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.

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 Mar 7, 2006 · N448DF · Grumav S2FSDR 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 51-1Feb 25, 2006 · N867UP · Doug DC873FSDR 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. Feb 23, 2006 · N355RM · Lear 55LEARSDR 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 RFeb 23, 2006 · N355RM · Lear 55LEARSDR 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. Feb 23, 2006 · N355RM · Lear 55LEARSDR 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 ASFeb 19, 2006 · N740TA · Beech 400ASDR 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 DAFeb 18, 2006 · N913AW · Boeing 757225SDR 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.Feb 8, 2006 · N814UP · Doug DC873FSDR 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.Jan 30, 2006 · N338SW · Boeing 7373H4SDR 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.Jan 22, 2006 · N818AL · Boeing 737230SDR 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 Jan 19, 2006 · N14629 · Boeing 737524SDR 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 CJan 19, 2006 · N432CW · Beech 400ASDR ABXA060057Spar · crackedHORIZONTAL STABILIZER CENTER SPAR BOX SKIN CRACKED ON UPPER SKIN, JUST FORWARD OF STRESS PLATE. COMPLIED WITH REA D955-53041 AND REPAIRED AREA.Jan 11, 2006 · N959AX · Doug DC941SDR 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.Jan 10, 2006 · N69311 · Boeing 7373T0SDR 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. FABRIJan 8, 2006 · N328AW · Boeing 7373B7SDR 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 51-70-11-0Jan 4, 2006 · N308AW · Boeing 7373G7SDR SWAA054080Spar · crackedDURING SCHEDULED C4 CHECK, FOUND RT HORIZONTAL STAB AFT SPAR CRACKED 5 INCHES FROM ROOT. REPAIRED HORIZONTAL STAB PER SRM.Dec 22, 2005 · N319SW · Boeing 7373H4SDR SWAA054049Rib · crackedDURING SCHEDULED D-CHECK, FOUND RT HORIZONTAL STAB L/E RIB CRACKED AT STAB STA 184.7. REMOVED AND REPLACED RIB PER SRM.Dec 20, 2005 · N623SW · Boeing 7373H4SDR AU510002029Spar · crackedHORIZONTAL STABILIZER FRONT SPAR CRACKED. FOUND DURING INSPECTION IAW AD/CESSNA170/59.Dec 12, 2005 · Cessna 172MSDR 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.Dec 8, 2005 · N423FE · Airbus A310SDR 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.Dec 7, 2005 · N423FE · Airbus A310SDR 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.Nov 23, 2005 · Cessna 172ESDR 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)Nov 18, 2005 · Cessna 152SDR 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. 727-55A00Nov 16, 2005 · N188FE · Boeing 72722SDR 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 Nov 10, 2005 · N24831 · Cessna 152SDR 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.Oct 26, 2005 · N813UP · Doug DC873FSDR 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.Oct 21, 2005 · N556FE · Doug DC1010SDR 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.Oct 5, 2005 · N556FE · Doug DC1010SDR 62310032005Rib · damagedON POST FLIGHT DAMAGE NOTED TO FAIRING ON OUTSIDE PORTION OF RIGHT STABILIZER LOWER SURFACE.Oct 3, 2005 · N506QS · Gulstm GULFSTREAMGVSDR 05FDEA03071Spar Cap · corrodedLEFT HORIZONTAL STAB UPPER SPAR CAP IS CORRODED AT NR 23 NUTPLATE COUNTING IB-OUT.Sep 23, 2005 · N425FE · Airbus A310203SDR 05FDEA03070Spar Cap · corrodedLEFT HORIZONTAL STAB FWD UPPER SPAR CAP IS CORRODED AT NR 10 NUTPLATE COUNTING IB-OUT.Sep 23, 2005 · N425FE · Airbus A310203SDR 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 T5Sep 19, 2005 · N425FE · Airbus A310203SDR 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-Sep 14, 2005 · N574FE · Doug MD11SDR 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.Sep 14, 2005 · N425FE · Airbus A310SDR 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.Sep 14, 2005 · N483FE · Boeing 727227SDR 05FDEA02853Rib · crackedLEFT HORIZONTAL L/E PANEL 331BB RIB NR 1 IS CRACKED AT UPPER AFT CORNER.Sep 13, 2005 · N425FE · Airbus A310203SDR 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)Sep 9, 2005 · Cessna A152SDR 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)Sep 8, 2005 · N772AS · Boeing 7374Q8SDR 62309302005Rib · damagedON POST FLIGHT DAMAGE NOTED TO FAIRING ON OUTSIDE PORTION OF RT STABILIZER LOWER SURFACE.Sep 3, 2005 · N506QS · Gulstm GVSDR 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.Sep 2, 2005 · N900AX · Doug DC932SDR 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)Aug 29, 2005 · N834NK · Doug DC983SDR 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)Aug 26, 2005 · N834NK · Doug DC983SDR 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 OTHJul 10, 2005 · Cessna 152SDR WRLA2005119Rib · corrodedDURING C04 CHECK, WHILE PERFORMING INSP PER EO 02-5510-098, FOUND CORROSION IN HST RT BARREL NUT HOLE NR 13.Jun 16, 2005 · N277 · Doug MD11SDR WRLA2005118Rib · corrodedDURING C04 CHECK, WHILE PERFORMING INSP PER EO 02-5510-098, FOUND CORROSION IN HST RT BARREL NUT HOLE NR 11.Jun 16, 2005 · N277 · Doug MD11SDR WRLA2005117Rib · corrodedDURING C04 CHECK, WHILE PERFORMING INSP PER EO 02-5510-098, FOUND CORROSION IN HST RT BARREL NUT HOLE NR 36.Jun 16, 2005 · N277 · Doug MD11SDR WRLA2005116Rib · corrodedDURING C04 CHECK, WHILE PERFORMING INSP PER EO 02-5510-098, FOUND CORROSION IN HST RT BARREL NUT HOLE NR 33.Jun 16, 2005 · N277 · Doug MD11SDR WRLA2005115Rib · corrodedDURING C04 CHECK, WHILE PERFORMING INSP PER EO 02-5510-098, FOUND CORROSION IN HST RT BARREL NUT HOLE NR 32.Jun 16, 2005 · N277 · Doug MD11SDR WRLA2005114Rib · corrodedDURING C04 CHECK, WHILE PERFORMING INSP PER EO 02-5510-098, FOUND CORROSION IN HST RT BARREL NUT HOLE NR 31.Jun 16, 2005 · N277 · Doug MD11SDR WRLA2005113Rib · corrodedDURING C04 CHECK, WHILE PERFORMING INSP PER EO 02-5510-098, FOUND CORROSION IN HST RT BARREL NUT HOLE NR 30.Jun 16, 2005 · N277 · Doug MD11
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