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 JGVR20230706002Unknown · unknownDRILLED OFF 32 NUTPLATES AND MECHANICALLY REMOVED CORROSION FOUND UNDERNEATH ON PANELS 341AL, 341BL, 341CL, 341AR, 341CR, 341DR, 341ER OF THE VERTICAL STABILIZER. PERFORMED NDT, TREATED AND PRIMED REPAIR AREAS, AND INSTALLED NEW NUTPLATES REFERENCING NETJETS RSDR VNAA202308040023Drag Angle · crackedDAMAGE DESCRIPTION: CRACK ON VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE LH/RH , BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). DRAG ANGLE LH AFT/RH FWD AND AFT WERE REPAIRED PER STEP CRJ-900 SRM 55-31-00-201-001-A01SDR FDEA202306241088Intercostal · crackedEMPENNAGE-DURING SKIN REPLACEMENT FOUND LEFT HAND INTERCOSTAL AFT EDGE CRACKS BETWEEN STATION 2160-2164 REAR CENTER SPAR TO REAR SPAR AREA. EMPENNAGE LEFT HAND INTERCOSTAL AFT EDGE CRACKED 1.2" BETWEEN STATION 2160-2164 REAR CENTER SPAR TO REAR SPAR AREA SDR FDEA202306241087Intercostal · crackedEMPENNAGE-DURING SKIN REPLACEMENT FOUND LEFT HAND INTERCOSTAL FORWARD EDGE CRACKS BETWEEN STATION 2140-2144 REAR CENTER SPAR TO REAR SPAR AREA. EMPENNAGE LEFT HAND INTERCOSTAL FORWARD EDGE CRACKED 0.3" BETWEEN STATION 2140- 2144 REAR CENTER SPAR TO REAR SPSDR 2023FA0000332Unknown · unknownFOUND SEVERAL DISBONDING ON LEFT HORIZONTAL STABILIZER LOWER SURFACE ON PANEL 335HB.SDR 2023FA0000330Unknown · unknownFOUND SEVER DELAMINATION ALONG WITH CRUSHING DAMAGE AT SEVERAL LOCATION ON VERTICAL STBILIZER, RH SIDE, EXTERNAL SKIN PNEL, FSS 11 TO FSS 92SDR 2023FA0000329Unknown · unknownFOUND SEVERAL DELAMINATION ALONG WITH EDGE CRUSHING DAMAGE ON VERTICAL STABILIZER, LH SIDE EXTERNAL SKIN PANEL, FSS 92 TO FSS 270SDR 2023FA0000328Unknown · unknownFOUND SEVERAL DELAMINATION ALONG WITH CRUSHING DAMAGE ON VERTICAL STABILIZER, LH SIDE EXTERNAL SKIN PANEL, FSS 11 TO FSS12SDR 2023FA0000327Unknown · unknownFOUND SEVERAL DELAMINATION ALONG WITH CRUSHING DAMAGE ON VERTICAL STABILIZER, LH SIDE EXTERNAL SKIN PANEL, FSS 11 TO FSS12SDR AALA202306277621Hinge Arm · wornAIRCRAFT IN BASE MAINTENANCE: VERTICAL STABILIZER RUDDER HINGE ARM BEARING #3 HAS 8 EACH FASTENER HOLES OUT OF ROUND ON THE LOWER FORK END. REPLACED HINGE ARM ASSEMBLY PER SRM 51-42-11.SDR AALA202306261349Hinge Arm · crackedAIRCRAFT IN BASE MAINTENANCE: VERTICAL STABILIZER RUDDER #1 HINGE ARM HAS CRACKED FASTENER HOLE IN THE LOWER FLANGE BEARING ATTACH PLATE AREA. REPLACED HINGE ARM PER SRM 55-36-42.SDR UIEA2023060600594Unknown · unknownVERTICAL STABILIZER, RH SURFACE, COMPOSITE PANEL DESBONDED BETWEEN AUXILIARY SPAR TO FRONT SPAR BETWEEN FSS 220.521 / FSS 321.046(<P>REPAIRED PER SRM 51-70-10-2R-4. NO FURTHER DEFECTS NOTED</P>)SDR REXA2022060700337Angle · crackedRIGHT VERTICAL STAB DRAG ANGLE IS CRACKED AT THE 67.5 REAR SPAR DATUM. REPAIRED R/H FWD VERTICAL STAB DRAG ANGLE IAW CRJ 900 SRM 55-31-00-201-001-A01.SDR JGVR20230531004Unknown · unknownMECHANICALLY REMOVED 2 AREAS OF CORROSION LOCATED ON VERTICAL STAB AFT SPAR RUDDER COVE LOCATED JUST ABOVE RUDDER FAIRING PANEL LH SIDE ON SPAR CLIP, PERFORMED NDT AND SUBMITTED FOR REPAIR DISPOSITION. TREATED AND PRIMED BLENDED AREAS IAW TEXTRON FIELD REPAIR SDR SWAA2023070563506Fitting · corrodedVERTICAL FIN FRONT SPAR FITTING AT STA 1016 L/H BOLT HAS A SPOT OF CORROSION.<[01] REMOVED AND REPLACED VERTICAL FINFRONT SPAR FITTINGAT STA 1016 L/H BOLT AS PER AMM 55-30-200-801 TORQUE WRENCH <BR> BC 175291 <BR> DUE DATE: 11/18/23;[02] REMOVED AND REPLACED VSDR SWAA2023062151970Skin · corrodedLITE SURFACE CORROSION ON UPPER CROWN SKIN UNDER VERTICAL STAB BETWEEN FUSELAGE STATION 1016 AND 1040 AND STRINGERS 2L AND 2R.<FOUND TO BE OUT OF LIMITS DUE TO MORE THAN THREE AREAS HAVING DAMAGED REMOVAL AROUND THREE FASTENERS OUT OF A GROUP OF TEN IAW SRM 53SDR VNAA202306220003Drag Angle · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) ON LEFT VERTICAL STABILIZER TO FUSELAGSDR AALA202306023037Hinge Arm · wornAIRCRAFT IN BASE MAINTENANCE: VERTICAL STABILIZER BEARING #1 RUDDER HINGE ARM HAS TWO EACH ELONGATED FASTENER HOLES. REPLACED HINGE ARM PER SRM 51-42-11.SDR AALA202306027938Hinge Arm · wornAIRCRAFT IN BASE MAINTENANCE: VERTICAL STABILIZER BEARING #3 RUDDER HINGE ARM HAS 7 EACH ELONGATED FASTENER HOLES. REPLACED HINGE ARM PER SRM 51-42-11.SDR IPXA2023070555790Torque Box · inoperativeL/H TORQUE BOX PANEL DISBONDED TREATED AND PRIMED PER SRM 51-20-01. INSTALLED TORQUE BOX PANEL IAW SRM 51-40-02. REVIEWED.SDR SWAA2023062050275Angle · brokenBROKEN SUPPORT ANGLE LEADING EDGE LOC. BTW STR2L TO STR2R APPROX STA 1016 AT VERTICAL STABILIZER (1 EA) 2023-334327<[01] REPLACED SUPPORT ANGLE LEADING EDGE LOC. BTW STR2L TO STR2R APPROX STA 1016 AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02 AND SRM 51-10-SDR FDEA202305190904Panel · delaminatedDURING AGING AIRCRAFT INSPECTION FOUND EXISTING REPAIR LOCATED ON THE VERTICAL STABILIZER L/H SIDE SKIN PANEL (P/N 175N2003-19) DOES NOT CONFORM TO CURRENT DOCUMENTATION AND SRM REPAIR REFERENCED. REPAIR IS METAL BONDED DOUBLER AND SRM REFERENCED IS FOR COSDR SWAA2023062149296Angle · brokenBROKEN ANGLE FRONT SPAR LOC. APPROX. STA 1016 UPPER AREA AT VERTICAL STABILIZER 2023-330206<[01] REPLACED ANGLE FRONT SPAR LOC. APPROX. STA 1016 UPPER AREA AT VERTICAL STABILIZER IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DWG 176A3101SHEET 4 REV-.SDR SWAA2023061446287Angle · crackedCRACK LEADING EDGE ANGLE BS 1016 BTW STR 2L TO STR 2R AT VERTICAL STABILIZER 2023-310347<[01] REPLACED LEADING EDGE ANGLE LOC BS 1016 BTW STR 2L TO STR 2R AT VERTICAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG #176A3101 SHEET 4 REV -.<BR>SEE INDIVIDUASDR REXA2022050200296Angle · crackedVERTICAL STAB. LH AFT DRAG ANGLE IS CRACKED. REMOVED AND INSTALLED SERVICEABLE AFT DRAG ANGLE LH SIDE WITH PN: AV670-21186-003 IAW CRJ900 SRM 51-42-21-001-001-A01, 51-42-14-001-001-A01 AND 51-42-27-001-001-A01 :SDR SWAA2023053041926Angle · crackedCRACK SUPPORT ANGLE LOCATED BS1016 AT LEVEL STR2L AT VERTICAL STABILIZER 2023-282677<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BS1016 AT LEVEL STR2L AT VERTICAL STABILIZE I.A.W. B737-700 SRM 51-10-02 ITEM 9; B737-700 SRM 51-40-02 AND DRAWING #176A3101;SDR AALA202305041028Hinge Arm · wornAIRCRAFT IN BASE MAINTENANCE: VERTICAL STABILZER BEARING 5 HINGE ARM ASSEMBLY HAS 4 EACH OUT OF ROUND FASTENER HOLES AT FORK END. REPLACED HINGE ARM PER SRM 51-42-11.SDR VNAA202304290001Drag Angle · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00)SDR VNAA202310040012Support Angle · corrodedBELLY FAIRING SUPPORT ANGLE IS CORRODED AT FS939.00 STGR 27.SDR VNAA202310040011Door · gougedFWD CARGO DOOR LOWER OUTER SEAL RETAINER IS GOUGED AND BENT AT SEVERAL LOCATIONS.SDR VNAA202310040010Door · chafedFORWARD BAGGAGE BAY DOOR INNER SKIN IS CHAFED AT (2EA) LOCATIONS.SDR VNAA202310040009Drag Angle · crackedLH AFT VERTICAL STAB DRAG ANGLE SUSPECTED POSSIBLE CRACKSDR VNAA202304290002Drag Angle · crackedCRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00)SDR AALA202304188540Hinge Arm · crackedAIRCRAFT IN BASE MAINTENANCE: VERTICAL STABILIZER RUDDER #1 HINGE ARM AT FORK END HAS 3 EACH FASTENER HOLES CRACKED AT RIB 2. REPLACED HINGE ARM FITTING PER SRM 51-42-11 AND EA 343845.SDR AALA202304104598Hinge Arm · crackedAIRCRAFT IN BASE MAINTENANCE: VERTICAL STABILIZER RUDDER #4 BEARING HINGE ARM ASSEMBLY FASTENER HOLE CRACKED. REPLACED HINGE ARM ASSEMBLY PER SRM 51-42-11,SDR ASAA2023033042657Rib · crackedDURING OKAY TO CLOSE INSPECTION FOR THE LEFT HAND HORIZONTAL STABILIZER LEADING EDGE FOUND A CRACK IN RIB AT APPROX STAB STA 111.10. GROUNDED - YES. CUT OUT DAMAGE AND REPAIRED RIB IAW B737-800 SRM 55-10-09-2R-4.SDR SWAA2023042819305Bracket · crackedCRACK LEADING EDGE BRACKET STA 1016 BTW STR 2R TO STR 2L AT VERTICAL STABILIZER 2023-200205<[01] REPLACED BRACKET AND FASTENERS LOCATED STA 1016 BTW STR 2R TO STR 2L AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02. SRM 51-10-02 ITEM 9. AND DWG 176A3001 REV-D.SDR VNAA202304270018Hinge Fitting · wornAFTER RUDDER REMOVAL, FREE PLAY ON SELF-ALIGN SELF-LUB BEARING PLAIN ON HINGE FITTING NO.2 AND NO. 3 AT VERYTICAL STABILIZER REAR SPAR MIDDLE SECTION.SDR REXA2022041200282Angle · crackedVERTICAL STAB R/H DRAG ANGLE IS CRACKED. LOCATED DRILLED AND INSTALLED NEW SERVICEABLE VERTICAL STAB R/H AFT DRAG ANGLE IAW CRJ 900 SRM 51-42-13-21-22-001-001-A01, 51-40-11-001-001-A01, AND 51-42-13-21-22-001-001-A01.SDR AALA202303318632Hinge Arm · wornAIRCRAFT IN BASE MAINTENANCE: VERTICAL STABILZER RUDDER #1 BEARING HINGE ARM FITTING HAS 2 OBLONG FASTENER HOLES IN THE FORK END AT VERTICAL STABILZER RIB 2.SDR FDEA202303140410Skin · unknownREFERENCE TO WORK CARD: T 1-5530-T0342799 A P3, LEFT HAND LOWER VERTICAL STABILIZER SKIN PART NUMBER: AJC7582-17 LOCATED BETWEEN STATION 2141 AND STATION 2164 REQUIRED TO BE REMOVED AND REPLACED AS PER DRAWING AJC7582. REFERENCE TO WORK CARD: T 1-5530-T03SDR SWAA2023032413588Retainer · crackedVERTICAL FIN PANEL ASSEMBLY 323CL - RETAINER IS CRACKED AS MARKED. 124-048 CRACKED RETAINER IS ON 324AL<[01] REMOVED AND REPLACED VERTICAL FIN PANEL ASSEMBLY 324AL RETAINER REF B737-700 SRM 51-40-02-0G-0;[02] VERIFIED STEP 1. R/R VERICAL FIN PANEL 324AL RETAINSDR R61A2023032100212Rib · chafedVERTICAL STABILIZER REAR SPAR RIB 14 UPPER SIDE HAVE 2 AREAS OF CHAFFING. REMOVED AND REPLACED VERTICAL STABILIZER REAR SPAR RIB 14. REF: SRM 51-40-08SDR HNAA2023031100079Unknown · unknownVERTICAL STABILIZER LH AND RH SPHERICAL BEARING HOUSINGS ARE OUT OF DIMENSIONAL TOLERANCE. REPAIRED IAW EO1-55-23-0044SDR UIEA2023022300178None · noneDEBONDED TWO AREAS ON RH PANEL OUTER SKIN LOCATED AT FRONT SPAR AND BETWEEN FSS145.128 TO FSS 270.784 FROM VERTICAL STABILIZER.(<P>IT WAS REPAIRED PER SRM 55-30-01-2R-1 REPAIR 1 FIG. 201 PAGE 2 AND SRM 51-70-10-2R-4 REPAIR 4 FIG. 201 SHEET 1 PAGE 1-3 REV. 121 SDR UIEA2023022300179None · noneDEBONDED TWO AREAS ON LH PANEL OUTER SKIN LOCATED AT FRONT SPAR AND BETWEEN FSS145.128 TO FSS 270.784 FROM VERTICAL STABILIZER.(<P>IT WAS REPAIRED PER SRM 55-30-01-2R-1 REPAIR 1 FIG. 201 PAGE 2 AND SRM 51-70-10-2R-4 REPAIR 4 FIG. 201 SHEET 1 PAGE 1-3 REV. 121 SDR IPXA2023032392164Skin · scratchedINSPECTION TYPE:C3VERTICAL STAB LEADING EDGE 371CL HAS DENT/CREASE ON L/H SIDE CENTERREPAIRED VERTICAL STAB LEADING EDGE 371CL SKIN IAW VTSAA EA 011-5530-01-A9861 P1 , VTSAA EA 011-5530-01-A9861 P2 DATED 03/09/2023 AND EA 011-5530-01- A9861 IR DATED 03/18/2023SDR FDEA202302280347Frame · crackedDURING THE BANJO FITTING REPAIR OF THE FASTENERS REMOVAL ACCESS, ZONE 360 RIGHT HAND LOWER VERTICAL STABILIZER #364QR ACCESS PANEL SURROUNDING FRAME FOUND CRACKED, LOCATED BETWEEN STATION 2142 AND STATION 2164. RIGHT LOWER VERTICAL STABILIZER #364QR ACCESSSDR AALA202303066646Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON BOLT FRONT SPAR FITTING FORWARD RIGHT AT VERTICAL STABILIZER BODY STA 959.8 AND VERTICAL FIN WATER LINE 0.0. LENGTH: 0.450 INCHES, WIDTH: 0.230 INCHES, AND DEPTH: 0.003 INCHES. REMOVED AND REPLACED BOLT PER JOB CARD.SDR UIEA2023022100161None · noneDELAMINATION ON INTERNAL / EXTERNAL AREA OF LH 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 PAGE 1-7 AND SRM 51-70-10-2R-4 FIG. 201 SHEET
Back to JASC 5530