# Service difficulty reports: N89427, cancelled Sep 20, 2011

A list on [N89427, cancelled Sep 20, 2011](https://openairdocs.org/deregistered/N89427-2011-09-20.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 · 161 reports

- [SDR C8GA2010000056](https://openairdocs.org/sdr/C8GA2010000056.md): Switch · inoperative · Oct 5, 2010 · N89427 · Boeing 727227 · Door Warning System
  > DURING TAKEOFF ROLL AT 80 KNOTS. THE AMBER AFT AIR-STAIR LIGHT ILLUMINATED. ACFT ABORTED TAKEOFF WHERE IT PRECEDED WITH OUT INCIDENT. POST FLIGHT INSP WAS PERFORMED, THE UPPER CONTROL HANDLE SWITCH DETERMINED TO BE AT FAULT. ITEM WAS DEFERRED AND ACFT WAS RE
- [SDR C8GA201000013](https://openairdocs.org/sdr/C8GA201000013.md): Switch · faulted · Jul 30, 2010 · N89427 · Boeing 727227 · Independent Instruments
  > DURING TAKEOFF ROLL WITH THE ACFT BELOW 60 KNOTS THE TAKEOFF WARNING HORN SOUNDED. TAKEOFF WAS ABORTED WITHOUT INCIDENT AND RETURNED TO THE BLOCKS. POST FLIGHT INSP WAS PERFORMED, STABILIZER TAKEOFF WARNING SWITCH S533 WAS AT FAULT. R & R THE STABILIZER TAKEO
- [SDR C8GA201000008](https://openairdocs.org/sdr/C8GA201000008.md): Door · out of adjust · Apr 16, 2010 · N89427 · Boeing 727227 · Landing Gear Door Retract Section
  > FLT 735 FROM MMY TO TOL ON VISUAL APPROACH INTO TOLEDO UPON SELECTING GEAR DOWN THE LEFT AND RIGHT MAIN GEAR CAME DOWN NORMALLY, BUT THE NOSE GEAR REMAINED IN THE WELL WITH NO DOOR LIGHT. THE GEAR UNSAFE CHECKLIST WAS PERFORMED. AFTER APPROXIMATELY ONE MINUT
- [SDR C8GA201000002](https://openairdocs.org/sdr/C8GA201000002.md): Duct · cracked · Jan 20, 2010 · N89427 · Boeing 727227 · Engine Anti-Icing System
  > DURING CLIMB OPERATION THE LOWER AFT BODY OVERHEAT ILLUMINATED IN FLIGHT. CREW PERFORMED APPROPRIATE CHECKLIST AND DIVERTED, WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSP REVEALED THAT THE NR 3 ENGINE ANTI-ICE DUCT WAS CRACKED. REMOVED AND REPAIRED DAMAG
- [SDR C8GA20090295](https://openairdocs.org/sdr/C8GA20090295.md): Spar · corroded · Jul 31, 2009 · N89427 · Boeing 727227 · Elevator, Spar/Rib
  > REMOVED AND REPLACED RT ELEVATOR SPAR AND SUPPORT FITTINGS. ACFT WAS RETURNED TO SERVICE.
- [SDR C8GA20090294](https://openairdocs.org/sdr/C8GA20090294.md): Stringer Splice · corroded · Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT BS 1010 28L SKIN IS CORRODED. REMOVED SPLICE, FABRICATED NEW SPLICE FROM BAC 1498-131 DIM 12.25" X 4.25" INSTALLED REPAIR, NO OTHER DEFECT NOTED. ACFT WAS RETURNED TO SERVICE.
- [SDR C8GA20090293](https://openairdocs.org/sdr/C8GA20090293.md): Stringer · corroded · Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT BS 1050-1030 STR 30 IS CORRODED. REMOVED DAMAGED AREA DIM 19". FABRICATED NEW STR FROM BAC 1449146 7075 T62 DIM 19" AND SPLICE FROM BAC 1498-131 DIM 10.5" INSTALLED REPAIR, NO OTHER DEFECT NOTED. ACFT WAS
- [SDR C8GA20090292](https://openairdocs.org/sdr/C8GA20090292.md): Frame · corroded · Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Frame
  > WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT FRAME AT BS 1010 IS CORRODED AT STR 29L. REMOVED DAMAGED AREA DIM 2" X 5.5". FABRICATED NEW SHEAR TIE FROM 7075 T6.063" X 5.5" X 2.3125" AND DOUBLER FROM 7075 T6.071" X 3.25" X 7". INSTALLED REPAIR, NO OT
- [SDR C8GA20090291](https://openairdocs.org/sdr/C8GA20090291.md): Stringer · corroded · Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT FRAME AT BS 1010 IS CORRODED AT STR 29R. REMOVED PREVIOUS REPAIR. FABRICATED NEW STRINGER FROM BAC1498-147, FWD SPLICE FROM BAC 1498-131 7075 T6 DIM 15" AND 12". INSTALLED REPAIR, NO OTHER DEFECT NOTED. AC
- [SDR C8GA20090290](https://openairdocs.org/sdr/C8GA20090290.md): Frame · dented · Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Frame
  > WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT FRAME AT BS 1030 IS DENTED. BETWEEN STR 27R AND 26R. REMOVED DAMAGED AREA, FABRICATED REPAIR DOUBLER, HEAT TREATED TO T6. INSTALLED REPAIR, NO OTHER DEFECT NOTED. ACFT WAS RETURNED TO SERVICE.
- [SDR C8GA20090289](https://openairdocs.org/sdr/C8GA20090289.md): Frame · corroded · Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Frame
  > WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT FRAME AT BS 1010 IS CRACKED BETWEEN STR 27R AND 26R. REMOVED DAMAGED AREA DIM 2.5" X 1.5" AND 1.5" X 1.5", FABRICATED REPAIR DOUBLER FROM 7075-0.071" X 7" X 28" HEAT TREATED TO T6. INSTALLED REPAIR, NO OTH
- [SDR C8GA20090288A](https://openairdocs.org/sdr/C8GA20090288A.md): Shear Tie · corroded · Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Internal Mounting Structure
  > WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT FRAME AT BS 1110 BETWEEN STR 27R AND 30 IS CORRODED. REMOVED DAMAGED AREA DIM 3.75" X.875", FABRICATED SHEAR TIE FROM 7075 T6.071" DIM 3.125" X 4. INSTALLED SHEAR TIE, NO OTHER DEFECT NOTED. ACFT WAS RET
- [SDR C8GA20090288](https://openairdocs.org/sdr/C8GA20090288.md): Stringer · corroded · Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT BS 1080-1130 27 HAS CORRODED IN CHANNEL. REMOVED DAMAGED AREA, FABRICATED NEW STR, & SPLICES. INSTALLED REPAIR PARTS, NO OTHER DEFECT NOTED. ACFT WAS RETURNED TO SERVICE.
- [SDR C8GA20090287](https://openairdocs.org/sdr/C8GA20090287.md): Fitting · corroded · Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Attach Fittings
  > WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT BS 1054-1057 27R HAS CORRODED TIE FITTING. REMOVED DAMAGED AREA, FABRICATED NEW FITTING FROM 7075 T6511DIM 8.250" X 2" INSTALLED TIE FITTING, NO OTHER DEFECT NOTED. ACFT WAS RETURNED TO SERVICE.
- [SDR C8GA20090286](https://openairdocs.org/sdr/C8GA20090286.md): Stringer · corroded · Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT BS 1050-1130 STR 27R HAS CORROSION. REMOVED DAMAGED AREA, FABRICATED NEW STR FROM BAC1498-146 7075 T62 DIM 24.625", 21", 19.750", 14.750", 14.375", 14.375", 14.375". INSTALLED REPAIRS, NO OTHER DEFECT NOTED.
- [SDR C8GA20090285](https://openairdocs.org/sdr/C8GA20090285.md): Angle · corroded · Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Miscellaneous Structure
  > WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT BS 1130 TIE CLIP IS CORRODED. FABRICATED NEW CLIP FROM 7075 T6.040" X 4" X 3.5". INSTALLED CLIP, NO OTHER DEFECT NOTED. ACFT WAS RETURNED TO SERVICE.
- [SDR C8GA20090284](https://openairdocs.org/sdr/C8GA20090284.md): Shear Tie · corroded · Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Internal Mounting Structure
  > WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT FRAME AT BS 1130 SHEAR TIE IS CORRODED BETWEEN STR 26R-29R. REMOVED DAMAGED SECTION, FABRICATED NEW SHEAR TIE. INSTALLED REPAIR, NO OTHER DEFECT NOTED. ACFT WAS RETURNED TO SERVICE.
- [SDR C8GA20090283](https://openairdocs.org/sdr/C8GA20090283.md): Frame · gouged · Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Frame
  > WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT FRAME AT BS 1090 STR 27L IS GOUGED. REMOVED DAMAGED SECTION, FABRICATED NEW FRAME FROM 7075-0 DIM.071" X 20" X 4" HEAT TREATED TO T6. INSTALLED REPAIR, NO OTHER DEFECT NOTED. ACFT WAS RETURNED TO SERVICE.
- [SDR C8GA20090282](https://openairdocs.org/sdr/C8GA20090282.md): Frame · gouged · Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Frame
  > WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT FRAME AT BS 1110 STR 27L IS GOUGED. REMOVED DAMAGED SECTION, FABRICATED REPAIR DOUBLER FROM 7075-0 DIM.071" X 10" X 6" HEAT TREATED TO T6. INSTALLED REPAIR, NO OTHER DEFECT NOTED. ACFT WAS RETURNED TO SERV
- [SDR C8GA20090281](https://openairdocs.org/sdr/C8GA20090281.md): Frame · gouged · Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Frame
  > WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT FAME AT BS 1130 STR 27L IS GOUGED. REMOVED DAMAGED SECTION, FABRICATED REPAIR DOUBLER FROM 7075-0 DIM.071" X 8.5" X 4.5" HEAT TREATED TO T6. INSTALLED REPAIR, NO OTHER DEFECT NOTED. ACFT WAS RETURNED TO SE
- [SDR C8GA20090280](https://openairdocs.org/sdr/C8GA20090280.md): Frame · corroded · Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Frame
  > WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT FAME AT BS 1110 STR 26R IS DENTED. REMOVED DAMAGED SECTION, FABRICATED REPAIR DOUBLER FROM 7075-0 DIM.071" X 5.5" X 16" HEAT TREATED TO T6. INSTALLED REPAIR, NO OTHER DEFECT NOTED. ACFT WAS RETURNED TO SER
- [SDR C8GA20090279](https://openairdocs.org/sdr/C8GA20090279.md): Frame · corroded · Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Frame
  > WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT FAME AT BS 1110 STR 27R HAS PUNCTURE. REMOVED DAMAGED SECTION, FABRICATED REPAIR DOUBLER FROM 7075-0 DIM.071" X 5.5" X 16" HEAT TREATED TO T6. INSTALLED REPAIR, NO OTHER DEFECT NOTED. ACFT WAS RETURNED TO S
- [SDR C8GA20090278](https://openairdocs.org/sdr/C8GA20090278.md): Repair · corroded · Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT BS 1130-1148 STR 30 PREVIOUS REPAIR IS CORRODED. REMOVED EXISTING REPAIR, FABRICATED NEW REPAIR FROM BAC 1498-131 7075 T6 DIN 10". INSTALLED REPAIR, NO OTHER DEFECT NOTED. ACFT WAS RETURNED TO SERVICE.
- [SDR C8GA20090277](https://openairdocs.org/sdr/C8GA20090277.md): Stringer · corroded · Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT BS 1148-1166 STR 30 PREVIOUS REPAIR IS CORRODED. REMOVED EXISTING REPAIR, FABRICATED NEW REPAIR FROM BAC 1498-131 7075 T6 DIN 10". INSTALLED REPAIR, NO OTHER DEFECT NOTED. ACFT WAS RETURNED TO SERVICE.
- [SDR C8GA20090276](https://openairdocs.org/sdr/C8GA20090276.md): Repair · punctured · Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Frame
  > WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT BS 1130 PREVIOUS REPAIR AT 27 R HAS A PUNCTURE. REMOVED PREVIOUS REPAIR AND FABRICATED NEW FROM FROM 7075-0.071" X 9.75" X 4.5" HEAT TREATED TO T6. INSTALLED REPAIR, NO OTHER DEFECTS NOTED. ACFT WAS RETUR
- [SDR C8GA20090275](https://openairdocs.org/sdr/C8GA20090275.md): Structure · cracked · Jul 31, 2009 · N89427 · Boeing 727227 · Passenger/Crew Doors
  > WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE L1 DOOR HAD AN OVER-SIZED FASTENER HOLE. REMOVED FASTENER AND EXISTING DOUBLER. TRIMMED OUT DAMAGE DIM 1.25" X 2.8" HFEC FOR CRACK CONTAINMENT. FABRICATED TIPPLER FROM 7075 T6.160" X 7" X 13", DOUBLER
- [SDR C8GA20090274](https://openairdocs.org/sdr/C8GA20090274.md): Stringer · cracked · Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED AT STA 620 STR 27R IS CORRODED. REMOVED DAMAGED SECTION DIM 18" FABRICATED NEW STR FROM BAC1498-147 7075 T62 DIM 17.75". FABRICATED 2EA SPLICES FROM BAC1498-131 7075-T6 DIM 13" X 14.5" INSTALLED REPAIR, NO OTHER
- [SDR C8GA20090273](https://openairdocs.org/sdr/C8GA20090273.md): Intercostal · cracked · Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Miscellaneous Structure
  > WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED AT STA 620 STR 24R WEB IS CRACKED. REMOVED AND FABRICATED NEW INTERCOSTAL FROM 7075-0.063" DIM 19.250" X 6" HEAT TREATED TO T6. INSTALLED INTERCOSTAL, NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.
- [SDR C8GA20090272](https://openairdocs.org/sdr/C8GA20090272.md): Intercostal · cracked · Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Miscellaneous Structure
  > WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED AT STA 620 STR 22R WEB IS CRACKED. REMOVED AND FABRICATED NEW INTERCOSTAL FROM 7075-0.063" DIM 19.250" X 5.750" HEAT TREATED TO T6. INSTALLED INTERCOSTAL, NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.
- [SDR C8GA20090271](https://openairdocs.org/sdr/C8GA20090271.md): Intercostal · cracked · Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Miscellaneous Structure
  > WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED AT STA 560, STR 23R WEB IS CRACKED. REMOVED AND FABRICATED NEW INTERCOSTAL FROM 7075-0.063" DIM 19.250" X 7" HEAT TREATED TO T6. INSTALLED INTERCOSTAL, NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.
- [SDR C8GA20090270](https://openairdocs.org/sdr/C8GA20090270.md): Intercostal · cracked · Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Miscellaneous Structure
  > WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED AT STA 560, STR 19R WEB IS CRACKED. REMOVED AND FABRICATED NEW INTERCOSTAL FROM 7075-0.063" DIM 19" X 7" HEAT TREATED TO T6. INSTALLED INTERCOSTAL, NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.
- [SDR C8GA20090269](https://openairdocs.org/sdr/C8GA20090269.md): Web · corroded · Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Miscellaneous Structure
  > WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE WEB AT BS 990 STR 27R-26R IS CORRODED. REMOVED DAMAGED SECTION DIM 1.750" X 2.5". FABRICATED FILLER FROM 7075 T6 DIM 1.750 X 2.5" AND DOUBLER FROM 7075 T6.080" 15.125" X 4.25". INSTALLED REPAIR, NO OT
- [SDR C8GA20090268](https://openairdocs.org/sdr/C8GA20090268.md): Stringer · corroded · Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT STR 27R HAS CORROSION BETWEEN BS 990-1010. FABRICATED DOUBLER FROM 7075 T6.071" 5.25" X 12.5, SHIM 7075 T6.071" X 4" X 25", SHIM 7075 T6.040X 4.5" X 15.5", ANGLE FROM 7075 T6.063" X 3"X 17.25", SHIM 7075
- [SDR C8GA20090267](https://openairdocs.org/sdr/C8GA20090267.md): Shear Tie · corroded · Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Internal Mounting Structure
  > WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE SHEAR TIE AT 970 STR 29R IS CORRODED. REMOVED DAMAGED AREA DIM 1" X 4.25". FABRICATED REPAIR DOUBLER FROM 7075-T6.071" DIM 6.375" X 6.25", ANGLE FROM 7075 T6.063" 2.25" X 5.25", ANGLE FROM 7075 T6.063"
- [SDR C8GA20090266](https://openairdocs.org/sdr/C8GA20090266.md): Intercostal · corroded · Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Miscellaneous Structure
  > WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE INTERCOSTAL AT STA 950A IS CORRODED AT STRINGER 28L. REMOVED INTERCOSTAL AND FABRICATED NEW FROM 7075 T6.040" 20" X 8" INSTALLED INTERCOSTAL, NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVICE.
- [SDR C8GA20090265](https://openairdocs.org/sdr/C8GA20090265.md): Bracket · corroded · Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Miscellaneous Structure
  > WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT STR 27L BRACKET CORRODED AT BS 950C. REMOVED BRACKET, FABRICATED NEW FROM 7075 T6.040" DIM 3.25" X 3". INSTALLED BRACKET, NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVICE.
- [SDR C8GA20090264](https://openairdocs.org/sdr/C8GA20090264.md): Intercostal · corroded · Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Miscellaneous Structure
  > WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT AT STA 950A, STR 29L THE INTERCOSTAL IS CORRODED. REMOVED DAMAGED INTERCOSTAL AND FABRICATED NEW FROM 7075 T6.040" DIM 8.875" X 19.625". INSTALLED REPAIR, NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERV
- [SDR C8GA20090263](https://openairdocs.org/sdr/C8GA20090263.md): Web · corroded · Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Miscellaneous Structure
  > WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT AT STA 560 STR 25R WEB IS CRACKED. CUT OUT DAMAGED WEB AND FABRICATED NEW FROM 7075 T6.063" DIM 29.5" X 4.5", DOUBLER SPLICE FROM 7075 T6.071" DIM 4.5" X 4.5", INBD DOUBLER SPLICE FROM 7075 T6.071" DIM 5.5
- [SDR C8GA20090262](https://openairdocs.org/sdr/C8GA20090262.md): Shear Tie · corroded · Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Internal Mounting Structure
  > WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT AT STA 970 RBL 15 TO RBL 20 LOWER FLANGE ON THE FRAME IS CORRODED. FABRICATED SHEAR TIE REPAIR FROM 7075-0.071" DIM 4" X 7" HEAT TREATED TO T6. INSTALLED REPAIR NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO
- [SDR C8GA20090261](https://openairdocs.org/sdr/C8GA20090261.md): Skin · corroded · Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Plate/Skin
  > WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT AT STA 720 BL 0 SKIN IS CORRODED. REMOVED PREVIOUS REPAIR, CUT OUT DAMAGE DIM 8.5" X 9.5. FABRICATED REPAIR DOUBLER FROM 2024 T3.071" X 16" X 18" AND 4 EACH FILLERS.75" X 14.5". INSTALLED REPAIR NO OTHER
- [SDR C8GA20090260](https://openairdocs.org/sdr/C8GA20090260.md): Stringer · corroded · Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT STR 27R STA 710 IS CORRODED. REMOVED DAMAGED SECTION OF STR AND FABRICATED NEW FROM BAC1498-144 7075 T6 DIM 20.5". INSTALLED STR, NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.
- [SDR C8GA200900259](https://openairdocs.org/sdr/C8GA200900259.md): Stringer · corroded · Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT STA 560-570, STR 27L IS CORRODED. FLOORBEAM SPLICE PLATE IS CRACKED. REMOVED DAMAGED SECTION OF STR DIM 18.25" FABRICATED NEW STR FROM BAC1498-147 DIM 18.25".090". FABRICATED 2 SPLICES 13.25" X 10" BAC 1
- [SDR C8GA200900258](https://openairdocs.org/sdr/C8GA200900258.md): Floorbeam · cracked · Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Floor Beam
  > WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT STA 660, STR 17L FLOORBEAM SPLICE PLATE IS CRACKED. REMOVED CRACKED SPLICE PLATE AND FABRICATED NEW FROM 2024 T3.125" DIM 18" X 9". INSTALLED SPLICE PLATE, NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO
- [SDR C8GA200900257](https://openairdocs.org/sdr/C8GA200900257.md): Floorbeam · cracked · Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Floor Beam
  > WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT STA 680, STR 17L FLOORBEAM IS CRACKED. REMOVED DAMAGED SECTION. HFEC FORT CONTAINMENT, FABRICATED FILLER FROM 7075 T6.090" DIM 5.5" X 7.2 AND REINSTALL SPLICE PLATE. NO OTHER DEFECTS WERE NOTED. ACFT WAS
- [SDR C8GA200900256](https://openairdocs.org/sdr/C8GA200900256.md): Failsafe · gouged · Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Structure
  > WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE FAIL SAFE IS GOUGED AT STA 540, STR 25L. FABRICATED NEW FAIL SAFE CHORD FROM BAC 1490-2763.090" DIM 8.75" X 1.75". INSTALLED CHORD, NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVICE.
- [SDR C8GA20090255](https://openairdocs.org/sdr/C8GA20090255.md): Web · cracked · Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Miscellaneous Structure
  > WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE WEB IS CRACKED AT STA 500, STR 27L. REMOVED AND REPLACE WEB, FABRICATED FROM 7075 T6.050" DIM 5.875" X 4. NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.
- [SDR C8GA20090254](https://openairdocs.org/sdr/C8GA20090254.md): Stringer · misrepaired · Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > WHILE IN HEAVY MX PERFORMING INSP STR SPLICE WAS FOUND TO BE NO-COMPLIANT AT BS 950E +5 - 969 STR 28R. REMOVED REPAIR AND FABRICATED NEW STR FROM 65-58387-2 DIM 60" FABRICATED SPLICE, INSTALLED REPAIR, NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.
- [SDR C8GA20090253](https://openairdocs.org/sdr/C8GA20090253.md): Skin · damaged · Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Plate/Skin
  > WHILE IN HEAVY MX PERFORMING DENT AND REPAIR MAPPING EXISTING EXTERNAL FUSELAGE REPAIR AT BS 1180 BETWEEN STR 19L- 20L IS NON COMPLIANT. REMOVED REPAIR AND FABRICATED NEW DOUBLER FROM 2024 T3.063" DIM 6" X 9". INSTALLED REPAIR, NO OTHER DEFECTS NOTED. ACFT WA
- [SDR C8GA20090252](https://openairdocs.org/sdr/C8GA20090252.md): Skin · damaged · Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Plate/Skin
  > WHILE IN HEAVY MX PERFORMING DENT AND REPAIR MAPPING EXISTING EXTERNAL FUSELAGE REPAIR AT BS 1151 BETWEEN STR 18L- 20L IS NON COMPLIANT. REMOVED REPAIR AND FABRICATED NEW DOUBLER FROM 2024 T3.063" DIM 13" X 13.5". INSTALLED REPAIR, NO OTHER DEFECTS NOTED.
- [SDR C8GA20090251](https://openairdocs.org/sdr/C8GA20090251.md): Stringer · corroded · Jul 31, 2009 · N89427 · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT STA 740 STR 24R HAS CORROSION. REMOVED DAMAGED SECTION DIM 11", FABRICATED NEW STR FROM BAC 1498-142 DIM 11" AND SPLICE REPAIR FROM BAC 1498-132 DIM 13.6". INSTALLED REPAIR, NO OTHER DEFECTS WERE NOTED. AC

Next page: https://openairdocs.org/deregistered/N89427-2011-09-20/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 = 'N89427' AND deregistration_id = 'N89427-2011-09-20'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N89427-2011-09-20/reports

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