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 C2XA99IA198Angle · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT VERTICAL STABILIZER DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE DAMAGED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION EC5330-01101, AND THE AIRCRAFTMar 21, 1999 · N15932 · Emb EMB145SDR DL72W990769Stringer · crackedSTR RT CRACKED INSIDE VERT STA AT B/H STA 133.8 LOC INSIDE VERT STAB. BEGAN FABRICATING REPAIR ANGLE. FABRICATED REPAIR ANGLES PER M/M 55-30-0 PG 803. OK TO INSTALL REPAIR. INSTALLED REPAIR PER M/M 55-30-0 PG 803.Mar 18, 1999 · N2820W · Boeing 727247SDR DL72S990589Stringer · crackedVERT FIN STR 10L CRACKED AT STA 180.600. INSTALLED DOUBLER PER M/M 55-30-0.Mar 18, 1999 · N523DA · Boeing 727232SDR CALA9900294Bolts · corrodedINSPECTION FOUND VERTICAL STABILIZER TENSION TIE BOLTS (8) PITTED AND CORRODED. THE TENSION TIE BOLTS WERE REMOVED AND REPLACED IAW MM 55-30-51, PAGE 406-408.Mar 18, 1999 · N77780 · Boeing 727232SDR USAA990250Doubler · gougedPIT - DURING C-1 CHECK, FOUND ICE SCRAPER SCREWS GOUGED DOUBLER IN 3 PLACES (.250 L BY .03125 D) (.9375 L BY .032 D) (1.750 L BY .015625 D) AT LEFT VERT STABILIZER, RIB 5 LEFT SIDE. INSTALLED DOUBLER AND BLENDED PER EA 31078A. (M)Mar 16, 1999 · N861US · Fokker F28MK0100SDR DL72K990590Web · crackedWEB CRACKED VERTICAL STAB INTERIOR - WEB AT STA 1303 IS CRACKED AT BOTH RT AND LT LOWER CORNERS, MARKED. STOP DRILLED CRACKS AND DYE PENETRATE INSP RT AND LT SIDE PER SRM 53-10-4 FIG 17. FABRICATED REPAIR DOUBLERS AND TAPERED SHIM PER SRM 53-10-4 FIG 17. TRMar 9, 1999 · N491DA · Boeing 727232SDR RRXA991376Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, VERTICAL STABILIZER, RT SIDE ATTACH ANGLE BRACKET STRIP AT STA 1542, LONGERON 2 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE SECMar 5, 1999 · N997CF · Doug DC862FSDR ABXA9900251Angle · crackedDURING C-CHECK, FOUND CRACKED ATTACH ANGLE AT VERTICAL STABILIZER WRAP AROUND PANEL. REPLACED ANGLE IAW DC9 SRM 51-30-5.Mar 5, 1999 · N931AX · Doug DC933FSDR SWAA990402Beam · crackedDURING SCHEDULED D-CHECK, FOUND LEFT VERTICAL STAB TRAILING EDGE BEAM CRACKED 15 FROM BOTTOM OF STAB. REPLACED BEAM SECTION FROM STA 13.33 TO 141.52 PER SRM.Feb 24, 1999 · N346SW · Boeing 7373H4SDR C2XA99IA177Angle · crackedIAH - DURING C-CHECK INSPECTIONI, THE RIGHT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE WAS FOUND TO BE CRACKED AT THE FORWARD END. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW EMB145 SST 0391/99, AND THE AIRCRAFT WAS APPROVED FOR REFeb 22, 1999 · N14925 · Emb EMB145SDR C2XA99IA176Angle · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE WAS FOUND TO BE CRACKED AT THE FORWARD END. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW EMB 145 SST 0391/99, AND THE AIRCRAFT WAS APPROVED FOR RETFeb 22, 1999 · N14925 · Emb EMB145SDR CA990308014Channel · cracked(CAN) CHANNEL RIVETED TO BULKHEAD STA 228 TO REINFORCE THE PICK-UP OF FOUR BOLTS FOR RUDDER POST WAS FOUND CRACKED. NEW PART INSTALLED. AREA ADDRESSED BY CF-98-38.Feb 17, 1999 · Dhav DHC2MK1SDR DL72S990268Rib · crackedVERTICAL FIN RIB CHORD CRACKED 1.25 INCH FIN STA 133.800, AT STR 8 ATTACH BOLT RT SIDE. REPAIR PER M/M 55-30-0 FIG 802.Feb 9, 1999 · N416DA · Boeing 727232SDR DL72S990267Clip · cracked1 IN CRACK IN LT VERT FIN SKIN TO RIB ATTACH CLIP, STA 180.600 ABOVE STR 10. REPAIR PER M/M 55-30-0 FIG 803.Feb 9, 1999 · N416DA · Boeing 727232SDR UPS99228631Stringer · crackedINSPECTION TYPE:SI INTERNAL VERTICAL FIN STRINGER 5-11R IS CRACKED AT BS 1362, 9 INCHES ABOVE FIN STA 6.0. REMOVED AND REPLACED STRINGER SEGMENT PER FER 99-5059.Feb 2, 1999 · N949UP · Boeing 72725CSDR DL72W990143Stringer · damagedWEAR WAS FOUND ON THE S7L ON THE VERT STAB. DAMAGE IS TO THE O/B SURFACE OF THE UPPER FLANGE AT APPROX FIN STA 230. REPAIRED PER ERA 332689-14.Jan 20, 1999 · N2810W · Boeing 727247SDR 99ZZZX519Tail Strut · brokenSTAINLESS STEEL STRUT ASSEMBLY BROKEN AT THREADS LOWER TERMINAL, TIE ROD.Jan 20, 1999 · N23HG · Chris A1SDR TWAA9901602Angle · crackedDURING OP 16 MAINT CHECK, FOUND FUSELAGE TO VERTICAL STABILIZER TIE ANGLE CRACKED APPROX 1.5 INCH LONG AT STA 1426 BETWEEN LONGERON 1L AND 2L, INSIDE LOWER STABILIZER. REPLACED ANGLE PART NR 5912188-35 PER STANDARD PROCESSES MANUAL 6-70-01.Jan 18, 1999 · N941AS · Doug DC983SDR MWEA99023Angle · crackedFOUND CRACKED ANGLE BRACKET AT BUSS OF RIGHT VERTICAL STABILIZER AFT SPAR BOX. MTC FABRICATED AND INSTALLED NEW ANGLE CLIP.Jan 11, 1999 · N207ME · Doug DC932SDR DL72S990030Stringer · crackedVERT FIN STR 9L CRACKED FIN STA 110.400. REPAIRED PER MM 55-30-0.Jan 6, 1999 · N484DA · Boeing 727232SDR MZZA99020Stiffener · crackedTNN - DURING S-CHECK INSPECTION AT AIR ASIA, CRACK 2 INCH LONG WAS FOUND ON VERTICAL FIN LEFT SIDE STIFFENER S-7 AT FS 112. THE DAMAGED STIFFENER 2 INCHES LONG WAS TRIMMED OUT AND REPAIRED PER B727 SRM 55-30-04 FIG 1. (M)Dec 28, 1998 · N75429 · Boeing 7272F9SDR DL72K982571Web · crackedAT HMV ON 12/8/98, FOUND VERTICAL STAB INTERIOR - VERT WEB AT STA 1303 IS CRACKED AT LT LWR CORNER, ABOVE S-DUCT. DYED CK, PER PS 900-6-3 NR 1 DRILLED CRACK PER SRM 53-10-4 FIG 17, FAB'D DOUBLER, TREATED, PAINTED, INSTALLED PER 53-10-4 FIG 17.Dec 8, 1998 · N525DA · Boeing 727232SDR CALA9802150Stringer · crackedINSPECTION FOUND A 1.5 INCH CRACK LT STRINGER 9 INSIDE VERTICAL STABILIZER AT RIB NR 8. THE CRACKED AREA WAS CUT OUT IAW SRM 55-30-4, PAGE 1. REPAIR ANGLES WERE INSTALLED IAW SRM 51-30-4 AND 51-10-2, PAGE 21.Dec 8, 1998 · N17407 · Boeing 727243SDR DL72S982482Stringer · crackedREF SHIP 538 TPA LTR CHK E-2 12-02-98, VERT FIN STRINGER 10L CRACKED STA 180.6. REPAIRED PER MM 55-30-0.Dec 2, 1998 · N8890Z · Boeing 727225SDR 99ZZZX202Rivet · shearedDURING C-CHECK INSPECTION, A RIVET HEAD WAS FOUND SEVERED FROM ITS SHAFT. THE RIVET LOCATION IS AT FRAME 47, STA X16128, AT THE LEFT HAND SIDE OF THE VERTICAL STABILIZER BASE. THERE IS NO INDICATION AS TO WHAT CAUSED THE RIVET HEAD TO BECOME SEVERED. THE HODec 2, 1998 · N260AS · Emb EMB120RTSDR ABXA9801146Angle · crackedDURING C-CHECK, FOUND VERTICAL STABILIZER ATTACH ANGLE RIGHT SIDE CRACKED AT LOWER AFT CORNER. REPAIRED ANGLE IAW DC9 SRM 51-30-2 AND 51-30-5.Nov 23, 1998 · N982AX · Doug DC932SDR CALA9802091Angle · crackedINSPECTION FOUND A .625 INCH CRACK IN LT VERTICAL STABILIZER ANGLE 37.5 INCHES AFT OF STA 1089.5. REPAIRED IAW SRM 55-02, FIGURE 26.Nov 21, 1998 · N69803 · Doug DC982SDR CALA9802040Stiffener · crackedINSPECTION FOUND A 1.5 INCH CRACK IN STIFFENER INSIDE VERTICAL FIN ABOVE S DUCT AREA AT BS 1303-1323, BL 0. A NEW STIFFENER WAS INSTALLED IAW SRM 51-10-1, PAGE 2 AND 51-30-2, PAGE 4.Nov 5, 1998 · N59792 · Boeing 727232SDR SWAA982755Tip · corrodedDURING SCHEDULED D-CHECK, FOUND VERT FIN CENTER TIP FAIRING HAS WING CORRODED AT FASTENER HOLES AND FWD EDGE. REPAIRED L/E VERT STAB PER BOEING SRM.Nov 4, 1998 · N339SW · Boeing 7373H4SDR AALA982065Strap · corrodedTUL - FOUND CORROSION ON HORIZ STAB REAR UPPER SRM FAIL/SAFE STRAP RIGHT SIDE. REPAIRED PER ESO 11697, DATED 10/15/98. (M)Nov 4, 1998 · N880AA · Boeing 727223SDR QXEA01553Angle · looseHI-LOK LOOSE IN LEFT-HAND V STAB CONNECTION ANGLE 31 FORWARD OF AFT END OF CONNECTION ANGLE. REPAIRED IAW FOKKER SRM 51-31-02.Oct 17, 1998 · N480AU · Fokker F28MK4000SDR QXEA01552Angle · looseHI-LOK LOOSE/SMOKING IN LEFT-HAND VERTICAL STAB CONNECTION ANGLE LOCATED 17 BACK FROM FORWARD END. REPAIRED IAW FOKKER SRM 51-31-02.Oct 16, 1998 · N480AU · Fokker F28MK4000SDR QXEA9801500Angle · crackedBETWEEN FRAMES 19976 AND 20075 BETWEEN STRINGERS 38 AND 39 CRACKS ARE NOTED ALONG RIVET LINE FOR VERTICAL STABILIZER CONNECTION ANGLE. REPAIRED IAW HORIZON AIR EA 4-53-567.Oct 12, 1998 · N491US · Fokker F28MK4000SDR QXEA9801499Angle · crackedBETWEEN FRAMES 19976 AND 20075 BETWEEN STRINGERS 36 AND 37 CRACKS ARE NOTED ALONG RIVET LINE FOR VERTICAL STABILIZER CONNECTION ANGLES. REPAIRED IAW HORIZON AIR EA 4-59-567.Oct 12, 1998 · N491US · Fokker F28MK4000SDR QXEA9801495Angle · crackedBACK UP ANGLE AT THE BASE OF THE VERTICAL STABILIZER LEADING EDGE HAS A SMALL CRACK. REPAIRED IAW FOKKER SRM 51-31-01.Oct 12, 1998 · N491US · Fokker F28MK4000SDR DL72S982083Tab · cracked59R FLANGE TAB AT FIN STA 133.8 CRACKED, HORIZONTALLY THROUGH ATTACH BOLT. REF NRC515 MV2. REPAIRED PER MM 55-30-0 FIG 803.Oct 8, 1998 · N421DA · Boeing 727232SDR MWEA98992Rib · crackedFOUND CRACKED RIB ON LEADING EDGE VERTICAL STABILIZER AT STATION ZFS 43 0 RIGHT SIDE. MTC FABRICATED AND INSTALLED NEW RIB.Oct 6, 1998 · N808ME · Doug DC982SDR MWEA98991Rib · crackedFOUND CRACKED RIB ON VERTICAL STABILIZER LEADING EDGE AT STATION ZFS 49 62 RIGHT SIDE. MTC FABRICATED AND INSTALLED NEW RIB.Oct 6, 1998 · N808ME · Doug DC982SDR DHL9871519CAngle · burntAT C-CHECK, AFT FACE OF TAIL CONE ATTACH HOUSING SUPPORT ANGLE IS BURNT AT CENTER TOP. REMOVED AND REPLACED Z ANGLE PER SRM 51-10-1, 24 INCHES LONG. N/R 4059Oct 6, 1998 · N715DH · Boeing 727155CSDR AALA981887Support · chafedTUL - AFT CENTER TENSION TIE SUPPORT LUG ON TOP OF VERTICAL STABILIZER HAS WORN AREA OUTBOARD OF LEFT HOLE. REMOVED CORROSION AND FLAP PEENED PER AARD 55-30-05-2 PAGE 1 AND 2 AND ESO 11697 DATED 8-28-98, TREATED AND PRIMED. (M)Oct 6, 1998 · N883AA · Boeing 727223SDR 98FDEA00637Angle · crackedREPLACED UPPER VERTICAL STAB REAR SPAR BASE ANGLE (CRACKED). REPLACED AMC7279-1 BASE ANGLE WITH AMC727950, BASE ANGLE PER EO 8-5630-7-4303B PT 2.Oct 6, 1998 · Doug DC1010FSDR VJ9800514Skin · chafedVERTICAL SKIN ON LT AND RT UPPER AND LOWER BANANA FAIRING CHAFED. RT UPPER BANANA FAIRING SKIN CHAFED OUT OF LIMIT IAW DC9 SRM 55-01. REMOVED SKIN, FABRICATED AND INSTALLED NEW SKIN IAW DC9 SRM 51-10-4, 51-10-3, 51-30-2 AND 55-01.Sep 28, 1998 · N911VV · Doug DC932SDR UPS98827908Angle · crackedINSPECTION TYPE-C, RT VERT STAB TO EMPENNAGE DRAG ANGLE CRACKED AND CORRODED IN HORIZONTAL LEG LOC APROX 11-14 AFT OF VERT STAB FRONT SPAR. REPAIRED IAW SRM 53-2-5.Sep 25, 1998 · N818UP · Doug DC873FSDR C2XA98IA379Angle · crackedIAH - DURING C-CHECK INSPECTION, FOUND VERTICAL STABILIZER LEFT SIDE DRAG ANGLE CRACKED. MAINTENANCE REMOVED THE DAMAGED FORWARD SECTION AND REPLACED IT IAW CONTINENTAL EXPERSS ENGINEERING CHANGE/REPAIR AUTHORIZATION (ECRA) EC5530-01013. THE AIRCRAFT WAS APPRSep 23, 1998 · N15730 · Emb EMB120RTSDR CALA9801826Fitting · corrodedINSPECTION FOUND TOP OF VERTICAL STABILIZER LT HORIZONTAL HINGE ATTACH FITTINGS CORRODED. THE FITTINGS WERE REMOVED AND REPLACED IAW SRM 51-30-2, 51-30-4, AND ECRA 5550-01033.Sep 19, 1998 · N14788 · Boeing 727232SDR DL72S981957Stringer · crackedSTRINGER 8R WAS FOUND WITH A CRACK THROUGH THE INBD FLANGE AT A RIB ATTACH POINT WHICH PROGRESSED TO THE CENTER OF THE STRINGER WEB. THE CRACK WAS REPAIRED WITH TWO ALUMINUM ANGLES PER ER/A 365679-14, REV A.Sep 17, 1998 · N527DA · Boeing 727232SDR SWAA982120Stiffener · crackedDURING SCHEDULED D CHECK, FOUND CRACKED STIFFENER ON RT VERTICAL FIN REAR SPAR AT FIN BS 119.0 IN TRAILING EDGE CAVITY. REPAIRED PER BOEING SRM.Sep 16, 1998 · N341SW · Boeing 7373H4SDR CALA9801769Angle · crackedINSPECTION FOUND A .25 INCH CRACK IN VERTICAL STABILIZER FORWARD RT DORSAL FIN ATTACH ANGLE. THE ANGLE WAS REMOVED AND REPLACED IAW EA 5340-01012.Sep 15, 1998 · N93738 · Boeing 727224SDR CA980922020Skin · cracked(CAN) BEACON CIRCUIT BREAKER TRIPPED. WATER INFILTRATING THE FRONT TOP END OF THE VERTICAL STABILIZER, AND RUNNING INTO POWER PACK IN THE BEACON. THE BEACON IS MOUNTED ON THE FIN TIP. THIS WAS ORIGINALLY USED FOR AN ADF ANTENNA INSTALLATION ALSO BUT WAS NO LSep 10, 1998 · Piper PA31SDR CALA9801651Bracket · crackedINSPECTION FOUND CRACKED BRACKETS AT LT LOWER VERTICAL STABILIZER FRONT SPAR FITTING AT FS 1218 AND STA 1228. THE CRACKS WERE 1.5 AND 1 INCH LONG. ANGLES WERE INSTALLED AT BOTH LOCATIONS IAW SRM 51-40-3, FIGURE 1 AND MM 51-20-11.Sep 8, 1998 · N14788 · Boeing 727232
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