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 AALA201907239021Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE #1 HAS EXCESSIVE PLAY ON THE VERTICAL STABILIZER AT RIB 2. REPLACED HINGE FITTING PER AMM 55-36-41-400-001-A.Jun 5, 2019 · N181UW · Airbus A321211SDR AALA201906079018Hinge Fitting · excess playAIRCRAFT IN BASE VISIT: EXCESSIVE PLAY BEARING HINGE ARM 3 ON VERTICAL STABILIZER (1 EA), EXCESSIVE PLAY IS 0.040". REMOVED AND REPLACED HINGE ARM FITTING #3 ON VERTICAL STABILIZER IAW AMM 55-36-41-400-001-A AND PERFORMED FUNCTIONAL TEST FO THE RUDDER MECHANICMay 21, 2019 · N154UW · Airbus A321211SDR AALA201906079014Hinge Fitting · excess playAIRCRAFT IN BASE VISIT: EXCESSIVE PLAY BEARING HINGE ARM 5 ON VERTICAL STABILIZER (1 EA), EXCESSIVE PLAY IS: 0.042". REMOVED AND REPLACED HINGE ARM FITTING #5 ON VERTICAL STABILIZER IAW AMM 55-39-41-400-001-A AND PERFORMED FUNCTIONAL TEST OF THE RUDDER MECHANIMay 21, 2019 · N154UW · Airbus A321211SDR AALA201906079013Hinge Fitting · excess playAIRCRAFT IN BASE VISIT: EXCESSIVE PLAY BEARING HINGE ARM 7 ON VERTICAL STABILIZER (1 EA), EXCESSIVE PLAY IS 0.041". REMOVED AND REPLACED HINGE ARM FITTING #7 ON VERTICAL STABILIZER IAW AMM 55-36-41-400-001-A AND PERFORMED FUNCTIONAL TEST OF THE RUDDER MECHANICMay 21, 2019 · N154UW · Airbus A321211SDR AALA201906079012Hinge Fitting · excess playAIRCRAFT IN BASE VISIT: EXCESSIVE PLAY BEARING HINGE ARM 2 ON ON VERTICAL STABILIZER (1EA), EXCESSIVE PLAY IS 0.041". REMOVED AND REPLACED HINGE ARM FITTING #2 ON VERTICAL STABILIZER IAW AMM 55-36-41-400-001-A AND PERFORMED FUNCTIONAL TEST FOR THE RUDDER MECHAMay 21, 2019 · N154UW · Airbus A321211SDR AALA201906209010Hinge · excess playAIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE FITTING #3 HAS EXCESSIVE PLAY ON VERTICAL STABILIZER AT RIB 5. REPLACED HINGE FITTING PER AMM 55-36-41.May 18, 2019 · N764US · Airbus A319112SDR AALA201906209023Hinge · excess playAIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE FITTING #4 HAS EXCESSIVE PLAY ON THE VERTICAL STABILIZER AT RIB 6. REPLACED HINGE FITTING PER SRM 51-72-11.May 16, 2019 · N179UW · Airbus A321211SDR AALA201906209009Hinge · excess playAIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE FITTING #5 HAS EXCESSIVE PLAY ON VERTICAL STABILIZER AT RIB 7. REPLACED HINGE FITTING PER AMM 55-36-41.May 13, 2019 · N764US · Airbus A319112SDR SIMA2019043029002Drag Angle · crackedVERTICAL STABILIZER LH LOWER DRAG ANGLE CRACKED AT FR 76. REMOVED AND REPLACED VERTICAL STABILIZER LH LOWER DRAG ANGLE AT FR 76 IAW EMB145 SRM 51-40-02Apr 29, 2019 · N607AE · Emb EMB145LRSDR AALA201905249010Hinge Fitting · wornAIRCRAFT IN BASE VISIT: EXCESSIVE PLAY BEARING HINGE ARM 7 ON VERTICAL STABILIZER (1 EA) PLAY 0.018". REMOVED AND REPLACED RUDDER HINGE ARM FITTING 7 ON VERTICAL STABILIZER (1EA) IAW AMM 55-36-41-000-001-A AND AMM 55-36-41-400-001-A PERFORMED FUNCTIONAL TEST AApr 27, 2019 · N177US · Airbus A321211SDR AALA201905249011Hinge Fitting · wornAIRCRAFT IN BASE VISIT: EXCESSIVE PLAY BEARING HINGE ARM 3 ON VERTICAL STABILIZER (1 EA) PLAY: 0.016" INCH. REMOVED AND REPLACED RUDDER HINGE ARM FITING #3 ON VERTICAL STABILIZER 1E/A IAW AMM 55-36-41-000001-A AND AMM 55-36-41-400-001-A, PERFORMED FUCTIONAL TEApr 26, 2019 · N177US · Airbus A321211SDR AALA201905249009Hinge Fitting · wornAIRCRAFT IN BASE VISIT: EXCESSIVE PLAY BEARING HINGE ARM 2 ON VERTICAL STABILIZER (1 EA )PLAY: 0.012" INCH. REMOVED AND REPLACED RUDDER HINGE-ARM FITTING NR 2 ON VERTICAL STABILIZER (1EA) IAW AMM 55-36-41-000-001-A AND 55-36-41-400-001-A PERFORMED FUNCTIONAL TApr 23, 2019 · N177US · Airbus A321211SDR DXTA201904230187Drag Angle · crackedVERTICAL FIN DRAG ANGLE DAMAGE. REFERENCE TEXTRON AVIATION ENGINEERING MEMO DQ19155M1 DATED APRIL 15, 2019.Apr 23, 2019 · N305QS · Cessna 680SOVSDR DXTA201904230184Drag Angle · crackedVERTICAL FIN DRAG ANGLE DAMAGE. REFERENCE TEXTRON AVIATION ENGINEERING MEMO DQ19155M1 DATED APRIL 15, 2019.Apr 23, 2019 · N305QS · Cessna 680SOVSDR DALA2019042392578Channel · crackedCRACK ON CHANNEL (WEB) SURROUNDING JACKSCREW ASSEMBLY ACTUATOR SUPPORT (RH SIDE) APROX. STA ZRS 134.02 AT VERTICAL STABILIZER. CRACK ON CHANNEL (WEB) SURROUNDING JACKSCREW ASSEMBLY ACTUATOR SUPPORT (RH SIDE) APROX. STA ZRS 134.02 AT VERTICAL STABILIZER WAS REApr 19, 2019 · N934DN · Doug MD9030SDR V6NA201904100001Fairing · corrodedAFTER PAINT STRIPPING PROCESS DETERMINED VERTICAL STABILIZER TOP AFT FAIRING TO BE CORRODED. CORROSION WAS REMOVED AND DOUBLER REPAIR INSTALLED PER APPROVED DATA IN FAA DER DRAWING.Apr 10, 2019 · N170LS · Lear 45LEARSDR SWAA2019061433709Drag Angle · corrodedAFT L/H UPPER FUSELAGE AT STA 1088 LEFT VERTICAL PRIMARY ATTACH FITTING ON AIRCRAFT SIDE FORWARD DRAG ANGLE FITTING CORRODED IN BORE. / R&R DRAG ANGLE IAW DWG.Apr 9, 2019 · N731SA · Boeing 7377H4SDR HALA2019040502239Profile · corrodedDURING H CHECK, VERTICAL STAB TRAILING EDGE RIGHT HAD SIDE VERTICAL PROFILE ABOVE NBR 2 T CHORD FOUND CORRODED. REPLACED CHORD TO VERTICAL STAB TRAILING EDGE PER SRM 51-42-11 AND AIRBUS DRAWING F55371707. LP 1017034Apr 5, 2019 · N393HA · Airbus A330243SDR HALA2019040500172Tee Fitting · corrodedVERTICAL STAB TRAILING EDGE RHS #2 T CHORD SUSPECT CORROSION AROUND FASTENER HOLES. #2 RHS VERT FIN T/E T-CHORD CORROSION BLENDED BEYOND LIMITS IAW HAL A330 SRM 51-74-00 REV 98.01. CHORD REPLACED IAW HAL A330 SRM 51-42-11, REV 98.01 AND AIRBUS DWG F553 717Apr 5, 2019 · N393HA · Airbus A330243SDR HALA2019040300163Tee Fitting · corrodedVERTICAL STAB TRAILING EDGE RT NR 3 TEE FITTING CORRODED AROUND FASTENER HOLES. REMOVAL OF CORROSION CARRIED OUT IAW SRM 51-74-00, REV 98.01. CORROSION STILL EVIDENT IAW NTM 51-10-02-221-001-A REV 96. BLEND DEPTH OF .054" IS BEYOND 50% MATERIAL THICKNESS. Apr 3, 2019 · N393HA · Airbus A330243SDR CA190319011Hinge Fitting · corroded(CAN) VERTICAL STABILIZER REAR SPAR MIDDLE RUDDER HINGE FITTING CORRODED.Mar 19, 2019 · Aerosp ATR42500SDR V0XD20190227008Drag Angle · crackedVERTICAL STAB L/H FWD DRAG ANGEL IS CRACKED. CORRECTIVE ACTION: CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW GO JET EO C70-55MR-001-0.Feb 21, 2019 · N163GJ · Cndair CL6002C10SDR ASOA201902197029Hinge Fitting · wornR/H AND L/H VERTICAL STAB HINGE FITTING BORES WORN TO LIMITS. REAMED R/H AND L/H BORES AND INSTALLED BEARINGS. AIRCRAFT STILL IN C CHECK.Feb 16, 2019 · Emb EMB145SDR HYIA20190215002Angle · corrodedDURING MAINTENANCE SURFACE CORROSION WAS DISCOVERED ON THE RIGHT HAND AFT VERTICAL STABILIZER ANGLE (P/N: 5131007-6) BETWEEN APPROXIMATE W.L. 143.52-167.52. THE DEEPEST CORRODED AREA IN THIS SPAN MEASURES APPROXIMATELY .029" DEEP. THIS ANGLE WILL BE REMOVED ANFeb 14, 2019 · N7037E · Cessna 402CSDR HYIA20190215001Angle · corrodedDURING MAINTENANCE SURFACE CORROSION WAS DISCOVERED ON THE LEFT AFT ANGLE OF THE VERTICAL STABILIZER BETWEEN APPROXIMATE WL 143.52-167.52. THE DEEPEST CORRODED AREA IN THIS SPAN MEASURES APPROXIMATELY .031 DEEP. THIS ANGLE WILL BE REMOVED AND REPLACED WITH NEWFeb 14, 2019 · N7037E · Cessna 402CSDR SWAA2022030303489Panel · elongatedVERTICAL STABILIZER PANEL 322A HAS ELONGATED HOLE. MARKED. / VERTICAL STAB PANEL 322 A HAS ELONGATED HOLE EVALUATED HOLE SIZE AS .450' MAX ALLOWED HOLE SIZE = .312' IS OUT OF LIMITS IAW 737-700 SRM 51-40-0G-05-0 FIG 3 VERIFIED NEW VERTICAL STAB PANEL 322 A AS Feb 9, 2019 · N7816B · Boeing 7377L9SDR SWAA2022030223655Panel · crackedR/H ELEVATOR PANEL 344GB IS CRACKED / REMOVED R/H ELEVATOR PANEL 344GB IAW SOPM 20-50-01 MATCH DRILLED NEW PANEL IAW SRM 51-20-07-0G-0 PARA'S 4 AND 6. INSTALLED NEW PANEL 344GB IAW SOPM 20-50-01 56790U 05FEB19Feb 5, 2019 · N272WN · Boeing 7377H4SDR DALA2019020540753Attach Angle · crackedINITIAL INSPECTION: CRACKED VERTICAL ATTACH ANGLE P/N: 5912188-50 RH (EHV). SUMMARY: OF NRC.00120 VERTICAL ATTACH ANGLE P/N: 5912188-50 RH WAS REPLACED PER MD-90 VOL.II SRM 51-30-05 AND VOL.II SRM 51-30-02. (LP# 0930800)Feb 3, 2019 · N918DH · Doug MD9030SDR DALA2019020540752Attach Angle · crackedINITIAL INSPECTION: CRACKED VERTICAL ATTACH ANGLE P/N: 5912188-49 LH (EHV). SUMMARY OF NRC. 00118 VERTICAL ATTACH ANGLE P/N: 5912188-49 LH WAS REPLACED PER MD-90 VOL.II SRM 51-30-05 AND VOL.II SRM 51-30-02. (LP# 0930777)Feb 3, 2019 · N918DH · Doug MD9030SDR DALA2019011800332Flange · damagedOPEN HOLE ETHF INSPECTION ON RIGHT VERTICAL STAB FRONT SPAR FWD. FLANGE SHOWS CRACK INDICATIONS AT FASTENER HOLES #1, 3, 4 BELOW SPLICE AND 5, 6 AND 13, ABOVE SPLICE. REFERENCE 5530-01045-0602. CLEANED HOLES WITH BRASS BRUSH. (668138). PERFORMED OPEN HOLE ETHFJan 1, 2019 · N906DL · Doug MD88SDR FDEA201812263609Support · corrodedVERTICAL STAB, BOTTOM SUPPORT BRACE FOR PANEL 374FR IS CORRODED. REPLACED BOTTOM SUPPORT WITH NEW SERVICEABLE SUPPORT ANGLE PER MD-10 SRM 51- 31-01 VOL. 2. AND DOUGLAS DRAWING AMC7202.Dec 26, 2018 · N10060 · Doug MD1010FSDR DALA2018122627393Doubler · crackedCRACK ON VERTICAL STABILIZER UPPER WEB AND DOUBLER AROUND JACKSCREW HOLE. VERTICAL STABILIZER UPPER WEB AND DOUBLER AROUND JACKSCREW HOLE WAS REPAIRED PER ETI-90-18-064 R1 AND ER/A 574084-14 SECTION I REV. ORIGINAL. FOLLOWED UNDER LOG PAGE 0872434. ASSOCIATED Dec 22, 2018 · N917DN · Doug MD9030SDR DALA2018122627392Channel · crackedCRACK ON CHANNEL (STIFFENER) RH SIDE STA ZV= 72 AT VERTICAL STABILIZER. CHANNEL (STIFFENER) RH SIDE STA ZV= 72 AT VERTICAL STABILIZER WAS REPAIRED PER ETI-90-18-068 REV. 3 AND ER/A 574101-14 REV.ORIG AND WAS ATTENDED WITH NRC 00276 AND LOG PAGE : 0873621. ASSODec 21, 2018 · N917DN · Doug MD9030SDR V0XD20181219001Drag Angle · crackedVERTICAL STAB, RIGHT HAND AFT DRAG ANGLE IS CRACKED. CORRECTIVE ACTION: REPAIRED R/H AFT DRAG ANGLE IAW BOMBARDIER REO 670-55-31-114 REV.- DATED 2018-12-12, AND 670-55-31-018 REV. A DATED 2016-11-10.Dec 15, 2018 · N658CA · Cndair CL6002C10SDR SCNA201812041131Retainer · wornREMOVED PANEL #324AR TO FOM AND FOUND BOTTOM RETAINER WORN ON PANEL. REMOVED WORN RETAINER ON BOTTOM EDGE OF PANEL. FABRACATED REPAIR PARTS. MATCHED DRILLED HOLES, ALODINED AND PRIMMED PARTS. REPAIR PARTS AND PANEL ARE IN SHEET METAL WORK AREA. INSTALLED NEW RDec 1, 2018 · N814SY · Boeing 7378BKSDR SCNA201812041130Retainer · wornREMOVED PANEL #323AR TO REMOVE PANEL #323BR. UPON REMOVAL OF PANEL FOUND LOWER RETAINER WORN, FABRACATED AND REPLACED WORN SECTION OF PANEL RETAINER. OK TO REINSTALL PANEL WHEN OTHER WORK IS COMPLETE. INSTALLED PANEL.Dec 1, 2018 · N814SY · Boeing 7378BKSDR SCNA201812041129Retainer · wornFOUND RETAINER ON LOWER PART OF PANEL 323BL WORN. REMOVED AND REPLACED RETAINER ON PANEL #323BL.Dec 1, 2018 · N814SY · Boeing 7378BKSDR SCNA201812041128Bracket · wornFOUND ANGLE BRACKET FOR PANEL 323BL WORN ON RIGHT SIDE OF FUSELAGE AT LOWER VERTICAL STAB. REMOVED ALL FASTENERS EXCEPT THOSE COMMON TO VORTEX GENERATOR ASSEMBLY. VORTEX GENERATOR ASSEMBLY MUST BE REMOVED TO ACCESS 1 HIDDEN FASTENER. REMOVED RIGHT SIDE VORTEX Dec 1, 2018 · N814SY · Boeing 7378BKSDR SCNA201812041127Cover · wornDURING INSCPECTION OF VERTICAL FIN - FRONT SPAR TO REAR SPAR FOUND PANEL #323BL ON LOWER SIDE GAP COVER WORN. REMOVED AND REPLACED PANEL 323BL LOWER RETAINER.Dec 1, 2018 · N814SY · Boeing 7378BKSDR SCNA201812041126Mount Bracket · wornDURING INSCPECTION OF VERTICAL FIN - FRONT SPAR TO REAR SPAR FOUND ANGLE MOUNTING BRACKET WHICH HOLDS PANEL # 323 BL WORN AT LEFT SIDE FUSELAGE LOWER VERTICAL STABILIZER. REMOVED LEFT SIDE VORTEX GENERATOR ASSEMBLY. REMOVED ANGLE BRACKET ON FUSELAGE AT LOWER Dec 1, 2018 · N814SY · Boeing 7378BKSDR V0XD20181126006Angle · crackedVERTICAL STABILIZER L/H FWD DRAG ANGLE IS CRACKED. CORRECTIVE ACTION REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW BOMBARDIER REO 670-5531-098 REV.-- DATED 2017-06-28, AND 670-55-31-018 REV. A DATED 2016-11-10Nov 26, 2018 · N668CA · Cndair CL6002C10SDR VNAA2018112099902Drag Angle · crackedR/H VERTICAL STAB AFT DRAG ANGLE IS CRACKED. C/A: INSTALLED NEW SERVICEABLE AFT DRAG ANGLE AS REPAIRED IAW CRJ 700 SRM 51-42-22-001-001-A01, 51-42-21-001-001-A01, AND 51-42-13-001-001-A01.Nov 17, 2018 · N515AE · Cndair CL6002C10SDR VNAA2018112099901Drag Angle · crackedR/H VERTICAL STAB FWD DRAG ANGLE IS CRACKED. C/A: INSTALLED FWD DRAG ANGLE REPAIR IAW CRJ 700 SRM 55-31-00-201-001-A01.Nov 17, 2018 · N515AE · Cndair CL6002C10SDR IPXA2018111425920Bracket · brokenFWD VERTICAL STABILIZER SIDE FAIRING PANEL 323AL HAD A BROKEN BRACKET, ATTACHED TO THE FUSELAGE. REMOVED AND REPLACED THE BRACKET IAW SRM 51-40-21.Nov 11, 2018 · N125UP · Airbus A300F4622RSDR AALA201812069018Hinge · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY RUDDER HINGE #4 BEARING ON VERTICAL STABILIZER. REPLACED STABILIZER PER AMM A319 55-36-41-400-01-A SRM 51-72-11.Nov 9, 2018 · N751UW · Airbus A319112SDR AALA2018121049015Hinge Fitting · excess playEXCESSIVE PLAY FOUND ON THE NR 5 HINGE FITTING FOR THE VERTICAL STABILIZER. REPLACED THE HINGE FITTING IAW SRM 51-72-11, DRAWING D55371041, AND AMM 55-36-41.Nov 6, 2018 · N769US · Airbus A319112SDR AALA201812049023Hinge Fitting · excess playEXCESSIVE PLAY ON THE VERTICAL STAB HINGE FITTING AT VSS 5606, RIB 11. REPLACED THE HINGE FITTING IAW SRM 51-72-11, AND AMM 55-36-41-400-001-A.Nov 6, 2018 · N769US · Airbus A319112SDR AALA201812049017Hinge Fitting · excess playEXCESSIVE PLAY ON THE VERTICAL STAB HINGE FITTING AT VSS 2279, RIB 5. REPLACED THE HINGE FITTING IAW SRM 51-72-11, AND AMM 55-36-41-400-001-A.Nov 6, 2018 · N769US · Airbus A319112SDR AALA2018111209013Torque Box · delaminatedVERTICAL STABILZER LEFT FORWARD TORQUE BOX PANEL WAS DELAMINATED 3 INCHES UP FROM BOTTOM EDGE. REPLACED THE TORQUE BOX PANEL IAW SRM 51-40-02.Nov 2, 2018 · N201UU · Boeing 7572B7SDR PAIR201811054652Angle · corrodedDURING INSPECTION, FOUND THE REAR SPAR LEFT ANGLE CORRODED BELOW THE RUDDER UPPER HINGE POINT, REPLACED THE ANGLE.Nov 1, 2018 · N919H · Beech 300BEECH
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