# Service difficulty reports: N17139

A list on [N17139](https://openairdocs.org/aircraft/N17139.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 · 71 reports

- [SDR CALA2026043015858](https://openairdocs.org/sdr/CALA2026043015858.md): Lamp · no test · Apr 29, 2026 · N17139 · Boeing 757224 · Emergency Lighting
  > EXTERIOR SLIDE LIGHT OUT AT DOOR R1 DURING EMERGENCY LIGHT TEST. R & R R1 SLIDE LIGHT LAMP IAW AMM 33-51-06 OPS CHECK GOOD.
- [SDR CALA2026040315057](https://openairdocs.org/sdr/CALA2026040315057.md): Threshold · fod · Apr 3, 2026 · N17139 · Boeing 757224 · Passenger/Crew Doors
  > L4 DOOR WILL NOT ARM, REMOVED DEBRIS FROM THRESHOLD AREA, ARMED AND DISARMED DOOR NORMALLY WITH ASSOCIATED SLIDE LIGHT OPS NORMALLY. CHECKED GOOD.
- [SDR CALA2025113011590](https://openairdocs.org/sdr/CALA2025113011590.md): Lamp · inoperative · Nov 30, 2025 · N17139 · Boeing 757224 · Emergency Lighting
  > UPON SERVICE2 INSPECTION FOUND L2 DOOR OVERHEAD EMERGENCY LIGHTS INOP RELAMPED EMERGENCY LIGHT NO HELP, SUPECT BATTERY PACK M&E 75-3351-3-00041 2013-LA REFERENCE LOGPAGE 7124123 FOR R AND R OF EMERGENCY LIGHT POWER SUPPLY, OPS CHECK GOOD PER AMM 33-51-07.
- [SDR CALA2025101309935](https://openairdocs.org/sdr/CALA2025101309935.md): Battery Pack · inoperative · Oct 11, 2025 · N17139 · Boeing 757224 · Emergency Lighting
  > SEAT EMERGENCY LIGHTS ROW 21 ABC THROUGH 31 ABC INOP. REMOVED AND REPLACED THE BATTERY PACK AS PER AMM 33-51-07-902-001. OPS CHECK GOOD.
- [SDR CALA2025100209548](https://openairdocs.org/sdr/CALA2025100209548.md): Indicator · out of position · Oct 2, 2025 · N17139 · Boeing 757224 · Emergency Equipment
  > R1 SLIDE ARM LIGHT IS OUT OF PLACE, R1 SLIDE ARM LIGHT ON DEFERAL. DDP COMPLIED WITH. APPROVED AC OK TO CONTINUE ON 2566R KNUCKLE KNOCKER OPS NORMAL. DM ADDED LIGHT (L404) IF NEEDED. REF WDM 25-66-11-1. REPLACED SLIDE LIGHT PER WDM 25-66-11-1. OPS CHECK GOOD.
- [SDR CALA2025093009423](https://openairdocs.org/sdr/CALA2025093009423.md): Proximity Sensor · sticking · Sep 23, 2025 · N17139 · Boeing 757224 · Emergency Equipment
  > SLIDE LIGHT OVER 2R ILLUMINATED ON GROUND WILL NOT EXTINGUISH DOOR SLIDE ARMED LIGHT STAYS ILLUMINATED WHEN DOOR IS DISARMED. LIGHT EXTINGUISHES WHE DOOR HANDLE IS MOVED TO THE OPEN POSITION, LIGHT ILLUMINATES WHEN DOOR IS CLOSED AND DISARMED. VERIFIED GIRT
- [SDR CALA2025080707416](https://openairdocs.org/sdr/CALA2025080707416.md): Door · no discrepancy · Aug 4, 2025 · N17139 · Boeing 757224 · Emergency Exits
  > REMOVED LT FWD OVERWING EMERGENCY EXIT HATCH TO FOM IAW AMM 52-22-02-002-001. INFO ONLY UPDATED REFERENCE FOR REMOVED AMM 52-22-01-902-001 INSTALLED L/H FWD OVERWING EMERGENCY EXIT HATCH IAW AMM 52-22-01-402-074. OPS CHECK OK. C/W RII INSP OF INSTALL OF ORIGIN
- [SDR CALA2025080507311](https://openairdocs.org/sdr/CALA2025080507311.md): Spring · broken · Aug 1, 2025 · N17139 · Boeing 757224 · Emergency Exits
  > LEFT FWD EMERGENCY DOOR WAS OPENED AND CLOSED TROUBLESHOOTING EXTERNAL TRIGGER HANDLE FLAPPER WITH BROKEN SPRING. REMOVED AND INSTALLED LT FWD OVERWING EXIT HATCH FOR INSPECTING EXTERNAL FLAPPER TRIGGER PANEL IAW AMM 52-22-01-902-001 AND 52-22-01-402-074.
- [SDR CALA2025071406561](https://openairdocs.org/sdr/CALA2025071406561.md): Power Supply · no test · Jul 11, 2025 · N17139 · Boeing 757224 · Emergency Lighting
  > WHILE PERFORMING EMERGENCY LIGHT CHECK FOUND AFT #4 RH DOOR EMERGENCY EXIT SIGN NOT ILLUMINATING PERFORMED REPLACED THE LAMP OF #4 R/H AFT DOOR EMERGENCY EXIT SIGN AS REQUIRED. NO HELP. REQUIRES FURTHER T/S. R & /R BATTERY ASSEMBLY AND BATTERY CHARGER IAW AMM
- [SDR CALA2025061305536](https://openairdocs.org/sdr/CALA2025061305536.md): Lanyard · unsecure · Jun 10, 2025 · N17139 · Boeing 757224 · Emergency Equipment
  > ROPE ON ESCAPE SLIDE DOOR 1R IS HANGING EXTERNAL OF A/C. PERFORMED INSTALLATION OF ROPE ON ESCAPE SLIDE AT DOOR 1R IAW AMM TASK 25-66-01-404-044, NOW IT IS IN NORMAL CONDITION
- [SDR CALA2025060505286](https://openairdocs.org/sdr/CALA2025060505286.md): Surge Valve · faulted · Jun 2, 2025 · N17139 · Boeing 757224 · APU Bleed Air System
  > F/AS REPORTED A THUMPING SOUND AND VIBRATION UNDE R THE AFT GALL EY JUMPSEA T. STARTED B4 GEAR DODEBRIEFED CREW SUSPECT APU BLEED VALVE. WITH APU RUNNING AND APU BLEED ON, PACKS RUNNING. WHEN EITHER PACK IS TURNED OFF, THE APU BLEED DUCT IN A/C AND WHEEL SHUTT
- [SDR CALA2025060305203](https://openairdocs.org/sdr/CALA2025060305203.md): Girt Bar · fod · May 30, 2025 · N17139 · Boeing 757224 · Emergency Equipment
  > DOOR 1R WILL NOT ARM, UPON INVESTIGATION FOUND FWD GIRT BAR FITTING FOULED, DEBRIS REMOVED AND SLIDE ARMING FUNCTION OPS TESTED SATIS IAW AMM 52-11-25-735--024 R136 20JAN25
- [SDR CALA2025040303471](https://openairdocs.org/sdr/CALA2025040303471.md): Door · obstructed · Mar 30, 2025 · N17139 · Boeing 757224 · Passenger/Crew Doors
  > L2 DOOR WILL NOT ARM. LEVER WILL NOT TRAVEL TO ARM POSITION. FOUND SURVIVAL KIT LANYARD PREVENTING DOOR ARM FUNCTION AT 2L, STOWED LANYARD AS NECESSARY REF AMM 25-66-01. DOOR 2L ARMS AND DISARMS NORMALLY
- [SDR CALA2024120303013](https://openairdocs.org/sdr/CALA2024120303013.md): Coffeemaker · inoperative · Dec 3, 2024 · N17139 · Boeing 757224 · Buffet/Galleys
  > STRONG ELECTRICAL SMELL FORWARD GALLEY DURING DESCENT. POSSIBLE ELECTRICAL FAILURE IN FWD GALLEY. AN ELECTRICAL ODORS SMELL. REMOVED AND REPLACED #1 COFFEE MAKER THAT STOPPED WORKING. WHICH POSSIBLE CAUSED THE SMELL. OPS CHK GOOD OK TO CONTINUE.
- [SDR CALA2024092602492](https://openairdocs.org/sdr/CALA2024092602492.md): Panel · damaged · Sep 24, 2024 · N17139 · Boeing 757224 · Engine Thrust Reverser
  > REF AMES NON ROUTINE 174011-0400-0096. PER CUSTOMER REQUEST; REPAIR #2 O/B T/R INNER LINER T/E. REPAIRED #2 O/B T/R INNER LINER IAW AIRBORNE DOCUMENT#47634REA02 AND UNITED EC/RA 7500-01389.
- [SDR CALA2024092302460](https://openairdocs.org/sdr/CALA2024092302460.md): Skin · dented · Sep 16, 2024 · N17139 · Boeing 757224 · Fuselage Structure (General)
  > REF AMES NON ROUTINE 174011-0200-0084.PER CUSTOMER REQUEST. FORWARD OF THEL2 DOOR,FORWARD REPAIR DOUBLER, THE UPPER FORWARD CORNER APPEARS TO BE DENTED. MEASURED DENT (A)=7.5" (Y)DEPTH.160" A/Y=46 DENT FOUND TO BE O REPAIR PERFORM INSP PER PART 2 OF LATEST R
- [SDR CALA2024091602424](https://openairdocs.org/sdr/CALA2024091602424.md): Floor Support · cracked · Sep 13, 2024 · N17139 · Boeing 757224 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT ANGLE CRACKED AROUND N UTPLATE IN ALC STA 1520 TO 1540 BL-0-LOOKING UP. REPORTED BY V89 4037 REMOVED AND REPLACED FLOOR SUPPORT ANGLE IN ALC STA 1520-1540 BL O IAW B757-200 SRM 51-40-02 PAR 7. SEE NON-ROUTINE 174011-0100-0 062 FOR DETIALS
- [SDR CALA2024090902404](https://openairdocs.org/sdr/CALA2024090902404.md): Floor Support · cracked · Sep 5, 2024 · N17139 · Boeing 757224 · Fuselage Miscellaneous Structure
  > GEN ITEM: 19-0650-1-2107 MAIN DECK FLOOR SUPPORT ANGLE CRACKED AROUND NUTPLATE IN ALC STA 1580 TO 1600 BL-0- LOOKING UP.......53021 REMOVED AND REPLACED FLOOR BOARD ANGLE PN 146N5180V59 @ STA 1580 -1600 BL-O IAW B757 SRM 51-40-02-06-0 PARAGRAPH 7 AND BOEING DW
- [SDR CALA2024080700383](https://openairdocs.org/sdr/CALA2024080700383.md): Sensor · faulty · Aug 5, 2024 · N17139 · Boeing 757224 · Engine RPM Indicating System
  > INFLIGHT RT ENGINE BLEED OFF. RT CTR FUEL PUMP INOP. RT ENGINE N3 INDICATING 0 REMOVED AND REPLACED E2 TACHOMETER REF 77-12-02 AND FIM 77-12-805 PARTS USED: 19-7712-9-9001,QTY:1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1928849 SN OFF 7761. INFLIGHT RT EN
- [SDR CALA2024072300272](https://openairdocs.org/sdr/CALA2024072300272.md): Hose · failed · Jul 19, 2024 · N17139 · Boeing 757224 · Hydraulic System, Main
  > FOUND LH MLG DOWNLOCK ACT PRESSURE FLEX HOSE LINE FAILED AT ACT B NUT. (REF LP #8664494) REPLACED HYD PRESSURE LINE ON LH MLG DOWNLOCK ACT PER AMM 32-32-02-404-010 FOR HOSE REPLACEMENT. STILL REQUIRES FUNCTIONAL CHECK PER ITEM 3E (12).PARTS USED: 19-3232-3-00
- [SDR CALA2023090802747](https://openairdocs.org/sdr/CALA2023090802747.md): Skin · unknown · Sep 4, 2023 · N17139 · Boeing 757200 · Fuselage Main, Plate/Skin
  > POSSIBLE LIGHTNING STRIKE LEFT SIDE. PER CREW DEBRIEF NO ABNORMALITIES TO RADIOS OR NAV EQUIPMENT ADDED PICS ADDED PIC FOUND 5 EA LIGHTNING STRIKE ON SECTION 41, LH SIDE, AT THE PERFORMED LIGHTNING STRIKE INSPECTION TO ALL AC AREAS,EXCEPT EXAMINED EXTERNAL
- [SDR CALA2023022200500](https://openairdocs.org/sdr/CALA2023022200500.md): Intercostal · corroded · Feb 20, 2023 · N17139 · Boeing 757200 · Cargo/Baggage Doors
  > (B757-53-3-0478) AFT CARGO DOOR LOWER INTERCOSTAL HAS CORROSION ON AFT SIDE, JUST FWD OF LOWER SERVICE LIGHT ASSY AT APPROX STA 1410 (MARKED). STREAMER ATTACHED. TRANSCRIBED FROM HAECO N/R 928 2570 REMOVED CORROSION AFT CARGO DOOR INTERCOSTAL, ORIG MAT THICKNE
- [SDR CALA2023022000471](https://openairdocs.org/sdr/CALA2023022000471.md): Floorbeam · corroded · Feb 17, 2023 · N17139 · Boeing 757200 · Fuselage Structure (General)
  > (B757-53-3-0479) MAIN CABIN STA 720 RBL 24 FLOOR BEAM UPPER SURF ACE CORRODED. TRANSCRIBED FROM HAECO GSO NR 9282317
- [SDR CALA2023021400433](https://openairdocs.org/sdr/CALA2023021400433.md): Unknown · cracked · Feb 13, 2023 · N17139 · Boeing 757200 · Fuselage Main, Frame
  > (B757-53-3-0571) AFT CABIN LH SIDE FRAME 1620 INTERCOSTAL SUPPOR T CRACKED. (LOCATED JUST ABOVE THE AFT CABIN WINDOW) TRANSCRIBED FROM HAECO GSO NR 9282500. REMOVED AND REPLACED LH STA 1620 INTERCOSTAL SUPPORT CHORD IAW B AC DWG 146NN3700 REV A AND B757-200 SR
- [SDR CALA2023021400432](https://openairdocs.org/sdr/CALA2023021400432.md): Frame · unknown · Feb 13, 2023 · N17139 · Boeing 757200 · Fuselage Main, Frame
  > "THE REPAIR INCORPORATED VIA ECRA 5360-01687 IS APPROVED AS TIME -LIMITED FOR 18 MONTHS PENDING THE RESULTS OF A DAMAGE TOLERANCE ANALYSIS (DTA). REMOVE THE AIRCRAFT FROM SERVICE ON OR BEFORE AU GUST 01, 2024, UNLESS ANOTHER 8110-3 FORM IS RECEIVED FINDING AP
- [SDR CALA2023020800353](https://openairdocs.org/sdr/CALA2023020800353.md): Intercostal · corroded · Feb 6, 2023 · N17139 · Boeing 757200 · Fuselage Main, Structure
  > SUPPORT TASK: AFT CARGO COMPARTMENT R/H INTERCOSTAL BETWEENFRAME 1360-1380 AND STR 26R-27R HAS CORROSION. TRANSCRIBED FROM HAEC O GSO NR 9282479 INSP Q467 REMOVED AND REPLACED STA 1360-1380 INTERCOSTAL BETWEEN RH STRING ERS 26R-27R IAW DWG 146N5212 AND B757-2
- [SDR CALA2023020300314](https://openairdocs.org/sdr/CALA2023020300314.md): Intercostal · corroded · Feb 2, 2023 · N17139 · Boeing 757200 · Fuselage Miscellaneous Structure
  > (B757-53-3-0478) AFT PIT RH INTERCOSTAL LOWER FLANGE HAS CORROSION AT STA 1280, BETWEEN S26R AND S27R (MARKED). TRANSCRIBED FROM HAECO N/R 9282563 S27R I.A.W B757-200 SRM 51-40-02 RECEIVED NEW INTERCOSTAL P/N 14 S26R-S27R I.A.W B757-200 SRM 51-40-02 AND I.A.W
- [SDR CALA2023020100278](https://openairdocs.org/sdr/CALA2023020100278.md): None · corroded · Jan 30, 2023 · N17139 · Boeing 757200 · Fuselage Structure (General)
  > (B757-53-3-0479) MAIN CABIN STA 1720 BLO TO LBL 36 AFT DECK PLAT E UPPER SURFACE CORRODED. TRANSCRIBED FROM HAECO GSO NR 9282403 REMOVED AFT DECK PLATE AND FABRICATED NEW PLATE PO: 1049326.1 AP PLIED FINISH AND TOP COAT AND INSTALLED NEW PLATE IAW B757-200 S
- [SDR CALA2023013000238](https://openairdocs.org/sdr/CALA2023013000238.md): Intercostal · corroded · Jan 27, 2023 · N17139 · Boeing 757224 · Fuselage Miscellaneous Structure
  > (B757-06-3-0243) AFT PIT BILGE AREA, RH INTERCOSTAL HAS CORROSIO N ON LOWER FLANGE AND VERTICAL WEB FROM STA 1310-S28R (MARKED). STREAMER ATTACHED. TRANSCRIBED FROM TASK CARD HAECO GSO NR 9282 611. B757-200 SRM 51-40-02, RECEIVED NEW INTERCOSTAL P/N 146N5700U
- [SDR CALA2023012500196](https://openairdocs.org/sdr/CALA2023012500196.md): Wedge · damaged · Jan 23, 2023 · N17139 · Boeing 757224 · Leading Edge Devices
  > (B757-06-3-0306) #3 SLAT WEDGE T/E PREVIOUS REPAIR SEPARATED 31" FROM INBD EDGE. TRANSCRIBED FROM HAECO NR 9282457. REPAIRED #3 SLAT WEDGE T/E IAW B757 SRM 57-43-02-2R-1, SRM 51-70 -10-2R-0 AND AMM 51-21-001/701. REMOVED HAECO DOT. TRANSCRIBED F ROM HAECO NR 9
- [SDR CALA2023012300179](https://openairdocs.org/sdr/CALA2023012300179.md): Angle · corroded · Jan 21, 2023 · N17139 · Boeing 757224 · Fuselage Miscellaneous Structure
  > MAIN CABIN STA 720-740 RBL 61 R2 LOWER SILL CHORD UPPER SURFACE CORRODED. REMOVED AND REPLACED LOWER SILL CHORD IAW DRAWING 143N83 22 REV-, SRM 51-40-06, SRM 51-40-05. REMOVED AND
- [SDR CALA2022121203361](https://openairdocs.org/sdr/CALA2022121203361.md): Fseu · warning message · Dec 11, 2022 · N17139 · Boeing 757224 · Trailing Flap Position Indicating System
  > TE FLAP DISAGREE EICAS MSG NO EICAS DISAGREE MESSAGE FOUND. PERFORMED FSEU BITE PER FIM NORMALLY. OK TO CONTINUE. 27-51 FAULT TREE 803. FOUND NO HYDRAULIC PRESSURE FAULT ON EXISTING FAULTS. FAULT CODE 302. OPERATED FLAPS SEVERAL TIMES AND FAULT CLEARED. NO FUR
- [SDR CALA2022072701888](https://openairdocs.org/sdr/CALA2022072701888.md): Window · warning message · Jul 27, 2022 · N17139 · Boeing 757200 · Windshield/Door Rain/Ice Removal
  > L SIDE WINDOW EICAS MSG ON T/O. LOWSPEED REJECT AT 60 KTS CREW REPORTED THAT MSG EXTINGUISHED ON TAXI TO STAND. OPS TEST OF SYSTEM C/O ALL INDICATIONS NORMAL C/O IAW MM 30-41-00. A/C RELEASED FOR SERVICE
- [SDR CALA2022021800437](https://openairdocs.org/sdr/CALA2022021800437.md): Hydraulic Line · leaking · Feb 17, 2022 · N17139 · Boeing 757224 · Hydraulic Power Accumulator, Main
  > COMPLETE LOSS OF LEFT HYD QTY ON SHORT FINAL. NO NOSEWHEEL STRNG AND BROUGHT THE AIRCRAFT TO A STOP AND SHUT DOWN THE ELECTRIC PUMPS, (HYD QTY WAS AT 1.6), STARTED APU AND SHUT DOWN #2 ENGINE. CALLED FOR TOW TO GATE. INFO ONLY PER CREW: ON SHORT FINAL AFTER GE
- [SDR CALA2022020700338](https://openairdocs.org/sdr/CALA2022020700338.md): Engine · vibration · Feb 7, 2022 · N17139 · Boeing 757224 · Engine Ignition Analyzer
  > NO 1 ENG VIBE 2.6-3.0 NO VIBE FELT 2.6-3.0 HIGHEST IND FL390 PER PREVIOUS UPDATE CODE B7 ON AVM CHECKED WIREING SECURITY AT ENGINE 1 TRANDUCER, FOUND ALL SECURE THIS LOG HAS BEEN LOCKED BY THE TOMC MGR DUE TO EMERGENCY UNLOCKED FOR MX UPDATE DECLARATION. L AVM
- [SDR CALA2020020200281](https://openairdocs.org/sdr/CALA2020020200281.md): Frame · dented · Jan 26, 2020 · N17139 · Boeing 757224 · Fuselage Main, Frame
  > B757-06-3-0230 DENT ON FWD CARGO FRAME UPPER FLANGE STA 660BETWE EN STRINGER 24 AN STRINGER 25 (034-038) LH SIDE REF ST ENG N/R 0 085668 FOUND DENT OUT OF LIMITS IAW B757-200 SRM 53-00-07 FIG 101 L=1.1 0, W=.90, D=.047. CUT OUT DAMAGE AND ACCOMPLISHED CATEGORY
- [SDR CALA2020020100269](https://openairdocs.org/sdr/CALA2020020100269.md): Web · dented · Jan 23, 2020 · N17139 · Boeing 757224 · Passenger/Crew Doors
  > B757-06-3-0366 L-4 PASSENGER DOOR, INTERNAL WEB IS PUNCTURED AT UPPER HINGE CAVITY. (96-03) REF ST ENG N/R 0085414 REPAIRED L4 PASSENGER DOOR INTERVAL WEB SKIN AT HINGE CAVITY IAW ECRA 5210-03049.
- [SDR CALA2020012600224](https://openairdocs.org/sdr/CALA2020012600224.md): Pan · dented · Jan 19, 2020 · N17139 · Boeing 757224 · Passenger/Crew Doors
  > SUPPORT TASK EA 5210-01360 REV J OP 001 SECONDARY FINDING UPON R EMOVAL OF THE L-1 EXTERNAL DOOR HANDLE, DISCOVERED A DEEP GOUGE ON THE PAN. (96-30) REF ST ENG N/R 0085800 CHECKED LIMITS TO GOUGE AT L1 DOOR HANDLE PAN L=.30 W=.20 D=.011 ORIGINAL MAT THICKNESS
- [SDR CALA2018120202477](https://openairdocs.org/sdr/CALA2018120202477.md): Rivet · sheared · Nov 30, 2018 · N17139 · Boeing 757224 · Trailing Edge Flaps
  > FOUND SHEARED RIVET ON NR 6 FLAP TRACK SUPPORT. REMOVED AND REPLACED DAMAGED RIVETS REF SRM 51-40-02.
- [SDR CALA2018011200109](https://openairdocs.org/sdr/CALA2018011200109.md): Torque Tube · damaged · Jan 12, 2018 · N17139 · Boeing 757224 · Trailing Edge Flap Control System
  > TE FLAP ASYM ON LANDING, LEFT FLAP INDICATION 10, RT FLAP 15. EMERGENCY DECLARED. TROUBLESHOT IAW FIM 27-51-00-815-809 BLOCK 22. R & R THE T/E FLAP TORQUE TUBE IAW AMM 27-51-25-422-016. NO FURTHER FLAP ASSYMETRY AFTER COMPLETION OF MX ACTION, OK TO CON
- [SDR CALA2017121204404](https://openairdocs.org/sdr/CALA2017121204404.md): Altimeter · sticks · Dec 12, 2017 · N17139 · Boeing 757224 · Altimeter, Barometric/Encoder
  > STANDBY ALTIMETER FREQUENTLY JAMS FOR SEVERAL HUNDRED FEET IN CLIMB AND DESCENT. R&R STANDBY ALTIMETER IAW AMM 34-13-06.
- [SDR CALA2017080802531](https://openairdocs.org/sdr/CALA2017080802531.md): Sensor · contaminated · Aug 8, 2017 · N17139 · Boeing 757224 · Emergency Equipment
  > R2 DOOR SLIDE LIGHT ILLUMINATED WITH DOOR DISARMED. CLEANED GREASE FROM SLIDE GIRT BAR SENSOR. SLIDE LIGHT OPERATED NORMAL.
- [SDR CALA2017063002034](https://openairdocs.org/sdr/CALA2017063002034.md): Bulb · inoperative · Jun 30, 2017 · N17139 · Boeing 757224 · Emergency Lighting
  > AFT LEFT OVERWIMG EMERGENCY LIGHT INOPERATIVE. REPLACED THE BULB. OPS CHECKED GOOD.
- [SDR CALA2017063002035](https://openairdocs.org/sdr/CALA2017063002035.md): Bulb · inoperative · Jun 30, 2017 · N17139 · Boeing 757224 · Emergency Lighting
  > EMERGENCY EXIT LIGHT OVER SEAT 1E INOPERATIVE. REPLACED THE BULB. OPS CHECKED GOOD.
- [SDR CALA2017051201364](https://openairdocs.org/sdr/CALA2017051201364.md): Outflow Valve · faulted · May 12, 2017 · N17139 · Boeing 757224 · Pressure Regulator/Outflow Valve
  > LOST PRESSURAZATION IN FLT AT FL380 ACCOMPLISHED AUTO CABIN PRESSURE CONTROLLERS TEST IAW AMM 21-31-00-705-085 NO FAULTS NOTED TEST PASSED, ACP MANUAL MODE CONTROL TEST IAW AMM 21-31-00-715-001 NO FAULTS NOTED TEST PASSED,ACP CABIN PRES OUTFLOW VALVE INSPECTIO
- [SDR CALA2017031300596](https://openairdocs.org/sdr/CALA2017031300596.md): Threshold · dirty · Mar 13, 2017 · N17139 · Boeing 757224 · Fuselage Miscellaneous Structure
  > DOOR-MOUNTED ESCAPE SYSTEM. DOOR 4L EVACUATION SLIDE ARMING LEVER, FAILED TO MOVE, BINDING, AT ENTRY/SERVICE DOOR. CLEANED LOWER DOOR THRESHOLD DEBRIS, DOOR ARMS AND DISARMS NORMALLY.
- [SDR CALA2017012000135](https://openairdocs.org/sdr/CALA2017012000135.md): Cusp Web · corroded · Jan 19, 2017 · N17139 · Boeing 757224 · Fuselage Miscellaneous Structure
  > CABIN FLOORS STA 560-580 RBL 64 ANGLE SUPPORT SHOWS CORROSION. REMOVED CORROSION AT I/B CREASE BEAM BETWEEN STA 560- STA 580 AND FOUND TO BE WITHIN LIMITS AS PER B757-2 SRM 53-00-01 AND REMOVED AND REPLACED CUSP WEB BETWEEN STA 560 THROUGH STA 580 AND RBL 64"
- [SDR CALA2017012000130](https://openairdocs.org/sdr/CALA2017012000130.md): Crease Beam · corroded · Jan 17, 2017 · N17139 · Boeing 757224 · Fuselage Main, Structure
  > PASSENGER CABIN CREASE BEAM DEEP CORROSION BETWEEN STA 1240 AND 1280 LT SIDE. INSTALLED CREASE BEAM I/B CHORD SPLICE REPAIR ON MAIN CABIN FROM STA 1230 TO 1290 LT SIDE PER REF SRM 53-00-13 REPAIR 1 DETAIL, FIG 201.
- [SDR CALA2016112100952](https://openairdocs.org/sdr/CALA2016112100952.md): Light · inoperative · Nov 21, 2016 · N17139 · Boeing 757224 · Emergency Lighting
  > SLIDE LIGHT BURNED OUT DURING CRUISE AT DOOR 1R. RELAMPED, CKS OKAY.
- [SDR CALA2015120400961](https://openairdocs.org/sdr/CALA2015120400961.md): Oven · odor · Nov 25, 2015 · N17139 · Boeing 757224 · Buffet/Galleys
  > GATE RETURN FOR OVEN ODOR. PERFORMED AMM 05-51-58 INSPECTION. VERIFIED OVEN 305 AS CAUSE REF 8326266 FOR OVEN 305. MEL FORMS 46-6020 FAXED TO MOC. IAW FORMS NO SMOKE OR BURNING ODOR PRESENT, ONLY OVEN SMELL. INSPECTED OVEN NO OVERHEAT CONDITION NOTICED.

Next page: https://openairdocs.org/aircraft/N17139/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 = 'N17139' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N17139/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.