# Service difficulty reports: N675MC, cancelled Jul 26, 2019

A list on [N675MC, cancelled Jul 26, 2019](https://openairdocs.org/deregistered/N675MC-2019-07-26.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 3 · 101 reports

- [SDR DALA13033600880](https://openairdocs.org/sdr/DALA13033600880.md): Wire · broken · Jun 30, 2013 · N675MC · Doug DC951 · Light System Wiring
  > SEAT 12DEF EMERGENCY LIGHT INOPERATIVE. FOUND WIRE BROKEN AT SEAT TRACK. REPAIRED WIRE IAW SWPM 20-10. OPS CHECKED GOOD.
- [SDR DALA13033400880](https://openairdocs.org/sdr/DALA13033400880.md): Battery Pack · inoperative · Jun 30, 2013 · N675MC · Doug DC951 · Emergency Lighting
  > EMERGENCY EXIT SIGNS INOPERATIVE. R & R 14A EXIT SIGN BATTERIES IAW AMM, OPS CHECKED NORMAL.
- [SDR DALA13024580880](https://openairdocs.org/sdr/DALA13024580880.md): Lamp · inoperative · May 21, 2013 · N675MC · Doug DC951 · Emergency Lighting
  > DURING SERVICE CHECK FOUND ESCAPE PATH LIGHTS INOPERATIVE AT ROWS 6-8 AND 3 OF 4 RT SIDE OVERWING EXIT BULBS INOPERATIVE. REPLACED LAMPS AND REPLACED FUSE IAW AMM 33-53. OPS CHECKED GOOD.
- [SDR DALA13017960880](https://openairdocs.org/sdr/DALA13017960880.md): Bushing · corroded · Apr 17, 2013 · N675MC · Doug DC951 · Wing, Landing Gear Attach Fittings
  > FOUND THAT INBD BUSHING IS OUT OF LIMITS FOR STANDARD BUSHING. RT MLG REF N/R 3. REAMED INBD BORE TO 2.136 FOR.010 OVER BUSHING IAW CMM 57-40-1. REPAIR GENERAL 2G1. C/W FPI INSPECTION IAW CMM 57-40-1. FOUND PITTING IN BORE. REAMED INBD BORE TO 2.1515 FO
- [SDR DALA13016970880](https://openairdocs.org/sdr/DALA13016970880.md): Wire · broken · Apr 12, 2013 · N675MC · Doug DC951 · Light System Wiring
  > ROW 8B EMERGENCY LIGHTS INOPERATIVE. SPLICED BROKEN WIRE IAW SWPM 20. OPS CHECKED GOOD.
- [SDR DALA13014730880](https://openairdocs.org/sdr/DALA13014730880.md): Light · damaged · Apr 1, 2013 · N675MC · Doug DC951 · Emergency Lighting
  > FWD GALLEY FLOOR LEVEL EMERGENCY EXIT LIGHT DAMAGED. REPLACED LIGHT ASSY IAW AMM 33-53. OPS CHECKED NORMAL.
- [SDR DALA12009910880](https://openairdocs.org/sdr/DALA12009910880.md): Intercostal · cracked · Oct 10, 2012 · N675MC · Doug DC951 · Fuselage Miscellaneous Structure
  > INTERCOSTAL CRACKED FORWARD RT CABIN, 4" FWD OF STA 160 AT LONGERON R-9. REMOVED 1 EA GUSSET TO FOM & DAMAGED ANGLE, 4" FWD OF STA 160 AT L-9R, FABRICATED TOP ANGLE REPAIR ON TRAVEL (SAA 700022065-T3 PN) 70002195820001. FABRICATED BOTTOM ANGLE REPAIR PN 70002
- [SDR DALA12009900880](https://openairdocs.org/sdr/DALA12009900880.md): Stringer · cracked · Oct 9, 2012 · N675MC · Doug DC951 · Fuselage Main, Longeron/Stringer
  > FUSELAGE CENTER SECTION FUEL AUXILIARY TANK LOWER STRINGER CRACKED, VIEWED THRU NR 5115A AND RBL 8. DOT 21-02. ACCOMPLISHED PERMANENT REPAIR ON CENTER FUEL AUXILIARY TANK LOWER STINGER RBL 8 IAW SRM 53-05, FIG 46. INSTALLED ID TAG IAW DPS 900-5-1 NR 4.
- [SDR DALA12009420880](https://openairdocs.org/sdr/DALA12009420880.md): Stringer · cracked · Oct 7, 2012 · N675MC · Doug DC951 · Fuel Storage
  > FUSELAGE CENTER SECTION FUEL AUXILIARY TANK LOWER STRINGER CRACKED VIEWED THRU 5115A & RBL6. CUT OUT DAMAGE IAW SRM 53-05, FIG 46. NDT VERIFY NO CRACKS NOTED AT CUT OUT. FABRICATED TWO REPAIR ANGLES. FABRICATED ONE REPAIR FILLER IAW SRM 53-05, FIG 46. LOCATED
- [SDR DALA12009350880](https://openairdocs.org/sdr/DALA12009350880.md): Floor Panel · cracked · Oct 4, 2012 · N675MC · Doug DC951 · Fuselage Floor Panel
  > MAIN CABIN ALUMINUM FLOOR PANEL 72A FWD EDGE BENT, BUCKLED, CRACKED BS 734. FABRICATED STIFFENER AND FLOOR PANEL 72, IAW SRM 53-23-0, FIG 5.
- [SDR DALA1166679880](https://openairdocs.org/sdr/DALA1166679880.md): Skin · damaged · Nov 29, 2011 · N675MC · Doug DC951 · Fuselage Main, Plate/Skin
  > WATER LEAKING FROM CEILING AT ROW 25. REPAIRED FUSELAGE SKIN LAP PER ERA 498220-14. (L/P 8497670, 0402767)
- [SDR DALA1161009880](https://openairdocs.org/sdr/DALA1161009880.md): O-Ring · leaking · Oct 29, 2011 · N675MC · Doug DC951 · Cabin Cooling System
  > DURING CLIMBOUT, AFTER A REQUEST FOR INCREASED CABIN TEMP INBACK OF AIRCRAFT, STRONG ODOR (OIL SMELL) ENTERED CABIN, CAUSING FLIGHT ATTENDANTS TO GET SICK. WITH CABIN TEMP CONTROL RETURNED TO AUTO, SMELL WENT AWAY. SECURED AND REPLACED O-RING ON RIGHT PACK AC
- [SDR DALA1149509880](https://openairdocs.org/sdr/DALA1149509880.md): Pin · loose · Aug 22, 2011 · N675MC · Doug DC951 · Emergency Lighting
  > MAINTENANCE FOUND SEAT 1C EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE. MAINTENANCE RECONNECTED LOOSE PIN ON SEAT BOTTOM. AIRCRAFT OK FOR SERVICE.
- [SDR DALA1149219880](https://openairdocs.org/sdr/DALA1149219880.md): Skin · cracked · Aug 20, 2011 · N675MC · Doug DC951 · Fuselage Main, Plate/Skin
  > CRACK IN SKIN AT CANTED FRAME STA 1303 JUST ABOVE STRINGER 14 LT SIDE. CRACK IS APPROXIMATELY 2.6 INCHES IN LENGTH. REPAIRED CRACK IN SKIN PER DC-9 SRM 53-01 FIG 4 SHEET 4 AND DC-9 TRM 53-30-01-801-663A-A. JOB COMPLETE.
- [SDR DALA1146399880](https://openairdocs.org/sdr/DALA1146399880.md): Skin · gouged · Jun 9, 2011 · N675MC · Doug DC951 · Leading Edge Devices
  > RT WING NR 1 SLAT PANEL INBOARD LOWER SKIN WITH GOUGE DUE TO CHAFING WITH L/E (MMO89) BLENDED AREA ON LWR SKIN INBD ON RT WING NR 1 SLAT REF DC9 SRM 57-01 FIG 1. BLENDED AREA FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED NR 1 RT SLAT IAW AMM DC9-27-80-01
- [SDR DALA1138819880](https://openairdocs.org/sdr/DALA1138819880.md): Skin · dented · Jun 9, 2011 · N675MC · Doug DC951 · Ailerons
  > LT WING AILERON UPPER SKIN WITH SEVERAL (7) DENTS FROM STA XRS 383 TO XRS 509 (MM067) RII: Y. PROCURED SERVICEABLE AILERON. AILERON REMOVED, REPLACED, AND ADJUSTED. RII INSPECTION COMPLETED (87761280001) & WC 2711-9800M, JOB 000-0022 (87761390001).
- [SDR DALA1138809880](https://openairdocs.org/sdr/DALA1138809880.md): Skin · worn · Jun 9, 2011 · N675MC · Doug DC951 · Vertical Stabilizer, Plate/Skin
  > RT SIDE VERTICAL STABILIZER LEADING EDGE TIP SKIN HAS A DEEP WEAR AREA APPROX 22 INCH LONG, CAUSED BY BANANA FAIRING. BLENDED AREA REF SRM 55-01 FIG 1. LOWER BLEND FOUND OUT OF LIMITS & WAS TRIMMED OUT. A REPAIR DOUBLER MADE AND INSTALLED. REF COMPLIED ER/
- [SDR DALA1138799880](https://openairdocs.org/sdr/DALA1138799880.md): Skin · dented · Jun 9, 2011 · N675MC · Doug DC951 · Fuselage Main, Plate/Skin
  > LWR FUSELAGE STA Y351, BETWEEN LONG 29LT AND LONG 30. EXT SKIN WITH DENT. RII: Y. DENT AT FUSELAGE AT STA Y351 BETWEEN LONG 29L AND LONG 30, OUT OF LIMITS. CUT OUT DAMAGE, FABRICATED, AND INSTALLED EXTERNAL REPAIR DOUBLER, FINGER DOUBLER, AND FILLER IAW SRM
- [SDR DALA1138769880](https://openairdocs.org/sdr/DALA1138769880.md): Floor Panel · damaged · Jun 9, 2011 · N675MC · Doug DC951 · Fuselage Floor Panel
  > CABIN FLOOR PNL 37 FWD END TOP SKIN IS CRACKED, DENTED, AND CORRODED. RII: Y. REMOVED EXISTING REPAIR WITH CRACK AT CENTER PORTION OF PANEL 37. FURTHER EVALUATION FOUND CRACK IN PNL. STOP DRILL CRACK IN PANEL. FABRICATED AND INSTALLED REPAIR IAW SRM 51-30-
- [SDR DALA1138829880](https://openairdocs.org/sdr/DALA1138829880.md): Skin · damaged · Jun 8, 2011 · N675MC · Doug DC951 · Ailerons
  > RT WING AILERON INBOARD LATERAL FACE SKIN WITH HOLES ELONGATED (MM095). RII: Y PROCURED SERVICIABLE AILERON, AILERON REMOVED, REPLACED AND ADJUSTED. AILERON, RIGHT; OFF 09-5751-9-0002 47321 ON 09-5751-9-0002 47659.
- [SDR DALA1138789880](https://openairdocs.org/sdr/DALA1138789880.md): Skin Panel · dented · Jun 2, 2011 · N675MC · Doug DC951 · Fuselage Main, Plate/Skin
  > DURING MCK AT SAT, 9 DENTS WERE FOUND IN THE FUSELAGE SKIN PANEL BETWEEN RT STA 297 - 333 AND L23R - L25R. ACCOMPLISHED PERMANENT REPAIR AT STA 298 TO STA 333.5 BETWEEN L-23R TO L-25R REFERENCE ERA 492119-14 REV ORIGINAL, 1. ASSOCIATED ER/A CHANGED FROM 13-
- [SDR DALA1137589880](https://openairdocs.org/sdr/DALA1137589880.md): Stringer · cracked · Jun 2, 2011 · N675MC · Doug DC951 · Fuselage Main, Longeron/Stringer
  > STRINGER 17L CRACKED ON RADIUS NEAR UPPER ATTACHMENT FASTENER OF FRAME STA 237. REMOVED DAMAGED SECTION PER SRM 53-02 FIG 18, NDT NO DAMAGE NOTED. FABBED STRINGER SECTION AND SPLICE PER 53-02 FIG 18. TREATED AND PRIMED ALL PARTS PER SRM 51-10-3 PAGE 31-40.
- [SDR DALA1137349880](https://openairdocs.org/sdr/DALA1137349880.md): Cusp Web · cracked · May 31, 2011 · N675MC · Doug DC951 · Fuselage Miscellaneous Structure
  > RT CUSP WEB AT STA 215 LIGHTENING HOLE HAS CRACK. STOP DRILLED CRACK AT FLOOR WEB BY LIGHTENING HOLE STA 218 IAW DC9 SRM 53-01 FIG 2. FABRICATED REPAIR DOUBLER IAW SRM 51-70-4 FIG 2. INSTALLED DOUBLER FLOOR WEB STA 215 IAW SRM 51-30-2.
- [SDR DALA1137179880](https://openairdocs.org/sdr/DALA1137179880.md): Skin · dented · May 30, 2011 · N675MC · Doug DC951 · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE STA Y1115.5 BETWEEN LONGERON 27R AND 28R, EXTERNAL SKIN WITH DENT. COMPLIED WITH PERMANENT REPAIR PER ERA#492136-14 REV ORIGINAL AT FUSELAGE STA 1115.5 BETWEEN LONGERON 27R AND 28R.
- [SDR DALA1137089880](https://openairdocs.org/sdr/DALA1137089880.md): Web · cracked · May 28, 2011 · N675MC · Doug DC951 · Fuselage Floor Panel
  > FLOOR WEB HAS CRACK INBD EDGE AT FS STA 261 RBL44. CUT OUT DAMAGED SECTION IAW SRM 51-70-4 FIG 2. FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 51-70-4 FIG 2. INSTALLED PER SRM 51-30-2 AND SRM 51-70-4 FIG 2.
- [SDR DALA1137069880](https://openairdocs.org/sdr/DALA1137069880.md): Floor Panel · damaged · May 28, 2011 · N675MC · Doug DC951 · Fuselage Floor Panel
  > PASS CABIN FLOOR PANEL NR 66 WITH ELONGATED HOLES. FABRICATED DOUBLER REPAIR WASHER IAW DC9 SRM 53-05 PG: 12 FIG 3 SRM 51-60-0 PG: 6 FIG 1 AND INSTALLED 3 DOUBLER REPAIR WASHER PERMACEL TAPE IAW AMM DC9 -A-53-20-01-201-925A-A AND SRM 53-05 PG 12 FIG 3.
- [SDR DALA1146299880](https://openairdocs.org/sdr/DALA1146299880.md): Skin · dented · May 27, 2011 · N675MC · Doug DC951 · Fuselage Main, Plate/Skin
  > UPPER FUSELAGE STA 251 BETWEEN LONG 17 LT AND 18 LT EXTERNAL SKIN WITH DENT. RII:Y. CUT OUT DAMAGED AREA, NDT NO DAMAGE NOTED, FABRICATED TREATED AND INSTALLED ALL REPAIR PARTS IAW DC-9 SRM 53-04 FIG 12B PAGE 60F. INSTALLED ID TAG PER PS900-5-1 NR 04.
- [SDR DALA1136769880](https://openairdocs.org/sdr/DALA1136769880.md): Floor Panel · damaged · May 26, 2011 · N675MC · Doug DC951 · Fuselage Floor Panel
  > PASS CABIN, FLOOR PANEL NR 67B, ELONGATED HOLES OFF A/C PART(JG022). FABRICATED AND INSTALLED 3 DOUBLER REPAIR WASHERS AND PERMACEL TAPE AT PASS CABIN FLOOR PANEL NR 67B IAW AMM DC9-A-53-20-01-201-925A-A AND SRM 53-05 PG 12 FIG 3.
- [SDR DALA1136759880](https://openairdocs.org/sdr/DALA1136759880.md): Floor Panel · damaged · May 26, 2011 · N675MC · Doug DC951 · Fuselage Floor Panel
  > PASS CABIN FLOOR PANEL NR 72B, ELONGATED HOLES OFF A/C PART. FABRICATED AND INSTALLED 3 DOUBLER REPAIR WASHERS AND PERMACEL TAPE IAW AMM DC-9-A-53-20-01-201-925A-A AND SRM 53-05 PG 12 FIG 3.
- [SDR DALA1136749880](https://openairdocs.org/sdr/DALA1136749880.md): Floor Panel · damaged · May 26, 2011 · N675MC · Doug DC951 · Fuselage Floor Panel
  > PASS CABIN FLOOR PANEL NR 29 ELONGATED HOLES. FABRICATED AND INSTALLED 2 DOUBLER REPAIR WASHERS AND PERMACEL TAPE AT PASS CABIN FLOOR PANEL NR 29 IAW AMM DC9-A-53-20-01-201-925A-A AND SRM 53-05 PG 12 FIG 3.
- [SDR DALA1138679880](https://openairdocs.org/sdr/DALA1138679880.md): Floorboard · corroded · May 25, 2011 · N675MC · Doug DC951 · Fuselage Floor Panel
  > FLOORBOARD 19 HAS CORROSION (DT-09). REMOVED, FABRICATED, AND INSTALLED FLOORBOARD PANEL SKIN 19 AND 2 EA U-CHANNELS AT FLOORBOARD PANEL 19 IAW DC-9 SRM 53-23-0, FIG 3, SHT 3, PG 6, AND DC-9 SRM 51-30-2, PG 24.
- [SDR DALA1138649880](https://openairdocs.org/sdr/DALA1138649880.md): Connector · broken · May 25, 2011 · N675MC · Doug DC951 · Light System Wiring
  > MAINTENANCE FOUND EMERGENCY LIGHT CONNECTOR BROKEN AT FORWARD LEFT OVERWING EXIT SIDEWALL PANEL. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT CONNECTOR. OPERATIONAL CHECK WAS GOOD.
- [SDR DALA1136739880](https://openairdocs.org/sdr/DALA1136739880.md): Floorboard · damaged · May 24, 2011 · N675MC · Doug DC951 · Fuselage Floor Panel
  > MAIN CABIN FLOOR BOARD NR 23, ENLONGATED HOLES, (5). FABRICATED 5 DOUBLER REPAIR WASHERS IAW DC9 SRM 53-05, PG 12, FIG 3, SRM 51-60-0, FIG 1, AND INSTALLED 5 DOUBLER. REPAIR WASHERS AND PERMACEL TAPE AT MAIN CABIN FLOOR BOARD NR 23 IAW AMM DC-9-A-53-20-01-20
- [SDR DALA1137119880](https://openairdocs.org/sdr/DALA1137119880.md): Vane · dented · May 19, 2011 · N675MC · Doug DC951 · Trailing Edge Flaps
  > LT FLAP, MOVABLE VANE LWR SURFACE HAS A DENT. REPAIRED DENT IAW DC9 SRM 57-03, FIG 11, DC9 SRM 51-70-2, DC9 SRM 57-50-9, ITEM 2, FIG 1A, PG 3, DC9 SRM 57-03, PARA. 11B, DC9 SRM 51-70-2, DC9 SRM 51-10-3, PARA 21, DC9 SRM 51-70-2, DC9 SRM 51-10-3, REPAIRED BY C
- [SDR DALA1137109880](https://openairdocs.org/sdr/DALA1137109880.md): Floorboard · cracked · May 11, 2011 · N675MC · Doug DC951 · Fuselage Floor Panel
  > FLOORBOARD PANEL NR 69 LOWER STIFFENER CRACKED AT SCREW HOLES. REMOVED AND REPLACED LOWER STIFFENER "SUPPORT" ON FLOORBOARD PANEL NR 69 IAW SRM 51-30-2, PG 1-24, P/N 9957925-110, BATCH NR 0002052379.
- [SDR DALA1137059880](https://openairdocs.org/sdr/DALA1137059880.md): Floor Panel · damaged · May 11, 2011 · N675MC · Doug DC951 · Fuselage Floor Panel
  > PASS CABIN FLOOR PANEL NR 65, ENLONGATED HOLES. FABRICATED DOUBLER REPAIR WASHERS IAW DC9 SRM 53-05, PG 12, FIG 3, SRM 51-60-0, PG 6 FIG 1, AND INSTALLED 3 DOUBLER REPAIR WAS HERS AND PERMACEL TAPE AT PASS CABIN FLOOR PANEL NR 65, IAW AMM DC9-A-53-20-01-201-9
- [SDR DALA1146409880](https://openairdocs.org/sdr/DALA1146409880.md): Floor Support · corroded · May 9, 2011 · N675MC · Doug DC951 · Fuselage Miscellaneous Structure
  > CORROSION LEVEL: 2. LAV FLOOR SUPPORT FITTING HAS HEAVY CORROSION AND ATTACH BOLT HOLE THREADS DAMAGED IN FITTING, STA 200, LBL 44 RL005. REMOVED AND REPLACED LAV SUPPORT FITTING AT STA 200, LBL 44, IAW SRM DC9 51-30-5, FIG 1, PG 2, 12, 29, PARA 7, SRM DC9 51
- [SDR DALA1138779880](https://openairdocs.org/sdr/DALA1138779880.md): Tie Clip · cracked · May 9, 2011 · N675MC · Doug DC951 · Fuselage Miscellaneous Structure
  > TIE CLIP CRACKED AT LT SIDE AFT WALL STA 1136, BELOW LONGERON 14L (MAJOR REPAIR) RII: Y FOUND IN COMING ELONGATED HOLE ON SKIN. EXTERNAL REPAIR DOUBLER AND FILLER INSTALLED TOGETHER WITH THE NEW TIE CLIPS (ANGLES). ACCOMPLISHED ER/A 493033-14, REV ORIG, 2 EA
- [SDR DALA1137869880](https://openairdocs.org/sdr/DALA1137869880.md): Floor Panel · damaged · May 9, 2011 · N675MC · Doug DC951 · Fuselage Floor Panel
  > CABIN FLOOR PNL 81B TOP SKIN IS TORN OUT AT ATTACH SCREWS. CUT OUT DAMAGE FROM PANEL 81B TOP SKIN IAW SRM 53-05, PTG 10, FIG 1, NO CRACKS NOTED, FABRICATED DOUBLER AND FILLER. INSTALLED REPAIR PARTS IAW SRM 53-05, FIG 1, PG 10, AND RII COMPLETED BY 883716, S
- [SDR DALA1137049880](https://openairdocs.org/sdr/DALA1137049880.md): Floor Panel · damaged · May 9, 2011 · N675MC · Doug DC951 · Fuselage Floor Panel
  > CABIN FLOOR PNL 89 TOP SKIN TORN WITH PULLED THRU SCREW. CUTOUT DAMAGE FROM TOP SKIN AND FABRICATED DOUBLER FROM SHT 7075T6,.040, BATCH #0001590589, IAW SRM 51-70-4, PG 6, FIG 2 AND SRM 53-23-0, PG 9. TREATED AND PRIMED IAW SRM 51-10-3,PG 31, 40, AND INSTAL
- [SDR DALA1137039880](https://openairdocs.org/sdr/DALA1137039880.md): Seat Track · corroded · May 9, 2011 · N675MC · Doug DC951 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK HAS AREAS OF CORROSION FROM STA 200 TO 315, RBL-44. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-05, FIG 4B FROM STA 284 TO STA 200, RBL 44 MAIN CABIN SEAT TRACK. CUT OUT DAMAGED SECTION SEAT TRACK T STA 284 TO STA 200 RBL 44 IAW SRM
- [SDR DALA1137029880](https://openairdocs.org/sdr/DALA1137029880.md): Floor Panel · cracked · May 9, 2011 · N675MC · Doug DC951 · Fuselage Floor Panel
  > CABIN FLOOR PNL 76 TOP SKIN HAS CRACK AT EDGE REMOVED EDGE DAMAGE AT CABIN FLOOR PANEL 76, ORG MAT 18 INCHES LONG, MAT LOSS.35, WITHIN LIMITS IAW SRM 53-01, PG 6. FOUND CRACK ON AFT END OF FLOOR PANEL 76, CUT OUT DAMAGE, FABRICATED DOUBLER IAW SRM 51-70-04,
- [SDR DALA1136729880](https://openairdocs.org/sdr/DALA1136729880.md): Floor Panel · punctured · May 9, 2011 · N675MC · Doug DC951 · Fuselage Floor Panel
  > CABIN FLOOR PNL 102B HAS PUNCTURES 77-27. CUT OUT DAMAGE ON FLOOR BOARD PANEL NR 102B IAW DC9 SRM 53-05, PG 11, SEC. B-B. FABRICATED AND INSTALLED FLOOR BOARD PANEL NR 102B. REPAIR DOUBLER IAW DC9 SRM 51-30-2, PGS 1-2, 4, 26B.
- [SDR DALA1136539880](https://openairdocs.org/sdr/DALA1136539880.md): Seat Track · corroded · May 9, 2011 · N675MC · Doug DC951 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK HAS AREAS OF CORROSION FROM STA 200 TO 315,LBL 44. BLENDED CORROSION AT 3 AREAS STA 210, 245, AND 260 ON SEAT TRACK LBL 44- OUT OF LIMITS, PER SRM 53-05, FIG 4B, SHEET 1. REMOVED AND REPLACED DAMAGED SECTION FROM STA 200 TO 268 AT PREVIOUS
- [SDR DALA1136439880](https://openairdocs.org/sdr/DALA1136439880.md): Seat Track · corroded · May 9, 2011 · N675MC · Doug DC951 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK HAS AREAS OF CORROSION FROM STA 200 TO 315,LBL -22. BLENDED OUT CORROSION AREAS OUT LIMITS PER SRM 53-05, FIG 4B, SHEET 1. REMOVED AND REPLACED SEAT TRACK AT MAIN CABIN STA 200-300 LBL 22 PER SRM 53-05, FIG 4F. 4EA AREAS OF SEAT TRACK REW
- [SDR DALA1136059880](https://openairdocs.org/sdr/DALA1136059880.md): Floor Panel · corroded · May 9, 2011 · N675MC · Doug DC951 · Fuselage Floor Panel
  > CABIN FLOOR PNL 36 FWD END TOP SKIN IS CORRODED, 77-40. BLENDED CORROSION AT MAIN CABIN FLOOR PNL 36 FWD END OF TOP SKIN ORG MAT..040 IAW SRM 53-23-0, FIG 4 OUT OF LIMITS IAW SRM 53-01, FIG 1, SHT 3. REMOVED 5 HAT CHANNELS IAW SRM 51-32-0, FABED NEW TOP SK
- [SDR DALA1136049880](https://openairdocs.org/sdr/DALA1136049880.md): Floor Support · corroded · May 9, 2011 · N675MC · Doug DC951 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT ANGLE HAS CORROSION AND LAV ATTACH BOLT SHEARED IN FITTING, FROM STA 200 TO 218, RBL-19. REMOVED AND REPLACED FLOOR SUPPORT ANGLE WITH "EXTRUSION" P/N 00-02-10-3-3672, AT STA 200 TO 218, RBL 19, IAW DWG 94FS481235 AND SRM 51-30-5, PG 12, PARA 7.
- [SDR DALA1135929880](https://openairdocs.org/sdr/DALA1135929880.md): Floorboard · damaged · May 9, 2011 · N675MC · Doug DC951 · Fuselage Floor Panel
  > FLOORBOARD, NR 102C LT AFT CORNER IS BROKEN CUT OUT DAMAGED AREA OF FLOORBOARD NR 102C IAW SRM 51-70-4, FABED (1) EA DOUBLER AND (1) EA SPLICE MAT, IAW SRM 51-70-4, FIG 1, PAGE 1, TREATED AND PRIMED IAW SRM 51-10-3, PAGE 27-31, INST REPAIR IAW SRM 51-70-4. C
- [SDR DALA1135619880](https://openairdocs.org/sdr/DALA1135619880.md): Floor Support · corroded · May 9, 2011 · N675MC · Doug DC951 · Fuselage Miscellaneous Structure
  > CABIN FLOOR SUPPORT ANGLE HAS CORROSION FROM BS 160 TO 313 AT BL-0. BLENDED OUT CORROSION MAIN CABIN FLOOR SUPPORT ANGLE AT BL0 BS 160 TO BS 313 IAW SRM 51-10-3 FROM BS 160 TO BS 218 WITHIN LIMITS IAW SRM 53-01, FIG 1, FROM STA 218 TO 285, OUT OF LIMITS AT B
- [SDR DALA1135609880](https://openairdocs.org/sdr/DALA1135609880.md): Floor Support · corroded · May 9, 2011 · N675MC · Doug DC951 · Fuselage Miscellaneous Structure
  > CABIN FLOOR SUPPORT ANGLE HAS CORROSION STA 160 TO 200, LBL 44. BLENDED CORROSION ON FLOOR SUPPORT, OUT OF LIMITS, PER SRM 53-01, FIG 1, SHEET 3. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-30-5, PG 1-29.

Next page: https://openairdocs.org/deregistered/N675MC-2019-07-26/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 = 'N675MC' AND deregistration_id = 'N675MC-2019-07-26'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N675MC-2019-07-26/reports

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