JASC 5521

Service difficulty reports · 520

Reports filed under 5521 · Elevator, 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 = '5521'
  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 AWXA200600019Structure · damagedDURING POST FLIGHT INSPECTION DISCOVERED A 6 INCH PIECE OF ALUMINUM STICKING UP FROM TRAILING EDGE OF LT ELEVATOR. TEMP REPAIR WAS PERFORMED AND AIRCRAFT WENT ON A ONE-TIME FERRY FLIGHT FOR PERMANENT REPAIR. MAINTENANCE REPAIRED LT ELEVATOR BY REMOVING CONDUJan 8, 2006 · N908AW · Boeing 7572G7SDR CA061201005Rib · cracked(CAN) WHILE PERFORMING AD CF-82-21 R1 USING A BORESCOPE, CRACKS WERE FOUND AT THE ATTACHMENT POINT OF THE TORQUE TUBE TO THE ELEVATOR RIB. SEE PHOTOS AND DAMAGE REPORT. (TC NR 20061201005)Dec 28, 2005 · Dhav DHC6200SDR AU510001985Spar · crackedLT ELEVATOR REAR SPAR CRACKED. FOUND DURING INSPECTION IAW AD/B727/100.Dec 12, 2005 · Boeing 727277SDR 05FDEA04177Rib · gougedWHILE WORKING CARD NR N00763 FOUND RT NR 5 ELEVATOR HINGE, SUPPORT RIB L/E GOUGED. REPAIRED RIB PER FED EX EA 7-5510-91427.Dec 8, 2005 · N485FE · Boeing 727200SDR CA051124002Spar · corroded(CAN) SEVERE CORROSION ON FACE OF SPAR UNDER BALANCE WEIGHT. AIRCRAFT IS A FLOAT PLANE.Nov 21, 2005 · Cessna 208SDR 2005FA0001559Bushing · seizedDURING COMPLIANCE WITH ELEVATOR TAB TO ACTUATOR PUSHROD INSPECTION FOR SAFETY NR 243, FOUND ELEVATOR TAB HORN BUSHING SEIZED. REPLACED TAB HORN BUSHING AND ACTUATOR PUSHROD TO HORN ATTACH BOLT BUSHING, VERIFIED TAB HORN TO ACTUATOR PUSHROD OPERATIONS NORMAL INov 16, 2005 · N439PW · Beech C90ASDR ASAA0510324Clevis · corrodedCORROSION ON VERTICAL STABILIZER AFT SPAR LT FAIL SAFE CLEVIS FACES NOT PARALLEL TO EACH OTHER. FACES MACHINED IAW EA. (K)Sep 22, 2005 · N740AS · Boeing 737290CSDR CA050607005Spar · cracked(CAN) WAS REPLACING RT ELEVATOR SKIN DUE TO HINGE WEAR (OB HINGE POINT IS PART OF SKIN). CRACKS WERE FOUND ON THE SPAR P/N 0432001-21 UNDER IB HINGE BRACKET P/N 0432001-72. THESE CRACKS COULD NOT BE SEEN THRU VISUAL INSPECTION ON THE FORWARD SIDE OF THE SPAR. Jun 7, 2005 · Cessna 152SDR QXEA200500705Rib · chafedPDX - RIGHTHAND ELEVATOR HORN, INBOARD CLOSING RIB HAS CHAFE DAMAGE ON TOP SURFACE. REPAIRED IAW DHC-8 200 SRM 51-00-02, 51-20-36 AND SRM 51-20-51.Apr 13, 2005 · N346PH · Dhav DHC8202SDR QXEA200500704Rib · chafedPDX - LEFT ELEVATOR HORN, INBOARD CLOSING RIB HAS CHAFE DAMAGE AT TOP AND BOTTOM. REPAIRED IAW DHC-8 200 SRM 51-20-11, 51-20-16 AND SRM 51-20-57.Apr 13, 2005 · N346PH · Dhav DHC8202SDR 05FDEA00492Rib · damagedUPON REMOVAL OF EXISTING REPAIR ON N/R N00817 ON RT ELEVATOR INBOARD T/E LWR SURFACE FOUND 2EA AREAS OF CORROSION .5 X .5 INCH 1 ON INBOARD SIDE OF REPAIR, 1 ON OUTBOARD SIDE OF REPAIR (RIB 5 AND RIB 9). REMOVED CORROSION PER A310-200 SRM 51-74-10, 1EA AREA IMar 10, 2005 · N446FE · Airbus A310222SDR CA050227001Rib · cracked(CAN) DURING ROUTINE INSPECTION THE AME FOUND THE TIP RIB ON THE RT ELEVATOR CRACKED. THE CRACK WAS LOCATED IN THE BEND WHERE THE RIB TRANSITIONS INTO THE FLANGE AT RIVET NR7 FROM THE TRAILING EDGE. UPON REMOVAL IT WAS DISCOVERED THAT THESAME CRACK COULD BE FFeb 27, 2005 · Piper PA31350SDR CA050204001Support · cracked(CAN) ONE SCREW HOLE HAS 2 QUARTER INCH CRACKS RADIATING OUT BUT STOPPING BEFORE REACHING PART EDGE. PROBLEM FOUND FROM NDT TESTING FOR THE 1000 HOUR REQUIREMENT IN MM FOR ELEVATOR TORQUE TUBES. THIS PART IS MADE OUT OF MAGNESIUM, IF MANUFACTURER WOULD CHANGEJan 28, 2005 · Beech 100BEECHSDR 04FDEA03505Rib · crackedRIGHT HORIZONTAL STAB ELEVATOR STATION 17.20, INBOARD RIB CRACK RUNS FROM RIVET ON UPPER. REMOVED RIB IAW SRM 51-30-2 & SB 727-55A0091. INSTALLED NEW RIB WITH P/N 65-17428-6 IAW SRM 51-30-2 & SB 727-55A0091.Dec 29, 2004 · N151FE · Boeing 727100SDR 04FDEA03033Rib · crackedRT ELEVATOR NR 5 HINGE SUPPORT RIB ELEVATOR STA 136.50 PREVIOUS REPAIR AT I/B LOWER FLANGE IS CRACKED. REPLACED PER E.O. 7-5510-7-5001 PT 2.Nov 8, 2004 · N166FE · Boeing 727100SDR GAIA04105Spar · looseDURING C-CHECK INSPECTION FOUND LT ELEVATOR REAR SPAR HAS 3 EA. LOOSE TAB HINGE FITTINGS. REF FASI NR 86375, REPLACED LT ELEVATOR REAR SPAR IAW SB 727-55-0089, REV 1.Sep 10, 2004 · N180AX · Boeing 727222SDR GAIA04104Spar · crackedDURING C-CHECK INSPECTION FOUND RT ELEVATOR REAR SPAR CRACKED. REF FASI NR 86374 REPLACED RT ELEVATOR REAR SPAR IAW SB 727-55-0089, REV 1.Sep 10, 2004 · N180AX · Boeing 727222SDR CA040915009Gusset · cracked(CAN) LT TOP ELEVATOR TIP GUSSET (LOCATED BETWEEN ELEVATOR TIP SKIN AND ELEVATOR SPAR) WAS FOUND CRACKED DURING INSPECTION. NOTE: THE PROPELLER WAS REMOVED AND OVERHAULED, AFTER 30.0 HRS SMOH,THE PROPELLER WAS REMOVED FOR REBALANCING DUE TO VIBRATION ISSUES.Aug 26, 2004 · Dhav DHC2*SDR CA040831003Rib · cracked(CAN) DURING REGULAR 100 HOUR INSPECTION AD CF-80-25 COMPLETED AND CRACK FOUND ON LT ELEVATOR IB RIB AT ATTACHMENT BOLT. CRACK WAS LARGER AND MORE VISIBLE ON DOUBLER. REMOVAL OF DOUBLER REVEALED CRACK ON RIB AS WELL. RIB REPLACED AND DOUBLER TOO.Aug 13, 2004 · Dhav DHC2*SDR MV5R055NARib · crackedREMOVED LT ELEVATOR FOR CRACKED OB RIB PN 430004 AND DAMAGED SKIN. SENT FOR RESKINED THE ELEVATOR WITH OUT CHANGING THE RIB. RETURNED THE ELEVATOR TO GET THE RIB CHANGED AND THEY INSTALLED .2500 INCH HYLOCK FASTENERS IN THE BALANCE WEIGHT INSTEAD OF .1875 IRJun 25, 2004 · N6034Q · Mooney M20CSDR IXXA060387SSpar Cap · corrodedDURING ROUTINE C CHECK, FOUND RIGHT ELEVATOR LOWER SPAR CAP CORRODED FROM STATION XE32 TO XE285. REPAIRED PER ALL APPLICABLE DATA.Jun 16, 2004 · N41CX · Doug DC862FSDR 2004UALA00548Rib · lightning strikeRIGHT ELEVATOR RIB 10 WAS DAMAGED BY LIGHTNING. REPLACED RIB AND INSTALLED BLIND FASTENERS.Jun 4, 2004 · N433UA · Airbus A320232SDR 2004UALA00547Rib · lightning strikeLEFT ELEVATOR RIB 10 WAS DAMAGED BY LIGHTNING. REPLACED RIB AND INSTALLED BLIND FASTENERS.Jun 4, 2004 · N433UA · Airbus A320232SDR 04FDEA00761Rib · corrodedUPON REMOVAL OF RIGHT DETACHABLE ELEVATOR LOWER INBOARD ACCESS PANEL NR 345BB FOUND STA XE53.50 LOWER INBOARD MOUNTING FLANGE CRACKED. COMPLIED WITH FEDEX EA 1-5520-75973, STABILIZERS - ELEVATORS RT INBOARD ELEVATOR RIB REPAIR.Mar 27, 2004 · N579FE · Doug MD11SDR 2004FA0000193Spar · crackedDURING ANNUAL INSPECTION WHAT APPEARED TO BE A DENT WAS FOUND ON THE LOWER LEADING EDGE SKIN OF THE LEFT ELEVATOR. THIS (DENT) WAS CROSSED BY A CRACK. EXCESSIVE MOVEMENT OF THE ELEVATOR HORN WAS NOTED WHEN THE ELEVATOR WAS FLEXED. FURTHER INSPECTION REVEALED Feb 11, 2004 · N6465A · Cessna 182SDR 2004FA0000192Spar · crackedDURING ANNUAL INSPECTION WHAT APPEARED TO BE A DENT WAS FOUND ON THE LOWER LEADING EDGE SKIN OF THE LT ELEVATOR. THIS (DENT) WAS CROSSED BY A CRACK. EXCESSIVE MOVEMENT OF THE ELEVATOR HORN WAS NOTED WHEN THE ELEVATOR WAS FLEXED. FURTHER INSPECTION REVEALED A CFeb 11, 2004 · N6465A · Cessna 182SDR LR7A04023Rib · crackedDURING SCHEDULED C5 INSPECTION PER JOB CARD HC5511 FOUND AFTER T/E SKIN REMOVAL, RIB FORMER CRACKED AT HSS77 LT ELEVATOR. RIB FORMER REPLACED IAW SMP583 CHP 51-60 & 51-70, HSS77 LT.Jan 24, 2004 · N402LC · Lkheed 382GSDR DL73S040033Spar · damagedRIGHT ELEVATOR REAR SPAR FOUND DAMAGED AT OUTBOARD END. REPAIR ACCOMPLISHED FROM ELEV STA 88 TO OUTBOARD END PER ER/A 426886-14.Jan 13, 2004 · N382DL · Boeing 737247SDR MV5R0551Rib · crackedCRACKED OB RIB PN 430004 AND DAMAGED SKIN.Jan 9, 2004 · N6034Q · Mooney M20CSDR 04FDEA00033Rib · crackedSTABILIZER- ELEVATOR HINGE SUPPORT RIB INSPECTION S/B 727-55A0091, COMPLY WITH EO 7-5510-7-5001 REV B1 POS PT2.Jan 5, 2004 · N193FE · Boeing 727100SDR GAIA03134STSpar · crackedDURNG C-CHECK INSPECTION FOUND LEFT ELEVATOR REAR SPAR CRACKED NEAR NR 3 HINGE FITTING. REF FASI N/R NR 61506, REPLACED LEFT ELEVATOR REAR SPAR IAW S/B 727-55-0089 REV 1. (M)Oct 24, 2003 · N1269Y · Boeing 727243SDR AUS20031077Rib · cracked(AUS) RT ELEVATOR FORWARD RIB CRACKED AT TORQUE TUBE OUTBOARD MOUNTING FLANGE. RIB CONTAINS TWO CRACKS FROM TOP AND BOTTOM ATTACHMENT RIVETS.Oct 22, 2003 · Gulstm 500SSDR CA031006004Rib · cracked(CAN) UPON REMOVAL OF LOOSE SKIN RIVETS (AFT OF BALANCE WEIGHT, OUTBOARD OF HINGE), AN ENLARGED HOLE WAS OBSERVED WITH APPARENT CRACKING OF THE UNDERLYING RIB. UPON FURTHER INVESTIGATION, RIB P/N 50-610000-415 WAS FOUND CRACKED ALONG THE BEND RADIUS IN 3 OUT Sep 29, 2003 · Beech C90ASDR AUS20031078Rib · cracked(AUS) RT ELEVATOR FORWARD RIB CRACKED AT TORQUE TUBE OUTBOARD MOUNTING FLANGE. RIB IS CRACKED IN TWO PLACES FROM TOP AND BOTTOM ATTACHMENT RIVETS.Sep 12, 2003 · Gulstm 500SSDR GAIA03098Rib · crackedDURING B-2 CHECK, FOUND RIGHT ELEVATOR SUPPORT RIB STATION 17.2 CRACKED. REF FASI N/R 53208, REPLACED ELEVATOR SUPPORT RIB PER S/B 727-55A0091. (M)Sep 10, 2003 · N6806 · Boeing 727223SDR CA030915005Spar · cracked(CAN) LT ELEVATOR FRONT SPAR UPPER ATTACH HOLE FOR CENTRE HINGE HAS A SMALL RADIAL CRACK AROUNG THE UPPER AN3 BOLT HOLE.Aug 7, 2003 · Dhav DHC2MK1SDR CA030915004Spar · cracked(CAN) LT AND RT ELEVATOR FRONT SPAR UPPER ATTACH HOLE FOR CENTRE HINGE POSITION HAS A SMALL CRACK(S) AROUND THE UPPER AN3 BOLT HOLE.Aug 7, 2003 · Dhav DHC2MK1SDR AUS20030786Rib · cracked(AUS) ELEVATOR END RIB CRACKED. FOUND DURING INSPECTION IAW SB-190.Jul 28, 2003 · Bnorm BN2A26SDR CA030915003Spar · cracked(CAN) LT AND RT ELEVATOR FRONT SPAR UPPER ATTACH HOLES FOR CENTER HINGE POSITION HAS A SMALL CRACKS AROUND THE UPPER AN3 BOLT HOLE.Jul 14, 2003 · Dhav DHC2MK1SDR DHL2003747511Spar · crackedDURING "C" CHECK N/R 53401 RT. ELEVATOR REAR SPAR AT ELEVATOR STATION 99.79 HAS A CRACK IN THE LOWER RADIUS. ( VERIFIED WITH HFEC) REMOVED AND REPLACED RT ELEVATOR REAR SPAR IAW S/B 727-55-0059 P/N 65C30825-24 PO 312612.May 11, 2003 · N747DH · Boeing 727224SDR 200FA0000645Rib · crackedEND RIB CRACKED SEVERAL PLACES. FWD SPAR, INBOARD END CRACKED.Apr 11, 2003 · N355JS · Beech E90SDR W0P2003F00000Rib · corrodedUPON COMPLYING WITH AD, FOUND CORROSION TO HAVE SEVERELY EATEN AWAY THE TIP RIB ON FOUR DIFFERENT ELEVATORS.Mar 25, 2003 · N9290Z · Dhav DHC2MK1SDR DHL2003741549Spar · crackedDURING C-CHECK, LT ELEVATOR NR 3 TAB HINGE LOOSE, INDICATION OF CRACK. REMOVED DAMAGED SPAR AND INSTALLED NEW P/N 65C30825-23 PO 307748 PER S/B 727-55-0089 R1. OP'S CHECK GOOD IAW M/M 27-30-00.Mar 24, 2003 · N741DH · Boeing 727200SDR AUS20030314Spar · corroded(AUS) RT ELEVATOR CORRODED IN AREA OF TORQUE TUBE. CAUSED BY LACK OF PRIMER DURING ASSEMBLY. INSPECTION ALSO FOUND RACKS FOUND EMANATING FROM UPPER AND LOWER RIVET HOLES EXTENDING TOWARDS INBOARD END OF ELEVATOR SPAR AND OUTBOARD END. UPPER RIVET CRACK18.9MM (Mar 11, 2003 · Cessna 152SDR AUS20030313Spar · cracked(AUS) ELEVATOR SPAR CRACKED AROUND UPPER RIVET HOLE FOR HINGE BRACKET ATTACHMENT. CRACK LENGTH 30.04MM (1.183IN). CRACK TRAVELS INBOARD AND OUTBOARD FROM RIVET HOLE.Mar 10, 2003 · Cessna 152SDR DHL2003740527Spar · crackedRT ELEVATOR TAB HAS 3 O/B HINGES LOOSE AT ELEVATOR REAR SPAR ATTACH POINT, CHECK FOR SPAR CRACKS PER S/B 55-0089. REMOVED DAMAGED SPAR AND INSTALLED NEW SPAR (P/N 65C30825-24) PO 301742 IAW S/B 727-55-0089 FIG 6 AND SUPPORT FITTINGS.Feb 26, 2003 · N740DH · Boeing 7272Q9SDR P5CA0300803Panel · delaminatedELE LEFT NR 334 ML HONEYCOMB PANEL INBOARD SURFACE HAS DELAMINATION. REPAIRED BY BONDING FIBERGLASS PLIES USING VACCUM BAG PER SRM 51-40-09.Jan 27, 2003 · N921FT · Boeing 747283BSDR UPS03240055Spar · crackedINSPECTION TYPE: C, DURING REPLACEMENT OF RT O/B RIB FOR ELEVATOR STA 209.5 LWR REAR SPAR FOUND TO BE CRACKED BETWEEN TWO FASTENERS AT O/B EDGE OF SPAR. REPAIRED IAW SRM 55-10-5 FIG 1.Jan 10, 2003 · N934UP · Boeing 72721CSDR LC12003F00000Rib · crackedDURING COMPLIANCE WITH SB FOR ELEVATOR RIVET INSTALLATION, THE ELEVATOR TOP, BOTTOM, AND TIP SKINS WERE CRACKED AND THE TIPS COULD BE FLEXED EASILY UP AND DOWN. AFTER REMOVING THE PLASTIC TIPS TO ACCOMPLISH THE SERVICE BULLETIN, IT WAS NOTED THAT THE ELEVATORNov 29, 2002 · N7275H · Cessna 182SSDR 2002FA0001264Spar · crackedFOUND CRACK EXTENDING ABOUT.5 INCH FROM OUTBOARD HINGE POINT TO SPAR ATTACHMENT.Oct 21, 2002 · N94268 · Cessna 152
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