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 TAMF20060012SSkin · erodedDURING C-CHECK INSPECTION WAS FOUND A EROSION ON NOSE SKIN AT HORIZONTAL STABILIZER TIP - LT. DAMAGE WAS REPAIRED IAW EWO 767 55-001 AND BOEING SERVICE REQUEST ID: 1-171213467. ERODED AREA WAS CLEANED UP IAW SRM 55-10-30 PAGE 1 TO 3, THICKNESS MEASUREMENT PEMar 9, 2006 · N767QT · Boeing 767200SDR TAMF20060002SPanel · delaminatedDURING INSPECTION CHECK WAS FOUND A DELAMINATION ON LT HORIZONTAL STABILIZER UPPER OB ALUMINUM HONEYCOMB SKIN PANEL, BETWEEN LE STA 250.251 - FSS 305.361. SKIN PANEL WAS REMOVED IAW SRM 51-40-02 PAGE 1, SENT TO FAA RS UL6R925Y, REPAIRED IAW B767 SRM 51-70-10 Mar 6, 2006 · N767QT · Boeing 767200SDR UPS06M46962Panel · corrodedHORIZ STAB POSITION NR R20 BARREL NUT BORE SIDEWALL AND BOTTOM FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 38, BORE REAMED TO 1.067" OD REMAIN ING BLEND OUT AT SIDEWALL SURFACE 0.020" DEEP EXCEED LIMIT IAW EO MD11- 5510-19409K. MAGNIFY 10X DMar 5, 2006 · N284UP · Doug MD11FSDR USAA060355Skin · crackedRIGHT STABILIZER, LOWER SKIN AT REAR SPAR, BETWEEN STATIONS 120.30 AND 129 CRACKED. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER IAW SRM 55-10-01 REPAIR 4, DEFECT SIZE: 3 INCH.Feb 24, 2006 · N439US · Boeing 7374B7SDR 06FDEA0823Skin · crackedDURING U/S INSPECTION OF HORIZONTAL STAB FOUND CRACK ON INTERIOR SKIN PANEL UPPER SURFACE. REMOVED AND REPLACED PANEL.Feb 24, 2006 · N563FE · Doug DC1010SDR MALA060091Panel · damagedDURING 2Y CHECK IN BNA, FOUND PANEL NR 324AR HAS AN ELONGATED SCREW HOLE THAT HAS BEEN REPAIRED IAW MESABA EO NR S55060. REF:EAMS WORK ORDER 213545 TASK 3504.Feb 21, 2006 · N415XJ · Saab 340BSDR 06FDEA0705Skin · unknownLEFT HAND HORIZONTAL STABILIZER, BARREL NUT AFT SKIN PLANK REPLACEMENT - TO COMPLY WITH FEDEX EA 1-5510-94597, SR11550010-77 STRINGER PANEL ASSY. COMPLIED WITH FEDEX EA 1-5510-94597.Feb 16, 2006 · N585FE · Doug MD11SDR 06FDEA0704Skin · unknownRIGHT HAND HORIZONTAL STABILIZER, BARREL NUT AFT SKIN PLANK REPLACEMENT - TO COMPLY WITH FEDEX EA 1-5510-94598 SR11550010-78 STRINGER PANEL ASSY. COMPLIED WITH FEDEX EA 1-5510-94598.Feb 16, 2006 · N585FE · Doug MD11SDR 2006UALA00278Skin · crackedLEFT HORIZONTAL STAB LWR SURFACE CRACKED, AFT SIDE JUST FWD OF ELEV STA 98. LT HORIZONTAL STAB LOWER SURFACE FOUND CRACKED. NEW SKIN SECTION WAS SPLICED IN BETWEEN STATIONS 105.7 AND 180. REFERENCE AAR EO 1060094 AND APPROVED WITH AN 8100-9 FORM.Feb 13, 2006 · N338UA · Boeing 737322SDR 2006UALA00260Skin · dentedRIGHT HORIZONTAL STABILZER HAS DENT APPROX 4 FT OUTBOARD ON LEADING EDGE. DENT MEASURES 2"L X 1.25W X .125D. RIGHT HORIZONTAL STABILIZER LEADING EDGE SKIN REPLACED TO ADDRESS DENT.Feb 9, 2006 · N338UA · Boeing 737322SDR SWAA060494Skin · crackedDURING SCHEDULED C4 CHECK, FOUND RH HORIZONTAL STAB LOWER SKIN CRACKED AT STAB STA 120.30. REPAIRED HORIZONTAL STAB SKIN PER SRM.Feb 8, 2006 · N356SW · Boeing 7373H4SDR 06FDEA0576Repair · unknownFOUND PREVIOUS REPAIR INSTALLED ON RT HORIZONTAL STAB LOWER I/B SURFACE WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 55-10-3 FIG 3. BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBEFeb 7, 2006 · N487FE · Boeing 727200SDR 06FDEA0575Repair · unknownFOUND PREVIOUS REPAIR INSTALLED AT RT HORIZONTAL STAB LOWER SURFACE WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 55-10-3 FIG 1. BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBERS, Feb 7, 2006 · N487FE · Boeing 727200SDR ASAA0640103Skin · gougedFOUND FUSELAGE SKIN PANEL IS CHAFED AND GOUGED JUST BELOW THE LT HORIZ STAB. BLENDED DAMAGED AREA OF SKIN, PERFORMED HFEC INSPECTION OF BLEND AREA TO ENSURE NO OTHER DEFECTS EXIST. FABRICATED AND INSTALLED AN EXTERNAL REPAIR DOUBLER IAW ASA EA 5380-01016 ANDFeb 1, 2006 · N765AS · Boeing 7374Q8SDR SWAA060382Skin · crackedDURING SCHEDULED C1 CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN CRACKED AT INBD AFT SPAR BETWEEN STAB STA 96 TO STAB STA 115. REPAIRED SKIN PER SRM.Jan 31, 2006 · N368SW · Boeing 7373H4SDR SWAA060350Skin · crackedDURING SCHEDULED C4 CHECK, FOUND RH HORIZONTAL STAB LOWER SKIN CRACKED AT AFT SPAR ATTACH POINT. REPAIRED HORIZONTAL STAB PER SRM.Jan 29, 2006 · N663SW · Boeing 7373Q8SDR SIMA200603706Skin · damagedLT HORIZONTAL TOP SKIN ON AIRCRAFT WAS FOUND TO HAVE HAIL DAMAGE. REMOVED THE DAMAGED TOP SKIN. POSITIONED THE NEW SKIN PANEL, INSTALLED. REPAIR DONE IAW SRM. (K)Jan 27, 2006 · N297AE · Saab 340BSDR SIMA200603707Skin · damagedHAIL DAMAGE TO THE RT HORIZONTAL STABILIZER TOP SKIN PANEL. REMOVED EXISTING RT STABILIZER TOP SKIN PANEL AND CLEANED THE AREA. INSTALLED NEW TOP SKIN. REPAIR DONE IAW REPAIR STATEMENT. (K)Jan 25, 2006 · N297AE · Saab 340BSDR 2006FA0000146Skin · bentDURING INSP OF HORIZ STAB, FWD SPAR AND CTR SECTION SKIN WAS FOUND BENT, DISTORTED AT CENTER LIGHTENING HOLE. SKIN AND SPAR BOTH SHOWED SIGNS OF WRINKLING AND DEFORMATION. CLOSE INSP OF PARTS DID NOT SHOW ANY CRACKS. SPAR HAD BEEN REINFORCED WITH SPAR REINFJan 19, 2006 · N7368Y · Piper PA30SDR 06FDEA0276Panel · crackedPANEL 9220 IS CRACKED. *S/D* REPLACED PANEL PER FED EX EA 7-5510-96548.Jan 19, 2006 · N490FE · Boeing 727200SDR SWAA060203Skin · crackedDURING SCHEDULED C2 CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN CRACKED AT INBOAD AFT SPAR. REPAIRED HORIZONTAL STAB SKIN PER SRM.Jan 16, 2006 · N624SW · Boeing 7373H4SDR 06FDEA0213Skin · gougedLT HORIZONTAL STABILIZER UPPER T/E PANEL BEADED SKIN IS GOUGED AT ELEVATOR BALANCE PANEL BAY 5.Jan 16, 2006 · N490FE · Boeing 727200SDR UPS06846110Skin · damagedINSPECTION TYPE:C1 LT UPPER AFT I/B SURFACE OF HORIZONTAL STAB HAS 3 CREASES. REMOVED, FABRICATED AND INSTALLED HORIZONTAL STAB SKIN PANELS 2 IAW DWG 5651747, SRM 51-1-21.Jan 4, 2006 · N852UP · Doug DC873FSDR SWAA060053Skin · crackedDURING SCHEDULED C4 CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN CRACKED AT OUTBOARD AFT SPAR. REPAIRED HORIZONTAL STAB PER SRM.Jan 3, 2006 · N320SW · Boeing 7373H4SDR VNAA0601002Skin · lightning strikeTHE CREW REPORTED A POSSIBLE LIGHTNING STRIKE IN FLIGHT. MAINTENANCE PERFORMED A DETAILED LIGHTNING STRIKE INSPECTION. DAMAGE WAS FOUND ON THE RT HORIZONTAL STABILIZER AFT TIP AND ON TOP OF THE FUSELAGE NOSE SECTION FORWARD OF THE COCKPIT. ALL DAMAGE WAS REJan 2, 2006 · N723PS · Cndair CL6002C10SDR USAA051645Skin · damagedFOUND SKIN DAMAGE RT HORIZ STAB LEADING EDGE FASTENER HOLE 3 FT FROM I/B EDGE. REMOVED DAMAGED SKIN, INSTALLED FILLER AND DOUBLER PER EA 97189 DEFECT SIZE: 1/4".Dec 29, 2005 · N781AU · Boeing 7374B7SDR UPS06446007Skin · crackedINSPECTION TYPE:C REF DMI# D305601 - INTERIM REPAIR TO FUSELAGE SKIN PUNCTURE AT FS 2565 (CRACK LENGTH 13"). SKIN AT BS 2553 - 2575 BETWEEN S46R AND S49R PERMANENT REPAIRED AS PER EO# B747-5330-22469-B APPENDIX B AND ZERO, TIME ALL FASTENER HOLES CARRIED OUT Dec 28, 2005 · N520UP · Boeing 747212BSDR SIMA200600303Skin · damagedHAIL DAMAGE ON THE RT HORIZONTAL STABILIZER TOP SKIN PANEL. REMOVED THE EXISTING SKIN PANEL AND MARKED AND DRILLED FASTENER HOLES. REPOSITIONED AND INSTALLED SKIN. REPAIR DONE IAW SRM. (K)Dec 23, 2005 · N317AE · Saab 340BSDR SIMA200600302Skin · damagedHAIL DAMAGE ON THE LT HORIZONTAL STABILIZER TOPSKIN. REMOVED THE EXISTING LT HORIZONTAL STAB TOP SKIN PANEL. POSITIONED NEW LT HORIZONTAL STABILIZER SKIN. MARKED AND DRILLED FASTENER HOLES. REPOSITIONED AND INSTALLED SKIN. REPAIR DONE IAW SRM. (K)Dec 23, 2005 · N317AE · Saab 340BSDR 05FDEA04056Repair · unknownREPAIR ASSESSMENT. HORIZONTAL STAB LE PANEL 331AB. EXISTING REPAIR BETWEEN RIB 2 - 3 LOWER SURFACE. EXISTING REPAIR NOT IAW A310-200 SRM 55-12-12. REMOVED 2 REPAIR ANGLES IAW A310-200 SRM51-40-21. FABRICATED AND INSTALLED NEW ANGLES IAW A310-200 SRM 55-12Dec 1, 2005 · N423FE · Airbus A310203SDR ASAA0540694Skin · dentedOKC - FOUND DENT IN LEFT HORIZONTAL L/E 10 INCH FROM OUTBOARD END. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND PLATE IAW B737-400 SRM 55-10-01, FIGURE 201, REPAIR 2. (M)Nov 21, 2005 · N796AS · Boeing 737490SDR ASAA0540693Skin · dentedOKC - FOUND RIGHT HORIZONTAL STAB HAS 2 EACH DENTS 4 FEET OUTBOARD FROM ROOT ON L/E. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND PLATE IAW B737-400 SRM 55-10-01, FIG 201, REPAIR REPAIR 2. (M)Nov 21, 2005 · N796AS · Boeing 737490SDR 05FDEA03830Repair · corrodedPT1 HORIZONTAL STABILIZER RT NR 25 BORE FOUND WITH EXISTING BUSHING REPAIR WITH CORROSION. CORROSION AND EXISTING REPAIR BUSHING ON HORIZONTAL STABILIZER RT NR 25 BORE REMOVED BY REAMING BORE TO 1.067 DIAMETER AND FOUND WITHIN LIMIT AS PER FEDEX EO 1-5510-7-5Nov 15, 2005 · N524FE · Doug MD11SDR DL76K050709Skin · gougedRT HORIZONTAL STABILIZER / UPPER SKIN AT RIB 12, S-5 / REPAIR OF GROUND DAMAGE. GOUGE DUE TO GROUND DAMAGE WAS CUT OUT OF THE RT HORIZONTAL STABILIZER UPPER SKIN AT RIB 12 AND S-5. AN ALUMINUM EXTERNAL DOUBLER IS INSTALLED WITH HI-LOKS TO REPAIR THE DAMAGE.Nov 13, 2005 · N173DZ · Boeing 767332SDR VNAA0511004Skin · lightning strikeAFTER LANDING THE CREW REPORTED A POSSIBLE LIGHTNING STRIKE ON THE NOSE OF THE AIRCRAFT. MAINTENANCE PERFORMED AN EN ROUTE LIGHTNING STRIKE INSPECTION AND FOUND EVIDENCE OF LIGHTNING DAMAGE ON THE RT HORIZONTAL STABILIZER TIP FAIRING. THE AIRCRAFT WAS FERRIENov 6, 2005 · N257PS · Cndair CL6002B19SDR SWAA053389Skin · delaminatedDURING SCHEDULED D CHECK, FOUND RT HORIZONTAL STAB OTBD T/E UPPER SKIN DELAMINATED. REPAIRED STAB PER SRM.Oct 28, 2005 · N318SW · Boeing 7373H4SDR UPS05845709Rib · crackedFOUND LT HORIZONTAL STAB IB L/E STA XFS 47.5 RIB HAS 1/2" CRACK ON LOWER FLANGE ANGLE. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 55-2- 0 FIG 2 AND 3.Oct 26, 2005 · N813UP · Doug DC873FSDR UPS05845788Skin · corrodedINSPECTION TYPE:C1 INTERGRANULAR CORROSION ON LT HORIZ STAB L/E UPPER SKIN AT SEGMENT JOINT. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER AND 2 EA. FILLERS IAW SRM 55-02-01 FIG 004.Oct 20, 2005 · N813UP · Doug DC873FSDR IXXA05SMN239SSkin · dentedDURING ROUTINE C CHECK INSPECTION, LT HORIZONTAL STABILIZER L/E UPPER SKIN DENTED, XFS 78.750 XFS 85.00. PERFORMED MAJOR REPAIR IAW DC8 SRM 55-2-1 FIG 4, EO SEMAN # 20051292 DATED 09-27-05. REMOVED EXISTING REPAIR DOUBLER NEXT DENT IAW DC8 SRM 51-1-21. REMOOct 13, 2005 · N829BX · Doug DC871FSDR SWAA053118Skin · crackedDURING SCHEDULED C2 CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN CRACKED AT INBD AFT SPAR, STAB STA 110. REPAIRED HORIZONTAL STAB PER SRM.Oct 9, 2005 · N620SW · Boeing 7373H4SDR 05FDEA03230Skin · crackedLT HORIZ STAB LEADING EDGE INBOARD FOUND CRACK 2 INCH LONG ON OUTBOARD EDGE LWR SIDE. STOPPED DRILL CRACK AND INSTALLED REPAIR ANGLE IAW SRM 55-00-01 FIG 2 VOL III.Oct 5, 2005 · N556FE · Doug DC1010SDR 05FDEA03115Panel · crackedLT IB HORIZONTAL STAB L/E HAS MULTIPLE CRACKS WHERE RIBS ATTACH TO SKIN.Sep 26, 2005 · N425FE · Airbus A310203SDR 05FDEA03040Panel · gougedRT HORIZONTAL STABILIZER UPPER T/E PANEL INNER SIDE IS GOUGED JUST 3 INCHES I/B OF NR 7 RIB. REPAIRED PER E.A. 7-5510-91362.Sep 21, 2005 · N483FE · Boeing 727227SDR UPS05845461Skin · corrodedLT HORIZONTAL LE HAS INTERGRANULAR CORROSION AROUND FASTENER HOLES ON LOWER SURFACE AT IB END OF OB SECTION. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 55-2-1 FIG 4.Sep 15, 2005 · N801UP · Doug DC873FSDR IXXA05RNG078SSkin · corrodedDURING INSPECTION CHECK, FOUND CORROSION ON RT HORIZONTAL STABILIZER UPPER PLATING AT OUTBOARD CENTER SECTION AROUND STA XE 173.656 BETWEEN AUXILIARY AND AFT UPPER SPAR CAP. CORRODED AREA WAS BLEND OUT AND REPAIR DOUBLER WAS INSTALLED IAW EO ATI 091505 AND EWSep 10, 2005 · N721CX · Doug DC872SDR IXXA05RNG077SPlate · corrodedDURING INSPECTION CHECK,CORROSION WAS FOUND ON STABILIZER UPPER TRAILING EDGE PLATING STA XE 28-RH. REPAIR ACCOMPLISHED, REMOVAL PANEL AND STIFFENER, FABRICATION AND INSTALLATION NEW PANEL AND STIFFENER IAW DRAWINGS 55-05467-1, 55-05467-2, 55-05467-3, 55-05467Sep 9, 2005 · N721CX · Doug DC872SDR IXXA05RNG066SDoubler · improperDURING INSPECTION CHECK, FOUND IMPROPER REPAIR ON RT HORIZONTAL STABILIZER L/E DOUBLER STA XFS 210-222.500. EXISTING DOUBLER WAS REMOVED AND A NEW REINFORCEMENT DOUBLER WAS INSTALLED IAW EO ATI 090805 AND EWO ATI-55-006.Sep 9, 2005 · N721CX · Doug DC872SDR IXXA05RNG070SSkin · corrodedDURING INSPECTION CHECK, FOUND CORROSION ON LH HORIZONTAL STABILIZER LOWER SURFACE SKIN, STATION XE 235. BLEND OUT IN CORRODED AREA WAS PERFORMED AND REPAIR DOUBLER WAS INSTALLED IAW EO ATI-091305 AND EWO ATI 55-007. FAA FORM 8110-3 WAS ISSUED APPROVING THISSep 7, 2005 · N721CX · Doug DC872SDR UPS05845613Skin · corrodedINSPECTION TYPE:C3 EXFOLIATING CORROSION AROUND FASTENER HOLE ON THE LT HORIZONTAL L/E AS MARKED ON TOP SURFACE. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW SAA SK 801-804772 .Aug 30, 2005 · N801UP · Doug DC873FSDR USAA051048Skin · crackedRIGHT STABILIZER LOWER SKIN, ELEV STA 106 (JUST FWD OF PNL 9208R) CRACKED. INSTALLED FILLER AND DOUBLER IAW TYPICAL REPAIR 55-10-07 REV-B, DEFECT SIZE: 1.25 INCHAug 23, 2005 · N420US · Boeing 737401
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