N912FD

Service difficulty reports · 154

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 = 'N912FD' AND registry_match = 'registration'
  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 FDEA201209053226Seat Track · corrodedSEAT TRACK CORRODED STA 900-1070, LBL 45.5. FOUND OUT OF LIMITS IAW SRM 53-00-52 AD1. REMOVED, FABRICATED, AND INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-40-52 FIG 1, DWG 144N5002 REV H AND SRM 51-40-02.Sep 5, 2012 · N912FD · Boeing 75728A · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201208183074Girt Bar · damagedLEFT FORWARD DOOR WILL NOT CLOSE OR OPEN. APPEARS TO HAVE JUMPED OFF A ROLLER. REMOVED SLIDE PACK COVER FROM L1 DOOR. FOUND GIRT BAR SLIDER NOT COMPLETELY CLEAR OF AFT FLOOR FITTING. FOUND ONCE GIRTBAR WAS FREED, THE MODE SELECTOR WAS FULLY DAug 18, 2012 · N912FD · Boeing 75728A · Emergency EquipmentSDR FDEA201207312777Window · failedLT FORWARD WINDOW SHATTERED ENROUTE, DIVERTED.Jul 31, 2012 · N912FD · Boeing 75728A · Flight Compartment WindowsSDR FDEA201206282387Girt Bar · out of trackFOUND GIRT BAR OUT OF TRACK. ADJUSTED GIRT BAR MECHANISM IAW MM 52-11-25-5. DOOR OPENED AND CLOSED NORMAL.Jun 28, 2012 · N912FD · Boeing 75728A · Emergency EquipmentSDR FDEA201204061277Lamp · inoperativeDOOR SLIDE ILLUMINATION LIGHT INOPERATIVE. RELAMPED IAW AMM 33-51-06-2-1. OPS CHECKED GOOD.Apr 6, 2012 · N912FD · Boeing 75728A · Emergency LightingSDR FDEA201202150588Skin · crackedFUSELAGE SKIN DAMAGED FOLLOWING TAIL STRIKE, BS 1701 TO 1745, REPAIRED IAW EA F-5330-158298, REV NR POS P1.Feb 15, 2012 · N912FD · Boeing 75728A · Fuselage Main, Plate/SkinSDR FDEA201201280362Cover · tornWHEN ARMING RT ENTRY DOOR ARM LIGHT WILL NOT ILLUMINATE. FOUND SLIDE COVER CORD TANGLED IN GIRT BAR. INSTALLED SLIDE COVER CORRECTLY IAW MM 52-11-02. OPS CKD GOOD. FINAL CLOSED.Jan 28, 2012 · N912FD · Boeing 75728A · Escape SlideSDR FDEA201201200276Switch · contaminatedR1 DOOR SLIDE ARM LIGHT WILL NOT COME ON WHEN SLIDE IS ARMED. FOUND GREASE AND ICE BLOCKING PROXIMITY SWITCH. REMOVED ICE AND CLEANED TRACK. DOOR LIGHT OPERATED NORMALY WHEN DOOR IS ARMED. FOUND GREASE AND ICE BLOCKING PROXIMITY SWITCH. REMOVED ICE ANJan 20, 2012 · N912FD · Boeing 75728A · Escape SlideSDR FDEA201201190275Proximity Switch · obstructedR1 DOOR SLIDE ARM LIGHT WILL NOT COME ON WHEN SLIDE IS ARMED. FOUND GREASE AND ICE BLOCKING PROXIMITY SWITCH. REMOVED ICE AND CLEANED TRACK. DOOR LIGHT OPERATED NORMALY WHEN DOOR IS ARMED.Jan 19, 2012 · N912FD · Boeing 75728A · Escape SlideSDR FDEA201010284245Skin · dentedDENT IN FUSELAGE SKIN AT STATION 475, STR 19L. EVALUATED DENT AND FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101, TRIMMED OUT DAMAGE AND FABRICATED REPAIR DOUBLER AND REPAIR FILLER 2 AND STRUCTURAL FILLER IAW EA F-5330-143914. TREATED, PRIMED AND INSTALLED REPAOct 28, 2010 · N912FD · Boeing 75728A · Fuselage Main, Plate/SkinSDR FDEA201001270276Landing Gear · malfunctionedLANDING GEAR FAILED TO COME UP. RAN QRH PROCEDURE USING LOCK OVERIDE AND GEAR CAME UP. UNCOVERD AND SELECTED TO ALTN POSITION. ALL 3 MLG PINS INSTALLED AND SAFETIED. GEAR LEVER LOCK CB ON P11 PANEL FOUND PULLED AND COLLARED. UNCOLLARED LEVER LATCH CB, ERAJan 27, 2010 · N912FD · Boeing 75728A · Landing Gear Retraction/Extension SystemSDR FDEA201001210209Valve · failedON APPROACH, PUT GEAR LEVER DOWN. GOT NO NOSE GEAR INDICATION. HAD GEAR DISAGREE MESSAGE, GEAR AND DOOR LIGHTS. RAN CHECKLIST AND LOWERED GEAR WITH ALT IXT SWITCH. COULD HEAR NOSE GEAR EXTENDING. GOT 3 GREEN INDICATIONS AND DOOR LIGHT. LANDED NORMALLY.Jan 21, 2010 · N912FD · Boeing 75728A · Landing Gear Retraction/Extension SystemSDR FDEA200912154471Frame · gougedFRAME AT STA 1280 RT, STR 14-10 HAS GOUGES. REPLACED FRAME SEGMENT FROM STR 7R TO 14R IAW SRM 51-40-05. FRAME SEGMENT FABRICATED ON MAE TR T/9/812786, CHANNEL 1 FABRICATED ON MAE TR T9/812787, CHANNEL 2 FABRICATED ON MAE TR T9/812788. ORIG MAT'L .071 AFTER Dec 15, 2009 · N912FD · Boeing 75728A · Fuselage Main, FrameSDR FDEA200904291467Panel · damagedVERTICAL STAB, RT SIDE CROWN PANEL ATTACHMENT STRIP HAS DAMAGED HOLES, LOWER AFT CORNER. ACCOMPLISHED VERTICAL STAB FIXED T/E BEAM REPAIR AND FITTING REPLACEMENT IAW EA F-5530-124086, AND ATTACHMENTS A AND B OF EA, RELEASE DATE 04/20/09. THIS REPAIR IS CLASSApr 29, 2009 · N912FD · Boeing 75728A · Rudder, Plate/SkinSDR FDEA200904291466Skin · dentedDENT ON FUSELAGE SKIN AT BS 1575, S-26R. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, DETAIL 3. ACCOMPLISHED REPAIR AND INSTALLED IAW SRM 53-00-01, REPAIR NR 16. THIS REPAIR IS CLASSIFIED AS A CAT "A" MAJOR REPAIR.Apr 29, 2009 · N912FD · Boeing 75728A · Fuselage Main, Plate/SkinSDR FDEA200904291465Skin · dentedDENT ON FUSELAGE BS 1628, AT S-26L. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, DETAIL 3. HFEC ACCOMPLISHED WITH NO CRACKS NOTED. ACCOMPLISHED REPAIR AND INSTALLED IAW SRM 53-00-01, REPAIR NR 7, FIG 1 AND 2. THIS REPAIR IS CLASSIFIED AS A CAT "A" MAJOR REApr 29, 2009 · N912FD · Boeing 75728A · Fuselage Main, Plate/SkinSDR FDEA200903010773Skin · dentedLOWER LOBE FUSELAGE SKIN, BS 485, LBL, DENTED. REPAIR ACCOMPLISHED ON MAE 757-5300-16-A1824.Mar 1, 2009 · N912FD · Boeing 75728A · Fuselage Main, Plate/SkinSDR FDEA200902230671Floorbeam · corrodedMAIN CABIN FLOORBEAM UPPER CHORD LOWER SURFACE HAS CORROSION, STA 1681. MAIN CABIN FLOORBEAM UPPER CHORD REPAIRED IAW EA 757-5365-16-F1710 REV-C AT STA 1681, LBL- 58, TO RBL- 58. REPAIR CLASSIFIED AS MAJOR ALTERATION.Feb 23, 2009 · N912FD · Boeing 75728A · Fuselage Main, Floor BeamSDR FDEA200902060479Skin · crackedLOWER FUSELAGE SKIN, DENT AT BS 1395 BL 0. CHECKED LIMITS IAW SRM 53-00-01 FIG 101 DETAIL LLL FOUND TO BE WITHIN LIMIT DEPTH=.016" WIDTH=0.69" LENGTH=0.75" A/Y RATIO=43. NDT CHECKED FOUND CRACK 0.075". REPAIRED CRACK IAW SRM 53-00-01 REPAIR 16 FIG 201 PAGE Feb 6, 2009 · N912FD · Boeing 75728A · Fuselage Main, Plate/SkinSDR FDEA200902060478Skin · damagedAFT CARGO DOOR LOWER FWD CORNER, REPAIR DOUBLER IS DAMAGED. REPAIRED IAW SRM 52-30-01 FIG 201 REPAIR NR 4. THIS REPAIR IS A CATEGORY "B" MAJOR REPAIR. REFER TO SRM 52-30-01 PAGE 204 TABLE IV FOR INSPECTION REQUIREMENT.Feb 6, 2009 · N912FD · Boeing 75728A · Cargo/Baggage DoorsSDR FDEA200902050465Skin · misrepairedRT WING SLAT NR 7 SKIN BETWEEN STA OSS 404.80 AND OSS 427.85 MISREPAIRED. REPAIRED IAW SRM 57-43-01, REPAIR 1, MAJOR REPAIR, CATEGORY "A".Feb 5, 2009 · N912FD · Boeing 75728A · Leading Edge DevicesSDR FDEA200902040453Sill · chafedDURING FOLLOW ON INSPECTION, FOUND FRAME AT BS 1420, 3" BELOW AFT CARGO DOOR SILL TO BE CHAFED. REMOVED 3 SUPPORT ANGLE, DOUBLER, DOOR STOP SUPPORT AND SUPPORT WEB PER SRM 51-40-02 AT BS 1420, BETWEEN RBL 16-23. REMOVED DAMAGED AREA OF FRAME AT BS 1420, 3 Feb 4, 2009 · N912FD · Boeing 75728A · Fuselage Miscellaneous StructureSDR FDEA200902030442Frame · crackedFRAME STA 860 CRACKED BETWEEN STRINGER 3L AND 4L DAMAGE AREA 0.6" OUT LIMITS IAW 757 SF SRM 53-00-07. FABRICATED REPAIR CHANNELS -1,-2. REMOVED DAMAGE AREA IAW 757 SRM 53-00-07. INSTALLED REPAIR IAW SRM 53-00-07, REPAIR 3, FIG. 201. MAJOR REPAIR, CATEGORY Feb 3, 2009 · N912FD · Boeing 75728A · Fuselage Main, FrameSDR FDEA200902030441Frame · damaged3 HOLES AT STA 1300 BETWEEN STRINGER 5R AND 4R ARE OUT OF LIMIT. REMOVED DAMAGED AREA IAW 757 SF SRM 53-00-07 REPAIR NR3 FIG 201. FABRICATED REPAIR CHANNELS -1 AND -2. INSTALLED REPAIR CHANNELS IAW SRM 53-00-07 REPAIR NR 3 FIG 201. THIS REPAIR IS A CATEGOFeb 3, 2009 · N912FD · Boeing 757236 · Fuselage Main, FrameSDR FDEA200902010408Stiffener · crackedLT WING FRONT SPAR STA FSS 295 VERTICAL ANGLE STIFFENER CRACKED AT UPPER END. REMOVED STIFFENER IAW SRM 51-40-02. FABRICATED NEW STIFFENER ON MAE TRAV NR T9/ 777512 DRAWING NR 112N2036. INSTALLED STIFFENER NR 1 PYLON STA FSS 295, IAW SRM 51-40-02. CATEGORYFeb 1, 2009 · N912FD · Boeing 75728A · Wing Miscellaneous StructureSDR FDEA200901290393Support · damagedDURING INSPECTION FOUND AFT CARGO PIT DOOR LOWER SILL TEE CHORD FIRST SCREW HOLE FROM STA 1400 TO BE ELONGATED. REMOVED AND REPLACED WITH NEW TEE CHORD P/N 146N8522-57. THIS IS A MAJOR CATEGORY 'A' REPAIR. NO FOLLOW-UP REQUIRED .Jan 29, 2009 · N912FD · Boeing 75728A · Fuselage Miscellaneous StructureSDR FDEA200901290392Frame · damagedAFT CARGO PIT STA 1380, STR 25-26L FRAME HAS MISDRILLED HOLE AND IS GOUGED. REPAIRED IAW SRM 53-00-07 REPAIR NR 5 FIG 201. THIS IS A MAJOR CATEGORY 'B' REPAIR WITH INITIAL INSPECTION 37,500 FLIGHT CYCLES OR 50,000 AIR FRAME CYCLES WHICHEVER COMES FIRST-REPEAJan 29, 2009 · N912FD · Boeing 75728A · Fuselage Main, FrameSDR FDEA200901260321Stringer Splice · corrodedFWD PIT BILGE, BS 770, LBL 15, S-27L, HAS CORROSION UNDER EXISTING REPAIR DOUBLER. REMOVED EXISTING REPAIR SPLICE IAW SRM 53-00-03, REPAIR NR 1, FIG 201. THERE WAS 100 PERCENT MATERIAL LOSS, REMOVED SPLICE. LOCATED AND DRILLED NEW STRINGER SPLICE IAW SRM 53Jan 26, 2009 · N912FD · Boeing 75728A · Fuselage Main, Longeron/StringerSDR FDEA200901220309Floorbeam · gougedMAIN CABIN FLOORBEAM WEB AT STA 365 RBL 41 HAS DAMAGE. REPAIRED IAW EA 757-5315-16-F1708, REV A. AS PER EA FUNCTION IS ALTERATION AND CLASSIFICATION IS FORM 8110-3/RAS/8100-9.Jan 22, 2009 · N912FD · Boeing 75728A · Fuselage Main, Floor BeamSDR FDEA200901190252Frame · gougedAFT CARGO PIT STA 1320 STR 26-27L FRAME IS GOUGED. REPAIRED FRAME AT STA 1320 STR 26-27L IAW SRM 53-00-07 FIG 201 SHEET 4. THIS REPAIR IS A CATEGORY "B" MAJOR REPAIR.Jan 19, 2009 · N912FD · Boeing 75728A · Fuselage Main, FrameSDR FDEA200901190253Frame · dentedFRAME STA 940 UPPER FLANGE HAS DENT AT STR 6L. REPAIRED FRAME AT STA 940 STR 6L IAW SRM 53-00-07 REPAIR NR 1 DETAIL II. THIS REPAIR IS A CATEGORY "A" MAJOR REPAIR AND NO FOLLOW UP ACTION REQUIRED.Jan 19, 2009 · N912FD · Boeing 75728A · Fuselage Main, FrameSDR FDEA200901190251Frame · gougedAFT CARGO PIT STA 1340, STR 25-27L FRAME IS GOUGED. REPAIRED FRAME AT STA 1320 BET STR 25-27L IAW SRM 53-00-07 FIG 201 REPAIR NR 5 DETAIL I. THIS REPAIR IS CATEGORY "B" MAJOR REPAIR.Jan 19, 2009 · N912FD · Boeing 75728A · Fuselage Main, FrameSDR FDEA200901130187Seat Track · corrodedSEAT TRACK STA 650 RBL 24 CORRODED. REMOVED CORROSION FOUND TO BE OUT OF LIMIT IAW SRM 53-00-52, ORIG MAT 0.100 REMAINING MAT 0.074. REMOVED SEAT TRACK IAW SRM 51-40-02 AND 53-00-52. FABRICATED NEW SEAT TRACK IAW SRM 53-00-52 FROM BAC1520-792/24 BATCH NR 11Jan 13, 2009 · N912FD · Boeing 75728A · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200901130186Channel · corrodedINTERCOSTAL ON L-1 DOOR THRESHOLD AREA HAS CORROSION, APPROX BS 346-361. REMOVED CHANNEL ON L-1 DOOR THRESHOLD FROM STA 346-STA 361 LT SIDE IAW SRM 51-40-02. REMOVED CORROSION IAW SRM 53-10-15. ORIG MAT 0.050 INCH REMAINING MAT 0.041 INCH FOUND TO BE OUT OFJan 13, 2009 · N912FD · Boeing 75728A · Fuselage Miscellaneous StructureSDR FDEA200901120169Floorbeam · corrodedMAIN CABIN FLOORBEAM STA 345 LBL 5 UPPER CHORD HAS CORROSION. REMOVED DAMAGED AREA STA 345 RBL 9 - LBL 52. FABRICATED T-CHORD MATERIAL BAC 1505-100617 BATCH NR 1512047. FABRICATED AND RECEIVED REPAIR PARTS ON MAE TRAVELER'S T8/775104, T8/775103, T8/775107,Jan 12, 2009 · N912FD · Boeing 75728A · Fuselage Main, Floor BeamSDR FDEA200901120168Stringer · corrodedELEVATOR COMPARTMENT BILGE AREA STRINGER SPLICE INNER SKIN OTBD OF DOOR 313AB LT CUTOUT AT STA 1868-1880 HAS SURFACE CORROSION. REMOVED CORROSION IAW SRM 51-10-02, FOUND OUT OF LIMITS IAW SRM 53-00-03 FIG 101 DETAIL II. RECEIVED NEW STRINGER ON TRAVELER NR TJan 12, 2009 · N912FD · Boeing 75728A · Fuselage Main, Longeron/StringerSDR FDEA200901070059Frame · gougedAFT CARGO PIT, BS 1480, S-26L, FRAME IS BENT AND GOUGED. CUT OUT DAMAGE AREA PER SRM 53-00-07, REPAIR NR 5, AT BS 1480, S-26L. REFORMED AREA PER NTM51-00-19, PART 6, NO CRACKS NOTED. FABRICATED AND RECEIVED REPAIR "J" CHANNEL PER MAE TRAVELER NR T8/772967. Jan 7, 2009 · N912FD · Boeing 75728A · Fuselage Main, FrameSDR FDEA200901040012Skin · damagedR1 DOOR INNER SKIN 5 INCH FROM TOP 10 INCH FROM AFT EDGE IS DAMAGED. REMOVED DAMAGED PORTION OF INNER SKIN IAW SRM 51-10-02 AND SRM 51-70-13 FIG 1. FABRICATED REPAIR DOUBLER PER MAE TRAVELER NR T8/773998. INSTALLED REPAIR DOUBLER IAW SRM 51-70-13 FIG 1 AND Jan 4, 2009 · N912FD · Boeing 75728A · Passenger/Crew DoorsSDR FDEA200901020006Seat Track · corrodedSEAT TRACK AT BS 640, RBL 45, HAS CORROSION. REMOVED CORROSION AT BS 640, RBL 45, IAW SRM 53-00-52, FIG 101. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101; ORIGINAL MATERIAL WAS .125 INCH, AFTER REWORK .070 INCH (L=1.0 INCH, W=.250 INCH, D=.055Jan 2, 2009 · N912FD · Boeing 75728A · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200812305321Seat Track · damagedSEAT TRACK, BS 1080-1180, RBL 45, HAS LUG DAMAGE. REMOVED AND REPLACED SEAT TRACK ASSY, IAW SRM 51-40-02. REPLACEMENT SEAT TRACK ASSY FABRICATED ON MAE TRAVELER T8/771189 IAW SRM 53-00- 52. LUG REWORK DIMENSIONS, ON DAMAGED SEAT TRACK, WERE AS FOLLOWS: L=.25Dec 30, 2008 · N912FD · Boeing 75728A · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200812265304Frame · dentedFRAME BS 760 S23 AND 24L DENTED. REPAIRED FRAME IAW SRM 53-00-07 FIG 201 REPAIR 5. THIS IS A MAJOR AND CATEGORY "B" REPAIR.Dec 26, 2008 · N912FD · Boeing 75728A · Fuselage Main, FrameSDR FDEA200812265303Door Frame · corrodedNR 2 PAX DOOR LEFT LOWER CUT OUT FRAME WEB AND ANGLE SUPPORT HAVE SEVERAL SPOT OF CORROSION AT STA 690-730. REMOVED ANGLE SUPPORT AND FABRICATED, LOCATED, DRILLED,TREATED, PRIMED AND INSTALLED NEW ANGLE SUPPORT IAW SRM51-40-02, 51-40-05, 51-40-06 AND 51-20-01.Dec 26, 2008 · N912FD · Boeing 75728A · Fuselage Main, StructureSDR FDEA200812265302Support Angle · corrodedNR 2 PASS DOOR RT SIDE LOWER CUT-OUT FRAME WEB SUPPORT ANGLE HAS SURFACE CORROSION. REMOVED AND REPLACED NR 2 PASS DOOR RT SIDE LOWER SUPPORT ANGLE IAW SRM 51-40-02 USING FABRITAED NEW CREASE BEAM . THIS IS A MAJOR AND CATEGORY "A" REPAIR.Dec 26, 2008 · N912FD · Boeing 75728A · Fuselage Miscellaneous StructureSDR FDEA200812265301Floor Panel · corrodedMAIN CABIN METAL FLOOR PANEL STA 1681 TO STA 1720 HAS CORRROSION SEVERAL SPOTS. ENTIRE AREA. REMOVED CORROSION ON IAW SRM 51-10-02, FOUND (2) SPOTS OUT OF LIMITS, FABRICATED. (2) DOUBLER REPAIRS IAW SRM 53-60- 51; ALTERNATIVE 1-REPAIR 2, TREATED, PRIMED ANDec 26, 2008 · N912FD · Boeing 75728A · Fuselage Floor PanelSDR FDEA200812245286Frame · dentedFWD PIT, FUSELAGE FRAME BS 780, INNER CHORD, (SLOPING), BETWEEN S24R AND S25R, HAS A DENT. REMOVED DAMAGED SECTION OF BS 780 FRAME, BETWEEN S24R AND S25R, PER SRM 53-00- 07, REPAIR NR 5. RECEIVED FABRICATED FRAME REPAIR PARTS ON MAE TRAVELER NR T8/772747. Dec 24, 2008 · N912FD · Boeing 75728A · Fuselage Main, FrameSDR FDEA200812205253Floorbeam · corrodedMAIN CABIN FLOORBEAM UPPER CHORD STA 365 FROM BL 0 TO RBL 65 HAS CORROSION. REMOVED PREVIOUS TEE REPAIR FROM STA 365 LBL 17 TO RBL 70 IAW SRM 53-00-51 FIG 201 REPAIR NR 3. FABRICATED TEE AND REPAIR PARTS IAW SRM 53-00-51 FIG 201. INSTALLED TEE AND REPAIR PADec 20, 2008 · N912FD · Boeing 75728A · Fuselage Main, Floor BeamSDR FDEA200812155172Frame · gougedMAIN CABIN STA. 1280 STR.11-14L FRAME IS GOUGED. CUT, REMOVED, FABRICATE AND INSTALLED REPAIR PARTS AS PER MAE TRAVELER NR T8/769971 AND T8/769950 IAW SRM 53-00-07 FIG 201, SRM 51-40-05 AND AMM 51-21-00-7. REPAIRED GOUGED FRAME IAW SRM 53-00-07, REPAIR NR 1 Dec 15, 2008 · N912FD · Boeing 75728A · Fuselage Main, FrameSDR FDEA200812145140Frame · damagedAFT CARGO PIT STA.1540 STR 25R FRAME HAS A MISDRILLED HOLE. REPAIRED AFT CARGO PIT STA 1540 STR 25R FRAME IAW SRM 53-00-07 FIG 201 REPAIR 5 ZONE 1.I INSPECTION THRESHOLD 37500 FLIGHT CYCLES AFTER REPAIR INSTALLATION OR 50000 AIRFRAME FLIGHT CYCLES, WHICHEVDec 14, 2008 · N912FD · Boeing 75728A · Fuselage Main, FrameSDR FDEA200812145139Frame Splice · gougedAFT CARGO PIT STA 1560 STR 24-25R, FRAME AND FRAME SPLICE ARE GOUGED. BLENDED AND SMOOTHED FRAME FOUND WITHIN LIMITS IAW SRM 53-60-07 AND SRM 53-00-07 FIG 101 DETAIL 2. REMOVED AND FABRICATED NEW SPLICE FRAME WITH MAE TRAVELER NR T8/771003, LOCATED, DRILLED Dec 14, 2008 · N912FD · Boeing 75728A · Fuselage Main, FrameSDR 08FDEA04971Seat Track · corrodedSEAT TRACK BS 418-440, RBL 45, IS GOUGED AND CORRODED. REMOVED CORROSION FROM SEAT TRACK, BS 418-440, RBL 45, IAW SRM 53-00-52. FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-00-52. .021 INCH MATERIAL REMOVED. REMOVED SEAT TRACK, BS 418-440, RBL 45, IAW SRM Nov 24, 2008 · N912FD · Boeing 75728A · Fuselage, Seat/Cargo Attach Fittings
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