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"

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 00FDEA00344Skin · crackedDURING ROUTINE INSPECTION, EXTERIOR SKIN LEFT SIDE VERTICAL STABILIZER CRACKED AT FIN STA 87, WL 290. REMOVED AND REPLACED PER IAW SRM 51-40-2 & SRM 51-30-2.May 16, 2000 · N480FE · Boeing 727227SDR DL72K000956Skin · crackedA CRACK WAS FOUND IN THE VERTICAL STABILIZER SKIN AT FS 1210 AND STRINGER 3A ON THE LEFT HAND SIDE. THE CRACK WAS REMOVED WITH A 1.4 X 2.7 CUTOUT AND AN EXTERNAL DOUBLER WAS INSTALLED PER ERA 334389-14 AT HMV.May 15, 2000 · N529DA · Boeing 727232SDR CALA0000673Panel · crackedINSPECTION FOUND VERTICAL STABILIZER REAR SPAR LOWER ACCESS PANEL CRACKED IN SEVERAL PLACES. THE CRACKS WERE APPROXIMATELY .5 INCH LONG. THE CRACKS WERE STOP DRILLED IAW SRM 53-01, FIGURE 2. DOUBLERS WERE INSTALLED IAW SRM 53-01, FIGURE 1 AND 51-10-3.May 11, 2000 · N72830 · Doug DC982SDR AT0000241Skin · gougedFOUND TOP OF VERTICAL STAB PANEL DEEPLY GOUGED ALONG AFT LEFT SIDE, 2 EACH. REMOVED AND REPLACED SKIN IAW TIMCO SERVICE ORDER 151015-36905.May 2, 2000 · N825AT · Doug DC932SDR QXEA0001173Skin · chafedYYC- VERTICAL SKIN CHAFED AT YW 48.00 RIGHT HAND 20 INCHES TO 41 INCHES AFT OF REAR SPAR. REPAIRED IAW DHC-8 MM 51-20-11 PAGE 7.Apr 25, 2000 · N829PH · Dhav DHC8102SDR DL72L000799Skin · crackedTEMP REPAIR ON VERTICAL STAB RT SIDE AT FUSELAGE SKIN. REPAIRED AREA PER M/M 55-30-0 FIG 801.Apr 25, 2000 · N509DA · Boeing 727232SDR QXEA0001181Skin · scratchedYYC- SCRATCH ON VERTICAL STAB JUST BELOW FWD RIGHT HAND HORIZONTAL STAB ATTACH POINT. REPAIRED IAW DHC-8 RD 8-55-584.Apr 24, 2000 · N829PH · Dhav DHC8102SDR CALA0000532Skin · gougedVERTICAL STAB LEFT UPPER PANEL AFT OF ROLLER RUBSTRIP GOUGED. REMOVED AND REPLACED PANEL ON VERTICAL STAB PER SRM 51-30-2, 51-30-5, AND 51-30-1.Apr 21, 2000 · N14831 · Doug DC982SDR DL72K000924Skin · crackedAT HMV2 FOUND SKIN CRACKED, LT SIDE VERT STAB AT FRONT SPAR. SKIN HAS TWO CRACKS ABOVE FS 1210, W/W N/R 1080. REMOVED DAMAGE PER DRD 55-30-3D, HFEC INSP PER DRD 55-30-3D NO DISCREPANCIES FOUND IN THIS AREA, REMOVED DAMAGE PER PRI 334389-14 DATED 4-27-00/190Apr 18, 2000 · N529DA · Boeing 727232SDR CALA0000501Skin · wornINSPECTION FOUND LT SIDE OF VERTICAL STABILIZER SKIN HAD A SMALL HOLE WORN INTO FORWARD LOWER EDGE OF OPENING FOR HORIZONTAL STABILIZER TRAVEL. THE WORN SKIN PANEL WAS REMOVED AND A NEW SKIN PANEL WAS INSTALLED IAW SRM 51-30-2.Apr 17, 2000 · N83870 · Doug DC982SDR CALA0000493Skin · wornINSPECTION FOUND RT SIDE OF VERTICAL STABILIZER SKIN WORN ALONG LOWER EDGE AT FORWARD END OF OPENING FOR HORIZONTAL STABILIZER TRAVEL. THE WORN SKIN SECTION WAS REMOVED AND A NEW SKIN SECTION WAS INSTALLED IAW SRM 51-30-2.Apr 14, 2000 · N83870 · Doug DC982SDR QXEA0001077Skin · chafedPDX - RT SIDE OF VERTICAL STABILIZER IS CHAFED WHERE HORIZONTAL STABILIZER ICE SCRAPER MOVES. REPAIRED IAW HORIZON AIR EA 4-55-72.Apr 4, 2000 · N494US · Fokker F28MK4000SDR 0000669151Skin · crackedVERTICAL STABILIZER SKIN CRACKED AT FASTENER HOLE LOWER LT SIDE OF STAB FS 900 AT ACCESS PANEL NR 5912188 ATTACH POINT LOG PAGE 1419162.Mar 30, 2000 · N8909E · Doug DC914SDR DL72K000624Skin · crackedAT HMV THE VERT SKIN WAS CRACKED AT PANEL 9523 LT FWD SIDE OF VERT STAB. REPAIR WAS FABRICATED PER MM 54-30-0 FIG 903 AND REPAIR WAS INSTALLED.Mar 20, 2000 · N410DA · Boeing 727232SDR DL72L000542Skin · damagedFATIGUE CRACK FOUND IN THE VERTICAL STABILIZER SKIN AT STRINGER 10R AND THE FUSELAGE CREASE LINE. DAMAGE IS TRIMMED OUT AND AN EXTERNAL REPAIR DOUBLER IS INSTALLED PER ER/A 334183-14.Mar 16, 2000 · N514DA · Boeing 727232SDR CALA0000273Skin · crackedINSPECTION FOUND TWO EACH CRACKS IN FLANGES OF DORSAL FIN LE AREA AT LOWER RT SIDE OF ACCESS, FS 1340. THE DORSAL FIN LE WAS REPAIRED IAW AD NR 89-08-10, SERVICE BULLETIN 53-223 (11-5-90), EA 5340-01012, AND ECRA 5330-02936.Mar 7, 2000 · N938MC · Doug DC983SDR CALA0000269Skin · gougedINSPECTION FOUND LEFT VERTICAL STABILIZER SKIN GOUGED ALONG HORIZONTAL STABILIZER RUN LINE. THE PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51-30-1, 51-30-2, 51-10-4, AND 51-30-5.Mar 4, 2000 · N37882 · Doug DC981SDR AT0000141Skin · damagedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND TEMPORARY REPAIR ON VERTICAL STABILIZER UPPER FORWARD RIGHT SIDE SKIN. CORRECTIVE ACTION: INSTALLED PERMANENT REPAIR DOUBLER IAW DC9 SRM 55-01 FIG 4 AND REO-L00085.Mar 2, 2000 · N848AT · Doug DC932SDR AALA2000499Skin · gougedTUL - FOUND FUSELAGE SKIN HAS HEAVY GOUGES VIEWED THROUGH VERTICAL STAB ACCESS PANEL. REPAIRED PER SRM 53-01 PAGE 9 FIG 2 SHEET 3. (M)Mar 1, 2000 · N287AA · Doug DC982SDR AALA2000329Skin · damagedTUL - LEADING EDGE SKIN BUTT JOINT BELOW LOWER VOR ANTENNA SEVERAL FASTENERS PULLED BELOW SKIN LEVEL L/E AREA. REPAIRED PER ESO 80559 DATED 2/11/00. (M)Feb 18, 2000 · N290AA · Doug DC982SDR DL72K000293Skin · crackedA .3/75 INCH CRACK AT BASE OF VERT STAB APPROX STA 1353. REPAIRED PER SRM 55-30-3 FIG 1.Feb 11, 2000 · N414DA · Boeing 727232SDR DL72K000292Skin · crackedA 1.75 INCH CRACK IN VERTICAL STAB SKIN LT SIDE FRONT SPAR BELOW ACCESS PANEL 9501. REPAIRED PER SRM 55-30-3 FIG 1.Feb 11, 2000 · N414DA · Boeing 727232SDR 2000ZZZX280Skin · damagedSCREW HOLE COUNTERSUNK SURFACE AREA DRILLED THROUGH NUMEROUS TIMES ON UPPER LEFT SIDE OF VERTICAL STABILIZER LEADING EDGE PANEL. REPAIRED WITH REPAIR BUSHINGS. DER APPROVED ON FORM 8110-3 DATED 9-11-23 ECRA 935-55-050-2.Feb 7, 2000 · N935F · Doug DC932FSDR DL72L000252Skin · crackedSTOP DRILLED CRACK AND BEGAN FABRICATING REPAIR PER M/M 55-30-0 FIG 803. CHEM TREATED PER PS 900-2-4-1 NR 2. TREATED AND PAINTED PER PS 900-2 NR 5. OK TO INSTALL. INSTALLED REPAIR ANGLE PER M/M 55-30-0 PG 803. STRINGER WAS FOUND CRACKED ON VERTICAL STAB.Jan 28, 2000 · N507DA · Boeing 727232SDR AT0000050Skin · corrodedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CORROSION ON PANEL NR 6402 OUT OF LIMITS. FABRICATED AND INSTALLED SKIN FOR PANEL NR 6402 IAW DC9 SRM 55-01 FIG 1, 51-70-02, AND 51-10-03.Jan 19, 2000 · N836AT · Doug DC932SDR MWEA00024Skin · gougedLEFT HAND VERTICAL STABILIZER SKIN IS GOUGED UNDER THE FORWARD UPPER HORIZONTAL STABILIZER FAIRING. MTC FABRICATED AND INSTALLED DOUBLER.Jan 12, 2000 · N207ME · Doug DC932SDR QXEA0000114Panel · crackedPDX - TOP ATTACH ANGLE FOR VERTICAL STABILIZER PANEL 57NB IS CRACKED FIVE INCHES. REPAIRED IAW HORIZON AIR EA 4-55-177.Dec 28, 1999 · N476US · Fokker F28MK4000SDR QXEA0000060Skin · damagedPDX - VERTICAL STABILIZER RIGHT SIDE PAINT/SKIN HAS TOOLING SCRATCH AT LOWER CORNER OF PANEL 56G CUT OUT. REPAIRED IAW FOKKER SRM 51-10-4 AND SRM 55-01-01, PAGE 3, PARAGRAPH D.Dec 26, 1999 · N476US · Fokker F28MK4000SDR QXEA0000061Skin · corrodedPDX - LEFT VERTICAL STABILIZER SKIN CUTOUT FOR PANEL 56D HAS FRETTING/PITTING AROUND ALL FASTENER HOLES. REPAIRED IAW FOKKER SRM 51-10-4, PARAGRAPH 4 B AND C.Dec 21, 1999 · N476US · Fokker F28MK4000SDR CALA9901679Panel · corrodedINSPECTION FOUND VERTICAL STABILIZER RT ACCESS PANEL NR 5216 AND STIFFENER CORRODED. A NEW PANEL AND NUT PLATES WERE INSTALLED IAW SRM 51-20-1, FIGURE 7, 51-30-2, 51-10-2, AND MM 51-20-0.Dec 21, 1999 · N33785 · Boeing 727232SDR QXEA0000062Skin · corrodedPDX - LEFT VERTICAL STABILIZER SKIN CUTOUT FOR PANEL 56C HAS FRETTING/PITTING AR0UND SEVERAL FASTENER HOLES. REPAIRED IAW FOKKER SRM 51-10-04, PARAGRAPH 4.Dec 20, 1999 · N476US · Fokker F28MK4000SDR CALA9901606Skin · damagedINSPECTION FOUND LEADING EDGE ACCESS PANEL SKIN OF VERTICAL STABILIZER WITH FASTENERS PULLING THROUGH AT STA 134. A DOUBLER WAS INSTALLED IAW SRM 55-30-7, 51-10-6, 51-20-0, AND 51-30-2.Dec 16, 1999 · N33785 · Boeing 727232SDR AALA991931Skin · dentedTUL - VERTICAL STABILIZER DENT IN SKIN 34 INCHES AFT OF RIGHT AMERICAN FLAG IN SKIN STA 1223 WITH CRACK IN DENT. INSTALLED DOUBLER PER SRM 54-10-3. TST: 72,089.43 HOURS. CYCLES: 46,585. (X)Dec 13, 1999 · N727AA · Boeing 727227SDR AALA991922Skin · crackedTUL - CRACK IN VERTICAL STABILIZER SKIN LEFT AT BOTTOM APPROXIMATE STA 1343. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SB 727-55-82 AND ESO 11697 DATED 12-10-99. TST: 62,106 HOURS. CYCLES: 37,884. (X)Dec 13, 1999 · N865AA · Boeing 727223SDR 20000511AP016Skin · crackedVERTICAL STABILIZER LOWER LEADING EDGE FAIRING NR 9501 HAS .5 INCH CRACK IN SKIN AND CHAFED AROUND END. CUT OUT DAMAGED AREA IAW 51-40-2 FIG 1. FABRICATED DOUBLER IAW 51-40-2 FIG 1. INSTALLED REPAIR IAW 51-30-2 PAGE 2. (M)Dec 8, 1999 · N889MA · Boeing 727225SDR CALA9901568Panel · delaminatedINSPECTION FOUND VERTICAL STABILIZER LOWER REAR CENTER PANEL DELAMINATED. A REPAIR WAS INSTALLED IAW ECRA 5533-01002.Dec 7, 1999 · N14090 · Doug DC1030SDR AALA991863Skin · crackedTUL - VERTICAL STABILIZER RIGHT SIDE SKIN IS CRACKED .5 INCH AT STABILIZER TO FUSELAGE MATE POINT. STOP DRILLED CRACK VISUAL AND NDT VERIFIED STOP DRILL OF CRACK. INSTALLED DOUBLER PER BOEING SERVICE BULLETIN 727-55-82. (M)Dec 1, 1999 · N863AA · Boeing 727223SDR DL72E992572Skin · crackedA CRACK WAS FOUND IN THE VERTICAL STABILIZER SKIN, LEFT HAND SIDE, WHERE THE SKIN MEETS THE UPPER TORQUE BOX AT APPROX FS 1210. THE DAMAGE WAS FOUND DURING HMV AND REPAIRED PER ERA 333807-14.Nov 22, 1999 · N831WA · Boeing 727247SDR DL72E992570Skin · crackedTHE SKIN OF THE VERTICAL STABILIZER WAS FOUND CRACKED AT THE FUSELAGE CREASE LINE AND STRINGER 10L. THE DAMAGE WAS FOUND AT HMV AND REPAIRED PER ERA 333830-14AD.Nov 22, 1999 · N831WA · Boeing 727247SDR 20000615AP003Panel · crackedDURING C-CHECK, FOUND VERTICAL STABILIZER L/E PANEL NR 9502, INNER AFT EDGE CRACKED. REMOVED INNER SKIN PER SRM 51-30-2 PAGE 1, FABRICATED NEW INNER SKIN PER SRM 55-10-2. INSTALLED PER SRM 55-10-2. (M)Nov 14, 1999 · N802EA · Boeing 727225SDR AT9900857Panel · corrodedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CORROSION ON VERTICAL STABILIZER AFT SPAR PANEL NR 6408 TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR AND DOUBLER IAW DC9 SRM 55-31 FIG 9 AND 51-30-02.Nov 14, 1999 · N833AT · Doug DC932SDR HEEA065127Skin · corrodedVERTICAL FIN HAD CORROSION AND SEPARATION.Nov 12, 1999 · N1073W · Bell 206L1SDR DL72S992360Skin · crackedTHE LT SKIN OF THE VERTICAL STABLIZER WAS DAMAGED RESULTING IN A 1.2 X 1.2 CUTOUT BETWEEN STRINGERS 7 AND 8 AT FIN STATION 204. REPAIRED PER ERA 333721-14 AT HMV.Oct 25, 1999 · N528DA · Boeing 727232SDR WXOA99012Panel · crackedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, VERTICAL STABILIZER ACCESS PANEL 3806 HAS CRACK PROPOGATING FROM EXISTING STOP DRILL. STOP DRILLED NEW CRACK, FABRICATED DOUBLER AND INSTALLED REPAIR DOUBLER IAW DC-9 SRM 51-10-2, 51-10-3, 51-30-2 Oct 14, 1999 · N127NK · Doug DC921SDR MWEA99683Skin · chafedLEFT VERTICAL STABILIZER SKIN HAS A HOLE CHAFED THROUGH. MAINTENANCE FABRICATED AND INSTALLED NEW SKIN.Oct 12, 1999 · N202ME · Doug DC932SDR CALA9901333Skin · gougedINSPECTION FOUND VERTICAL STABILIZER LEADING EGDE SKIN GOUGED AND DENTED AT STA ZFS 159. THE DAMAGED AREA WAS TRIMMED OUT. A DOUBLER AND FILLER REPAIR WAS INSTALLED IAW SRM 55-01, FIGURE 4, 51-10-3, AND 51-30-2.Oct 6, 1999 · N16815 · Doug DC982SDR CALA9901293Panel · crackedINSPECTION FOUND TWO 3 CRACKS IN VERTICAL STABILIZER SADDLE PANEL. THE SADDLE PANEL WAS REMOVED, REPAIRED IAW SRM 55-30-7, FIGURE3, AND REINSTALLED IAW MM 55-30-1, PAGE 201.Sep 27, 1999 · N79748 · Boeing 727224SDR MWEA99623Panel · chafedVERTICAL STABILIZER CANOE PANEL WAS CHAFED AT AFT END FROM HORIZONTAL STABILIZER FAIRINGS ON LEFT AND RIGHT SIDE. MTC FABRICATED AND INSTALLED REPLACEMENT PANEL.Sep 24, 1999 · N302ME · Doug DC932SDR MWEA99622Skin · chafedVERTICAL STABILIZER WAS CHAFED AT AFT END FROM HORIZONTAL STABILIZER FAIRINGS ON RIGHT SIDE. MTC FABRICATED AND INSTALLED NEW SKIN AND ANGLE.Sep 24, 1999 · N302ME · Doug DC932SDR MWEA99619Skin · chafedVERTICAL STABILIZER IS CHAFED AT AFT END. MTC FABRICATED AND INSTALLED NEW SKIN AND ANGLE.Sep 24, 1999 · N302ME · Doug DC932
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