Boeing 737-244

Service difficulty reports · 176

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  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = '737244'
  ORDER BY difficulty_date DESC"

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SDR P2EA00252Frame · crackedSJO - DURING C-CHECK, FORWARD CARGO COMPARTMENT FRAME CRACKS AT BS 420 BETWEEN STRINGER 20L AND STRINGER 23L, THREE EACH 5 INCHES. REPAIRED FRAME AT BS 420 FROM STRINGER 19L TO STRINGER 26L IAW SRM 53-10-4 FIG 1. (M)Sep 23, 2000 · N620PC · Boeing 737244 · Fuselage Main, FrameSDR P2EA00257Frame · crackedSJO - DURING C-CHECK, FRAME INNER FLANGE CRACKED .450 INCH LONG AT BS 500 BETWEEN STRINGERS 21R AND 22R. REPAIRED FRAME AT BS 500 BETWEEN STRINGERS 20R AND 26R IAW SRM 53-10-4 FIG 1. (M)Sep 23, 2000 · N620PC · Boeing 737244 · Fuselage Main, FrameSDR P2EA00268Frame · crackedSJO - DURING C-CHECK, FRAME INNER FLANGE CRACKED, LENGTH .250 INCH, AT BS 500A BETWEEN STRINGERS 21R AND 22R. REPAIRED FRAME AT BS 500A BETWEEN STRINGERS 20R AND 26R IAW SRM 53-10-4 FIG 1. (M)Sep 23, 2000 · N620PC · Boeing 737244 · Fuselage Main, FrameSDR P2EA00267Frame · crackedSJO - DURING C-CHECK, INNER FRAME CRACKED, LENGTH .375, AT BS 500B BETWEEN STRINGER 20R AND 22R. REPAIRED FRAME AT BS 500B FROM STRINGER 20R TO 26R IAW SRM 53-10-4 FIG 1. (M)Sep 23, 2000 · N620PC · Boeing 737244 · Fuselage Main, FrameSDR P2EA00266Frame · crackedSJO - DURING C-CHECK, INNER FRAME CRACKED, .125 INCH LENGTH, AT BS 500B STRINGER 26R. REPAIRED FRAME AT BS 500B BETWEEN STRINGERS 26R AND 27R IAW SRM 51-40-3 FIG 1. (M)Sep 23, 2000 · N620PC · Boeing 737244 · Fuselage Main, FrameSDR P2EA00283Skin · crackedSJO - DURING C-CHECK, HFEC CRACK INDICATIONS 3 EACH (AVG. L = .025 INCH) ON LEFT SIDE 1 EACH BS 227 WL 221, 1 EACH BS 227 WL 226 AND 1 EACH BS 235 WL 222. REPAIRED SKIN FROM BS 224 TO BS 255 AND BETWEEN STRINGERS 10L AND 18L IAW SB 737-53-1111, SECTION III PSep 22, 2000 · N620PC · Boeing 737244 · Fuselage Main, Plate/SkinSDR P2EA00286Skin · dentedDURING Q CHECK FOUND THE LEFT HAND INBOARD MID-FLAP LEADING EDGE SKIN AT STA RSS 215 WITH DENT L=1.0 IN, W=2.0 IN, D=0.200 IN. REPAIRED LT INBOARD MID-FLAP LEADING EDGE SKIN AT STA RSS 215 DENT IAW BOEING SREM 57-50-4 FIG 3Sep 22, 2000 · N620PC · Boeing 737244 · Trailing Edge FlapsSDR P2EA00261Skin · crackedSJO - DURING C-CHECK, HFEC SKIN CRACK INDICATION ON UPPER ROW OF RIVETS BETWEEN BS 939 AND BS 946 AT STRINGER 20L. REPAIRED SKIN FROM BS 923 TO BS 950 AND FROM STRINGER 19L TO 21L IAW SRM 53-30-3 FIG 13 DETAIL III. (M)Sep 21, 2000 · N620PC · Boeing 737244 · Fuselage Main, Plate/SkinSDR P2EA00254Skin · crackedSJO - DURING C-CHECK, LFEC SKIN CRACK INDICATION BETWEEN BS 386 AND BS 392 ON TOP ROW OF FASTENERS AT STRINGER 26R. REPAIRED SKIN FROM BS 386 TO BS 392 BETWEEN STRINGERS 25R AND 27R IAW SRM 53-30-3 FIG 13, DETAIL III. (M)Sep 21, 2000 · N620PC · Boeing 737244 · Fuselage Main, Plate/SkinSDR P2EA00265Skin · crackedDURING C-CHECK, HFEC SKIN CRACK INDICATION, LENGTH 2.5 INCH, AT BS 448 STRINGER 10R. REPAIRED SKIN FROM BS 442 TO BS 453 AND BETWEEN STRINGERS 10R AND 11R IAW SRM 53-30-3 FIG 13 DETAIL III. (M)Sep 21, 2000 · N620PC · Boeing 737244 · Fuselage Main, Plate/SkinSDR P2EA00264Skin · crackedDURING C-CHECK, HFEC SKIN CRACK INDICATION ON UPPER ROW OF RIVETS AT STRINGER 26R, BS 404. REPAIRED SKIN FROM BS 397 TO BS 412 AND BETWEEN STRINGERS 25L AND 27L IAW SRM 53-30-3 FIG 13 DETAIL II. (M)Sep 21, 2000 · N620PC · Boeing 737244 · Fuselage Main, Plate/SkinSDR P2EA00253Angle · crackedSJO - DURING C-CHECK, FOUND LT WING FRONT SPAR VERTICAL ANGLE AT FSS 346 CRACKED (L = 1.5 INCHES). FABRICATED AND REPLACED ANGLE IAW SRM 51-10-00 PAGE 8. (X)Sep 21, 2000 · N620PC · Boeing 737244 · Wing SparSDR P2EA00275Skin · crackedSJO - FOUND DURING C-CHECK, HFEC SKIN CRACK INDICATION ON UPPER ROW OF FASTENERS AT BS 500 STRINGER 26L. REPAIRED SKIN FROM BS 492 TO BS 506 AND FROM STRINGER 25L TO 27L IAW SRM 53-30-3 FIG 13 DETAIL 11. (M)Sep 21, 2000 · N620PC · Boeing 737244 · Fuselage Main, Plate/SkinSDR P2EA00247Fitting · gougedMCI - DURING COMPLIANCE OF VANGUARD EO NR 993753A43, FOUND THE LEFT INBOARD 1088 VERTICAL LUG FITTING LOWER INBOARD HOLE WITH STEEL BUSHING INSTALLED. REPAIRED THE LEFT INBOARD 1088 VERTICAL LUG FITTING LOWER INBOARD HOLE IAW BOEING MESSAGE NR VAG-MCI-00-0009Sep 2, 2000 · N620PC · Boeing 737244 · Vertical StabilizerSDR P2EA00246Fitting · gougedMCI - DURING COMPLIANCE OF VANGUARD EO NR 993753A43, FOUND THE LEFT OUTBOARD 1088 VERTICAL LUG FITTING UPPER OUTBOARD HOLE GOUGED, LEFT .392 INCH, WIDTH .156 INCH, DEPTH .030 INCH. REPAIRED THE LEFT OUTBOARD 1088 VERTICAL LUG FITTING UPPER OUTBOARD HOLE IAW BSep 2, 2000 · N620PC · Boeing 737244 · Vertical StabilizerSDR P2EA00201Sensor · out of positionORD - FLT 420 - DIVERTED ORD, NO EMERGENCY DECLARED, LANDING UNEVENTFUL. ON CLIMB-OUT, NR 6 SLAT LIGHT CAME ON ALONG WITH LEADING EDGE FLAP TRANSIT LIGHT. LIGHTS WENT OUT AFTER 30 SECONDS, THEN CAME BACK ON FOR A SHORT PERIOD OF TIME, THEN BACK OUT. NO FURTJun 8, 2000 · N620PC · Boeing 737244 · Leading Edge Slat Position Indicating SystemSDR P2EA00196Circuit Breaker · trippedFLT 562 - MDW - WHEN GEAR WAS SELECTED DOWN FOR APPROACH, GEAR INDICATION LIGHTS WERE INOPERATIVE. TOWER CONFIRMED GEAR DOWN ON GO AROUND. FOUND LANDING GEAR LIGHTS CIRCUIT BREAKER POPPED. RESET CIRCUIT BREAKER. INDICATION WORKED NORMALLY. LANDING WAS UNEJun 2, 2000 · N620PC · Boeing 737244 · Landing Gear Position and WarningSDR P2EA00118Fire Loop · looseORD - FLT 564 - NR 1 ENGINE FIRE WARNING SOUNDED TWICE FOR ONE SECOND EACH TIME DURING CRUISE FLIGHT AND DURING DESCENT. ENGINE SHUT DOWN AND SECURED EIGHT MINUTES BEFORE LANDING, OIL PRESSURE REMAINED ABOVE 10 PSI. NOTE: ORIGINAL FLIGHT DESTINATION WAS MDW.Apr 27, 2000 · N620PC · Boeing 737244 · Fire DetectionSDR P2EA00013Floorbeam · corrodedDURING C-CHECK, FLOORBEAM UPPER CORD CORRODED AT BS 259.5 BETWEEN LBL 15.0 INCHES AND RBL 16.0 INCHES. REPAIRED FLOORBEAM WEB AT BS 259.5 BETWEEN LBL 25 INCHES AND RBL 22 INCHES WL 208.1 IAW COOPESA EO COO-3-53-028-00 DATED 1-14-00. DOCUMENTED ON FAA FORM 81Jan 20, 2000 · N620PC · Boeing 737244 · Fuselage Main, Floor BeamSDR P2EA00012Floorbeam · corrodedDURING C-CHECK, FLOORBEAM AT BS 259.5 BETWEEN LBL 7.0 INCHES AND RBL 10.0 INCHES, FLOORBEAM WEB HAS CORROSION. DEFECT SIZE LENGTH - 17.0 INCHES. WIDTH - 2.0 INCHES. DEPTH - 0.050 INCH. REPAIRED FLOORBEAM WEB AT BS 259.5 BETWEEN LBL 8.75 AND RBL 13.875, IAWJan 20, 2000 · N620PC · Boeing 737244 · Fuselage Main, Floor BeamSDR P2EA00006Skin · delaminatedSJO - RIGHT WING FLIGHT SPOILER NR 3 DELAMINATED, DEFECT SIZE VARIOUS. REPAIRED NR 3 FLIGHT SPOILER PER COOPESA EO COO-CMP-3-57-033-00 DATED JANUARY 16, 2000. (M)Jan 13, 2000 · N620PC · Boeing 737244 · SpoilersSDR P2EA00011Skin · damagedDURING C-CHECK, LEFT MAIN LANDING GEAR OUTER DOOR WITH MISSING SKIN MATERIAL. DEFECT SIZE: LENGTH - 5.0 INCHES, WIDTH - 0.25 INCH. REPAIRED LT MAIN LANDING GEAR OUTER DOOR SKIN PER COOPESA EO NR COO-3-52-024-00 DATED JAN 14, 2000 AND BOEING FAX COO-SJO-00.Jan 10, 2000 · N620PC · Boeing 737244 · Landing Gear DoorsSDR P2EA00014Skin · delaminatedDURING C-CHECK, FOUND LT WING NR 2 SPOILER UPPER AND LOWER SURFACE DELAMINATED AND UPPER SURFACE OUTBOARD END CORNER HAS SKIN DAMAGED. DEFECT SIZE: LENGTH - 8.00 INCHES, WIDTH - 9.50 INCHES. REPAIRED LT WING NR 4 SPOILER UPPER SKIN PER COOPESA EO COO-CMP-35Jan 9, 2000 · N620PC · Boeing 737244 · SpoilersSDR P2EA00010Skin · delaminatedSJO - C-CHECK. NR 3 SPOILER UPPER SURFACE DELAMINATED AT WBL 227. DEFECT SIZE: LENGTH - 52.0 INCHES WIDTH = 20.75 INCHES. REPAIRED SPOILER PER COOPESA EO COO-CMP-3-57-032-00 DATED JAN 16, 2000. DOCUMENTED ON FAA FORM 8110-3. APPROVED AND SUBMITTED BY FAAJan 9, 2000 · N620PC · Boeing 737244 · SpoilersSDR P2EA00009Intercostal · crackedSJO - C-CHECK. INTERCOASTAL CRACKED AT S 194.5, BETWEEN STR 111RH AND STR 12RH. DEFECT SIZE: LENGTH - 4.0 INCHES. REPLACED FITTING AT BS 194.5 PER SRM 51-10-1, PAGE 5, 51-30-2. COOPESA WO N1-0004-2-309, VAM 100 NR 503. (X)Jan 9, 2000 · N620PC · Boeing 737244 · Fuselage Miscellaneous StructureSDR P2EA00008Frame · crackedSJO - DURING C-CHECK, FOUND CRACK AT BW 360 BETWEEN STR 19LT AND STR 20LT. DEFECT SIZE: LENGTH - 2.0 INCHES. REPAIRED FUSELAGE FRAME SECTION AT BS 360 BETWEEN STR'S 19LT AND 23LT PER SB 737-53A1064 SECTION III, PART II, PAR A AND B, FIG 2 REV 6, DATED JUNE Jan 9, 2000 · N620PC · Boeing 737244 · Fuselage Main, FrameSDR P2EA00007Skin · crackedSJO - FUSELAGE SKIN DOUBLER CRACKED AT BS 178, WL 170, DEFECT SIZE LENGTH 1.5 INCH. REWORKED EXTERNAL DOUBLER AT BS 178 BETWEEN RBL 2.250 AND RBL 5 WL 170 PER COOPESA EO COO-3-53-023-00 DATED JAN 13, 2000 AND BOEING FAX COO-00-000-49H JAN 12, 2000. (M)Jan 8, 2000 · N620PC · Boeing 737244 · Fuselage Main, Plate/SkinSDR P2EA00004Web · crackedDURING C-CHECK, FOUND NOSE WHEEL WELL, UPPER FORWARD RIB WEB WITH CRACK. FABRICATED WEB IAW SRM 51-20-1. REMOVED AND REPLACED WEB AT BS 227.8 TO BS 259.5, BL 0 IAW SRM 51-10-1 PAGE 5 AND SRM 51-30-2. (M)Jan 8, 2000 · N620PC · Boeing 737244 · Fuselage Structure (General)SDR P2EA00003Skin · dentedSJO - DURING C-CHECK, SKIN DENTED AT BS 1064 BETWEEN 24R AND 25R. REPAIRED SKIN FROM BS 1064 TO BS 1068 AND BETWEEN 24R AND 25R IAW 53-30-03 FIG 5. (M)Jan 8, 2000 · N620PC · Boeing 737244 · Fuselage Main, Plate/SkinSDR P2EA99343Connector · contaminatedMSP - FLT 705 - DURING FLIGHT, THE NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED, THE SAME LIGHT REMAINED EXTINGUISHED AT REDUCED THROTTLE SETTINGS. EMERGENCY WAS DECLARED AND AIRCRAFT LANDED WITH NO INCIDENT. CLEANED CANNON PLUG ON FIRE TEST UNIT AND FIRE PROTECTIDec 10, 1999 · N620PC · Boeing 737244 · Overheat DetectionSDR P2EA99308Fitting · crackedMCI - RUNNING FUEL LEAK AT RIGHT WING ROOT, LOWER SURFACE AT WING-TO-BODY AREA NEAR SUMP DRAIN. PRESSURE CHECKED. CLEANED AND SEALED LEAK AREA. LEAK NOW CLASSIFIED AS STAIN PER MM 28-11-0. FOUND TIE FITTING CRACKED IN RADIUS, BL 70.85. STRINGER S9R WING LOOct 16, 1999 · N620PC · Boeing 737244 · Fuel StorageSDR P2EA99302Retract Mech · malfunctionedMCI - FLT 588 - NR 1 LEADING EDGE SLAT TRANSIT LIGHT ON. VISUALLY CONFIRMED INBOARD END OF SLAT NOT FULLY EXTENDED WITH SLATS IN MID EXTEND POSITION. SLAT EXTENDED NORMAL WITH SLATS SELECTED TO FULL EXTEND POSITION. LUBED NR 1 LEADING EDGE SLAT. OPS CHECKSOct 8, 1999 · N620PC · Boeing 737244 · Leading Edge Slat Control SystemSDR CA990728051Track · broken(CAN) NR 7 FLAP TRACK LUG ON FORWARD ATTACH POINT FOUND BROKEN AT PIVOT BOLT HOLE. REPLACED.Jul 8, 1999 · Boeing 737244 · Trailing Edge FlapsSDR P2EA99164Prsov · malfunctionedATL - FLT 406 - NO EMERGENCY DECLARED, LANDING UNEVENTFUL. DESCENDING THROUGH 15,000 FEET, THROTTLES NEAR IDLE, A LOUD BOOM HEARD IN COCKPIT AND CABIN IN THE AIRCONDITIONING SYSTEM. THE LEFT DUCT OVERHEAT LIGHT AND MASTER CAUTION/OVERHEAD LIGHT CAME ON. QRHApr 22, 1999 · N620PC · Boeing 737244 · Compressor Bleed ValveSDR P2EA99130Wire · loosePIT - FLT 701 - ON TAKEOFF ROLL, NR 2 ENGINE EPR DID NOT RESPOND WITH ENGINE RUN-UP. FOUND NR 1 ENGINE EPR AND LANDING GEAR WARNING CIRCUIT BREAKERS POPPED. RESET CIRCUIT BREAKERS AND NR 2 EPR CAME UP. FOUND NR 1 AND NR 2 EPR CIRCUIT BREAKERS REVERSED POSITApr 7, 1999 · N620PC · Boeing 737244 · Engine Indicating System WiringSDR P2EA99029Psu · malfunctionedFLT 404 - ATL - DURING LANDING, SEVERAL PASSENGERS NOTED SPARKS EMITTING FROM PASSENGER SERVICE UNIT AT ROW 18-19 DEF (RT).Jan 26, 1999 · N620PC · Boeing 737244 · Passenger Compartment EquipmentSDR P2EA99027Bleed Control · failedMSP - FLT 416 - DURING THROTTLE ADVANCEMENT FOR TAKEOFF, HEARD LOUD NOIS FROM LEFT SIDE OF AIRCRAFT. TAKEOFF ABORTED (LESS THAN 60 KNOTS), RETURNED TO GATE. REPLACED LEFT ENGINE PRESSURE RATIO BLEED CONTROL REGULATOR PER MM 75-31-11, OPERATIONAL CHECK OK. (Jan 25, 1999 · N620PC · Boeing 737244 · Compressor Bleed ControlSDR P2EA99002Roller · brokenMDW - FLT 560 - DURING CLIMB-OUT OF MCI, THE L-1 DOOR SEAL DID NOT SEAT PROPERLY ALLOWING LOUD WIND NOISE. AFTER SEVERAL MOMENTS THE SEAL DID SET CORRECTLY, PRESSURE WAS THEN NORMAL. FIVE MINUTES LATER, LOUD POP AT DOOR, NO PRESSURE PROBLEMS RESULTED FROM THJan 12, 1999 · N620PC · Boeing 737244 · Passenger/Crew DoorsSDR P2EA98282Torsion Bar · out of adjustMCI - FLT 586 - NO EMERGENCY DECLARED LANDING UNEVENTFUL AT DESTINATION. AIRCRAFT ROLLS RIGHT WHEN FLAPS ARE EXTENDED. RETORQUED TORSION BAR ON NR 1 SLAT PER MM 27-81-21 AND LUBRICATED TRACKS, OPS CHECKED OK. (M)Dec 11, 1998 · N620PC · Boeing 737244 · Trailing Edge FlapsSDR P2EA98279Bolt · looseMDW - FLT 418 - NO EMERGENCY DECLARED LANDING UNEVENTFUL. AT FLAPS 1 RECEIVED UNCOMMANDED ROLL. POST FLIGHT REVEALS LOOSE, LEADING EDGE SLAT. FOUND NR 4 SLAT, INBOARD AUX TRACK ADJUSTMENT BOLT LOOSE. REPLACED BUSHING AND TIGHTENED BOLT PER MM 27-81-21, SLADec 9, 1998 · N620PC · Boeing 737244 · Leading Edge DevicesSDR P2EA98256Adc · failedMCI - FLT 819 - AIR RETURN NO EMERGENCY DECLARED LANDING UNEVENTFUL. BOTH AIRSPEED INDS HAD FALSE INDICATIONS ON CLIMB-OUT, F/O HIGH, CAPT'S LOW, CAPTS AIRSPEED THEN WENT OT ZERO AND STAYED THERE. CAPT'S LOW, CAPT'S AIRSPEED THEN WENT OT ZERO AND SYATED THERNov 22, 1998 · N620PC · Boeing 737244 · Air Data ComputerSDR P2EA98246Fitting · damagedSJO - INTERNAL FITTING FOUND OUT OF LIMITS AT RT WING FRONT SPAR SECTION AS FSS 432. REPLACED RIGHT WING FRONT SPAR FITTING AT FSS 432 SRM 51-10-1 PAGE 5. (M)Nov 8, 1998 · N620PC · Boeing 737244 · Wing Miscellaneous StructureSDR P2EA98245Spar · corrodedSJO - RIGHT WING FRONT SPAR UPPER CHORD CORRODED AT FSS 430. REPAIRED RIGHT WING FRONT SPAR UPPER CHORD BETWEEN FSS 401.95 AND FSS 460 PER COOPESA EO COO-3-57-597 DATED OCT 30, 1998 AND BOEING INSTRUCTION LIST OF DATA INCLUDED ON FAA FORM 8110-3. (M)Nov 8, 1998 · N620PC · Boeing 737244 · Wing SparSDR P2EA98222Frame · crackedSJO - FORWARD ENTRY DOOR LOWER AFT SECTION CRACKED, DEFECT SIZE LENGTH 1 INCH. REPAIRED FORWARD ENTRY DOOR LOWER AFT FRAME SECTION PER SRM 51-40-3 FIG 1 AND SRM 51-30-2. (M)Oct 26, 1998 · N620PC · Boeing 737244 · Passenger/Crew DoorsSDR P2EA98202Skin · corrodedSJO - FUSELAGE SKIN SECTION CORRODED AT BS 967 BETWEEN STRINGER 26 LT AND STRINGER 26 RT. REPAIRED FUSELAGE SKIN SECTION FROM BS 962 TO BS 983, BETWEEN STRINGER 26 LT TO STRINGER 26 RT PER SRM 53-30-3 FIG 17. (M)Oct 26, 1998 · N620PC · Boeing 737244 · Fuselage Main, Plate/SkinSDR P2EA98201Spar · wornSJO - RIGHT WING FRONT SPAR LOWER CHORD WORN AT WSL 475, DEFECT SIZE LENGTH 2.625 INCH, WIDTH .812 INCH DEPTH .055 INCH. REPAIRED FRONT SPAR LOWER CHORD AT WS 475 PER COOPESA EO C00-SJO-57-567-98 DATED OCT 15, 1998 AND BOEING FAX COO-SJO-98-0755RR DATED OCT 9Oct 20, 1998 · N620PC · Boeing 737244 · Wing SparSDR P2EA98185Fitting · crackedSJO - RIGHT WING SPAR FITTING CRACKED AT FSS 525, DEFECT SIZE LENGTH=1 INCH. REPLACED FRONT SPAR FITTING PER SRM 51-10-01 PAGES 5 AND SRM 51-30-2. (M)Oct 20, 1998 · N620PC · Boeing 737244 · Wing Miscellaneous StructureSDR P2EA98240Fairing · delaminatedSJO - LEFT WING TO BODY FAIRING (LT A/C BAY DOOR) INNER SKIN DELAMINATED. REPAIRED LEFT WING TO BODY FAIRING PER COOPESA EO C00-3-53-587-98 DATED OCT 26, 1998. (M)Oct 16, 1998 · N620PC · Boeing 737244 · Aerodynamic FairingsSDR P2EA98239Fairing · delaminatedSJO - RIGHT WING TO BODY FAIRING (RT A/C BAY DOOR) INNER DOOR SKIN AND SEAL DELAMINATED. REPAIRED RT WING TO BODY FAIRING PER COOPESA EO C00-3-53-588-98 DATED OCT 26, 1998. (M)Oct 16, 1998 · N620PC · Boeing 737244 · Aerodynamic FairingsSDR P2EA98196Seat Track · corrodedSJO - PAX CABIN SEAT TRACK CORRODED FROM BS 360 TO BS 400, RBL 45 INCHES. REPLACED SEAT TRACK SECTION FROM BS 360 TO BS 400, RBL 45 INCHES, WL 208.1 PER SRM 51-10-1 PAGE 5, 51-30-2, AND 53-10-5 FIG 2. (M)Oct 15, 1998 · N620PC · Boeing 737244 · Fuselage, Seat/Cargo Attach Fittings
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