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 SWAA2021051294331Skate Angle · chafedCHAFING ON RIGHT HAND SKATE ANGLE AT B.S. 1007-1016; W.L. 306.5; R.B.L. 14. / REMOVED AND REPLACED SKATE ANGLE AT BS1007 TO BS1016 WL306.5 RBL14 IAW SRM 51-40-02 AND DWG 147A0030 REV. A 57049U 25JUNE2020Jun 22, 2020 · N7733B · Boeing 73776NSDR JGVR20200616002Stiffener · gougedFOUND UPPER RT BOLT HOLE ON THE VERTICAL STABILIZER AFT SPAR STIFFENER GOUGED, BLENDED DAMAGED. REPLACED THE STIFFENER.Jun 16, 2020 · N387QS · Cessna 680ASDR SWAA2021051291219Skate Angle · chafedLT FWD VERT FIN CLOSURE SKATE ANGLE IS CHAFED / REMOVED & REPLACED LT FWD; VERT FIN CLOSURE (SKATE) ANGLE IAW SRM 51-40-02-0G-0; 51-40-05-0G-0; 51-40-08-0G-0 DWG #'S 147A0030 & 147A0070. RESTORED DECORATIVE FINISH ON NEW SKATE ANGLE IAW AMM 51-21-99-300-801 56Jun 9, 2020 · N481WN · Boeing 7377H4SDR AALA202006191013Hinge Arm · damagedAIRCRAFT WAS GROUNDED: NR 1 RUDDER HINGE ARM HAD ELONGATED HOLES. REPLACED THE NR 1 RUDDER HINGE ARM IAW SRM 55-36-42 AND EA 306408.Jun 2, 2020 · N775XF · Airbus A319112SDR SWAA2021072987917Fitting · corrodedVERTICAL STABILIZER R/H AFT SPAR FITTING I/B BOLT SHOWING STRESS CORROSION. / RECEIVED NEW SERVICABLE VERTICAL STABILIZER R/H AFT SPAR FITTING I/B BOLT P/N 170A1611-4 TO BE INSTALLED ON CUSTOMER CARD J753-480-00-00May 30, 2020 · N286WN · Boeing 7377H4SDR SWAA2021072987916Bolt · corrodedVERTICAL STABILIZER AFT RIGHT SPAR FITTING O/B BOLT SHOWING STRESS CORROSION. / RECEIVED NEW SERVICABLE VERTICAL STABILIZER AT RIGHT SPAR FITTING O/B BOLT P/N 170A1611-1 TO BE INSTALLED ON CUSTOMER CARD J753-480-00-00May 30, 2020 · N286WN · Boeing 7377H4SDR SIMA2020072753004Housing · out of limitsLEFT AND RIGHT SPHERICAL BEARING HOUSINGS FOUND TO BE OUT OF LIMITS IAW SRM 55-30-02. REPAIRED THE SPHERICAL BEARING HOUSINGS IAW SRM 55-30-02.May 30, 2020 · N615AE · Emb EMB145LRSDR SWAA2021080393119Structure · erodedVERTICAL STAB. RUDDER ARM WEIGHT EDGES ARE ERODED / REMOVED AND INSTALLED NEW VERTICAL STAB. RUDDER ARM WEIGHT IAW B737 51-21-73-370-801; CMM 55-40-09; AMM 20-50-11-910-801; SRM 51-40-02-0G-0; AMM 27-21-11-400-801 SEAL GAP CHECK GOOD ATAG: WN0643May 27, 2020 · N928WN · Boeing 7377H4SDR SWAA2021072980153Nut Plate · brokenVERTICAL STABILIZER RIGHT SIDE; STRUCTURE SUPPORT PANEL 323BR BROKEN SCREWS ( 3 EA) / REMOVED AND REPLACED NUTPLATES 4EA AT VERTICAL STABILIZER RIGHT SIDE STRUCTURE SUPPORT PANEL #323BR IN REF B737-700 SRM 51-40-02-0G-0.May 23, 2020 · N286WN · Boeing 7377H4SDR IPXA2020052215601Bracket · crackedINSPECTION TYPE:SEGVERT STAB R/H SIDE PANEL 323AR DAMAGED NUTPLATENO NUT PLATE DAMAGED - FOUND BRACKET CRACKED - REMOVED AND INSTALLED NEW BRACKET SRM 51-40-21May 21, 2020 · N171UP · Airbus A300F4622RSDR DALA2020051302393Hinge Fitting · crackedCRACK DOOR ON HINGE ARM FITTING ASSY #4 TRAILING EDGE ON VERTICAL STABILIZER (1 EA), PERFORMED PERMANENT REPAIR ON DOOR HINGE ARM FITTING ASSY #4 TRAILING EDGE ON VERTICAL STABILIZER (1EA) ASPER A320 SRM 55-36-42-300-003May 12, 2020 · N321US · Airbus A320211SDR SWAA2021080975346Retainer · damagedVERTICAL STAB PANEL 323BL FWD RETAINER IS DAMAGED / REMOVED DAMAGED FWD RETAINER FROM PANEL 323BL AND REPLACED IT WITH A NEW FWD RETAINER IAW SRM 51-40-02-0G-0 STEP 2.D. AND STEP 4 7041U 07MAY20 3426C 07MAY20 AND DWG 172A6125 3426C 07MAY20May 5, 2020 · N7736A · Boeing 7377BDSDR SWAA2020050874524Attach Bolt · damagedVERT FIN L/H AFT SPAR O/B ATTACH BOLT IS DAMAGED. / RECIEVED NEW VERT FIN L/H AFT SPAR O/B ATTACH BOLT. BOLT WILL BE INSTALLED ON CUST CARD # 753-400-00-00.May 1, 2020 · N467WN · Boeing 7377H4SDR SWAA2020050874525Attach Bolt · damagedVERT. FIN R/H AFT SPAR O/B ATTACH BOLT IS DAMAGED. / RECIEVED NEW VERT. FIN R/H AFT SPAR O/B ATTACH BOLT. BOLT WILL BE INSTALLED ON CUST CARD # 753-480-00-00May 1, 2020 · N467WN · Boeing 7377H4SDR SWAA2021051387518Skate Angle · chafedFORWARD SECTION OF LEFT SKATE ANGLE HAS MATERIAL CHAFFED; MISSING AT BS 1005 TO BS 1016. / REMOVED AND REPLACED LEFT FWD SKATE ANGLE PER SRM 51-40-02 AND AMM 51-21-73Apr 15, 2020 · N948WN · Boeing 7377H4SDR SWAA2021051387519Skate Angle · chafedLEFT SKATE ANGLE HAS MATERIAL LOSS; CHAFFING AT BS 1106 TO 1109. / REPAIRED SKATE ANGLE PER SRM 53-80-71-2R-6.Apr 15, 2020 · N948WN · Boeing 7377H4SDR SWAA2020050442558Bolt · wornCUSTOMER CARD J753-480-00-00; VERTICAL STAB L\H OTBD AFT SPAR FITTING BOLT HAS WEAR. / REMOVED AND REPLACED VERTICAL STAB L/H O/B AFT SPAR FITTING BOLT PER WORK CAR J753-480-00-00 PAGE 3 STEP 2A(1)(C) REFFERANCE AMM 55-30-00-400-801 STEP 3H(1)(C) TORQUE WRENCHApr 15, 2020 · N470WN · Boeing 7377H4SDR SWAA2021051336710Skate Angle · chafedCHAFED RH CROWN SKATE ANGLE AT BS1009 RBL14. / REMOVED AND REPLACED R/H CROWN SKATE ANGLE AT BS1006-BS1016 RBL14 IAW SRM 51-40-02-0G-0 AND DWG 147A3200Apr 7, 2020 · N468WN · Boeing 7377H4SDR SWAA2021051336442Skate Angle · chafedLH CROWN SKATE ANGLE FROM BS 1010_1017 IS CHAFED. / REMOVED AND REPLACED L/H CROWN SKATE ANGLE FROM BS1006-BS1017 IAW SRM 51-40-02-0G-0 AND DWG 147A3200Apr 6, 2020 · N468WN · Boeing 7377H4SDR SWAA2021051336443Skate Angle · chafedLH CROWN SKATE ANGLE IS CHAFED AT BS 1109 AREA. NO VERIFICATION OF CHAFE REMOVED PRIOR TO APPLICATION OF TOP COAT. / WORK ACCOMPLISH WITH SAM 326 A1296390.Apr 6, 2020 · N468WN · Boeing 7377H4SDR SWAA2021051386101Skate Angle · chafedR/H VERTICAL TAIL SKATE ANGLE CHAFFING ON I/B SIDE BETWEEN STA 1016 TO STA 1016 +2' / REMOVED DAMAGE ON RH SKATE ANGEL I/B SIDE STA 1016 TO 1016+2' IAW SRM 51-10-02-0G-0. MESSURED MATERIAL LOSS TO BE .007' ORIGINAL (T) .075' REMAINING (T) .068 IN LIMITS IAW SRApr 1, 2020 · N8628A · Boeing 7378H4SDR SWAA2021051386100Skate Angle · chafedL/H VERTICAL TAIL SKATE ANGLE CHAFFING ON I/B SIDE BETWEEN STA 1016 TO STA 1016 +2' / REMOVED DAMAGE ON L/H SKATE ANGLE I/B SIDE STA 1016 TO 1016+2' IAW SRM 51-10-02-0G-0 MESSURED MATERIAL LOSS TO BE .004' ORIGINAL (T) .075' REMAINING (T) .071 FOUND TO BE IN LApr 1, 2020 · N8628A · Boeing 7378H4SDR SWAA2021081032392Panel · erodedVERT STAB LE HF ANTENNA FIBERGLASS PANEL HAS EROSION DAMAGE .400 X .450 X .050 DEEP AT LWR AREA OF PANEL / REPAIRED PER EA 1-A55-3775 REF ECTC FOR TLD CARRY OVER REPAIR# 55EA-07960. 55EA-07961; 55EA-07962 AMT 56504Mar 18, 2020 · N8313F · Boeing 7378H4SDR AALA202003309011Hinge Arm · wornAIRCRAFT IN BASE MAINTENANCE: #3 VERTICAL STABILIZER LOWER ATTACHMENT HINGE ARM FOR RUDDER HINGE FITTING HAS SEVERAL OUT OF ROUND HOLES. REPLACED HINGE ARM PER AMM 55-36-42 AND EA 304554.Mar 16, 2020 · N124US · Airbus A320214SDR HNAA2020040700116Housing · corrodedSPHERICAL BEARING HOUSING ON LH AND RH SIDES HAS CORROSION. REPAIRED SPHERICAL BEARING HOUSING CORROSION ON LH AND RH SIDES IAW PIEDMONT EO1-55-20-0131.Mar 12, 2020 · N686AE · Emb EMB145LRSDR SWAA2021051383640Skate Angle · chafedCHAFED SKATE ANGLE AT B.S. 1007-1009; R.B.L. 14; W.L. 308. / REMOVED AND REPLACED SKATE ANGLE P/N 147A3000 PO# 773653/3 AT BS 1007 TO BS 1016 RBL 14 WL 308 IAW SRM 51-40-02 AND DWG 147A0030 REV B 57049U 19MAR2020Mar 6, 2020 · N762SW · Boeing 7377H4SDR SWAA2021051383639Skate Angle · chafedCHAFED SKATE ANGLE AT B.S. 1009-1016; L.B.L. 14; W.L. 308. / REMOVED AND REPLACED SKATE ANGLE 147A3200U11 PO# 786342/1 AT BS 1007 TO BS 1016 LBL 14 WL 308 IAW SRM 51-40-02 AND DWG 147A0030 REV B 57049U 19MAR2020Mar 6, 2020 · N762SW · Boeing 7377H4SDR SWAA2021051383638Skate Angle · chafedCHAFED SKATE ANGLE AT B.S. 1122; L.B.L. 14; W.L. 308. / REMOVED AND REPLACED SKATE ANGLE PO# 777690/1 AT BS 1016 TO BS 1132 LBL 14 WL 308 IAW SRM 51-40-02 AND DWG 148A8300 REV C 57049U 19MAR2020Mar 6, 2020 · N762SW · Boeing 7377H4SDR VNAA2020022499901Drag Angle · crackedSUSPECTED CRACK ON LH AFT VERTICAL STAB DRAG ANGLE. F.HENRY 01/30/20 (ROSEM) M/A: 1. N/A. C/A: 1. PERFORMED EDDY CURRENT INSPECITON OF SUSPECTED CRACKED AREA IAW CRJ 900 NDTM PART 1 51-20-006-250-A01. FOUND ONE INDICATION 1" LONG BY 100% FSH IN THE RADIUS OF TFeb 24, 2020 · N562NN · Bombdr CL6002D15SDR SWAA2021080919714Retainer · crackedVERTICAL STAB ACCESS PANEL 323AL LOWER METAL SEAL RETAINER WITH A CRACK AT AFT END DOT 107-023 / RECEIVED NEW PANEL 323AL P/N 172A6122-1; 51#7551015; NEW PANEL TO BE INSTALLED J-PANEL CLOSE -320Feb 20, 2020 · N424WN · Boeing 7377H4SDR DALA2020022001257Hinge Fitting · damagedAFTER REMOVED BEARING FOUND WITH SCRATCH ON BORE OF HINGE #4 VERTICAL STABILIZER. REPLACED HINGE #4 ON VERTICAL STABILIZER AS PER AMM FAM A319- A320 55-36-41-400-001 PROCEDURE 4(A) STEP (4) AND SRM A319 55-36-42- 300-003 AND DWG 55371042.Feb 20, 2020 · N352NB · Airbus A319114SDR SWAA2021051381768Skate Angle · chafedSKATE ANGLE IS CHAFED AT 1007-1016; W.L. 306; R.B.L. 14. / REMOVED AND REPLACED SKATE ANGLE P/N 147A3200U12 BS 1007 TO BS 1016; RBL14; WL 306 IAW SRM 51-40-02 AND DWG 147A0030 REV A. 89004U; 29FEB20.Feb 18, 2020 · N271LV · Boeing 737705SDR SWAA2021072924360Fastener · pulledL/H SIDE OF VERTICAL STABILIZER; SKIN PANEL FASTENERS (2) ARE PULLED/PULLING TRHOUGH PANEL. 1.) 8.5' AFT OF DORSIL FIN T/E AND 44' UP FROM FUSELAGE SKIN. 2.) 11' AFT OF DORSIL FIN T/E AND 42' UP FROM FUSELAGE SKIN. / REPLACED 2 EACH FASTENERS AT L/H SIDE OF VEFeb 9, 2020 · N7727A · Boeing 73776NSDR V0XD20200209601Drag Angle · crackedLH FWD AND AFT VERTICAL STAB DRAG ANDGLES CRACKED. CORRECTIVE ACTION: REPAIRED LH FWD AND AFT DRAG ANGLE IAW BOMBARDIER REO# 670-55-31-018 REV A DATED 2016-11-10, BOMBARDIER REO# 670-55-31-128 DATED 2020-01-29 AND GOJET EO C700-55MR-001O DATED 11-24-2018.Feb 6, 2020 · N340CA · Cndair CL6002C10SDR ABXR2020020540002Angle · crackedCLOSE OUT ANGLE UNDER RUDDER HAS CRACK AT LEFT END OF ANGLEFeb 5, 2020 · N695GT · Boeing 767281SDR V0XD20200217002Drag Angle · crackedRH FWD AND AFT VERTICAL STABILIZER DRAG ANGLES CRACKED. CORRECTIVE ACTION: REPAIRED RH FWD AND AFT DRAG ANGLES IAW BOMBARDIER REO# 670-55-31-018 REV A DTED 2019-11-10, BOMBARDIER REO# 670-55-31-128 DATED 2020-01-29, AND GOJET EO C700-55MR -001-O DATED 11-24-20Jan 31, 2020 · N340CA · Cndair CL6002C10SDR SWAA2020020651068Support Angle · crackedINSIDE VERTICAL STABILIZER LATERAL SUPPORT ANGLE CRACKED IN RADIUS AT BS. 1016, LBL 12, 8" ABOVE FUSELAGE SKIN / R&R ANGLE IAW DWG AND SRM.Jan 30, 2020 · N718SW · Boeing 7377H4SDR SWAA2021051306515Attach Bracket · damagedVERTICAL STABILIZER ACCESS PANEL 323BL AFT SKATE ANGLE ATTACH BRACKET DAMAGED / REMOVED AND REPLACED BRACKET PER SRM 51-40-02.Jan 28, 2020 · N247WN · Boeing 7377H4SDR SWAA2021051306514Skate Angle · damagedLEFT HAND VERTICAL STABILIZER AFT FUSELAGE SKATE ANGLE DAMAGED / KNIFE EDGED IN MULTIPLE AREAS ALONG THE ENTIRE LENGTH OF SKATE ANGLE / REMOVED AND REPLACED CLOSURE ANGLE PER SRM 51-40-02.Jan 28, 2020 · N247WN · Boeing 7377H4SDR ASOA202001237010Housing · damagedTYS- THE VERTICAL STAB RH SPHERICAL BEARING MOUNT HOLE TOO BIG. THE SPHERICAL BEARING HOUSING WAS OVER-SIZED AND BUSHINGS WERE INSTALLED IAW SRM 55-30-02.Jan 23, 2020 · N16170 · Emb EMB145XRSDR FDEA202001210189Spar · damagedAUXILIARY SPAR FSS 340 TO FSS 371 TORN/DAMAGED REMOVED AND REPLAICED AUX SPAR IAW SRM 51-40-02 MAJOR REPAIRJan 21, 2020 · N922FD · Boeing 75723ASDR FDEA202001210188Web · damagedVERTICAL STABILIZER RIB FSS 371.308 WEB IS BUCKLED AT FORWARD SIDE REMOVED AND REPLACED WEB IAW SRM 51-40-02 MAJOR REPAIRJan 21, 2020 · N922FD · Boeing 75723ASDR REXA2020020500159Drag Angle · cracked"VERTICAL STABILIZER, RH AFT DRAG ANGLE IS CRACKED "REPAIRED RH AFT DRAG ANGLE IAW CRJ 900 SRM 55-31-00-201-001-A01. WVACSTAMP EMP# 769 MTC "Jan 20, 2020 · N181PQ · Cndair CL6002D24SDR REXA2020020500157Drag Angle · cracked"VERTICAL STABILIZER, L/H AFT DRAG ANGLE IS CRACKED. ""OK TO INSTALL. INSTALLED THE FABRICATED PARTS IAW CRJ 900 SRM 55-31-00-201-001-A01 STEP 9, PLUS COMPLIED WITH REMAINING STEPS, 10 THROUGH 14AND STEP 6 A OF THE VERTICAL STABILIZER TO THE FUSELAGE ATTACHMEJan 20, 2020 · N181PQ · Cndair CL6002D24SDR SWAA2021081908814Bracket · crackedDORSAL FIN FWD ATTACH BRACKET CRACKED. / REPLACED FWD ATTACH BRACKET IAW SRM 51-40-02Jan 19, 2020 · N495WN · Boeing 7377H4SDR AALA202001149004Attach Bolt · looseAIRCRAFT IN BASE MAINTENANCE: VERTICAL STABILIZER MID AND AFT ATTACHMENT BOLTS (4 EACH) ON BOTH SIDES HAVE APPEARED TO MIGRATED LOOSE AS REFLECTED BY THE TORQUE STRIPE INDICATION MARK ON THE NUTS. REPLACED 4 BOLTS AND RETORQUED PER AMM 55-31-11-400-801-A.Jan 13, 2020 · N290AY · Airbus A330243SDR SWAA2021051325891Skate Angle · chafedEXTERNAL FUSELAGE STA 1016 TO 1128; RBL 14.5; RH VERTICAL FIN CLOSER SKATE ANGLE HAS CHAFING DAMAGE. / REMOVED AND REPLACED EXTERNAL FUSELAGE STA 1016-1128 RBL 14.5 R/H VERTICAL FIN SKATE ANGLE IAW SRM 51-40-02-0G-0; DWG 148A8700 ID:0001 REV CJan 9, 2020 · N7868K · Boeing 73779PSDR SWAA2021051325889Skate Angle · chafedEXTERNAL FUSELAGE STA 1016 TO 1128; LBL 14.5; LH VERTICAL FIN CLOSER SKATE ANGLE HAS CHAFING DAMAGE. / REMOVED AND CUT DAMAGE; REPAIRED I/A/W SRM 53-80-71-2R-6 REPAIR 6 AT EXTERNAL FUSELAGE STA 1016 TO 1128 LBL 14.5 L/H VERTICAL FIN CLOSER SKATE ANGLE.Jan 9, 2020 · N7868K · Boeing 73779PSDR SWAA2021051325890Skate Angle · chafedEXTERNAL FUSELAGE STA 1006 TO 1016; RBL 14.5; RH VERTICAL FIN CLOSER SKATE ANGLE HAS CHAFING DAMAGE. / REMOVED AND REPLACED RH SKATE ANGLE AT RBL 14.5 STA 1006 TO 1016 REF DWG 147A0030 REV B; B737 SRM 51-40-02 NO PUBLISHED LIMITS IN SRMJan 9, 2020 · N7868K · Boeing 73779PSDR SWAA2021051325888Skate Angle · chafedEXTERNAL FUSELAGE STA 1006 TO 1016; LBL 14.5; LH VERTICAL FIN CLOSER SKATE ANGLE HAS CHAFING DAMAGE. / REMOVED AND REPLACED LH SKATE ANGLE AT LBL 14.5 STA 1006 TO 1016 REF DWG 147A0030 REV B; B737 SRM 51-40-02 NO PUBLISHED LIMITS IN SRMJan 9, 2020 · N7868K · Boeing 73779P
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