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 95ZZZX5608Skin · crackedDURING AN ANNUAL INSPECTION, FOUND THE CENTER SECTION OF THE HORIZONTAL STABILIZER WAS DEFORMED AND CRACKED. IT IS POSSIBLE THAT MISHANDLING DURING GROUND HANDLING IS THE CAUSE. CESSNA HAS A HEAVY DUTY CENTER SECTION SPAR AND SKIN REPLACEMENT.Sep 19, 1995 · N1261U · Cessna 172MSDR AR082251Skin · corrodedDURING C-CHECK INSPECTION, FOUND RT HORIZONTAL STABILIZER UPPER TIP WITH EXFOLIATION (LEVEL 2) CORROSION. CUT OUT CORRODED AREA, FABRICATED AND INSTALLED DOUBLER IAW SRM 55-2-1. SEALED REPAIR IAW SRM 51-20-0. (X)Aug 22, 1995 · N791AL · Doug DC862FSDR 9515489607Skin · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE LEFT HORIZONTAL UPPER AFT SKIN. REPAIRED SKIN (P/N 5922578-502), PER EA 96-98094.Aug 16, 1995 · N607NW · Doug DC932SDR DL72E953121Panel · damagedUPON ARRIVAL PDX, FOUND ON RIGHT HORZ STAB LOWER SURFACE A CLOSURE PANEL FOR AN ELEV BALANCE PANEL BAY. PANEL 9216 THE FWD THIRD OF PANEL HAD SEPARATED FROM THE ACFT AND EMBEDDED ITSELF INTO THE TAIL CONE. ALSO, FOUND LOWER SKIN DAMAGED ON RIGHT ELEVATOR. Jul 20, 1995 · N831WA · Boeing 727247SDR 95ZZZX3973Skin · crackedUPON STRIPPING OF PAINT ON THE HORIZONTAL STABILIZER, A SERIES OF SMALL CRACKS WAS DETECTED ON THE UPPER SKIN RIGHT SIDE OF THE HORIZONTAL STABILIZER. THERE WERE 5 CRACKS RANGING IN SIZE FROM .5 INCH TO 5.5 INCHES LOCATED BETWEEN STA 91.25 AND STA 113.25. THJul 17, 1995 · N238SA · Dhav DHC6300SDR 95ZZZX3615Skin · crackedDURING ANNUAL INSPECTION, THE FRONT SPAR AND SKID OF THE HORIZONTAL STABILIZER WERE FOUND SEVERELY CRACKED AND BUCKLED. NEW PARTS FROM CESSNA WERE REINFORCED AND MUCH STRONGER THAN ORIGINAL. SUSPECT IMPROPER GROUND HANDLING OR SEVERE TURBULENCE.Jul 13, 1995 · N1261U · Cessna 172MSDR UPS803831Skin · damagedSUPPLEMENTAL MRR - WHILE ON GROUND, MAINTENANCE FOUND DAMAGE TO LEADING EDGE OF RT STABILIZER, DENT 5 INCHES WIDE, 5.5 INCHES TALL, 2 INCHES DEEP WITH 5 INCH VERTICAL CRACK IN CTR, 100 INCHES OUTBOARD FROM FUSELAGE. CUT 5 INCH BY 5 INCH HOLE TO REMOVE DAMAGE Jul 11, 1995 · N867UP · Doug DC873FSDR CAL950671Skin · dentedDHN - FLT MIDD - INSPECTION FOUND A 3 INCH BY 1.5 INCH BY .25 INCH DEEP DENT IN RT HORIZONTAL STABILIZER LEADING EDGE. A DOUBLER REPAIR WAS INSTALLED IAW SRM 55-10-01. (X)Jul 8, 1995 · N14324 · Boeing 7373T0SDR DLL13952923Skin · crackedDURING HANGER INSPECTION, THE LT HORZ STAB WAS FOUND TO HAVE CRACKED RIBS AND L/E PANEL. REPAIRED PER SRM 55-12-00.Jul 5, 1995 · N781DL · Lkheed 10113851SDR P5CA9500371Strip · crackedRIGHT STABILIZER TRAILING EDGE STRIP CRACKED BETWEEN NAV LIGHT AND ELEVATOR. REPAIRED PER BOEING SRM 51-40-04.Jun 30, 1995 · N831FT · Boeing 747121SDR DL72S952870Skin · crackedRT HORIZONTAL STABILIZER I/B EDGE OF UPPER SKIN BENT AND CRACKED WHERE SEAL ATTACHES AT CENTER BOX AREA, BETWEEN FWD AND AFT SPAR. REPAIRED PER SRM 55-10-3 FIG 4.Jun 27, 1995 · N489DA · Boeing 727232SDR 95ZZZM443Skin · corrodedDURING C-CHECK INSPECTION, FOUND LEFT SIDE HORIZONTAL STABILIZER, UPPER SKIN HAD CORROSION LEVEL 2 FROM XE 219.979 TO XE 312.500 AT TRAILING EDGE. REMOVED PANEL AND ROUTED TO OUTSIDE SERVICE. PANEL WAS RESKINNED AND REINSTALLED.Jun 15, 1995 · N802BN · Doug DC862SDR 95ZZZM436Skin · corrodedDURING C-CHECK INSPECTION, FOUND LEFT SIDE HORIZONTAL STABILIZER, LOWER SKIN SURFACE AT TRAILING EDGE BETWEEN XE 272.00 TO STABILIZER TIP WITH LEVEL 2 CORROSION. REPLACED PANEL IAW SRM 51-1-21 PG 20-25 AND SRM 55-1-0.Jun 15, 1995 · N802BN · Doug DC862SDR 95ZZZM435Skin · corrodedDURING C-CHECK INSPECTION, FOUND LEFT SIDE HORIZONTAL STABILIZER LOWER SKIN SURFACE AT TRAILING EDGE BETWEEN XE 272.00 TO STAB TIP WITH LEVEL 2 CORROSION. REMOVED DAMAGED SKIN PANELS, FABRICATED, TREATED AND INSTALLED NEW PANELS IAW SRM 51-1-8, 51-1-21 PG 20-Jun 15, 1995 · N802BN · Doug DC862SDR 95ZZZM433Skin · corrodedDURING C-CHECK, FOUND LEVEL 2 CORROSION AROUND ATTACH FASTENERS ON UPPER SURFACE OF RT HORIZONTAL STABILIZER LEADING EDGE OUTBOARD FROM XFS 178.00 TO XH 285.00. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED FILLERS AND DOUBLERS IAW DER DWG ARW 950051-0968.Jun 15, 1995 · N802BN · Doug DC862SDR 95ZZZM431Skin · corrodedDURING C-CHECK, FOUND LEVEL 2 CORROSION AROUND ATTACH FASTENERS ON UPPER SURFACE OF LEFT HORIZ STAB L/E OUTBOARD FROM XH 285.00 TO XFS 178.00. CUTOUT DAMAGED AREA. FABRICATED AND INSTALLED FILLERS AND DOUBLERS IAW DER DWG ARW 950051-0969 SRM 51-3-0.Jun 15, 1995 · N802BN · Doug DC862SDR 95ZZZM429Skin · corrodedFOUND DURING C-CHECK, LEFT HORIZONTAL STABLE INBOARD FROM XAR TO XFS 178 HAS LEVEL II CORROSION ON UPPER SIDE AROUND ATTACH FASTENERS. CUT OUT CORRODED AREA, FABRICATED DOUBLERS AND FILLERS IAW DER ARW 950051-0966 AND SRM 57-2-1 FIG 38 DAC 274118/G1P1518.Jun 15, 1995 · N802BN · Doug DC862SDR 95ZZZM420Skin · corrodedDURING C-CHECK INSPECTION, FOUND LEFT SIDE HORIZONTAL STABILIZER, UPPER SKIN HAS CORROSION LEVEL 2 FROM XE 219.979 TO XE 312.500 AT T/E. REMOVED PANEL AND ROUTED TO OUTSIDE SERVICE. PANEL WAS RESKINNED AND REINSTALLED. (M)Jun 15, 1995 · N802BN · Doug DC862SDR 9513429612Skin · corrosionDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LEFT HORIZONTAL STABILIZER UPPER AFT SKIN, LOWER SURFACE OF THE STRINGER NR 3 LAP FLANGE. REPAIRED PER EA 96-98094.Jun 13, 1995 · N612NW · Doug DC932SDR P5CA9500029Panel · damagedHOLE IN PANEL 334GRB LOWER STABILIZER. REPAIRED PER BOEING SRM 51-40-01.Jun 2, 1995 · N851FT · Boeing 747122SDR 95ZZZM172Panel · holeFOUND HOLE IN PANEL 334GRB LOWER STABILIZER. REPAIRED PER BOEING SRM 51-40-01.Jun 2, 1995 · N851FT · Boeing 747122SDR 95ZZZX5888Skin · corrodedWHEN AIRCRAFT WAS STRIPPED FOR PAINTING, SEVERE CORROSION WAS NOTED WITH HOLES THROUGH SKIN AND INTO HONEYCOMB, APPEARS TO BE INTERGRANULAR CORROSION, POSSIBLY STARTED AT MANUFACTURING PROCESS.May 25, 1995 · N129LP · Beech 60SDR DL73E952264Skin · crackedDURING SHOP INSPECTION, THE LEFT HORIZONTAL STABILIZER LEADING EDGE PANEL WAS FOUND CRACKED. REPAIRED PER SRM 55-10-3.May 23, 1995 · N244WA · Boeing 737247SDR ABXA9500517Skin · crackedDURING D-CHECK AND COMPLIANCE OF ASB A55-16, FOUND THE RIGHT HORIZONTAL STABILIZER OUTBOARD UPPER CENTER SKIN PLANK CRACKED AT BOLT HOLES 10 AND 11. REMOVED AND REPLACED THE RIGHT HORIZONTAL STABILIZER IAW DC-8 MM CHAPTER 55.May 16, 1995 · N849AX · Doug DC861SDR UPS403215Panel · delaminatedMAINTENANCE REPORTED PANEL DELAMINATED ON RT HORIZONTAL STAB, LWR SURFACE, 2ND PANEL FROM OUTBOARD. INSTALLED REPAIR PER UPS EO B747-5510-6994A.May 11, 1995 · N674UP · Boeing 747123FSDR HEEA954937Skin · crackedCRACK ON L/H LOWER OUTER SKIN. STOP DRILLED CRACK.May 9, 1995 · N60951 · Snias AS350B2SDR UPS203186Panel · crackWHILE IN C-CHECK, MAINTENANCE FOUND CRACK IN HORIZONTAL STAB. L/E PANEL 9203, AT 4TH RIB FROM I/B EDGE. INSTALLED REPAIR PER SRM 55-10-3.May 8, 1995 · N949UP · Boeing 72725CSDR DL767951989Wedge · damagedFOUND DURING INSPECTION DFW, HOLE IN T/E WEDGE LEFT HORIZ STAB 3 INCHES FWD OF T/E 30 INCH INBD OF TIP. REPAIRED PER SRM 55-10-01.Apr 30, 1995 · N114DL · Boeing 767232SDR SCNA95111Skin · disbondingDURING C-CHECK, FOUND DISBONDING OF PREVIOUS REPAIR ON RIGHT HAND SIDE OF HORIZONTAL STABILIZER. CUT OUT DAMAGED AREA, FABRICATED FILLER AND DOUBLER AND INSTALLED IAW SRM 55-10-03 FIGURE 2.Apr 26, 1995 · N275AF · Boeing 727227SDR 95ZZZM6Skin · delaminatedDURING SERVICE CHECK, FOUND OUTBOARD ELEVATOR UPPER SKIN DELAMINATED. REPAIRED PER SRM 51-40-09 FIG B-200 DEGREES WET LAYUP. REPAIR IS CLASSIFIED AS TIME LIMITED. PERMANENT REPAIR MUST BE ACCOMPLISHED PER SRM 51-40-12 AT NEXT C-CHECK NOT TO EXCEED 18 MONTHSApr 24, 1995 · N832FT · Boeing 747121SDR CAL950312Skin · gougedFLT NR 0225 - FLL - ON OVERNIGHT INSPECTION, FOUND 5 INCH .125 INCH DEEP GOUGE WITH SMALL HOLE ON THE MOST INBOARD LEFT HORIZ STABILIZER, REQUIRED PER ECRA 55-10-01299 AND SETUP REPETIVE INSPECTION. (W)Apr 22, 1995 · N70330 · Boeing 7373T0SDR 95FDEA00226Skin · damaged9503-11 LEFT HORIZONTAL STABILIZER INTERSPAR SKIN (LWR SURFACE) IS DAMAGED BETWEEN STAB STA 151.81 AND STAB 169.81. REPAIRED DAMAGED AREA ON LEFT HORIZONTAIL STAB LOWER SKIN IAW FEDEX SRM 55-10-3.Mar 10, 1995 · N190FE · Boeing 72722SDR 95ZZZW535Skin · corrodedLEVEL 2 CORROSION, LEFT HORIZONTAL STABILIZER LOWER SURFACE SKI AT REAR SPAR CAP HAS BULGING CORROSION AROUND RIVETS FROM INBOARD END TO TIP. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PER SRM 51-1-2. (W)Mar 3, 1995 · N772CA · Doug DC862SDR 95ZZZW533Skin · corrodedLEVEL 2 CORROSION, RT HORIZONTAL STAB UPPER SURFACE SKIN AT REAR SPAR CAP HAS BULGING CORROSION AROUND RIVETS FROM INBOARD END TO TIP. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PER SRM 55-3-0. (W)Mar 3, 1995 · N772CA · Doug DC862SDR 95ZZZW531Skin · corrodedLEVEL 2 CORROSION, RT HORIZONTAL STABILIZER LOWER SURFACE SKIN AT REAR SPAR CAP HAS BULGING CORROSION AROUND RIVETS FROM INBOARD END TO TIP. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PER SRM 51-1-1. (W)Mar 3, 1995 · N772CA · Doug DC862SDR UPS202473Skin · corrodedDURING "C" CHECK MAINTENANCE FOUND CORR. ON RT HORIZONTAL STAB UPPER T/E IN BAY NR 5 NEAR O/B END. REPLACED PER SRM 51-30-2, 55-10-06.Feb 22, 1995 · N933UP · Boeing 72725CSDR CAL950108Skin · crackedGSO - INSPECTION FOUND A .50 INCH CRACK IN THE LT HORIZONTAL STABILIZER TRAILING EDGE LOWER SKIN AT STA 66. THE CRACK WAS STOP DRILLED AND REPAIR DOUBLERS WERE INSTALLED IAW SRM 55-10-3 AND SRM 51-30-2. (X)Feb 1, 1995 · N14233 · Boeing 737217
Back to JASC 5512