JASC 5530

Service difficulty reports · 2,534

Reports filed under 5530 · Vertical Stabilizer, 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 = '5530'
  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.

SDR 2000ZZZX378Rudder Opening · contaminatedA LARGE AND VERY WELL HIDDEN BIRD'S NEST WAS FOUND IN RUDDER OPENING. FORWARD MIDWAY WHERE RUDDER TRIM COMES IN. EVERYTHING HAD SCREENS, BUT THE BIRDS FOUND A PLACE.Dec 30, 1999 · N5AY · Cessna 421SDR TWAA9917403Angle · crackedDURING CHECK-C MAINT, THE FUSELAGE TO VERTICAL STAB ATTACH ANGLE WAS CRACKED .875 INCH LONG AT RT SIDE, STA 1121. CRACK IS BEYOND STOP DRILLED HOLES OF LOWER LEG CRACK. REPAIRED PER SRM 53-05, FIG 230. DOUBLER INSTALLED.Dec 23, 1999 · N988Z · Doug DC931SDR DL72L992760Web · dentTHE NR 4 RIB OF THE VERTICAL STABILIZER HAS A DENT IN THE WEB THAT RESULTED IN A 1 INCH DIAMETER CUTOUT. THE DAMAGE WAS FOUND AT HMV AND REPAIRED PER ERA 333924-14.Dec 16, 1999 · N505DA · Boeing 727232SDR GAIA99234Tee · worn'NO FLIGHT', FOUND DURING 'HEAVY 2 MAINTENANCE CHECK' AT TIMCO HEAVY MAINTENANCE FACILITY (OSCODA MI). VERTICAL STABLIZER LEFT SIDE T-CHORD WORN AT PANEL NR 9601. REMOVED DAMAGE IAW ENGINEERING DEVIATION REQUEST (EDR B2-07298). PERFORMED HFEC IAW B 727 NDT Dec 14, 1999 · N6816 · Boeing 727223SDR 20000511AP026Web · crackedVERTICAL FIN LEADING EDGE PANEL 9602 INNER CURVED WEB HAS 1 INCH CRACK AT CORNER. STOP DRILLED CRACK IAW 51-10-1 PAGE 613. FABRICATED DOUBLER IAW 51-40-2 PAGE 2, 3, 6. TREATED AND PRIMED IAW 51-10-2 PAGE 1. INSTALLED DOUBLER AND WEB IAW 51-30-2 PAGE 1. (MDec 8, 1999 · N889MA · Boeing 727225SDR 20000511AP025Web · tornVERTICAL LEADING EDGE CENTER SECTION INTERIOR WEB IS DAMGED AT THREE CORNERS. CUT OUT DAMAGED AREAS IAWS 51-40-2 PAGES 2/3. HFEC SHOWS NO CRACKS IAW 51-00-00 PAR 6. TREATED AND PRIMED IAW 51-10-2 PAGE 1. INSTALLED REPAIR IAW 51-40-2. (M)Dec 8, 1999 · N889MA · Boeing 727225SDR CA991231004Angle · cracked(CAN) DURING INSPECTION CARRIED OUT IAW AD 64-21-04, CRACK WAS FOUND ON THE REINFORCEMENT ANGLE AT THE AFT END OF THE RIB AT W.L. 201.575Dec 1, 1999 · Frchld F27FSDR 99FDEA00497Fitting · crackedWHILE ACCOMPLISHING EO 1-5510-7-3304 PART 2 AT RT AFT MOST BOTTOM HOLE, WHILE REAMING TO CLEAR-OFF CRACK FOUND A SLEEVE BUSHING ON THE HOLE SKIN SIDE. (SLEEVE BUSHING HAD COME OUT DURING REAMING PROCESS). RT AFT MOST BOTTOM HOLE REPAIR CARRIED OUT AS PER FEDNov 26, 1999 · N582FE · Doug MD11FSDR 20000615AP004Bracket · crackedDURNIG C-CHECK, FOUND VERTICAL STABILIZER L/E PANEL 9503 LEFT AND RIGHT LOWER SECTION BRACKETS CRACKED. REMOVED BRACKETS, FABRICATED, TREATED AND INSTALLED PER SRM 51-30-3 APGE 14A. (M)Nov 14, 1999 · N802EA · Boeing 727225SDR 9905029140Angle · pittedDURING M-CHECK, FOUND LEFT LEADING EDGE ATTACH ANGLE FOR LEADING EDGE NR 6321 PITTED. REPAIRED PER EA 91-169335.Nov 14, 1999 · N930RC · Doug DC914SDR AALA991724Lug · corrodedTUL - RIGHT OUTBOARD AND INBOARD LUGS FOR THE HORIZONTAL STABILIZER PIVOT BEARING CORRODED. BORED AND SPOT FACED, MANUFACTURED AND INSTALLED NEW BUSHINGS PER ESO 11697 DATED 11-11-99. TST: 63,321 HOURS. CYCLES: 40,522. (X)Nov 11, 1999 · N848AA · Boeing 727223SDR ABXA9900774Angle · crackedDURING C-CHECK, FOUND VERTICAL STABILIZER, LOWER LEFT ATTACH ANGLE CRACKED AT AFT END. REPAIRED IAW ABX REA D953-34140MR.Nov 8, 1999 · N958AX · Doug DC941SDR CALA9901475Angle · crackedINSPECTION FOUND A 1 CRACK IN ANGLE AT BASE OF LT LOWER AFT SIDE VERTICAL STABILIZER. FILLER AND DOUBLER WERE INSTALLED IAW SRM 53-05, FIGURE 23A.Nov 7, 1999 · N69803 · Doug DC982SDR 99ZZZX4442Fitting · crackedLEFT HAND AFT VERTICAL STABILZIER ATTACH FITTING FOUND CRACKED.Nov 5, 1999 · N6249H · Cessna 152SDR MWEA99737Former · crackedVERTICAL STABLIZER FORMER CRACKED IN TWO PLACES UNDER FORWARD WEB ATTACH ANGLES. MAINTENANCE FABRICATED AND INSTALLED FORMER WEB REPAIR.Oct 26, 1999 · N806ME · Doug DC981SDR ABXA9900757Shear Tie · crackedDURING C-CHECK, FOUND VERTICAL STABILIZER ATTACH FITTING SHEAR-TIE AT STATION 1094 CRACKED. REPLACED SHEAR-TIE IAW DC9 SRM 51-30-2 AND 51-30-5.Oct 26, 1999 · N928AX · Doug DC932SDR MWEA99709Fairing · chafedLEFT HAND HORIZONTAL VERTICAL STAB FAIRING CHAFING AT AFT VERTICAL SKIN. MTC FABRICATED AND INSTALLED NEW DOUBLER ON VERTICAL STAB.Oct 21, 1999 · N202ME · Doug DC932SDR WXOA99011Duct · crackedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, VERTICAL STABILIZER AIR INTAKE DUCT AT 12 O'CLOCK POSITION HAS A CRACK APPROXIMATELY .25 INCHES LONG. REPAIRED CRACK IAW BOEING EA M-7200-99-09364. (M)Oct 14, 1999 · N127NK · Doug DC921SDR TWAA0000305Rib · crackedDURING OP 16 MAINT CHECK, FOUND VERTICAL STABILIZER DORSAL FIN WITH RIBS CRACKED AT LOWER END, NUMBER 1 AND 5 ON LT SIDE AND 4, 7, AND 8 ON RT SIDE. REPAIRED RIBS 1, 5, 4, 7 PER SRM 55-02 FIG 19. REPLACED NUMBER 8 PER SPM 6-70-01.Oct 7, 1999 · N950U · Doug DC982SDR EISA99204Fitting · misdrilledDURING REPLACEMENT OF VERTICAL FIN FRONT SPAR UPPER RIGHT TERMINAL FITTING AND SUBSEQUENT REMOVAL OF PREVIOUS REPAIR FOUND MIS-DRILLED HOLES IN LEFT HAND TERMINAL FITTING. REMOVED AND REPLACED LEFT TERMINAL FITTING PER SB 55-0060 AND BAC DRAWING 65-89361. (MOct 5, 1999 · N315NE · Boeing 727223SDR AU991030Bracket · damaged(AUS) CENTER RUDDER ATTACHMENT BRACKET DAMAGED.Oct 1, 1999 · Bnorm BN2A20SDR 99FDEA00401Fitting · crackedSNRM 712, 719, 720, NR 4 BANJO FITTING CRACK AT RT - 712, 719, 720. REPAIR PER SRM 55-20-00 712, UPPER HOLE OVERSIZE NO CRACK FOUND 719, MID HOLE OVERSIZE NO CRACK FND 720.Sep 29, 1999 · N607FE · Doug MD11SDR UF6A990940Angle · crackedSBN - THE ANGLE WHICH ATTACHES THE VERTICAL STABILIZER TO THE FUSELAGE IS CRACKED ON THE RIGHT SIDE. MAINTENANCE REPAIR ANGLE. ALL WORK WAS DONE IAW ENGINEERING ORDER 99-184. (M)Sep 27, 1999 · N858AW · Bag ATPSDR UF6A990923Fairing · crackedSBN - THE TOP ANGLE WHICH ATTACHES THE VERTICAL STABILIZER TO THE FUSELAGE ON THE LEFT SIDE IS CRACKED AT THE FORWARD SECTION. MAINTENANCE REPAIRED CRACK. ALL WORK WAS DONE IAW ENGINEERING ORDER 99-184. (M)Sep 23, 1999 · N858AW · Bag ATPSDR UF6A990922Fairing · crackedSBN - THE ANGLE WHICH ATTACHES THE VERTICAL STABILIZER TO THE FUSELAGE ON THE LEFT SIDE IS CRACKED AT THE AFT SECTION. MAINTENANCE REPAIRED CRACKED. ALL WORK WAS DONE IAW ENGINEERING ORDER 99-184. (M)Sep 23, 1999 · N858AW · Bag ATPSDR DL72S992115Casting · crackedVERT STAB LT TENSION TIE BOLT CASTING CRACKED I/B SIDE. REPLACED FITTING PER BAC DWG 65-17509 REV M. TPA LTR CHK D-2 09/21/99.Sep 21, 1999 · N492DA · Boeing 727232SDR EISA99205Fitting · crackedDURING ACCOMPLISHMENT OF A ROUTINE C-CHECK WORKCARD, FOUND 1 INCH CRACK IN VERTICAL FIN SPAR TERMINAL FITTING RIGHT SIDE. REMOVED DAMAGED FITTING REPLACED WITH NEW FITTING PER SB 55-0060 AND BAC BLUEPRINT 65-89361. (M)Sep 14, 1999 · N315NE · Boeing 727223SDR C2XA99IA470Angle · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT VERTICAL STABILIZER DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-01101, AND THE AIRSep 9, 1999 · N14943 · Emb EMB145ERSDR C2XA99IA469Angle · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICLE STABILIZER DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-01101, AND THE AISep 9, 1999 · N14943 · Emb EMB145ERSDR DL72L991998Stringer · wornSTRINGER 7L OF THE VERTICAL STABILIZER WAS FOUND TO BE WORN AT FIN STATION 228. THE DAMAGE WAS REPAIRED PER ER/A 333496.Sep 5, 1999 · N501DA · Boeing 727232SDR 99FDEA00370Fitting · crackedDURING EDDY CURRENT INSP ON RT BANJO NR 4 FOUND INNER FWD FLANGE WITH .5 INCH CRACK AT RADIUS AREA FWD CTR FASTENER HOLE DIA 0.371 IN AND LWR FWD FASTENER HOLE DIA 0.325 IN WITH SHORT EDGE MARGIN AND CRACK=FREE COND-585., FOUND FOR UPPER AND LWR FASTENER HOLE Sep 3, 1999 · N602FE · Doug MD11FSDR 99FDEA00360Bushing · oversizeRT BANJO NR 4 FITTING AFT LWR FASTENER'S HOLE FOUND INSTALL WITH BUSHING OF DIAMETER 0.593 IN EXCEED MAX REWORK DIAMETER OF HOLE SIZE 0.450. REPAIRED FITTING AS PER EA 1-5530-47413 & EA 1-5530-47414.Sep 2, 1999 · N585FE · Doug MD11FSDR 20000515AP007Bracket · damagedFOUND VERTICAL STABILIZER LEADING EDGE THROUGH PANEL 9502 UPPER RIGHT CORNER BRACKET AND WEB DAMAGED. REMOVED INNER PANEL, CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED REPAIR IAW SRM 51-10-1 PAGE 4, 51-40-2 PAGE 2, 51-30-1 PAGE 1, 55-10-1 PAGE 6. (M)Aug 31, 1999 · N803MA · Boeing 727225SDR USAA990854Angle · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTINO, FOUND A ..25 INCH CRACK AT DRAG ANGLE VERT FIN ATTACH FITTING. INSTALLED DOUBLER AND FILLERS PER EA 65234 AND 65234A. (M)Aug 29, 1999 · N397US · Boeing 7373B7SDR 20000515AP027Angle · crackedFOUND VERTICAL STAB INNER COMPARTMENT RIB NR 9 RIGHT STRINGER NR 9 CRACKED AT ATTACH BOLT. REMOVED CRACKED AREA. NDT AREA FABRICATED AND INSTALLED REPAIR IAW SRM 53-30-4 FIG 1, 55-30-5 FIG 1. (M)Aug 28, 1999 · N803MA · Boeing 727225SDR 20000515AP026Angle · crackedFOUND VERTICAL STABILIZER INNER COMPARTMENT NR 8 RIGHT STRINGER NR 8 CRACKED AT ATTACH BOLT. REMOVED CRACKED AREA. NDT AREA FABRICATED AND INSTALLED REPAIR IAW SRM 53-30-4 FIG 1, 55-30-5 FIG 1. (M)Aug 28, 1999 · N803MA · Boeing 727225SDR 20000515AP025Angle · crackedFOUND VERTICAL STAB INNER COMPARTMENT NR 6 RIGHT SUPPORT WEB BETWEEN STRINGER NR 8 AND NR 9 CRACKED AT LOWER CORNER. REMOVED CRACKED ANGLE. FABRICATED AND INSTALLED ANGLE IAW SRM 51-40-3 PAGE 7. (M)Aug 28, 1999 · N803MA · Boeing 727225SDR MWEA99547Skin · crackedA 1 INCH SKIN CRACK TO THE LEFT OF THE VERTICAL FIN RAM AIR INTAKE AT STATION 894 - 908 BETWEEN LONGERON 2L AND 3L. MTC FABRICATED AND INSTALLED DOUBLER.Aug 25, 1999 · N500ME · Doug DC914SDR C2XA99IA449Drag Angle · crackedIAH - DURING C-CEHCK INSPECTION, THE VERTICLE STABILIZER TO FUSELAGE LEFT DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-01101,Aug 25, 1999 · N14942 · Emb EMB145SDR C2XA99IA448Drag Angle · crackedIAH - DURING C-CHECK INSPECTION, THE VERTICLE STABILIZER TO FUSELAGE RIGHT DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-01101Aug 25, 1999 · N14942 · Emb EMB145SDR DHL9972740CAngle · crackedAT C CHECK, VERT STAB HAS A T ANGLE CRACKED JUST AFT OF RT LWR ICE SHIELD. REMOVED ANGLE AT VERT STAB JUST AFT RT LWR ICE SHIELD AS PER SRM 51-30-2, INSTALLED NEW T ANGLE AT VERT STA JUST AFT RT LWR ICE SHIELD PER SRM 51-30-2 USING 60-3783 8 LONG. ALODINED AAug 20, 1999 · N727DH · Boeing 727228SDR 99FDEA00340Fitting · crackedVERTICAL STAB REAR SPAR (P/N AJC7054-501) BANJO FITTING HAS CRACK IND APPROX 4.5 AFT TANG LWR SURFACE ALONG THE RADIUS. *S/D* REPAIRED IAW EO 8-5430-7-2302 PT 2.Aug 18, 1999 · Doug DC1010FSDR C2XA99IA432Drag Angle · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICLE STABILIZER TO FUSELAGE DRAG ANGLE WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-01101; AND Aug 15, 1999 · N15941 · Emb EMB145SDR C2XA99IA431Drag Angle · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT VERTICLE STABILIZER TO FUSELAGE DRAG ANGLE WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-01101, AND TAug 15, 1999 · N15941 · Emb EMB145SDR DL72S991844Stringer · crackedVERTICAL STAB INTERIOR, STRINGER CRACKED AT TIE TO RIB LEFT SIDE AT FIN STA 1338. INSTALLED REPAIR PER SRM 55-30-0 FIG 803.Aug 9, 1999 · N8882Z · Boeing 727225SDR AT9900605Skin · chafedSCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND THE LEFT LOWER AFT BANANA FAIRING ON THE VERTICAL STABILIZER AND SKIN CHAFFED AT YV 227-247. BLEND CHAFFED AREA ON THE BANANA FAIRING AND FABRICATED NEW SKIN PANEL FOR THE VERTICAL STABILIZER. HEAT TREATED, Aug 4, 1999 · N803AT · Doug DC932SDR DHL9974203CAngle · wornAT C CHECK, ANTI-ICE SUPPORT BRACKETS WORN AT VERTICAL FIN FRONT SPAR. REMOVED AND REPLACED BRACKETS PER SRM 51-30-2 9.25 BY 2 BY .75, N/R 4267.Jul 26, 1999 · N742DH · Boeing 727225SDR C2XA99IA379Drag Angle · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-01101, AND TJul 23, 1999 · N14938 · Emb EMB145SDR C2XA99IA378Drag Angle · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICAL STABILZIER TO FUSELAGE DRAG ANGLE WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-01101, AND Jul 23, 1999 · N14938 · Emb EMB145SDR DHL9970316CFairing · delaminatedAT C CHECK, V STABILIZER HAS FAIRING DELAMINATED ON BOTH SIDES BELOW TAIL CONE. INSTALLED BONDING REPAIR AT VERTICAL STABILIZER FAIRINGS BELOW TAIL CONE PER SRM 51-20-3 FIG 1, MATERIAL USED EPOCAST 1652 A/B, N/R 4127.Jul 21, 1999 · N703DH · Boeing 72730C
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