# Service difficulty reports: N264FE, cancelled Aug 10, 2015

A list on [N264FE, cancelled Aug 10, 2015](https://openairdocs.org/deregistered/N264FE-2015-08-10.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 · 122 reports

- [SDR FDEA201203201029](https://openairdocs.org/sdr/FDEA201203201029.md): Bracket · loose · Mar 20, 2012 · N264FE · Boeing 727233 · Emergency Equipment
  > ESCAPE SLIDE GIRT BAR IS VERY LOOSE AND DOES NOT STAY SECURELY IN THE BRACKET. REMOVED SLIDE, REPLACED GIRT BAR BRACKET AND REINSTALLED SLIDE IAW AMM 25-60-015-2-0. FINAL CLOSED.
- [SDR FDEA201203130941](https://openairdocs.org/sdr/FDEA201203130941.md): Wire · burned · Mar 13, 2012 · N264FE · Boeing 727233 · Ice/Rain Protection System Wiring
  > L2 WINDOW (CAPT SIDE) WIRE TO CONNECTOR SMOLDERED, CAUGHT ON FIRE, & MELTED. CIRCUIT BREAKER DID NOT TRIP. REMOVED L2 WINDOW AND REPLACED WIRE FROM WINDOW TO CONNECTOR D9489P. REINSTALLED WINDOW AND WINDOW HEAT OPS NORMAL IAW MM 30-41-032-4 AND WDM 30-41-1
- [SDR FDEA201202180612](https://openairdocs.org/sdr/FDEA201202180612.md): Windshield · cracked · Feb 18, 2012 · N264FE · Boeing 727233 · Flight Compartment Windows
  > R1 WINDSHIELD CRACKED. R & R R1 WINDOW IAW MM 56-11-011-4. CHECKED GOOD.
- [SDR FDEA201104271650](https://openairdocs.org/sdr/FDEA201104271650.md): Controller · malfunctioned · Apr 27, 2011 · N264FE · Boeing 727233 · Cabin Pressure Controller
  > COULD NOT MAINTAIN PRESSURIZATION IN STANDBY OR MANUAL MODE S AFTER TAKE OFF. UPON ARRIVAL CREW REPORTED PRESSURE COULD NOT BE CONTROLLED IN ANY MODE. THE OUTFLOW VALVE INDICATION WAS VERY ERRATIC. PERFORMED TEST ON PRESSURE CONTROLLER AND TEST FAILED SEV
- [SDR FDEA201104161505](https://openairdocs.org/sdr/FDEA201104161505.md): Wire · damaged · Apr 16, 2011 · N264FE · Boeing 727233 · Flight Control System Wiring
  > ON CLIMBOUT, FLAPS WOULD NOT RETRACT PAST THE "2" POSITION. RAN THE QRH AND FOUND NR 8 SLAT WAS STILL OUT. IAW QRH, PLACED THE FLAPS AT "5" AND RETURNED TO DEPARTURE. UPON TROUBLESHOOTING, DETERMINED THAT NR 1 SLAT WAS SHOWING "GREEN" AND DOWN AT FLAPS "2"
- [SDR FDEA201104071388](https://openairdocs.org/sdr/FDEA201104071388.md): Actuator · failed · Apr 7, 2011 · N264FE · Boeing 727233 · Leading Edge Slat Actuator
  > NR 1 LED FAILED TO RETRACT ON FLAP RETRACTION. REF 27-82-000-1 NR 1 SLAT HAS L/E JUMPER CABLE INSTALLED REF AMM 27-82-000-1 C/0473391. INSTALLED JUMPER ADAPTER ON NR 1 SLAT IAW MM 27-82-000-1. OPS CHECKED FLAP/SLAT SYSTEM PER MM 27-81-000-5 SYSTEM OPS.
- [SDR FDEA200912244513](https://openairdocs.org/sdr/FDEA200912244513.md): Actuator · failed · Dec 24, 2009 · N264FE · Boeing 727233 · Trailing Edge Flap Actuator
  > ON FLAP RETRACTION FROM 5 TO 2 DEGREE THE NR 5 SLAT WOULD NOT RETRACT. THE OTBD AND INBD FLAP NEEDLES TRAVEL FURTHER INTO THE WHITE BAND WHEN OPS TESTED ON THE GROUND. AIRPLANE FLEW WITH NO SIGNIFICANT ROLL. REPLACED NR 5 SLAT ACTUATOR REF AMM 27-81-032-4.
- [SDR FDEA200912104399](https://openairdocs.org/sdr/FDEA200912104399.md): Door Frame · damaged · Dec 10, 2009 · N264FE · Boeing 727233 · Fuselage Main, Structure
  > FWD ENTRY DOOR FRAME STA 303.9 WEB CUT-OUT AT STR 15L HAS TOOLING MARK ON INBD EDGE. TRIMMED OUT GOUGE AREA AND INCREASED CORNER RADIUS, TREATED AND PRIMED IAW EA NR 7-5310-135516.
- [SDR FDEA200912094415](https://openairdocs.org/sdr/FDEA200912094415.md): Skin · cracked · Dec 9, 2009 · N264FE · Boeing 727233 · Emergency Exits
  > RT FWD OVERWING HATCH UPPER EDGE EXT SKIN IS BENT OUT AND CRACKED AT FASTENER. STOP DRILLED CRACK IAW IAW SRM 52-00-3 FIG 4. FABRICATED NEW DOUBLER IAW SRM 52-00-3 FIG4. TREATED AND PRIMED DOUBLER IAW SRM 51-10-2. INSTALLED DOUBLER ON RT FWD OVERWING HATC
- [SDR FDEA200912094393](https://openairdocs.org/sdr/FDEA200912094393.md): Seat Track · corroded · Dec 9, 2009 · N264FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > SURFACE CORROSION ON SEAT TRACK INBD FLANGE BETWEEN BS 1130 TO BS 1110 RBL 45. REMOVED DAMAGED SEAT TRACK, FABRICATED NEW SEAT TRACK SECTION & INSTALLED NEW SEAT TRACK FROM BS 1010 - 1130 RBL 45 IAW SRM 53-10-1 FIG 3, SRM 51-30-2 & SRM 51-10-2 & SRM 53-10-5
- [SDR FDEA200912094391](https://openairdocs.org/sdr/FDEA200912094391.md): Shear Tie · corroded · Dec 9, 2009 · N264FE · Boeing 727233 · Fuselage Internal Mounting Structure
  > FWD PIT- CORROSION ON SHEAR TIE AT BS 720A AFT SIDE BETWEEN STRINGERS 28R AND 27R. CUT-OUT DAMAGED AREA OF SHEAR TIE. FABRICATED SHEAR TIE REPAIR AND INSTALLED SHEAR TIE REPAIR IAW SRM 53-10-4, FIG 15, REV 101 AND SRM 51-30-2.
- [SDR FDEA200912084384](https://openairdocs.org/sdr/FDEA200912084384.md): Skin · damaged · Dec 8, 2009 · N264FE · Boeing 727233 · Elevator, Plate/Skin
  > LT ELEVATOR OTBD LWR SKIN DAMAGED AT STATIC WICK BASE, ELEV STA 215. FABRICATED DOUBLER REPAIR ON LT ELEVATOR OTBD LOWER SKIN AT STATIC WICK BASE IAW SRM 55-20-3, INSTALLED REPAIR PARTS, DOUBLER AND FILLER IAW SRM 51-30-2, REV 101.
- [SDR FDEA200912044361](https://openairdocs.org/sdr/FDEA200912044361.md): Seat Track · corroded · Dec 4, 2009 · N264FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK FLANGES RBL 24 BETWEEN BS 1130 TO BS 1183. REMOVED SECTION OF SEAT TRACK IAW SRM 51-30-2, REV 101, FABRICATED NEW SEAT TRACK SECTION IAW DWG 53FX976, LOCATED AND DRILLED NEW SEAT TRACK IAW SRM 51-30-5 AND DWG 53FX976, TREATED AND PRI
- [SDR FDEA200912044360](https://openairdocs.org/sdr/FDEA200912044360.md): Skin · chafed · Dec 4, 2009 · N264FE · Boeing 727233 · Trailing Edge Flaps
  > RT WING INBD FOREFLAP CHAFING UNDER NR 9 SPOILER PANEL WS 265 REMOVED DAMAGED AREA (7 1/2" X 5") SANDED, CLEANED AND PREPPED AREA IAW REV 102 SRM 51-40-20 PARAGRAPH NR 7. REPAIRED RT WING INBD FOREFLAP UPPER SURFACE BY HOT-BONDING REPAIR ON IAW SRM 51-40-20
- [SDR FDEA200912044354](https://openairdocs.org/sdr/FDEA200912044354.md): Stringer · corroded · Dec 4, 2009 · N264FE · Boeing 727233 · Fuselage Main, Longeron/Stringer
  > FWD PIT BS 710-720A 10 INCHES STR 26R CORRODED. CUT-OUT DAMAGED AREA, FABRICATED STRINGER REPAIR IN 2 SECTIONS, ONE FROM BS 700, 10 TO BS 720, 10 STR 26R, 2 FROM BS 720, 10 TO BS 720A, 8 STR 26R, FABRICATED 2 STRINGER SPLICES REPAIR (1), INSTALLED STRINGER RE
- [SDR FDEA200912034352](https://openairdocs.org/sdr/FDEA200912034352.md): Frame · corroded · Dec 3, 2009 · N264FE · Boeing 727233 · Fuselage Main, Frame
  > SURFACE CORROSION, AFT PIT AT BS 1010 FRAME, 2 EACH PLACES ABOVE STR 27R. CUT-OUT DAMAGED AREA FABRICATED FRAME REPAIR ANGLE AND INSTALLED REPAIR ANGLE AT BS 1010 ABOVE 27R IAW SRM 51-40-3, FIG 1, SRM 51-10-6, SRM 51-30-2, SRM 51-40-2, AND SRM 53-10-1, FIG 1.
- [SDR FDEA200912034348](https://openairdocs.org/sdr/FDEA200912034348.md): Frame · corroded · Dec 3, 2009 · N264FE · Boeing 727233 · Fuselage Main, Frame
  > AFT PIT, UPPER SURFACE OF FRAME IS CORRODED AT BS 1142.7, STR 28R. CUT OUT DAMAGED AREA, FABRICATED FRAME REPAIR CHANNEL AND INSTALLED NEW REPAIR CHANNEL AT BS 1142.7 STR 28R IAW SRM 51-10-6, SRM 51-30-5, SRM 51-30-2 AND EA 7-5310-135514.
- [SDR FDEA200912024331](https://openairdocs.org/sdr/FDEA200912024331.md): Frame · corroded · Dec 2, 2009 · N264FE · Boeing 727233 · Fuselage Main, Frame
  > SURFACE CORROSION, AFT PIT AT BS 1030, 2 EACH PLACES ON FRAME, ABOVE STR 27R. REMOVED CORROSION FROM BS 1030 FRAME ABOVE STR 27R, ORIGINAL THICKNESS.063", MATERIAL LOSS.002", MATERIAL REMAINING.061", FOUND MATERIAL LOSS TO BE WITHIN LIMITS, TREATED AND PRI
- [SDR FDEA200912024330](https://openairdocs.org/sdr/FDEA200912024330.md): Frame · corroded · Dec 2, 2009 · N264FE · Boeing 727233 · Fuselage Main, Frame
  > AFT PIT, UPPER SURFACE OF FRAME IS CORRODED AT BS 1110, OTBD OF STR 27R. REMOVED CORROSION FROM FRAME AT BS 1110 O/B OF STR 27R, ORIGINAL THICKNESS.063", MATERIAL LOSS.007", MATERIAL REMAINING.056", FOUND MATERIAL LOSS TO BE WITHIN LIMITS, TREATED AND PRI
- [SDR FDEA200912024329](https://openairdocs.org/sdr/FDEA200912024329.md): Skin · corroded · Dec 2, 2009 · N264FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > SURFACE CORROSION AFT PIT ON SKIN SURFACE AT BS 1010 STR 28L. CUT-OUT DAMAGED AREA APPROX DIM: 3 7/8" X 1", FABRICATED REPAIR DOUBLER AND INSTALLED REPAIR DOUBLER IAW SRM 51-10-6, SRM 53-30-1 FIG 1, SRM 51-10-2 AND SRM 53-30-3 FIG 3A.
- [SDR FDEA200912024325](https://openairdocs.org/sdr/FDEA200912024325.md): Skin · corroded · Dec 2, 2009 · N264FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > FWD PIT BS 710 STR 27R LAP SEAM INNER SKIN CORRODED. CUT-OUT DAMAGED AREA OF SKIN, FABRICATED DOUBLER REPAIR AND FILLERS, INSTALLED DOUBLER AND FILLERS IAW SRM 53-30-3 FIG 5 AND SRM 51-30-2.
- [SDR FDEA200912024324](https://openairdocs.org/sdr/FDEA200912024324.md): Skin · cracked · Dec 2, 2009 · N264FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > FWD ENTRY DOOR FRAME BS 303.9 WEB CUT-OUT AT STR 16L HAS A CRACK AT OTBD LWR CORNER. STOP DRILLED CRACK UP TO.250" DIA, FABRICATED REPAIR REINFORCEMENT ANGLE AND INSTALLED REPAIR ANGLE AT BS 303.9 STR 16L IAW EO 7-5310-7-3362 AND DWG NR 65C38447, SRM 51-30-2
- [SDR FDEA200911304273](https://openairdocs.org/sdr/FDEA200911304273.md): Angle · cracked · Nov 30, 2009 · N264FE · Boeing 727233 · Leading Edge Devices
  > NR 1 SLAT T/E CHORD ANGLE CRACKED AT INBD UPSTOP PAD, APPROX SLAT STA 348. CUT-OUT CRACKED SECTION OF NR1 SLAT T/E CHORD ANGLE 25 3/4" LONG IAW SRM REV 101, 51-10-1. FABRICATED CHORD ANGLE SECTION AND SPLICE IAW SRM 51-40-4 AND 57-50-2. INSTALLED ANGLE AND S
- [SDR FDEA200911304272](https://openairdocs.org/sdr/FDEA200911304272.md): Shear Tie · corroded · Nov 30, 2009 · N264FE · Boeing 727233 · Fuselage Internal Mounting Structure
  > FWD PIT- CORROSION ON SHEAR TIE AT BS 720C, AFT SIDE OF FRAME, BL0. REMOVED SHEAR TIE ANGLE AT BS 720C AFT SIDE OF FRAME IAW SRM REV 101 51-30-2. FABRICATED NEW SHEAR TIE ANGLE IAW SRM 51-20-1 AND 51-30-5. INSTALLED NEW SHEAR TIE ANGLE IAW SRM 51-30-2.
- [SDR FDEA200911304269](https://openairdocs.org/sdr/FDEA200911304269.md): Skin · corroded · Nov 30, 2009 · N264FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > FWD PIT-SKIN CORRODED AT BS 720C, AFT SIDE OF FRAME, OTBD OF STRINGER 27R. CUT OUT SKIN AT BS 720C IAW SRM 51-10-6 REV 101, FABRICATED REPAIR DOUBLER IAW SRM 53-30-3, FIG 3, INSTALLED DOUBLER AND FILLER IAW SRM 51-30-2, REV 101.
- [SDR FDEA200911304268](https://openairdocs.org/sdr/FDEA200911304268.md): Stringer · corroded · Nov 30, 2009 · N264FE · Boeing 727233 · Fuselage Main, Longeron/Stringer
  > FWD PIT-OTBD SIDE OF OF STR 27R IS CORRODED AT BS 720C, AFT SIDE OF FRAME. REMOVED CORROSION IAW SRM 51-10-6 REV 101, ORIGINAL THICKNESS.100", MATERIAL REMOVED.003", MATERIAL REMAINING.097" WITHIN LIMITS IAW SRM 53-10-1, TREATED AND PRIMED STR 27R AFT
- [SDR FDEA200911284270](https://openairdocs.org/sdr/FDEA200911284270.md): Stringer · corroded · Nov 28, 2009 · N264FE · Boeing 727233 · Fuselage Main, Longeron/Stringer
  > SURFACE CORROSION, AFT PIT INSIDE STR 29L CHANNEL BS 1166. CUT-OUT DAMAGED AREA, FABRICATED STR REPAIR FILLER, FABRICATED REPAIR SPLICE FROM AND INSTALLED REPAIR PARTS AT BS 1106 STR 29L IAW SRM 53-10-3 FIG 1 AND SRM 51-30-2.
- [SDR FDEA200911274276](https://openairdocs.org/sdr/FDEA200911274276.md): Angle · corroded · Nov 27, 2009 · N264FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > C-2 DOOR CUT OUT AFT FRAME BS 990, INNER CHORD ANGLE IS CORRODED ON UPPER FLANGE LWR SURFACE BTWN STR 27R-26R. CUT OUT DAMAGED AREA, FABRICATED FRAME REPAIR ANGLE AND FILLER, AND INSTALLED NEW FRAME ANGLE REPAIR AND FILLER AT C-2 DOOR FRAME BS 990 BETWEEN S
- [SDR FDEA200911274275](https://openairdocs.org/sdr/FDEA200911274275.md): Angle · corroded · Nov 27, 2009 · N264FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > C-2 DOOR CUT OUT FWD FRAME BS 950E, INNER CHORD ANGLE IS CORRODED ON UPPER FLANGE LWR SURFACE BTWN STR 27R-26R. REMOVED DAMAGED AREA, FABRICATED NEW ANGLE REPAIR, FILLER, AND INTERCOSTAL; INSTALLED REPAIR PARTS AT BS 950E INNER CHORD ANGLE BETWEEN STR 27R - S
- [SDR FDEA200911274274](https://openairdocs.org/sdr/FDEA200911274274.md): Doubler · cracked · Nov 27, 2009 · N264FE · Boeing 727233 · Passenger/Crew Doors
  > CRACK DOUBLER AT RADIUS UPPER HINGE EXTERIOR SKIN L-1 DOOR. REMOVED CRACK, MADE SKIN CUTOUT, FABRICATED NEW REPAIR DOUBLER, FILLER, AND STRUCTURAL FILLER AND INSTALLED NEW REPAIR PARTS AT L1 DOOR CUT-OUT SKIN IAW EA NR 7-5330-135518, SRM 51-30-2, SRM 51-10-2
- [SDR FDEA200911274271](https://openairdocs.org/sdr/FDEA200911274271.md): Skin · corroded · Nov 27, 2009 · N264FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > FWD PIT- SKIN CORRODED AROUND DOME NUT AT BS 720A AFT SIDE OF FRAME, OTBD OF STRINGER 28R. CUT-OUT TWO DAMAGED AREA OF SKIN, FABRICATED REPAIR DOUBLER, STRUCTURAL FILLER AND FABRICATED 3 FILLER, INSTALLED REPAIR WASHERS, STRUCTURAL FILLER, DOUBLER AND FILLE
- [SDR FDEA200911234136](https://openairdocs.org/sdr/FDEA200911234136.md): Spar · cracked · Nov 23, 2009 · N264FE · Boeing 727233 · Wing Spar
  > RT WING T/E FALSE SPAR LWR CHORD CRACKED AT WBL 118. CUT-OUT DAMAGED SECTION IAW SRM 51-10-1. FABRICATED NEW WEB SECTION IAW DWG NR SR27-57-038 REV C. FABRICATED ANGLES IAW DWG NR SR27-57-038 REV C. FABRICATED WEB DOUBLER IAW DWG NR SR27-57-038 REV C. LOC
- [SDR FDEA200911234135](https://openairdocs.org/sdr/FDEA200911234135.md): Spar · cracked · Nov 23, 2009 · N264FE · Boeing 727233 · Wing Spar
  > LT WING T/E FALSE SPAR CRACKED AT WBL 118. CUT OUT SECTION 20 1/2" LONG AND WEB 9 1/2" X 12" IAW SRM 51-10-1 REV 101, FABRICATED WEB SECTION AND DOUBLER, 2 SPLICE ANGLES,, RADIUS FILLER, 2 FILLERS IAW DWG NR SR27-57-038 REC C, INSTALLED ALL REPAIR FILLER
- [SDR 08FDEA03562](https://openairdocs.org/sdr/08FDEA03562.md): Roller Cam · broken · Aug 23, 2008 · N264FE · Boeing 727233 · Passenger/Crew Doors
  > AFTER TAKEOFF CREW REPORTS 2 LOUD BANGS OR POPS. NO ENG INDICATION FLUCTUATIONS OR PRESSURIZATION CHANGES. CREW REPORTS ENTRY DOOR WAS HARD TO CLOSE, BUT NO LIGHTS EVER CAME ON. OCCURED APPROXIMATELY AROUND 14,000 FT. INSPECT CABIN ENTRY DOOR AND FOUND T
- [SDR 07FDEA05138](https://openairdocs.org/sdr/07FDEA05138.md): Ejector Valve · failed · Dec 24, 2007 · N264FE · Boeing 727233 · Air Intake Anti/De-Ice System
  > ENG ANTI ICE VALVES WERE ON FOR T/O. IMMEDIATELY AFTER T/O, THE NR 2 ENGINE ANTI ICE DUCT TEMP WENT FULL SCALE HOT AND THE OVERHEAT LIGHT ILLUMINATED. WITHIN 30 SECS, LT PACK TRIPPED AND ENG FAIL LIGHT ILLUMINATED. STANDARD BLEED/PACK CONFIGURATION FOR T/O.
- [SDR 07FDEA04366](https://openairdocs.org/sdr/07FDEA04366.md): Floorbeam · corroded · Sep 28, 2007 · N264FE · Boeing 727233 · Fuselage Main, Floor Beam
  > MAIN DECK FLOORBEAM AT STA 720A LBL62 WL 208 T-CAP CORRODED OUT OF LIMITS. REMOVED CORRODED AREA, INSTALLED T-ANGLE AND SPLICE PLATE REPAIR IAW SRM 51-30-2.
- [SDR 07FDEA04351](https://openairdocs.org/sdr/07FDEA04351.md): Floorbeam · corroded · Sep 27, 2007 · N264FE · Boeing 727233 · Fuselage Main, Floor Beam
  > MAIN CARGO DECK, STA 560 RBL 1-24, WL 208, FLOORBEAM TOP SURFACE HAS CORROSION. REMOVED AND REPLACED FLOORBEAM TEE CAP AND ANGLES IAW SR 27-53-034.
- [SDR 05FDEA03730](https://openairdocs.org/sdr/05FDEA03730.md): Fan · failed · Nov 8, 2005 · N264FE · Boeing 727233 · Air Distribution Fan
  > STRONG FUMES IN COCKPIT AT FL 320 CRUISE FLT RAN EMERGENCY CHECKLIST AND LANDED AT KSWF. FOUND GASPER FAN C/B POPPED, RESET C/B AND IT POPPED AGAIN. SUSPECT BAD GASPER FAN. REMOVED AND REPLACED GASPER FAN IAW MM 21-23-011-4. 0PS CKS GOOD. R/I FROM FACT PR
- [SDR 05FDEA01664](https://openairdocs.org/sdr/05FDEA01664.md): Floorbeam · corroded · Jun 23, 2005 · N264FE · Boeing 727233 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM LBL 10, BS 560. REPAIRED PER SRM 53-10-8.
- [SDR 05FDEA01649](https://openairdocs.org/sdr/05FDEA01649.md): Intercostal · cracked · Jun 22, 2005 · N264FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > INTERCOSTAL CRACKED STA 358, STR 16 LT. REPAIRED INTERCOSTAL PER SRM 51-40-2.
- [SDR 05FDEA01628](https://openairdocs.org/sdr/05FDEA01628.md): Floorbeam · corroded · Jun 21, 2005 · N264FE · Boeing 727200 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM LBL 25 - RBL 25 BS 620. CORROSION FOUND TO BE OUT OF LIMITS REPAIRED FLOORBEAM IAW SRM 53-10-8 FIG 3
- [SDR 05FDEA01629](https://openairdocs.org/sdr/05FDEA01629.md): Floorbeam · corroded · Jun 21, 2005 · N264FE · Boeing 727200 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM LBL 12 BS 480. FABRICATED AND INSTALLED FLOORBEAM REPAIR LBL 12, BS 480 PER SRM 53-10-08 FIG 3
- [SDR 05FDEA01398](https://openairdocs.org/sdr/05FDEA01398.md): Skin · deformed · May 21, 2005 · N264FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > WHILE WORKING NOSE AREA DOUBLER FOUND SKIN DEFORMED ALONG LT SIDE. REPLACED DOUBLER PER FED-EX EA 7-5330-86293.
- [SDR 05FDEA01379](https://openairdocs.org/sdr/05FDEA01379.md): Skin · damaged · May 20, 2005 · N264FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > EXTERNAL REPAIR BS 1100, STR 26R (8 INCH BY 9 INCH) REQUIRES EVALUATION TO DETERMINE PER SRM OR APPROVED DATA. REMOVED OLD REPAIR AND INSTALLED NEW REPAIR PER FED-EX EA 7-5330-86292.
- [SDR 05FDEA01376](https://openairdocs.org/sdr/05FDEA01376.md): Skin · dented · May 19, 2005 · N264FE · Boeing 727200 · Cargo/Baggage Doors
  > AFT LOWER CARGO NR 3 HAS DENT 18 INCHES FROM LOWER CORNER 2 INCHES FROM LOWER EDGE. REPLACED SKIN PER SRM 51-30-2
- [SDR 05FDEA01374](https://openairdocs.org/sdr/05FDEA01374.md): Depressor · damaged · May 19, 2005 · N264FE · Boeing 727200 · Cargo/Baggage Doors
  > FWD LOWER CARGO DOOR FWD CORNER IS DAMAGED AT AFT END. REPLACED FWD LOWER CARGO DOOR FWD CORNER PER SRM 51-30-2
- [SDR 05FDEA01375](https://openairdocs.org/sdr/05FDEA01375.md): Seal Depressor · damaged · May 19, 2005 · N264FE · Boeing 727200 · Cargo/Baggage Doors
  > AFT LOWER CARGO DOOR NR 2 FWD CORNER DAMAGED.
- [SDR 05FDEA01233](https://openairdocs.org/sdr/05FDEA01233.md): Frame · corroded · May 11, 2005 · N264FE · Boeing 727200 · Fuselage Main, Frame
  > BS 740 LOWER CHORD CORRODED AT RBL 6. *S/D* REPAIRED PER EA 7-5310-86287.
- [SDR 05FDEA01222](https://openairdocs.org/sdr/05FDEA01222.md): Hinge Fitting · gouged · May 6, 2005 · N264FE · Boeing 727200 · Leading Edge Devices
  > GOUGE IN THE NR 6 K-FLAP CENTER HINGE FITTING COMMON TO L/E FIXED. REPLACED NR 6 K-FLAP CENTER HINGE FITTING PER SRM 51-30-2.
- [SDR 05FDEA01206](https://openairdocs.org/sdr/05FDEA01206.md): Flap Track · corroded · May 4, 2005 · N264FE · Boeing 727200 · Trailing Edge Flaps
  > NR 2 FLAP TRACK REAR SPAR ATTACH AREA IS CORRODED. REPLACED NR 2 FLAP TRACK ON FED EX CARD 27X5706-03.

Next page: https://openairdocs.org/deregistered/N264FE-2015-08-10/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 = 'N264FE' AND deregistration_id = 'N264FE-2015-08-10'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N264FE-2015-08-10/reports

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