N244FE, cancelled Aug 27, 2013

Service difficulty reports · 104

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR FDEA201108173307Light · inoperativeFLIGHT DECK EMERGENCY EXIT LIGHT INOPERATIVE. R & R FLIGHT DECK EMERGENCY EXIT LIGHT REF MM 33-50-101-2-0. OPS CHECKED NORMAL.Aug 17, 2011 · N244FE · Boeing 727277 · Emergency LightingSDR FDEA201008203055Receiver · failedVOR'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 ATAug 20, 2010 · N244FE · Boeing 727277 · Visual Omnirange (VOR) SystemSDR FDEA200906011866Floorbeam · corrodedMAIN 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 FJun 1, 2009 · N244FE · Boeing 727277 · Fuselage Main, Floor BeamSDR FDEA200905211765Seat Track · corrodedMAIN 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 51-30-2May 21, 2009 · N244FE · Boeing 727277 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200905211760Stringer · corrodedART 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 PRIMEMay 21, 2009 · N244FE · Boeing 727277 · Fuselage Main, Longeron/StringerSDR FDEA200905211759Stringer · corrodedAFT 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. ANMay 21, 2009 · N244FE · Boeing 727277 · Fuselage Main, Longeron/StringerSDR FDEA200905181713Stringer · corrodedFWD 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.May 18, 2009 · N244FE · Boeing 727277 · Fuselage Main, Longeron/StringerSDR FDEA200905181712Stringer · corrodedFWD 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.May 18, 2009 · N244FE · Boeing 727277 · Fuselage Main, Longeron/StringerSDR FDEA200905171697Skin · corrodedRT 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. INSTALLEDMay 17, 2009 · N244FE · Boeing 727277 · Wing, Plate/SkinSDR FDEA200905161690Skin · damagedFUSELAGE 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, TREATEDMay 16, 2009 · N244FE · Boeing 727277 · Fuselage Main, Plate/SkinSDR FDEA200905151681Skin · crackedRIGHT 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 51-30-2May 15, 2009 · N244FE · Boeing 727277 · Trailing Edge FlapsSDR FDEA200905141660Skin · crackedLEFT 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 FMay 14, 2009 · N244FE · Boeing 727277 · Trailing Edge FlapsSDR FDEA200905141659Skin · gougedLEFT 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 May 14, 2009 · N244FE · Boeing 727277 · Trailing Edge FlapsSDR FDEA200905121770Support Bracket · corrodedAFT 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 5May 12, 2009 · N244FE · Boeing 727277 · Fuselage Miscellaneous StructureSDR FDEA200905121627Skin · corrodedCORROSION 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 FIMay 12, 2009 · N244FE · Boeing 727277 · Fuselage Main, Plate/SkinSDR FDEA200905121626Structure · crackedLEFT 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 AMay 12, 2009 · N244FE · Boeing 727277 · Trailing Edge FlapsSDR FDEA200905121625Angle · crackedRIGHT 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 57-5May 12, 2009 · N244FE · Boeing 727277 · Trailing Edge FlapsSDR FDEA200905121624Stringer · corrodedCORROSION 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.May 12, 2009 · N244FE · Boeing 727277 · Fuselage Main, Longeron/StringerSDR FDEA200905121623Floorbeam · crackedWING 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 51-1May 12, 2009 · N244FE · Boeing 727277 · Fuselage Main, Floor BeamSDR FDEA200905121622Floorbeam · crackedWING 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 51-30-2May 12, 2009 · N244FE · Boeing 727277 · Fuselage Main, Floor BeamSDR FDEA200905111621Skin · crackedRIGHT 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 May 11, 2009 · N244FE · Boeing 727277 · Trailing Edge FlapsSDR FDEA200905091596Spar · corrodedLT 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 630May 9, 2009 · N244FE · Boeing 727277 · Wing SparSDR FDEA200905091599Floor Support · corrodedFWD 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 FIMay 9, 2009 · N244FE · Boeing 727277 · Fuselage Miscellaneous StructureSDR FDEA200905091598Floorbeam · corrodedFLOORBEAM HAS PITTING CORROSION STA 312 LBL45.May 9, 2009 · N244FE · Boeing 727277 · Fuselage Main, Floor BeamSDR FDEA200905091597Stringer · corrodedAFT 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.May 9, 2009 · N244FE · Boeing 727277 · Fuselage Main, Longeron/StringerSDR FDEA200905091595Skin · corrodedSKIN 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.May 9, 2009 · N244FE · Boeing 727277 · Fuselage Main, Plate/SkinSDR FDEA200905091592Skin · dentedSKIN 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 REPAIRMay 9, 2009 · N244FE · Boeing 727277 · Fuselage Main, Plate/SkinSDR FDEA200905091591Skin · corrodedSKIN 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.May 9, 2009 · N244FE · Boeing 727277 · Cargo/Baggage DoorsSDR FDEA200905091590Spar · crackedRIGHT 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).May 9, 2009 · N244FE · Boeing 727277 · Wing SparSDR FDEA200905091589Bracket · crackedCRACKED 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 May 9, 2009 · N244FE · Boeing 727277 · Fuselage Miscellaneous StructureSDR FDEA200905091588Spar · crackedLEFT 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.May 9, 2009 · N244FE · Boeing 727277 · Wing SparSDR FDEA200905091587Skin · dentedSEVERAL 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 May 9, 2009 · N244FE · Boeing 727277 · Electrical/Electronic Compartment DoorsSDR FDEA200905091586Skin · dentedPROTRUDING 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 53-30-3May 9, 2009 · N244FE · Boeing 727277 · Fuselage Main, Plate/SkinSDR FDEA200905081580Skin · dentedRT 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 FIGMay 8, 2009 · N244FE · Boeing 727277 · Emergency ExitsSDR FDEA200905061851Skin · misrepairedIMPROPER 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 FITTIMay 6, 2009 · N244FE · Boeing 727277 · Fuselage Main, Plate/SkinSDR 07FDEA03668Seal · failedAT 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. SECUREDSep 13, 2007 · N244FE · Boeing 727277 · Cargo/Baggage DoorsSDR 07FDEA00102Landing Gear · failedLANDING 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 STJan 16, 2007 · N244FE · Boeing 727277 · Landing Gear Retraction/Extension SystemSDR 06FDEA04231Frame · corrodedDURING 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 VERIFIEDDec 13, 2006 · N244FE · Boeing 727277 · Fuselage Main, FrameSDR 06FDEA04217Skin · misrepairedREPAIR 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 RDec 12, 2006 · N244FE · Boeing 727277 · Fuselage Main, Plate/SkinSDR 06FDEA04216Skin · damagedPREVIOUSLY 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 NRDec 12, 2006 · N244FE · Boeing 727277 · Fuselage Main, Plate/SkinSDR 06FDEA04210Skin · misrepairedLT 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.Dec 11, 2006 · N244FE · Boeing 727277 · Fuselage Main, Plate/SkinSDR 06FDEA04199Skin · gougedPREVIOUSLY 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.Dec 8, 2006 · N244FE · Boeing 727277 · Trailing Edge FlapsSDR 06FDEA04198Floorbeam · corrodedCABIN 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.Dec 8, 2006 · N244FE · Boeing 727277 · Fuselage Main, Floor BeamSDR 06FDEA04197Depressor · wornAFT PIT NR 2 DOOR LWR SEAL DEPRESSOR HAS LIGHT WEAR. REMOVED AND REPLACED SEAL DEPRESSOR REF SRM 51-30-02.Dec 8, 2006 · N244FE · Boeing 727277 · Cargo/Baggage DoorsSDR 06FDEA04196Frame · damagedLT 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.Dec 8, 2006 · N244FE · Boeing 727277 · Fuselage Main, FrameSDR 06FDEA04194Floorbeam · corrodedLT 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 ADec 8, 2006 · N244FE · Boeing 727277 · Fuselage Main, Floor BeamSDR 06FDEA04195Skin · unknownREPAIR 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 RDec 8, 2006 · N244FE · Boeing 727277 · Fuselage Main, Plate/SkinSDR 06FDEA04190Seat Track · corrodedLT 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.Dec 7, 2006 · N244FE · Boeing 727277 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA04188Stringer · crackedLT 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.Dec 7, 2006 · N244FE · Boeing 727277 · Vertical Stabilizer, Plate/SkinSDR 06FDEA04187Repair · misinstalledFOUND 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 INSTALLEDDec 7, 2006 · N244FE · Boeing 727277 · Fuselage Main, Plate/Skin
Back to N244FE, cancelled Aug 27, 2013