# Service difficulty reports: N273FE, cancelled Aug 27, 2013

A list on [N273FE, cancelled Aug 27, 2013](https://openairdocs.org/deregistered/N273FE-2013-08-27.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 · 85 reports

- [SDR FDEA201009283775](https://openairdocs.org/sdr/FDEA201009283775.md): Engine · failed · Sep 28, 2010 · N273FE · Boeing 727233 · Engine (Turbine/Turboprop)
  > LOUD BANG/ ACFT SHUDDER DURING TAKEOFF, ACFT TAKEOFF REJECTED AT 115 KNOTS. GROUND PERSONNEL REPORTED HEARING 3 DISTINCT LOUD BANGS, NO APPARENT ENGINE MALFUNCTION NOTED PRIOR TO REJECT (ON GAUGE) WITH ALL INDICATIONS NORMAL AT IDLE. INSPECT ALL THE ACFT AI
- [SDR FDEA201002130419](https://openairdocs.org/sdr/FDEA201002130419.md): Inlet · obstructed · Feb 13, 2010 · N273FE · Boeing 727233 · Cabin Cooling System
  > LT AND RT PACK "TRIP OFF" LIGHTS W/ "DUCT OVER" LIGHT. ON POST FLIGHT, PACK COOLING DOOR FILLED WITH SNOW. INSPECTED PACK INTAKES AND FOUND SNOW PACKED INSIDE. MELTED SNOW FROM PACK INLET AREA. OPERATED PACKS IAW MM 21-61-000-5 AND 21-55-000-5. OPS CHECK
- [SDR FDEA200909233364](https://openairdocs.org/sdr/FDEA200909233364.md): Motor · leaking · Sep 23, 2009 · N273FE · Boeing 727233 · Hydraulic System, Main
  > LOST SYS A HYD FLUID DURING CLIMBOUT DID QRH CHECKLIST. SECURED SYS A HYD PUMPS AND CLOSED FLUID SHUTOFF SWITCHES IAW QRH. REMOVED AND REPLACED BOTH FLAP MOTORS IAW 27-51-062-4, REMOVED AND REPLACED ENG NR 1 AND 2 CASE DRAIN FILTERS IAW 29-11-041-2, REMOVED S
- [SDR 08FDEA03042](https://openairdocs.org/sdr/08FDEA03042.md): Channel · corroded · Jul 24, 2008 · N273FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > LOWER FUSE WING BODY FILLET FRG SUPPORT FRAME U CHANNEL IS CORRODED BS 773, LBL 9 - RBL 9, WL 140. REMOVED U CHANNEL REF SRM 51-30-2. FABRICATED "U" CHANNEL ON SHOP SNRM NR N00692, DRILLED UP, TREATED, PRIMED AND PAINTED "U" CHANNEL REF DWR 65-58504, SRM 51
- [SDR 08FDEA02994](https://openairdocs.org/sdr/08FDEA02994.md): Intercostal · corroded · Jul 21, 2008 · N273FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > DELTA BEAM AT STA 740 HAS CORROSION AROUND AND UNDER HEADS OF SEVERAL FASTENERS. CAN BE SEEN THRU ACCESS HOLE BELOW BEAM. REMOVED CORROSION. ORIGINAL "T".107 LOSS AT LOWEST POINT IS.028 REMAINING "T" IS.079. OUT OF LIMITS REF SRM 53-10-1 FIG 101 DETAI
- [SDR 08FDEA02985](https://openairdocs.org/sdr/08FDEA02985.md): Bracket · cracked · Jul 19, 2008 · N273FE · Boeing 727233 · Nacelle/Pylon Miscellaneous Structure
  > NR 1 ENG UPPER COWL, BRACKET CRACKED AT FWD O/B LOWER CORNER REMOVED AND REPLACED CRACKED SEGMENT, PAINTED AFFECTED AREA OF COWLING. REF SRM 51-30-2 PG 2, MM 51-20-151-7 PG1-5. THIS IS CLASSIFIED AS A MINOR REPAIR.
- [SDR 08FDEA02984](https://openairdocs.org/sdr/08FDEA02984.md): Fairing · cracked · Jul 19, 2008 · N273FE · Boeing 727233 · Aerodynamic Fairings
  > RT BODY FAIRING PANEL NR 3349 CRACKED AT EDGE. REMOVED DAMAGED EDGE PLATE. VERIFIED MATERIAL FOR NEW EDGE PLATE, FABRICATED NEW EDGE PLATE, TREATED AND PRIMED AND INSTALLED. REF DWR 65-58505 AND SRM 51-10- 2 PG1, 51-30-2 PG1. THIS IS CLASSIFIED AS A MINOR
- [SDR 08FDEA02983](https://openairdocs.org/sdr/08FDEA02983.md): Retainer · corroded · Jul 19, 2008 · N273FE · Boeing 727233 · Wing Miscellaneous Structure
  > LEFT MLG W/W LOWER FWD WING PANEL HAS CORROSION ON SEAL RETAINER STRIP NEAR LOWER MLG SUPPORT BEAM, WSS 217. REMOVED AND REPLACED LEFT MLG W/W LOWER FWD WING PANEL SEAL RETAINER AT WSS 217 REF SRM 51-30-2 PG 2 AND DWR 65-21656. THIS IS CLASSIFIED AS A MINOR
- [SDR 08FDEA02958](https://openairdocs.org/sdr/08FDEA02958.md): Bulkhead · corroded · Jul 17, 2008 · N273FE · Boeing 727233 · Fuselage Main, Bulkhead
  > CORROSION AT BS 1166 BULKHEAD RT SIDE "T" ANGLE (AT BOTTOM NUTPLATE AFT SIDE OF BULKHEAD). REPLACED T-CHORD AT AFT PIT BULKHEAD BS 1166 RBL 25 INCHES. REMOVED CORROSION AND FOUND NOT WITHIN ALLOWABLE LIMITS ORIG MATERIAL THICKNESS IS.063, MATERIAL LOSS IS.
- [SDR 08FDEA02954](https://openairdocs.org/sdr/08FDEA02954.md): Floor Support · corroded · Jul 17, 2008 · N273FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > UNDER FWD LAV STA 328 TO 344 FLOOR SUPPORT RBL 52 HAS CORROSION AROUND NUTPLATES REMOVED AND REPLACED SUPPORT FROM STA 326-344 RBL REF SRM 51-30-2 PG 2, FLOOR SUPPORT AT RBL 52 STA 328-344. FOUND TO BE WITHIN LIMITS OF SRM 53-10-06, TREATED AND PRIMED REF SRM
- [SDR 08FDEA02949](https://openairdocs.org/sdr/08FDEA02949.md): Web · cracked · Jul 17, 2008 · N273FE · Boeing 727200 · Leading Edge Devices
  > RIGHT WING O.B. L.E. NR 5 SLAT BN 279, CRACKED LWR. AFT INTERNAL WEB ANGLE AT INBD. SIDE OF ACTUATOR RAM ATACH STRUCTURE REMOVED ACCESS PANEL, INSPECTED FOR CRACKS, VERIFIED MATERIAL, FABRICATED, LOCATED AND DRILLED REPAIR PART. INSTALLED REPAIR, INSTALLED AC
- [SDR 08FDEA02926](https://openairdocs.org/sdr/08FDEA02926.md): Floor Support · corroded · Jul 16, 2008 · N273FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > FLOORBOARD, FWD LAV SUPPORT NUT PLATES RUSTED STA 305 - RBL 44. REMOVED FLOOR SUPORT ANGLE, REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. ORIG. MATERIAL THICKNESS.040 INCH. REMAINING.031 INCH REMOVED.009'. FABRICATED NEW ANGLE, PENATRANT INSP FOR CRAC
- [SDR 08FDEA02945](https://openairdocs.org/sdr/08FDEA02945.md): Panel · delaminated · Jul 16, 2008 · N273FE · Boeing 727233 · Horizontal Stabilizer, Plate/Skin
  > UPPER TAIL PANEL NR 9607, INNER FOIL DISBONDED REPAIRED TEDLAR COVERING ON INNER SURFACE REF SRM 51-40-9 STEP 11 PG 18. THIS IS CLASSIFIED AS A MINOR REPAIR.
- [SDR 08FDEA02939](https://openairdocs.org/sdr/08FDEA02939.md): Panel · cracked · Jul 16, 2008 · N273FE · Boeing 727233 · Wing, Plate/Skin
  > PANEL 3617 BOTTOM AFT END CRACKED REPAIRED PANEL 3617 REF SRM 51-40-9 STEPS 3D, 4E, 4F, PGS 3-7 AND AMM 51-20-051 PG1, AMM 51-20-151-7 PG 1. THIS IS CLASSIFIED AS A MINOR REPAIR.
- [SDR 08FDEA02938](https://openairdocs.org/sdr/08FDEA02938.md): Panel · delaminated · Jul 16, 2008 · N273FE · Boeing 727233 · Leading Edge Devices
  > NR 3 SLAT UNDERWING PANEL NR 6224 HAS AREA OF DELAMINATION REPAIRED PANEL 6224 REF SRM 51-40-9 STEPS 3D, 4E, 4F PG3-7 AND AMM 51-20-151-7 PG 1. THIS IS CLASSIFIED AS A MINOR REPAIR.
- [SDR 08FDEA02927](https://openairdocs.org/sdr/08FDEA02927.md): Door · gouged · Jul 16, 2008 · N273FE · Boeing 727233 · Cargo/Baggage Doors
  > MAIN CARGO DOOR, AFT EDGE LOWER CORNER GOUGED LOWER AFT CORNER GOUGED BEYOND LIMIT. REMOVED DOUBLER FABRICATED NEW DOUBLER, TREATED AND PRIMED. INSTALLED NEW DOUBLER REF 727 P-FSRM 52-30-2 PG 1/2. THIS IS CLASSIFIED AS A MAJOR REPAIR.
- [SDR 08FDEA02925](https://openairdocs.org/sdr/08FDEA02925.md): Frame · corroded · Jul 16, 2008 · N273FE · Boeing 727233 · Emergency Exits
  > RT AFT EMERGENCY EXIT HATCH LOWER FRAME OUTER SURFACE HAS CORROSION. REMOVED CORROSION REF SRM 52-00-2 NDT THICKNESS ORIGINAL "T".063,.005 LOSS,.058, DAMAGE WITHIN LIMITS REF SRM 53-10-1 FIG 1 SHEETS 1, 2, 3. TREATED PRIMED AND PAINTED REWORKED AREAS REF
- [SDR 08FDEA02924](https://openairdocs.org/sdr/08FDEA02924.md): Frame · corroded · Jul 16, 2008 · N273FE · Boeing 727233 · Emergency Exits
  > RIGHT FWD EMERGENCY HATCH FRAME LOWER OUTER SURFACE CORRODED BETWEEN SEAL RETAINER AND SKIN REMOVED CORROSION REF SRM 52-00-2. NDT THICKNESS ORIG "T".063 LOSS.005.058. REMAINING DAMAGE WITHIN LIMITS REF SRM 53-10-1 FIG 1 SHEETS 1, 2, 3. TREATED, PRIMED A
- [SDR 08FDEA02922](https://openairdocs.org/sdr/08FDEA02922.md): Skin · cracked · Jul 16, 2008 · N273FE · Boeing 727233 · Trailing Edge Flaps
  > LEFT WING INBD AFT FLAP, 3RD ATTACH FITTING OUTBD SKIN CRACKED FABRICATED REPAIR PARTS AT LEFT WING T/E AFT FLAP, THIRD ATTACH FITTING O/B SKIN, REF 27-50-4 FIG 11. TREATED, PRIMED AND INSTALLED, REF SRM 51-20-2 PG 1-7, 57-50-04 FIG 11, 51-30-2 PG 2-4. PAI
- [SDR 08FDEA02921](https://openairdocs.org/sdr/08FDEA02921.md): Floor Support · corroded · Jul 16, 2008 · N273FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > FLOORBOARD SUPPORT NUTPLATES RUSTED STA 305-312 RBL 55 FWD LAV. REMOVED FLOOR SUPPORT ANGLE, REMOVED CORROSION, FOUND TO BE OUT OF LIMITS ORIG MATERIAL THICKNESS.040, REMAINING.033, REMOVED.007. INSTALLED NEW ANGLE REF SRM 51-30-2 PG 2, SRM 53-10-1 PG 1
- [SDR 08FDEA02917](https://openairdocs.org/sdr/08FDEA02917.md): Skin · corroded · Jul 16, 2008 · N273FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > C1 PIT BILGE AREA-STR 28R STA 680 LEVELING COMPOUND BULGING WITH CORROSION ON SKIN. REMOVED DAMAGED COMPOUND. FOUND CORROSION AT SKIN AND NDT FOR LIMITS ORIGINAL "T".070 LOSS AT LOWEST POINT IS.034, REMAINING T IS.036 IS OUT OF LIMITS REF SRM 53-30-3. RE
- [SDR 08FDEA02916](https://openairdocs.org/sdr/08FDEA02916.md): Floor Panel · corroded · Jul 16, 2008 · N273FE · Boeing 727233 · Fuselage Floor Panel
  > MAIN DECK LAV FLOOR WEB PANEL, UPPER LWR SURFACES ARE CORRODED BS 304 - 340, RBL 40 - 60, WL 208. REMOVED CORROSION, ORIGINAL MATERIAL THICKNESS.042 INCH, REMAINING.035', REMOVED.007. FOUND TO BE OUT OF LIMITS REF DRM 53-10-1 PG 2, TOOL ID AAR 9800 CAL D
- [SDR 08FDEA02915](https://openairdocs.org/sdr/08FDEA02915.md): Floor Support · corroded · Jul 16, 2008 · N273FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > FWD LAV FLOOR SUPPORT STA 305-312 RBL 42 NUTPLATES RUSTED AND FLOORBEAM CORRODED. REMOVED CORROSION FROM FLOORBEAM, ORIGINAL THICKNESS.070, REMAINING.066. REMOVED.004, FOUND TO BE WITHIN LIMITS, REMOVED CORROSION FROM FLOOR SUPPORT, ORIG THICKNESS.070,
- [SDR 08FDEA02913](https://openairdocs.org/sdr/08FDEA02913.md): Channel · cracked · Jul 16, 2008 · N273FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > E/E DOOR CUT-OUT FWD ANGLE CRACKED BY LATCH REPLACED CUT OUT FWD ANGLE AND RIGGED E/E DOOR REF BOEING DWR 65-16351, SRM 51-30-01 PG 1-10, SRM 51-30-5 PG 3, SRM 51-30-2 PG 2/3, AMM 51-20-151 PG 1-6, AMM 20-60-001 PG10, MM 52-40-011 PG 1. THIS IS CLASSIFIED AS
- [SDR 08FDEA02841](https://openairdocs.org/sdr/08FDEA02841.md): Angle · corroded · Jul 12, 2008 · N273FE · Boeing 727233 · Fuselage Main, Bulkhead
  > BS 740 BULKHEAD LOWER FWD SURFACE, ANGLE LBL 4.5 TO RBL 4.5, WL 146.5 HAS CORROSION ON AFT SURFACE FABRICATED NEW ANGLE REF SRM 51-10-2 PG 2, DWR 65-23555. TREATED AND PRIMED REF 51-10-2 PG 2. THIS IS CLASSIFIED AS A MAJOR REPAIR.
- [SDR 08FDEA02834](https://openairdocs.org/sdr/08FDEA02834.md): Fitting · corroded · Jul 12, 2008 · N273FE · Boeing 727233 · Fuselage Main, Bulkhead
  > BS 740 BULKHEAD LOWER SURFACE, "T" ANGLE AT RBL 5" WL 146.5 CONNECTION TO DELTA BEAM "T" FLANGE IS CORRODED NEW T ANGLE FABRICATED ON SHOP NON-ROUTINE N00670. REMOVAL AND INSTALLATION ACCOMPLISHED ON N00167. THIS IS CLASSIFIED AS A MAJOR REPAIR.
- [SDR 08FDEA02796](https://openairdocs.org/sdr/08FDEA02796.md): Structure · cracked · Jul 9, 2008 · N273FE · Boeing 727233 · Cargo/Baggage Doors
  > NUMBER 3 CARGO DOOR LOWER FWD "T" CHORD CRACKED AT FASTENERS REPAIRED LOWER FWD "T" CHORD. REMOVED LWR INNER DOOR SKIN REF SRM 51-30-2. FABRICATED REPAIR ANGLES AND FILLER REF SRM 51-40-04 PG 14-16 FIG 3. TREATED AND PRIMED REPAIR PARTS REF SOPM 20-44-04 PG
- [SDR 08FDEA02780](https://openairdocs.org/sdr/08FDEA02780.md): Support Bracket · corroded · Jul 9, 2008 · N273FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > CORROSION AROUND BOLT HOLE AT STA 340 FITTING SUPPORT BRACKET JUST BEHIND NOSE WHEEL WELL LT SIDE. REMOVED FITTING SUPPORT AT STA 340 AFT OF NOSE WHEEL WELL LT SIDE. TREATED AND PRIMED NEW SUPPORT FITTING REF SRM 51-30-2 PG 1-20 AND MM 51-20-7. THIS IS CLAS
- [SDR 08FDEA02778](https://openairdocs.org/sdr/08FDEA02778.md): Retainer · corroded · Jul 9, 2008 · N273FE · Boeing 727233 · Wing Miscellaneous Structure
  > RT WING REAR SPAR LWR CHORD, APPROX 12" IB OF FWD MLG TRUNNION, SEAL RETAINER CORRODED AT OB END. REMOVED FAIRING AND SEAL RETAINER REF SRM PG 2 LOCATED AND DRILLED NEW SEAL RETAINER REF SRM 51-30-5 PG 1, INSTALLED SEAL RETAINER AND FAIRING REF SRM 51-30-2
- [SDR 08FDEA02777](https://openairdocs.org/sdr/08FDEA02777.md): Frame · corroded · Jul 9, 2008 · N273FE · Boeing 727233 · Fuselage Main, Frame
  > LWR AFT CARGO PIT, CORROSION ON UPPER FLANGE OF FRAME AT STA 1090 STR 27L REMOVED CORROSION, ORIGINAL "T".063, REMOVED.017, REMAINING.046 OUT OF LIMITS. FABRICATED REPAIR DOUBLER FROM 7075-0.063, HEAT TREAT T6, APPLIED ALODINE, PRIMER AND INSTALLED REPAI
- [SDR 08FDEA02739](https://openairdocs.org/sdr/08FDEA02739.md): Slat · cracked · Jul 8, 2008 · N273FE · Boeing 727233 · Leading Edge Devices
  > LT WING NR 4 SLAT FENCE UPPER AFT END COMPOSITE IS CRACKED AND DELAMED. REPAIRED NR 4 SLAT FENCE REF SRM 51-40-9 STEP 7 PG 9 AND AMM 51-20-051-7 PG 1 AND 51-20-151-7 PG 1. THIS IS CLASSIFIED AS A MINOR REPAIR.
- [SDR 07FDEA01818](https://openairdocs.org/sdr/07FDEA01818.md): Line · failed · May 15, 2007 · N273FE · Boeing 727233 · Hydraulic System, Main
  > AFTER TOUCHDOWN AMD SPOILER DEPLOYMENT, EXPERIENCED LOSS OF "A" HYDRAULIC SYSTEM QUANTITY AND PRESSURE. FOUND BLOWN FLEX LINE ON LT ELEVATOR PCU. PART IS IN STOCK AT SAV. REMOVED AND REPLACED I/B FLEX LINE PER MM27-30-081-4. SERVICED "A" HYD SYS TO FULL PE
- [SDR 06FDEA1317](https://openairdocs.org/sdr/06FDEA1317.md): Pressure Switch · malfunctioned · Apr 6, 2006 · N273FE · Boeing 727233 · Fuel Flow Sensor
  > AT FL350, AND FUEL TEMPERATURE 5, NR 2 FUEL ICING LIGHT ILLUMINATED. PERFORMED RELEVANT EMERG CK-LIST. DECLARED EMERGENCY. RELEASED FOR SERVICE PER MEL/CDL: 73-04 CATEGORY: C "MEL 73-04. TWO FUEL FILTER DIFFERENTIAL PRESSURE WARNING SYSTEM INOP. REMOVED A
- [SDR 06FDEA0499](https://openairdocs.org/sdr/06FDEA0499.md): Repair · unknown · Feb 2, 2006 · N273FE · Boeing 727200 · Aircraft Structures
  > FOUND PREVIOUSLY REPAIR INSTALLED AT FS 500 STR.30 WAS ACCOMPLISHED IAW SRM 53-30- 3, FIG. 24 BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTED OF LOCATION OF THE REPAIR, SIZE, SHAPE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE, THICKNESS, GENERAL WORKMANSH
- [SDR 06FDEA0472](https://openairdocs.org/sdr/06FDEA0472.md): Repair · unknown · Feb 1, 2006 · N273FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > FOUND PREVIOUSLY INSTALLED REPAIR AT AFT INBD CORNER OF PNEUMATIC GROUND CONNECTION CUTOUT WAS DETERMINED TO BE IAW SR 27-53-024, BASED ON AN EXTERNAL VISUAL EVALUATION WITH REPAIR INSTALLED, EVALUATION CONSISTED OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND
- [SDR 03FDEA01785](https://openairdocs.org/sdr/03FDEA01785.md): Switch · malfunctioned · Oct 21, 2003 · N273FE · Boeing 727200 · Leading Edge Slat Control System
  > ON FLAP RETRACTION FROM 5 DEG TO 2 DEG, LED NR 5 (RT SIDE) DID NOT FULLY RETRACT. AMBER LIGHT ILLUMINATED ON LED POSITION INDICATOR AFT BULKHEAD. COMPLIED WITH RED TABS, DID NOT CORRECT PROBLEM. REMOVED AND REPLACED NR 5 L/E FLAP POSITION SWITCH IAW MM 27-8
- [SDR 03FDEA00885](https://openairdocs.org/sdr/03FDEA00885.md): Skin · dented · Jun 16, 2003 · N273FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAS A DENT, STRINGER 6L, BS 720C. REPAIR DENTED SKIN PER SRM 53-30-3 FIG 3.
- [SDR 03FDEA00886](https://openairdocs.org/sdr/03FDEA00886.md): Skin · corroded · Jun 16, 2003 · N273FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > CORROSION (C53-113-01, 2) BULGING SKIN ON STR 28L, BS 1055.
- [SDR 02FDEA00838](https://openairdocs.org/sdr/02FDEA00838.md): Warning Light · illuminated · Nov 14, 2002 · N273FE · Boeing 727200 · Leading Edge Slat Position Indicating System
  > DURING FLAP RETRACTION FROM FLAPS 2 TO FLAPS UP. LED AMBER LIGHT REMAINED ILLUMINATED. POSITION TEST SELECTOR INDICATED NR 2 LED WAS STILL EXTENDED, NR 2 SLAT.
- [SDR 01FDEA00018](https://openairdocs.org/sdr/01FDEA00018.md): Skin · cracked · Jan 11, 2001 · N273FE · Boeing 727233 · Elevator, Plate/Skin
  > CRACK IN SKIN, VERTICAL STAB, LEFT SIDE, STR 10, BOTTOM OF STAB. *S/D* REMOVED AND REPLACED PER IAW FEDEX SRM 55-30-3 AND FEDEX EA 7-5510-56226.
- [SDR 01FDEA00014](https://openairdocs.org/sdr/01FDEA00014.md): Frame · dented · Jan 9, 2001 · N273FE · Boeing 727233 · Fuselage Main, Frame
  > FRAME IS DENTED AT BS 520, STRINGER 22 RT. *S/D* REMOVED, REPLACED AND FAB PER FEDEX SRM 51-40-3.
- [SDR 01FDEA00011](https://openairdocs.org/sdr/01FDEA00011.md): Doubler · gouged · Jan 8, 2001 · N273FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > MAIN CARGO DOOR AFT FRAME BS 620 IS GOUGED AT PREVIOUS REPAIR. INGD RADIUS APPROX 21 INCHES UP FROM THE BOTTOM EDGE. *S/D* REMOVED, REPLACED AND FAB PER IAW FEDEX SRM 51-40-3. PREVIOUS REPAIR. INSTALL REPAIR DOUBLER PER IAW FEDEX SRM 51-30-2.
- [SDR 01FDEA00003](https://openairdocs.org/sdr/01FDEA00003.md): Stringer · damaged · Jan 4, 2001 · N273FE · Boeing 727233 · Fuselage Main, Longeron/Stringer
  > NR 319 TEN OPEN FASTENER HOLES ON SIDE OF STRINGER 24 LT AT BS 480. ** S/D ** R&R & FAB PER FEDEX SRM 53-10-3, 53-10-3.
- [SDR 01FDEA00004](https://openairdocs.org/sdr/01FDEA00004.md): Stringer · cracked · Jan 4, 2001 · N273FE · Boeing 727233 · Fuselage Main, Longeron/Stringer
  > CRACK AT STR 15 LT SIDE BS 720C-4 AFT OF EXT LIGHT. ** S/D ** R&R PER IAW FEDEX SRM 53-10-3 FIG 1.
- [SDR 01FDEA00005](https://openairdocs.org/sdr/01FDEA00005.md): Stringer · cracked · Jan 4, 2001 · N273FE · Boeing 727233 · Fuselage Main, Longeron/Stringer
  > NR 419 CRACK AT STR 15 LT SIDE BS 720D+4 FWD OF EXT LIGHT. ** S/D ** R&R PER IAW FEDEX SRM 53-10-3 FIG 1.
- [SDR 01FDEA00006](https://openairdocs.org/sdr/01FDEA00006.md): Stringer · cracked · Jan 4, 2001 · N273FE · Boeing 727233 · Fuselage Main, Longeron/Stringer
  > NR 420 CRACK AT STR 15 RT SIDE BS 720B+4 FWD OF EXT LIGHT. ** S/D ** COMING
- [SDR 01FDEA00002](https://openairdocs.org/sdr/01FDEA00002.md): Keelbeam · corroded · Jan 4, 2001 · N273FE · Boeing 727233 · Fuselage Main, Keel
  > CORROSION ON LT KEELBEAM AT BS 960 O/B FLANGE AROUND FASTENERS. ** S/D ** COMING
- [SDR 00FDEA00753](https://openairdocs.org/sdr/00FDEA00753.md): Switch · out of adj · Nov 1, 2000 · N273FE · Boeing 727233 · Landing Gear Position and Warning
  > RT MG DOOR REMAIN ILLUM AFT GEAR RETRACTION GOES OUT IN UP POSITION. *S/D* ADJUSTED RT GEAR DOOR SWITCH PER 2 B (2) OF MM 32-62-11-4.
- [SDR 98FDEA00512](https://openairdocs.org/sdr/98FDEA00512.md): Bellframe · damaged · Aug 5, 1998 · N273FE · Boeing 727233 · Fuselage Main, Frame
  > NR 0546 - LOWER AFT CARGO COMP FS 1010 BELLFRAME BETWEEN STRINGERS 25L AND 26L CREASED. REMOVED DAMAGED AREA. FABRICATED DOUBLERS, TREATED, PRIMED AND INSTALLED DOUBLER AND FILLER PER SRM 53-10-4.
- [SDR 96FDEA00133](https://openairdocs.org/sdr/96FDEA00133.md): Floorbeam · corrosion · Jan 26, 1996 · N273FE · Boeing 727233 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM BS 460 RBL 10 AND 15 WL 208. REPAIRED FLOORBEAM AT BS 460 RBL 10 TO 15 WL 208. ALL WORK DONE IAW FEDEX EA 7-5310-26943.

Next page: https://openairdocs.org/deregistered/N273FE-2013-08-27/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 = 'N273FE' AND deregistration_id = 'N273FE-2013-08-27'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N273FE-2013-08-27/reports

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