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 RRXA000568Skin · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO RT HORIZONTAL STAB I/B LEADING EDGE AT BL-R 177, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIRED DAMAGE IAW DC-8 SRM 55-2-1 FIFeb 27, 2000 · N831AL · Doug DC873FSDR RRXA000724Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO TAIL RT HORIZ STAB REAR SPAR UPPER SURFACE INSIDE AT STA XE 99 TO XE 123, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW STAB PANEL IFeb 24, 2000 · N994CF · Doug DC862SDR RRXA000723Panel · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO TAIL RT HORIZ STAB REAR SPAR UPPER SURFACE AT STA XE 219 TO XE 245, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW PANEL IAW DC-8 SRFeb 24, 2000 · N994CF · Doug DC862SDR RRXA000722Panel · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO TAIL RT HORIZ STAB REAR SPAR UPPER SURFACE INSIDE BETWEEN STA XE245 TO XE270, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW PANEL IFeb 24, 2000 · N994CF · Doug DC862SDR RRXA000721Panel · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO TAIL RT HORIZ STAB REAR SPAR UPPER SURFACE INSIDE AT STA XE52.825 -XE.75.672, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW RT STABFeb 24, 2000 · N994CF · Doug DC862SDR UPS00831981Skin · crackedINSPECTION TYPE:C123, LEFT HORIZ STAB L/E AT STA FSX0, THE LOWER CAP IS CRACKED. REMOVED, FABRICATED AND REPLACED CAP IAW DWG565449.Feb 24, 2000 · N706UP · Doug DC871FSDR CALA0000198Skin · dentedINSPECTION FOUND SKIN OF HORIZONTAL STABILIZER LE OB SECTION IB END DENTED. A DOUBLER WAS INSTALLED IAW EA 9-5513-2-A0602 AND SRM 51-30-2.Feb 24, 2000 · N938MC · Doug DC983SDR ABXA000130Plate · crackedRIGHT HORIZONTAL STAB PLANK WAS CRACKED AT STRINGER NR 1 XHS 204 AND STRINGER NR 2 STATION FHS 244. REPAIRED PLANK IAW DC9 SRM 55-02, FIGURE 16.Feb 22, 2000 · N933AX · Doug DC933FSDR ABXA000129Plate · crackedRIGHT HORIZONTAL STAB PLANK WAS CRACKED AT STRINGER NR 2 AND NR 3 STATION XFS 40.7 UPPER PLANK. REPAIRED PLANK IAW DC9 SRM 55-02, FIGURE 16.Feb 22, 2000 · N933AX · Doug DC933FSDR P5CA0000104Skin · dentedLEFT HORIZ STAB L/E SKIN DENT 4 LOCATIONS STAB STA L/E 165, 235, 3335 AND 385. SMOOTH OUT DENTS AND NDT CKD OK PER NDT DT-6, MM 51-00-00 SRM 51-10-01.Feb 7, 2000 · N853FT · Boeing 747122SDR RRXA000332Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO HORIZONTAL STABILIZER SKIN OUTBOARD L/E INBOARD AT STA XFS 210.000. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA DER Feb 5, 2000 · N792FT · Doug DC873FSDR CALA0000113Skin · dentedINSPECTION FOUND LEFT HORIZONTAL STABILIZER LEADING EDGE LOWER SURFACE DENTED AT XFS 71 TO XFS 77.50. A DOUBLER WAS INSTALLED IAW EA9-5513-2-AD577 AND ECRA 5510-01482.Feb 1, 2000 · N16808 · Doug DC982SDR CALA0000111Skin · dentedINSPECTION FOUND RT HORIZONTAL STABILIZER DENTED EIGHT FEET AND NINE FEET FROM STABILIZER ROOT AT LEADING EDGE. THE AREA WAS REPAIRED IAW SRM 55-03, PAGE 6 AND 6A. A DIP WAS ISSUED TO REINSPECT THE REPAIR EVERY 125 FLIGHT HOURS AND TO INSTALL A PERMANENT REPFeb 1, 2000 · N16808 · Doug DC982SDR TWAA0002006Skin · delaminatedDURING CHECK-C MAINTENANCE, THE RT HORIZ STAB TE WAS DELAMINATED, 26 IN INBD OF THE OTBD END TO 69 IN INBD OF THE OTBD END. REPAIRED TE OF RT ELEVATOR PER ARA 16277. RECHECKED BALANCE PER SRM 51-80-7 AND FOUND WITHIN MOMENT ARM REQUIRED. MOMENT 119.240.Jan 25, 2000 · N54352 · Boeing 727231SDR USAA000083Skin · crackedSTATION 129.50 TO 120.30 HORIZONTAL STABILIZER SKIN HAS A 2 INCH CRACK. INSTALLED FILLER AND DOUBLER PER TR 55-10-07 REV A. (M)Jan 21, 2000 · N448US · Boeing 7374B7SDR DHL200080376CSkin · dentedAT C-CHECK, LT HORIZONTAL STABLIZER L/E DENTED 12 FROM XRS 72 TO XRS 97.5. REMOVED LEADING EDGE IAW MM 55-10-3 PG 201, 202, 203. PERFORMED LEADING EDGE STRUCTURAL REPAIR IAW SRM 55-2-1 PG 13, 15, 16 & 17. REINSTALLED LEADING EDGE IAW MM 55-10-3 PG 201, 201 Jan 20, 2000 · N803DH · Doug DC873FSDR RRXA000051Skin · debondedDURING A MAINTENANCE VISIT FOUND SKIN DEBONDED AT CORNER, LT O/B HORIZONTAL STABILIZER. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8.Jan 18, 2000 · N792FT · Doug DC873FSDR RRXA000649Skin · crackedDURING A MAINTENANCE VISIT FOUND A DEEP DENT AND CRACK AT THE RT HORIZONTAL STAB UPPER PLATING JUST FWD OF ACCESS HOLE AT STA XE 36, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED IAW DC-8Jan 10, 2000 · N831AL · Doug DC873FSDR UPS00231263Skin · dentedRT HORIZNATAL STAB HAS DENTS WHICH ARE OUT OF LIMITS. REINSPECTED DENT AREA, DENT FOUND TO BE WITHIN LIMITS PER SRM 55-105 1.Jan 7, 2000 · N940UP · Boeing 727185CSDR CALA9901607Panel · corrodedINSPECTION FOUND RT HORIZONTAL STABILIZER LE PANEL 9202 CORRODED. A NEW PANEL WAS INSTALLED IAW SRM 51-10-5, 51-10-2, AND MM 51-20-0.Dec 16, 1999 · N33785 · Boeing 727232SDR UPS99831194Skin · puncturedINSPECTION TYPE:N/A, PUNCTURE IN LT HORIZONTAL STABILIZER LEADING EDGE. *S/D* REMOVED DAMAGED SECTION OF L/E SKIN PER SRM 55-2-1 BPT 92716 PC 1565 0. FABRICATED AND DRILLED REPAIR DOUBLER PER SRM 55-2-1. BAT 92716 12-13-99. INSTALLED DOUBLER PER SRM 55-2-1Dec 9, 1999 · N836UP · Doug DC873FSDR USAA991339Skin · crackedCLT - DURING AN OVERNIGHT CHECK VISUAL AND EDDY CURRENT, FOUND A 1.8 INCH CRACK RT HORIZONTAL STABILIZER LOWER SKIN AT REAR SPAR STA 125-126.8 SKIN. INSTALLED REPAIR DOUBLER PER TR 55-10-07 REV A. (X)Dec 5, 1999 · N528AU · Boeing 7373B7SDR GAIA99187Skin · dentedLEFT HORIZONTAL STABILIZER L/E HAS SKIN DENT, APPROXIMATELY 15 INCHES FROM INBOARD END. INSTALLED DOUBLER REPAIR AT LEFT HORIZONTAL STABILIZER LEADING EDGE. REPAIR ACCOMPLISHED IAW SRM 55-10-3 FIG 1. REF: N/R 4315. (X)Nov 23, 1999 · N916PG · Boeing 727287SDR F3LA99157Skin · corrodedDEN - DURING C-7 CHECK INSPECTION, REPORTED FORWARD TIP OF RIGHT STABILIZER CORRODED. MAINTENANCE FABRICATED REPLACEMENT PARTS AND REPAIRED PER EA NR 55-737-010. (M)Nov 22, 1999 · N1PC · Boeing 7372P6SDR AT9900877Skin · corrodedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND RIGHT HORIZONTAL STABILIZER WING TIP UPPER SKIN CORRODED BEYOND LIMITS. FABRICATED AND INSTALLED UPPER SKIN IAW DC9 SRM 51-10-04, 55-11 FIG 1, 55-03 FIG 4, AND 51-10-03.Nov 19, 1999 · N833AT · Doug DC932SDR MWEA99814Skin · chafedHORIZONTAL STABILIZER TO VERTICAL STABILIZER FAIRING ON RIGHT HAND SIDE UPPER WAS CHAFED AT AFT END, FAIRING SKIN WAS DAMAGED (OUT OF LIMITS). MTC REMOVED DAMAGED SKIN THEN DRILLED AND INSTALLED NEW SKIN.Nov 16, 1999 · N300ME · Doug DC915SDR DL72S992621Panel · wornFOUND DURING MV2 CORROSION VISIT NRC 165, A .75 INCH HOLE IN NR 4 BALANCE BOARD CLOSURE PANEL. REPAIRED PER SRM 55-20-3.Nov 16, 1999 · N538DA · Boeing 727232SDR CALA9901469Skin · brokenINSPECTION FOUND UPPER LT HORIZONTAL STABILIZER BANANA PANEL SKIN AND DOUBLER BROKEN. THE DAMAGED AREA WAS REMOVED. A DOUBLER AND FILLER WERE INSTALLED IAW SRM 55-03, FIGURE 17, 51-10-3, AND 51-10-4.Nov 5, 1999 · N69803 · Doug DC982SDR MWEA99756Skin · corrodidRIGHT HORIZONTAL STABILIZER HAD MODERATE CORROSION ON OUTBOARD HALF OF LEADING EDGE. CORROSION WAS OUT OF LIMITS. MTC FABRICATED AND INSTALLED DOUBLER ON RIGHT STABILIZER.Nov 1, 1999 · N202ME · Doug DC932SDR DL72S992319Skin · crackedTPA LTR CHECK F-2, 1 CRACK IN VERT STAB SKIN LT SIDE AT LWR SIDE OF CUTOUT FOR ACCESS PANEL 9523. REPAIRED PER MM 54-30-0.Oct 21, 1999 · N419DA · Boeing 727232SDR USAA991068Skin · crackedCLT - DURING WALK AROUND VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1.25 INCH CRACK LEFT HORIZ STABILIZER LOWER SKIN AT REAR SPAR STAB STATION 117.5. CUTOUT CRACK AND INSTALLED DOUBLER AND FILLER PER EA 65824. (M)Oct 2, 1999 · N443US · Boeing 7374B7SDR RRXA991521Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, HORIZONTAL STAB, CENTER SECTION, UPPER CENTER PLANK, UPPER SURFACE AT BL -30 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PLANK IAW DC8 SBSep 21, 1999 · N8087U · Doug DC871FSDR DLM88992071Skin · crackedTHE UPPER, AFT SKIN PANEL OF THE HORIZONTAL STABILIZER WAS FOUND CRACKED DURING AN INSPECTION BY EO 9-61905-3AD, (LT AND RT) THE DAMAGE WAS FOUND AT HMV AND REPAIRED PER ERA 333575-14AD.Sep 14, 1999 · N911DL · Doug MD88SDR CALA9901212Panel · crackedINSPECTION FOUND A 1.5 CRACK IN RT HORIZONTAL STABILIZER PANEL NR 3804 L/E. THE CRACKED AREA WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-30-2, 55-01, 51-30-2, 55-01, FIGURE 4, AND 55-12.Sep 14, 1999 · N93875 · Doug DC982SDR USAA990977Skin · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .75 INCH CRACK RT HORIZONTAL STAB TORQUE BOX LOWER SKIN ACCESS. INSTALLED REPAIR DOUBLER ACCESS PANEL PER EA 65418. (M)Sep 13, 1999 · N418US · Boeing 737401SDR SWAA991510Skin · crackedDURING SCHEDULED BC1 CHECK, FOUND RT HORIZONTALSTABILIZER LOWER SKIN CRACKED FWD OF 1ST BALANCE PANEL ALONG REAR SPAR. REPAIRED SKIN PER SWA RA NR 1-555-0313.Sep 11, 1999 · N515SW · Boeing 7375H4SDR MWEA99538Skin · damagedLEFT HORIZONTAL STABILIZER UPPER FORWARD, CENTER AND AFT SKIN PANEL HAD MANY ELONGATED HOLES. MTC REAMED HOLES, INSTALLED FASTENERS, PLY WASHERS, AND BUSHING.Aug 26, 1999 · N600ME · Doug DC914SDR MWEA99535Skin · damagedAFT HORIZONTAL STABILIZER LEFT AFT SKIN HAD DIMENSIONAL DISCREPANCIES AT STATION XE 49.720. MTC FABRICATED AND INSTALLED DOUBLER.Aug 26, 1999 · N600ME · Doug DC914SDR 2000ZZZX707Skin · damagedLEFT HORIZONTAL LEADING EDGE SCREW HOLES DEFORMED, STA XFS 123 AND XFS 160. REAMED HOLES TO .500 INCH. FABRICATED PLUG AND INSTALLED. FABRICATED STRAP AND INSTALLED PER EO 99-136 WITH APPROVED 8110-3 DATED 8-3-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC.,Aug 16, 1999 · N812TC · Doug DC8F55SDR USAA990857Skin · crackedCLT - DURING AN OVERNIGHT CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1.5 INCH CRACK LOWER SKIN RIGHT HORIZ STAB STATION 96 TO 97.5, 1.25 INCH FORWARD OF AFT SPAR. CUTOUT DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER PER TR 55-10-07 REV A. Aug 14, 1999 · N423US · Boeing 737401SDR USAA990856Skin · crackedCLT - DURING AN OVERNIGHT CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1.625 INCH CRACK LOWER SKIN RIGHT HORIZ STABILIZER STATION 124 TO STATION 125.6, 1.25 INCH FORWARD OF AFT SPAR. CUTOUT DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER PER TRAug 14, 1999 · N423US · Boeing 737401SDR UF6A990807Skin · crackedSBN - CRACK IN THE LEFT HORIZONTAL STABILIZER TRAILING EDGE AT STATION 45.72. MAINTENANCE REPAIRED DAMAGE. ALL WORK WAS DONE IAW BAE ATP SRM 51-60-01 FIGURE 1. (M)Aug 12, 1999 · N853AW · Bag ATPSDR SWAA991350Skin · crackedDURING SCHEDULED D CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN CRACKED, STA 157.10 AT REAR SPAR. REPAIRED SKIN PER ER NR 99-5774.Aug 12, 1999 · N350SW · Boeing 7373H4SDR MWEA99485Skin · crackedUPPER LEFT HORIZONTAL STABILIZER SKIN FOUND CRACKED. MTC FABRICATED AND INSTALLED NEW SKIN PANEL.Aug 12, 1999 · N600ME · Doug DC914SDR CALA9901006Skin · crackedINSPECTION FOUND TWO 1 INCH CRACKS IN LEFT L/E HORIZONTAL STABILIZER I/B SECTION ON L/E SIDE AT STA XHS 9.652. THE CRACKS WERE STOP DRILLED AND A REPAIR WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND ECRA 5510-01458.Aug 5, 1999 · N83872 · Doug DC982SDR DHL9970347CSkin · damagedAT C CHECK, LT INBD HORIZONTAL STABILIZER LEADING EDGE DAMAGED. REMOVED LEADING EDGE FOR APPROX STA 20 LE TO LE STA 147.32 PER SRM 51-30-2. REMOVED RIBS TO AID IN MAINTAINING CONTOUR OF LEADING EDGE IAW SRM 51-30-2. CUT OUT DAMAGED AREA AT LT LEADING I/B HOJul 29, 1999 · N703DH · Boeing 72730CSDR DLL14991656Skin · crackedHORIZONTAL STABILIZER LEFT UPPER SKIN, HSS 80, STIFFENER NR 31 SKIN CRACK. REPAIR THE NR 4 UPPER SKIN PANEL OF THE LEFT HORIZONTAL STABILIZER WAS FOUND WITH A 1.25 CRACK AT THE RUNOUT OF STIFFENER NR 31. THE CRACK WAS ROUTED OUT OF THE SKIN AND AN EXTERNAL AJul 23, 1999 · N740DA · Lkheed 1011385115SDR CALA9900857Skin · delaminatedINSPECTION FOUND THREE AFT T/E PANELS DELAMINATED FROM I/B HINGE POINT TO HORIZONTAL TIP AT LOWER RIGHT HORIZONTAL STABILIZER. THE THREE PANELS WERE REMOVED AND REPLACED IAW MM 51-31-01.Jul 23, 1999 · N68043 · Doug DC1010SDR UF6A990751Skin · dentedSBN - DENT IN TRAILING EDGE OF THE RIGHT HORIZONTAL STABILIZER INBOARD OF THE INBOARD HINGE. MAINTENANCE REPAIRED DENT. ALL WORK WAS DONE IAW BAE ATP SRM 51-60-01. (M)Jul 20, 1999 · N859AW · Bag ATPSDR CALA9900832Panel · corrodedINSPECTION FOUND RT HORIZONTAL STABILIZER MOST I/B UPPER L/E AFT SECTION CORRODED UNDER SKIN. REMOVED ACCESS PANEL DOUBLER AND SPLICES. DOUBLERS AND PANEL WERE INSTALLED IAW ECRA 5530-01245 AND SRM 51-31-01.Jul 16, 1999 · N68043 · Doug DC1010
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