# Service difficulty reports: N308DL, cancelled Oct 1, 2009 A list on [N308DL, cancelled Oct 1, 2009](https://openairdocs.org/deregistered/N308DL-2009-10-01.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 2 · 51 reports - [SDR DL73S060241](https://openairdocs.org/sdr/DL73S060241.md): Floor Support · misinstalled · Apr 1, 2006 · N308DL · Boeing 737232 · Fuselage Miscellaneous Structure > FUSELAGE OVERWING FLOOR SUPPORT CHANNELS ARE NOT APPROVED PER AD 2001-17-18. FLOORBEAM CHANNELS REPLACED. - [SDR DL73S060255](https://openairdocs.org/sdr/DL73S060255.md): Lap Joint · cracked · Mar 29, 2006 · N308DL · Boeing 737232 · Fuselage Main, Plate/Skin > TWO CRACKS WERE FOUND IN THE FUSELAGE SKIN AT BS 440 AND BS 460 ALONG THE S-10L LAP JOINT. THE DAMAGED SKIN WAS REMOVED AND A REPAIR DOULBER WAS INSTALLED. - [SDR DL73S060254](https://openairdocs.org/sdr/DL73S060254.md): Lap Joint · cracked · Mar 29, 2006 · N308DL · Boeing 737232 · Fuselage Main, Plate/Skin > TWO CRACKS WERE FOUND AT STA 777 IN THE STR-4R LAP JOINT. REMOVED CRACKED SKIN AND INSTALLED REPAIR DOUBLER PER SRM 53-30-03. - [SDR DL73S060253](https://openairdocs.org/sdr/DL73S060253.md): Lap Joint · cracked · Mar 29, 2006 · N308DL · Boeing 737232 · Fuselage Main, Plate/Skin > THREE CRACKS ALONG THE S-10R LAP JOINT WERE FOUND. THE DAMAGED SKIN WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED. - [SDR DL73S060252](https://openairdocs.org/sdr/DL73S060252.md): Lap Joint · cracked · Mar 29, 2006 · N308DL · Boeing 737232 · Fuselage Main, Plate/Skin > FOUR CRACKS WERE FOUND ALONG THE S14R LAP JOINT AT BS 460, BS 470, BS 480-500, AND BS 500A. CRACKED SKIN WAS CUT OUT AND A DOUBLER WAS INSTALLED. - [SDR DL73S060251](https://openairdocs.org/sdr/DL73S060251.md): Lap Joint · cracked · Mar 29, 2006 · N308DL · Boeing 737232 · Fuselage Main, Plate/Skin > A CRACK WAS FOUND AT STA 867 IN THE S4R LAP JOINT. DAMAGED SKIN WAS REMOVED AND A DOULBER WAS INSTALLED. - [SDR DL73S060249](https://openairdocs.org/sdr/DL73S060249.md): Lap Joint · cracked · Mar 29, 2006 · N308DL · Boeing 737232 · Fuselage Main, Plate/Skin > MULTIPLE CRACKS WERE FOUND IN THE S4R LAP JOINT BETWEEN BS 360-540. SKIN LAP JOINT WAS REMOVED AND REPLACED WITH A FULL PANEL LENGTH LAP SPLICE REPAIR. - [SDR DL73S060240](https://openairdocs.org/sdr/DL73S060240.md): Frame · cracked · Mar 29, 2006 · N308DL · Boeing 737232 · Fuselage Main, Frame > THE STA 787 FRAME WEB AT S-13L IS CRACKED. INSTALLED REPAIRS PER SRM 53-10-4, FIG 1. - [SDR DL73S050516](https://openairdocs.org/sdr/DL73S050516.md): Coalescer Bag · contaminated · Sep 5, 2005 · N308DL · Boeing 737232 · Humidity Control System > STRONG BURNING RUBBER ODOR ON LIFT OFF. ODOR NOTICED IN COCKPIT AND CABIN. RAN ENGS TO TAKEOFF PWR PER PFHB NTF. REPLACED WATER SEPARATOR BAGS AS PRECAUTIONARY. - [SDR DL73S050496](https://openairdocs.org/sdr/DL73S050496.md): Skin · cracked · Aug 27, 2005 · N308DL · Boeing 737232 · Fuselage Main, Plate/Skin > FUSEALGE SKIN CRACKS WAS FOUND AT FS 727B ABOVE STRINGER 20R AT A CHEM MILL LOCATION. THE DAMAGE WAS IDENTIFIED AND REMOVED AN A REPAIR INSTALLED FOLLOWING THE INSTRUCTIONS OF THE B737-200 SRM 53-30-3 FIGURE 48. THE REPAIR IS INSTALLED FOLLOWING INSTRUCTIONS - [SDR DL73S050060](https://openairdocs.org/sdr/DL73S050060.md): Engine · malfunctioned · Jan 26, 2005 · N308DL · Boeing 737232 · Engine (Turbine/Turboprop) > AFTER TAKEOFF WHEN THROTTLES RETARDED NR 2 ENGINE REMAINED AT 1.6 EPR. REPLACED FUEL CONTROL. - [SDR DL73S040766](https://openairdocs.org/sdr/DL73S040766.md): Keelbeam · corroded · Aug 13, 2004 · N308DL · Boeing 737232 · Fuselage Main, Keel > THE KEEL CHORDS AT STRINGERS 27L & 27R WERE FOUND CORRODED NEAR THE SPLICE END AT FS 727A. THE CHORDS WERE CUT AT FS 727B+10 AND THE CORRODED ENDS REMOVED. NEW SECTIONS OF CHORD WERE SPLICE IN WITH ALUMINUM REPAIR ANGLES PER ER/A 092557-14 AND ER/A 092126-14 - [SDR DL73S040758](https://openairdocs.org/sdr/DL73S040758.md): Skin · cracked · Aug 11, 2004 · N308DL · Boeing 737232 · Fuselage Main, Plate/Skin > INSPECTION OF THE STRINGER 10R SKIN LAP JOINT PER AD 2003- 08-15 REVEALED A CRACKED FASTENER HOLE AT FS 727C. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER B737 SRM AND PER ER/A 092157 -14AD. - [SDR DL73S040755](https://openairdocs.org/sdr/DL73S040755.md): Floorbeam · cracked · Aug 11, 2004 · N308DL · Boeing 737232 · Fuselage Main, Floor Beam > THE UPPER CAP OF THE FS 294.5 FLOORBEAM WAS FOUND CRACKED OUTBOARD OF RBL 45. THE DAMAGED SECTION OF CAP WAS CUT OUT AT RBL 28.5 AND A NEW SECTION SPLICED IN PER ER/A 092282-14. - [SDR DL73S040754](https://openairdocs.org/sdr/DL73S040754.md): Skin · cracked · Aug 11, 2004 · N308DL · Boeing 737232 · Fuselage Main, Plate/Skin > A CRACK WAS FOUND AT A FASTENER HOLE IN THE UPPER FWD CORNER OF THE L1 DOOR CUTOUT. THE CRACK WAS REMOVED WITH A CUT OUT IN THE SKIN AND REPAIRED WITH EXTERNAL ALUMINUM REPAIR DOUBLERS PER BAC S/B 737-53-1163 AND ER/A 092229-14. - [SDR DL73S040748](https://openairdocs.org/sdr/DL73S040748.md): Skin · cracked · Aug 6, 2004 · N308DL · Boeing 737232 · Fuselage Main, Plate/Skin > INSPECTION OF THE STRINGER 10L SKIN LAP JOINT PER AD 2003- 08-15 REVEALED A CRACKED FASTENER HOLE AT FS 500A AND AT FS 500B. THE CRACKS WERE REMOVED WITH CUTOUTS AND REPAIRED SEPARATELY WITH ALUMINUM REPAIR DOUBLERS PER THE B737 SRM AND PER ER/A 092153-14AD. - [SDR DL73S040747](https://openairdocs.org/sdr/DL73S040747.md): Skin · cracked · Aug 6, 2004 · N308DL · Boeing 737232 · Fuselage Main, Plate/Skin > INSPECTION OF THE STRINGER 4R SKIN LAP JOINT PER AD 2003-08 -15 REVEALED A SINGLE CRACKED FASTENER HOLE AT FS 400. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER B737 SRM AND PER ER/A 092151-14AD. - [SDR DL73S040732](https://openairdocs.org/sdr/DL73S040732.md): Skin · cracked · Aug 6, 2004 · N308DL · Boeing 737232 · Fuselage Main, Plate/Skin > FUSELAGE SKIN STR-14R LAP JOINT FS 380 REPAIR OF CRACK. INSPECTION PER SI 03-086337-12AD DISCOVERED A CRACK AT A FASTENER HOLE IN THE LOWER ROW OF THE STRINGER S-14R LAP SPLICE AT STA 380. THE DAMAGE IS REPAIRED BY ER/A 092107-14 WHICH IS PER B737-200 SRM 53 - [SDR DL73S040451](https://openairdocs.org/sdr/DL73S040451.md): Coffeemaker · malfunctioned · May 20, 2004 · N308DL · Boeing 737232 · Buffet/Galleys > DURING FLIGHT AFT CABIN ATTENDANTS NOTICE ELECTRICAL SMELL IN THE AFT GALLEY. SHORTLY AFTER SMELL STARTED SMOKE DETECTOR IN AFT LAV STARTED TO SOUND. THE C/B FOR THE AFT GALLEY COFFEEMAKER POPPED AND THE SMELL WENT AWAY. THE AFT LAV SMOKE DETECTOR CONTINUED - [SDR DL73S030909](https://openairdocs.org/sdr/DL73S030909.md): Coffeemaker · overheated · Oct 9, 2003 · N308DL · Boeing 737232 · Buffet/Galleys > PASSING 10,000 FT ON CLIMB STRONG BURNING ODOR. F/A'S CONFIRMED OVENS OFF, ODOR STRONGER, RETURNED TO ATL. FOUND FIRST CLASS COFFEEMAKER OVERHEATING. REPLACED COFFEEMAKER, OPERATION GOOD. - [SDR DL73S030412](https://openairdocs.org/sdr/DL73S030412.md): Door Frame · cracked · May 1, 2003 · N308DL · Boeing 737232 · Fuselage Main, Structure > THE UPPER FRAME PORTION OF THE FWD FRAME ON THE C2 CARGO DOOR WAS FOUND WITH A CRACK IN THE LOWER FASTENER ROW OF THE FRAME AT THE LAP JOINT BETWEEN THE UPPER AND LOWER FRAME. THE CRACK WAS STOP DRILLED AND REPAIRED WITH 2 TITANIUM REPAIR ANGLES PER ER/A - [SDR DL73S030413](https://openairdocs.org/sdr/DL73S030413.md): Gusset · cracked · Apr 30, 2003 · N308DL · Boeing 737232 · Fuselage Main, Structure > FUSELAGE / L1 DOOR OPENING / FWD FRAME / LOWER HINGE CUTOUT:GUSSET CRACK REPAIR THE FWD FRAME OF THE L1 DOOR OPENING STRUCTURE WAS FOUND WITH A CRACK IN THE 'H' GUSSET AT THE LOWER HINGE CUTOUT. THE CRACK WAS STOP DRILLED AND REPAIRED WITH A TITANIUM DOU - [SDR DL73S030370](https://openairdocs.org/sdr/DL73S030370.md): Power Supply · inoperative · Apr 17, 2003 · N308DL · Boeing 737232 · Emergency Lighting > ON LAYOVER FOUND EMERGENCY LIGHTS INOP ROWS 1-4----REMOVED AND REPLACED POWER SUPPLY AND SYSTEM CHKS OK - [SDR DL73S030368](https://openairdocs.org/sdr/DL73S030368.md): Power Supply · inoperative · Apr 17, 2003 · N308DL · Boeing 737232 · Emergency Lighting > ON LAYOVER FOUND EMERGENCY LIGHTS OUT ROW 1-4 - REPLACED POWER SUPPLY - [SDR DL73K021039](https://openairdocs.org/sdr/DL73K021039.md): Wire · broken · Sep 5, 2002 · N308DL · Boeing 737232 · Emergency Lighting > AT 0700 FLT CREW REPORTED EMERGENCY LIGHT AT SEAT 8 DEF WAS INOP. FOUND BROKEN WIRE AND REPAIRED SAME. LIGHT NOW OP NML - [SDR DL73K020686](https://openairdocs.org/sdr/DL73K020686.md): Transceiver · malfunctioned · Jun 19, 2002 · N308DL · Boeing 737232 · Weather Radar System > EN ROUTE GOT R/T FAULT ON THE RADAR INDICATOR. REMOVED AND REPLACED RADAR TRANSCEIVER PER M/M. OPS CHECKS GOOD. - [SDR DL73K020332](https://openairdocs.org/sdr/DL73K020332.md): Doubler · corroded · Mar 18, 2002 · N308DL · Boeing 737232 · Fuselage Main, Plate/Skin > FUSELAGE / SKIN CUTOUT / FS 967-981 / STRG. 26R-27R: INTERNAL CUTOUT DOUBLER CORROSION THE INTERNAL SURROUND DOUBLER AROUND A FUSELAGE CUTOUT FOR A LAVATORY VENT WAS FOUND CORRODED BETWEEN FS 967 & 981 AND BETWEEN STRINGER - [SDR DL73S040294](https://openairdocs.org/sdr/DL73S040294.md): Warning Horn · activated · Apr 1, 2001 · N308DL · Boeing 737232 · Central Warning > RTO AT 30KTS DUE TO T/O WARNING HORN. FOUND LEADING EDGE IND C/B POPPED. RESET AND ALL CHECKS OK. - [SDR DL73K001580](https://openairdocs.org/sdr/DL73K001580.md): Frame · cracked · Aug 14, 2000 · N308DL · Boeing 737232 · Fuselage Main, Frame > THE INBOARD STRAP WAS FOUND CORRODED AND CRACKS WERE FOUND IN THE FORWARD FRAME OF THE C2 DOOR OPENING AT APPROX WL 160. THE STRAP WAS REPLACED AND THE FRAME MODIFIED PER S/B 737-53-1096 WITH SOME DEVIATIONS PER ERA 334753-14 AT HMV. - [SDR DL73K001579](https://openairdocs.org/sdr/DL73K001579.md): Skin · cracked · Aug 14, 2000 · N308DL · Boeing 737232 · Fuselage Main, Plate/Skin > A CRACK WAS FOUND IN THE FUSELAGE SKIN AT THE AFT GALLEY DOOR UPPER AFT CORNER. THE CRACK WAS ROUTED OUT AND A DOUBLER AND TRIPLER WAS INSTALLED PER ERA 334709-14 AT HMV. - [SDR DL73K001578](https://openairdocs.org/sdr/DL73K001578.md): Skin · cracked · Aug 14, 2000 · N308DL · Boeing 737232 · Fuselage Main, Plate/Skin > A CRACK WAS FOUND IN THE FUSELAGE SKIN AT THE AFT ENTRY DOOR LOWER HINGE CUTOUT. A REPAIR WAS INSTALLED SIMILIAR TO B737-200 SRM 53-30-3, FIGURE 36 PER ERA 334778-14 AT HMV. - [SDR DL73K001577](https://openairdocs.org/sdr/DL73K001577.md): Attach Fitting · corroded · Aug 14, 2000 · N308DL · Boeing 737232 · Vertical Stabilizer, Attach Fittings > THE RT AND LT ATTACH FITTINGS OF THE HORIZONTAL STABILIZER WERE FOUND CORRODED. THE BORES WERE OVERSIZED AND SOME OF THE FACES WERE BLENDED PER ERA 334715-14 AT HMV. - [SDR DL73K001576](https://openairdocs.org/sdr/DL73K001576.md): Attach Fitting · corroded · Aug 14, 2000 · N308DL · Boeing 737232 · Vertical Stabilizer, Attach Fittings > THE NUMBER 2 LUG ON THE VERTICAL STABILIZER ATTACH FITTING WAS FOUND CORRODED. THE BORE WAS OVERSIZED AND NEW BUSHINGS WERE MANUFACTURED PER ERA 334730-14 AT HMV. - [SDR DL73K001575](https://openairdocs.org/sdr/DL73K001575.md): Attach Fitting · corroded · Aug 14, 2000 · N308DL · Boeing 737232 · Fuselage, Stabilizer Attach Fittings > THE HORIZONTAL STABILIZER RT AND LT CLEVIS LUGS WERE FOUND CORRODED. THE LUG DIAMETER WAS ENLARGED AND NEW BUSHINGS WERE INSTALLED PER ERA 334719-14 AT HMV. - [SDR DL73K001574](https://openairdocs.org/sdr/DL73K001574.md): Floorbeam · cracked · Aug 14, 2000 · N308DL · Boeing 737232 · Fuselage Main, Floor Beam > A CRACK WAS FOUND IN THE RBL 24 LONGITUDINAL FLOORBEAM AT APPROX FS 656. THE CRACK WAS REMOVED AND A DOUBLER WAS INSTALLED PER ERA 334706-14 AT HMV. - [SDR DL73K001573](https://openairdocs.org/sdr/DL73K001573.md): Frame · corroded · Aug 14, 2000 · N308DL · Boeing 737232 · Fuselage Main, Frame > THE FS 500 FRAME WAS FOUND CORRODED BETWEEN STR 25R AND STR 26R. THE DAMAGE WAS CUT OUT AND A FORMED SECTION REPAIR INSTALLED PER ERA 334713-14 AT HMV. - [SDR DL73K001455](https://openairdocs.org/sdr/DL73K001455.md): Skin · cracked · Jul 27, 2000 · N308DL · Boeing 737232 · Fuselage Main, Plate/Skin > THE FUSELAGE SKIN WAS FOUND CRACKED AT FS 765 JUST ABOVE S-19R. THE CRACK WAS APPROX 1 INCH IN LENGTH AND RAN ALONG THE EDGE OF THE BONDED DOUBLER. THE CRACK IS TYPICAL OF THAT DESCRIBED IN BACO S/B 737-53-1065 EVEN THOUGH THIS S/B IS NOT EFFECTIVE FOR THIS - [SDR DL73K001454](https://openairdocs.org/sdr/DL73K001454.md): Rib · damaged · Jul 27, 2000 · N308DL · Boeing 737232 · Wing, Rib/Bulkhead > CRACKS DISCOVERED IN THE UPPER CHORD OF THE WING CENTER SECTION LBL 24 FLOORBEAM IMMEDIATELY FWD STA 680. INSTALLED REPAIR IN ACCORDANCE WITH ER/A 334695-14. - [SDR DL73K001336](https://openairdocs.org/sdr/DL73K001336.md): Frame · cracked · Jul 17, 2000 · N308DL · Boeing 737232 · Fuselage Main, Frame > ONE CRACK WAS FOUND IN EACH OF THE LEFT AND RIGHT FS 616 IN THE LOWER FASTENER OF THE INNER CHORD AT FRAME TO STUB BEAM JOINT. THE CRACKS WERE 1.25 INCH IN LENGTH AND WERE TYPICAL TO THOSE SHOWN IN S/B 737-53-1182. ERA 334694-14 AUTHORIZES A REPAIR SIMILIAR - [SDR DL73K001323](https://openairdocs.org/sdr/DL73K001323.md): Frame · mismanufactured · Jul 12, 2000 · N308DL · Boeing 737232 · Fuselage Main, Frame > WHILE ACCOMPLISHING THE MODIFICATION TO THE RS FS 440 FRAME PER S/B 737-53-1125 IT WAS NOTED THAT THE INITIAL FASTENERS AT THE SUBJECT LOCATIONS (5) WERE MS20470D8 RIVETS. THE S/B CALLS FOR THESE LOCATIONS TO BE OVERSIZED TO.2187 INCH RIVETS. ERA 334686-14 - [SDR DL73K001254](https://openairdocs.org/sdr/DL73K001254.md): Acm · seized · Jul 3, 2000 · N308DL · Boeing 737232 · Cabin Cooling System > DUCT TEMP HIGH WITH NR PACK MIX VALVE IN FULL COLD. INTERMITTENT BURNING SMELL PRESENT IN AFT GALLEY AREA. NR 2 PACK APPEARS TO WORK FINE. - FOUND LT ACM FROZEN - REPLACED SAME - [SDR DL73K990289](https://openairdocs.org/sdr/DL73K990289.md): Fan · failed · Feb 13, 1999 · N308DL · Boeing 737232 · Air Distribution Fan > SLIGHT SMELL IN CABIN. FOUND GASPER FAN BREAKER POPPED. DEFERRED PER MINIMUM EQUIPMENT LIST AND COLLARED BREAKER FOR FAN. REPLACED FAN. - [SDR DL73K981870](https://openairdocs.org/sdr/DL73K981870.md): Battery Pack · discharged · Sep 9, 1998 · N308DL · Boeing 737232 · Emergency Lighting > AFT RIGHT SERVICE DOOR SLIDE LIGHT INOP. REPLACED BATTERY PACK. CKS GOOD. - [SDR DL73K981566](https://openairdocs.org/sdr/DL73K981566.md): Door · not latched · Jul 29, 1998 · N308DL · Boeing 737232 · Cargo/Baggage Doors > FWD CARGO DOOR LIGHT ILLUMINATE UPON TOUCH DOWN. FOUND DOOR OPEN, CHECKED DOOR LATCHES AND ALL WARNING SYS ALL CKS NML. - [SDR DL73K980240](https://openairdocs.org/sdr/DL73K980240.md): Fuse · blown · Jan 29, 1998 · N308DL · Boeing 737232 · Emergency Lighting > EMERGENCY LIGHT EXIT SIGN ABOVE L2 DOOR WOULD NOT TEST. REPLACED FUSE. - [SDR DL73K972176](https://openairdocs.org/sdr/DL73K972176.md): Power Supply · inoperative · Oct 27, 1997 · N308DL · Boeing 737232 · Emergency Lighting > LT AFT OVER DOOR EMERG EXIT SIGN AND AFT OVERHEAD CENTER AISLE EMERG EXIT SIGN WILL NOT TEST. REPLACED PWR SUPPLY L1076 AT STATION 975L LIGHTS TEST NORMAL. - [SDR DL73K972194](https://openairdocs.org/sdr/DL73K972194.md): Skin · cracked · Oct 22, 1997 · N308DL · Boeing 737232 · Fuselage Main, Plate/Skin > FUSELAGE SKIN L2 DOOR SURROUND, LWR FWD HINGE CUT OUT. REPAIR FOR CRACK. 1.5 INCH CRACK FOUND IN SKIN AND BEAR STRAP AT THE LOWER HINGE CUT OUT OF THE L2 DOOR SURROUND AREA. TIME LIMITED DOUBLER REPAIR INSTALLED PER ER/A 363028-14. - [SDR DL73S962117](https://openairdocs.org/sdr/DL73S962117.md): Bulkhead Web · cracked · Sep 6, 1996 · N308DL · Boeing 737232 · Fuselage Main, Bulkhead > DURING INSPECTION, 2 CRACKS WERE DISCOVERED IN THE FWD. FACEOF THE STA. 178 BULKHEAD WEB. FIRST CRACK CUTOUT MEASURES 1 1/8 X 1 AND IS LOCATED AT RBL 5.7 VERTICAL STRAP AT_WL 198. THE SECOND CRACK CUTOUT MEASURES 1.5 X 1 LOCATED_AT THE LBL 5.7 VERTICAL STRAP - [SDR DL73S962051](https://openairdocs.org/sdr/DL73S962051.md): Fitting · cracked · Aug 30, 1996 · N308DL · Boeing 737232 · Wing, Landing Gear Attach Fittings > RIGHT WING OUTBOARD AFT SUPPORT FITTING FOR THE MAIN LANDING GEAR BEAM WAS FOUD CRACKED. THE FITTING WAS INSPECTED PER BACO S/B 737-57-1216, BUT THIS DAMAGE IS NOT TYPICAL OF DAMAGE DESCRIBED IN THE SERVICE BULLETIN. THE CRACKED FITTING WILL REMAIN IN SERVIC - [SDR DL73S960904](https://openairdocs.org/sdr/DL73S960904.md): Bolt · loose · Apr 16, 1996 · N308DL · Boeing 737232 · Landing Gear Retraction/Extension System > ON ARRIVAL, A/C HAD NOSE GEAR UNSAFE LIGHT. CYCLED GEAR SEVERAL TIMES, NO HELP. A/C MADE UNEVENTFUL LANDING. FOUND OVER CENTER MECH STOP BLOCK ATTACH BOLT BACKED OUT, PREVENTING OVER CENTER LINKS FROM FULLY LOCKING. RESECURED STOP BLOCK BOLT, MADE SEVERA Next page: https://openairdocs.org/deregistered/N308DL-2009-10-01/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 = 'N308DL' AND deregistration_id = 'N308DL-2009-10-01' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N308DL-2009-10-01/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.