JASC 5522

Service difficulty reports · 3,272

Reports filed under 5522 · Elevator, Plate/Skin, 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 = '5522'
  ORDER BY difficulty_date DESC"

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SDR 2020F00458Skin · dentedRIGHT HAND HORIZONTAL STABILIZER, LEADING EDGE, ELEVATOR STATION 90 + -, JUST OUTBOARD OF PREVIOUS REPAIR, DENTED.Nov 5, 2020 · N303KH · Boeing 737319SDR T17A20200811042Skin · crackedSUPPLEMENTAL INFORMATION, RT ELEVATOR OUTBOARD COVER HAS A CRACK. INSTALLED NEW ACCESS PANEL, IAW BEECHJET 400XP AMM CH 27-30-00.Oct 30, 2020 · N489TM · Beech 400ASDR ANCF20210113006Skin · damagedN284AV FLIGHT AV8598 PSO-BOG. DURING WALKAROUND AT BOG, EVIDENCE OF DAMAGES BY FOD WERE FOUND ON RT THS AND RT ELEVATOR, IAW AMM 05-51-14-200-803-A. INSPECTION OF THE AIRCRAFT AFTER A BIRD STRIKE AND/OR FOD WAS PERFORMED. EVIDENCE OF DAMAGE BY FOD (STONE-ROOct 28, 2020 · N284AV · Airbus A320214SDR FDEA202010242639Skin · scratchedRT INBOARD ELEVATOR TRAILING EDGE HAS A SCRATCH 2" FRIM INBOARD EDGE AND 9.25" FROM TRAILING EDGE. REPAIRED SCRATCH ON RIGHT HAND INBOARD ELEVATOR TRAILING EDGE AND RESTORED PAINT FINISH, IAW B767 SRM 51-70-17 PARA 4G AND FEDEX EA H-5520-T0357497-P1. STABILIOct 24, 2020 · N145FE · Boeing 7673S2FSDR FDEA202010242638Skin · puncturedSMALL PUNCTURE ON TOP SURFACE OF ELEVATOR APPROXIMATELY 20.5 IN. FROM INBOARD EDGE AND APPROXIMATELY 11.25 IN. FROM ELEVATOR TRAILING EDGE REPAIRED PUNCTURE ON TOP SURFACE OF ELEVATOR AND RESTORED PAINT FINISH, IAW B767 SRM 55-20-01 FIG 201 AND SRM 51-70-17-Oct 24, 2020 · N145FE · Boeing 7673S2FSDR IPXA2020100961103Skin · dentedINSPECTION TYPE: C RT ELEVATOR UPPER SURFACE 1 EA DENT AT APPROX 18" OUTBOARD OF ER 13 AND 15" FROM L/E. REPAIRED IAW A300-600 SRM 55-21-12 PAR 5 H AND SRM 51-77-12 PAR 3 G.Oct 8, 2020 · N172UP · Airbus A300F4622RSDR IPXA2020100961102Skin · dentedINSPECTION TYPE: C RT ELEVATOR UPPER SURFACE 1 EA DENT APPROX AT 40" OUTBOARD OF ER 13 AND 14 FROM LE. REPAIRED IAW A300-600 SRM 55-21-12 PAR 5H AND SRM 51-77-12 PAR 3G.Oct 8, 2020 · N172UP · Airbus A300F4622RSDR LR7A2020100502645Skin · damagedDURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5511, FOUND THE LT ELEVATOR UPPER SKIN WITH LOOSE RIVET AND ELONGATED HOLE AT HSS67L, FS 1152, WL 285. REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-10 NR 7708.Oct 5, 2020 · N410LC · Lkheed 382GSDR ANCF20210115007Skin · damagedN740AV FLIGHT 8598 PSO-BOG DURING WALK AROUND AT BOG, EVIDENCE OF DAMAGES BY FOD WERE FOUND ON RT THS AND RT ELEVATOR, IAW AMM 05-51-14-200-803-A. INSPECTION OF THE AIRCRAFT AFTER A BIRD STRIKE AND/OR FOD WAS PERFORMED. EVIDENCE OF DAMAGE BY FOD (STONE-ROCK-Oct 4, 2020 · N740AV · Airbus A320214SDR IPXA2020101761381Rib · crackedINSPECTION TYPE: 2C CRACK ON LT DETACHABLE ELEVATOR INBOARD LEADING EDGE RIB AT LOWER NUTPLATE FLANGE AT XE=53.5. REPAIRED CRACKED RIB ON LT DETACHABLE ELEVATOR INBOARD LEADING EDGE STA XE=53.5, IAW EA 011-5520-01-A8596 AND EO MD11-5520-78207-A. (MAJOR)Oct 3, 2020 · N253UP · Doug MD11FSDR DALA2020092703180Skin · puncturedDURING INSPECTION FOUND PUNCTURE OUTBOARD RIB AND BROKEN LOWER SKIN ON LT ELEVATOR OUTOARD EDGE. LT ELEVATOR OUTBOARD EDGE SKIN WAS REPAIRED, PER B-737-800 SRM 51-70-05-2R-10 PARAGRAPH 4 A TO H (IN REFERENCE B737-800 SRM 55-20-01-2R-1 PAR 4 D TABLE 202). LT Sep 26, 2020 · N380DA · Boeing 737832SDR FDEA202009252327Skin · damagedRT ELEVATOR HAS WATER INGRESS AND VISIBLE DAMAGE 34 1/2" FROM ER 13 AND 22 1/4" FROM THE T/E. INDICATION MEASURES APPROXIMATELY 1" IN DIAMETER, DOT 151-02. REPAIRED RT ELEVATOR WATER INGRESS, IAW SRM 55-21-12-201 PARA 5H FIG 211, MAJOR REPAIR.Sep 25, 2020 · N677FE · Airbus A300F4605RSDR FDEA202009242317Skin · damagedLT ELEVATOR HAS WATER INGRESS AND DELAMINATION 8" FROM THE INBOARD EDGE OF ER 2 AND 11" FROM THE T/E DELAMINATION/WATER INDICATION MEASURES APPROXIMATELY 1" IN DIAMETER, DOT 151-04. REPAIRED LT ELEVATOR WATER INGRESS, IAW SRM 55-21-12-201 PARA 5H FIG 211, MAJSep 24, 2020 · N677FE · Airbus A300F4605RSDR FDEA202009242315Skin · damagedRT ELEVATOR HAS WATER INGRESS AND VISIBLE DAMAGE 13" FROM THE INBOARD EDGE OF ER 2 AND 21 1/4" FROM THE T/E AND MEASURES APPROXIMATELY 1" IN DIAMETER, DOT 151-01. REPAIRED RT ELEVATOR WATER INGRESSION, IAW SRM A300-600 55-21-12-201 PARA 5H FIG 211, MAJOR REPASep 24, 2020 · N677FE · Airbus A300F4605RSDR FDEA202009242314Skin · damagedLT ELEVATOR HAS WATER INGRESS 13 1/2" FROM ER 2 AND 12 1/4" FROM THE T/E. INDICATION MEASURES APPROXIMATELY 1" IN DIAMETER DOT 151-03. REPAIRED LT ELEVATOR WATER INGRESS, IAW SRM 55-21-12-201 PARA 5H FIG 211 MAJOR REPAIR.Sep 24, 2020 · N677FE · Airbus A300F4605RSDR FDEA202009242312Skin · delaminatedLT ELEV TOP SURFACE HAS DENT/DELAMINATED IN THE AREA BETWEEN NR 6 AND 7 HINGES. REPAIRED LT ELEVATOR TOP SURFACE DENT, IAW SRM 55-21-12-201 PARA 5H FIG 211, MAJOR REPAIR.Sep 24, 2020 · N677FE · Airbus A300F4605RSDR FDEA202009172231Skin · gougedLT ELELATOR UPPER SKIN HAS A GOUGE AT OUTBOARD SIDE, DOT 168 004. APPLIED PERMANENT REPAIR TO LT ELEVATOR UPPER SKIN, IAW B757 SRM 55-20-01-2R FIG 201 TABLE 1 AND SRM 51-70-17-OG PAR 4B.Sep 17, 2020 · N912FD · Boeing 75728ASDR SWIA202053304Skin · chafedRT AILERON ALONG THE TOP UPPER LEADING EDGE, MULTIPLE AREA'S OF CHAFING, FLAGGED. C-CHECK RO 10/13/2020. REMOVED AND REPLACED WITH NEW RT AILERON UPPER LEDING EDGE SKIN, REF CRJ 200 SRM AND BOMBARDIER DRAWING.Sep 1, 2020 · N494CA · Cndair CL6002B19SDR LR7A2020083162282Skin · crackedDURING SCHEDULED A-CHECK UNDER JOB CARD HA1200, FOUND THE LT LOWER ELEVATOR SKIN CRACKED NEAR PREVIOUS REPAIR AT HSS69-78L, FS1138.5 - 1150.5. REPAIRED LT LOWER ELEVATOR SKIN HSS69-78L, FS1138.5 - 1150.5, IAW MEA 382-55-20-073, SMP583 51-140-12.Aug 26, 2020 · N401LC · Lkheed 382G44K30SDR LR7A2020083162281Skin · crackedDURING SCHEDULED A-CHECK UNDER JOB CARD HA1200, FOUND THE RT ELEVATOR LOWER INBOARD SKIN CRACKED ALONG HSS70.5R RIB RIVET LINE AT FS1148.5-1149.25. REPAIRED RT LOWER ELEVATOR AT FS1132-1153,HSS62-76.25R, INCORPORATING PREVIOUS REPAIR (MEA 382-55-20-072) IAW SAug 26, 2020 · N401LC · Lkheed 382G44K30SDR LR7A2020080762277Skin · crackedDURING SCHEDULED INSPECTION FOUND 1 INCH CRACK ON THE RT ELEVATOR LOWER SKIN. REPAIRED IAW SMP 583 51-140-12.Aug 6, 2020 · N401LC · Lkheed 382GSDR LR7A2020080762276Skin · crackedDURING SCHEDULED INSPECTION FOUND 6.25 INCH CRACK ON THE LT ELEVATOR LOWER SKIN. REPAIRED IAW SMP 583 51-140-12.Aug 6, 2020 · N401LC · Lkheed 382GSDR LR7A2020080762275Skin · crackedDURING SCHEDULED INSPECTION FOUND 5 INCH CRACK ON THE LT ELEVATOR LOWER SKIN. REPAIRED IAW SMP 583 51-140-12.Aug 6, 2020 · N401LC · Lkheed 382GSDR SIMA2020082104002Skin · damagedLEFT ELEVATOR TRAIL EDGE UPPER SKIN HAS HOLE. PERFORMED A REPAIR ON THE LT ELEVATOR TRAIL EDGE IAW ERS-EM-55MR-854.Aug 4, 2020 · N619AE · Emb EMB145LRSDR FDEA202008031763Skin · corrodedNR 4 LIGHTNING STRIP, OUTBOARD OF NR 3, RT ELEVATOR HAS SEVERAL AREAS OF CORROSION. REMOVED AND REPLACED THE NR 4 LIGHTNING STRIP IAW SRM:55-21-12 PARA 5.E.Aug 3, 2020 · N744FD · Airbus A300B4622RSDR FDEA202008031762Skin · corrodedNR 3 LIGHTNING STRIP, OUTBOARD OF NR 2, RT ELEVATOR HAS SEVERAL AREAS OF CORROSION. REMOVED AND REPLACED NR 3 LIGHTNING STRIP IAW SRM 55-21-12 PARA 5.E.Aug 3, 2020 · N744FD · Airbus A300B4622RSDR FDEA202008031761Skin · corrodedNR 2 LIGHTNING STRIP, OUTBOARD OF NR 1, RT ELEVATOR HAS SEVERAL AREAS OF CORROSION REMOVED AND REPLACED NR 2 LIGHTNING STRIP IAW SRM: 55-21-12 PARA 5.EAug 3, 2020 · N744FD · Airbus A300B4622RSDR FDEA202008031760Skin · corrodedNR 1 LIGHTNING STRIP, MOST INBOARD. RT ELEVATOR HAS SEVERAL AREAS OF CORROSION REMOVED AND REPLACED THE NR 1 LIGHTNING STRIP INBD RT ELEVATOR IAW SRM: 55-21-12, PARA 5.EAug 3, 2020 · N744FD · Airbus A300B4622RSDR FDEA2020082001752Skin · delaminatedRIGHT ELEVATOR UPPER SKIN CONDUCTOR STRIP AT RIB ER2 DELAMINATED. REPAIRED THE AREA AT RIB ER2 ADJACENT TO THE RT ELEVATOR UPPER SKIN IAW SRM: 55-20-00, & 55-21-12 PARA 5.E. REMOVED & REPLACED THE LIGHTNING CONDUCTOR STRIP IAW SRM: 55-21-12, PARA 5.E. MAJORAug 2, 2020 · N744FD · Airbus A300B4622RSDR IPXA2020080328542Skin · damagedLEFT OTBD ELEVATOR UPPER SKIN DAMAGED 25.25", OTBD AND 10.25" FWD OF T/E. REPAIRED IAW B767-5520-77296.Aug 2, 2020 · N317UP · Boeing 76734AFSDR FDEA2020080321752Skin · delaminatedRIGHT ELEVATOR UPPER SKIN CONDUCTOR STRIP AT RIB ER2 DELAMINATED REPAIRED DELAMINATED AREA AT RIB ER2 ADJACENT TO RH ELEVATOR UPPER SKIN IAW A300- 600 SRM: 55-20-00 & 55-21-12 PARA 5.E. REMOVED & REPLACED LIGHTNING CONDUCTOR STRIP IAW A300-600 SRM: 55-21-12Aug 2, 2020 · N744FD · Airbus A300B4622RSDR SWIA2020091652541Skin · crackedELEVATOR TRAILING EDGE PANEL 334AB IS CRACKED. C-CHECK RO 9/12/2020. RECEIVED NEW ELEVATOR TRAILING EDGE PANEL NR 601R24029-5. LOCATED, DRILLED MOUNTING HOLES, COMPLIED WITH CRJ-200 SRM PANEL READY FOR INSTALL.Jul 25, 2020 · N916EV · Cndair CL6002B19SDR IPXA2020081218949Skin · damagedINSPECTION TYPE:SEGWATER INGRESS FOUND 64" FROM THE OB EDGE OF FR 10 AND 5" FROM THE TRAILING EDGE INDICATION MEASURES. 2" DIAMETERACCOMPLISH REPAIR PER A300-600 SRM 55-21-12 PAR. 5JJul 25, 2020 · N139UP · Airbus A300F4622RSDR IPXA2020081218948Skin · damagedINSPECTION TYPE:SEGDELAMINATION, DAMAGE AND WATER INGRESS 29" FROM OB EDGE OF FR2 AND 36 1/2" FROM THE TRAILING EDGE. DAMAGE MEASURES APPROX. 1.0" DIAMETERACCOMPLISH REPAIR PER A300-600 SRM 55-21-12 PAR S.H. AND 51-77-12 PAR. 3.GJul 25, 2020 · N139UP · Airbus A300F4622RSDR IPXA2020081218947Skin · damagedINSPECTION TYPE:SEG, WATER INGRESS FOUND 7 1/2" FROM THE OTBD EDGE OF ER 13 AND 5" FROM THE TRAILING EDGE INDICATION MEASURES 2 1/2" X 1" IN SIZE. ACCOMPLISH A REPAIR IAW SRM 55-21-12 PARAGRAPH 5J.Jul 25, 2020 · N139UP · Airbus A300F4622RSDR FDEA202007171575Skin · delaminatedLEFT ELEVATOR HAD WATER ENTRAPMENT 30 7/8 INCHES FROM THE OTBD EDGE OF ER13, APPROXIMATELY 21 INCHES FROM THE TRALING EDGE AND MEASURES 1 X 1 INCH IN SIZE. REPAIRED THE LT ELEVATOR IAW SRM 55-21-12, PARA 5H. MAJOR REPAIR.Jul 17, 2020 · N676FE · Airbus A300F4605RSDR FDEA202007171574Skin · delaminatedLEFT ELEVATOR HAD WATER ENTRAPMENT 12 INCHES FROM THE OUTBD EDGE OF ER2, APPROXIMATELY 21 1/4 INCHES FROM THE TRALING EDGE AND MEASURES 1 1/4 X 1 3/8 INCHES IN SIZE. REPAIRED THE LT ELEVATOR IAW SRM 55-21-12, PARA 5H, MAJOR REPAIR.Jul 17, 2020 · N676FE · Airbus A300F4605RSDR FDEA202007171573Skin · delaminatedLEFT ELEVATOR HAD WATER ENTRAPMENT 19 1/2 INCHES FROM THE OUTBD EDGE OF ER2, APPROXIMATELY 21 3/8 INCHES FROM THE TRAILING EDGE AND MEASURES 5/8 X 3/4 INCH IN SIZE. REPAIRED THE LT ELEVATOR IAW SRM 55-21-12, PARA 5H. MAJOR REPAIR.Jul 17, 2020 · N676FE · Airbus A300F4605RSDR FDEA202007171572Skin · delaminatedRIGHT ELEVATOR HAD WATER ENTRAPMENT ON THE LT EDGE OF ER13 APPROIMATELY 12 3/4 INCHES FROM THE TRAILING EDGE AND MEASURES 1 5/8 INCHES X 2 INCHES IN SIZE. REPAIRED THE RT ELEVATOR IAW SRM 55-21-12 PARA 5H, FIG 212. MAJOR REPAIR.Jul 17, 2020 · N676FE · Airbus A300F4605RSDR FDEA202007131834Skin · delaminatedTRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS LOCATED AT 1 INCH. OUTBOARD FROM RIB 5 AND 4 INCH. FROM TRAILING EDGE ON RH HORIZONTAL STABILIZER (1 EA) (L=6 INCH. W=1.5 INCH) REPAIRED RH ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE Jul 13, 2020 · N651FE · Airbus A300F4605RSDR FDEA202007131816Skin · delaminatedTRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 12 INCH OUTBOARD FROM RIB 7 AND 16 INCH FROM TRAILING EDGE ON LT HORIZONTAL STABILIZER (1EA) (L=7.5 INCH. W=3 INCH). REPAIRED ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLJul 13, 2020 · N651FE · Airbus A300F4605RSDR FDEA202007131815Skin · delaminatedTRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 10 INCH INBOARD FROM RIB 16 AND 8 INCH FROM TRAILING EDGE ON LT HORIZONTAL STABILIZER (1EA) (L=2.75 INCH. W=2.25 INCH). REPAIRED LT ELEVATOR UPPER SKIN PANEL HONEY COMB COJul 13, 2020 · N651FE · Airbus A300F4605RSDR FDEA202007131814Skin · delaminatedTRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 27 INCH OUTBOARD FROM RIB 13 AND 7 INCH FROM TRAILING EDGE ON LT HORIZONTAL STABILIZER (1EA) (L=2.25 INCH. W=1.5 INCH). REPAIRED LT ELEVATOR UPPER SKIN PANEL HONEYCOMB CORJul 13, 2020 · N651FE · Airbus A300F4605RSDR FDEA202007131813Skin · delaminatedTRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 1 INCH INBOARD FROM RIB 13 AND 14 INCH FROM TRAILING EDGE ON LT HORIZONTAL STABILIZER (1EA) (L=5.5 INCH. W=4.5 INCH). REPAIRED LT ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE Jul 13, 2020 · N651FE · Airbus A300F4605RSDR FDEA202007131812Skin · delaminatedTRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 7 INCH INBOARD FROM RIB 7 AND 16 INCH FROM TRAILING EDGE ON LT HORIZONTAL STABILIZER (1 EA) (L=2 INCH W=1.5 INCH). REPAIRED LT ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELJul 13, 2020 · N651FE · Airbus A300F4605RSDR FDEA202007131811Skin · delaminatedTRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 20 INCH OUTBOARD FROM RIB 13 AND 18 INCH FROM TRAILING EDGE ON LT HORIZONTAL STABILIZER (1EA) (L=2.5 INCH. W=2 INCH). REPAIRED LT ELEVATOR UPPER SKIN PANEL HONEY COMB COREJul 13, 2020 · N651FE · Airbus A300F4605RSDR FDEA202007131810Skin · delaminatedTRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 3 INCH OUTBOARD FROM RIB 13 AND 19 INCH FROM TRAILING EDGE ON LT HORIZONTAL STABILIZER (1EA) (L=2 INCH. W=1.5 INCH). REPAIRED LT ELEVATOR UPPER SKIN PANEL HONEY COMB CORE Jul 13, 2020 · N651FE · Airbus A300F4605RSDR FDEA202007131809Skin · delaminatedTRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 9 INCH INBOARD FROM RIB 5 AND 13 INCH FROM TRALING EDGE. ADDITIONALLY, A DISBONDED AREA WAS FOUND WITHIN THIS SPOT, ON LT HORIZONTAL STABILIZER (1 EA) (L=3 INCH. W=2.3 IJul 13, 2020 · N651FE · Airbus A300F4605RSDR FDEA202007131808Skin · delaminatedTRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 17 INCH OUTBOARD FROM RIB 2 AND 5.5 INCH FROM TRAILING EDGE ON LT HORIZONTAL STABILIZER (1 EA) (L=3 INCH. AND W=1 INCH). REPAIRED LT ELEVATOR UPPER SKIN PANEL HONEY COMB CJul 13, 2020 · N651FE · Airbus A300F4605RSDR FDEA202007131807Skin · delaminatedTRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 27 INCH OUTBOARD FROM RIB 13 AND 26 INCH FROM TRAILING EDGE ON LT HORIZONTAL STABILIZER (1EA) (L=1.75 INCH. W=1.5 INCH). REPAIRED LT ELEVATOR UPPER SKIN PANEL HONEY COMB CJul 13, 2020 · N651FE · Airbus A300F4605R
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