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 C2XA01CL219Skin · crackedDURING OVERNIGHT MAINTENANCE RUDDER II SKIN WAS FOUND TO BE CRACKED 8 INCHES LONG AND ALSO HAD A I 1/4 INCH HOLE IN IT. THE CRACK STARTED APPROX 4 INCH FROM THE BOTTOM OF THE RUDDER. THE CRACK FOLLOWED THE TRAILING EDGE. MAINTENANCE REMOVED AND REPLACED RUDDEROct 31, 2001 · N13908 · Emb EMB145LRSDR USAA011330Skin · delaminatedPIT - FOUND RUDDER DELAMINATED 2.5 INCHES BY 8 INCH AREA, LEFT SIDE STATION 33 AND 34 APPROXIMATELY 10 INCHES FROM LEADING EDGE. REPAIRED PER EA 72581 AND SRM 51-70-17. (M)Oct 11, 2001 · N387US · Boeing 7373B7SDR CALA0100931Skin · gougedINSPECTION FOUND R/H RUDDER L/E SKIN GOUGED BELOW ACCESS PANEL 9559. REPAIRED IAW SRM 51-70-17 AND ECRA 5543-01017.Oct 4, 2001 · N10323 · Boeing 7373T0SDR GTIA010969Skin · delaminatedFTW - FOUND LEFT SIDE OF RUDDER HAS DELAMINATED IN MANY PLACES. REMOVED DAMAGED AREAS OF DELAMINATED. REPAIRED LEFT SIDE OF RUDDER IAW BOEING. BALANCED RUDDER PER SRM 55-40-01. (M)Aug 24, 2001 · N814NK · Doug DC983SDR QXEA0101377Cap · crackedPDX - CRACK ON RUDDER TOP CAP. REMOVED TOP CAP. FABRICATED NEW TOP CAM FROM 2024T3 .040 AND INSTALLED IAW E.A. # 6-55-02Aug 24, 2001 · N402QX · Dhav DHC8*SDR 01FDEA00735Skin · tornUPPER FWD LT CORNER OF LWR RUDDER HAS SECTION OF OUTER SKIN TORN. REMOVED AND REPLACED RUDDER PER EA 7-5540-58476.Aug 14, 2001 · N236FE · Boeing 727247SDR UPS01836203Skin Panel · corrodedINSPECTION TYPE:C2 RIGHT RUDDER PANEL IS CORRODED BEYOND LIMITS AT ZR 253. REMOVED, FABRICATED, AND REPLACED SKIN IAW DWG 5655077 AND EO M-5100-11491-B.Jun 14, 2001 · N705UP · Doug DC871FSDR USAA010741Skin · delaminatedPIT - FOUND RUDDER DELAMINATION .75 INCH BY .375 INCH AREA, FORWARD LOWER SKIN CORNER. REPAIRED PER EA 71466 PER SRM 5160-07, 51-70-17 FIG 18 OF BOEING MM. (M)Jun 10, 2001 · N524AU · Boeing 7373B7SDR UPS01836210Skin Panel · corrodedINSPECTION TYPE:C2 RUDDER TRAILING EDGE IS CORRODED BEYOND LIMITS AT APPROX ZR 168 P/N 5655077-80, JUST ABOVE RUDDER TAB. REMOVED, FABRICATED AND REPLACED RUDDER SKIN PANEL IAW DWG 5655077 AND SRM 51-1-21.Jun 6, 2001 · N705UP · Doug DC871FSDR QXEA0101023Skin · chafedYYC - CHAFE DAMAGE ON NOSE OF RUDDER 8 INCHES BELOW MID HINGE OPENING. REPAIRED IAW FOKKER SRM 55-02-07, FIGURE 1.May 29, 2001 · N481US · Fokker F28MK4000SDR USAA010547Skin · delaminatedPIT - FOUND RUDDER DELAMINATED AND GOUGED IN SEVERAL AREAS, LT AND RT RUDDER SKIN AND ONE LEADING EDGE GOUGE. COMPOSITE WET LAYUP REPAIR 230. (M)Apr 30, 2001 · N574US · Boeing 737301SDR MWEA010654Skin · crackedRUDDER SKIN IS CRACKED AT RIB NR 3 LEFT SIDE. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER.Apr 25, 2001 · N204ME · Doug DC932SDR QXEA0100603Skin · delaminatedYYC- RUDDER TRAILING EDGE TO BE REPLACED DUE TO EXCESSIVE DELAMINATION. REPAIRED IAW FOKKER SRM 51-10-05.Apr 2, 2001 · N493US · Fokker F28MK4000SDR MWEA010508Skin · dentedDENT IN RUDDER SKIN AT STATION ZR 117 ON LEFT SIDE JUST AFT OF LEADING EDGE PANEL. FABRICATED SKIN PANEL AND SKIN, INSTALLED SKIN, FABRICATED AND INSTALLED NEW BALANCE TAG.Apr 2, 2001 · N800ME · Doug DC914SDR SWAA010962Skin · delaminatedDURING SCHEDULED A2 CHECK, FOUND 12 X 6 DELAMINATION ON RUDDER, LT SIDE, 35 ABOVE BOTTOM, 12 AFT OF L/E. MX FERRIED AIRCRAFT TO HOU. REMOVED AND REPLACED RUDDER PER MM.Mar 29, 2001 · N762SW · Boeing 7377H4SDR QXEA0100379Doubler · misinstalledYYC-RUDDER ACCESS PANEL 57V DOUBLER PLATE WAS INCORRECTLY INSTALLED. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13, 14.Mar 12, 2001 · N497US · Fokker F28MK4000SDR QXEA0100378Doubler · crackedYYC-RUDDER ACCESS PANEL 57V DOUBLER CRACKED. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13, 14.Mar 8, 2001 · N497US · Fokker F28MK4000SDR QXEA0100376Doubler · crackedYYC-RUDDER ACCESS PANEL 57Y RIGHT HAND DOUBLER CRACKED. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13, 14.Mar 8, 2001 · N497US · Fokker F28MK4000SDR RRXA10747Skin · damagedDURING A MAINTENANCE VISIT FOUND HOLE DAMAGE TO SKIN AT HOLE 62 AND RUDDER POWER PACK LEDGE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND ISTALLED IAW SRM 51-1-4 AND DC-8 SRM 51-1-21.Mar 1, 2001 · N8091U · Doug DC871FSDR UPS01235107Fairing · damagedINSPECTION TYPE:N/A BTB-DURING T/O ROLL SOMETHING RESTRICTED THE RUDDER WHEN LT RUDDER PEDAL APPLIED. *S/D* FOUND WEAR STRIP ON TOP/LT CORNER OF LOWER RUDDER AND THE FAIRING JUST FORWARD OF STRIP DAMAGED. REMOVED FAIRING SECTION, RUDDER OPS WAS NORMAL. OK Feb 28, 2001 · N951UP · Boeing 72725CSDR TWAA0103406Skin · damagedDURING CHECK-C MAINT FOUND RUDDER WITH DAMAGE SPOT ON RT SIDE, FWD OF RUDDER TAB UPPER HINGE AREA, GROUND THRU FLAME SPRAY. REPAIRED DAMAGE PER SRM 51-70-1A, FIG 58. RUDDER PAINTED AND BALANCED.Feb 21, 2001 · N957U · Doug DC982SDR MWEA010166Skin · dentedRUDDER LEFT SKIN HAS .75 INCH BY .75 INCH DENT .010 INCH DEEP AT ZR 28.936. REMOVED AND REPLACED DOUBLER.Feb 19, 2001 · N212ME · Doug DC932SDR MWEA010156Skin · dentedLEFT LOWER SIDE OF RUDDER HAS FOUR DENTS ON SKIN. MAINTENANCE INSTALLED REPAIR DOUBLER.Feb 13, 2001 · N809ME · Doug DC981SDR USAA010171Skin · wornPIT - FOUND SKIN WORN .25 INCH BY .5 INCH THROUGH 4 PLIES, RUDDER STATION 0.0 RT SIDE LEADING EDGE. STEP SAND INSTALLED 6 LAY OF CLOTH CURED 200-230 FINISHED PER APPEAR MN PER EA 70006 AND SRM 51-70-17. (M)Feb 2, 2001 · N519AU · Boeing 7373B7SDR QXEA0100112Skin · crackedPDX- TOP RIGHT HAND SIDE OF TRAILING RUDDER SKIN HAS A CRACK PROGRESSING OUT FROM RIVET HOLE AT PREVIOUS REPAIR SKIN PATCH. REPAIRED IAW DHC-8 SRM 55-40-28 AND 51-40-00.Jan 30, 2001 · N814PH · Dhav DHC8102SDR COMA0160176Skin · dentedRUDDER SKIN IS DENTED ON THE LEFT SIDE SKIN PANEL AT RS 99.43. PERFORMED A MAJOR REPAIR TO THE LEFT SIDE OF THE RUDDER RS 99.43 BY CUTTING OUT THE DAMAGE, FABRICATING A EXTERNAL DOUBLER MADE FROM 2024-T3 .040 PO 12676/1 AND INSTALLED IAW WVAC EO 601R-55-2174AJan 29, 2001 · N937CA · Cndair CL6002B19SDR 20010226CW004Fabric · damagedRUDDER WAS BEYOND PATCHING. NEEDS RECOVER.Jan 23, 2001 · N44911 · Doug C54BDCSDR USAA001947Skin · delaminatedPIT - FOUND RUDDER DELAMINATED IN 7 AREAS, LEFT AND RIGHT RUDDER SKIN DELAMINATE 1ST LAYER. 200-230 DEGREE CURE. WET LAY UP REPAIR USING 51-70-17 THEN BALANCED PER 51-60-00 AND EA 56867. (M)Nov 18, 2000 · N376US · Boeing 7373B7SDR CA001207007Skin · cracked(CAN) DURING ROUTINE MAINTENANCE INSPECTION, STARBOARD SIDE OF FORE RUDDER FOUND TO HAVE A 10 INCH C SHAPE CRACK. FORE RUDDER ASSEMBLY REPLACED IN ACCORDANCE WITH DEHAVILLAND DASH 8 MM CHP 27-20-00.AIRCRAFT RETURNED TO SERVICE.Nov 15, 2000 · Dhav DHC8102SDR PCAA0011073Skin · crackedBGM- DURING ROUTINE MAINTENANCE INSPECTION STARBOARD SIDE OF FORE RUDDER FOUND TO HAVE A 10 INCH C-SHAPE CRACK. FORE RUDDER ASSEMBLY REPLACED IN ACCORDANCE WITH DEHAVILLAND DASH 8 MAINTENANCE MANUAL CHAPTER 27-20-00. AIRCRAFT RETURNED TO SERVICE.Nov 15, 2000 · N835EX · Dhav DHC8102SDR P2EA00285Rudder · delaminatedSJO - DURING C-CHECK, RUDDER DELAMINATION BETWEEN STA 17.25 AND STA 35.25. REPAIRED RUDDER IAW SRM 51-40-9, PARAGRAPH 3 AND PARAGRAPH 5, FIG 3. (X)Sep 28, 2000 · N620PC · Boeing 737244SDR QXEA0002798Skin · damagedYXX- VERTICAL STABILIZER SHROUD AND RUDDER SKIN DAMAGED ON RIGHT HAND SIDE AT RIB 12. REPAIRED IAW DHC-8 SRM 51-40-11, PAGE 1-4, SRM 51-40-00, PAGE 1-6, AND SRM 55-40-28.Sep 26, 2000 · N368PH · Dhav DHC8202SDR MZZA00021Skin · corrodedTNN - DURING 1/4D CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SKIN BULGED WAS FOUND ON UPPER RUDDER TAB LEFT SIDE SKIN FROM FS 175 TO FS 212. THE DAMAGED SKIN WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. (M)Sep 18, 2000 · N79743 · Boeing 727224SDR QXEA0002349Skin · dentedYXX- DENT IN UPPER RIGHT HAND SIDE OF FORWARD RUDDER 4 INCHES FORWARD OF AFT SPAR AT UPPER HINGE LINE. REPAIRED IAW DHC-8 SRM 55-40-16, 55-40-28, AND 51-00-06.Aug 17, 2000 · N822PH · Dhav DHC8102SDR MWEA00569Skin · corrodedRUDDER HAS LIGHT CORROSION ON INSIDE SURFACE OF SKIN. FABRICATED AND INSTALLED REPAIR DOUBLER.Jul 20, 2000 · N502ME · Doug DC932SDR SWAA001092Skin · delaminatedDURING SCHEDULED D-CHECK, FOUND 2 X 2 INCH AREA OF DELAMINATION ON RT SIDE OF RUDDER SKIN, 98 INCHES FROM BOTTOM SIDE NEAR T/E. REPAIRED SKIN SECTION PER SRM.Jun 13, 2000 · Boeing 7372H4SDR QXEA0001556Skin · dentedYXX- DENTS ON TRAILING RUDDER AT LEFT HAND SKIN. REPAIRED IAW DHC-8 SRM 55-40-16 AND SRM 55-40-28, FIGURE 3.Jun 6, 2000 · N361PH · Dhav DHC8202SDR AU000438Skin · cracked(AUS) FORE RUDDER SKIN CRACKED IN TOP LH CORNER. INSPECTION FOUND THAT THE LAST (REARMOST) RIVET ON THE STIFFENER PNO 85540025-101 WAS INCORRECTLY FITTED.Jun 3, 2000 · Dhav DHC8102SDR QXEA0001626Access Panel · crackedYYC- ACCESS PANEL REBATE CRACKED UNDER PANEL 57V ON LEFT HAND SIDE OF RUDDER. REPAIRED IAW FOKKER SRM 51-31-01.May 18, 2000 · N480AU · Fokker F28MK4000SDR 20000614SH010Skin · dentedDURING THE STRIPPING/PAINTING PROCESS OF THE AIRCRAFT THAT IS CURRENTLY IN WORK AT CRS QU2R122L, A DENT WAS UNCOVERED ON THE UPPER RIGHT HAND SIDE OF THE RUDDER. THE DENT WAS HIDDEN DAMAGE AND COVERED WITH PAINT AND FILLER. GULFSTREAM IS CURRENTLY INSPECTINGMay 11, 2000 · N102CX · Gulstm G1159SDR L1GA200000123Skin · corrodedLEVEL 2 CORROSION LWR RUDDER ACCESS HOLES.May 10, 2000 · N27509 · Doug DC932SDR CALA0000471Skin · dentedINSPECTION FOUND EXTERNAL SKIN OF LT SIDE OF RUDDER DENTED BETWEEN CENTER AND LOWER HINGE POINT. A REPAIR DOUBLER WAS INSTALLED IAW SRM 55-01, FIGURE 10A, 51-10-4, 51-10-3, AND 51-30-6.Apr 14, 2000 · N16804 · Doug DC982SDR L1GA200000015Access Panel · corrodedCORROSION ON RIGHT RUDDER ACCESS PANEL 3602A HARDWARE.Apr 10, 2000 · N12508 · Doug DC932SDR TWAA0005604Skin · crackedDURING OP 16 MAINT CHECK, FOUND CRACK ON RUDDER APPROX .75 INCH AT LOWER LT EDGE, 29 INCHES AFT OF FWD EDGE. REPAIRED PER ARA 16712.Mar 25, 2000 · N984Z · Doug DC931SDR ASAA0040037Skin · gougedSEA - DURING SCHEDULED C-CHECK, THE RIGHT SIDE OF THE RUDDER LEADING EDGE SKIN WAS FOUND TO BE GOUGED. REPAIRED PER EA 5540-01041. (M)Mar 22, 2000 · N786AS · Boeing 7374S3SDR CALA0000299Skin · dentedINSPECTION FOUND RUDDER SKIN DENTED AT UPPER LEFT SIDE. THE DENTED AREA WAS REMOVED. A FILLER AND DOUBLER REPAIR WAS INSTALLED IAW SRM 55-03 AND 51-10-3.Mar 11, 2000 · N17812 · Doug DC982SDR UPS00432146Skin · damagedINSPECTION TYPE:C 44. DAMAGE TO L/E OF UPPER RUDDER JUST BELOW PCU (LHS), PLEASE INVESTIGATE. NEW SKIN PANEL FABRICATED IAW E0097709 AND INSTALLED IAW SRM 51-30-02.Feb 26, 2000 · N522UP · Boeing 747212BSDR TWAA0003015Skin · bentDURING CHECK-C MAINT, FOUND SKIN DAMAGED/BENT AT TOP OF RUDDER SPAR CAP, RT SIDE. ACCOMP HIGH FREQ EDDY CURRENT AND CHECKED AREA. RECONTOURED AREA RECHECKED WITH HFEC PER ARA 16525.Feb 16, 2000 · N952U · Doug DC982SDR EISA2000024Skin · gougedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND GOUGE IN SKIN OF LOWER RUDDER RIGHT SIDE TRAILING EDGE. BURNISHED GOUGE. MATERIAL LOSS OUT OF LIMITS. FABRICATED EXTERNAL DOUBLER AND INSTALLED PER SRM 55-40-2 FIG 1. (M)Jan 18, 2000 · N721RW · Boeing 7272M7SDR QXEA0000441Skin · crackedPDX - BOTTOM END PLATE OF RUDDER COVE DENTED AND CRACKED OUT AROUND RIVET, LEFT-HAND SIDE. REPAIRED IAW FOKKER SRM 53-02-02, SRM 51-31-01 AND SRM 51-30-02.Jan 16, 2000 · N477AU · Fokker F28MK4000
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