N791FT, cancelled May 17, 2006

Service difficulty reports · 159

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 n_number = 'N791FT' AND deregistration_id = 'N791FT-2006-05-17'
  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 RRXA1136Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LOWER BELLY SKIN AT STA. 600-680 AND L33R-L34L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED SKIN REPAIR AND INSTALLED IAJul 26, 2001 · N791FT · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA11337Door · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO R/H KEEL PRESSURE PANEL AT STA. 705, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORRJul 26, 2001 · N791FT · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA011048Skin · corrodedAFTER LANDING DISCOVERED CORROSION ON OUTER FUSELAGE, LEFT LOWER SIDE AT FS 1320.Jun 19, 2001 · N791FT · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA001056Landing Gear · noisyAFTER T/O UPON GEAR RETRACTION THERE WAS A LOUD NOISE FROM NOSE GEAR THAT SOUNDED LIKE NOSE WHELL SCRUBBER WASN'T STOPPING ONE OF THE TIRES HOWEVER AS A/S INCREASED NOISE GOT MUCH LOUDER AND A STRONG VIBRATION COULD BE FELT BENEATH THE PILOTS EGT CYCLEDSep 20, 2000 · N791FT · Doug DC873F · Nose/Tail Landing Gear Strut/AxleSDR RRXA001050Connector · loosePRECAUTIONARY SHUTDOWN OF NR 3 ENG DUE TO NO EGT, ANALOG OR DIGITAL AT 1123Z. NO OIL PRESSURE IND WITH WINDMILLING ENGINE. INSPECTED NR 3 EGT INDICATION SYS, FOUND FIREWALL CONNECTOR NOT FULLY SEATED, TIGHTENED CONNECTOR, AND PERFORMED SHAKE TEST ON ACCESSIBAug 22, 2000 · N791FT · Doug DC873F · Engine EGT/TIT Indicating SystemSDR RRXA001046Indicator · inoperativeNR 4 EGT INOP, NR 4 EGT 870 DEG ON CLIMBOUT 3000 FT. N1 89 PERCENT, ALL OTHER PARAMETERS NORMAL. REMOVED AND REPLACED EGT INDICATOR, LEFT AND RIGHT HARNESS IAW M/M 72-20-4. PERFORMED PWR ASSURANCE RUN IAW EWWA RUN UP HANDBOOK PG 48, PER DYNAMIC RIG ON VSV IAug 12, 2000 · N791FT · Doug DC873F · Engine EGT/TIT Indicating SystemSDR RRXA001045Door · malfunctionedAFTER T/O FROM MTY AND AFTER GEAR RETRACTION, LOUD VIBRATION AND NOISE WAS PRESENT FROM NOSE WHEEL AND FWD RIGHT SIDE OF FUSELAGE. ON APP GEAR LOWERED AND NOISE STILL PRESENT, LOUD NOISE WAS HEARD AND VIBRATION WENT AWAY. GEAR CYCLED AND NOISE DID NOT RE-OCCAug 11, 2000 · N791FT · Doug DC873F · Landing Gear Door Retract SectionSDR RRXA001019Ballast · defectiveSTRONG ELECTRICAL SMELL COMING FROM GLARESHIELD AREA. FOUND GLARESHEILD OVERHEAD LIGHTS BALLAST DEFECTIVE. ORDERED PARTS. LIGHTS DEFFERED PER MEL 33-1, CAT C, DMI C9960051-7702, DUE DATE 07-31-00, PLACARD INSTALLED. REMOVED AND REPLACED LIGHTING BALLAST MAJul 21, 2000 · N791FT · Doug DC873F · Flight Compartment LightingSDR RRXA000260Skin · corrodedCORROSION STA 1260 L36 SKIN PANEL A. IN WORK (OPEN).CLOSING ACTION. REMOVED PAINT IAW DC8 SRM 51-1-8. CUTOUT CORROSION AT L36,L35R & L35L AT STA. 12600 AND FABRICATED FILLERS AND DOUBLER. 1.25 AND INSTALLED IAW DC-8 SRM 53-21. TREATED & PRIMEDApr 20, 2000 · N791FT · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA991587Switch · malfunctionedLM GEAR DOWN (GREEN) LIGHT WILL NOT ILLUMINATE GEAR WARNING (RED) LIGHTS NORMAL RECYCLED GEAR. NO HELP LIGHT CAME ON DURING FINAL APPROACH. REMOVED AND REPLACED LT MAIN LANDING GEAR SWITCH OP'S CHECK NORMAL ON GROUND AS PER MM 32-60-00.Nov 25, 1999 · N791FT · Doug DC873F · Landing Gear Position and WarningSDR RRXA991525Rectifier · failedLOST POWER TO EGT INDICATORS ANS SAI WHILE IN FLIGHT AT FL330. FOUND DC BUS BLOCKER RECTIFIER R7-5 WDM 24-4-1 P44 BAD. REMOVED AND REPLACED SAME, OPS CKS NORMAL AT THIS TIME.Nov 8, 1999 · N791FT · Doug DC873F · Engine EGT/TIT Indicating SystemSDR RRXA991685Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FORWARD PRESSURE PANEL BETWEEN Y=-52 TO Y=-12 AND Z=-8. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVEDSep 6, 1999 · N791FT · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA991683Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LEFT WING, LEADING EDGE, UPPER SURFACE SKIN BETWEEN XFS=20 TO XFS=38.750. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLESep 5, 1999 · N791FT · Doug DC873F · Wing, Plate/SkinSDR RRXA991511Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FINGER DOUBLER AT LONGERON 31 LEFT BETWEEN STA 440 AND STA 460 LT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED TENNESSEESep 5, 1999 · N791FT · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA991507Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, WING, SCREWS PULLING THROUGH SKIN LEFT WING INBOARD LEADING EDGE UPPER BETWEEN STA XFS 20 AND STA XFS 38.750 AT FRONT SPAR. CORROSION FOUND IN SCREW HOLES. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREASep 5, 1999 · N791FT · Doug DC873F · Wing, Plate/SkinSDR RRXA991488Skin · damagedDURING A MAINTENANCE VISIT, FOUND FASTENERS LOOSE RIGHT WING O/B SLOT L/E O/B END AT STA XS 491.193. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW DOUBLER IAW FAA APPROVED TENNESSEE TECSep 5, 1999 · N791FT · Doug DC873F · Wing, Plate/SkinSDR RRXA991495Skin · crackedDURING A MAINTENANCE VISIT FOUND 4 CRACK EXTENDING FROM RIVET RT WING UPPER SURFACE AT STA 69.5 AT REAR SPAR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED REPAIR IAW DC8 SRM 57-2-1 AND FAA APPROVED TENNESSep 3, 1999 · N791FT · Doug DC873F · Wing, Plate/SkinSDR RRXA991502Insert · strippedDURING A MAINTENANCE VISIT, FOUND NUMEROUS TRAY TIE DOWN INSERTS STRIPPED. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED DYNA SYSTEM THREAD INSERTS P/N: 021-1-8200 IN PLACE OF P/N: 3755486-1 IAW FAA APPROVSep 2, 1999 · N791FT · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA991501Support · damagedDURING A MAINTENANCE VISIT, REMOVED AND REPLACED FLAP LINK SUPPORT ASSY RT O/B STA 340. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED AND REPLACED FLAP LINK SUPPORT IAW DC8 M/M 57-51-12 AND IAW FAA APPROVED TAug 31, 1999 · N791FT · Doug DC873F · Trailing Edge Flap ActuatorSDR RRXA991500Support · damagedDURING A MAINTENANCE VISIT REMOVE AND REPLACE FLAP LINK SUPPORT ASSY RT MID STA 219. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED AND REPLACED FLAP LINK SUPPORT IAW DC8 M/M 27-51-12 AND IAW FAA APPROVED TENAug 31, 1999 · N791FT · Doug DC873F · Trailing Edge Flap ActuatorSDR RRXA991719Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL E-2 BETWEEN Y=1500 TO Y=1540. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER ENGAug 28, 1999 · N791FT · Doug DC873F · Fuselage Floor PanelSDR RRXA991513Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, AT FINGER DOUBLERS ABOVE M/W/W BETWEEN STA 940 AND STA 980, 8 CENTER OF FLOOR PRESS PANEL. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLEAug 28, 1999 · N791FT · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA991496Duct · damagedDURING A MAINTENANCE VISIT FOUND DUCT THAT GOES UNDER CONSTANT SECTION HAS HOLE (EO). DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SPLIT SLEEVE AND WELDED OVER CUT OUT. NDT WELD. NO DEFECAug 28, 1999 · N791FT · Doug DC873F · Air Distribution SystemSDR RRXA991749Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL E-2 BETWEEN Y=1580 TO Y=1680. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER ENGAug 27, 1999 · N791FT · Doug DC873F · Fuselage Floor PanelSDR RRXA991747Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL C-2 BETWEEN Y=1500 TO Y=1540 AND X=-10. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVAug 27, 1999 · N791FT · Doug DC873F · Fuselage Floor PanelSDR RRXA991720Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL D-2 AT Y=1560. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER ENGINEERING SKETCHAug 27, 1999 · N791FT · Doug DC873F · Fuselage Floor PanelSDR RRXA991504Retract Pin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, MAIN LANDING GEAR STRUT, LT AND RT MLG RETRACT PIN ASSY (EO). DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. COMPLIED WITH MA-A1-3210 AND S/B 32-102 REPLACED PINS AND REWORAug 25, 1999 · N791FT · Doug DC873F · Landing Gear Retraction/Extension SystemSDR RRXA991491Skin · damagedDURING A MAINTENANCE VISIT, FOUND NR 4 STUB WING MOUNTING HOLE BROKEN OUT AT DOUBLER AT STA XS 515.720, 26 FWD OF FRONT SPAR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW DOUBLER IAW FAAug 25, 1999 · N791FT · Doug DC873F · Wing, Plate/SkinSDR RRXA991696Finger Doubler · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FINGER DOUBLER BETWEEN Y=940 TO Y=960 AND BETWEEN X=0 TO X=-6 AND Z=-8. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR FINGER DAug 24, 1999 · N791FT · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA991510Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, UPPER CARGO COMPARTMENT FLOOR PANEL CORRODED (EXFOLIATION) REQUIRES REPAIR DOUBLERS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED FLOOR PANELS IAW DC8 Aug 20, 1999 · N791FT · Doug DC873F · Fuselage Floor PanelSDR RRXA991508Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, UPPER CARGO COMPARTMENT FLOOR PANEL CORRODED (EXFOLIATION) REQUIRES SKIN REPLACEMENT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FILLED GAP WITH HYSOLEA934NA.Aug 20, 1999 · N791FT · Doug DC873F · Fuselage Floor PanelSDR RRXA991498Support · damagedDURING A MAINTENANCE VISIT, REMOVED AND REPLACED FLAP LINK SUPPORT ASSY LT MID STA 219. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED AND REPLACED FLAP LINK SUPPORT IAW DC8 M/M 27-51-12 AND FAA APPROVED TENNAug 19, 1999 · N791FT · Doug DC873F · Trailing Edge Flap ActuatorSDR RRXA991494Skin · crackedDURING A MAINTENANCE VISIT FOUND RT W/W FWD PRESS WEB CRACKED IN RECESS OF REMOVEABLE PANEL O/B OF PANEL AT STA 849 XCW 64. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW PRESSURE WEB IAWAug 18, 1999 · N791FT · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA991492Door Track · bentDURING A MAINTENANCE VISIT FOUND A PIT RT TRACK WORN AND BENT AT STA 360. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED TRACK IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-10Aug 18, 1999 · N791FT · Doug DC873F · Cargo/Baggage DoorsSDR RRXA991493Panel · missingDURING A MAINTENANCE VISIT FOUND ROBBED PYLON PANEL ASSY FOR A/C N8085U NR 3 PYLON (EO). DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW PANEL IAW FAA APPROVED TENNESSEE TECHNICAL SERVICESAug 17, 1999 · N791FT · Doug DC873F · Nacelle/Pylon, Plate/SkinSDR RRXA991499Support · damagedDURING A MAINTENANCE VISIT, REMOVED AND REPLACED FLAP LINK SUPPORT ASSY LT O/B AT STA 340. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED AND REPLACED FLAP LINK SUPPORT IAW DC8 M/M 27-51-12 AND IAW FAA APPROVAug 12, 1999 · N791FT · Doug DC873F · Trailing Edge Flap ActuatorSDR RRXA991489Duct · crackedDURING A MAINTENANCE VISIT FOUND UPPER CARGO COMPT AIR DUCT AT STA 70, LT SIDE DUCT CRACKED. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED AND WELDED IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENAug 11, 1999 · N791FT · Doug DC873F · Air Distribution SystemSDR RRXA991725Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL B-3 BETWEEN Y=280 TO Y=580 AND X=40. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED Jul 27, 1999 · N791FT · Doug DC873F · Fuselage Floor PanelSDR RRXA991723Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL C-1 BETWEEN Y=280 TO Y=580 AND X=30. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED Jul 27, 1999 · N791FT · Doug DC873F · Fuselage Floor PanelSDR RRXA991698Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL E BETWEEN Y=280 TO Y=580 AND X=45. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DJul 27, 1999 · N791FT · Doug DC873F · Fuselage Floor PanelSDR RRXA991483Bulkhead · crackedDURING A MAINTENANCE VISIT FOUND CRACK, AFT PRESSURE BULKHEAD AT STA 1766 BETWEEN LONGERONS 10 LEFT AND LONGERON 11 LEFT, APPROX 2-1/2, BETWEEN BL 25.0 RIGHT AND BL 27.250 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRMJul 22, 1999 · N791FT · Doug DC873F · Fuselage Main, BulkheadSDR RRXA991481Bulkhead · crackedDURING A MAINTENANCE VISIT FOUND CRACK, AFT PRESSURE BULKHEAD AT STA 1766, I/B AREA BETWEEN LONGERONS 10 RIGHT AND LONGERON 11 RIGHT, A 2.75 CRACK BETWEEN BL 24.750T LEFT AND BL 27.250 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA Jul 22, 1999 · N791FT · Doug DC873F · Fuselage Main, BulkheadSDR RRXA991490Skin · dentedDURING A MAINTENANCE VISIT FOUND DENT, NR 1 ENGINE RING COWL AT 5 O'CLOCK POSITION. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. CUT ACCESS HOLE, STRAIGHTENED DENT WITHIN LIMITS DC8 SRM 71-5-2. FABRICATED AND INSTJul 21, 1999 · N791FT · Doug DC873F · Engine Air Intake SystemSDR RRXA991713Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL BETWEEN Y=968 TO Y=973 AND BETWEEN X=45 TO X=59. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FJul 20, 1999 · N791FT · Doug DC873F · Fuselage Floor PanelSDR RRXA991712Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL BETWEEN Y=949 TO Y=952 AND BETWEEN X=45 TO X=59. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FJul 20, 1999 · N791FT · Doug DC873F · Fuselage Floor PanelSDR RRXA991752Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO EXTERIOR SKIN PANEL BETWEEN Y=857 TO Y=980 AND LONGERON 36. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPRJul 19, 1999 · N791FT · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA991684Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO EXTERNAL SKIN BETWEEN Y=857 TO Y=980 AND LONGERON 36. REMOVED DAMAGE SKIN, TREATED AREA IAW DC-8 SRM. FABRICATED AND INSTALLED NEW SKIN PANEL IAW DC-8 SRM 53-3-0.Jul 19, 1999 · N791FT · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA991509Web · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION BLISTER AT STA 1766, LONGERON 10 RIGHT, 24 LEFT OF RBL ON STAB FRONT SPAR ANGLED WEB DIRECTLY BEHIND AFT BULKHEAD INSIDE ACCESS HOLE 60. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRJul 17, 1999 · N791FT · Doug DC873F · Horizontal Stabilizer StructureSDR RRXA991505Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, AT STA 718, LONGERON 35 RIGHT ON EXTERNAL SKIN UNDER FWD FILLET PANEL. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW FAA APPJul 17, 1999 · N791FT · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA991711Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL A-3 BETWEEN Y=940 TO Y=980 AND X=50. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED Jul 16, 1999 · N791FT · Doug DC873F · Fuselage Floor Panel
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