JASC 5544

Service difficulty reports · 270

Reports filed under 5544 · Rudder Miscellaneous Structure, 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 = '5544'
  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 QXEA200500078Structure · crackedPDX - TOP OF FORE RUDDER HAS A CRACK NEAR A RIVET. INSTALLED THE REPAIRED PARTS AND SEALED IAW RD 8-55-335.Dec 29, 2004 · N359PH · Dhav DHC8202SDR DHL2004801560Rib · crackedRUDDER RIB CRACKED 1.000 ZR 105.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 55-1-0 PG.1, DWG 5656226. REMOVED CRACKED RIB IAW SRM 51-1-21 PG. 1. FABRICATED NEW RIB IAW SRM 55-6-1 PG.4 FIG.2 SHEET 2 DWG 5656226, SRM 51-1-4 PG.1. DPS 3.69-4. PERFORMED HSep 27, 2004 · N801DH · Doug DC873FSDR MWEA040047Bracket · corrodedFOUR AREAS OF CORROSION ON LOWER RUDDER BRACKET. REMOVED AND REPLACED LOWER BRACKETS.Mar 31, 2004 · N806ME · Doug DC981SDR CA040401004Attach Bracket · cracked(CAN) RUDDER UPPER ATTACHED BRACKET WAS FOUND CRACKED.Mar 29, 2004 · Cessna 172PSDR 2004FA0000120Balance Weight · missingRUDDER BALANCE WEIGHT WAS MISSING FROM IT'S LOCATION. UPON INSP OF RAMP AREA, MISSING WEIGHT ASSY WAS FOUND FROM TAXIWAY. RUDDER TAB, AC WERE DETERMINED TO NOT BE DAMAGED FROM PART DEPARTING ITS LOCATION. WEIGHT ASSY WAS INSP, CAUSE OF PART COMING OFF AC WAS RJan 19, 2004 · N4726V · Cessna 172RGSDR 2004FA0000079Balance Weight · missingIT WAS NOTED THAT RUDDER BALANCE WEIGHT WAS MISSING FROM LOCATION IN TOP LE OF RUDDER. UPON INSP OF RAMP AREA, IT WAS RECOVERED FROM TAXIWAY. RUDDER TAB AND AC WERE UNDAMAGED FROM IT DEPARTING AC, WEIGHT ASSY WAS INSPECTED TO DETERMINE CAUSE OF DEFECT. SCREW IJan 19, 2004 · N4726V · Cessna 172RGSDR DHL2003742524Web · chafedDURING C-CHECK, LWR RUDDER UPPER WEB AND FASTENERS CHAFED. REMOVED DAMAGED WEB AND FASTENERS IAW B-727 SRM 51-30-2. FABBED NEW WEB IAW B-727 SRM 55-40-2 FIG 2. NEW WEB TREATED AND PRIMED IAW B-727 SRM 51-10-2. WEB AND FASTENERS INSTALLED IAW B-727 SRM 51-3Dec 12, 2003 · N742DH · Boeing 727225SDR UPS03841164Web · crackedINSPECTION TYPE: C2, WEB IN RUDDER LE AT FORWARD SPAR IS CRACKED AT XR 160 REMOVED WEB SECTION,FABRICATED AND INSTALLED REPLACEMENT WEB SECTION IAW SRM. 55-2-4 FIG. 1Aug 28, 2003 · N809UP · Doug DC873FSDR UPS03841024Web · crackedINSPECTION TYPE:C2 INSIDE RUDDER NR 2 HINGE CUTOUT WEB IS CRACKED AT ZR 159.094. REMOVED, FABRICATED AND REPLACED WEB IAW DWG 5656229 AND SRM 51-1-21, 51-1-20D.Jul 23, 2003 · N874UP · Doug DC873FSDR GTIA030345Hinge Bracket · corrodedFTW - VERTICAL STAB RUDDER HINGE CENTER 'V' BRACKET ASSEMBLY HAS CORROSION STATION ZR 97.207. REMOVED VERTICAL STAB RUDDER HINGE CENTER 'V' BRACKET. INSTALLED BRACKET ASSEMBLY. (M)May 7, 2003 · N800NK · Doug DC982SDR C2XA02SH150Support · damagedSHV - DURING C-CHECK RUDDER 1 CENTER HINGE POINT LOWER LEADING EDGE SKIN SUPPORT WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED AFFECTED SUPPORT IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.Dec 23, 2002 · N15941 · Emb EMB145ERSDR C2XA02SH149Support · damagedSHV- DURING C-CHECK RUDDER NUMBER 1 CENTER HINGE POINT UPPER LEADING EDGE SKIN SUPPORT WAS FOUND BENT. MAINTENANCE REMOVED AND REPLACED AFFECTED SUPPORT IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.Dec 23, 2002 · N15941 · Emb EMB145ERSDR QXEA0202214Bracket · damagedPDX- BOTTOM BRACKET ON FORE RUDDER THAT CONNECTS TO THE TRAILING RUDDER HAS STEP WEAR AROUND FASTENER HOLE. REPAIRED IAW DHC-8 SRM 51-40-11.Dec 16, 2002 · N347PH · Dhav DHC8202SDR 2002FA0001263Fitting · crackedFOUND RUDDER TO BE OUT OF RIG FOR 2ND TIME IN 17 HRS INSPECTED AND FOUND LOWER STRUT FITTING TO BE CRACKED WERE STRUT FITTING TO BE CRACKED WERE STRUT ATTACHES TO FITTING.Oct 21, 2002 · N97784 · Cessna 182QSDR UPS02839264Pan · crackedINSPECTION TYPE:C2 LOWER RUDDER PANS ARE CRACKED AT 2ND AND 3RD HINGE FROM BOTTOM AT XE 77 AND XE 149. REMOVED, FABRICATED, AND REPLACED PANS IAW DWG 5656233, AND SRM 51-1-21, 51-3-0.Jul 31, 2002 · N806UP · Doug DC873FSDR CA020722008Support Bracket · cracked(CAN) RUDDER SUPPORT BRACKET DEVELOPED CRACKS ON THE WELD.Jul 8, 2002 · Diamon DA20C1SDR F3LA200200195Structure · corrodedDURING C-2 CHECK, INSPECTION REPORTED CORROSION ON RUDDER BULLNOSE BY NR 3 HINGE. REPLACED CORRODED AREA OF RUDDER BULLNOSE PER SRM 51-40-02 AND BOEING DRAWING 65-53740.Jul 5, 2002 · N272 · Boeing 7372P6SDR QXEA0200657Rub Strip · chafedPDX- FORE RUDDER RUB STRIP CHAFED. REPAIRED IAW DHC-8 SRM 51-20-51, 51-40-11 AND HORIZON AIR EA 2-55-65.Apr 17, 2002 · N351PH · Dhav DHC8202SDR C2XA02TY061Bracket · chafedTYS DURING A SCHEDULED INSPECTION THE RUDDER II MID-BEARING BRACKET WAS FOUND TO BE CHAFED AT THE CONNECTING ROD ATTACH POINT. MAINTENANCE REMOVED AND REPLACED THE BRACKET IAW EMB-145 SRM 51-40-02, THE REPAIR WAS FOUND TO BE SATISFACTORY. THE AIRCRAFT WILL Apr 7, 2002 · N22971 · Emb EMB145SDR QXEA0200611Rub Strip · chafedPDX- FORE RUDDER TOP RUB STRIP HAS CHAFE WEAR. REPAIRED IAW DHC-8 SRM 51-20-36, 51-40-11 AND 20-21-50.Mar 25, 2002 · N358PH · Dhav DHC8202
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