# Service difficulty reports: N482FE, cancelled Jul 2, 2015

A list on [N482FE, cancelled Jul 2, 2015](https://openairdocs.org/deregistered/N482FE-2015-07-02.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 · 153 reports

- [SDR FDEA201303270675](https://openairdocs.org/sdr/FDEA201303270675.md): Cam · out of adjust · Mar 27, 2013 · N482FE · Boeing 727227 · Passenger/Crew Doors
  > FORWARD ENTRY DOOR IS VERY HARD TO CLOSE FROM INSIDE. INSPECTED FWD ENTRY DOOR IAW AMM 52-11-001-6 AND ADJUST UPPER AFT LATCH CAM FITTING IAW AMM 52-11-001-5, CHECKED OPENING AND CLOSING DOOR SEVERAL TIMES, CHECKED GOOD. ACFT OK FOR SERVICE.
- [SDR FDEA201301040016](https://openairdocs.org/sdr/FDEA201301040016.md): Slide · dislodged · Jan 4, 2013 · N482FE · Boeing 727227 · Escape Slide
  > ESCAPE SLIDE POPPED OUT OF BOX. POSSIBLY DUE TO ENROUTE TURBULENCE. INSPECTED AND REINSTALLED DOOR SLIDE IAW AMM 25-60-015-2. OK FOR SERVICE.
- [SDR FDEA201212084270](https://openairdocs.org/sdr/FDEA201212084270.md): Shutoff Valve · malfunctioned · Dec 8, 2012 · N482FE · Boeing 727227 · Cabin Cooling System
  > CLIMBOUT, HAD LESS THAN 2 PSID AT 10,000 MGL, LT AIR MIX VALVE WOULD NOT WORK, LT PACK WOULD NOT PRODUCE ANY AIR FOR PRESSURIZATION ON ENG 1 OR 2 BLEED. PRESSURIZED ACFT USING BOTH PACKS, EQUIPMENT COOLING AIR SHUTOFF VALVE DID NOT CLOSE BY 3 PSID. WRENCH
- [SDR FDEA201206292412](https://openairdocs.org/sdr/FDEA201206292412.md): Stringer · corroded · Jun 29, 2012 · N482FE · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 27R AT BS 720F, PLUS 15 INCHES. CORROSION OUT OF LIMITS IAW SRM 53-10-1 FIG 7. CUT OUT DAMAGED AREA IAW SRM 53-10-3 FIG 1. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-10-3 FIG 1 AND SRM 53-10-2 FIG 9.
- [SDR FDEA201206292410](https://openairdocs.org/sdr/FDEA201206292410.md): Stringer · corroded · Jun 29, 2012 · N482FE · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 27L AT BS 720F TO 740. CUT OUT DAMAGED AREA OF STRINGER 27L AT BS 720F PLUS 9 INCHES IAW SRM 53-10-3 FIG 1. FABRICATED STRINGER SECTION FILLER AND SPLICE IAW SRM REV 103, 53-10-3 FIG 1 AND 53-10-2. INSTALLED STRINGER REPAIR IAW SR
- [SDR FDEA201206282380](https://openairdocs.org/sdr/FDEA201206282380.md): Stringer Splice · corroded · Jun 28, 2012 · N482FE · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER SPLICE AT BS 950, STRINGER 27 LEFT. REMOVED DAMAGED SPLICE IAW SRM 51-30-2. FABRICATED SPLICE IAW SRM 51-20-1, REV 103, FIG 7 AND DWG 66-2521. INSTALLED SPLICE IAW SRM 51-30-2.
- [SDR FDEA201206282395](https://openairdocs.org/sdr/FDEA201206282395.md): Shear Tie · corroded · Jun 28, 2012 · N482FE · Boeing 727227 · Fuselage Internal Mounting Structure
  > CORROSION ON SHEAR TIE AT BS 1050, BETWEEN STRINGER 30 AND 29R. CUT OUT DAMAGED AREA OF BS 1050 SHEAR TIE IAW SRM 53-10-4 FIG 15. FABRICATED SHEAR TIE REPAIR ANGLE IAW SRM 53-10-4 FIG 15 REV 103. INSTALLED REPAIR IAW SRM 51-30-2 AND 53-10-4 FIG 15.
- [SDR FDEA201206282378](https://openairdocs.org/sdr/FDEA201206282378.md): Shear Tie · corroded · Jun 28, 2012 · N482FE · Boeing 727227 · Fuselage Internal Mounting Structure
  > CORROSION ON SHEAR TIE AT BS 970, BETWEEN STRINGER 29 AND 30 LEFT. REMOVED SECTION OF SHEAR TIE IAW SRM 53-10-4, FIG 15. FABRICATED SHEAR TIE REPAIR ANGLE IAW SRM 53-10-4 REV 103, FIG 15 AND 51-20-1 FIG 7 AND INSTALLED IAW SRM 51-30-2.
- [SDR FDEA201206282377](https://openairdocs.org/sdr/FDEA201206282377.md): Shear Tie · corroded · Jun 28, 2012 · N482FE · Boeing 727227 · Fuselage Internal Mounting Structure
  > CORROSION ON SHEAR TIE AT BS 970, BETWEEN STRINGER 28 AND 29 LEFT. CUT OUT SHEAR TIE IAW SRM 53-10-4 REV 103 FIG 15. FABRICATED SHEAR TIE REPAIR IAW SRM 53-10-4 FIG 15. INSTALLED IAW SRM 51-30-2.
- [SDR FDEA201206282375](https://openairdocs.org/sdr/FDEA201206282375.md): Stringer · damaged · Jun 28, 2012 · N482FE · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > FORWARD CARGO BAY WIRE BUNDLE STAND-OFF BRACKET BROKEN OFF AT BS 570, LBL 15. CUT OUT SECTION OF STRINGER 28L AT BS 570, 3 INCHES LONG IAW SRM 53-10-3 FIG 1. FABRICATED FILLER AND STRINGER REPAIR SECTION IAW SRM 53-10-3 FIG 1 REV 103. INSTALLED FILLER AND
- [SDR FDEA201206272371](https://openairdocs.org/sdr/FDEA201206272371.md): Stringer · corroded · Jun 27, 2012 · N482FE · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 27R AT BS 625. REMOVED DAMAGED PORTION OF STRINGER IAW SRM 53-10-3 FIG 1 AND 51-10-1. FABRICATED STRINGER REPAIR SECTION IAW SRM 53-10-3 FIG 1. INSTALLED STRINGER REPAIR PARTS IAW SRM 51-30-2 REV 103 AND SRM 53-10-3 FIG 1.
- [SDR FDEA201206272373](https://openairdocs.org/sdr/FDEA201206272373.md): Shear Tie · corroded · Jun 27, 2012 · N482FE · Boeing 727227 · Fuselage Internal Mounting Structure
  > CORROSION ON SHEAR TIE AT BS 950B, BETWEEN STRINGER 30 AND 29L. CUT OUT DAMAGED AREA SHEAR TIE IAW SRM 53-10-4 REV 103, FIG 15. FABRICATED SHEAR TIE REPAIR ANGLE IAW SRM 51-20-1 FIG 7 AND 53-10-4 FIG 15 AND 53-10-2 FIG 5. INSTALLED SHEAR TIE REPAIR AN
- [SDR FDEA201206272362](https://openairdocs.org/sdr/FDEA201206272362.md): Stringer · corroded · Jun 27, 2012 · N482FE · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 30, BS 1050. CUT OUT DAMAGED PORTION OF STRINGER 30 IAW B727 SRM 51-10-1 AND 53-10-3 FIG 1. FABRICATED STRINGER SECTION AND TWO SPLICES IAW SRM REV 103, 53-10-3 FIG 1. INSTALLED STRINGER REPAIR SECTION AND TWO SPLICES IAW SRM 53-10-
- [SDR FDEA201206272370](https://openairdocs.org/sdr/FDEA201206272370.md): Shear Tie · corroded · Jun 27, 2012 · N482FE · Boeing 727227 · Fuselage Internal Mounting Structure
  > CORROSION ON SHEAR TIE AT BS 1010, BETWEEN STRINGER 30 AND 29R. CUT OUT DAMAGED SHEAR TIE 1" X 6" IAW SRM 53-10-4 FIG 15 REV 103. FABRICATED SHEAR TIE REPAIR ANGLE IAW SRM 53-10-2 FIG 5 AND 53-10-4 FIG 15. INSTALLED SHEAR TIE REPAIR ANGLE IAW SRM 53-10-4
- [SDR FDEA201206262349](https://openairdocs.org/sdr/FDEA201206262349.md): Frame · worn · Jun 26, 2012 · N482FE · Boeing 727227 · Fuselage Main, Frame
  > AFT CARGO BAY, ELONGATED FASTENER HOLE IN UPPER FLANGE OF FRAME AT BS 1030, LBL 25. CUT OUT DAMAGED AREA OF FRAME 1/2" X7/8" IAW SRM REV 103 51-40-3 FIG 1. FABRICATED REPAIR DOUBLER FROM 7075-0,.063"X 14"X 4 1/2" IAW SRM 51-40-3 AND SRM 51-30-5 INSTALLED
- [SDR FDEA201206262389](https://openairdocs.org/sdr/FDEA201206262389.md): Skin · damaged · Jun 26, 2012 · N482FE · Boeing 727227 · Fuselage Main, Plate/Skin
  > DAMAGED AND SHEARED FASTENERS STA 1170, STR 27R. CUT OUT DAMAGED SKIN AREA IAW SRM 53-30-3 FIG 24. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-30-3 FIG 24 AND SRM 53-30-2 FIG 2.
- [SDR FDEA201206232372](https://openairdocs.org/sdr/FDEA201206232372.md): Intercostal · bent · Jun 23, 2012 · N482FE · Boeing 727227 · Fuselage Miscellaneous Structure
  > MAIN E/E BAY HATCH INTERIOR ENTRY AREA RT SIDE INTERCOSTAL BENT, FASTENER HEADS GOUGED BS 440, FROM CATCHING ON HATCH DURING OPERATION. REPAIRED DOUBLER IAW SRM 51-30-02, FABRICATED DOUBLER IAW SRM 51-40-2 FIG 1 AND 53-10-2 FIG 3 INSTALLED REPAIR IAW SRM 51
- [SDR FDEA201206212292](https://openairdocs.org/sdr/FDEA201206212292.md): Bracket · cracked · Jun 21, 2012 · N482FE · Boeing 727227 · Fuselage Miscellaneous Structure
  > L1 DOOR CUTOUT, STR 15L, SMALL BRACKET ATTACHED TO FORWARD DOOR STOP FITTING CRACKED, VIEWED FROM BOTTOM. REMOVED CRACKED BRACKET, FABRICATED AND INSTALLED NEW BRACKET IAW DWG 50-7946 REV K AND SRM 51-30-2.
- [SDR FDEA201206212293](https://openairdocs.org/sdr/FDEA201206212293.md): Skin · gouged · Jun 21, 2012 · N482FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > SKIN GOUGED AND DENTED STA 1087 STR 24R. CUT OUT DAMAGED AREA IAW SRM 51-10-1 AND 53-30-3 FIG 3 FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 53-30-3 FIG 3 AND 53-30-2 FIG 2 INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 51-30-02
- [SDR FDEA201206202280](https://openairdocs.org/sdr/FDEA201206202280.md): Web · cracked · Jun 20, 2012 · N482FE · Boeing 727227 · Fuselage Miscellaneous Structure
  > AFT AIR STAIR AREA FWD LT LIGHTNING HOLE CRACKED, BS 1227. CUT OUT DAMAGED AREA OF L/H AFT TORQUE BOX VERTICAL WEB STA 1227, FABRICATED, AND INSTALLED REPAIR DOUBLER IAW B727 SRM 53-10-2 FIG 6 AND 51-40-2 FIG 1
- [SDR FDEA201111224996](https://openairdocs.org/sdr/FDEA201111224996.md): Oil System · leaking · Nov 22, 2011 · N482FE · Boeing 727227 · Turbine Engine Oil System
  > NR 1 ENGINE LOST OIL QTY AND PRESSURE AT FL 320. ENGINE WINDMILLED FOR 30 MINS, OIL PRESSURE WAS ZERO. REMOVED AND REPLACED THE ENGINE
- [SDR FDEA201107192790](https://openairdocs.org/sdr/FDEA201107192790.md): Switch · inoperative · Jul 19, 2011 · N482FE · Boeing 727227 · Leading Edge Slat Control System
  > DURING FLAP RETRACTION FROM 5 DEG TO 2 DEG THE NR1 L/E FLAP IN TRANSIT LIGHT AND L/E FLAP YELLOW LIGHT REMAINED ILLUMINATED. NO ASSYEMETRY NOTED IN FLIGHT CONTROLS. NR 1 L/E FLAP, IAW MM REF 27-82-000-1, NO HELP. NEED POSITION SWITCH. PHL U TRIED JUMPER OF
- [SDR FDEA201101280405](https://openairdocs.org/sdr/FDEA201101280405.md): Slide · low pressure · Jan 28, 2011 · N482FE · Boeing 727227 · Escape Slide
  > ESCAPE SLIDE READS 2300 WHICH IS UNDER THE LIMIT FOR THIS TEMP. R & R EMERGENCY ESCAPE SLIDE IAW MM 25-60-015-2. OPS NORMAL.
- [SDR FDEA201008223090](https://openairdocs.org/sdr/FDEA201008223090.md): Power Supply · inoperative · Aug 22, 2010 · N482FE · Boeing 727227 · Emergency Lighting
  > RIGHT EMERGENCY EXTERIOR SLIDE LIGHT INOPERATIVE. REMOVED AND REPLACED EMER EXIT LIGHT POWER SUPPLY AND TESTED IAW AMM 33-50-051-2-0. OPS CHECKS GOOD. OK FOR SERVICE.
- [SDR FDEA201008062869](https://openairdocs.org/sdr/FDEA201008062869.md): Switch · failed · Aug 6, 2010 · N482FE · Boeing 727227 · Leading Edge Slat Control System
  > NR 6 LED FAILED TO RETRECT. NR 6 SLAT EXTEND LIGHT ON SO'S PANEL REMAINS ON AT ALL FLAP POSITIONS. WITH THE NR 6 SLAT CONNECTOR PLUG DISCONNECTED THE EXTEND LIGHT WILL EXTINGUISH. WITH THE JUMPER WIRE INSTALLED THE RETRACT REMAINS ON AT ALL FLAP SETTINGS AG
- [SDR FDEA201005051466](https://openairdocs.org/sdr/FDEA201005051466.md): Hose · leaking · May 5, 2010 · N482FE · Boeing 727227 · Hydraulic System, Main
  > CLIMBING THRU 16,000 FT NOTICED SYS A HYD QTY WAS ZERO, SHORTLY AFTER SYS PRESSURE WENT TO ZERO & BOTH LOW PRESSURE LIGHTS CAME ON. PERFORMED STABILIZER & QRH SYS A LEAK OR LOSS CHECKLIST, PERFORMED MANUAL GEAR EXTENTION & ALT MASTER FLAP EXTENTION. LANDED 16
- [SDR FDEA201004011046](https://openairdocs.org/sdr/FDEA201004011046.md): Indicator · inoperative · Apr 1, 2010 · N482FE · Boeing 727227 · Fuel Quantity Indicator
  > AIRCRAFT VERY DIFFICULT TO TRIM PROPERLY. REQUIRED OVER 2 UNITS OF LEFT AILERON TRIM, AND OVER 1 UNIT OF L RUDDER TRIM. NR 1 FUEL TANK GAUGE INOP, WAS FUELED TO A KNOWN QTY. A FUEL IMBALANCE COULD HAVE BEEN PART OF THE PROBLEM THOUGH WE COULD NOT TELL. WH
- [SDR FDEA201002260652](https://openairdocs.org/sdr/FDEA201002260652.md): Rib · cracked · Feb 26, 2010 · N482FE · Boeing 727227 · Leading Edge Devices
  > NR 8 SLAT SECOND RIB FROM INBD END IS CRACKED WING STA 355.4. REMOVED DAMAGED RIB, INSTALLED NEW RIB PN 65-17321-4 IAW SRM 51-30-2.
- [SDR FDEA201002190498](https://openairdocs.org/sdr/FDEA201002190498.md): Frame · corroded · Feb 19, 2010 · N482FE · Boeing 727227 · Fuselage Main, Frame
  > AFT CARGO STATION 990 STUB FRAME CORRODED AT STR 29R. CUT OUT DAMAGED AREA IAW SRM 53-10-4 FIG 15 AND 51-10-1. FABRICATED DOUBLER, ANGLE AND SHIM IAW SRM 53-10-4 FIG 15. INSTALLED REAIR PARTS IAW SRM 51-30-2.
- [SDR FDEA201002170441](https://openairdocs.org/sdr/FDEA201002170441.md): Shear Tie · corroded · Feb 17, 2010 · N482FE · Boeing 727227 · Fuselage Internal Mounting Structure
  > AFT CARGO STATION 1110, STRINGER 27L, SHEAR TIE CORRODED. REMOVED SHEAR TIE TEE ANGLE AT BS 1110, STR 27L IAW SRM, REV 102, 51-30-2. FABRICATED REPLACEMENT SHEAR TIE FROM PM60-5632, 7075-T6511, 4.5" LONG IAW DRAWING NR. 65-16346 REV P. INSTALLED SHEAR TIE I
- [SDR FDEA201002170445](https://openairdocs.org/sdr/FDEA201002170445.md): Web · cracked · Feb 17, 2010 · N482FE · Boeing 727227 · Fuselage Main, Structure
  > CRACK NOTED - RIGHT HAND LOWER TORQUE BOX WEB, RBL 20.5 AT BS 1223. UPPER LIGHTING HOLE, FORWARD OF PREVIOUS REPAIR RIVET LINE. REMOVED PREVIOUS REPAIR DOUBLER AT BS 1223, RBL 20.5 IAW SRM 51-30-2. ROUTED OUT DAMAGED AREA IAW SRM 51-10-1. FABRICATED NEW REPA
- [SDR FDEA201002170444](https://openairdocs.org/sdr/FDEA201002170444.md): Floorbeam · corroded · Feb 17, 2010 · N482FE · Boeing 727227 · Fuselage Main, Floor Beam
  > AFT CARGO STATION 1070, BOTTOM OF FLOORBEAM, CORROSION AROUND SCREW HOLES. RBL 12-45. CUT OUT 2 DAMAGED AREAS IAW SRM 53-10-8 FIG 8. FABRICATED 2 REPAIR ANGLES AND 2 FILLERS IAW SRM 53-10-8 FIG 8. HEAT TREATED ANGLES TO T6 CONDITION IAW FASI ER 2-37153-801 R
- [SDR FDEA201002170438](https://openairdocs.org/sdr/FDEA201002170438.md): Floorbeam · damaged · Feb 17, 2010 · N482FE · Boeing 727227 · Fuselage Main, Floor Beam
  > ELONGATED HOLE MAIN CABIN FLOOR BEAM BS 1110 LBL 45. CUT OUT DAMAGED AREA IAW SRM 53-10-8 FIG 8. FABRICATED 2 ANGLE REPAIRS. IAW SRM 53-10-8 FIG. 8. FABRICATED 2 SHIMS. IAW SRM 53-10-8. FABRICATED CHANNEL. FABRICATED FILLER IAW SRM 53-10-8, 51-10-3, AND 51-
- [SDR FDEA201002160434](https://openairdocs.org/sdr/FDEA201002160434.md): Skin · damaged · Feb 16, 2010 · N482FE · Boeing 727227 · Fuselage Main, Plate/Skin
  > EVALUATE TRIM OUT EXTERIOR FUSELAGE LAP SEAM BS 178 STR 18R CUT OUT DAMAGE ON UPPER SKIN 2" X 2 1/8" AND REMOVED FASTENERS COMMON TO REPAIR DOUBLER IAW EA 7-5330-135526, FABRICATED REPAIR PARTS, DOUBLER AND FILLER USING 2024-T3, 0.071" PO NR 9009068 DIMENSION
- [SDR FDEA201002160539](https://openairdocs.org/sdr/FDEA201002160539.md): Floorbeam · corroded · Feb 16, 2010 · N482FE · Boeing 727227 · Fuselage Main, Floor Beam
  > CORROSION FLOORBEAM MAIN CABIN BS 560, LBL10 CUT-OUT DAMAGED AREA IAW SRM 53-10-8 FIG 3, FABRICATED CHORD FAB 2 EA SUPPORT ANGLES, FAB 2 EA REINFORCEMENT STRAP IAW SRM 53-10-8 FIG REV 102, INSTALLED FLOORBEAM REPAIR AT BS 560 LBL 10 IAW SRM 51-30-2 REV 102.
- [SDR FDEA201002160437](https://openairdocs.org/sdr/FDEA201002160437.md): Skin · chafed · Feb 16, 2010 · N482FE · Boeing 727227 · Elevator, Plate/Skin
  > LT ELEVATOR INSIDE NR 5 BALANCE BAY, GOUGE ON UPPER PANEL, OTBD END. REMOVED DAMAGE BY STOP DRILLING GOUGE ON UPPER PANEL INSIDE NR 5 BALANCE BAY FOR LT ELEVATOR IAW SRM 51-10-1, REV 102. COMPLIED WITH HFEC INSP IAW NDTM 51-00-00, FIGURE 23, WITH NO DEFECTS
- [SDR FDEA201002150433](https://openairdocs.org/sdr/FDEA201002150433.md): Structure · cracked · Feb 15, 2010 · N482FE · Boeing 727227 · Trailing Edge Flaps
  > LT INBD MID FLAP LOWER AFT CLOSE OUT CHORD WBL 106 IS CRACKED AT ACT ROD CUTOUT. CUT OUT DAMAGED SECTION DIM 47 1/4 " LONG IAW SRM 51-40-4 FIG 1. FABRICATED LOWER CHORD AND SPLICE IAW SRM 51-40-4 FIG 4. LOCATED AND DRILLED HOLES IAW SRM 51-30-5. INSTALLED LOW
- [SDR FDEA201002150432](https://openairdocs.org/sdr/FDEA201002150432.md): Skin · cracked · Feb 15, 2010 · N482FE · Boeing 727227 · Trailing Edge Flaps
  > RT INBD FORE FLAP, STA 224, CRACK ON THE SKIN, L/E, FWD OF ATTACH FITTING. CUT OUT DAMAGED AREA IAW SRM 57-50-4 FIG 1. FABRICATED DOUBLER AND FILLER IAW SRM 57-50-4 FIG 1. INSTALLED DOUBLER AND FILLER IAW SRM 51-30-2.
- [SDR FDEA201002150431](https://openairdocs.org/sdr/FDEA201002150431.md): Floorbeam · corroded · Feb 15, 2010 · N482FE · Boeing 727227 · Fuselage Main, Floor Beam
  > FWD LAV AREA - CORROSION ON FLOOR SUPPORT ANGLE AT BS 328 FROM BL 0 TO LBL 55, UPPER AND LOWER SURFACES. CUT OUT DAMAGED AREA APPROX DIM 2" IAW SRM 53-10-8 FIG 9. FABRICATED REPAIR FLOORBEAM. FABRICATED ANGLES 2. FABRICATED 2 ANGLES IAW SRM 53-10-8 FIG 9.
- [SDR FDEA201002150430](https://openairdocs.org/sdr/FDEA201002150430.md): Angle · cracked · Feb 15, 2010 · N482FE · Boeing 727227 · Fuselage Miscellaneous Structure
  > AFT AIRSTAIRS RT LOWER TORQUE BOX TEE ANGLE CRACKED AT BS 1263, AFT SIDE. REMOVED RT LOWER TORQUE BOX TEE ANGLE IAW SRM, REV 102, 51-30-2. LOCATED, DRILLED AND DEBURRED HOLES ON NEW TEE ANGLE IAW SRM 51-30-5. INSTALLED NEW TEE ANGLE IAW SRM 51-30-2.
- [SDR FDEA201002130425](https://openairdocs.org/sdr/FDEA201002130425.md): Door Frame · cracked · Feb 13, 2010 · N482FE · Boeing 727227 · Fuselage Main, Structure
  > BS 783, RT OVERWING FRAME, STR 17R, CRACK ORIGINATING FROM FASTENER HOLE. STOP DRILLED CRACK, FABRICATED REPAIR ANGLE, STRAP, SPLICE ANGLE, NEW CHANNEL, AND INSTALLED REPAIR PARTS IAW SRM 51-10-1, SRM 51-30-2, SRM 51-30-5, SRM 51-10-2, ER NR 2-37153-0801 REV
- [SDR FDEA201002130422](https://openairdocs.org/sdr/FDEA201002130422.md): Seat Track · corroded · Feb 13, 2010 · N482FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK NUMEROUS AREAS MAIN CABIN BS 690 TO BS 720E 10 INCHES, RBL 45. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK, FABRICATED ANGLE SPLICES AND STRAP SPLICES IAW SRM 53-10-5 FIG 1. TREATED AND PRIMED REPAIR PARTS IAW
- [SDR FDEA201002120418](https://openairdocs.org/sdr/FDEA201002120418.md): Floorbeam · corroded · Feb 12, 2010 · N482FE · Boeing 727227 · Fuselage Main, Floor Beam
  > AFT CARGO, BL 0 FLOORBEAM REPAIR, SCREW HOLES CORRODED, 3EA AT RBL5, STA 1070. REMOVED FLOORBEAM REPAIR LOWER STRAP IAW SRM 51-30-2. FABRICATED NEW STRAP IAW SRM 53-10-8 FIG 2. TREATED AND PRIMED NEW STRAP IAW SRM 51-10-2 INSTALLED NEW STRAP IAW SRM 53-10-
- [SDR FDEA201002120414](https://openairdocs.org/sdr/FDEA201002120414.md): Web · cracked · Feb 12, 2010 · N482FE · Boeing 727227 · Fuselage Miscellaneous Structure
  > AFT AIRSTAIR RT LOWER TORQUE BOX WEB IS CRACKED AT UPPER LIGHTING HOLE BS 1243. STOP DRILLED CRACK AT LOWER RIGHT LIGHTING HOLE IAW SRM 51-10-1 AND 51-40-2. COMPLIED WITH HFEC INSPECTION IAW NDTM PT6 51-00-00, FIG. 23, AND VERIFIED CRACK ENDS AT STOP DRILL.
- [SDR FDEA201002120413](https://openairdocs.org/sdr/FDEA201002120413.md): Web · cracked · Feb 12, 2010 · N482FE · Boeing 727227 · Fuselage Main, Structure
  > AFT AIRSTAIR RT LOWER TORQUE BOX WEB IS CRACKED AT LOWER LIGHTING HOLE BS1223. STOP DRILLED CRACK AT RT LOWER LIGHTING HOLE IAW SRM 51-10-1 AND 51-40-2 FIG 1. HFEC INSP IAW NDTM PT6 51-00-00 FIG 23 VERIFIED CRACK ENDS AT STOP DRILL. FABRICATED NEW DOUBLER IAW
- [SDR FDEA201002120417](https://openairdocs.org/sdr/FDEA201002120417.md): Support Angle · cracked · Feb 12, 2010 · N482FE · Boeing 727227 · Fuselage Miscellaneous Structure
  > AFT AIRSTAIR RT LOWER TORQUE BOX, SUPPORT ANGLE IS CRACKED AT FASTENER, BS 1263, ON AFT SIDE. REMOVED RT LOWER TORQUE BOX SUPPORT ANGLE IAW SRM, REV 102, 51-30-2. FORMED SUPPORT ANGLE IAW DWG NR 65-17517. HEAT TREATED GUSSET TO T-6 CONDITION IAW ENGINEERING R
- [SDR FDEA201002120416](https://openairdocs.org/sdr/FDEA201002120416.md): Support Angle · cracked · Feb 12, 2010 · N482FE · Boeing 727227 · Fuselage Miscellaneous Structure
  > AFT AIRSTAIR RT LOWER TORQUE BOX, SUPPORT ANGLE HAS CRACK INDICATION AND WORKING FASTENERS. BS 1263, FWD SIDE. REMOVED RT TORQUE BOX WEB DOUBLER FROM BS1243 TO 1283 IAW SRM, REV 102, 51-30-2. CUT WEB AT BS 1263 IAW SRM 51-10-1. REMOVED RT LOWER TORQUE BOX A
- [SDR FDEA201002120415](https://openairdocs.org/sdr/FDEA201002120415.md): Support Angle · cracked · Feb 12, 2010 · N482FE · Boeing 727227 · Fuselage Miscellaneous Structure
  > AFT AIRSTAIR LT LOWER TORQUE BOX, SUPPORT ANGLE IS CRACKED AT RIVET, BS 1250. REMOVED SUPPORT ANGLE FROM AFT AIRSTAIR LT LOWER TORQUE BOX AT BS 1250 IAW SRM, REV 102, 51-30-2. FABRICATED SUPPORT ANGLE IAW DWG NR 65-17516 AND BAC 1517-1457. INSTALLED SUPPORT A
- [SDR FDEA201002110397](https://openairdocs.org/sdr/FDEA201002110397.md): Skin · gouged · Feb 11, 2010 · N482FE · Boeing 727227 · Fuselage Main, Plate/Skin
  > EVALUATE EXTERNAL SKIN REPAIR BS 360, STR 17L, DIM: 25 1/2 X 20 IAW EO 7-5100-7-5005, PT1. REMOVED PREVIOUS REPAIR DOUBLER, HFEC AND AND UT INSP IAW NDTM 51-00-00 AND FOUND SKIN GOUGED, CUT OUT DAMAGED AREA IAW SRM 51-10-1, HFEC INSPECTED. CUTOUT AND HOLES W
- [SDR FDEA201002110396](https://openairdocs.org/sdr/FDEA201002110396.md): Stringer · corroded · Feb 11, 2010 · N482FE · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > AFT CARGO STA 1030, STR 26R CORRODED. REMOVED 2" SECTION OF DAMAGED STRINGER AND FABRICATED FILLER AND STRINGER REPAIR SPLICE IAW SRM 53-10-2 FIGURE 9 AND 53-10-3 FIGURE 1 DETAIL 1. INSTALLED SPLICE AND FILLER IAW SRM 51-30-2, REV. 102.

Next page: https://openairdocs.org/deregistered/N482FE-2015-07-02/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 = 'N482FE' AND deregistration_id = 'N482FE-2015-07-02'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N482FE-2015-07-02/reports

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