JASC 5511
Service difficulty reports · 6,462
Reports filed under 5511 · Horizontal Stabilizer, Spar/Rib, 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 = '5511' 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 = '5511' 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 QXEA9800383Spar Web · crackedPDX - HORIZONTAL STAB SPAR WEB BETWEEN RIBS 3145 AND 3800 ON LEADING EDGE. INSTALLED NUT PLATES ON LEADING EDGE TOP AND BOTTOM BETWEEN RIBS 3145 AND 3800.SDR 98ZZZX1629Bracket · crackedCRACK FOUND DURING ROUTINE 100 HOUR INSPECTION. CRACK FOUND IN BRACKET ASSY THAT ATTACHES TO REAR SPAR OF HORIZONTAL STABILIZER WHICH ALSO HOUSES FITTING FOR ELEVATOR. SUBMITTER RECOMMENDATIONS: CLOSE INSPECTION OF AREA TO POSSIBLY INCLUDE DYE PENETRANT AFTSDR P5CA9800417Spar · corrosionLEVEL 1 CORROSION, FOUND INSIDE HORIZONTAL STAB REAR SPAR UPPER CHORD AND SKIN AREA AT RBL 43.5. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-10-02. BLEND OUT PER SRM LIMIT 55-10-01.SDR 98FDEA00107Spar · crackedLT HORIZONTAL STABILIZER UPPER REAR SPAR CAP FWD BARREL NUT HOLE HAS A 1 INCH LONG CRACK INDICATION ON THE FWD EXPOSED FACE. THE CRACK IS ONE INCH DOWN AND MARKED. REF WORK CARD 8551073310BPC SEQ 269. *S/D* REPLACED SECTION OF REAR UPPER SPAR CAP PER EA 8-SDR DL757980355Spar Web · wrinkledTHE AUX SPAR WEB OF THE RT HORIZ STAB WAS FOUND WRINKLED FROM AUX SPAR STA 220 TO 285. REPAIRED AND REWORKED PER ERA 331336-14.SDR MASA98044Spar · crackedDURING NIGHT MAINTENANCE, FOUND THE HORIZONTAL STABILON SPAR CRACKED AROUND THE DEICE HOSE. MAINTENANCE REPAIRED THE CRACKED WEBBING IN THE HORIZONTAL STABILIZER MAIN SPAR CENTER WEB IAW RO NR B1900D-55-0001. ACFT TT: 11,800 HOURS. ACFT TC: 18,212. (X)SDR UPS98425715Rear Spar · corrodedINSPECTION TYPE:C, RT STABILIZER REAR SPAR LWR CHORD CORRODED AT STA 473-476. SECTION SPLICED AT LWR CHORD IAW 55-10-05.SDR SWAA980135Support · damagedDURING SCHEDULED D-CHECK, FOUND RT STAB RIB AT STAB STA 129.5 HAD GOUGED L-ANGLE SUPPORT. REMOVED AND REPLACED RIB PER BOEING SRM.SDR AU980392Structure · misinstalled(AUS) HORIZONTAL STABILIZER SPAR CAP CRACKED IN AREA OF THE LOWER REAR MOUNT BOLT HOLES. CRACK LENGTHS 12.7MM (0.5 INCH). INVESTIGATION FOUND NEW PN 1232624-1 REINFORCEMENTS (SE 84-17) HAD BEEN FITTED IN AMERICA (29JUL84), BUT HAD BEEN INSTALLED UPSIDE DOWN SDR ABXA9800107Rib · crackedRIGHT HORIZONTAL STABILIZER LEADING EDGE RIB LWR ARM CRACKED AT STA XFS 141.250. REPAIRED IAW DC8 SRM 55-31.SDR 98ZZZX1636Spar · crackedCRACKS HAVE BEEN FOUND ON THE REAR STABILIZER SPAR. SUSPECT CRACKS ARE CAUSED BY IMPROPER USE OF A RIVET SQUEEZER DURING FACTORY INSTALLATION. SUBMITTER STATED THESE CRACKS AND TOOLING MARKS HAVE BEEN FOUND ON 4 OTHER ASSEMBLIES. CRACKS RANGE IN SIZE FROM .SDR DL73K980221Spar Chord · corrodedCORROSION FOUND ON THE UPPER SURFACE OF THE AFT FLANGE OF THE HORIZ STAB REAR SPAR UPPER CHORD. REPAIRED PER ERA 331272-14.SDR USAA980029Spar Lug · corrodedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .125 INCH BY 1 INCH CORRODED AREA CENTER SECTION FRONT SPAR CLEVEIS LUG BORE LEFT HORIZONTAL LOWER STABILIZER. INSTALLED OVERSIZED BUSHINGS, REPAIRED PER EA 43494. (M)SDR USAA980028Spar Lug · corrodedINT - DUIRNG Q-6 CHECK VISUAL INSPECTION, FOUND .125 INCH BY 1 INCH CORRODED AREA CENTER SECTION FRONT SPAR CLEVIS LUG BORE RT LOWER HORIZONTAL STABILIZER. INSTALLED OVERSIZED BUSHINGS, REPAIRED PER EA 43494. (M)SDR USAA980024Spar · corrodedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY .125 INCH CORRODED AREA RT HORIZONTAL STABILIZER UPPER OUTBOARD REAR SPAR TERMINAL LUG. INSTALLED OVERSIZED BUSHING, REPAIRED PER EA 43472. (M)SDR USAA980020Spar · corrodedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .125 INCH BY 1 INCH CORRODED AREA CENTER SECTION FRONT SPAR CLEVIS LUG BORE RT HORIZONTAL UPPER STABILIZER. INSTALLED OVERSIZED BUSHING, REPAIRED PER 43494. (M)SDR USAA980019Spar · corrodedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .125 INCH BY 1 INCH CORRODED AREA CENTER SECTION SPAR CLEVIS LUG LEFT UPPER HORIZONTAL STABILIZER. INSTALLED OVERSIZED BUSHING, REPAIRED PER EA 43494. (M)SDR P5CA9800188Frame · crackedCRACKED INTERNAL FRAMES AND ATTACH PLATES (6) AT PANEL 341CL ON LEFT HORIZONTAL STABILIZER. REPAIRED FRAMES AND PLATES PER BAC SRM 55-10-06.SDR P5CA9800187Frame · crackedCRACKED INTERNAL FRAMES (2) AT PANEL 341BR ON RIGHT HORIZONTAL STABILIZER. REPAIRED FRAMES PER BAC SRM 55-10-06.SDR SWAA980051Rib · crackedDURING SCHEDULED D CHECK, LT HORZ STAB L/E PANEL CRACKED RIB AT STA 105.26. REPLACED DAMAGED SECTION AND INSTALLED REPAIR DOUBLER PER BOEING SRM.SDR UPS98825534Spar Cap · crackedINSPECTION TYPE-D, LT HORIZ STAB ATTACH ANGLE INSIDE AUX SPAR AREA CRACKED. REMOVED AND REPLACED ANGLE IAW SRM 51-1-20 AND 51-1-21.SDR CALA9701678Spar Cap · crackedINSPECTION FOUND A 2 INCH CRACK AT OUTBOARD END OF RT HORIZONTAL STABILIZER LOWER SPAR CAP. THE OUTBOARD FITTING AND BULKHEAD WERE REMOVED IAW SRM 51-30-1. THE CRACKED SECTION OF SPAR WAS CUT OUT IAW SRM 55-02, FIGURE 8. A REPLACEMENT SPAR SECTION AND REPAISDR CALA9701660Spar Cap · crackedINSPECTION FOUND A 2 INCH CRACK AT OUTBOARD END OF LT HORIZONTAL STABILIZER LOWER SPAR CAP. THE OUTBOARD FITTING AND BULKHEAD WERE REMOVED IAW SRM 51-30-1. THE CRACKED SECTION OF SPAR CAP WAS CUT OUT IAW SRM 55-02, FIGURE 8. A REPLACEMENT SECTION OF SPAR CASDR CALA9701659Spar Cap · crackedINSPECTION FOUND A 2 INCH CRACK AT OUTBOARD END OF RT HORIZONTAL STABILIZER UPPER SPAR CAP. THE OUTBOARD FITTING AND BULKHEAD WERE REMOVED IAW SRM 51-30-1. THE CRACKED SPAR SECTION WAS CUT OUT IAW SRM 55-02, FIGURE 8. A REPLACEMENT SPAR SECTION AND REPAIR ASDR 97FDEA00842Spar · crackedAFT FACE OF HORIZONTAL STAB CENTER SECTION UPPER SPAR LT SIDE CRACKED.SDR AALA972154Spar Chord · corrodedTUL - RIGHT FORWARD SPAR CHORD ANGLE HAS CORROSION FROM FUSELAGE 2073-2088, SECTION OF CHORD PREVIOUSLY GROUND AWAY APPROX 1.187 BY 2.5O. INSTALLED DOUBLER REPAIR PER ESO 11697, DATED 10/27/97. (M)SDR AWXA9700667Spar · chafedDURING SCHEDULED C-9 INSPECTION, FOUND LT HORIZONTAL STABILIZER BALANCE BAY NR 3 BALANCE PANEL IDLER HINGE CHAFING ON HORIZONTAL STABILIZER REAR SPAR LOWER O/B SIDE. REPAIRED PER ER 3-55-11-06.SDR HAIHQEA0019Rib · brokenRIB IS BROKEN. THE LEAD TIP WT BOLTED TO THE OUTB RIB (APPROX. 4 LBS.), WAS FOUND RATTLING AROUND IN THE LT HORIZ STAB TIP CAP. FURTHER INVEST REVEALED THAT THE TIP WT, SECURED TO THE OUTB RIB WITH BOLTS AND ALUM RIVNUTS, PULLED THE RIVNUTS OUT OF THE RIB ELSDR 97ZZZX4800Rib · crackedINSPECTION FOUND FAR RIGHT RIB IN HORIZONTAL STABILIZER CRACKED. LOWER CRACK FOUND TO BE 1 INCH, WHILE TOP, .75 INCH. THESE CRACKS ARE OVER AND BELOW THE ELEVATOR HINGE ATTACH POINT. IF NOT FOUND, COULD, IN TIME, CAUSE SEPARATION OF ELEVATOR FROM STABILIZER.SDR AALA971993Spar Cap · corrodedTUL - HEAVY CORROSION ON UPPER T/E SPAR CAP AT OUTBOARD END OF RIGHT HORIZ STAB. REMOVED CORROSION AND INSTALLED DOUBLER PER ESO 11697, DATED 10-9-97. (M)SDR 97ZZZX4829Rib · brokenRIB IS BROKEN. THE LEAD TIP WEIGHT THAT IS BOLTED TO THE OUTBOARD RIB (APPROXIMATELY 4 POUNDS), WAS FOUND RATTLING AROUND IN THE LEFT HORIZONTAL STABILIZER TIP CAP. FURTHER INVESTIGATION REVEALED THE TIP WEIGHT, WHICH IS SECURED TO THE OUTBOARD RIB WITH BOLTSSDR 97UAL900791Rib · crackedRIB WAS FOUND CRACKED AT THE UPPER CAP ATTACHMENT AT LT STA XFS=106.834 DURING HORIZONTAL STABILIZER LEADING EDGE RIB CAP INSPECTION. *S/D* RIB WAS REPLACED.SDR 98ZZZX1002Spar · missingREINFORCEMENT CHANNEL/SPAR WAS MISSING/NOT INSTALLED. IT APPEARED THE SPAR HAD NEVER BEEN INSTALLED FROM THE FACTORY.SDR CKSA97554Spar · crackedDURING ROUTINE CPCP INSPECTION, FOUND RT HORIZONTAL STAB STA 32.108 OUTSIDE OF REAR SPAR LONG. FRAME FORWARD TOP PART HAS 2.5 INCH CRACK COVERING 3 FASTENERS MOST FORWARD EDGE. NDT VERIFIED CRACK. INSTALLED REPAIR IAW AIA/E/2643, EDR B2-05517. CORROSION TASDR AALA971939Spar Cap · corrodedTUL - FOUND CORROSION AFT SPAR CAP BULGED TOP LEFT HORIZ STAB, FORWARD AND INBOARD OF NR 6 HINGE BEARING. REPAIRED CORROSION AREA PER ESO 11697. (M)SDR ABXA9701675Spar Cap · corrodedDURING C-CHECK, FOUND THE AFT SIDE OF THE UPPER FWD SPAR T-CAP OF THE LT HORIZONTAL STABILIZER EXFOLIATED AT STATION XHS 15. REPAIRED T-CAP IAW ABX REA D955-21339-MR.SDR ABXA9701674Spar Cap · corrodedDURING C-CHECK, FOUND THE LT HORZ STABILIZER AFT SPAR T-CAP, FWD SIDE, EXFOLIATED AT STA XHS 86. REPAIRED T-CAP IAW ABX REA D955-21288-MR.SDR DHL9780774CRib · crackedAT C-CHECK, RT HORIZ STAB I/B LEADING EDGE ASSY LOWER RIB END CRACK AT XFS 47.5. STOP DRILLED CRACK AND FABRICATED REPAIR PARTS AND INSTALLED PER SRM 55-2-0.SDR DHL9780768CRear Spar · elongate holesRT H/S REAR SPAR ASSY, I/B SIDE MOUNT CAP, HAS ELONGATED HOLES. REMOVED DAMAGED REAR SPAR FITTING IAW SRM 51-1-12. FABRICATED NEW REAR SPAR FITTING PER ATM NR C1-P63-, ATM-621 AND PER DACO DRAWINGS NR 5653912. TREATED AND PRIMED NEW FITTING IAW SRM 51-1-8. SDR DHL9780754CRib · crackedRT H/S I/B L/E ASSY UPPER RIB END CRACK AT XFS 53.750. STOP DRILLED CRACK AND FABRICATED REPAIR PARTS IAW SRM 55-2-0. TREATED AND PRIMED IAW SRM 51-1-8. INSTALLED REPAIR PARTS IAW SRM 55-2-0.SDR DHL9780753CRib · crackedR/H H/S I/B L/E ASSY UPPER RIB END CRACKED AT XFS 66.250 . STOP DRILLED CRACK AND FABRICATED REPAIR PARTS IAW SM 55-2-0. TREATED AND PRIMED IAW SRM 51-1-8. INSTALLED REPAIR PARTS IAW SRM 55-2-0.SDR DHL9780751CRib · crackedRT H/S I/B L/E ASSY LWR RIB END CRACK AT XFS 53.750. STOP DRILLED CRACK AND FABRICATED REPAIR PARTS IAW SRM 55-2-0. TREATED AND PRIMED PARTS IAW SRM 51-1-8. INSTALLED REPAIR PARTS IAW SM 55-2-0.SDR DHL9780750CRib · crackedRT H/S I/B L/E ASSY LWR RIB END CRACK AT XFS 66.250 DOT 159. STOP DRILLED CRACK AND FABRICATED REPAIR PARTS IAW SRM 55-2-0. TREATED AND PRIMED IAW SRM 51-1-8. INSTALLED REPAIR PARTS IAW SM 55-2-0.SDR DHL9780749CRib · crackedR/H H/S I/B L/E ASSY LWR RIB END CRACK AT XFS 47.500 DOT 157. STOP DRILLED CRACK AND FABRICATED REPAIR PARTS IAW SM. 55-2-0. TREATED AND PRIMED IAW SM 51-1-8. INSTALLED REPAIR PARTS IAW SM. 55-2-0.SDR DHL9780748CRib · crackedRT H/S I/B L/E ASSY UPPER RIB END CRACK AT XFS 197, DOT 152. STOP DRILLED CRACK AND FABRICATED REPAIR PARTS IAW SRM 55-2-0. TREATED AND PRIMED IAW SRM 51-1-8. INSTALLED REPAIR PART IAW SRM 55-2-0.SDR 97ZZZX4646Spar · crackedDURING ROUTINE INSPECTION OF AIRCRAFT, TWO CRACKS WERE FOUND ON THE LT HORIZONTAL STABILIZER'S AFT SPAR LOWER CHORD. EACH CRACK WAS APPROXIMATELY 1.5 INCH LONG. ONE CRACK WAS AT STABILIZER STA 169 AND THE OTHER WAS AT STABILIZER STA 179.SDR MASA97146Spar Web · crackedDURING NIGHT MAINTENANCE, THE FORWARD SPAR WEB OF HORIZONTAL STABILIZER TO HAVE TWO CRACKS (APPROX .25 INCH) COMING FROM THE AREA WHERE THE GROMMET IS INSTALLED. MAINTENANCE REPAIRED THE CRACK IAW BEECHCRAFT FIELD DRAWING FR-00-00042. (M)SDR ABXA9701434Spar · crackedDURING D-CHECK, FOUND THE RT HORIZ STAB REAR SPAR LOWER SPAR CAP CRACKED WHERE IT BOLTS TO THE CENTER BOX SECTION. *S/D* NO DEFECT, PERFORMED DYE PEN INSPECTION AND NO CRACKS NOTED.SDR 97ZZZX3968Rib · crackedDURING REPAIR TO THE LEADING EDGE OF THE HORIZONTAL STABILIZER, DISCOVERED THAT 13 OF 15 RIBS IN THE INBOARD SECTION (RT LEADING EDGE) HAD CRACKS AT THE TRAILING EDGE IN THE RADIUS OF THE BEND IN THE RIB. SUBSEQUENT INSPECTION OF THE LT SIDE REVEALED ONLY ONESDR IH971355010Spar Cap · crackedHORIZONTAL STABILIZER FORWARD TOP CENTER FRAME CRACKED. REMOVED AND REPLACED CENTER SECTION UPPER SPAR CAP PER SRM 53-30-2.
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