JASC 5512

Service difficulty reports · 7,886

Reports filed under 5512 · Horizontal Stabilizer, 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 = '5512'
  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 AALA202411134809Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN LEFT HAND HORIZONTAL STABILIZER LOWER SKIN LOCATED AT STABILIZER STA 138.70, 25 INCHES FROM FRONT SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11.Oct 27, 2024 · N952AA · Boeing 737823SDR CALA2024102802744Skin · crackedRH HORIZONTAL STABILIZER, LOWER SKIN, ONE CRACK INDICATION AT ST A 129.50, 8 INCHES AFTER OF FRONT SPAR.Oct 24, 2024 · N37267 · Boeing 737824SDR SWI2025F00145Skin · dented1 EA HOLE MISDRILLED IN RH HORIZONTAL STAB UPPER SKIN AT STRINGER 8 BETWEEN RIBS 5 AND 6 (FILED CLOSED) REMOVED AND REPLACED STRINGER 8 ON RH HORIZONTAL STAB UPPER SKIN PER SRM 51-40-08 OEM PART REPLACEMENT NO CHANGE IN WEIGHT AND BALANCEOct 16, 2024 · N127SY · Emb ERJ170200LRSDR UIEA2024101100977Skin Splice · crackedCRACK DAMAGE ON THE HST OUTBOARD SECTION RH SIDE DURING INSPECTION PER SB 747-55A2050.(<P>1. REMOVE FASTENERS I.A.W SRM 51-40-02-0G-0 REV.101. 2. REPAIR DAMAGE AREA I.A.W EL T2024A55M-2240 REV.4. 3. INSTALL SPLICE I.A.W DWG 65B03560 SH14 REV.D AND 65B03621 SH6Oct 12, 2024 · N419MC · Boeing 74748EFSDR CALA2024110602803Skin · crackedRH HORIZONTAL STABILIZER, LOWER SKIN, ONE CRACK INDICATION AT ST A 157.10, 9 INCHES IN FRONT OF REAR SPAR (REF. AAR NR 1000019416 ). N THRESHOLD 56,000 TOTAL FLIGHT CYCLE, INTERVALS 9,000 FLIGHT CY CLES, METHOS DVI AND LFEC INSPECTION IAW B737-800 SRM 55-10-01Oct 10, 2024 · N87513 · Boeing 737824SDR CALA2024110402783Skin · crackedLH HORIZONTAL STABILIZER, LOWER SKIN HAS THREE CRACKS INDICATIO NS AT STA 101.90, LOCATION 1 10.5 INCHES IN FRONT OF REAR SPAR, LOCATION 2 19 1/4 INCHES IN FRONT OF REAR SPAR, LOCATION 3 28 IN CHES IN FRONT OF REAR SPAR (REF. AAR NR 1000019415).Oct 10, 2024 · N87513 · Boeing 737824SDR DALA2024101009964Access Panel · damagedSHIP 3143 ELONGATED HOLE ACCESS PANEL 335AB ON LH HORIZONTAL STABILIZER. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON ACCESS PANEL 335AB AT LH HORIZONTAL STABILIZER AS PER ER/A 620628-14. (0601055)Oct 9, 2024 · N343NB · Airbus A319114SDR SWAA2024102946477Panel · crackedHORIZONTAL STAB GAP PANEL 343AT HAVES CRACKED CORD<[01] REMOVED AND INSTALLED NEW CHORD AT HORIZONTAL STAB GAP PANEL 343AT AS PER SRM-51-40-02-0G-0;[02] VERIFIED STEP 1Oct 8, 2024 · N498WN · Boeing 7377H4SDR R61A2024102800513Skin · crackedR/H H STAB LEADING EDGE FOUND CRACK AT RIB 4Oct 8, 2024 · N864RW · Emb ERJ170100SESDR CALA2024100902608Skin · crackedLH HORIZONTAL STABILIZER, LOWER SKIN HAS ONE CRACK INDUCATION AT STA 157.10, 16 INCHES IN FRONT REAR SPAR.(REF AAR NR 1000018834 )Oct 8, 2024 · N18220 · Boeing 737824SDR DALA2024103010525Access Door · detachedHORIZONTAL STABILIZER BEARING AND CENTER SECTION ACCESS DOORS WERE DISCOVERED MISSING DURING POSTFLIGHT INSPECTION. MEL NUMBER ADDED FOR DISPATCH RELEASE, LOG REDEFERRAL REQUIRED. DISPATCH APPROVAL VALIDATION IS ACCOMPLISHED PANEL 370SL BEARING COVER PANEL MISOct 1, 2024 · N983AT · Boeing 717200SDR CALA2024100102535Skin · crackedLH HORIZONTAL STABILIZER, LOWER SKIN, ONE CRACK INDICATION AT ST A 138.7, LOCATED 10 INCHES IN FRONT, REAR SPAR (REF AAR NR 10000 17197)Sep 29, 2024 · N76265 · Boeing 737824SDR DALA2024100109601Access Panel · crackedSHIP 3148 CRACK ACCESS PANEL 342AB ON RH HORIZONTAL STABILIZER. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON ACCESS PANEL 342AB HORIZONTAL STABILIZER AS PER ER/A 620592-14 REV. (0581239)Sep 28, 2024 · N348NB · Airbus A319114SDR SWAA2024110143012Access Panel · crackedCRACK ON BLADE OF ACCESS PANEL 333AB AT LT HORIZONTAL STABILIZER 2024-600434<[01] REPLACED BLADE OF ACCESS PANEL 333AB AT LT HORIZONTAL STABILIZER IAW B737-800 SRM 51-40-02.;[02] REPLACED BLADE OF ACCESS PANEL 333AB AT LT HORIZONTAL STABILIZER IAW B737-800 SRMSep 27, 2024 · N8327A · Boeing 7378H4SDR DALA2024093009543Panel · delaminatedSHIP 3117 LT THS TRAILING EDGE PANEL 334BT SEVERELY DELAMINATED. CORRECTIVE ACTION: REPLACED PANEL 334BT PER A319 AMM 55-13. (0577971)Sep 26, 2024 · N317NB · Airbus A319114SDR SWAA2024103041527Skin · crackedCRACK INDICATION FOUND ON RT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.90 RIB AND 8 INCH. FROM REAR SPAR. INBOARD SIDE OF RIB. CRACK LENGTH = 0.900 INCH. APPROX. 2024-593167<[01] TOOL USED IN STEP 5: EDDY CURRENT EQUIPMENT P/N: NORTEC 600Sep 25, 2024 · N268WN · Boeing 7377H4SDR CALA2024093002533Skin · crackedRH HORIZONTAL STABILIZER, LOWER SKIN, ONE CRACK INDICATION AT STA 129.5, LENGTH 1 3/4 INCHES, 27 INCHES INFRONT REAR SPAR. (REF: AAR NR 1000016458)Sep 25, 2024 · N33262 · Boeing 737824SDR CALA2024093002532Skin · crackedLH HORIZONTAL STABILIZER, LOWER SKIN, ONE CRACK INDICATION AT STA 101.9, LENGTH 1 1/2 INCHES, 12 INCHES INFRONT REAR SPAR. (REF: AAR NR 1000016457)Sep 25, 2024 · N33262 · Boeing 737824SDR SWAA2024103041526Skin · crackedCRACK INDICATION FOUND ON LT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.90 RIB AND 8 INCH. FROM REAR SPAR. INBOARD SIDE OF RIB. CRACK LENGTH = 0.900 INCH. APPROX. 2024-593165<[01] STEP 5 TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; SSep 24, 2024 · N268WN · Boeing 7377H4SDR DALA2024092309312Skin · gougedSHIP 3170 FOUND GOUGES ON RH HORIZONTAL STABILIZER LEADING EDGE PLATE. CORRECTIVE ACTION: REPAIRED PER ER/A 621102-14. (0569615)Sep 22, 2024 · N370NB · Airbus A319114SDR DXTR2024092201Access Panel · corrodedCORROSION ON LH HORIZONTAL STAB ACCESS PANEL NUT PLATES FOR PANEL 351AB,351BB,341AR, 341CR, 341DR, 341ER,341AL AND 341CL. CORRECTIVE ACTION....ADDED PRIMER TO THE BLENDED AREA AFTER NDT WAS ACCOMPLISHED. AWAITING NUTPLATE INSTALLATION AFTER PRIMER CURES. REF.Sep 22, 2024 · N515QS · Cessna 680ASDR CALA2024092602491Skin · crackedLEFT HORIZONTAL STAB LOWER SKIN CRACK 1 INCH IN LENGTH AT STA 120.30 36" AFT OF FWD SPAR . A REPAIR DOUBLER WAS INSTALLED SEE BAM NON-ROUTINE 2130744 FOR ALL WORK ACCOMPLISHED. THIS NON-ROUTINE IS ISSUED TO GENERATE A SIGNIFICANT FINDINGS REPORT. ISSUED SFR # Sep 20, 2024 · N37281 · Boeing 737824SDR AALA202409230862Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN LEFT HAND HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 129.50, 9 INCHES AFT OF FORWARD SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11.Sep 20, 2024 · N953AN · Boeing 737823SDR CALA2024092302470Skin · crackedCRACK FOUND AT RT HORIZONTAL STABILIZER LOWER SKIN STA 157.10.8. 5 FROM FRONT SPAR, I/B LENGTH OF CRACK 0.312 TRIMMED CRACKED AREA AT RT HORIZONTAL STAB LOWER SKIN STA 157.10 ,8.5 FROM SPAR I/B ROW FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER AS PER B737Sep 20, 2024 · N76515 · Boeing 737824SDR AALA202409239945Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN LEFT HAND HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 129.50, 17 INCHES AFT OF FORWARD SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11.Sep 18, 2024 · N953AN · Boeing 737823SDR SWIA20240917Skin · dentedRH HORIZONTAL STABILIZER UPPER SKIN (P/N 170-62726-016) HAS 294 HAIL DAMAGE DENTS. ITEMS 1 THRU 294. FOUND 294 DENTS ON RH HORIZONTAL STAB UPPER SKIN PN# 170-62726-016 BETWEEN RIBS 1-14 AND FWD SPAR AND REAR SPAR. DENTS FOUND TO BE WITHIN PERMANENT ALLOWABLE DSep 17, 2024 · N127SY · Emb ERJ170200LRSDR SWAA2024102337559Skin · crackedCRACK INDICATION FOUND ON LT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.9 RIB AND 16 INCH. FROM FRONT SPAR. INBOARD SIDE OF RIB. CRACK LENGTH = 0.900 INCH. APPROX. 2024-572755<[01] TOOL USED ON STEP 7 AND 8 ET EQUIPMENT: P/N: NORTEC 600D; Sep 14, 2024 · N7854B · Boeing 73771BSDR SWAA2024102837360Skin · crackedCRACK INDICATION FOUND ON RT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.9 RIB AND 16 INCH. FROM FRONT SPAR. INBOARD SIDE OF RIB. CRACK LENGTH = 0.600 INCH. APPROX. 2024-572219<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; Sep 13, 2024 · N7740A · Boeing 7377BDSDR SWAA2024102837359Skin · crackedCRACK INDICATION FOUND ON LT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.9 RIB AND 16 INCH. FROM FRONT SPAR. INBOARD SIDE OF RIB. CRACK LENGTH = 0.800 INCH. APPROX. 2024-572217<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; Sep 12, 2024 · N7740A · Boeing 7377BDSDR SWAA2024101637131Access Panel · crackedCRACK BLADE ACCESS PANEL 343AT AT RT HORIZONTAL STAB 2024-565546<[01] REPLACED BLADE ACCESS PANEL 343AT AT RT HORIZONTAL STAB IAW B737-700 SRM 51-40-02;[02] TASK COMPLETED.Sep 12, 2024 · N7738A · Boeing 7377BDSDR SWAA2024102336845Access Panel · crackedCRACK BLADE ACCESS PANEL 333AB AT LT HORIZONTAL STAB 2024-572586<[01] REPLACED BLADE ACCESS PANEL 333AB AT LT HORIZONTAL STAB IAW B737-700 SRM 51-10-02-0G-0 ITEM 9 AND B737-700 SRM 51-40-02-0G-0.;[02] JOB COMPLETEDSep 11, 2024 · N7854B · Boeing 73771BSDR SWAA2024092037795Skin · damagedACCOMPLISH REPAIR AT L/H HORIZONTAL STAB LOWER SKIN STA 120.3 AFT POSITION<[01] ACCOMPLISHED REPAIR AT L/H HORIZONTAL STAB LOWER SKIN AFT POSITION STA 120.3 PER 737-700 SRM 55-10-01-2R REPAIR 11; 24-155-02458-WIP1 (COMPONENT - AAR (MIA) - HORIZONTAL STAB (LH) Sep 11, 2024 · N555LV · Boeing 7377BDSDR SWAA2024092037796Skin · damagedACCOMPLISH REPAIR AT L/H HORIZONTAL STAB LOWER SKIN STA 120.3 FWD POSITION<[01] ACCOMPLISHED REPAIR AT L/H HORIZONTAL STAB LOWER SKIN FWD POSITION STA 120.3 PER 737-700 SRM 55-10-01-2R REPAIR 11; 24-155-02458-WIP1 (COMPONENT - AAR (MIA) - HORIZONTAL STAB (LH) Sep 11, 2024 · N555LV · Boeing 7377BDSDR SWAA2024092036747Skin · damagedLT HORIZONTAL STAB LOWER SKIN AT #4 RIB INSTALLATION AREA AT FASTENER HOLE 15 AFT OF FWD EDGE OF SKIN I/B ROW FOUND ELONGATED<[01] ACCOMPLISHED REPAIR OF LOWER SKIN AT LT HORIZONTAL STAB AT #4 RIB INSTALLATION AREA AT FASTENER HOLE 15 AFT OF FWD EDGE OF SKIN ISep 11, 2024 · N555LV · Boeing 7377BDSDR SWAA2024092036745Skin · damagedLT HORIZONTAL STAB LOWER SKIN AT #4 RIB INSTALLATION AREA AT FASTENER HOLE 2 FWD OF AFT EDGE OF SKIN O/B ROW FOUND ELONGATED<[01] ACCOMPLISHED REPAIR OF LOWER SKIN AT LT HORIZONTAL STAB AT #4 RIB INSTALLATION AREA AT FASTENER HOLE 2 FWD OF AFT EDGE OF SKIN O/BSep 11, 2024 · N555LV · Boeing 7377BDSDR SWAA2024092036746Skin · damagedLT HORIZONTAL STAB LOWER SKIN AT #4 RIB INSTALLATION AREA AT FASTENER HOLE 10 FWD OF AFT EDGE OF SKIN O/B ROW FOUND ELONGATED<[01] ACCOMPLISHED REPAIR OF LOWER SKIN AT LT HORIZONTAL STAB AT #4 RIB INSTALLATION AREA AT FASTENER HOLE 10 FWD OF AFT EDGE OF SKIN OSep 11, 2024 · N555LV · Boeing 7377BDSDR DALA2024090908825Skin · cracked(LOG 0541727) CRACK ON LOWER SKIN (STAB.STA.101.90 AND 45 IN OF LEADING EDGE APPROX) AT HORIZONTAL STABILIZER LH. LOWER SKIN (STAB.STA.101.90 AND 45 IN OF LEADING EDGE APPROX) AT HORIZONTAL STABILIZER LH WAS REPAIRED PER B737-800 SRM 55-10-01-2R PROCEDURE 11 RSep 6, 2024 · N3733Z · Boeing 737832SDR DALA2024090908824Skin · cracked(LOG 0541724) CRACK ON LOWER SKIN (STAB.STA.101.90 AND 45 IN OF LEADING EDGE APPROX) AT HORIZONTAL STABILIZER LH. LOWER SKIN (STAB.STA.101.90 AND 45 IN OF LEADING EDGE APPROX) AT HORIZONTAL STABILIZER LH WAS REPAIRED PER B737-800 SRM 55-10-01-2R PROCEDURE 11 RSep 6, 2024 · N3733Z · Boeing 737832SDR DALA2026080404487Skin · corrodedCORROSION STABILIZERS RT HORIZONTAL STABILIZER UPPER AFT SKIN PANEL BARREL NUT HOLE #11. REPAIRED PER ERA 620136-14. (0541097) AIRCRAFT WAS GROUNDED.Sep 5, 2024 · N989AT · Boeing 717200SDR NACA2024090500003Skin · unknownLH HORIZONTAL STABILIZER EXTERIOR SURFACE BLEND OUT FROM FUSELAGE 136 INCH AND LEADING EDGE 37.5 INCH. FAA 8100-9 SEPT 3, 2024 REPETATIVE INSPECTION 3000FC OR 24 MTHS EARN N399CM-0017 - EO 767-57-0030Sep 5, 2024 · N399CM · Boeing 767323SDR IXXA20241003005Skin Panel · corrodedHORIZONTAL STAB CENTER SECTION UNDER CENTER STRAP IS CORRODED BETWEEN STRINGER 7 AND STRINGER 8 ABOVE RIB 1 LEFT. HAECO WO 320008 NON ROUTINE 40691Sep 5, 2024 · N491AZ · Boeing 767323SDR SWAA2024092034462Skin · damagedLT HORIZONTAL STAB UPPER SKIN AT #4 RIB INSTALLATION AREA HAS ELONGATED HOLES<[01] REMOVED DAMAGED AT L/H HORIZONTAL STAB UPPER SKIN AT#4 RIB AREA AS PER SRM 51-10-02-0G-0 AND SRM 55-10-01-2R-3. FABRICATED REPAIR PARTS DOUBLER AND FILLER AT LT HORIZONTAL STAB Sep 5, 2024 · N555LV · Boeing 7377BDSDR SWAA2024092034463Skin · damagedLT HORIZONTAL STAB LOWER SKIN AT #4 RIB INSTALLATION AREA HAS ELONGATED HOLES<[01] FAULT ACCOMPLISHED ON ASSIGNED EA 24-155-02458-WIP1 [TTG8Q00VP5ED];[02] CORRECTION TO STEP 1 EA #: FAULT ACCOMPLISHED ON ASSIGNED EA 24-155-02458-WIP1 [TTG8Q00VSG87].;[03] VERIFSep 5, 2024 · N555LV · Boeing 7377BDSDR DXTA2024090500689Skin · corrodedREMOVED 2 AREAS OF CORROSION ON TOP SIDE OF LH HORIZONTAL STAB UPPER SKIN, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, PRIMED AND TOPCATED REPAIR AREAS IAW NETJETS REQUEST FOR TECHNICAL SERVICES RFTS-111665 REV. 0.Sep 5, 2024 · N397QS · Cessna 680CESDR CALA2024090500570Skin · crackedLH HORIZONTAL STABILIZER, LOWER SKIN, ONE CRACK INDICATION AT STA 101.9, 14 INCHES INFRONT REAR SPAR. REPAIRED DAMAGE CRACK AT L/H HORIZONTAL STAB LOWER SKIN AT STA 1 01.9 IAW SRM 51-40-02-0G-0, 55-10-01-2R-11, AMM 51-31 -00-930-804,51-21-73-370-801 THIS REPASep 4, 2024 · N75425 · Boeing 737924ERSDR SWAA2024092032788Skin · damagedLT HORIZONTAL STAB UPPER AND LOWER SKIN AT RIB #4 INSTALLATION AREA WITH MULTIPLE ATTACHING HOLES ELONGATED.<[01] REPAIR OF L/HORIZONTAL STAB UPPER SKIN AT #4 RIB INSTALLATION AREA WILL BE ACCOMPLISHED ON CUSTOMER CARD [TTG8Q00VP5EB];[02] REPAIR OF L/HORIZONTASep 1, 2024 · N555LV · Boeing 7377BDSDR SWAA2024100732728Skin · crackedCRACK INDICATION FOUND ON RT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.9 RIB AND 16 INCH. FROM FRONT SPAR. INBOARD SIDE OF RIB. CRACK LENGTH = 0.900 INCH. APPROX. 2024-533690<[01] TOOL USED ON STEP 5 EDDY CURRENT EQUIPMENT P/N: NORTEC 600Aug 31, 2024 · N266WN · Boeing 7377H4SDR FDEA202408251172Skin · corrodedHORIZONTAL STABILIZER, CENTER SECTION, UPPER SKIN AT EXTERNAL SURFACE, CORROSION AT RBL 27 AND 6" FROM FRONT SPAR. HORIZONTAL STABILIZER, CENTER SECTION, UPPER SKIN AT EXTERNAL SURFACE, CORROSION AT RBL 27 AND 6" FRON SPAR WAS REPAIRED IAW H-5510-T0380306 Aug 25, 2024 · N142FE · Boeing 7673S2FSDR IXXA20241003007Skin · corrodedHORIZONTAL STAB CENTER SECTION UPPER SKIN HAS CORROSION BETWEEN RIB 1R AND 2R IN FRONT OF EXISTING REPAIR DOUBLER AT 2 EA PLACES. HAECO WO 320008 NON ROUTINE 40204Aug 21, 2024 · N491AZ · Boeing 767323SDR IXXA2024081606Doubler · corrodedEXISTING REPAIR DOUBLER ON UPPER SURFACE OF HORIZONTAL STAB CENTER SECTION IS CORRODED. INSIDE TAIL COMPARTMENT AT APPROX STA1735 ON RH SIDE.Aug 16, 2024 · N337AZ · Boeing 767323
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