Boeing 737-277

Service difficulty reports · 1,584

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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 = '737277'
  ORDER BY difficulty_date DESC"

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SDR AWXA0001535Web · crackedCRACKED FLOOR WEB AT FS 179-180 LBL 38 WL 207. REMOVED AND REPLACED WEB IAW SRM 51-30-2 PGS 2 & 8.Mar 26, 2001 · N179AW · Boeing 737277 · Fuselage Miscellaneous StructureSDR AWXA0001534Tee Chord · crackedMAIN WHEEL WELL FWD BLKHD UPPER T-CHORD CRACKED AT FS 663.75 LBL 24 AND RBL 24. REPAIRED IAW BOEING DWG 65C37732, B737-200 SRM 51-30-2 PGS 2-3, 5, 7-9 AND AWA ER 15-5702-01073-JS3.Mar 26, 2001 · N179AW · Boeing 737277 · Fuselage Main, StructureSDR AWXA0001531Skin · crackedUSING HFEC .25 INCH CRACK FOUND AT DOOR 2L UPPER HINGE CUTOUT. CRACK REMOVED IAW SRM 52-00-2 FIG 6 (BEYOND LIMIT); NDT CHECKED. CRACK REMOVED IAW NDT PT.6 51-00-00; CRACK REPAIRED IAW ER 15-5210-01072-JS4.Mar 21, 2001 · N188AW · Boeing 737277 · Fuselage Main, Plate/SkinSDR AWXA0001530Stiffener · chafedNR 1 ENG O/B COWL 4TH RIB FROM AFT AND 7TH, 8TH, AND 9TH CHAFING TO THE ENGINE. NR 4 AND 9 RIB REPAIRED IAW SRM 51-40-3; NR 7 AND 8 RIBS (STIFFENERS) BLENDED W/I SRM 54-10-1 FIG 1 LIMITS; AREAS ALODINED AND PRIMED IAW SRM 51-10-2 AND DWG 65-73773.Mar 21, 2001 · N188AW · Boeing 737277 · Engine Cowling SystemSDR AWXA0001529Skin · dentedDENT IN FUSELAGE SKIN JUST FWD OF EQUIPMENT BAY DOOR AND AFT OF RADOME REQ''S TERMINATION REPAIR. AREA REPAIRED IAW SRM 53-30-3 FIG 6.Mar 21, 2001 · N188AW · Boeing 737277 · Fuselage Main, Plate/SkinSDR AWXA0001528Skin · dentedTWO DENTS COVERED BY REPAIR DOUBLERS BELOW CARGO BIN AT STA 460. OLD REPAIRS REMOVED, NDT CONFIRMED NO CRACKS IN CUTOUT AREAS; NEW REPAIRS FABBED AND INSTALLED IAW SRM 53-30-3 FIG 6.Mar 21, 2001 · N188AW · Boeing 737277 · Fuselage Main, Plate/SkinSDR AWXA0001527Floorbeam · corrodedSURFACE CORROSION ON TOP OF CABIN FLOORBEAM AT BS 986.5. FLOORBEAM REPAIRED IAW SRM 53-10-9 FIG 2.Mar 21, 2001 · N188AW · Boeing 737277 · Fuselage Main, Floor BeamSDR AWXA0001526Skin · dentedDENT AT BS 1064 STR 14L. REMOVED DOUBLER AND ASSESSED IAW SRM 53-30-1 FIG 1; INSTALLED NEW DOUBLER IAW SRM 53-30-3 FIG 17.Mar 21, 2001 · N188AW · Boeing 737277 · Fuselage Main, Plate/SkinSDR AWXA0001525Bulkhead · crackedFWD PRESSURE BLKHD CRACKED (APPROX 2 INCHES) AT BL 0 WL 190. REPAIRED IAW SRM 53-10-11 FIG 4 DET II.Mar 21, 2001 · N188AW · Boeing 737277 · Fuselage Main, BulkheadSDR AWXA0001524Intercostal · crackedFWD PRESSURE BLKHD INTERCOSTAL CRACKED AT STA 178 WL 195 LT SIDE (1 INCH CRACK) FWD CORNER. REPLACED INTERCOSTAL IAW DWG 65-16300 AND SRM 51-30-2.Mar 21, 2001 · N188AW · Boeing 737277 · Fuselage Miscellaneous StructureSDR AWXA0001523Bulkhead · crackedFWD PRESSURE BLKHD CRACKED AT FASTENER HOLE AT RBL 12 WL 234; 2 CRACKS APPROX .0625 INCH BEYOND FASTENER HEAD. WEB REPAIRED IAW SRM 53-10-11 FIG 1 DET II AND SRM 51-30-2.Mar 21, 2001 · N188AW · Boeing 737277 · Fuselage Main, BulkheadSDR AWXA0001522Floor Panel · crackedCOCKPIT FLOOR PANEL CORNER PIECE BROKEN OFF AT STA 188 WL 207 JUST BELOW -40 WEB AT RT SIDE. REPAIRED FLOOR PANEL IAW REF DWG 65-45833 AND SRM 51-40-02 FIG 1 AND SRM 51-30-2.Mar 21, 2001 · N188AW · Boeing 737277 · Fuselage Floor PanelSDR AWXA0001521Frame · crackedFWD PRESSURE BLKHD SIDE CHORD CRACKED AT RT SIDE AND LT SIDE AT WL 207; RIVET MISSING FROM FLOOR WEB. RT SIDE CHORD (P/N 65-16300-86) REPLACED IAW DWG 65-16300-40 AND SRM 51-30-2; LT SIDE CHORD (P/N 65-16300-87) REPLACED IAW DWG 65-16300 & SRM 51-30-2; WEB REMar 21, 2001 · N188AW · Boeing 737277 · Fuselage Main, FrameSDR AWXA0001520Seal · misinstalledLT WING (WBL 92.5 - WBL 114) LWR INBOARD T/E PANEL BULB SEAL JUST INBOARD OF GEAR INSTALLED INCORRECTLY AND WRONG FASTENERS ARE CAUSING DAMAGE TO MLG SUPPORT BEAM. SUPPORT BEAM DAMAGED AREA BLENDED IAW SRM 57-20-1 FIG 5 - MAT LOSS .003; SEAL INSTALLATION CORRMar 21, 2001 · N188AW · Boeing 737277 · Trailing Edge FlapsSDR AWXA0001519Channel · crackedNOSE GEAR RETRACT ACTUATOR SUPPORT BEAM AFT CHANNEL CRACKED IN RADIUS. GUSSET REPLACED IAW DWG 65-45819.Mar 21, 2001 · N188AW · Boeing 737277 · Fuselage Miscellaneous StructureSDR AWXA0001518Web · crackedNOSE GEAR RETRACT ACTUATOR SUPPORT BEAM WEB CRACKED AT FWD AREA AS MARKED. MADE AND INSTALLED WEB IAW DWG 65-45819.Mar 21, 2001 · N188AW · Boeing 737277 · Fuselage Miscellaneous StructureSDR AWXA0001510Angle · crackedCRACK IN I/B LEG OF VERTICAL ANGLE BS 578 LBL 60. REMOVED AND REPLACED VERTICAL ANGLE IAW BOEING DWG 65-46537, B737-200 SRM 51-30-2 PG 2, 3, 8.Mar 21, 2001 · N179AW · Boeing 737277 · Fuselage Miscellaneous StructureSDR AWXA0001509Web · crackedAFT CARGO COMPARTMENT, AFT OF DOOR OPENING, WEB CRACKED AND TORN ALONG EDGE OF DOOR OPENING. REPAIRED TORQUE BOX WEB AT BS 847 STR 21R IAW B737-200 SRM 51-40-2 FIG 1.Mar 21, 2001 · N179AW · Boeing 737277 · Fuselage Miscellaneous StructureSDR AWXA0001494Rib · crackedLT WING L/E RIB CRACKED IN RADIUS, I/B OF NR 1 PYLON WBL 183.4. STOP DRILLED CRACK; FORMED, DRILLED AND INSTALLED REPAIR ANGLES IAW SRM 51-40-3 FIG 1.Mar 13, 2001 · N179AW · Boeing 737277 · Wing, Rib/BulkheadSDR AWXA0001480Duct · deterioratedEN ROUTE TO PHX, ONCE AGAIN EXPERIENCED A VIBRATION. IN PHX ADDITIONAL CHECKS WERE PERFORMED TO THE RUDDER SYSTEM; THE STANDBY RUDDER FAIL AMM TEST 27-21-141 STEP 2B; THE STANDBY RUDDER DEAD BAND WAS ADJUSTED IN LIMITS PER AMM 27-21-14-1. THE PROBLEM CAUSINGMar 6, 2001 · N187AW · Boeing 737277 · Air Distribution SystemSDR AWXA0001479Duct · deterioratedLAS - DIVERTED FLIGHT - 2/27/01 - EN ROUTE FROM RNO TO PHX THE AIRCRAFT EXPERIENCED AIRFRAME VIBRATIONS THAT WERE NOTICED IN THE COCKPIT AND AFT GALLEY; THE CREW FELT IT IN THE CONTROL WHEEL AND RUDDER PEDALS. IT INCREASED IN FREQUENCY FROM 230 KTS TO .77 MACMar 6, 2001 · N187AW · Boeing 737277 · Air Distribution SystemSDR AWXA0001435Skin · crackedCRACK IN FUSELAGE SKIN AT FS 1153 RIGHT SIDE 12 INCHES ABOVE THE HORIZONTAL STABILIZER. REMOVED DAMAGED AREA AND INSTALLED A REPAIR DOUBLER AND FILLER IAW SRM 53-30-03 FIG 2.Mar 1, 2001 · N185AW · Boeing 737277 · Fuselage Main, Plate/SkinSDR AWXA0001449Skin · crackedCRACK IN FUSELAGE SKIN RT BS 747 STR 17R. REPLACED FUSELAGE SKIN RT SIDE BS 727-817 STR 14R - 20R IAW AWA ER 15-5330-01045-JS1 AND SRM 51-30-02 PG 2 AND 51-30-01 PG 2&3.Mar 1, 2001 · N185AW · Boeing 737277 · Fuselage Main, Plate/SkinSDR AWXA0001448Stringer · damagedELONGATED HOLES THRU SKIN AND STRINGER AT FS 790 STR 20R. REPAIRED MISDRILLED HOLES IAW AWA ER 15-5330-01049-DL1 AND SRM 53-10-03 FIG 1 AND 53-30-03 FIG 10.Mar 1, 2001 · N185AW · Boeing 737277 · Fuselage Main, Longeron/StringerSDR AWXA0001447Stringer · damagedELONGATED HOLES THRU SKIN AND STRINGER AT FS 760 STR 20R. REPAIRED MISDRILLED HOLES IAW AWA ER 15-5330-01049 DL2 AND SRM 53-10-03 FIG 1 AND 53-30-03 FIG 10.Mar 1, 2001 · N185AW · Boeing 737277 · Fuselage Main, Longeron/StringerSDR AWXA0001446Skin · crackedR2 SERVICE DOOR UPPER HINGE LWR AFT CORNER OF CUTOUT HAS A .125 INCH CRACK. REMOVED FASTENERS, ROUTED OUT CRACK AND INSTALLED REPAIR DOUBLER IAW SRM 51-10-02 AND 51-30-02.Mar 1, 2001 · N185AW · Boeing 737277 · Fuselage Main, Plate/SkinSDR AWXA0001445Floorbeam · crackedFLOORBEAM AT FS 520 LBL 44 HAS A 3 INCH CRACK IN UPPER RADIUS AND HAS BEEN PREVIOUSLY STOP DRILLED. REMOVED EXISTING DOUBLERS AND REPAIRED IAW AWA ER 15-5346-00354-JL1A AND SRM 51-30-02 PG 5.Mar 1, 2001 · N185AW · Boeing 737277 · Fuselage Main, Floor BeamSDR AWXA0001444Floorbeam · crackedFLOORBEAM AT FS 520 LBL 24 HAS A 3 INCH CRACK IN UPPER RADIUS THAT HAS BEEN PREVIOUSLY STOP DRILLED. REMOVED EXISTING DOUBLERS AND INSTALLED REPAIR IAW AWA ER 15-5346-00354-JL1A AND SRM 51-30-02 PG 2 & 5.Mar 1, 2001 · N185AW · Boeing 737277 · Fuselage Main, Floor BeamSDR AWXA0001443Skin · crackedEXTERNAL SKIN CRACKED IN RADIUS AT L2 DOOR UPPER HINGE CUTOUT. INSTALLED SKIN REPAIR IAW SRM 53-30-03 AND 51-10-02.Mar 1, 2001 · N185AW · Boeing 737277 · Fuselage Main, Plate/SkinSDR AWXA0001442Tie Clip · crackedCABIN STR CLIP AT FS 597 STR 8L IS CRACKED. REMOVED AND REPLACED STR CLIP IAW SRM 51-30-02 PG 5.Mar 1, 2001 · N185AW · Boeing 737277 · Fuselage Miscellaneous StructureSDR AWXA0001441Tie Clip · crackedCABIN STR CLIP AT FS 727B STR 8L IS CRACKED. REMOVED AND REPLACED STR CLIP IAW SRM 51-30-02 PG 5.Mar 1, 2001 · N185AW · Boeing 737277 · Fuselage Miscellaneous StructureSDR AWXA0001440Stringer Clip · crackedCABIN STR CLIP AT FS 727A STR 6L IS CRACKED. REMOVED AND REPLACED STR CLIP IAW SRM 51-30-02 PG 5.Mar 1, 2001 · N185AW · Boeing 737277 · Fuselage Miscellaneous StructureSDR AWXA0001439Stringer Clip · crackedCABIN STR CLIP AT FS 727A 3L IS CRACKED. REMOVED AND REPLACED CLIP IAW SRM 51-30-02 PG 5.Mar 1, 2001 · N185AW · Boeing 737277 · Fuselage Miscellaneous StructureSDR AWXA0001438Stringer Clip · crackedCABIN STR CLIP AT FS 727B STR 4R IS CRACKED. REMOVED AND REPLACED STR CLIP IAW SRM 51-30-02 PG 5.Mar 1, 2001 · N185AW · Boeing 737277 · Fuselage Miscellaneous StructureSDR AWXA0001437Stringer Clip · crackedCABIN STR CLIP AT FS 787 STR 2R IS CRACKED. REMOVED AND REPLACED STR CLIP IAW SRM 51-30-02 PG 5.Mar 1, 2001 · N185AW · Boeing 737277 · Fuselage Miscellaneous StructureSDR AWXA0001436Stringer Clip · crackedCABIN STR CLIP AT FS 787 STR 5R IS CRACKED. REMOVED AND REPLACED STR CLIP IAW SRM 51-30-02 PG 5.Mar 1, 2001 · N185AW · Boeing 737277 · Fuselage Miscellaneous StructureSDR AWXA0001434Angle · crackedNR 2 VHF ANTENNA SUPPORT ANGLE IS CRACKED OUT OF FASTENER HOLE ON RT SIDE AT FS 500 TO 500A BETWEEN STR 28L AND 28R. REMOVED CRACKED ANGLE AND SUPPORTING STRUCTURE; INSTALLED NEW SUPPORTS, CLIPS, ANGLE, FITTING AND DOUBLER IAW AWA EO 53-33-02 AND DWG 65C27810Mar 1, 2001 · N185AW · Boeing 737277 · Fuselage Miscellaneous StructureSDR AWXA0001433Web · crackedAFT CARGO DOOR INTERNAL WEB IS CRACKED AT ATTACH POINT TO LWR CROSS BEAM, LOCATED IN CENTER OF DOOR BELOW HANDLE MECHANISM. INSTALLED FILLER AND DOUBLER IAW SRM 51-10-03, 52-30-01, 51-10-01, 51-30-02 AND 51-40-03.Mar 1, 2001 · N185AW · Boeing 737277 · Cargo/Baggage DoorsSDR AWXA0001432Stringer Clip · crackedSTRINGER CLIP AT FS 807, STRINGER 3L IS CRACKED. REMOVED AND REPLACED CLIP IAW SRM 51-30-01 PG 5.Mar 1, 2001 · N185AW · Boeing 737277 · Fuselage Miscellaneous StructureSDR AWXA0001431Skin · buckledKEEL BEAM SKIN PANEL BETWEEN GEAR WELLS BUCKLED AND HAS LOOSE RIVETS. REMOVED AND REPLACED KEEL BEAM SKIN PANEL IAW ER 15-5331-01040-JS2.Mar 1, 2001 · N185AW · Boeing 737277 · Fuselage Main, Plate/SkinSDR AWXA0001430Door Frame · crackedCRACK IN L2 DOOR JAMB FWD UPPER WEB AT BS 947. REMOVED DAMAGED AREA AND INSTALLED A REPAIR DOUBLER AND FILLER IAW SRM 51-40-03.Mar 1, 2001 · N185AW · Boeing 737277 · Fuselage Main, StructureSDR AWXA0001429Skin · crackedAFT CARGO DOOR INNER SKIN HAS A 1 INCH CRACK AT LIGHTENING HOLE BELOW HANDLE MECHANISM. STOP DRILLED CRACK; FABED, DRILLED, TREATED AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-02, 51-10-01, 51-30-01.Mar 1, 2001 · N185AW · Boeing 737277 · Cargo/Baggage DoorsSDR AWXA0001428Web · crackedFLOOR WEB ON AFT SIDE OF FS 178 BLKHD SIDE CHORD AREA CRACKED. REPAIRED FLOOR WEB IAW SRM 53-20-04 PG 1-7, SRM 51-30-01 PG 2, 3, 5, 32, SRM 51-10-03 PG 1-10, SRM 51-10-01 PG 20-24 AND B737-200 MM 51-21-41 PG 702-706.Mar 1, 2001 · N185AW · Boeing 737277 · Fuselage Miscellaneous StructureSDR AWXA0001427Web · crackedFLOOR WEB ON AFT SIDE OF BS 178 BLKHD SIDE CHORD AREA AT WL 207 CRACKED. REPLACED FLOOR WEB IAW SRM 51-20-4 PG 1-7, SRM 51-30-5 PG 32, 2, 3, 5, SRM 51-40-03 PG 1-10, SRM 51-10-01 PG 20-24 AND MM 51-21-41 PG 702-706.Mar 1, 2001 · N185AW · Boeing 737277 · Fuselage Miscellaneous StructureSDR AWXA0001426Bulkhead · crackedFS 178 BLKHD HAS 3 CRACKS IN WEB MEASURING 1.3, 0.2, AND 0.3 INCH. REPAIRED WEB IAW SRM 53-10-02 PG 3, 5, 8-10, 53-10-11 PG 1-8, 53-30-02 PG 2, 3, 5, 32, 51-20-04 PG 1-7 AND B737-200 MM 51-21-40 PG 702-706.Mar 1, 2001 · N185AW · Boeing 737277 · Fuselage Main, BulkheadSDR AWXA0001425Skin · crackedFWD ENTRY DOOR INNER SKIN CRACKED AT UPPER FWD ACCESS OPENING. FABED REPAIR DOUBLER AND INSTALLED IAW B737-200 SRM 51-40-02.Mar 1, 2001 · N185AW · Boeing 737277 · Passenger/Crew DoorsSDR AWXA0001424Bulkhead · crackedFS 178 BLKHD HAS A CRACK IN WEB EMINATING FROM FASTENER HOLE. CUT OUT DAMAGED AREA; HFEC CONFIRMS NO CRACKS ON EDGE OF CUTOUT. FABED, DRILLED AND INSTALLED FILLER AND DOUBLER IAW B737-200 SRM 53-30-02.Mar 1, 2001 · N185AW · Boeing 737277 · Fuselage Main, BulkheadSDR AWXA0001410Acm · overservicedPHX - AIR TURNBACK - 2/25/01 - AFTER LEVELING OFF AT FL 310, FLIGHT ATTENDANTS REPORTED A BURNING SMELL IN THE CABIN; THE CREW STARTED A DESCENT AND TURNED OFF THE GRASPER FAN AND THE SMELL SEEMED TO GO AWAY; THE FLIGHT RETURNED TO PHX. IN PHX, MAINTENANCE FOFeb 26, 2001 · N183AW · Boeing 737277 · Cabin Cooling SystemSDR AWXA0001337Packing · brokenINFLIGHT NR 2 ENGINE OIL PRESSURE DROPPED BELOW THE RED RADIAL; THE CREW ACCOMPLISHED ENGINE SHUTDOWN PER THE ORH, RETURNED TO OAK. THE ENGINE WAS SHUTDOWN FOR 25 MIN WITH WINDMILLING OIL PRESSURE OF 20 PS. IN OAK THE OIL PRESSURE TRANSMITTER AND OIL PRESSURFeb 14, 2001 · N181AW · Boeing 737277 · Turbine Engine Oil SystemSDR AWXA0001338Packing · brokenIN PHX OIL PUMP WAS REPLACED. UPON REMOVAL THE CENTER O-RING WAS FOUND TO BE BROKEN. THE OTHER 2 WERE OK. PUMP WAS REPLACED THOUGH IT APPEARED TO BE NORMAL.Feb 14, 2001 · N181AW · Boeing 737277 · Turbine Engine Accessory Drive
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