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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR CALA9900827Panel · delaminatedINSPECTION FOUND LT HORIZONTAL STABILIZER THIRD T/E PANEL FROM FUSELAGE GOING OUTBOARD ON LOWER SURFACE DELAMINATED. THE PANEL WAS REMOVED, REPAIRED AND REINSTALLED IAW SRM 51-31-01AND WO 99-0653.SDR CALA9900826Panel · delaminatedINSPECTION FOUND RT UPPER HORIZONTAL STABILIZER 4TH T/E UPPER AFT PANEL FROM FUSELAGE DELAMINATED. THE PANEL WAS REMOVED, REPAIRED AND REINSTALLED IAW SRM 51-31-01 AND WO 99-0648.SDR CALA9900825Panel · delaminatedINSPECTION FOUND LT HORIZONTAL STABILIZER 4TH T/E PANEL FROM FUSELAGE GOING O/B DELAMINATED. THE PANEL WAS REMOVED, REPAIRED AND REINSTALLED IAW SRM 51-31-01 AND WO 99-0651 AND TRAVELER 105996.SDR UPS99830148Skin · corrodedINSPECTION TYPE:C2, RT HORZ STAB O/B LEADING EDGE, I/B END, HAS CORROSION AROUND SCREW HOLES. FABBED AND INSTALLED REPAIR FILLED AND DOUBLER IAW DC8 SRM 51-1-21, 51-2 -0, & REO 06610.SDR P5CA9900667Skin · delaminatedLEFT HORIZONTAL STABILIZER LOWER SURFACE OF TRAILING EDGE NEAR OUTBOARD ELEVATOR FOUND DELAMINATION. REPAIRED PER SRM 51-40-09.SDR P5CA9900660Skin · delaminatedRIGHT HORIZONTAL STABILIZER NR 5 ACCESS PANEL HAS SEVERE AREAS OF DELAMINATION. REBONDED SKIN TO THE HONEYCOMB PER SRM 51-40-06.SDR P5CA9900659Skin · delaminatedLEFT HORIZONTAL STABILIZER NR 3 ACCESS PANEL 334JB DELAMINATED ON INNER SKIN. REBONDED SKIN TO HONEYCOMB PER SRM 51-10-06.SDR SWAA991153Skin · crackedDURING SCHEDULED D-CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN CRACKED IN AFT SPAR, FWD OF NR 1 BALANCE BAY. REPAIRED SKIN PER BFG ER NR 99-5642 AND SRM.SDR T64R387ARCover · puncturedARROW AIR - NR 2073, LEFT HORIZ STABILIZER T/E OUTBOARD DAMPER WELL HOLE PUNCHED THROUGH. REMOVED DAMPER WELL COVER IAW DC-8 SRM 51-1-21, WELDED HOLE PER EO 99-061 AND REINSTALLED IAW DC-8 SRM 51-1-21. (M)SDR DLL10991496Skin · crackedTHE UPPER SKIN OF THE LT HORIZONTAL STABILIZER WAS FOUND WITH A .75 INCH LONG CRACK AT FS 80 AT THE RUNOUT OF STRINGER 31. THE CRACK WAS ROUTED OUT OF THE SKIN WITH A 1.5 INCH DIA HOLE AND REPAIRED WITH AN ALUMINUM DOUBLER AND TRIPLER PER ER/A 367701-1SDR MWEA99375Skin · dentedSHARP DING IN LEFT HORIZONTAL STABILIZER LOWER SKIN. MTC REPAIRED WITH FASTENER.SDR AT9900482Skin · corrodedSCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND CORROSION ON THE RIGHT HORIZONTAL STABILIZER LEADING EDGE AT BS 73. REMOVED CORROSION, FABRICATED REPAIR DOUBLER, DRILLED, HEAT TREATED, PRIMED, AND INSTALLED DOUBLER IAW DC9 SRM 51-30-2, 51-30-5, AND 51-30-8.SDR USAA990618Skin · crackedCLT - DURING RON VISIT, FOUND 3 INCH CRACK AT HORIZONTAL STAB MAIN BOX SKIN. LOCATION IS LOWER SURFACE OF RIGHT HORIZ STAB, JUST FORWARD OF THE AFT SPAR ABOUT 5 FEET FROM FROM FUSELAGE. INSTALLED REPAIR DOUBLER PER SRM 55-10-07 REV A. (M)SDR DL72S991288Skin · dentedBULGE AT LT HORIZONTAL STABILIZER UPPER SKIN 6 IN FWD OF ELEVATOR 2ND FROM O/B HINGE(MARKED). INSTALLED DOUBLER PER SRM 55-20-3.SDR P5CA9900603Skin · dentedLEFT HAND HORIZONTAL STABILIZER LEADING EDGE IS DENTED IN 2 PLACES. DENTED AREAS REPAIRED IAW SRM 51-40-01.SDR GTIA9901014Panel · wornMHV - HORIZONTAL STABILIZER CENTER SECTION PANEL NR 3804A AFT AND LOWER SECTION WORN TO KNIFE EDGE. FABRICATED REPAIR DOUBLERS REF DC9 SRM 5503. HEATED TREATED AND AGE HARDENED PER AMS H 6088. ASSEMBLED AND ISSUED FOR INSTALLATION ON WO A092107022. (X)SDR GTIA9901007Skin · crackedMHV - HORIZONTAL STABILIZER CENTER SECTION UPPER RIGHT PANEL NR 3806A CRACKED AT AFT UPPER AREA ALSO WORN TO KNIFE EDGE. FABRICATED DOUBLER AND FILLER TO COVER DAMAGED PANEL, INSTALLED PER DC9 IAW SRM 55-03-0 PAGE 28 VIEW F ALODINE AND PRIMED PER DC9 IAW SRM SDR DLL14990998Skin · crackedTHE NR 4 UPPER SKIN PANEL OF THE RT HORIZONTAL STABILIZER WAS FOUND WITH A .05 CRACK AT THE RUNOUT OF AN INTEGRAL STIFFENER AT HSS 80. THE CRACK WAS ROUTED OUT OF THE PANEL AND AN ALUMINUM DOUBLER AND TRIPLER WERE INSTALLED PER ER/A 367318-14.SDR ABXA9900457Skin · crackedRIGHT HORIZONTAL STABILIZER OUTBOARD LEADING EDGE CRACKED AT INBOARD END. REPAIRED IAW DC8 SRM 51-1-11 AND 51-1-21A.SDR 2000ZZZX393Spar · crackedFRONT SPAR WAS REMOVED FROM HORIZONTAL STABILATOR RECAUSE OF CRACKS IN SPAR P/N 169-620001-59 AT THE UPPER RADIUS IN THE CUT-OUT SLOT FOR HINGE, P/N 169-620000-107, TO FIT. A NEW FACTORY SPAR WAS PURCHASED. INCOMING INSPECTION FOUND A .3750 INCH CRACK WAS FOSDR SWAA990692Skin · crackedDURING SCHEDULED D-CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED 1 INCH FWD OF REAR SPAR CENTER LINE AT STA 125 (CRACK IS APPROX 1 INCH LONG). REPAIRED SKIN PER ER 99-5225.SDR HEEA061781Skin · mismanufacturedSTABILIZER MISMANUFACTURED. COULD NOT INSTALL TAILBOOM SUPPORT PANELS DUE TO WHAT APPEARS TO BE A TWIST IN STABILIZER MANUFACTURE WITH ONE UPPER SIDE ATTACHED, OTHER SIDE BOLT HOLES APPROXIMATELY .50 INCH MISALIGNED ON ONE END.SDR 99T64R246ARSkin · misinstalledNR 1780, RT HORIZONTAL STABILIZER OUTBOARD L/E TOP OUTBOARD DOUBLER REMOVE/REPLACE AND INSTALL WITH CONICAL WASHERS. FABRICATED DOUBLERS IAW DC-8 SRM 51-1-4 ALODINED AND PRIMED IAW DC-8 SRM 51-1-8, AND INSTALLED IAW DC-8 SRM'S 55-2-1, 51-1-21, AND 51-1-4. RESDR UPS99829179Skin · corrodedINSPECTION TYPE-C1, RT HORIZ STAB L/E SKIN AT MID SPAN HAS HEAVY CORROSION UNDER THE SURFACE. REPAIRED AREA IAW SRM 55-2-1 FIG 4.SDR DHL9980714CSkin · crackedAT C-CHECK, LT HORIZ STAB L/E I/B SECTION I/B INTERIOR LOWER AREA AT APPROX STA FS 53.75 HAS CRACK DAMAGE ON SURFACE AT FASTENER HOLE POINT. STOP DRILLED CRACK, FABRICATED ANGLE REPAIR 6 X 1 X 1 AND 5 X 1 X 1 PER SRM 51-1-8.SDR CALA9900276Skin · gougedINSPECTION FOUND LT HORIZONTAL STABILIZER I/B LEADING EDGE AREA GOUGED. A DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-10-6 AND 51-30-2, PAGE 4.SDR CALA9900270Skin · dentedINSPECTION FOUND RT HORIZONTAL STABILIZER LEADING EDGE DENTED AT FS 207.093. REPAIRED IAW SRM 51-70-10, PARAGRAPH 2M, FIGURE 7.SDR CALA9900262Panel · puncturedINSPECTION FOUND RT HORIZONTAL STABILIZER PANEL NR 345DB PUNCTURED. THE PANEL WAS REMOVED, REPAIRED IAW SRM 51-70-05, PARAGRAPH 4C, AND REFITTED.SDR ABXA9900333Skin · corrodedRIGHT HORIZONTAL STABILIZER LEADING EDGE AT STATION XFS 147.5 HAD INTERGRANULAR CORROSION. REPAIRED IAW DC8 SRM 55-2-1.SDR DHL9980712CSkin · crackedAT C-CHECK, LT HORIZONTAL STAB L/E I/B SECTION O/B INTERIOR LOWER AREA AT APPROX FS 166 HAS CRACK DAMAGE. STOP DRILLED CRACK AND FABRICATED REPAIR DOUBLER PER SRM 55-2-0, 1 X 1 X 7 AND 10 X 1 X 6.SDR DHL9980705CPanel · crackedAT C-CHECK, LT HORIZ STAB REAR SPAR STA XE 270.9 CRACKED ON COVER PANEL. REMOVED AND FABRICATED NEW COVER AND INSTALLED PER SRM 52-3-0.SDR DHL9980760CSkin · corrodedAT C CHEK, LEFT HORIZONTAL STA L/E I/B LOWER AREA AT STA XFS 60 FOUND CORROSION UNDER SKIN SURFACE. CUT OUT DAMAGED SECTION, FABRICATED FILLER AND DOUBLER PER EO 18R5511080 AND INSTALLED PER SRM 51-1-8. N/R 426SDR DHL9980759CSkin · corrodedAT C CHECK, LEFT HORIZONTAL STAB L/E UPPER AREA AT STA XFS 172.5, FOUND CORROSION UNDER SKIN SURFACE. CUT OUT DAMAGED AREA FABRICATED FILLERS AND REPAIR DOUBLER PER EO 18R5511079. INSTALLED FILLER S AND DOUBLER PER EO FILLER 4 BY 2 AND 1 BY 1, DOUBLER 5.75 SDR 99T64R364ARPlate · corrodedLEFT HORIZ STAB LEADING EDGE CORROSION ALONG SCREW ROW TOP STATION XFS 166 TO 328. REMOVED CORROSION, FABRICATED FILLERS AND DOUBLERS AND INSTALLED PER EO 99-061 AND 99-025. (M)SDR SWAA990438Skin · crackedDURING SCHEDULED D-CHECK, FOUND HORIZONTAL STAB LOWER SURFACE SKIN CRACKED FWD OF REAR SPAR, (CRACK APPROX 2 LONG). REPAIRED STAB PER SWA ER NR 99-0169, AND SRM.SDR P5CA9900230Panel · delaminatedRIGHT LOWER TRAILING EDGE PANEL 334 IS BADLY DELAMINATED ON HORIZ STAB. REMOVED AND REPLACED PANEL PER SRM 51-30-02.SDR MWEA083Skin · damagedMKE - RIGHT HORIZONTAL STABILIZER HAS BLEND OUTS ON LEADING EDGE AT XFS 163.375 XFS 200.00 AND XFS 232.00 TO XH 209.125. MTC FABRICATED AND INSTALLED DOUBLER REPAIR. (X)SDR UPS99228654Skin · corrodedINSPECTION TYPE-C, CORROSION ON UPPER SKIN OF RT HORIZONTAL STABILIZER STAB STA 68. REMOVED CORROSION IAW SRM 51-10-6. REPAIRED AREA IAW SMRO EO 99-03-008 UPS ENGINEERING FILE NR 727-55-0383.SDR ABXA9900115Skin · corrodedLEFT HORIZONTAL STABILIZER LEADING EDGE, UPPER SURFACE HAD BULGING CORROSION ALONG AFT END FROM STATION XFS235 TO XFS320. REPAIRED IAW DC8 SRM 55-21.SDR HEEA060212Skin · dentedFIN ASSEMBLY HAS HOLE IN LEADING EDGE, DENTED, AND SEPARATED.SDR HEEA060211Skin · crackedFIN ASSEMBLY CRACKED AND SEPARATED.SDR HEEA060208Skin · corrodedSTABILIZER ASSEMBLY HAS CORROSION RT LEADING EDGE.SDR HEEA060207Skin · dentedSTABILIZER ASSEMBLY HAS EXCESSIVE DENTS.SDR HEEA060206Skin · corrodedSTABILIZER ASSEMBLY CORRODED BEYOND LIMITS ON LEFT EDGE.SDR HEEA060205Skin · corrodedSTABILIZER ASSEMBLY HAS CORROSION UNDER UPPER DOUBLER.SDR AT9900056Skin · misrepairedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND RIGHT HORIZONTAL STABILIZER STA 166 SKIN REPAIR HAS NO EDGE DISTANCE ON FILLER. REMOVED EXISTING REPAIR AND FABRICATED DOUBLERS, DRILLED, DEBURRED, TREATED, PRIMED AND INSTALLED REPAIR PARTS PER B737 SRM 51-30-2 ASDR SWAA990132Skin · dentedDURING SCHEDULED CHECK, FOUND LARGE DENT ON LT HORIZ STAB L/E APPROX 8 INCHES FROM WING ROOT. REPAIRED PER BOEING SRM.SDR AT9900105Skin · crackedSHEDULED INSPECTION AT AERO CORP, FL, FOUND RIGHT SIDE OF UPPER VERTICAL STABILIZER HAS CRACKED AND GOUGED SKIN AT STA 240 BELOW AFT BANANA FAIRING ATTACH POINTS. BLENDED RIGHT HAND VERTICAL STABILIZER. REMOVED AND FABRICATED NEW SKIN, TREATED, PRIMED, SEALESDR P2EA99014Skin · damagedSJO - RIGHT HORIZONTAL STAB STATION 88.5 LOWER SURFACE WITH A PROVISIONAL REPAIR. REPAIRED HORIZONTAL STAB LOWER SKIN SECTION BETWEEN STAB STATION 81.5 AND STAB STATION 95.5 PER 55-10-3 FIG 3. (M)SDR CALA9900047Skin · corrodedRIGHT HORIZONTAL STAB HAS BULGE IN UPPER SKIN AT AFT SPAR APPROX 12 INCHES FROM OUTBOARD END AT FIRST RIB FROM END. CUT OUT DAMAGE AND ACCOMPLISHED REPAIR PER 55-10-5 AND 12-30-8 MM.
Back to JASC 5512