JASC 5532

Service difficulty reports · 1,754

Reports filed under 5532 · Vertical Stabilizer, 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 = '5532'
  ORDER BY difficulty_date DESC"

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SDR AALA20010690Skin · scratchedTUL - LOWER LEFT VERTICAL STABILIZER HAS DEEP SCRATCH 3 INCHES BY .25 INCH JUST ABOVE TAIL NR. INSTALLED DOUBLER PER SRM 53-30-3 FIG 1. (M)Apr 3, 2001 · N729AA · Boeing 727227SDR 2001UALA00339Skin · dentedDENT IN VERTICAL STABILIZER LEADING EDGE APPROXIMATELY 8 INCHES ABOVE THE FUSELAGE. REPAIRED DENT IN VERTICAL STABILIZER LEADING EDGE. MAJOR REPAIR ACCOMPLISHED.Mar 27, 2001 · N309UA · Boeing 737322SDR GAIA01112STSkin · crackedDURING A ROUTINE INSPECTION BEING PERFORMED AT FLIGHTSTAR AIRCRAFT SERVICES AT JAX, IT WAS DISCOVERED THAT THE RIGHT VERTICAL STABILIZER ROOT AT BS 1342, STRINGER S-10R IS CRACKED. REPAIRED PER BOEING SERVICE BULLETIN 727-55-82. THE AIRCRAFT WAS RETURNED TO Mar 12, 2001 · N278US · Boeing 727251SDR AT0100115Skin · chafedFOUND UPPER VERTICAL STAB PANEL CHAFING ON FORWARD STRUCTURE. BLENDED CHAFED AREAS, FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR SECTIONS AND INSTALLED IAW DC9 SRM 55-01 FIGURE 2 AND 51-10-2.Mar 6, 2001 · N847AT · Doug DC932SDR 2001UALA00224Skin · delaminatedRT VERTICAL FIN PANEL 9608 IS DELAMINATED. REPAIRED PANEL PER GN MM 1-0-1-24 AND GN MM 1-0-1-66. INSTALLED NEW CORE FILLER AND REPLACED INNER AND OUTER SKIN.Mar 1, 2001 · N7467U · Boeing 727222SDR EIA2001075Fairing · delaminatedMZJ-EAC - FOUND LEFT ELEVATOR BOTTOM FAIRING WORN, DELAMINATION PRESENT, RIVETS POPPED AND FINGER DOUBLERS PEELING UP. METAL AND METAL LAMINATED HOT BOND REPAIR MADE PER ECRA 933-55-080-2. (M)Feb 28, 2001 · N933F · Doug DC933FSDR EIA2001080Fairing · delaminatedMZJ-EAC - FOUND RIGHT ELEVATOR BOTTOM FAIRING WORN WITH DELAMINATION PRESENT AND RIVETS POPPED. METAL AND METAL LAMINATED HOT BOND REPAIR MADE PER ECRA 933-55-080-2 REV A AND DC9 SRM 51-70-2 PAGE 183. (M)Feb 28, 2001 · N933F · Doug DC933FSDR GAIA01048STSkin · crackedDURING A LTC INSPECTION AT FLIGHTSTAR JAX, THE RIGHT VERTICAL STAB ROOT AT BS 1342 SKIN CRACKED AT STRINGER 10R. ACCOMPLISHED DOUBLER REPAIR IAW B727 SERVICE BULLETIN 727-55-82 FIG 2 AND FIG 3 MATERIAL 2024 T3 .063 PO NR 9812 DIM''S 10 INCH BY 5.5 INCH. THE Feb 28, 2001 · N281KH · Boeing 7272J0SDR 20010403CW018Skin · damagedCORROSION FOUND EXFOLIATING (1) SPAR CAP ON RIGHT WING HEAVY CORROSION ON (2) UPPER CABIN CARRY THRU STRUCTURE. (3) VERTICAL STABILIZER SKIN PILLOWED AND RIVETS POPPED. FOUND 15 RIVET HEADS PULLED THRU SKIN ON (4)CANTED BULKHEAD AT FUSELAGE STATION 20.5 BOTTFeb 26, 2001 · N3232X · Cessna 150GSDR CA010409002Strap · worn(CAN) FAIRINGS WERE REMOVED FOR OTHER WORK AND PLATE AND STRAP WERE FOUND WORN. THESE PARTS ENGAGE TO PREVENT FLUTTER OF THE FAIRINGS. THE STRAP IS RIVETED TO THE TOP OF THE REAR VERTICAL STABILIZER SPAR AND THE PLATE IS ATTACHED TO THE FAIRING. BOTH PARTS WERFeb 14, 2001 · Pilats PC1245SDR 0101062284Skin · crackedDURING H-CHECK, FOUND CRACK ON THE LT VERTICAL FIN SKIN AT FIN STA 13.7 STRINGER 10. REPAIRED PER EA 22-182196.Feb 14, 2001 · N284US · Boeing 727251SDR AT0100104Panel · chafedFOUND VERTICAL STABILIZER UPPER FAIRING CHAFED OUT OF LIMITS. REPLACED SKIN PANEL IAW DC9 SRM 55-01 FIG 1, 55-31, 51-10-02, 51-10-03, 51-10-04, AND 51-30-02.Feb 8, 2001 · N824AT · Doug DC932SDR DHL2001367507Attach Angle · corrodedC-CHECK--VERT STAB RIB 1 ATTACH ANGLE TO FRONT SPAR HAS CORROSION ON SURFACE. N/R 78826. CORROSION REMOVED IAW SRM 51-40-11, METAL REMOVED= .006-.008, WITHIN LIMITS REF SRM 55-30-00, PG 602 LIMITS, REPROTECTED AREA.Jan 30, 2001 · N367DH · Airbus A300B4203SDR DL72S010047Skin · crackedA CRACK WAS FOUND IN THE RT SIDE SKIN OF THE VERTICAL STABILIZER EMANATING FROM UNDER THE FUSELAGE TO STABILIZER CREASE CHORD AT STA 1209. THE CRACK IS REPAIRED WITH AN EXTERNAL DOUBLER INSTALLED PER SRM 55-30-3, FIG 7 AND PER THE REQUIREMENTS OF ER/A 379749-Jan 9, 2001 · N535DA · Boeing 727232SDR ERKR200100058Skin · gougedAUTHORIZES THE REPAIR OF GOUGE DAMAGE TO THE SKIN AND FINGER DOUBLER OF THE VERTICAL STABILLIZER REMOVABLE TIP FAIRING AT YV248, ZV141, R/H, L/H. THE REPAIR CONSISTS OF TRIMMING OUT THE DAMAGE AND ADDING A REPAIR DOUBLER BEHIND THE SKIN AND FINGER DOUBLER. PERJan 8, 2001 · N933F · Doug DC933FSDR DL72S002485Skin · crackedFOUND ON F2 LETTER CK 1 INCH AND 3/8 IN CRACK IN VERTICAL STAB SKIN BELOW L/H SIDE OF ACCESS PANEL 9501. REPAIRED PER SRM 55-30-3.Dec 20, 2000 · N533DA · Boeing 727232SDR QXEA0003347Skin · dentedPDX- RIGHT SIDE VERTICAL STABILIZER SKIN IS DENTED AFT OF FRONT SPAR AND 16 INCHES BELOW RIB 5. REPAIRED IAW HORIZON AIR EA 4-55-269, FOKKER SRM 51-70-0 AND 55-01-01.Dec 3, 2000 · N492US · Fokker F28MK4000SDR SWAA002528Skin · crackedDURING SCHEDULED A1 CHECK, FOUND .5 EXTERNAL SKIN CRACK ON L/H VERTICAL STAB PITOT CUTOUT. REPAIRED VERTICAL STAB SKIN PER RA 1-755-0382.Dec 2, 2000 · N747SA · Boeing 7377H4SDR QXEA0003361Skin · damagedPDX- VERTICAL STABILIZER OUTER SKIN HAS 5 WORKING FASTENERS ON BOTTOM RIGHT HAND SIDE AT FORWARD SPAR. REPAIRED IAW FOKKER SRM 51-30-02 AND 51-31-01.Nov 30, 2000 · N492US · Fokker F28MK4000SDR AT0100031Skin · chafedFOUND CHAFE MARKS OUT OF LIMITS IN VERTICAL STABILIZER LEADING EDGE. REPLACED LEADING EDGE OF VERTICAL STABILIZER IAW DC9 SRM 55-01 FIG 1.Nov 17, 2000 · N839AT · Doug DC932SDR COMA0060864Pin · scoredHORIZONTAL STAB INNER PIVOT PIN AND OUTER PIVOT P/N SEIZED. REMOVED SCORED/GAUGED BUSHING FROM RT VERT STAB FITTING AT HORIZONTAL STAB PIVOT POINT. INSTALLED NEW BUSHING P/N 600-21061-7 (THAT WAS MACHINED IAW WVAC EO 601R-55-1842) IAW CRJ MM 20-26-00-910-803Oct 27, 2000 · N938CA · Cndair CL6002B19SDR CALA0001643Skin · crackedINSPECTION FOUND A 1 INCH CRACK ACROSS FASTENER IN VERTICAL STABILIZER LEADING EDGE AT RT SIDE JUST BELOW RIGHT LOWER VOR ANTENNA. REPAIRED IAW ECRA 5530-01285.Oct 24, 2000 · N16883 · Doug DC981SDR CA001107020Stabilizer · cracked(CAN) CRACK FOUND ON UPPER VERTICAL FIN LOWER SECTION OF LEADING EDGE BETWEEN TWO RIVETS, 2.6250 INCHES ABOVE STAMPED FITTING, 2.50 INCHES, LENGTH OF CRACK. (X)Oct 20, 2000 · Snias AS350BSDR RRXA003225Plate · damagedDURING A MAINTENANCE VISIT FOUND ELONGATED HOLE IN PLATE VERT STAB AT STA 1680 LEFT L/E, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 20, 2000 · N500MH · Doug DC871FSDR CALA0001612Skin · chafedINSPECTION FOUND A HOLE CHAFED THROUGH VERTICAL STABILIZER SKIN AT UPPER LT SIDE ABOVE RUDDER FAIRING. A FREEZE PLUG AND DOUBLER WERE INSTALLED IAW EA 9-5532-2-A0792.Oct 20, 2000 · N14871 · Doug DC981SDR CALA0001605Doubler · chafedINSPECTION FOUND RT SIDE UPPER VERTICAL STABILIZER DOUBLER CHAFED ABOVE RUDDER FAIRING. THE FAIRING WAS REMOVED IAW SRM 51-30-1. THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-30-2, 51-10-4, 51-10-3, AND EA 9-5532-2-A0792. REINSTALLED FAOct 20, 2000 · N14871 · Doug DC981SDR DL72L002131Plate · corrodedAT HMV, THE VERT STAB TENSION TIE PLATE AFT CTR ATTACH POINTS WERE CORRODED AROUND FACE AND IN BORES. REMOVED CORR DYE PEN CK GOOD WITHIN LIMITS PER SRM 55-30-5D FIG 801D. REAMED HOLES TO .691 TI REM CIRR BHEC INSP NO ITEMS OPENED HOLES TO .737 BFEC INSP NO Oct 9, 2000 · N508DA · Boeing 727232SDR 2000UALA00663Skin · puncturedDUE TO CONTACT WITH GROUND EQUIPMENT, THE VERTICAL STABILIZER LT SIDE SKIN SUSTAINED SCRATCH, PUNCTURE AND DELAMINATION DAMAGE FROM AFT OF S-2 TO S-4, AND OVER A 7 INCHES REGION UP FROM RIB 4. THE SKIN ATTACH AND BOUND FLANGES OF S-3 WERE DAMAGED ABOUT 6 INCHOct 4, 2000 · N802UA · Airbus A319131SDR 20001120SH041Skin · dentedDENT IN VERTICAL LEAKING EDGE AT STA 236. FOUND DURING C-CHECK. CAUSE UNKNOWN. (X)Oct 2, 2000 · N362PRSDR 20001106SH041Fairing · gougedGOUGES IN VERTICAL STABILIZER TIP FAIRING. RIGHT, YV248, ZV141. (X)Sep 20, 2000 · N944F · Doug DC933FSDR DHL200070806CPanel · crackedVERT STAB RT LWR SLIDING SEAL TRACK AREA LWR FIX PANEL HAS 2 CRACKS. REMOVED AND REPLACED PANEL PER SRM 55-30-2. ALODINED AND PRIMED PER SRM 51-10-2.Sep 20, 2000 · N708DH · Boeing 72725SDR EIA2000339Skin · gougedEAC-MZJ - VERTICAL STABILIZER REMOVEABLE TIP FAIRING AT YV248, ZV141 RHS GOUGE DAMAGE TO SKIN AND FINGER DOUBLER. TRIMMED OUT DAMAGE AND INSTALLED REPAIR FILLER AND DOUBLER PER ECRA 944-55-123-2 REV A. (M)Sep 18, 2000 · N944F · Doug DC933FSDR AT0000445Skin · gougedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND VERTICAL STABILIZER RIGHT SKIN GOUGED BEYOND LIMITS. REMOVED AND REPLACED SKIN IAW DC9 SRM 51-10-02, 51-10-04, 51-30-01, 51-30-02, AND 51-30-05.Sep 11, 2000 · N832AT · Doug DC932SDR QXEA0002385Skin · misdrilledPDX- 7 HOLES DRILLED IN LEFT HAND VERTICAL STABILIZER BELOW PANEL 56C. REPAIRED IAW FOKKER SRM 51-10-04.Aug 22, 2000 · N479AU · Fokker F28MK4000SDR AWXA0000543Skin · crackedC-CHECK, DORSAL FIN TOP AFT SKIN CRACKED. REMOVED DAMAGE, FABED, AND INSTALLED REPAIR DOUBLER AND FILLER IAW 737 SRM 55-30-6.Aug 17, 2000 · N184AW · Boeing 737277SDR DHL200070925CPanel · damagedVERT STABILIZER, L/E FIN PANEL NR 9501, SEVERAL FASTENER HOLES ARE OVERSIZED. INSTALLED DOUBLER PER SRM 51-10-2. ALODINED AND PRIMED PER SRM 51-10-2.Jul 8, 2000 · N709DH · Boeing 72782CSDR QXEA0002057Skin · dentedPDX- DENT IN RIGHT HAND VERTICAL SKIN FORWARD OF SPAR 1 AND BELOW RIB 3, 4. REPAIRED IAW HORIZON AIR EA 4-53-234.Jul 8, 2000 · N491US · Fokker F28MK4000SDR CALA0001000Skin · crackedINSPECTION FOUND A 1.8 INCH CRACK IN VERTICAL STABILIZER SKIN AT BASE OF STABILIZER, STA 1437, LT SIDE. A 4 INCH CRACK WAS FOUND IN VERTICAL STABILIZER SKIN AT BASE OF STABILIZER, STA 1437, RT SIDE. REPAIR DOUBLERS WERE INSTALLED AT EACH LOCATION IAW ECRA 5340Jun 30, 2000 · N13881 · Doug DC981SDR MWEA00528Skin · gougedMKE - VERTICAL STABILIZER SKIN IS GOUGED AT RIGHT SIDE LEADING EDGE JUST BELOW HORIZONTAL STABILIZER. MAINTENANCE REMOVED DAMAGED AREA AND FABRICATED AND INSTALLED REPAIR DOUBLERS AND FILLER. (X)Jun 19, 2000 · N700ME · Doug DC914SDR CALA0000852Panel · crackedINSPECTION FOUND A 1 INCH CRACK IN VERTICAL STABILIZER PANEL NR 6310. A REPAIR DOUBLER WAS INSTALLED IAW SRM 55-01, FIGURE 2, 51-10-3, AND 51-30-2.Jun 9, 2000 · N14879 · Doug DC983SDR DHL200070729CPanel · chippedAT C CK; RT VERTICAL STAB PANEL 9604-HONEYCOMB SHOWING THRU AND CHIPPED SURFACE. INSTALLED FIBERGLASS CLOTH OVERLAY REPAIR PER B727 SRM 51-40-8 FIG. 1. PAINTED RH VERT STAB IAW B727 M/M 51-20-0. REF: N/R 4543.Jun 8, 2000 · N707DH · Boeing 72722SDR QXEA0001624Skin · dentedYYC- DENT FOUND BETWEEN RIB 3.5 AND 3.4 1/2, 2 1/2 FORWARD OF STATION 27060 (RIGHT HAND VERTICAL STABILIZER). REPAIRED IAW HORIZON AIR EA 4-55-210.Jun 1, 2000 · N480AU · Fokker F28MK4000SDR ABXA000280Skin · crackedDURING C-CHECK, FOUND THE VERTICAL STABILIZER SKIN CRACKED UNDER PANEL NR 3804. REPLACED SKIN IAW DC9 SRM 51-30-1.May 26, 2000 · N947AX · Doug DC931SDR ABXA000279Skin · crackedDURING C-CHECK, FOUND VERTICAL STABILIZER SKIN CRACKED AT PANEL NR 3703. REPLACED SKIN IAW DC9 SRM 51-30-1.May 26, 2000 · N947AX · Doug DC931SDR QXEA0001628Skin · crackedYYC- VERTICAL STABILIZER TRAILING EDGE SKIN HAS TWO CRACKS. REPAIRED IAW FOKKER SRM 55-31-01 FIGURE 1, 55-02-05 FIGURE 5 AND 51-31-01.May 24, 2000 · N480AU · Fokker F28MK4000SDR RAAA00B1062Skin · corrodedDURING SCHEDULED C2 CHECK, FOUND CORROSION ON VERTICAL FIN SKIN. REPLACED IAW 727 SRM 55-30-3 FIG 1 SHEET 2, 51-20-4, 51-30-2.May 24, 2000 · N831RV · Boeing 72722CSDR QXEA0001631Skin · looseYYC- VERTICAL STABILIZER UPPER SECTION INTERMITTENT SPAR II AND SKIN CONNECTION, BOTH LEFT HAND AND RIGHT HAND SKIN LOOSE. REPAIRED IAW HORIZON AIR EA 4-55-209.May 22, 2000 · N480AU · Fokker F28MK4000SDR F3LA00104Skin · damagedDEN - DURING C-7 CHECK, INSPECTION REPORTED VERTICAL STABILIZER LEADING EDGE SKIN DAMAGED. MAINTENANCE REMOVED DAMAGED AREA, FABARICATED PATCH AND DOUBLER, AND REPAIRED PER SRM 55-30-6. (X)May 21, 2000 · N270FL · Boeing 7372L9SDR QXEA0001630Skin · crackedYYC- VERTICAL STABILIZER RIGHT HAND AFT LOWER SECTION REPAIR PATCH IS CRACKED. REPAIRED IAW FOKKER SRM 51-31-01.May 20, 2000 · N480AU · Fokker F28MK4000SDR ABXA000290Skin · crackedDURING C-CHECK, FOUND RIGHT SIDE VERTICAL STABILIZER CRACKED ABOVE TOP OF RUDDER, 4 INCHES LONG. REPAIRED IAW DC9 SRM 55-01.May 17, 2000 · N946AX · Doug DC931
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