JASC 5101

Service difficulty reports · 482

Reports filed under 5101 · Aircraft Structures, newest first.

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  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE jasc_code = '5101'
  ORDER BY difficulty_date DESC"

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SDR AWXA200501568Unknown · oscillatesDURING CLIMB, REPORTED AIRFRAME OSCILLATIONS, SIDE TO SIDE ON T/O FROM 1000 TO 5000 FT & CEASED AFTER THROTTLE RETARDED. CREW RETURNED & LANDED WITHOUT EVENT, ACFT OUT OF SERVICE FOR TROUBLESHOOTING. MX R&R NR 1 ENG MEC, NR 1 ENG FUEL PUMP & YAW DAMPER COUPLEDec 20, 2005 · N158AW · Boeing 7373G7SDR 05FDEA04375Repair · undamagedFOUND PREVIOUSLY INSTALLED REINFORCEMENT DOUBLER AT STA 344 BETWEEN STR 4L AND 5L WAS ACCOMPLISHED IAW RIGID BARRIER MODIFICATION DOCUMENT EA 7-5340-7-5002, PAGE 1 AND VENTURA AEROSPACE DWG 2942, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTED OF LOCATION, SDec 19, 2005 · N274FE · Boeing 727233SDR 05FDEA04374Repair · undamagedFOUND PREVIOUSLY INSTALLED REPAIR AT STA 720D, STR 19R WAS ACCOMPLISHED IAW SRM 53-30-3, FIG 6, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTED OF LOCATION, SHAPE, SIZE, FASTENERS SPACING AND NUMBERS, MATERIAL THICKNESS AND TYPE, GENERAL WORKMANSHIP, REPAIRDec 19, 2005 · N274FE · Boeing 727233SDR 05FDEA04373Repair · undamagedFOUND PREVIOUSLY INSTALLED REPAIR AT AFT LOWER CORNER OF FWD GALLEY DOOR CUT OUT WAS ACCOMPLISHED IAW SB 727-53-0188, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTED OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL THICKNESS AND TYPE, GENERALDec 19, 2005 · N274FE · Boeing 727233SDR 05FDEA04372Repair · undamagedFOUND PREVIOUSLY INSTALLED REPAIR AT STA 680, STR 28 WAS ACCOMPLISHED IAW SRM 51-40-3, FIG 1 PAGE 1, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTED OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL THICKNESS AND TYPE, GENERAL WORKMANSHIP, REPDec 19, 2005 · N274FE · Boeing 727233SDR 05FDEA04371Repair · noneFOUND PREVIOUSLY INSTALLED REPAIR AT LT ENTRY DOOR STR 13L WAS ACCOMPLISHED IAW EO 7-5330-7-2345 PT.2, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTED OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL THICKNESS AND TYPE, GENERAL WORKMANSHIP, RDec 19, 2005 · N274FE · Boeing 727233SDR 05FDEA04370None · noneFOUND PREVIOUSLY REPAIR INSTALLED AT STA 660, STR 28R TO 28L WAS ACCOMPLISHED IAW SRM 53-30-3, FIG 2, PAGE 9, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTED OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL THICKNESS AND TYPE, GENERAL WORKMANDec 19, 2005 · N274FE · Boeing 727233SDR 0501766739None · noneABORTED TAKEOFF BECAUSE PILOT FELT SOMETHING WAS WRONG WITH THE RUDDER, BUT IS WAS JUST A STRONG CROSS WIND. NRT MAINTENANCE CHECKED ALL MAIN WHEEL BRAKES AND FOUND OK. RUDDER OPERATION CHECKED OK. NO TROUBLE FOUND, AIRCRAFT RETURNED TO SERVICE.Dec 17, 2005 · N639US · Boeing 747251FSDR 05FDEA04354Repair · unknownFOUND DOUBLER LENGTH 9" WIDTH 8" ON RT EXT FUSELAGE AT STA 879 LONG 36. REMOVED AND REPLACED REPAIR IAW 1-109812697-7 AND SRM 53-20-00 FIG 6 SHT 5- 6 VOL 1 AND FEDEX EA# 8-5310-93218. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F160401-2 INNER EXTERNAL DOUBLDec 16, 2005 · N302FE · Doug DC1030SDR 05FDEA04353Repair · noneFOUND MAIN CARGO COMPT STA 1921 Z 31 BY 92 FOUND 1 NEW SECTION OF FRAME 33" LONG WITH 2 SPLICE. PERFORMED INSPECTION ON FRAME IAW SRM 53-30-00 FIG 5 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2, RESTORED PAINT ON STRIPPED AREA IDec 16, 2005 · N302FE · Doug DC1030SDR 05FDEA04347Repair · noneRT FUSELAGE SKIN REPAIR DOUBLER, 14" BY 7" LOCATED AT BS 1223-1243 REQUIRES EVALUATION TO DETERMINE IF THE REPAIR IS MAJOR OR MINOR AND IF REPAIR IS IN ACCORDANCE WITH FAA APPROVED DATA. REPAIRED SKIN DOUBLER PER SRM 53-30-3 FIG 1.Dec 15, 2005 · N485FE · Boeing 727227SDR 05FDEA04318Repair · unknownREPAIR LOCATED AT STA 303.9 STRINGER 15-L REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. ITEM NR 4, VISUALLY INSPECTED REPAIR AT STA 303.9 STRINGER 15-L. FOUND TO BE IAW SB 727-53A0198 AND EA 7-5Dec 15, 2005 · N486FE · Boeing 727200SDR 05FDEA04298Repair · noneSEAT TRACK MISMATCH RIGHT OUTBOARD CURVED TRACK FS1879. SNRM N2649: PREVIOUS REPAIR AT RIGHT HAND OUTBOARD CURVED SEAT TRACK AT FUSELAGE STATION 1879 MISMATCH EVALUATED AND FOUND REPAIR PREVIOUSLY ACCOMPLISHED IN ACCORDANCE WITH DELTA AIRLINES ENGINEERING REPDec 14, 2005 · N524FE · Doug MD11SDR 05FDEA04308Repair · noneLT WING L/E EXT SKIN FOUND FLUSH DOUBLER DIM 2.75 INCHES BY 2.75 INCHES AT STA XORS 521. PERFORMED A GVI OF REPAIR IAW SRM 57-10-00 FIG 39 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001-2P E3.Dec 14, 2005 · N302FE · Doug DC1030SDR 05FDEA04307Repair · noneRT HORIZONTAL STABILIZER UPPER SURFACE ON SKIN FOUND AN EXTERNAL DOUBLER. REPAIR BETWEEN STA XE 67.333 AND XE 87.167 DIM. 15 INCHES X 11 INCHES. PERFORMED INSPECTION ON DOUBLER REPAIR IAW SB 55-16 FIG 19 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100Dec 14, 2005 · N563FE · Doug DC1010SDR 05FDEA04306Repair · noneFOUND RT SIDE HORIZONTAL STABILIZER IB ELEVATOR UPPER SURFACE ON SKIN HAS AN EXTERNAL DOUBLER REPAIR AT STA XE 216.885 DIM. 8 INCHES BY 8.5 INCHES. PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 55-10-00 FIG 8 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUESDec 14, 2005 · N563FE · Doug DC1010SDR 05FDEA04305Repair · noneLT HORIZONTAL STABILIZER LOWER SURFACE TRAILING EDGE PANEL FOUND AN EXTERNAL DOUBLER REPAIR AT STA XE 169.333 DIM. 8.5 INCHES BY 5.5 INCHES. PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 55-00-01 FIG 3 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO Dec 14, 2005 · N563FE · Doug DC1010SDR 05FDEA04304Repair · noneUPPER LIP AIR CONDITIONING DOOR RT SIDE PACK NR 3 HAS AN EXTERNAL DOUBLER REPAIR DIM 31 INCHES BY 2 INCHES. PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 52-10-00 FIG 2 VOL 1 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2.Dec 14, 2005 · N563FE · Doug DC1010SDR 05FDEA04303Repair · noneCENTER CARGO DOOR LOWER AFT CORNER HAS AN EXTERNAL DOUBLER REPAIR DIM 7 INCHES BY 4 INCHES. PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 52-10-00 FIG 17 VOL 1 . FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2.Dec 14, 2005 · N563FE · Doug DC1010SDR 05FDEA04300Repair · noneDISCREPANCY CENTER CARGO DOOR FWD LWR CORNER HAS AN EXTERNAL REPAIR DOUBLER INSTALLED CORRECTIVE ACTION PERFORMED INSPECTION ON EXTERNAL REPAIR DOUBLER IAW 1255201JP ESO 7349 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.Dec 14, 2005 · N563FE · Doug MD1010FSDR 05FDEA04299Repair · noneDISCREPANCY FOUND SPLICE REPAIR INSTALLED AT FRAME STATION 1159 LT SIDE CORRECTIVE ACTION PERFORMED INSPECTION ON SPLICE REPAIR IAW ESO NR 7346-1275302JP FOUND IAW CRITERIA REQUEST BY EO 8-5100-7-5001 P2.Dec 14, 2005 · N563FE · Doug DC1010SDR 05FDEA04287Repair · unknownPYLON NR 1 HAS AN EXTERNAL DOUBLER REPAIR ON THE UPPER SPAR WEB AFT SECTION BETWEEN STA YN 410 AND YN 417 DIM 7" BY 3.5". PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 54-20-00 FIG 34 VOL 1 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO# 8-5100-7-5001 P2.Dec 13, 2005 · N563FE · Doug DC1010SDR 05FDEA04285Repair · unknownMAIN CABIN CTR FUSELAGE L3 DOOR JAMB AFT HAS AN EXTERNAL DOUBLER REPAIR STA 1311 DIM 11" BY 12" BOTTOM PART. PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 53-50-00 FIG 19 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO# 8-5100-7-5001 P2.Dec 13, 2005 · N563FE · Doug DC1010SDR 05FDEA04279Repair · noneLOWER FUSELAGE BELLY SKIN FOUND AN EXTERNAL DOUBLER REPAIR AT STA 1211 LONG 52 DIM 5 X 4.5 INCHES. PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 53-40-00 FIG 20 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P1.Dec 13, 2005 · N563FE · Doug DC1010SDR 05FDEA04278Repair · noneLOWER FUSELAGE FWD PRESSURE BULKHEAD PANEL HAS A WEB REPAIR ON RIGHT SIDE AT STA 1156 BETWEEN 39 TO 42 DIM 12 X 18 INCHES, 20 X 28 INCHES, 20 X 28 INCHES. PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 53-40-00 FIG 4A VOL 1 FOUND IN COMPLIANCE WITH CRITERIA RDec 13, 2005 · N563FE · Doug DC1010SDR 05FDEA04277Repair · noneLOWER FUSELAGE FWD CARGO COMPT LOWER FRAME AT STA 879 HAS AN ANGLE REPAIR BETWEEN LONG 49 TO LONG 52 DIM 15 X 2 INCHES. PERFORMED INSPECTION ON ANGLE REPAIR IAW SRM 53-30-00 FIG 8 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.Dec 13, 2005 · N563FE · Doug DC1010SDR 05FDEA04276Repair · noneRAM AIR DUCT CUTOUT ON SKIN HAS AN EXTERNAL TRIPLE DOUBLER REPAIR ON THE UPPER AFT CORNER BETWEEN STA 576-590 LONG 44 TO 46 DIM 14 X 12.5 INCHES, 10 X 11.5 INCHES. PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 53-20-00 FIG 2 VOL 1. FOUND IN COMPLIANCE WITH Dec 13, 2005 · N563FE · Doug DC1010SDR 05FDEA04275Repair · noneRAM AIR DUCT CUTOUT HAS AN EXTERNAL TRIPLER DOUBLER ON LOWER FWD CORNER BETWEEN STA 557 TO 572 AND LONG 46 TO 48 LT SIDE DIM 15 X 15 INCHES, 12 X 13 INCHES. PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 53-20-00 FIG 2 VOL 1. FOUND IN COMPLIANCE WITH CRITERIDec 13, 2005 · N563FE · Doug DC1010SDR 05FDEA04274Repair · noneLOWER FUSELAGE FWD CARGO COMPT FOUND A SPLICE REPAIR ON FLOORBEAM AT STA 1099 X-46 DIM 10 X 5 INCHES. PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 53-60-01 FIG 3 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.Dec 13, 2005 · N563FE · Doug DC1010SDR 05FDEA04273Repair · noneLOWER FUSELAGE FWD CARGO COMPT FOUND A SPLICE REPAIR ON FLOORBEAM AT STA 1099 X 46 DIM 10 X 5 INCHES. PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 53-60-01 FIG 3 VOL 1 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.Dec 13, 2005 · N563FE · Doug DC1010SDR 05FDEA04271Repair · unknownFWD LOWER CARGO DOOR FOUND EXTERNAL DOUBLER FROM STA 885 TO STA 959 DIM 11 X 12 INCHES. REMOVED AND REPLACED REPAIR IAW SRM 52-10-00 FIG 6 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER F161770-3, DOUBLER IAW SRM 52-10-00 FIG 6 VOL 1.Dec 13, 2005 · N302FE · Doug DC1030FSDR 05FDEA04270Repair · unknownPERFORMED INSPECTION IAW EO# 8-5100-7-5001-1D FOUND DOUBLER LENGTH 12" WIDTH 9" ON TOP INTERNAL BULKHEAD NLG AT STA 560 Z-38 X11. NO ACTION TAKEN IAW EO NR 8-5100-7-5001 P1 E3 ATTACHMENT "A" NOTE 3 TREATED AND PRIMED AREA IAW SRM 57-21-01 VOL 1.Dec 13, 2005 · N302FE · Doug DC1030FSDR 05FDEA04221Unknown · unknownTO CARRY OUT TRIMMING OF LEFT HAND AFT CHORD TO FACILITATE LEFT HAND NR 35 BORE CLEANING ACCESS. REPAIRED AS PER FEDEX EA 1-5510-94569.Dec 11, 2005 · N524FE · Doug MD11SDR 62512082005Unknown · unknownWHILE TAXING AIRCRAFT RT MAIN GEAR DEPARTED TAXI WAY.Dec 8, 2005 · N507QS · Gulstm GULFSTREAMGVSDR 05FDEA04171Doubler · nonePREVIOUS REPAIR INSTALLED AT FUSELAGE LT EXT DOUBLER ABOVE AND AFT OF CAPT,S SIDE WINDOW, STA. 881 TO 904 FR 7 TO FR 8 NEEDS EVALUATION FOR MAJOR MINOR CLASSIFICATION AND APPROVED REPAIR DATA REF N00696 REPAIR GOOD IAW EA 6-5330-95466.Dec 7, 2005 · N423FE · Airbus A310SDR 05FDEA04169Repair · nonePREVIOUSLY REPAIR INSTALLED ON L/W NR 1 SLAT IB LEADING EDGE, SKIN BLIND FASTENER FLUSH. REPAIR WS RIB 2 TO RIB 3, NEEDS EVALUATION FOR MAJOR MINOR CLASSIFACATION AND APPROVED REPAIR DATA REF N00708. REPAIR EVALUATED AS GOOD IAW EA 6-5750-95471.Dec 7, 2005 · N423FE · Airbus A310SDR 05FDEA04167Fastener · incorrectPREVIOUS REPAIR INSTALLED ON NR 1 PYLON RT SIDE IB AFT LOWER FAIRING EXT DOUBLER STA 1050 RIB 20 NEEDS EVALUATION FOR MAJOR MINOR CLASSIFACATION AND APPROVED REPAIR DATA REF N00705. EVALUATION OF REPAIR REVEALED INCORRECT FASTENERS INSTALLED REPLACED REPADec 7, 2005 · N423FE · Airbus A310SDR 05FDEA04150Doubler · noneDISCREPANCY FOUND EXTERNAL DOUBLER BETWEEN STA 735 AND 755 AND LONGERONS 34 AND 35 LT SIDE, WHERE POTABLE WATER SERVICE PANEL USED TO BE LOCATED. PERFORMED INSPECTION ON REPAIR IAW SRM 53-20-00 FIG 6 VOL 1 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-Dec 6, 2005 · N68056 · Doug DC1010SDR 05FDEA04146Fastener · incorrectPREVIOUS REPAIR INSTALLED ON NR 1 PYLON RT SIDE IB AFT LOWER FAIRING EXT DOUBLER STA 1050 RIB 20 NEEDS EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA, REF N00705. REPAIR REVEALED INCORRECT FASTENER INSTALLED REMOVED AND REPLACED REPAIR IAWDec 5, 2005 · N423FE · Airbus A310SDR 05FDEA04108Repair · misrepairedCOMPLY WITH AGING 9-AGING-INSP, PREVIOUS MAJOR REPAIR INSTALLED ON RUDDER FRONT SPAR PER FEDEX EA 6-5540-89212 IS NOT IN ACCORDANCE REPAIR DATA SRM 51-77-12 REFERENCED IN EA INJECTION HOLES ARE NOT COMPLETELY FILLED LEAVING AVOID. REPAIRED PER SRM 51-77-12 REDec 3, 2005 · N424FE · Airbus A310203SDR 05FDEA04107Repair · misinstalledCOMPLY WITH AGING 9-AGING-INSP, PREVIOUS REPAIR INSTALLED AT LEFT HAND HORIZONTAL STABILIZER (LEADING EDGE ROOT SECTION) AT WS 95 TO WS 105. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATIONDec 3, 2005 · N424FE · Airbus A310203SDR 05FDEA04106Repair · unknownCOMPLY WITH AGING 9-AGING-INSP, PREVIOUS REPAIR INSTALLED AT LEFT HAND WING ROOT (LEADING EDGE ABOVE KRUEGER FLAP) AT WS 57 TO WS 77. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APDec 3, 2005 · N424FE · Airbus A310203SDR 05FDEA04105Repair · unknownCOMPLY WITH AGING 9-AGING-INSP, PREVIOUS REPAIR INSTALLED AT LEFT HAND OUTBOARD FLAP (TOP TRAILING EDGE WEDGE SECTION - COMPOSITE) AT WS 823 TO WS 835. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLADec 3, 2005 · N424FE · Airbus A310203SDR 05FDEA04104Repair · unknownCOMPLY WITH AGING 9-AGING-INSP, PREVIOUS REPAIR INSTALLED AT LEFT HAND INBOARD FLAP (TRAILING EDGE WEDGE SECTION - COMPOSITE) AT WS 40 TO WS 50. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICDec 3, 2005 · N424FE · Airbus A310203SDR 05FDEA04099Repair · nonePREVIOUS REPAIR INSTALLED AT RIGHT HAND INBOARD FLAP (METAL CENTER SECTION), AT WS 192 TO WS 222. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVDec 3, 2005 · N424FE · Airbus A310SDR 05FDEA04097Repair · nonePREVIOUS REPAIR INSTALLED AT FUSELAGE LEFT HAND SIDE, BELOW REGISTRATION NR N424FE AT STA 4181 TO STA 4241, FR77 TO FR78, STR 23 LT TO STR 24 LT. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICADec 3, 2005 · N424FE · Airbus A310SDR 05FDEA04098Repair · unknownPREVIOUS REPAIR INSTALLED AT FUSELAGE RT SIDE OF TAIL CONE AT STA 5094 TO STA 5122, FR101 TO FR102, STR 07RH TO STR 08RH. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIRDec 3, 2005 · N424FE · Airbus A310SDR 05FDEA04096Repair · unknownPREVIOUS REPAIR INSTALLED AT FUSELAGE LT SIDE, L2 REAR DOOR FRAME AT STA 4669, FR75A, STR 20LH TO STR 24LH. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA.Dec 3, 2005 · N424FE · Airbus A310SDR 05FDEA04095Repair · unknownAGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NO. POS PT1. PREVIOUS REPAIR INSTALLED AT FUSELAGE LEFT HAND SIDE, L2 FORWARD DOOR FRAME AT STA 4551, FS 73A, STR 20 LT TO STR 24 LT. UNABLE TO DETERMINE APPROVED RDec 3, 2005 · N424FE · Airbus A310203SDR 05FDEA04094Repair · noneSMIS 424 51-00 0007102 27SEP05 MC1 CLOSE R MOD TYPE Y MOD NO. 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1 ENT BY: 067708 INFO 30NOV05 21:26 MC1 R DISCREPANCY Dec 3, 2005 · N424FE · Airbus A310
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