JASC 5532
Service difficulty reports · 1,753
Reports filed under 5532 · Vertical Stabilizer, Plate/Skin, 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 = '5532' 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 = '5532' 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 DHLA201000045Skin · corrodedVERT STAB-CORROSION BETWEEN SKIN AND BEADED DOUBLER STA ZR 253.000-281-963. RESOLUTION PERFORMED MAJOR REPAIR IAW SRM 55-5-1, FIG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-20. FOUND OUT OF LIMITS IAW SRM 55-2-0 FIG 6. REMOVED PLATING BEADED DOUBLER IAW SRM 55SDR IPXA10658863Panel · delaminatedINSPECTION TYPE:C, EMP - VERT STAB RT EXTERIOR SURFACE AREA (NEAR NR 321E UPPER) FOUND DELAMINATED, REF UPS EO B767-5530-37028-A.SDR IPXA10658862Panel · damagedINSPECTION TYPE:C, VERTICAL STAB RT SIDE PANEL (175T2001-4) AFTER REMOVAL FOUND PANEL MID SECTION FWD EDGE 1 EA LOCATION DAMAGED. REF SRM 55-30-01-2R REPAIR 1, FIG 201, SHEET 1, REF SRM 51-70-10-2R REPAIR 4 FIG 202, SHEET 3 REV 46.SDR USAA2010031090559Panel · delaminatedDELAMINATION ON RT SIDE OF VERTICAL STABILIZER PANEL. SUPPLEMENT WILL BE FILED WHEN REPAIR IS COMPLETE. REPAIRED RIGHT SIDE VERTICAL STABILIZER LOWER FORWARD TORQUE BOX PANEL IAW EA 121513A.SDR FDEA201003040633Frame · crackedCRACK - VERTICAL STABILIZER LOWER ACCESS PANEL NR 364QR CUTOUT AFT. CRACK AT VERTICAL STABILIZER LOWER ACCESS PANEL NR 364QR CUTOUT R & R AS PER SRM 51-31-01 REVISION 43. NEW FRAME FABRICATED AS PER EA NR 1-5530-137929, REPAIR IS CLASSIFIED AS MINOR PER GSDR QXEA2010030800153Skin · scratchedRFD - C CHECK - TWO SCRATCHES FOUND ON LT VERTICAL STAB SKIN UNDER VOR ANTENNA. BLENDED SKIN IAW SRM 51-12-00-001-001-A01. ALL BLENDS WITHIN LIMITS IAW SRM 55-00-01-101-001-A01. TREATED IAW SRM 51-21-11-001-001-A01.SDR RMXA418TY21610Skin · crackedAN 38MM CRACK IN THE UPPER FIN WAS DISCOVERED DURING A DAILY INSP. THE CRACK IS LOCATED ON THE INNER LT UNDERSIDE LOWER L/E RIB STARTING FROM A RIVET AND PROGRESSING AFT ALONG THE RADIUS. ACFT WAS PLACED OUT OF SERVICE AND THE UPPER FIN REPLACED.SDR UIEA201000004Skin · wornPART 1-4 FOUND DAMAGE WEAR ON LT AND RT SIDE VERTICAL STAB SEAL INTERFACE SKIN AREA BETWEEN BS 2360-2390 AND BS 2521-2598 AND BS 2280- 2360. BLEND OUT DAMAGE AREA IAW SRM 53-00-01 REV 53 RESIDUAL MATERIAL THICKNESS WITHIN ALLOWABLE DAMAGE, APPLY PROTECTIVE COSDR UALA2010012100259Panel · delaminatedRT VERT STAB LWR FWD BOX PANEL NR 1 HAS A LARGE DELAM AREA. DELAM AREA IS 12" X 7" APP ROX 4" FROM UPPER EDGE OF PANEL AND 14" FROM AFT EDGE OF PANEL. NEED PN 177W3101-2 & 177W3102-5. REPAIRED IAW SMB WU NR K4610E AND R & R NR R13333. REPAIRED ON SMB WU K4SDR IPXA10658222Panel · delaminatedINSPECTION TYPE: 7C EMP - VERTICAL FIN L/E RT LOWER FIXED PANEL FOUND DELAMINATED. METAL HOT BAND REPAIR PERFORMED IAW SRM 51-70-10 REPAIR 4 FIG 201. SHEET 1, REV. 45.SDR USAA2011011390197Panel · delaminatedCLT - C2 - MAJOR REPAIR - DELAMINATION ON RIGHT VERTICAL STABILIZER PANEL AT FIN STA 116 APPROX 12 INCHES AFT OF LEADING EDGE. REPLACED RIGHT VERTICAL STABILIZER PANEL IAW B757 SRM 55-30-01.SDR IXXA10SMN002SSkin · crackedDURING ROUTINE C CHECK INSP, FOUND VERTICAL STABILIZER L/E SKIN CRACKED AT STA ZFS 179.750. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA, PERFORMED EDDY CURRENT INSP. NO DISCREPANCY FOUND. FABRICATED INTERNAL, EXTERNAL DOUBLERS AND FILLESDR IXXA10WSAP068SSkin · dentedDURING ROUTINE C CHECK INSP FOUND DENTS IN RT VERTICAL STABILIZER BETWEEN STA FSS 245 AND FSS 92. BLENDED OUT DENTS. FOUND TO BE WITHIN LIMITS. PERFORMED NDT INSP, NO CRACKS OR CORROSION NOTED. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-10-01, 51-20-01 RESDR IXXA10WSAP055SSkin · dentedDURING ROUTINE C-CHECK INSP, FOUND DENTS ON L/E RT SIDE OF VERTICAL STABILIZER. BLENDED OUT DENTS. FOUND TO BE WITHIN LIMITS. PERFORMED NDT INSP, NO CRACKS OR CORROSION NOTED. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-10-01, 51-20-01, 55-30-01 FIGURE 10SDR IXXA10WSAP046SSkin · dentedDURING ROUTINE C-CHECK INSP, FOUND DENTS IN VERTICAL STABILIZER AT STA FSS118. REMOVED DENTS. FOUND TO BE WITHIN LIMITS. PERFORMED NDT INSP. NO CRACK OR CORROSION NOTED. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-10-01REV 101, SRM 51-20-01 REV 101, 55-SDR ASAA1047230Doubler · chafedDOUBLER CHAFED STN 887 TO 915 UNDER DORSAL FIN L/E AREA. REMOVED PREVIOUS DOUBLER, FABBED NEW DOUBLER AND REPAIR PARTS AND INSTALLED.SDR IXXA10WSAP027SSkin · delaminatedDURING ROUTINE C CHECK INSP FOUND DELAMINATING ON VERTICAL STABILIZER RT SIDE SKIN. ACCOMPLISHED REPAIR IAW SRM 51-70-03 REV 101, SRM 51-21-10 REV 97.SDR IXXA10WSAP026SPanel · erodedDURING ROUTINE C-CHECK INSP, FOUND VERTICAL STABILIZER L/E PANEL NR 321E ERODED. ACCOMPLISHED REPAIR IAW SRM 51-70-06 REV101 AND 51-20-10 REV 97.SDR DLM88092003Skin · crackedDURING HMV A CRACK WAS FOUND ON RT UPPER SKIN ON VERTICAL STABILIZER L/E CRACK WAS REPAIRED IAW ERA 478005-14 REV ORIG.SDR A6WA201040062Panel · crackedFWD CORNER OF PANEL 326BL CRACKED OFF. (VISOR PANEL FAIRING). TRIMMED DAMAGE IAW REO 601R-55-32-246.SDR ABXR200912170045Skin · chafedDURING A ROUTINE HEAVY MX VISIT FOUND 2 (EA) CHAFE MARKS IN VERTICLE STAB RT SIDE. (TOP/FWD) REMOVED AND REPLACED SKIN WITH RIVITS IAW SRM 51-30-2 AND HILOCKS IAW SRM 51-30-5. ITEM RETURNED TO SERVICE.SDR DALA1170340930Skin · damagedVERT STAB L/E SKIN UPPER XFS-52 HOLE. REPAIRED IAW ERA 478349- 14.SDR IPXA09657953Panel · delaminatedVERTICAL STAB AREA OF DELAMINATION, LEFT SIDE, FSS 195.39. REMOVED, REPAIRED AND INSTALLED PER SRM 51-40-02-OG, AND BOEING DWG 175T0000.SDR FDEA200911083904Skin · crackedVERTICAL STABILIZER LT SURFACE FOUND CRACKED AT FWD OF REAR SPAR PLANE AT APPROX ZFR 540 AREA. REPAIR CARRIED OUT ON VERT STAB LT SURFACE SKIN AT FWD OF REAR SPAR PLANE AT APROX ZFR 540 IAW EA 1-5530-135661. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV. 1SDR DLM88091748Skin · damagedON UPPER LEADING EDGE PANEL NUMEROUS HOLES WERE FOUND ELONGATED, WITH VISIBLE CRACKS IN THE COUNTERSINKS OF THE FASTENERS. REPAIRED ON ER/A 478045-14 ORIG: VERTICAL STABLIZER / UPPER FIXED LEADING EDGE / ZFS=52 / HOLE DAMAGE.SDR IPXA09657665Panel · delaminatedVERTICAL STAB L/E AREA LT UPPER PANEL. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-70 PAR 5C FIG 10 REV 45.SDR USAA2009090392369Skin · crackedCLT - RON - MAJOR REPAIR - CRACK ON RIGHT SKIN OF VERTICAL STABILIZER AT RIB 12, S09R. REPAIRED RIGHT SKIN OF VERTICAL STABILIZER AT RIB 12, S09R IAW US AIRWAYS EA 101390C.SDR IPXA09657195Panel · delaminatedINSPECTION TYPE:C EMP - VERT STAB LT LWR FIXED PANEL FOUND DELAMINATION. METAL HOT BOND REPAIR PERFORMED AS PER SRM REV 44, 51-70-10 REPAIR 4 FIG 201.SDR RMXA029H226080609Skin · crackedWHILE INSTALLATION OF THE ELEVATOR FOLLOWING MAINTENANCE A SUSPECTED CRACK WAS FOUND IN THE SHEET METAL SKIN ON THE RH SIDE OF THE VERTICAL STABILIZER. THE CRACK IS LOCATED AT THE RH FORWARD MOUNT HOLE FOR THE 32CT FAIRING. THE CRACK EMANATES FORWARD FROM THE SDR IPXA09556999Panel · delaminatedINSPECTION TYPE:C1 VERTICAL STAB PANEL 322AL PREVIOUS REPAIR FAILS TO MEET REPAIR REQUIREMENTS OF SRM (EVALUATED PER VALIDATION EO B757-5100-341151) 2.7 INCH DIAMETER LOCATED AT FSS 91-650-94-350 (415-S4-20). REPAIRED PER SRM 51-70-07.SDR IPXA09556998Skin · delaminatedINSPECTION TYPE:C1 VERTICAL STAB PANEL 322AL PREVIOUS REPAIR FAILS TO MEET REPAIR REQUIREMENTS OF SRM (EVALUATED PER VALIDATION EO B757-5100-34115A) 1.0 INCH DIAMETER LOCATED AT FSS 85.750-86.750 (415-S4-23). REPAIRED PER SRM 51-70-07.SDR IPXA09556997Skin · delaminatedINSPECTION TYPE:C1 VERTICAL STAB PANEL 332AL PREVIOUS REPAIR FAILS TO MEET REPAIR REQUIREMENTS OF SRM (EVALUATED PER VALIDATION EO B757-5100-34115A) 1.4 INCH DIAMETER LOCATED AT FSS 90.250-91.650 (415-S4-21). REPAIRED PER SRM 51-70-07.SDR IPXA09556996Skin · delaminatedINSPECTION TYPE:C1 VERTICAL STAB PANEL 322AL PREVIOUS REPAIR FAILS TO MEET REPAIR REQUIREMENTS OF SRM (EVALUATED PER VALIDATION EO B757-5100-34115A) .70 INCH DIA. LOCATED AT FSS 90.750-91.450 (415-S4-22). REPAIRED PER SRM 51-70-07.SDR IPXA09556995Skin · delaminatedINSPECTION TYPE:C1 VERTICAL STAB PANEL 332AL PREVIOUS REPAIR FAILS TO MEET REPAIR REQUIREMENTS OF SRM (EVALUATED PER VALIDATION EO B757-5100-34115A) 5.0 INCH DIAMETER LOCATED AT FSS 81.050-86.050 (415-S4-24). REPAIRED PER SRM 51-70-07.SDR IPXA09556994Skin · misrepairedINSPECTION TYPE:C1 VERTICAL STAB PANEL 332AL PREVIOUS REPAIR FAILS TO MEET REPAIR REQUIREMENTS OF SRM (EVALUATED PER VALIDATION EO B757-5100-34115A) .70 INCH DIAMETER LOCATED AT FSS 79.550-80.250 (415-S4-25). REPAIRED PER SRM 51-70-07.SDR IPXA09556993Skin · misrepairedINSPECTION TYPE:CQ VERTICAL STAB PANEL 332AL PREVIOUS REPAIR FAILS TO MEET REPAIR REQUIREMENTS OF SRM (EVALUATED PER VALIDATION EO B757-5100-34115A) 1.3 INCH DIAMETER LOCATED AT FSS 75.950-77.250 (415-54-26). REPAIRED PER SRM 51-70-07.SDR FDEA200907272760Panel · crackedVERTICAL STABILIZER - NR 2 ENGINE INTAKE DUCT INTERNAL INBD SUPPORT PANEL STA ZID 2160 FOUND CRACKED. REPAIR CARRIED OUT AS PER SRM 55-20-00 VOLUME I FIGURE 2, REVISION 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.SDR ASAA0956166Skin · dentedDENT LEADING EDGE OF VERTICAL FIN. CUT OUT DAMAGE, INSTALLED REPAIR DOUBLER AND FILLER.SDR IPXA09556791Skin Panel · damagedINSPECTION TYPE:C RUDDER T/E HAS LIGHTNING STRIKES AT 127 INCHES FROM TIP. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 55-40-01 FIG 101. REMOVED F FASTENERS TO OBTAIN ACCESS IAW SRM 51-40-02. ACCOMPLISHED COMPOSITE REPAIR TO THE DAMAGED PANEL IAW SRM 55-40-01 SDR IPXA09656430Skin Panel · delaminatedINSPECTION TYPE:C EMP - VERTICAL STAB LT EXTERIOR SURFACE FWD MIDDLE AREA FOUND DELAMINATION. METAL HOT BOND REPAIR PERFORMED AS PER SRM 51-70-10 REV 44, REPAIR 4 FIG 201.SDR IPXA09856170Skin · misrepairedINSPECTION TYPE:SV SURVEY SEQ 852-S4-30418 RT SIDE OF VERTICAL STAB L/E AT STATION XFS 74. 00 EXTERNAL DOUBLER DOES NOT CORRELATE TO SRM. ACCOMPLISHED REPAIR PER TIMCO REO-G12834 REV B AND EO DC8-5530-33667-A.SDR IPXA09656122Panel · delaminatedINSPECTION TYPE:C EMP VERTICAL STAB RT LWR FWD EXTERNAL FOUND DELAMINATION. METAL HOT BOND REPAIR PERFORMED AS PER SRM REV 43, 51-70-10 REPAIR 4 FIG 201, DOUBLER MATERIAL 7075T6BARE0025IN, REPAIR DOUBLER SIZE: 16.125 X 13 INCHES.SDR AALA20090609TUL06Skin · crackedVERTICAL STAB L/E SKIN CRACKED AFT OF RAM AIR INTAKE LEFT SIDE. INSTALLED DOUBLER PER SRM 55-01-00 FIGURE 2 SHEET 2.SDR MALA090058Skin · dented4 DENTS IN RT SIDE OF VERTICAL STAB AROUND LOC ANTENNA. DENT NOTED ON RT VERTICAL STABILIZER AT WL 219.8, 14.88 FROM FWD EDGE. FOUND DENT NR 4 DISBONDED AND REPAIRED NR 4 WITH BONDED DOUBLER IAW EO NR S55017 FOR MORE INFO SEE CONT CARD 089351 FOR DETAILS.SDR HALA2009042700164Skin · cracked8 INCH CRACK ON LEFT VERTICAL SKIN FWD JACKSCREW CUTOUT. REPAIR IN WORK. CRACK VERIFIED BY EDDY CURRENT. REMOVED LT VERTICAL STABILIZER TIP SKIN. ALL GAPS CHECK OK. REPAIR PER HALM 105 FILE 487114.SDR DALA1255440634Skin · damagedLIGHTNING STRIKE DAMAGES ON THE FUSELAGE VERTICAL STABILIZER, RUDDER AND LT ELEVATOR. REPAIR IAW ERA 474515-14.SDR FDEA200904191330Spar Cap · crackedCRACK INDICATION FOUND APPROXIMATELY 0.250 INCH IN LENGTH DURING HFEC INSPECTION ON LEFT SIDE OF THE LOWER VERTICAL STABILIZER FORWARD FLANGE OF UPPER REAR SPAR CAP. REPAIR CARRIED OUT AS PER SRM 55-20-00 FIGURE 3 VOLUME I REVISION 40. REPAIR PARTS INSTALLED SDR IPXA09555566Skin · dentedVERTICAL STAB LT SIDE PANEL DENTED. TEMPORARY REPAIR PER EO B757-5530-33134-A. INSTALLED TEMP DOUBLER.SDR IPXA09655423Skin Panel · delaminatedINSPECTION TYPE:C EMP - VERTICAL STAB LT LWR EXTERIOR SURFACE AREA DELAMINATION. METAL HOT BOND REPAIR PERFORMED AS PER SRM 51-70-10 REPAIR 4 FIG 201 REV 43.SDR DLM88090528Skin · crackedVERTICAL STABILIZER LEADING EDGE SKIN AT ZFS=136.803 UPPER PANEL RIGHT SIDE AFT CORNER ATTACH TANG WAS FOUND CRACKED APPROXIMATELY 0.281 INCH. THE CRACK WAS TRIMMED OUT APPROXIMATELY 1 INCH BY 1 INCH AND REPAIRED WITH AN EXTERNAL DOUBLER.
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