# Service difficulty reports: N63305, cancelled Mar 21, 2013 A list on [N63305, cancelled Mar 21, 2013](https://openairdocs.org/deregistered/N63305-2013-03-21.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 · 111 reports - [SDR CALA2009121700730](https://openairdocs.org/sdr/CALA2009121700730.md): Cooling Fan · inoperative · Dec 17, 2009 · N63305 · Boeing 7373T0 · Air Distribution Fan > VERY STRONG SMELL OF SOMETHING BURNING THROUGHOUT CABIN, MADE IT INTO COCKPIT. SULFUR LIKE SMELL. PERFORMED CONDITIONAL INSP AMM 05-51-95 FOUND NORMAL FAN C/B OUT VERIFIED BLOWER WAS CAUSE OF SMELL. PERFORMED ENG RUN IN NORMAL CONDITION, NO FAULTS NOTED. R - [SDR CALA2009071500372](https://openairdocs.org/sdr/CALA2009071500372.md): Skin · cracked · Jul 15, 2009 · N63305 · Boeing 7373T0 · Fuselage Main, Plate/Skin > FUSELAGE SKIN CRACKED AT EMERGENCY LIGHT S22L, CRACK APPROXIMATELY 1 INCH LONG. INSTALLED REPAIR PER SRM 53-00-01, REPAIR 31, FIG 201, PROCEDURE V. ISSUED DIP PER EC/RA 5331-01399 TO READ, BEFORE THE ACCUMULATION OF 60,000 TOTAL AIRCRAFT FLIGHT CYCLES. ACCO - [SDR CALA2009061500312](https://openairdocs.org/sdr/CALA2009061500312.md): Light · inoperative · Jun 13, 2009 · N63305 · Boeing 7373T0 · Emergency Lighting > L1 INSIDE EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LIGHT ASSY, OPS NORMAL. - [SDR CALA2009041400198](https://openairdocs.org/sdr/CALA2009041400198.md): Skin · cracked · Apr 14, 2009 · N63305 · Boeing 7373T0 · Fuselage Main, Plate/Skin > RT AFT FUSELAGE SKIN CRACKED 11 INCHES AFT OF FAIRING AND 11 INCHES ABOVE LAP JOINT. FABRICATED AND INSTALLED REPAIR PER SRM 53-00-01 FIG 201. - [SDR CALA2009020500086](https://openairdocs.org/sdr/CALA2009020500086.md): Skin · cracked · Feb 4, 2009 · N63305 · Boeing 7373T0 · Fuselage Main, Plate/Skin > AFT RIGHT FUSELAGE SKIN 36 INCHES FORWARD OF CARGO AT S19 R CRACKED 1.125 INCH LONG. COMPLIED WITH HFEC, CRACK VERIFIED PER NDT PART 61-00-00 FIG 23. REPAIRED IN ACCORDANCE WITH SRM 53-00-01, REPAIR 31, DETAIL FIG 201. - [SDR CALA2009011300031](https://openairdocs.org/sdr/CALA2009011300031.md): Cable · frayed · Jan 1, 2009 · N63305 · Boeing 7373T0 · Escape Slide > L-2 DOOR EMERGENCY ESCAPE SLIDE CABLE HAS BROKEN STRANDS. REMOVED AND REPLACED L2 DOOR EMERGENCY ESCAPE SLIDE CABLE IAW AMM 25-61-35. - [SDR CALA2009011300030](https://openairdocs.org/sdr/CALA2009011300030.md): Cable · frayed · Dec 31, 2008 · N63305 · Boeing 7373T0 · Escape Slide > R-2 DOOR EMERGENCY ESCAPE SLIDE CABLE HAS BROKEN STRANDS. REMOVED AND REPLACED R2 DOOR EMERGENCY ESCAPE SLIDE CABLE IAW AMM 25-61-35. - [SDR CALA0700691](https://openairdocs.org/sdr/CALA0700691.md): Bracket · corroded · Nov 15, 2007 · N63305 · Boeing 7373T0 · Fuselage Miscellaneous Structure > INSPECTION FOUND INTERGRANULAR CORROSION ON AFT LAV SERVICE SUPPORT HAT BRACKET AT STA 986.5-1016, S24R TO 25R. THE BRACKET ASSEMBLY WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND BAC DRAWING 69-36677. - [SDR CALA0700690](https://openairdocs.org/sdr/CALA0700690.md): Channel · corroded · Nov 15, 2007 · N63305 · Boeing 7373T0 · Fuselage Miscellaneous Structure > INSPECTION FOUND AFT DRAIN MAST MOUNTING CHANNEL CORRODED FROM STA 967-986.5 BETWEEN S24L AND S25L. THE DRAIN MAST CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND BAC DRAWING 65-55843. - [SDR CALA0700680](https://openairdocs.org/sdr/CALA0700680.md): Stringer · corroded · Nov 12, 2007 · N63305 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND STRINGER 26L CORRODED AT STA 907-1016. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 51-40-02, PAGE 1. - [SDR CALA0700681](https://openairdocs.org/sdr/CALA0700681.md): Shear Tie · corroded · Nov 10, 2007 · N63305 · Boeing 7373T0 · Fuselage Internal Mounting Structure > INSPECTION FOUND FUSELAGE SKIN BULGED WITH RIVETS PULLED TO THE RIGHT OF STRINGER 27L AT STA 1006. A CORRODED SKIN CLIP WAS REMOVED AND REPLACED IAW SRM 51-10-02. - [SDR CALA0700679](https://openairdocs.org/sdr/CALA0700679.md): Stringer · corroded · Nov 10, 2007 · N63305 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND STRINGER 27L CORRODED AT STA 980-996. THE CORRODED SECTION OF STRINGER WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-00-03, REPAIR 1. - [SDR CALA0700678](https://openairdocs.org/sdr/CALA0700678.md): Stringer · corroded · Nov 10, 2007 · N63305 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND STRINGER 25L CORRODED AT STA 960-980. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 53-00-03, REPAIR 1. - [SDR CALA0700413](https://openairdocs.org/sdr/CALA0700413.md): Stringer · corroded · Aug 5, 2007 · N63305 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND O/B SIDE OF STRINGER 27L CORRODED APPROXIMATELY 2 INCHES FORWARD OF STA 500D IN FORWARD BAGGAGE BIN. A DOUBLER REPAIR WAS INSTALLED IAW SRM 5331-01336. - [SDR CALA0700412](https://openairdocs.org/sdr/CALA0700412.md): Shear Tie · corroded · Aug 5, 2007 · N63305 · Boeing 7373T0 · Fuselage Internal Mounting Structure > INSPECTION FOUND SHEAR TIE CORRODED AT STA 460 BETWEEN STRINGERS 27R AND S28R. THE SHEAR TIE WAS REPAIRED IAW SRM 53-00-07. - [SDR CALA0700410](https://openairdocs.org/sdr/CALA0700410.md): Skin · cracked · Aug 3, 2007 · N63305 · Boeing 7373T0 · Fuselage Main, Plate/Skin > INSPECTION FOUND A.25 INCH CRACK IN RIGHT FUSELAGE SKIN ABOVE SKIN LAP S25R APPROXIMATELY 6 INCHES FORWARD OF STA 887. THE SKIN WAS REPAIRED IAW SRM 53-00-01, PRODECURE 5, PAGE 203, REPAIR 31. - [SDR CALA0700409](https://openairdocs.org/sdr/CALA0700409.md): Frame · cracked · Aug 3, 2007 · N63305 · Boeing 7373T0 · Fuselage Main, Frame > INSPECTION FOUND A.25 INCH CRACK IN FRAME AT STA 727D, S9L. THE FRAME WAS REPAIRED IAW ECRA 5310-04643. - [SDR CALA0700408](https://openairdocs.org/sdr/CALA0700408.md): Stringer Splice · cracked · Aug 3, 2007 · N63305 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND A.25 INCH CRACK IN STRINGER SPLICE AT STA 359, S15L. REPAIRED IAW ECRA 5311-01346. - [SDR CALA0700407](https://openairdocs.org/sdr/CALA0700407.md): Frame · cracked · Aug 3, 2007 · N63305 · Boeing 7373T0 · Fuselage Main, Frame > INSPECTION FOUND A.25 INCH CRACK IN FRAME AT STA 867, S9R. REPAIRED IAW ECRA 5310-04643. - [SDR CALA0700406](https://openairdocs.org/sdr/CALA0700406.md): Frame · cracked · Aug 3, 2007 · N63305 · Boeing 7373T0 · Fuselage Main, Frame > INSPECTION FOUND A.25 INCH CRACK IN FRAME AT STA 887, S9R. REPAIRED IAW ECRA 5310-04643. - [SDR CALA0700405](https://openairdocs.org/sdr/CALA0700405.md): Frame · cracked · Aug 3, 2007 · N63305 · Boeing 7373T0 · Fuselage Main, Frame > INSPECTION FOUND A.25 INCH CRACK IN FRAME AT STA 867, S9L. THE FRAME WAS REPAIRED IAW ECRA 5310-04643. - [SDR CALA0700404](https://openairdocs.org/sdr/CALA0700404.md): Frame · cracked · Aug 3, 2007 · N63305 · Boeing 7373T0 · Fuselage Main, Frame > INSPECTION FOUND A.25 INCH CRACK IN FRAME AT STA 887, S9L. THE FRAME WAS REPAIRED IAW ECRA 5310-04643. - [SDR CALA0700403](https://openairdocs.org/sdr/CALA0700403.md): Frame · cracked · Aug 3, 2007 · N63305 · Boeing 7373T0 · Fuselage Main, Frame > INSPECTION FOUND A.25 INCH CRACK IN FRAME AT RIVET THAT ATTACHES AIR GRILL, STA 380, S9R. REPAIRED IAW ECRA 5310-04643. - [SDR CALA0700402](https://openairdocs.org/sdr/CALA0700402.md): Frame · cracked · Aug 3, 2007 · N63305 · Boeing 7373T0 · Fuselage Main, Frame > INSPECTION FOUND A.25 INCH CRACK IN FRAME AT RIVET THAT ATTACHES AIR GRILL, STA 400, S9L. A FRAME REPAIR WAS INSTALLED IAW ECRA 5310-04643. - [SDR CALA0700401](https://openairdocs.org/sdr/CALA0700401.md): Stringer · cracked · Aug 3, 2007 · N63305 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND A.25 INCH CRACK IN STRINGER 14L AT STA 360. REPAIRED IAW ECRA 5311-01346. - [SDR CALA0700400](https://openairdocs.org/sdr/CALA0700400.md): Frame · cracked · Aug 3, 2007 · N63305 · Boeing 7373T0 · Fuselage Main, Frame > INSPECTION FOUND A.25 INCH CRACK IN FRAME AT RIVET THAT ATTACHES AIR GRILL, STA 480, S9R. REPAIRED IAW ECRA 5110-04643. - [SDR CALA0700399](https://openairdocs.org/sdr/CALA0700399.md): Frame · cracked · Aug 3, 2007 · N63305 · Boeing 7373T0 · Fuselage Main, Frame > INSPECTION FOUND A.25 INCH CRACK IN FRAME AT STA 767, S9L. THE FRAME WAS REPAIRED IAW ECRA 5310-04643. - [SDR CALA0700398](https://openairdocs.org/sdr/CALA0700398.md): Frame · cracked · Aug 3, 2007 · N63305 · Boeing 7373T0 · Fuselage Main, Frame > INSPECTION FOUND A.25 INCH CRACK IN FRAME AT STA 787, S9R. THE FRAME WAS REPAIRED IAW ECRA 5310-04643. - [SDR CALA0700397](https://openairdocs.org/sdr/CALA0700397.md): Frame · cracked · Aug 3, 2007 · N63305 · Boeing 7373T0 · Fuselage Main, Frame > INSPECTION FOUND A.25 INCH CRACK IN FRAME AT STA 847, S9L. THE FRAME WAS REPAIRED IAW ECRA 5310-04643. - [SDR CALA0700394](https://openairdocs.org/sdr/CALA0700394.md): Keelbeam · corroded · Aug 3, 2007 · N63305 · Boeing 7373T0 · Fuselage Main, Keel > INSPECTION FOUND LEFT KEEL BEAM CORRODED ON O/B FLANGE IN FORWARD BAGGAGE BIN AT STA 520, S28L. THE KEEL BEAM WAS REPAIRED IAW SRM 53-60-12. - [SDR CALA0700393](https://openairdocs.org/sdr/CALA0700393.md): Frame · corroded · Aug 3, 2007 · N63305 · Boeing 7373T0 · Fuselage Main, Frame > INSPECTION FOUND AFT BAGGAGE BIN FRAME CORRODED AT STA 794.3, S25R TO S26R. A NEW FRAME WAS INSTALLED IAW SRM 51-40-02. - [SDR CALA0700390](https://openairdocs.org/sdr/CALA0700390.md): Skin · burned · Aug 2, 2007 · N63305 · Boeing 7373T0 · Fuselage Main, Plate/Skin > INSPECTION FOUND A BURN SPOT ON FUSELAGE SKIN 2.25 INCHES AFT OF STA 727 AND 2.25 INCHES ABOVE S23L. A REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 201, REPAIR 31, PAGE 231. - [SDR CALA0700385](https://openairdocs.org/sdr/CALA0700385.md): Rail · cracked · Jul 30, 2007 · N63305 · Boeing 7373T0 · Fuselage Main, Attach Fittings > INSPECTION FOUND A 1 INCH CRACK IN AFT BAGGAGE BIN TIE DOWN RAIL AT STA 727E, S27R. THE TIE DOWN RAIL WAS REMOVED AND A NEW SECTION OF TIE DOWN RAIL WAS INSTALLED IAW SRM 53-00-53, REPAIR 2, PAGE 202. - [SDR CALA0700384](https://openairdocs.org/sdr/CALA0700384.md): Channel · corroded · Jul 30, 2007 · N63305 · Boeing 7373T0 · Fuselage Miscellaneous Structure > INSPECTION FOUND AFT BAGGAGE BIN FLOOR CHANNEL CORRODED AT STA 727D + 8 INCHES, RBL 3. REPAIRED IAW SRM 53-00-53. - [SDR CALA0700383](https://openairdocs.org/sdr/CALA0700383.md): Channel · cracked · Jul 30, 2007 · N63305 · Boeing 7373T0 · Fuselage Miscellaneous Structure > INSPECTION FOUND A 1 INCH CRACK IN NR 1 VHF ANTENNA MOUNT CHANNEL ON BOTH ENDS AT STA 500-500A, S29R TO 29L. THE ANTENNA CHANNEL WAS REPLACED IAW SRM 51-40-02. - [SDR CALA0700382](https://openairdocs.org/sdr/CALA0700382.md): Structure · corroded · Jul 30, 2007 · N63305 · Boeing 7373T0 · Fuselage Miscellaneous Structure > INSPECTION FOUND LOWER FUSELAGE O/B CHORD CORRODED AT STA 227.8, LBL5.7 TO RBL 5.7. REPAIRED IAW ECRA 5311-01345. - [SDR CALA0700376](https://openairdocs.org/sdr/CALA0700376.md): Frame · corroded · Jul 26, 2007 · N63305 · Boeing 7373T0 · Fuselage Main, Frame > INSPECTION FOUND FRAME CORRODED AT STA 847, S25R TO S26R. THE FRAME WAS REPLACED IAW SRM 51-40-02. - [SDR CALA0700375](https://openairdocs.org/sdr/CALA0700375.md): Skin · cracked · Jul 26, 2007 · N63305 · Boeing 7373T0 · Fuselage Main, Plate/Skin > INSPECTION FOUND A.5 INCH CRACK IN FUSELAGE SKIN ABOVE L-2 DOOR UPPER HINGE, STA 947.5, S11L T0 14L. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-60-01. - [SDR CALA0700372](https://openairdocs.org/sdr/CALA0700372.md): Intercostal · cracked · Jul 23, 2007 · N63305 · Boeing 7373T0 · Fuselage Miscellaneous Structure > INSPECTION FOUND A.75 INCH CRACK IN INTERCOSTAL WEB AT STA 357, S16L. REPAIR PARTS WERE INSTALLED IAW SRM 53-10-04. - [SDR CALA0700371](https://openairdocs.org/sdr/CALA0700371.md): Seat Track · corroded · Jul 21, 2007 · N63305 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND THE FORWARD ENTRY RIGHT O/B SEAT TRACK CORRODED BETWEEN STA 328 AND 360, RBL 36. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52. - [SDR CALA0700370](https://openairdocs.org/sdr/CALA0700370.md): Angle · corroded · Jul 21, 2007 · N63305 · Boeing 7373T0 · Fuselage Miscellaneous Structure > INSPECTION FOUND R-1 DOOR Z-ANGLE CORRODED IN SEVERAL AREAS FROM STA 294.5 TO 360, RBL 48. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02. - [SDR CALA0700369](https://openairdocs.org/sdr/CALA0700369.md): Seat Track · corroded · Jul 21, 2007 · N63305 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND FORWARD ENTRY RIGHT I/B SEAT TRACK CORRODED BETWEEN STA 328 AND 360, RBL 20. A REPAIR WAS INSTALLED IAW SRM 53-00-52. - [SDR CALA0700368](https://openairdocs.org/sdr/CALA0700368.md): Skin · cracked · Jul 19, 2007 · N63305 · Boeing 7373T0 · Fuselage Main, Plate/Skin > INSPECTION FOUND A 1 INCH CRACK AT AFT LOWER CORNER OF R-1 DOOR CUTOUT OUTER SKIN, STA 344-360, S16R TO S17R. THE SKIN WAS REPAIRED IAW SRM 53-10-01. - [SDR CALA0700367](https://openairdocs.org/sdr/CALA0700367.md): Floorbeam · corroded · Jul 19, 2007 · N63305 · Boeing 7373T0 · Fuselage Main, Floor Beam > INSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED THE ENTIRE LENGTH, AT STA 328, LBL 45 TO RBL 45. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-51. - [SDR CALA0700366](https://openairdocs.org/sdr/CALA0700366.md): Floorbeam · corroded · Jul 19, 2007 · N63305 · Boeing 7373T0 · Fuselage Main, Floor Beam > INSPECTION FOUND UPPER SURFACE OF FLOORBEAM CORRODED AT STA 344, LBL 17 TO RBL 12. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-51. - [SDR CALA0700440](https://openairdocs.org/sdr/CALA0700440.md): Door Frame · cracked · Jul 18, 2007 · N63305 · Boeing 7373T0 · Fuselage Main, Structure > INSPECTION FOUND A CRACK IN THE AFT CARGO DOOR CUTOUT STA 794.3 FRAME. THE FRAME WAS REPAIRED IAW ECRA 5311-01344. - [SDR CALA0700365](https://openairdocs.org/sdr/CALA0700365.md): Skin · cracked · Jul 18, 2007 · N63305 · Boeing 7373T0 · Fuselage Main, Plate/Skin > INSPECTION FOUND A.5 INCH CRACK IN FUSELAGE SKIN BELOW R-2 DOOR LOWER HINGE AT STA 947.5-967, S13R TO S14R. - [SDR CALA0700363](https://openairdocs.org/sdr/CALA0700363.md): Frame · cracked · Jul 16, 2007 · N63305 · Boeing 7373T0 · Fuselage Main, Frame > INSPECTION FOUND A.25 INCH CRACK IN MAIN FRAME AT STA 616, LBL 55. A REPAIR WAS INSTALLED IAW ECRA 5311-01158. - [SDR CALA0700362](https://openairdocs.org/sdr/CALA0700362.md): Floorbeam · corroded · Jul 16, 2007 · N63305 · Boeing 7373T0 · Fuselage Main, Floor Beam > INSPECTION FOUND FLOORBEAM CORRODED AT STA 1016, LBL 26 TO RBL 30. THE FLOORBEAM UPPER CHORD WAS REPLACED IAW ECRA 5310-03851. - [SDR CALA0700357](https://openairdocs.org/sdr/CALA0700357.md): Seat Track · corroded · Jul 15, 2007 · N63305 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND RIGHT O/B SEAT TRACK CORRODED AT STA 887-927, RBL 20. A REPAIR SPLICE SEAT TRACK WAS INSTALLED IAW SRM 53-00-52, REPAIR 3, FIGURE 201. Next page: https://openairdocs.org/deregistered/N63305-2013-03-21/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 = 'N63305' AND deregistration_id = 'N63305-2013-03-21' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N63305-2013-03-21/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.