# Service difficulty reports: N306WA, cancelled May 4, 2007 A list on [N306WA, cancelled May 4, 2007](https://openairdocs.org/deregistered/N306WA-2007-05-04.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR DL733060250](https://openairdocs.org/sdr/DL733060250.md): Stiffener · cracked · Mar 29, 2006 · N306WA · Boeing 737347 · Wing Miscellaneous Structure > DURING ACCOMPLISHMENT OF 05-086589-12AD, THE WING CENTER SECTION REAR SPAR STIFFENER AT LBL 6.15 WAS FOUND CRACKED. REPLACED REAR SPAR STIFFENER. - [SDR DL733050148](https://openairdocs.org/sdr/DL733050148.md): Skin · cracked · Mar 3, 2005 · N306WA · Boeing 737347 · Fuselage Main, Plate/Skin > THE FUSELAGE SKIN WAS FOUND WITH A 4 INCH CRACK AT FS 870 JUST ABOVE THE BONDED DOUBLER MILL LINE AT STRINGER 23R. THE CRACK IS TYPICAL OF AD 2004-18-06. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER B737-300 S - [SDR DL733030081](https://openairdocs.org/sdr/DL733030081.md): Coffeemaker · odor · Jan 23, 2003 · N306WA · Boeing 737347 · Buffet/Galleys > FLT ATTENDANT VERBAL REPORT, LT AFT GALLEY COFFEEMAKER HAS ELECTRIC ODOR. REPLACED COFFEEMAKER, OPS CHECK NORMAL. NO ODOR. - [SDR DL733021369](https://openairdocs.org/sdr/DL733021369.md): Attach Fitting · corroded · Nov 25, 2002 · N306WA · Boeing 737347 · Vertical Stabilizer, Attach Fittings > CORROSION WAS FOUND ON THE AFT FACE OF THE #3 LUG AND THE FORWARD FACE OF THE #6 LUG OF THE VERTICAL STABILIZER FIN ATTACH LUGS. THE CORROSION WAS REMOVED AND NEW BUSHINGS INSTALLED. THE DAMAGE WAS FOUND AT HMV. - [SDR DL733021368](https://openairdocs.org/sdr/DL733021368.md): Skin Panel · cracked · Nov 25, 2002 · N306WA · Boeing 737347 · Fuselage Main, Floor Beam > SEVERAL CRACKS WERE FOUND IN THE KEEL BEAM LOWER SKIN PANEL FROM FS 661 TO FS 727. THE SKIN PANEL WAS REPLACED PER S/B 737-53-1104. THE DAMAGE WAS FOUND AT HMV. - [SDR DL733021367](https://openairdocs.org/sdr/DL733021367.md): Fitting · corroded · Nov 25, 2002 · N306WA · Boeing 737347 · Fuselage, Stabilizer Attach Fittings > CORROSION WAS FOUND IN THE LUB BORE OF THE LHS FORWARD CLEVIS LUG. THE LUG BORE WAS OVERSIZED TO 1.4385" AND AN OVERSIZED BUSHING WAS INSTALLED. THE DAMAGE WAS FOUND AT HMV. - [SDR DL733021366](https://openairdocs.org/sdr/DL733021366.md): Wedge · delaminated · Nov 25, 2002 · N306WA · Boeing 737347 · Trailing Edge Flaps > RH INBD MID FLAP T/E WEDGE DISBONDED. REPAIRED PER ER/A 418047-14. - [SDR DL733021365](https://openairdocs.org/sdr/DL733021365.md): Wedge · delaminated · Nov 25, 2002 · N306WA · Boeing 737347 · Trailing Edge Flaps > TE WEDGE DISBONDED. REPAIRED PER ER/A 418046-14. - [SDR DL733021347](https://openairdocs.org/sdr/DL733021347.md): Beam · worn · Nov 20, 2002 · N306WA · Boeing 737347 · Nacelle/Pylon, Main Frame > WORN AREAS WERE FOUND ON THE CROWN BEAM LUG BORES OF THE #1 AND #2 PYLONS. THE BORES WERE OVERSIZED TO 3.100" AND 3.102 RESPECTIVELY. REPAIR BUSHINGS WERE INSTALLED. THE DAMAGE WAS FOUND AT HMV. - [SDR DL733021346](https://openairdocs.org/sdr/DL733021346.md): Spar · damaged · Nov 20, 2002 · N306WA · Boeing 737347 · Wing Spar > WHILE REPLACING THE MLG BEAM SUPPORT FITTING A FASTENER HOLE WAS DAMAGED IN THE REAR SPAR CHORD AND REAR SPAR WEB. THE HOLE WAS OVERSIZED AND A REPAIR BUSHING INSTALLED. - [SDR DL733021059](https://openairdocs.org/sdr/DL733021059.md): Skin · delaminated · Sep 6, 2002 · N306WA · Boeing 737347 · Trailing Edge Flaps > RT WING INBOARD MID FLAP WEDGE IS DISBONDED. REPAIR PER ER/A 417696-14. - [SDR DL733021057](https://openairdocs.org/sdr/DL733021057.md): Wedge · damaged · Sep 4, 2002 · N306WA · Boeing 737347 · Trailing Edge Flaps > DAMAGE TO LT WING INBOARD MID FLAP WEDGE. REPAIR PER ER/A 417684-14. - [SDR DL733010042](https://openairdocs.org/sdr/DL733010042.md): Frame · cracked · Jan 7, 2001 · N306WA · Boeing 737347 · Fuselage Main, Bulkhead > INSPECTIONS OF THE FS 178 BULKHEAD PER AD 200-05-29 REVEALED A 2 INCH CRACK IN THE RT SIDE CHORD AT WL 207. THE DAMAGED CHORD WAS REMOVED AND A NEW SECTION INSTALLED TO ELIMINATE THE CRACK CONDITION. THE REPAIR WAS ACCOMPLISHED PER ER/A 379675-14AD, REV A. - [SDR DL733002248](https://openairdocs.org/sdr/DL733002248.md): Generator · failed · Nov 17, 2000 · N306WA · Boeing 737347 · AC Generation System > FLT1799/16 SLC-COS. DURING DESCENT FROM FL370 RT GEN DROPPED OFFLINE, 10 SEC LATER LT GEN DROPPED OFFLINE. UNABLE TO RESET GENERATORS PER POM. DID NOT START APU. CONCLUDED DESCENT AND APPROACH. REPLACED NR 1 GCU PER MM. MCO''D NR 2 GENERATOR PER MEL 24-0 - [SDR DL733000730](https://openairdocs.org/sdr/DL733000730.md): Slide · deployed · Apr 15, 2000 · N306WA · Boeing 737347 · Escape Slide > THE R-1 DOOR SLIDE WAS INADVERTENTLY DEPLOYED. SLIDE INFLATED AND DEPLOYED CORRECTLY. - [SDR DL733992711](https://openairdocs.org/sdr/DL733992711.md): Socket · failed · Dec 11, 1999 · N306WA · Boeing 737347 · Passenger Compartment Lighting > ELECTRICAL SMELL IN CABIN. FOUND FLUORESCENT OVERHEAD LIGHT TUBE FWD SOCKET AT 13 A, B, C MELTING. REMOVED LIGHT TUBE AND REPLACED SOCKET. - [SDR DL733991658](https://openairdocs.org/sdr/DL733991658.md): Reverse Light · illuminated · Jul 23, 1999 · N306WA · Boeing 737347 · Engine Thrust Reverser > NR 2 ENG REV LIGHT CAME ON DURING TAKEOFF. ABORTED TAKE OFF JUST UNDER 100 KTS. LOCKED OUT NR 2 ENG REV PER MEL 78-00-02. MCO - CLEANED CONNECTORS. UNABLE TO DUPLICATE, REMOVED. - [SDR DL733991265](https://openairdocs.org/sdr/DL733991265.md): Smoke Detector · failed · Jun 5, 1999 · N306WA · Boeing 737347 · Smoke Detection > LAV SMOKE FALSE ALARM. ACTIVATED TWICE IN FLIGHT. CIRCUIT BREAKER PULLED TO SILENCE ALARM. REPLACED FWD SMOKE DETECTOR. - [SDR DL733982662](https://openairdocs.org/sdr/DL733982662.md): Skin · damaged · Dec 31, 1998 · N306WA · Boeing 737347 · Fuselage Main, Plate/Skin > DURING INSPECTION OF C1 DOOR CUTOUT SKIN AN EXISTING REPAIR WAS REMOVED FOR INSPECTABILITY OF THE AREA. REPAIRED AND REWORKED PER ERA 332586-14. - [SDR DL733982661](https://openairdocs.org/sdr/DL733982661.md): Skin · cracked · Dec 31, 1998 · N306WA · Boeing 737347 · Fuselage Main, Plate/Skin > FUSE SKIN FOUND CRACKED AT BS 727E, S23L. DAMAGE REMOVAL RESULTED IN A 4.75 BY 2 INCH CUT OUT. REPAIRED PER ERA 332622-14. - [SDR DL733982660](https://openairdocs.org/sdr/DL733982660.md): Web · cracked · Dec 31, 1998 · N306WA · Boeing 737347 · Fuselage Miscellaneous Structure > CRACK WAS FOUND DURING INSPECTION PER EO 5-70166-3 IN THE WEB AT BS 727, S18A (LHS). THE CRACK EXCEEDED EO/SB LIMITS. REPAIRED PER ERA 332607-14. - [SDR DL733982646](https://openairdocs.org/sdr/DL733982646.md): Bulkhead Web · cracked · Dec 29, 1998 · N306WA · Boeing 737347 · Fuselage Main, Bulkhead > DURING ACCOMPLISHMENT OF SI 5-69482-12, SEVERAL CRACKS WERE DISCOVERED ON THE FWD FACE OF THE BS 178 BLKD. REPAIRED PER ERA 332599-14. - [SDR DL733961361](https://openairdocs.org/sdr/DL733961361.md): Window · cracked · Jun 4, 1996 · N306WA · Boeing 737347 · Passenger Compartment Windows > SEAT 10A PSGR CABIN WINDOW HAS SEVERAL CIRCULAR CRACKS ON OUTER WINDOW. WINDOW CRACKED AT SEAT 10F DURING PRESSURE CK FOR BROKEN WINDOW AT 10A. CABIN WAS PRESSURIZED TO 4.2 PSI, CABIN RATE OF CLIMB UP AND DOWN NEVER EXCEEDED 1,000 FPM. ## 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 = 'N306WA' AND deregistration_id = 'N306WA-2007-05-04' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N306WA-2007-05-04/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.