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 06FDEA1052Rib · corrodedVERTICAL FIN TENSION TIE RIB, LT AFT VERTICAL BOLT HOLE HAS CORROSION. REPAIRED PER FED EX EA 7-5530-99604 MAJOR REPAIRMar 14, 2006 · N488FE · Boeing 727200SDR 06FDEA1051Rib · corrodedN00716 VERTICAL FIN TENSION TIE RIB, R/H AFT VERTICAL BOLT HOLE HAS CORROSION. REPAIRED PER FED EX EA 7-5530-99604 MAJOR REPAIR.Mar 14, 2006 · N488FE · Boeing 727200SDR 06FDEA1050Rib · gougedVERTICAL FIN TENSION TIE RIB, LT FWD VERTICAL BOLT HOLE IS GOUGED. COMING REPAIRED PER FED EX EA 7-5530-99604 MAJOR REPAIR.Mar 14, 2006 · N488FE · Boeing 727200SDR CALA0600084Rib · crackedINSPECTION FOUND A 1 INCH CRACK IN VERTICAL STABILIZER FRAME (T/E HINGE RIB) WHERE RUDDER RIG PIN R-5 GOES THROUGH FEEL AND CENTERING FRAME, FIN STA 142-150. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5530-01445. A DIP WAS ISSUED TO PERFORM AT PERMANENT REPAIR Mar 9, 2006 · N54711 · Boeing 737724SDR GUUA03020601Spar · corrodedAT SCHEDULED ROUTINE MAINTENANCE, VERTICAL FIN AFT RIGHT SPAR ANGLE 3.0 THRU 4.5 INCHES BELOW UPPER HINGE BRACKET SHOWS SIGN OF EXFOLIATION. REMOVED CORRODED MATERIAL, BLENDED AREA AND INSTALLED REINFORCEMENT DOUBLER IN ACCORDANCE WITH FAA APPROVED DATA CONTAMar 2, 2006 · N87550 · Beech 1900DSDR QXEA200600592Spar Cap · damagedVERT STAB DAMAGED, LT SIDE ATTACH FLANGE & SKIN ROLLED 40" BY 34" LONS, VERT RIB 8-9 DEFORMED .250" SPAN WEB ALSO BUCKLED BETWEEN RIB 8-9 LT SIDE, 18" CREASE IN SKIN 2 LOOSE RIVETS OF FWD END OF SKIN STIFFENER, TOP HAT CHANNEL ALSO, 2- .500" CRACKS AT BEND RAFeb 15, 2006 · N417QX · Bombdr DHC8402SDR 06FDEA0619Spar · chafedRT VERT FIN MIDSPAR CHORD CHAFED AT FIN STA 225. REPAIRED PER FED EX EA 7-5530-96609.Feb 9, 2006 · N488FE · Boeing 727227SDR 06FDEA0618Spar · chafedLT VERT FIN MIDSPAR CHORD CHAFED AT FIN STA 225. REPAIRED THE LT VERTICAL FIN MIDSPAR AT FIN STA 225 IAW FED-EX EA 7-5530-96609.Feb 9, 2006 · N488FE · Boeing 727227SDR 06FDEA0242Rib · chafedWHILE WORKING VERTICAL CLOSE FOUND L/E ATTACH RIB AT LEADING EDGE FIN STA 55.8 CHAFED.Jan 17, 2006 · N490FE · Boeing 727200SDR 05FDEA04418Stringer · crackedVERTICAL FIN TUNNEL STR 8 RT CRACKED AT RIB 7. REPAIRED VERTICAL FIN TUNNEL STR 8 RT AT RIB 7 IAW SRM 55-30-4 FIG 1.Dec 27, 2005 · N490FE · Boeing 727227SDR 05FDEA04416Stringer · crackedVERTICAL FIN TUNNEL STR 8RT CRACKED AT RIB 8. REPAIRED STRINGER PER SRM 55-30-4 FIG 1.Dec 27, 2005 · N490FE · Boeing 727227SDR ASAA0510323Clevis · corrodedYXX - FOUND CORROSION ON VERTICAL STABILIZER AFT SPAR LEFT PRIMARY FORWARD CLEVIS FORWARD FACE. FACES MACHINED PER EA 5340-01138. (M)Sep 22, 2005 · N740AS · Boeing 737290CSDR ASAA0510322Clevis · corrodedYXX - FOUND CORROSION ON VERTICAL STABILIZER AFT SPAR RIGHT PRIMARY FORWARD CLEVIS FORWARD FACE. CLEVIS REPLACED PER BOEING DWG 6546575 AND B737-200 SRM 51-30-2 PARAGRAPH 17. (M)Sep 22, 2005 · N740AS · Boeing 737290CSDR ASAA0510321Clevis · corrodedYXX - FOUND CORROSION ON VERTICAL STABILIZER AFT SPAR RIGHT PRIMARY FORWARD CLEVIS AFT FACE. CLEVIS REPLACED PER BOEING DWG 6546575 AND B737-200 SRM 51-30-2 PARAGRAPH 17. (M)Sep 22, 2005 · N740AS · Boeing 737290CSDR ASAA0510320Spar · corrodedYXX - FOUND CORROSION ON VERTICAL STABILIZER AFT SPAR RIGHT PRIMARY AFT CLEVIS FORWARD FACE. CLEVIS REPLACED PER BOEING DWG 65-46572 AND B737-200 SRM 51-30-2. (M)Sep 22, 2005 · N740AS · Boeing 737290CSDR ASAA0510319Clevis · corrodedYXX - FOUND CORROSION ON VERTICAL STABILIZER AFT SPAR RIGHT PRIMARY AFT CLEVIS AFT FACE. CLEVIS REPLACED PER EA 5340-01137. (M)Sep 22, 2005 · N740AS · Boeing 737290CSDR 05FDEA01612Stringer · crackedCRACKED STRINGER INSIDE VERTICAL STAB AT STRINGER 7 FIN STATION 157.2 LT. REPAIRED STRINGER PER SRM 55-30-4 FIG 1.Jun 16, 2005 · N477FE · Boeing 727200SDR DHL2005784510Rib · wornVERT STAB L/E PNL NR 9501 UPPER FORMER RIB IS WORN FIN STA 87. DAMAGED AREA FOUND TO BE OUT OF LIMITS IAW B727 SRM 55-30-1. REPAIRED IAW B727 SRM.May 17, 2005 · N784DH · Boeing 727227SDR DHL2005741540Stringer · crackedVERT STAB FIN STA 180 STRGR 8LT IS CRACKED AT FRAME ATTACH BOLT. REMOVED FASTENERS IN VERTICAL STAB FIN STA 180 STR 8LT IAW B727 SRM 51-30-2. CUT OUT DAMAGED AREA 2.0625 X 1.0625 IAW B727 55-30-5 FIG 1. FABRICATED REPAIR PARTS AS FOLLOWS FILLER FROM FROM 70Apr 21, 2005 · N741DH · Boeing 7272Q9SDR DHL2005740500Stringer · crackedVERT STAB FIN STA 157 STRINGER 8 LEFT IS CRACKED AT FRAME ATTACH BOLT. REMOVED FASTENERS FOR ACCESS AT VERT STAB FIN STA 157 S-8 LT AND TRIM OUT DAMAGED AREA SIZE 3 1/2" BY 3" IAW B727 SRM 55-30-4 FIG 1. FABRICATED REPAIR PARTS FILLER BAC 1517-1363 7075-T651Apr 21, 2005 · N740DH · Boeing 7272Q9SDR CA050414012Frame · crackedSMALL CRACKS AND LOOSE RIVETS FOUND IN FRAME AS PER SB 218 TWIN COMMANDER KIT CK175-1 INSTALLED.Apr 14, 2005 · Gulstm 690SDR 05FDEA00920Rib · chafedVERTICAL STAB T/E CAVITY RIB WEB IS CHAFED AT UPPER SURFACE, FIN STA 180, 5 RBL, THROUGH ACCESS PNL 9510. REPAIRED THE CHAFED RIB WEB, VERTICAL STAB T/E CAVITY AT UPPER SURFACE FIN STA 180, 5 RBL IAW FEDEX EA 7-5530-86275.Apr 10, 2005 · N272FE · Boeing 727200SDR 05FDEA00830Rib · corrodedVERTICAL STAB RT SIDE 6" BELOW RIB 21 TO RIB 1 HAS CORROSION ON REAR CHORD SPAR CHORD FLANGE IN FASTERNER HOLES, AROUND FASTERNER HOLE AREA EXTENDING TO STAB SKIN AS MARKED. REMOVED NUPLATES IAW A310-200 SRM 51-40-21. REMOVED CORROSION IAW A310-200 SRM 51-74Apr 4, 2005 · N419FE · Airbus A310SDR DHL2005740507Stringer · crackedVERT STAB FIN STA 180 STRINGER S-8 LT IS CRACKED AT FRAME ATTACH SCREW. REMOVED FASTENERS FOR ACCESS AT VERT STAB FIN STA 180 S-8 LT AND TRIMMED OUT DAMAGED AREA SIZE 3 1/2 INCH BY 3 INCH IAW B727 SRM 55-30-4 FIG1. FABRICATED REPAIR PARTS P/N BAC 1517-1367 7Mar 29, 2005 · N740DH · Boeing 7272Q9SDR UPS05844258Rib · crackedC2 VER. FIN L/E HAS CRACKED RIB 3/4 INCH AT ACCESS PNL 51I. STOP DRILLED CRACK IAW DC-8 SRM 55-02-00. REPAIRED RIB IAW 55-02-00, 51 -1-20D, AND 51-3-0.Mar 21, 2005 · N819UP · Doug DC873FSDR UPS05844251Rib · crackedINSPECTION TYPE: C2, VERTICAL FIN L/E HAS CRACKED RIB .75 INCH AT ACCESS PNL 51F. REPAIRED VERTICAL FIN RIB IAW DC-8 SRM 55-02-00 FIG 002 AND SRM 51-1-20D.Mar 21, 2005 · N819UP · Doug DC873FSDR C2XA05TY028Fitting · corrodedTYS, DURING A SCHEDULED INSPECTION FRAME 75, SPAR 1 FITTING SHOWS SIGNS OF FRETTING. MAINTENANCE REMOVED THE FITTING, BLENDED CORROSION ON INNER SKIN SURFACE, DYE PENATRANT TESTED THE AREA, TREATED FOR CORROSION, DRILLED AND INSTALLED A NEW FITTING IAW EC5310Mar 20, 2005 · N15941 · Emb EMB145ERSDR DHL2005782546Stringer · crackedVERT STAB STR 8L CRACKED AT FIN STA 180.6. REMOVED FASTENERS CUT OUT DAMAGED AREA FABBED NEW STIFFENER FROM BAC 1517-1367 PO NR 501953 DIM 4 5/8" BY 3" SPLICE FROM AND 10133-1401 PO NR 501952 DIM 19 1/8" BY 2" SPLICE FROM AND 10134-1201 PO NR 501952 DIM 19 1/Mar 18, 2005 · N782DH · Boeing 727227SDR HDS0315051Frame · crackedTHIS IS TO REPORT CRACKS IN THE FRAMES ON THE VERTICAL FIN, IN THE AREAS AT WL 2145.0 AND 2520.0. THESE CRACKS ARE OCCURRING APPROXIMATELY BETWEEN FS 9350.0 TO 9850.0. (SW19200508005) (K)Mar 16, 2005 · N521RC · Agusta A119SDR DHL2005782547Stringer · crackedVERT STAB STR 6L CRACKED AT FIN STA 180.6. REMOVED FASTENERS CUT OUT DAMAGED AREA FABBED NEW STIFFENER FROM BAC 1517-1367 PO NR 501953 DIM 5 1/8" BY 3 INCH SPLICE FROM AND 10133-1401 PO NR 501952 DIM 21 3/8" BY 2" SPLICE FROM AND 10134-1201 PO NR 501952 DIM 2Mar 16, 2005 · N782DH · Boeing 727227SDR DHL2005782542Stringer · crackedSTRINGER 9R CRACKED AT FIN STA 157.2 INSIDE VERTICAL FIN. REMOVED FASTENERS CUT OUT DAMAGED AREA FABBED NEW STIFFENER FROM BAC 1517-1387 PO NR 501953 DIM 4 3/8 INCH BY 3 INCH SPLICE FROM AND 10133-1401 PO NR 501952 DIM 17 3/8" BY 2" SPLICE FROM AND 10134-1201Mar 14, 2005 · N782DH · Boeing 727227SDR SWAA050776Beam · crackedDURING SCHEDULED D-CHECK, FOUND RT VERTICAL FIN T/E BEAM CRACKED 4 BELOW NR 1 RUDDER HINGE. REMOVED AND REPLACED BEAM SECTION PER SRM.Mar 14, 2005 · N605SW · Boeing 7373H4SDR CA050225007Rib · cracked(CAN) VERTICAL RIB WAS REMOVED FOR RIB REPLACEMENT. ONCE FIN WAS REMOVED, FORWARD RIB WAS FOUND TO HAVE 2 CRACKS IN THE REAR 90 DEGREE BEND. CRACKS ORIGINATE FROM LT AND RT RADIUS CUTS AND GO ALONG THE BEND RADIUS. LT CRACK IS A HALF AN INCH LONG AND THE RT CFeb 24, 2005 · Piper PA60600SDR DHL2005781560Clip · crackedDURING C-CHECK, VERT STAB FIN STA 157 AT STR 9 LT HAS 2 FRAME CLIPS CRACKED. REMOVED FRAME CLIP BS 157 STR 9 LT IAW B727 SRM 51-30-2. FABRICATED (2 EA) FRAME CLIP MATERIAL USED 7075T6 .050 PO NR 9001777 DIM .750 BY 2.50 BY 5 INCHES IAW B727 SRM 55-30-2 FIG 2Feb 24, 2005 · N781DH · Boeing 727227SDR DHL2005781559Frame · crackedDURING C-CHECK, VERT STAB FIN STA 133 AT STR 9LT HAS 1 FRAME CLIP CRACKED. REMOVED FRAME CLIP AT VERT STAB FIN STA 133 AT STR 9 LT IAW B727 SRM 51-30-2. FABRICATED NEW CLIP MATERIAL USED 7075T6 .050 PO NR 9001777 DIM 7/8" BY 2.50 BY 5.50 IAW B727 SRM 55-30-2Feb 24, 2005 · N781DH · Boeing 727227SDR DHL2005781558Frame · crackedDURING A C-CHECK, THE FOLLOWING DISCREPANCY WAS NOTED: VERT STAB FIN STA 133 AT STR 8 LT HAS 1 FRAME CLIP CRACKED. REMOVED FRAME CLIP AT VERT STAB FIN STA 133 AT STR 8 LT IAW B727 SRM 51-30-2. FABRICATED NEW CLIP MATERIAL USED 7075T6 .050 PO NR 9001777 DIM 7Feb 24, 2005 · N781DH · Boeing 727227SDR DHL2005781557Frame · crackedDURING C-CHECK, VERT STAB FIN STA 55.8 STR 3 LT IS CRACKED AT FRAME ATTACH BOLT. REMOVED FRAME CLIP BS 55.8 STR 3 LT IAW B727 SRM 51-30-2. FABRICATED CLIP MATERIAL USED 7075-T6 .050 PO NR 9001777 DIM .750 INCH 2.5 INCH X 5 INCHES IAW B727 SRM 55-30-2 FIG 2 Feb 24, 2005 · N781DH · Boeing 727227SDR DHL2005805504Frame · crackedVERTICAL STAB L/E FORMER CRACKED 1.000, STA ZFS 114.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE AND FABRICATED ANGLE DOUBLER (AL7075-T6 0.032) IAW SRM 55-2-0 PG 7-8 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. APPLIED PRC SEALANFeb 20, 2005 · N805DH · Doug DC873FSDR DHL2005805509Frame · crackedVERTICAL STABILIZER L/E FORMER CRACKED 1.000, STA ZFS 96.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE AND FABRICATED (2EA) ANGLE DOUBLERS (AL7075-T6 0.032) IAW SRM 55-2-0 PG 7-8 FIG 2. CLEANED, TREATED AND PRIMED AREA, ANGLE DOUBLERS IAWFeb 20, 2005 · N805DH · Doug DC873FSDR DHL2005805507Frame · crackedVERTICAL STABILIZER L/E FORMER CRACKED 1.000 AT STA ZFS 198.250. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE AND FABRICATED ANGLE DOUBLER (2EA) (AL7075-T6 0.032) IAW SRM 55-2-0 PG 7-8 FIG 2. CLEANED, TREATED AND PRIMED AREA, ANGLE DOUBLERS IFeb 20, 2005 · N805DH · Doug DC873FSDR DHL2005805508Frame · crackedRIGHT VERTICAL STABILIZER L/E FORMER CRACKED 1.000, STA ZFS 198.500. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE AND FABRICATED (2EA) ANGLE DOUBLERS (AL7075-T6 0.032) IAW SRM 55-2-0 PG 7-8 FIG 2. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOFeb 20, 2005 · N805DH · Doug DC873FSDR DHL2005805501Frame · crackedVERTICAL STABILIZER LT L/E INTERNAL FORMER CRACKED 2.000, ZFS 198.500. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP DRILL ON CRACK END AND FABRICATED ANGLE DOUBLERS (2EA) (AL7075-T6 0.032) IAW SRM 55-2-0 PG 7-8 FIG 2. CLEANED, TREATED AND PRIMED IFeb 20, 2005 · N805DH · Doug DC873FSDR DHL2005805500Frame · crackedVERTICAL STABILIZER LT L/E INTERNAL FORMER CRACKED 1.000, ZFS 264.750. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP DRILL ON CRACK END AND FABRICATED ANGLE DOUBLERS (2EA) (AL 7075-T6 0.032) IAW SRM 55-2-0 PG 7-8 FIG 2. CLEANED, TREATED AND PRIMED Feb 20, 2005 · N805DH · Doug DC873FSDR DHL2005805503Frame · crackedVERTICAL STABILIZER L/E FORMER CRACKED 1.000, STA ZFS 86.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE AND FABRICATED (2EA) ANGLE DOUBLER (AL7075-T6 0.032) IAW SRM 55-2-0 PG 7-8 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. APPLIEDFeb 20, 2005 · N805DH · Doug DC873FSDR DHL2005805502Frame · crackedVERTICAL STABILIZER L/E FORMER CRACKED 1.000, STA ZFS 104.750. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE AND FABRICATED ANGLE DOUBLER (2EA) (AL7075-T6 0.032) IAW SRM 55-2-0 PG 7-8 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. APPLIEFeb 20, 2005 · N805DH · Doug DC873FSDR SWAA050505Spar · corrodedDURING SCHEDULED D-CHECK, FOUND VERTICAL FIN FWD AND AFT SPAR, RT AND LT CLEVIS LUGS, CORRODED. REPAIRED VERTICAL FIN PER ER.Feb 20, 2005 · N662SW · Boeing 7373Q8SDR DHL2005781555Frame · crackedDURING A C-CHECK, VERT STAB FIN STA 133 STR 9 LT IS CRACKED AT FRAME ATTACH BOLT. REMOVED FASTENERS FOR ACCESS, CUT-OUT DAMAGED DIM 4.5 X 3 INCHES STIFFENER AND REMOVED FILLER IAW B727 SRM 55-30-4 FIG 1. FABRICATED STIFFENER REPAIR. INSTALLED STIFFENER REPAFeb 16, 2005 · N781DH · Boeing 727227SDR DHL2005781554Frame · crackedDURING A C-CHECK, VERT STAB FIN STA 133 STR S-8LT IS CRACKED AT FRAME ATTACH BOLT. REMOVED FASTENERS FOR ACCESS, CUT OUT DAMAGED DIM 4.50 X 3 INCHES STIFFENER AND REMOVED FILLER IAW B727 SRM 55-30-4 FIG 1. FABRICATED STIFFENER REPAIR. INSTALLED STIFFENER REFeb 16, 2005 · N781DH · Boeing 727227SDR DHL2005781553Frame · crackedDURING A C-CHECK, VERT STAB FIN STA 133 STR 7 LT IS CRACKED AT FRAME ATTACH BOLT. REMOVED FASTENERS FOR ACCESS, CUT-OUT DAMAGED STIFFENER IAW B727 SRM 55-30-4 FIG 1 (4 X 5 INCHES). FABRICATED REPAIR STIFFENER. INSTALLED REPAIR STIFFENER IAW B727 SRM 55-30-4Feb 16, 2005 · N781DH · Boeing 727227SDR DHL2005781551Frame · crackedDURING A C-CHECK, VERT STAB AT FIN STA 157 STR 9 LT IS CRACKED AT FRAME ATTACH BOLT. REMOVED FASTENERS FOR ACCESS, CUT OUT DAMAGED 6 X 3 INCHES STIFFENER & REMOVED FILLER IAW B727 SRM 55-30-4 FIG 1, FABRICATED STIFFENER REPAIR PN BAC1517-1367, PO NR 501953 DIFeb 16, 2005 · N781DH · Boeing 727227
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