# Service difficulty reports: N6827, cancelled Sep 26, 2011

A list on [N6827, cancelled Sep 26, 2011](https://openairdocs.org/deregistered/N6827-2011-09-26.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 2 · 61 reports

- [SDR GAIA05036OP](https://openairdocs.org/sdr/GAIA05036OP.md): Light · inoperative · Dec 16, 2005 · N6827 · Boeing 727223 · Emergency Lighting
  > DURING MAINTENANCE THE CREW ENTRY DOOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT. OPS CHECK GOOD. AC WAS RETURNED TO SERVICE. (K)
- [SDR GAIA05023](https://openairdocs.org/sdr/GAIA05023.md): Engine · failed · Sep 8, 2005 · N6827 · Boeing 727223 · Engine (Turbine/Turboprop)
  > DURING CRUISE, NR 2 ENGINE LOW OIL PRESSURE LIGHT CAME ON BRIGHT, NOTICED NR 2 OIL PRESSURE DROPPED RAPIDLY TO ZERO. OIL TEMPS AND QUANTITY REMAINED NORMAL. ENGINE FAILURE CHECKLIST WAS PERFORMED. N1S WIND MILLED FOR APPROXIMATELY 25 MINUTES. EMERGENCY WAS
- [SDR GAIA04075OP](https://openairdocs.org/sdr/GAIA04075OP.md): Light · inoperative · May 6, 2004 · N6827 · Boeing 727223 · Emergency Lighting
  > L-1 EMERGENCY EXIT LIGHT DIM, COCKPIT EMERGENCY EXIT LIGHT DIM. REMOVED AND REPLACED (L-1 AND COCKPIT) EMERGENCY LIGHTS. OPS CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR GAIA04048OP](https://openairdocs.org/sdr/GAIA04048OP.md): Smoke Detector · inoperative · Mar 10, 2004 · N6827 · Boeing 727223 · Smoke Detection
  > LOWER CARGO FIRE WARNING ILLUMINATED SHORTLY AFTER TAKEOFF, RETURNED TO FWA. LIGHT WENT OUT BEFORE LANDING. BITE TEST CARRIED OUT. FOUND THREE SMOKE DETECTORS WEAK IN THE AFT CARGO. REMOVED AND REPLACED THREE WEAK SMOKE DETECTORS, RESET THE SYSTEM. OPS CH
- [SDR GAIA01305OP](https://openairdocs.org/sdr/GAIA01305OP.md): Actuator · failed · Aug 31, 2001 · N6827 · Boeing 727223 · Leading Edge Slat Actuator
  > FLT - 1843 - PHL-FWA - ON APPROACH TO FWA, THE FLIGHT CREW NOTICED THAT THE NR 8 SLAT DID NOT INDICATE EXTENDED WHEN THE FLAP HANDLE WAS MOVED FROM 2 DEGREES TO THE 5 DEGREE POSITION. AN EMERGENCY WAS DECLARED AND A UNEVENTFUL LANDING WAS MADE AT FWA. REMOVE
- [SDR GAIA01291OP](https://openairdocs.org/sdr/GAIA01291OP.md): Coalescer Bag · dirty · Aug 7, 2001 · N6827 · Boeing 727223 · Humidity Control System
  > FLT 2031 - RNO-DEN - AFTER TAKEOFF, THERE WAS A STRONG ODOR OF JET FUEL IN THE COCKPIT. THIS AIRCRAFT MADE AN UNEVENTFUL RETURN TO RNO. REMOVED AND REPLACED BOTH CONDENSER BAGS. INSPECTED AND CHECKED FOR LEAKS. RAN APU AND ENGINES WITH NO LEAKS OR SMELL NO
- [SDR GAIA01257ST](https://openairdocs.org/sdr/GAIA01257ST.md): Frame · Jul 6, 2001 · N6827 · Boeing 727223 · Fuselage Structure (General)
  > DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED BS 380 FRAME HAS SEVERAL HOLES IN THE INBOARD RADIUS BETWEEN STRINGER 4-7L. ACCOMPLISHED BS 380 FRAME REPAIR STRINGER 4-7. IAW B727 SRM 53-10-4 FIG 1. FASI NON ROUTINE 08343. (M)
- [SDR GAIA01256ST](https://openairdocs.org/sdr/GAIA01256ST.md): Skin · cracked · Jul 6, 2001 · N6827 · Boeing 727223 · Wing, Plate/Skin
  > DURING A LTC INSPECTION, IT WAS DISCOVERED RIGHT WING UPPER SURFACE LEADING EDGE SKIN CRACKED IN 2 PLACES AT AFT END OF NR 6 SLAT OUTBOARD HOOK SEAL CUTOUT. (M)
- [SDR GAIA01255ST](https://openairdocs.org/sdr/GAIA01255ST.md): Skin · corroded · Jul 6, 2001 · N6827 · Boeing 727223 · Fuselage Structure (General)
  > DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED BULGING SKIN, POPPED FASTENER HEADS, CORROSION ALONG STRINGER 24L, BS 294-310. ACCOMPLISHED FUSELAGE SKIN LAP REPAIR AT BS 294-310, STRINGER 24L IAW B727 SRM 53-30-3 FIG 5. (M)
- [SDR GAIA01253ST](https://openairdocs.org/sdr/GAIA01253ST.md): Web · cracked · Jul 6, 2001 · N6827 · Boeing 727223 · Fuselage Structure (General)
  > DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED BS 178 BULKHEAD CRACKED AT RBL 2, WL 198, ALSO STIFFENERS (HORIZONTAL) ABOVE WL 200 AND BELOW WL 196 ARE CRACKED AT RBL 5. ACCOMPLISHED BS 178 BULKHEAD WEB REPAIR AND STIFFENERS REPLACEMENT WL 196-200,
- [SDR GAIA01252ST](https://openairdocs.org/sdr/GAIA01252ST.md): Web · cracked · Jul 6, 2001 · N6827 · Boeing 727223 · Fuselage Miscellaneous Structure
  > DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED RIGHT TORQUE BOX LIGHTNING HOLE AT STATION 1225 HAS A CRACK 1 INCH LONG. ACCOMPLISHED RIGHT TORQUE BOX WEB REPAIR AT BS 1225 IAW B727 SRM 51-40-2 AND SRM 53-10-2 FIG 6. (M)
- [SDR GAIA01251ST](https://openairdocs.org/sdr/GAIA01251ST.md): Frame · cracked · Jul 6, 2001 · N6827 · Boeing 727223 · Fuselage Structure (General)
  > DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED C-3 CARGO DOOR CUT OUT FORWARD OUTBOARD CHORD IS CRACKED 1.5 INCH BS 1090, STRINGER 24R. ACCOMPLISHED BS 1090 FRAME REPAIR AT STRINGER 24R IAW B727 SRM 53-10-2 FIG 5 AND SRM 51-40-3 FIG 1. (M)
- [SDR GAIA01250ST](https://openairdocs.org/sdr/GAIA01250ST.md): Web · cracked · Jul 6, 2001 · N6827 · Boeing 727223 · Fuselage Structure (General)
  > DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED BS 178 BULKHEAD WEB IS CRACKED AT APPROXIMATELY WL 218, LBL 12 (POSITION 1L PER W/C 2210). ACCOMPLISHED BS 178 BULKHEAD WEB REPAIR AT LBL 12, WL 218 (POSITION 1L) PER KHA W/C 2210. (M)
- [SDR GAIA01249ST](https://openairdocs.org/sdr/GAIA01249ST.md): Angle · cracked · Jul 6, 2001 · N6827 · Boeing 727223 · Fuselage Structure (General)
  > DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED C-2 DOOR CUT OUT FORWARD FRAME LOWER STANCHION ADAPTER ATTACH ANGLE BROKEN AT BS 950E, STRINGER 26R. ACCOMPLISHED STANCHION ADAPTER ATTACH ANGLE REPLACEMENT BS 950E, STRINGER 26R IAW B727 SRM 53-10-2 FI
- [SDR GAIA01248ST](https://openairdocs.org/sdr/GAIA01248ST.md): Skin · corroded · Jul 6, 2001 · N6827 · Boeing 727223 · Fuselage Main, Plate/Skin
  > DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED BULGING SKIN AND DISHED FASTENER HEADS AT BS 215, STRINGER 24R. ACCOMPLISHED FUSELAGE SKIN LONGITUDINAL LAP SPLICE REPAIR IAW B727 SRM 53-30-3 FIG 14. (M)
- [SDR GAIA01247ST](https://openairdocs.org/sdr/GAIA01247ST.md): Skin · cracked · Jul 6, 2001 · N6827 · Boeing 727223 · Fuselage Main, Plate/Skin
  > DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED L1 DOOR AFT UPPER CORNER FRAME IS CRACKED 1.5 INCH BS 344, STRINGER 5L-6L. ACCOMPLISHED FORWARD ENTRY DOOR UPPER CUT OUT SKIN/FRAME REPAIR IAW S/B 727-53-0186 (ACTUAL CRACK WAS IN DOOR CUTOUT SKIN/DOUBL
- [SDR GAIA01246ST](https://openairdocs.org/sdr/GAIA01246ST.md): Seat Track · Jul 6, 2001 · N6827 · Boeing 727223 · Fuselage Structure (General)
  > DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED SEAT TRACK AT BS 520-540, LBL 45.5 HAS ELONGATED HOLES. ACCOMPLISHED SEAT TRACK REPLACEMENT AT BS 480-550, LBL 45.5 IAW B727 SRM 53-10-5 FIG 1. (M)
- [SDR GAIA01237ST](https://openairdocs.org/sdr/GAIA01237ST.md): Web · corroded · Jul 6, 2001 · N6827 · Boeing 727223 · Fuselage Structure (General)
  > DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED WEB AT BS 328 LBL 45 CORRODED, FLIGHTSTAR AIRCRAFT SERVICES, INC. ACCOMPLISHED FLOORWEB REPLACEMENT BS 295-351, LBL 15-45 IAW B727 SRM 51-40-2 AND SRM 53-10-2 FIG 2. (M)
- [SDR GAIA01236ST](https://openairdocs.org/sdr/GAIA01236ST.md): Web · cracked · Jul 6, 2001 · N6827 · Boeing 727223 · Fuselage Structure (General)
  > DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED BS 620 FRAME FORWARD WEB CRACKED THROUGH SEAL RETAINER FASTENER HOLES ABOVE STRINGER 25 RT. ACCOMPLISHED BS 620 FRAME WEB REPAIR AT STRINGER 2R IAW B727 SRM 51-40-2 FIG 1 AND SRM 53-10-2 FIG 3. (M)
- [SDR GAIA01235ST](https://openairdocs.org/sdr/GAIA01235ST.md): Angle · cracked · Jul 6, 2001 · N6827 · Boeing 727223 · Fuselage Structure (General)
  > DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED IN THE AFT AIRSTAIR, THE LOWER TORQUE BOX TO BS 1342 LOWER SPANWISE CHORD STIFFENER ATTACH ANGLE IS CRACKED AT BS 1338, RBL 20, WL 200. ACCOMPLISHED STIFFENER ATTACH ANGLE REPLACEMENT BS 1338, RBL 20, W
- [SDR GAIA01234ST](https://openairdocs.org/sdr/GAIA01234ST.md): Stringer · cracked · Jul 6, 2001 · N6827 · Boeing 727223 · Fuselage Structure (General)
  > DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED STRINGER 15L CRACKED AT FORWARD END OF LEFT WING SCANNING LIGHT BS 720B PLUS 5. ACCOMPLISHED STRINGER 15L REPAIR AT BS 720B PLUS 5 IAW B727 SRM 53-10-3 FIG 5. (M)
- [SDR GAIA01233ST](https://openairdocs.org/sdr/GAIA01233ST.md): Stringer · cracked · Jul 6, 2001 · N6827 · Boeing 727223 · Fuselage Structure (General)
  > DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED STRINGER 15L CRAKED AT AFT END OF LEFT WING SCANNING LIGHT BS 720B PLUS 15. ACCOMPLISHED STRINGER 15L REPAIR AT BS 720B PLUS 15 IAW B727 SRM 53-10-3 FIG 5. (M)
- [SDR GAIA01232ST](https://openairdocs.org/sdr/GAIA01232ST.md): Frame · dented · Jul 6, 2001 · N6827 · Boeing 727223 · Fuselage Structure (General)
  > DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED BS 720 FRAME DENTED IN RADIUS BETWEEN STRINER 16-17 LEFT. ACCOMPLISHED BS 720 FRAME REPAIR AT STRINER 16-17L IAW B727 SRM 53-10-2 FIG 3 AND SRM 51-40-3 FIG 1. (M)
- [SDR GAIA01231ST](https://openairdocs.org/sdr/GAIA01231ST.md): Stringer · cracked · Jul 6, 2001 · N6827 · Boeing 727223 · Fuselage Structure (General)
  > DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED STRINGER 15R CRACKED AT FORWARD END OF WING SCANNING LIGHT CUT OUT BS 720B PLUS 5. ACCOMPLISHED STRINGER 15R REPAIR AT BS 720B PLUS 5 IAW B727 SRM 53-10-2 FIG 5. (M)
- [SDR GAIA01230ST](https://openairdocs.org/sdr/GAIA01230ST.md): Frame · dented · Jul 6, 2001 · N6827 · Boeing 727223 · Fuselage Structure (General)
  > DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED IN AFT CARGO FRAME BS 1110 HAS A DENT AT STRINGER 26L. ACCOMPLISHED BS 1110 FRAME REPAIR AT STRINGER 26L IAW B727 SRM 51-40-3 FIG 1 AND SRM 53-40-2 FIG 5. (M)
- [SDR GAIA01229ST](https://openairdocs.org/sdr/GAIA01229ST.md): Frame · dented · Jul 6, 2001 · N6827 · Boeing 727223 · Fuselage Structure (General)
  > DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED IN FORWARD CARGO FRAME BS 720 HAD A DENT BELOW STRINGER 25R. ACCOMPLISHED BS 720 FRAME REPAIR AT STRINGER 25R IAW B27 SRM 51-40-3 FIG 1 AND SRM 53-10-2 FIG 3. (M)
- [SDR GAIA01228ST](https://openairdocs.org/sdr/GAIA01228ST.md): Frame · dented · Jul 6, 2001 · N6827 · Boeing 727223 · Fuselage Structure (General)
  > DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED IN FORWARD CARGO FRAME BS 720 HAS 2 DENTS AT STRINGER 25L. ACCOMPLISHED BS 720 FRAME REPAIR AT STRINGER 25L IAW B727 SRM 51-40-3 FIG 1 AND SRM 53-10-2 FIG 3. (M)
- [SDR GAIA01227ST](https://openairdocs.org/sdr/GAIA01227ST.md): Frame · dented · Jul 6, 2001 · N6827 · Boeing 727223 · Fuselage Main, Frame
  > DURING A LTC INSPECTION, IT WAS DISCOVERED IN FORWARD CARGO FRAME BS 700 HAS 2 DENTS AT STRINGER 25L AND 24L. ACCOMPLISHED BS 700 FRAME REPAIR AT STRINGER 25L AND 24L IAW B727 SRM 51-40-4 FIG 1 AND SRM 53-10-2 FIG 3. (M)
- [SDR GAIA01226ST](https://openairdocs.org/sdr/GAIA01226ST.md): Floorbeam · corroded · Jul 6, 2001 · N6827 · Boeing 727223 · Fuselage Main, Floor Beam
  > DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED IN DOG HOUSE AREA, FLOORBEAM T-CAP IS CORRODED AT BS 312 LBL 3. ACCOMPLISHED BS 312 FLOORBEAM UPPER CHORD REPAIR AT LBL 3 IAW B727 SRM 53-10-2 FIG 7 AND SRM 51-40-3 FIG 1. (M)
- [SDR GAIA01225ST](https://openairdocs.org/sdr/GAIA01225ST.md): Bulkhead · cracked · Jul 6, 2001 · N6827 · Boeing 727223 · Fuselage Main, Bulkhead
  > DURING A LTC INSPECTION, IT WAS DISCOVERED IN 2 CRACKS AT FASTENER LOCATIONS BS 178, RBL 10, WL 235. ACCOMPLISHED BS 178 BULKHEAD WEB REPAIR AT RBL 10, WL 235 IAW B727 SRM 53-10-9 FIG 4. (M)
- [SDR GAIA01224ST](https://openairdocs.org/sdr/GAIA01224ST.md): Skin · cracked · Jul 6, 2001 · N6827 · Boeing 727223 · Wing, Plate/Skin
  > DURING A LTC INSPECTION, IT WAS DISCOVERED RIGHT WING LEADING EDGE CAVITY LOWER SKIN CRACKED. ACCOMPLISHED RIGHT WING LEADING EDGE LOWER SKIN REPAIR AT WS 474 IAW B727 SRM 57-30-4 FIG 1. (M)
- [SDR GAIA01223ST](https://openairdocs.org/sdr/GAIA01223ST.md): Angle · cracked · Jul 6, 2001 · N6827 · Boeing 727223 · Wing Structure
  > DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED RIGHT WING LEADING EDGE CAVITY UPPER ATTACH ANGLE CRACKED AT SLAT STATION.260, WL 343. ACCOMPLISHED RIGHT WING LEADING EDGE CAVITY UPPER ATTACH ANGLE REPLACEMENT WS 343, SLAT STATION.260 IAW B727 SRM
- [SDR GAIA01222ST](https://openairdocs.org/sdr/GAIA01222ST.md): Skin · cracked · Jul 6, 2001 · N6827 · Boeing 727223 · Wing, Plate/Skin
  > DURING A LTC INSPECTION,IT WAS DISCOVERED LEFT WING INBOARD INTERNAL LEADING EDGE SKIN, ACCESS THROUGH PANEL 6301, L/E STATION 130.5 IS CRACKED AROUND SEVERAL FASTENERS. ACCOMPLISHED LEFT WING INBOARD INTERNAL LEADING EDGE SKIN CRACK REPAIR AT WS 130.5 IAW B
- [SDR GAIA01221ST](https://openairdocs.org/sdr/GAIA01221ST.md): Pressure Panel · cracked · Jul 6, 2001 · N6827 · Boeing 727223 · Fuselage Main, Bulkhead
  > DURING A LTC INSPECTION, IT WAS DISCOVERED LEFT MAIN WHEEL WELL PRESSURE WEB IS CRACKED AT BS 948, LBL 65, WL 200. ACCOMPLISHED LEFT MAIN WHEEL WELL PRESSURE DECK CRACK REPAIR AT BS 948, LBL 65, WL 200 IAW BOEING DRAWING 65-89360. (M)
- [SDR GAIA01220ST](https://openairdocs.org/sdr/GAIA01220ST.md): Pressure Panel · cracked · Jul 6, 2001 · N6827 · Boeing 727223 · Fuselage Main, Bulkhead
  > DURING A LTC INSPECTION, IT WAS DISCOVERED RIGHT MAIN WHEEL WELL PRESSURE WEB IS CRACKED AT BS 948, RBL 65, WL 200. ACCOMPLISHED RIGHT MAIN WHEEL WELL PRESSURE DECK CRACK REPAIR AT BS 948, RBL 65, WL 200 IAW BOEING DRAWING 65-89360. (M)
- [SDR GAIA01219ST](https://openairdocs.org/sdr/GAIA01219ST.md): Pressure Panel · cracked · Jul 6, 2001 · N6827 · Boeing 727223 · Fuselage Main, Bulkhead
  > DURING A LTC INSPECTION,DISCOVERED 2 CRACKS IN NWW CEILING RECESSED WEB AT BS 285, RBL 4-8 AND BS 290, BL 0. ACCOMPLISHED NOSE WHEEL WELL RECESSED CEILING WEB CRACK REPAIR AT BS 285-290, BL 0 RBL 8 IAW B727 SRM 51-40-2 FIG 1 AND SRM 53-10-2 FIG 2. (M)
- [SDR GAIA01218ST](https://openairdocs.org/sdr/GAIA01218ST.md): Pressure Panel · cracked · Jul 6, 2001 · N6827 · Boeing 727223 · Fuselage Main, Bulkhead
  > DURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE NLG WW LEFT WEB IS CRACKED HORIZONTALLY AT BS 240-250, WL 180. ACCOMPLISHED LEFT NOSE WHEEL WELL WEB CRACK REPAIR AT BS 240-250, WL 180 IAW B727 SRM 51-40-2 FIG 1 AND SRM 53-10-2 FIG 2. (M)
- [SDR GAIA01217ST](https://openairdocs.org/sdr/GAIA01217ST.md): Skin · cracked · Jul 6, 2001 · N6827 · Boeing 727223 · Doors
  > DURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED C-3 DOOR SKIN CRACKED AT OUTER HANDLE COVER PLATE BS 1125 BETWEEN STRINGER 23-24 RIGHT, FILGHT STAR AIRCRAFT SERVICES, INC. ACCOMPLISHED NR 3 CARGO DOOR SKIN REPAIR AT BS 1125, STRINGER 23-24R IAW B727
- [SDR GAIA01254ST](https://openairdocs.org/sdr/GAIA01254ST.md): Web · cracked · Jul 1, 2001 · N6827 · Boeing 727223 · Fuselage Structure (General)
  > DURING A LTC INSPECTION AT FLIGHTSTAR, IT WS DISCOVERED VERTICAL CRACK NOSE WHEEL WELL LEFT WEB BS 260, WL 160. ACCOMPLISHED WEB REPAIR BS 260, WL 160 IN LEFT NWW IAW B727 SRM 51-40-2 FIG 1 AND SRM 53-10-2 FIG 2. (M)
- [SDR GAIA01239ST](https://openairdocs.org/sdr/GAIA01239ST.md): Floorbeam · corroded · May 21, 2001 · N6827 · Boeing 727223 · Fuselage Main, Floor Beam
  > DURING A ROUTINE MAINTENANCE INSPECTION, IT WAS DISCOVERED THAT THE FLOORBEAM AT BS 1030, RBL 34.5 WAS CORRODED OUT OF LIMITS. REPAIRED FLOORBEAM AT BS 1030, RBL 34.5 IAW BOEING 727 SRM 53-10-8, FIGURE 3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA01110OP](https://openairdocs.org/sdr/GAIA01110OP.md): Gcu · faulty · Mar 9, 2001 · N6827 · Boeing 727223 · AC Regulator
  > FLT 2019 - ABQ-PHX, NO CLIMB-OUT, SHORTLY AFTER FLAP RETRACTION, EXPERIENCED DIFFERENTIAL FAULT IN NR 2 SYSTEM IN COMBINATION WITH ESSENTIAL POWER LOSS AND OVER EXCITATION IN SYSTEMS 1 AND 3, WHICH RESULTED IN THE LOSS OF THE SYNCHRONIZING BUS. AIRCRAFT MADE
- [SDR GAIA01108OP](https://openairdocs.org/sdr/GAIA01108OP.md): Generator · malfunctioned · Mar 6, 2001 · N6827 · Boeing 727223 · AC Generator-Alternator
  > FLT 2071 - GEG-PHX - AFTER TAKEOFF, LOSS OF ALL GENERATORS OCCURRED. AIRCRAFT MADE AN UNEVENTFUL LANDING IN GEG. RAN ENGINES AND GENERATORS. LOADED GENERATORS UP ELECTRICALLY, HYDRAULICALLY AND PNEUMATICALLY. RAN FOR 15 MINUTES WITH NO DEFECTS NOTED, PER B
- [SDR GAIA01075OP](https://openairdocs.org/sdr/GAIA01075OP.md): Clamp · leaking · Feb 23, 2001 · N6827 · Boeing 727223 · Engine Bleed Air System
  > FLT 2507 - GEG-IND - AT 1000 FEET AGL, ENGINE AND WING HEAT OPENED. ONE MINUTE LATER NR 1 STRUT OVER HEAT LIGHT ILLUMINATED AS A/C CLIMBED THROUGH CLOUDS INTO CLEAR. ALL ANTI-ICE SYSTEMS CLOSED AND STRUT OVER HEAT LIGHT EXTINGUISHED. NORMAL CONDITIONS THROU
- [SDR GAIA01014](https://openairdocs.org/sdr/GAIA01014.md): Light · intermittent · Jan 24, 2001 · N6827 · Boeing 727223 · Overheat Detection
  > FLT 1777 - BOS-FWA - LOWER AFT BODY HEAT LIGHT INTERMITTENT TEST. PTT WORKS GOOD. AIRCRAFT MADE AN UNEVENTFUL LANDING IN FWA. REPLACED AFT BODY OVERHEAT LAMP. OPS CHECKS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA00793](https://openairdocs.org/sdr/GAIA00793.md): Light · inoperative · Dec 22, 2000 · N6827 · Boeing 727223 · Emergency Lighting
  > MAINTENANCE ONLY, MHR, EMERGENCY EXIT LIGHT IN COCKPIT DOES NOT ILLUMINATE.REMOVED AND REPLACED COCKPIT EMERGENCY EXIT LIGHT. SYSTEM OPERATIONALLY CKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR GAIA00721](https://openairdocs.org/sdr/GAIA00721.md): Handle · stuck · Nov 27, 2000 · N6827 · Boeing 727223 · Trailing Edge Flap Control System
  > FLT 8106 - SEA-ANC - ON APPROACH, FLAP HANDLE WOULDN'T MOVE. AIRCRAFT MADE AN UNEVENTFUL ZERO FLAP LANDING IN ANC. CANNOT DUPLICATE PROBLEM ON GROUND. FLAP SYSTEM CHECK GOOD PER BAC B727 MM, 27-51-0, THROUGH NUMEROUS CYCLES. LUBED CABLES AND FLAP CONTROL V
- [SDR GAIA9931](https://openairdocs.org/sdr/GAIA9931.md): Bulb · failed · Mar 3, 1999 · N6827 · Boeing 727223 · Smoke Detection
  > EN ROUTE FROM YIP TO HUF, THE CARGO SMOKE LIGHT ILLUMINATED. THE FLIGHT CREW FOLLOWED EMERGENCY CHECKLIST PROCEDURES. THERE WAS NO SMOKE OR SMELL INTHE COCKPIT OR THE CARGO COMPARTMENT. LIGHT EXTINGUISHED 15 MINUTES LATER. ALL TEST WERE GOOD. THE AIRCRAFT
- [SDR GAIA9857A](https://openairdocs.org/sdr/GAIA9857A.md): Seal · worn · May 27, 1998 · N6827 · Boeing 727223 · Turbine Engine Oil System
  > DFW - AFTER DEPARTING, NR 2 ENGINE OIL PRESSURE LOW, (LOSS OF PRESSURE). ENGINE SHUT DOWN. AIRCRAFT MADE AN UNEVENTFUL RETURN TO DFW. INSPECTED ENGINE WITH NO DEFECTS NOTED. NO DEFECTS NOTED IN OIL SCREEN. GARLOCK SEAL FOR STARTER REPLACED FOR OIL QUANTIT
- [SDR GAIA9838](https://openairdocs.org/sdr/GAIA9838.md): Light · inoperative · Apr 8, 1998 · N6827 · Boeing 727223 · Emergency Lighting
  > DURING MAINTENANCE AT OKC, FOUND EMERGENCY LIGHT ABOVE L-1 DOOR FAILED TO ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY. SYSTEM OPERATIONALLY CHECKS GOOD. (M)
- [SDR GAIA9809](https://openairdocs.org/sdr/GAIA9809.md): Light · inoperative · Feb 6, 1998 · N6827 · Boeing 727223 · Emergency Lighting
  > UPON ARRIVAL TOL, CREW REPORTS EMERGENCY EXIT LIGHT OVER L-1 DOOR INOP. REMOVED AND REPLACED EXIT LIGHT IAW MM ATA 33-50. SYSTEM CHECK NORMAL ON GROUND. AIRCRAFT RETURNED TO SERVICE. (M)

Next page: https://openairdocs.org/deregistered/N6827-2011-09-26/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 = 'N6827' AND deregistration_id = 'N6827-2011-09-26'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N6827-2011-09-26/reports

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