JASC 5511

Service difficulty reports · 6,462

Reports filed under 5511 · Horizontal 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 = '5511'
  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 WRLA2005112Rib · corrodedDURING C04 CHECK, WHILE PERFORMING INSP PER EO 02-5510-098, FOUND CORROSION IN HST RT BARREL NUT HOLE NR 29.Jun 16, 2005 · N277 · Doug MD11SDR WRLA2005104Rib · corrodedDURING C04 CHECK, WHILE PERFORMING INSP PER EO 02-5510-098, FOUND CORROSION IN HST RT BARREL NUT HOLE NR 14.Jun 14, 2005 · N277 · Doug MD11SDR WRLA20051040Rib · corrodedDURING C-04 CHECK, WHILE PERFORMING INSP PER EO 02-5510-098, FOUND CORROSION IN HST RT BARREL NUT HOLE NR 14.Jun 14, 2005 · N277 · Doug MD11SDR WRLA2005103Rib · corrodedDURING C-04 CHECK, WHILE PERFORMING INSP PER EO 02-5510-098, FOUND CORROSION IN HST LT BARREL NUT HOLE NR 35.Jun 14, 2005 · N277 · Doug MD11SDR WRLA200599Rib · corrodedDURING C-04CHECK, WHILE PERFORMING INSP PER EO 02-5510-098, FOUND CORROSION IN HST LT BARREL NUT HOLE NR 30.Jun 14, 2005 · N277 · Doug MD11SDR WRLA200592Panel · corrodedDURING C04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST LT BARREL NUT HOLE NR 15.(OPEN)Jun 14, 2005 · N277 · Doug MD11SDR AWXA200500717Spar · crackedDURING C-21 CHECK, DISCOVERED RT HORIZONTAL STAB CHANNEL CRACKED ON AFT SPAR WEB AT STAB STATION 170. MX CUT OUT CRACKED SECTION ON AFT SPAR WEB AT STAB STATION 170 AND FABRICATED REPLACEMENT PARTS IAW BOEING 737-300 SRM 51-70-11-0 FIG 1. BONDED AND INSTALLEJun 12, 2005 · N173AW · Boeing 73733ASDR UPS05844762Rib · crackedLT HORIZ STAB L/E 2ND INBD LWR RIB REPAIR HAS DOUBLER AND TRIPLER CRACKED. REMOVED, FABRICATED, AND INSTALLED REPAIR DOUBLER AND TRIPLER IAW SRM 55-2-0, 51-1-21, AND SRM 55-2-0 FIG 2.Jun 5, 2005 · N705UP · Doug DC871FSDR 2005UALA00550Rib · crackedLT HORIZONTAL STAB L/E RIB LOWER FLANGE AT STA 151.8 WAS FOUND CRACKED. *S/D* REPAIR ACP' D PER EVA-50305, FABRICATED REPAIR ANGLE REPAIR SCHEME AT HMV-4.May 29, 2005 · N313UA · Boeing 737322SDR DU4R106Bushing · corrodedLT HORIZONTAL STAB AFT SPAR, UPPER ATTACH LUG, CENTER SECTION, AFT FACE HAS CORROSION AROUND BUSHING. S/O 109001, N/R 22994May 27, 2005 · N312FL · Boeing 7373L9SDR DU4R05105Bushing · corrodedLT HORIZONTAL STAB FRONT SPAR, UPPER ATTACH BOLT BORE, BUSHINGS HAVE PITTING CORROSION. S/O 109001, N/R 22971.May 27, 2005 · N312FL · Boeing 7373L9SDR 05FDEA01357Spar Cap · corrodedNR 36R BORE FOUND EXCEEDED LIMIT AFTER CORROSION REMOVAL. EMPENNAGE NR 36R BORE REWORKED AS PER FEDEX EA NR 1-5510-83129. HORIZONTAL STABILIZER, BARREL NUT BORE 36R. REWORKED BEYOND S/B MD11-55-023 REV 2 LIMITS. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-10May 17, 2005 · N580FE · Doug MD11SDR 20030846Spar · crackedDURING ROUTINE INSPECTION, FOUR CRACKS APPROX .5 INCH LONG FOUND EXTENDING FROM THE DE-ICE LINE HOLE IN THE HORIZONTAL MAIN SPAR WEB. REPAIRED IAW WITH COMPANY EO. AIRCRAFT RETURNED TO SERVICE.May 17, 2005 · N202UX · Beech 1900DSDR 05FDEA01296Spar Cap · corrodedHORIZONTAL STABILIZER RIGHT HAND AFT SPAR CAP NR 36R BARREL NUT BORE CORROSION REMOVAL FOUND EXCEEDED LIMITATIONS. REWORKED AS PER FEDEX EA 1-5510-83007.May 15, 2005 · N621FE · Doug MD11SDR OMKR200600001Rib · crackedROLLER RIB AT INBOARD END CRACKED (ASSY P/N 45A21104-642) IN THREE PLACES. RIB, AND BOTH CLIPS. CRACKING IS FROM RIB MATERIAL BEING TOO THIN, IMPROPER RIGGING, OR EXCESSIVE WEAR OF HORIZONTAL STABILIZER HINGE POINTS. SUSPECT RIB MATERIAL IS JUST TOO THIN TOApr 25, 2005 · N743TA · Beech 400ASDR 20030837Spar · crackedDURING ROUTINE INSPECTION, FOUR CRACKS APPROX .65 INCH LONG FOUND EXTENDING FROM THE DE-ICE LINE HOLE IN THE HORIZONTAL MAIN SPAR WEB. REPAIRED IAW WITH EO, AIRCRAFT RETURNED TO SERVICE.Apr 25, 2005 · N219GL · Beech 1900DSDR CALA0500108Spar · wornHORIZONTAL STABILIZER CENTER SECTION REAR SPAR RIGHT LOWER AFT CLEVIS WORN INTO BY ACCESS PANEL 9224R. BLENDED THE GOUGE PER ECRA 5550-01035.Apr 18, 2005 · N12319 · Boeing 7373T0SDR CA050416001Spar · cracked(CAN) FRONT SPAR CRACKED CENTER SECTION AT LIGHTNING HOLE.Apr 15, 2005 · Cessna R172KSDR 05FDEA00796Spar Cap · corrodedCORROSION REMOVED ON HORIZ STAB RT UPPER AFT SPAR CAP NR 36R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82959.Apr 1, 2005 · N616FE · Doug MD11FSDR 05FDEA00724Spar Cap · corrodedCORROSION REMOVED ON HORIZ STAB LT FWD SPAR CAP NR 1L BARREL NUT BORE FOUND EXCEEDED LIMITS. REWORK/REPAIR - 1-5510-7-5000 HAS BEEN COMPLIED WITH.Mar 31, 2005 · N616FE · Doug MD11SDR 20030808Spar · crackedHORIZONTAL STAB MAIN SPAR CENTER WEB SKIN CRACKED AT DEICE HOLE IN FOUR PLACES APPROX 1 INCH LONG. REPAIRED PER EO. AIRCRAFT RETURNED TO SERVICE.Mar 26, 2005 · N251GL · Beech 1900DSDR 2005FA0000550Rib · misinstalledUPON INSPECTION OF HORIZONTAL STABILIZER, MECHANIC NOTED THAT ALL RIVETS SECURING FORWARD FLANGE OF RIB P/N 2632021-25 TO FORWARD SPAR WERE MISSING. HOLES WERE DRILLED THRU WITH BARE METAL SHOWING (NO PRIMER IN HOLES). ASSUMPTION IS THAT RIVETS WERE OMITTED Mar 25, 2005 · N103VE · Cessna 208BSDR SWAA050886Spar · corrodedDURING SCHEDULED D-CHECK, FOUND LT HORIZONTAL STAB, AFT SPAR, UPPER CHORD CORRODED AT STA 276.70. REPAIRED LT HORIZONTAL STAB PER SRM & SB.Mar 22, 2005 · N663SW · Boeing 7373Q8SDR UPS05844260Rib · crackedINSPECTION TYPE: C2, CRACKED LOWER RIB ON L/H HORIZONTAL LEADING EDGE 40 INCHES FROM IB END. STOPDRILLED CRACK IAW DC-8 SRM 55-2-0 FIG.2. REPAIRED CRACKED RIB IAW DC-8 SRM 55-3-1 FIG. 3, 55-2-0 FIG. 2, & 51-1-20D.Mar 20, 2005 · N819UP · Doug DC873FSDR 05FDEA00580Rib · crackedRIGHT HORIZONTAL STAB, INTERIOR RIB WEB CRACKED L/E STA 131, 2 INCHES FROM FWD EDGE ALONG TOP. *S/D* REPAIRED FRONT SPAR WEB, RIGHT STAB LEADING EDGE STA 131 PER SRM 55-10-4.Mar 17, 2005 · N481FE · Boeing 727200SDR USAA050495Spar · crackedBFM - FOUND AUX FRONT SPAR CRACKED 2.35 INCHES, LT L/E HORIZ STAB STA 191-240.7 SPAR. REPAIRED SPAR CHORD WITH ANGLES, SHIMS AND FILLERS PER EA 96343. (M)Mar 16, 2005 · N648US · Boeing 767201SDR 05FDEA00402Spar · corrodedLEFT STAB REAR SPAR STA 158, 2 INCHES OF CORROSION AND STA 258 HAS 1 INCH OF CORROSION REF N00264. REMOVED CORROSION FOUND OUT OF LIMITS, REPAIRED IAW SRM 55-11-21 FIG 215.Mar 7, 2005 · N446FE · Airbus A310222SDR 05FDEA00401Spar · corrodedRIGHT STAB REAR SPAR STA 812 HAS 1 INCH OF CORROSION, 1 INCH AT STA 258, 1 INCH AT STA 158. REMOVED CORROSION FOUND OUT OF LIMITS, REPAIRED SPAR IAW SRM 55-11-21.Mar 7, 2005 · N446FE · Airbus A310222SDR R9E2005F00000Spar · corrodedDURING AN (I) CHECK INSPECTION THE UPPER AND LOWER HORIZONTAL SPAR CAPS WERE FOUND WITH CORROSION IN THE AREA OF THE ELEVATOR HINGES. THIS AREA WAS NOT TREATED OR PRIMED BY THE FACTORY DURING AC MANUFACTURE AND THUS WAS CONDUCIVE TO CORROSION. THIS IS CONSIDMar 1, 2005 · N46AR · Beech 1900DSDR SWAA050618Rib · crackedDURING SCHEDULED D-CHECK, FOUND LT HORIZONTAL STAB L/E NR 1 RIB CRACKED. REPAIRED LT HORIZONTAL STAB RIB PER SRM.Feb 28, 2005 · N663SW · Boeing 7373Q8SDR DJFA2005067Rib · crackedDURING A ROUTINE MAINTENANCE VISIT WHILE PERFORMING PHASE A AND PHASE B INSPECTIONS A CRACKED RIB WAS DISCOVERED ON THE LEFT HORIZONTAL STABILIZER AT THE LEFT ROLLER ASSEMBLY. THE RIB WAS REPLACED ALONG WITH SUPPORT BRACKETS. THE AIRCRAFT WAS RETURNED TO SERFeb 21, 2005 · N718TA · Beech 400ASDR SWAA050461Spar · corrodedDURING SCHEDULED D-CHECK, FOUND LT HORIZONTAL STABILIZER REAR SPAR UPPER CHORD, CORRODED. REPAIRED CHORD PER SRM.Feb 17, 2005 · N662SW · Boeing 7373Q8SDR MASA200500123Rib · crackedIN C-CHECK EMPENNAGE INTERNAL RIB IS CRACKED AND IS BEING REPLACED IAW SRM 51-40-02.Feb 16, 2005 · N851MJ · Emb EMB145LRSDR WRLA2005057Spar Cap · corrodedDURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST LT BARREL NUT HOLE NR 01.Feb 7, 2005 · N276 · Doug MD11FSDR 2003788Spar · crackedDURING ROUTINE STRUCTURAL "I" INSPECTION, FOUR CRACKS WERE IDENTIFIED EMANATING FROM THE DE-ICE HOLE ON THE HORIZONTAL CENTER MAIN SPAR CENTER WEB SKIN APPROX 1 INCH LONG EACH UNDER PANEL 332 ATC. REPAIR WAS MADE AND AIRCRAFT RETURNED TO SERVICE.Feb 7, 2005 · N100UX · Beech 1900DSDR SWAA050333Spar · corrodedDURING SCHEDULED D-CHECK, FOUND RT AND LT HORIZONTAL STABILIZER FWD AND AFT SPARS, UPPER ATTACH LUGS AND CLEVIS, CORRODED. REPAIRED HORIZONTAL STAB PER SRM.Feb 6, 2005 · N662SW · Boeing 7373Q8SDR 20030789Spar · crackedDURING ROUTINE STRUCTURAL "I" INSPECTION, FOUR CRACKS WERE IDENTIFIED EMANATING FROM THE DE-ICE HOLE ON THE HORIZONTAL CENTER MAIN SPAR CENTER WEB SKIN APPROX 1" LONG EACH UNDER PANEL 332 ATC. REPAIR WAS MADE AND AIRCRAFT RETURNED TO SERVICE.Feb 5, 2005 · N253GL · Beech 1900DSDR CA050209004Spar · cracked(CAN) FOUND 2 SMALL CRACKS (0.200 INCH LONG) IN THE SPAR CENTER LIGHTNING HOLE FLANGE, ALSO, THE REINFORCEMENT HAS BEEN SLIGHTLY BENT AND A REPLACEMENT IS NECESSARY. SPAR IS THE SAME ONE USED ON THE EARLIER MODEL EXCEPT THAT MFG HAS INCLUDED THE REINFORCEMENTFeb 3, 2005 · Cessna 172SSDR 05FDEA00212Rib · corrodedLT HORIZONTAL STAB T/E, JUST O/B OF RIB 3, 1 EA AREA OF CORROSION ON WEB ATTACH UPPER FLANGE LOWER SURFACE. REMOVED CORROSION PER A300600 SRM 51-74-10, MATERIAL LOSS OUT OF LIMITS PER A300600 SRM 55-10-00. FABRICATED AND INSTALLED REPAIR ANGLE IAW A300600 SFeb 1, 2005 · N716FD · Airbus A300B4622SDR 05FDEA00198Spar · corrodedRT HORIZONTAL STAB UPPER TRAILING EDGE LOWER SURFACE FROM INBOARD END AND EXTENDING OUTBOARD 31.0 INCHES. THERE IS LIGHT TO SEVERE CORROSION AROUND AND BETWEEN NUT PLATES. REMOVED CORROSION IAW A310-200 SRM 51-74-10 AND FOUND A SECTION OUT OF LIMITS IAW A310Jan 29, 2005 · N405FE · Airbus A310203SDR 20030785Spar · crackedDURING ROUTINE STRUCTURAL "I" INSPECTION, FOUR CRACKS WERE IDENTIFIED EMANATING FROM THE DE-ICE HOLE ON THE HORIZONTAL CENTER MAIN SPAR CENTER WEB SKIN APPROX 1" LONG EACH UNDER PANEL 332 ATC. REPAIR WAS MADE AND AIRCRAFT RETURNED TO SERVICE.Jan 26, 2005 · N154GL · Beech 1900DSDR CA050202004Spar · cracked(CAN) DURING THE 200 HOUR INSPECTION CRACKS WERE FOUND STARTING FROM THE CENTRAL LIGHTENING HOLE IN THE FORWARD HORIZONTAL STABILIZER SPAR. THE CRACKS WERE STOP DRILLED AND REINFORCEMENT P/N 0531037-1 AND SKIN P/N 0523001-25 WERE INSTALLED IAW SEB94-8.Jan 25, 2005 · Cessna 172NSDR ASAA0540050Rib · gougedOKC- RT HORIZONTAL STAB T/E NR3 RIB IS GOUGED ON THE OB SIDE. PREPARED AREA, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM. (K)Jan 23, 2005 · N771AS · Boeing 7374Q8SDR SWAA050113Spar · corrodedDURING SCHEDULED D-CHECK, FOUND LT AND RT HORIZONTAL STAB FWD SPAR FWD AND AFT CLEVIS LUGS CORRODED. REPAIRED HORIZONTAL STAB PER SRM.Jan 17, 2005 · N606SW · Boeing 7373H4SDR 05FDEA00114Spar · damagedRT HAND HORIZ STAB REAR SPAR LWR CHORD HAS DAMAGE FASTENER HOLE AT NR 4 BAL BAY. *S/D* TRIMMED DAMAGED AREA OUT, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 55-10-5.Jan 17, 2005 · N465FE · Boeing 727200SDR 05FDEA00092Rib · crackedSTABILIZER-ELEVATOR HINGE SUPPORT RIB INSPEC - S/B 727-55A0091 R1 COMPLY WITH EO 7-5510-7-5001. FOUND CRACK IN RIB AT ELEVATOR STA 50.50 DURING INSPECTION IAW EO 7-5510-5001. REMOVED AND REPLACED RIB IAW EO 7-5510-5001.Jan 14, 2005 · N107FE · Boeing 727100SDR CA050308005Rib · cracked(CAN) RT LEADING EDGE IB RIB WAS FOUND CRACKED AT REAR LOWER CORNER (RADIUS).Jan 13, 2005 · Cessna 152SDR CA050308006Rib · cracked(CAN) LT LEADING EDGE IB RIB WAS FOUND CRACKED AT REAR TOP CORNER (RADIUS).Jan 13, 2005 · Cessna 152SDR CA050308004Rib · cracked(CAN) LEADING EDGE, LT IB RIB WAS FOUND CRACKED AT THE TOP REAR CORNER (RADIUS).Jan 10, 2005 · Cessna A152SDR 05FDEA00007Spar · corrodedRIGHT HAND HORIZONTAL STABILIZER: STA XE159 RIB NR 12 LOWER FRONT TO REAR SPAR FOUND CORRODED. REPAIRED IAW FEDEX EA 1-5510-78109.Jan 3, 2005 · N577FE · Doug MD11
Back to JASC 5511