# Service difficulty reports: N993CF, cancelled Aug 31, 2009 A list on [N993CF, cancelled Aug 31, 2009](https://openairdocs.org/deregistered/N993CF-2009-08-31.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 2 · 69 reports - [SDR RRXA001040](https://openairdocs.org/sdr/RRXA001040.md): Control Panel · failed · Aug 2, 2000 · N993CF · Doug DC862 · ATC Transponder System > NR 1 TRANSPONDER SQUAKS 7777 NO MATTER WHAT THE INPUT (THE VARIOUS CODES) ON THE BOX IS, NR 2 TRANSPONDER INOP (NO SQUAK) FOR VARIOUS CODES. REMOVED AND REPLACED ATC CONTROL PANEL, NR 1 AND NR 2 TRANSPONDER, OP CHECKS GOOD IAW DC-8 M/M CH 34-53. - [SDR RRXA991586](https://openairdocs.org/sdr/RRXA991586.md): Valve · inoperative · Nov 24, 1999 · N993CF · Doug DC862 · Cabin Pressure Control System > DURING FLIGHT AT FL 26.0 MADE AN EMERGENCY DESCENT DUE TO LOSS OF CABIN PRESSURIZATION. REPLACED LEFT AND RIGHT PRESSURIZATION VALVES. PERFORMED PRESSURIZATION CHECK PER MM 21-31-00 WITH ENGINES 2 AND 3 RUNNING. PRESSURIZED TO 8.0 PSID, NO LEAK OR DEFECTS N - [SDR RRXA991585](https://openairdocs.org/sdr/RRXA991585.md): Controller · malfunctioned · Nov 19, 1999 · N993CF · Doug DC862 · Cabin Pressure Control System > AT FL 260, AIRCRAFT EXPERIENCED A RAPID CLIMB IN CABIN PRESSURE CREW DESCENDED TO FL 120 AND LANDED IN (MKE). PRESSURIZED A/C TO 1.5 DPSI NO MAJOR LEAKS NOTED. INSPECTED ALL DOOR SEALS, AIRCRAFT EXTERIOR AND OUT FLOW VALVE. NO DEFECTS NOTE. A/C IS SAFE FOR - [SDR RRXA991377](https://openairdocs.org/sdr/RRXA991377.md): Valve · malfunctioned · Aug 31, 1999 · N993CF · Doug DC862 · Rudder Control System > AFTER TAKEOFF, DURING RIGHT TURN AIRCRAFT HAD STUDDERING, TURNING OUT OF TURN SAME BUFFETING EFFECT IN AIRFRAME. DID NOT FEEL IN YOKE, NO VISIBLE ENGINE INDICATIONS OF MALFUNCTION. NO LEFT TURNS MADE). FOUND RUDDER PRESSURE REDUCER VALVE BYPASSING. REMOVED - [SDR RRXA991541](https://openairdocs.org/sdr/RRXA991541.md): Strap · corroded · Jul 23, 1999 · N993CF · Doug DC862 · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO CIRCUMFERENCIAL STRAP AT STA 1180, LONGERON 34 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW CIRCUMFERENCIAL STRAP IAW DC8 - [SDR RRXA991528](https://openairdocs.org/sdr/RRXA991528.md): Skin · corroded · Jul 22, 1999 · N993CF · Doug DC862 · Wing, Plate/Skin > DURING A MAINTENANCE VISIT FOUND CORROSION, RIGHT WING SKIN AT STA XCW=69.5 AND STRINGER 9 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8.. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DAC DWG EAF-MIA-99-0032RR. - [SDR RRXA991563](https://openairdocs.org/sdr/RRXA991563.md): Skin · corroded · Jul 9, 1999 · N993CF · Doug DC862 · Fuselage Main, Plate/Skin > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO DOOR JAMB PAN SKIN BETWEEN STA 1240 AND STA 1280, AND BETWEEN LONGERONS 31 RIGHT AND LONGERON 33 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICAT - [SDR RRXA991561](https://openairdocs.org/sdr/RRXA991561.md): Fitting · corroded · Jul 8, 1999 · N993CF · Doug DC862 · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, AT DOOR JAMB TORQUE BOX FITTING AT STA 490, BETWEEN LONGERONS 32 RIGHT AND LONGERON 33 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW FITTING - [SDR RRXA991562](https://openairdocs.org/sdr/RRXA991562.md): Fitting · corroded · Jul 7, 1999 · N993CF · Doug DC862 · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO DOOR JAMB TORQUE BOW FITTING AT STA 500, BETWEEN LONGERONS 32 RIGHT AND LONGERON 33 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTAL - [SDR RRXA991546](https://openairdocs.org/sdr/RRXA991546.md): Longeron · corroded · Jul 2, 1999 · N993CF · Doug DC862 · Fuselage Main, Longeron/Stringer > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO LONGERON 36 AT STA 1260. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW DAC DRAWING 3648359. (CORROSION DAMAG - [SDR RRXA991545](https://openairdocs.org/sdr/RRXA991545.md): Intercostal · corroded · Jul 2, 1999 · N993CF · Doug DC862 · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO INTERCOSTAL BETWEEN STA 1240 AND STA 1280, AT WL 4 RIGHT, AND LONGERON 33 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW INT - [SDR RRXA991530](https://openairdocs.org/sdr/RRXA991530.md): Skin · corroded · Jun 19, 1999 · N993CF · Doug DC862 · Fuselage Main, Plate/Skin > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO INNER SKIN BETWEEN STA 480 AND STA 580, AND BETWEEN LONGERONS 34 LEFT AND LONGERON 35 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLE - [SDR RRXA991542](https://openairdocs.org/sdr/RRXA991542.md): Frame · corroded · Jun 12, 1999 · N993CF · Doug DC862 · Fuselage Main, Frame > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO FRAME AT STA 1200, BETWEEN LONGERONS 35 LEFT AND LONGERON 35 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR SPLICE IAW D - [SDR RRXA991559](https://openairdocs.org/sdr/RRXA991559.md): Longeron · corroded · Jun 7, 1999 · N993CF · Doug DC862 · Fuselage Main, Longeron/Stringer > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO LONGERON 34 RIGHT, AT STA 1260. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW DAC DRAWING 5754184. (CORROSI - [SDR RRXA991558](https://openairdocs.org/sdr/RRXA991558.md): Frame · corroded · Jun 7, 1999 · N993CF · Doug DC862 · Fuselage Main, Frame > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO FRAME AT STA 1250 AND LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FRAME IAW DC8 SRM 53-4-1, FIGURE 52. (CORROSION - [SDR RRXA991557](https://openairdocs.org/sdr/RRXA991557.md): Longeron · corroded · Jun 7, 1999 · N993CF · Doug DC862 · Fuselage Main, Longeron/Stringer > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO LONGERON 34 LEFT, BETWEEN STA 1240 AND STA 1260. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW DAC DRAWING 3 - [SDR RRXA991555](https://openairdocs.org/sdr/RRXA991555.md): Shear Tie · corroded · Jun 7, 1999 · N993CF · Doug DC862 · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO SHEAR TIE AT STA 1240 AND LONGERON 35 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SHEAR TIE IAW DC8 SRM 53-2-0, FIGURE 2 - [SDR RRXA991554](https://openairdocs.org/sdr/RRXA991554.md): Shear Tie · corroded · Jun 7, 1999 · N993CF · Doug DC862 · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO SHEAR TIE AT STA 1220, BETWEEN LONGERONS 35 RIGHT AND LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SHEAR TIE IAW DC - [SDR RRXA991553](https://openairdocs.org/sdr/RRXA991553.md): Fitting · corroded · Jun 7, 1999 · N993CF · Doug DC862 · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO FITTING AT STA 560, BETWEEN LONGERONS 33 LEFT AND 34 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW FITTING AND INSTALLED IAW DC8 SRM 51-1-2 - [SDR RRXA991552](https://openairdocs.org/sdr/RRXA991552.md): Shear Tie · corroded · Jun 7, 1999 · N993CF · Doug DC862 · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO SHEAR TIE AT STA 1220, BETWEEN LONGERONS 35 LEFT AND LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SHEAR TIE IAW DC8 - [SDR RRXA991551](https://openairdocs.org/sdr/RRXA991551.md): Shear Tie · corroded · Jun 7, 1999 · N993CF · Doug DC862 · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO SHEAR TIE AT STA 1200, BETWEEN LONGERONS 35 RIGHT AND LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SHEAR TIE IAW DC - [SDR RRXA991550](https://openairdocs.org/sdr/RRXA991550.md): Shear Tie · corroded · Jun 7, 1999 · N993CF · Doug DC862 · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO SHEAR TIE AT STA 1200, BETWEEN LONGERONS 35 LEFT AND LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SHEAR TIE IAW DC8 - [SDR RRXA991547](https://openairdocs.org/sdr/RRXA991547.md): Longeron · corroded · Jun 7, 1999 · N993CF · Doug DC862 · Fuselage Main, Longeron/Stringer > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO LONGERON 35 RIGHT AT STA 1280. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW DAC DRAWING 3646937. (CORROSION - [SDR RRXA991544](https://openairdocs.org/sdr/RRXA991544.md): Shear Tie · corroded · Jun 7, 1999 · N993CF · Doug DC862 · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO SHEAR TIE AT STA 1235, BETWEEN LONGERONS 33 RIGHT AND LONGERON 34 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED ENW SHEAR TIE - [SDR RRXA991543](https://openairdocs.org/sdr/RRXA991543.md): Shear Tie · corroded · Jun 7, 1999 · N993CF · Doug DC862 · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO SHEAR TIE BETWEEN STA 1220 AND STA 1240, AND BETWEEN LONGERONS 35 RIGHT AND LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLE - [SDR RRXA991538](https://openairdocs.org/sdr/RRXA991538.md): Angle · corroded · Jun 7, 1999 · N993CF · Doug DC862 · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO FRAME ATTACHMENT ANGLE AT STA 580, BETWEEN LONGERONS 33 LEFT AND LONGERON 34 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW - [SDR RRXA991537](https://openairdocs.org/sdr/RRXA991537.md): Fitting · corroded · Jun 7, 1999 · N993CF · Doug DC862 · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO FITTING AT STA 560, BETWEEN LONGERONS 35 RIGHT AND LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC8 SRM - [SDR RRXA991534](https://openairdocs.org/sdr/RRXA991534.md): Longeron · corroded · Jun 7, 1999 · N993CF · Doug DC862 · Fuselage Main, Longeron/Stringer > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, LONGERON 34 RIGHT AT STA 580. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW DC8 SRM 53-1-20 FIGURE 1. (CORROSI - [SDR RRXA991532](https://openairdocs.org/sdr/RRXA991532.md): Fitting · corroded · Jun 7, 1999 · N993CF · Doug DC862 · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO FITTING AT STA 540, BETWEEN LONGERONS 35 RIGHT AND LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC8 SRM - [SDR RRXA991531](https://openairdocs.org/sdr/RRXA991531.md): Fitting · corroded · Jun 7, 1999 · N993CF · Doug DC862 · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO FITTING AT STA 500, LONGERON 32 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DAC DWG 3755827. (CORROSION DAM - [SDR RRXA991529](https://openairdocs.org/sdr/RRXA991529.md): Longeron · corroded · Jun 7, 1999 · N993CF · Doug DC862 · Fuselage Main, Longeron/Stringer > DURING A MAINTENANCE VISIT FOUND CORROSION TO LONGERON 32 RIGHT, BETWEEN STA 460 TO STA 600. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED LONGERON 32 RIGHT BY CLAD PLATING AND INSTALLED IAW DC8 SRM 51-1-21 - [SDR RRXA991536](https://openairdocs.org/sdr/RRXA991536.md): Angle · corroded · Jun 6, 1999 · N993CF · Doug DC862 · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO ATTACHMENT ANGLE AT STA 500, LONGERON 33 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ATTACHMENT ANGLE IAW DC8 SRM 5-1-20 - [SDR RRXA991564](https://openairdocs.org/sdr/RRXA991564.md): Fitting · corroded · Jun 1, 1999 · N993CF · Doug DC862 · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO FITTING AT STA 260 AND BL 21 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED NEW FITTING IAW DC8 SRM 53-1-0. (CORROSION DAMAGE RECORDED IN EWA - [SDR RRXA991560](https://openairdocs.org/sdr/RRXA991560.md): Frame · corroded · May 31, 1999 · N993CF · Doug DC862 · Fuselage Main, Frame > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO NUMBER 2 LOWER CARGO DOOR JAMB FRAME WEB AT STA 461, BETWEEN LONGERONS 33 RIGHT AND 34 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INS - [SDR RRXA991535](https://openairdocs.org/sdr/RRXA991535.md): Longeron · corroded · May 31, 1999 · N993CF · Doug DC862 · Fuselage Main, Longeron/Stringer > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO LONGERON 30 RIGHT, SPLICE DOUBLER BETWEEN STA 600 AND STA 620. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SPLICE DOUBLER IAW D - [SDR RRXA991549](https://openairdocs.org/sdr/RRXA991549.md): Frame · corroded · May 30, 1999 · N993CF · Doug DC862 · Fuselage Main, Frame > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO FRAME STRAP AT STA 1180, BETWEEN LONGERONS 33 RIGHT AND LONGERON 34 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR ANGLE - [SDR RRXA991548](https://openairdocs.org/sdr/RRXA991548.md): Frame · corroded · May 27, 1999 · N993CF · Doug DC862 · Fuselage Main, Frame > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FRAME AT STA 1420, BETWEEN LONGERONS 34 LEFT AND LONGERON 34 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 - [SDR RRXA991539](https://openairdocs.org/sdr/RRXA991539.md): Finger Doubler · corroded · May 27, 1999 · N993CF · Doug DC862 · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO FINGER DOUBLER AT STA 310 AND LONGERON 21 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FINGER DOUBLER IAW DC8 SRM 53-1-0. - [SDR RRXA991556](https://openairdocs.org/sdr/RRXA991556.md): Frame · corroded · May 26, 1999 · N993CF · Doug DC862 · Fuselage Main, Frame > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO FRAME AT STA 1240, BETWEEN LONGERONS 34 RIGHT AND LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 - [SDR RRXA991540](https://openairdocs.org/sdr/RRXA991540.md): Bracket · corroded · May 26, 1999 · N993CF · Doug DC862 · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO BRACKET AT STA 1165, BETWEEN LONGERONS 29 RIGHT AND LONGERON 30 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW BRACKET IAW - [SDR RRXA991527](https://openairdocs.org/sdr/RRXA991527.md): Skin · corroded · May 26, 1999 · N993CF · Doug DC862 · Wing, Plate/Skin > DURING A MAINTENANCE VISIT FOUND CORROSION, RIGHT WING UPPER SKIN BETWEEN FRONT SPAR AND CENTER SPAR, BETWEEN STA XW=22.750 AND STA XW=107. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPA - [SDR RRXA991526](https://openairdocs.org/sdr/RRXA991526.md): Skin · corroded · May 26, 1999 · N993CF · Doug DC862 · Wing, Plate/Skin > DURING A MAINTENANCE VISIT FOUND CORROSION, RIGHT WING, UPPER SKIN SURFACE AT STA XRS=421 AND STRINGER 9. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DAC FAX NR EAF-MIA- - [SDR RRXA991584](https://openairdocs.org/sdr/RRXA991584.md): Longeron · corroded · May 25, 1999 · N993CF · Doug DC862 · Fuselage Main, Longeron/Stringer > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO LONGERON 24 RIGHT AT STA 920, BL 24 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8.. FABRICATED AND INSTALLED REPAIR ANGLE IAW DC8 SRM 53-2-2. (CORROSIO - [SDR RRXA991583](https://openairdocs.org/sdr/RRXA991583.md): Longeron · corroded · May 25, 1999 · N993CF · Doug DC862 · Fuselage Main, Longeron/Stringer > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO LONGERON 24 RIGHT AT STA 920, BL 64 RIGHT, AND WL 3 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR ANGLE IAW DC8 SRM 53 - [SDR RRXA991582](https://openairdocs.org/sdr/RRXA991582.md): Seat Track · corroded · May 25, 1999 · N993CF · Doug DC862 · Fuselage, Seat/Cargo Attach Fittings > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO MAIN DECK SEAT TRACK BETWEEN STA 560 AND STA 660 AT BL 45 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SEAT TRACK IAW DC8 - [SDR RRXA991581](https://openairdocs.org/sdr/RRXA991581.md): Seat Track · corroded · May 25, 1999 · N993CF · Doug DC862 · Fuselage, Seat/Cargo Attach Fittings > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO MAIN DECK SEAT TRACK BETWEEN STA 500 AND STA 560 AT BL 56 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SEAT TRACK IAW DC8 - [SDR RRXA991579](https://openairdocs.org/sdr/RRXA991579.md): Seat Track · corroded · May 25, 1999 · N993CF · Doug DC862 · Fuselage, Seat/Cargo Attach Fittings > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO MAIN DECK SEAT TRACK BETWEEN STA 270 AND STA 340 AT BL 0. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SEAT TRACK IAW DC8 SRM 5 - [SDR RRXA991571](https://openairdocs.org/sdr/RRXA991571.md): Seat Track · corroded · May 25, 1999 · N993CF · Doug DC862 · Fuselage, Seat/Cargo Attach Fittings > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO MAIN DECK SEAT TRACK BETWEEN STA 580 AND STA 620 AT BL 0. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SEAT TRACK IAW DC8 SRM 5 - [SDR RRXA991570](https://openairdocs.org/sdr/RRXA991570.md): Seat Track · corroded · May 25, 1999 · N993CF · Doug DC862 · Fuselage, Seat/Cargo Attach Fittings > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO MAIN DECK SEAT TRACK BETWEEN STA 560 AND STA 660 AT BL 56 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SEAT TRACK IAW DC8 - [SDR RRXA991569](https://openairdocs.org/sdr/RRXA991569.md): Seat Track · corroded · May 25, 1999 · N993CF · Doug DC862 · Fuselage, Seat/Cargo Attach Fittings > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO MAIN DECK SEAT TRACK BETWEEN STA 500 AND STA 560 AT BL 22 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SEAT TRACK IAW DC8 Next page: https://openairdocs.org/deregistered/N993CF-2009-08-31/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 = 'N993CF' AND deregistration_id = 'N993CF-2009-08-31' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N993CF-2009-08-31/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.