JASC 5511
Service difficulty reports · 6,462
Reports filed under 5511 · Horizontal Stabilizer, Spar/Rib, 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 = '5511' 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 = '5511' 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 DALA2022020400721None · none#2 HORIZONTAL STAB ELEVATOR RIB HINGE IS CRACKED. ADDITIONAL INFORMATION 001-0293:2090-2039-RH/002 00152 ACCOMPLISHED PRI 596562-14, REV. 0; 596562-14, REV. 1; 596562-14 , REV. 2 AND ERA 596562-14, REV. ORIGINAL. (LP# 2102394)SDR DALA2022020400720None · noneL/H HORIZONTAL STABILIZER #2 RIB ELEVATOR HINGE CRACKED. ADDITIONAL INFORMATION 001-0291:2090-2039-LH/001 00147 ACCOMPLISHED PRI 596563-14, REV. 0; 596563-14, REV. 1 AND ERA 596563-14, REV. ORIGINAL. (LP# 2102249)SDR DALA2022012800579None · noneON OK TO INSTALL RH ELEVATOR, FOUND HORZ STAB SHROUD RIB 4 CRACKED. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0293:2090-2039-RH/ 007 00239 COMPLETED INSTALL OF REPAIR PER A220 ASRP 51-71-59. (LP# 2099959)SDR DALA2022012800578None · noneON OK TO INSTALL RH ELEVATOR, FOUND HORZ STAB SHROUD RIB 2 CRACKED. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0293:2090-2039-RH/ 006 00238 COMPLETED INSTALL OF REPAIR PER A220 ASRP 51-71-59. (LP# 2099956)SDR SWAA2022021664179Stiffener · crackedL/H HORIZ. STAB RIB AT STAB STA 129.50 HAS A CRACK AT 2ND VERT STIFFENER. / [01] VERIFIED APPLICABILITY OF SRM 55-10-09-2R-4.;[13] ACCOMPLISHED A GVI ON ALL AREAS WITHIN REPAIR AREA FOR CORROSION; EXISTING REPAIRS OR ANY OTHER DEFECTS. NO DISCREPANCIES FOUND ISDR AALA202202101902Rib · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN RIB OF LH HORIZONTAL STABILIZER AT STA 101.90, 12.0 IN AFT OF FRONT SPAR, MEASURING L=1.50 IN, W=0.004 IN, D=0.068 IN. ACCOMPLISHED PERMANENT REINFORCING DOUBLER REPAIR IAW SRM 51-10-09-2R.SDR DALA2022012800580None · noneER/A 596551-14 SECTION I ACCOMPLISHED FOR REPAIR OF THE RH HORIZONTAL STABILIZER, TRAILING EDGE, HINGE RIB #3. THE REPAIR WAS ACCOMPLISHED DURING 'C' CHECK IN MSP, NR # 148. ANALYSIS (DTA). ADDITIONAL ENGINEERING APPROVAL, ER/A REVISION, IS REQUIRED FOR CONTINSDR SWAA2022021063402Rib · crackedL/H HORIZONTAL RIB # 4 AT STIFFENER #4 LOWER AREA CRACK ; / [01] CUT OUT AND REMOVE DAMAGE ON VERTICAL STIFFENER ON RIB # 4 AT STIFFENER #4 PER REF 737 SRM 55-10-09-2R-4; [ FABRICATED LOWER ANGLE.063 BAC1480-2793 7075 T6PER REF 737 SRM 55-10-09-2R05 AND LOCATESDR SWAA2022020262902Spar · corrodedLT HORIZONTAL STAB UPPER FLANGE OF REAR SPAR CORRODED AT STAB STA 321 TO 330 ; / [01] UPDATED CHART OF MEASUREMENTS.; [02] UPDATED MEASUREMENTS A FAR AS POSSIBLE IN CURRENT STATE OF ASSEMBLY. PHOTOS ATTACHED.; [03] VERIFIED CORRECTIVE ACTION 1 AND 2; [04] CHANSDR SWAA2022013162799Rib · crackedHORIZONTAL STAB RT RIB 5 HSS 129.50 2ND STIFFENER FROM FWD END CRACKED AT BOTTOM. HFEC INSP ON RIB IAW NDT PART 6 51-00-00 PROC. 23. CRACK CONFIRMED. REMOVED CRACK IAW SRM 51-10-02-0G-0 & 55-10-09-2R-4, REPAIR 4. HFEC INSP IN REPAIR AREA IAW NDT PART 6 51SDR SWAA2022012662798Rib · crackedHORIZONTAL STABILIZER RT RIB #4 HSS 120.30 AFT STIFFENER CRACKED AT BOTTOM. PERFORMED HFEC INSP ON HORIZ. STAB RT RIB NR 4 IAW NDT PART 6 51-00-00 PROC. 23. CRACK CONFIRMED. INSTALLED REPAIR PARTS AT HORIZONTAL STAB RIB # 40 IAW SRM 51-40-02.SDR AALA202201250512Rib · crackedAIRCRAFT WAS NOT GROUNDED: INSPAR RIB AT STA 92.70 HAS ALL 4 STIFFENERS CRACKED. INSTALLED NEW RIB PER SRM 51-40-02.SDR SWAA2022021461737Rib · crackedCRACK INSPAR RIB STAB STA 157.10 LOWER CHORD COMMON TO FRONT SPAR LT HORIZONTAL STAB ; 2021-585238 / [01] TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 500D; S/N: N500X12101V022236 ; DUE DATE: 02-JUN-22; [02] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES000SDR AALA202201255788Rib · inoperativeAIRCRAFT IN BASE MAINTENANCE: FOUND CRACKS IN VERTICAL STIFFENERS OF HORIZONTAL STABILIZERS RIB. LOCATED AT STA 92.70. INSTALLED RIB AT STA 92.70 PER AARD 55-10-00.SDR SWAA2022022161341Rib · crackedCRACK LEADING EDGE RIB LOC AT LE STA 105.26 AT LT HORIZONTAL STABILIZER 2022-16019 / [01] REPLACED RIB AND FASTENERS LOC AT LE STA 105.26 AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02; B737-700 SRM 51-10-02 ITEM 9; AND DRAWING #186A1001 SHEET 10 REV A;SDR SWAA2022022161340Rib · crackedCRACK LEADING EDGE RIB LOC AT LE STA 95.96 AT LT HORIZONTAL STABILIZER 2022-16018 / [01] REPLACED RIB AND FASTENERS LOC AT LE STA 95.96 AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02; B737-700 SRM 51-10-02 ITEM 9; AND DRAWING #186A1001 SHEET 10 REV A; SSDR SWAA2022021460727Rib · crackedR/H HRZ STABILIZER RIB #4 AT STIFFENER #3 HAS A CRACK. ; / [01] CUT AND REMOVED THE DAMAGE FROM THE VERTICAL STIFFENER OF RIB #4 STIFFENER #3 AS PER B737-700 SRM 55-10-09-2R-4.; [02] VERIFIED STEP 1. NDT REQUIRE.; [ [14] REPAIRED R/H HORIZONTAL STAB.MACHINED ISDR SWAA2022020260657Rib · crackedL/H HOR. STAB L/E SKIN (331B) RIB CRACKED AT LE STA 96 ; / [01] REMOVED AND REPLACED RIB AS PER B737-700 SRM 51-440-02-0G-0 AND DWG 186A1303; [02] CORRECTION TO STEP 1:SRM 51-40-02-0G-0; [03] VERIFIED STEP 1; AND CORRECTION ON STEP 2SDR SWAA2022020260658Rib · crackedL/H HOR. STAB L/E SKIN (331B) RIB CRACKED AT LE STA 105 ; / [01] REMOVED AND INSTALLED AS PER BOEING DRAWING 186A1304; [02] REMOVED AND INSTALLED AS PER B737-700 SRM 51-40-02-0G-0 AND BOEING DRAWING 186A1304; [03] VERIFIED STEP 1; AND VERIFIED CORRECTED STEP 2SDR JR2R20210111803Rib · crackedLH H-STAB RIB #12 CRACKEDSDR SWAA2022021560369Rib · crackedCRACK LEADING EDGE RIB LOCATED STA 95.96 AT LT HORIZONTAL STABILIZER (1 EA) ; 2022-12318 / [01] REPLACED NEW CHORD LOC. LEADING EDGE STA 95.96 AT LT HORIZONTAL STABILIZER I.A.W B737-700 SRM 51-40-02 AND DWG 186A1303; SHEET 1; REV -; [02] CORRECTIVE ACTION STEPSDR SWAA2022013160465Rib · crackedRIGHT HAND HORIZONTAL STABILIZER INSPAR RIB; STATION 120.30.; 3RD VERTICAL STIFFENER IS CRACKED. ; / REMOVED DAMAGE FROM RH HORIZONTAL STABILIZER INSPAR RIB STA. 120.30 3RD VERTICAL STIFFENER IAW SRM 53-10-09-2R-4 REPAIR-4; [03] REMOVED DAMAGE FROM RH HORIZONTSDR SWAA2022013160466Rib · crackedRIGHT HAND HORIZONTAL STABILIZER INSPAR RIB; STATION 120.30.; 4TH VERTICAL STIFFENER IS CRACKED. ; / REMOVED DAMAGE FROM RH HORIZONTAL STABILIZER INSPAR RIB STA. 120.30 2ND VERTICAL STIFFENER IAW SRM 55-10-09-2R-4 REPAIR-4; [04] VERIFIED CORRECTIVE ACTION 1-3;SDR AALA202201255717Rib · crackedAIRCRAFT IN BASE MAINTENANCE: RIGHT HORIZONTAL STABILIZER RIB AT STA 92.70 HAS A CRACK IN EACH OF THE THREE AFT STIFFENERS. INSTALLED FASTENERS THROUGH REPAIR AND VERTICAL WEB OF RIB AT 3RD STIFFENER FROM SPAR PER SRM 55-10-09-2R-4.SDR SWAA2022021559543Rib · crackedCRACK LEADING EDGE RIB LOCATED LE STA 95.96 AT RT HORIZONTAL STABILIZER ; 2022-12207 / [01] REPLACED RIB LOC. LEADING EDGE STA 95.96 AT RT HORIZONTAL STABILIZER I.A.W B737-700 SRM 51-40-02 AND DWG 186A1001; SHEET 10; REV A; [02] REPLACED RIB LOC. LEADING EDGE SDR SWAA2022021559544Rib · crackedCRACK LEADING EDGE RIB LOCATED LE STA 114.55 AT RT HORIZONTAL STABILIZER ; 2022-12211 / [01] REPLACED RIB LOC. LEADING EDGE STA 114.55 AT RT HORIZONTAL STABILIZER I.A.W B737-700 SRM 51-40-02 AND DWG 186A1001; SHEET 10; REV A. SEE INDIVIDUAL SIGN-OFF BELOW; [02SDR SWAA2022021559545Rib · crackedCRACK LEADING EDGE RIB LOCATED LE STA 151.75 AT RT HORIZONTAL STABILIZER ; 2022-12215 / [01] REPLACED RIB LOC. LEADING EDGE STA 151.75 AT RT HORIZONTAL STABILIZER I.A.W B737-700 SRM 51-40-02 AND DWG 186A1001; SHEET 10; REV A; [02] CORRECTIVE ACTION STEP 1.<BR>SDR SWAA2022021559547Rib · crackedCRACK LEADING EDGE RIB LOCATED LE STA 105.26 AT RT HORIZONTAL STABILIZER ; 2022-12209 / [01] REPLACED NEW CHORD LOC. LEADING EDGE STA 105.26 AT RT HORIZONTAL STABILIZER I.A.W B737-700 SRM 51-40-02 AND DWG 186A1304; SHEET 1; REV -; [02] CORRECTIVE ACTION STEP 1SDR SWAA2022021559541Rib · crackedCRACK LEADING EDGE RIB LOCATED LE STA 95.96;LE STA 105.26;LE STA 114.55 AND LE STA 151.75 RT HORIZONTAL STAB ; 2022-12201 / [01] FAULT RAISED IN ERROR NEWS FAULT WERE CREATED FOR REPLACEMENT OF RIB SEE NEX FAULT TTG8Q00A6LAV; TTG8Q00A6M7V; TTG8Q00A6LBY AND TTGSDR A6WA202101118061Angle · gougedMAINTENANCE FOUND SCRATCH DAMAGE ON L/H HORIZONTAL STABILIZER ATTACHMENT VISOR SUPPORT ANGLE AT LBL 6. DIMENSIONS OF SCRATCH ARE: 4.100"L X 0.900"W X 0.004"D. ************AIRCRAFT REMOVED FROM SERVICE************************* BLENDED DAMAGED AREA TO SDR A6WA202101118060Visor · gougedMAINTENANCE FOUND SCRATCH DAMAGE ON L/H HORIZONTAL STABILIZER ATTACHMENT VISOR AT LBL6. DIMENSIONS OF SCRATCH ARE: 35.00"L X 0.900"W X 0.004"D. ************AIRCRAFT REMOVED FROM SERVICE************************* BLENDED DAMAGED AREA TO A SMOOTH CONTOUR. DIMENSDR A6WA202101108058Visor · gougedMAINTENANCE FOUND SCRATCH DAMAGE ON R/H HORIZONTAL STABILIZER ATTACHMENT VISOR AT RBL 6. DIMENSIONS OF SCRATCH ARE: (P1) = 4.300"L X .700"W X .006"D AND (P2) = 7.00"L X .200"W X .002"D. ************AIRCRAFT REMOVED FROM SERVICE************************* BLENDSDR A6WA202101108057Visor · gougedMAINTENANCE FOUND SCRATCH DAMAGE ON L/H HORIZONTAL STABILIZER ATTACHMENT VISOR AT LBL6. DIMENSIONS OF SCRATCH ARE: 19.00"L X 0.800"W X 0.007"D. ************AIRCRAFT REMOVED FROM SERVICE************************* BLENDED DAMAGED AREA TO A SMOOTH CONTOUR. DIMENSDR R61A2022011870036Rib · crackedWHILE AC WAS IN FOR HVY CK FOUND MAJOR*** RH H STAB RIB 12 FOUND CRACKED. MX REPLACED RH H-STAB RIB IAW 170 EO-55-10-0004 SEE REPUBLIC JC # 170 EO-55-10-0004 FOR DETAILS OF WORK PERFORMED.SDR SWAA2022021558228Rib · crackedCRACK INSPAR RIB LOCATED STAB STA 101.90 AT LEVEL FRONT SPAR LT HORIZONTAL STAB ; 2022-11920 / [01] TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC500D; SN: N500X12101V022235; DUE DATE: 03 JUN 22; [02] TOOL USED EDDY CURRENT FLAW DETECTOR PN NORTEC 600D SN 2101365SDR SWAA2022021458015Rib · crackedCRACK INSPAR RIB LOCATED STAB STA 129.50 AND 27 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER ; 2021-585081 / [01] EDDY CURRENT EQUIPMENT P/N: NORTEC500D; S/N: N500X12101U102020; DUE DATE: 01-JUN-22.; [02] PERFORMED REPAIR ON INSPAR RIB LOC STAB STA 129.50 SDR SWAA2022021458016Rib · crackedCRACK INSPAR RIB LOCATED STAB STA 129.50 AND 10 INCH FROM REAR SPAR AT RT HORIZONTAL STABILIZER ; 2021-585082 / [01] EDDY CURRENT EQUIPMENT P/N: NORTEC500D; S/N: N500X12101U102020; DUE DATE: 01-JUN-22.; [02] PERFORMED REPAIR ON INSPAR RIB LOC STAB STA 129.50 ASDR SWAA2022021458010Rib · crackedCRACK INSPAR RIB LOCATED STAB STA 157.10 AND 25 INCH FROM FRONT SPAR LT HORIZONTAL STAB ; 2021-585078 / [01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 210138503 DUE DATE: 05-MAR-22; [02] REPAIRED INSPAR RIB LOCATED STAB STA 157.10 AND 25 INSDR DALA2022010800151None · none(LOG 2075046) DURING INSPECTION FOUND WORN AREAS AFFECTING THE H.S CENTER BOX FRONT SPAR FITTING AND SPLICE ANGLE AT STATION 1093. MAINTENANCE REPAIRED THE DAMAGE PER ERA 596323-14.SDR SWAA2022021456574Rib · crackedCRACK LEADING EDGE RIB LOCATED LE STA 105.26 AT LT HORIZONTAL STABILIZER ; 2021-576026 / [01] REPLACED CHORD RIB LOCATED LEADING EDGE RIB; LE STA 105.26 AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-10-02 AND DWG 186A1001 REV ?A?; DWG 186A1304 REV -; [02] RESDR SWAA2022021456487Rib · crackedCRACK INSPAR RIB 4 (STAB STA 120.30) FRONT SPAR PLUS 27.5 INCHES AT LT HORIZONTAL STABILIZER ; 2021-575990 / [01] TOOL USED P/N: NORTEC 600D S/N: 2000053402 CAL DUE DATE: 23-APR-22; [02] PERFORMED REPAIR ON INSPAR RIB 4 (STAB STA 120.30) FRONT SPAR PLUS 27.5 ISDR A6WA202101178076Rib · corrodedLH HORIZONTAL STABILIZER TIP CLOSING RIB #9 P/N 600-23037-22 HAS TWO ELONGATED FASTENER HOLES CAUSED BY CORROSION. HORIZONTAL REAR SPAR AND LBL112.0. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED DAMAGED SECTIONS OF CLOSING RIB AT TWO LOCATIONS. MEASUREMENTS SDR A6WA202112238041None · gougedMAINTENANCE FOUND SCRATCH DAMAGE ON R/H HORIZONTAL STABILIZER ATTACHMENT VISOR SUPPORT ANGLE AT RBL 6. DIMENSIONS OF SCRATCH ARE: .900"L X 0.600"W X 0.002"D. ************AIRCRAFT REMOVED FROM SERVICE************************* BLENDED DAMAGED AREA TO A SMOOTHSDR A6WA202112238039None · gougedMAINTENANCE FOUND SCRATCH DAMAGE ON R/H HORIZONTAL STABILIZER ATTACHMENT VISOR AT RBL 6. DIMENSIONS OF SCRATCH ARE: 38.00"L X 0.70"W X 0.005"D. ************AIRCRAFT REMOVED FROM SERVICE************************* BLENDED DAMAGED AREA TO A SMOOTH CONTOUR. DIMENSDR A6WA202112238040None · gougedMAINTENANCE FOUND SCRATCH DAMAGE ON R/H HORIZONTAL STABILIZER ATTACHMENT VISOR SUPPORT ANGLE AT RBL 6. DIMENSIONS OF SCRATCH ARE: 4.20"L X 0.70"W X 0.005"D. ************AIRCRAFT REMOVED FROM SERVICE************************* BLENDED DAMAGED AREA TO A SMOOTH SDR A6WA202102018092None · damagedL/H HORIZONTAL STABILIZER SPLICE AT CLOSING RIB #9 HAS DAMAGE FROM LIGHTNING STRIKE. PREVIOUS TEMPORARY REPAIR COMPLIED WITH IAW MHIRJ REO 601R-55-11-677 REV A. PERMANENT REPAIR REQUIRED. *************AIRCRAFT REMOVED FROM SERVICE************************ CUTSDR A6WA202102018089Fitting · gougedR/H H STAB FITTING #2 HAS 2 EACH GOUGES AT ES60.525 (RBL55.8865). DIMENSIONS ARE: (P1) 1.00L X 0.200W X .006D (P2) 1.100L X 0.200W X .015D. BOTH GOUGES ARE NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 55-11-27 REV. 38. ****************AIRCRAFT REMOVED FROM SESDR A6WA202102018088None · gougedR/H ELEVATOR I/B AND O/B FITTING HAS GOUGE ON FITTING ASSY AT ES60.525 (RBL55.8865). DIMENSIONS ARE: (P1) 2.100L X 0.300W X .005D. EVALUATED GOUGE AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 55-11-27 REV. 38. ****************AIRCRAFT REMOVED FROM SESDR A6WA202101318087Bracket · gougedL/H HORIZONTAL STABILIZER JACKSCREW FITTING HAS GOUGE ON I/B FASTENER BRACKET. DIMENSIONS ARE: (P1) 2.150L X 1.650W X .010D. EVALUATED GOUGE AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 55-11-27 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE**SDR SWAA2022011053098Stiffener · crackedLEFT HAND HORIZONTAL STABILIZER INSPAR RIB AT STATION 129.50 3RD VERTICAL STIFFENER IS CRACKED ; / [01] REMOVED THE DAMAGED PART AT LH HORIZONTAL STABILIZER STA 129.50 RIB 3RD VERTICAL STIFFENER IAW SRM 55-10-09-2R-4; [02] VERIFIED CORRECTIVE ACTION 1; [03] HF
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