# Service difficulty reports: N204FE, cancelled Oct 1, 2015

A list on [N204FE, cancelled Oct 1, 2015](https://openairdocs.org/deregistered/N204FE-2015-10-01.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 · 70 reports

- [SDR FDEA201307051482](https://openairdocs.org/sdr/FDEA201307051482.md): Light · inoperative · Jul 5, 2013 · N204FE · Boeing 7272S2F · Emergency Lighting
  > ON SERVICE CHECK, FOUND L1 DOOR EXIT LIGHT INOPERATIVE. R & R L1 DOOR EMERGENCY LIGHT, REF AMM 33-50-101-2. OPS CHECKED GOOD. ACFT OK TO CONTINUE.
- [SDR FDEA201305060923](https://openairdocs.org/sdr/FDEA201305060923.md): Battery Pack · inoperative · May 6, 2013 · N204FE · Boeing 7272S2F · Emergency Lighting
  > FOUND EMERGENCY LIGHT ABOVE MAIN ENTRY DOOR INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERIES IAW MM 33-50-101-2. OPS CHECKED NORMAL. OK FOR SERVICE.
- [SDR FDEA201303010488](https://openairdocs.org/sdr/FDEA201303010488.md): Transmitter · malfunctioned · Mar 1, 2013 · N204FE · Boeing 7272S2F · Hydraulic Indicating System
  > DURING FLAP RETRACTION, SYS A PRESSURE DECREASED TO APROX 1000 PSI FROM FLAPS 5 -2 PRESSURE DECREASED. ENG 1 A PUMP LIGHT ILLUMINATED INT AND WITH FLAP RETRACTION SYS A QTY WAS JUST UNDER 1 GAL, COMPLIED WITH QRH RETURNED IND. INSPECTED ACFT FOR LEAKS, NO
- [SDR FDEA201211073901](https://openairdocs.org/sdr/FDEA201211073901.md): Battery Pack · inoperative · Nov 7, 2012 · N204FE · Boeing 7272S2F · Emergency Lighting
  > EMERGENCY EXIT LIGHT ABOVE COCKPIT DOOR DOES NOT ILLUMINATE DURING BATTERY AND STANDBY POWER CHECK. R & R BATTERIES IN EMERGENCY EXIT LIGHT ABOVE COCKPIT DOOR IAW AMM 33-50-101-2, OPS CHECKED GOOD.
- [SDR FDEA201209293512](https://openairdocs.org/sdr/FDEA201209293512.md): Hinge · damaged · Sep 29, 2012 · N204FE · Boeing 7272S2F · Passenger/Crew Doors
  > LOUD SQUEL COMING FROM AREA UPPER FRONT SIDE OF COCKPIT NEXT TO S/O PANEL. CLOSING CARGO OUTFLOW VALVE HAS NO EFFECT. STARTED DURING CLIMB AROUND 250. WENT AWAY AT LEVEL OFF AT 350 THEN IMMEDIATELY CAME BACK. CONTINUED TO 370. ALL PRESSURIZATION INDICATI
- [SDR FDEA201208183072](https://openairdocs.org/sdr/FDEA201208183072.md): Battery Pack · failed · Aug 18, 2012 · N204FE · Boeing 7272S2F · Emergency Lighting
  > L1 DOOR EMERGENCY EXIT LIGHTS LT SIDE, LIGHT INOPERATIVE. BATTERY PACK ONLY READS 1.3VDC, REMOVED AND REPLACED EMERGENCY EXIT LIGHT POWER SUPPLY LIGHTS. OPS CHECKED NORMAL IAW MM 33-50-051-2.
- [SDR FDEA201207282729](https://openairdocs.org/sdr/FDEA201207282729.md): Bottle · discharged · Jul 28, 2012 · N204FE · Boeing 7272S2F · Extinguishing System
  > LEFT "BOTTLE DISCHARGED" LIGHT ILLUMINATED ON OVERHEAD PANEL. R & R LT ENGINE FIRE EXTINGUISHER BOTTLE IAW MM 26-21-001-4 AND PERFORMED INSPECTION CHECK IAW MM26-21-001-6. OPS NORMAL.
- [SDR FDEA201206062104](https://openairdocs.org/sdr/FDEA201206062104.md): Door · out of adjust · Jun 6, 2012 · N204FE · Boeing 7272S2F · Passenger/Crew Doors
  > ON LANDING, FWD ENTRY DOOR LIGHT ILLUMINATED ON S/O PANEL VISUAL INSPECTION, DURING SHUTDOWN VERIFIED FWD ENTRY DOOR WAS SLIGHTLY AJAR. ADJUSTED UPPER LINK ARM AND ALIGNED TORQUE TUBES REF 52-11-001-5. START WITH C. STEP (8). ADJUSTED IAW STEP 3. FORWARD
- [SDR FDEA201206022057](https://openairdocs.org/sdr/FDEA201206022057.md): Warning Light · false activation · Jun 2, 2012 · N204FE · Boeing 7272S2F · Door Warning System
  > ON LANDING, FWD ENTRY DOOR LIGHT ON S/O PANEL ILLUMINATED. VISUAL INSPECTION DURING SHUTDOWN, CHECKLIST VERIFIED FWD ENTRY DOOR WAS SLIGHTLY AJAR. OPS CHECK OF FWD ENTRY DOOR WARNING SWITCH CHECKED GOOD REF AMM CH 52-70-001-5.
- [SDR FDEA201205302014](https://openairdocs.org/sdr/FDEA201205302014.md): Door · out of adjust · May 30, 2012 · N204FE · Boeing 7272S2F · Passenger/Crew Doors
  > DURING CLIMB, PASSING 2000 AGL. FWD ENTRY ANNUNCIATOR LIGHT ON, SO PANEL ANNUNCIATED. RAN QRH. INSPECTED DOOR HANDLE AND LIGHT EXTINGUISHED. PRESSURIZATION OK THROUGHOUT. CONTINUED IAW QRH. FOUND LT ENTRY DOOR NOT LATCHING IN DETENT. ADJUSTED DOOR TO CO
- [SDR FDEA201205231937](https://openairdocs.org/sdr/FDEA201205231937.md): Door · out of adjust · May 23, 2012 · N204FE · Boeing 7272S2F · Passenger/Crew Doors
  > FWD ENTRY DOOR HANDLE MOVED SLIGHTLY TOWARD OPEN DURING LANDING AND FWD ENTRY DOOR LIGHT ILLUMINATED. ADJUSTED FWD ENTRY DOOR FOR SOFT UNLATCHING AND OPS CHECKED FWD ENTRY DOOR OK IAW MM 52-11-001-5.
- [SDR FDEA201204171447](https://openairdocs.org/sdr/FDEA201204171447.md): Light · loose · Apr 17, 2012 · N204FE · Boeing 7272S2F · Emergency Lighting
  > EMERGENCY EXIT LIGHT CAME LOOSE ON LANDING. RE-INSTALLED LIGHT IAW AMM 33-50-001-2-0. OPS NORMAL.
- [SDR FDEA201112285452](https://openairdocs.org/sdr/FDEA201112285452.md): Wire · damaged · Dec 28, 2011 · N204FE · Boeing 7272S2F · Flight Control System Wiring
  > UPON INTIAL FLAP RETRACTION FROM 5 DEG TO 2 DEG, NR6 L/E FLAP DID NOT RETRACT, QRH PROCEDURE RAN WITH NO SUCCESSFUL RETRACTION. ON TAXI-IN, FLAP HANDLE BROUGHT UP AND NR6 L/E FLAP STILL INDICATED EXTENDED. TROUBLE SHOT TO WIRES AT CONNECTOR D916. BUILT UP A
- [SDR FDEA201110124477](https://openairdocs.org/sdr/FDEA201110124477.md): Battery Pack · inoperative · Oct 12, 2011 · N204FE · Boeing 7272S2F · Emergency Lighting
  > EMERGENCY EXIT LIGHT INOPERATIVE DURING STBY POWER TEST OVER COCKPIT DOOR & OVER MAIN ENTRANCE DOOR. REPLACED EMERGENCY EXIT LIGHTS BATTERY IAW SMP. OPS CHECKED GOOD. AC OK FOR SERVICE.
- [SDR FDEA201109224037](https://openairdocs.org/sdr/FDEA201109224037.md): Door · out of adjust · Sep 22, 2011 · N204FE · Boeing 7272S2F · Passenger/Crew Doors
  > UPON LANDING THE FWD ENTRY LIGHT ON THE SO DOOR WARNING PANEL ILLUMINATED. ON INSPECTION, CREW FOUND CREW ENTRY DOOR TO BE OPEN AND UNSECURED. PERFORMED ADJUSTMENT TEST REF AMM 52-11-001-5 NO DEFECTS NOTED. ACFT OK TO CONTINUE SERVICE.
- [SDR FDEA201109113992](https://openairdocs.org/sdr/FDEA201109113992.md): Door · unsecure · Sep 11, 2011 · N204FE · Boeing 7272S2F · Passenger/Crew Doors
  > UPON LANDING THE FWD ENTRY LIGHT ON THE SO DOOR WARNING PANEL ILLUMINATED. UPON INSP, CREW FOUND CREW ENTRY DOOR TO BE OPEN AND UNSECURED. PERFORMED ADJUSTMNET TEST REF AMM 52-11-001-5. NO DEFECTS NOTED. OK FOR SERVICE.
- [SDR FDEA201105111800](https://openairdocs.org/sdr/FDEA201105111800.md): Engine · overheated · May 11, 2011 · N204FE · Boeing 7272S2F · Engine (Turbine/Turboprop)
  > NR 2 ENG FIRE LIGHT AT 340, BOTH BOTTLES FIRED AFTER FOLLOWING QRH. FIRE DEPT INDICATED NR 2 ENG HAD SIGNIFICANT HEAT SIGNATURE. R & R NR 2 ENG FIRE SENSING ELEMENTS BOTH BOTTOM & TOP. INSTALLED SQUIBS & FIRE BOTTLES. C/W HIGH POWER RUN.
- [SDR FDEA201012214734](https://openairdocs.org/sdr/FDEA201012214734.md): Fire Loop · dirty · Dec 21, 2010 · N204FE · Boeing 7272S2F · Fire Detection
  > RECEIVED NR 1 ENGINE FIRE INDICATION ON FINAL APPROACH WITH POWER AT IDLE. SYS TESTED OK & ENGINE WAS SHUTDOWN AND BOTTLE DISCHARGED IAW CHECKLIST. FIRE WARNING SYS STILL DID NOT SILENCE UNTIL ON THE GROUND & NR 1 ENGINE DET "B" CB PULLED. EMERGENCY VEHICLE
- [SDR FDEA201010033888](https://openairdocs.org/sdr/FDEA201010033888.md): Smoke Warning · false activation · Oct 3, 2010 · N204FE · Boeing 7272S2F · Fire Detection
  > DURING FLIGHT, LOWER AFT CARGO SMOKE AND ARMED LIGHT ILLUMINATE WITH ASSOCIATED BELL. THIS OCCURED 10 SECONDS AFTER WING ANTI-ICE SELECTED OPEN. LIGHT WENT OUT AFTER THE BOTTLE WAS DISCHARGED AND THE SYSTEM TESTED GOOD. REMOVED FWD/AFT CARGO COMPARTMENT L
- [SDR FDEA201009263714](https://openairdocs.org/sdr/FDEA201009263714.md): Seat Track · corroded · Sep 26, 2010 · N204FE · Boeing 7272S2F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK AT BS 495 LBL 45 INBD FLANGE LOWER SURFACE IS CORRODED.
- [SDR FDEA201009253710](https://openairdocs.org/sdr/FDEA201009253710.md): Seat Track · gouged · Sep 25, 2010 · N204FE · Boeing 7272S2F · Fuselage, Seat/Cargo Attach Fittings
  > AFT CABIN STA 1150-1160 BL0 AFT SEAT TRACK SECTION HAS GOUGES AND DAMAGE AROUND SEVERAL SCALLOPS.
- [SDR FDEA201009243705](https://openairdocs.org/sdr/FDEA201009243705.md): Stiffener · cracked · Sep 24, 2010 · N204FE · Boeing 7272S2F · Nacelle/Pylon Miscellaneous Structure
  > NR 1 ENGINE NOSE COWL EXTERIOR AFT BACKSIDE BULKHEAD I/B AT 5 O'CLOCK POSITION VERTICAL ANGLE STIFFENER SUPPORT IS CRACKED AT TOP END REMOVED VERTICAL STIFFENER NR 1 ENG NOSE COWL AFT AT 5 O'CLOCK BULKHEAD IAW SRM REV 103 51-30-2 FABRICATED NEW STIFFENER FROM
- [SDR FDEA201009233660](https://openairdocs.org/sdr/FDEA201009233660.md): Nose Cowl · damaged · Sep 23, 2010 · N204FE · Boeing 7272S2F · Nacelle/Pylon, Main Frame
  > DAMAGE BOTTOM NR 3 NOSE COWL. REMOVED AND REPLACED NR 3 ENGINE NOSE COWL IAW MM 71-10-021-4. REFERENCE NON-ROUTINE N00917 WORK ORDER 00049152.
- [SDR FDEA201009223663](https://openairdocs.org/sdr/FDEA201009223663.md): Seat Track · damaged · Sep 22, 2010 · N204FE · Boeing 7272S2F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK AT BS 500-510 BL 0 HAS BROKEN SCALLOPS. REMOVED SEAT TRACK SECTION AT STA 360 TO 550 BL0, FABRICATED SEAT TRACK FROM BAC 1520-1331 7178-T6511 DIM. 189 1/2", TREATED AND PRIMED SEAT TRACK, AND INSTALLED SEAT TRACK AND SPLICE IAW SRM 51-30-
- [SDR FDEA201009223666](https://openairdocs.org/sdr/FDEA201009223666.md): Seat Track · damaged · Sep 22, 2010 · N204FE · Boeing 7272S2F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK SEAT TRACK BS 835 LBL 45 HAS BROKEN SCALLOP. REMOVED AND REPLACE SEAT TRACK SECTION FROM BAC 1520-1331 7178-T6511 DIM 95 1/8" IAW SRM 51-30-2, 51-10-1, 53-10-2 FIG 7, 51-20-2 FIG 21, 51-30-5, AND 51-10-2 AT BS 760 TO 850 RBL 45.
- [SDR FDEA201009223653](https://openairdocs.org/sdr/FDEA201009223653.md): Skin · gouged · Sep 22, 2010 · N204FE · Boeing 7272S2F · Leading Edge Devices
  > NR 2 SLAT LOWER T/E SKIN GOUGED AT O/B SLAT HOOK AREA TRIMMED OUT DAMAGED AREA DIM: 1/2" X 1/2" IAW SRM 51-10-1. FABRICATED REPAIR PLATE FROM 2024 T-3.125" DIM: 4" X 6" IAW SRM 57-50-3 FIG 10. INSTALLED REPAIR PLATE IAW SRM 51-30-2, REV 103.
- [SDR FDEA201009203664](https://openairdocs.org/sdr/FDEA201009203664.md): Seat Track · damaged · Sep 20, 2010 · N204FE · Boeing 7272S2F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK AT BS 680-700, LBL 62.5 HAS DAMAGED SCALLOPS. CUT OUT DAMAGED AREA BS 656 TO 728 LBL 62.5, FABRICATED NEW SECTION, SPLICE REPAIR, ANGLES, AND FILLERS IAW SRM 53-10-5 FIG 1. INSTALLED REPAIR IAW SRM 53-10-5 FIG 1.
- [SDR FDEA201009173521](https://openairdocs.org/sdr/FDEA201009173521.md): Web · cracked · Sep 17, 2010 · N204FE · Boeing 7272S2F · Fuselage Miscellaneous Structure
  > AFT AIRSTAIRS LT LOWER TORQUE BOX INBD WEB HAS CRACK AT LIGHTING HOLE BS 1220. TRIMMED OUT DAMAGED AREA DIM. 3/4" X 3/8" IAW SRM 51-10-1. FABRICATED REPAIR DOUBLER FROM 7075T6 0.032" DIM. 4" X 2" IAW SRM 53-10-2 FIG 6 AND 51-40-2 FIG 1. INSTALLED REPAIR D
- [SDR FDEA201009163511](https://openairdocs.org/sdr/FDEA201009163511.md): Shear Tie · corroded · Sep 16, 2010 · N204FE · Boeing 7272S2F · Fuselage Internal Mounting Structure
  > CORROSION ON SHEAR TIE AT BS 950E BETWEEN STRINGERS 29R AND 28R. FABRICATED NEW STUB FRAME FROM 7075 0.040" DIM 22" X 5" IAW SRM 51-10-3 AND 51-20-1 FIG 7 REV 103. REMOVED SHEAR TIE AT BS 950E BETWEEN STR 29R AND 28R IAW SRM 51-30-2 AND REINSTALLED SHEAR
- [SDR FDEA201009153526](https://openairdocs.org/sdr/FDEA201009153526.md): Floorbeam · corroded · Sep 15, 2010 · N204FE · Boeing 7272S2F · Fuselage Main, Floor Beam
  > MAIN CABIN FLOORBEAM AT BS 400 BETWEEN LBL 45 AND 25 UPPER I BEAM TOP AND BOTTOM SURFACE IS CORRODED. CUT OUT DAMAGED AREA IAW SRM 53-10-8 FIG 3. FABRICATED REPAIR PARTS. INSTALLED REPAIR IAW SRM 53-10-8 FIG 3 AND 51-10-2.
- [SDR FDEA201009143414](https://openairdocs.org/sdr/FDEA201009143414.md): Frame Splice · damaged · Sep 14, 2010 · N204FE · Boeing 7272S2F · Fuselage Main, Frame
  > UPON FRAME REMOVAL, FOUND DOUBLE DRILLED HOLES IN FRAME SPLICE, STA 950B, STR 24L. REMOVED PRODUCTION SPLICE/DOUBLER IAW SRM 51-30-2 FORMED NEW DOUBLER IAW SRM 51-20-1 FIG 7 INSTALLED NEW DOUBLER IAW SRM 51-30-2 REV 103.
- [SDR FDEA201009133422](https://openairdocs.org/sdr/FDEA201009133422.md): Floorbeam · corroded · Sep 13, 2010 · N204FE · Boeing 7272S2F · Fuselage Main, Floor Beam
  > CORROSION ON UPPER FLANGE OF FLOORBEAM AT BS 344 FROM LBL 10 TO RBL 10. REMOVED DAMAGED AREA 8' SECTION IAW SRM 53-10-8 AND 51-30-2. FABRICATED REPAIR TEE SECTION, ANGLES, AND SHIMS IAW SRM 53-10-8 FIG 9 DETAIL 1. INSTALLED REPAIR PARTS IAW SRM 51-30-2 AND 5
- [SDR FDEA201009103343](https://openairdocs.org/sdr/FDEA201009103343.md): Attach Angle · cracked · Sep 10, 2010 · N204FE · Boeing 7272S2F · Wing, Attach Fittings
  > LT WING FALSE SPAR ATTACH ANGLE IS CRACKED WBL 118. REMOVED DOUBLER AND CUT OUT LOWER CHORD IAW DRAWING SR27-57-038 REV C. FABRICATED REPAIR ANGLES, NEW WEB, NEW I/B CHORD SECTION, NEW STRAP, RADIUS FILLERS, AND NEW WEB IAW DRAWING SR 27-57-038 REV C. INS
- [SDR FDEA201009093329](https://openairdocs.org/sdr/FDEA201009093329.md): Keelbeam · cracked · Sep 9, 2010 · N204FE · Boeing 7272S2F · Fuselage Main, Keel
  > RT WW, RT KEEL BEAM IS CRACKED AT BS 875 RBL10 TRIMMED OUT DAMAGED AREA AT LOWER CHORD OF KEEL BEAM STA 875 RBL 6 IAW SRM 51-10-1. FABRICATED DOUBLER FROM PN 15-5PH 0.071" DIM. 8.6250' X 4" AND INSTALLED DOUBLER IAW EA 7-5310-135591.
- [SDR FDEA201009083316](https://openairdocs.org/sdr/FDEA201009083316.md): Stringer · corroded · Sep 8, 2010 · N204FE · Boeing 7272S2F · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 29L BETWEEN BS 950D AND 950E. REMOVED AND REPLACED STRINGER 29L FROM BS 950 - 1010 IAW B727 SRM 53-10-2 FIG 9, 51-30-5 AND 51-30-2 REV 103
- [SDR FDEA201009043277](https://openairdocs.org/sdr/FDEA201009043277.md): Skin · corroded · Sep 4, 2010 · N204FE · Boeing 7272S2F · Fuselage Main, Plate/Skin
  > UPON REMOVAL OF STRINGER SECTION, FOUND SKIN CORRODED, BS 1030 AFT OF FRAME AT STRINGER 26R. CUT OUT DAMAGED AREA AT BS 1045 DIM 9" X 3" IAW B727 SRM 53-30-3 FIG 5 FABRICATED DOUBLER, FILLER, AND SKIN FILLER IAW 53-30-3 FIG 5 REV 103, INSTALLED REPAIR
- [SDR FDEA201009033341](https://openairdocs.org/sdr/FDEA201009033341.md): Skin · corroded · Sep 3, 2010 · N204FE · Boeing 7272S2F · Fuselage Main, Plate/Skin
  > SKIN BULGE STA 1173 AT LAP SEAM STR 20R. COMPLIED WITH EA 7-5330-135593.
- [SDR FDEA201009033269](https://openairdocs.org/sdr/FDEA201009033269.md): Stringer · corroded · Sep 3, 2010 · N204FE · Boeing 7272S2F · Fuselage Main, Longeron/Stringer
  > STRINGER 26L AT BS 1040-1055 IS CORRODED AT LOWER SURFACED. CUT OUT DAMAGED STRINGER FROM STA 1040 TO 1055 IAW SRM 53-10-1 FIG 1. FABRICATED STRINGER FROM BAC1498-147 7075T6 DIM 15 7/8" AND 2EA SPLICES FROM BAC1498-131 7075T6 DIM 12 1/4". INSTALLED REPAIR
- [SDR FDEA201009033266](https://openairdocs.org/sdr/FDEA201009033266.md): Web · cracked · Sep 3, 2010 · N204FE · Boeing 7272S2F · Fuselage Miscellaneous Structure
  > AFT AIRSTAIRS RT LOWER TORQUE BOX INBD WEB HAS CRACK AT LIGHTING HOLE BS 1303. TRIMMED OUT DAMAGED AREA DIM. 1" X 1/2" IAW SRM 51-10-1. FABRICATED REPAIR DOUBLER IAW SRM 53-10-2 FIG 6 AND 51-40-2 FIG 1. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2.
- [SDR FDEA201009033265](https://openairdocs.org/sdr/FDEA201009033265.md): Web · cracked · Sep 3, 2010 · N204FE · Boeing 7272S2F · Fuselage Miscellaneous Structure
  > AFT STAIRWELL LT LOWER TORQUE BOX INBD WEB IS CRACKED AT LIGHTING HOLE BS 1223. TRIMMED OUT DAMAGED AREA DIM. 1/2" X 1/4" AND 1/2" X 1/8" IAW SRM 51-10-1. FABRICATED REPAIR DOUBLERS. IAW SRM 53-10-2 FIG 6 AND 51-40-2 FIG 1. INSTALLED REPAIR DOUBLERS IAW S
- [SDR FDEA201009033268](https://openairdocs.org/sdr/FDEA201009033268.md): Skin · bulged · Sep 3, 2010 · N204FE · Boeing 7272S2F · Fuselage Main, Plate/Skin
  > SKIN BULGE STA 1052, STR 26L, LAP SEAM. CUT OUT LOWER SKIN DIM. 2" X 2" AT STA 1052 STR 26L LAP SEAM. FABRICATED REPAIR FROM 2024T3 0.071" DIM. 9.750" X 9", DOUBLER FROM 2024T3 0.063" DIM. 11" X 5", AND FILLER FROM 2024T3 0.050" DIM. 2" X 2". IAW SRM 53-30-
- [SDR FDEA201009023342](https://openairdocs.org/sdr/FDEA201009023342.md): Skin · cracked · Sep 2, 2010 · N204FE · Boeing 7272S2F · Fuselage Main, Plate/Skin
  > RT LOWER AFT FUSELAGE AT BS 1010 STR 28R EXTERIOR SKIN IS CRACKED AND BULGING. CUT OUT DAMAGED AREA IAW SRM 53-30-3 FIG 3A REV 103. FABRICATED REPAIR DOUBLER AND FILLER IAW EA 7-5330-135592. INSTALLED REPAIR DOUBLER AND FILLER IAW EA 7-5330-135592.
- [SDR FDEA201009023272](https://openairdocs.org/sdr/FDEA201009023272.md): Skin · bulged · Sep 2, 2010 · N204FE · Boeing 7272S2F · Fuselage Main, Plate/Skin
  > SKIN BULGE STA 1045 STR 26R LAP SEAM. REMOVED CORRODED STRINGER SECTION FROM BS 1026 TO 1070, STR 26R IAW SRM 51-30-2. FABRICATED 3 (EA) STRINGER SECTIONS FROM BAC1498-147 7075 T62 DIM 19" AND 4 (EA) SPLICE SECTIONS FROM BAC1498-131 7075 T6 DIM 9" IAW SRM 53
- [SDR FDEA200902070480](https://openairdocs.org/sdr/FDEA200902070480.md): Indicator · burned · Feb 7, 2009 · N204FE · Boeing 7272S2F · Indicating/Recording System
  > AT FLIGHT LEVEL 390 SMELLED FUMES IN COCKPIT. DECLARED AN EMERGENCY AND LANDED AT DEN AIRPORT. MED BRAKE WAS USED AND EMERGENCY EGRESS CONDUCTED. FSFO CHECKLIST EXECUTED. ISOLATED BURNED ODOR TO FLT ENGINEERS PANEL AND FOUND NR 3 ENGINE OIL QUANTITY IND I
- [SDR FDEA200901200268](https://openairdocs.org/sdr/FDEA200901200268.md): Indicator · failed · Jan 20, 2009 · N204FE · Boeing 7272S2F · Airspeed/Mach Indicator
  > F/O AIRSPEED INDICATOR FAILED: NEEDLE STOPPED AT 200 KTS AND OFF FLAG, RESTORED THEN SECOND FAILURE AT 250 KTS AND OFF FLAG. REMOVED AND REPLACED NR 2 AIRSPEED INDICATOR. SYS CKS NORMAL. NO LEAKS NOTED IAW 727 M/M 34-12-000-5. PREMATURE REMOVAL/INSTALLATIO
- [SDR FDEA200812025037](https://openairdocs.org/sdr/FDEA200812025037.md): Actuator · broken · Dec 2, 2008 · N204FE · Boeing 7272S2F · Door Warning System
  > AFT AIRSTAIR LIGHT ILLUMINATED IN-FLIGHT CLIMBING THROUGH 4,500 FEET. ACN RELEASED FOR SERVICE PER MEL/CDL: 52-06-B. AMBER AFT AIRSTAIR DOOR WARNING LIGHT INOP." REPLACED WARN RT HAND UPLOCK ROLLER FITTING PER SMP, FOUND SWITCH S395 ROLLER ACTUATOR BROKEN A
- [SDR 07FDEA04548](https://openairdocs.org/sdr/07FDEA04548.md): Transmitter · loose · Oct 10, 2007 · N204FE · Boeing 7272S2F · Engine Oil Quantity
  > NR 2 LOW OIL PRESSURE FILTER BYPASS LIGHT ILLUMINATED IN DESCENT FOLLOWED BY OIL PRESSURE DROP TO ZERO. QRH PERFORMED, ENGINE SHUT DOWN WITH OIL PRESSURE AT 5 TO 10 PSI OIL QUANTITY NORMAL. TEMP RISING GRADUALLY ENGINE SHUTDOWN 13 MINUTES AFTER FIRST INDICAT
- [SDR 05FDEA02424](https://openairdocs.org/sdr/05FDEA02424.md): Window · delaminated · Aug 11, 2005 · N204FE · Boeing 7272S2F · Flight Compartment Windows
  > UPPER PORTION OF WINDOW R1 IS DELAMINATING, AND A BUBBLING FLUID IS PRESENT INSIDE THE DELAM, R1 OUTER PANE CRACKED. REMOVED AND REPLACED RT NR 1 WINDSHIELD PER MM 56-11-011-4. REMOVED AND REPLACED WINDOW HEAT CONTROLLER PER MM 30-41-02, PRECAUTIONARY R/I.
- [SDR 05FDEA02124](https://openairdocs.org/sdr/05FDEA02124.md): Pump · failed · Jul 28, 2005 · N204FE · Boeing 7272S2F · Hydraulic Pump (Electric/Engine), Main
  > HYD SYS B OVERHEAT LIGHT IN FLT TURNED ELEC PUMP NR 1 OFF AND LIGHT WENT OUT. REMOVED AND REPLACED NR 1 B PUMP PER MM-29-12-011-2. OPS CKS AND LEAK CKS GOOD. CYCLED ALL FLIGHT CONTROLS ON B SYS TO ENSURE NO AIR IN SYSTEM. NOTE, CASE DRAIN ALSO REMOVED AND
- [SDR 05FDEA01866](https://openairdocs.org/sdr/05FDEA01866.md): Flap · jammed · Jul 8, 2005 · N204FE · Boeing 7272S2F · Trailing Edge Flap Control System
  > ASYMETRICAL INBOARD TRAILING EDGE FLAPS AT 2 DEGREES UPON FLAP RETRACTION. RAN APPROPRIATE QRH PROCEDURES, FOUND LT INBD FLAP COCKED AND JAMMED INTO INBD AILERON. UPON FURTHER TROUBLESHOOTING FOUND BEARING WALKED OUT OF SCREWSHAFT END OF LT INBD TRANSMISSION.

Next page: https://openairdocs.org/deregistered/N204FE-2015-10-01/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 = 'N204FE' AND deregistration_id = 'N204FE-2015-10-01'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N204FE-2015-10-01/reports

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OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.