JASC 5543

Service difficulty reports · 196

Reports filed under 5543 · Rudder, Tab 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 = '5543'
  ORDER BY difficulty_date DESC"

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SDR UPS04242981Skin · delaminatedINSPECTION TYPE: C, UPPER RUDDER TAB HAS DELAMINATION AT LWR LT SIDE UPPER RUDDER REPLACED IAW MM 27-20-11.Jul 29, 2004 · N945UP · Boeing 72722CSDR ASAA0580019Tab · delaminatedOKC - HV-CHECK, RUDDER TAB IS DELAMINATED AT BASE WEDGE. BOND REPAIRED. (M)Jan 23, 2004 · N964AS · Doug DC983SDR C1HA200382011Skin · crackedLOWER RUDDER TAB UPPER LEFT AND RIGHT SIDE IS DEBONDED AND CRACKED.Dec 15, 2003 · N682CA · Boeing 7272S7SDR 03FDEA01263Tab · delaminatedLOWER RUDDER TAB 2FH SIDE UPPER END IS DELAMINATED AT AFT END.Jul 21, 2003 · N103FE · Boeing 727100SDR 03FDEA01264Tab · delaminatedLOWER RUDDER TAB 2FH SIDE IS DELAMINATED 13 22 ABOVE PUSH ROD ATTACH FITTING.Jul 21, 2003 · N103FE · Boeing 727100SDR GTIA030395Tab · delaminatedFOUND RUDDER TAB AREAS OF DELAMINATED. REPAIRED DAMAGE ON RUDDER TAB. (M)May 9, 2003 · N800NK · Doug DC982SDR DHL2003804772Tab · delaminatedREMOVAL /INSTALLATION OF RUDDER TAB REQUIRED DUE TO DELAMINATION IN BOTH SIDES OF SKIN. R & R RUDDER TAB IAW MM 27-21-2 PG. 201-204 ADJUSTED RUDDER TAB IAW MM 27-21-2 PG. 204-207 REFER TO N/R 0607 FOR OPS CKMar 4, 2003 · N804DH · Doug DC873FSDR GTIA020851Skin · puncturedFTW - FOUND RUDDER TAB HAS PUNCTURE MARK (HOLE) APPROX .25 INCH DIAMETER 3 INCHES ABOVE FIXED TAB. RUDDER TRIM TAB FIXED TAB DEBONDED. THIS TAB REPLACED. (M)Jul 10, 2002 · N801NK · Doug DC982SDR ABXA010881Trim Tab · delaminatedUPPER LEFT CORNER OF RUDDER TAB WAS DELAMINATED. REPLACED RUDDER TRIM TAB IAW DC-9 MM.Apr 22, 2002 · N900AX · Doug DC932SDR ABXA010728Tab · delaminatedRIGHT SIDE OF RUDDER TAB DELAMINATED. REPLACED RUDDER CONTROL TAB IAW DC-9 AMM 27-20-02-4-0001.Feb 7, 2002 · N906AX · Doug DC931SDR C1HA200282005Tab · delaminatedLOWER RUDDER TAB HAS DELAMINATED ON LT UPPER FWD CORNER. (C CHECK FINDING) REPAIR APPROVED BY 8110.Feb 1, 2002 · N682CA · Boeing 7272S7SDR CALA0100725Skin · dentedINSPECTION FOUND RUDDER CONTROL TAB SKIN DENTED IN THE LOWER LEFT SIDE. THE RUDDER TAB WAS REMOVED IAW MM 27-20-02. THE TAB WAS REPAIRED, WEIGHED, AND BALANCED IAW SRM 55-40-1. THE TAB WAS INSTALLED AND THROW CHECKS WERE COMPLETED IAW MM 27-20-02.Jul 30, 2001 · N16815 · Doug DC982SDR DHL2001806633Hinge Bracket · crackedC-CHECK - UPPER RUDDER TAB HINGE LUG CRACKED AT ZRT 134.618. REMOVED CRACKED HINGE (BRACKET) IAW SRM 51-1-21 PAGE 1. FABRICATED NEW HINGE (BRACKET) IAW ATM NR 044010A, EA 2001058, DWG 34701452. CLEANED, TREATED, AND PRIMED IAW SRM 51-1-8B AND INSTALLED HINGMar 30, 2001 · N806DH · Doug DC873FSDR AT0100112Skin · dentedFOUND RUDDER TAB DENTED. FABRICATED AND INSTALLED FILLER AND DOUBLERS IAW DC9 SRM 51-70-02 AND 55-40-01.Mar 8, 2001 · N833AT · Doug DC932SDR CALA0100002Tab · looseINSPECTION FOUND RUDDER TAB T/E METAL TAB LOOSE ON RT SIDE. THE RUDDER TRIM TAB WAS REMOVED, REPAIRED, AND REINSTALLED IAW MM 27-20-02, PARAGRAPH B & C.Jan 1, 2001 · N16807 · Doug DC982SDR CALA0001620Tab · dentedINSPECTION FOUND RUDDER TAB DENTED ON RT SIDE. THE RUDDER TAB WAS REMOVED IAW MM 27-20-02. THE RUDDER TAB WAS REPAIRED IAW SRM 51-30-3. THE RUDDER AB WAS REINSTALLED IAW MM 27-20-02. A WEIGHT AND BALANCE WAS PERFORMED IAW SRM 55-40-01.Oct 21, 2000 · N14871 · Doug DC981SDR RRXA003217Tab · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE RUDDER FLIGHT TAB, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 6, 2000 · N500MH · Doug DC871FSDR CALA0000985Trim Tab · dentedINSPECTION FOUND RT SIDE OF RUDDER TRIM TAB DENTED. THE TRIM TAB WAS REMOVED AND REPLACED IAW MM 27-20-02, PARAGRAPH 3A, B, C. A WEIGHT AND BALANCE WAS PERFORMED ON THE TAB IAW SRM 55-40-1 AND THE CHECK WAS WITHIN LIMITS.Jun 26, 2000 · N819NY · Doug DC982SDR DHL200070733CTab · delaminatedAT C CK; LWR RUDDER TAB LWR LT & RT SURFACE DELAMINATED. ACCOMPLISHED FIBERGLASS CLOTH OVERLAY REPAIR PER B727 SRM 51-40-8 FIG 1. REF: N/R 4545.May 26, 2000 · N707DH · Boeing 72722SDR ABXA000292Skin · delaminatedDURING C-CHECK, FOUND RUDDER TAB DELAMINATED. REPLACED RUDDER TAB IAW DC9 SRM 27-20-02.May 24, 2000 · N946AX · Doug DC931SDR 20000511SH020Hinge · damagedTHE RUDDER AND TRIM TAB VIBRATE ON THIS INSTALLATION. RUDDER TRIM TAB RIVETS ARE ALSO LOOSE.Apr 24, 2000 · N398RS · Cessna 560CESSNASDR TWAA0002909Tie Clip · crackedDURING CHECK-C MAINT, FOUND 8 DORSAL FIN FORMER TIE CLIPS CRACKED, 3 ON THE LT SIDE AND 5 ON THE RT SIDE. REPAIRED PER SSRM 55-30-102, PAGE 201, AND SRM 55-02 FIG 19.Feb 17, 2000 · N953U · Doug DC982SDR DHL200071720DTab · delaminatedAT D CK, UPPER RUDDER TAB RT F/G DELAMINATED. INSTALLED FIBERGLASS OVERLAY REPAIR PER B727 SRM 51-40-8, FIG 1, REF: N/R 4691.Jan 20, 2000 · N717DH · Boeing 72723SDR DHL200071725DTab Skin · delaminatedAT D-CK, UPPER RUDDER TAB RIGHT LOWER SECTION OF SKIN HAS ABOUT 15 SQUARE INCH OF DELAMINATION AND SPOTS OF CORROSION. INSTALLED FIBERGLASS OVERLAY REPAIR AS PER B727 SRM 51-40-8, FIG 8. SIZE; 12 BY 6. REF: N/R 4685.Jan 19, 2000 · N717DH · Boeing 72723SDR DHL200071726DPanel · dentedAT D CK, UPPER RUDDER PANEL RT DENT WITH FILLER. INSTALLED FIBERGLASS OVERLAY REPAIR PER BOEING 727 SRM 51-40-8, FIG 1. SIZE; 12 BY 6. EF:N/R 4622.Jan 14, 2000 · N717DH · Boeing 72723SDR ABXA9900767Tab · delaminatedDURING C-CHECK, FOUND RUDDER TAB DELAMINATED. REPLACED RUDDER TAB IAW DC9 MM 27-20-2.Nov 8, 1999 · N958AX · Doug DC941SDR CALA9901198Tab · disbondedINSPECTION FOUND RUDDER TRIM TAB METAL TAB DISBONDED ON RT SIDE OF TAB. THE RUDDER TAB WAS REMOVED AND THE METAL TAB WAS REMOVED AND REPLACED. THE RUDDER TAB WAS REINSTALLED AND RIGGED IAW MM 27-20-02.Sep 12, 1999 · N93875 · Doug DC982SDR UPS99230116Skin · delaminatedINSPECTION TYPE:C, RUDDER LOWER TAB DELAMINATED AT UPPER T/E LEFT SIDE PREVIOUS REPAIR. REPAIRED IAW SRM 51-40-10 FIG 3.Jul 9, 1999 · N928UP · Boeing 72722CSDR CALA9900812Skin · delaminatedINSPECTION FOUND RUDDER TRIM TAB DELAMINATED ON TRAILING EDGE AT AFT TOP CORNER AND BOTTOM CORNER. THE RUDDER TAB WAS REMOVED, REPAIRED, AND REINSTALLED IAW MM 27-20-2 AND SRM 51-90-2.Jul 8, 1999 · N478AC · Doug DC982SDR CALA9900766Tab · dentedINSPECTION FOUND RT SIDE OF RUDDER TAB DENTED. THE TAB WAS REMOVED AND REPAIRED IAW SRM 55-04, PARAGRAPH 2. THE TAB WAS BALANCED AND REINSTALLED IAW MM 27-20-02.Jul 1, 1999 · N16813 · Doug DC982SDR ABXA990559Tab · delaminatedDURING C-CHECK, FOUND RUDDER TRIM TAB DELAMINATED. REPLACED RUDDER TRIM TAB IAW DC9 MM 27-20-2.Jun 30, 1999 · N941AX · Doug DC931SDR UPS99229649Skin · delaminatedINSPECTION TYPE:C, UPPER RUDDER TAB RT SIDE HAS EVIDENCE OF DELAMINATION T/E AREA, AFT OF CENTER HINGE FITTINGS. REPAIRED IAW SRM 51-40-10 FIG 1.May 5, 1999 · N921UP · Boeing 727180CSDR EISA99106Skin · delaminatedDURING C-CHECK INSPECTION, FOUND UPPER RUDDER TRIM TAB T/E DELAMINATED ON UPPER EDGE. REPAIRED IAW BOEING SRM CHAPTER 51-40-09 FIGURE 7. (M)Apr 8, 1999 · N15DF · Boeing 727264SDR EISA99088Skin · delaminatedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND UPPER RUDDER TRIM TAB T/E DELAMINATED ON UPPER EDGE. REPAIR PERFORMED BY OUTSIDE VENDOR. REPAIRED ON AIRCRAFT. (M)Apr 8, 1999 · N15DF · Boeing 727264SDR UPS99229346Skin · delaminatedINSPECTION TYPE:C+SI, LOWER RUDDER TAB HAS NUMEROUS PREVIOUS REPAIRS WITH DELAMINATION. REPAIRED IAW SRM 51-40-10 FIG 1.Mar 25, 1999 · N922UP · Boeing 72731CSDR DHL9980529CTab · delaminatedAT C-CHECK, RUDDER TAB DELAMINATED AT LT LOWER AREA. REMOVED TAB, REPAIRED AND REPAINTED AND REBALANCED. N/R 55Jan 31, 1999 · N805DH · Doug DC873FSDR AT0099104Trim Tab · out of positionSCHEDULED INSPECTION AT AERO CORP, FL. RUDDER TRIM TAB DOES NOT HAVE MINIMUM CLEARANCE AT TOP END PER DC9 MM 27-20-1 PG 602. TRIMMED TOP OF TRIM TAB TO 5/32 TO COMPLY WITH MM 27-20-0 PG 603, TREATED, AND PRIMED IAW DC9 SRM 51-10-3, 55-01 PG 1, AND RES NR 992Jan 19, 1999 · N806AT · Doug DC932SDR CA981214006Skin · cracked(CAN) MILLED SKIN FOUND WITH A CRACK FORWARD OF FRONT MOUNTING HOLES ON BOTH LOWER MASS BALANCE WEIGHTS. EXPOSED RIB IS ALSO CRACKED AT FLANGE RADIUS. SB 215-A435 ADDITIONAL WEIGHTS WERE INCORPORATED. CRACKED MASS BALANCE ARM COULD BE ASSOCIATED. ALL FOUR Nov 24, 1998 · Cndair CL2151A10SDR CA981209004Tab · cracked(CAN) MILLED SKIN P/N 215-15062-2 HAS A 2.75 INCH CRACK FORWARD OF FRONT MOUNTING HOLES ON BOTH LOWER MASS BALANCE WEIGHTS. (APPROXIMATELY .3125 INCH TO .3750 INCH FORWARD OF HOLES). EXPOSED RIB IS CRACKED AT FLANGE RADIUS. SB 215-A435 ADDITIONAL WEIGHTS WENov 24, 1998 · Cndair CL2151A10SDR 98ZZZX4575Rudder · crackedWHILE C/W AD 63-07-03 AND SB 213 WHICH REQUIRES INSPECTION OF THE RUDDER TRIM TAB HORN AND ATTACHMENT AREA SKIN, CRACKS WERE DISCOVERED IN SEVERAL RIVET HOLES AS WELL AS A MODERATE AMOUNT OF DISSIMILAR METAL CORROSION AND PITTING. WHILE REPAIRING THE ABOVE DINov 19, 1998 · Piper PA23SDR AU981123Trim Tab · cracked(AUS) RUDDER TRIM TAB CRACKED.Sep 1, 1998 · Govt N24ASDR EISA98165Skin · delamintatedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND LOWER RUDDER TAB DELAMINATED AT TRAILING EDGE LOWER CORNER. REPAIRED DELAMINATION PER SRM 51-40-6. (M)Jun 28, 1998 · N315NE · Boeing 727223SDR TC8A98023Tab · damagedTRIP NR 01787, AIRCRAFT VIBRATING AFTER 290 KTS (SUSPECT RUDDER) WITH AUTO-PILOT ON OR OFF, YAW DAMPER ON OR OFF. VIBRATION INCREASED WITH RUDDER HYDRAULIC POWER IN OFF POSITION. REMOVED AND REPLACED TAB ASSY, RUDDER OPS CHECK ON GROUND GOOD IAW DC8 MM 27-21May 10, 1998 · N181SK · Doug DC862SDR DHL9870723CTab · damagedAT C-CHECK, LOWER RUDDER TAB SEPARATING AT LOWER RT AFT EDGE. INSTALLED REPAIR PER SRM 51-40-8, 15 X 15. N/R 4840Apr 23, 1998 · N707DH · Boeing 72722SDR CALA9800563Skin · deterioratedINSPECTION FOUND LT LOWER SIDE OF UPPER RUDDER TAB FIBERGLASS REPAIR DETERIORATED. THE FIBERGLASS REPAIR WAS SANDED, REWORKED, AND PRIMED IAW SRM 51-40-9 AND 51-10-6.Mar 20, 1998 · N73751 · Boeing 727227SDR EISA98041Tab · moistureDURING D-CHECK, X-RAY INSPECTION OF RUDDER MOISTURE IN HONEYCOMB AS SHOWN IN SHOTS NR 5C, 9C AND 9D. CUT OUT PORTION OF RUDDER TAB TO REMOVE WATER. REMOVED WATER FROM HONEYCOMB PER SRM 51-40-09 USING VAC BAG METHOD. POTTED HONEY CORE PER SRM 51-40-06. FABRFeb 16, 1998 · N6819 · Boeing 727223SDR ABXA9701677Tab · delaminatedDURING C-CHECK, FOUND THE RUDDER TRIM TAB DELAMINATED AND SEPARATING. REPLACED RUDDER TAB IAW DC9 MM 27-20-2.Oct 13, 1997 · N954AX · Doug DC941SDR UPS97224046Tab · delaminatedINSPECTION TYPE-C, UPPER RUDDER TAB DELAMINATED. REPAIRED UPPER RUDDER TAB IAW SRM 51-40-6.Aug 6, 1997 · N940UP · Boeing 727185CSDR DHL9771705Tab · delaminatedDURING A CHECK, UPPER RUDDER TAB WAS FOUND DELAMINATED AT UPPER END. REMOVED UPPER RUDDER TAB AND INSTALLED BONDING REPAIR PER BOEING SRM 51-4-06, SIZE OF REPAIR 4 BY 20. UPPER RUDDER TAB WAS REINSTALLED PER M/M 27-20-11.Jul 28, 1997 · N717DH · Boeing 72723SDR MWEA97503Tab · delaminatedDURING D-CK, RUDDER CNTRL TAB LWR AFT CORNER DELAMINATED. MAINT REPAIRED IAW SRM 51-70-02.Jun 11, 1997 · N204ME · Doug DC932
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