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 A6WA200360046Skin · dentedDENTS ON THE LEFT AND RIGHT HORIZONTAL STAB MAINTENANCE HAS REQUESTED REPAIR FROM BAE SYSTEMS RED AMAX FAX 1683-6810002. (M)Oct 6, 2003 · N181US · Bag BAE146200ASDR CA031015014Doubler · cracked(CAN) HORIZONTAL ATTACHMENT POINT DOUBLER FORWARD RT CRACKED AT TOP NUTPLATE RIVET. DOUBLER REPLACED WITH NEW. AREA INSPECTED. NO OTHER FAULTS FOUND. CAUSE IMPROPER GROUND HANDLING (SPECULATION).Oct 2, 2003 · Cessna U206BSDR CALA0300565Skin · dentedINSPECTION FOUND LOWER SURFACE OF LT HORIZONTAL STABILIZER SKIN DENTED APPROXIMATELY 8 INCHES FORWARD OF AFT SPAR AND 102 INCHES O/B OF FUSELAGE. A REPAIR WAS INSTALLED IAW SRM 55-10-01.Sep 27, 2003 · N16647 · Boeing 737524SDR CALA0300561Panel · crackedINSPECTION FOUND CRACKS ON THE LOWER SIDE OF THE LT HORIZONTAL STABILIZER LEADING EDGE PANEL. THE CRACKS WERE CONFINED TO THE BONDED INTERNAL DOUBLER AT ONE FASTENER HOLE, 5.2 INCHES OB OF THE STA 188 RIB. THE AREA WAS REPAIRED IAW ECRA 5510-01695.Sep 22, 2003 · N16646 · Boeing 737524SDR SIMA200326502Skin · damagedAIRCRAFT SUSTAINED HAIL DAMAGE THAT NECESSITATED THE REPLACEMENT ON THE RIGHT HORIZONTAL STABILIZER UPPER SKIN. REMOVED DAMAGED UPPER SKIN. TRIMMED NEW SKIN AND INSTALLED. REPAIR DONE IAW SAAB 340 SRM (72LKS 3079, REV 41) 51-40-21, 22, 40, 51-20-40, 41, 43.Sep 10, 2003 · N903AE · Saab 340BSDR IXXA060545SSkin · corrodedDURING ROUTINE C-CHECK, FOUND RIGHT HORIZONTAL STABILIZER LEADING EDGE UPPER SURFACE CORRODED AT STATION XFS178. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS IAW DC8 SRM 55-2-1, 51-1-21, Sep 7, 2003 · N829BX · Doug DC871FSDR TSAA0255264Skin · gougedCUT AND REMOVED GOUGE AREA. FABRICATED REPAIR .063 DOUBLER AND .040 FILLER FROM 2024 T3 CLAD. INSTALLED REPAIR PARTS AND FASTENERS WET WITH MBS 5-95 SEALANT. REPAIR COMPLETED IAW SRM 55-10-1 FIGURE 2. AIRCRAFT RETURNED TO SERVICE. (M)Sep 5, 2003 · N824AL · Boeing 737282SDR TSAA0255266Skin · gougedCUT OUT DAMAGED AREA. FABRICATED REPAIR .063 DOUBLER AND .040 FILLER FROM 2024 T3 CLAD. INSTALLED REPAIR PARTS AND FASTENERS WET WITH MBS 5-95 SEALANT. REPAIR COMPLETED IAW SRM 55-10-1 FIGURE 2. AIRCRAFT RETURNED TO SERVICE. (M)Sep 5, 2003 · N824AL · Boeing 737282SDR QXEA200301053Skin · dentedDENT IN UNDERSIDE OF LT HORIZONTAL STABILIZER INBOARD OF LOGO LIGHT AT LT STABILIZER STATION XH19.903 - YH103.25. REPAIRED IAW Q400 RD 8/4-55-121 AND HORIZON AIR EA 6-55-50.Aug 30, 2003 · N407QX · Bombdr DHC8401SDR QXEA200301108Skin · scratchedEMPENNAGE LEFT HAND SIDE UPPER SKIN IS AN ABRASION ONE INCH LONG FORWARD OF FRAME NR 1 OUTBOARD OF STRINGER 5. REPAIRED IAW DHC-8 SRM 51-20-16.Aug 26, 2003 · N347PH · Dhav DHC8202SDR QXEA200301034Vortex Gen · loosePDX- HORIZONTAL STABILIZER LEFT INBOARD VORTEX GENERATOR IS LOOSE AND SEPERATING FROM THE BOTTOM OF THE STABILIZER. REPAIRED IAW DHC-8 SRM 55-10-10 AND TASK 55-10-10-000-801.Aug 25, 2003 · N347PH · Dhav DHC8202SDR CALA0300470Skin · bird strikeINSPECTION FOUND RT HORIZONTAL STABILIZER LEADING EDGE SKIN AND RIB AT STA 86.66 DAMAGED DUE TO A BIRD STRIKE.Aug 17, 2003 · N14346 · Boeing 7373T0SDR CALA0300471Skin · crackedMAINTENANCE FOUND A SMALL CRACK IN THE LT HORIZONTAL STABILIZER LOWER SKIN JUST FORWARD OF THE REAR SPAR FORWARD FLANGE, STAB STA 152. AN INTERIM REPAIR WAS PERFORMED IAW ECRA 5510-01692. A DIP WAS ISSUED TO PERFORM A DETAILED VISUAL INSPECTION OF THE INTERIAug 14, 2003 · N70330 · Boeing 7373T0SDR SWAA031817Skin · crackedDURING SCHEDULED CHECK, FOUND LT HORIZ STAB SKIN CRACKED AT STA 157.10 JUST FWD OF REAR SPAR. REPAIRED SKIN PER SRM.Aug 11, 2003 · N387SW · Boeing 7373H4SDR 03FDEA01199Skin · corrodedHORIZONTAL STAB RT UPPER CENTER PLANK NR 26R BARREL NUT BORE FOUND CORROSION BEYOND EO 1-5510-7-5000 LIMITATIONS. HORIZONTAL STABILIZER RT UPPER CTR PLANK NR 26R FITTING REMOVED & REPLACED AS PER FEDEX EA 1-5510-69397 - STABILIZERS - HORIZONTAL STABILIZERJul 29, 2003 · N605FE · Doug MD11SDR 03FDEA01179Skin · corrodedRH HOR STAB UPPER AFT PLANK NR 27R BARREL NUT BORE FOUND CORROSION BEYOND EO 1-5510-7-5000 LIMITATIONS. RT HORIZONTAL STAB UPPER AFT PLANK NR 27R BARREL NUT BORE REPAIR CARRIED-OUT AS PER FEDEX EA 1-5510-69279 - STABILIZERS - HORIZONTAL STABILIZER - CJul 28, 2003 · N605FE · Doug MD11SDR UPS03841025Skin · corrodedINSPECTION TYPE:C2 RIGHT HORIZONTAL STAB L/E UPPER SKIN IS CORRODED BEYOND LIMITS BETWEEN XFS 172.5 TO XFS 178. CUT OUT CORRODED AREA, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 55-2-0 FIG 2, 51-1-21 FIG 33.Jul 26, 2003 · N874UP · Doug DC873FSDR AMTA200301015Skin · delaminatedFOUND LEFT HORIZONTAL STABILIZER UPPER SKIN DELAMINATED. REPAIRED SURFACE OF SKIN PANEL IAW SRM 51-50-06. (M)Jul 23, 2003 · N161AT · Lkheed 10113853SDR SIMA200320807Skin · dentedABI - AIRCRAFT SUSTAINED HAIL DAMAGE THAT NECESSITATED THE REPLACEMENT OF THE LEFT HORIZONTAL STABILIZER UPPER SKIN. REMOVED DAMAGED UPPER SKIN. INSTALLED NEW SKIN IAW SAAB 340 SRM, 72LKS 3079, REV 41, 51-40-22, 23, 40, 51-20-40, 41-43. (M)Jul 22, 2003 · N375AE · Saab 340BSDR SIMA200320803Skin · dentedABI - AIRCRAFT SUSTAINED HAIL DAMAGE THAT NECCESSITATED THE REPLACEMENT OF THE RIGHT HORIZONTAL STABILIZER UPPER SKIN. REMOVED DAMAGED SKIN AND INSTALLED NEW SKIN IAW SAAB 340 SRM, 72LKS 3079, REV 41, 51-40-21, 22, 23, 40, 51-20-40, 41, 43. (M)Jul 22, 2003 · N375AE · Saab 340BSDR DHL2003873550Skin · damagedINTERIM REPAIR ON RT HORIZ STAB OB L/E AT XFS.180.000. PERFORMED MAJOR REPAIR IAW SRM 55-2-1 FIG 4, PG 17. REMOVED FASTENERS AND INTERIM REPAIR IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED DOUBLER IAW SRM 55-2-1 FIG 4 PG 1Jun 30, 2003 · N873SJ · Doug DC873FSDR DHL2003873548Skin · damagedINTERIM REPAIR ON RT HORZ STAB INBD L/E AT STA XFS 178.750 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 55-2-1 FIG 4 PG 17. REMOVED FASTENERS AND INTERIM REPAIR IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED DOUBLER IAJun 30, 2003 · N873SJ · Doug DC873FSDR DHL2003873542Skin · damagedINTERIM REPAIR ON RT HORIZONTAL STABILIZER OTBD L/E XFS.210.000 - XFS.222.500. PERFORMED MAJOR REPAIR IAW SRM 55-2-1 FIG 4 PG 17. REMOVED FASTENERS AND INTERIM REPAIR IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED DOUBLEJun 30, 2003 · N873SJ · Doug DC873FSDR DHL2003873549Skin · damagedINTERIM REPAIR ON RIGHT HORZ STAB INBOARD L/E (STA.XFS.53.750-78.250) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 55-2-1 FIG 4 PG 17. REMOVED FASTENERS AND INTERIM REPAIR IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED DOUBJun 30, 2003 · N873SJ · Doug DC873FSDR DHL2003873553Skin · damagedINTERIM REPAIR ON RT HORIZONTAL STABILIZER INBOARD LE (STA.XFS.85.000-110.000) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 55-2-1 FIG 4 PG 17. REMOVED FASTENERS AND INTERIM REPAIR IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICJun 29, 2003 · N873SJ · Doug DC873FSDR SROM200300033Skin · scratchedDURING D CHECK INSPECTION FOUND FOUND SEVERAL SCRATCHES IN LOWER AND UPPER SURFACES OF THE RT IB HORIZONTAL STABLIZER LEADING EDGE. REMOVED AND REPLACED RT IB HORIZONTAL LEADING EDGE IAW SRM 51-30-2.Jun 29, 2003 · N736BP · Boeing 737205SDR CALA0300359Skin · dentedMAINTENANCE REMOVED AN INTERIM REPAIR ON THE RT HORIZONTAL STABILIZER AT THE LEADING EDGE. THE DENT WAS NEAR A RIB AT LEADING EDGE STATION 184.66. THE FINAL TRIM OUT WAS 3.5 INCHES BY 4.5 INCHES. A PERMANENT REPAIR WAS PERFORMED BY INSTALLING A FLUSH REPAIRJun 27, 2003 · N14660 · Boeing 737524SDR CALA0300341Skin · dentedINSPECTION FOUND RT HORIZONTAL STABILIZER LEADING EDGE DENTED WITH A SHARP CREASE IN THE CENTER OF THE DENT AT LEADING EDGE STA 184. REPAIRED IAW SRM 55-10-01 AND ECRA 5510-01647.Jun 27, 2003 · N14660 · Boeing 737524SDR 03FDEA00973Skin · corrodedSNRM N0897 - LT HOR STAB UPPER FWD PLANK NR 8L BORE FOUND CORROSION BEYOND EO 1- 5510-7-5000 LIMITATIONS. CORRECTIVE ACTION: SNRM N0897 - LT HOR STAB UPPER FWD PLANK NR 8L BORE REPAIR CARRIED OUT IAW EA 1-5510-71721, STABILIZERS- HORIZONTAL STABILIZER- Jun 20, 2003 · N588FE · Doug MD11SDR 03FDEA00929Skin · corrodedHORIZONTAL STAB UPPER FWD PLANK 14L BARREL NUT BORE FOUND CORROSION BEYOND EO 1-5510-7-5000 B PT1 LIMITATIONS. HORIZONTAL STAB UPPER FWD PLANK 14L FITTING REMOVED AND REPLACED AS PER FEDEX EA 1-5510-71721, STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT REWORKJun 19, 2003 · N588FE · Doug MD11SDR 03FDEA00887Skin · dentedON WALKAROUND UPON A/C ARRIVAL FOUND DENT ON LT HORIZONTAL STABILIZER LEADING EDGE LOWER SURFACE. THIS WILL BE C/W IN C-CHECK. FOUND DENT TO BE IN V-SHAPE 4 X 3 X .0265 INCH DEEP. LOCATION IS 5FT FROM WING TIP, APPROX STA 750 LOWER LEADING EDGE. C/W EA 6-5Jun 16, 2003 · N655FE · Airbus A300B4605RSDR EIA2003088Skin · corrodedSEVERAL SMALL AREAS OF SURFACE CORROSION ON LOWER SURFACE LT HORIZONTAL STAB APPROX STA 410 AT STR 7. REMOVED CORROSION, FOUND OUT OF LIMITS. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED PER B747 SRM 51-10-01, 51-20-01, 51-30-00, 51-10-02 AND Jun 14, 2003 · N478EV · Boeing 747SR46SDR SWAA031296Skin · crackedDURING SCHEDULED C4 CHECK, FOUND BOTH LEFT AND RIGHT HORIZ STAB SKIN CRACKED ON LOWER SURFACE AT REAR SPAR ATTACHMENT POINT, LEFT AND RIGHT AT STA 145 AND RT AT STA 152. REPAIRED SKIN PER SRM.Jun 9, 2003 · N524SW · Boeing 7375H4SDR CALA0300299Skin · dentedA DENT WAS DISCOVERED IN THE LT HORIZONTAL STABILIZER SKIN 15 INCHES O/B OF FUSELAGE ON LEADING EDGE AT STA 60. THE DENTED AREA PREVIOUSLY HAD AN INTERIM REPAIR INSTALLED AND HAD BEEN PLACED ON DIP. A PERMANENT REPAIR WAS PERFORMED BY INSTALLING AN EXTERNAL Jun 9, 2003 · N16339 · Boeing 7373T0SDR DHL2003604677Skin · dentedLT HORIZ STAB L/E OUTER SKIN DENTED FROM STA XFS 91.250 - XFS 116.250. PERFORMED MAJOR REPAIR IAW EODHL-030515, ED-3270. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. TRIMMED OUT THE DAMAGED SKIN SEGMENT IAW EODHL-030515, ED-3270. CLEANED, TREATED AND PRIMED AREJun 6, 2003 · N604AL · Doug DC873FSDR DHL2003604662Skin · dentedLT HORZ STAB L/E HAS INTERIM REPAIR & SEVERAL DENTS BETWEEN STA XFS 47.500 AND XFS 91.250 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EO DHL 030505, ED 3270. REMOVED FASTENERS & EXISTING INTERIM REPAIR IAW SRM 51-1-21 PG 1, SRM 51-1-21A PG 4. CLEANED, TREATEJun 6, 2003 · N604AL · Doug DC873FSDR USAA030097Skin · crackedPIT - FOUND SKIN CRACKED 1.5 INCH, RIGHT HORIZONTAL STAB LOWER SKIN APPROX STATION 115. DAMAGE CUTOUT AND EXTERNAL SKIN DOUBLER INSTALLED PER SRM 55-10-01 FIG 204. (M)Jun 5, 2003 · N421US · Boeing 737401SDR ASAA0310496Skin · dentedDURING SCHEDULED C-CHECK, FOUND THE HORIZONTAL STABILIZER LEADING EDGE AT FUSELAGE STATION 1049.602, STABILIZER STATION 75 DENTED. (M)Jun 2, 2003 · N746AS · Boeing 7372X6CSDR QXEA200300717Skin · gougedPDX - GOUGE IN LEFT HAND HORIZONTAL STAB TOP SKIN AT FRONT SPAR AND F605D-75.20. REPAIRED IAW Q400 WRM 51-21-10, PAGES 204-205 AND SRM 51-25-10, PAGES 201-205.Jun 1, 2003 · N408QX · Bombdr DHC8401SDR QXEA200300716Skin · gougedPDX - GOUGE IN LEFT HAND HORIZONTAL STAB TOP SKIN AT FRONT SPAR AND Y605D-73.00. REPAIRED IAW Q400 SRM 51-21-10, PAGES 204-205 AND SRM 51-25-10, PAGES 201-205.Jun 1, 2003 · N408QX · Bombdr DHC8401SDR QXEA200300715Skin · gougedPDX - GOUGE IN LEFT HAND HORIZONTAL STAB TOP SKIN AT FRONT SPAR AND Y605D-52.96. REPAIRED IAW Q400 SRM 51-21-10, PAGES 204-205 AND SRM 51-25-10, PAGES 201-205.Jun 1, 2003 · N408QX · Bombdr DHC8401SDR QXEA200300714Skin · gougedPDX - GOUGE IN LEFT HAND HORIZONTAL STAB TOP SKIN AT SPAR CAP AND Y605D-39.17. REPAIRED IAW Q400 SRM 51-21-10, PAGE 204-205 AND SRM 51-25-10, PAGE 201-205.Jun 1, 2003 · N408QX · Bombdr DHC8401SDR QXEA200300713Skin · gougedPDX - GOUGE IN LEFT HAND HORIZONTAL STAB TOP SKIN AT FORWAD SPAR CAP AND Y605D-26.40. REPAIRED IAW Q400 SRM 51-21-10, PAGE 204-205 AND SRM 51-25-10, PAGE 201-205.Jun 1, 2003 · N408QX · Bombdr DHC8401SDR CALA0300269Skin · dentedINSPECTION FOUND A DENT WITH GOUGE IN LT HORIZONTAL STABILIZER UPPER SPAR SKIN. THE DENT WAS LOCATED 51 INCHES O/B FROM I/B EDGE AND 3.5 INCHES AFT OF FORWARD SPAR. THE DENTED AREA WAS CUTOUT AND A DOUBLER WAS INSTALLED IAW SRM 55-10-01, FIGURE 207.May 28, 2003 · N14639 · Boeing 737524SDR SWAA031150Skin · crackedDURING SCHEDULED C4 CHECK, FOUND 4 EA CRACKS AT LT HORIZONTAL STAB LOWER SKIN EMANATING FROM FASTENERS HOLES, BETWEEN STA 124 AND STA 173. REPAIRED SKIN PER SRM.May 21, 2003 · N105SW · Boeing 7372H4SDR SWAA031149Skin · crackedDURING SCHEDULED C4 CHECK, FOUND 14 EA CRACKS AT RT HORIZONTAL STAB LOWER SKIN EMANATING FROM FASTENERS HOLES, BETWEEN STA 107 AND STA 173. REPAIRED SKIN PER SRM.May 21, 2003 · N105SW · Boeing 7372H4SDR DHL2003604647Skin · corrodedLT HORIZONTAL STAB. LE EXTERNAL SKIN SHOWS CORROSION ON SEVERAL SPOTS AT STA. XFS.178.750. PERFORMED MAJOR REPAIR. REMOVED FASTENERS, REMOVED CORROSION ON LT HORIZ. STAB. L/E EXTERNAL SKIN IAW SRM 51-1-8 PG.17-18. FOUND OUT OF LIMITS IAW SRM 55-2-1 FIG.3. TMay 20, 2003 · N604AL · Doug DC873FSDR 2003F00495Skin · crackedAT C-CHECK, FOUND LEFT HORIZONTAL STABILIZER LEADING EDGE CRACKED AND SEVERAL DENTS. REPAIRED CRACK IAW SRM 55-14-11, FIGURE 205. DENTS WERE REPAIRED PER PER SRM 51-77-11, REV 61. (M)May 15, 2003 · N951LF · Airbus A320233SDR A6WA200360027Panel · chafedCHAFE DAMAGE TO LEFT STABILIZER PANEL 275CL. MAINTENANCE BLENDED AND POLISHED DAMAGE AREA IAW BAE FAX BARA/AVR/3037/03-DC. (M)May 12, 2003 · N612AW · Bac 146300ASDR DHL2003604646Skin · damagedRT HORIZONTAL STAB INTERIM REPAIR ON INBD L/E XFS 178.750. PERFORMED MAJOR REPAIR IAW EODHL-030504, ED-3275. REMOVED FASTENERS, EXISTING INTERIM REPAIR AND FILLER IAW SRM 51-1-21 PG 1. TRIMMED OUT DAMAGED AREA IAW EODHL-030504, ED-3275. CLEANED, TREATED ANMay 9, 2003 · N604AL · Doug DC873F
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