JASC 5542

Service difficulty reports · 1,373

Reports filed under 5542 · Rudder, Plate/Skin, 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 = '5542'
  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 AWXA200601825Skin · delaminatedMCN - MAJOR REPAIR - C-16 CHECK - FOUND RIGHT RUDDER SKIN HAS AREA OF DELAMINATION, RUDDER STATION 101.00. REPAIRED RIGHT RUDDER SKIN, RUDDER STATION 101.00 IAW B737-300 SRM 51-70-04 FIGURE 10, REPAIR 1.Oct 16, 2006 · N311AW · Boeing 7373G7SDR 2006UALA01929Skin · wornRUDDER LE ON RT SIDE HAS WEAR AND DAMAGE INTO FIBER, 8" FROM BOTTOM EDGE. MAJOR REPAIR: INSTALLED 2 PLY REPAIR.Oct 6, 2006 · N373UA · Boeing 737322SDR C2XA06TY061Skin · damagedTYS, DURING AN INSPECTION THE RUDDER 2 TRAILING EDGE WAS FOUND DAMAGED. MAINTENANCE CUT OUT THE DAMAGED AREA, RECONTOURED ALL REQUIRED STRUCTURES AND SKIN, NO CRACKS FOUND ON NDI INSPECTION, FABRICATED SKIN SECTION, STRAPS AND STIFFENERS, ALODINED, PRIMED AND Oct 5, 2006 · N22909 · Emb EMB145LRSDR AWXA200601703Skin · delaminatedSAL - MAJOR REPAIR - DELAMINATION ON RUDDER RIGHT SKIN PANEL, 7" AFT OF RUDDER STATION BR7 / 569. REPAIRED RUDDER RIGHT SIDE SKIN PANEL, 7" AFT OF RUDDER STATION BR7 IAW A319 SRM 55-41-00, FIGURE 217.Sep 29, 2006 · N823AW · Airbus A319132SDR USAA061191Skin · damagedFOUND HOLE 6 INCHES DOWN FROM TOP, 12 INCHES AFT OF FWD L/E ON LT SIDE. REMOVED DAMAGED AND LAYED UP REPAIR DOUBLER PER EA 97998, DEFECT SIZE: .200 INCH.Sep 21, 2006 · N502UW · Boeing 737301SDR IXXA06SMN311SSkin · misrepairedDURING ROUTINE C-CHECK INSPECTION FOUND NON STANDARD REPAIR ON THE LEFT HAND SIDE OF THE RUDDER FROM STATION ZR 178.000 TO STATION ZR 188.781. REMOVED SKIN WITH NON STANDARD REPAIR. FABRICATED NEW SKIN (AL 2024 T3 0.040). CLEANED, TREATED, AND PRIMED AREA, Sep 18, 2006 · N825BX · Doug DC871FSDR DLM88070398Panel · crackedA 25.8 INCH LONG CRACK ALONG THE UPPER EDGE OF THE LEFT SIDE. AFT RUDDER PANEL AT STA ZR 143.00. PERMANENT REPAIR INSTALLED PER SRM 51-70-01A, PARA 22 AND FIG 60 AND INCLUDING MINOR DEVIATIONS PER SPECIFIED IN AEROMEXICO'S REPAIR DRAWING AMR0955064 R01. APPSep 11, 2006 · N934DL · Doug MD88SDR HALA0600891Skin · damagedRUDDER HAS FIBER DAMAGE 15" AND 36" FROM THE L/E, 35" FROM THE BOTTOM LT SIDE. REPAIRED RUDDER 15" AND 36" FROM THE T/E AND 35" FROM THE BOTTOM LT SIDE IAW SRM 55-40-01, SRM 51-70-17 AND SRM 51-60-03.Sep 7, 2006 · N597HA · Boeing 767332SDR HALA0600892Skin · damagedRUDDER HAS FIBER DAMAGE 7.5", 21.5", 22.5", 24", 33", AND 37" FROM THE T/E, 44", 86", 41.5", 43", 81", AND 34", FROM THE BOTTOM LT HAND SIDE. REPAIRED RUDDER, 7.5", 21.5", 22.5", 24", 33" AND 37" FROM THE BOTTOM LT SIDE, IAW SRM 55-40-01, SRM 51-70-17, AND SRSep 7, 2006 · N597HA · Boeing 767332SDR DHL2006805517Skin · corrodedLT RUDDER SKIN CORRODED STA ZR 257.908 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 55-6-1 FIG 1 PG 2. REMOVED CORROSION IAW SRM 51-1-8. FOUND OUT OF LIMITS IAW SRM 55-2-0 PG 12. REMOVED CORRODED PANEL PLATING IAW SRM 55-1-0 PG.1, SRM 51-1-21. FABRICATESep 7, 2006 · N805DH · Doug DC873FSDR USAA061018Skin · delaminatedDELAMINATION 20 INCHES AFT OF NR 6 HINGE POINT LT SIDE OF RUDDER. REMOVED DAMAGE, POTTED IN HONEYCOMB & FINISHED PER SRM 55-41-00 PG 243 FIG 206, DEFECT SIZE: 2 INCH DIA.Aug 7, 2006 · N758US · Airbus A319112SDR A6WA200640267Skin · dentedTEMPORARY DISPOSITION FOR THE DENTS TO RUDDER SKIN BETWEEN RS 108.25 AND RS 113.98. MAINTENANCE REPAIRED RUDDER BY CUTTING AWAY DAMAGE AND INSTALLING NON FLUSH DOUBLER IAW CRJ200 SRM 55-40-00. (M)Jun 26, 2006 · N408AW · Cndair CL6002B19SDR ASAA0640719Skin · gougedRUDDER LEADING EDGE IS GOUGED AT NUMBER 1 HINGE CUTOUT. PREPPED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW ASA EA 5540 01124.Jun 20, 2006 · N767AS · Boeing 737490SDR QXEA200602193Skin Panel · damagedPDX: TRAILING RUDDER: LT LOWER SKIN PANEL HAS 1 REPAIR DOUBLER INSTALLED BETWEEN FRONT TO REAR SPAR AND BETWEEN RIB 2 - RIB 4. RT UPPER SKIN PANEL HAS 1 REPAIR DOUBLER BETWEEN FRONT TO REAR SPAR AND BETWEEN RIB 26-RIB 28. BOTH REPAIR DOUBLERS ARE OUTSIDE LIMJun 17, 2006 · N424QX · Bombdr DHC8402SDR QXEA200602192Doubler · damagedPDX: FORE RUDDER, LT AND RT UPPER AND LOWER SKIN PANEL HAS REPAIRS INSTALLED REAR SPAR AND BETWEEN RIB 21-18, RIB 5-RIB 9. ALL REPAIR DOUBLER ARE OUTSIDE LIMITS OF RD 8/4-555-148 ISSUE 1. MAINTENANCE REPAIRED IAW Q400 SRM 51-42-05-330-801 AND HORIZON EA 6-55-1Jun 17, 2006 · N424QX · Bombdr DHC8402SDR QXEA200601671Skin · dentedYYC C3 TRAILING RUDDER IS DENTED ON THE LEFT HAND SIDE NEAR THE TRAILING EDGE BETWEEN THE LOWER AND MID HINGE HEIGHT. REPAIRED IAW RD 8/4-55-0273 AND EA 6-55-152.Jun 17, 2006 · N425QX · Bombdr DHC8402SDR MALA060427Skin · damagedRUDDER SUSTAINED HAIL DAMAGE AT 62 INCHES UP FROM BOTTOM AND 22 INCHES FWD OF TRAILING EDGE ON LT SIDE, 57.5 INCHES FROM BOTTOM AND 24 INCHES FWD OF TRAILING EDGE ON LT SIDE, 31 INCHES UP FROM BOTTOM AND 21 INCHES FWD OF TRAILING EDGE ON LT SIDE, 17 INCHES UP Jun 9, 2006 · N422XJ · Saab 340BSDR QXEA200601682Skin · dentedYYC C3 FORE RUDDER UPPER RIGHT HAND SKIN DENTS BETWEEN FRONT AND REAR SPAR AND BETWEEN RIB 16-17. REPAIRED IAW RD 8/4-55-0253, ISSUE 1 AND EA 6-55-132.Jun 6, 2006 · N425QX · Bombdr DHC8402SDR IXXA06SMN158SRepair · improperDURING ROUTINE C CHECK INSPECTION FOUND RUDDER LEADING EDGE LEFT HAND SKIN WITH NON STANDARD REPAIR AT STATION ZR 96.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 55-6-1 FIGURE 1. REMOVED EXISTING SKIN WITH NON STANDARD REPAIR IAW DC-8 SRM 51-1-21, DC-8 SRM 55-1-0May 19, 2006 · N830BX · Doug DC871FSDR IXXA06SMN154SRepair · improperDURING ROUTINE C CHECK INSPECTION FOUND RUDDER LEADING EDGE LT SKIN WITH IMPROPER REPAIR AT STATION ZR 159.094. PERFORMED MAJOR REPAIR IAW SRM 55-6-1 FIGURE 1. REMOVED SKIN WITH NON STANDARD REPAIR IAW SRM 51-1-21, DC-8 SRM 55-1-0 PAGE 1. FABRICATED NEW SKIN May 19, 2006 · N830BX · Doug DC871FSDR 06FDEA1827Wedge · chafedUPPER RUDDER, LEFT T/E WEDGE CHAFED APPROX 7.75 INCHES FROM UPPER T/E EDGE. REPAIRED UPPER RUDDER LT TE WEDGE CHAFED APPROX. 7.75" FROM UPPER EDGE UAW FED EX EA 7-5530-100549.May 11, 2006 · N493FE · Boeing 727200SDR 06FDEA1826Wedge · chafedUPPER RUDDER, RIGHT T/E WEDGE CHAFED APPROX 7.75 INCHES FROM UPPER T/E. REPAIRED UPPER RUDDER RT TE WEDGE CHAFF APPROX 7.75" FROM UPPER EDGE IAW FEDEX EA 7-5530-100549.May 11, 2006 · N493FE · Boeing 727200SDR 06FDEA1825Wedge · chafedUPPER RUDDER, RIGHT T/E WEDGE CHAFED APPROX 52 INCHES FROM BOTTOM EDGE. REPAIRED UPPER RUDDER RT TE WEDGE CHAFF APPROX 52" FROM BOTTOM IAW FED EX EA 7- 5530-100549.May 11, 2006 · N493FE · Boeing 727200SDR 06FDEA1824Wedge · chafedUPPER RUDDER, RIGHT T/E WEDGE CHAFED APPROX 46.5 INCHES FROM BOTTOM EDGE. REPAIRED UPPER RUDDER RT TE WEDGE APPROX 46.5" FROM BOTTOM IAW FED EX EA 7-5530- 100549.May 11, 2006 · N493FE · Boeing 727200SDR 06FDEA1823Wedge · chafedUPPER RUDDER, RIGHT T/E WEDGE CHAFED APPROX 43.75 INCH FROM BOTTOM EDGE. REPAIRED UPPER RUDDER RT TE WEDGE CHAFF APPROX 43.75" FROM BOTTOM IAW FEDEX EA 7-5530-100549.May 11, 2006 · N493FE · Boeing 727200SDR 06FDEA1819Wedge · chafedUPPER RUDDER, LEFT T/E WEDGE CHAFED APPROX 2 INCHES FROM BOTTOM EDGE.May 11, 2006 · N493FE · Boeing 727200SDR 06FDEA1817Wedge · chafedUPPER RUDDER LEFT T/E WEDGE CHAFED APPROX 24 INCHES FROM BOTTOM EDGE. REPAIRED UPPER RUDDER LT TE WEDGE APPROX 24" FROM BOTTOME IAW FED EX EA 7-5530-100549.May 11, 2006 · N493FE · Boeing 727200SDR 06FDEA1815Wedge · chafedUPPER RUDDER LEFT T/E WEDGE CHAFED APPROX 28.5 INCHES FROM BOTTOM EDGE. REPAIRED UPPER RUDDER LT TE WEDGE CHAFF APPROX 28.5" FROM BOTTOM IAW FEDEX EA 7-5530-100549.May 11, 2006 · N493FE · Boeing 727200SDR 06FDEA1814Wedge · chafedUPPER RUDDER RIGHT T/E WEDGE CHAFED APPROX 28.5 INCHES FROM BOTTOM EDGE. REPAIRED UPPER RUDDER RT TE WEDGE CHAFF APPROX. 28.5 " FROM BOTTOM IAW FED EX EA 7-5530-100549.May 11, 2006 · N493FE · Boeing 727200SDR 06FDEA1813Wedge · chafedUPPER RUDDER, RIGHT T/E WEDGE CHAFED APPROX 24 INCHES FROM BOTTOM EDGE. REPAIRED UPPER RUDDER RT TE WEDGE CHAFF APPROX. 24" FROM BOTTOM IAW FED EX EA 7-5530-100549.May 11, 2006 · N493FE · Boeing 727200SDR 06FDEA1812Wedge · chafedUPPER RUDDER, RT TIE WEDGE CHAFED APPROX 2 INCHES FROM BOTTOM EDGE. REPAIRED UPPER RUDDER RH T.E. WEDGE CHAFF APPROX 2" FROM BOTTOM EDGE IAW FED EX EA 7-5530-100549.May 11, 2006 · N493FE · Boeing 727200SDR 06FDEA1453Skin · puncturedUPPER RUDDER L/E SKIN HAS PUNCTURE AT LT SIDE AT RUDDER STA 160. REPAIRED PUNCTURE ON UPPER RUDDER L/E SKIN AT LT SIDE AT RUDDER STA 160 IAW EA 7-5530-96539.Apr 14, 2006 · N485FE · Boeing 727200SDR QXEA200601666Skin · damagedYYC C3 TRAILING RUDDER, LEFT HAND UPPER SKIN PANEL HAS A CREASE ON RIB 18 BETWEEN FRONT AND REAR SPAR. REPAIRED IAW RD 8/4-55-254, ISSUE 1 AND EA 6-55-134.Apr 12, 2006 · N425QX · Bombdr DHC8402SDR QXEA200601173Rivet · loosePDX: THERE ARE SEVERAL SMOKING RIVETS ON UPPER 12 INCH SQUARE OF TRAILING RUDDER BOTH SIDES. MAINTENANCE REPAIRED IAW HORIZON EO 6-55-120 AND SRM 51-25-15-370-801.Apr 10, 2006 · N405QX · Bombdr DHC8402SDR DHL2006764513Skin · dentedL/S UPPER RUDDER T/E DENTED (RED DOT). REMOVED AT L/S UPPER TRL ANGLE AS REQ IAW B727 SRM 51-30-2. FAB`D NEW RUDDER TRL ANGLE MAT USED 2024T3 .032 PO NR 53081 DIM 54 1/2" BY 7" IAW B727 SRM 55-40-2 FIG 2 AND 51-30-5. TREATED AND PRIMED AREA AND PART IAW B7Mar 31, 2006 · N764AT · Boeing 727264SDR UIEA200600071Panel · crackedLWR RUDDER SENT TO W/SHOP FOR THE FOLLOWING REPAIRS, LOWER CLOSURE PANEL BONDED STIFFENER FOUND BADLY WORN AT SEVERAL LOCATION. LOWER MOST FWD RIB FOUND CRACKED. LOWEST HINGE BEARING COVER MISSING PART NR 65B05501-1 S/N NSN. REPAIRED RUDDER INSTALLED IAW AMMar 23, 2006 · N540MC · Boeing 747243BSDR 06FDEA1192Skin · dentedWHILE WORKING LWR RUDDER CARD N01322 FOUND DENT AT 2 INCHES FROM LOWER END AT RT CENTER SKIN AREA. *S/D* REPAIRED LOWER RUDDER PER SRM 55-40-1.Mar 22, 2006 · N492FE · Boeing 727200SDR DHL2006801508Skin · corrodedRIGHT RUDDER EXTERNAL SKIN CORRODED, STA ZR 257.906 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 55-6-1 FIG 1. REMOVED CORROSION FROM RIGHT RUDDER EXTERNAL SKIN STA ZR 257.906 IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 55-2-0 PG 12. REMOVED CORMar 21, 2006 · N801DH · Doug DC873FSDR 2006UALA00513Skin · damagedRUDDER MR55225-133 LT SKIN 11.75 INCHES FROM T/E & 113.5 INCHES FROM BOTTOM SKIN HAS AREA APPROX 0.250 LONG DAMAGE DOWN TO TOP OF THIRD PLY. LT SPAR CAP FLANGE & RT EXTERNAL NOSE SKIN RUDDER STATION 3.0 ALSO DAMAGED. RUDDER SKIN, LH SPAR CAP FLANGE AND RT EMar 16, 2006 · N928UA · Boeing 737522SDR DHL2006750513Skin · dentedLT T/E SIDE OF UPPER RUDDER DENTED AT RUDDER TAB COURT (2ND FROM BOTTOM). FOUND DENT TO BE OUT OF LIMITS, ROUTED OUT DAMAGED AREA SIZE 3/8 BY 3/4 IAW B727 SRM 51-10-01. FABBED DOUBLER FROM 2024 T3 SIZE 4 BY 6 PO 9002416 IAW B727 SRM 51-40-2 FIG 3. TREATED Mar 15, 2006 · N750DH · Boeing 7272M7SDR 2006UALA00445Skin · damagedRUDDER AT NR 4 HINGE CUTOUT RIGHT UPPER EDGE DAMAGED. DAMAGE TO RUDDER AT NR 4 HINGE CUTOUT WAS REPAIR PER AAR EO I060062.Mar 8, 2006 · N326UA · Boeing 737322SDR ASAA0680223Skin · damagedFOUND RUDDER LEFT SURFACE IS DINGED 23 INCHES FROM T/E 20.5 INCHES AFT OF LOWER DAMPER CUTOUT. APPLIED FILLER PER SRM 51 70 1A PARA 21.Mar 2, 2006 · N962AS · Doug DC983SDR QXEA200600723Skin · wornYYC - C4 FORE RUDDER, LEADING EDGE, LEFT HAND SIDE AT UPPER HINGE POINT, SKIN HAS A WEAR MARK APPROXIMATELY 2" LONG BY .005" DEEP. REPAIRED IAW DHC-8-200 SRM 51-40-11, PAGES 1-4 AND HORIZON AIR EA 2-55-113.Feb 28, 2006 · N350PH · Dhav DHC8202SDR P5CA0601452Structure · damagedDURING PUSH OUT OF HANGAR AFTER A-CHECK, AIRCRAFT'S LT STABILIZER IMPACTED THE RUDDER OF A 767. DAMAGED AREA REPAIRED PER MM 55-10-01, AREA INSPECTED PER MM 05-00-00. ALL OPS CHECKS NORMAL.Feb 20, 2006 · N454PA · Boeing 74746NFSDR USAA060279Skin · gougedBELOW RUDDER STA 17.25 COMPOSITE LEADING EDGE. REPAIRED PER EA 82094 FIG 1 PG 2 & 3. DEFECT SIZE: 6 EA. GOUGESFeb 16, 2006 · N441US · Boeing 7374B7SDR 06FDEA0577Repair · unknownFOUND PREVIOUS REPAIR INSTALLED ON LOWER RUDDER, LT SIDE WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 55-40-3 FIG 1, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBER, GENERAL WORKMFeb 7, 2006 · N487FE · Boeing 727200SDR DHL2006804522Skin · crackedRT RUDDER L/E PLATING CRACKED 3 INCHES STA ZR 257.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 55-6-1 FIG 1 PG 2. REMOVED DAMAGED PLATING IAW SRM 55-1-0, SRM 51-1-21. FABRICATED NEW PLATING (AL2024T3 0.040") IAW SRM 55-6-1 FIG 1 PG 2 ITEM C. CLEANED,Jan 31, 2006 · N804DH · Doug DC873FSDR DHL2006804521Skin · crackedRIGHT RUDDER L/E PLATING CRACKED 0.75 INCH STA ZR 326.000 (MAJOR REPAIR) (DAMAGED). PERFORMED MAJOR REPAIR IAW SRM 55-6-1 FIG 1 PG 2. REMOVED DAMAGED PLATING IAW SRM 55-1-0, SRM 51-1-21. FABRICATED NEW PLATING (AL2024T3 0.040") IAW SRM 55-6-1 FIG 1 PG 2 ITEJan 31, 2006 · N804DH · Doug DC873FSDR 06FDEA0369Skin · dentedWHILE WORKING N01571 FOUND LT SKIN DENT AND GOUGE ON LOWER RUDDER. REPAIRED LOWER RUDDER PER SRM 55-40-3 FIG 1.Jan 24, 2006 · N490FE · Boeing 727200SDR IXXA06SMN032SSkin · corrodedDURING C CHECK INSPECTION, LT RUDDER EXTERNAL SKIN CORRODED, STA ZR 257.906. PERFORMED MAJOR REPAIR IAW DC8 SRM 55-6-1. REMOVED CORROSION IAW DC8 SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW DC8 SRM 55-2-0 PG 12. REMOVED CORRODED PLATING IAW DC8 SRM 55-1-0Jan 12, 2006 · N722CX · Doug DC872
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