JASC 5100

Service difficulty reports · 4,244

Reports filed under 5100 · Standard Practices/Structures, newest first.

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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 = '5100'
  ORDER BY difficulty_date DESC"

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SDR 06FDEA0962Repair · unknownRIGHT WING NR 5 SPOILER UPPER SKIN HAS BONDED REPAIR. PERFORMED INSPECTION ON REPAIR DOUBLER FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.Mar 7, 2006 · N68054 · Doug DC1010SDR 06FDEA0953Repair · noneREPAIR DOUBLER STATION 1059 - 1085 L51 - L52 MARKED NR 15 REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. VISUALLY INSPECTED REPAIR LOCATED AT STA 1059 - 1085 L51 - L52. ACCOMPLISHED PARTMar 6, 2006 · N68057 · Doug MD1010FSDR USAA060409Repair · unknownRIGHT ELEVATOR LOWER SURFACE 9 INCHES I/B OF O/B END AND 16 INCHES AFT OF FRONT SPAR. PREVIOUS REPAIR IAW SRM 55-20-01-2, DEFECT SIZE: 2.5 INCHES.Mar 6, 2006 · N527AU · Boeing 7373B7SDR USAA060410Repair · unknownRIGHT ELEVATOR LOWER SURFACE 59 INCHES I/B OF O/B END AND 10 INCHES AFT OF RIGHT. PREVIOUS REPAIR IAW SRM 55-20-01-2, DEFECT SIZE: 6 INCHES.Mar 6, 2006 · N527AU · Boeing 7373B7SDR USAA060411Repair · unknownRIGHT ELEVATOR, LOWER SURFACE 30 INCHES O/B OF I/B END AND 12 INCHES AFT OF RIGHT DAMAGED. PREVIOUS REPAIR IAW SRM 55-20-01-2, DEFECT SIZE: 6 INCHES.Mar 6, 2006 · N527AU · Boeing 7373B7SDR 06FDEA0950Repair · unknownCNT CARGO COMPT LONG 52 HAS A SPLICE REPAIR BETWEEN STA 1741 AND 1761. FITTED NEW SPLICE IAW SRM 53-10-00 FIG 2 SHT 1 VOL 1 AND EA 8-5310-95690, FAB PARTS IAW DETAIL PARTS TRAVELER N01188 AND SRM 53-10-00 FIG 2 VOL 1.Mar 6, 2006 · N563FE · Doug DC1010SDR 06FDEA0949Repair · unknownCNT CARGO COMPT BETWEEN STA 1741 AND 1761 HAS A SPLICE REPAIR ON LONG 51 RIGHT. FITTED NEW SPLICE IAW SRM 53-10-00 VOL 1 AND EA 8-5310-95690. FAB PART IAW DETAIL PART TRAVELER N01186 AND SRM 53-10-00 VOL 1.Mar 6, 2006 · N563FE · Doug DC1010SDR 06FDEA0947Repair · unknownEXTERNAL DOUBLER FUSELAGE SKIN. REMOVED OLD REPAIR IAW SRM 53-33-01 VOL 2. PERFORMED NEW REPAIR DOUBLER IAW SRM 53-20-00 FIG 6 VOL 1.Mar 6, 2006 · N68054 · Doug DC1010SDR 06FDEA0946Repair · unknownEXT PLUG REPAIR STA 1986 - 1995 LONG 44 RIGHT. REMOVED OLD REPAIR IAW SRM 51-35-01 VOL 2. PERFORMED NEW REPAIR DOUBLER IAW SRM 53-20-00 FIG 6 VOL 1.Mar 6, 2006 · N68054 · Doug DC1010SDR 06FDEA0945Repair · noneSTA 1009 - 1089 X = 8.5 SEAT TRACK SPLICE REPAIR. PERFORMED INSPECTION ON SEAT TRACK SPLICE REPAIR FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.Mar 6, 2006 · N68054 · Doug DC1010SDR 06FDEA0930Repair · misinstalledEXTERNAL UPPER FUSELAGE LEFT SIDE STA 393 WL 272 CIRCULAR DENT APPROX 1 X 1 INCH. REPAIR REQUIRES EVALUATION FOR MAJOR MINER DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. CIRCULAR DENT APPROX 1 X 1 INCH STA 393 WL 272 WAS NOT IAW Mar 3, 2006 · N492FE · Boeing 727200SDR CWQR2006002Oxygen Bottle · unserviceableRECEIVED OXYGEN CYLINDER AND REGULATOR FROM CESSNA WITH A CYLINDER BEYOND ITS SERVICE LIFE. BOTTLE HAS 15 YEAR SERVICE LIFE PER CE750 M/M CHAP 5. BOTTLE MFD DATE 9/87. RED TAGGED BOTTLE AND RETURNED TO CESSNA PARTS.Mar 2, 2006 · N942QS · Cessna 750SDR 06FDEA0924Repair · unknownREPAIR LT OB FLAP UPPER SKIN,STA.XOF 587 MARKED NR 71. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. VISUALLY INSPECTED REPAIR AT LT OB FLAP UPPER SKIN, FOUND TO BE WITHIN SRM 57-20-00 FIMar 2, 2006 · N68057 · Doug MD1010FSDR 06FDEA0890Repair · noneREPAIR DOUBLER AT STA 370, STRINGER STR 18-L , REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR DOUBLER AT STA 370 STR 18-L WAS INSTALLED USING FAA APPROVED DATA. DOUBLER WAS REMOVED Mar 2, 2006 · N467FE · Boeing 727200SDR 06FDEA0900Repair · unknownDISCREPANCY LT WING OB FLAP UPPER SKIN AT STA XOF 458 HAS DOUBLER REPAIR. REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-35-01 VOL 1 AND PERFORMED NEW REPAIR. DOUBLER IAW SRM 57-10-00 FIG 9 VOL 1.Mar 2, 2006 · N68054 · Doug DC1010SDR 06FDEA0907Repair · unknownFWD CARGO DOOR FWD PAN HAS A SPLICE REPAIR. PERFORMED REPAIR BY REMOVING SPLICE AND INSTALLED NEW ONE IAW SRM 51-33-01 VOL 2, SRM 51-35-01 VOL 2 AND SRM 52-00-01 FIG 7 SHT 2-3 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER N01204 AND SRM 52-00-01 FIG 7 SHMar 2, 2006 · N563FE · Doug DC1010SDR 06FDEA0908None · noneFOUND REPAIR STRAP IN LEFT ACC AT STA 561 LONG 48 LEFT. PERFORMED GVI ON REPAIR STRAP FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.Mar 2, 2006 · N563FE · Doug DC1010SDR 06FDEA0909Repair · noneFOUND AN EXT TRIPLE DOUBLER REPAIR ON SKIN RIGHT SIDE BETWEEN STA 1129 AND 1159 LONG 43 - 48 DIM 25" X 36" , 25" X 35". PERFORMED GVI ON DOUBLER FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8- 5100-7-5001 P1.Mar 2, 2006 · N563FE · Doug DC1010SDR 06FDEA0910Repair · noneFOUND AN EXT DOUBLER REPAIR ON SPLICED AREA BETWEEN STA 780 AND 809 LT HAND SIDE AND LONG 45-48 DIM 24.5 X 29.5 INCHES. PERFORMED GVI ON DOUBLER FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8- 5100-7-5001 P1.Mar 2, 2006 · N563FE · Doug DC1010SDR 06FDEA0911Repair · noneFWD CARGO DOOR AFT PAN HAS AN ANGLE REPAIR DIM 7 X 4 X 1.6 INCHES. PERFORMED GVI ON REPAIR FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100- 7-5001 P2.Mar 2, 2006 · N563FE · Doug DC1010SDR 06FDEA0912Repair · noneFOUND REPAIR ANGLE IN NLG W/W AT STA 515 LONG 48 LEFT. PERFORMED GVI ON REPAIR ANGLE FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.Mar 2, 2006 · N563FE · Doug DC1010SDR 06FDEA0913Repair · noneFOUND EXT DOUBLER APPROX 4 X 4 INCH ON RIGHT T/E HORIZ STAB AT STA XE 87.167 UPPER SIDE. PERFORMED GVI ON REPAIR FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100- 7-5001 P2.Mar 2, 2006 · N563FE · Doug DC1010SDR 06FDEA0888Repair · noneFOUND 3 REPAIRS LOCATED ON NR 3 CARGO DOOR OUTER SKIN, REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIRS WERE ACCOMPLISHED USING FAA APPROVED DATA. REPAIRS FOUND TO BE IAW SRM 52-00-3 FIG 3. REPAIRS CLASSIFIED AS MAJOR.Mar 2, 2006 · N275FE · Boeing 727233SDR 06FDEA0887Repair · noneFOUND REPAIR LOCATED ON RIGHT WING L/E ABOVE THE NR 4 KRUGER FLAP REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR FOUND TO IAW SRM 57-30-4 FIG 2. REPAIR CLASSIFIED AS MAJOR IAW FEDMar 2, 2006 · N275FE · Boeing 727233SDR 06FDEA0886Repair · unknownFOUND 2 REPAIRS LOCATED ON THE RIGHT L/E WING UPPER SURFACE STA 450 AND 460. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIRS WERE DETERMINED TO BE IAW SRM 57-30-4 FMar 2, 2006 · N275FE · Boeing 727227SDR 06FDEA0883Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 400 STR 17L-18L WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 53-30-3 FIG 1, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL THICKNESS AND TYPE, FASTENER SPACING AND NUMBER, GENERAL WORKMMar 1, 2006 · N275FE · Boeing 727233SDR 06FDEA0882Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 188 STR 21R WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 53-30-3 FIG 5, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBERS, GENERAL WORKMar 1, 2006 · N275FE · Boeing 727233SDR 06FDEA0881Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 1030 STR 18L-19L WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 53-30-3 FIG 1, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SIZE, SHAPE, MATERIAL THICKNESS AND TYPE, FASTENER SPACING AND NUMBER, GENERAL WORKMar 1, 2006 · N275FE · Boeing 727233SDR 06FDEA0880Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 720E STR 19L WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 53-30-3, FIG 4 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL THICKNESS AND TYPE, FASTENER SPACING AND NUMBERS, GENERAL WORKMANSMar 1, 2006 · N275FE · Boeing 727233SDR 06FDEA0879Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 1050 STR 27R-28R WAS DETERMINED TO BE ACCOMPLISHED PER SRM 53-30-3 FIG 1, BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL THICKNESS AND TYPE, FASTENER SPACING AND NUMBERS, GENERAL WORKMar 1, 2006 · N275FE · Boeing 727233SDR 06FDEA0870Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 540 STR 27R WAS ACCOMPLISHED PER FEDEX EA 7-5330-85285, BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBERS, GENERAL WORKMANSHIP, REPAIR ISFeb 28, 2006 · N275FE · Boeing 727233SDR DXTA200601269Pcb · inoperativeUNCORRECTABLE T/O CONFIGURATION MASTER CAUTION ON TAKEOFF ROLL. ALL PARAMETERS WERE MET. BRAKES, FLAPS, AIRBRAKES, TRIM, AND AUTOPILOT WERE IN CORRECT POSITION. NO MESSAGES ON EIED EITHER. CAN'T CORRECT. AUDIO WARNING, "NO TAKEOFF", ALSO CAME ON. REMOVEDFeb 27, 2006 · N265QS · Amd FALCON2000SDR MASA200600574None · noneASH 6519 PVR - ABORTED TAKEOFF, FO SUSPECTED THE ELEVATOR WAS STIFF. AFTER REDUCING THRUST, FO DECIDED ELEVATOR WAS FINE, BUT NOT ENOUGH RUN-WAY TO CONTINUE TAKEOFF. FLIGHT CREW DETERMINED ELEVATOR FUNCTIONING PROPERLY. NO FURTHER ACTION REQUIRED.Feb 26, 2006 · N904FJ · Cndair CL6002D24SDR F06022Transducer · malfunctionedTHE CREW REPORTED A SPOILER MESSAGE ON LANDING. MAINTENANCE REPLACED THE WHEEL SPEED TRANSDUCER.Feb 25, 2006 · N829MJ · Emb EMB145LRSDR 06FDEA0843Repair · misinstalledREPAIR DOUBLER RT I/B FLAP LOWER T/E SKIN STA XIFH 311 MARKED NR 41 REPAIR REQUIRES EVALUATION FOR MAJOR/ MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR DOUBLER FOUND TO BE NOT IN COMPLIANCE WITH THE FAA APPROVED DATA. Feb 25, 2006 · N68057 · Doug MD1010FSDR IXXA06SMN068SNone · noneDURING ROUTINE C-CHECK INSPECTION, ELT ANTENNA REMOVAL AND BLANKING PLATE INSTALLATION. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 02-06-06, ENGINEERING AUTHORIZATION AA71-2 REV IR DATE 01-24-06. REMOVED ELT ANTENNA IAW DC-8 MM 25-60-0 PAGE 201. FABRICFeb 24, 2006 · N722CX · Doug DC872SDR IXXA06SMN066SNone · noneDURING ROUTINE C-CHECK INSPECTION, EO 25-DC8-198 R9 INSTALL COMAT BOX. PERFORMED MAJOR ALTERATION IAW FAA FORM 8110-3 DATE 09-23-05, ATI DWG A95166-4 REV N DATE 09-23-05. INSTALLED COMAT BOX IAW ATI DWG 95166-4. COMPLIED WITH EO 25-DC8-198.Feb 24, 2006 · N722CX · Doug DC872SDR 06FDEA0834Repair · noneLT WING INBOARD AILERON AT STA XIA 341 LOWER SKIN HAS DOUBLER REPAIR. PERFORMED GVI ON DOUBLER REPAIR FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.Feb 24, 2006 · N68054 · Doug DC1010SDR 06FDEA0830Repair · noneLT WING INBOARD AILERON AT XIA 341 UPPER SKIN HAS DOUBLER REPAIR. PERFORMED A GVI ON DOUBLER REPAIR AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.Feb 24, 2006 · N68054 · Doug DC1010SDR 06FDEA0829Repair · noneSTA 1809 X 27.5 EXISTING SEAT TRACK PLUG REPAIR. PERFORMED A GVI OF REPAIR AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8- 5100-7-5001 P2.Feb 24, 2006 · N68054 · Doug DC1010SDR 06FDEA0828Repair · noneEXISTING DOUBLER REPAIR ON LT HORIZONTAL STAB UPPER SKIN AT XE 77.100. PERFORMED GVI OF REPAIR AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8- 5100-7-5001 P2.Feb 24, 2006 · N68054 · Doug DC1010SDR 06FDEA0827Repair · noneSTA 1491 X -47.5 EXISTING SEAT TRACK PLUG REPAIR. PERFORMED GVI OF REPAIR AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8- 5100-7-5001 P2.Feb 24, 2006 · N68054 · Doug DC1010SDR 06FDEA0826Repair · noneSTA 939 X 27.5 EXISTING TRACK PLUG REPAIR. PERFORMED GVI OF REPAIR AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8- 5100-7-5001 P2.Feb 24, 2006 · N68054 · Doug DC1010SDR 06FDEA0825Repair · noneSTA 1440 X - 47.5 EXISTING SEAT TRACK PLUG REPAIR. PERFORMED GVI OF REPAIR AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8- 5100-7-5001 P2.Feb 24, 2006 · N68054 · Doug DC1010SDR 06FDEA0824Repair · unknownRT OUTBOARD FLAP LOWER SKIN: DURING ACCOMPLISHED NRC N01229 FOUND EXISTING REPAIR INTERNAL LOWER SKIN WITH CUTOUT NOT IN COMPLIANCE WITH SRM. REMOVED PANEL SECTION TO PERFORM REPAIR IAW MM 20-50-02 AND REMOVED SEALANT IAW SRM 51-41-01 VOL 2. REPAIRED SKIN IFeb 24, 2006 · N563FE · Doug DC1010SDR 06FDEA0808Repair · noneDURING AIRPLANE'S MODIFICATION FROM P TO F/ACF FOUND BETWEEN STA 840-859, STR 39-42, RT, 3 EA FLUSH PATCH WITH INTERNAL DOUBLER. NO ACTION REQUIRED. REPAIR IS CONFORM TO SRM 53-20-00 FIG 13 SH 8/9. PERFORMED EA 8-5330-94668 PART 1 INSPECTION. NO DEFECT FOUFeb 22, 2006 · N568FE · Doug DC1010SDR KPVA20065Skin · ground damageCOMMISSARY CART HIT AIRCRAFT, MADE A 4 INCH HOLE NEAR THE EXTERNAL POWER RECEPTACLE. REPAIRED FWD PUNCTURE AT STA X136.8 - X151.6 BETWEEN STRINGERS 24P AND 26P IAW BOMBARDIER REPAIR DRAWING 8-53-8934. REPAIRED AFT PUNCTURE AT STA X182.00 - X201.15 BETWEEN STFeb 20, 2006 · N805WP · Dhav DHC8103SDR AWXA200600354None · noneLAS - FLIGHT CONTROL - CREW REPORTED THE SLATS OVERSPEED ON DEPARTURE, APPROXIMATELY 5 KTS FOR 5 SECS WITH SLATS IN MOTION FROM 1 TO ZERO POSITION. MAINTENANCE INSPECTED THE SLATS IAW AIRBUS 319 MM 05-51-13. NO DEFECTS WERE NOTED AND NO FURTHER ACTION WAS REFeb 20, 2006 · N802AW · Airbus A319132SDR AWXA200600422Repair · noneMCN - DURING C19 CHECK SKIN PANEL FROM BS 727 TO BS 907 AND FROM STR 20L TO STR 25L WAS BEING REPLACED IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5360-06030-SS2. IT WAS DISCOVERED THAT AN EXISTING REPAIR WAS OVER LAPPING THE OLD SKIN PANEL AT BS 727D-Feb 17, 2006 · N166AW · Boeing 73733ASDR QXEA200600491Fitting · looseSEA FLT 2232 - AFTER START DE-ICE PRESSURE STAYED AT 1200PSI AND A/C DID NOT PRESSURIZE FOR ABOUT 1.5 MINUTES. AFTER THAT TIME PRESSURE CAME UP TO 18PSI AND PRESSURIZATION RETURNED TO NORMAL. DURING AUTO FEATHER TEST OF ENG NR 1 DE-ICE PRESSURE RETURNED TO 12PFeb 15, 2006 · N368PH · Dhav DHC8202
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