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 06FDEA02870Panel · corrodedCORROSION EXCEEDED LIMIT PER EO 1-5510-7-5000 D1 PT1 AT BARREL NUT BORE NR 25 RT OF HORIZONTAL STABILIZER. RT HORIZONTAL STABILIZER NR 25 BARREL NUT BORE REPAIRED AS PER HORIZONTAL STABILIZER-BARREL NUT BORE REWORK/REPAIR EA1-5510-95649 ATTACHMENT 6. CLASSIAug 7, 2006 · N521FE · Doug MD11SDR 06FDEA02869Panel · corrodedCORROSION EXCEEDED LIMIT PER EO 1-5510-7-5000 D1 PT1 AT BARREL NUT BORE NR 33 RT OF HORIZONTAL STABILIZER. RT HORIZONTAL STABILIZER NR 33 BARREL NUT BORE REPAIRED AS PER HORIZONTAL STABILIZER-BARREL NUT BORE REWORK/REPAIR EA 1-5510-95649 ATTACHMENT 5. CLASSIAug 7, 2006 · N521FE · Doug MD11SDR 06FDEA02868Panel · corrodedFOUND CORROSION EXCEEDED LIMIT PER EO 1-5510-7-5000 D1 PT1 AT BARREL NUT BORE NR 31 RT OF HORIZONTAL STABILIZER. RT HORIZONTAL STABILIZER NR 31 BARREL NUT BORE REPAIRED AS PER HORIZONTAL STABILIZER-BARREL NUT BORE REWORK/REPAIR EA1-5510-95649 ATTACHMENT 10.Aug 7, 2006 · N521FE · Doug MD11SDR 06FDEA02867Panel · corrodedFOUND CORROSION EXCEEDED LIMIT PER EO 1-5510-7-5000 D1 PT1 AT BARREL NUT BORE NR 29 RT OF HORIZONTAL STABILIZER. RT HORIZONTAL STABILIZER NR 29 BARREL NUT BORE REPAIRED AS PER HORIZONTAL STABILIZER-BARREL NUT BORE REWORK/REPAIR E.A.1-5510-95649 ATTACHMENT 1Aug 7, 2006 · N521FE · Doug MD11SDR 06FDEA02866Panel · corrodedFOUND CORROSION EXCEEDED LIMIT PER EO 1-5510-7-5000 D1 PT1 AT BARREL NUT BORE NR 27 RT OF HORIZONTAL STABILIZER. RT HORIZONTAL STABILIZER NR 27 BARREL NUT BORE REPAIR CARRIED OUT PER HORIZONTAL STABILIZER-BARREL NUT BORE REWORK/REPAIR E.A.1-5510-95649 ATTACAug 7, 2006 · N521FE · Doug MD11SDR 06FDEA02865Panel · corrodedCORROSION EXCEEDED LIMIT PER EO 1-5510-7-5000 D1 PT1 AT BARREL NUT BORE NR 15 RT OF HORIZONTAL STABILIZER. RT HORIZONTAL STABILIZER NR 15 BARREL NUT BORE REPAIRED AS PER HORIZONTAL STABILIZER-BARREL NUT BORE REWORK/REPAIR E.A.1-5510-95649 ATTACHMENT 3. CLASSAug 7, 2006 · N521FE · Doug MD11SDR 06FDEA02863Panel · corrodedCORROSION EXCEEDED LIMIT PER EO 1-5510-7-5000 D1 PT1 AT BARREL NUT BORE NR 21 LT OF HORIZONTAL STABILIZER. LEFT HORIZONTAL STABILIZER NR 21 BARREL NUT BORE REPAIRED AS PER HORIZONTAL STABILIZER-BARREL NUT BORE REWORK/REPAIR E.A.1-5510-95649 ATTACHMENT 23. CLAug 7, 2006 · N521FE · Doug MD11SDR 06FDEA02862Panel · corrodedCORROSION EXCEEDED LIMIT PER EO 1-5510-7-5000 D1 PT1 AT BARREL NUT BORE NR 25 LT OF HORIZONTAL STABILIZER. LT HORIZONTAL STABILIZER NR 25 BARREL NUT BORE REPAIRED AS PER HORIZONTAL STABILIZER-BARREL NUT BORE REWORK/REPAIR EA1-5510-95649 ATTACHMENT 18. CLASSIAug 7, 2006 · N521FE · Doug MD11SDR 06FDEA02861Panel · corrodedCORROSION EXCEEDED LIMIT PER EO 1-5510-7-5000 D1 PT1 AT BARREL NUT BORE NR 17 LT OF HORIZONTAL STABILIZER. LT HORIZONTAL STABILIZER NR 17 BARREL NUT BORE REPAIRED AS PER HORIZONTAL STABILIZER-BARREL NUT BORE REWORK/REPAIR E.A.1-5510-95649 ATTACHMENT 17. CLASSAug 7, 2006 · N521FE · Doug MD11SDR 06FDEA02859Panel · corrodedCORROSION EXCEEDED LIMIT PER EO 1-5510-7-5000 D1 PT1 AT BARREL NUT BORE NR 20 LT OF HORIZONTAL STABILIZER. LT HORIZONTAL STABILIZER NR 20 BARREL NUT BORE REPAIRED AS PER HORIZONTAL STABILIZER-BARREL NUT BORE REWORK/REPAIR E.A.1-5510-95649 ATTACHMENT 8. CLASSAug 7, 2006 · N521FE · Doug MD11SDR 06FDEA02858Panel · corrodedCORROSION EXCEEDED LIMIT PER EO 1-5510-7-5000 D1 PT1 AT BARREL NUT BORE NR 18 LT OF HORIZONTAL STABILIZER. LT HORIZONTAL STABILIZER NR 18 BARREL NUT BORE REPAIRED AS PER HORIZONTAL STABILIZER-BARREL NUT BORE REWORK/REPAIR EA1-5510-95649 ATTACHMENT 7. CLASSIFAug 7, 2006 · N521FE · Doug MD11SDR SWAA062851Skin · crackedDURING SCHEDULED C4 CHECK, FOUND LT HORZONTAL STAB LOWER SKIN CRACKED AT STA 117. REPAIRED SKIN PER SRM.Aug 4, 2006 · N325SW · Boeing 7373H4SDR 06FDEA2771Skin · dentedLEFT HAND HORIZONTAL STABILIZER LEADING EDGE SKIN DENT MEASURES APPROXIMATELY 2 X 1 X 0.210 DEEP. NO SRM REPAIR ON DENT AREA ALC8400-5. REPAIR CARRIED OUT PER FEDEX E.A. 1-5510-103523, STABILIZERS - HORIZONTAL STABILIZER - REPAIR LEADING EDGE DENT. REPAIRAug 2, 2006 · N592FE · Doug MD11SDR ASAA0640831Skin · crackedLT HORIZ STAB LWR SKIN CRACKED APPROX 1" LONG AT REAR SPAR. ACCOMPLISHED TEMP REPAIR IAW PEMCO EA PD37 55 0111 AND ASA EA 5510 01245 AND PER BOEING MESSAGE 1 209186222 8 DATED 19 JUL 06.Aug 2, 2006 · N763AS · Boeing 7374Q8SDR 06FDEA2748Skin · damagedEXISTING EXTERNAL DOUBLER REPAIR APPROX 2 X 2 INCHES ON RT HORIZONTAL STABILIZER UPPER SURFACE T/E AREA, ELEVATOR STA 99.79 NR 2 BALANCE BAY UPPER PANEL. REPAIR REQUIRES EVALAUTION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPJul 31, 2006 · N201FE · Boeing 727200SDR USAA06999Skin · crackedFOUND CRACK RT HORIZ STAB LOWER SKIN STAB STA 160. INSTALLED DOUBLER IAW TR 55-10-07, DEFECT SIZE: 1.75".Jul 31, 2006 · N425US · Boeing 737401SDR UIEA200600195Skin · damagedON WALKAROUND, FOUND HOLE IN LEADING EDGE OF RIGHT HORIZONTAL STABILIZER. REPAIR CARRIED OUT AS PER SRM 55-10-03 FIG 1. XEO 55-072806 ALL ORIGINAL SIGNATURES HELD ON XEO 55-072806 ITEM 2. FURTHER INSPECTION REVEALED HOLE IN LEADING EDGE OF RIGHT INBOARD FOREJul 29, 2006 · N506MC · Boeing 7472D3BSDR IXXA06SMN243SSkin · misrepairedDURING ROUTINE C-CHECK INSPECTION FOUND RIGHT HAND HORIZONTAL STABILIZER OUTBOARD LEADING EDGE WITH NON STANDARD REPAIR FROM STATION XFS 272.150 TO STATION XFS 285.000. REMOVED NON STANDARD REPAIR IAW DC-8 SRM 51-1-21, TRIMMED OUT DAMAGED AREA AND FABRICATED Jul 28, 2006 · N605AL · Doug DC8*SDR IXXA06SMN242SSkin · dentedDURING ROUTINE C-CHECK INSPECTION FOUND RT HORIZONTAL STABILIZER OB LEADING EDGE DENTED FROM STA XFS222.500, TO STA XFS241.250. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-21A. TRIMMED OUT DAMAGED AREA AND FABRICATED REPAIR DOUBLER , AND FILLER (AL 7075 T6 Jul 28, 2006 · N605AL · Doug DC8*SDR IXXA06SMN240SSkin · misrepairedDURING ROUTINE C-CHECK INSPECTION FOUND RT HORIZONTAL STABILIZER IB LEADING EDGE WITH NON STANDARD REPAIR BETWEEN STATIONS XFS. 172.500, AND STATION 178.750. REMOVED NON STANDARD REPAIR IAW SRM 51-1-21. TRIMMED OUT DAMAGED AREA AND FABRICATED REPAIR DOUBLEJul 28, 2006 · N605AL · Doug DC8*SDR IXXA06SMN239SSkin · dentedDURING ROUTINE C-CHECK INSPECTION FOUND RT HORIZONTAL STABILIZER IB LEADING EDGE DENTED BETWEEN STA XFS103.750 AND STA XFS128.750. REMOVED FASTENERS. REMOVED DAMAGE. FABRICATED REPAIR PARTS. LOCATED, DRILLED, TRIMMED, TREATED, PRIMED AND INSTALLED REPAIR PARTSJul 21, 2006 · N605AL · Doug DC8*SDR IXXA06SMN237SSkin · misrepairedDURING ROUTINE C-CHECK INSPECTION FOUND LEFT HAND HORIZONTAL STABILIZER OUTBOARD LEADING EDGE WITH NON STANDARD REPAIR FROM STATION XFS 178.750 TO STATION XFS 185.000. REMOVED EXISTING REPAIR IAW DC-8 SRM 51-1-21, DC-8 SRM 51-3-0. REMOVED DAMAGED AREA IAW SEJul 21, 2006 · N605AL · Doug DC8*SDR IXXA06SMN238SSkin · misrepairedDURING ROUTINE C-CHECK INSPECTION FOUND LT HORIZONTAL STABILIZER IB LEADING EDGE WITH NON STANDARD REPAIR FROM STATION XFS 110.000 TO STATION XFS 116.250. REMOVED NON STANDARD REPAIR IAW SRM 51-1-21. TRIMMED OUT DAMAGED AREA. FABRICATED REPAIR DOUBLER, AND Jul 21, 2006 · N605AL · Doug DC8*SDR MALA060476Skin · dentedDURING 4K CHECK IN BNA FOUND RT HORIZONTAL STABILIZER HAS 2 DENTS LOCATED AT HS103.72 AND 102.50. THE DENTS ARE OUT OF LIMITS. INSTALLED BONDED DOUBLER OVER BOTH DAMAGED AREAS IAW EO NR S55017. REF: EAMS WORK ORDER 214182-3510.Jul 17, 2006 · N437XJ · Saab 340BSDR C2XA06SH075Skin · corrodedSHV DURING C-CHECK, RT HORIZONTAL STAB L/E HAS SEVERAL AREAS OF CORROSION ON SKIN AROUND RIVET HEAD AND SOME RIVET HEADS PULLING THROUGH SKIN. MAINTENANCE REPAIRED RT HORIZONTAL STAB L/E IAW EC5530-01101. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.Jul 16, 2006 · N13969 · Emb EMB145LRSDR KCSA061206Skin Panel · corrodedLT HORIZ STAB UPPER SURFACE HAS CORROSION AT STAB STA 165.Jul 14, 2006 · N706CK · Boeing 747249FSDR ARWA20060702Panel · corrodedDURING C-CHECK INSPECTION, THE FOLLOWING WAS FOUND; LT HORIZONTAL STABILIZER BETWEEN XE 312.500 AND XE 149.000 T/E UPPER PANELS WITH CORROSION.Jul 8, 2006 · N441J · Doug DC863FSDR SWAA062316Skin · crackedDURING SCHEDULED 20Y CHECK, FOUND LT HORIZONTAL STAB LOWER SKIN CRACKED AT STA 135.70. REPAIRED SKIN PER ER.Jul 5, 2006 · N689SW · Boeing 7373Q8SDR 2006UALA01268Skin · crackedRT HORIZ STAB LOWER SKIN HAS 1.5 INCH CRACK, 2 INCHES FWD OF AFT EDGE AND 63 INCHES FROM INBD END. [06-27-07] MAJOR REPAIR: INSTALLED EXTERNAL SKIN DOUBLER REPAIR.Jun 27, 2006 · N339UA · Boeing 737322SDR MALA060441Panel · dentedDURING INSPECTION OF THE LEFT HORIZONTAL STAB FOR OTHER MAINTENANCE NOTED TWO DENTS ON THE TOP SKIN. ONE DENT LOCATION WAS 10 INCHES FORWARD OF THE AFT SPAR, 4 INCHES OUTBOARD OF STATION 51.92. DENT DIMENSIONS WERE 1.25 INCHES BY 1.25 INCHES AND .038 INCHES Jun 23, 2006 · N451XJ · Saab 340BSDR C2XA06SH068Skin Panel · corrodedSHV - DURING C-CHECK LT AND RT HORIZONTAL STAB LEADING HAVE RIVETS WITH CORROSION. MAINTENANCE REMOVED CORROSION AND REPLACED RIVETS IAW EC5530-01101. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.Jun 21, 2006 · N14974 · Emb EMB145LRSDR UIEA200700249Panel · crackedLT HORIZONTAL STABILIZER, LOWER T/E ACCESS PANEL 334 GBL HAS 2 EACH CRACKS ON INBOARD SIDE OF PANEL. CRACKS ARE 2.0 INCH IN LENGTH. ACCOMPLISHED PERMANENT REPAIR AS PER 747-200 SRM 51-40-09 FIG 13, 747-200 SRM 51-40-12. ALSO REFERENCE ATLAS AIR XEO 55-06150Jun 16, 2006 · N809MC · Boeing 747228FSDR SWAA062081Skin · crackedDURING SCHEDULED 20Y CHECK, FOUND RT HORIZONTAL STAB SKIN CRACKED AT LOWER SURFACE STA 133.5. REPAIRED SKIN PER ER.Jun 15, 2006 · N687SW · Boeing 7373Q8SDR SWAA062063Skin · crackedDURING SCHEDULED C1 CHECK, FOUND RT HORIZONTAL STAB SKIN CRACKED AT LOWER SURFACE, STA 70. REPAIRED SKIN PER SRM.Jun 14, 2006 · N392SW · Boeing 7373H4SDR SWAA062009Skin · corrodedDURING SCHEDULED PM CHECK, FOUND RIGHT HORIZONTAL STAB UPPER SKIN CORRODED. REMOVED AND REPLACED RIGHT HORIZONTAL STAB PER MM.Jun 11, 2006 · N330SW · Boeing 7373H4SDR PIDR2006009Skin · damagedDURING A-CHECK/BRIDGING CHECK FOR RETURN TO SERVICE FROM STORAGE, DAMAGE NOTED ON THE RIGHT HORIZONTAL STABILIZER APPROXIMATELY 8 FEET FROM THE INBOARD END. REPAIRED PER SRM 55-10-01.Jun 6, 2006 · N231DN · Boeing 7373L9SDR USAA200606004Skin · crackedLEFT HORIZ STAB LOWER SKIN AT AFT SPAR CAP, STAB STA 14.5 CRACKED. INSTALLED FILLER AND DOUBLER (TEMPORARY REPAIR) PER EA 82547, SRM 51-20-05, AMM 51-21.Jun 5, 2006 · N422US · Boeing 737401SDR USAA200606003Skin · crackedLT HORIZ STAB LWR SKIN AT AFT SPAR CAP, STAB STA 12.5. INSTALLED FILLER AND DOUBLER (TEMPORARY REPAIR), PER EA 82547, SRM 51-20-05, AMM 51-21.Jun 5, 2006 · N422US · Boeing 737401SDR USAA200606002Skin · crackedLEFT HORZ STAB LOWER SKIN CRACK 2.375 INCH AT STA 125. INSTALLED DOUBLER PER EA 97771.Jun 5, 2006 · N422US · Boeing 737401SDR QXEA200601384Paint · scratchedPDX - C4 SCRATCH THROUGH PAINT ON TOP OF LEFT HAND HORIZONTAL STABILIZER. REPAIRED IAW DHC-8-200 SRM 51-20-26.May 26, 2006 · N352PH · Dhav DHC8202SDR MALA060372Skin · dentedHAIL CONTACT DAMAGE ON LEFT HORIZONTAL STABILIZER CAUSED 2 DENTS IN UPPER ALUMINUM SKIN AT HS51.92, DENT 67 .012 INCH DEEP AND 7/8 INCH DIAMETER LOCATED 33 INCHES FROM THE LEADING EDGE AND DENT 66 .017 INCH DEEP AND 7/8 INCH DIAMETER 34.5 INCHES FROM LEADING EMay 25, 2006 · N436XJ · Saab 340BSDR SWAA061726Skin · crackedDURING SCHEDULED C1 CHECK, FOUND RT HORIZONTAL STAB LOWER SURFACE SKIN CRACKED AT STA 107. REPAIRED SKIN PER SRM.May 22, 2006 · N355SW · Boeing 7373H4SDR IXXA06SMN159SFinger Doubler · corrodedDURING ROUTINE C CHECK INSPECTION FOUND RIGHT HAND HORIZONTAL STABILIZER RIGHT HAND ELEVATOR CENTER LOWER PANEL FINGER DOUBLER WITH SPOTS OF CORROSION, FROM STATION XE 132.750 TO STATION XE 251.562. PERFORMED MAJOR REPAIR IAW DC-8 SRM 55-4-1 FIGURE 1 SHEET 1,May 19, 2006 · N830BX · Doug DC871FSDR MALA060343Skin · damagedLEFT HORIZONTAL STABILIZER SUSTAINED DAMAGE FROM HAIL. TWO DENTS REQUIRED REPAIRS. FIRST DENT DAMAGE MEASURES 3/8 INCH IN DIAMETER AND .006 INCH IN DEPTH, LOCATED 13.5 INCH FROM TRAILING EDGE AND AT STATION 84.64. SECOND DENT DAMAGE MEASURES 5/8 INCH IN DIAMay 19, 2006 · N417XJ · Saab 340BSDR MASA200601361Fairing · crackedASH 7285 IAD - HORIZONTAL STAB LT FAIRING TIP APPEARS CRACKED. MX INSPECTED AND NO DEFECTS NOTED.May 18, 2006 · N509MJ · Cndair CL6002C10SDR IXXA06RNG048SSkin · corrodedDURING ROUTINE C CHECK, FOUND CORROSION ON HORIZONTAL STABILIZER UPPER SKIN LEADING EDGE FROM STATION XFS 178.00 TO STATION 203.750 TO THE RIGHT HAND REAR. DAMAGED AREA WAS CLEANED AND EXTERNAL DOUBLER WAS FABRICATED AND INSTALLED IAW EWO ATI 55-018.May 18, 2006 · N823BX · Doug DC871FSDR 06FDEA1958Skin · corrodedLOWER SKIN OF LEFT HORIZONTAL STAB HAS NUMEROUS AREAS OF CORROSION FROM STAB TIP TO I/B END, FWD SRAP TO AFT SPAR. REPAIRED PER FED EX EA 7-5510-102242.May 17, 2006 · N192FE · Boeing 72722SDR 06FDEA1885Panel · damagedPREVIOUS REPAIR FOUND LOCATED ON THE LT HORIZONTAL STABILIZER LEADING EDGE PANEL 331CB, FLUSH REPAIR ON OUTBD LEADING EDGE. EXISTING REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN SRM REPAIR NEW REPAIR ACCOMPLISHED PER SRM 55-12-12 REPAIR EVALUATED PER GMMMay 12, 2006 · N450FE · Airbus A310222SDR 06FDEA1884Panel · damagedPREVIOUS REPAIR FOUND LOCATED ON THE LT HORIZONTAL STABILIZER LEADING EDGE PANEL 331BB, FLUSH REPAIR ON OUTBD LEADING EDGE. EXISTING REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN SRM REPAIR NEW REPAIR ACCOMPLISHED PER SRM 55-12-12 FIG. 203 REPAIR EVALUATEMay 12, 2006 · N450FE · Airbus A310222SDR 06FDEA1800Skin · damagedLT HORIZONTAL STAB HAS A BLEND OUT THAT EXCEEDS SRM LIMITS AT STAB STA 77.1, .500 FWD OF THE EDGE OF THE T/E SKIN. REPAIRED LT HORIZONTAL STAB LWR SKIN PER FED EX EA 7-5510-102242.May 11, 2006 · N192FE · Boeing 727100
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