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 SWAA2021110920601Fitting · corroded>>> CORROSION >> VERTICAL STABILIZER CENTER SECTION; LEFT O/B REAR SPAR FITTINGS CORROSION ; / [01] PERFORMED CORRECTIVE ACTION ON BARCODE TTG8Q006LXMS. REF FAULT TTG8Q006KMKF; [02] PERFORMED CORRECTIVE ACTION ON BARCODE TTG8Q006LXMS. REF FAULT TTG8Q006KMKFSDR AALA202109204532Rib · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN VERTICAL RIB AT 3RD STIFFENER OF RH HORIZONTAL STABILIZER AT STA 92.70, MEASURING L=0.5 IN, W=0.002 IN, D=0.04 IN. REPLACED RIB WITH NEW IAW AARD 51-00-05-1.SDR SWAA2021100518395Rib · crackedLH HORIZONTAL STAB L/E ACCESS PANEL RIB 4 HAS A CRACK. ; / [01] REMOVED CRACKED RIB P/N 186A1304-1 PER B737-700 SRM 51-40-02-0G-0.; [02] VERIFIED RIB REMOVAL; [03] LOCATED AND DRILLED NEW RIB P/N 186A1304-1 PER B737-700 SRM 51-10-02-0G-0.; [04] VERIFIED DRILLISDR SWAA2021100518396None · crackedLH HORIZONTAL STAB L/E ACCESS PANEL RIB 5 HAS A CRACK. ; / [01] REMOVED RIB #5 AT LH HORIZONTAL STAB L/E ACCESS PANEL AS PER B737-700 SRM 51-40-02 -0G-0; [02] REMOVED RIB CRACKED P/N 186A1305-1 AT LH HORIZONTAL STAB PANEL AS PER B737-700 SRM 51-40-02-0G-0; [03SDR SWAA2021102518065None · crackedSUPPLEMENTAL INFORMATION: CRACK INSPAR RIB LOCATED RIB 4 STA 120.30 AT LEVEL FRONT SPAR 37 IN LT HORIZONTAL STAB (1 EA) ; 2021-429615 / [21] REPAIRED INSPAR RIB LOCATED RIB 4; STAB STA 120.30 AT 37 IN. OF FRONT SPAR LT HORIZONTAL STAB. IAW SRM B737-700 55-10-0SDR SWAA2021102518064None · crackedSUPPLEMENTAL INFORMATION: CRACK INSPAR RIB LOCATED RIB 4 STA 120.30 AT LEVEL FRONT SPAR 28 IN LT HORIZONTAL STAB (1 EA) ; 202-429614 / [18] REPAIRED INSPAR RIB LOCATED RIB 4 STA 120.30 AT 28 IN. OF FRONT SPAR LT HORIZONTAL STAB. IAW SRM B737-700 55-10-09-2R-4 SDR SWAA2021102518063None · crackedSUPPLEMENTAL INFORMATION: CRACK INSPAR RIB LOCATED RIB 4 STA 120.30 AT LEVEL FRONT SPAR 19 IN. LT HORIZONTAL STAB (1 EA) ; 2021-429611 / [19] REPAIRED INSPAR RIB LOCATED RIB 4; STAB STA 120.30 AT 19 IN. OF FRONT SPAR LT HORIZONTAL STAB. IAW SRM B737-700 55-10-SDR SWAA2021092018445Rib · crackedRIGHT HORIZONTAL STAB. INSPAR RIB ASSY 5 (STAB STA 129.50); STIFFENER 2 CRACKED. ACCOMPLISHED HFEC OF WEB SECTION AFTER VERTICAL RIB REMOVAL FOUND WEB AREA HAS A CRACK INDICATION PER NDT PART 6 51-00-00 PROC. 23 REMOVED FASTENERS FOR RIB REMOVAL TO FOM. REMOVSDR SWAA2021110917696Spar · corrodedRIGHT HORIZONTAL STABILIZER; FRON SPAR CLEVIS 'G' CORROSION ; / [01] SUMMARY EA 21-155-02738 HAS BEEN APPROVED; ACTIVATED; AND ADDED AS A SUBTASK TO FAULT TTG8Q006HUQF.; [02] SUMMARY EA 21-155-02738 HAS BEEN APPROVED; ACTIVATED; AND ADDED AS A SUBTASK TO FAULTSDR SWAA2021110917683Spar · corrodedRIGHT HORIZONTAL STABILIZER; CENTER SECTION REAR SPAR CLEVIS 'E' WORNOUT AND CORROSION ; / [01] SUMMARY EA 21-155-02705 HAS BEEN APPROVED; ACTIVATED; AND ADDED AS A SUBTASK TO FAULT TTG8Q006HSWB.; [02] SUMMARY EA 21-155-02705 HAS BEEN APPROVED; ACTIVATED; AND SDR SWAA2021110917691Spar · corrodedRIGHT HORIZONTAL STABILIZER; CENTER SECTION REAR SPAR CLEVIS 'D' WORNOUT AND CORROSION ; / [01] SUMMARY EA 21-155-02723 HAS BEEN APPROVED; ACTIVATED; AND ADDED AS A SUBTASK TO FAULT TTG8Q006HUPH.; [02] SUMMARY EA 21-155-02723 HAS BEEN APPROVED; ACTIVATED; AND SDR SWAA2021110917692None · corrodedRIGHT HORIZONTAL STABILIZER; CENTER SECTION REAR SPAR CLEVIS 'C' WORNOUT AND CORROSION ; / [01] SUMMARY EA 21-155-02687 HAS BEEN APPROVED; ACTIVATED; AND ADDED AS A SUBTASK TO FAULT TTG8Q006HUPK.; [02] SUMMARY EA 21-155-02687 HAS BEEN APPROVED; ACTIVATED; AND SDR SWAA2021110917690None · corrodedLEFT HORIZONTAL STABILIZER; CENTER SECTION REAR SPAR CLEVIS 'D' WORNOUT AND CORROSION ; / [01] SUMMARY EA 21-155-02706 HAS BEEN APPROVED; ACTIVATED; AND ADDED AS A SUBTASK TO FAULT TTG8Q006HUP3.; [02] SUMMARY EA 21-155-02706 HAS BEEN APPROVED; ACTIVATED; AND ASDR SWAA2021110917682None · corrodedLEFT HORIZONTAL STABILIZER; CENTER SECTION REAR SPAR CLEVIS 'E' CORROSION ; / [01] SUMMARY EA 21-155-02721 HAS BEEN APPROVED; ACTIVATED; AND ADDED AS A SUBTASK TO FAULT TTG8Q006HSVZ.; [02] SUMMARY EA 21-155-02721 HAS BEEN APPROVED; ACTIVATED; AND ADDED AS A SUSDR SWAA2021110917689Spar · corrodedLEFT HORIZONTAL STABILIZER; REAR SPAR CLEVIS 'K' CORROSION ; / [01] SUMMARY EA 21-155-02739 HAS BEEN APPROVED; ACTIVATED; AND ADDED AS A SUBTASK TO FAULT TTG8Q006HUNW.; [02] SUMMARY EA 21-155-02739 HAS BEEN APPROVED; ACTIVATED; AND ADDED AS A SUBTASK TO FAULT SDR SWAA2021110917688Spar · corrodedLEFT HORIZONTAL STABILIZER; REAR SPAR CLEVIS 'J' PITTING CORROSION ; / [01] SUMMARY EA 21-155-02720 HAS BEEN APPROVED; ACTIVATED; AND ADDED AS A SUBTASK TO FAULT TTG8Q006HUNS.; [02] SUMMARY EA 21-155-02720 HAS BEEN APPROVED; ACTIVATED; AND ADDED AS A SUBTASK TSDR SWAA2021110917681Spar · corrodedLEFT HORIZONTAL STABILIZER; REAR SPAR CLEVIS 'H' PITTING CORROSION ; / [01] SUMMARY EA 21-155-02690 HAS BEEN APPROVED; ACTIVATED; AND ADDED AS A SUBTASK TO FAULT TTG8Q006HSVP.; [02] SUMMARY EA 21-155-02690 HAS BEEN APPROVED; ACTIVATED; AND ADDED AS A SUBTASK TSDR SWAA2021110917687Spar · corrodedLEFT HORIZONTAL STABILIZER; FRONT SPAR CLEVIS 'G' CORROSION ; / [01] SUMMARY EA 21-155-02741 HAS BEEN APPROVED; ACTIVATED; AND ADDED AS A SUBTASK TO FAULT TTG8Q006HUNG.; [02] SUMMARY EA 21-155-02741 HAS BEEN APPROVED; ACTIVATED; AND ADDED AS A SUBTASK TO FAULTSDR SWAA2021110917685None · corrodedLEFT HORIZONTAL STABILIZER CENTER SECTION; FRONT SPAR CLEVIS 'B' WORN AND CORROSION ; / [01] SUMMARY EA 21-155-02704 HAS BEEN APPROVED; ACTIVATED; AND ADDED AS A SUBTASK TO FAULT TTG8Q006HUMV.; [02] SUMMARY EA 21-155-02704 HAS BEEN APPROVED; ACTIVATED; AND ADDSDR SWAA2021110917680None · corrodedLEFT HORIZONTAL STABILIZER CENTER SECTION; FRONT SPAR CLEVIS 'A' WORN AND CORROSION ; / [01] SUMMARY EA 21-155-02689 HAS BEEN APPROVED; ACTIVATED; AND ADDED AS A SUBTASK TO FAULT TTG8Q006HSUB.; [02] SUMMARY EA 21-155-02689 HAS BEEN APPROVED; ACTIVATED; AND ADDSDR SWAA2021110917698None · corrodedRIGHT HORIZONTAL STABILIZER; FRON SPAR CLEVIS 'B' WORNOUT CORROSION ; / [01] SUMMARY EA 21-155-02719 HAS BEEN APPROVED; ACTIVATED; AND ADDED AS A SUBTASK TO FAULT TTG8Q006HUQL. <BR>EA-GENERAL AS REPAIR REFERENCE TO CLOSE THE OPEN FAULT ( TTG8Q006HUQL).; [02] SSDR AALA202109178474Rib · crackedAIRCRAFT IN BASE MAINTENANCE: FOUND A CRACK ON THE RIGHT HORIZONTAL STABILIZER IN RIB 3RD STIFFENER FROM FORWARD SPAR AT STA 166.30. INSTALLED DOUBLER REPAIR TO VERTICAL RIB PER SRM 55-10-09-2R-4.SDR AALA202109178151Rib · crackedAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER INTERNAL RIB LOCATED AT STABILIZER STA 101.90, CRACKED AT VERTICAL STIFFENER. REPLACED RIB PER SRM 55-10-09.SDR AALA202109178975Rib · crackedAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER INTERNAL RIB LOCATED AT STABILIZER STA 92.70, CRACKED AT VERTICAL STIFFENER. REPLACED RIB PER SRM 55-10-09.SDR SWAA2021100116007Rib · crackedSUPPLEMENTAL INFORMATION: LT HORIZONTAL STAB REMOVEABLE L/E HAS CRACKED RIB AT L/E STA 105.26 ; / [01] REMOVED AND REPLACED L/H HORIZONTAL STAB REMOVABLE L/E RIB AT STA 105.26 IAW SRM 51-40-05-0G-0; [02] VERIFIED THE L/H LE RIB INSTALLATION AT L/E STA. 105.26 SDR SWAA2021101815560Rib · crackedCRACK LEADING EDGE RIB LOCATED AT ACCESS PANEL 314B LE STA 114.55 AT RT HORIZONTAL STABILIZER ; 2021-403770 / [11] INSTALLED NEW RIB AND FASTENER LOCATED AT ACCESS PANEL 341B LE STA 114.55 AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02 AND DWG 186A1001 SDR AALA202109137007Rib · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN RIB OF LH HORIZONTAL STABILIZER AT STA 92.70, 3RD STIFFENER FROM FRONT SPAR, MEASURING L=0.25 IN, W=0.002 IN. ACCOMPLISHED PERMANENT REINFORCING REPAIR WITH NESTED ANGLES IAW SRM 55-10-09.SDR AALA202109134314Rib · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN RIB OF LH HORIZONTAL STABILIZER ON 2ND STIFFENER FROM FRONT SPAR AT STA 92.70, MEASURING L=0.25 IN, W=0.002 IN. ACCOMPLISHED PERMANENT REINFORCING REPAIR WITH NESTED ANGLES IAW SRM 55-10-09.SDR SWAA2021110815021None · crackedL/H HORIZONTAL STABILIZER L/E FAIRING RIB # 3 CRACKED AT END ; / [01] PERFORMED HFEC INSP ON LH HORIZ STAB L/E FAIRING RIB#3 IAW B737 NDT P6 51-00-00 PROC.23; CRACK NOTED MARKED.<BR>TOOL USED : NORTEC 600 B/C 172389 CALDUE: 02-JUL-22; [02] REMOVED CRACK RIB ONSDR SWAA2021092719041None · nickedSUPPLEMENTAL INFORMATION: LEFT HAND HORIZONTAL STABILIZER INSPAR RIB AT STABILIZER STATION 129.50 3RD VERTICAL STIFFENER HAS NICK IN VERTICAL WEB. ; / [01] UT REQUEST FOR REMAINING THICKNESS AT L/H HORIZ. STAB. ISNPAR RIB AT STAB STA 129.50 3RD VERTICAL STIFFESDR SWIA202164041None · corrodedR/H HORIZONTAL REAR SPAR RBL 16 & RBL 95 GROUND STUDS CORRODED 2 EACH FLAGGED (C CHECK RO 1/20/22) REMOVED & REPLACED RH HORIZONTAL REAR SPAR RBL 16 AND RBL 95 GROUND STUDS IAW CRJ200 AMM 51-80-00. / CALIBRATED TOOL USE . TORQUE WRENCH AV7326, CAL DUE DASDR SWAA2021100413963None · crackedINSPAR RIB ASSY 4 (STAB STA 120.30); STIFFENER 3 CRACKED ; / [01] PERFORMED HFEC INSP. ON INSPAR RIB ASSY 4 (STAB. STA 120.30) STIFFENER 3 IAW B737 NDT PART 6 51-00-00 PROC. 23. CRACK CONFIRMED. EQUIP: NORTEC 600 CAL DUE: 10/21 B/C 166317; [02] PERFORMED LAYOUSDR SWAA2021100413962None · crackedINSPAR RIB ASSY 4 (STAB STA 120.30); STIFFENER 2 CRACKED ; / [01] PERFORMED HFEC INSP. ON INSPAR RIB ASSY 4 (STAB STA 120.30) STIFFENER 2 IAW B737 NDT PART 6 51-00-00 PROC. 23. CRACK CONFIRMED. EQUIP: NORTEC 600 B/C 166317 CAL DUE: 10/21; [02] PERFORMED LAYOUTSDR SWAA2021092112595Web · crackedRIGHT HORIZONTAL STABILIZER LEADING EDGE HAS #3 RIB CRACKED. ; / [01] REMOVED #3 RIB ASSEMBLY FROM R/H HORIZONTAL STAB LEADING EDGE AS PER B737-700 SRM 51-40-02-0G-0.; [02] VERIFIED #3 RIB REMOVAL.; [03] REMOVED WED #3 RIB AT R/H H/STAB L/E.IAW B733 SRM 51-40-SDR SWAA2021092121324Rib · crackedRIGHT HORIZONTAL STABILIZER LEADING EDGE HAS #3 RIB CRACKED. ; / [01] REMOVED #3 RIB ASSEMBLY FROM R/H HORIZONTAL STAB LEADING EDGE AS PER B737-700 SRM 51-40-02-0G-0.; [02] VERIFIED #3 RIB REMOVAL.; [03] REMOVED WED #3 RIB AT R/H H/STAB L/E.IAW B733 SRM 51-40-SDR SWAA2021092112597Rib · crackedRIGHT HORIZONTAL STABILIZER LEADING EDGE HAS #5 RIB CRACKED. ; / [01] REMOVED RIB #5 FOR RT HORIZONTAL STAB AS PER B737-7 SRM 51-40-02-0G-0 STEP 4.; [02] VERIFIED STEP 1.; [03] LOCATED AND DRILLED RIB AND ASSEMBLY AT #4RIB FROM R/H H/STAB L/E IAW B737 SRM51-40SDR SWAA2021100812544Fitting · corrodedCORROSION TRAILING EDGE VERTICAL FIN AFT SPAR FITTING FWD OUTBOARD LUG AT VERTICAL STABILIZER (1EA) ; 2021-369555 / [15] REPLACED FITTING LOC TRAILING EDGE VERTICAL FIN AFT SPAR FWD OUTBOARD LUG AT VERTICAL STABILIZER LH SIDE IAW EA 21-153-02648 SUMMARY AND EASDR SWAA2021091010655Rib · crackedCRACK LEADING EDGE SKIN ACCESS PANEL 341B AT STA 95.96 AT RT HORIZONTAL STABILIZER (1 EA) ; 2021-368797 / [01] TOOK MEASURES OF CRACK RIB LEADING EDGE SKIN ACCESS PANEL 241B AT STA 95.96 RT HORIZONTAL STABILIZER MEASURES ARE: L:0.245 TOOL USED IS CALIPER P/N: SDR SWAA2021091010656Rib · crackedCRACK LEADING EDGE SKIN ACCESS PANEL 341B AT STA 105.26 AT RT HORIZONTAL STABILIZER (1 EA) ; 2021-368798 / [01] TOOK MEASURES OF CRACK RIB LEADING EDGE SKIN ACCESS PANEL 241B AT STA 105.26 AT RT HORIZONTAL STABILIZER MEASURES ARE: L:0.235 TOOL USED IS CALIPER SDR SWAA2021092209040Rib · crackedCRACK LEADING EDGE LOC ON RIB LE STA 105.26 AT LT HORIZONTAL STABILIZER ; 2021-391874 / [19] REPLACE RIB AND FASTENER LOC. ON LE STA 105.26 AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02; 51-10-02 ITEM 9 AND DWG:186A1001 SHEET:10 REV:A; RII.SDR SWAA2021100509609None · crackedREMOVE RH HORIZONTAL STABILIZER RIB #5 FOR CRACK REPAIR AND REINSTALL WHEN REPAIR IS COMPLETED. ; / [01] REMOVED RH HORIZONTAL STABILIZER RIB #5 AS PER REF B737-700 SRM 51-40-02-0G-0; [02] DISPLACED ELEVATOR BALANCE PANEL AT R/H HORIZONTAL STABILIZER T/E BAY 2SDR SWAA2021100509546None · crackedCRACK INSPAR RIB LOCATED STAB STA 129.50 AT 26 INCHES FROM FRONT SPAR AT RT HORIZONTAL STABILIZER ; 2021-392694 / [18] REPAIRED INSPAR RIB STAB STA 129.50 AT 26 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER IAW SRM B737-700 55-10-09-2R-4 FIG 202 SHEET 1 VIESDR SWAA2021100509602None · crackedRH HORIZONTAL STAB RIB #5 STIFFENER #3 HAS A CRACK. ; / [01] REMOVED THE DAMAGED PART FROM R/H HORIZONTAL STAB. RIB#5 STIFFENER #3 AS PER REF SRM 55-10-09-2R-4; [02] VERIFIED STEP 1; DAMAGED REMOVED.; [03] VERIFIED STEP 1; DAMAGED REMOVED.; [04] PERFORMED HFECSDR SWAA2021091609154Spar · corrodedCORROSION FOUND ON RH REAR SPAR LOWER LUG K HAS CORROSION ON BOTH FACE OF THE LUG. ; / [01] REPAIR ACCOMPLISHED PER EA 21-155-02337. REFER TO FAULT TTG8Q0065LLA.; [02] VERIFIED STEP 1SDR R61A2021091200733Rib · crackedRH H-STAB INTERNAL RIBS 10A, 11A & 12A FOUND CRACKED. REPLACED IAW REPUBLIC AIRWAYS EO 170EO-55-10-0004_1 (P/N'S 170-62571-002, 170-62783-002 & 170-62642-002)SDR R61A2021091200732Rib · crackedLH H-STAB INTERNAL RIBS 11A & 12A FOUND CRACKED. REPLACED IAW REPUBLIC AIRWAYS EO 170EO-55-10-0004_1 (P/N'S 170-62783-001 & 170-62642-001)SDR JR2R202018224884Rib · crackedR\H HORZ RIB 12 CRACKEDSDR SWAA2021092108761Rib · crackedCRACK INSPAR RIB 129.50 AT 18 INCHES OF FRONT SPAR LT HORIZONTAL STAB ; 2021-384030 / [01] REMOVED INSPAR RIB 129.50 HORIZONTAL STAB AREA AND FASTENER IAW B737-700 SRM 51-40-02.; [02] VERIFYED STEP 1; [03] PERFORM CUT OUT DAMAGE : PERFORMED CUT OUT DAMAGE FROMSDR SWAA2021092108768Rib · crackedCRACK INSPAR RIB 129.50 AT 27 INCH OF FRONT SPAR AT LT HORIZONTAL STABILIZER ; 2021-384031 / [18] INSTALLED REPAIR PART ;ANGLE (1E/A);FILLER. (1E/A);T-SECTION (1E/A); SHIM (2E/A) AND FASTENER ON INSPAR RIB LOC.STAB STA 129.50 AND AT 27 INCH FROM FRONT SPAR AT SDR SWAA2021092108762Rib · crackedCRACK INSPAR RIB 129.50 AT 35 INCH OF FRONT SPAR AT LT HORIZONTAL STABILIZER ; 2021-384032 / [18] CERTIFIED STEP 14 AS RII. OK TO INSTALL GRANTED.; [19] INSTALLED REPAIR PART;A,NG,NRC,2021-09-07 21:25:09,22Y,Y,MX,0,0,,CRACK INSPAR RIB 129.50 AT 35 INCH OF FRON
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