JASC 5531

Service difficulty reports · 1,234

Reports filed under 5531 · Vertical Stabilizer, Spar/Rib, 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 = '5531'
  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 UPS96220940Rib · crackedINSPECTION TYPE-C, FS 135 AND FIN STA 22.5 RT RIB IS CRACKED. CUT OUT DAMAGED AREA PER SRM 51-40-3, FAB'D AND INSTALLED ANGLE DOUBLER PER SRM 51-40-3 AND 51-30-2.Jul 8, 1996 · N951UP · Boeing 72725CSDR TSAA9655052Rear Spar · corrodedDURING HEAVY MAINTENANCE VISIT, FOUND EXFOLIATION ON RIGHT VERTICAL STABILIZER REAR SPAR AT FS 67 TO 83. REPAIRED PER ECO 2509R2. AIRCRAFT RETURNED TO SERVICE. (M)Jun 24, 1996 · N804AL · Boeing 7372Q9SDR DHL9672165CSpar Web · gougedAT C-CHECK, VERTICAL STAB HAS GOUGES ON FWD SPAR WEB RT TENSION TIE BEAM. INSTALLED WEB REPAIR PER SRM 51-40-2, 4 BY 3.Jun 7, 1996 · N721DH · Boeing 727228SDR UPS96220537Mid Spar · corrodedINSPECTION TYPE SI, CORROSION VERTICAL FIN MID SPAR CHORD IS CHAFED AND FRETTING AT ACCESS PANEL 9601. REMOVED CORROSION FOUND TO BE OUT OF LIMITS, FABRICATED REPAIR PARTS AND INSTALLED ON A/C IAW SRM 51-30-2 AND EWO 96-2334.May 29, 1996 · N929UP · Boeing 72722CSDR UPS96220536Mid Spar · corrodedINSPECTION TYPE SI, RT VERT FIN MID SPAR CHORD IS CHAFED AND FRETTING AT ACCESS PANEL 9602. REMOVED CORROSION FOUND OUT OF LIMITS, FABRICATED REPAIR PARTS AND INSTALLED ON A/C SRM 51-30-2 EWO 96-2333.May 29, 1996 · N929UP · Boeing 72722CSDR 97ZZZX2657Rib · corrodedDURING ANNUAL INSPECTION OF AIRCRAFT, FOUND CORROSION ON RIB AT BASE OF VERTICAL STABILIZER. FORWARD 6 INCHES OF RIB WAS COMPLETELY DELAMINATED. AIRCRAFT HAD BEEN ON FLOATS IN SALT WATER ENVIRONMENT. REST OF AIRCRAFT IN GOOD CONDITION.May 5, 1996 · N6964N · Cessna A185FSDR AALA960586Spar · crackedTUL - FOUND CRACK IN FWD VERT STAB LEFT SPAR LEG ON AFT SIDE OF STATION 1388 CANT FRAME IN AFT ACCY. STOP DRILLED CRACK MANUFACTURED DOUBLER AND INSTALLED PER ESO 80559, DATED 4-12-96. (M)Apr 12, 1996 · N294AA · Doug DC982SDR UPS96220048Forging · crackedINSPECTION TYPE C-NFEC, DET A CRACK ON RT SIDE OF VERT STAB FRONT SPAR FORGING AT 1ST HOLE OF STA 1233 BOTTOM ROW OF FASTENERS. CRACK IS 1 INCH LONG AND RUNS A FT OF HOLE. STOP DRILLED CRACK, REPAIRED PER DRAWING 65-62346 AND SRM 51-30-2.Apr 10, 1996 · N948UP · Boeing 72725CSDR UPS96206009Spar Skin · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED BS 1342 RT INTERSPAR SKIN IS CORRODED BEYOND LIMITS AT TERMINAL FITTING. CUT OUT DAMAGED AREA, FAB AND INSTALLED REPAIR PARTS IAW BAC DRWG 65C29055 AND SRM 51-30-2.Mar 22, 1996 · N948UP · Boeing 72727CSDR UPS96206008Spar Skin · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED BS 1342 LT INTERSPAR SKIN IS CORRODED BEYOND LIMITS. CUTOUT DAMAGED AREA, FAB AND INSTALLED REPAIR PARTS IAW BAC DRWG 65C29055.Mar 22, 1996 · N948UP · Boeing 72727CSDR CA960327010Rear Spar · cracked(CAN)DURING AN INSPECTION THE RUDDER SPAR AND ONE DOUBLER WAS FOUND STARTING TO CRACK BETWEEN THE FIRST AND SECOND BOLTS LOCATED AT THE BOTTOM OF THE SPAR.Mar 18, 1996 · Cessna A185FSDR 96FDEA00550Fitting · corrodedCORROSION (C53-137-01) BS 1342 RBL 17 STR 5R ON FITTING ANGLE. REMOVED CORRODED TERMINAL FITTING AND INSTALLED NEW RT SPAR TERMINAL FITTING ON VERTICAL STABILIZER AT BS 1342 IAW BOEING SB 727-55-088.Mar 11, 1996 · N194FE · Boeing 72722SDR 96FDEA00407Mid Spar · wornVERTICAL FIN MID SPAR, STR 7 AND PANEL SUPPORT HAS WORN FASTENER HOLE AT FIN STA 225.707 RT. REPAIRED PER FEDEX EA 7-5510-27728.Mar 5, 1996 · N194FE · Boeing 72722SDR 96FDEA00378Mid Spar · wornVERTICAL FIN MID SPAR, STR 7 AND PANEL SUPPORT HAS WORN FASTENER HOLE AT FIN STA 225.707 LT. REPAIRED PER FEDEX EA 7-5510-27728.Feb 28, 1996 · N194FE · Boeing 72722SDR ABXA9600351Rib · crackedDURING C-CHECK INSPECTION, FOUND THE VERTICAL STABILIZER TOP LEADING EDGE HAD A CRACKED LEFT RIB BELOW PANEL 6307. REPAIRED IAW DC-9 SUPP SRM DRAWING K05159.Feb 26, 1996 · N941AX · Doug DC931SDR 96ZZZX1820Spar Web · corrodedMAJOR INSPECTION FOUND VERTICAL STABILIZER SPAR WEB DOUBLER WITH INTERGRANULAR CORROSION. DOUBLER WAS REPLACED.Feb 26, 1996 · N1547N · Skrsky S76ASDR 96ZZZX1819Rib · corrodedMAJOR INSPECTION FOUND VERTICAL STABILIZER RIB WITH INTERGRANULAR CORROSION. RIB WAS REPLACED.Feb 26, 1996 · N1547N · Skrsky S76ASDR ABXA9600353Rib · crackedDURING C-CHECK INSPECTION, FOUND THE VERTICAL STABILIZER LEADING EDGE RIB CRACKED. REPAIRED IAW DC-9 SUPP SRM DRAWING K05159.Feb 23, 1996 · N941AX · Doug DC931SDR ABXA9600352Rib · crackedDURING C-CHECK INSPECTION, FOUND THE VERTICAL STABILIZER LEADING EDGE RIB CRACKED. REPAIRED IAW DC-9 SUPPLEMENTAL SRM DRAWING K05159.Feb 23, 1996 · N941AX · Doug DC931SDR ABXA9600350Rib · crackedDURING C-CHECK INSPECTION, FOUND VERTICAL STABILIZER LEADING EDGE RIB CRACKED. REPAIRED IAW DC-9 SUPP SRM DRAWING K05498.Feb 19, 1996 · N941AX · Doug DC931SDR ABXA9600349Rib · crackedDURING C-CHECK INSPECTION, FOUND VERTICAL STABILIZER LEADING EDGE RIB CRACKED. REPAIRED IAW DC-9 SUPP SRM DRAWING K05159.Feb 19, 1996 · N941AX · Doug DC931SDR ABXA9600348Rib · crackedDURING C-CHECK INSPECTION, FOUND VERTICAL STABILIZER LEADING EDGE RIB CRACKED. REPAIRED IAW DC-9 SUPP SRM DRAWING K05498.Feb 19, 1996 · N941AX · Doug DC931SDR 9606519605Spar Web · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE VERTICAL STABILIZER AFT SPAR WEB AT ZRS 65 AND 75. REPAIRED WEB (P/N 9911834-175) PER EA 99-108802.Feb 12, 1996 · N605NW · Doug DC932SDR UPS96205641Spar · crackedWHILE IN FOR MOD WORK, MAINTENANCE REPORTED FS 1342, THE VERTICAL FIN REAR SPAR CHORD CRACKED. REPAIRED I.A.W. BOEING DWG 69-70556.Jan 17, 1996 · N949UP · Boeing 72725CSDR UPS96205642Rib · crackedWHILE IN FOR MOD WORK, MAINTENANCE REPORTED RT RIB CRACKED BS 1367 FIN STA 22.5. CUT OUT DAMAGE AND REPAIRED WEB I.A.W. SRM 51-40-2.Jan 10, 1996 · N949UP · Boeing 72725CSDR USAA951352Spar · crackedPIT - DURING Q-1/C-3 INSPECTION, FOUND A 3 INCH CRACK, VERTICAL STABILIZER FRONT SPAR AFT OF CANTED FRAME 1388. REMOVED DAMAGED AREA AND INSTALLED REPAIR ANGLES PER SRM 55-02-26. (X)Dec 27, 1995 · N819US · Doug DC981SDR DL72S960393Rib Tab · crackedDURING INSPECTION, STRINGER 8R OF THE VERTICAL STAB. HAS A CRACK ON THE FIN STA. 157.2 RIB ATTACHMENT TAB. THE SUBJECT CRACK RUNS FROM FASTENER HOLE TO EDGE OF TAB. A REPAIR ANGLE WAS INSTALLED IN ACCORDANCE WITH B727 S/B 55-0075.Dec 20, 1995 · N493DA · Boeing 727232SDR SWAA950751Rib · crackedDURING SCHEDULED 1/2 D-CHECK, FOUND VERT STAB 5TH RIB ASSEMBLY CRACKED AT FASTENER HOLE ON LEFT SIDE. REPAIRED PER BOEING M/M.Nov 28, 1995 · N129SW · Boeing 7372T4SDR 95ZZZX7065Closure Rib · corrodedWHILE PERFORMING CPC TASK CARD C55-391-30, THE VERTICAL STABILATOR'S UPPER RT CLOSURE RIB WAS FOUND EXFOLIATED ON ITS OUTBOARD SIDE JUST FORWARD OF THE FORKED END OF THE AFT HINGE POINT FITTING FOR THE HORIZONTAL STABILIZER. CORROSION WAS REMOVED AND FOUND TONov 28, 1995 · N1972 · Boeing 72723SDR EISA95436Rib · crackedINSIDE VERTICAL STAB THROUGH ACCESS PANEL 9504, FOURTH COMPARTMENT UP FROM ENTRANCE, THE EIGHTH RIB FROM THE TOP IS CRACKED. REPAIRED CRACK IN RIB PER SRM 55-30-4. (M)Nov 18, 1995 · N368PA · Boeing 727221SDR UPS804965Rib · crackedWHILE IN FOR D-CHECK, MAINTENANCE FOUND VERTICAL STAB LE LOWER INTERIOR SECTION HAS THE ENDS OF FRAME RIBS CRACKED AT XFS 104.75 LT AND RT, XFS 111.15 AND LT XFS 122.75. STOP DRILLED CRACKS, FABRICATED REPAIR ANGLE AND INSTALLED REPAIR PER SRM 55-2-0 AND 51-1Nov 10, 1995 · N729UP · Doug DC871FSDR UPS804964Rib · crackedWHILE IN FOR D-CHECK, MAINTENANCE FOUND VERTICAL STAB SECTION INTERIOR HAS TWO RIB ENDS CRACKED AT STA ZFS 279 AND ZFS 273. STOP DRILLED CRACK, FABRICATED REPAIR ANGLE AND INSTALLED IAW SRM 55-2-0 AND 51-1-20D.Nov 10, 1995 · N729UP · Doug DC871FSDR UPS204789Spar · corrosionWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON VERTICAL FIN REAR SPAR CHORD, RUDDER STA 223-STA 238 WHERE PANEL 9515 MATES LT SIDE. REMOVED AND INSTALLED FABRICATED PARTS. WORK DONE IAW E.O. B727-5530-7482A.Oct 10, 1995 · N936UP · Boeing 727108CSDR CA951018027Doubler · cracked(CAN)CRACK FOUND DURING INSPECTION ON THE LEFT HAND SIDE OF THE RECESS FOR THE TORQUE TUBE. REFERENCE SB 95-2.Oct 10, 1995 · Cessna A185FSDR UPS204777Spar · corrodedWHILE ON GROUND, MAINTENANCE FOUND CORROSION ON RT SIDE VERT FIN UPPER FLANGE ON FRONT SPAR ENTIRE LENGTH STA 6.372 TO 180.6. CORROSION OUT OF LIMITS, REPAIRED RT SPAR CHORD IAW UPS EO B727-5530-7473-A.Oct 9, 1995 · N936UP · Boeing 727108CSDR UPS204776Spar · corrodedWHILE ON GROUND, MAINTENANCE FOUND CORROSION ON LT SIDE VERTICAL FIN FRONT SPAR FROM FIN STA 108.8 TO 6.372. CORROSION OUT OF LIMITS, REPAIRED LT SPAR CHORD IAW UPS EO B727-5530-7473-A.Oct 9, 1995 · N936UP · Boeing 727108CSDR UPS204763Mid Spar · crackedWHILE ON GROUND, MAINTENANCE FOUND RT VERT FIN MID SPAR UPPER FLANGE HAS BROKEN FASTENER HOLE. REMOVED DAMAGE, FABRICATED, INSTALLED REPAIR ANGLES PER SRM 51-30-2 UPS EO 727-55-0303.Oct 9, 1995 · N936UP · Boeing 727108CSDR 95ZZZX6021Rib · rivets looseRIVETS IN VERTICAL STABILIZER AT RIB TB 10.31.000.103 LOOSENED CAUSING TOP OF STABILIZER TO BE LOOSE.Oct 7, 1995 · N20KP · Socata TB20TRINIDADSDR UPS204599Rib · crackedWHILE IN FOR SI CHECK, MAINTENANCE FOUND LT HORIZ STAB NR 2 T/E SUPPORT RIB, AT ELEV STA 50.05 IS CRACKED ON LOWER SURFACE. REPLACED CRACKED SUPPORT RIB PER SRM 51-30-2, 51-30-5, 51-10-2.Sep 29, 1995 · N936UP · Boeing 727108CSDR DL72S953779Rib · crackedDURING HMV, FOUND ON VERTICAL FIN 4TH RIB DOWN FROM ACCESS HOLE STA 6.372 RIB NR 6 CHORD ANGLE CRACKED AT STR 7 LEFT. REPAIRED PER M/M 55-30-0 PG 802.Sep 20, 1995 · N544DA · Boeing 727232SDR EISA95333Frame · brokenDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, TWO FRAME WEBS WERE FOUND TO BE CRACKED AND BROKEN VSS 1365.5R AND 1387.5R. REMOVED CRACKED AND BROKEN WEBS. FABRICATED AND INSTALLED TWO WEBS IAW B727 SRM 51-40-2. (M)Sep 14, 1995 · N357NE · Boeing 72782SDR DL72S953814Rib · crackedDURING HMV, FOUND VERTICAL FIN INTERIOR STATION 1303 RIB CRACKED AT BOTTOM. DYE CHECKED AND REPAIRED PER SRM 53-10-4.Sep 8, 1995 · N544DA · Boeing 727232SDR DL72S953764Rib · crackedFOUND ON HMV, 4TH RIB DOWN FROM HOLE STA 6 STR 8L CRACKED. FABRICATED REPAIR PER M/M 55-33-0 PG 803.Sep 8, 1995 · N544DA · Boeing 727232SDR HALA95112L/E Ribs · crackedIN C-CHECK, FOUND CRACKS ON VERTICAL STABILIZER LEADING EDGE RIBS ZFS = 142 AND 148, RIGHT LOWER ENDS. REMOVED CRACKED VERTICAL STABILIZER LEADING EDGE RIBS, ZFS = 142 AND 148 PER SRM 53-05-84. FABRICATED, TREATED AND PRIMED REPAIR ANGLES PER SRM 51-10-02, 5Aug 22, 1995 · N601AP · Doug DC951SDR HALA95111Le Ribs · crackedIN C-CHECK, UPON REMOVAL OF VERTICAL STABILIZER LEADING EDGE FOR DPM 119846, 3 ADDITIONAL CRACKS FOUND IN RIBS LEFT SIDE NR 2, NR 7 AND NR 8 FROM BOTTOM. STOP DRILLED CRACKS AND INSTALLED DOUBLER PER SRM 55-02 FIG 19. (M)Aug 22, 1995 · N601AP · Doug DC951SDR DL72S953540Rib · crackedCRACK INSIDE VERTICAL STABILIZER, RIGHT SIDE 4TH BAY UP, 7TH RIB FROM TOP. CRACK FOUND AT HMV, REPAIRED PER MM 53-30-0 PG 802.Aug 17, 1995 · N515DA · Boeing 727232SDR UPS204156Spar Chord · chafedWHILE IN FOR C-CHECK, MAINTENANCE FOUND THE VERTICAL FIN MID SPAR CHORD WAS CHAFED AT ACCESS PANEL 9602 CROSS BRACE, RT. MAINTENANCE REMOVED AND REPAIRED IAW UPS EO 727-55-0292.Aug 16, 1995 · N939UP · Boeing 72727CSDR 96ZZZM447Spar Web · crackDURING C-CHECK, FOUND VERTICAL STABILIZER FORWARD SPAR WEB HAS CRACK AT EXISTING REP OUTBOARD SIDE OF FWD TERMINAL FITTING LEFT AT TOP OUTBOARD LEFT SIDE CABLE PULLEY CASTING UNDER PNL 9707. TWO CRACKS FOUND UPPER CRACK ROUTED OUT PER SRM 51-10-1, LOWER CRACKAug 8, 1995 · N703DH · Boeing 72730CSDR DL72L953311Rib · crackedFOUND ON CV2 CHECK, CRACK FOUND INSIDE VERTICAL STABILIZER, 2 BULKHEADS UP FROM ACCESS HOLE AT LT SIDE 2ND RIB UP. CRACKED AT BOLT ATTACHED TO BULKHEAD. REPAIRED PER M/M 55-30-0 PG 803.Jul 31, 1995 · N505DA · Boeing 727232SDR DL72L953310Rib · crackedFOUND ON CV2 CHECK, CRACK FOUND INSIDE VERTICAL STABILIZER, 2 BULKHEADS UP FROM ACCESS HOLE AT LT SIDE 3RD RIB UP. CRACKED AT RIB TO BULKHEAD ATTACH POINT. REPAIRED PER M/M 55-30-0 FIG 803.Jul 31, 1995 · N505DA · Boeing 727232
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