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 HEEA0015363Skin · delaminatedSTABILIZER ASSEMBLY SEPARATED AND DELAMINATED ON LOWER SIDE.Jul 29, 1998 · N2764F · Bell 206L1SDR SWAA981502Skin · dentedDURING SCHEDULED D-CHECK, FOUND DENTED RIGHT HORIZONTAL REMOVABLE L/E AT BS 124.5. REMOVED AND REPLACED PER BOEING SRM.Jul 24, 1998 · N671SW · Boeing 7373G7SDR SWAA981485Skin · delaminatedDURING SCHEDULED TRAN CHECK, FOUND DELAMINATED RT HORIZ STAB UPPER SURFACE O/B T/E PANEL. REMOVED AND REPLACED PER BOEING SRM.Jul 23, 1998 · N659SW · Boeing 737301SDR S9BA604YSkin · crackedDURING EMMA INSPECTION NR 13, A CRACK WAS FOUND ON ELEVATOR CENTER HINGE BRACKET UPPER SUPPORT DOUBLER. REPLACED HORIZONTAL STABILIZER, RIGGED CONTROLS, AND TEST FLIGHT SATISFACTORY IAW DHC-6-300 MM AND SEABORNE GMM. (X)Jul 21, 1998 · N288SA · Dhav DHC6300SDR TWAA9812006Skin · damagedDURING OP 16 MAINT CHECK, FOUND LT HORIZ STAB, LEADING EDGE OF STAB DAMAGED AND FILLET DETERIORATED APPROX 20 IN FROM O/B END. INSTALLED DOUBLER PER SRM 55-03, FIG 3 PG 5.Jul 17, 1998 · N998R · Doug DC932SDR IXXA9800101Panel · corrodedDURING ROUTINE C CHECK INSPECTION, A CORROSION BULGE WAS DETECTED ON THE RIGHT HORIZONTAL STABILIZER UPPER TRAILING EDGE PANEL BETWEEN STATION XE 77 AND XE 148. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF A NEW PANEL IN ACCORDJul 17, 1998 · N21CX · Doug DC862SDR IXXA9800098Panel · corrodedDURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON RIGHT HORIZONTAL STABILIZER UPPER TRAILING EDGE PANEL BETWEEN STATIONS XE 272 AND XE 275. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF A NEW PANEL IN ACCORDANCE WITH Jul 17, 1998 · N21CX · Doug DC862SDR IXXA9800097Panel · corrodedDURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON RIGHT HORIZONTAL STABILIZER UPPER TRAILING EDGE PANEL BETWEEN STATIONS XE 149 AND XE 221. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF A NEW PANEL IN ACCORDANCE WITH Jul 17, 1998 · N21CX · Doug DC862SDR IXXA9800102Panel · corrodedDURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON LEFT HORIZONTAL STABILIZER LOWER TRAILING EDGE PANEL BETWEEN STATIONS XE 221 AND XE 272. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF A NEW PANEL IN ACCORDANCE WITH FJul 16, 1998 · N21CX · Doug DC862SDR TWAA9812012Skin · crackedDURING OP 15 MAINT CHECK, FOUND RT STAB L/E CRACKED 3 INCHES IN UPPER FLANGE OF L/E SECT AT XFS 40. FABRICATED DOUBLER AND INSTALLED PER SRM 55-01, PAGE 8.Jul 13, 1998 · N980Z · Doug DC931SDR SWAA981338Skin · crackedDURING SCHEDULED D-CHECK, FOUND CRACKED RT HORIZONTAL STABILIZER, L/E SKIN AT FASTENER, STAB BS 66 TO 93 AND BS 84.93. REMOVED AND REPLACED PER BOEING SRM.Jul 11, 1998 · N336SW · Boeing 7373H4SDR SIMA981802Skin · chafedABI- DURING COMPLIANCE OF SB 34-53-042, INSTALLATION OF PROTECTION PLATE ON LT FUSELAGE AT HORIZONTAL STABILIZER, A CHAFE WAS DISCOVERED BEYOND SRM LIMITATIONS. BLENDED AREA. PERFORMED EDDY CURRENT INSPECTION. INSTALLED EXTERNAL DOUBLER 11.0 INCHES BY 10.7Jun 29, 1998 · N268AE · Saab 340BSDR AU980901Skin · corroded(AUS) RIGHT HORIZONTAL STABILIZER LOWER SKIN CORRODED IN AREA 63.5MM (2.5 INCHES) OUTBOARD OF THE FUSELAGE AND 127MM (5 INCHES) AFT FROM THE LEADING EDGE SKIN.Jun 25, 1998 · Cessna 441SDR MWEA98759Skin · corrodedFOUND CORROSION ON HORIZONTAL STABILIZER CENTER SECTION LOWER PLATING. MTC REMOVED CORROSION AND FABRICATED AND INSTALLED REPAIR STRAP.Jun 24, 1998 · N809ME · Doug DC982SDR RRXA99196Skin · corrodedDURING A MAINTENANCE VISI, FOUND CORROSION DAMAGE TO HORIZONTAL STABILIZER SKIN PANEL AT XE 181, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SKIN PANEL IAW SK8550002. (CORROSION DAMAGE Jun 23, 1998 · N995CF · Doug DC862SDR P5CA9801034Skin · corrosionRT HORIZONTAL STAB UPPER SURFACE CORROSION REVEALED. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01 AND 51-10-02.Jun 23, 1998 · N858FT · Boeing 747123SDR P5CA9801030Skin · corrodedLT HORIZONTAL STAB LOWER SURFACE CORROSION REVEAL AT AREA JUST BELOW AFT OF LOWER AIR GATE SEAL FAIRING STA 2600. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01 AND 51-10-02.Jun 23, 1998 · N858FT · Boeing 747123SDR P5CA9801022Skin · corrodedLEVEL ONE CORROSION FOUND ON RIGHT HAND HORIZONTAL STABILIZER LOWER SURFACE AT LEADING EDGE STA 260. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01 AND 51-10-02.Jun 23, 1998 · N858FT · Boeing 747123SDR GAIA9865Skin · damagedDURING ROUTINE C-CHECK, SEVERAL HOLES ALONG THE RIGHT STABILIZER LOWER TRAILING EDGE AT ELEVATOR STATION 99 TO 136, HOLDING PLASTIC FAIRING WHERE FOUND ENLARGED. EXISTING HOLES WHERE PLUGGED PER SRM. NEW HOLES WHERE MADE 2D FROM PLUGGED HOLES. REINSTALLED PJun 23, 1998 · N6810 · Boeing 727223SDR USAA980274Skin · crackedCLT - DURING INTERIOR MOD CHECK VISUAL INSPECTION, FOUND 1.5 INCH CRACK IN LOWER SKIN RT HORIZ STAB STATION 125.5 AND HORIZ STAB FRONT SPAR. INSTALLED DOUBLER PER TYPICAL REPAIR 55-10-07. (M)Jun 22, 1998 · N443US · Boeing 7374B7SDR DL72S981305Skin · damagedOUTER SKIN DAMAGED AT FASTENER HOLE ON PANEL 9115. REPAIRED PER SRM 55-30-3 FIG 3.Jun 15, 1998 · N416DA · Boeing 727232SDR DL72L981240Panel · holeFOUND ON F1 LETTER CHECK, HOLE .25 IN LOWER LT HORIZONTAL STAB ACCESS PANEL INBD OF ELEV PWR PACK. INSTALLED DOUBLER PER SRM 55-20-3.Jun 10, 1998 · N503DA · Boeing 727232SDR 98ZZZX2423Skin · crackedFOUND SPANWISE CRACK IN HORIZONTAL STABILIZER LEADING EDGE SKIN BETWEEN STA 98.00 AND STA 103.00. CRACK POSSIBLY CAUSED BY FATIGUE TO THIN SKIN CAUSED BY REPETITIVE REPLACEMENT AND ROLLING DOWN OF EDGES OR STABILIZER DEICER BOOT.Jun 8, 1998 · N331SA · Dhav DHC6300SDR CALA9800923Plates · corrodedINSPECTION FOUND LT HORIZONTAL STABILIZER PIVOT OUTBOARD PLATES AND RT HORIZONTAL STABILIZER PIVOT OUTBOARD PLATES CORRODED. THE PLATES WERE REPLACED IAW SRM 51-30-00.May 30, 1998 · N35832 · Doug DC982SDR SWAA980988Skin · dentedDURING SCHEDULED BC 3 CHECK, FOUND LT HORIZ STAB HAS A DENT 4 FT FROM FUSELAGE. REMOVED AND REPLACED PER BOEING SRM.May 28, 1998 · N692SW · Boeing 7373T5SDR SWAA980968Skin · dentedDURING SERVICE CHECK, FOUND LT HORIZONTAL STABILIZER LEADING EDGE DENTED 3 FT OUTBD OF INBD SIDE. REPAIRED PER BOEING SRM.May 28, 1998 · N635SW · Boeing 7373H4SDR 98ZZZX2015Stabilizer · damagedRIGHT-HAND HORIZONTAL STABILIZER AND ELEVATOR FOUND DAMAGED ON TRANSIT CHECK IN MONTEGO BAY BY MAINTENANCE. THERE WAS NO REPORT FROM THE FLIGHT CREW. INVESTIGATION REVEALED DEBRIS (ASPHALT) EMBEDDED IN THE RIGHT-HAND ELEVATOR. THE DETAILS OF THE TOTAL DAMAGMay 20, 1998 · N630AJ · Airbus A320214SDR SWAA980897Skin · dentedDURING SERVICE CHECK, FOUND 2.5 BY 2.0 BY .218 DENTED HORIZONTAL STABILIZER L/E 24 O/B OF FUSELAGE. REPAIRED PER BOEING SRM.May 19, 1998 · Boeing 7372H4SDR MWEA98610Skin · misrepairedFOUND PREVIOUS REPAIR ON LEFT HAND HORIZONTAL STABILIZER LEADING EDGE INBOARD PANEL. FABRICATED AND INSTALLED REPAIR DOUBLER.May 19, 1998 · N809ME · Doug DC982SDR RRXA98282Skin · corrodedDURING A MAINTENANCE VISIT, FOUND HORIZONTAL STABILIZER LEADING EDGE RIGHT SIDE WITH EXFOLIATION CORROSION BEYOND DC-8 SRM LIMITS, AT STA XFS 178 TO STA XFS 200. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLMay 16, 1998 · N990CF · Doug DC862SDR SWAA980853Panel · gougedDURING SCHEDULED D CHECK, FOUND GOUGE AT RT HORIZ STAB LEADING EDGE PANEL LE BS 100.56. REMOVED AND REPLACED PER BOEING SRM.May 14, 1998 · N670SW · Boeing 7373G7SDR SWAA980852Skin · gougedDURING SCHEDULED D CHECK, FOUND GOUGE AT RT HORIZ STAB LEADING EDGE PANEL LE BS 149.75. REMOVED AND REPLACED PER BOEING SRM.May 14, 1998 · N670SW · Boeing 7373G7SDR CALA9800843Skin · corrodedLEFT HORIZ STAB LOWER AFT SKIN PANEL NR 3 FOUND CORROSION BETWEEN STA XHS86 AND XHS104. INSTALLED REPAIR DOUBLERS PER EC/RA 5510-01409.May 10, 1998 · N819NY · Doug DC982SDR CALA9800778Access Panel · corrodedLT LOWER HORIZ STAB BAL BAY ACCESS PANEL CORRODED. CUT OUT CORRODED AND DELAMINATED AREA, FABRICATED DOUBLER AND BONDED TO CUT OUT AREA PER SRM 55-20-3 AND 51-40-5.May 5, 1998 · N69741 · Boeing 727224SDR SWAA980727Skin · dentedDURING SCHEDULED 1/4 D-CHECK, FOUND LT HORIZONTAL STAB LEADING EDGE FIX COWL HAS A BULGE AND IS DENTED. REPAIRED PER BOEING SRM.Apr 30, 1998 · N129SW · Boeing 7372K6SDR SWAA980704Skin · crackedDURING SCHEDULED SERVICE CHECK, FOUND CRACKED SKIN RT HORIZ STAB-FIXED L/E. REPAIRED PER BOEING SRM.Apr 27, 1998 · N658SW · Boeing 7373H4SDR P5CA9800878Skin · dentedLT STABILIZER ROOT UPPER SURFACE T/E FIXED PANEL HAS DENTS. FIBERGLASS REPAIRED PER SRM 51-40-15 AND MM 51-26-11.Apr 24, 1998 · N851FT · Boeing 747122SDR ARWA980497Skin · damagedDURING D-CHECK, FOUND LEFT HAND HORIZONTAL STABILIZER OUTBOARD LEADING EDGE HAS TEMPORARY REPAIR. REMOVED EXISTING REPAIR. FABRICATED AND INSTALLED NEW REPAIR DOUBLER IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, SRM 55-2-1. WORK ACCOMPLISHED UNDER ARROW AIRApr 24, 1998 · N791AL · Doug DC862SDR ARWA980496Skin · damagedDURING D-CHECK, FOUND LEFT HAND HORIZONTAL STABILIZER INBOARD LEADING EDGE HAS TEMPORARY REPAIR. REMOVED EXISTING REPAIR. FABRICATED AND INSTALLED REPAIR DOUBLER IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY SRM 55-2-1. WORK ACCOMPLISHED UNDER ARROW AIR FORM Apr 24, 1998 · N791AL · Doug DC862SDR ARWA980495Skin · crackedDURING D-CHECK, FOUND LEFT HAND HORIZONTAL STABILIZER INBOARD LEADING EDGE HAS A CRACK ON SKIN. STOP DRILLED CRACK. FABRICATED REPAIR DOUBLER AND INSTALLED IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, SRM 55-2-1, WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WApr 24, 1998 · N791AL · Doug DC862SDR ARWA980494Skin · corrodedDURING D-CHECK, FOUND RIGHT HAND HORIZONTAL STABILIZER, INBOARD LEADING EDGE HAS CORROSION. REMOVED CORROSION. FABRICATED REPAIR DOUBLER AND INSTALLED IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, SRM 55-2-1 AND 51-1-20. WORK ACCOMPLISHED UNDER ARROW AIR JW3Apr 24, 1998 · N791AL · Doug DC862SDR MWEA98488Plate · corrodedHORIZONTAL STABILIZE STRESSED PLATE SHOWS EVIDENCE OF CORROSION AND CHAFING. REMOVED OLD PLATE AND INSTALLED FABRICATED REPLACEMENT.Apr 20, 1998 · N212ME · Doug DC932SDR DL72W980971Panel · damagedHORIZONTAL STABILIZER T/E LT SIDE HAS HOLE PUNCHED IN THE UPPER PANEL APPROX 10 INCHES INBD OF ELEVATOR POWERPACK CUTOUT. REMOVED DAMAGE WITH .375 DIA HOLE. DYE CHECKED, NO CRACKS FOUND. MANUFACTURED REPAIR PER SRM 55-10-3 FIG 3. INSTALLED REPAIR PER SRM 5Apr 15, 1998 · N2811W · Boeing 727247SDR CA980602076Skin · cracked(CAN) TWO CRACKS NOTED ON THE HORIZONTAL STABILIZER LOWER SKIN AT THE OUTBOARD HINGE. THE HINGE BRACKET WAS FOUND LOOSE. TWO RIVETS THAT SECURE THE HINGE TO THE REAR SPAR WERE LOOSE AND HOLES IN THE SPAR ELONGATED. THE HORIZONTAL STABILIZER END RIB WAS ALSO CApr 13, 1998 · Dhav DHC3SDR MWEA98396Skin · crackedFOUND CRACK IN LEFT HAND HORIZONTAL STABILIZER UPPER AFT SKIN PANEL AT STATION XH8. MTC REMOVED AND REPLACED SKIN PANEL.Apr 4, 1998 · N600ME · Doug DC914SDR UPS98826426Skin · corrodedINSPECTION TYPE-D, LT HORZ STAB INBD L/E HAS FILLIFORM CORROSION OUTBD END L/E XFS 197.5. REPAIRED IAW SRM 55-2-1.Mar 29, 1998 · N803UP · Doug DC873FSDR ABXA9800260Skin · corrodedDURING C-CHECK, FOUND CORROSION ON LEFT HORIZONTAL STABILIZER UPPER SKIN FROM STATION XHS 32 - XHS 140. REPAIRED IAW ABX REA D955-2067.Mar 26, 1998 · N957AX · Doug DC941SDR 98ZZZX2503Skin · misdrilledDURING C-CHECK INSPECTION DISCOVERED OVERSIZED FASTENER HOLE IN THE HORIZONTAL STABILIZER UPPER AFT SKIN PANELS/STRINGERS (PN 5922578-501) REFERENCED IN DAC SB 55-42R1 AND AD 96-10-11. REPAIRED BY OVERSIZING HOLE, SPLIT-SLEEVE COINING THE OVERSIZED HOLE, FABRMar 24, 1998 · N679HA · Doug DC951SDR CA971216028Plate · cracked(CAN) TRAILING EDGE OF HORIZONTAL STABILIZER BEAM ASSY CRACKED ON FORWARD EDGE OF THE COVER PLATE ALONG THE RADIUS IN 4 LOCATIONS. THE LONGEST CRACK WAS APPROX 2 INCHES LONG. BEAM LENGTH IS 12 FEET. THE RADIUS SHOULD BE .25 INCH RADII AND WAS ONLY.10 INCH RMar 17, 1998 · Boeing 737242CSDR AU980315Stabilizer · fod(AUS) LT HORIZONTAL STABILIZER LEADING EDGE FOD. DAMAGE LOCATED INBOARD OF STN 78.5.Mar 8, 1998 · Piper PA31
Back to JASC 5512