JASC 5530

Service difficulty reports · 2,534

Reports filed under 5530 · Vertical Stabilizer, 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 = '5530'
  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 SWAA2022022468949Panel · delaminatedLEFT HAND VERTICAL STABILIZER PANEL 324 AL EDGE OF PANEL IS DELAMINATED / REPAIRED DELAMINATED EDGE OF L/H VERTICAL STAB PANEL 324 AL IAW 737-700 SRM 55-30-01-2R-9 AND 51-70-05-2R-6 LEAD 191 10-24-18Oct 10, 2018 · N709SW · Boeing 7377H4SDR SCNA20180926115Antenna · damagedHF ANTENNA MISSING PAINT. HF ANTENNA FIBERGLASS IS DAMAGED BEYOND LIMITS. HF ANTENNA FIBERGLASS IS DAMAGED BEYOND LIMITS. NEW ANTENNA ON ORDER. REMOVED AND INSTALLED HF ANTENNA. VERTICAL FIN SIDE FASTENERS INSTAELLD. COUPLER SLEEVE AND FEEDER TUBE TO BE INSTASep 26, 2018 · N805SY · Boeing 7378Q8SDR DALA2018082855295Web · crackedCRACKED WEB SURROUNDING JACKSCREW ASSEMBLY, RT SIDE AT THE VERTICAL STABILIZER. THE WEB WAS REPAIRED IAW ER/A 570884-14, REV ORIGINAL, AND ETI-90-18-043, REV 1.Aug 24, 2018 · N960DN · Doug MD9030SDR HYIA20180815001Angle · corrodedCORROSION WAS DISCOVERED ON ONE OF THE LEFT SIDE VERTICAL STABILIZER AFT ANGLES. REMOVED AND REPLACED THE ANGLE.Aug 13, 2018 · N223PB · Cessna 402CSDR FDEA2018082990Intercostal · crackedVERT STAB REAR CENTER SPAR TO REAR SPAR INTERCOSTAL RIGHT SIDE AFT END WAS FOUND CRACKED AT VSS 2164. REPAIRED IAW EA 1-5530-T0341715, PART 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 10, 2018 · N585FE · Doug MD11FSDR FDEA2018082989Intercostal · crackedVERTICAL STABILIZER REAR CENTER SPAR TO REAR SPAR INTERCOSTAL LT SIDE, AFT END, WAS CRACKED AT VSS 2164. REPAIRED IAW EA 1-5530-T0341716, PART 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 10, 2018 · N585FE · Doug MD11FSDR V0XD20180810002Drag Angle · crackedVERTICAL STABILIZER FWD DRAG ANGLE WAS CRACKED AT BS 1200. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED A REPAIR IAW REO 670-55-31-018, REV A, AND 670-55-31-108.Aug 9, 2018 · N369CA · Cndair CL6002C10SDR V0XD2018081001Drag Angle · crackedLEFT VERTICAL STABILIZER AFT DRAG ANGLE WAS CRACKED AT BS 1200. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED A REPAIR IAW REO 670-55-31-018, REV.Aug 9, 2018 · N369CA · Cndair CL6002C10SDR HNAA2018080800182Drag Angle · crackedVERTICAL STAB DRAG ANGLE ON THE LEFT SIDE OF FRAME 75 REPAIR DOUBLER WAS CRACKED AFT OF DOUBLER. R & R THE LT VERTICAL STABILIZER FWD LOWER DRAG ANGLE IAW SRM 51-40-02, AND 53-31-01, ITEM 11, AND FIGURE 219.Aug 2, 2018 · N635AE · Emb EMB145LRSDR ASOA201807257141Bearing · wornTYS A/C IS IN C-CHECK WHEN INSPECTION FOUND EVIDENCE OF SOME WEAR ON THE VERTICAL STAB BORES OR SPHERICAL BEARINGS. MAINTENANCE PERFORMED OPS CHECKS OF BOTH DIHEDRAL AND FOUND TO BE GOOD IAW AMM 51-50-01. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OJul 25, 2018 · N19554 · Emb EMB145LRSDR K11A2018112124013Beam · crackedVERTICAL STAB KICK LOAD BEAM WEB POST CRACKED.Jul 21, 2018 · N724CK · Boeing 727225SDR FDEA2018082902188Rib · wornAFT FUSELAGE BULKHEAD, LEFT SIDE BELOW THE UPPER LIGHT ASSEMBLY, HORIZONTAL RIB HAD DEEP WEAR. REPAIRED THE DAMAGED RIB IAW EA 8-5310-TO341640.Jul 19, 2018 · N381FE · Doug MD1010FSDR ASOA201806157109Bushing · damagedTYS A/C IS IN FOR A C-CHECK INSPECTION WHEN INSPECTORS FOUND PITTING IN THE LT VERTICAL STAB SPHERICAL BEARING BEYOND LIMITS. MAINTENANCE REMOVED AND INSTALLED A NEW FIRST OVERSIZED BUSHING IAW SRM 55-30-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE ENJun 15, 2018 · N14203 · Emb EMB145XRSDR ASOA201806157108Bushing · damagedTYS A/C IS IN FOR A C-CHECK INSPECTION WHEN INSPECTION FOUND THE RT VERTICAL STAB SPHERICAL BEARING HOUSING PITTED BEYOND LIMITS. MAINTENANCE REMOVED AND INSTALLED THE FIRST OVERSIZED BUSHING IAW SRM 55-30-02,ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE EJun 15, 2018 · N14203 · Emb EMB145XRSDR DALA2018061404006Structure · crackedCRACKS FOUND ON RT SIDE OF STRUCTURE SURROUNDING JACKSCREW ASSEMBLY. THE CRACKS WERE ATTENDED IAW ETI-90-18-035, REV 2, AND ER/A 569425-14, REV ORIGINAL.Jun 13, 2018 · N937DN · Doug MD9030SDR DALA2019102506148Structure · crackedCRACK INDICATION ON RHS VERTICAL STABILIZER NEAR ZFS=52. FOLLOW ON ACTION IS REQUIRED. ERA 569170-14AD ISSUED FOR REPAIR TO CRACK INDICATION ON RHS VERTICAL STABILIZER NEAR ZFS=52. FOLLOW ON ACTION IS REQUIRED. TEMPORARY REPAIR APPROVAL GRANTED FOR 24 MONTHS FJun 9, 2018 · N960DL · Doug MD88SDR ASOA2018060871051Housing · damagedRT AND LT SPHERICAL BEARING HOUSINGS HAVE DISPLACED METAL. REPAIRED LT AND RT SPHERICAL BEARING HOUSING IN ACCORDANCE WITH SRM 55-30-02.Jun 8, 2018 · N11565 · Emb EMB145LRSDR JGVR201806054001Hinge Bracket · corrodedMECHANICALLY BLENDED CORROSION ON THE MIDDLE RUDDER HINGE BRACKET UPPER HINGE HALF ON VERTICAL STABILIZER NEAR THE BONDING STRAP HOLE, PERFORMED EDDY CURRENT AND ULTRASONIC THICKNESS INSPECTIONS AND SUBMITTED FINDINGS TO MANUFACTURER ENGINEERING. TREATED METALJun 5, 2018 · N324QS · Cessna 680CESDR DALA2018050303012Angle · crackedRAM AIR INLET RIGHT INTERNAL SKATE ANGLE HAD A 01 INCH CRACK AT AFT END. REMOVED AND REPLACED THE ANGLE IAW DWG 5912188.May 2, 2018 · N924DN · Doug MD9030SDR GTIA2018042502605Hinge Arm · distortedDISTORTION FOUND ON THE HINGE ARMS AT RIB 5, VERTICAL STAB.Apr 25, 2018 · N525NK · Airbus A319132SDR WVER2018050100010Drag Angle · crackedRIGHT VERTICAL DRAG ANGLE, FWD, CRACKED. CONFIRMED BY EDDY CURRENT.Apr 21, 2018 · N904FJ · Cndair CL6002D24SDR FDEA201804211079Intercostal · crackedRIGHT REAR CENTER EMPENNAGE SPAR TO REAR SPAR INTERCOSTAL FOUND CRACKED.Apr 21, 2018 · N595FE · Doug MD11FSDR SIMA20180414002Hinge Fitting · damagedDAMAGED UPPER RUDDER 1 HINGE FITTING ON VERTICAL STAB. REMOVED AND REPLACED THE DAMAGED HINGE IAW SRM 51-40-02, AMM 20-10-01. SRM 51-20-03, CPM 51-21-04. CPM 51-21-05 AND 51-21-06.Apr 14, 2018 · N841AE · Emb EMB135KLSDR GQVA20180413002Beam · corrodedCORROSION WAS FOUND AT MULTIPLE SITES ON THE VERTICAL STABILIZER REAR SPAR CAPS. AFTER BLENDING, THE REMAINING THICKNESS AT EACH SITE WAS MEASURED USING ULTRASOUND. ALL CORROSION DAMAGE WAS REMOVED BY BLENDING AND CESSNA ENGINEERING ISSUED A REPAIR DEFINITION Apr 10, 2018 · N915FG · Cessna 680CESDR SWAA2022021006560Stabilizer · erodedVERTICAL STAB; RH FWD ATTACH BOLT HOLE HAS ERROSION MEASURED AT 1.0' BEFORE DAMAGE REMOVAL. / REPAIRED PER EA 1-755-4082.Apr 7, 2018 · N220WN · Boeing 7377H4SDR SWAA2022021006559Stabilizer · erodedVERTICAL STAB. LH FWD ATTACH BOLT HOLE HAS EROSION. MEASURED AT 1.O' BEFORE DAMAGE REMOVAL / REPAIRED PER EA 1-755-4082Apr 7, 2018 · N220WN · Boeing 7377H4SDR 2019FA0000363Tube · crackedUPON VISUAL INSPECTION, FOUND THE MOST AFT VERTICAL TUBING OF AIRCRAFT STRUCTURE SHEARED ABOVE TAIL GEAR ATTACH POINT BUT BELOW 45 ANGLE BRACE. AIRCRAFT USED DAILY FOR FLIGHT TRAINING WITH AN AVERAGE OF 100 HOURS OF FLIGHT TIME EVERY 45 DAYS.Apr 2, 2018 · N797L · Bbavia 7ECASDR DALA2018070504360Structure · crackedWHILE PERFORMING VISUAL INSPECTION PER SRM 55-30-04 P 4, FOUND CRACK TO GO EXCEEDED PAST STOP DRILLS AND TO BE PAST MAX TOLERANCE. PERFORMED FPI INSPECTION OF SUBJECT AREA TO MARK ENDS OF CRACKS PER SRM 55-30-05. COMPLETED PERM REPAIR PER SRM 55-30-05 PAR 5.Mar 26, 2018 · N920DN · Doug MD9030SDR IPXA2018040628278Panel · delaminatedINSPECTION TYPE: SEG4, VERTICAL STAB RT SIDE LOWER FORWARD TORQUE BOX PANEL DELAMINATED. REPLACED THE PANEL IAW SRM 51-40-02-0G.Mar 17, 2018 · N451UP · Boeing 75724APFSDR DALA2018031001547Channel · crackedCHANNEL CRACKED AROUND JACKSCREW.Mar 9, 2018 · N911DA · Doug MD9030SDR DALA2018021500939Structure · crackedA CRACK WAS FOUND AT CF 1200, RT FWD SIDE JUST FORWARD OF THE RUDDER HYD SHUTOFF VALVE. REPAIRED IAW ER/A 565689-14, REV ORG.Feb 14, 2018 · N945AT · Boeing 717200SDR DALA2021122908127Skate Angle · crackedA CRACK WAS FOUND FORWARD OF THE VERTICAL STABILIZER CANTED FRAME AT STA 1189 AT LH SKATE ANGLE ATTACH FASTENER. ACCOMPLISH SECTION II: INITIAL INSPECTION 3800 FLIGHT CYCLES AFTER ACCOMPLISHMENT OF SECTION I: PERMANENT REPAIR. ACCOMPLISH SECTION III: REPETITIVFeb 11, 2018 · N945AT · Boeing 717200SDR WVER2018021090203Drag Angle · crackedRIGHT VERTICAL FORWARD DRAG ANGLE CRACKED. REPAIRED THE DRAG ANGLE IAW REO 670-55-31-018.Feb 10, 2018 · N902FJ · Cndair CL6002D24SDR 2018F00088Drag Angle · damagedVERTICAL STAB DRAG ANGLE DAMAGEJan 31, 2018 · N349QS · Cessna 680CESDR DALA2018011900299Structure · crackedOPEN HOLE INSPECTION IAW NDTSPM 06-10-01.003 OF SEVENTH HOLE FROM BOTTOM OF REPAIR INDICATES A CRACK. REPAIRED IAW ERA 565018-14, REV ORG.Jan 18, 2018 · N914DL · Doug MD88SDR V0XD20180116002Drag Angle · crackedAFT DRAG ANGLE ON THE LH SIDE OF THE VERTICAL STABILIZER IS CRACKED. CORRECTIVE ACTION: REPAIRED AFT DRAG ANGLE ON THE LH SIDE OF THE VERTICAL STABLIZER IAW BOMBARDIER REO 670-55-31-018 REV A DATED 2016-10-11 AND REO 670-55-31-103 REV -- DATED 2017-12-27.Jan 16, 2018 · N642CA · Cndair CL6002C10SDR N6WA2018011101Drag Angle · crackedVERTICAL STAB LEFT FWD DRAG ANGLE IS CRACKED. R & R THE DRAG ANGLE IAM SRM 55-31-00.Jan 11, 2018 · N173GJ · Cndair CL6002C10SDR AALA201801109005Fitting · excess playEXCESSIVE PLAY ON FITTING ASSEMBLY FORK END OF THE BEARING HINGE ARM 3 ON VERTICAL STABILIZER AT HSS 2279, RIB 5. REPLACED THE FITTING ASSEMBLY IAW SRM 51-72-11.Dec 7, 2017 · N661AW · Airbus A320232SDR AALA201711289043Hinge Arm · looseLOOSE BEARING HINGE ARM NR 7 ON VERTICAL STABILIZER. REPLACED THE HINGE ARM AND FASTENERS IAW SRM 51-72-11.Nov 11, 2017 · N662AW · Airbus A320232SDR SWAA2017111617857Skin · corrodedVERTICAL STABILIZER LEADING EDGE CORRODED ON LOWER END LEADING EDGE STA 102.3. R&R STABILIZER IAW AMM.Oct 19, 2017 · N713SW · Boeing 7377H4SDR V0XD20171010002Drag Angle · crackedVERTICAL STABILIZER RT FORWARD AND AFT DRAG ANGLES ARE CRACKED. REPAIRED THE DRAG ANGLES IAW REO 670-55-31-018, REV. A, REO 670-55-31-101 REV --, AND NDTM PART 1, 51-20-006.Oct 10, 2017 · N656CA · Cndair CL6002C10SDR AALA201710259005Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE. EXCESSIVE PLAY ON RUDDER TO VERTICAL STABILIZER HINGE ARM NR 2 AT RIB 4. REPLACED HINGE ARM FITTING NR 2 PER SRM A320 51-72-11 AND AMM 55-36-41-400-001-A.Sep 28, 2017 · N110UW · Airbus A320214SDR AALA201710129001Hinge Fitting · excess playEXCESSIVE PLAY ON VERTICAL STABILIZER HINGE ARM NR 7 BEARING. REPLACED THE HINGE FITTING IAW SRM 51-72-11, AND AMM 55-36-41-400-001-A.Sep 28, 2017 · N110UW · Airbus A320214SDR CALA2017092903339Beam · damagedLT TRAILING EDGE OF VERTICLE STAB AFT BEAM DAMAGED. REMOVED DAMAGED AREA AND INSTALLED A REPAIR DOUBLERS AND FILLER IAW ECRA 5330-01859.Sep 27, 2017 · N15712 · Boeing 737724SDR DALA2017092707105Structure · damagedVERTICAL STAB LEFT AND RIGHT SIDE ZFS 52.267 UPPER TWO ROWS FASTENERS 85 LOOSE AND ELONGATED HOLES. COMPLIED WITH PRI 560974-14AD REV. 0, REV. 1, AND REV. 2. REPAIRED REF ER/A 560974-14AD REV ORIG. COMPLIED WITH ER/A 560974-14AD REV A.Sep 26, 2017 · N947AT · Boeing 717200SDR DALA2017091806957Structure · damagedVERTICAL STABILIZER LEADING EDGE SKIN AT ZFS 52.287 DAMAGED. THREE BUSHINGS WERE REPLACED IAW ERA 535916-14, AD, REV ORIGINAL AND DWG SG 09550004, REV D.Sep 19, 2017 · N916DE · Doug MD88SDR AALA201710039026Hinge Fitting · wornEXCESSIVE PLAY ON HINGE ARM NR 5 FORK END FITTING ON VERTICAL STABILIZER AT RIB 8. REPLACED HINGE ARM FITTING IAW AMM 55-36-41-400-001-A, AND SRM 51-72-11.Sep 6, 2017 · N730US · Airbus A319112SDR AALA201710039025Hinge Fitting · wornEXCESSIVE PLAY ON HINGE ARM NR 2 FITTING ASSEMBLY FORK END ON VERTICAL STABILIZER AT RIB 3. REPLACED THE HINGE ARM FITTING IAW AMM 55-36-41-400-001-A, AND SRM 51-72-11.Sep 6, 2017 · N730US · Airbus A319112SDR AALA201710039024Hinge Fitting · wornEXCESSIVE PLAY, LOOSE BEARING, HINGE ARM NR 4 FITTING ASSEMBLY FORK END ON VERTICAL STABILIZER AT RIB 6. REPLACED HINGE ARM FITTING IAW AMM 55-36-41-400-001-A, AND SRM 51-72-11.Sep 6, 2017 · N730US · Airbus A319112SDR AALA201710039023Hinge Fitting · wornEXCESSIVE PLAY, LOOSE BEARING ON HINGE ARM NR 1 FITTING ASSEMBLY FORK END ON VERTICAL STABILIZER AT RIB 2. REPLACED HINGE ARM FITTING AMM 55-36-41-0401, AND SRM 51-72-11.Sep 6, 2017 · N730US · Airbus A319112
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