JASC 5100

Service difficulty reports · 4,244

Reports filed under 5100 · Standard Practices/Structures, 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 = '5100'
  ORDER BY difficulty_date DESC"

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SDR 06FDEA1443Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 1090 STR 26L WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 3 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS. GENERAL WORKMANSHIP AND REPAIR ISApr 13, 2006 · N468FE · Boeing 727225SDR 06FDEA1441Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 1100 STR 23R WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 1, BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SIZE, SHAPE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS, GENERAL WORKMANSHIP. REPAIR IS CApr 13, 2006 · N468FE · Boeing 727225SDR 06FDEA1442Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 1140 STR 29L WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 3 BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS. REPAIR IS CLASSIFED AS MAJOR PERApr 13, 2006 · N468FE · Boeing 727225SDR 06FDEA1440Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 1050 STR 28R WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 3, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SIZE, SHAPE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS, GENERAL WORKMANSHIP. REPAIR IS Apr 13, 2006 · N468FE · Boeing 727225SDR 06FDEA1439Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 415 STR 17R WAS ACCOMPLISHED IAW EO 7- 5313-7-2304 PT2 SECT A, BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTING OF LOCATION, SIZE, SHAPE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS, GENERAL WORKMANSHIP,Apr 13, 2006 · N468FE · Boeing 727225SDR 06FDEA1433Repair · unknownAT FS 83 STRINGER 35L REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR WAS DETERMINED NOT IN COMPLIANCE WITH APPROVED DATA DUE TO INCORRECT REPAIR MATERIAL. REMOVED EXISTING REPAIR AND Apr 12, 2006 · N455FE · Airbus A310222SDR ASAA0610442Repair · noneTIME LIMITED SKIN REPAIR. REPAIRED PER ASA EA 5330 02075Apr 11, 2006 · N742AS · Boeing 737290CSDR ASAA0610424Repair · noneTIME LIMITED REPAIR. REPAIRED PER ASA EA 5330 02075.Apr 11, 2006 · N742AS · Boeing 737290CSDR MALA060237Repair · misinstalledDURING F1.I, F1.E, C5.I IN YYC, FOUND EXISTING REPAIR AT FRAME 19 DOES NOT CONFORM TO EO#A53047. REPAIRED IAW EO#A53474.Apr 5, 2006 · N515XJ · Bac AVRO146RJ85ASDR MASA200601024None · noneASH 6015 PHX, BANDAID REMOVED FROM FIRST AID KIT. MX REPLACED THE KIT.Apr 5, 2006 · N7264V · Cndair CL6002B19SDR UPS06546617None · pilot errorNOSE GEAR UNSAFE LEFT ON WITH GEAR HANDLE DOWN.Apr 4, 2006 · N405UP · Boeing 75724APFSDR 06FDEA1290Structure · damagedFOUND VERTICAL LEADING EDGE RIGHT SIDE ATTACH LANDING HAS ELONGATED FASTENER HOLE AT APPROXIMATELY RIB 14. COMPLIED WITH EA 6-5530-97607 PART 1.Apr 3, 2006 · N455FE · Airbus A310322SDR 06FDEA1289Repair · unknownREPAIR LOC, ON LT O/B FLAP UPPER SURFACE 48 INCH FROM I/B END REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. COMPLIED WITH EA 6-5750-97513 PART 1.Apr 3, 2006 · N455FE · Airbus A310322SDR 06FDEA1287Repair · unknownREPAIR LOC, ON R1 DOOR UPPER EDGE REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. COMPLIED WITH EA 6-5210-97507.Apr 3, 2006 · N455FE · Airbus A310322SDR 06FDEA1286Repair · unknownREPAIR LOC, AT FS 87 STRG 34R REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. COMPLIED WITH EA 6-5330-97506 PART 1.Apr 3, 2006 · N455FE · Airbus A310322SDR 06FDEA1284Repair · unknownREPAIR LOC, LT HORIZ STAB REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIRED IAW EA 6-5510-97564 DUE TO EXISTING REPAIR MATERIAL NOT PER A310-200 55-12-12.Apr 3, 2006 · N455FE · Airbus A310322SDR EIA2006043Switch · damagedON LANDING, RT WING OVERHEAT LIGHT ON. FOUND SWITCH S874 NOT IN BRACKET AND PINCHED AGAINST STRINGERS. REINSTALLED SWITCH AS PER MM 26-18-02. OPS CHK GOOD AS PER MM 26-18-00.Apr 2, 2006 · N471EV · Boeing 747273CSDR MASA200600979None · noneASH 7152 CLT, THE ELEVATOR DISCONNECT WAS FOUND EXTENDED. ELEVATOR DISCONNECT FOUND PULLED. MX RESEATED THE HANDLE.Apr 1, 2006 · N857MJ · Emb EMB145LRSDR IXXA06RNG001SSkin · misrepairedDURING A ROUTINE C-CHECK INSPECTION FOUND A TEMPORARY REPAIR ON INBOARD EXTENDED LEADING EDGE AROUND STA XFS 51.250 TO 57.500 LT. IMPROPER REPAIR WAS REMOVED AND NEW REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW EWO ATI 57-065. FAA FORM 8110-3 WAS ISSUED AMar 31, 2006 · N823BX · Doug DC871FSDR 06FDEA1252Repair · noneDURING AIRPLANE'S MODIFICATION FROM P TO F/ACF FOUND: LT WING, LEADING EDGE, XORS 506, EXISTING REPAIR ON LOWER SKIN. NO ACTION REQUIRED. REPAIR MEETS SRM 57-10-00 FIG 68 REQUIREMENTS.Mar 28, 2006 · N568FE · Doug DC1010SDR 06FDEA1251Repair · noneDURING AIRPLANE'S MODIFICATION FROM P TO F/ACF FOUND: CAC COMPT, BETWEEN STR 50-51 LT, STA 1129 FRAME WITH EXISTING REPAIR. REMOVED EXISTING FRAME REPAIR SPLICE IAW SRM 51-31-01 VOL II AND REPLACED FRAME FROM L48 LT TO L48 RT IAW DWG AAA 7046. FRAME P/N: AAMar 28, 2006 · N568FE · Doug DC1010SDR 06FDEA1250Repair · noneDURING AIRPLANE'S MODIFICATION FROM P TO F/ACF FOUND: AIR CONDITIONING COMPT, STA 535, LT SIDE, EXISTING REPAIR AT BULKHEAD. NO ACTION REQUIRED, BULKHEAD WEB REPAIRED PER ENGINEERING ROD 01-03-06-002 AND IS FAA 8110-3 APPROVED ON 2/21/01.Mar 28, 2006 · N568FE · Doug DC1010SDR 06FDEA1249Repair · noneCOMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED AT FUSELAGE ON RT MCD SEAT TRACK BETWEEN FR 62 TO FR 63 FS 3355 TO FS 3408, AT -145. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATMar 28, 2006 · N426FE · Airbus A310203SDR 06FDEA1248Repair · unknownCOMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED AT FUSELAGE ON RT AFT PIT CROSSBEAM AT FR 65 TO FR 65 FS 3514 TO FS 3514, AND -Y20 UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATIONMar 28, 2006 · N426FE · Airbus A310203SDR DL76L060225Switch · pilot errorRUDDER RATIO LIGHT AND EICAS ILLUM ON TAXI OUT. RUDDER WILL NOT SHOW FULL MOVEMENT ON FLIGHT CONTROL CHECK. FOUND RUDDER RATIO IN TEST POSITION. CYCLED SWITCH TO NORMAL, OPS CHECK GOOD.Mar 27, 2006 · N194DN · Boeing 767332SDR MALA060221Repair · unknownCARRY OUT A DETAILED VISUAL INSPECTION OF REPAIR ON FORWARD CARGO DOOR OUTER SKIN. INSPECTION CARRIED OUT IAW EO#A52104.Mar 27, 2006 · N517XJ · Bac AVRO146RJ85ASDR MALA060220Repair · unknownCARRY OUT A DETAILED VISUAL AND EDDY CURRENT INSPECTION OF EXISTING REPAIR ON RT AIRBRAKE. INSPECTION CARRIED OUT IAW EO#A53468.Mar 27, 2006 · N517XJ · Bac AVRO146RJ85ASDR MASA200600921Unknown · pilot errorASH 7315 JFK, CAPTAIN REPORTED A SPOILER FAULT. MAINTENANCE CONTROL TROUBLESHOT TO HYDRAULICS ARE IN THE AUTO POSITION.Mar 27, 2006 · N75996 · Cndair CL6002B19SDR 06FDEA1244Repair · noneDURING AIRPLANE'S MODIFICATION FROM P TO F/ACF FOUND: AIR CONDITIONING COMPT, BULKHEAD, RT SIDE, STA 535: EXISTING REPAIR. NO ACTION REQUIRED. BULKHEAD WEB REPAIRED PER ENGINEERING ROD 01-03-06-002 AND IS FAA 8118-3 APPROVED ON 2/21/01.Mar 27, 2006 · N568FE · Doug DC1010SDR 06FDEA1183Repair · noneDURING AIRPLANE'S MODIFICATION FROM P TO F/ACF FOUND: RIGHT WING, INBOARD FLAP, STA XIFH 140, EXISTING REPAIR WITH CHARRY RIVETS. NO ACTION TAKEN, EXISTING REPAIR MEETS SRM 57-00-01 FIG 4 SH 2 REQUIREMENTS. BLIND FASTENER ACCEPTABLE PER SRM 57-00-01 PAR 14)Mar 21, 2006 · N568FE · Doug DC1010SDR 06FDEA1181Repair · noneDURING AIRPLANE'S MODIFICATION FROM P TO F/ACF FOUND: CENTER CARGO COMPT STA 1721, EXISTING REPAIR ON BEAM. NO ACTION TAKEN, REPAIR IS CONFORM TO SRM 53-00-01 FIG 9 SH 7.Mar 21, 2006 · N568FE · Doug DC1010SDR 06FDEA1180Repair · noneDURING AIRPLANE'S MODIFICATION FROM P TO F/ACF FOUND: CENTER CARGO COMPT, STA 1701, EXISTING REPAIR ON BEAM. NO ACTION TAKEN, REPAIR IS CONFORM TO SRM 543-60-00 FIG 3.Mar 21, 2006 · N568FE · Doug DC1010SDR 06FDEA1179Repair · noneDURING AIRPLANE'S MODIFICATION FROM P TO F/ACF FOUND: RT WING, LEADING EDGE STA XFS 155, EXISTING REPAIR ON SKIN. NO ACTION TAKEN, REPAIR IS CONFORM TO SRM 57-10-00 FIG 40.Mar 21, 2006 · N568FE · Doug DC1010SDR 06FDEA1178Repair · noneDURING AIRPLANE'S MODIFICATION FROM P TO F/ACF FOUND: LT WING, LEADING EDGE, STA XFS 150, EXISTING REPAIR ON EXT SIDE. NO ACTION TAKEN, REPAIR IS CONFORM TO SRM 57-10-00 FIG 40.Mar 21, 2006 · N568FE · Doug DC1010SDR 06FDEA1177Repair · noneDURING AIRPLANE'S MODIFICATION FROM P TO F/ACF FOUND: STA 1159, STR 42-43, RT, EXTERNAL REPAIR DOUBLER. NO ACTION TAKEN, REPAIR IS CONFORM TO SR10530073-7003.Mar 21, 2006 · N568FE · Doug DC1010SDR 06FDEA1163Repair · noneDURING AIRPLANE'S MODIFICATION FROM P TO F/ACF FOUND: BETWEEN STA 575-595, STR 44-46, LT EXTERNAL REPAIR DOUBLER. NO ACTION REQUIRED, REPAIR MEETS CRITERIA OF SRM 53-20-00 FIG 2.Mar 20, 2006 · N568FE · Doug DC1010SDR UPS06146467None · noneINTERIOR EMERGENCY LIGHTS IN SUPERNUMERARY AREA FAFCS OPERATIONAL CHECK BY PRESSING THE EMERG TEST PUSH BUTTON ON THE PURSERS PANEL. OPS CKS NORMAL PER PS CHK METHODS CARD STEP 9 MC NO 050000-01-1-999 TEMP REVISION NR 3-33-PSC-06-0023.Mar 18, 2006 · N139UP · Airbus A300F4622RSDR 03212006AUnknown · unknownDURING T/O ROLL, BOTH TORQUE GAUGES LEAPED TO ABOUT 90 PERCENT AS POWER WAS APPLIED. CTOT SELECTED TO APR, ONLY THE L APR LIGHT ILLUMINATED. PERFORMED ENGINE OPS CHECK, AND HIGH POWER RUNS WITH CREW, APR AND CTOT OPS CHECK GOOD AT THIS TIME. NO DEFECTS NOTEMar 17, 2006 · N341CJ · Saab 340BSDR 06FDEA1136Repair · unknownFOUND AN ANGLE AND SPLICE REPAIR ON FWD CARGO DOOR FWD PAN CLOSE TO THE UPPER CORNER. REMOVED AND REPLACED REPAIR IAW SRM 52-10-00 FIG 17 VOL 1. FAB PART IAW DETAIL PART TRAVELER N01205 AND SRM 52-10-00 FIG 17 VOL 1.Mar 17, 2006 · N563FE · Doug DC1010SDR 06FDEA1134None · noneLT HORIZONTAL STAB REAR SPAR STA XE 77.100 HAS DOUBLER REPAIR UPPER SKIN. PERFORMED INSPECTION ON REPAIR FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2.Mar 17, 2006 · N68054 · Doug MD1010FSDR 06FDEA1133Repair · misinstalledEXISTING DOUBLER STA 1871-1877 LONG 51-52 RT. REMOVED EXISTING REPAIR IAW SRM 51-35-01 VOL 2, PERFORMED NEW REPAIR DOUBLER IAW SRM 53-20-00 FIG 6 VOL 1. FAB PART IAW DETAIL PART TRAVELER F167062/N01062 AND SRM 53-20-00 FIG 6 VOL 1.Mar 17, 2006 · N68054 · Doug MD1010FSDR 06FDEA1132None · noneRT WING NR 8 L/E SLAT FLUSH REPAIR ON EXT SKIN. REMOVED EXISTING REPAIR IAW SRM 51-35-01 PAR 6 VOL 2, PERFORMED NEW REPAIR IAW SRM 57-10-00 FIG 11 VOL 1, FAB PART IAW DETAIL PART TRAVELER F167113/N01113 AND SRM 57-10- 00 FIG 11 VOL 1.Mar 17, 2006 · N68054 · Doug MD1010FSDR 06FDEA1130None · noneEXT DOUBLER REPAIR DIM 43" BY 46" FROM STA 1089 TO 1129 LONG 42-48 RT. PERFORMED GVI ON DOUBLER FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P1. PERFORMED EA NR 8-5330-95691 P1.Mar 17, 2006 · N563FE · Doug DC1010SDR 06FDEA1123Repair · unknownRIGHT WING NR 3 SLAT EXISTING REPAIR REQUIRES FILLER TO BE REMOVED FOR NDT OF DOUBLER FOR MATERIAL IDENTIFICATION FOR ASSESSMENT OF REPAIR REF N00300. REMOVED AND REINSTALLED FILLER IAW A300-600 SRM 51-40-21.Mar 16, 2006 · N719FD · Airbus A300B4622SDR 06FDEA1121Repair · noneDURING AIRPLANE'S MODIFICATION FROM P TO F/ACF FOUND: BETWEEN STA 1099-1139, STR 46-48, LT, EXTERNAL REPAIR DOUBLER. NO ACTION REQUIRED, REPAIR IS CONFORM TO SRM 53-20-00 FIG 6 BEFORE MARCH 2000.Mar 16, 2006 · N568FE · Doug DC1010SDR 06FDEA1119Repair · noneDURING AIRPLANE'S MODIFICATION FROM P TO F/ACF FOUND: CTR CARGO DOOR, EXTERNAL SIDE SKIN 2 EA REPAIR. NO ACTION REQUIRED, REPAIR MEETS CRITERIA OF SRM 52-10-00 FIG 17.Mar 16, 2006 · N568FE · Doug DC1010SDR 06FDEA1117Repair · noneDURING AIRPLANE'S MODIFICATION FROM P TO F/ACF MODIFICATION FOUND: STA 959, STR 39-42 RT, EXTERNAL REPAIR DOUBLER. NO ACTION REQUIRED, REPAIR IS CONFORM TO SRM 53-50-00 FIG 9 SH 1.Mar 16, 2006 · N568FE · Doug DC1010SDR 06FDEA1116Repair · noneDURING AIRPLANE'S MODIFICATION FROM P TO F/ACF FOUND: BETWEEN STA 695-715, STR 51-52 RT, FLUSH REPAIR. NO ACTION REQUIRED, REPAIR IS PER DWG SR10530038-7013.Mar 16, 2006 · N568FE · Doug DC1010SDR 06FDEA1101Repair · unknownPREVIOUS REPAIR INSTALLED ON RIGHT HAND AFT PIT CROSSBEAM AT FR 64 TO FR 64, FS 3461 TO FS 3461 AND -Y 117. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPLAMar 15, 2006 · N426FE · Airbus A310203SDR 06FDEA1094Repair · unknownPREVIOUS REPAIR INSTALLED ON RIGHT HAND MCD FLOORBEAM AT FR 12A TO FR 13, FS 1091 TO FS 1125 AND -YC 145.6. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIMar 15, 2006 · N426FE · Airbus A310203
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