JASC 5510
Service difficulty reports · 5,966
Reports filed under 5510 · Horizontal Stabilizer Structure, 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 = '5510' 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 = '5510' 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 SWAA2022100678801None · crackedCRACK INSPAR RIB 120.30 AT 36 INCHES OF FRONT SPAR AT RT HORIZONTAL STABILIZER 2022-466793 / [01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 210138503; CAL DUE DATE: 19-MAY-23;[02] TOOL USED: DIGITAL CALIPER P/N:500-197-30; S/N:B16152123; DUSDR SWAA2022100678802Skin Panel · crackedCRACK INDICATION FOUND ON LT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.9 AND 16 INCH. FROM FRONT SPAR. CRACK LENGTH = 1.100 INCH. APPROX. 2022-466843 / [01] TOOL USED: ET EQUIPMENT P/N: NORTEC 600D; S/N: 60009161631; CAL DUE DATE: 03-DEC-SDR ASAA2022091440105Skin · crackedR/H HORIZONTAL LOWER SKIN CRACKED AT STA 94.0 AND REAR SPAR. GROUNDED - YES. REMOVED EXISTING REPAIR PREFORMED CUTOUT OF DAMAGE AND ISNTALLED NEW REPAIR IAW B737-900 SRM 55-10-01-2R-11 CAT B REPAIR WITH AN INSPECTION THRESHOLD OF 56,000 FLT CYCLES.SDR ASAA2022091440104Skin · crackedR/H HORIZONTAL LOWER SKIN IS CRACKED AT STA 147 AND REAR SPAR. GROUNDED - YES. REMOVED EXISTING REPAIR PREFORMED CUTOUT OF DAMAGE AND INSTALLED NEW REPAIR IAW B737-900 SRM 55-10-01-2R-11 CAT B REPAIR WITH AN INSPECTION THRESHOLD OF 56,000 FLT CYCLES.SDR SWAA2022101252303None · crackedCRACK INDICATION FOUND ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 16.0 INCH FROM FRONT SPAR; INBD SIDE OF RIB. CRACK LENGTH IS 1.000 INCH. PERFORMED REPAIR ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 16.0 ISDR AALA202209153085Hinge Fitting · wornAIRCRAFT IN BASE MAINTENANCE LEFT HAND ELEVATOR #6 HINGE ARM END FITTING WORN. REPLACED HINGE ARM FITTING PER AMM 55-16-42.SDR R61A2022101800642Stabilizer · cracked"MAJOR" CRACKED FOUND R/H H-STAB AT RIB 12. REPLACED ON REPUBLIC AIRWAYS TASK CARD 4501219-3000-0101 MAJOR REPAIR. REFERENCE SB 170-55-0014 FOR REPAIR.SDR SWAA2022090750622Attach Angle · crackedRIGHT HORIZONTAL STABILIZER FORWARD UPPER SLIDER CRACKED. / [01] REMOVE AND REPLACED R/H HORIZONTAL STABILIZER FORWARD UPPER SLIDER IAW AMM 53-31-31SDR CALA2022090702290None · crackedLH HORZ STAB STA 92.70 VERTICAL RIB STIFFENER #3 CRACKED. LH HOR Z STAB LOWER SKIN REQUIRES CUTOUT FOR STA 92.70 VERTICAL RIB STI FFENER #3 CRACK REPAIR.CUTOUT SKIN STA 92.70 AT VERTICAL STIFFEN ER #3 IAW B737-900 SRM 55-10-01-2R-11 REPAIR 11 STEP 4.(2). VERI SDR CALA2022090702289None · noneL/H HORIZONTAL STAB LOWER SKIN AT STA 92.70 REQUIRES LOWER SKIN CUTOUT FOR ACCESS TO REPAIR THE #3 RIB STIFFENER. ER. REPEATINSPECTIONS EVERY 9,000 FLIGHT CYCLES THERE AFTER SEE PLISHED ON MAIN TASK (REFERENCE SUB TASK ST-001: PERFORMED 737 N 1-2R.REFERENCESDR CALA2022090702292None · noneRETURN TO GATE REF REJECTED TAKE OFF ACP CHECK OF BRAKES REF AMM 05--51-16-200-001. CREW REPORTS BRAKE TEMP IN THE MID 400 DEGREES. BRAKES CK OK, NO DAMAGE NOTED PER CREW REJECTED T-O OCCURRED DUE TO FLEX T-O TEMPERATURE CLOSE TO STATION OATSDR CALA2022090702306Skin · noneDURING C-SCAN INSPECTION EA5510-01843 OP 1 AT GYR, CRACK FOUND AT LH HORIZONTAL STAB LOWER SURFACE AT APPROX STA 120.30. TOTAL FLIGHT CYCLES, INTERVAL 9000 FLIGHT CYCLES. INFO TRANSCRIBED FROM AERSALE NON-ROUTINE CARD 23472. LH HORIZONTAL STAB LOWER SURFACE SSDR CALA2022090702298Skin · crackedDURING C-SCAN INSPECTION EA5510-01843 OP 1 AT GYR, CRACK FOUND AT LH HORIZONTAL STABILIZER LOWER SURFACE AT APPROX STA 129.50 TOTAL FLIGHT CYCLES, INTERVAL 9000 FLIGHT CYCLES. INFO TRANSCRIBED FROM AERSALE NON-ROUTINE CARD 23471. LH HORIZONTAL STAB LOWER SURFASDR AALA202209061723Sleeve · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY, RIGHT HAND HORIZONTAL STABILIZER MAST ARM BEARING. REPLACED MAST ARM BEARING (AALA202209066801) AND SLEEVE (AALA202209061723) PER CMM 55-20-17 MAST ARM ASSEMBLY REPAIR 2-1, SOPM 20-50-03 AND DWG 183A1200 REV B. ACCSDR AALA202209061083Sleeve · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY, LEFT HAND HORIZONTAL STABILIZER MAST ARM BEARING. REPLACED MAST ARM BEARING (AALA202209061930) AND SLEEVE (AALA202209061083) PER CMM 55-20-17 MAST ARM ASSEMBLY REPAIR 2-1, SOPM 20-50-03 AND DWG 183A1200 REV B. ACCOSDR AALA202209061930Bearing · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY, LEFT HAND HORIZONTAL STABILIZER MAST ARM BEARING. REPLACED MAST ARM BEARING (AALA202209061930) AND SLEEVE (AALA202209061083) PER CMM 55-20-17 MAST ARM ASSEMBLY REPAIR 2-1, SOPM 20-50-03 AND DWG 183A1200 REV B. ACCOSDR AALA202209066801Bearing · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY, RIGHT HAND HORIZONTAL STABILIZER MAST ARM BEARING. REPLACED MAST ARM BEARING (AALA202209066801) AND SLEEVE (AALA202209061723) PER CMM 55-20-17 MAST ARM ASSEMBLY REPAIR 2-1, SOPM 20-50-03 AND DWG 183A1200 REV B. ACCSDR SIMA20220902001None · crackedLH HORIZONTAL STAB. RIB 12A IS CRACKED.-C/A-REMOVED AND REPLACED RIB 12A IAW EO-EJ-5500-006.SDR SIMA20220901001None · crackedRT HORIZONTAL STAB RIB 12A IS CRACKED.-C/A-REMOVED AND REPLACED RIB 12A IAW EO-EJ-5500-006.SDR SWAA2022093048199None · crackedL/H HORIZONTAL STABILIZER RIB #4 AFT LOWER SURFACE CRACKED. L/H HORIONTAL STABILIER RIB #4 FWD LOWER SURFACE CRACKED. / [01] TRIMMED DAMAGED AREA AFT LOWER SURFACE PER REFERENCE 51-10-02-0G-0.;[02] CORRECTION TO STEP 1; TRIMMED DAMAGED AREA FWD LOWER SURFACE PSDR SWAA2022093048200None · crackedL/H HORIZONTAL STABILIZER RIB #4 AFT UPPER SURFACE CRACKED. L/H HORIONTAL STABILIER RIB #4 FWD UPPER SURFACE CRACKED. / [01] TRIMMED DAMAGED AREA AT AFT UPPER SURFACE PER REFERENCE SRM 51-10-02-0G-0.;[02] CORRECTION TO STEP 1; TRIMMED DAMAGED AREA AT FWD UPPERSDR SWAA2022093048703None · crackedL/H HORIZONTAL STABILIZER RIB #4 LOWER FLANGE HAS (7 EACH) CRACKS. / [01] TRIMMED 4 EACH AREAS ON LOWER FLANGE OF RIB #4 REF. SRM 51-10-02-0G-0 FABRICATED LOWER ANGLE USING BAC 1490 7075-T6 PER REF SRM 55-10-09-2R-5;[06] LOCATED AND DRILLED REPAIR PARTS PER SRSDR SWAA2022093048704None · elongatedL/H HORIZONTAL STABILIZER RIB #4 UPPER FLANGE HAS ( 1 EACH) HOLE ELONGATED. / [01] TRIMMED ONE EACH HOLE ON FLANGED PER REFERENCE SRM 51-10-02-0G-0.;[02] VERIFIED STEP 1.;[03] PERFORMED HFEC INSP ON CUT OUT AREA IAW B737 NDT P6 51-00-00 PROC.23; NO CRACKS<BR>TSDR IPXA2022091086098Bracket · gougedINSPECTION TYPE:A300IH HOR,STAB,TOP BRACKET HAS GOUGE WITHREMOVED AND REPLACED BRACKET IAW AMM 10-88-0401SDR IPXA2022091086097Bracket · gougedINSPECTION TYPE:A300IH HOR STAB TOP BRACKET HAS GOUGE WITHREMOVED AND REPLACED BRACKET IAW-AMM 53-10-88-0401SDR IPXA2022091086096Bracket · noneINSPECTION TYPE:A300IH HOR,STAB,TOP BRACKET HAS GOUGE WITHREMOVED AND REPLACED BRACKET IAW AMM 53-10-88-0401SDR SWAA2022090248132None · crackedRH HORIZONTAL STABILIZER UPPER SLIDING SEAL IS CRACKED / [01] REMOVED AND REPLACED RH HORIZONTAL STABILIZER UPPER SLIDING SEAL IN ACCORDANCE WITH AMM 53-31-31.SDR AALA202209076767Hinge Fitting · wornAIRCRAFT IN BASE MAINTENANCE RIGHT HAND HORIZONTAL STABILIZER #6 HINGE FITTING IS WORN. REPLACED HINGE FITTING PER AMM 55-16-42.SDR AALA202209074488Hinge Fitting · wornAIRCRAFT IN BASE MAINTENANCE RIGHT HAND HORIZONTAL STABILIZER #3 HINGE FITTING IS WORN. REPLACED HINGE FITTING PER AMM 55-16-42.SDR AALA202209077096Hinge Fitting · wornAIRCRAFT IN BASE MAINTENANCE RIGHT HAND HORIZONTAL STABILIZER #2 HINGE FITTING IS WORN. REPLACED HINGE FITTING PER AMM 55-16-42.SDR CALA2022082902214Seal · missingPDA 3 LEFT HORIZONTAL STAB - SEAL FWD OF ELEVATOR DAMAGED. PART OF SEAL MISSING. PIC REPLACED ELEVATOR SEAL ASSY.SDR CALA2022082902212None · noneL/H HORIZONTAL STAB REQUIRES ACCESS HOLES TO BE CUT OUT IN LOWER SKIN FOR #3 RIB STIFFENER REPAIR AT STA 92.7 A HT CYCLES REPEAT INTERVAL THEREAFTER. , NEED TO PLACE ON DIP FO T INITIAL THRESHOLD OF 56,000 TOTAL FLIGHT CYCLES AND 9,000 FLIG REPAIRED LEFT HORZ.SDR CALA2022082902211None · crackedRIGHT HORZ STAB HAS A 3 1/2 INCH CRACK BETWEEN THE R HORZ STAB STA 101.90 AND 111.10 AT THE R HORZ STUB REAR SPAR. 56,000 TOTAL FLIGHT CYCLES AND 9,000 FLIGHT CYCLES REPEAT AND INSPECTION BUYBACKS. AT INITIAL THRESHOLD OF INTERVAL THEREAFTER. REPAIRED RH HORZSDR CALA2022082902210None · crackedLEFT HORIZ STAB HAS A 1 INCH CRACK AT THE L HORIZ STAB STA 147.0 ,32 INCHES FROM FRONT SPAR. 56,000 TOTAL FLIGHT CYCLES AND 9,000 FLIGHT CYCLES REPEAT AND INSPECTION BUYBACKS. AT INITIAL THRESHOLD OF INTERVAL THEREAFTER. REPAIRED LEFT HORZ. STAB. LOWER INSPAR SDR CALA2022082902209None · crackedLEFT HORIZ STAB HAS A CRACK AT THE L.HORIZ STAB STA 157.10, 32 INCHES FROM THE FRONT SPAR THIS N/R IS FOR SFR REPORTING PURPOSES REPAIR 11, 737 ND L FLIGHT CYCLES AND 9,000 FLIGHT CYCLES REPEAT INTERVAL THEREAFT D INSPECTION BUYBACKS. AT INITIAL THRESHOLD OF SDR YENA2022083000843Hinge · damagedFLT#994, DEN-BOS. ' RIB ON RIGHT HORIZONTAL STAB ITEM 6 ASRP 55-12-18-02 BROKEN. RIB HINGE ON RIGHT HORIZONTAL STAB ITEM 4 ASRP 55-11-18-02 DAMAGED; RIB SHROUD 1 (RH) REPLACED UNDER WORK INSTRUCTIONS OF EC A22-610-01. REF LOG PAGE 3394236-2 (W/O #1187189 COMPLSDR DALA2022082605768None · noneSHIP 3329 RH UPPER APRON SIDESLIPS MISSING. CORRECTIVE ACTION:REMOVED AND INSTALLED L/H UPPER THS APRON FAIRING IAW A330 AMM 55-15. (9204824)SDR SWAA2022093046364None · crackedL/H HORIZONTAL STAB INSPAR RIB ASSEMBLY #4 STIFFENER #3 CRACKED. / [01] PERFORMED HFEC INSP ON STIFFENER #3 IAW B737 NDT P6 51-00-00 PROC.23; CRACK NOTED<BR>TOOL USED : NORTEC 600 B/C 166317 CALDUE: 10/22;[02] CUT DAMAGED AREA OF STIFFER #3 ON L/H HORIZONTAL SSDR SWAA2022093046363None · crackedL/H HORIZONTAL STAB INSPAR RIB ASSEMBLY #4 STIFFENER #2 CRACKED. / [01] PERFORMED HFEC INSP ON STIFFENER #2 IAW B737 NDT P6 51-00-00 PROC.23; CRACK NOTED<BR>TOOL USED : NORTEC 600 B/C 166317 CALDUE: 10/22;[02] CUT DAMAGED AREA OF STIFFER #2 ON L/H HORIZONTAL SSDR SWAA2022092169633Skin · crackedCRACK IN LH HORIZ STAB LWR SKIN AT OUTBD ROW OF FASTENERS COMMON TO RIB STA 193.9. .7 INCHES IN LENGTH. FOUND ON HFEC INSPECTION. MARKED IN RED. / [01] TRIMMED OUT THE DAMAGE PART OF THE STAB SKIN AT DISCREPANCY AREA; CUT OUT DIMENSIONS 1.8' X 1.0' IAW SRM 55-SDR ASAA2022082439990Rib · crackedLH HORIZONTAL LE: 3RD RIB FROM INBD END CRACKED. GROUNDED - YES. CUT OUT DAMAGE AND REPAIRED RIB IAW B737-900 SRM 55-10-09-2R-4.SDR CALA2022082402164Window · openHIGH SPEED ABORT DUE TO FIRST OFFICERS WINDOW COMING OPEN ON TAK EOFF ROLL. HIGH ENERGY STOP INSPECTION COMPLETED ON L/P 9359946. PERFORMED OPERATIONAL CHECK OF F/O''S SLIDING WINDOW REF AMM 56-11-02-715-020. NO FAULTS NOTED AT THIS TIME.SDR CALA2022082402150Stabilizer · crackedRIGHT HORIZONTAL STABILIZER-CRACK FOUND AT APPROXIMATE STAB STA 147.90 AND 23.5 INCHESS AFT OF THE FRONT SPAR. REF.BAM N/R 000803532 REQUIREMENTS PER SRM 55-10-01-2R REPAIR 11 TABLE 204. INSPECTION PERFORM DETAILED VISUAL INSPECTION AND EXTERNAL LFEC EVERY 9,0SDR R61A2022092000563Rib · crackedDURING HEAVY CHECK MAINTENANCE FOUND HORIZONTAL STAB RIB 12 RH CRACKED. HORIZONTAL STAB RIB 12A REPLACED IAW REPUBLIC 170EO-55-10-0004_1. REF SB170-55-0014 REV 1SDR SWAA2022091244110None · crackedCRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB BTW RBL 39 TO RBL 50 STA 663 AT PASSENGER CABIN (1E/A). CRACK LENGTH APPROXIMATELY: 0.312 INCH. 2022-447263 / [01] TOOL EDDY CURRENT USED P/N: NORTEC 600D S/N: 200048001 AND DUE DATE: 30-MAR-23.;[02] TOOL USED ESDR CALA2022082202133Rib · corrodedEA 5510-01843 REV H OP 001: LH HORZ STAB AT RIB 147.9 HAD RELEVANT INDICATION OF CRACK DURING C-SCAN. REF BY PEMCO NR.12666.0378 STALLED REPAIR DOUBLER REPAIR IAW SRM 55-10-01-2R-11 REPAIR 11. L FLIGHT CYCLES WITH REPEAT INSPECTIONS EVERY 9000 FLIGHT CYCLES 51SDR SWAA2022093065335None · crackedLHS LEADING EDGE HAS RIB 4 CRACKED. 8-22 / [01] REMOVED AT LT HORIZONTAL STABILIZER OF LEADING EDGE RIB #4 IN IAW SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW RIB IN IAW SRM 51-40-05-0G-0;[03] VERIFIED 1-2. OK TO INSTALL NEW RIB.;[04] INSTALLED NEW RIB #4 ATSDR SWAA2022093065336None · crackedLHS LEADING EDGE HAS RIB 5 CRACKED. 8-23 / [01] REMOVED RIB# 5 AT LT HORIZ STAB L/E REF B737-700 SRM 51-40-02-0G-0.;[02] LOCATED AND DRILLED NEW RIB AT LT HORIZ STAB L/E REF B737-700 SRM 51-40-05-0G-0 AND DWG# 186A1001.;[03] VERIFIED STEPS #1 AND #2.;[04] OK TSDR SWAA2022093065347None · crackedLEADING EDGE PANEL RIB ASSY. #2; CRACK NOTED AT RIVET HOLE (DOT 223-HLE002). / [01] REMOVED RIB ASSY #2 AT LEADING EDGE PANEL AS PER B737-700 SRM 51-40-02-0G-0.;[02] LOCATED AND DRILLED NEW RIB #2 POSITION AT LEADING EDGE R/H HORIZONTAL STABILIZER IN IAW SRM 5SDR SWAA2022093065350None · crackedLEADING EDGE PANEL RIB ASSY. #4; CRACK NOTED AT RIVET HOLE (DOT 223-HLE004). / [01] REMOVED RIB ASSY #4 AT LEADING EDGE PANEL AS PER B737-700 SRM 51-40-02-0G-0.;[02] LOCATED AND DRILLED NEW RIB ASSY #4 AT LEADING EDGE PANEL AS PER B737-700 SRM 51-40-05-0G-0; D
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