# Service difficulty reports: N244FE, cancelled Aug 27, 2013

A list on [N244FE, cancelled Aug 27, 2013](https://openairdocs.org/deregistered/N244FE-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 3 · 104 reports

- [SDR FDEA201108173307](https://openairdocs.org/sdr/FDEA201108173307.md): Light · inoperative · Aug 17, 2011 · N244FE · Boeing 727277 · Emergency Lighting
  > FLIGHT DECK EMERGENCY EXIT LIGHT INOPERATIVE. R & R FLIGHT DECK EMERGENCY EXIT LIGHT REF MM 33-50-101-2-0. OPS CHECKED NORMAL.
- [SDR FDEA201008203055](https://openairdocs.org/sdr/FDEA201008203055.md): Receiver · failed · Aug 20, 2010 · N244FE · Boeing 727277 · Visual Omnirange (VOR) System
  > VOR'S CHECKED GOOD ON PREFLIGHT. DURING CLIMBOUT BOTH VOR'S SHOWED A 30 DEGREE SPLIT ON VOR STA COULD NOT CTR EITHER CDI ON VOR STATION. TRIED ANOTHER VOR STA, SAME SITUATION. BOTH RMI'S HAD VOR NEEDLES 30 - 40 ' SPLIT. COMPASS SYS MATCHED. HAD TO RELY ON AT
- [SDR FDEA200906011866](https://openairdocs.org/sdr/FDEA200906011866.md): Floorbeam · corroded · Jun 1, 2009 · N244FE · Boeing 727277 · Fuselage Main, Floor Beam
  > MAIN CABIN FLOORBEAM BS 312, LBL 6 IS EXFOLIATED ON AFT LIP OF UPPER CHORD. CUT OUT DAMAGED AREA 2 BY 1 INCH IAW DWG NR SR27-53-017 REV A. FABRICATED 2 REPAIR ANGLES AND REPAIR FILLER IAW DWG NR SR27-53-017 REV A. HEAT TREATED REPAIR ANGLES FROM TO T6 IAW F
- [SDR FDEA200905211765](https://openairdocs.org/sdr/FDEA200905211765.md): Seat Track · corroded · May 21, 2009 · N244FE · Boeing 727277 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN FUSELAGE SEAT TRACK AT BS 1110, LBL 24 IS CORRODED. REMOVED CORRODED SECTION OF SEAT TRACK IAW 51-30-2 FABRICATED NEW SECTION IAW DRAWING 53FX976 REV B. TREATED & PRIMED SECTION IAW SRM 51-10-2 INSTALLED SEAT TRACK SECTION IAW SRM 51-30-2
- [SDR FDEA200905211760](https://openairdocs.org/sdr/FDEA200905211760.md): Stringer · corroded · May 21, 2009 · N244FE · Boeing 727277 · Fuselage Main, Longeron/Stringer
  > ART PIT STR 27L CORRODED IN CHANNEL BETWEEN BS 950E-950F. REMOVED CORROSION IAW SRM 51-10-6. UT INSPECTED AREA FOUND OUT OF LIMITS. CUT OUT DAMAGE AREA IAW SRM 53-10-3 FIG 1. FABRICATED REPAIR PARTS AND 2 SPLICES IAW SRM 53-10-2 FIG 9. TREATED AND PRIME
- [SDR FDEA200905211759](https://openairdocs.org/sdr/FDEA200905211759.md): Stringer · corroded · May 21, 2009 · N244FE · Boeing 727277 · Fuselage Main, Longeron/Stringer
  > AFT PIT STR 27L CORRODED IN CHANNEL BETWEEN BS 970-990. REMOVED CORROSION IAW SRM 51-10-6. INSPECTED AREA AND FOUND OUT OF LIMITS IAW SRM 53-10-1. FIG 1. CUT OUT DAMAGED AREA IAW SRM 53-10-3, FIG. 1. FABRICATED STRINGER, & SPLICERS IAW SRM 53-10-3 FIG. 1. AN
- [SDR FDEA200905181713](https://openairdocs.org/sdr/FDEA200905181713.md): Stringer · corroded · May 18, 2009 · N244FE · Boeing 727277 · Fuselage Main, Longeron/Stringer
  > FWD PIT CORROSION ON STR 26 L STA 720B. CUT OUT DAMAGE AREA IAW SRM 53-10 3 FIG 1. FABRICATED REPAIR PART AND 2 SPLICES IAW SRM 53-10-2 FIG 1 AND 53-10-2 FIG 9. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 51-30-2.
- [SDR FDEA200905181712](https://openairdocs.org/sdr/FDEA200905181712.md): Stringer · corroded · May 18, 2009 · N244FE · Boeing 727277 · Fuselage Main, Longeron/Stringer
  > FWD PIT - CORROSION ON STR 26 L BETWEEN STA 700 AND 720. CUT OUT DAMAGE AREA IAW SRM 53-10-3 FIG 1. FABRICATED STRINGER AND 1 SPLICE IAW SRM 53-10-2 FIG 9. TREATED AND PRIMED IAW SRM 51-10-2, INSTALLED REPAIR PARTS IAW B727 SRM 51-30-2.
- [SDR FDEA200905171697](https://openairdocs.org/sdr/FDEA200905171697.md): Skin · corroded · May 17, 2009 · N244FE · Boeing 727277 · Wing, Plate/Skin
  > RT WING LEADING EDGE HAS BULGING SEALANT AND CORROSION AT WS 510 UPPER SURFACE ABOVE SPAR. FABRICATED REPAIR FILLERS & DOUBLER IAW B727 SRM 57-30-4 FIG 6. TREATED & PRIMED PARTS & AREA IAW SRM 51-10-2. FLAP SHOT PEEN AREA IAW EA 7-5710-127964. INSTALLED
- [SDR FDEA200905161690](https://openairdocs.org/sdr/FDEA200905161690.md): Skin · damaged · May 16, 2009 · N244FE · Boeing 727277 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN AT STA 300 STRINGER 21LT IS GOUGED BLENDED OUT DAMAGED AREA IAW SRM 51-10-1, FOUND TO BE OUT OF LIMITS IAW SRM 53-30-1 FIG 1 AND 2, CUT OUT DAMAGED AREA IAW SRM 51-10-1, FABRICATED REPAIR DOUBLER IAW SRM 53-30-3 FIG 1 AND 53-30-2 FIG 2, TREATED
- [SDR FDEA200905151681](https://openairdocs.org/sdr/FDEA200905151681.md): Skin · cracked · May 15, 2009 · N244FE · Boeing 727277 · Trailing Edge Flaps
  > RIGHT FOREFLAP, INBOARD WBL 124, CRACK ON SKIN ABOVE CARRIAGE ATTACH FITTING CUT OUT DAMAGED AREA IAW SRM 51-10-1, FABRICATED REPAIR DOUBLER & FILLER IAW SRM 57-50-2 FIG 4 AND 57-50-2 FIG 1, TREATED AND PRIMED IAW SRM 51-10-2 INSTALLED REPAIR IAW SRM 51-30-2
- [SDR FDEA200905141660](https://openairdocs.org/sdr/FDEA200905141660.md): Skin · cracked · May 14, 2009 · N244FE · Boeing 727277 · Trailing Edge Flaps
  > LEFT HAND FORE FLAP OUTBD WBL 348 CRACK ON SKIN ABOVE CARRIAGE ATTACH FITTING. TRIMMED OUT CRACKED AREA IAW SRM 57-50-4 FIG 1 AND 51-10-1. FABRICATED REPAIR DOUBLER, TREATED, PRIMED, AND INSTALLED DOUBLER AT LEFT HAND FOREFLAP O/B WBL 348 IAW SRM 57-50-4 F
- [SDR FDEA200905141659](https://openairdocs.org/sdr/FDEA200905141659.md): Skin · gouged · May 14, 2009 · N244FE · Boeing 727277 · Trailing Edge Flaps
  > LEFT WING OUTBD T/E FOREFLAP HAS GOUGE EXTERNAL DOUBLER FROM PREVIOUS REPAIR, INBD END. REMOVED DAMAGED REPAIR IAW SRM 51-30-2. FABRICATED NEW DOUBLER IAW SRM 57-50-4 FIG 1. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED NEW DOUBLER AT LT. WING O/B T/E
- [SDR FDEA200905121770](https://openairdocs.org/sdr/FDEA200905121770.md): Support Bracket · corroded · May 12, 2009 · N244FE · Boeing 727277 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT LBL 17.8 VERTICAL BEAM SUPPORT BRACKET HAS CORROSION AT UPPER SIDE STA 1183. REMOVED VERTICAL BEAM SUPPORT BRACKET IAW SRM 51-30-2. FABRICATED NEW SUPPORT BRACKET(FITTING) IAW DRAWING 65-19608. TREATED AND PRIMED NEW FITTING IAW SRM 5
- [SDR FDEA200905121627](https://openairdocs.org/sdr/FDEA200905121627.md): Skin · corroded · May 12, 2009 · N244FE · Boeing 727277 · Fuselage Main, Plate/Skin
  > CORROSION UNDER SEALANT ON FUSELAGE SKIN STA 680 S27L. REMOVED CORROSION AND FOUND OUT OF LIMITS SRM 51-10-6 AND 53-30-1 FIG.1 REMOVED TRANSITION PANELS FOR ACCESS IAW SRM 51-30-2. CUT OUT SKIN SECTION IAW SRM 53-30-3 FIG.12 AND REPAIRED IAW SRM 53-30-3 FI
- [SDR FDEA200905121626](https://openairdocs.org/sdr/FDEA200905121626.md): Structure · cracked · May 12, 2009 · N244FE · Boeing 727277 · Trailing Edge Flaps
  > LEFT WING INBOARD MID-FLAP LOWER CHORD CRACKED WBL 124. DISPLACED SKIN, REMOVED SEAL, AND SEAL RETAINER FOR ACCESS IAW SRM 51-30-2. CUTOUT DAMAGE AND REPAIRED IAW SRM 51-40-4 FIG 3 AND 57-50-2 FIG 5. TREATED, PRIMED AND INSTALLED REPAIR IAW SRM 51-10-2 A
- [SDR FDEA200905121625](https://openairdocs.org/sdr/FDEA200905121625.md): Angle · cracked · May 12, 2009 · N244FE · Boeing 727277 · Trailing Edge Flaps
  > RIGHT WING INBOARD MID-FLAP LOWER TRAILING EDGE ANGLE IS CRACKED AT WBL 90. OPENED LOWER INNER SKIN IAW SRM 51-30-2. REMOVED 3EA LOWER INBD SEAL RETAINERS IAW SRM 51-30-2. REMOVED CRACKED LOWER INBD ANGLE IAW SRM 51- 30-2. FABRICATED NEW ANGLE IAW SRM 57-5
- [SDR FDEA200905121624](https://openairdocs.org/sdr/FDEA200905121624.md): Stringer · corroded · May 12, 2009 · N244FE · Boeing 727277 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 29R AT STA 950E AFT PIT. REMOVED CORROSION AND FOUND OUT OF LIMITS, FABRICATED REPAIR STRAP AND INSTALLED IAW DWG SR27-53-023 REV A.
- [SDR FDEA200905121623](https://openairdocs.org/sdr/FDEA200905121623.md): Floorbeam · cracked · May 12, 2009 · N244FE · Boeing 727277 · Fuselage Main, Floor Beam
  > WING CENTER SECTION OVERWING FLOORBEAM TEE FITTING CRACKED BS 760.9 RBL45. REMOVED TEE FITTING IAW SRM 51-30-2. FABRICATED NEW TEE FITTING IAW SRM 51-30- 5 AND PF SRM 53-10-2 FIG 7A. LOCATED, DRILLED, TREATED, AND PRIMED NEW FITTING IAW SRM 51-30-5 AND 51-1
- [SDR FDEA200905121622](https://openairdocs.org/sdr/FDEA200905121622.md): Floorbeam · cracked · May 12, 2009 · N244FE · Boeing 727277 · Fuselage Main, Floor Beam
  > WING CENTER SECTION OVERWING FLOORBEAM TEE CRACKED BS 760.9 LBL 45. REMOVED CRACKED TEE IAW SRM 51-30-2, FABRICATED NEW ANGLE IAW SRM 53-10-2 FIG 7 AND 51-30-5, TREATED AND PRIMED NEW TEE IAW SRM 51-10-2, INSTALLED NEW TEE IAW SRM 53-10-2 AND 51-30-2
- [SDR FDEA200905111621](https://openairdocs.org/sdr/FDEA200905111621.md): Skin · cracked · May 11, 2009 · N244FE · Boeing 727277 · Trailing Edge Flaps
  > RIGHT FORE FLAP, INBOARD, WBL 224, CRACK ON SKIN ABOVE CARRIAGE ATTACH FITTING CUT OUT DAMAGED AREA OF SKIN IAW SRM 51-10-1. FABRICATED REPAIR DOUBLER MATERIAL USED 2024 T3 0.063" PO NR 9008130 DIM 5 1/2 INCH BY 4 3/8 INCH IAW SRM 57-50-2 FIG 4 AND 57-50-4
- [SDR FDEA200905091596](https://openairdocs.org/sdr/FDEA200905091596.md): Spar · corroded · May 9, 2009 · N244FE · Boeing 727277 · Wing Spar
  > LT LWR FWD CTR TANK SPAR CORRODED AT STA 744 LBL 20 TO LBL 30. DISPLACED SEAL AT BS 740, OPENED FUEL PANELS NR 7540 AND 7340 FOR ACCESS IAW SRM 51-30-2, MM 51-30-011-4 AND 28-11-021-4, REMOVED SEAL RETAINER, CORNER FITTINGS AND PANELS NR 3445, 6402R AND 630
- [SDR FDEA200905091599](https://openairdocs.org/sdr/FDEA200905091599.md): Floor Support · corroded · May 9, 2009 · N244FE · Boeing 727277 · Fuselage Miscellaneous Structure
  > FWD LAV AREA, CORROSION ON FLOOR SUPPORT ANGLE BS 312 TO 344 LBL 45. REMOVED CORROSION IAW SRM 51-10-6 AND FOUND OUT OF LIMITS IAW SRM 53-10-1 FIG 1. REMOVED FLOOR SUPPORT IAW SRM 51-30-2. CUT OUT DAMAGED AREA AND REPAIRED FLOOR SUPPORT IAW SRM 51-40-4 FI
- [SDR FDEA200905091598](https://openairdocs.org/sdr/FDEA200905091598.md): Floorbeam · corroded · May 9, 2009 · N244FE · Boeing 727277 · Fuselage Main, Floor Beam
  > FLOORBEAM HAS PITTING CORROSION STA 312 LBL45.
- [SDR FDEA200905091597](https://openairdocs.org/sdr/FDEA200905091597.md): Stringer · corroded · May 9, 2009 · N244FE · Boeing 727277 · Fuselage Main, Longeron/Stringer
  > AFT PIT - STR 22L IS CORRODED FROM BS 1170 TO 1183. CUT-OUT DAMAGED STRINGER SECTION AND FABRICATED STRINGER REPAIR FILLER AND 2 SPLICES AND INSTALLED IAW SRM 53-10-3, 53-10-2 AND 51-10-2.
- [SDR FDEA200905091595](https://openairdocs.org/sdr/FDEA200905091595.md): Skin · corroded · May 9, 2009 · N244FE · Boeing 727277 · Fuselage Main, Plate/Skin
  > SKIN BULGE AND BROKEN FASTENER STA 1166 STR 21L. FOUND CORROSION ON AFT LAV TRIPLER OUT OF LIMITS, REMOVED TRIPLER, FABRICATED NEW TRIPLER AND INSTALLED IAW DWG 65-54583, SRM 51-30-2 AND 51-30-5.
- [SDR FDEA200905091592](https://openairdocs.org/sdr/FDEA200905091592.md): Skin · dented · May 9, 2009 · N244FE · Boeing 727277 · Fuselage Main, Plate/Skin
  > SKIN DENTED STA 410 STR 21R. EVALUATED DENTS AND FOUND OUT OF LIMITS IAW B727 SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA IAW SRM 53-30-3. FABRICATED DOUBLER IAW SRM 53-30-3 FIG 3 AND 53-30-2 FIG 2. TREATED AND PRIMED DOUBLER IAW SRM 51-10-2. INSTALLED REPAIR
- [SDR FDEA200905091591](https://openairdocs.org/sdr/FDEA200905091591.md): Skin · corroded · May 9, 2009 · N244FE · Boeing 727277 · Cargo/Baggage Doors
  > SKIN BULGE IN C-3 DOOR SKIN AFT UPPER CORNER. REMOVED DAMAGED SKIN, FABRICATED NEW SKIN, TREATED, PRIMED AND INSTALLED NEW C3 DOOR EXTERIOR SKIN IAW EA NR 7-5230-126820 AND SRM'S 51-30-2, 51-30-5, AND 51-10-2.
- [SDR FDEA200905091590](https://openairdocs.org/sdr/FDEA200905091590.md): Spar · cracked · May 9, 2009 · N244FE · Boeing 727277 · Wing Spar
  > RIGHT WING TRAILING EDGE FALSE SPAR LOWER CHORD IS CRACKED AT WBL 118. REPAIRED RT. WING T/E FALSE SPAR LOWER CHORD IAW DRAWING SR27-57-038 REV. C (STD REWORK DRAWING INBD SPOILER SUPT. BEAM CRACK REPAIR).
- [SDR FDEA200905091589](https://openairdocs.org/sdr/FDEA200905091589.md): Bracket · cracked · May 9, 2009 · N244FE · Boeing 727277 · Fuselage Miscellaneous Structure
  > CRACKED BRACKET AT MAIN CARGO DOOR UPPER SILL STA 640 BETWEEN STR 3L AND 4L. REMOVED CRACKED FITTING IAW SRM 51-30-2 FABRICATED NEW FITTING IAW DRAWING 53FX1280 REV E TREATED & PPRIMED NEW FITTING IAW SRM 51-10-2 & INSTALLED NEW MAIN CARGO DOOR UPPER SILL
- [SDR FDEA200905091588](https://openairdocs.org/sdr/FDEA200905091588.md): Spar · cracked · May 9, 2009 · N244FE · Boeing 727277 · Wing Spar
  > LEFT WING TRAILING EDGE FALSE SPAR LOWER CHORD IS CRACKED AT WBL 118. REPAIRED RT WING T/E FALSE SPAR LOWER CHORD ANGLE IAW DRAWING SR27-57-038 REV C.
- [SDR FDEA200905091587](https://openairdocs.org/sdr/FDEA200905091587.md): Skin · dented · May 9, 2009 · N244FE · Boeing 727277 · Electrical/Electronic Compartment Doors
  > SEVERAL DENTS IN E/E DOOR SKIN. REMOVED E/E DOOR IAW MM 52-40-001-4, REMOVED SKIN IAW SRM 51-30-2, FABRICATED NEW SKIN IAW SRM 52-40-4 FIG 2 AND 51-30-8, TREATED AND PRIMED SKIN IAW SRM 51-10-2, OPENED INNER SKIN TO FOM IAW SRM 51-30-2, INSTALLED NEW SKIN
- [SDR FDEA200905091586](https://openairdocs.org/sdr/FDEA200905091586.md): Skin · dented · May 9, 2009 · N244FE · Boeing 727277 · Fuselage Main, Plate/Skin
  > PROTRUDING DENT STA 675 STR 23R. UPON EVALUATION DETERMINED PROTRUDING DENT IS OIL CANNING IAW B727SRM 53-30-1 FIG 1, REMOVED PREVIOUS REPAIR, AND CUT OUT DAMAGE AREA, 2 DAMAGE AREAS DIM (3 1/2 INCHES BY 3 3/8 INCH) AND (2 INCH BY 2 INCH) IAW B727 SRM 53-30-3
- [SDR FDEA200905081580](https://openairdocs.org/sdr/FDEA200905081580.md): Skin · dented · May 8, 2009 · N244FE · Boeing 727277 · Emergency Exits
  > RT AFT OVERWING EMERGENCY HATCH HAS DENT AT PREVIOUS REPAIR DOUBLER, TOP OF DOOR AT VENT CUT OUT, EXTERIOR SKIN. REMOVED PREVIOUS REPAIR AT RT AFT OVERWING EMERGENCY HATCH IAW SRM 51-30-2. FABRICATED NEW REPAIR DOUBLE IAW SRM 52-20-01 FIG 1 AND 52-00-03 FIG
- [SDR FDEA200905061851](https://openairdocs.org/sdr/FDEA200905061851.md): Skin · misrepaired · May 6, 2009 · N244FE · Boeing 727277 · Fuselage Main, Plate/Skin
  > IMPROPER FASTENERS IN REPAIR AT STA 1180 STR 21L REMOVED AFT LAV DOOR, PAN, PREVIOUS REPAIR & STRINGER FITTINGS 21 & 22LT IAW SRM 51-30-2 FOR ACCESS, CUT OUT SKIN SECTION AND REPAIRED IAW SRM 53-30-03 FIGURE 12. REINSTALLED AFT LAV DOOR & PAN STRINGER FITTI
- [SDR 07FDEA03668](https://openairdocs.org/sdr/07FDEA03668.md): Seal · failed · Sep 13, 2007 · N244FE · Boeing 727277 · Cargo/Baggage Doors
  > AT FL250, CABIN ALT HORN WENT OFF. RAN QRH REGAINED PRESS WITH CARGO OUTFLOW CLOSED. MECHANIC STATED LOWER CARGO DOOR SEAL FAILURE. FOUND THE LWR FWD CARGO DOOR SEAL ON THE LOWER EDGE PUSHED UNDER. LEFT SEAL AS IT WAS FOUND FOR FURTHER EVALUATION. SECURED
- [SDR 07FDEA00102](https://openairdocs.org/sdr/07FDEA00102.md): Landing Gear · failed · Jan 16, 2007 · N244FE · Boeing 727277 · Landing Gear Retraction/Extension System
  > LANDING GEAR FAILED TO RETRACT NORMALLY. FOLLOWED QRH PROCEDURE TEST 1: INTERMITTENT HORN SOUNDED WHEN RETRACTING FLAPS FROM 5' TO 2'. UNABLE TO TEST WING ANTI-ICE DUE TO SYSTEM OPERATING ALREADY. NOSEWHEEL STEERING ALIGNMENT APPEARED NORMAL. QRH STATES ST
- [SDR 06FDEA04231](https://openairdocs.org/sdr/06FDEA04231.md): Frame · corroded · Dec 13, 2006 · N244FE · Boeing 727277 · Fuselage Main, Frame
  > DURING ACCOMPLISHMENT OF C CHECK MX, AAR AIRCRAFT SERVICES, IND CORROSION WAS FOUND COMMON TO THE FORWARD SIDE OF THE AFT FRAME AT THE NR 3 CARGO DOORWAY AT STA 1142.7 BETWEEN STRINGERS 25R AND 27R (RBL 26). THE DAMAGE WAS BLENDED TO A 20:1 RATIO AND VERIFIED
- [SDR 06FDEA04217](https://openairdocs.org/sdr/06FDEA04217.md): Skin · misrepaired · Dec 12, 2006 · N244FE · Boeing 727277 · Fuselage Main, Plate/Skin
  > REPAIR LOCATED AT 680-700 STR 27L-28L FOUND NOT TO BE INSTALLED USING APPROVED DATA. FILLER DOES NOT PICK UP 2 ADDITIONAL ROWS BEFORE BUTT SPLICE. REMOVED AND REPLACED DOUBLER FILLER ADDED ADDITIONAL ROWS. INSTALLED REPAIR BETWEEN STA 680-710, STR 27L-25R R
- [SDR 06FDEA04216](https://openairdocs.org/sdr/06FDEA04216.md): Skin · damaged · Dec 12, 2006 · N244FE · Boeing 727277 · Fuselage Main, Plate/Skin
  > PREVIOUSLY INSTALLED REPAIR INSTALLED ON THE LT OTBD FORE FLAP 10" FROM INBD END HAS GOUGE ON DOUBLER, WITH DEPTH OF DAMAGE AT.040". REMOVED DAMAGED DOUBLER AND INSTALLED NEW DOUBLER REF SRM 57-50-4 FIG 1 PG 2. THIS IS A MAJOR REPAIR ON WO NR 34160 SNRM NR
- [SDR 06FDEA04210](https://openairdocs.org/sdr/06FDEA04210.md): Skin · misrepaired · Dec 11, 2006 · N244FE · Boeing 727277 · Fuselage Main, Plate/Skin
  > LT PASSENGER DOOR, LOWER HINGE CUTOUT DOUBLER, HAS INCORRECT FASTENER SIZE, ACCORDING TO SB 727-53A-0198 FIG 5 COMPLIED WITH FED EX EO NR 7-5330-7-2345 PT3. INSTALLED EXTERNAL DOUBLER REPAIR REF SB727-53AO0198 R3.
- [SDR 06FDEA04199](https://openairdocs.org/sdr/06FDEA04199.md): Skin · gouged · Dec 8, 2006 · N244FE · Boeing 727277 · Trailing Edge Flaps
  > PREVIOUSLY INSTALLED REPAIR ON LT OTBD FORE FLAP 10" FROM INBD END HAS GOUGE ON DOUBLER REMOVED DAMAGED DOUBLER AND INSTALLED NEW DOUBLER REF SRM 57-50-4 FIG PG 1. THIS REPAIR CLASSIFIED AS MAJOR ON WO NR 34610, SNRM NR N01238.
- [SDR 06FDEA04198](https://openairdocs.org/sdr/06FDEA04198.md): Floorbeam · corroded · Dec 8, 2006 · N244FE · Boeing 727277 · Fuselage Main, Floor Beam
  > CABIN FLOOR STRUCTURE CORROSION ON UPPER SURFACE OF BEAM STA 950, LBL 38-46 STR 17L. REMOVED CORRODED SECTION OF BS 950 AND REPAIRED REF EA NR 7-5310-109942 CLASSIFIED AS A MAJOR REPAIR ON WO NR 34610, SNRM # N00520.
- [SDR 06FDEA04197](https://openairdocs.org/sdr/06FDEA04197.md): Depressor · worn · Dec 8, 2006 · N244FE · Boeing 727277 · Cargo/Baggage Doors
  > AFT PIT NR 2 DOOR LWR SEAL DEPRESSOR HAS LIGHT WEAR. REMOVED AND REPLACED SEAL DEPRESSOR REF SRM 51-30-02.
- [SDR 06FDEA04196](https://openairdocs.org/sdr/06FDEA04196.md): Frame · damaged · Dec 8, 2006 · N244FE · Boeing 727277 · Fuselage Main, Frame
  > LT FOWARD CABIN, FRAME WEB BETWEEN STR 3L AND 4L HAS (7 EA.) UNPLUGGED HOLES. REMOVED DAMAGED AND REPAIRED WITH A FORMED SECTION REPAIR REF. SRM 51-40-03 PG 1-6.
- [SDR 06FDEA04194](https://openairdocs.org/sdr/06FDEA04194.md): Floorbeam · corroded · Dec 8, 2006 · N244FE · Boeing 727277 · Fuselage Main, Floor Beam
  > LT FWD CABIN FLOORBEAM UPPER CAP IS CORRODED AT STA 480, LBL 27-LBL32. CLASSIFIED AS A MAJOR REPAIR ON WO 34610, SNRM # N00525. REMOVED CORROSION, MATERIAL LOSS OUT OF LIMITS REF SRM 51-10-1. CUT OUT DAMAGED SECTION OF BEAM, FABRICATED REPAIR PARTS, TREAT A
- [SDR 06FDEA04195](https://openairdocs.org/sdr/06FDEA04195.md): Skin · unknown · Dec 8, 2006 · N244FE · Boeing 727277 · Fuselage Main, Plate/Skin
  > REPAIR LOCATED AT STA 720D-720E AT STR 18L-19L FOUND NOT TO BE INSTALLED USING APPROVED DATA. REMOVED EXISTING DOUBLER, FABRICATED NEW DOUBLER, ADDING ADITIONAL FASTENERS TO THE REPAIR. REF SRM 53-30-03 PG 76-82 AND DETAIL 3. THIS IS CLASSIFIED AS A MAJOR R
- [SDR 06FDEA04190](https://openairdocs.org/sdr/06FDEA04190.md): Seat Track · corroded · Dec 7, 2006 · N244FE · Boeing 727277 · Fuselage, Seat/Cargo Attach Fittings
  > LT FWD CABIN SEAT TRACK BEAM IS CORRODED FROM STA 580 - STA 620 LBL 45 REMOVED CORRODED SECTION OF SEAT TRACK AND REPLACED, REF SRM 53-10-1 FIGURE 3, SRM 53-10-2 FIGURE 7A.
- [SDR 06FDEA04188](https://openairdocs.org/sdr/06FDEA04188.md): Stringer · cracked · Dec 7, 2006 · N244FE · Boeing 727277 · Vertical Stabilizer, Plate/Skin
  > LT VERTICAL STAB INTERIOR STRINGER 9L IS CRACKED AT INSPAR RIB CHORDS AT FIN STA 157.2. REMOVED DAMAGE AND REPAIRED REF SRM 51-40-4 FIGURE 3, PAGES 14-17. CLASSIFIED AS A MAJOR REPAIR ON WO 34160, SNRM NR N00685.
- [SDR 06FDEA04187](https://openairdocs.org/sdr/06FDEA04187.md): Repair · misinstalled · Dec 7, 2006 · N244FE · Boeing 727277 · Fuselage Main, Plate/Skin
  > FOUND FLUSH REPAIR LOCATED AT APPROX STA 227.8, LBL 12, UPPER FUSELAGE ABOVE CAPT'S WINDOW. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED EXISTING NON-CONFORMING DOUBLER AND INSTALLED

Next page: https://openairdocs.org/deregistered/N244FE-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 = 'N244FE' AND deregistration_id = 'N244FE-2013-08-27'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N244FE-2013-08-27/reports

---
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.