JASC 5553
Service difficulty reports · 586
Reports filed under 5553 · Vertical 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 = '5553' 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 = '5553' 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 VNAA20250715043Drag Angle · crackedCRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUM. CRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DASDR DALA2024092309309Flap Track · corrodedSHIP 3148 RH WING INB'D FLAP TRACK #2 / ATTCHT BEARING AT RIB 9 CORROSION. CORRECTIVE ACTION: REPAIRED PER ER/A 620272-14. (0568620)SDR SWAA2024031554034Fitting · corrodedCORROSION ON FWD AND AFT FACE OF FITTING FDW VERTICAL BST 1016 RBBL 11.55 2024-124241, PERFORMED REPAIR LOCATED FWD AND AFT FACE OF FITTING FDW VERTICAL BST 1016 RBBL 11.55 IAW B737-700 EA 24-153-00515. CORRECTED STEP 4. PERFORMED REPAIR LOCATED FWD AND AFSDR VNAA202403010005Drag 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). AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) WAS REPAIRED PER CRJ900 SRM 55-31-00SDR VNAA202403010004Drag Angle · crackedCRACK 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) AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) WAS REPAIRED PER SRM 55-31-00-201-001SDR SWI2024F00056Drag Angle · cracked*SUSPECTED CRACK AT R/H VERTICAL TO FUSELAGE AFT DRAG ANGLE (MARKED), (C-CHECK RO 1/30/2024) REPAIRED R/H VERTICAL TO FUSELAGE AFT DRAG ANGLE REF CRJ-700-SRM 55-31-00-201-001-A01. COMPLIED WITH 51-900-1002-SKY AND SEE CONTINUATION CARD FOR DETAILSSDR SWI2024F00055Drag Angle · cracked*AFT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE IS CRACKED AT L/H SIDE (MARKED) (C-CHECK RO 1/30/2024) REMOVED AFT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE REF CRJ 700 SRM 51-42-10-001-001-A01 AND SRM 51-42-21-001-001-A01 AND INSTALLED NEW AFT VERTICAL SSDR SWIA202401301028Drag Angle · cracked*FWD VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE IS CRACKED AT L/H SIDE (MARKED) (C-CHECK RO 1/30/2024) REMOVED FWD VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE AND INSTALLED NEWLY FABRICATED FWD DRAG ANGLE, FILLER, AND DOUBLER ON LH SIDE REF CRJ700 SRM 55-31SDR SWI2023F00473Unknown · crackedVERTICAL STABILIZER TO FUSELAGE ATTACHMENT RH AFT DRAG ANGLE POSSIBLE CRACK (C-CHECK RO 11/10/2023) REMOVED, FABRICATED AND REPLACED WITH NEW RH AFT DRAG ANGLE AT FUSELAGE TO VERT STAB ATTACHMENT REF REO 670-55-31-018 REV -A DATED 2016-11-10. COMPLIED WITHSDR SWIA202311070905Unknown · crackedVERTICAL STABILIZER TO FUSELAGE ATTACHMENT LH FORWARD DRAG ANGLE DOUBLER POSSIBLE CRACK (C-CHECK RO 11/10/2023) REMOVED, FABRICATED AND REPLACED WITH NEW LH FWD DRAG ANGLE AT FUSELAGE TO VERT STAB ATTACHMENT REF CRJ700 SRM 55-31-00-201-001-A01 AND ALL STEPSDR AALA202308154399Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON VERTICAL STABILIZER RIGHT HAND FAILSAFE FITTING LOCATED AT BS 1088, S2R. REPLACED FITTING PER SRM 51-40-02.SDR AALA202308157476Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON VERTICAL STABILIZER RIGHT HAND AFT FAILSAFE FITTING LOCATED AT BS 1088, S2R. REPLACED FITTING PER SRM 51-40-02.SDR FDEA202210062486Fitting · damagedTO CARRY OUT BANJO FORWARD AND AFT FITTING HIGH FREQUENCY EDDY CURRENT SURFACE INSPECTION AT STATION 2164. REPAIR CARRIED OUT ALONG STATION 2164 RIGHT HAND BANJO FITTING FORWARD AND AFT FLANGE AREA IAW EA 1-5530-T0313159 B P4. REPAIR CLASSIFIED AS MAJOR ISDR FDEA202210062485Fitting · crackedWHILE ACCOMPLISHING LEFT HAND BANJO FORWARD FITTING INSPECTION, FOUND LEFT HAND BANJO AFT FITTING SUSPECTED CRACK AT STATION 2164. LEFT HAND BANJO FITTING FORWARD AND AFT FLANGE AREA REPAIR CARRIED OUT PER E.A #: 1-5530-T0313159 B P4. REPAIR CLASSIFIED ASDR DALA2022041102515None · noneSHIP 3101 - CRACK SUPPORT VERTICAL WEB LOCATED BETWEEN HINGE 5 TO HINGE 6 ON VERTICAL STABILIZER. CORRECTIVE ACTION: REPAIR VERTICAL WEB LOCATED BETWEEN HINGE 5 TO HINGE 6 AS PER ER/A 598239-14.(2188943)SDR HNAA2022052500187None · noneE912345 - VERTICAL STAB TO FUSELAGE LH DRAG ANGLE IS CRACKED AT FWD END .... RAR LH VERTICAL STAB TO FUSELAGE DRAG ANGLE FWD SECTION IAW EMB 145 SRM 51-40-02SDR DALA2022012400475None · noneSHIP 3267 VERTICAL STABILIZER HINGE FITTING #4 CORRODED. CORRECTIVE ACTION: REPLACED HINGE FITTING #4 AND FASTENERS PER A320 SRM 55-36-42. (2095237)SDR DALA2022012400474None · noneSHIP 3267 VERTICAL STABILIZER HINGE FITTING #2 CORRODED. CORRECTIVE ACTION: REPLACED HINGE #2 AND FASTENERS PER A320 SRM 55-36-42. (2095233)SDR DALA2022012400473None · noneSHIP 3267 VERTICAL STABILIZER HINGE FITTING #7 CORRODED. CORRECTIVE ACTION: REPLACED HINGE FITTING PER SRM A320 55-36-42. (2095222)SDR DALA2022012400472None · noneSHIP 3267 VERTICAL STABILIZER HINGE FITTING #5 CORRODED. CORRECTIVE ACTION: REPLACED FITTING PER A320 SRM 55-36-42. (2095217)SDR DALA2022012400471None · noneSHIP 3267 VERTICAL STABILIZER HINGE FITTING #3 CORRODED. CORRECTIVE ACTION: REPLACED FITTING PER A320 SRM 55-36-42. (2095211)SDR DALA2022012400476None · noneSHIP 3267 HINGE FITTING NUMBER 1 VERTICAL STABILIZER CORRODED. CORRECTIVE ACTION: REPLACED HINGE FITTING PER A320 SRM 55-36-42. (2094068)SDR SWAA2022010658653Fitting · corrodedCORROSION FITTING ON DRAG BRACE OUTBOARD FWD LOCATED AFT REAR SPAR RT SIDE AT VERTICAL STABILIZER. REPLACED THE FITTING AND FASTENERS ON DRAG BRACE IAW SRM 51-40-02 & DWG 148A8200 REV A.SDR SWIA202164581None · cracked* VERTICAL STABILIZER R/H DRAG ANGLE CRACKED AT APPROX. VERTICAL STABILIZER REAR SPAR DATUM 67.5%. (C-CHECK RO 2/22/2022) CUT AWAY CRACKED FWD AND AFT VERTICAL STAB DRAG ANGLES AND INSTALLED REPAIR DOUBLERS AND FILLERS ON R/H SIDE OF VERTICAL STAB. REF:SDR SWIA202164580None · cracked* VERTICAL STABILIZER L/H DRAG ANGLE CRACKED AT APPROX. VERTICAL STABILIZER REAR SPAR DATUM 67.5%. (C-CHECK RO 2/22/2022) CUT AWAY CRACKED FWD AND AFT VERTICAL STAB DRAG ANGLES AND INSTALLED REPAIR DOUBLERS AND FILLERS ON L/H SIDE OF VERTICAL STAB. REF:SDR MASA20211101488Visor · damagedRH LOWER VISOR OF THE VERTICAL TO HORIZONTAL STABILIZER WAS FOUND WITH MULTIPLE ELONGATED HOLES AFFECTING THE INNER PANEL AND BLOCK. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 55-32-86-001-001-A02, FIGURE 55-32-86-991-808, ITEM 136, 128, AND 153, EA 48-202SDR DATA20210921001Fitting · corrodedWHILE PERFORMING AN INSPECTION OF THE VERTICAL STABILIZER ATTACH FITTING PER AD 2005-13-31 AND SERVICE BULLETIN SD360-53-45, FOUND CORROSION ON SHEAR ATTACHMENT FITTING P/N SD3-12-6978. FITTING WAS REMOVED AND REPLACED WITH NEW FITTING IAW SB SD360-53-45 AND ASDR SWAA2021091607868Fitting · corrodedLH O/B REAR SPAR FITTING OF VERTICAL STABILIZER(FTG-LH FWD MAIN)HAS PITTING CORROSION. ; / [01] REMOVED LH O/B REAR SPAR FITTING OF VERTICAL STABILIZER - LH FWD MAIN IN IAW SRM 51-40-02-0G-0; [02] VERIFIED 1. OK TO LOCATE AND DRILL NEW FITTING.; [03] PARTIALLYSDR SWAA2021092107654Angle · chafedVERTICAL STAB. FUSELAGE FIN TO BODY INTERFACE CLOSURE ANGLES HAVE CHAFED ; WEAR MARKS ; / [01] ORIGINAL MAT THICKNESS 0.063' MINIMUM MAT FOUND 0.032' NO ALLOWABLE MAT LIMITS FOUND; [02] REMOVED 98% OF L/H SKATE ANGLE AS PER B737-700 SRM 51-40-02-0G-0; [03] REMSDR SWIA202161736None · excess playBOTH CENTER HINGE POINTS AND UPPER HINGE POINT BEARINGS ON THE RUDDER VERTICAL STAB TRAILING EDGE SIDE HAVE EXCESSIVE PLAY, ALL FLAGGED (C-CHECK RO 10/8/2021) REMOVED AND REPLACED WORN BEARINGS ON UPPER AND CENTER HINGE FITTINGS ON RUDDER R VERTICAL STASDR SWIA2021091060831Drag Angle · elongatedVERTICAL STAB RH SIDE HAS (3) ELONGATED HOLES ON LOWER BOTTOM UNDER AFT DRAG ANGLE. (C-CHECK RO 9/8/2021) VERTICAL STAB RH SIDE (3) ELONGATED HOLES ON LOWER BOTTOM UNDER AFT DRAG ANGLE REPAIRED PER MHIRJ REO 670-55-31-146 REV €“ DATE 2021-08-05. COMPLSDR SWIA2021091060877Drag Angle · cracked*VERTICAL STAB HAS A CRACKED DRAG ANGLE ON RH SIDE (MARKED) (C-CHECK RO 9/8/21) REPLACED CRACKED VERTICAL STAB DRAG ANGLE WITH NEW, REF BOMBARDIER DWG BA670-35002 REV -F, CRJ 700 SRM 51-42-13-001-001-A01, CRJ 700 SRM 51-42-21-001-001-A01 AND CRJ 700 SRM SDR SWIA2021091060876Drag Angle · cracked*VERTICAL STAB HAS A CRACKED DRAG ANGLE ON LH SIDE (MARKED) (C-CHECK RO 9/8/21) REMOVED CRACKED VERTICAL STAB LH SIDE DRAG ANGLE AND REPLACED WITH A SERVICEABLE UNIT (P/N: A670-21186-003) REF CRJ-700 SRM 51-42-21-001-001-A01, CRJ-700 SRM 51-42-13-001-001SDR SWAA2021080287364Attach Angle · crackedCRACK LEADING EDGE SUPPORT ANGLE AT LEVEL BS 1016 AT VERTICAL STABILIZER ; 2021-295416 / [01] REPLACED SUPPORT ANGLE AND FASTENERS LOC. AT LEVEL BS 1016 AT VERTICAL STABILIZER I.A.W B737-700 SRM 51-10-02; ITEM 9 AND DWG 176A3001; SHEET 20; REV -; [02] REPLACEDSDR SWIA2021081060201Drag Angle · cracked*RH SIDE VERTICAL/FUSELAGE AFT DRAG ANGLE IS CRACKED (C-CHECK RO 8/6/2021) REPLACED R/H AFT DRAG ANGLE AT THE VERTICAL/FUSELAGE ATTACHMENT AREA REF. CRJ 700 SRM 51-42-21-001-001-A01, 51-42-22-001-001-A01, 51-42-13-001-001-A01 DWG BA670-35002 REV F / C/WSDR SWIA2021081060200Drag Angle · cracked*RH SIDE VERTICAL/FUSELAGE FWD DRAG ANGLE IS CRACKED (C-CHECK RO 8/6/2021) REPAIRED THE R/H VERTICAL/FUSELAGE FWD DRAG ANGLE, CUT AWAY DAMAGE, FABRICATED AND INSTALLED ALL REPAIR PARTS, REF. CRJ 700 SRM 55-31-00-201-001-A01 AND CRJ 700 SRM 51-42-21-001-SDR SWIA2021081060199Drag Angle · cracked*LH SIDE VERTICAL/FUSELAGE AFT DRAG ANGLE IS CRACKED (C-CHECK RO 8/6/2021) REMOVED AND REPLACED NEW *LH SIDE VERTICAL/FUSELAGE AFT DRAG ANGLE REF CRJ700 SRM 51-42-13-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01, CRJ700 SRM 51-42-22-001-001-A01 AND DWG SDR SIMA20210526005Drag Angle · crackedVERTICAL STAB TO FUSELAGE RT SIDE DRAG ANGLE IS CRACKED IN 2 AREAS. (MAJOR REPAIR)-C/A-C/W VERTICAL STAB TO FISELAGE DRAG ANGLE REPAIR IAW ERS-EM-53MR-4355SDR SWAA2021061772822Angle · chafedRT FWD BS 1008 - 1016 FUSELAGE FIN TO BODY INTERFACE CLOSURE ANGLE HAS CHAFED AREAS. ; DOT 8-29 / CERTIFIED REMOVED AND REPLACED CLOSURE ANGLE AT RT FWD BS 1008 - 1016 FUSELAGE FIN TO BODY INTERFACE; FINAL INSPECTED.;INSPECTED AND CERTIFIED (STEPS #8; #9 AND #SDR SWAA2021061772821Angle · chafedLT FWD BS 1008 - 1016 FUSELAGE FIN TO BODY INTERFACE CLOSURE ANGLE HAS CHAFED AREAS. 8-28 ; / CERTIFIED (RII) STEPS #8; #9 AND #10 INSPECTED.;CERTIFIED LT CLOSURE ANGLE INSTALLATION AND 100% FASTENERS INSTALLATION BY SQUEEZE OUT TIME; INSPECTED.;FINAL INSPECTISDR HNAA2021051900206Drag Angle · crackedRH FUSELAGE TO VERTICAL STAB DRAG ANGLE IS CRACKED AT FWD FITTING AFT END. REMOVED AND REPLACED FWD RH FUSELAGE TO VERTICAL STABILIZER DRAG ANGLE IAW EMB 145 SRM 51-40-02.SDR DALA2021031001365Hinge · corrodedSHIP 3253 FOUND CORROSION ON BORE OF VERTICAL STABILIZER RUDDER HINGE. CORRECTIVE ACTION: REPLACED HINGE PER A320 SRM 55-36-42. (1750426)SDR REXA2021012200023Drag Angle · crackedVERTICAL STAB LT AFT DRAG ANGLE CRACKED. REMOVED ADN REPLACED LT AFT DRAG ANGLE P AV670-21186-003, IAW CRJ 900 SRM 51-42-13-001-001-A01, 51-42-21-001-001-A01, 51-42-22-001-001-A01, 51-40-11-001-001-A01 AND 51-42-20-001-001-A01.SDR SWIA202156262Drag Angle · crackedRH VERTICAL STAB TO FUSELAGE AFT DRAG ANGEL HAS A POSSIBLE CRACK (C-CHECK) RO 2/13/2021 REMOVED AND REPLACED RH AFT DRAG ANGLE ON VERTICAL STAB TO FUSELAGE REF CRJ 700 SRM 51-42-21-001-001-A01, SRM 51-42-22-001-001-A01 , SRM 51-42-13-001-001-A01 AND BOMBASDR SWIA202056242Attach Angle · gouged* THE VERTICAL STABILIZER'S LH AND RH FRONT SPAR TO FUSELAGE SPLICE STRAP RIB ATTACH ANGLES ARE GOUGED ON THEIR OUTBOARD SIDES. (MARKED WITH RED GREASE PENCIL) (C-CHECK) RO 2/9/2021 REMOVED GOUGED DAMAGE ON VERTICAL STAB FRONT SPAR TO FUSELAGE SPLICE STRAPSDR SCNA20201201373Skate Angle · wornRT AFT SKATE ANGLE IS WORN. ACCOMPLISHED BLEND REPAIR TO VERTICAL FIN CLOSURE ANGLE RT, BS 1032 TO BS 1104, PER ATS ER 20-03566 REV IR AND SCA EA 53-0068 REV 0.SDR SWIA202055346Drag Angle · crackedVERTICAL STAB TO FUSELAGE ATTCHMENT AFT DRAG ANGLE ON RT SIDE IS CRACKED. C-CHECK RO 1/6/2021. REMOVED AND REPLACED VERTICAL STAB TO FUSELAGE ATTACHMENT AFT DRAG ANGLE ON RT SIDE, IAW CRJ 700 SRM 51-42-13-001-001-A01, 51-42-21-001-001-A01 & 51-42-22-001-00SDR SWIA202055779Drag Angle · cracked*LH SIDE OF VERTICAL STAB TO FUSELAGE ATTACH AFT DRAG ANGLE POSSIBLE CRACK (MARKED) (C-CHECK) RO 2/1/2021 REPARIED LH SIDE OF VERTICAL STAB TO FUSELAGE ATTACH AFT DRAG ANGLE IAW CRJ 900 SRM 55-31-00-201-001-A01. COMPLIED WITH 51-900-1002-SKY.SDR SWIA202054268Doubler · corrodedVERTICAL STABILIZER MOUNT DOUBLER COMMON TO TAIL STINGER HAS CORRODED HARDWARE, MARKED. C-CHECK RO 11/21/2020. REPLACED WITH NEW BOLTS (2 EACH), NEW WASHERS (2 EACH) AND NEW NUTS (2 EACH) ON THE VERTICAL STAB MOUNT DOUBLER COMMON TO TAIL STINGER, REF CRJ-200SDR SWAA2020101319566Attach Angle · chafedUPPER FUSELAGE STA 1018, 1077, 1106 & 1124; RBL 13; FUSELAGE TO VERTICAL STAB SKATE ANGLE INBOARD SIDE CHAFE WEAR, MARKED. REMOVED AND REPLACED RT VERTICAL STAB SKATE ANGLE STA 1018 TO 1124 RBL 13, IAW SRM 51-40-02-0G-0 AND BOEING DWG 148A8300 REV. APPLIED T
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