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 RRXA991061Fitting · misdrilledDURING A MAINTENANCE VISIT FOUND OVERSIZED HOLE, RUDDER SPAR FITTING AT STA ZR 61.156 HAS OVERSIZED ATTACH HOLE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW OVERSIZED BUSHING IAW FAA AFeb 3, 1999 · N105WP · Doug DC873SDR TSAA9951050Spar · corrodedPOSSIBLE REAR SPAR CORROSION AT APPROXIMATELY RS 136.00 VERTICAL STABILIZER RIGHT HAND SIDE. REPAIRED PER ECO 2509R5 PART 2. TAT: 47,785.0 HOURS. TAC: 63,219. (X)Jan 19, 1999 · N809AL · Boeing 7372Q9SDR TSAA9951049Spar · corrodedPOSSIBLE REAR SPAR CORROSION AT APPROXIMATELY RS 156.00 VERTICAL STABILIZER RIGHT HAND SIDE. REPAIRED PER ECO 2509R5 PART 2. TAT: 47,785.0 HOURS. TAC: 63,219. (X)Jan 19, 1999 · N809AL · Boeing 7372Q9SDR AALA982062Spar · corrodedTUL - HORIZ STABILIZER FRONT SPAR CENTER SECTION LEFT UPPER AND LEFT LOWER 'A' FRAME ATTACH LUGS CORRODED. REPAIRED PER ESO 11697, DATED 10/15/98. (M)Nov 4, 1998 · N880AA · Boeing 727223SDR GAIA98106Chord · corrosionTHE FOLLOWING ITEM WAS INITIAL LEVEL 2 CORROSION FOUND DURING A HEAVY C-CHECK. LEFT STABILIZER, UPPER TRAILING EDGE CHORD HAS SEVERAL AREAS OF CORROSION. REMOVED DAMAGED T/E UPPER CHORD, PER 727 SRM 51-30-2. (M)Oct 23, 1998 · N6834 · Boeing 727223SDR UPS98828130Rib · crackedINSPECTION TYPE-C3, VERTICAL STAB L/E RIB AT ZFS 223 IS CRACKED AT THE LT AFT END. STOPPED DRILLED CRACK AND REPAIRED RIB IAW SRM 55-2-0.Oct 21, 1998 · N779UP · Doug DC871FSDR AU981594Spar · cracked(AUS) VERTICAL FIN REAR SPAR CRACKED UNDER DOUBLERS AS INDICATED IN CESSNA SE-80-85.Oct 18, 1998 · Cessna 180KSDR AU981397Spar · corroded(AUS) FIN STRUCTURE EXTENSIVELY CORRODED. FORWARD ATTACHMENT POINT, REAR SPAR AND LOWER RIB AS WELL AS THE INNER SKIN AND UPPER FIN STRUCTURE CORRODED.Oct 16, 1998 · Piper PA36375SDR MWEA98995Rib · crackedFOUND CRACKED RIB ON LEADING EDGE OF VERTICAL STABILIZER AT STATION ZFS 49 62 LEFT SIDE. MTC FABRICATED AND INSTALLED NEW RIB.Oct 6, 1998 · N808ME · Doug DC982SDR MWEA98994Rib · crackedFOUND CRACKED RIB ON LEADING EDGE OF VERTICAL STABILIZER AT STATION ZFS 430 LEFT SIDE. MTC FABRICATED AND INSTALLED NEW RIB.Oct 6, 1998 · N808ME · Doug DC982SDR MWEA98993Rib · crackedFOUND CRACKED RIB ON LEADING EDGE VERTICAL STABILIZER AT STATION ZFS 30 0 RIGHT SIDE. MTC FABRICATED AND INSTALLED NEW RIB.Oct 6, 1998 · N808ME · Doug DC982SDR EIAA980309Spar · corrodedPHX - DURING C-CHECK, VERTICAL STABILIZER REAR SPAR LEFT AND RIGHT AFT CHORD HAS CORROSION FROM ZRS .5 TO ZRS154. OUT OF LIMITS AT ZRS 112. NRC N062, N063. REPAIRED PER EA DC9-55-013 AND ECRA 935-51-038-1. (M)Oct 2, 1998 · N935F · Doug DC932FSDR AU981246Rib · cracked(AUS) VERTICAL STABILIZER RIB CRACKED IN FOUR PLACES. ONE OF THE CRACKS WAS IN A PREVIOUS REPAIR. PART TC: 2,294.Sep 24, 1998 · Gulstm 112SDR TSAA9833550Spar · corrodedVERTICAL STABILIZER REAR SPAR SKIN BULGING DUE TO CORROSION. REPAIR PER ECO 2509 R5. AIRCRAFT RETURNED TO SERVICE. (M)Sep 21, 1998 · N805AL · Boeing 7372M6CSDR TSAA9833549Spar · corrodedVERTICAL STABILIZER REAR SPAR SHOWS SIGNS OF EXFOLIATION. REPAIRED PER ECO 2509 R5. AIRCRAFT RETURNED TO SERVICE. (M)Sep 21, 1998 · N805AL · Boeing 7372M6CSDR UPS98227732Rib · corrodedINSPECTION TYPE:D TENSION TIE RIB FWD AND AFT VERTICAL HOLES ARE PITTED. REPAIR CARRIED OUT IAW SRS EO 98-27-021 ENGINEERING FILE NO 727-55-0374.Sep 10, 1998 · N934UP · Boeing 72721CSDR UPS98227731Rib · corrodedINSPECTION TYPE:D TENSION TIE RIB ATTACH FITTINGS FWD AND AFT VERTICAL HOLES HAVE PITTING CORROSION. REPAIR CARRIED OUT IAW SRS EO 98-27-021 ENGINEERING FILE NR 727-55-0374.Sep 10, 1998 · N934UP · Boeing 72721CSDR CALA9801681Spar · crackedINSPECTION FOUND A 1.5 CRACK IN BRACKET AT RT LOWER VERTICAL STABILIZER FRONT SPAR, FS 1218 AN ANGLE WAS INSTALLED IAW SRM 51-40-3, FIGURE 1 AND MM 51-20-11.Sep 9, 1998 · N14788 · Boeing 727232SDR AALA981762Rib · crackedTUL - FOUND STRINGER NR 3 CRACKED RIGHT SIDE OF VERTICAL 1ST RIB BELOW ACCESS PANEL VERT INTERIOR. STOP DRILLED CRACK AND INSTALLED REPAIR PER SRM 55-30-4, PAGE 6 FIG 1. (M)Sep 3, 1998 · N720AA · Boeing 727227SDR AALA981761Rib · crackedTUL - STRINGER NR 1 CRACKED RIGHT SIDE OF VERTICAL, FIRST RIB BELOW ACCESS INTERIOR OF VERTICAL. STOP DRILLED CRACK AND INSTALLED REPAIR PER SRM 55-30-4, PAGE 5 FIG 1. (M)Sep 3, 1998 · N720AA · Boeing 727227SDR AU981121Spar · corroded(AUS) VERTICAL STABILIZER SPAR CORRODED.Aug 28, 1998 · Beech E55SDR ABXA9800796Rib · crackedDURING C-CHECK, FOUND RIB CRACKED IN THE VERTICAL STABILIZER LEADING EDGE. REPLACED RIB IAW DC9 SRM CHAPTERS 51-30-2 AND 51-30-5.Aug 7, 1998 · N975AX · Doug DC941SDR AU981111Spar · corroded(AUS) FIN POST SUSPECT INTERNAL CORROSION. WATER CAN ENTER THE POST VIA THE TRIM TAB CONTROL CONDUIT. AIRCRAFT OPERATES AS A FLOAT PLANE. PART TC: 390.Jul 18, 1998 · Maule M7235SDR MWEA98627Rib · crackedFOUND CRACK ON VERTICAL STABILIZER RIB AT STATION ZFS 4.750. MAINTENANCE FABRICATED AND INSTALLED NEW RIB.May 29, 1998 · N809ME · Doug DC982SDR QXEA9800812Spar · gougedVERTICAL STABILIZER AFT SPAR UPPER RADIUS ROD FITTING LOWER LUG INSIDE FACE GOUGED. REPAIRED IAW DHC 51-20-00, 51-20-16 AND 51-20-26.May 27, 1998 · N820PH · Dhav DHC8102SDR ARWA980493Spar Cap · corrodedDURING D-CHECK, FOUND VERTICAL STABILIZER, REAR SPAR CAP, LEFT AND RIGHT SIDE HAS CORROSION AT STATION 161. REMVOED CORROSION IN AREA. FABRICATED REPAIR DOUBLERS AND INSTALLED IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, ACTION NR 35887, FILE NR 98-01-005. Apr 24, 1998 · N791AL · Doug DC862SDR ARWA980490Spar Cap · corrodedDURING D-CHECK, FOUND VERTICAL STABILIZER REAR SPAR CAP LEFT HAND HAS CORROSION. REMOVED SECTION OF SPAR CAP. MACHINED NEW SECTION OF SPAR CAP AND INSTALLED IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, DRAWING NR 5611409 AND SRM 51-1-21. WORK ACCOMPLISHED UApr 24, 1998 · N791AL · Doug DC862SDR CALA9800677Spar · corrodedINSPECTION FOUND VERTICAL STABILIZER FRONT SPAR FIN STA 87 TO 100 CORRODED ON RT SIDE. THE CORRODED AREA WAS CUT OUT, A REPAIR ANGLE AND STRAP WERE FABRICATED AND INSTALLED IAW ENGINEERING ORDER 98-833.Apr 17, 1998 · N15781 · Boeing 727232SDR AU980368Spar · cracked(AUS) VERTICAL STABILIZER REAR SPAR CRACKED BETWEEN TOP AND BOTTOM ATTACHMENT BOLTS. SPAR HAD PREVIOUSLY BEEN CRACKED AND STOP DRILLED WITH CRACKING NOW CONTINUING PAST THE STOP DRILL HOLES. CRACK LENGTHS APPROXIMATELY 12.7MM (0.5 INCH). PART TC: 2,150.Mar 23, 1998 · Cessna A188BSDR CALA9800549Rib · crackedINSPECTION FOUND A .25 INCH CRACK IN VERTICAL STABILIZER NR 6 RIB AT STRINGER 3L. THE CRACK WAS STOP DRILLED, DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 55-30-4, 51-10-6, AND 51-30-2.Mar 19, 1998 · N73751 · Boeing 727227SDR CALA9800548Rib · wornINSPECTION FOUND VERTICAL STABILIZER NR 7 RIB WORN AT STRINGER 2R. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 55-30-4, 51-10-6, AND 51-30-2.Mar 19, 1998 · N73751 · Boeing 727227SDR DL72S980349Rib · crackedVERTICAL STAB RIB CHORD CRACKED AT FASTENER HOLE, FIN STA 157.2 AND STR 9 RT, FOUND ON E-2 LETTER CHECK. INSTALLED DOUBLER PER M/M 55-30-3 NR 2.Feb 9, 1998 · N528DA · Boeing 727232SDR UPS98225711Rib · corrodedINSPECTION TYPE-SI, FRETTING CORROSION ON VERTICAL STAB L/E FAIRING RIB, FWD LIP AT FIN STA 55.9. RECEIVED NEW TEE-EXTRUDED RIB AND INSTALLED WEB TO NEW RIB PER 727 SRM 51-30-2.Feb 2, 1998 · N214UP · Boeing 7272A1SDR AU980142Stabilizer · corroded(AUS) VERTICAL STABILIZER SEVERELY CORRODED. FORWARD SPAR CORRODEDTHROUGH.Jan 30, 1998 · Cessna 182HSDR UPS98825838Spar · corrodedINSPECTION TYPE:D CHECK VERTICAL STABILIZER 5 LEFT FRONT SPAR CORRODED STA 1700-1740 FROM LONGERON 9 LEFT TO 18 LEFT ( AFT CABIN). REMOVED CORROSION IAW 51-1-8 TIMCO RFTS ENGINEERING DISPOSITION ALODINED AND PRIMED IAW DC8 SRM 51-1-8.Jan 23, 1998 · N703UP · Doug DC871FSDR UPS98825837Spar · corrodedINSPECTION TYPE:D, CK VERTICAL STABILIZER FRONT SPAR CORRODED STA 1730 AT LONGERON 11 RIGHT. REMOVED CORROSION FROM FRONT SPAR OF VERTICAL STABILIZER IAW DC8 SRM 51-1-8 ALODINED AND PRIMED AREA IAW DC8 SRM 51-1-8.Jan 23, 1998 · N703UP · Doug DC871FSDR UPS98825830Spar · corrodedINSPECTION TYPE:D CHECK, VERTICAL STABILIZER FRONT SPAR LOWER CAP CORRODED STA 1750 FROM X 10 TO X 30. REMOVED CORROSION FROM VERTICAL STAB FRONT SPAR LOWER CAP AT FS 1750 FROM X30 TO X10 IAW DC8 SRM 51-1-8. ALODINED AND PRIMED AREA IAW DC 8 SRM 51-1-8Jan 23, 1998 · N703UP · Doug DC871FSDR 98FDEA00055Spar · crackedUPPER VERT STAB REAR SPAR HAS TWO CRACKS AT LT O/B HI-LOK HOLE, .75 INCH LONG GOING OUT OF THE HI-LOK HOLE AND A .625 INCH LONG GOING TANGENT WITH ANGLE RADIUS. CRACKED BASE ANGLE ON CONDITION II PER EO 8-5530-7-4303. REMOVED CRACKED ANGLE, INSTALLED NEW ANGJan 22, 1998 · Doug DC1010FSDR USAA990002Former · crackedPIT - DURING C-4 CHECK, FOUND VERTICAL STABILIZER L/E FORMERS CRACKED ON AFT ENDS. SEE EA 49052 FOR DETAILS. REPLACED FORMERS ON VERTICAL STAB PER EA 49052. (M)Jan 8, 1998 · N803US · Doug DC981SDR 97FDEA00894Spar · corrodedNR 0970 054 CORROSION ON VERTICAL STABILIZER INTER SPAR SKIN BS 1340 - 1344, LBL 18, WL 260.Dec 19, 1997 · N146FE · Boeing 72727CSDR 97FDEA00847Spar Web · corrodedNR 0952 039 CORROSION (C53-395-11) ON VERTICAL STABILIZER INTER SPAR SKIN BS 1340 - 1344, RBL 18, WL 260. REPAIRED CORROSION ON RT INNER SPAR SKIN OF VERT STAB BS 1340-1344, RBL 18, WL 260 IAW FED-EX EA NR 75510-37338 AND FED-EX EA NR 7-5330-37334.Nov 20, 1997 · N146FE · Boeing 72727CSDR 97FDEA00846Spar Chord · corrodedNR 0949 038 WHILE WORKING (FEDEX CARD NR 0652) FOUND LT REAR VERTICAL SPAR CORRODED AT BS 1342. REMOVED AND REPLACED SECTION OF THE LT VERTICAL SPAR CHORD BS 1342, FIN STA 0.00 TO FIN STA 99.0 IAW FED-EX EA NR 7-5530-37380.Nov 20, 1997 · N146FE · Boeing 72727CSDR 97ZZZX5104Spar · crackedVERTICAL FIN SPAR CRACKED ON BOTH SIDES RIGHT BEHIND TOP RUDDER HINGE. CRACKS MEASURE CLOSE TO .75 INCH ON BOTH SIDES. VERTICAL FIN NOT DISTORTED AND RUDDER HINGE SHOWS NO DAMAGE. CAUSE OF CRACKS UNKNOWN.Nov 17, 1997 · N691DB · Cessna 177RGSDR DL72S972249Rib · crackedFOUND DURING D-2 LETTER CHECK - VERTICAL FIN RIB CRACKED AT RIB TO STRINGER ATTACH BOLT FIN STA 133.8 R/H SIDE 5TH \ATRINGER UP FROM BOTTOM REPAIRED PER M/M 55-30-0Nov 4, 1997 · N421DA · Boeing 727232SDR UPS97224762Spar Chord · corrodedINSPECTION TYPE:SI CORROSION ON MIDSPAR ON LT VERTICAL STAB BEHIND PANEL 9601 LOCATION CORROSION REWORK OUT OF LIMITS IAW SRM 55-30-1. REPAIRED LT MIDSPAR BEHIND PANEL 9601 IAW TRAMCO/BFG EWO 97-2621 UPS FILE NR 727-55-0358.Oct 22, 1997 · N903UP · Boeing 72751CSDR UPS97224808Spar · corrodedINSPECTION TYPE:SI CORROSION (C55-300-01.00-01) ON MID SPAR ON RT VERTICAL STAB BEHIND PANEL 9602 LOCATION. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 55-30-1 REMOVED AND REPLACED ANGLE PER EO 97-26-21 (727-55-0358).Oct 10, 1997 · N903UP · Boeing 72751CSDR DL72S972065Rib · crackedRIB CRACKED 5TH FROM BOTTOM SPAR, LT SIDE, 2ND CANTED BLKHD INTERIOR VERT STAB. FABRICATED REPAIR DOUBLER AND INSTALLED PER M/M 55-30-0 FIG 802.Sep 30, 1997 · N546DA · Boeing 727232SDR DL72S972064Rib · brokenRIBS BROKEN LT SIDE NR 4 AND 5 RIBS BROKEN FROM REAR SPAR 3RD CANTED BLKHEAD AFT OF ACCESS INTERIOR VERTICAL STAB. REMOVED ATTACH BOLTS AND BROKEN PIECES FOR FURTHER EVALUATION. FABRICATED ANGLE DOUBLER FOR STRINGER NR 4. FABRICATED STRINGER CLIP FOR NR 4 ASep 30, 1997 · N546DA · Boeing 727232SDR HEEA0010986Spar · damagedR/H SIDE OF SPAR 1/8" SHORTER THAN EXISTING SPAR. DAMAGE TOP L/H RADIUS AS MARKED IN RED.Sep 9, 1997 · Bell 412SDR HEEA0010985Spar · damagedR/H SIDE OF SPAR 1/8" SHORTER THAN EXISTING SPAR. DAMAGE TOP L/H RADIUSSep 9, 1997 · Bell 412
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