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.
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
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 UIEA2023022100162None · noneDELAMINATION ON EXTERNAL AREA OF RH ACCESS PANELS FROM VERTICAL STABILIZER BETWEEN FSS 118.75 TO FSS 246.653 AND FRONT SPAR TO AUXILIARY SPAR.(<P>REPAIRED THE AFFECTED AREA PER SRM 55-30-01-2R-1 FIG. 201 SHEET 1 AND SRM 51-70-10-2R-4 FIG. 201 SHEET 1.</P>)SDR REXA2022022300237Angle · crackedR/H VERTICAL STAB. AFT DRAG ANGLE APPEARS TO BE CRACKED AT FORWARD END. FURTHER INVESTIGATION REQUIRED. REPLACED R/H AFT DRAG ANGLE IAW CRJ 900 SRM 51-42-13-001-001-A01, 51-42-21-001-001-A01, AND 51-42-22-001-001-A01SDR 2023FA0000339Attach Bolt · looseALL 4 BOLTS HOLDING VERTICAL STABILIZER SPAR TO REAR BULKHEAD WERE LOOSE. I SAW BLACK ALUMINUM DUST AROUND THE LOWER TWO DURING A ROUTINE INSPECTION. I REMOVED THE BOLTS AND DID NOT FIND SIGNIFICANT WEAR ON THE STRUCTURES. THE NUTS HAD TORQUE STRIPE ON THEM, CSDR FDEA202302080227Frame · crackedEMPENNAGE: ZONE 360, LEFT HAND LOWER VERTICAL STABILIZER #363HL ACCESS PANEL SURROUNDING FRAME FOUND CRACKED, LOCATED BETWEEN STATION 2125 AND STATION 2137. EMPENNAGE: ZONE 360, LEFT HAND LOWER VERTICAL STABILIZER #363HL ACCESS PANEL BETWEEN STATION 2125 SDR FDEA202302070216Spar · crackedWHILE ACCOMPLISHING RIGHT HAND NUMBER 4 BANJO FITTING INSPECTION AS PER WORK CARD T1-5530-49623C P4, LEFT HAND FORWARD LOWER SPAR RADIUS FOUND CRACK BETWEEN LOWEST TWO FASTENERS STATION Y = 2164. CRACK AT LEFT HAND FORWARD LOWER SPAR RADIUS BETWEEN LOWEST SDR FDEA202302070215Spar · crackedDURING HIGH FREQUENCY EDDY CURRENT SURFACE INSPECTION ON THE RIGHT HAND FORWARD FLANGE OF LOWER VERTICAL STABILIZER REAR SPAR CAP, FOUND 01 EACH CRACK WITH LENGTH APPROXIMATELY 0.4Ï¿½ FROM 03RD FASTENERS BELOW ZEE CHANNEL STATION Y = 2164. 01 EACH CRACK SDR DALA2023020901035Unknown · unknownSHIP 5645 REF. N/R-002 VERTICAL STABILIZER / FWD TORQUE BOX LOWER PANEL RHS FASTENER HOLES DAMAGED. CORRECTIVE ACTION: C/W PRI 605782-14 REV 0. ,1,2 AND 3 C/W ERA 605782-14 REV. ORIGINAL SECTION I PERMANENT REPAIR. (9557432)SDR DALA2023020901034Unknown · unknownSHIP 5645 ON WALKAROUND FOUND EVIDENCE OF POSSIBLE MISSING BONDED DOUBLER ON RT. SIDE OF VERT STAB. CORRECTIVE ACTION: REMOVED VERTICAL LOWER FWD TORQUE BOX PANEL AND ERA 605782-14 REV. 0 INSTALLED VERTICAL LOWER FWD TORQUE BOX PANEL AND ERA 605782-14 REV 0. CSDR DALA2023102608827Unknown · unknownSHIP 5645 **DTE 605782-14 REQUIRED*** B757-200 / VERTICAL STABILIZER TORQUE BOX PANEL DELAMINATION. CORRECTIVE ACTION: REF ERA 605782-14. (2617625)SDR AALA202302157809Hinge Arm · wornAIRCRAFT IN BASE MAINTENANCE: VERTICAL STABILZER RUDDER #3 HINGE FITTING AT RIB 5, HINGE ARM HAS ELONGATED FASTENER HOLE #1. MAINTENANCE REPLACED HINGE ARM FITTING PER SRM 51-42-11.SDR REXA2022012700185Drag Angle · crackedFWD VERTICAL STABILIZER DRAG ANGLE IS CRACKED NEAR 67.5% REAR SPAR DATUM (LH) REPAIRED LH FWD VERTICAL STABILIZER DRAG ANGLE IAW CRJ 900 SRM 55-31-00-201-001-A01SDR UIEA2023011800059Skin Panel · delaminatedDELAMINATION DAMAGES ON VERTICAL STABILIZER SKIN PANEL BETWEEN FSS 18.037 / FSS 92.5, FSS 245.653 / FS 321.046 AND AUXILIARY /FR (REPAIR WAS ACCOMPLISHED PER BOEING SR# 3-5540076887 AND SRM 55-30-01 REPAIR SRM 51-70-10 REQUIREMENTS.)SDR AALA202301233589Hinge Arm · wornAIRCRAFT IN BASE MAINTENANCE: VERTICAL STABILIZER RUDDER # 4 BEARING HINGE ARM ASSEMBLY HAS ELONGATED FASTENER HOLE. MAINTENANCE REPAIRED THE HINGE ARM ASSEMBLY PER EA 341726.SDR DALA2023012400523Splice · crackedNOTED CRACK ON RT SIDE 2ND SCREW HOLE BELOW SPLICE 4NE 52.267. AFTER ACCOMPLISHMENT OF SEPARATION OF LAYERS, PERFORMED BHEC IAW STEP 14 OF AA5530-01048-02 AD 2618-10-08 & NOTED CRACK APPEARED TO BE IN SPAR RUNNING TOWARD 7 O'CLOCK. REMOVED VERTICAL STAB LEADISDR AALA202302030401Hinge Arm · wornAIRCRAFT IN BASE MAINTENANCE: VERTICAL STABILIZER #2 RUDDER LOWER HINGE ARM #7 FASTENER HOLE IS ELONGATED / WORN AT STA 1926 AND RIB 4. MAINTENANCE REPAIRED HINGE ARM PER EA 341900.SDR SWAA2023020180630Skin · corrodedCORROSION EXTERNAL SKIN VERTICAL FIN AFT EDGE LOCATED APROX. STA 169.0 AT VERTICAL STABILIZER 2022-694959<[01] TOOL USED ULTRASONIC EQUIPMENT PN: 45MG; SN: 130064101; DUE DATE: 12 OCT 23;[02] REMOVED DAMAGE AND REWORKED AREA FOUND WITHIN LIMITS IAW B737-700 SRSDR FDEA202212110159Angle · corrodedVERTICAL STABILIZER; RIGHT PANEL 374FR ATTACH POINT STRUCTURE EXFOLIATED AT NUTPLATE. REMOVED CORRODED ANGLE AMC 7202-49 AND INSTALLED NEW SERVICEABLE ANGLE AMC7202-49 FOR PANEL 374FR IAW SRM 51-33-01-0G.SDR WX0A1900010031664Attach Fitting · unknownNRC 3000-0045: FOLLOWING DETAILED INSPECTION OF RUDDER ATTACHMENT FITTINGS, MULTIPLE DISCREPANCIES FOUND SEE AWS FOR DETAILS. NOTE: REPLACE ONE HINGE FITTING AT A TIME./RUDDER ATTACHMENT FITTINGS FORK END BR1, BR2, BR3, BR4, BR5 AND BR 7 REPLACED PER SRM 55SDR SWAA2022120773167Support · crackedCRACK SUPPORT PLATE ASSY LOC. FRONT SPAR APPROX STA 1016 AT VERTICAL STABILIZER. REPLACED SUPPORT PLATE ASSY LOC. FRONT SPAR APPROX BS 1016 AT VERTICAL STABILIZER AND FASTENER IAW DWG 176A3101 SHEET 4 REV -, AND SRM 51-10-02 ITEM 9.SDR AALA202212281735Hinge Arm · wornAIRCRAFT IN BASE MAINTENANCE. NR 4 HINGE ARM HAS NINE HOLES ELONGATED AT RIB 6 ON THE VERTICAL STABILIZER. MAINTENANCE. REPAIRED THE HINGE ARM IAW EA 340509.SDR REXA2022120102630Drag Angle · crackedVERTICAL STABILIZER, L/H AFT DRAG ANGLE IS CRACKED. REPLACED AFT L/H VERT DRAG ANGLE IAW CRJ-900-SRM-51-42-13-001-001-A01, 51-42-22-001-001-A01 AND 51-42-21-001-001-A01.SDR FDEA202211112754Flange · crackedDURING ULTRASONIC INSPECTION FOR VERTICAL CRACKS BEHIND SERVICE REPAIR SR10550013 PER DRAWING NUMBER SN10550000 REVISION C ON LEFT HAND SIDE LOWER VERTICAL STABILIZER FORWARD FLANGE OF UPPER REAR SPAR CAP, STATION 2164, EXISTING CRACK INDICATION FOUND FRSDR SWAA2022120969879Access Panel · crackedCRACK ACCESS PANEL 323CL PLATE VERTICAL STABILIZER. REPLACED PLATE ON ACCESS PANEL 323CL VERTICAL STABILIZER IAW SRM 51-10-02, SRM 51-40-02, AND DWG: 172A6124, SHEET: 1 REV:ESDR N6WA2022111405Drag Angle · crackedAFT VERTICAL SUPPORT DRAG ANGLE ON R/H SIDE IS CRACKED. REMOVED AFT VERTICAL SUPORT DRAG ANGLE IAW CRJ 700 SRM 51-40-11, INSTALLED RH AFT DRAG ANGLE IAW SRM 55-31-00 AND SRM 51-42-24SDR N6WA2022111404Drag Angle · crackedFWD VERTICAL SUPPORT DRAG ANGLE ON L/H SIDE IS CRACKED. REMOVED AREA FROM LOCATION FASTENERS IAW CRJ 700 SRM 51-26-01, PERFORMED NDT INSPECTION OF CUT OFF EDGE NO DEFFECTS NOTED, MANUFACTURRED DOUBLER AND FILLER AND INSTALL IAW CRJ700 SRM 55-31-00. INSTALL FWDSDR IXXA2022110402Stabilizer · delaminatedVERTICAL L/E PANEL DIRECTLY BELOW 322BL R/H SIDE IS DELAMINATED IN 4 AREAS ON INTERNAL SKIN FOUND DURING CURSORY INSPECTION.SDR REXA2022110302382Drag Angle · crackedVERTICAL STAB. RH FWD DRAG ANGLE HAS POSSIBLE CRACK (FLAGGED) PERFORMED CUT OUT OF RH FWD DRAG ANGLE, BUCKET SKIN, AND COMPLIED WITH ALL STEPS OF REO 690-55-31-071 REV. – DATED: 2022-09-26SDR 2022F00420Hinge Arm · crackedDURING A DROP-IN AT STS MOD CENTER IN MELBOURNE, FL (MLB), THE VERTICAL STABILIZER WAS REPORTED WITH RUDDER VIBRATION DURING FLIGHT. MAINTENANCE PERFORMED ALLEGIANT EO NO. E554-0010 TO INSTALL NEW VERTICAL TAIL PLANE (VTP) HINGE ARM FITTINGS EQUIPPED WITH BEARSDR REXA2022102602296Drag Angle · crackedVERTICAL STAB RH AFT DRAG ANGLE HAS POSSIBLE CRACK CUT AWAY DAMAGED AREA & PERFORMED DRAG ANGLE REPAIR REF CRJ 900 SRM 55-31-00-201-001-A01SDR REXA2022111002427Angle · crackedSUSPECTED CRACK NOTED AT R/H AFT VERTICAL DRAG ANGLE REPLACED DRAG ANGLESDR ASAA2022101540511Stiffener · corrodedCORROSION ON RH OB VERTICAL STAB AFT SPAR ATTACH FITTING FWD AND AFT STIFFENERS. GROUNDED - YES. REMOVED AND REPLACED FWD AND AFT SPAR ATTACH FITTINGS STIFFENERS (FAIL SAFE) IAW B737-700 SRM 51-40-02-0G-0.W= .750 O= 1.200 R= 1.080 L= .850 D= .120.SDR IXXA2022100801Pivot Pin · corrodedHORIZONTAL PIVOT PIN CORRODEDSDR SWAA2022102451971Panel · damagedPANEL 323CL HAS ELONGATED FASTENER HOLE ON FWD END. / [01] REMOVED PANEL 323CL DUE TO DAMAGE.;[02] REPAIRED PER EA 22-155-03124 (SWA - REPAIR - VERTICAL STAB AFT CLOSEOUT PANEL 323CL PN 172A6124-11 FASTENER HOLE DAMAGE ON PN: 176A1000-46; SN: XA003412 ON A/C 8SDR AALA202210188259Hinge Arm · crackedAIRCRAFT IN BASE MAINTENANCE: VERTICAL STABILIZER RUDDER HINGE ARM #4 HAS FASTENER HOLE WITH CRACK INDICATION. REPLACED HINGE ARM PER SRM 55-36-42.SDR REXA2022093002154Angle · crackedL/H VERTICAL STAB AFT DRAG ANGLE CRACKED. REMOVED AND REPLACED IAW CRJ 900 SRMS 51-40-11-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01, AND 51-42-22-001-001-A01.SDR REXA2022110102357Drag Angle · crackedVERTICAL STAB L/H AFT DRAG ANGLE IS CRACKED INSTALLED NEW AFT DRAG ANGLE ON LH VERTICAL STAB IAW CRJ900 SRM 51-42-21-001-001-A01 AND CRJ900 SRM 51-42-10-001-001-A01.SDR IXXA2022092304Panel · delaminatedLEFT SIDE VERTICAL STAB IS DELAMINATEDSDR SWAA2022101278409Angle · crackedCRACK LEADING EDGE SUPPORT ANGLE LOCATED AT BS 1016 BETWEEN S-2R AND S-2L WL 308.5 AT VERTICAL STABILIZER 2022-510342 / [01] REPLACED NEW LEADING EDGE SUPPORT ANGLE LOCATED AT BS 1016 BETWEEN S-2R AND S-2L WL 308.5 AT VERTICAL STABILIZER IAW B737-700 SRM 51-10SDR SWAA2022101952791Bracket · crackedCRACK SUPPORT BRACKET LOCATED BS 1016 BTW STR2L TO STR2R AT VERTICAL STABILIZER 2022-518028 / [01] REPLACED SUPPORT BRACKET AND FASTENERS LOCATED BS 1016 BTW STR2L TO STR2R AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02; SRM 51-10-02 PARAGRAPH 9 AND DWG 176ASDR REXA2022091602100Angle · crackedVERTICAL STAB. LH AFT DRAG ANGLE HAS POSSIBLE CRACK REPLACD ANGLE PER CRJ 900 SRM 55-31-00-201-001-A01SDR SWAA2022092251034None · crackedCRACK ON RIB 8 OF DORSAL FIN 321A 2022-493542 / [01] REPLACED RIB 8 LOCATED ON DORSAL FIN 321A. IAW B737-700 SRM 51-10-02 PARAGRAPH 9. AND DWG 174A0101 REV. ?D?. SEE INDIVIDUAL SIGN OFF BELOW.;[02] CERTIFIED STEP 1 COMPLETE <BR>IAW B737-700 SRM 51-10-02 PARAGRSDR SWIA202266868Fitting · chafedVERTICAL STABILIZER REAR SPAR BOTH CENTER FITTINGS CHAFED (C-CHECK RO 11/12/2022) REPLACED UPPER AND LOWER RUDDER CENTER FITTINGS LOCATED ON THE VERTICAL STABILIZER REAR SPAR WITH NEW UNITS. REF CRJ200 SRM 51-42-20, RIL #0602 REV J, AND DWG 600-21029 RSDR FDEA202208312247Intercostal · crackedINTERCOSTAL P/N AJC 7582-3 IS CRACKED ACCESED THOUGH PANEL 363 PL BOTH FWD AND AFT UPPER CORNERS INSTALLED REPAIR DOUBLER PER MD-11 SRM 55-30-02-2R REPAIR 7 FIGURE 203SDR SWAA2022093048201None · deterioratedL/H SIDE VERTICAL FIN L/E 322B INTERNAL SURFACE LOWER SECTION DISBONDED. (18-045) / [01] BONDED LOWER INTERNAL SECTION OF VERTICAL FIN L/E AS PER AMM 51-31-00-390-803;[02] VERIFIED STEP 1.SDR UIEA2022082200879Fairing · dentedEMP - VERT FIN L/E FAIRING 321B P/N : 65B03289-9 RHS FOUND DENT.(<P>EMP - VERT FIN L/E FAIRING 321B P/N : 65B03289-9 RHS DENT AREA REWORKED IAW SRM 51-70-01-0G-0 AND 1EA HOLE RIVET REPAIRED IAW SRM 55-30-01-1A-1 ADL NOTED E.</P>)SDR HNAA2022091200260None · noneE932899 - LH AND RH STAB BEARING BORES OUT OUT OF LIMITS .... REPAIRED THE LH AND RH STAB BEARING BORES IAW PIEDMONT EO1-55-22-0177.SDR SWAA2022091546955None · crackedCRACK ACCESS PANEL 321A RIB 8 AT VERTICAL STABILIZER 2022-452153 / [01] REPLACED RIB 8 LOC AT VERTICAL STABILIZER ACCESS PANEL 321A IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DRAWING 174A0103 SHEET 7 REV.-.;[02] COMPLETE TASK CERTIFIEDSDR SWAA2022100365428Angle · crackedVERTICAL FIN L/E FRONT SPAR FITTING FIX AFT EDGE SPRING ANGLE 2EA. CRACKS NOTED (DOT 223-VLE002). VERTICAL FIN L/E FRONT SPAR FITTING FIX FWD EDGE SPRING ANGLE 2EA. CRACKS NOTED (DOT 223-VLE002). / [01] REMOVED FWD SPRING ANGLE AT VERTICAL FIN L/E FRONT SPAR FSDR SWAA2022092944308Angle · crackedVERTICAL FIN L/E FRONT SPAR FITTING FIX AFT EDGE SPRING ANGLE 2EA. CRACKS NOTED (DOT 223-VLE002). VERTICAL FIN L/E FRONT SPAR FITTING FIX FWD EDGE SPRING ANGLE 2EA. CRACKS NOTED (DOT 223-VLE002). / [01] REMOVED FWD SPRING ANGLE AT VERTICAL FIN L/E FRONT SPAR FSDR FDEA202208172246Skin Panel · crackedL/H LOWR VERT STAB SKIN PANEL UPPER AFT FASTENER HOLE HAS A 1.5 IN. CRACK PROPAGATING THROUGH FASTENER. (STA. 2160 AT REAR SPAR AND BELOW PYLON CARRY THROUGH CAP) REPAIRED L/H LOWR VERT STAB SKIN PANEL PER EA 1-5530-T0370603
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