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 AU001021Skin · cracked(AUS) LT HORIZONTAL STABILISER LOWER SKIN CRACKED AT THE CHEMICALLY MILLED EDGE BETWEEN STN 156.00 AND STN 158.00. CRACK LENGTH 50.8MM(2IN).Aug 23, 2000 · Boeing 737377SDR AWXA0000538Skin · dentedC-CHECK, RT HORIZ STAB UPPER SKIN DENTED STA 111.1 - 120.3. REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW 737 SRM 51-30-2 AND 55-10-3.Aug 17, 2000 · N184AW · Boeing 737277SDR AT0000492Skin · dentedFOUND RIGHT HORIZONTAL STABILIZER LOWER SURFACE APPROX XHS 104 DENTED. HFEC INSPECTED RIGHT HORIZONTAL STAB LOWER SURFACE. IAW DC9 SRM PT06. NO CRACKS NOTED. REO-L00263 NOTES DENTS ACCEPTABLE FOR STRENGTH AS IS WITH NO REPAIR REQUIRED, NO SPECIAL REPETITAug 12, 2000 · N830AT · Doug DC932SDR SWAA001518Skin · crackedDURING SCHEDULED BC4 CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN CRACKED AT REAR SPAR. REPAIRED SKIN PER SRM.Aug 12, 2000 · N354SW · Boeing 7373H4SDR CALA0001248Panel · dentedINSPECTION FOUND LEADING EDGE OF HORIZONTAL STABILIZER I/B RIGHT SIDE DENTED. THE LEADING EDGE WAS REPAIRED IAW SRM 55-10-01, PAGE 207-208.Aug 11, 2000 · N14334 · Boeing 7373T0SDR SWAA001506Skin · crackedDURING SCHEDULED C4 CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN CRACKED BETWEEN REAR SPAR AND NR 1 BALANCE PANEL. REPAIRED SKIN PER SRM.Aug 9, 2000 · N392SW · Boeing 7373H4SDR 20000801SH016Panel · corrodedCORROSION ON LEFT AND RIGHT HORIZONTAL STABILIZER LEADING EDGE PANELS. REPAIRED PER ECRA N11FQ-55-004-EAC. SUBMITTER STATED CAUSE MAY BE DUE TO OPERATING OVER SALT WATER. (X)Aug 1, 2000 · N11FQ · Doug MD88SDR USAA001534Skin · corrodedPIT - FOUND CORROSION ON HORIZ STAB LE, NR 5 RIB PANEL 9450. CORROSION LEVEL 1. REMOVED CORROSION, TREATED AND PRIMED PER SRM 51-20-02. (M)Jul 31, 2000 · N577US · Boeing 737301SDR TWAA0012104Skin · damagedDURING CHECK-C MAINT, CHECK FOUND ON LT HORIZONTAL STABILIZER LOWER SURFACE, 15 FEET FROM THE FUSELAGE AND 2 FEET FROM THE LEADING EDGE, AN OLD REPAIR HAD COME LOOSE. INSTALLED AN 8 INCH BY 9 INCH HOT BOND METAL DOUBLER PER SRM 55-10-01 AND 51-70-10. PRIMED Jul 26, 2000 · N605TW · Boeing 767231SDR AT0000413Panel · corrodedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND HORIZONTAL STABILIZER CENTER BOX, AFT SECTION UPPER PANEL TO HAVE EXFOLIATION CORROSION. REMOVED AND REPLACED CENTER BOX AFT SECTION UPPER PANEL IAW TIMCO SERVICE ORDER 151072-42730.Jul 25, 2000 · N845AT · Doug DC932SDR HALA0000245Panel · crackedTUL - LEFT HORIZONTAL STAB AFT UPPER OUTBOARD PLANK CRACKED 2 INCHES. REMOVED AND REPLACED WITH NEW PLANK. (M)Jul 24, 2000 · N152AA · Doug DC1010SDR AWXA0000462Skin · dentedC-CHECK, LT HORIZONTAL STAB LEADING EDGE HAS 2 AREAS OF DAMAGE 72 INCHES AND 74 INCHES FROM THE I/B END. FABRICATED AND INSTALLED LEADING EDGE REPAIR IAW B737 SRM 55-10-01 AND SRM 55-10-09.Jul 17, 2000 · N172AW · Boeing 73733ASDR SWAA001302Skin · crackedDURING SCHEDULED C4 CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN HAS A 2 INCH LONG CRACK NEAR FRONT SPAR, I/B BALANCE PANEL. REPAIRED SKIN PER SRM.Jul 16, 2000 · N373SW · Boeing 7373H4SDR QXEA0001978Panel · crackedPDX- CRACKS IN FASTENER HOLES ON PANEL 53N. REPAIRED IAW HORIZON AIR EA 4-55-240.Jul 14, 2000 · N491US · Fokker F28MK4000SDR QXEA0002014Panel · corrodedPDX- CORROSION AROUND PANEL 56F. REPAIRED IAW FOKKER SRM 55-01-01, PAGE 4.Jul 13, 2000 · N491US · Fokker F28MK4000SDR QXEA0002013Panel · corrodedPDX- CORROSION AROUND PANEL 56F APERTURE. REPAIRED IAW FOKKER SRM 55-01-01, PAGE 4.Jul 13, 2000 · N491US · Fokker F28MK4000SDR QXEA0001975Skin · scratchedPDX- LOWER SKIN OF LEFT HORIZONTAL STABILIZER HAS SCRATCHES INBOARD OF 52K. REPAIRED IAW FOKKER SRM 55-11-01, PAGE 6, AND HORIZON AIR EA 4-55-235.Jul 6, 2000 · N491US · Fokker F28MK4000SDR SWAA001172Skin · crackedDURING SCHEDULED 1/2 D CHECK, FOUND LT HORIZONTAL STAB LOWER SKIN HAS A CRACK .75 LONG AT REAR SPAR. REPAIRED SKIN PER SRM.Jun 28, 2000 · N333SW · Boeing 7373H4SDR UPS00233024Skin · crackedINSPECTION TYPE:N/A SMALL CRACK ON LT HORIZANTAL LEADING EDGE VERIFIED CRACK WITH HFEC REPAIRED CRACK PER SRM 55-10-3. THIS EXTERNAL DOUBLER MUST BE REPLACED WITH A FLUSH REPAIR PER SRM 5501003, FIG 2 NO LATER THAN NEXT C CHECK.Jun 27, 2000 · N936UP · Boeing 727108CSDR CALA0000987Skin Panel · corrodedINSPECTION FOUND THAT THE LT AND RT HORIZONTAL STABILIZERS HAD BARREL NUT HOLES CORRODED WITH MISSING SEALANT. THE CORRODED BARREL NUTS AND PLI WASHERS WERE REMOVED AND REPLACED IAW MM 20-10-14. THE CORROSION WAS REMOVED AND BUSHINGS WERE INSTALLED IAW ECRA Jun 26, 2000 · N819NY · Doug DC982SDR P5CA0000212Panel · delaminatedLEFT HORIZONTAL STABILIZER UNDERSIDE PANEL 334KBL DELAMINATED. REMOVED DAMAGE, REPLACED CORE, POTTED, APPLIED GLASS OVERLAYS AND APPLIED FINISH PER SRM 51-40-06.Jun 23, 2000 · N855FT · Boeing 747124SDR AWXA0000403Skin · dentedC-CHECK, LT HORIZ STAB APPROX STA 200 HAS DENT OUT OF LIMITS. CUT OUT DAMAGE IAW 737 SRM 55-10-3, FABRICATED DOUBLER AND FILLER, AND INSTALLED PARTS IAW 737 SRM 55-10-3 FIG 2.Jun 21, 2000 · N187AW · Boeing 737277SDR DHL200080146CSkin · dentedAT C CK; LT HORIZONTAL STABILIZER ELEVATOR UPPER PART DENTED 2 INCHES AT XE. 66.250. CUTOUT DAMAGED SKIN IAW SRM 51-1-21A, FABRICATED AND INSTALLED FILLER AND NEW SKIN IAW SRM 51-1-21A PAGE 3. REF: N/R 2116.Jun 19, 2000 · N801DH · Doug DC873FSDR DHL200080143CSkin · canningAT C CK; LT HORIZONTAL STABLIZER ELEVATOR UPPER SKIN SHOWS OIL CANNING AT XS. 272.00. REMOVED DAMAGED SKIN IAW SRM 51-1-21 PAGE 1, FABRICATED AND INSTALLED NEW SKIN IAW SRM 55-2-1 PAGE 6. REF: N/R 2119.Jun 19, 2000 · N801DH · Doug DC873FSDR DHL200080144CSkin · dentedAT C CK; LT HORIZONTAL STABLIZER ELEVATOR UPPER SKIN SHOWS DENTS FROM XS. 99.241 REMOVED DAMAGED SKIN IAW SRM 51-1-21 PAGE 1. FABRICATED AND INSTALLED NEW SKIN IAW SRM 51-1-21. REF: N/R 2118.Jun 18, 2000 · N801DH · Doug DC873FSDR RRXA002698Skin · damagedDURING A MAINTENANCE VISIT FOUND A DIMPLED WASHER ON THE RT HORZ STAB I/B LEADING EDGE SCREW AT STA XFS 178.7, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED PART IAW EO NR 00-107 WITH APPROJun 12, 2000 · N8084U · Doug DC871FSDR LR7A0078Skin · puncturedDURING SCHEDULED C2 INSPECTION PER JOB CARD HC2704, FOUND RT HORIZONTAL STAB LOWER L/E SKIN HOLED DUE SMALL PUNCTURE AT HSS 238. REPAIRED IAW LAC MEA 382-55-00-068.Jun 3, 2000 · N402LC · Lkheed 382GSDR MALA000405Skin · dentedFOUND DURING C-CHECK, DENTS ON RT UPPER HORIZONTAL STABILIZER BETWEEN STATIONS HS 75.90 AND HS 99:13. MAINTENANCE MEASURED DENTS AND FOUND MOST O/B DENTS TO FALL WITHIN AREA LIMITS .023 DEEP & DIA OF .734. I/B 2 DENTS ARE OUT OF LIMITS BEING LESS THAN 4X THEMay 30, 2000 · N442XJ · Saab 340BSDR AT0000340Skin · corrodedDURING A SCHEDULED INSPECTION AT PEMCO IN DOTHAN ALA, FOUND LEFT HORIZONTAL #21 BAL PANEL BS 94.07 TO HAVE CORROSION OUT OF LIMITS. CORRECTIVE ACTION: FILLED WITH EPOCAST 1619 AND APPLIED TEFMay 28, 2000 · N737Q · Boeing 7372L9SDR SWAA000930Skin · crackedDURING SCHEDULED C2 CHECK, FOUND LT HORIZONTAL STAB LOWER SKIN CRACKED, STA 155 FWD OF FRONT SPAR. REPAIRED SKIN PER SRM.May 19, 2000 · N344SW · Boeing 7373H4SDR DHL200070723CSkin · crackedLT HORIZ STAB L/E SKIN HAS A CRACK AT RIVET HEAD STA 47.3. PERFORMED HFEC INSP AND CONFIRMED CRACK PER NDT MAN 51-00-00 PART 6 FIG 4. CUT OUT DAMAGED AREA 2.5 X 1.75 INCH PER SRM 55-10-3. APPLIED ALODINE AND PRIMER PER SRM 51-10-2. INSTALLED REPAIR AT LT HMay 18, 2000 · N707DH · Boeing 72722SDR DHL200070727CSkin · delaminatedLT HORIZONTAL STAB, ELEVATOR UPPER SURFACE, HAS SEVERAL AREAS DELAMINATED. OPENED ACCESS PANEL FOR EVALUATION. REMOVED LT HORIZONTAL STAB ELEVATER UPPER SKIN FROM STA 151.81 TO STA 188.65. INSTALLED PANEL SKIN.INSTALLED BALANCE PANEL SEALED PANEL REBALANCED ELMay 15, 2000 · N707DH · Boeing 72722SDR P2EA00194Panel · delaminatedSJO - DURING C-CHECK, FOUND THE LOWER SKIN OF THE RIGHT HORIZONTAL STAB TRAILING EDGE UPPER PANEL, P/N 65-52493-2 WITH DELAM LENGTH 63 INCHES, WIDTH 6 INCHES. REPAIRED THE LOWER SKIN OF THE RIGHT HORIZONTAL STAB TRAILING EDGE UPPER PANEL P/N 65-52493-2 IAW COMay 4, 2000 · N209US · Boeing 737222SDR 20000503SH019Skin · corrodedLEFT HORIZONTAL UPPER SURFACE, INBOARD SIDE HAS CORROSION REMOVAL BLEND-OUTS WHICH ARE OUT OF LIMITS. REPAIRED BY ECRA 479-55-132-1. (X)May 3, 2000 · N479EV · Boeing 747132SDR 20000503SH018Skin · corrodedRIGHT HORIZONTAL STABILIZER, UPPER SURFACE FROM FRONT SPAR TO REAR SPAR STA 143.6 TO TIP HAS AREAS OF CORROSION. REPAIRED BY ECRA 479-55-133-2. (X)May 3, 2000 · N479EV · Boeing 747132SDR SWAA000818Skin · crackedDURING SCHEDULED 1/4D CHECK, FOUND LT HORIZONTAL STAB LOWER SKIN CRACKED FWD OF I/B ELEVATOR BALANCE BAY. REPAIRED SKIN PER SWA RA NR 1-A55-0334.May 1, 2000 · N367SW · Boeing 7373H4SDR TWAA0006804Panel · gougedDURING CHECK-C MAINT, THE LT HORIZ STAB L/E REMOVABLE PANEL 3320L, TOP SIDE HAD A 3.5 FOOT BY. 125 INCH WIDE BY.0625 INCH DEEP GOUGE. REMOVED GOUGE PER SRM 55-10-01, PAGE 103 DETAIL II AND BLENDED AND ALODINED.Apr 28, 2000 · N709TW · Boeing 7572Q8SDR RRXA003703Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE UPPER PANEL RT HORIZ STAB AT STA XE 248, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED NEW PANEL. (CORROSION DAMAGE RECORDEDApr 24, 2000 · N8084U · Doug DC871FSDR RRXA003501Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE T/E RT HORIZ STAB AT STA XE99, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 53-2-0, 51-1-21 AND 51-3-Apr 24, 2000 · N8084U · Doug DC871FSDR RRXA003487Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE T/E OF THE RT HORIZONTAL STABILIZER AT STA XE 278, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 53-2-Apr 24, 2000 · N8084U · Doug DC871FSDR SWAA000782Skin · crackedDURING SCHEDULED C2 CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN CRACKED, BS 125 ON AFT SPAR. REPAIRED SKIN PER SRM.Apr 24, 2000 · N327SW · Boeing 7373H4SDR UPS00232616Skin · corrodedINSPECTION TYPE:C+SI, LT HORIZ STAB REAR SPAR UPPER CHORD SKIN UNEVEN AT 2 AREAS. FWD OF NR 4 ELEV HINGE AND FWD OF NR 6 ELEV HINGE. DAMAGE REPAIRED IAW SRM 55-10-5 FIG 1.Apr 19, 2000 · N938UP · Boeing 727173CSDR CALA0000473Skin · dentedINSPECTION FOUND LT HORIZONTAL STABILIZER O/B LEADING EDGE SKIN DENTED. DOUBLERS WERE INSTALLED IAW SRM 55-03, FIGURE 3.Apr 15, 2000 · N16804 · Doug DC982SDR AU000369Skin · cracked(AUS) RT HORIZONTAL STABILIZER LOWER SKIN CRACKED BETWEEN STABILISER STN 120.3 AND STN 129.5 LOCATED 38.1MM (1.5IN) FORWARD OF THE REAR SPAR. CRACK LENGTH 57.15MM (2.25IN).Apr 11, 2000 · Boeing 737377SDR 00FDEA00281Skin · wornSKIN DAMAGED AND CUTTING ANTI-CHAFING PLATE BENEATH RT HORIZONTAL STAB. INSTALLED DOUBLER ON FUSELAGE PER EA NR 6-5319- 50270.Apr 4, 2000 · N405FE · Airbus A310203SDR AWXA0000227Skin · puncturedC-CHECK, LARGE PUNCTURE, RT HORIZ STAB SKIN MID WAY OUT FROM HORIZONTAL ROOT JUST AFT OF LEADING EDGE BOTTOM SIDE. CUT OUT DAMAGE AND EVALUATED INNER STRUCTURE, NO DAMAGE NOTED. FABRICATED FILLER AND DOUBLER, INSTALLED IAW 737 SRM 55-10-3. MAT USED (2024T3Apr 4, 2000 · N186AW · Boeing 737277SDR EIAA2000083Skin · corrodedEAC-MZJ - C6/D-CHECK - LEFT HORIZONTAL UPPER SURFACE, INBOARD SIDE HAD CORROSION REMOVAL BLEND-OUTS WHICH WERE OUT OF LIMITS. REPAIRED PER ECRA 479-55-132-2. FLAP PEENED, INSTALLED NEW FASTENERS, AND TREATED ALL BLEND-OUT AREAS. (X)Mar 30, 2000 · N479EV · Boeing 747132SDR AALA2000544Skin · corrodedTUL - FOUND CORROSION ON TRAILING EDGE OF HORIZ STAB APPROX 30 INCH INBOARD OF OUTBOARD END RIGHT SIDE. CUT OUT DAMAGE 14.625 LONG AND .875 DEEP FROM TRAILING EDGE FORWARD AND INSTALLED FILLER (.100) AND DOUBELR .125 2024 T3 PER ESO 11697 DATED 3-21-00 AND SRMar 24, 2000 · N721AA · Boeing 727227SDR USAA000439Skin · crackedCLT - FOUND SKIN CRACKED 2.75 INCHES, RIGHT HORIZ STABILIZER LOWER SKIN AT STATION 125. INSTALLED DOUBLER PER TR 55-10-07. (M)Mar 23, 2000 · N434US · Boeing 7374B7SDR USAA000308Skin · crackedCLT - FOUND SKIN CRACKED 2 INCHES, BOTTOM RIGHT STAB FORWARD REAR SPAR STATION 150. INSTALLED REPAIR FILLER AND DOUBLER PER TR 55-10-07 REV A. (M)Mar 6, 2000 · N780AU · Boeing 7374B7
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