JASC 5523
Service difficulty reports · 1,033
Reports filed under 5523 · Elevator, Tab Structure, 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 = '5523' 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 = '5523' 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 UFTA990544Skin · dentedORD - DENT FOUND IN TWO LOCATIONS ON RIGHT ELEVATOR TRIM TAB. MAINTENANCE INSPECTED TRIM TAB IAW BAE ATP SRM 55-20-00 AND 51-10-01, DAMAGE WAS FOUND TO BE WITHIN LIMITS. REPAIR OF DAMAGE IS PENDING IAW BAE ATP SRM 51-10-01. (M)SDR LR7A9992Beam · crackedDURING SCHEDULED B1 INSPECTION FOUND RT ELEVATOR TAB BEAM CRACKED, APPROX 7 INCH AT INBD END AND 4 INCH CRACK IN LE SKIN AT HSS 92. BEAM CRACK CUT OUT AND REPAIRED PER EDG 88-R01, REV IR, DATED 4/20/99. LE SKIN REPLACED IAW SRM SMP 583-51-140-10. DRC 0034.SDR 99UAL900231Bearing · wornSIGNIFICANT AIRFRAME VIBRATION FELT IN CONTROLS, FLOOR, AND GLARESHIELD. *S/D* THE VIBRATION WAS CAUSED BY A WORN BEARING AND BUSHINGS ON THE LEFT HAND ELEVATOR TAB INBOARD HINGE. THE WORN PARTS WERE REPLACED. OPS CHECK OK.SDR AU990476Trim Tab · corroded(AUS) ELEVATOR TRIM TAB CORRODED AND DAMAGED DUE TO FOD. THE TRIM TAB HAD ALSO BEEN REPAIRED AT SOME TIME PREVIOUSLY DUE TO TIP DAMAGE.SDR CALA9900396Control Tab · dentedINSPECTION FOUND THE RT ELEVATOR CONTROL TAB UPPER O/B TRAILING EDGE SKIN DENTED. THE ELEVATOR TAB WAS REMOVED AND REPLACED IAW MM 27-30-11.SDR DHL9980763CTab · delaminatedAT C CHECK, LEFT ELEVATOR GEAR TAB IS DELAMINATED. REPAIRED AND INSTALLED PER MM 27-30-3. N/R 38.SDR CALA9900371Tab · dentedINSPECTION FOUND LEFT ELEVATOR CONTROL TAB LOWER O/B LEADING EDGE SKIN DENTED. THE LEFT ELEVATOR CONTROL TAB WAS REMOVED AND REPLACED IAW MM 27-30-11.SDR CALA9900275Skin · separatedINSPECTION FOUND LT ELEVATOR CONTROL TAB TRAILING EDGE SKIN SEPARATING IN TWO PLACES. THE ELEVATOR CONTROL TAB WAS REMOVED AND REPLACED IAW 55-20-2.SDR DHL9980764CTab · delaminatedAT C CHEK, RT ELEVATOR CONTROL TAB DELAMIANTED. REMOVED ELEVATOR TAB AND OVERHAULED AND INSTALLED PER MM 27-30-00. N/R 39SDR 99UAL900129Hinge · failedHEAVY VIBRATION FELT THROUGH OUT THE CABIN. *S/D* RIGHT ELEVATOR TAB INBOARD HINGE FITTING SEPARATED FROM THE TAB LEADING EDGE. TEAR OUT OF THE TAB SKIN INDICATES THAT AT LEAST THREE OF FOUR FASTENERS WERE INSTALLED WHEN SEPARATION OCCURRED. SIGNS OF WEAR ONSDR CALA9900140Tab · delaminatedINSPECTION FOUND LT ELEVATOR CONTROL TAB DELAMINATED ON UPPER SURFACE. THE LT ELEVATOR CONTROL TAB WAS REMOVED AND REPLACED IAW MM 27-30-00 AND 27-30-3.SDR DHL9980527CTab · delaminatedAT C-CHECK, LT ELEVATOR DELAMINATED ON UPPER SURFACE. REMOVED AND INSTALLED REPAIRED TAB PER MM 27-30-2. N/R 51SDR DHL9980526CTab · dentedAT C-CHECK, RT ELEVATOR GEAR TAB HAS DENT AT MID SECTION OF T/E AND UPPER SURFACE. REMOVED AND INSTALLED SERVICEABLE GEAR TAB PER MM 27-30-00. N/R 50SDR ASAA9880240Hinge · gougedLCQ - DURING 30K CHECK GOUGES WERE FOUNDON LEFT ELEVATOR ANTI FLOAT TAB HINGE, 3RD FROM OUTBOARD. REPAIRED IAW ASA EA 5520-01062. (M)SDR CALA9801970Skin · delaminatedINSPECTION FOUND RT ELEVATOR CONTROL TAB TRAILING EDGE DELAMINATED. THE CONTROL TAB WAS REMOVED AND REPLACED IAW MM 27-30-11.SDR CALA9801906Skin · delaminatedINSPECTION FOUND RT ELEVATOR CONTROL TAB TRAILING EDGE DELAMINATED. THE RT ELEVATOR CONTROL TAB WAS REMOVED AND REPLACED IAW MM 27-30-11.SDR VJ9800513Tab · corrodedRT ELEVATOR GEAR TAB HAS 1 INCH DIAMETER CORROSION SPOT. CUT OUT CORROSION, CLEANED AREA, FABRICATED AND INSTALLED DOUBLER IAW DC9 SRM 51-70-2.SDR CALA9801747Tab · delaminatedINSPECTION FOUND TWO AREAS OF DELAMINATION ON UPPER SURFACE OF LT ELEVATOR CONTROL TAB BETWEEN THIRD AND OUTBOARD HINGES. THE DELAMINATED AREAS WERE TRIMMED OUT AND FILLER AND DOUBLER WERE INSTALLED IAW SRM 51-70-2.SDR CALA9801732Tab · debondedINSPECTION FOUND LT ELEVATOR TAB INBOARD MOST TRAILING EDGE AREA DEBONDED. THE ELEVATOR TAB WAS REMOVED AND REPLACED IAW MM 27-30-11.SDR CALA9801706Tab · delaminatedINSPECTION FOUND RT ELEVATOR GEAR TAB DELAMINATED. THE RT ELEVATOR GEAR TAB WAS REMOVED AND REPLACED IAW MM 27-30-04.SDR ABXA9800904Tab · crackedWHILE COMPLYING WITH C-INSPECTION, FOUND THE LEFT ELEVATOR GEAR TAB CRACKED. REPLACED LEFT ELEVATOR GEAR TAB IAW DC-9 SUPPLEMENTAL MAINTENANCE MANUAL CHAPTER 27-30-4.SDR DHL9880415CSkin · delaminatedAT C-CHECK, RT ELEVATOR CONTROL TAB UPPER AND LOWER L/E AND O/B LOWER SURFACE DELAMINATED. REMOVED AND REPLACED PER MM 27-30-0. N/R 608SDR DHL9880414CSkin · delaminatedAT C-CHECK, LEFT ELEVATOR CONTROL TAB UPPER SURFACE I/B DELAMINATED AND DENTED. REMOVED AND REPLACED PER MM 27-30-3. N/R 607SDR CALA9801552Skin · delaminatedINSPECTION FOUND RT ELEVATOR CONTROL TAB INBOARD TRAILING EDGE DELAMINATED. THE ELEVATOR CONTROL TAB WAS REMOVED AND REPLACED IAW MM 27-30-11.SDR CA980916049Tab · cracked(CAN) DURING INSPECTION, THE ELEVATOR TRIM TAB WAS FOUND CRACKED BOTH TOP AND BOTTOM AT THE PUSH ROD END. RACK APPROXIMATELY 2 INCHES LONG CAUSING SUBSTANTIAL LOSS IN STRENGTH.SDR CALA9801082Housing · crackedINSPECTION FOUND THE LT ELEVATOR OUTBOARD TRIM TAB INBOARD TRIM ROD HOUSING SHIELD CRACKED AT THE INBOARD UPPER COUNTERSUNK HOLE. THE CRACK WAS STOP DRILLED IAW SRM 55-01, FIGURE 2. A PATCH DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 55-01, FIGURE 2, 51-10-SDR AU980662Hinge · cracked(AUS) ELEVATOR TRIM TAB FORWARD HINGE CRACKED AT THE LT FORWARD EDGE. CRACK LENGTH 3MM (0.118 INCH). PART TC: 2,815.SDR MZZA98158Skin · puncturedDURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, PUNCTURE WAS FOUND ON RT ELEVATOR TAB UPPER SKIN AT ELEV STA 110. THE DAMAGED SKIN 0.5 INCH DIAMETER WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. (X)SDR AU980469Hinge · disbonded(AUS) ELEVATOR TRIM TAB PN 115C-3551 HINGE APPEARS DISBONDED TO FIBER REINFORCED PLASTIC STRUCTURE SECOND INBOARD SEGMENT. ALSO, AN OUTBOARD EDGE CRACK WAS DEVELOPING FROM SAME LOCATION. PART TC: 171.SDR AU980456Trim Tab · cracked(AUS) ELEVATOR TRIM TAB CRACKED IN AREA ADJACENT TO THE SECOND INBOARD HINGE SEGMENT. PART TC: 1,672.SDR AU980455Trim Tab · cracked(AUS) ELEVATOR TRIM TAB CRACKED IN THE AREA ADJACENT TO THE SECOND INBOARD HINGE SEGMENT. PART TC: 86.SDR AU980454Trim Tab · cracked(AUS) ELEVATOR TRIM TAB CRACKED IN AREA ADJACENT TO THE SECOND INBOARD HINGE SEGMENT. PART TC: 1,142.SDR AU980444Trim Tab · cracked(AUS) ELEVATOR TRIM TAB CRACKED IN AREA ADJACENT TO THE SECOND INBOARD HINGE SEGMENT. PART TC: 53.SDR AU980443Trim Tab · cracked(AUS) ELEVATOR TRIM TAB CRACKED IN AREA ADJACENT TO THE SECOND INBOARD HINGE SEGMENT. PART TC: 977.SDR CALA9800533Skin · separatedINSPECTION FOUND THE LT ELEVATOR CONTROL TAB INBOARD CORNER SEPARATED. THE ELEVATOR CONTROL TAB WAS REMOVED AND REPLACED.SDR CALA9800532Skin · separatedINSPECTION FOUND THE RT ELEVATOR CONTROL TAB TRAILING EDGE SEPARATED. THE ELEVATOR CONTROL TAB WAS REMOVED AND REPLACED.SDR AU980242Trim Tab · separated(AUS) ELEVATOR TRIM TAB SEPARATED. HINGE SEGMENTS TORN FROM ELEVATOR. SUSPECT CAUSED BY AIRCRAFT OVERSPEED.SDR AU980085Bracket · cracked(AUS) ELEVATOR TRIM TAB HINGE BRACKETS PNO 4042-010, PNO 4042-009 AND PNO 4042-008 CRACKED.SDR MZZA98041Tab Skin · delaminationTNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, 5 INCH LONG DELAMINATION WAS FOUND ON LEFT ELEVATOR TAB TRAILING EDGE SKIN EDGE. THE DELAMINATION SKIN EDGE WAS REPAIRED PER B727 SRM 51-40-6 FIGURE 26. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 84SDR MZZA98040Skin · delaminationTNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, 3 INCH LONG DELAMINATION WAS FOUND ON RT ELEVATOR TAB TRAILING EDGE SKIN EDGE. THE DELAMINATION SKIN EDGE WAS REPAIRED PER B727 SRM 51-40-6 FIGURE 26. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 8408SDR ABXA9701938Skin · delaminatedELEVATOR GEARED TAB WAS 25 PERCENT DELAMINATED ON OUTBOARD UPPER AND LOWER SKIN. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKIN.SDR CALA9701702Control Tab · disbondedINSPECTION FOUND RT ELEVATOR CONTROL TAB TRAILING EDGE DISBONDING. THE TAB WAS REMOVED AND A SERVICEABLE TAB WAS INSTALLED IAW SRM 51-40-10.SDR CALA9701691Control Tab · disbondedINSPECTION FOUND LT ELEVATOR CONTROL TAB OUTBOARD TRAILING EDGE CORNER SEPARATING. THE ELEVATOR TAB WAS REMOVED AND A SERVICEABLE TAB WAS INSTALLED IAW MM 27-30.SDR MZZA97289Skin · tornKUL - NRC: 844100 - S-CHECK FOUND SKIN OF LT ELEVATOR TAB TORN AT DELAMINATED AREA ON UPPER SURFACE OUTBOARD END OF SPAR, 0.200 INCH LONG AND 0.020 WIDE. REPAIRED ELEVATOR TAB PER B 727 SRM 55-20-3. (X)SDR ABXA9701665Tab · corrodedDURING C-CHECK, FOUND RT ELEVATOR CONTROL TAB CORRODED. REPLACED CONTROL TAB IAW DC9 MM 27-30-3 PARA 3.SDR 97ZZZX4475Trim Tab Assy · brokenLEFT ELEVATOR TRIM TAB HORN ATTACH BROKE IN-FLIGHT JUST AFTER TAKEOFF. AIRCRAFT ENCOUNTERED VIBRATION AND RETURNED TO LAND. INSPECTION FOUND ATTACH HORN OF TRIM TAB BROKEN AND SHOWED SIGNS OF PREVIOUS CRACK. SUSPECT CAUSE TIGHTENING BOLT AND PINCHING HORN CSDR DHL9780772CSkin · dentedRT ELE GEAR TAB UPPER SKIN HAS TWO DENTS. REMOVED RT ELEVATOR GEAR TAB AND CONTROL TAB LT IAW DC-8 MM 27-30-3. INSTALLED RT ELEVATOR GEAR TAB IAW DC-8 MM CH 27-30-3. P/N ON 564444-501, SN ON ACI-114. RIGGED AND OPS CHECKED IAW MM 27-30-0.SDR CALA9701447Skin · crackedLEFT ELEVATOR CONTROL TAB SKIN LEADING EDGE CRACKED 1.5 INCH JUST ABOVE NUMBER 2 HINGE FROM INBOARD. REMOVED AND REPLACED TAB PER MM 27-30-0.SDR DHL9780713CFairing · crackedAT C-CHECK, LT ELEV CONTROL TAB MECH FAIRING ASSY CRACKED AT T/E. INSTALLED NEW FAIRING PER MM 27-30-2.SDR ABXA9701529Tab · delaminatedDURING C-CHECK, FOUND LEFT ELEVATOR TAB DELAMINATED ON UPPER SURFACE. REPLACED LT ELEVATOR TAB I.A.W. DC-9 MM 27-30-3
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