# Service difficulty reports: N791FT, cancelled May 17, 2006

A list on [N791FT, cancelled May 17, 2006](https://openairdocs.org/deregistered/N791FT-2006-05-17.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 4 · 159 reports

- [SDR RRXA1136](https://openairdocs.org/sdr/RRXA1136.md): Skin · corroded · Jul 26, 2001 · N791FT · Doug DC873F · Fuselage Main, Plate/Skin
  > DURING 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 IA
- [SDR RRXA11337](https://openairdocs.org/sdr/RRXA11337.md): Door · corroded · Jul 26, 2001 · N791FT · Doug DC873F · Fuselage Main, Plate/Skin
  > DURING 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 CORR
- [SDR RRXA011048](https://openairdocs.org/sdr/RRXA011048.md): Skin · corroded · Jun 19, 2001 · N791FT · Doug DC873F · Fuselage Main, Plate/Skin
  > AFTER LANDING DISCOVERED CORROSION ON OUTER FUSELAGE, LEFT LOWER SIDE AT FS 1320.
- [SDR RRXA001056](https://openairdocs.org/sdr/RRXA001056.md): Landing Gear · noisy · Sep 20, 2000 · N791FT · Doug DC873F · Nose/Tail Landing Gear Strut/Axle
  > AFTER 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 CYCLED
- [SDR RRXA001050](https://openairdocs.org/sdr/RRXA001050.md): Connector · loose · Aug 22, 2000 · N791FT · Doug DC873F · Engine EGT/TIT Indicating System
  > PRECAUTIONARY 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 ACCESSIB
- [SDR RRXA001046](https://openairdocs.org/sdr/RRXA001046.md): Indicator · inoperative · Aug 12, 2000 · N791FT · Doug DC873F · Engine EGT/TIT Indicating System
  > NR 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 I
- [SDR RRXA001045](https://openairdocs.org/sdr/RRXA001045.md): Door · malfunctioned · Aug 11, 2000 · N791FT · Doug DC873F · Landing Gear Door Retract Section
  > AFTER 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-OCC
- [SDR RRXA001019](https://openairdocs.org/sdr/RRXA001019.md): Ballast · defective · Jul 21, 2000 · N791FT · Doug DC873F · Flight Compartment Lighting
  > STRONG 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 MA
- [SDR RRXA000260](https://openairdocs.org/sdr/RRXA000260.md): Skin · corroded · Apr 20, 2000 · N791FT · Doug DC873F · Fuselage Main, Plate/Skin
  > CORROSION 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 & PRIMED
- [SDR RRXA991587](https://openairdocs.org/sdr/RRXA991587.md): Switch · malfunctioned · Nov 25, 1999 · N791FT · Doug DC873F · Landing Gear Position and Warning
  > LM 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.
- [SDR RRXA991525](https://openairdocs.org/sdr/RRXA991525.md): Rectifier · failed · Nov 8, 1999 · N791FT · Doug DC873F · Engine EGT/TIT Indicating System
  > LOST 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.
- [SDR RRXA991685](https://openairdocs.org/sdr/RRXA991685.md): Skin · corroded · Sep 6, 1999 · N791FT · Doug DC873F · Fuselage Main, Plate/Skin
  > DURING 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 APPROVED
- [SDR RRXA991683](https://openairdocs.org/sdr/RRXA991683.md): Skin · corroded · Sep 5, 1999 · N791FT · Doug DC873F · Wing, Plate/Skin
  > DURING 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 DOUBLE
- [SDR RRXA991511](https://openairdocs.org/sdr/RRXA991511.md): Skin · corroded · Sep 5, 1999 · N791FT · Doug DC873F · Fuselage Main, Plate/Skin
  > DURING 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 TENNESSEE
- [SDR RRXA991507](https://openairdocs.org/sdr/RRXA991507.md): Skin · corroded · Sep 5, 1999 · N791FT · Doug DC873F · Wing, Plate/Skin
  > DURING 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, TREA
- [SDR RRXA991488](https://openairdocs.org/sdr/RRXA991488.md): Skin · damaged · Sep 5, 1999 · N791FT · Doug DC873F · Wing, Plate/Skin
  > DURING 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 TEC
- [SDR RRXA991495](https://openairdocs.org/sdr/RRXA991495.md): Skin · cracked · Sep 3, 1999 · N791FT · Doug DC873F · Wing, Plate/Skin
  > DURING 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 TENNES
- [SDR RRXA991502](https://openairdocs.org/sdr/RRXA991502.md): Insert · stripped · Sep 2, 1999 · N791FT · Doug DC873F · Fuselage, Seat/Cargo Attach Fittings
  > DURING 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 APPROV
- [SDR RRXA991501](https://openairdocs.org/sdr/RRXA991501.md): Support · damaged · Aug 31, 1999 · N791FT · Doug DC873F · Trailing Edge Flap Actuator
  > DURING 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 T
- [SDR RRXA991500](https://openairdocs.org/sdr/RRXA991500.md): Support · damaged · Aug 31, 1999 · N791FT · Doug DC873F · Trailing Edge Flap Actuator
  > DURING 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 TEN
- [SDR RRXA991719](https://openairdocs.org/sdr/RRXA991719.md): Floor Panel · corroded · Aug 28, 1999 · N791FT · Doug DC873F · Fuselage Floor Panel
  > DURING 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 ENG
- [SDR RRXA991513](https://openairdocs.org/sdr/RRXA991513.md): Skin · corroded · Aug 28, 1999 · N791FT · Doug DC873F · Fuselage Main, Plate/Skin
  > DURING 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 INSTALLE
- [SDR RRXA991496](https://openairdocs.org/sdr/RRXA991496.md): Duct · damaged · Aug 28, 1999 · N791FT · Doug DC873F · Air Distribution System
  > DURING 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 DEFEC
- [SDR RRXA991749](https://openairdocs.org/sdr/RRXA991749.md): Floor Panel · corroded · Aug 27, 1999 · N791FT · Doug DC873F · Fuselage Floor Panel
  > DURING 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 ENG
- [SDR RRXA991747](https://openairdocs.org/sdr/RRXA991747.md): Floor Panel · corroded · Aug 27, 1999 · N791FT · Doug DC873F · Fuselage Floor Panel
  > DURING 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 APPROV
- [SDR RRXA991720](https://openairdocs.org/sdr/RRXA991720.md): Floor Panel · corroded · Aug 27, 1999 · N791FT · Doug DC873F · Fuselage Floor Panel
  > DURING 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 SKETCH
- [SDR RRXA991504](https://openairdocs.org/sdr/RRXA991504.md): Retract Pin · corroded · Aug 25, 1999 · N791FT · Doug DC873F · Landing Gear Retraction/Extension System
  > DURING 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 REWOR
- [SDR RRXA991491](https://openairdocs.org/sdr/RRXA991491.md): Skin · damaged · Aug 25, 1999 · N791FT · Doug DC873F · Wing, Plate/Skin
  > DURING 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 FA
- [SDR RRXA991696](https://openairdocs.org/sdr/RRXA991696.md): Finger Doubler · corroded · Aug 24, 1999 · N791FT · Doug DC873F · Fuselage Miscellaneous Structure
  > DURING 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 D
- [SDR RRXA991510](https://openairdocs.org/sdr/RRXA991510.md): Floor Panel · corroded · Aug 20, 1999 · N791FT · Doug DC873F · Fuselage Floor Panel
  > DURING 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
- [SDR RRXA991508](https://openairdocs.org/sdr/RRXA991508.md): Floor Panel · corroded · Aug 20, 1999 · N791FT · Doug DC873F · Fuselage Floor Panel
  > DURING 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.
- [SDR RRXA991498](https://openairdocs.org/sdr/RRXA991498.md): Support · damaged · Aug 19, 1999 · N791FT · Doug DC873F · Trailing Edge Flap Actuator
  > DURING 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 TENN
- [SDR RRXA991494](https://openairdocs.org/sdr/RRXA991494.md): Skin · cracked · Aug 18, 1999 · N791FT · Doug DC873F · Fuselage Main, Plate/Skin
  > DURING 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 IAW
- [SDR RRXA991492](https://openairdocs.org/sdr/RRXA991492.md): Door Track · bent · Aug 18, 1999 · N791FT · Doug DC873F · Cargo/Baggage Doors
  > DURING 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-99-10
- [SDR RRXA991493](https://openairdocs.org/sdr/RRXA991493.md): Panel · missing · Aug 17, 1999 · N791FT · Doug DC873F · Nacelle/Pylon, Plate/Skin
  > DURING 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 SERVICES
- [SDR RRXA991499](https://openairdocs.org/sdr/RRXA991499.md): Support · damaged · Aug 12, 1999 · N791FT · Doug DC873F · Trailing Edge Flap Actuator
  > DURING 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 APPROV
- [SDR RRXA991489](https://openairdocs.org/sdr/RRXA991489.md): Duct · cracked · Aug 11, 1999 · N791FT · Doug DC873F · Air Distribution System
  > DURING 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 EN
- [SDR RRXA991725](https://openairdocs.org/sdr/RRXA991725.md): Floor Panel · corroded · Jul 27, 1999 · N791FT · Doug DC873F · Fuselage Floor Panel
  > DURING 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
- [SDR RRXA991723](https://openairdocs.org/sdr/RRXA991723.md): Floor Panel · corroded · Jul 27, 1999 · N791FT · Doug DC873F · Fuselage Floor Panel
  > DURING 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
- [SDR RRXA991698](https://openairdocs.org/sdr/RRXA991698.md): Floor Panel · corroded · Jul 27, 1999 · N791FT · Doug DC873F · Fuselage Floor Panel
  > DURING 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 D
- [SDR RRXA991483](https://openairdocs.org/sdr/RRXA991483.md): Bulkhead · cracked · Jul 22, 1999 · N791FT · Doug DC873F · Fuselage Main, Bulkhead
  > DURING 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 SRM
- [SDR RRXA991481](https://openairdocs.org/sdr/RRXA991481.md): Bulkhead · cracked · Jul 22, 1999 · N791FT · Doug DC873F · Fuselage Main, Bulkhead
  > DURING 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
- [SDR RRXA991490](https://openairdocs.org/sdr/RRXA991490.md): Skin · dented · Jul 21, 1999 · N791FT · Doug DC873F · Engine Air Intake System
  > DURING 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 INST
- [SDR RRXA991713](https://openairdocs.org/sdr/RRXA991713.md): Floor Panel · corroded · Jul 20, 1999 · N791FT · Doug DC873F · Fuselage Floor Panel
  > DURING 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 F
- [SDR RRXA991712](https://openairdocs.org/sdr/RRXA991712.md): Floor Panel · corroded · Jul 20, 1999 · N791FT · Doug DC873F · Fuselage Floor Panel
  > DURING 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 F
- [SDR RRXA991752](https://openairdocs.org/sdr/RRXA991752.md): Skin · corroded · Jul 19, 1999 · N791FT · Doug DC873F · Fuselage Main, Plate/Skin
  > DURING 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 APPR
- [SDR RRXA991684](https://openairdocs.org/sdr/RRXA991684.md): Skin · corroded · Jul 19, 1999 · N791FT · Doug DC873F · Fuselage Main, Plate/Skin
  > DURING 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.
- [SDR RRXA991509](https://openairdocs.org/sdr/RRXA991509.md): Web · corroded · Jul 17, 1999 · N791FT · Doug DC873F · Horizontal Stabilizer Structure
  > DURING 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 SR
- [SDR RRXA991505](https://openairdocs.org/sdr/RRXA991505.md): Skin · corroded · Jul 17, 1999 · N791FT · Doug DC873F · Fuselage Main, Plate/Skin
  > DURING 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 APP
- [SDR RRXA991711](https://openairdocs.org/sdr/RRXA991711.md): Floor Panel · corroded · Jul 16, 1999 · N791FT · Doug DC873F · Fuselage Floor Panel
  > DURING 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

Next page: https://openairdocs.org/deregistered/N791FT-2006-05-17/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/deregistered/N791FT-2006-05-17/reports

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