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 SWAA2022072728958Stiffener · crackedR/H HORIZONTAL STABILIZER RIB #4 STIFFENER #3 LOWER FLANGE WITH A CRACK / [01] CRACK CONFIRMED IAW NDTM PART 6; 51-00-00 PROCEDURE 23. CRACK LENGTH : 1.339'<BR>[NORTEC 600 ; B/C 166317 ; CALIB.DUE- 10/22];[02] CUTOUT THE DAMAGE AREA AT RH HORIZONTAL STAB RIB #SDR SWAA2022072729277Support Angle · crackedFOUND T SUPPORT ANGLE CRACKED AT RT STAB RIB #5 / [01] REMOVED FWD T SUPPORT ANGLE FROM RT STAB RIB #5 AS PER B737-700 51-40-02-0G-0;[02] CORRECTION FOR STEP #1 SHOULD READ: REMOVED FWD T SUPPORT ANGLE FROM RT STAB RIB #5 AS PER B737-700 SRM 51-40-02-0G-0;[03]SDR SWAA2022081628057Rib · crackedCRACK LEADING EDGE RIB LOCATED L/E STA 105.26 AT RT HORIZONTAL STABILIZER 2022-381242 / [01] REPLACED RIB AND FASTENERS ON LEADING EDGE LOCATED L/E STA 105.26 AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02; B737-700 SRM 51-10-02 ITEM 9; AND DWG 186A1001SDR SWAA2022081628171Rib · crackedCRACK INSPAR RIB LOCATED STAB STA 120.30 AND 10 INCH FROM REAR SPAR LT HORIZONTAL STAB 2022-368107 / [01] TOOL USED EDDY CURRENT INSTRUMENT P/N NORTEC600D S/N 190023010 DUE DATE 14-FEB-23.;[02] TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 500D; S/N: N500X12101SDR SWAA2022080228210Rib · crackedCRACK LEADING EDGE RIB AT L/E STA 95.96 AT LT HORIZONTAL STABILIZER 2022-384009 / [01] REPLACED NEW RIB LOCATED LEADING EDGE RIB AT L/E STA 95.96 AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02-0G-0 AND DWG 186A1001 REV:B SHET:1 <BR><BR>SEE INDIVIDUAL SISDR SWAA2022080228211Rib · crackedCRACK LEADING EDGE RIB AT L/E STA 105.26 AT LT HORIZONTAL STABILIZER 2022-384010 / [01] REPLACED RIB LT STA 105.26 AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02 AND DWG 186A1001 REV:B SHEET:1 <BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW;[02] STEP 1 VERIFIED ASDR SWAA2022080228212Rib · crackedCRACK LEADING EDGE RIB AT L/E STA 114.55 AT LT HORIZONTAL STABILIZER 2022-384011 / [01] REPLACED RIB LT STA 114.55 AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02 AND DWG 186A1001 REV:B SHEET:1 <BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW;[02] STEP 1 VERIFIED ASDR SWAA2022081727891Angle · crackedCRACK INSPAR RIB 3 STAB STAB 111 AT 29 INCH OF FRONT SPAR AT RT HORIZONTAL STABILIZER 2022-381074 / [01] TOOL USED: EDDY CURRENT EQUIPMENT; PN: NORTEC 600D; SN:200048001; DUE DATE: 30-MAR-23;[02] TOOL USED: EDDY CURRENT EQUIPMENT; PN: NORTEC 600D; SN:200048001SDR SWAA2022081627892Rib · crackedCRACK INSPAR RIB 9 STAB STA 166 AT 24INCH OF FRONT SPAR AT RT HORIZONTAL STABILIZER 2022-381075 / [01] ET TOOL USED: PN: MIZ-21C ; SN: 769680; DUE DATE: 07-JUL-23;[02] TOOL EDDY CURRENT USED P/N: NORTEC 600D S/N: 210136503 AND DUE DATE: 11-APR-23.;[03] PERFORMSDR CALA2022071101712Bracket · damagedR/H HORIZONTAL STAB L/E FRONT SPAR INTERNAL STRUCTURAL RIG NO.5 SUPPORT TOP FWD BRACKET IS BROKEN REF AAR N/R 9657235 ACCOMPLISHED REPAIR AT R/H STAB INSPAR RIB NO.5 STA 129.50 UPPER CHORD O/B FLANGE AND ACCOMPLISHED INSTALLATION OF RIB PER B737 SRM 51-46-02 ASDR CALA2022071101696Rib · damagedR/H HORIZONTAL STAB L/E FRONT SPAR INTERNAL STRUCTURAL RIG NO.5 SUPPORT TOP FWD BRACKET IS BROKEN REF AAR N/R 9657235 ACCOMPLISHED REPAIR AT R/H STAB INSPAR RIB NO.5 STA 129.50 UPPER CHORD O/B FLANGE AND ACCOMPLISHED INSTALLATION OF RIB PER B737 SRM 51-46-02 ASDR SWAA2022072726079Rib · crackedFOUND CRACK AT FWD LOWER RIB #4 AFTER REMOVAL OF RIB #4 FOUND A CRACK AT THE LOWER FWD SIDE OF THE RIB / [01] PERFORMED HFEC INSP ON FWD LWR AREA OF RIB#4 IAW B737 NDT P6 51-00-00 PROC.23; CRACK CINFIRMED MARKED<BR>TOOL USED : NORTEC 600 B/C 172389 CALDUE: 03/SDR SWAA2022082225924Stiffener · crackedRIGHT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 120.30; 3RD VERTICAL STIFFENER IS CRACKED. / [01] VALIDATED APPLICABILITY OF SRM 55-10-09-2R-4&5.11] FABRICATED REPAIR T-SECTION FROM 60-5872 7075T6511 .063' CLAD LOT#476286-1. REPAIR ANGLE FROSDR SWAA2022080425630Rib · crackedCRACK INSPAR RIB LOCATED STAB STA 120.30 AND 27 INCH FROM FRONT SPAR LT HORIZONTAL STAB 2022-354604 / [01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 60009161631; DUE DATE: 03- DEC-22.;[02] EDDY CURRENT EQUIPMENT USED: P/N: NORTEC 600D; S/N:SDR SWAA2022080425626Rib · crackedCRACK INSPAR RIB LOCATED STAB STA 120.30 AND 10 INCH FROM REAR SPAR LT HORIZONTAL STAB 2022-354605 / [01] ET TOOL USED: PN: NORTEC 600D; SN: 200053492; DUE DATE: 13-MAY-23;[02] ET TOOL USED: PN: NORTEC 600D; SN: 200053492; DUE DATE: 13-MAY-23;[03] EDDY CURRENTSDR JR2R20220630862Rib · crackedLEFT HORIZONTAL STAB LEADING EDGE RIB 13 IS CRACKEDSDR SWAA2022072723940Stiffener · crackedL/H HORIZONTAL STABILIZER RIB #2 STIFFENER #2 LOWER FLANGE HAS A CRACK. / [01] PERFORMED HFEC INSP ON RIB STIFFENER LOWER FLANGE IAW B737 NDT P6 51-00-00 PROC.23; CRACK CONFIRMED.<BR>TOOL USED : NORTEC 600 B/C 172389 CALDUE: 03/23;[02] PERFORMED HFEC INSP ON RSDR SWAA2022072723941Stiffener · crackedL/H HORIZONTAL STABILIZER RIB #5 STIFFENER #2 LOWER FLANGE; WITH A CRACK. STAB. STA-129.50 / [01] PERFORMED HFEC INSP ON RIB STIFFENER LOWER FLANGE IAW B737 NDT P6 51-00-00 PROC.23; CRACK CONFIRMED.<BR>TOOL USED : NORTEC 600 B/C 172389 CALDUE: 03/23;[06] CUT OSDR SWAA2022072723942Stiffener · crackedL/H HORIZONTAL STABILIZER RIB #5 STIFFENER #3 LOWER FLANGE; WITH A CRACK. STAB. STA-129.50 / [01] PERFORMED HFEC INSP ON RIB STIFFENER LOWER FLANGE IAW B737 NDT P6 51-00-00 PROC.23; CRACK CONFIRMED.<BR>TOOL USED : NORTEC 600 B/C 172389 CALDUE: 03/23;[02] CUT OSDR SWAA2022072723943Stiffener · crackedL/H HORIZONTAL STABILIZER RIB #5 STIFFENER #4 LOWER FLANGE; WITH A CRACK. STAB. STA-129.50 / [01] PERFORMED HFEC INSP ON RIB STIFFENER LOWER FLANGE IAW B737 NDT P6 51-00-00 PROC.23; CRACK CONFIRMED.<BR>TOOL USED : NORTEC 600 B/C 172389 CALDUE: 03/23;[02] CUT OSDR JR2R20220629992Rib · crackedLH HORIZONTAL OB/ RIB #14 CRACKED ON THE AFT UPPER FLANGESDR SWAA2022072723921Stiffener · crackedR/H HORIZONTAL STABILIZER RIB #4 STIFFENER #3 LOWER FLANGE WITH A CRACK. / [01] PERFORMED HFEC INSP ON RIB STIFFENER LOWER FLANGE IAW B737 NDT P6 51-00-00 PROC.23; CRACK CONFIRMED.<BR>TOOL USED : NORTEC 600 B/C 172389 CALDUE: 03/23;[02] RT STABILAIZER RIB 4 STSDR SWAA2022072723923Stiffener · crackedR/H HORIZONTAL STABILIZER RIB #4 STIFFENER #4 LOWER FLANGE WITH A CRACK. / [01] PERFORMED HFEC INSP ON RIB STIFFENER LOWER FLANGE IAW B737 NDT P6 51-00-00 PROC.23; CRACK CONFIRMED.<BR>TOOL USED : NORTEC 600 B/C 172389 CALDUE: 03/23;[02] CUTOUT THE DAMAGE AREA SDR SWAA2022072922272Rib · crackedL/H HORIZONTAL RONT SPAR MOVEABLE L/E FAIRING CRACKED @ RIB 2 END MKD DOT / [01] PERFORMED HFEC INSP. ON L/H HORIZ STAB. FRONT SPAR MOVABLE L/E FAIRING @ RIB #2 END IAW B737 NDT PART 6 51-00-00 PROC. 23. CRACK CONFIRMED; EQUIP: NORTEC 600 B/C 172389 CAL DUE: 3SDR AALA202207120728Rib · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN LEFT HAND HORIZONTAL STABILIZER INSPAR RIB LOCATED AT STABILIZER STA 101.90. REPAIRED PER SRM 55-10-09-2R PROCEDURE 4 REPAIR 4.SDR SWAA2022071921704Rib · crackedR/H HORIZONTAL STABILIZER MOVEABLE L/E FAIRING RIB 5 CRACKED @ EDGE MKD DOT C0RRECTION OF RIB 5 TO RIB 6 R/H HORIONTAL STAB FRONT SPAR FAIRING / [01] PERFORMED HFEC INSP ON R/H HORIZ STAB MOVEABLE L/E FAIRING RIB#5 IAW B737 NDT P6 51-00-00 PROC.23; CRACK NOTEDSDR SWAA2022071921705Rib · crackedR/H HORIZONTAL STABILIZER MOVEABLE L/E FAIRING RIB 7 CRACKED @ EDGE MKD DOT FAULT CORRECTION FROM RIB 7 TO RIB 8 R/H HORIONTAL. STAB FRONT SPAR MOVEABLE FAIRING / [01] PERFORMED HFEC INSP ON R/H HORIZ STAB MOVEABLE L/E FAIRING RIB#7 IAW B737 NDT P6 51-00-00 PRSDR SWAA2022071921706Rib · crackedL/H HORIZONTAL STABILIZER MOVEABLE L/E FAIRING RIB 3 CRACKED @ EDGE MKD DOT / [01] PERFORMED HFEC INSP ON L/H HORIZ STAB MOVEABLE L/E FAIRING RIB#3 IAW B737 NDT P6 51-00-00 PROC.23; CRACK NOTED (CRACK LENGTH 0.500')<BR>TOOL USED : NORTEC 600 B/C 172389 CALDUE:SDR SWAA2022071921707Rib · crackedL/H HORIZONTAL STABILIZER MOVEABLE L/E FAIRING RIB 4 CRACKED @ EDGE MKD DOT / [01] PERFORMED HFEC INSP ON L/H HORIZ STAB MOVEABLE L/E FAIRING RIB#4 IAW B737 NDT P6 51-00-00 PROC.23; CRACK NOTED (CRACK LENGTH 0.250')<BR>TOOL USED : NORTEC 600 B/C 172389 CALDUE:SDR AALA202207068351Rib · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK FOUND ON LEFT HORIZONTAL STABILIZER RIB STIFFENER LOCATED AT STABILIZER STA 101.9 AND WATER LINE 0. INSTALLED RIB REINFORCEMENT REPAIR PER SRM 55-10-09-2R-4.SDR AALA202206206643Rib · crackedAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER RIB CRACKED, LOCATED AT STABILIZER STA 92.70, THIRD STIFFENER FROM THE FRONT SPAR. REPLACED RIB PER AARD 55-10-00-2 AND DRAWING 182A5301.SDR SWAA2022072517830Stiffener · crackedRIGHT HORIZONTAL STABILIZER INSPAR RIB ASSY. #5 (STAB STA 129.50); STIFFENER #3 CRACK NOTED. / [01] CUT AND REMOVED DAMAGE AT RT HORIZONTAL STABILIZER RIB #5 STIFFENER#3 AND PERFORMED SURFACE ROUGNESS OF 125 MICROINCHES RA OR BETTER TOOL USED ROUGNESS BLOCK B/SDR SWAA2022071117496Rib · crackedCRACK ON FRONT SPAR LOWER AREA OF INSPAR RIB STAB STA 129.50 AT LT HORIZONTAL STABILIZER 2022-307381 / [01] TOOL USED: ULTRASONIC THICKNESS GAGE; P/N:38DL PLUS; S/N:120398603; CAL DUE DATE: 18-OCT-22;[02] REPAIRED IAW EA# 22-155-01950; AND EA# 22-155-01950-WIPSDR SWAA2022070117352Rib · crackedR/H HORIZONTAL STABILIZER L/E FRONT SPAR INTERNAL RIB # 4 CRACKED AT LOWER FLANGE FWD INB END / [01] REMOVED DAMAGE AREA FROM LOWER CHORD OF RIB #4 AS REF. B737-700 SRM 55-10-09-2R-5.;[08] FABRICATED REPAIR ANGLE AS REF. B737-700 SRM 55-10-09-2R-5 FIG 205 DETASDR SWAA2022070116742Rib · crackedLH HORIZONTAL STAB L/E ACCESS PANEL #5 RIB CRACK. / [01] REMOVED # 5 RIB CRACKED AT L/H HORIZONTAL STAB.AS PER B-737-700 SRM# 51-40-02-OG-0;[02] LOCATED AND DRILLED NEW RIB #5 L/E HORIZ. STAB.AS PER B-737-700 SRM # 51-10-02-OG-0;[03] VERIFIED STEPS #1 AND #2.;SDR SWAA2022070116113Stiffener · crackedR/H HORIZONTAL STAB. FRONT SPAR INTERNAL RIB 4 ;STEFFINER # 2 CRACKED @ LOWER RADIUS / [01] CUT OUT CRACKED AREAS AT LOWER VERTICAL STIFFNER; WEB OF THE RIB AND LOWER I/B FLANGE PER B737-700 SRM 55-10-09-2R-5 FIG.204 DETAIL 'A';[02] VERIFIED CRACKS REMOVAL (3ESDR SWAA2022070116114Stiffener · crackedR/H HORIZONTAL STAB. FRONT SPAR INTERNAL RIB 4 ;STEFFINER # 3 CRACKED @ LOWER RADIUS / [01] REMOVED DAMGAE AREA AT #4 RIB STEFFINER #3 AS REF. B737-700 SRM 55-10-09-2R-4;[02] VERIFIED STEP #1;[03] PERFORMED HFEC INSP ON REWORKED AREA IAW B737 NDT P6 51-00-00 PSDR SWAA2022070116115Stiffener · crackedR/H HORIZONTAL STAB. FRONT SPAR INTERNAL RIB 4 ;STEFFINER # 4 CRACKED @ LOWER RADIUS / [01] REMOVED DAMGAE AREA AT #4 RIB STEFFINER #4 AS REF. B737-700 SRM 55-10-09-2R-4;[02] VERIFIED STEP #1;[03] PERFORMED HFEC INSP ON REWORKED AREA IAW B737 NDT P6 51-00-00 PSDR SWAA2022071115500Rib · crackedCRACK INSPAR RIB 129.50 AT 16.5 INCHES FROM FRONT SPAR AT LT HORIZONTAL STABILIZER 2022-307287 / [01] EQUIPMENT P/N PHASEC 3D; S/N CZ1026/09; DUE DATE 08-SEP-22 WAS USED;[02] PERFORMED REPAIR ON INSPAR RIB 129.50 AT 16.5 INCHES FROM FRONT SPAR AT LT HORIZONTALSDR SWAA2022071115501Rib · crackedCRACK INSPAR RIB 129.50 AT 25 INCHES FROM FRONT SPAR AT LT HORIZONTAL STABILIZER 2022-307288 / [01] EQUIPMENT P/N PHASEC 3D; S/N CZ1026/09; DUE DATE 08-SEP-22 WAS USED;[02] PERFORMED REPAIR ON INSPAR RIB 129.50 AT 25 INCHES FROM FRONT SPAR AT LT HORIZONTAL STASDR SWAA2022071115504Rib · crackedCUSTOMER REQUEST CRACK INTERNAL CAVITY ON UPPER STRINGER U13 LOCATED BETWEEN INSPAR RIB 24 AND 25 FUEL TANK AT RT WING 2022-307306 / [01] REPAIRED RH WING - UPPER STRINGER LOCATED BTW RIB 24 & RIB 25 AT U-13 IAW EA# 22-157-01834-WIP1; EA# 22-157-01834-WIP2 ANDSDR DALA2022060804007Hinge · crackedR/H HORIZONTAL STAB. #2 ELEVATOR HINGE RIB CRACKED.SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0259:2090-2039-RH/ 001 00019 REPAIRED PER PRI 599786-14, REV. 3 AND ERA 599786-14, REV. ORIGINAL. (LP# 2264276)SDR DALA2022060804006Rib · crackedR/H HORIZONTAL STAB. #3 ELEVATOR HINGE RIB CRACKED. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0259:2090-2039-RH/ 003 00021 REPAIRED W/REF. TO PRI 599778-14, REV. 0 AND ERA 599778-14, REV. ORIGINAL. (LP# 2264257)SDR DALA2022060804005Rib · crackedR/H HORIZONTAL STABILIZER, TRAILING EDGE COIL RIB CRACKED. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0259:2090-2039-RH/ 005 00082 REPAIRED PER PRI 599790-14, REV. 0 AND ERA 599790-14, REV. ORIGINAL. (LP# 2264301)SDR JR2R20220602571Rib · crackedLH HORIZONTAL STAB RIB #12 CRACKEDSDR AALA202206063084Rib · crackedAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER RIB CRACKED AT SECOND STIFFENER FROM AFT SPAR, LOCATED AT STABILIZER STA 92.70. REPAIRED RIB PER SRM 55-10-09-2R-4.SDR AALA202206027473Rib · crackedAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER INSPAR RIB 1 CRACKED, LOCATED AT STABILIZER STA 101.90. REPAIRED RIB PER SRM 55-10-09-2R PROCEDURE 4 REPAIR 4.SDR SWAA2022070112950Skin · crackedCRACK INDICATION FOUND ON RH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 17.500 INCH FROM FRONT SPAR; INBD SIDE OF RIB. CRACK LENGTH IS 1.125 INCH 2022-287601 / [01] TOOL USED EDDY CURRENT EQUIPMENT PN. NORTEC 600D; SN. 60009161631; DUE DATSDR AALA202206030740Rib · damagedAIRCRAFT WAS NOT GROUNDED: LEFT HORIZONTAL STABILIZER INTERNAL RIB HAS TOOLING MARKS AT APPROXIMATELY STAB STA 129. 6 INCHES AFT OF FRONT SPAR. REMOVED DAMAGE AND ADDED DOUBLER REPAIR PER EA 336294.SDR SWAA2022070111348Rib · crackedCRACK LEADING EDGE RIB LOCATED AT LE STA 78.29 AT LT HORIZONTAL STABILIZER 2022-266012 / [01] REPLACED RIB AND FASTENERS LEADING EDGE LOCATED AT LE STA 78.29 AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02 AND B737-700 DWG 186A1001 SHEET 10 REV A; SEE IN
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