# Service difficulty reports: N795FT, cancelled Oct 5, 2005 A list on [N795FT, cancelled Oct 5, 2005](https://openairdocs.org/deregistered/N795FT-2005-10-05.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 5 · 205 reports - [SDR RRXA010050](https://openairdocs.org/sdr/RRXA010050.md): Transmitter · failed · Jun 10, 2001 · N795FT · Doug DC873F · Engine Oil Pressure > REJECTED T/O AT DAY, GREATER 60 KTS, NR 2 OIL PRESSURE GAUGE SHOWED AT LEAST 15 PSI HIGHER THAN OTHERS, AND APPEARED TO CONTINUE TO CLIMB. REMOVED AND REPLACED NR 2 ENGINE OIL PRESSURE TRANSMITTER IAW M/M 79-32-1. OPS CHECKS GOOD IAW M/M 71-00-00. - [SDR RRXA010012](https://openairdocs.org/sdr/RRXA010012.md): Control Cable · defective · Feb 16, 2001 · N795FT · Doug DC873F · Landing Gear Steering System > ON TAXI OUT LOST NOSE STEERING AIRCRAFT WAS TOWED BACK TO EMERGENCY RAMP BY AIRPORT DELTA SUPER TUG. GEAR PIN INSTALLED. REMOVED AND REPLACED RIGHT SIDE NOSE STEERING CABLE IAW DC-8 M/M 22-51-0. OPS CHECK GOOD. - [SDR RRXA003602](https://openairdocs.org/sdr/RRXA003602.md): Panel · delaminated · Feb 1, 2001 · N795FT · Doug DC873F · Wing, Plate/Skin > DURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO THE L/H WING BOTTOM T/E PANEL AT STA XRS 419 TO XRS 435, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLE - [SDR RRXA010006](https://openairdocs.org/sdr/RRXA010006.md): Engine · fod · Feb 1, 2001 · N795FT · Doug DC873F · Turbine Engine Air Inlet Section > ON WALK-AROUND FOUND FOD ON NR 3 ENGINE. - [SDR RRXA010034](https://openairdocs.org/sdr/RRXA010034.md): Mechanism · out of adj · Jan 31, 2001 · N795FT · Doug DC873F · Landing Gear Retraction/Extension System > AFTER T/O ACFT DIDN'T GROUND SHIFT; COULD NOT RETRACT MLG. ADJUSTED NOSE GEAR GROUND SHIFT MECHANISM IAW DC-8 M/M CH 32-23-01, OP CHKS GOOD. - [SDR RRXA003799](https://openairdocs.org/sdr/RRXA003799.md): Fitting · corroded · Jan 17, 2001 · N795FT · Doug DC873F · Wing, Nacelle/Pylon Attach Fittings > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LT.WW BATHTUB FITTING AT STA. 960 AND L24L FWD SIDE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW D - [SDR RRXA003592](https://openairdocs.org/sdr/RRXA003592.md): Fitting · cracked · Jan 8, 2001 · N795FT · Doug DC873F · Spoilers > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE RT WING #1 GROUND SPOILER O/B MOUNT FITTING, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1- - [SDR RRXA003591](https://openairdocs.org/sdr/RRXA003591.md): Panel · delaminated · Jan 8, 2001 · N795FT · Doug DC873F · Wing, Plate/Skin > DURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO THE R/H WING BOTTOM T/E PANEL AT STA XRS 340 TO XRS 419, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLE - [SDR RRXA003595](https://openairdocs.org/sdr/RRXA003595.md): Track · cracked · Jan 6, 2001 · N795FT · Doug DC873F · Cargo/Baggage Doors > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE "D-PIT" DOOR AFT TRACK (3" CRACK), DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-21. - [SDR RRXA003594](https://openairdocs.org/sdr/RRXA003594.md): Longeron · corroded · Jan 6, 2001 · N795FT · Doug DC873F · Fuselage Main, Longeron/Stringer > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE UNDER RT LONGERON 24 SUPPORT FITTING AT STA 920 RT W/W Y-920 X-66, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATD REPAIR AND INSTALLED IAW EO 00-316 WITH - [SDR RRXA003593](https://openairdocs.org/sdr/RRXA003593.md): Fitting · cracked · Jan 5, 2001 · N795FT · Doug DC873F · Spoilers > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE #1 GND SPOILER I/B MOUNT FITTING, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8.RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-21 & 51-1-20 - [SDR RRXA003596](https://openairdocs.org/sdr/RRXA003596.md): Fastener · missing · Jan 3, 2001 · N795FT · Doug DC873F · Wing Main, Frame Structure > DURING A MAINTENANCE VISIT FOUND MISSING FASTENER ON THE RT UPPER WING THRU ACCESS HOLE 505C & THROUGH MID SPAR ACCESS HOLE 560C INSIDE TANK I/B BETWEEN STA 252 & 255, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. - [SDR RRXA003603](https://openairdocs.org/sdr/RRXA003603.md): Longeron · cracked · Jan 2, 2001 · N795FT · Doug DC873F · Fuselage Main, Longeron/Stringer > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP ON LONGERON JUST FWD OF 'C' PIT DOOR AT STA 1140 AND L33R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED - [SDR RRXA003601](https://openairdocs.org/sdr/RRXA003601.md): Panel · delaminated · Jan 2, 2001 · N795FT · Doug DC873F · Wing, Plate/Skin > DURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO THE R/H WING BOTTOM T/E PANEL AT STA XRS 5 TO XRS 98, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED I - [SDR RRXA003599](https://openairdocs.org/sdr/RRXA003599.md): Door · delaminated · Jan 2, 2001 · N795FT · Doug DC873F · Cargo/Baggage Doors > DURING A MAINTENANC EVISIT FOUND DELAMINATION IN 2 PLACES ON THE LEFT MLG TOP DOOR TO WING, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-3-0 - [SDR RRXA003598](https://openairdocs.org/sdr/RRXA003598.md): Angle · cracked · Jan 2, 2001 · N795FT · Doug DC873F · Fuselage Main, Bulkhead > DURING A MAINTENANCE VISIT FOUND THE BULKHEAD ATTACH ANGLE BROKEN AND CRACKED ON THE AFT LWR CARGO COMPT AT STA 1320 X35 Z-8, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED RE - [SDR RRXA003597](https://openairdocs.org/sdr/RRXA003597.md): Skin · cracked · Jan 2, 2001 · N795FT · Doug DC873F · Cargo/Baggage Doors > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE AFT LWR CORNER OF THE "D" PIT DOOR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8.FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 52-2-0 FIG. - [SDR RRXA003608](https://openairdocs.org/sdr/RRXA003608.md): Web · chafed · Dec 29, 2000 · N795FT · Doug DC873F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND A CHAFFED WEB IN COCKPIT BETWEEN FRAMES -52 & -67, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 53-2-0 & 51-1-21. - [SDR RRXA003607](https://openairdocs.org/sdr/RRXA003607.md): Panel · delaminated · Dec 29, 2000 · N795FT · Doug DC873F · Fuselage Floor Panel > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE COCKPIT FLOOR PANEL CAPT'S SIDE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-2 - [SDR RRXA003605](https://openairdocs.org/sdr/RRXA003605.md): Pressure Panel · corroded · Dec 29, 2000 · N795FT · Doug DC873F · Fuselage Floor Panel > DURING A MAINTENANCE VISIT FOUND 21 SHEAR RIVETS ON THE FINGER DOUBLER AT THE COCKPIT AREA FLOOR BELOW AFT END OF CAPT'S CHAIR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC- - [SDR RRXA003604](https://openairdocs.org/sdr/RRXA003604.md): Floor Panel · broken · Dec 29, 2000 · N795FT · Doug DC873F · Fuselage Floor Panel > DURING A MAINTENANCE VISIT FOUND ELONGATED SCREW HOLES BROKEN OUT ON THE FLOOR PANEL 681, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-4 - [SDR RRXA003606](https://openairdocs.org/sdr/RRXA003606.md): Skin · punctured · Dec 28, 2000 · N795FT · Doug DC873F · Fuselage Main, Plate/Skin > DURING A MAINTENANCE VISIT FOUND A PUNCTURE HOLE IN THE OUTER SKIN ON THE FUSELAGE AT STA 220 TO 240 AND L25L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-20D & - [SDR RRXA003800](https://openairdocs.org/sdr/RRXA003800.md): Skin · corroded · Dec 22, 2000 · N795FT · Doug DC873F · Fuselage Main, Bulkhead > DURING A MAINTENANCE VISIT FOUND CORROSION/SHEARED RIVITS DAMAGE TO DOUBLER AT STA. 1697 AND L29L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW EO#0 - [SDR RRXA003612](https://openairdocs.org/sdr/RRXA003612.md): Skin · cracked · Dec 20, 2000 · N795FT · Doug DC873F · Wing, Plate/Skin > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE MOST O/B HOLE ON THE R/H WING LWR SKIN AT STR 64, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 - [SDR RRXA003611](https://openairdocs.org/sdr/RRXA003611.md): Fitting · cracked · Dec 20, 2000 · N795FT · Doug DC873F · Wing, Attach Fittings > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE BATHRUB FITTING BETWEEN STA 1690 & 1700 AND L34L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM - [SDR RRXA003610](https://openairdocs.org/sdr/RRXA003610.md): Fitting · cracked · Dec 20, 2000 · N795FT · Doug DC873F · Fuselage Main, Floor Beam > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE FLOOR STRUT FITTING AFT LWR CARGO COMPT AT STA 1160 AND L27R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED I - [SDR RRXA003609](https://openairdocs.org/sdr/RRXA003609.md): Flange · cracked · Dec 20, 2000 · N795FT · Doug DC873F · Fuselage Main, Floor Beam > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE FLOOR BEAM R/H O/B LWR LEG ON FWD SIDE AT STA 920, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW EO#0 - [SDR RRXA003502](https://openairdocs.org/sdr/RRXA003502.md): Intercostal · cracked · Dec 19, 2000 · N795FT · Doug DC873F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE INTERCOSTAL W/W AT STA 940 AND WING STA 69.5 RT W/W, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. - [SDR RRXA003506](https://openairdocs.org/sdr/RRXA003506.md): Skin · corroded · Dec 18, 2000 · N795FT · Doug DC873F · Fuselage Main, Plate/Skin > DURING A MAINTENANCE VISIT FOUND CORROSION BLISTERS ON THE SKIN AT STA 1714 AND L29L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. - [SDR RRXA003505](https://openairdocs.org/sdr/RRXA003505.md): Structure · corroded · Dec 18, 2000 · N795FT · Doug DC873F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE REPAIR PATCH RIVETS ON COCKPIT SUB-FLOOR FWD OF L/H AVIONICS RACK, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////OPEN///// - [SDR RRXA003504](https://openairdocs.org/sdr/RRXA003504.md): Fitting · cracked · Dec 18, 2000 · N795FT · Doug DC873F · Fuselage Main, Attach Fittings > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE ANGLE SUPPORT FITTING AT STA 960 R/H, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. - [SDR RRXA003503](https://openairdocs.org/sdr/RRXA003503.md): Web · corroded · Dec 18, 2000 · N795FT · Doug DC873F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE ON WEB ABOVE RT LONGERON 24Y AT STA 879 X=-59 Z=10 INCH, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. - [SDR RRXA003507](https://openairdocs.org/sdr/RRXA003507.md): Skin · corroded · Dec 15, 2000 · N795FT · Doug DC873F · Cargo/Baggage Doors > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE "D-PIT" DOOR BOTTOM AFT CORNER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. - [SDR RRXA003513](https://openairdocs.org/sdr/RRXA003513.md): Sill · cracked · Dec 14, 2000 · N795FT · Doug DC873F · Fuselage Main, Structure > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE REPAIR AFT SIDE OF "C-PIT" DOOR SILL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////OPEN///// - [SDR RRXA003512](https://openairdocs.org/sdr/RRXA003512.md): Frame · broken · Dec 14, 2000 · N795FT · Doug DC873F · Fuselage Main, Structure > DURING A MAINTENANCE VISIT FOUND THE AFT SIDE FWD FRAME BROKEN OFF "C-PIT" DOOR SILL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. - [SDR RRXA003511](https://openairdocs.org/sdr/RRXA003511.md): Sill · cracked · Dec 14, 2000 · N795FT · Doug DC873F · Fuselage Main, Structure > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE "C-PIT" DOOR SILL REPAIR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. - [SDR RRXA003510](https://openairdocs.org/sdr/RRXA003510.md): Web · cracked · Dec 14, 2000 · N795FT · Doug DC873F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND A CRACK IN WEB AT RT. CUSP AT STA 1300 Y=1300 X-66 Z-0, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. - [SDR RRXA003509](https://openairdocs.org/sdr/RRXA003509.md): Floor Panel · damaged · Dec 14, 2000 · N795FT · Doug DC873F · Fuselage Floor Panel > DURING A MAINTENANCE VISIT FOUND TORN OUT SCREW HOLES ON THE COCKPIT FLOOR PANEL BETWEEN PILOT & CO-PILOTS SEAT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. - [SDR RRXA003508](https://openairdocs.org/sdr/RRXA003508.md): Web · torn · Dec 14, 2000 · N795FT · Doug DC873F · Cargo/Baggage Doors > DURING A MAINTENANCE VISIT FOUND A TORN STRUCTURE ON 'A' PIT DOOR INTERNAL WEB, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. - [SDR RRXA003518](https://openairdocs.org/sdr/RRXA003518.md): Track · cracked · Dec 13, 2000 · N795FT · Doug DC873F · Cargo/Baggage Doors > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE "C-PIT" DOOR DOOR COVER AT TRACK, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. - [SDR RRXA003517](https://openairdocs.org/sdr/RRXA003517.md): Floor Panel · cracked · Dec 13, 2000 · N795FT · Doug DC873F · Fuselage Floor Panel > DURING A MAINTENANCE VISIT FOUND A CRACK AND TORN OUT SCREW HOLES ON THE COCKPIT FLOOR PANEL PILOTS SEAT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. - [SDR RRXA003516](https://openairdocs.org/sdr/RRXA003516.md): Floor Panel · cracked · Dec 13, 2000 · N795FT · Doug DC873F · Fuselage Floor Panel > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE FLOOR PANEL 678, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. - [SDR RRXA003515](https://openairdocs.org/sdr/RRXA003515.md): Skin · cracked · Dec 13, 2000 · N795FT · Doug DC873F · Cargo/Baggage Doors > DURING A MAINTENANCE VISIT FOUND 2 CRACKS ALONG BOTTOM OF MAIN CARGO DOOR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. - [SDR RRXA003514](https://openairdocs.org/sdr/RRXA003514.md): Fitting · cracked · Dec 13, 2000 · N795FT · Doug DC873F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE RT LONGERON 24 SUPPORT FITTING FWD EDGE AT STA 902, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////OPEN///// - [SDR RRXA003806](https://openairdocs.org/sdr/RRXA003806.md): Door Frame · corroded · Dec 12, 2000 · N795FT · Doug DC873F · Fuselage Main, Structure > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO A-PIT DOOR FRAME AT STA. 300, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8.FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 53-2-0 & 51-1-21. - [SDR RRXA003522](https://openairdocs.org/sdr/RRXA003522.md): Threshold · cracked · Dec 12, 2000 · N795FT · Doug DC873F · Fuselage Main, Structure > DURING A MAINTENANCE VISIT FOUND A CRACK AND DENTED EDGES TO THE "D-PIT" THRESHOLD/KICK PLATE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////OPEN///// - [SDR RRXA003521](https://openairdocs.org/sdr/RRXA003521.md): Doubler · cracked · Dec 12, 2000 · N795FT · Doug DC873F · Cargo/Baggage Doors > DURING A MAINTENANCE VISIT FOUND 'C-PIT' DOOR HAS REPAIR CRACKING OFF, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. - [SDR RRXA003520](https://openairdocs.org/sdr/RRXA003520.md): Bulkhead · damaged · Dec 12, 2000 · N795FT · Doug DC873F · Fuselage Main, Bulkhead > DURING A MAINTENANCE VISIT FOUND GILLINER ATTACH ANGLE & BULKHEAD ATTACH HOLES BROKEN OUT ON THE AFT LWR CARGO BILGE AT STA 1320 AND L31L TO L31R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. - [SDR RRXA003519](https://openairdocs.org/sdr/RRXA003519.md): Frame · cracked · Dec 12, 2000 · N795FT · Doug DC873F · Cargo/Baggage Doors > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE "C-PIT" DOOR FWD FRAME (DOOR COVER), DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. - [SDR RRXA003529](https://openairdocs.org/sdr/RRXA003529.md): Bracket · worn · Dec 11, 2000 · N795FT · Doug DC873F · Fuselage Main, Attach Fittings > DURING A MAINTENANCE VISIT FOUND A WORN "T-BOLT" RETAINING BRACKET (TOP SIDE) NR 5 BOTTOM, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. Next page: https://openairdocs.org/deregistered/N795FT-2005-10-05/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 = 'N795FT' AND deregistration_id = 'N795FT-2005-10-05' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N795FT-2005-10-05/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.