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 2002FA0001142Structure · brokenDURING 100 HOUR INSPECTION, ELEVATOR TRIM BEARINGS WERE SUSPECTED TO BE LOOSE AND REQUIRE REPLACEMENT. TO REPLACE THESE BEARINGS, ELEVATOR TRIM TAB HORN WAS REMOVED. WHEN FORCE WAS APPLIED TO TWO OF FOUR ATTACHING NUTS TO EFFECT THEIR REMOVAL FROM THE MATINSDR SWAA021885Hinge Fitting · wornAIRFRAME VIBRATION FELT ABOVE 280 KNOTS. REMOVED AND REPLACED LEFT INBD ELEVATOR TAB HINGE FITTING PER MM.SDR SWAA021847Fitting · wornDURING SCHEDULED PM CHECK, SWA SI 11038-55, FOUND LT ELEVATOR TAB NR 1, NR 2 AND NR 3 ATTACH LUGS WORN. REMOVED AND REPLACED LEFT ELEVATOR ATTACH LUGS PER MM.SDR SWAA021846Fitting · wornDURING SCHEDULED PM CHECK, SWA SI 11038-55, FOUND RT ELEVATOR TAB NR 2, NR 3 AND NR 4 ATTACH LUGS WORN. REMOVED AND REPLACED RT ELEVATOR TAB ATTACH LUGS PER SWA EASDR SWAA021845Fitting · wornDURING SCHEDULED SERVICE CHECK, SWA SI 11038-55, FOUND RT ELEVATOR TAB NR 2 ATTACH LUG WORN. REMOVED AND REPLACED RT ELEVATOR ATTACH LUG PER MM.SDR QXEA0201224Arm · chafedPDX - RIGHT HAND ELEVATOR SPRING TAB NR 3 HINGE ARM HAS CHAFE DAMAGE. REPAIRED IAW HORIZON AIR EA 2-55-72.SDR 2002FA0001000Bracket · corrodedSUBJECT PART IS A BRACKET MOUNTING, A TORQUE TUBE FOR THE ELEVATOR TRIM CONTROL SYSTEM TO THE REAR SPAR OF THE HORIZONTAL STABILIZER, AND WAS BEING REPLACED DURING COMPLIANCE OF MFG SB. PART WAS FOUND WITH SEVERE EXFOLIATION CORROSION OF THE ALUMINUM UNDER THSDR GTIA020920Structure · corrodedFTW - FOUND RIGHT ELEVATOR ANTI-FLOAT TAB LOWER SURFACE LE HAS CORROSIN FROM INBOARD SIDE TO OUTBOARD SIDE. MATERIAL LOSS FOUND TO BE OUT OF LIMITS. REMOVED RIGHT ELEVATOR ANTI-FLOAT TAB. INSTALLED RIGHT ELEVATOR ANTI-FLOAT TAB. (M)SDR GTIA020919Skin · delaminatedFTW - FOUND RT ELEVATOR CONTROL TAB IS DELAMINATED UPPER LOWER. REMVOED RIGHT ELEVATOR CONTROL TAB. TAB HAS CORROSION DAMAGE TO FRONT. REPLACED CONTROL TAB. INSTALLED RIGHT ELEVATOR CONTROL TAB. (M0SDR GTIA020918Skin · delaminatedFTW - FOUND LEFT ELEVATOR GEAR TAB DELAMINATED LOWER SURFACE AT 1/B AND OUTBOARD SIDES. REMOVED GEARED TAB. REPAIRED LEFT ELEVATOR GEARED TAB. INSTALLED GEARED TAB ON LEFT ELEVATOR. (M)SDR GTIA020917Skin · delaminatedFTW - FOUND LEFT ELEVATOR CONTROL TAB UPPER SURFACE DELAMINATED AT 2/3 HINGE FITTINGS. REMOVED LEFT ELEVATOR CONTROL TAB. REPAIRED LEFT ELEVATOR CONTROL TAB. INSTALLED LEFT ELEVATOR TAB. (M)SDR CUX2002F00001Skin · crackedRIGHT ELEVATOR TRIM TAB OUTER SKIN WAS DISCOVERED CRACKED AT THE UPPER INBOARD AFT CORNER DURING A ROUTINE PHASE 1 INSPECTION. THE CRACK BEGAN AT A SKIN ATTACH COUNTER SUNK RIVET AND EXTENDED FORWARD AND FAT APPROXIMATELY .350 INCH IN EACH DIRECTION. THE TABSDR SWAA021537Hinge · wornDURING SCHEDULED SERVICE CHECK, SWA SI 11038-55, BOTH LT AND RT ELEVATOR TABS FAILED FREE PLAY CHECK. REMOVED AND REPLACED HARDWARE AT ALL HINGE ATTACH POINTS PER MM.SDR AUS20020613Bearing · worn(AUS) LT AND RT ELEVATOR TAB BEARINGS WORN BEYOND LIMITS. FOUND DURING INSPECTION IAW SB B737-55A 1070.SDR SWAA021284Bushing · wornDURING SCHEDULED SERVICE CHECK, SWA SI 11111-55, LT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR TAB BUSHINGS PER MM.SDR SWAA021275Bushing · wornDURING SCHEDULED SERVICE CHECK, SWA SI 11038-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED TAB HINGE BUSHINGS AT NR 2, 3 AND 4 HINGES PER MM.SDR SWAA021280Bushing · wornDURING SCHEDULED C3 CHECK, SWA SI 11111-55, FOUND LT ELEVATOR TAB CONTROL MECHANISM FWD LINKS WORN. REMOVED AND REPLACED LT ELEVATOR LINKS AND BUSHINGS PER MM.SDR COOSDR02154Tab · delaminatedLEFT ELEVATOR TAB (PN 6572799-43)(SN 74084) UPPER AND LOWER SKIN DELAMINATED.SDR COOSDR02103Skin · damagedHORIZONTAL STABILIZER RIGHT ELEVATOR GEAR TAB SKIN, INTERNAL DOUBLERS AND HONEY COMB CORE DAMAGE.SDR COOSDR02127Tab · delaminatedELEVATOR TAB DELAMINATED.SDR HNAA0300070Tab · damagedREPAIR TO ELEVATOR SPRING TAB TRAILING EDGE.SDR P2EA2002V0036Tab · delaminatedDURING C1+C2 INSPECTION:-L-H ELEVATOR GEAR TAB, UPPER SKIN DELAMINATED AT Sta. XET116.-REPAIRED ELEVATOR GEAR TAB P/N 5910414-403, S/N 583KDL DUE TO DELAMINATION IAW COOPESA E.O. No. COO-CMP-9-55-274-02, DATED MAY 09,2002 & DOCUMENTED ON FAA 8110-3 FORM.NOTE: SDR 2002F00650Trim Tab · crackedDURING ELEVATOR TAB HINGE INSPECTION, FOUND .3125 INCH CRACK ON LEFT ELEVATOR TRIM TAB ON TOP SIDE BY NUMBER TWO HINGE. REMOVED AND REPLACED ELEVATOR TRIM TAB. (M)SDR RYN2003F00007Tab · brokenON CLIMBOUT, FLIGHT CREW NOTED AIRFRAME VIBRATION. REDUCING THRUST ON BOTH ENGINES HAD NO EFFECT. FLIGHT CREW SELECTED FLAPS FIVE DEGREE POSITION DURING LANDING AND VIBRATION STOPPED, PERFORMED OVERWEIGHT LANDING WITHOUT INCIDENT. POST FLIGHT INSPECTION REVSDR 2002F00627Trim Tab · damagedON CLIMB-OUT FROM MBJ, FLIGHT CREW NOTED AIR FRAME VIBRATION. REDUCING THRUST ON BOTH ENGINES HAD NO EFFECT. FLIGHT CREW SELECTED FLAPS FIVE DEGREE POSITION DURING LANDING AND VIBRATION STOPPED. PERFORMED OVERWEIGHT LANDING IN MIA WITHOUT INCIDENT. POST FLSDR GTIA020452Trim Tab · delaminatedFTW - LEFT ELEVATOR ANTI-FLOAT TAB HAS THREE DENTS AND AREAS OF DELAMINATION. REMOVED ANTI-FLOAT TAB. INSTALLED LEFT ELEVATOR ANTI-FLOAT TAB. (M)SDR SWAA020876Tab · crackedDURING SCHEDULED A1 CHECK, FOUND LT ELEVATOR TAB INBD CONTROL ROD ATTACH POINT CRACKED. REMOVED AND REPLACED LT ELEVATOR TAB PER MM.SDR SWAA020855Tab · crackedDURING SCHEDULED 1/4D CHECK, FOUND RT ELEVATOR TAB CRACKED AT NR 4 HINGE. REMOVED AND REPLACED RT ELEVATOR TAB PER MM.SDR DHL2002726515Tab · puncturedDURING C-CHECK, LT AND ELEVATOR CONTROL TAB SHOW PUNCTURED HOLE TOP SIDE STA 73.0 APPROX. CUT OUT PUNCTURED AREA ON LT ELEVATOR TAB, IAW B-727 SRM 55-20-1 FIG 1 AND 51-40-10 FIG 2. INSTALLED REPAIR IAW B-727 SRM 51-40-10 FIG 2. OPS CHECK GOOD IAW B-727 MM 2SDR CA020422006Structure · damaged(CAN) DURING REGULAR SCHEDULED MAINTENANCE INSPECTION (AD:02-01-01)THE RT ELEVATOR FAILED THE TAB HINGE FREEPLAY CHECK AT THE NR 2 ELEVATOR TAB HINGE POSITION - SUSPECTED CRACK AT ELEVATOR REAR SPAR. EDDY CURRENT INSPECTION CARRIED OUT ON RT ELEVATOR REAR SPARSDR GTIA020432Trim Tab · corrodedFTW - FOUND LEFT ELEVATOR CONTROL TAB BOTTOM SIDE HAS TWO OUTBOARD WEEP HOLES CORRODED. REMOVED LEFT ELEVATOR CONTROL TAB. INSTALLED CONTROL TAB ON LEFT ELEVATOR. (M)SDR LR7A02027Horn · crackedDURING SCHEDULED B3 INSPECTION, FOUND LT ELEVATOR TRIM TAB INBOARD AFT HORN BRACKET CRACKED AT HSS 99, FS 1153, WL 277. REPLACED HORN ASSY IAW SMP 581 91-00. OPERATIONAL CHECK AND RIGGING COMPLIED WITH IAW SMP 581 27-31 PG 218 AND 201.SDR C2XA02TY034Lever · gougedTYS DURING A SCHEDULED 1-C INSPECTION THE RT SERVO TAB DOG BONE WAS FOUND WEARING INTO THE ELEVATOR SUPPORT BRACKET WHICH REQUIRED A GST. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF THE INSPECTION.SDR C2XA02TY033Lever · gougedTYS DURING A SCHEDULED 1-C INSPECTION THE LT SERVO TAB DOG BONE WAS FOUND WEARING AGAINST THE ELEVATOR SUPPORT BRACKET, WHICH REQUIRED A GST. ALL WORK WAS ACCOMPLISHED IAW GST-0522/02 AND WILL BE RELEASED UPON COMPLETION OF THE INSPECTION.SDR AUS20020240Balance Weight · corroded(AUS) RH ELEVATOR TAB CENTRE BALANCE WEIGHT SPLIT OPEN DUE TO CORROSION.SDR SWAA020132Tab · delaminatedDURING SCHEDULED SPECIAL VISIT, FOUND LT ELEVATOR TAB DELAMINATED ON TOP T/E. REMOVED AND REPLACED ELEVATOR TAB PER MM.SDR CA020131009Stop · deteriorated(CAN) DURING CREW WALKAROUND, THEY NOTICED DAMAGE TO LT TRAILING EDGE OF THE ELEVATOR SPRING TAB. THE DAMAGE TO THE TAB WAS INBOARD, ADJACENT TO THE RUDDER. THE TRAILING RUDDER WAS ALSO DAMAGED FROM CONTACT WITH ELEVATOR SPRING TAB. THE LT ELEVATOR SPRING TAB SDR RIVA011217Tab · delaminatedRIGHT ELEVATOR TAB DELAMINATED AT AFT OUTBOARD END. REMOVED DELAMINATED AREA OF SKIN .75 INCH BY .75 INCH IAW BOEING SRM 51-40-20 FIG 20. FABRICATED AND INSTALLED DOUBLER IAW BOEING SRM 51-40-20 FIG 20. (M)SDR GTIA020152Tab · delaminatedFTW - FOUND RIGHT ELEVATOR ANTI-FLOAT TAB TOPSIDE HAS AREA OF DELAMINATION. BONDED REPAIR DOUBLER IAW DC9 MD80 SRM 51-70-2. (M)SDR EISA20010137Trim Tab · damagedL/H ELEVATOR TRIM TAB HAS ELONGATED HOLES AT FWD HINGE POINT.FOUND DURING 'D' CHK.CORRECTIVE ACTION:FAB AND INSTALLED REPAIR DOUBLER IAW B727-55-20-2. WEIGH AND BALANCE IAW B727 SRM 51-80-9 FIG. 2.SDR DL738011887Skin · erodedWHILE ACCOMPLISHING INSPECTIONS OF THE LT ELEVATOR TAB PER AD 2001-08-09 & 2001-14-05, A SMALL AREA OF EROSION WAS FOUND ON THE UPPER SKIN OF TRAILING EDGE. THE DAMAGE WAS REPAIRED WITH A SEALING REPAIR PER THE B737-800 SRM AND APPROVED/DOCUMENTED PER ER/A SDR AUS20011366Cap · dislodged(AUS) ELEVATOR BALANCE HORN BLANKING CAP DISLODGED AND RESTRICTED ELEVATOR MOVEMENT. FOD.SDR MWEA011420Skin · dentedLEFT HAND ELEVATOR CONTROL TAB UPPER SURFACE HAS A DENT BETWEEN THE NR 3 AND NR 4 HINGE POINTS, .75 BY .5 INCH. FABRICATED CORE, FILLER AND DOUBLER. HOT BONDED REPAIR AND REPAINTED TRIM TAB. PERFORMED WEIGHT AND BALANCE.SDR C2XA01TY159Tab · damagedTYS DURING A SCHEDULED INSPECTION THE RIGHT HAND ELEVATOR SPRING TAB WAS FOUND TO BE DAMAGED ON THE TRAILING EDGE. MAINTENANCE ACCOMPLISHED A COMPOSITE REPAIR IAW EMB-145 SRM 51-70-01 AND EMB-145 CPM 51-21-05, 51-21-06. THE AIRCRAFT WILL BE RELEASED UPON COMSDR SWAA012791Tab · delaminatedDURING SCHEDULED 1/4D CHECK, FOUND RH ELEVATOR TAB DELAMINATED NEAR OTBD HINGE ON LOWER SIDE. R&R TAB PER MM.SDR CA011004005Attach Fitting · cracked(CAN) DURING INSPECTIONS FOUND THAT ELEVATOR SERVO TAB HAD TWO SHEARED OFF RIVETS UPPER FORWARD ENGINE AT ARM ATTACHMENT BLOCK AND CRACK AT LOWER BETWEEN RIVET HOLES ON ELEVATOR SERVO TAB.SDR MWEA011273Tab · damagedLEFT ELEVATOR STUCK BY TAIL OF 812ME DURING PUSH BACK. -- OUTBOARD TRAILING EDGE OF TAB WAS CHIPPED. REPAIRED IAW SRM (HOT BOND).SDR GTIA010967Tab · dentedFTW - RIGHT ELEVATOR GEAR TAB HAS MANY DENTS. CLEANED DENTS. REPAIRED DENTS ON RIGHT ELEVATOR GEAR TAB IAW MD-80 SRM 55-04. (M)SDR GTIA010937Skin · dentedFTW - RIGHT ELEVATOR CONTROL TAB HAS MANY DENT (TOP SIDE). CLEANED DENT AREAS 6 ON RIGHT INBOARD ELEVATOR CONTROL TAB IAW DC9/MD-80 SRM 55-04 PAR 5B. REPAIRED DENTS ON RIGHT ELEVATOR CONTROL TAB IAW DC9 MD80 SRM 55-04. (M)SDR DHL2001727622Skin · delaminatedON "C" CHECK DISCREPANCY----- LT ELEVATOR TAB T/E DELAMINATED.
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