# Service difficulty reports: N288FE, cancelled Aug 27, 2013

A list on [N288FE, cancelled Aug 27, 2013](https://openairdocs.org/deregistered/N288FE-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 · 88 reports

- [SDR FDEA201208313201](https://openairdocs.org/sdr/FDEA201208313201.md): Slide · damaged · Aug 31, 2012 · N288FE · Boeing 7272D4 · Escape Slide
  > INDIVIDUAL EXPULTED THE EVACUATION SLIDE. R & R L1 DOOR ESCAPE SLIDE IAW MM 25-60-015-2.
- [SDR FDEA201207292814](https://openairdocs.org/sdr/FDEA201207292814.md): Battery Pack · discharged · Jul 29, 2012 · N288FE · Boeing 7272D4 · Emergency Lighting
  > FOUND EMERGENCY LIGHTS ARMED AND ACFT POWER OFF. BOTH COCKPIT AND ENTRY EMERGENCY LIGHTS, AND EXTERIOR DOOR SLIDE LIGHT INOPERATIVE. REPLACED BATTERIES IAW MM 33-50-001-0. REPLACED EXTERIOR DOOR SLIDE POWER SUPPLY IAW 33-50-051-2. ALL LIGHTS OPS CHECKED NOR
- [SDR FDEA201203030767](https://openairdocs.org/sdr/FDEA201203030767.md): Slide · dislodged · Mar 3, 2012 · N288FE · Boeing 7272D4 · Escape Slide
  > ESCAPE SLIDE FELL OUT OF CONTAINER. REINSTALLED DOOR MOUNTED ESCAPE SLIDE IAW AMM 25-60-015-2. ACFT OK FOR SERVICE.
- [SDR FDEA201109284194](https://openairdocs.org/sdr/FDEA201109284194.md): Skin · misrepaired · Sep 28, 2011 · N288FE · Boeing 7272D4 · Fuselage Main, Plate/Skin
  > FWD ENTRY DOOR UPPER HINGE MISREPAIRED. FABRICATED DOUBLER, TRIPLER, AND STRUCTURAL FILLER, AND INSTALLED IAW EA 7-5330-152453.
- [SDR FDEA201109214017](https://openairdocs.org/sdr/FDEA201109214017.md): Web · cracked · Sep 21, 2011 · N288FE · Boeing 7272D4 · Cargo/Baggage Doors
  > CARGO DOOR INNER WEB IS CRACKED AT LIGHTING HOLE NEAR LEADING EDGE. CUT OUT DAMAGED AREA IAW SRM 51-10-1 REV103. FABRICATED REPAIR DOUBLER IAW SRM 52-00-3 FIG 3 AND 52-30-1 FIG 7. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2 AND EA 7-5230-152450.
- [SDR FDEA201109183952](https://openairdocs.org/sdr/FDEA201109183952.md): Skin · gouged · Sep 18, 2011 · N288FE · Boeing 7272D4 · Trailing Edge Flaps
  > LEFT WING OTBD FLAP INBD FAIRING AREA HAS A GOUGE ON L/E SKIN. CUT OUT DAMAGED AREA IAW SRM 51-10-1 AND 57-10-4 FIG 2. FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 57-50-4 FIG 1. INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 57-50-4 FIG 1 AND EA 7-5750-
- [SDR FDEA201109163900](https://openairdocs.org/sdr/FDEA201109163900.md): Skin · gouged · Sep 16, 2011 · N288FE · Boeing 7272D4 · Trailing Edge Flaps
  > RIGHT WING I/B FOREFLAP O/B L/E GOUGED. FABRICATED AND INSTALLED REPAIR IAW SRM 57-50-4 FIG 1 REV 103
- [SDR FDEA201109103815](https://openairdocs.org/sdr/FDEA201109103815.md): Shear Tie · corroded · Sep 10, 2011 · N288FE · Boeing 7272D4 · Fuselage Internal Mounting Structure
  > CORROSION ON SHEAR TIE AT BS 950E BETWEEN STRINGERS 29R AND 28R. REMOVED SHEAR TIE IAW SRM 51-30-2. FABRICATED NEW SHEAR TIE IAW SRM 51-20-1 FIG 7 AND DWG 65-56129 INSTALLED NEW SHEAR TIE IAW SRM 51-30-2 REV 103.
- [SDR FDEA201109083748](https://openairdocs.org/sdr/FDEA201109083748.md): Shear Tie · damaged · Sep 8, 2011 · N288FE · Boeing 7272D4 · Fuselage Internal Mounting Structure
  > IMPROPER SPACING BETWEEN FASTENERS IN SHEAR TIE AT BS 950A, FORWARD AND AFT, BETWEEN STR 29R AND 28R. REMOVED SHEAR TIE IAW SRM 51-30-2 LOCATED,DRILLED AND DEBURRED NEW SHEAR TIE IAW SRM 51-30-5 INSTALLED SHEAR TIE IAW SRM 51-30-2
- [SDR FDEA201109073745](https://openairdocs.org/sdr/FDEA201109073745.md): Vertical Beam · damaged · Sep 7, 2011 · N288FE · Boeing 7272D4 · Fuselage Miscellaneous Structure
  > 1183 BULKHEAD HAS INSUFFICIENT FASTENER SPACING ON VERTICAL BEAM, LBL 17.8. TRIMMED DAMAGED AREA AT STA 1183 BULKHEAD 3EA AND AFT FLANGE VERTICAL BEAM LBL 17.8, FABRICATED DOUBLER REPAIR, FILLERS, TEE SECTION, SPLICE REPAIRS AND INSTALLED DOUBLER REPAIR,
- [SDR FDEA201109073746](https://openairdocs.org/sdr/FDEA201109073746.md): Skin · gouged · Sep 7, 2011 · N288FE · Boeing 7272D4 · Fuselage Main, Plate/Skin
  > SKIN BS 720C, STR 28L IS GOUGED. REPAIRED.
- [SDR FDEA201109073760](https://openairdocs.org/sdr/FDEA201109073760.md): Skin · damaged · Sep 7, 2011 · N288FE · Boeing 7272D4 · Fuselage Main, Plate/Skin
  > SKIN, BS 464 ABOVE STR 26L HAS A DRILL START. ACCOMPLISHED REPAIR ON NR N00405.
- [SDR FDEA201109073759](https://openairdocs.org/sdr/FDEA201109073759.md): Skin · misrepaired · Sep 7, 2011 · N288FE · Boeing 7272D4 · Fuselage Main, Plate/Skin
  > SKIN MISREPAIRED AT BS 460, STR 24 TO 26L. CUT OUT DAMAGED SKIN, DOUBLER, AND TRIPLER. FABRICATED STRUCTURAL FILLER, DOUBLER, TRIPLER, AND FILLERS. INSTALLED REPAIR PARTS IAW SRM 53-30-3, FIG 1B.
- [SDR FDEA201109073744](https://openairdocs.org/sdr/FDEA201109073744.md): Skin · gouged · Sep 7, 2011 · N288FE · Boeing 7272D4 · Fuselage Main, Plate/Skin
  > BS 720 BELOW S28L SKIN IS GOUGED ABOVE LT RAM AIR DUCT. CUT OUT GOUGED AREA OF SKIN IAW SRM 53-30-3 FIG 3. FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 53-30-3 FIG 3. INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-30-3 FIG 3 REV 103.
- [SDR FDEA201103010804](https://openairdocs.org/sdr/FDEA201103010804.md): Switch · failed · Mar 1, 2011 · N288FE · Boeing 7272D4 · Leading Edge Slat Control System
  > AFTER TAKEOFF LEADING EDGE FLAPS FAILED TO INDICATE RETRACTED. FE PANEL SHOWED NR 2 LED NOT RETRACTED. FOUND SWITCH S203 FROZEN AND VERY HARD TO MOVE. REPLACE SWITCH 203 REF WDM27-81-02 AND MM 27-82-001-4. OPS CHECK NORMAL ACFT OK FOR SERVICE.
- [SDR FDEA201008293174](https://openairdocs.org/sdr/FDEA201008293174.md): Light · failed · Aug 29, 2010 · N288FE · Boeing 7272D4 · Emergency Lighting
  > DURING MAINT PRE-DEPARTURE CHECKS OF EMERGENCY EXIT LIGHTING, NOTED THAT EXIT LIGHT OVER L1 DOOR IS DIM AND FLICKERING. REMOVED COVER AND SWITCHED LIGHT "ON" IT IS BRIGHT & STEADY. REMOVED LIGHT AND AGAIN, BRIGHT AND STEADY ON BATTERY PACK. WHEN INSTALLED IN
- [SDR FDEA201008173014](https://openairdocs.org/sdr/FDEA201008173014.md): Gyro · failed · Aug 17, 2010 · N288FE · Boeing 7272D4 · Attitude Gyro and Indicating System
  > DURING FLT, HSI SHOWS HDG FLAG RAN QRH HSI WORKS WHEN SWITCHED TO BOTH ON 2. DIVERTED TO ALTERNATE STA R & R NR 1 DG IAW M/M 34-21-071-4-0. OPS CHECK NORMAL, OK FOR SVC. ACFT IS NOT CAT II IAW GMM 6-5-400, CAT II CHECK.
- [SDR FDEA200903180955](https://openairdocs.org/sdr/FDEA200903180955.md): Floorbeam · corroded · Mar 18, 2009 · N288FE · Boeing 7272D4 · Fuselage Main, Floor Beam
  > MAIN CARGO DECK FLOORBEAM UPPER "T " BS 1130 HAS CORROSION BETWEEN LBL25 AND LBL46. CUTOUT CORRODED SECTION IAW SRM 53-10-8 FIG 10 (SHEET 9). HFEC INSPECTED IAW NTM 51-00-19 PT.6, NO CRACK INDICATION NOTED. FABRICATED FILLER FROM 7075-T6.156. FABRICATED D
- [SDR FDEA200903120909](https://openairdocs.org/sdr/FDEA200903120909.md): Floorbeam · corroded · Mar 12, 2009 · N288FE · Boeing 7272D4 · Fuselage Main, Floor Beam
  > MAIN CARGO DECK FLOORBEAM AT STA 720A HAS CORROSION AND SCRIBE MARKS ON UPPER " T " SECTION BETWEEN LBL25 AND RBL25. REMOVED DAMAGED AND CORRODED SECTION IAW SRM 53-10-8 FIG 3, FABRICATED REPAIR PARTS ON TRAVELERS T9/783984,T9/783989,T9/784001,T9/783983,AND
- [SDR FDEA200903120908](https://openairdocs.org/sdr/FDEA200903120908.md): Frame · cracked · Mar 12, 2009 · N288FE · Boeing 7272D4 · Fuselage Main, Frame
  > FUSELAGE FRAME STA 890 OUTER CHORD CRACKED AT STRINGER 14R. REMOVED DAMAGE IAW SRM 51-30-2. FABRICATED NEW ANGLE AND NEW DOUBLER IAW SRM 53- 10-2 AND TRAVELERS NR T9/783599 ANDT9/783600, LOCATED AND DRILLED ANGLE AND ANGLE DOUBLER IAW SRM 51-30-2. INSTALLE
- [SDR FDEA200903110901](https://openairdocs.org/sdr/FDEA200903110901.md): Seat Track · corroded · Mar 11, 2009 · N288FE · Boeing 7272D4 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK LBL 25 CORRODED ON NUMEROUS LOCATIONS FROM STA 500-690. REMOVED SEAT TRACK IAW SRM 51-30-2, FABRICATED NEW SEAT TRACK FROM 60-6549/24 BATCH NR 1514987 LOCATED AND DRILLED IAW SRM 51-30-2. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED NEW SEAT TR
- [SDR FDEA200903100879](https://openairdocs.org/sdr/FDEA200903100879.md): Floorbeam · corroded · Mar 10, 2009 · N288FE · Boeing 7272D4 · Fuselage Main, Floor Beam
  > MAIN CARGO DECK FLOORBEAM UPPER TEE BS 1130 HAS CORROSION BETWEEN LBL 0 AND LBL 13. REMOVED CORROSION ON FLOORBEAM UPPER TEE BS 1130 BETWEEN LBL 0 AND LBL 13 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-8 FABBED 3 (EA) FILLERS AND NEW ANGLE P/N BAC 1505/100393 IA
- [SDR FDEA200903090875](https://openairdocs.org/sdr/FDEA200903090875.md): Floorbeam · corroded · Mar 9, 2009 · N288FE · Boeing 7272D4 · Fuselage Main, Floor Beam
  > LAVATORY AREA FLOORBEAM AT STA 328 HAS CORROSION AT APPROX RBL 36 ON THE UPPER CHORD FWD EDGE (MARKED) REMOVED CORROSION 0.080 ORIGINAL 0.025 MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-10-1. CUT OUT DAMAGE AND FABRICATED REPAIR ON TRAVELER T9/783
- [SDR FDEA200903090874](https://openairdocs.org/sdr/FDEA200903090874.md): Floorbeam · corroded · Mar 9, 2009 · N288FE · Boeing 7272D4 · Fuselage Main, Floor Beam
  > MAIN CARGO DECK FLOORBEAM UPPER 'T' BS 1030 HAS CORROSION BETWEEN LBL 0 AND LBL 25 FABRICATED ANGLES REPAIRS FOR FLOORBEAM UPPER 'T' ON MAE TRAVELER T9/783860 IAW WITH SRM 53-10-8, FABRICATED 2 FILLERS BATCH NR 000104977, TREATED AND PRIMED ANGLES REPAIRS, FIL
- [SDR FDEA200903080864](https://openairdocs.org/sdr/FDEA200903080864.md): Bulkhead · corroded · Mar 8, 2009 · N288FE · Boeing 7272D4 · Fuselage Main, Bulkhead
  > AFT CARGO LT SIDE OF 1183 BULKHEAD FWD FACE DOME NUT AT LBL 27 HAS CORROSION ON IT AND ON SKIN 6 O'CLOCK POS UNDER AIR DUCT (INNER MOST). REMOVED CORROSION IAW SRM 51-10-6 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1 FIG 1 SH2 NOTE C. FABRICATED REPAIR DOUBLER
- [SDR FDEA200903080863](https://openairdocs.org/sdr/FDEA200903080863.md): Seat Track · corroded · Mar 8, 2009 · N288FE · Boeing 7272D4 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK LBL 45 CORRODED ON NUMEROUS LOCATIONS FROM STA 500 - 690. REMOVED AND REPLACED DAMAGED SEAT TRACK SECTION FROM STA 500 - 690 LBL 45 IAW SRM 51305, FABRICATED FROM PN 60-6549/24 BATCH NR 1514987.
- [SDR FDEA200903070861](https://openairdocs.org/sdr/FDEA200903070861.md): Seat Track · corroded · Mar 7, 2009 · N288FE · Boeing 7272D4 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK LBL 0 CORRODED ON NUMEROUS LOCATIONS FROM STA 500 - 575. INSTALLED NEW SEAT TRACK SECTION IAW SRM 51-30-2 BS 500 TO 580, REINSTALLED 4 STRAPS IAW SRM 51-30-2, FABRICATED SEAT TRACK SECTION ON MAE TRAV NR T9/ 82953, BATCH NR 0001541987, LOCATED AND
- [SDR FDEA200903050850](https://openairdocs.org/sdr/FDEA200903050850.md): Skin · canning · Mar 5, 2009 · N288FE · Boeing 7272D4 · Fuselage Main, Plate/Skin
  > AFT CARGO BILGE SKIN OIL CANNING BETWEEN STA 1100 AND 1130, HAS WORKING RIVETS AT STR 27L, STR 28L, AND STR 29L. CUT-OUT DAMAGED AREA IAW SRM 53-30-3 FIG 3, FABBED FILLERS IAW SRM 53-30-3. FABBED DOUBLER IAW SRM 53-30-3 LOCATED AND DRILLED IAW SRM 51-30-5 AN
- [SDR FDEA200902270762](https://openairdocs.org/sdr/FDEA200902270762.md): Bulkhead · cracked · Feb 27, 2009 · N288FE · Boeing 7272D4 · Fuselage Main, Bulkhead
  > NOSE LANDING GEAR BULKHEAD STA NR 351.20 HAS 3 CRACKS MIGRATING FROM 1 FASTENER HOLE ATTACHING THE NOSE GEAR LOCK ACTUATOR FITTING TO BULKHEAD. IN CORRECT TAIL NUMBER ENTERED IN BLOCK 1C, PLEASE SEE SDR 09-0763 FOR AIRCRAFT N482FE.
- [SDR FDEA200810284587](https://openairdocs.org/sdr/FDEA200810284587.md): Controller · malfunctioned · Oct 28, 2008 · N288FE · Boeing 7272D4 · Windshield/Door Rain/Ice Removal
  > L1 WINDOW HEAT FAILED EN ROUTE. TURNED OFF AND BACK ON SEVERAL TIMES BUT WINDOW HEAT CONTINUED TO FAIL. CHECKED/RESET BOTH L1 AC AND DC CONTROL PER MOCC. NO HELP. WINDOW VERY COLD. ACN RELEASED FOR SERVICE PER MEL/CDL: 30-15-A CATEGORY: C. REPLACED BROKE
- [SDR 08FDEA04587](https://openairdocs.org/sdr/08FDEA04587.md): Heater · inoperative · Oct 28, 2008 · N288FE · Boeing 7272D4 · Windshield/Door Rain/Ice Removal
  > L1 WINDOW HEAT FAILED EN ROUTE. TURNED OFF AND BACK ON SEVERAL TIMES BUT WINDOW HEAT CONTINUED TO FAIL. CHECKED/RESET BOTH L1 AC AND DC CONTROL PER MOCC. NO HELP. WINDOW VERY COLD. RELEASED FOR SERVICE PER MEL/CDL: 30-15-A CATEGORY: C EXPIRATION: 07NOV08
- [SDR 05FDEA04173](https://openairdocs.org/sdr/05FDEA04173.md): Switch · misinstalled · Dec 8, 2005 · N288FE · Boeing 727200 · Door Warning System
  > AFT AIRSTAIR AMBER LT ILLUMINATED PRIOR TO BLOCKOUT- ADJUSTED BY MAINTENANCE WHEN AFT AIRSTAIR AMBER LT ILLUMINATED IN FLIGHT- RAN QRH RED TABS. ENT BY: 353958 MEL 08DEC05 10:15 IND ACN RELEASED FOR SERVICE PER MEL/CDL: 52-06-B CAT: C EXP: 16DEC05 C/
- [SDR 05FDEA03962](https://openairdocs.org/sdr/05FDEA03962.md): Switch · malfunctioned · Nov 26, 2005 · N288FE · Boeing 727200 · Door Warning System
  > AMBER AFT AIRSTAIR LIGHT ILLUMINATED DURING CLIMB THROUGH 27,000 MSL. ACCOMPLISHED QRH. LANDED UNEVENTFULLY. OPENED AFT AIRSTAIRS, CLEANED SWITCHES, AND CHECKED DOOR WARNING SYSTEM PER M/M 52-70-001-5. OPS CHECKS NORMAL. OK FOR SERVICE.
- [SDR 05FDEA03313](https://openairdocs.org/sdr/05FDEA03313.md): Uplock Switch · malfunctioned · Oct 8, 2005 · N288FE · Boeing 7272D4 · Entrance Stairs
  > AMBER AIRSTAIR LIGHT ON S/O PANEL CAME ON IN FLIGHT. CHECKED A/C ON ARRIVAL, FOUND DOOR UP AND LOCKED. RAN DOOR SEVERAL TIMES. LIGHT STAYED ON ON FIRST TRY. ADJUSTED UPLOCK SWITCH ON LEFT AND RIGHT SIDE UPLOCK SWITCHES, PER AMM 52-62-001-5. OPS CHECK NORM
- [SDR 05FDEA03161](https://openairdocs.org/sdr/05FDEA03161.md): Line · cracked · Sep 29, 2005 · N288FE · Boeing 727200 · Pneumatic Distribution System
  > AT 800' AGL AND 180 KIAS NR 2 FIRE LIGHT ILLUMINATED PERFORMED PHASE 1 AND CHECKLIST LANDED UNEVENTFULLY.
- [SDR 04FDEA00413](https://openairdocs.org/sdr/04FDEA00413.md): Skin · gouged · Feb 16, 2004 · N288FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERNAL SKIN IS GOUGED AT BS 1143 JUST 3 INCHES ABOVE STRINGER 12 LT.
- [SDR 04FDEA00412](https://openairdocs.org/sdr/04FDEA00412.md): Skin · gouged · Feb 16, 2004 · N288FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERNAL SKIN HAS GOUGES AT BS 1149 BETWEEN STRINGER 6 & 7 LT. SKIN AT BS 1149 BETWEEN STR 6 & 7 LT WAS FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGE & REPAIRED SKIN PER FED EX EA 7-5330-55232.
- [SDR 04FDEA00374](https://openairdocs.org/sdr/04FDEA00374.md): Beam · corroded · Feb 9, 2004 · N288FE · Boeing 727200 · Fuselage Main, Structure
  > CORROSION, STA 760 BL 0 WL 148, DELTA BEAM LWR L-ANGLE HAS CORROSION. ACCESSED DELTA BEAM WEB. REMOVED L-ANGLE AND FOUND L-ANGLE OUT OF LIMITS. FABRICATED NEW L-ANGLE, INSTALLED ANGLE AND REINSTALLED ACCESSED DELTA BEAM WEB FASTENERS AND DME NR 2 ANTENNA CL
- [SDR 04FDEA00373](https://openairdocs.org/sdr/04FDEA00373.md): Stringer · corroded · Feb 9, 2004 · N288FE · Boeing 727200 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STR 24L BS 306. REMOVED DAMAGE ON STR 24L BS 306. DAMAGE FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR PARTS. ALODINED, PRIMED AND INSTALLED IAW SRM 51-30-2, 53-10-3.
- [SDR 04FDEA00332](https://openairdocs.org/sdr/04FDEA00332.md): Stringer · cracked · Feb 6, 2004 · N288FE · Boeing 727200 · Vertical Stabilizer, Spar/Rib
  > VERTICAL STAB LT STRINGER CRACKED, FIN STA 157.2 STR NR 7 FROM TOP, AT BOLT HOLE. REPAIRED CRACKED STRINGER NR 7L FIN STA 157.2 PER SRM 55-30-4 FIG 1.
- [SDR 04FDEA00331](https://openairdocs.org/sdr/04FDEA00331.md): Floorbeam · corroded · Feb 6, 2004 · N288FE · Boeing 727200 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM AT FLOOR PANEL FASTENER HOLES BS 400 LBL 10 - RBL 10. REMOVED CORROSION IN A 1.0 X2.0 X.038 AREA. ORIG THICKNESS IS.125, TOP CHORD IS OUT OF LIMITS PER SRM 53-10-1. CUT-OUT DAMAGED UPPER CHORD PER SRM 53-10-8. FABRICATED CHORD
- [SDR 04FDEA00330](https://openairdocs.org/sdr/04FDEA00330.md): Floorbeam · corroded · Feb 6, 2004 · N288FE · Boeing 727200 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM BS 360 LBL 17 - RBL 7 WL 208. FOUND CORROSION ON FLOORBEAM BS 360, LBL 17 TO RBL 17 WL 208 TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED FLOORBEAM IAW SRM 53-10-8 FIG 8.
- [SDR 04FDEA00286](https://openairdocs.org/sdr/04FDEA00286.md): Floorbeam · corroded · Feb 2, 2004 · N288FE · Boeing 727200 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM AT FASTENER HOLES BS 344 LBL 59 - RBL 17 WL 208. REMOVED CORROSION AREAS 77 X 2 X.040 INCHES FROM ORIGINAL.100. FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPALCED UPPER CHORD OF FLOORBEAM BS 344 LBL 65 TO RBL 65 PER SRM 51-30-
- [SDR 04FDEA00285](https://openairdocs.org/sdr/04FDEA00285.md): Skin · corroded · Feb 2, 2004 · N288FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > CORROSION IN FWD CARGO BAY, CORROSION ON INNER SURFACE OF SKIN STA 684 BETWEEN STR 27 LT AND 28 LT. FOUND CORROSION ON SKIN AT BS 684, STR 27L AND 28L TO BE.015 DEEP X 4 X 6 INCHES FROM AN ORIGINAL THICKNESS OF.050 AND IS OUT OF LIMITS IAW SRM 53-30-3. CUT
- [SDR 04FDEA00246](https://openairdocs.org/sdr/04FDEA00246.md): Floorbeam · corroded · Jan 29, 2004 · N288FE · Boeing 727200 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM BS 380 LBL 8-55 WL 208. BLENDED CORROSION ON BS 380 FLOORBEAM PER SRM 51-10-1. FOUND LBL 8 OUT OF LIMITS PER SRM 53-10-1. CUT OUT DAMAGED AREA PER SRM 53-10-8. FABRICATED REPAIR PARTS PER SRM 53-10-8. APPLIED ALODINE AND PRIMER TO CU
- [SDR 04FDEA00235](https://openairdocs.org/sdr/04FDEA00235.md): Frame · dented · Jan 28, 2004 · N288FE · Boeing 727200 · Fuselage Main, Frame
  > FWD CARGO BAY, FRAME DENTED STA 660 STR 24 LT. CUT OUT DENTED MATERIAL FROM FRAME AT BS 660, STR 24L AND PER SRM 51-40-3, 53-10-1, USING 7075-T6,.050 LOT #466242. CUT OUT WAS 1X1
- [SDR 04FDEA00241](https://openairdocs.org/sdr/04FDEA00241.md): Beam · corroded · Jan 28, 2004 · N288FE · Boeing 727200 · Fuselage Main, Structure
  > LEFT A/C BAY, DELTA BEAM LWR PLATE HAS CORROSION AT STA 800 LBL 6 WL 140. REMOVED CORROSION ON DELTA BEAM LWR PLATE AT BS 800, LBL 6, WL 140 IN A 2.500X1.00X.029 DEEP. FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED AREA 2.00X.500X.090. FABRICATED FILLER
- [SDR 04FDEA00240](https://openairdocs.org/sdr/04FDEA00240.md): Floorbeam · corroded · Jan 28, 2004 · N288FE · Boeing 727200 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM BS 1110, RBL 22, WL 208. CUT OUT CORRODED SECTION OF FLOORBEAM'S TOP CHORD BS 1110 WL 208 RBL 8-23 AND INSTALLED REPAIR ANGLES, TEE CHORD AND STRAPS PER SRM 53-10-8.
- [SDR 04FDEA00237](https://openairdocs.org/sdr/04FDEA00237.md): Floorbeam · corroded · Jan 28, 2004 · N288FE · Boeing 727200 · Fuselage Main, Floor Beam
  > CORROSION ON FLOOR BEAM AT FLOOR PANEL FASTENER HOLE BS 440, LBL 7.75 - 10.75 (100 PERCENT MATERIAL LOSS). REMOVED DAMAGE AREA OF TOP FLANGE OF FLOORBEAM AT BS 440. FABRICATED, ALODINE, PRIMED, PAINTED AND INSTALLED REPAIR IAW SRM 53-10-8.
- [SDR 04FDEA00236](https://openairdocs.org/sdr/04FDEA00236.md): Frame · dented · Jan 28, 2004 · N288FE · Boeing 727200 · Fuselage Main, Frame
  > FWD CARGO BAY, FRAME DENTED STA 680 STR 23 LT COMING CUT OUT DENTED MATERIAL 1 X 1 INCH FROM FRAME AT BS 680 STR 23L AND REPAIRED PER SRM 53-10-1, 51-40-3 USING 7075-T6.050 LOT #466242.

Next page: https://openairdocs.org/deregistered/N288FE-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 = 'N288FE' AND deregistration_id = 'N288FE-2013-08-27'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N288FE-2013-08-27/reports

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