Boeing 737-990

Service difficulty reports · 2,333

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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 aircraft_model_key = '737990'
  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 ASAA2016032116345Floor Support · corrodedAFT CARGO COMPARTMENT, LT FLOOR SUPPORT ZEE CHANNEL SECTION IS CORRODED, APPROXIMATELY BS 727+4 TO BS 727F+10. ACFT GROUNDED. REMOVED CORROSION ON AFT CARGO LT FLOOR SUPPORT ZEE CHANNEL AT BS 727+4 TO BS 727F+10, ORIGINAL MATERIAL IS .040 REMOVED .007 REMAIMar 21, 2016 · N320AS · Boeing 737990 · Fuselage Miscellaneous StructureSDR ASAA2016032116326Floor Support · corrodedAFT CARGO COMPARTMENT, LT FLOOR SUPPORT ZEE CHANNEL SECTION IS CORRODED, APPROXIMATELY BS 727F+10 TO BS 727I+8. ACFT GROUNDED. REMOVED CORROSION AND FOUND BEYOND ALLOWABLE LIMITS IAW SRM 53-00-53-1A-2. ORIGINAL MATERIAL THICKNESS IS 0.040, REMAINING THICKNMar 21, 2016 · N320AS · Boeing 737990 · Fuselage Miscellaneous StructureSDR ASAA2016032116325Channel · corrodedAFT CARGO COMPARTMENT, RT FLOOR SUPPORT ZEE CHANNEL SECTION IS CORRODED, APPROXIMATELY BS 727J+6 TO BS 767. ACFT GROUNDED. REMOVED CORROSION AND FOUND BEYOND ALLOWABLE LIMITS IAW SRM 53-00-53-1A-2. ORIGINAL MATERIAL THICKNESS IS 0.040 IN, REMAINING THICKNESSMar 21, 2016 · N320AS · Boeing 737990 · Fuselage Miscellaneous StructureSDR ASAA2016032116297Frame · corrodedAFT CARGO COMPARTMENT, FUSELAGE FRAME SPLICE IS CORRODED AT BS 787, BETWEEN S25-26R. ACFT GROUNDED. CORROSION ON FRAME SPLICE IS FOUND TO BE OUT OF LIMITS DUE TO LOCATION ON INNER CHORD IAW SRM 53-00-07-1A-1. R & R FRAME SPLICE IAW SRM 51-40-02 AND IAW DWG 1Mar 21, 2016 · N320AS · Boeing 737990 · Fuselage Main, FrameSDR ASAA2016032116289Angle · corrodedAFT CARGO COMPARTMENT, DOOR SURROUND LOWER SILL WEB ANGLE, BS 767-BS 787 IS CORRODED. ACFT GROUNDED. REMOVED CORROSION AND FOUND BEYOND ALLOWABLE LIMITS IAW SRM 53-60-15-1A-1, ORIGINAL MATERIAL THICKNESS IS 0.050 IN, REMOVED 0.007 IN, REMAINING THICKNESS IS Mar 21, 2016 · N320AS · Boeing 737990 · Fuselage Miscellaneous StructureSDR ASAA2016032116288Floorbeam · corrodedAFT CARGO COMPARTMENT, FLOOR PANEL SUPPORT TEE ASSY AT BS 727D+5 IS CORRODED, EXFOLIATED. ACFT GROUNDED. REMOVED CORROSION ON AFT CARGO TEE ASSY FLOOR SUPPORT IAW SRM 53-00-53-1A-2, ORIGINAL MATERIAL .070", MATERIAL LOSS .022" REMAINING MATERIAL .048" OUT OF Mar 21, 2016 · N320AS · Boeing 737990 · Fuselage Main, Floor BeamSDR ASAA2016032116287Floorbeam · corrodedPARTS RACK AFT CARGO COMPARTMENT, FLOOR PANEL SUPPORT TEE ASSY AT BS 727I+5 IS CORRODED, EXFOLIATED. ACFT GROUNDED. REMOVED CORROSION ON AFT CARGO FLOOR SUPPORT TEE ASSY IAW SRM 53-00-53-1A-2, ORIGINAL MATERIAL .070", MATERIAL LOSS .020" REMAINING MATERIAL .Mar 21, 2016 · N320AS · Boeing 737990 · Fuselage Main, Floor BeamSDR ASAA2016032116286Floorbeam · corrodedAFT CARGO COMPARTMENT, FLOOR PANEL SUPPORT TEE ASSY AT BS 772 IS CORRODED, EXFOLIATED. ACFT GROUNDED. REMOVED CORROSION ON AFT CARGO FLOOR SUPPORT TEE ASSY ON BS 772 IAW SRM 53-00-53-1A-2, ORIGINAL MATERIAL .070" MATERIAL LOSS .013", REMAINING MATERIAL .057"Mar 21, 2016 · N320AS · Boeing 737990 · Fuselage Main, Floor BeamSDR ASAA2016032116285Web · corrodedAFT CARGO COMPARTMENT, DOOR SURROUND LOWER SILL WEB IS CORRODED AT APPROXIMATELY BS 772. ACFT GROUNDED. REMOVED CORROSION ANDD FOUND BEYOND ALLOWABLE LIMITS IAW SRM 53-60-15-1A-1. ORIGINAL MATERIAL THICKNESS IS 0.050", REMOVED 0.006 IN, REMAINING THICKNESSMar 21, 2016 · N320AS · Boeing 737990 · Fuselage Miscellaneous StructureSDR ASAA2016032116284Shield · corrodedAFT CARGO COMPARTMENT, FWD DOOR SURROUND SHIELD, BS 767-BS 794 IS CORRODED. ACFT GROUNDED. REMOVED CORROSION FROM AFT CARGO FWD DOOR SURROUND SHIELD AT BS 737-BS 794, ORIGINAL THICKNESS .050 IAW SRM 53-60-15-01-1. REMAINING THICKNESS 0.043 MATERIAL LOSS .00Mar 21, 2016 · N320AS · Boeing 737990 · Fuselage Main, StructureSDR ASAA2016032116073Stop Fitting · crackedL1 DOOR FWD STOP FITTING IS CRACKED. ACFT GROUNDED. R & R DOOR STOP FITTING IAW SRM 51-40-02 AND AMM 52-11-41.Mar 21, 2016 · N303AS · Boeing 737990 · Fuselage Main, StructureSDR ASAA2016031616065Shield · corrodedAFT CARGO COMPARTMENT AFT SHIELD ASSY BETWEEN BS 847 AND BS 867, RBL 21.0 IS CORRODED. ACFT GROUNDED. REMOVED CORROSION FROM AFT CARGO COMPARTMENT AFT SHIELD ASSY FROM IAW SRM 51-10-02. ORIGINAL MATERIAL THICKNESS 0.050, MATERIAL LOSS 0.007, MAXIMUM ALLOWABLMar 16, 2016 · N303AS · Boeing 737990 · Fuselage Main, StructureSDR ASAA2016031615985Floor Panel · corrodedFWD CARGO COMPARTMENT FLOOR PANEL 120EF IS CORRODED AROUND THE EDGES OF THE UPPER SURFACE. ACFT GROUNDED. UPPER SURFACE CORROSION FOUND OUT OF LIMITS, DAMAGED EXTENDED MORE THAN 3" IAW SRM 53-00-53-1A-1, PARA FA, 1, CB. FABRICATED NEW FLOOR PANEL 120EF IAW DMar 16, 2016 · N303AS · Boeing 737990 · Fuselage Floor PanelSDR ASAA2016031416076Transition Panel · puncturedAFT CARGO COMPARTMENT RT TRANSITION PANEL IS PUNCTURED AT BS 727F+14, RBL 21.0. ACFT GROUNDED. REMOVED PUNCTURED PANEL AT BS 727F AND 14, RBL 21.0 AND FABRICATED NEW TRANSITION PANEL IAW SRM 53-00-53-2R-5, REPAIR 5. ALODINED AND PRIMED IAW SEM 51-20-01. TOP Mar 14, 2016 · N303AS · Boeing 737990 · Fuselage Miscellaneous StructureSDR ASAA2016031115950Floor Panel · damagedAFT CARGO COMPARTMENT FLOOR PANEL 140EF HAS SEVERAL ELONGATED FASTENER HOLES. ACFT GROUNDED. FABRICATED AFT CARGO COMPARTMENT FLOOR PANEL 140EF IAW DWG 453A2610, REV A AND ALODINED AND PRIMED IAW SRM 51-20-01. PANEL IS GONNA BE INSTALLED, CUSTOMER CARD G6600Mar 11, 2016 · N303AS · Boeing 737990 · Fuselage Floor PanelSDR ASAA2016030916075Bulkhead Web · crackedLEFT MLG WHEEL WELL FWD BULKHEAD WEB POSSIBLE CRACK ABOVE AILERON AUTOPILOT VALVE. ACFT GROUNDED. REMOVED DAMAGE AND ACCOMPLISHED DOUBLER REPAIR IAW SRM 57-10-10-2R-3, REPAIR 3. REPAIR 3 IS CATEGORY B WITH AN INSPECTION THRESHOLD DUE 56,000 FLIGHT CYCLES. RMar 9, 2016 · N303AS · Boeing 737990 · Fuselage Main, BulkheadSDR ASAA2016030815948Floor Panel · damagedFWD CARGO COMPARTMENT FLOOR PANEL 120DF HAS SEVERAL ELONGATED FASTENER HOLES. ACFT GROUNDED. FABRICATED FWD CARGO COMPARTMENT FLOOR PANEL 120DF IAW BAC DWG 453A1610 REV APPLIED ALODINE AND PRIME TO FLOOR PANEL IAW SRM 51-20-01, DOT REMOVED.Mar 8, 2016 · N303AS · Boeing 737990 · Fuselage Floor PanelSDR ASAA2016030415839Support Frame · chafedWING TO BODY FAIRING SUPPORT FRAME UNDER PANEL 193AL IS CHAFED. ACFT GROUNDED. REMOVED AND REINSTALLED PANEL 192JL IAW AMM 53-51-21. R & R SUPPORT IAW SRM 51-40-02 AND DWG 149A7216. TOPCOATED IAW AMM 51-21-73.Mar 4, 2016 · N319AS · Boeing 737990 · Fuselage Miscellaneous StructureSDR ASAA2016030115713Lens · brokenEMERGENCY LIGHT EXIT LOCATOR SIGN AT R-2 DOOR HAS BROKEN LENS. ACFT GROUNDED. R & R LENS AND TESTED LIGHT ASSY IAW AMM 33-51-00-960-801. OPS NORMAL.Mar 1, 2016 · N315AS · Boeing 737990 · Emergency LightingSDR ASAA2016022315850Floor Support · corrodedAFT CARGO FLOOR SUPPORT AT RT BS 747+6 TO 847, RBL 12 CORRODED IN SEVERAL SPOTS. ACFT GROUNDED. CHECKED LIMITS IAW SRM 51-10-02 ORIGINAL MATERIAL .070", MATERIAL REMAINING AFTER BLENDOUT .059" FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53, FIG 103 TOOL T8225.5. Feb 23, 2016 · N319AS · Boeing 737990 · Fuselage Miscellaneous StructureSDR ASAA2016022315840Channel · corrodedAFT PIT TRANSITION PANEL AT RT BS 727I+6 TO BS 787 CORRODED IN SEVERAL SPOTS. ACFT GROUNDED. REMOVED CORROSION FROM AFT PIT TRASITION PANEL RT BS 727I+6 TO BS 787 ORIGINAL THICKNESS IS.040 IAW DWG BAC1496-377, REMAINING THICKNESS IS.000 LOST MATERIAL IS .04Feb 23, 2016 · N319AS · Boeing 737990 · Fuselage Miscellaneous StructureSDR ASAA2016022315788Transition Panel · corrodedFWD PIT LT TRANSITION PANEL FROM BS 500B+10 TO 500F+10 CORRODED IN SEVERAL PLACES. ACFT GROUNDED. REMOVED CORROSION FWD PIT LT TRANSITION PANEL FROM BS 500B+10 TO 500F+10 IAW SRM 51-10-02 ORIGINAL THICKNESS IS.040 IAW SRM 53-30-53 FROM BS 500B-BS 500C+14 FOUFeb 23, 2016 · N319AS · Boeing 737990 · Fuselage Miscellaneous StructureSDR ASAA2016022315787Support · corrodedAFT PIT TRANSITION PANEL AT LT BS 727+4 TO 727F+6 CORRODED IN SEVERAL SPOTS. ACFT GROUNDED. REMOVED CORROSION LT TRANSITION PANEL BS 727+4 TO BS 727F+6 IAW SRM 51-10-02. ORIGINAL THICKNESS IS .040" IAW BAC 1496-377. REMOVED .040", REMAINING .000. TRANSITIONFeb 23, 2016 · N319AS · Boeing 737990 · Fuselage Miscellaneous StructureSDR ASAA2016022315786Floorbeam · corrodedFWD CARGO FLOORBEAM ANGLE AT BS 500L LBL 24 TO RBL 24 CORRODED SEVERAL PLACES. ACFT GROUNDED. REMOVED CORROSION ON FWD PIT FLOOR SUPPORT ANGLE AT BS 500L, LBL24 TO RBL24 IAW SRM 51-10-02. ORIGINAL THICKNESS IS .080 IAW DWG 143A9485, REMAINING THICKNESS IS .06Feb 23, 2016 · N319AS · Boeing 737990 · Fuselage Main, Floor BeamSDR ASAA2016022315785Angle · corrodedAFT PIT TRANSITION PANEL AT LT BS 727F+6 TO 727H+8 CORRODED IN SEVERAL SPOTS. ACFT GROUNDED. REMOVED SECTION PANEL FROM BS 727F+6 TO 727H+8 IAW SRM 51-40-02, AMT ID FOR FAB BAC 1496-377-7075-T62 CLAD IAW SRM 53-00-53-2R-5, PO 860620.2 FABRICATED NEW SECTION IFeb 23, 2016 · N319AS · Boeing 737990 · Fuselage Miscellaneous StructureSDR ASAA2016022315784Angle · corrodedAFT PIT TRANSITION PANEL AT LT BS 727H+8 TO 727J+8 CORRODED IN SEVERAL SPOTS. ACFT GROUNDED. REMOVED SECTION PANEL FROM 727H+8 TO 727J+8 IAW SRM 51-40-02 AMT ID. FOR FABRICATED 1496-377-7075-T62 CLAD IAW SRM 53-00-53-2R-5, PO 860620.2, FABRICATED NEW SECTIOFeb 23, 2016 · N319AS · Boeing 737990 · Fuselage Miscellaneous StructureSDR ASAA2016022315782Shield · corrodedAFT CARGO RT SHIELD AT BS 767-792 BETWEEN STR 25-26R CORRODED. ACFT GROUNDED. R & R AFT PIT RT SHIELD AT BS 767-792 BETWEEN STR 25-26R IAW SRM 51-40-02 AND BAC DWG 146A0081, REV A ORIGINAL THICKNESS IS .050, REMAINING .040, REMOVED .010. FOUND TO BE OUT OF LIFeb 23, 2016 · N319AS · Boeing 737990 · Fuselage Miscellaneous StructureSDR ASAA2016022315781Angle · corrodedAFT PIT TRANSITION PANEL AT RT BS 727D+6 TO 727I+6 CORRODED IN SEVERAL SPOTS. ACFT GROUNDED. REMOVED CORROSION FROM THE AFT PIT TRANSITION PANEL BS 727D+6 TO 727I+6 ORIGINAL THICKNESS IS 0.040 IAW DWG BAC 1496-377, REMAINING THICKNESS IS 0.070, REMOVED MATFeb 23, 2016 · N319AS · Boeing 737990 · Fuselage Miscellaneous StructureSDR ASAA2016022315776Transition Panel · corrodedAFT PIT TRANSITION PANEL AT LT BS 727J+8 TO 747+6 CORRODED IN SEVERAL SPOTS. ACFT GROUNDED. REMOVED SECTION PANEL FROM BS 727J+8 TO 747+6 IAW SRM 51-40-02 MATERIAL ID FOR FABRICATED BAC 1496-377, 7075, T62 CLAD IAW SRM 53-00-53-2R-5, PO 860620.2 FABRICATEDFeb 23, 2016 · N319AS · Boeing 737990 · Fuselage Miscellaneous StructureSDR ASAA2016022315775Transition Panel · corrodedAFT PIT TRANSITION PANEL AT LT BS 747+6 TO 847 CORRODED IN SEVERAL SPOTS. ACFT GROUNDED. REMOVED SECTION PANEL FROM BS 747+6 TO 847 IAW SRM 51-40-02. MATERIAL ID FOR FAB BAC 1496-377 7075T62 CLAD IAW SRM 53-00-53-2R-5, PO 860620.1 FABED NEW SECTION IAW SRM 53Feb 23, 2016 · N319AS · Boeing 737990 · Fuselage Miscellaneous StructureSDR ASAA2016022315772Transition Panel · corrodedFWD PIT RT TRANSITION PANEL FROM BS 500A TO 500G+4 CORRODED SEVERAL PLACES. ACFT GROUNDED. REMOVED CORROSION ON FWD PIT RT TRANSITION PANEL FROM BS 500A TO 522G+4 IAW SRM 51-10-02, ORIGINAL THICKNESS IS .40 IAW SRM 53-30-53. REMOVED .010 REMAINING THICKNESS Feb 23, 2016 · N319AS · Boeing 737990 · Fuselage Miscellaneous StructureSDR ASAA2016022315770Transition Panel · corrodedFWD PIT LT TRANSITION PANEL FROM BS 500J+10 TO 500L CORRODED IN SEVERAL PLACES. ACFT GROUNDED. REMOVED CORROSION FWD PIT LT TRANSITION PANEL FROM BS 500J+10 TO BS 500L IAW SRM 51-10-02. AFTER FURTHER EVALUATION CORROSION FOUND TO BE MORE THAN 50 PERCENT, OUT Feb 23, 2016 · N319AS · Boeing 737990 · Fuselage Miscellaneous StructureSDR ASAA2016022315651Retainer · crackedFS 289 BULKHEAD SEAL RETAINER CRACKED AT T/E CAVITY. ACFT GROUNDED. R & R 1152953-2AAR FITTING IAW SRM 51-40-02. DOT REMOVED.Feb 23, 2016 · N319AS · Boeing 737990 · Fuselage Main, BulkheadSDR ASAA2016022215783Floor Panel · gougedAFT CARGO FLOOR PANEL 140CF CORRODED AND GOUGED ALL ARROUND. ACFT GROUNDED. FABRICATED NEW AFT CARGO FLOOR PANEL 140 OF IAW DWG 453A2610, REV C. ALODINED & PRIMED IAW SRM 51-20-01.Feb 22, 2016 · N319AS · Boeing 737990 · Fuselage Floor PanelSDR ASAA2016022115777Floor Panel · gougedPARTS RACK ITEM, AFT PIT FLOOR PANEL 140BF GOUGED AND CORRODED ALL ARROUND. ACFT GROUNDED. FABRCIATED NEW AFT CARGO FLOOR PANEL 140BF IAW DWG 453A2610, REV E. ALODINED AND PRIMED IAW SRM 51-20-01.Feb 21, 2016 · N319AS · Boeing 737990 · Fuselage Floor PanelSDR ASAA2016022015773Floor Panel · corrodedFWD PIT FLOOR PANEL 120EF CORRODED ALL AROUND THE EDGES. ACFT GROUNDED. FABRICATED NEW FWD CARGO FLOOR PANEL 120EF IAW BAC DWG 453A1610, REV B ALODINED AND PRIMED IAW SRM 51-20-01.Feb 20, 2016 · N319AS · Boeing 737990 · Fuselage Floor PanelSDR ASAA2016022015771Floor Panel · corrodedPARTS RACK, FWD PIT FLOOR PANEL 120 DF CORRODED ALL AROUND THE EDGES. ACFT GROUNDED. FLOOR PANEL 120DF FOUND TO BE BEYOND LIMITS IAW SRM 53-00-53 MAT ID 2024-T3 .071 PO 860430.3 AND FABRICATED IAW DWG 453A1610, REV A ALODINED IAW SRM 51-20-01 PRIMED IAW AMM Feb 20, 2016 · N319AS · Boeing 737990 · Fuselage Floor PanelSDR ASAA2016022015768Floor Panel · crackedPARTS RACK AFT PIT FLOOR PANEL 140AF CORRODED AROUND EDGES. ACFT GROUNDED. FABRICATED NEW PANEL IAW DWG 453A2610, REV C ALODINED AND PRIMED IAW SRM 51-20-01. REMOVED DOT H250.Feb 20, 2016 · N319AS · Boeing 737990 · Fuselage Floor PanelSDR ASAA2016011314773Battery Pack · failedEMERGENCY LIGHTS OPS CHECK, FWD ENTRY LIGHTS INOPERATIVE. ACFT GROUNDED. VERIFIED POWER SUPPLY M1675 TEST BUTTON INOPERATIVE. REPLACED M1675 REF AMM 33-51-06. OPS NORMAL.Jan 13, 2016 · N319AS · Boeing 737990 · Emergency LightingSDR ASAA2015122514478Pump · low pressureACFT POWER FELL OFFLINE WHEN SELECTING APU GEN. WHEN RESELECTING GROUND POWER,"A" SYSTEM ELEC HYDRAULIC PUMP INDICATES LOW PRESSURE. ACFT GROUNDED.Dec 25, 2015 · N315AS · Boeing 737990 · Hydraulic Pump (Electric/Engine), MainSDR ASAA2015122414474Lens · detachedSMALL "EXIT" LIGHT COVER IMMEDIATELY LT OF L1 JUMP SEAT CAME OFF & WILL NOT STAY IN PLACE. ACFT GROUNDED. REINSTALLED "EXIT SALIDA" SIGN COVER FWD OF L1 DOOR. OK FOR SERVICE.Dec 24, 2015 · N302AS · Boeing 737990 · Emergency LightingSDR ASAA2015110113591Door · lack of lubeL1 DOOR DIFFICULT TO CLOSE FROM INSIDE. ACFT GROUNDED. LUBED L-1 DOOR, OP'S CK NORMAL. REF FIM TASK 52-10, TASK 807.Nov 1, 2015 · N303AS · Boeing 737990 · Passenger/Crew DoorsSDR ASAA2015081212866Battery Pack · no testBATTERY PACK FAILED CAPACITY CHECK. ACFT GROUNDED. REPLACED BATTERY PACK. OPS CHECKED NORMAL.Aug 12, 2015 · N318AS · Boeing 737990 · Emergency LightingSDR ASAA2015081212865Battery Pack · no testBATTERY PACK, FAILED CAPACITY CHECK. ACFT GROUNDED. REPLACED BATTERY PACK. OPS CHECKED NORMAL.Aug 12, 2015 · N318AS · Boeing 737990 · Emergency LightingSDR ASAA2015081212863Lamp · inoperativeEMERGENCY AISLE LIGHTS INOPERATIVE ROWS 10 DEF & 30 DEF. ACFT GROUNDED. REPLACED THE LAMPS AND TESTED IAW MM 33-51-00-960-801. OPS NORMAL.Aug 12, 2015 · N318AS · Boeing 737990 · Emergency LightingSDR ASAA2015080612778Lamp · failedR1 OUTSIDE DOOR EMERGENCY EXIT LIGHT OUT. ACFT GROUNDED. REPLACED THE LAMP IAW AMM 33-51-04.Aug 6, 2015 · N320AS · Boeing 737990 · Emergency LightingSDR ASAA2015072512599Power Supply · no testRIGHT EXTERIOR AFT OVERWING EMERGENCY LIGHT AND RT FUSELAGE EMERGENCY LIGHT INOPERATIVE. ACFT GROUNDED. R & R BATTERY PACK AT APPROXIMATELY BS 727C RT, OPS CHECK NORMAL, REF AMM 33-51-06.Jul 25, 2015 · N315AS · Boeing 737990 · Emergency LightingSDR ASAA2015070512338Light · failedWHILE PERFORMING TC 78233008, EMERGENCY LIGHTS OPS, FOUND EMERGENCY LIGHT AT OVERHEAD BIN 29 ABC BURNED OUT. ACFT GROUNDED. SEVERAL ATTEMPTS AT REPLACING LAMPS UNSUCCESSFUL. REPLACED LIGHT ASSY. OPS CK GOOD. REF AMM 33-51-03.Jul 5, 2015 · N323AS · Boeing 737990 · Emergency LightingSDR ASAA2015052711888Door · lack of lubeL1 DOOR OPENS PART WAY. ACFT GROUNDED. LUBED L1 DOOR AND CYCLED SEVERAL TIMES WITHOUT BINDING REF AMM 12-25-11.May 27, 2015 · N309AS · Boeing 737990 · Passenger/Crew DoorsSDR ASAA2015052711858Door · lack of lubeL1 DOOR OPENS PART WAY. ACFT GROUNDED. LUBED L1 DOOR AND CYCLED SEVERAL TIMES WITHOUT BINDING IAW AMM 12-25-11.May 27, 2015 · N309AS · Boeing 737990 · Passenger/Crew Doors
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