# Service difficulty reports: N213FE, cancelled May 5, 2014

A list on [N213FE, cancelled May 5, 2014](https://openairdocs.org/deregistered/N213FE-2014-05-05.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 · 73 reports

- [SDR FDEA201212114315](https://openairdocs.org/sdr/FDEA201212114315.md): Slide · dislodged · Dec 11, 2012 · N213FE · Boeing 7272S2F · Escape Slide
  > DURING CLOSING FORWARD ENTRY DOOR, ESCAPE SLIDE DROPPED OUT FROM BOTTOM OF RETAINING CASE. REINSTALLED ENTRY DOOR SLIDE IAW AMM 25-60-015-2. CHECKS GOOD FOR SECURITY.
- [SDR FDEA201212054249](https://openairdocs.org/sdr/FDEA201212054249.md): Module · malfunctioned · Dec 5, 2012 · N213FE · Boeing 7272S2F · Overheat Detection
  > CLIMBING THROUGH 4000' MSL LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED, RAN QRH LIGHT DID NOT EXTINGUISH, RTB. LIGHT DID NOT EXTINGUISH UNTIL IN CHOCKS, SHUTTING DOWN ALL ENGINES. R & R OVERHEAT PROTECTION MODULE IAW SMP, PERFORMED TEST IAW MM REF. 26-14-000-
- [SDR FDEA201110254640](https://openairdocs.org/sdr/FDEA201110254640.md): Skin · damaged · Oct 25, 2011 · N213FE · Boeing 7272S2F · Fuselage Main, Plate/Skin
  > SKIN HAS 2 EA DOUBLE DRILLED HOLES AT BS 970 BETWEEN STRINGERS 24L AND 25L. CUT OUT DAMAGED SKIN IAW SRM 53-30-3, FIG 1. FABRICATED FILLER AND REPAIR DOUBLER IAW SRM 53-30-3, FIG 1. TREATED AND PRIMED REPAIR PARTS IAW SRM 51-10-2. INSTALLED REPAIR FILLER A
- [SDR FDEA201110184645](https://openairdocs.org/sdr/FDEA201110184645.md): Web · cracked · Oct 18, 2011 · N213FE · Boeing 7272S2F · Wing Miscellaneous Structure
  > LT WING FIXED L/E INTERIOR, INBD MOUNT ANGLE FOR NR 1 SLAT ACTUATOR IS CRACKED. REMOVED CRACKED WEB IAW SRM 51-30-2. FABRICATED NEW WEB AND HEAT TREATED WEB TO 7076-T6 IAW EA 75740-152461. TREATED, PRIMED AND INSTALLED NEW WEB AT LT WING INBD MOUNT FOR NR 1
- [SDR FDEA201110174553](https://openairdocs.org/sdr/FDEA201110174553.md): Skin · gouged · Oct 17, 2011 · N213FE · Boeing 7272S2F · Fuselage Main, Plate/Skin
  > LEFT FUSELAGE SKIN GOUGED AT BS 720D PLUS 15" STRINGER 19L. CUT OUT DAMAGE, FABRICATED DOUBLER AND STRUCTURAL FILLER AND INSTALLED REPAIR IAW SRM 53-30-3 FIG 14.
- [SDR FDEA201110174552](https://openairdocs.org/sdr/FDEA201110174552.md): Skin · corroded · Oct 17, 2011 · N213FE · Boeing 7272S2F · Fuselage Main, Plate/Skin
  > CORROSION ON SKIN JUST OTBD OF STRINGER 28L FROM 990 TO 1030. CUTOUT AREA OUT OF LIMITS ON FUSELAGE SKIN DIMENSION 2.5 INCHES BY 1.8750 ", FABRICATED REPAIR DOUBLER FROM 2024T3.080, DIM 11.3750" BY 9.3750 " IAW SRM 53-30-2, FIG 2 AND 53-30-3, FIG 1. INSTALLE
- [SDR FDEA201110154511](https://openairdocs.org/sdr/FDEA201110154511.md): Skin · punctured · Oct 15, 2011 · N213FE · Boeing 7272S2F · Elevator, Plate/Skin
  > RIGHT ELEVATOR LOWER SKIN IS PUNCTURED. CUT OUT DAMAGE, FABRICATED REPAIR DOUBLER AND INSTALLED IAW SRM 55-20-3 FIG. 1. THIS REPAIR IS A CATEGORY B REPAIR.
- [SDR FDEA201110144505](https://openairdocs.org/sdr/FDEA201110144505.md): Spar · chafed · Oct 14, 2011 · N213FE · Boeing 7272S2F · Vertical Stabilizer, Spar/Rib
  > VERTICAL STAB RT MID SPAR CHORD IS CHAFED AT AFT END. REMOVED DAMAGED AREA IAW SRM 55-30-6 FIG 3. FABRICATED AND INSTALLED REPAIR ANGLE AND FILLERS IAW SRM 55-30-6 FIG 3.
- [SDR FDEA201110144501](https://openairdocs.org/sdr/FDEA201110144501.md): Shear Tie · misinstalled · Oct 14, 2011 · N213FE · Boeing 7272S2F · Fuselage Internal Mounting Structure
  > IMPROPER FASTENERS IN SHEAR TIE AT BS 970 BETWEEN S24-25L. REMOVED SHEAR TIE AND FAIRING SUPPORT FITTING IAW SRM 51-30-2. FABRICATED NEW SHEAR TIE IAW SRM 53-10-2 FIGURE 5 AND 51-30-05. LOCATED AND DRILLED NEW SHEAR TIE AND NEW FAIRING SUPPORT FITTING IAW
- [SDR FDEA201110144507](https://openairdocs.org/sdr/FDEA201110144507.md): Skin · damaged · Oct 14, 2011 · N213FE · Boeing 7272S2F · Nacelle/Pylon, Plate/Skin
  > NR 1 ENGINE NOSE COWL T/E SKIN DAMAGED 8 O'CLOCK POSITION. CUT OUT DAMAGED SKIN NOSE COWL NR 1 ENGINE IAW SRM 54-30-3 FIG 3A. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 54-30-3 FIG 3A.
- [SDR FDEA201110144504](https://openairdocs.org/sdr/FDEA201110144504.md): Shear Tie · corroded · Oct 14, 2011 · N213FE · Boeing 7272S2F · Fuselage Internal Mounting Structure
  > CORROSION ON SHEAR TIE AT BS 1148 BETWEEN STRINGER 30 AND 29R. CUT OUT DAMAGED SHEAR TIE IAW SRM 51-10-1 AND 53-10-4, FIG 15, FABRICATED NEW SHEAR TIE IAW SRM 53-10-4 FIG 15. INSTALLED SHEAR TIE IAW SRM 53-10-4, FIG 15.
- [SDR FDEA201110134463](https://openairdocs.org/sdr/FDEA201110134463.md): Seat Track · corroded · Oct 13, 2011 · N213FE · Boeing 7272S2F · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK INBD BS 373, LBL 60 HAS CORROSION. REMOVED CORROSION FROM SEAT TRACKIAW SRM 51-10-6. FOUND SEAT TRACK ASSY OUT OF LIMITS IAW B727 SRM 53-10-1 FIGURE 3. REMOVED SEAT TRACK IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK IAW SRM 51-30-5 AND 53-10-2 FIG
- [SDR FDEA201110124622](https://openairdocs.org/sdr/FDEA201110124622.md): Keelbeam · cracked · Oct 12, 2011 · N213FE · Boeing 7272S2F · Fuselage Main, Keel
  > RT KEELBEAM CHORD IS CRACKED AT 2ND FASTENER, BS 870, RBL 6, BELOW AND TO THE RT OF THE DUCTING. HFEC INSPECTED AREA AND VERIFIED CRACK, TRIMMED OUT CRACKED AREA AND FABRICATED REPAIR DOUBLER IAW EA 7-5310-152459. HEAT TREATED DOUBLER TO 177 KSI AND CAD PLAT
- [SDR FDEA201110124429](https://openairdocs.org/sdr/FDEA201110124429.md): Seat Track · corroded · Oct 12, 2011 · N213FE · Boeing 7272S2F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK UPPER OTBD FLANGE BS 515 TO 520, RBL 24 HAS CORROSION.
- [SDR FDEA201110124430](https://openairdocs.org/sdr/FDEA201110124430.md): Seat Track · corroded · Oct 12, 2011 · N213FE · Boeing 7272S2F · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK BS480 TO 560, LBL60 INBD FLANGE HAS CORROSION SEVERAL PLACES. REMOVED SEAT TRACK SECTION STA 480 - 655 IAW SRM 51-30-2, FABRICATED, LOCATED AND DRILLED NEW SEAT TRACK SECTION IAW SRM 53-10-2 FIG 7 AND 51-30-5. INSTALLED SEAT TRACK IAW
- [SDR FDEA201110124453](https://openairdocs.org/sdr/FDEA201110124453.md): Frame · corroded · Oct 12, 2011 · N213FE · Boeing 7272S2F · Fuselage Main, Frame
  > CORROSION ON STUB FRAME WEB AT BS 950E, PLUS 5 BOTH FWD AND AFT OF FRAME BETWEEN STRINGERS 29R AND 28R. REMOVED STUB FRAME BS 950E PLUS 5 IAW SRM 51-30-2 FABRICATED, LOCATED AND DRILLED NEW STUB FRAME IAW DRAWING 65-56129 AND SRM 51-30-5. INSTALLED NEW
- [SDR FDEA201110124432](https://openairdocs.org/sdr/FDEA201110124432.md): Floorbeam · corroded · Oct 12, 2011 · N213FE · Boeing 7272S2F · Fuselage Main, Floor Beam
  > CABIN FLOORBEAM BS 344 UPPER AFT. FLANGE LBL 24 TO 44 HAS CORROSION. UPPER TEE REPAIR ACCOMPLISHED ON NR NOO585.
- [SDR FDEA201110124427](https://openairdocs.org/sdr/FDEA201110124427.md): Floorbeam · corroded · Oct 12, 2011 · N213FE · Boeing 7272S2F · Fuselage Main, Floor Beam
  > FLOORBEAM BS 344, LBL 24- RBL24 CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW B727 SRM 51-10-6 AND 53-10-1 FIG.5. REMOVED UPPER TEE SECTIONS AND SPLICE REPAIR PARTS IAW SRM 51-30-2. FABRICATED NEW TEE SECTIONS IAW SRM 53-10-8 FIG. 9. TEATED, PR
- [SDR FDEA201110124433](https://openairdocs.org/sdr/FDEA201110124433.md): Frame · corroded · Oct 12, 2011 · N213FE · Boeing 7272S2F · Fuselage Main, Frame
  > CORROSION ON STUB FRAME WEB AT BS 950E PLUSE 5 INCHES, BOTH FWD AND AFT OF FRAME BETWEEN STRINGER 29R AND 28R.
- [SDR FDEA201110114431](https://openairdocs.org/sdr/FDEA201110114431.md): Floorbeam · corroded · Oct 11, 2011 · N213FE · Boeing 7272S2F · Fuselage Main, Floor Beam
  > FLOORBEAM WEB CORRODED BS 880, LBL 45 TO LBL 62. REMOVED CORROSION IAW SRM 51-10-6. NDT INSPECTED AFFECTED AREA IAW EA 7-5310-152465. TREATED AND PRIMED AFFECTED AREA IAW SRM 51-10-2, AND EA 7-5310-152465.
- [SDR FDEA201110104415](https://openairdocs.org/sdr/FDEA201110104415.md): Stringer · corroded · Oct 10, 2011 · N213FE · Boeing 7272S2F · Fuselage Main, Longeron/Stringer
  > STRINGER 4L HAS AREAS OF CORROSION BS 335 TO 360. REMOVED CORROSION IAW SRM 51-10-6. FOUND OUT OF LIMITS IAW SRM 53-10-1. CUT OUT DAMAGED SECTION IAW EA 3 7-5310-152464. FABRICATED NEW STRINGER SECTION AND SPLICE IAW EA 7-5310-152464. TREATED AND PRIMED NEW
- [SDR FDEA201110094393](https://openairdocs.org/sdr/FDEA201110094393.md): Spar · cracked · Oct 9, 2011 · N213FE · Boeing 7272S2F · Trailing Edge Flaps
  > RT WING, INBD FLAP, MOST INBD NR 2 HINGE AREA HAS REAR SPAR CHORD CRACKED AT CUT-OUT. CUT OUT DAMAGED SECTION OF SPAR IAW SRM 51-40-4 FIG 3. FABRICATED NEW SPAR SECTION AND SPLICE IAW SRM 51-40-4 FIG 3 AND 57-50-2 FIGURE 5. TREATED, PRIMED AND INSTALLED NE
- [SDR FDEA201110094392](https://openairdocs.org/sdr/FDEA201110094392.md): Spar · cracked · Oct 9, 2011 · N213FE · Boeing 7272S2F · Trailing Edge Flaps
  > RT WING, INBD FLAP, MID FLAP, MOST INBD NR1 HINGE AREA HAS REAR SPAR CRACKED AT CUT-OUT. REPAIRED SPAR.
- [SDR FDEA201108033082](https://openairdocs.org/sdr/FDEA201108033082.md): Light · inoperative · Aug 3, 2011 · N213FE · Boeing 7272S2F · Emergency Lighting
  > WHILE COCKING ACFT, FOUND COCKPIT EMERGENCY EXIT LIGHT INOP IN ARMED/ON POSITION. REPLACED LIGHT REF MM 33-50-101-2-0. GROUND OPS CK NORMAL AT THIS TIME. ACFT OK FOR SERVICE. PREMATURE REMOVAL/INSTALLATION.
- [SDR FDEA201106142247](https://openairdocs.org/sdr/FDEA201106142247.md): Actuator · failed · Jun 14, 2011 · N213FE · Boeing 7272S2F · Leading Edge Slat Actuator
  > NR 2 SLAT FAILED TO RETRACT. RAN QRH AND NO HELP IAW QRH, FLAPS SET TO 5 DEG AND THEN RAN CONFIGURED ON SCHEDULE FOR RTB MEM. DISCONNECTED THE CONNECTOR PLUG ON THE NR 2 LT SLAT ACTUATOR AND LIGHT WENT OUT. REMOVED NR 2 SLAT ACTUATOR AND CHECKED ADJUSTMENT
- [SDR FDEA201106092182](https://openairdocs.org/sdr/FDEA201106092182.md): Actuator · failed · Jun 9, 2011 · N213FE · Boeing 7272S2F · Leading Edge Slat Actuator
  > DURING FLAP RETRACTION, NR 2 SLAT REMAINED IN TRANSIT IAW QRH, EXTENDED FLAPS TO 2 DEGREES. HAD NORMAL INDICATIONS. RETRACTED FLAPS AGAIN AND NR 2 SLAT DID NOT RETRACT. ACFT APPEARED TO FLY NORMAL. NO UNDUE CROSS CORRECTION. INSTALLED NEW NR 2 ACTUATOR P
- [SDR FDEA201106092181](https://openairdocs.org/sdr/FDEA201106092181.md): Actuator · failed · Jun 9, 2011 · N213FE · Boeing 7272S2F · Leading Edge Slat Actuator
  > DURING FLAP RETRACTION, NR 2 SLAT REMAINED IN TRANSIT IAW QRH, EXTENDED FLAPS TO 2 DEGREES. HAD NORMAL INDICATIONS. RETRACTED FLAPS AGAIN AND NR 2 SLAT DID NOT RETRACT. ACFT APPEARED TO FLY NORMAL. NO UNDUE CROSS CORRECTION. INSTALLED NEW NR 2 ACCUATOR
- [SDR FDEA201010264168](https://openairdocs.org/sdr/FDEA201010264168.md): Slide · misaligned · Oct 26, 2010 · N213FE · Boeing 7272S2F · Escape Slide
  > DOOR SLIDE PRESSURE GAUGE UNREADABLE. REMOVED AND REPOSITIONED SLIDE IN DOOR COVER REF AMM 25-60-015-2-0.
- [SDR FDEA200902250718](https://openairdocs.org/sdr/FDEA200902250718.md): Engine · failed · Feb 25, 2009 · N213FE · Boeing 7272S2F · Engine (Turbine/Turboprop)
  > NR 3 ENG FIRE WARNING INDICATION. SHUT DOWN ENG IAW QRH. INDICATION PERSISTED. BLEW BOTH FIRE BOTTLES. INDICATION PERSISTED INTERMITTENTLY THROUGHOUT LANDING AND TAXI-IN. NR 3 ENG WINDMILLED FOR 6 MINS. UNABLE TO DETERMINE IF OIL PRESS WAS GREATER THAN 1
- [SDR FDEA200812025038](https://openairdocs.org/sdr/FDEA200812025038.md): Angle · cracked · Dec 2, 2008 · N213FE · Boeing 7272S2F · Wing Miscellaneous Structure
  > CRACKED LOWER ANGLE FALSE SPAR AT SPOILER NR 8 RT WING. REMOVED SPAR DOUBLER & INBD WEB SECTION IAW SRM 51-30-2. FABBED NEW DOUBLER IAW SRM 51-30-2 & DWG NR SR 27-57-038 REV C. FABBED NEW INBD WEB SECTION IAW DWG NR SR 27-57-038 REV C & SRM 51-30-2. FABBED
- [SDR 08FDEA04896](https://openairdocs.org/sdr/08FDEA04896.md): Skin · misrepaired · Nov 16, 2008 · N213FE · Boeing 7272S2F · Fuselage Main, Plate/Skin
  > SKIN AT STA 1290 STR 20R HAS TOOLING MARKS, FASTENERS WITH IMPROPER ED AND THE SKIN IS BULGING. REMOVED PREVIOUS REPAIR IAW B727 SRM 51-30-02. CUT-OUT DAMAGE PER B727 SRM 51-10-01, FABRICATED REPAIR DOUBLER IAW B727 SRM 53-30-3 & 53-30-2 FIG 3. FABRICATED
- [SDR 08FDEA00646](https://openairdocs.org/sdr/08FDEA00646.md): Wire Harness · burned · Feb 26, 2008 · N213FE · Boeing 7272S2F · Electrical Power System Wiring
  > WHILE WORKING WRI 31-30/9464, TECH FOUND A SHORTED WIRE HARNESS IN AVIONICS COMPT. THE 3 PHASE WIRE HARNESS FROM THE EXTERNAL POWER RELAY HAS MADE CONTACT WITH GND BUS STRIP T268 (LOCATED DIRECTLY ABOVE APU GCU). INITIAL VISUAL INSPECTION SHOWS SEVERAL GND S
- [SDR 07FDEA05001](https://openairdocs.org/sdr/07FDEA05001.md): Windshield · cracked · Dec 3, 2007 · N213FE · Boeing 7272S2F · Flight Compartment Windows
  > AT APPROX 27000' ON CLIMB-OUT, CAPT'S L-1 WINDOW CRACKED/SHATTERED AND BEGAN ARCING. COMPLIED WITH RED TABS PROCEDURES. RETURNED TO MEMPHIS. REMOVED CAPT'S NR 1 WINDOW AND COMPLIED WITH PREPARATION FOR INSTALL IAW B727-200 AMM 56-11-011-4. COMPLETED INSTAL
- [SDR 05FDEA04315](https://openairdocs.org/sdr/05FDEA04315.md): Unknown · ground damage · Dec 14, 2005 · N213FE · Boeing 7272S2F · Fuselage Main, Structure
  > AIRCRAFT DAMAGED ON PUSHBACK, ON BELLY. REPAIRED AND INSPECTED.
- [SDR 05FDEA03757](https://openairdocs.org/sdr/05FDEA03757.md): Repair · undamaged · Nov 10, 2005 · N213FE · Boeing 7272S2F · Fuselage Main, Plate/Skin
  > FOUND REPAIR STA 500-520 LT BOTTOM FUSELAGE SKIN, BELOW MAIN CARGO DOOR. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT FS 500-FS520 S24L-S25L WAS DETERMINED TO
- [SDR 05FDEA03756](https://openairdocs.org/sdr/05FDEA03756.md): Repair · undamaged · Nov 10, 2005 · N213FE · Boeing 7272S2F · Trailing Edge Flaps
  > FOUND REPAIR RT INBD FORE FLAP. LEADING EDGE REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION, AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA, PREVIOUSLY INSTALLED REPAIR AT RT INBD FORE FLAP WAS DETERMINED TO BE IAW SRM 57-50-4 FIG 1.
- [SDR 05FDEA03755](https://openairdocs.org/sdr/05FDEA03755.md): Repair · undamaged · Nov 10, 2005 · N213FE · Boeing 7272S2F · Wing Main, Frame Structure
  > FOUND REPAIR AT NR 4 L/E KRUGER FLAP, RT WING TOP SIDE. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT NR 4 L/E KRUGER FLAP, RT WING TOP SIDE WAS DETERMINED
- [SDR 05FDEA03754](https://openairdocs.org/sdr/05FDEA03754.md): Repair · damaged · Nov 10, 2005 · N213FE · Boeing 7272S2F · Trailing Edge Flaps
  > FOUND REPAIR LT I/B FORE FLAP, L/E REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT LT I/B, FORE FLAP WAS DETERMINED TO BE IAW SRM 57-50-4 FIG 1. BASED ON AN E
- [SDR 05FDEA03758](https://openairdocs.org/sdr/05FDEA03758.md): Repair · undamaged · Nov 10, 2005 · N213FE · Boeing 7272S2F · Leading Edge Devices
  > FOUND REPAIR TOP SIDE NR 3 L/E KRUGER FLAP LT WING. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT NR 3 L/E KRUGER FLAP, TOP SIDE ON LT WING WAS DETERMINED T
- [SDR 05FDEA03746](https://openairdocs.org/sdr/05FDEA03746.md): Repair · undamaged · Nov 9, 2005 · N213FE · Boeing 7272S2F · Fuselage Main, Structure
  > FOUND REPAIR AFT CARGO COMPARTMENT STA 1010 RBL 8, REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT STA 1010, RBL 8 WAS DETERMINED TO BE IAW SRM 51-40-4-FIG 1, BASE
- [SDR 05FDEA03745](https://openairdocs.org/sdr/05FDEA03745.md): Skin · undamaged · Nov 9, 2005 · N213FE · Boeing 7272S2F · Fuselage Main, Plate/Skin
  > FOUND REPAIR FORWARD CARGO COMPARTMENT, STA. 560- STA 620 RBL 20. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT STA 560 STA 620 RBL 20 WAS DETERMINED TO B
- [SDR 05FDEA03744](https://openairdocs.org/sdr/05FDEA03744.md): Stringer · undamaged · Nov 9, 2005 · N213FE · Boeing 7272S2F · Fuselage Main, Longeron/Stringer
  > FOUND REPAIR AT STA 1030, RT SIDE OF FUSELAGE AT CUSP. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT FS STA 1030 RT S 17R WAS DETERMINED TO BE IAW SRM 53-30
- [SDR 05FDEA03743](https://openairdocs.org/sdr/05FDEA03743.md): Skin · undamaged · Nov 9, 2005 · N213FE · Boeing 7272S2F · Fuselage Main, Plate/Skin
  > FOUND REPAIR AFT CARGO COMPARTMENT STA 1135 RBL 8, REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT STA 1135 RBL 8 WAS DETERMINED TO BE IAW SRM 53-10-5 FIG 4 SHT 1
- [SDR 05FDEA03741](https://openairdocs.org/sdr/05FDEA03741.md): Skin · undamaged · Nov 9, 2005 · N213FE · Boeing 7272S2F · Fuselage Main, Plate/Skin
  > FOUND REPAIR AFT, CARGO COMPARTMENT STA 1105, RBL 5. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT STA 1105, RBL 5 WAS DETERMINED TO BE IAW SRM 53-10-5 FIG 4 BA
- [SDR 05FDEA03740](https://openairdocs.org/sdr/05FDEA03740.md): Skin · undamaged · Nov 9, 2005 · N213FE · Boeing 7272S2F · Fuselage Main, Plate/Skin
  > FOUND REPAIR AFT CARGO COMPARTMENT STA 1080, LBL3. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT STA 1080 LBL 3 WAS DETERMINED TO BE IAW SRM 53-10-5 FIG 4 BASED
- [SDR 05FDEA03644](https://openairdocs.org/sdr/05FDEA03644.md): Floorbeam · corroded · Nov 4, 2005 · N213FE · Boeing 7272S2F · Fuselage Main, Floor Beam
  > LATERAL / LONGITUDINAL FLOORBEAM HAS SEVERAL CORRODED NUT PLATES AND SURFACE UNDER NUT PLATES,FROM STA. 1090 TO 1110 BL 0 TO RBL 15., REMOVED CORROSION ON LWR. CHORD.090 BEFORE REWORK.040AFTER REWORK OUT OF LIMITS. IAW SRM 53-10-1. REMOVED CORRODED N
- [SDR 05FDEA03617](https://openairdocs.org/sdr/05FDEA03617.md): Skin · dented · Nov 4, 2005 · N213FE · Boeing 7272S2F · Fuselage Main, Plate/Skin
  > EXTERNAL FUSELAGE SKIN DENTED BS 1050 S-17R. CHECKED LIMITS MEASURED DENT.900 WIDE.750 LONG AND.055 DEEP A/Y =13.6 OUT OF LIMITS IAW SRM 53-10-1 FIG 1 SHEET 3 DETAIL II. NDT PERFORMED NO CRACK NOTED, FABRICATED DOUBLER AND CUT OUT DAMAGE. INSTALLED DOU
- [SDR 05FDEA03514](https://openairdocs.org/sdr/05FDEA03514.md): Flap Track · corroded · Oct 26, 2005 · N213FE · Boeing 7272S2F · Trailing Edge Flaps
  > NR 3 FLAP TRACK AFT MOUNT PAD HAS HEAVY CORROSION. REPLACED FLAP TRACK WITH SERVICEABLE FLAP TRACK IAW MM 27-51-031-4.
- [SDR 05FDEA03513](https://openairdocs.org/sdr/05FDEA03513.md): Flap Track · corroded · Oct 26, 2005 · N213FE · Boeing 7272S2F · Trailing Edge Flaps
  > NR 6 FLAP TRACK HAS CORROSION ON AFT MOUNT PAD. REPLACED FLAP TRACK WITH SERVICEABLE FLAP TRACK IAW MM 27-51-031-4.
- [SDR 05FDEA03512](https://openairdocs.org/sdr/05FDEA03512.md): Flap Track · corroded · Oct 26, 2005 · N213FE · Boeing 7272S2F · Trailing Edge Flaps
  > NR 6 FLAP TRACK HAS CORROSION ON AFT MOUNT PAD. REPLACED FLAP TRACK WITH SERVICEABLE FLAP TRACK IAW MM 27-51-031-4.

Next page: https://openairdocs.org/deregistered/N213FE-2014-05-05/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 = 'N213FE' AND deregistration_id = 'N213FE-2014-05-05'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N213FE-2014-05-05/reports

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