT #2 T CHORD CORRODED. REPLACED T CHORD PER SRM 51-44-11, 51-21-11, AND 51-46-11. LP 0980976Mar 12, 2019 · N390HA · Airbus A330243SDR HALA2019031201616Structure · corrodedVERTICAL STABILIZER TRAILING EDGE RT NR 3 T CHORD CORRODED. REPLACED T CHORD PER SRM 51-44-11, 51-21-11, AND 51-46-11. LP 0980967Mar 12, 2019 · N390HA · Airbus A330243SDR HALA2019031201615Structure · corrodedVERTICAL STABILIZER TRAILING EDGE RT NR 2 T CHORD CORRODED. REPLACED T CHORD PER SRM 51-44-11, 51-21-11, AND 51-46-11. LP 0980963Mar 12, 2019 · N390HA · Airbus A330243SDR HALA2019031200120Structure · corrodedVERTICAL STAB TRAILING EDGE RHS #2 T CHORD SUSPECT CORROSION AROUND FASTENER HOLES. REMOVAL OF CORROSION C/OUT IAW SRM 51-74-00 REV.98.01. CORROSION STILL EVIDENT IAW NTM 51-10-02-221-001-A REV. 96 AT BLEND DEPTH OF .058". BLEND DEPTH BEYOND 50% MATERIAL THICKMar 12, 2019 · N390HA · Airbus A330243SDR HALA2019031200119Structure · corrodedVERTICAL STAB TRAILING EDGE RHS #3 T CHORD SUSPECT CORROSION AROUND FASTENER HOLES. // REMOVAL OF CORROSION C/OUT IAW SRM 51-74-00 REV.98.01. CORROSION STILL EVIDENT IAW NTM 51-10-02-221-001-A REV. 96 AT BLEND DEPTH OF .058". BLEND DEPTH BEYOND 50% MATERIAL THMar 12, 2019 · N390HA · Airbus A330243SDR FDEA201902160428Intercostal · crackedEMPENNAGE : UPON REMOVAL VERTICAL STABILIZER RIGHT HAND REAR CENTER SPAR TO REAR SPAR INTERCOSTAL STATION 2164 FOUND CRACK ON AFT END. VERTICAL STABILIZER RIGHT HAND CENTER SPAR TO REAR SPAR INTERCOSTAL AT STATION 2164 CRACK ON AFT END REPAIR CARRIED OUT AS PFeb 16, 2019 · N608FE · Doug MD11FSDR V0XD201902030004Drag Angle · crackedVERTICAL STAB LT AFT DRAG ANGLE IS CRACKED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW EO C700-55MR-001-0.Feb 2, 2019 · N158GJ · Cndair CL6002C10SDR V0XD201902030003Drag Angle · crackedVERTICAL STAB RT AFT DRAG ANGLE IS CRACKED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW EO C700-55MR-005-0.Feb 2, 2019 · N158GJ · Cndair CL6002C10SDR ASOA201902027026Stiffener · crackedTYS A/C IS IN FOR A C-CHECK WHEN INSPECTION FOUND THE VERTICAL STAB TRAILING EDGE R/H LOWER STIFFENER CRACKED AT THE LOWER RIVETS. MAINTENANCE REPAIRED THE AREA IAW ETD 2019-145-010869. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.Feb 2, 2019 · N16546 · Emb EMB145LRSDR SWAA2022030238314Retainer · crackedRETAINER WHICH SECURES VERTICAL STABILIZER PANEL 324AL TO STRUCTURE IS CRACKED. / INSTALLED NEW RETAINER PER SRM 51-40-02Jan 24, 2019 · N412WN · Boeing 7377H4SDR DALA2019011800370Attach Angle · crackedCRACKED RT INTERNAL VERTICAL STABILIZER ATTACH ANGLE ON STA. Y= 1475. RT INTERNAL VERTICAL STABILIZER ATTACH ANGLE ON STA. Y= 1475 WAS REPLACED PER SRM 51-30-02 AND 51-30- 05VOL.II. (LP# 0907778)Jan 17, 2019 · N919DN · Doug MD9030
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