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 2006FA0000388Rib · crackedDURING MAINTENANCE ON THE RT SIDE HORIZONTAL STABILIZER, CRACKS WERE ON 2 RIB SECTIONS. CRACKS WERE DETECTED ON RIBS PN 89T920543, STA 138.858 AND PN 89T1029-1, STA 80.608. THESE CRACKS WERE FOUND ON THE UPPER FWD LEADING EDGE TABS WHERE THE RIB ATTACHES TO SDR UPS06846430Rib · crackedINSPECTION TYPE:C3 REF EO DC8-5510-1074-N APPD B PAGE 8, STIFFENING PLANK RIB IS CRACKED BETWEEN BOLTS NR 36 AND NR 37. REMOVED STIFFENING PLANK RIB BETWEEN BOLTS 36 AND 37 IAW SRM 51-01-20D-0, LOCATED, DRILLED UP, AND INSTALLED REPLACEMENT PLANK IAW SRM 51-1SDR 2006FA0000256Spar · corrodedINSPECTIONS HAVE FOUND SERIOUS EXFOLIATION CORROSION IN THE REAR SPAR FLANGES, NEAR THE ELEVATOR HINGE BRACKETS OF AT LEAST 2 AIRCRAFT. CORROSION HAD PROGRESSED TO THE EXTENT REQUIRING REMOVAL/REPLACEMENT OF THE SPAR FLANGES OR REPLACEMENT OF THE STABILIZER. SDR 2006FA0000255Spar · corrodedDURING 12,000/12 YR DEMATE INSPECTIONS WE HAVE FOUND SERIOUS EXFOLIATION CORROSION IN THE REAR SPAR FLANGES, NEAR THE ELEVATOR HING BRACKETS OF AT LEAST TWO AIRCRAFT. CORROSION HAD PROGRESSED TO THE EXTENT REQUIRING REMOVAL/REPLACEMENT OF THE SPAR FLANGES OR RSDR 2006FA0000254Spar · corrodedINSPECTIONS, HAVE FOUND SERIOUS EXFOLIATION CORROSION IN THE REAR SPAR FLANGES, NEAR THE ELEVATOR HINGE BRACKETS OF AT LEAST 2 AIRCRAFT. CORROSION HAD PROGRESSED TO THE EXTENT REQUIRING REMOVAL/REPLACEMENT OF THE SPAR FLANGES OR REPLACEMENT OF THE STABILIZER. SDR DJFA2006205Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION AS PART OF THE -B- LEVEL INSPECTION A RIGHT INBOARD HORIZONTAL STABILIZER RIB WAS FOUND CRACKED NEXT TO THE SIDE ROLLER BRACKET. THE RIB WAS REPLACED WITH A NEW ASSDR AWXA200600447Spar · corrodedSAL - MAJOR REPAIR - DURING C-CHECK FOUND THE RT HORIZONTAL STABILIZER REAR SPAR UPPER CHORD, FROM STAB STATION 104.25 TO STAB STATION 364.44 UPPER SURFACE AND TRAILING EDGE WERE CORRODED. CORROSION WAS OUT OF SRM ALLOWABLE LIMITS. MAINTENANCE REMOVED ALL DASDR UPS06846298Spar · crackedINSPECTION TYPE:C2 CRACKS ON I/B WEB SUPPORT ANGLES ON LT HORIZ STAB FRONT SPAR. REMOVED CRACKED UPPER AND LWR T-CAP ANGLES IAW SRM 51-03-00-0. LOCATED AND DRILLED UP REPLACEMENT T-CAP ANGLES AND INSTALLED IAW SRM 51-3-0, 51-3-2, 51-01-21, AND SRM 51-01-20D.SDR SWAA060362Spar · crackedDURING SCHEDULED C1 CHECK, FOUND RT HORIZONTAL STAB AFT SPAR CRACKED BETWEEN STAB STA 157.10 AND STAB STA 166.30. REPAIRED HORIZONTAL STAB PER SRM.SDR TSAA0655005Spar · corrodedLEFT HAND HORIZONTAL STABILIZER REAR SPAR UPPER CHORD CORROSION SS 111.1 - SS 101.9. MAINTENANCE REPAIRED WITH FILLERS TO SEAT IN BLEND OUTS AND SKIN TRIM OUT. FABRICATED EXTERNAL SKIN DOUBLER PER ECO 3392.SDR CALA0600021Spar · corrodedINSPECTION FOUND LT HORIZONTAL STABILIZER UPPER REAR SPAR CAP CORRODED JUST O/B OF STAB STA 193.90. AN INTERIM REPAIR WAS INSTALLED IAW ECRA 5510-01826. A DIP WAS ISSUED TO PERFORM A PERMANENT REPAIR PER PART 3 OF ECRA 5510-01826 WITH NO FURTHER INSPECTIONS SDR 2006F00005Rib · crackedHORIZONTAL STABILIZER INBOARD RIB P/N 45A21104-012 FOUND WITH 3 INCH CRACK ALONG LOWER EDGE OF STAB CENTERING ROLLER BRACKET. BEEF UP ANGLES P/N 45A21085-004, AND 45A21086-004 ALSO FOUND WITH MULTIPLE STRESS CRACKS. EXCESSIVE LOADS ON ROLLER APPEAR TO HAVE CSDR ABXA060057Spar · crackedHORIZONTAL STABILIZER CENTER SPAR BOX SKIN CRACKED ON UPPER SKIN, JUST FORWARD OF STRESS PLATE. COMPLIED WITH REA D955-53041 AND REPAIRED AREA.SDR CALA0600005Spar · corrodedINSPECTION FOUND THE LT HORIZONTAL STABILIZER REAR SPAR UPPER CAP CORRODED FROM STAB STA 196.2 TO 200.3. THE LT HORIZONTAL STABILIZER ASSEMBLY WAS REMOVED AND REPLACED MM 27-41-11, PAGE 401, FIGURE 401.SDR AWXA200600374Spar · crackedMCN - DURING C24 CHECK DISCOVERED RT HORIZONTAL STAB LEADING EDGE SPAR WEB CRACKED, .890 INCHES IN LENGTH, AT THE THIRD LIGHTENING HOLE FROM THE OUTBOARD END AT STAB STATION 198.5R. MAINTENANCE REMOVED CRACK IAW BOEING 737-300 SRM 55-10-10-1A1 FIG 101. FABRISDR AWXA200600106Rib · crackedMCN - DURING C15 CHECK DISCOVERED RIB CRACKED, .4 INCHES, INSIDE THE LT HORIZONTAL STABILIZER LEADING EDGE, 65" FROM THE INBOARD END AT SS 73L. MAINTENANCE REMOVED CRACKED RIB FROM STABILIZER AND CUTOUT DAMAGED SECTION OF RIB IAW BOEING 737-300 SRM 51-70-11-0SDR SWAA054080Spar · crackedDURING SCHEDULED C4 CHECK, FOUND RT HORIZONTAL STAB AFT SPAR CRACKED 5 INCHES FROM ROOT. REPAIRED HORIZONTAL STAB PER SRM.SDR SWAA054049Rib · crackedDURING SCHEDULED D-CHECK, FOUND RT HORIZONTAL STAB L/E RIB CRACKED AT STAB STA 184.7. REMOVED AND REPLACED RIB PER SRM.SDR AU510002029Spar · crackedHORIZONTAL STABILIZER FRONT SPAR CRACKED. FOUND DURING INSPECTION IAW AD/CESSNA170/59.SDR 05FDEA04178Spar · corrodedLT HORIZONTAL T/E UPPER IB SPAR ON LOWER SIDE HAS SEVERE EXFOLIATION, REF N00541. REPAIRED LT UPPER IB THS SPAR CORD IAW A310-200 SRM 55-11-21 PARA 7.H PAGES 315TO, 320 FIG 211,213 AND 219 SHEET 2.SDR 05FDEA04166Spar · corrodedRT HORIZONTAL T/E UPPER IB SPAR ON LOWER SIDE HAS SEVERE EXFOLIATION, REF N00542. REPAIRED RT HORIZONTAL T/E UPPER SPAR CORD IAW SRM 55-11-21 PARA 7.H PAGES 315 TO 324 FIG SHEET 2 AND FIG 213.SDR CA051221007Spar · crackedTHE STABILIZER FORWARD SPAR WAS CRACKED AND BUCKLED AT THE CENTER LIGHTENING HOLE. THERE WERE 2 SMALL CRACKS RADIATING OUTWARD. STABILIZER WAS REPAIRED AS PER CESSNA SEB94-8.SDR CA070214003Spar · cracked(CAN) DURING 100 HOUR INSPECTION, VERIFICATION OF AD 80-11-04, THE TECHNICIAN FOUND A CRACKED BRACKET. CLOSER INSPECTION INDICATED THAT THE SPAR WAS ALSO CRACKED. (TC NR 20070214003)SDR 05FDEA03835Rib · damagedDURING INSPECTION OF THE LT HORIZ STAB ELEVATOR RIB AT ELEV STA 136.5, FOUND TO HAVE EXISTING REPAIRS ON THE LOWER IB AND OB FLANGES OF THE RIB AT THE TRAILING EDGE BEAM. RIB REQUIRES REPLACEMENT PER FEDEX EO 7-5510-7-5001 PT 1. REPAIRED PER S.B. 727-55A00SDR 2006FA0000012Spar · crackedON ROUTING 100 HR INSPECTION FOUND CRACK ON HORIZONTAL STABILIZER FRONT APEK, LOWER ANGLE PN 0432001-37 AND REINFORCEMENT PLATE PN 0432001-44, 1 LOWER SKIN RIVET SEAM FRETTED AND LOOSE. UPON REMOVAL AND DISASSEMBLY DISCOVERED CRACKED SKIN (PN 0432001-55) AND SDR UPS05845710Rib · crackedFOUND LT HORIZ STAB I/B L/E STA 141.250 RIB HAS CRACK ON LWR FLANGE ANGLE. STOP DRILLED CRACK, FABBED, AND INSTALLED REPAIR IAW DC-8 SRM 55-2-0 FIG 2 AND 3.SDR 05FDEA03475Rib · corrodedLT HORIZ STAB LEADING EDGE OB FOUND CORROSION BETWEEN SKIN AND RIB. REMOVED CORROSION AND REPAIRED WITH NR 2EA DOUBLER IAW SRM 55-13-01 FIG 1 VOL3.SDR 05FDEA03229Rib · crackedLT HORIZ STAB TIP INTERNAL SIDE FOUND CRACK 1 INCH LONG ON RIB FROM THE EDGE. STOPPED DRILL CRACK AND INSTALLED REPAIR ANGLE IAW SRM 55-00-01 FIG 2 VOL I.SDR 62310032005Rib · damagedON POST FLIGHT DAMAGE NOTED TO FAIRING ON OUTSIDE PORTION OF RIGHT STABILIZER LOWER SURFACE.SDR 05FDEA03071Spar Cap · corrodedLEFT HORIZONTAL STAB UPPER SPAR CAP IS CORRODED AT NR 23 NUTPLATE COUNTING IB-OUT.SDR 05FDEA03070Spar Cap · corrodedLEFT HORIZONTAL STAB FWD UPPER SPAR CAP IS CORRODED AT NR 10 NUTPLATE COUNTING IB-OUT.SDR 05FDEA02997Frame · corrodedLT HORIZ STAB T/E FORMER/WEB CORRODED AROUND NUTPLATES AND WEB FROM REAR SPAR TO 10" AFT OF REAR SPAR AND 54" FROM FUSELAGE. REMOVED CORROSION FOUND OUT OF LIMITS IAW SRM 55-10-00 FIG 101. REMOVED FORMER WEB RIB IAW SRM 51-40-21. RIB FABRICATED ON PCT NR T5SDR 05FDEA02883Spar · corrodedHORIZ STAB RT NR 1 BARREL NUT BORE AREAS CORRODED. HORIZ STAB BARREL NUT BORE NR 1 RT REPAIRED IAW STABILIZERS, HORIZONTAL STABILIZER, BARREL NUT BORE REWORK/REPAIR AD 2003-22-08 - EA NR 1-5510-87628 ATTACHMENT 11. CLASSIFIED AS MAJOR REPAIR IAW FEDEX GMM 6-SDR 05FDEA02901Spar · corrodedLT HORIZ STAB UPPER REAR SPAR T-CAP LOWER SIDE CORRODED AT NUTPLATES 51 TO 57 IN FROM FUSELAGE. REMOVED NUTPLATES, REMOVED CORROSION, MODIFIED RIB SUPPORT FABED REPAIRS, AND INSTALLED REPAIRS IAW SRM 51-40-21, 55-11-21, AND 51-74-10.SDR 05FDEA02887Rib · gougedLEFT HORIZONTAL STAB NR 3 BALANCE BAY OB RIB IS GOUGED FROM CONTACT WITH IDLER HINGE PIN. REMOVED AND REPLACED L/HORIZ. STAB NO. 3 BALANCE BAY OUTBD RIB IAW EA 7-5510-70689, PART 1 AND 727 SRM 51-30-2 AND 51-30-5.SDR 05FDEA02853Rib · crackedLEFT HORIZONTAL L/E PANEL 331BB RIB NR 1 IS CRACKED AT UPPER AFT CORNER.SDR AU510001919Bracket · cracked(AUS) HORIZONTAL STABILIZER UPPER PLATE CRACKED IN AREA ADJACENT TO VERTICAL STABILIZER BRACKET ATTACHMENT. CRACK LENGTH 7MM (0.275IN). (AD/SB DESC: SEB 03-6 ) (CASA NR 510001919)SDR ASAA0540445Rib · crackedOKC - FOUND LEFT HORIZONTAL L/E HAS CRACKED RIB AT BS 244.72. REMOVED AND REPLACED RIB ON L/E AT BS 244.72 IAW B737-400 SRM 51-40-02. (M)SDR 62309302005Rib · damagedON POST FLIGHT DAMAGE NOTED TO FAIRING ON OUTSIDE PORTION OF RT STABILIZER LOWER SURFACE.SDR ABXA050221Spar Cap · crackedRIGHT HORIZONTAL STABILIZER UPPER REAR SPAR TEE CAP MOST OUTBOARD END CRACKED. REPAIRED HORIZONTAL REAR SPAR CAP IAW DC-9 SRM 55-02.SDR GTIA050250Rib · crackedFOUND RIGHT HORIZONTAL STABILIZER L/E, OUTBOARD L/E RIB CRACKED AT UPPER EDGE. STOPPED DRILLED CRACKED AREA. FABRICATED REPAIR PART. TREATED, PRIMED AND INSTALLED REPAIR PART. (M)SDR GTIA050242Spar · damagedLEFT HORIZ STAB AFT SPAR CHANNEL DAMAGED STATION XHS 85. REMOVED CHANNEL ON LEFT HORIZONTAL STAB ON AFT SPAR. FABRICATED CHANNEL. TREATED, PRIMED AND INSTALLED REPAIR CHANNEL. (M)SDR AU510001964Rib · crackedHORIZONTAL STABILIZER INBOARD LEADING EDGE RIBS CRACKED. REMOVAL OF HORIZONTAL STABILIZER INBOARD RIBS REVEALED ONE PIECE 0.5 SQ INCH OF FLANGE COMPLETELY CRACKED AWAY STARTING FROM APEX RELIEF HOLE. THIS AREA IS NOT NORMALLY VISIBLE FOR INSPECTION. ONE OTHSDR WRLA2005119Rib · corrodedDURING C04 CHECK, WHILE PERFORMING INSP PER EO 02-5510-098, FOUND CORROSION IN HST RT BARREL NUT HOLE NR 13.SDR WRLA2005118Rib · corrodedDURING C04 CHECK, WHILE PERFORMING INSP PER EO 02-5510-098, FOUND CORROSION IN HST RT BARREL NUT HOLE NR 11.SDR WRLA2005117Rib · corrodedDURING C04 CHECK, WHILE PERFORMING INSP PER EO 02-5510-098, FOUND CORROSION IN HST RT BARREL NUT HOLE NR 36.SDR WRLA2005116Rib · corrodedDURING C04 CHECK, WHILE PERFORMING INSP PER EO 02-5510-098, FOUND CORROSION IN HST RT BARREL NUT HOLE NR 33.SDR WRLA2005115Rib · corrodedDURING C04 CHECK, WHILE PERFORMING INSP PER EO 02-5510-098, FOUND CORROSION IN HST RT BARREL NUT HOLE NR 32.SDR WRLA2005114Rib · corrodedDURING C04 CHECK, WHILE PERFORMING INSP PER EO 02-5510-098, FOUND CORROSION IN HST RT BARREL NUT HOLE NR 31.SDR WRLA2005113Rib · corrodedDURING C04 CHECK, WHILE PERFORMING INSP PER EO 02-5510-098, FOUND CORROSION IN HST RT BARREL NUT HOLE NR 30.
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