JASC 5342
Service difficulty reports · 578
Reports filed under 5342 · Fuselage, Stabilizer Attach Fittings, 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 = '5342' 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 = '5342' 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 SWIA202503171229Drag Angle · crackedRH FWD VERTICAL STAB. DRAG ANGLE HAS SUSPECTED CRACK. (C-CHECK RO 3/14/2025) REPAIRED RH FWD VERTICAL STAB DRAG ANGLE IAW MHI RJ R.E.O. 670-55-31-187 REV. -- DATED 2025-02-18 AND COMPLIED WITH TASK CARD 51-900-1002-SKYSDR SWI2025F00334Drag Angle · crackedLH AFT VERTICAL STAB. DRAG ANGLE HAS SUSPECTED CRACK. (C-CHECK RO 3/14/2025) REPAIRED IAW REO 670-55-31-018 REV-A DATE 2016-11-10 AND COMPLIED WITH TASK CARD 51-900-1002-SKYSDR VNAA202409240008Angle · crackedCRACK ON LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE PREVIOUS REPAIR BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM. PREVIOUS REPAIR ON LH VERTICAL AFT DRAG ANGLE WAS REPLACED PER CRJ 900 SRM 55-31-00-201-001-A01SDR VNAA202409240007Angle · crackedCRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM. RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE WAS REPAIRED PER CRJ 900 SRM 55-31-00-201-001-A01SDR VNA20240531001Drag Angle · crackedNITIAL INSPECTION': CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). (SM) RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5%SDR VNA20240531003Drag Angle · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). (SM) CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DSDR SWAA2024052073719Fitting · corrodedCORROSION ON LOWER LUG FITTING LOCATED AFT FACE POSITION RT HORIZONTAL STABILIZER 2024-253371<[01] REPAIRED LOWER LUG REAR SPAR RH HORIZONTAL STABILIZER IAW EA 24-155-00979 WIP 1 TTG8Q00T0Q6J ; EA 24-155-00979 WIP 2 TTG8Q00T0TDD; EA 24-155-00979 WIP 3 TTG8Q00TSDR HNAA2024051400386Angle · corrodedE031084 LH VERTICAL STAB TO FUSELAGE ANGLE HAS POSSIBLE CRACK TOWARDS THE FWD END. RAR CRACKED LH VERTICAL STAB TO FUSELAGE ANGLE AND REPAIR ANGLE DOUBLER INCORPORATED WITH ANGLE IAW EMB 145 SRM 51-40-02SDR SWI202405080361Drag Angle · crackedR/H VERTICAL STAB TO FUSELAGE ATTACHMENT DRAG ANGLE AFT POSSIBLE CRACK. (MARKED) (C-CHECK RO 5/6/2024) COMPLIED WITH ALL STEPS OF REPAIR TO RH VERTICAL TO FUSELAGE AFT DRAG ANGLE AND INSTALLED ALL FABRICATED REPAIR PARTS -6 R/H AFT ANGLE DOUBLER AND -8 R/HSDR SWAA2024031453527Angle · crackedCRACK ANGLE FRONT SPAR LOCATED BS 1016 AT VERTICAL STABILIZER 2024-123384<[01] REPLACED ANGLE AND FASTENERS LOCATED FRONT SPAR BSTA 1016 AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02. SRM 51-10-02 PARAGRAPH 9. AND DWG# 173A3001. SHEET 23. REV. ?D?. SEE INDISDR AALA202403066471Lug · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND HORIZONTAL STABILIZER REAR SPAR LOWER LUG AT BS 1130, RBL 20. BLENDED LUG PER EA 353168.SDR YENA2023101101232Unknown · unknownCRACK INDICATION ON FRAME 68 LH, DOOR STOP 4, LOWER INB HOLE AT AFT GA LLEY AREA (1 EA) (CRACK DIRECTION AT 5 O CLOCK.D= 0.130); (RESOLVED ON W/O: 1242939 TASKCARD: NR-00026) FUR-A320-53-00896 REF AEROMAN N/R 2023- 482975, PERFORMED PERMANENT REPAIR ON FRAME 6SDR JTAA20230803003Fitting · crackedDURING A 1Y, 2Y, 4Y CPCP INSPECTION OF THE EMPENNAGE OF S/N 289 IT WAS FOUND 6 OUT OF 8 OF THE HORIZONTAL STABILIZER FITTINGS CRACKED. THE CRACKS WERE FOUND IN THE RADIUS OF ONE OF THE FITTINGS & FROM FASTNER TO FASTNER ON OTHERS.SDR SWIA2023050100014Unknown · unknownUPON REMOVAL ON THE RIGHT STAB TIP FOUND HOLE THE FLANGE UPPER SIDE WHERE THE NUTPLATE WAS. (C-CHECK RO 4/26/2023) REMOVED AND INSTALLED NEW SPLICE P/N 600-23037-22. REF: DWG 600-23037, REV: L, DWG 600-23026, REV: T, CRJ200 SRM 51-42-06, CRJ200 SRM 51-SDR HYIA20230321003Hinge · out of limitsDURING SCHEDULED INSPECTION, EXCESSIVE RADIAL END PLAY WAS NOTED IN THE AFT ATTACH BEARINGS (HINGE ASSY.) FOR THE HORIZONTAL STABILIZER PN: 212-55-10-1006-000. THESE ATTACH BEARING ASSEMBLIES WILL BE REMOVED AND REPLACED USING NEW PARTS.SDR SWAA2023032004103Angle · crackedAFT CARGO STA. 867; LAV POST ANGLE CRACKED.<[01] R&R?D ANGLE IAW SRM 51-40-02.SDR HYIA20230321002Hinge · wornDURING SCHEDULED INSPECTION, EXCESSIVE RADIAL END PLAY WAS NOTED IN THE AFT ATTACH BEARINGS (HINGE ASSY.) FOR THE HORIZONTAL STABILIZER PN: 212-55-10-1006-000. THESE ATTACH BEARING ASSEMBLIES WILL BE REMOVED AND REPLACED USING NEW PARTS.SDR CALA2022112503214Cover Plate · corrodedCORROSION ON TORSION BOX COVER SHEET. AS NOTED ON LTPR NR# 5001183828-0010. PERFORMED REPLACEMENT OF TORSION BOX COVER SHEET PER SRM 51-72-11-911-001 REV.142.SDR CALA2022112503213Threshold · corrodedCORROSION ON AFT CARGO DOOR THRESHOLD SHEET.AS NOTED ON LTPR NR# 5001183828-0010. PERFORMED REPLACEMENT OF THRESHOLD SHEET AS PER SRM 51-72-11-911 -001 REV.142.SDR YENA2022111001102None · noneDURING HEAVY MAINTENANCE: CRACK INDICATION ON EMERGENCY EXIT DOOR 844 INSIDE INNER FRAME SEGMENT FORWARD POSITIONS. THE LONGEST CRACK IS 2.23 INCHES APPROX. PASSENGER CABIN; REF AEROMAN W/O 2022-283/1 NR 2022-557954. PERFORMED PERMANENT REPAIR ON EMERGENCY ESDR YENA2022110101078None · noneDURING HEAVY MAINTENANCE: CORROSION ON LONGITUDINAL BEAM BTW FR 87/85 AND Y=-300; REF TOMX WO 2047-NR 00230; REMOVED AND REPLACED LONGITUDINAL BEAM BTW FR 85/86 PER SRM 51-41-01 AND SRM 51-43-03.SDR YENA2022110101068None · noneDURING HEAVY MAINTENANCE: CORROSION ON TRANSVERSAL BEAM BTW FR 84 AND Y=+300/1200; REF TOMX WO 2047 NR 00233. REMOVED AND REPLACED TRANSVERSAL BEAM REF SRM 51-41-01, 51-42-01, AND 51-43-01.SDR YENA2022110101067None · noneDURING HEAVY MAINTENANCE: CORROSION ON TRANSVERSAL BEAM BTW FR 84 AND Y=+300/1200; REF TOMX WO 2047 NR 00233. REMOVED AND REPLACED TRANSVERSAL BEAM REF SRM 51-41-01, 51-42-01, AND 51-43-01.SDR YENA2022092700974None · noneDURING HEAVY MAINTENANCE: REF. AEROMAN N/R 2022-486863 - CRACK INDICATION ON FRAME 35 PRESSURE BULKHEAD LH SIDE FROM FASTENER L OWER OUTBOARD COMMON TO MILLED COUPLING, CRACK DIRECTIONS ARE 3 AND 9 O'CLOCK, CRACK LENGTH IS 0.500 INCHES APPROX, IN FWD CARGO COMSDR YENA2022091300916None · noneDURING HEAVY MAINTENANCE: CORROSION ON REPAIRED DOUBLER BTW FR84 AND FR85 Y=350 AT W2; REF TOMX WO 1974 N/R00189
THE DAMAGED DOUBLER REPAIR LOCATED BETWEEN FR84 AND FR85 Y=350R AT W2 WAS REPLACED WITH A NEW DOUBLER REPAIR PER EMB-190 SRM 51-43-04 AND SRM 53-2SDR YENA2022091300894None · noneFLT#1578, DTW-BOS. (AIRCRAFT DECLARED AN EMERGENCY INTO BOS) ' REMOVED PANEL 481CL,485AL,485BL,481DR & 485AR FOR MX HYD Y RSVR LOW ITEM 1: HYD Y RSVR LOW LVL ECAM IN FLIGHT; SEE WO# 12001476 AND NON-ROUTINE #00003 AND NR00004 FOR CORRECTIVE ACTION. REMOVED ANDSDR CALA2022090502266None · corrodedSTRINGER RH 41 FR 61-63 CORRODED, REQUIRES FURTHER EVALUATION. AS NOTED ON LTPR NR# 5001170029-0010. CORRODED STRINGER AND SECTION-CONNECTING BTW FR.61-63, STGR.41RH INSPECTED BY HT1218. PERFORMED REPLACEMENT AS PER A319 SRM 51-42-11 AND SRM 51-72-11 REV.142. SDR CALA2022080801985None · corrodedAFT CRG THRESSHOLD CORRODED, REQUIRES FURTHER EVALUATION. A3NB-05-3-6022. SEQ#9 ZONE #153. AS NOTED ON LTPR NR# 5001170024-0010.SDR YENA2022080800755Floor Splice · corrodedDURING HEAVY MAINTENANCE: INITIAL INSPECTION: "CPCP FINDING": CORROSION ON AFT CARGO INTERNAL STRUCTURE SHEARCLIP BTW FR 76 AND STGR 28RH/29RH; SUMMARY OF NRC 00272: CORROSION ON AFT CARGO INTERNAL STRUCTURE SHEARCLIP BTW FR 76 AND STGR 28RH/29RH WAS REMOVED ASDR YENA2022060200545Floorbeam · corrodedDURING HEAVY MAINTENANCE, CORROSION FLOORBEAM AND Y765 LOC BTW FR 41 AND FR47 IN PASSENGER CABIN; REF AEROMAN WO# 2022-5/1, NR 2022-1555841. REMOVED AND REPLACED FLOORBEAM Y765, SPLICE (1E/A), AND FASTENERS LOC BTW FR 41 TO FR 47 AT LEVEL STRG 23L IAW A320 SRMSDR YENA2022051700483None · noneDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 43 RH SIDE, UPPER OPEN FASTENER HOLE SIDE BOX BEAM FLANGE IN PASSENGER CABIN; REF AEROMAN N/R 2022-234656, PERFORMED SERVICE BULLETIN A320-53-1258, LOCATED FUSELAGE / TORSION BOX / LOWER SIDE SHELL / FRAME 43SDR YENA2022051700482None · noneDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 43 RH SIDE, MIDDLE OPEN FASTENER HOLE SIDE B OX BEAM FLANGE IN PASSENGER CABIN; REF AEROMAN N/R 2022-234655, PERFORMED SERVICE BULLETIN A320-53-1258, LOCATED FUSELAGE / TORSION BOX / LOWER SIDE SHELL / FRAME SDR YENA2022051700481None · noneDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 43 LH SIDE, MIDDLE OPEN FASTENER HOLE SIDE BOX BEAM FLANGE IN PASSENGER CABIN; REF AEROMAN N/R 2022-237654, PERFORMED SERVICE BULLETIN A320-53-1258, LOCATED FUSELAGE / TORSION BOX / LOWER SIDE SHELL / FRAME 4SDR CALA2022051601244Skin · crackedB767-53-3-7018 RH HORI STAB LOWER FAIRING QATTACH SKIN FOUND CRACK AT BS 1809-1820 , TRANSFER TO HX NRC WO 738612 AND ORIGINATED BY V896832 R/H HORI STAB LOWER FAIRING ATTACH SKIN AT BS1809-1820 BETWEEN STA 12AR TO STR 22R SKIN REPAIRED AS PER EC/RA 5381-01018SDR YENA2022050500444None · noneDURING HEAVY MAINTENANCE: A CRACK INDICATION WAS FOUND INSIDE OF THE INNER EMERGENCY EXIT HATCH FRAME SEGMENT (1) OF THE FWD RH SIDE DOOR 843; REF AEROMAN WO # 2022 71/1, NR 2022-205389; PERFORMED FRAME / RE-ENFORCE DOOR STRUCTURE MODIFICATION ON EEH DOOR 843SDR YENA2022050500443None · noneDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND INSIDE OF THE INNER EEH FRAME SEGMENT (), OF THE AFT LH SIDE DOOR 834 AT AFT AND FWD SIDE POSITION; REF AEROMAN WO 2022 71/1, NR 2022-205390, PERFORMED FRAME / REINFORCEMENT DOOR STRUCTURE MODIFICATION ON EEH DOSDR YENA2022050500442Nonskid · noneDURING HEAVY MAINTENANCE: A CRACK INDICATION WAS FOUND INSIDE OF THE INNER EEH FRAME SEGMENT (1), OF THE FWD LH SIDE DOOR 833 AT AFT SIDE POSITION; REF AEROMAN WO 2022 71/1, NR 2022-205388; PERFORMED FRAMED FRAME / REINFORCEMENT DOOR STRUCTURE MODIFICATION ON SDR GTIA2022032436335Panel · corrodedCORROSION FOUND ON AFT RH THRESHOLD PANEL 262LG. RAF 2782398-2 OPENED. REF LTPR 5001141315-0060-REVIEWED NR# 5001141315-0060, 5001141315-0040 AND TC# 1003673443-0010. REPAIR HAS BEEN PERFORMED ON 262LG I.A.W SPIRIT EO 5342-2208 REV. 01. SDR CREATEDSDR CALA2022022200488Panel · missingPDA 3 DURING WALK AROUND FOUND PANEL ON LOWER O/B TRAILING EDGE OF L/H HORIZ. STAB MISSING. PANEL IS APROX 4.75 X 6.75 INCHEC. WEIGHING APROX. O.2 LBS. REPLACED MISSING PANEL PER ECRA 2741-01293SDR YENA2022031500201Shear Tie · corrodedDURING HEAVY MAINTENANCE, CORROSION ON INTERNAL STRUCTURE SHEAR CLIP AT WASTE CUT OUT FR88 BTW STGR 25R/28R, CENTER FUSELAGE III; CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 51-12-01, REMOVED AND REPLACED SHEAR CLIP IAW SRM 51-41-02. REFERENCE TECHOPSMX NR 000SDR YENA2022031500199Hinge Fitting · wornDURING HEAVY MAINTENANCE, (E/C E22-044-01) FUSELAGE / REAR FUSELAGE / H. STABILIZER HINGE / FR 100 / LH FITTING
/ WEAR - TEMPORARY REPAIR (CLASSIFIED AS A MAJOR REPAIR)SDR YENA2022031500198Hinge Fitting · misalignedDURING HEAVY MAINTENANCE, (E/C E22-045-01) FUSELAGE / REAR FUSELAGE / H. STABILIZER HINGE / FR 100 / RH FITTING
/ MISALIGNMENT - TEMPORARY REPAIR (CLASSIFIED AS A MAJOR REPAIR)SDR A6WA202101178071Strap · corrodedCORROSION ON PRESSURE FLOOR STRAP PN 601R31025-29 LOCATED AT FS559.00 AND RBL30 TO RBL44 PRESSURE FLOOR STRUCTURE. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED PRESSURE FLOOR STRAP PN 601R31025-29 LOCATED AT FS559.00 AND RBL30 TO RBL44 WITH A NSDR SWAA2022010347687Angle · crackedCRACK ANGLE LOCATED AT BS 1016 BETWEEN STRINGER 2L AND STRINGER 2R UPPER FUSELAGE AT VERTICAL STABILIZER ; 2021-544333 / [01] TOOL USED DIGITAL CALIPER P/N: DIGITAL 150 S/N: AE-412601; DUE DATE: 31-MAY-22; [02] REPLACED ANGLE LOC. AT BS 1016 BETWEEN STRINGER 2SDR A6WA202111297989Angle · corrodedCORROSION COMMON TO PRESSURE FLOOR ANGLE AT FS 513.00 TO FS 513.00+4 AND LBL 40 TO LBL 43. ****************AIRCRAFT REMOVED FROM SERVICE************************** BLENDED 2 EACH AREAS: FS 513.00 AT LBL 41 (P1) 1.20"L X .800"W X .004"D; FS 513.00+4 AT LBL 43 SDR SWAA2022011045658Fitting · corrodedVERTICAL STAB FRONT SPAR LEFT FWD FUSELAGE FITTING FWD SURFACE HAS LIGHT PITTING ON SURFACE. ; / [01] PERFORMED PENETRANT INSPECTION ON VERTICAL STAB.FRONT SPAR LEFT FWD FUSELAGE FITTING FWD.SURFACE IAW SOPM 20-20-02. NO CRACKS.; [02] PERFORMED HFEC ROTO ON VESDR SWAA2022011045434Fitting · corrodedVERTICAL STAB FRONT SPAR RIGHT FWD FUSELAGE FITTING FWD SURFACE HAS LIGHT PITTING ON SURFACE. ; / [01] PERFORMED PENETRANT INSPECTION ON VERTICAL STAB.FRONT SPAR RIGHT FWD FUSELAGE FITTING FWD.SURFACE IAW SOPM 20-20-02. NO CRACKS.; [02] PERFORMED HFEC ROTO ON SDR SWAA2022011045661Fitting · corrodedVERTICAL STAB FRONT SPAR LEFT FWD FUSELAGE FITTING BORE HAS PITTING ; / [01] REMOVED CORROSION AT VERTICAL STAB. FUSELAGE FRONT SPAR LH SIDE LUG BORE ; REAM FITTING HOLE FWD 1.2040'' AND AFT 1.1197'' AS PER B737 SRM -51-10-02-0G-0; [02] CORRECTION FOR STEP 1 <SDR SWAA2022011045662Fitting · corrodedVERTICAL STAB FRONT SPAR RIGHT FWD FUSELAGE FITTING BORE HAS PITTING ; / [01] REMOVED CORROSION AT VERTICAL STAB. FUSELAGE FRONT SPAR RH SIDE LUG BORE ; REAM HOLE FITTING FWD 1.1195'' AS PER B737 SRM 51-10-02-0G-0.; [02] VERIFIED 1.; [03] NEW BUSHING WAS FABRISDR YENA2021111200765Skin · gougedDURING HEAVY MAINTENANCE, WEIGHT VARIANT UPGRADE FOR A/C N635JB- SRM REPAIR SURVEY - FUSELAGE - GOUGE, 1.1 INCH AFT OF FR 34 AND 1.8 INCH LEFT OF STR 44 ; REF AEROMAN N/R 2021-4548703 WO# 2021 367/1 PERFORMED PERMANENT REPAIR LOC FUSELAGE LOC FUSELAGE 1.1 INCH
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