JASC 5512

Service difficulty reports · 7,887

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 AWXA960095Skin · dentedPAE - FLT NR 3868 - DURING SCHEDULED C-14 MAINTENANCE CHECK, FOUND 2 DENTS AT RIBS NR 12 AND NR 1 ON THE RIGHT HAND HORIZONTAL STABILIZER. FOUND DENT AT RIB 12 OUT OF LIMITS. RECONTOURED DENT. SERVICEABLE PER SRM 55-10-1. (M)Feb 26, 1996 · N182AW · Boeing 737277SDR AWXA960086Skin · dentedPAE - FLT NR 3889 - DURING ROUTINE C-8 MAINTENANCE CHECK, FOUND DENT ON LEFT HORIZONTAL STAB LEADING EDGE AT LEADING EDGE STATION 203. RECONTOURED DENT ON LEFT HORIZONTAL STABILIZER LEADING EDGE STATION 203 IAW SRM 55-10-01. (M)Feb 20, 1996 · N305AW · Boeing 7373G7SDR 96ZZZX1972Skin · crackedDURING REPLACEMENT OF HORIZONTAL STABILIZER SKINS AFT, FOUND SKINS CRACKED AT THE UPPER, INBOARD ATTACHMENT AREA. REPLACING THE SKINS DETAILED ABOVE DUE TO OTHER DEFECTS, BUT HAPPENED TO FIND THESE CRACKS. RECOMMEND CLOSER ATTENTION TO THE AREA ADJACENT THE Feb 19, 1996 · N37SH · Snias AS350BSDR 96ZZZX1971Skin · crackedDURING REPLACEMENT OF HORIZONTAL STABILIZER SKINS AFT, FOUND SKINS CRACKED AT THE UPPER, INBOARD ATTACHMENT AREA. REPLACING THE SKINS DETAILED ABOVE DUE TO OTHER DEFECTS, BUT HAPPENED TO FIND THESE CRACKS. RECOMMEND CLOSER ATTENTION TO THE AREA ADJACENT THE Feb 19, 1996 · N37SH · Snias AS350BSDR AWXA960080Skin · dentedPAE - FLT NR 3887 - DURING ROUTINE C-7 MAINTENANCE CHECK, FOUND DENT ON LEFT HORIZONTAL STAB LEADING EDGE AT LEADING EDGE STATION 203, OUT OF LIMITS. RECONTOURED DENT IAW SRM 55-10-01. (M)Feb 17, 1996 · N187AW · Boeing 737277SDR USAA960250Skin · dentedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND FIVE 1 INCH BY 1 INCH BY .050 INCH DENTS, RIGHT HORIZONTAL STABILIZER LOWER INTERSPAR SKIN STABILIZER STATION 184.7 TO 193.9 AT MID CHORD. CUT OUT DAMAGE PLUS INSTALLED DOUBLER PER SRM 55-10-01 FIG 206. (M)Feb 16, 1996 · N424US · Boeing 737401SDR 96ZZZX1358Skin · crackedFOUND UPPER SURFACE OF HORIZONTAL STABILIZER CRACKED DURING DEICE BOOT CHANGE. MITSUBISHI TECH SERVICE HAS BEEN NOTIFIED. REPAIR WILL BE IAW SRM.Feb 16, 1996 · N16CG · Mtsbsi MU2B40SDR CAL960209Skin · gougedHOU - INSPECTION FOUND MINOR GOUGES ON RIGHT HORIZONTAL STABILIZER SKIN AT STATION XS 142. THE GOUGES WERE REMOVED BY BURNISHING OUT IAW SRM 55-01, FIGURE 1, PAGE 3. (M)Feb 15, 1996 · N14839 · Doug DC982SDR AALA960293Skin · damagedAFW - DAMAGE ON THE LOWER SURFACE AT FS 127 WAS REPAIRED PER SMM/AFW 1371 AND ESO 9196 13DEC95. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-1138. TST: 41,252.20 HRS. CYCLES, 7,600. (X)Feb 14, 1996 · N322AA · Boeing 767223SDR SWAA960076Skin · crackedDURING SCHEDULED 1/4 D-CHECK, FOUND LOWER SKIN OF RIGHT HORZI STAB CRACKED BETWEEN STA 120 AND 129. REPAIRED PER SWA RA 1-355-0215.Feb 13, 1996 · N350SW · Boeing 7373H4SDR 96004122802Skin · crackedCRACK 0.9 INCHES LONG AND .812 INCHES DEEP IN RIGHT FORWARD CENTER SECTION OF HORIZONTAL STABILIZER PANEL AT LOWER HOLE NR 6 AND NR 7. CRACK IS WITHIN FLYABLE LIMITS IAW SA 42248-3. TREATED HOLE AND SURROUNDING AREAS WITH LPS 3 AND NOTIFIED NWA ENGINEERING OFeb 6, 1996 · N228NW · Doug DC1030SDR 96003122801Skin · crackedCRACK 0.9 INCHES LONG AND .650 INCHES DEEP IN LEFT AFT UPPER CENTER SECTION OF HORIZONTAL STABILIZER PANEL AT HOLE NR 5 AND HOLE NR 6. CRACK IS WITHIN FLYABLE LIMITS IAW SA 42248-3. TREATED HOLE AND SURROUNDING AREAS WITH LPS 3 AND NOTIFIED NWA ENGINEERING OFeb 6, 1996 · N228NW · Doug DC1030SDR 96ZZZX877Skin · crackedLEFT HORIZONTAL STABILIZER HAD DAMAGE TO THE RIB AND THE LEADING EDGE. THE RIB HAD BEEN CRUSHED AND THE SKIN AT THE RIB HAD A SMALL CRACK. SUBMITTER STATED THIS DAMAGE DEVELOPED FROM THE IMPROPER HANDLING OF THE AIRCRAFT ON THE GROUND. ALL OTHER AREAS OF TAFeb 5, 1996 · N92747 · Cessna 172MSDR P5CA9600082Panel · delaminatedFOUND DELAMINATED PANELS 334DB, 334HB, 334KB ON LEFT HORIZONTAL STABILIZER. REPAIRED SAME IAW SRM 51-40-06.Jan 24, 1996 · N855FT · Boeing 747124SDR P5CA9600071Panel · delaminatedFOUND RT STABILIZER PANELS 344HB, 344QB, 344JB DELAMINATED. REPAIRED IAW SRM 51-40-06.Jan 24, 1996 · N855FT · Boeing 747124SDR 96FDEA00122Skin · crackedCRACK INDICATION ON LT STAB L/E AT UPPER FWD TANG. CRACK EXTENDS ITSELF ACROSS FASTENER HOLE APPROX 1.25 INCH IN LENGTH. CRACK LOCATION IS 5 INCHES I/B OF CLOSURE RIB AREA. REPAIRED CRACK IN REF TO SRM 55-20-00 FIG 9 AND 10. ALSO, PER EA 8-5510-21035A.Jan 24, 1996 · N68051 · Doug DC1010SDR 96FDEA00103Skin · crackedTWO CRACKS FOUND AT L/E OF LT STABILIZER UPPER SKIN PANEL, AT CLOSING RIB AREA STA XE = 28.426, XFS = 86.616. CRACKS ARE APPROX .25 INCH AND 2.0 INCH IN LENGTH. REPAIRED AS PER EO 8-5510-7-3312 PART 4 AND SRM 55-20-00.Jan 20, 1996 · N68049 · Doug DC1010SDR DL72S960187Skin · crackedFROM HMV ATL, THE LOWER SKIN ON THE LT HORIZ STAB IS GOUGED AND CRACKED I/B END. ACCOMPLISHED REPAIRS PER SRM 55-10-3 FIG 3.Jan 19, 1996 · N517DA · Boeing 727232SDR ABXA9600394Skin · chafedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE HORIZONTAL STABILIZER RIGHT AND LEFT UPPER SKIN PANELS CHAFED AND BLENDED BEYOND THE DC-9 SRM LIMITS. REPAIRED HORIZONTAL STABILIZER LEFT AND RIGHT UPPER SKIN PANELS IAW ABX REA D955-14035-MR.Jan 15, 1996 · N936AX · Doug DC931SDR ABXA9600393Skin · chafedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE HORIZONTAL STABILIZER RIGHT AND LEFT UPPER SKIN PANELS CHAFED AND BLENDED BEYOND THE DC-9 SRM LIMITS. REPAIRED HORIZONTAL STABILIZER LEFT AND RIGHT UPPER SKIN PANELS IAW ABX REA D955-14035-MR.Jan 15, 1996 · N936AX · Doug DC931SDR 96FDEA00018Plank · crackedLT HORIZ STAB FWD UPPER PLANK CRACKED JUST INBOARD OF CLOSING RIB, FROM FWD EDGE AFT THROUGH FASTENER HOLE 1.5 TOTAL CRACK CONTINUES PAST HOLE. REMOVED FASTENERS AND TRIMMED OUT CRACKED AREA. NDT AT CRACKED AREA AND OPEN HOLES C/W. COLD WORKED HOLES FINAL RJan 6, 1996 · N68052 · Doug DC1010CFSDR AWXA96004Skin · dentedLAS-PHX - FLT NR 1229 - CREW FOUND MULTIPLE DENTS IN LE OF HORIZONTAL STABILIZER OUT OF LIMITS. INTERIM REPAIR PER SRM 55-10-01, FILLED 1 DENT PER PARAGRAPH 'P' AND INSTALLED DMI 57834. ON 01/07, REMOVED AND REPLACED AND RESEALED LEFT HORIZONTAL STABILIZER LJan 5, 1996 · N155AW · Boeing 7373G7SDR CAL960245Panel · crackedINSPECTION FOUND A .25 INCH CRACK AT MOUNT HOLE OF LT HORIZONTAL STABILIZER PANEL NR 9113. THE CRACKED SECTION OF PANEL WAS REMOVED. A DOUBLER AND FILLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-30-2, AND MM 51-20-1. (X)Jan 4, 1996 · N73751 · Boeing 727227SDR ABXA9600386Skin · damagedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND AN EXISTING REPAIR ON THE LEFT HORIZONTAL STABILIZER LOWER CENTER SKIN PANEL THAT WAS NOT IAW THE DC-9 SRM. REPAIRED LEFT HORIZONTAL STABILIZER LOWER SKIN IAW ABX REA D955-13852-MR.Jan 2, 1996 · N936AX · Doug DC931SDR 96ZZZW40Panels · corrodedLEVEL 2 CORROSION - RIGHT HORIZONTAL STABILIZER OUTBOARD UPPER SURFACE PANELS ARE CORRODED BETWEEN RIVETS AT TRAILING EDGE. REPLACED PANEL WITH NEW PANELS.Jan 1, 1996 · N4935C · Doug DC863SDR 96ZZZM111Panels · corrodedFOUND LEVEL 2 CORROSION ON RIGHT HORIZONTAL STABILIZER OUTBOARD UPPER SURFACE PANELS AREA CORRODED BETWEEN RIVETS AT TRAILING EDGE. REPLACED PANEL WITH NEW PANELS. (M)Jan 1, 1996 · N4935C · Doug DC863SDR 96ZZZM110Panels · corrodedFOUND LEVEL 2 CORROSION ON RIGHT HORIZONTAL STABILIZER OUTBOARD UPPER SURFACE PANELS AREA CORRODED BETWEEN RIVETS AT TRAILING EDGE. REPLACED PANEL WITH NEW PANELS. (M)Jan 1, 1996 · N4935C · Doug DC863SDR AWXA9500835Skin · dentedPHX/SNA - FLT 0661 - DENT FOUND IN LT HORIZONTAL STABILIZER 8 FEET INBOARD OF TIP. PERFORMED INTERIM REPAIR PER SRM 55-10-01. (X)Dec 30, 1995 · N509DC · Boeing 73733ASDR ABXA9600388Skin · damagedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND AN EXISTING REPAIR ON THE LEFT HORIZONTAL STABILIZER UPPER AFT SKIN PANEL THAT WAS NOT IAW THE DC-9 SRM. REPAIRED LEFT HORIZONTAL STABILIZER UPPER AFT SKIN PANEL IAW ABX REA D955-13859-MR.Dec 29, 1995 · N936AX · Doug DC931SDR 96ZZZW18Skin · corrodedLEVEL 2 CORROSION - VERTICAL STABILIZER LEADING EDGE SEGMENT NR 1 UPPER END HAS CORROSION. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 55-2-1.Dec 29, 1995 · N4935C · Doug DC863SDR 96ZZZM152Skin · corrodedLEVEL 2 CORROSION, LEFT HORIZONTAL STABILIZER LEADING EDGE SKIN IS CORRODED AROUND FASTENERS 144 INCHES OUTBOARD OF INBOARD END. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 55-2-1. (M)Dec 29, 1995 · N4935C · Doug DC863SDR CKSA95156Panel · crackedKOSC - DURING C-CHECK INSPECTION, FOUND REF R/O 801-363 CRACK INDICATION HORIZONTAL STABILIZER CONSTANT SECTION UPPER FORWARD PANEL RIGHT SIDE BOLT HOLE NR 4 TO NEXT HOLE FORWARD TO FORWARD END OF PANEL. REMOVED AND REPLACED FORWARD UPPER PANEL IAW REFERENCE Dec 17, 1995 · N801CK · Doug DC855SDR AALA952021Skin · damagedTULE - FOUND LEFT LOWER SURFACE OF ELEVATOR DAMAGED. REMOVED LOWER LEFT ELEVATOR SKIN AND REPLACED WITH NEW SKIN. (M)Nov 30, 1995 · N870AA · Boeing 727223SDR CA951204015Skin · cracked(CAN)LH HORIZONTAL STABILIZER LEADING EDGE OUTER SKIN AT STA 89 CRACKED. REPAIRED SRM 51-140-14.Nov 27, 1995 · Lkheed 382GSDR CA951204013Skin · cracked(CAN)LH HORIZONTAL STABILIZER STA 219 UPPER SKIN CRACKED. REPAIRED DWG #SK382-55-024.Nov 27, 1995 · Lkheed 382GSDR 96ZZZM1114Skin · corrosionDURING D-CHECK INSPECTION, CORROSION WAS FOUND ON RT HORIZONTAL STABILIZER UPPER AND LOWER SURFACES OF SKIN FROM STATION XE 221 TO XE 272. REMOVED THE DAMAGED UPPER AND LOWER SKIN PANELS AND FABRICATED PANELS OF .808 7075-T6 MATERIAL. ALSO, REPLACED EACH BEANov 24, 1995 · N54FA · Doug DC8F54SDR 96ZZZM1113Skin · corrosionDURING D-CHECK INSPECTION, CORROSION WAS FOUND ON LEFT HORIZONTAL STABILIZER UPPER AND LOWER SURFACES OF SKIN FROM STATION XE 221 TO XE 272. REMOVED THE DAMAGED UPPER AND LOWER SKIN PANELS AND FABRICATED PANELS OF .080 7075-T6 MATERIAL. ALSO, REPLACED EACH BNov 24, 1995 · N54FA · Doug DC8F54SDR UPS405107Panel · crackedWHILE ON GROUND, MAINTENANCE FOUND RT HORIZ STAB T/E CRACKED AT NAV LIGHT AREA. ACCOMP COMPOSITE REPAIR PER SRM 51-40-09.Nov 20, 1995 · N673UP · Boeing 747123SDR DL72S954616Skin · wornFOUND ON CV2 CHECK WEAR MARK FROM CONTACT ON UPPER SKIN OF LT HORIZONTAL STABILIZER INBOARD OF ELEVATOR ACTUATOR ACCESS PANEL AND ABOVE BALANCE BOARD BAY NR 1.Nov 20, 1995 · N470DA · Boeing 727232SDR 95FDEA01779Skin · crackedHORIZONTAL STAB HAS ONE CRACK .948 INCH LONG IN THE AFT UPPER CONSTANT SECTION PANEL. CRACK STARTS AT AFT BOLT HOLE GOING FWD AND CRACK IS WITHIN FLYABLE LIMITS. REPETITIVE INSP PART 1 AT 24 MONTHS INTERVALS AND SPECIAL INSP TO START PART 2 AT 3 MONTHS INTERNov 19, 1995 · N68053 · Doug DC1010CFSDR DLL10954514Skin · crackedTHE RT HORIZ STAB L/E WAS FOUND WITH EXTENSIVE DAMAGE FWD OF THE FRONT SPAR BETWEEN STA 'H' LE 332.7 TO 455.2. ACCOMPLISHED REPAIRS PER DL ERA 272204-14.Nov 2, 1995 · N723DA · Lkheed 10113851SDR DLL10954510Skin · crackedTHE RT HORIZ STAB L/E WAS FOUND WITH EXTENSIVE DAMAGE FWD OF THE FRONT SPAR BET STA-H LE 332.7 TO 455.2. A REPLACEMENT FROM A/C 781 IS BEING SPLICED IN. AS A RESULT OF THE DIFFERENT CONFIGURATION RIBS AT 'H' LE 332.7 AND 455.2 AND REPLACEMENT AUX SPAR CAP SENov 2, 1995 · N723DA · Lkheed 10113851SDR CAL960221Skin · warpedKUL - INSPECTION FOUND THE RIGHT OUTBOARD ELEVATOR UPPER SKIN WARPED. THE SKIN WAS REPAIRED IAW SRM 55-10-00, PAGE 15, FIGURE 8. (M)Nov 1, 1995 · N41068 · Doug DC1030SDR DLL10954509Skin · crackedTHE RT HORIZ STAB L/E WAS FOUND WITH EXTENSIVE DAMAGE FWD OF THE FRONT SPAR BETWEEN STA 'H' LE 332.7 TO 455.2. REPAIRED PER DL ERA 272226-14.Oct 25, 1995 · N723DA · Lkheed 10113851SDR COMA9520393Skin · dentedTHE LEFT HORIZONTAL STABILIZER LEADING EDGE WAS DENTED BY A BIRD STRIKE. THE DENT WAS FIVE INCHES LONG AT BL 73.43. A FLUSH DOUBLER REPAIR WAS FABRICATED AND INSTALLED PER FAIRCHILD SRM 55-90-10, ARP 55-10-8817.Oct 23, 1995 · N703CA · Swrngn SA227ACSDR UPS204778Skin · delaminatedWHILE ON GROUND, MAINTENANCE FOUND DAMAGE AROUND FASTENERS AT APPROX STAB STA 32.08 TO 44.00 ON LT HORIZONTAL STAB UPPER SURFACE. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED IAW EO B727-5510-7485-A.Oct 9, 1995 · N936UP · Boeing 727108CSDR UPS804619Skin · crackedWHILE IN FOR D-CHECK, MAINTENANCE FOUND SKIN CRACKED AND APPEARS TO HAVE CORROSION O/B L/E AT I/B END OF RT HORZ STAB. INSTALLED REPAIR PER SRM 55-2.Oct 2, 1995 · N798UP · Doug DC871FSDR 95FDEA01457Skin · crackedRIGHT HORIZONTAL STABILIZER, UPPER AFT SKIN PANEL CRACKED AT I/B AFT CORNER O/B OF THE OPERATION BULKHEAD, CRACK LENGTH .6250 INCH. REPAIRED UPPER AFT SKIN STAB PANEL PER EA NR 8-5510-25166. INSTALLED AND SEALED ALL ACCESS AND L/E PANELS AS REQ IAW MM 55-10-Sep 28, 1995 · N301FE · Doug DC1030FSDR AALA951713Skin · dentedAFW - RIGHT HORIZ SKIN PANEL HAS DENT ON LOWER SURFACE (HONEYCOMB PANEL), PER MRB 757-616. (M)Sep 25, 1995 · N633AA · Boeing 757223SDR P5CA9500775Panel · delaminatedLEFT HAND HORIZONTAL STABILIZER UPPER TRAILING EDGE PANEL, JUST OUTBOARD OF ELEVATOR ACTUATOR DELAMINATED THREE PLACES. REPAIRED PANEL IAW 51-40-06.Sep 22, 1995 · N853FT · Boeing 747122
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