JASC 5512

Service difficulty reports · 7,887

Reports filed under 5512 · Horizontal 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 = '5512'
  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 AWXA0001290Skin · dentedHORIZONTAL STABILIZER LEADING EDGE SKIN DENTED STA 258.28. REPAIRED DENT IN LEADING EDGE SKIN OF LEFT HORIZONTAL STABILIZER IAW B737-300 SRM 55-10-01 FIG 203 WITH -1 PLATE, -2 FILLER.Feb 8, 2001 · N509DC · Boeing 73733ASDR DHL2001367505Structure · damagedC-CHECK, THS 341AB RT SIDE HAS SLIGHT SURFACE DAMAGE AROUND O/B EDGE. (NON-ROUTINE 78827) SCRATCHES REMOVED FROM L/E IAW SRM 51-40-10, MATERIAL REMOVED 0.001 TO 0.002 INCH WITHIN LIMITS OF SRM 55-10-00, REPROTECTED AREA.Jan 30, 2001 · N367DH · Airbus A300B4203SDR ASAA0110020Skin · chafedPHX - DURING SCHEDULED D-CHECK, FOUND RIGHT HORIZONTAL STABILIZER CHAFED ON TRAILING EDGE OF STATION 121.5. REPAIRED PER SRM. (M)Jan 26, 2001 · N742AS · Boeing 737290CSDR AWXA0001213Skin · gougedLT HORIZ STABILIZER L/E UPPER SURFACE AT STA 166.30 HAS A DENT WITH A GOUGE (APPROX. 2.5 X 1.5). BLENDED GOUGE OUT OF LIMITS IAW SRM 51-10-02; CUTOUT DMGD AREA IAW 55-10-01; FABED SHIMS, FILLER AND DOUBLER; TREATED AND PRIMED PARTS AND INSTALLED PARTS IAW 51-4Jan 4, 2001 · N314AW · Boeing 7373S3SDR AWXA0001193Skin · dentedLT HORIZ STABILIZER L/E AT L/E STA 233.59 HAS DENT OUT OF LIMITS. REMOVED FASTENERS AND RIB AND CUT OUT DMG IAW SRM 55-10-01; HFEC INSPEC IAW B737 NTM PT.6 51-00-00 FIG 23 - NO CRACKS NOTED; FABED DOUBLER AND FILLER IAW 55-10-01; FABED REPLACEMENT RIB IAW 55-1Jan 3, 2001 · N154AW · Boeing 7373G7SDR AWXA0001192Skin · dentedLT HORIZ STABILIZER L/E AT L/E STA 122.39 HAS DENT OUT OF LIMITS. REMOVED FASTENERS AND RIB AND CUT OUT DMG IAW SRM 55-10-01; HFEC INSPEC IAW B737 NTM PT.6 51-00-00 FIG 23 - NO CRACKS NOTED; FABED DOUBLER AND FILLER IAW 55-10-01; FABED REPLACEMENT RIB IAW 55-1Jan 3, 2001 · N154AW · Boeing 7373G7SDR AWXA0001184Skin · dentedLT HORIZ STABILIZER L.E. SKIN DENTED OUT OF LIMITS AT LES 24.0.: REMOVED, FABED REPLACEMENT, AND INSTALLED REPLACEMENT LE SKIN IAW BOEING DWG 65-54821 AND SRM 51-40-02Jan 3, 2001 · N154AW · Boeing 7373G7SDR UPS01834671Panel · crackedINSPECTION TYPE:C2, LEFT HAND SIDE OF LOWER HORIZONTAL STAB FWD CONSTANT PANEL IS CRACKED BETWEEN 1ST THREE BOLT HOLES. REMOVED AND REPLACED LOWER FWD CONSTANT PANEL IAW DC8-5510-1074L.Jan 2, 2001 · N713UP · Doug DC871FSDR SWA002773Skin · crackedDURING SCHEDULED C4 CHECK, FOUND 1.5 RT HORIZ STAB LOWER SKIN CRACKED AT REAR SPAR, 6'' OTBD OF ROOT. REPAIRED SKIN PER SRM.Dec 29, 2000 · N342SW · Boeing 7373H4SDR AWXA0001141Skin · dentedDENT ON LT HORIZONTAL STABILIZER LEADING EDGE AT APPROX STA 135. REPAIRED IAW ENG. REPAIR 03-5510-00356-552Dec 29, 2000 · N328AW · Boeing 7373B7SDR SWAA002738Skin · crackedDURING SCHEDULED C2 CHECK, FOUND 2 CRACK AT LT HORIZ STAB SKIN, 4 FT OTBD AT AFT SPAR. REPAIRED SKIN PER SRM.Dec 23, 2000 · N676SW · Boeing 7373A4SDR AALA20010009Skin · bird strikeTUL - FOUND DENT IN HORIZONTAL STAB LEADING EDGE 133.15 TO 198.23, BIRD STRIKE. REPAIRED DENT PER SRM 51-10-02. INSTALLED DOUBLER PER SRM 55-10-01 PAGE 201-206. INSTALLED LEADING EDGE PER ESO 61000 DATED 12-19-2000. (M)Dec 20, 2000 · N912AN · Boeing 737*SDR USAA002132Skin · crackedCLT - FOUND SKIN CRACKED 1.5 INCH, RIGHT HORIZ STABILIZER LOWER SKIN STATION 133. INSTALLED DOUBLER PER TR 55-10-07. (M)Dec 13, 2000 · N417US · Boeing 737401SDR USAA002137Skin · crackedTPA - FOUND SKIN CRACKED 1.5 INCH, RIGHT HORIZ STAB LOWER SKIN STATION 125. INSTALLED REPAIR DOUBLER PER SRM 55-10-01 AND TR 55-10-07. (M)Dec 13, 2000 · N445US · Boeing 7374B7SDR ARWA0001211Panel · corrodedN/R 251 - DURING C CHECK INSPECTION FOUND THE FOLLOWING: LEVEL I CORROSION AT LT HORIZONTAL STABILIZER LOWER PANEL AT STA.XE 312.500.REMOVED AND REPLACED SKIN PANEL IAW DRAWING # AS11210, DATED 10/07/00, SEALED AREA IAW SRM 51-1-15.Dec 4, 2000 · N661AV · Doug DC863FSDR ARWA0001212Skin · damagedN/R 785 - DURING C CHECK INSPECTION FOUND THE FOLLOWING: RT HORIZONTAL STABILIZER LEADING EDGE SHOWS TEMP REPAIR. REMOVED I/B L/E; FABRICATED & INSTALLED REPAIRED IAW DRAWING AS11212, DATED 10/07/00, SEALED AREA IAW SRM 51-1-15 AND INSTALLED LEADING EDGE IAW Dec 4, 2000 · N661AV · Doug DC863FSDR ARWA0001210Panel · corrodedN/R 288 - DURING C CHECK INSPECTION, FOUND THE FOLLOWING: LEVEL I CORROSION AT LT HORIZONTAL STABILIZER LOWER PANEL AT STA.XE 260.00.REMOVED AND REPLACED SKIN PANEL IAW DRAWING AS11210, DATED 10/07/00, SEALED AREA IAW SRM 51-1-15.Dec 4, 2000 · N661AV · Doug DC863FSDR ARWA0001209Panel · corrodedN/R 257 - DURING C CHECK INSPECTION FOUND THE FOLLOWING: LEVEL I CORROSION AT UPPER PANEL RT HORIZONTAL STABILIZER AT STA.XE 1272.00 TO 219.979. REMOVED AND REPLACED PANEL IAW DRAWING AS11210, DATED 10/07/00, SEALED AREA IAW SRM 51-1-15.Dec 4, 2000 · N661AV · Doug DC863FSDR ARWA0001208Panel · corrodedN/R 252 - DURING C CHECK INSPECTION FOUND THE FOLLOWING: LEVEL I CORROSION AT UPPER L/H HORIZONTAL STABILIZER AT STA.XE 312.500.CORRECTIVE ACTION: REMOVED AND REPLACED SKIN PANEL IAW DRAWING # AS11210, DATED 10/07/00, SEALED AREA IAW SRM 51-1-8.Dec 4, 2000 · N661AV · Doug DC863FSDR SWAA002432Skin · crackedDURING SCHEDULED 1/4D CHECK, FOUND 1.5 CRACK ON LT HORIZ STAB LOWER SKIN BELOW INBD BALANCE BAY. REPAIRED SKIN PER SRM.Nov 22, 2000 · N371SW · Boeing 7373H4SDR CALA0001805Skin · crackedINSPECTION FOUND A 1.5 INCH CRACK AND BEND IN LT HORIZONTAL STABILIZER TIP O/B LOWER AFT CORNER SKIN. A REPAIR DOUBLER WAS INSTALLED IAW SRM 55-11-0, 51-30-2, AND 51-30-3.Nov 19, 2000 · N14816 · Doug DC982SDR SWAA002382Skin · damagedDURING SCHEDULED D-CHECK, FOUND 27 INCH LONG SKIN CREASE IN RT HORIZ STAB, GOING THROUGH A PREVIOUS REPAIR; EXTENDING DIAGONALLY FROM 2 AFT OF L/E SPAR AT L/E STA 198.23 TO 5.5 FWD OF REAR SPAR AT APPROX ELEV STA 168.67. REPAIRED SKIN PER DWG 65C36195 & SRM.Nov 18, 2000 · Boeing 7372H4SDR TWAA0019001Skin · dentedDURING CHECK-C MAINT THE LOWER SURFACE OF THE RT HORIZONTAL STAB HAD DENT APPROX. 1.5 IN BY 1.5 IN BY 0.080 DEEP, SIX FEET OTBD FROM FUSELAGE. INSTALLED 5 IN DIA METAL TO METAL BOND DOUBLER PER SRM 51-70-10, PAGE 1 AND PAGE 30, FIG 3. PRIMED AND PAINTED.Nov 16, 2000 · N651TW · Boeing 767205SDR L1GA200000382Skin · gougedGOUGE AT RT HORIZONTAL L/E. BLENDED, TREATED AND PRIMED.Nov 14, 2000 · N12510 · Doug DC932SDR USAA001925Skin · crackedCLT - FOUND SKIN CRACKED .5 INCH, UNDER STRINGER 5L, STATION 1138 LEFT STAB. INSTALLED DOUBLER PER EA 68315. (M)Nov 13, 2000 · N252AU · Boeing 737201SDR CALA0001683Skin · crackedINSPECTION FOUND A 4 INCH CRACK IN RT HORIZONTAL STABILIZER UPPER AFT O/B SKIN. THE RT UPPER AFT O/B SKIN PANEL WAS REPAIRED IAW ECRA 5511-01035.Nov 3, 2000 · N14079 · Doug DC1030SDR SWAA002215Skin · crackedDURING SCHEDULED C3 CHECK, FOUND RT HORIZ STAB LOWER SURFACE, 7'' FROM ROOT, CRACKED .25 INCH. REPAIRED SKIN PER SRM.Nov 2, 2000 · N364SW · Boeing 7373H4SDR SWAA002185Skin · crackedDURING SCHEDULED C1 CHECK, FOUND 1.25 INCH CRACK AT LT HORIZ STAB LWR SKIN, AFT SPAR, APPROX STA 157. REPAIRED SKIN PER SRM.Oct 30, 2000 · N306SW · Boeing 7373H4SDR CALA0001614Skin · dentedINSPECTION FOUND RIGHT I/B HORIZONTAL STABLIZER LEADING EDGE SKIN DENTED. THE DENTED AREA WAS TRIMMED OUT. A DOUBLER WAS INSTALLED IAW SRM 51-10-4, 51-10-3, ECRA 5513-01006, AND EA 9-5512-A0795.Oct 20, 2000 · N14871 · Doug DC981SDR CALA0001613Skin · dentedINSPECTION FOUND DENTS IN LT I/B HORIZONTAL STABILIZER LEADING EDGE SKIN. A SKIN DOUBLER REPAIR WAS INSTALLED IAW EA 9-5512-A0792, DRAWING SRO9550009, SRM 51-10-4, 51-10-3, 51-30-2, 51-30-5, AND ECRA 5513-01006.Oct 20, 2000 · N14871 · Doug DC981SDR MALA00709Skin · dentedFOUND DURING C-CHECK, RT UPPER HORIZONTAL STAB SKIN DENTED IN SEVERAL PLACES. REFER TO CELSIUS W/O 18910, TASK CARD 3508, AND SAAB STATEMENT 340SDS000299. MAINTENANCE MEASURED DENTS AND FOUND TO BE OUT OF LIMITS BY DENTS BEING LESS THAN 4 TIMES THERE LENGTH Oct 19, 2000 · N421XJ · Saab 340BSDR SWAA002016Skin · crackedDURING SCHEDULED C4 CHECK, FOUND 1.75 INCH CRACK ON LT HORIZ STAB LOWER SKIN AFT SPAR 5 FT O/B OF ROOT. REPAIRED SKIN PER SRM.Oct 14, 2000 · N329SW · Boeing 7373H4SDR USAA001734Skin · crackedTPA - FOUND SKIN CRACKED 2 INCHES, LT HORIZ STAB LOWER SKIN STATION 188. INSTALLED REPAIR DOUBLER PER SRM 55-10-3 FIG 3. (M)Oct 12, 2000 · N285AU · Boeing 7372B7SDR P2EA00290Skin · dentedSJO - DURING Q-CHECK, FOUND THE LEFT HORIZONTAL STABILIZER AT SS 119.5, 5 INCHES FORWARD OF REAR SPAR WITH DENT. L = 2.25 INCHES. W = 1.50 INCHES. D = 0.10 INCH. REPAIRED THE LEFT HORIZONTAL STABILIZER AT SS 119.5, 5 INCHES FORWARD OF REAR SPAR IAW BOEING Oct 6, 2000 · N912MP · Boeing 737247SDR MALA000642Rib · crackedFOUND DURING C-CHECK, LEADING EDGE 611BR HAS SEVERAL CRACKED RIBS. REFER TO CELSIUS TASK CARD 6514, W/O18737. MAINTENANCE NDTPERFFVND T006EC NO CRACKS NOTED. CUT OUT CRACKED AREA, FABRICATED DOUBLER, ALODINED, PRIMED, AND INSTALLED IAW 57-10-30.Sep 29, 2000 · N418XJ · Saab 340BSDR USAA001612Skin · crackedCLT - Q-4, SKIN HAD 1 INCH CRACK AT LOWER SKIN STABILIZER, STA 134, FORWARD OF REAR SPAR. INSTALLED DOUBLER PER 55-10-07. (X)Sep 28, 2000 · N516AU · Boeing 7373B7SDR MALA000623Skin · dentedFOUND DURING C-CHECK, RT HORIZONTAL STABILIZER UPPER SURFACE AT HS STA 439.2 HAS SEVERAL DENTS. REFER TO CELSIUS TASK CARD 3510, W/O 18843 AND SAAB STATEMENT 340SDS000144. MAINTENANCE FOUND DENTS OUT OF ALLOWABLE LIMIT REF SAAB SRM 51-10-10 LEXX THAN 4L AND 5Sep 26, 2000 · N416XJ · Saab 340BSDR AU001020Skin · cracked(AUS) LT HORIZONTAL STABILISER LOWER SKIN CRACKED IN AREA BETWEEN STN 125 AND STN 127. CRACK LENGTH 44.45MM (1.75IN).Sep 22, 2000 · Boeing 73733ASDR 20001106SH050Skin · corrodedCORROSION TO LEFT HORIZONTAL STABILIZER SKIN. (X)Sep 20, 2000 · N944F · Doug DC933FSDR 20001106SH043Skin · damagedOVERSIZE HOLE IN LEFT HORIZONTAL STABILIZER UPPER AFT SKIN PANEL. (X)Sep 20, 2000 · N944F · Doug DC933FSDR SWAA001793Rib · crackedDURING SCHEDULED D-CHECK, FOUND LT HORIZONTAL STAB L/E HAS CRACKED NR 4 RIB. REMOVED AND REPLACED RIB PER SRM.Sep 20, 2000 · N352SW · Boeing 7373H4SDR EIA2000334Skin · damagedEAC-MZJ - HORIZONTAL STABILIZER LEFT UPPER AFT SKIN PANEL STATION XH 10.0, HOLE OVERSIZED AT .199 DIAMETER PER SB 55-42. REPAIRED OVERSIZED HOLE PER ECRA 944-55-121-2. (M)Sep 18, 2000 · N944F · Doug DC933FSDR EIA2000333Skin · corrodedEAC-MZJ - FOUND CORROSION ON LEFT HORIZ STAB SKIN. REPAIRED LEFT HORIZ STAB SKIN. BLENDED TO REMOVE CORROSION, FABRICATED AND INSTALLED EXTERNAL DOUBLER PER ECRA 944-55-117-2. (M)Sep 18, 2000 · N944F · Doug DC933FSDR EIA2000348Plate · damagedEAC-MZJ - DURING C6 CHECK INSPECTION, FOUND ELONGATED HOLE IN HORIZ STABILIZER CENTER SECTION ACCESS PLATE. OVERSIZED HOLE AND INSTLALED NUTPLATE PER ECRA 944-55-099-2. (M)Sep 18, 2000 · N944F · Doug DC933FSDR 20001106SH038Plate · damagedDURING C-CHECK, FOUND ELONGATED HOLE, HORIZONTAL STABILIZER, CENTER SECTION ACCESS PLATE. (X)Sep 18, 2000 · N944F · Doug DC933FSDR SWAA001742Skin · crackedDURING SCHEDULED C4 CHECK, FOUND RT HORIZ STAB LOWER SKIN CRACKED, STA 128 ABOVE REAR SPAR. REPAIRED SKIN PER SRM.Sep 14, 2000 · N330SW · Boeing 7373H4SDR MALA000605Skin · dentedFOUND DURING C-CHECK, RT HORIZONTAL STABILIZER TIP DENTED ON LEADING EDGE. REFER TO CELSIUS TASK CARD 3506, W/O18829. DENTS OUT OF ALLOWABLE LIMIT REF SRM 51-10-10. RETURNED DENTED TIP TO ORIGINAL CONTOUR SRM 51-10-10. NO CRACKS NOTED IAW FFVNDT006. TOUCHSep 12, 2000 · N449XJ · Saab 340BSDR UPS00833755Skin · corrodedINSPECTION TYPE:C123, LEFT HORIZONTAL STAB L/E SKIN IS CORRODED BEYOND LIMITS AT XFS 172.5. REPAIRED SKIN IAW SRM 55-2-1 FIG 4.Sep 11, 2000 · N729UP · Doug DC871FSDR CALA0001405Access Panel · crackedINSPECTION FOUND A .5 INCH CRACK AT LAST RIVET HOLE IN THE FIXED SECTION ON O/B SIDE OF RT HORIZONTAL STABILIZER ELEVATOR ACCESS TO ELEVATOR GEAR TAB MECHANISM 3616A. THE PUSH ROD AND CONDUIT WERE REMOVED TO GAIN ACCESS IAW SRM 51-30-2. THE CRACK WAS STOP DSep 8, 2000 · N35832 · Doug DC982SDR AU000704Skin · cracked(AUS) LT HORIZONTAL STABILISER LOWER SKIN CRACKED IN AREA OF CHEMICALLY MILLED EDGE BETWEEN STN 147.9 AND STN157.1 JUST FORWARD OF THE REAR SPAR. CRACK LENGTH 38.1MM (1.5IN). FOUND DURING EDDY CURRENT INSPECTION.Sep 1, 2000 · Boeing 737377
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