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 AWXA0002002Web · crackedD: Floor beam cracked @ BS 712, LBL 25C: Repaired floor beam web at BS 712, LBL 25 IAW AWA ER #15-5715-01195-SS1Jul 7, 2001 · N182AW · Boeing 737277 · Fuselage Main, Floor BeamSDR AWXA0002147Floorbeam · corrodedCORROSION ON FLOORBEAM BS 947 RBL 43.0 TOP AND BOTTOM OF UPPER FLANGE. CUT OUT CORRODED SECTION OF BS 947 RBL 43 FLOORBEAM UPPER FLANGE. INSTALLED REPAIR IAW B737 SRM 53-10-9 FIG 3.Jul 6, 2001 · N187AW · Boeing 737277 · Fuselage Main, Floor BeamSDR AWXA0002082Intercostal · crackedD: E.T. INSP reveals cracks in intercostal on both LH & RH sides @ WL 195, just AFT 178 Each intercostal has one crack.C: LH & RH intercostal replaced per ref DWG 65-16300 SHT.3 & SRM 51-30-2 pg 2-3Jul 6, 2001 · N183AW · Boeing 737277 · Fuselage Main, Longeron/StringerSDR AWXA0002068Floorbeam · corrodedCORROSION ON FLOOR BS 947 RBL 43.0 TOP AND BOTTOM OF UPPER FLANGE. CUT OUT CORRODED SECTION OF BS 947 RBL 43 FLOORBEAM UPPER FLANGE. INSTALLED REPAIR IAW B737 SRM 53-10-9 FIG 3.Jul 6, 2001 · N187AW · Boeing 737277 · Fuselage Main, Floor BeamSDR AWXA0002131Skin · crackedD: During "D" check inspection found belly skin cracked approx BS 520 STR 27 RT at OTBD corner of groud air conditioning service doorC: repaired crack at BS 520 STR 27 RT IAW engineering repair No 15-5331-01193-SS3Jul 2, 2001 · N187AW · Boeing 737277 · Fuselage Main, Plate/SkinSDR AWXA0002047Skin · crackedD: During "C-12" check inspection found belly skin cracked approx BS 520 STR 27 RT at Fwd OTBD corner of ground air conditioning service doorC: Repaired crack at BS 520 STR 27 RT IAW AWA engineering repair No 15-01193-SS3Jul 2, 2001 · N187AW · Boeing 737277 · Fuselage Main, Plate/SkinSDR AWXA0002138Floorbeam · corrodedDURING D-CHECK INSPECTION FOUND CORROSION ON MAIN CABIN FLOORBEAM BS 312 LBL 8 TO RBL 14 WL 207.5. REMOVED CORROSION AND REPAIRED FLOORBEAM BS 312 IAW B737 SRM 53-10-9.Jul 1, 2001 · N187AW · Boeing 737277 · Fuselage Main, Floor BeamSDR AWXA0002123Frame · crackedD: During "D" check inspection found upper lobe frame cracked BS 344 Stringer 6LC: Repaired crack on upper lobe frame BS 344, at stringer 6L Iaw B737-200 SRM 53-10-4Jun 30, 2001 · N187AW · Boeing 737277 · Fuselage Main, FrameSDR AWXA0002020Skin · crackedD: R-2 door upper hinge cut out has crack in the radius of lower corner of exterior skin,C: repaired R-2 Door upper hinge cut out IAW AWA ER 15-521001191-KB2Jun 30, 2001 · N182AW · Boeing 737277 · Fuselage Main, Plate/SkinSDR AWXA0002007Frame · crackedD: During "C-12" check inspection found upper lobe frame cracked BS 344, stringer 6LC: Repaired crack on upper lobe frame BS 344, at stringer 6L IAW B737-200 SRM 53-10-4Jun 30, 2001 · N187AW · Boeing 737277 · Fuselage Main, Longeron/StringerSDR AWXA0002127Frame · crackedD: Fus frame @ BS 460 bent and cracked at S 26R to S 28LC: Formed and installed repair parts IAW 737-200 SRM 51-30-2 Pg 2&3Jun 29, 2001 · N187AW · Boeing 737277 · Fuselage Main, FrameSDR AWXA0002064Web · crackedD: Aft. pressure bulkhead web at the 8th and 9th fastener holes above S-7L, 2 ea cracks were noted on the S-8L and one at S-9LC: Repaired Aft pressure bulkhead web at the 8th and 9th fastener holes above S-7L, S-8L and S-9L IAW AWA ER 15-5383-1205-KB1Jun 29, 2001 · N182AW · Boeing 737277 · Fuselage Main, Longeron/StringerSDR AWXA0002141Skin · corrodedD: Bulge in fuselage skin exterior approx BS 800 STR 26 RTC: Repaired section of fuselage skin approx BS 800 STR 26 RT IAW AWA ER 15-5361-01205-JS1Jun 28, 2001 · N187AW · Boeing 737277 · Fuselage Main, Plate/SkinSDR AWXA0002140Skin · crackedD: R2 door fuselage skin upper hinge cut out is cracked BS 947.C: Repaired R2 door fuselage skin upper hinge cut out IAW B737 SRM 53-30-3Jun 28, 2001 · N187AW · Boeing 737277 · Fuselage Main, Plate/SkinSDR AWXA0002139Skin · crackedD: L2 door upper hinge fuselage cut out cracked BS 937C: Repaired R-2 Door fuselage skin upper hinge cut out IAW B737 SRM 53-30-3Jun 28, 2001 · N187AW · Boeing 737277 · Fuselage Main, FrameSDR AWXA0002053Skin · crackedD: R2 door fuselage skin upper hinge cut out is cracked BS 947C: repaired R2 door fuselage skin upper hinge cut out IAW B737 SRM 53-30-3 Pg 78 & 78BJun 28, 2001 · N187AW · Boeing 737277 · Fuselage Main, StructureSDR AWXA0002052Skin · crackedD: L2 Door upper hinge fuselage cut out cracked BS 979C: Repaired R2 Door fuselage skin upper hinge cut out IAW B737 SDRM 53-30-3Jun 28, 2001 · N187AW · Boeing 737277 · Fuselage Main, StructureSDR AWXA0001850Spindle · brokenELP - 5/30/01 - FLT 459 - pilot reported the aircraft used excessive lateral trim when the flaps were down. MX ferry to PHX. MX found NR 7 flap carriage spindle broken. flap carriage changed, aircraft returned to service.Jun 11, 2001 · N187AW · Boeing 737277 · Trailing Edge FlapsSDR AWXA0001824Skin · crackedfuselage skin cracked at FWD entry door upper hinge cutout, crack is APPROX .625 inch long. crack repaired IAW SRM 53-30-3 fig 21.Jun 4, 2001 · N186AW · Boeing 737277 · Fuselage Main, Plate/SkinSDR AWXA0001823Seat · wornthe sides of FWD F/A seat where the pivot arms attach have elongated holes. seat removed; repaired IAW ER 15-2525-01120-TB1; seat installed IAW MM 25-25-12 pg 201.Jun 4, 2001 · N186AW · Boeing 737277 · Passenger Compartment EquipmentSDR AWXA0001822Stiffener · crackedaft cargo pit door cracked on web radius at FWD LWR upper corner - FWD LWR door stop fitting LWR inside upper corner. aft cargo door removed; repaired stiffener radius by replacing IAW SRM 51-10-1 and DWG 65-46994; door reinstalled.Jun 4, 2001 · N186AW · Boeing 737277 · Cargo/Baggage DoorsSDR AWXA0001821Floorbeam · crackedcracks on FLOORBEAM LBL 0 STA 660 across top cap and vert web. repaired IAW ER 15-5710-01137-SS2.Jun 4, 2001 · N186AW · Boeing 737277 · Fuselage Main, Floor BeamSDR AWXA0001820Floorbeam · crackedcracks on FLOORBEAM web LBL 0 BS 708-713. repair parts made and installed IAW ER 15-5710-01137-SS2.Jun 4, 2001 · N186AW · Boeing 737277 · Fuselage Main, Floor BeamSDR AWXA0001819Floorbeam · crackedcracks on FLOORBEAM web RBL 24 BS 707-715. NDT confirmed cracks in FLOORBEAM web; area repaired IAW SRM 51-40-2 fig 2 pg 1-3.Jun 4, 2001 · N186AW · Boeing 737277 · Fuselage Main, Floor BeamSDR AWXA0001818Angle · crackedRT WING - SUSPECTED CRACK ON ANGLE RADIUS AT I/B SIDE OF ENGINE TOWER SHAFT ACCESS PANEL CUTOUT JUST FWD OF WING FRONT SPAR. FORMER P/N 69-37894-8 AT STA 226.47 CRACK REPAIRED IAW ER 15-6740-01137-JS4 AND REF DWG 65-49535 AND SRM 51-30-2 PG 2-5; NDT CONFIRMEDJun 4, 2001 · N186AW · Boeing 737277 · Wing Miscellaneous StructureSDR AWXA0001817Door Frame · crackedaft cargo FWD doorway frame cracked from just above stop fitting NR 5 to area covered by fitting (refer to AWA EO 53-10-01) marked APPROX STA 807. replaced FWD frame segment IAW REF DWG 65C35243(-3) and DWG 65-47959(-2) and REF SRM 51-10-1 pg 8 and SRM 51-30-Jun 4, 2001 · N186AW · Boeing 737277 · Fuselage Main, StructureSDR AWXA0001816Bulkhead · crackedFWD pressure BLKHD BS 178 cracked web at WL 189 BL 0. repaired IAW SRM 51-40-2 fig 1 and SRM 51-30-2 pgs 2&3.Jun 4, 2001 · N186AW · Boeing 737277 · Fuselage Main, BulkheadSDR AWXA0001763Bulkhead · crackedULTRASONIC INSP REVEALS CRACK - HORIZ POSITION AT UPPER EDGE OF WL 218 ANGLE RBL 5.7-17; APPROX LENGTH 1 INCH. REPAIRED IAW SRM 53-10-11 FIG 1 DET 3 AND SRM 51-30-2 PG 5 AND REF DWG 65-16300.May 29, 2001 · N186AW · Boeing 737277 · Fuselage Main, BulkheadSDR AWXA0001762Frame · crackedBS 178 BLKHD LT CHORD O/B HAS CRACK INDICATION AT WL 207. NDT INSP IAW BOEING NDTM PT 6 51-00-00 FIG 23; LT SIDE CHORD REPLACED IAW SRM 51-10-1 PG 8 AND SRM 51-10-2 PG 2-3 AND DWG 65-16300; METAL REPROTECTED IAW SRM 51-30-2 PG 7; EDGE SEALED IAW SRM 51-24-0; May 16, 2001 · N186AW · Boeing 737277 · Fuselage Main, FrameSDR AWXA0001761Frame · crackedBS 178 BLKHD RT CHORD O/B HAS CRACK INDICATION AT WL 207 ON FUSE SKIN. NDT INSP IAW BOEING NDTM PT 6 51-00-00 FIG 23; RT SIDE CHORD REPLACED IAW SRM 51-10-1 PG 8 AND SRM 51-30-2 PG 2-3 AND DWG 65-16300; METAL REPROTECTED IAW SRM 51-10-2 PG 7; EDGE SEALED IAWMay 16, 2001 · N186AW · Boeing 737277 · Fuselage Main, FrameSDR AWXA0001719Pin · installedPHX - AIR TURNBACK, AFTER TAKEOFF WHEN THE LANDING GEAR HANDLE WAS SELECTED UP, THE NOSE GEAR DIDN''T RETRACT AND THE AIRCRAFT RETURNED TO PHX MAKING AN UNEVENTFUL LANDING. UPON ARRIVAL AT THE GATE IT WAS FOUND THAT THE NOSE GEAR DOWNLOCK PIN WAS INSTALLED. May 9, 2001 · N188AW · Boeing 737277 · Landing Gear Retraction/Extension SystemSDR AWXA0001699Radar · unreliablePHX - AIR TURNBACK, EN ROUTE FROM PHX TO AUS THE WEATHER RADAR BECAME UNRELIABLE; EXCESSIVE TILT UP, 6 DEG TO ELIMINATE GROUND CLUTTER (CLIMB THRU 16000 FT) WINGS LEVEL RADAR POINTS IMAGES TO RIGHT, OCCASIONALLY LEFT EVEN WITH TILT 6 DEG; STABILIZATION OFF IMPMay 8, 2001 · N187AW · Boeing 737277 · Weather Radar SystemSDR AWXA0001694Bulkhead · crackedULTRASONIC INSP REVEALS CRACK VERT POSITION AT I/B EDGE LBL 5.7 AT WL 234 BS 178 LOCATION .75 INCH LENGTH. REPAIRED IAW SRM 53-10-11 FIG 1 DETAIL III AND SRM 51-30-2 PG 5 AND REF DWG 65-16300.May 7, 2001 · N186AW · Boeing 737277 · Fuselage Main, BulkheadSDR AWXA0001645Switch · brokenOAK - ABORTED TAKEOFF - 4/21/01 - AS POWER WAS APPLIED FOR TAKEOFF, THE CONFIGURATION WARNING HORN SOUNDED AND THE TAKEOFF WAS ABORTED; THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE TROUBLESHOT AND FOUND THE SPEED BRAKE TAKEOFF WARNING SWITCH (S651) BROKEN. Apr 25, 2001 · N188AW · Boeing 737277 · Central WarningSDR AWXA0001605Beam · crackedAFT CARGO DOOR LWR CROSS BEAM CRACKED AT FWD END. REPAIRED IAW EO 52-33-01 REV D AND SRM 51-30-2 PG 2-3 AND 51-20-1 PG 13.Apr 9, 2001 · N179AW · Boeing 737277 · Cargo/Baggage DoorsSDR AWXA0001604Floorbeam · crackedFLOORBEAM REPAIR RBL 25 BS 675 CRACKED. REMOVED AND REPLACED FLOORBEAM REPAIR IAW B737-200 SRM 51-20-1 PG 13 FIG 2, 51-40-02 AND 51-70-11 FIG 1 PG 1-6.Apr 9, 2001 · N179AW · Boeing 737277 · Fuselage Main, Floor BeamSDR AWXA0001603Tee Chord · crackedMAIN WHEEL WELL FWD BLKHD UPPER T-CHORD CRACKED AT FS 663.75 RBL 24. REPAIRED IAW BOEING DWG 65C37732, SRM 51-30-2 PG 2 - 3, 5, 7 - 9 AND AWA ER 15-5702-01073-JS3.Apr 9, 2001 · N179AW · Boeing 737277 · Fuselage Main, StructureSDR AWXA0001581Angle · crackedANGLE CRACKED AT FS 663 BLKHD WL 207. REMOVED AND REPLACED ANGLE IAW B737-200 SRM 51-40-4 PG 1 FIG 1 AND 51-30-2 PG 1.Apr 2, 2001 · N179AW · Boeing 737277 · Fuselage Miscellaneous StructureSDR AWXA0001580Rib · chafedLEFT I/B MID FLAP I/B RIB CHAFED. CUT OUT DAMAGED AREA; CUT, FITTED, DRILLED AND INSTALLED REPAIR FILLER, PLATE AND DOUBLER IAW B737-200 SRM 51-30-2 PG 2, 3, 8, 9, 13 & 14 AND 57-50-4 PG 8 & 9 FIG 4.Apr 2, 2001 · N179AW · Boeing 737277 · Trailing Edge FlapsSDR AWXA0001578Frame · crackedCRACK IN ANGLE AT BS 597 LBL 69 WL 203. REMOVED FRAME AND WEBS; REPLACED FRAME AND REINSTALLED WEBS IAW SRM 51-30-5 PG 4 & 5 AND 51-30-2 PG 1.Apr 2, 2001 · N179AW · Boeing 737277 · Fuselage Main, FrameSDR AWXA0001577Rib · chafedRT PYLON L/E FAIRING FWD SEAL RETAINER AND RIB CHAFED BEYOND LIMITS. FORMED, DRILLED AND INSTALLED REPAIR ANGLE IAW SRM 51-40-3 PG1-5 AND 51-30-2 PG 2 & 3.Apr 2, 2001 · N179AW · Boeing 737277 · Nacelle/Pylon, Frame/Spar/RibSDR AWXA0001576Pressure Panel · crackedLT WHEEL WELL UPPER PRESSURE WEB CRACKED AT BS 664 LBL 34 AND BS 673 LBL 31. REPAIRED CRACKS IAW AWA ER 15-5702-01082-GF2.Apr 2, 2001 · N179AW · Boeing 737277 · Fuselage Main, BulkheadSDR AWXA0001575Pan · crackedFWD GALLEY DOOR PAN CRACKED AT UPPER HINGE CUTOUT. REPAIRED DOOR PAN IAW AWA ER 15-5210-01086-GF2.Apr 2, 2001 · N179AW · Boeing 737277 · Service DoorsSDR AWXA0001573Web · crackedCRACK IN LWR FLOOR SUPPORT FLANGE AND WEB BS 704-717 BL 0. REPAIRED CRACK IAW B737-200 SRM 51-40-4 PG 1-4 AND SB 737-57-1210 PG 44-47.Apr 2, 2001 · N179AW · Boeing 737277 · Fuselage Miscellaneous StructureSDR AWXA0001572Floorbeam · crackedFLOORBEAM REPAIR RBL 25 BS 675 CRACKED. REMOVED AND REPLACED FLOORBEAM REPAIR AT RBL 25 BS 675 IAW B737-200 SRM 51-20-1 PG 13 FIG 2; AND COMPARTMENT BS 500 FRAME IAW SRM 51-40-02 AND 51-70-11 FIG 1 PG 1-6.Apr 2, 2001 · N179AW · Boeing 737277 · Fuselage Main, Floor BeamSDR AWXA0001571Fitting · damagedDURING MAINTENANCE CHECK REMOVAL OF BOLT, RIGHT O/B FWD VERT FIN ATTACH LUG BOLT HOLE WAS DAMAGED AT FS 1088. REMOVED AND REPLACED LUG AWA ER 15-5383-00029-JS1A.Apr 2, 2001 · N179AW · Boeing 737277 · Vertical Stabilizer, Attach FittingsSDR AWXA0001550Bulkhead · crackedCRACK IN 178 BLKHD WEB AT LBL 11.5 WL 218.5 BENEATH U-CHANNEL REINFORCEMENT. REPAIRED CRACK IAW B737-200 SRM 53-10-11 FIG 1 PG 1-4 & 6.Mar 27, 2001 · N179AW · Boeing 737277 · Fuselage Main, BulkheadSDR AWXA0001549Frame · crackedFUSELAGE FRAME CRACKED IN RADIUS AFT SIDE AT FS 597 RBL 65 WL 206. REPLACED FRAME IAW B737-200 SRM 51-30-2 PG 2.Mar 27, 2001 · N179AW · Boeing 737277 · Fuselage Main, FrameSDR AWXA0001537Skin · crackedAFT CARGO DOOR INNER SKIN CRACKED AT 3 PLACES, AT LIGHTNING HOLES IN CENTER SKIN BETWEEN BEAMS 2 AND 3. REPAIRED CRACKS IN INNER SKIN IAW SRM 51-20-1 PG 10A AND 51-30-2 PG 2.Mar 26, 2001 · N179AW · Boeing 737277 · Cargo/Baggage DoorsSDR AWXA0001536Floorbeam · crackedFLOORBEAM AT FS 520 RBL 24.75 HAS A CRACK IN THE RADIUS OF UPPER CHORD EXTENDING PAST STOP DRILL. REMOVED EXISTING DOUBLERS; VERIFIED CRACK LENGTH; STOP DRILLED CRACK; VERIFIED CRACK TERMINATION AT STOP DRILL. REINSTALLED DOUBLERS IAW SRM 51-30-2 PG 1.Mar 26, 2001 · N179AW · Boeing 737277 · Fuselage Main, Floor Beam
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